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INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO TRANSMITTER Details Info Part no AGD 1C 458MKS Description Gyro Transmitter Wpn Sys AN-32 Major Assembly Self Annual Requirement 29 2. RPM INDICATOR Details Info Part No STA/ITE-2T Description RPM Indicator Wpn Sys AN-32 Major Assembly Self Annual Requirement 25 3. HYDRAULIC OIL QTY INDICATOR Details Info Part No ME-1866T Description Hyd Oil Qty Indicator Wpn Sys AN-32 Major Assembly Self Annual Requirement 08

INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

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Page 1: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INDIGENISATION REQUIRMENT OF IAF : 1CIMD

1. GYRO TRANSMITTER

Details Info

Part no AGD 1C 458MKS

Description Gyro Transmitter

Wpn Sys AN-32

Major Assembly Self

Annual Requirement 29

2. RPM INDICATOR

Details Info

Part No STA/ITE-2T

Description RPM Indicator

Wpn Sys AN-32

Major Assembly Self

Annual Requirement 25

3. HYDRAULIC OIL QTY INDICATOR

Details Info

Part No ME-1866T

Description Hyd Oil Qty Indicator

Wpn Sys AN-32

Major Assembly Self

Annual Requirement 08

Page 2: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

4. RUBBER SLEEVE

Details Info

Part No RH1-89-26-006-201

Description Rubber Sleeve

Wpn Sys IL-76

Major Assembly Surge Suppressor Assembly

Annual Requirement 15

5. FILTER ELEMENT

Details Info

Part No 226AV/ MEHA151

Description Filter Element

Wpn Sys AVRO

Major Assembly Hydraulic System

Annual Requirement 06

6. FILTER ELEMENT

Details Info

Part No 226AV/ MFHA317

Description Filter Element

Wpn Sys AVRO

Major Assembly Hydraulic System

Annual Requirement 15

Page 3: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

7. BEARING BALL FLANGED

Details Info

Part No VJA/303-128-705-0

Description Bearing Ball Flanged

Wpn Sys AGB

Major Assembly M-53

Annual Requirement

04

8. BALL BEARING FLANGED

Details Info

Part No 303-141-902-0

Description Ball Bearing Flanged

Wpn Sys AGB

Major Assembly M-53

Annual Requirement

04

9. FUNNEL RH

Details Info

Part No 32.02.7602.115.000

Description Funnel RH

Wpn Sys AN-32

Major Assembly Air Conditioning System

Annual Requirement 40

Page 4: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

10. IFF ANTENNA

Details Info

Part No 62138889AA

Description IFF Antenna

Wpn Sys Mig-29

Major Assembly Self

Annual Requirement 05

11. DISK

Details Info

Part No NBUO-97-410-15

Description Disk

Wpn Sys IL-76

Major Assembly Brake Unit

Annual Requirement 684

12. UNROTATABLE DISK

Details Info

Part No KT 199-070

Description Unrotatable Disk

Wpn Sys IL-76

Major Assembly Main Wheel Brake Unit

Annual Requirement 94

Page 5: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

13. SUPPORTING DISK

Details Info

Part No KT 199-080

Description Supporting Disk

Wpn Sys IL-76

Major Assembly Brake Unit

Annual Requirement 94

14. ROTATABLE DISK

Details Info

Part No KT 199-060

Description Rotatable Disk

Wpn Sys IL-76

Major Assembly Main Wheel Brake Unit

Annual Requirement 202

15. PRESSING DISK

Details Info

Part No KT 199-050

Description Pressing Disk

Wpn Sys IL-76

Major Assembly Brake Unit

Annual Requirement 24

Page 6: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

16. BRAKE

Details Info

Part No KT 158-030-1

Description Brake

Wpn Sys IL-76

Major Assembly Main Wheel Brake System

Annual Requirement 228

17. BRAKE

Details Info

Part No KT 158-030-2

Description Brake

Wpn Sys IL-76

Major Assembly Main Wheel Brake System

Annual Requirement 120

18. PRESSURE PLATE

Details Info

Part No KT 158-040

Description Pressure Plate

Wpn Sys IL-76

Major Assembly Brake Unit

Annual Requirement 228

Page 7: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

19. METAL CERAMIC DISK

Details Info

Part No KT 126-120

Description Metal Ceramic Disk

Wpn Sys IL-76

Major Assembly Brake Unit

Annual Requirement 876

20. LAMP

Details Info

Part No LFSM 28-600-180

Description Lamp

Wpn Sys IL-76

Major Assembly Landing Taxing Light

Annual Requirement 180

21. VALVE

Details Info

Part No 204C/895

Description Regulating Valve

Wpn Sys BEFAB 6:3 Arrester Barrier

Major Assembly Brake Drum

Annual Requirement 12

Page 8: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

22. SHUTTLE VALVE

Details Info

Part No 104C/52D10418-2

Description Shuttle Valve

Wpn Sys P-IV Arrester Barrier

Major Assembly Energy Absorber

Annual Requirement 06

23. FLOW CHECK VALVE

Details Info

Part No 104C/153

Description Flow Check Valve

Wpn Sys G+W Arrester Barrier

Major Assembly Stanchion System

Annual Requirement 06

24. PURCHASE TAPE

Details Info

Part No 204C/44307-65

Description Purchase Tape

Wpn Sys BEFAB 44B-8F Arrester Barrier

Major Assembly Purchase Tape Assy

Annual Requirement 12

Page 9: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

25. LIMIT SWITCH DOWN

Details Info

Part No 104C/52B6567-100

Description Limit Switch Down

Wpn Sys G+W Arrester Barrier

Major Assembly Stanchion System

Annual Requirement 06

26. MAGNETIC STARTER MOTOR

Details Info

Part No 104C/354

Description Magnetic Starter Motor

Wpn Sys G+W Arrester Barrier

Major Assembly Stanchion System

Annual Requirement 06

Page 10: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INDIGENISATION REQUIRMENT OF IAF : 1 BRD

1. SPRING

Details Info

Part No 24.5603.299

Description Spring

Wpn Sys AN-32

Main System/Major Assembly

Filter Desicator

Annual Requirement 12

2. FILLER NECK PLUG

Details Info

Part No 1584A-2T

Description Filler Neck Plug

Wpn Sys AN-32

Main System/Major Assembly

Wing And Fuel System (Distribution)

Annual Requirement 48

3. PRESSURE SEAL

Details Info

Part No 32.01.7217.336.005

Description Pressure Seal

Wpn Sys AN-32

Main System/Major Assembly

Engine Nacelle JB

Annual Requirement 50

Page 11: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

4. THERMO COUPLE

Details Info

Part No T31-1

Description Thermo Couple

Wpn Sys AN-32

Main System/Major Assembly

Engine Transmitters Installation

Annual Requirement 10

5. SPARKING PLUG

Details Info

Part No SPN-4-3-T

Description SPARKING PLUG

Wpn Sys AN-32

Main System/Major Assembly

AI20D AERO ENGINE

Annual Requirement 298

6. PRESSURE GAUGE TRANSMITTER (V)

Details Info

Part No STA/DMP 100 A

Description Pressure Gauge Transmitter (V)

Wpn Sys AN-32

Main System/Major Assembly

SELF

Annual Requirement 12

Page 12: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

7. MAGNETIC AMPLIFIER

Details Info

Part No STA/1143

Description Magnetic Amplifier

Wpn Sys AN-32

Main System/Major Assembly

FDS Computer

Annual Requirement 12

8. AMPLIFIER YRT 2T

Details Info

Part No STA/12-530-38 T

Description Amplifier YRT 2T

Wpn Sys AN-32

Main System/Major Assembly

Fuel Measuring Unit

Annual Requirement 12

Page 13: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INDIGENISATION REQUIRMENT OF IAF : 3 BRD

1. COUPLING CLUTCH

Details Info

Part No NSH39-006

Description Coupling Clutch

Wpn Sys MI17 (3 BRD AF)

Main System/Major Assembly

Hydraulic Gear Pump

Annual Requirement 62 Each

2. CAGE

Details Info

Part No 07613-0088

Description Cage

Wpn Sys MI-17/3 BRD

Main System/Major Assembly

Main Gear Box

Annual Requirement 18

3. INSERT LOCKING STAGE III

Details Info

Part No 7842-0115

Description Insert Locking Stage III

Wpn Sys MI17

Main System/Major Assembly

Free Turbine Assy

Annual Requirement 25

Page 14: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

4. INSERT LOCKING STAGE IV

Details Info

Part No 7842-0124

Description Insert Locking Stage IV

Wpn Sys MI-17

Main System/Major Assembly

Free Turbine Assy

Annual Requirement 25

5. SPRING

Details Info

Part No 8-3914-561

Description Spring

Wpn Sys MI-17

Main System/Major Assembly

Tail Rotor Assy

Annual Requirement 400

6. SPRING

Details Info

Part No 78029-9054

Description Spring

Wpn Sys MI-17

Main System/Major Assembly

Carbon Seal

Annual Requirement 45

7. SPRING

Details Info

Part No 7884-0577

Description Spring

Wpn Sys MI-17

Main System/Major Assembly

Air Blow off Valve

Annual Requirement 30

Page 15: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

8. FILTER ELEMENT

Details Info

Part No 8D2-966-022-3

Description Filter Element

Wpn Sys MI-17/17 1V

Main System/Major Assembly

Hydraulic Filter

Annual Requirement 20

9. FILTER ELEMENT

Details Info

Part No 340-146

Description Filter Element

Wpn Sys Fuel Filter

Main System/Major Assembly

MI17

Annual Requirement 10

10. FILTER ELEMENT

Details Info

Part No 611400

Description Filter Element

Wpn Sys MI-17/17 1V

Main System/Major Assembly

Automated Cut Out Valve

Annual Requirement 15

11. FIRST STAGE CYLINDER

Details Info

Part No AK50-207

Description First Stage Cylinder

Wpn Sys Air Compressor

Main System/Major Assembly

MI 17

Annual Requirement 20

Page 16: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

12. GEAR DRIVEN

Details Info

Part No 7867-9088-01

Description Gear Driven

Wpn Sys MI-17

Main System/Major Assembly

Oil Pump Block

Annual Requirement 09

13. HOSE END FITTING SET

Details Info

Part No 140-6210-20-EF-25

Description Hose End Fitting Set

Wpn Sys MI-17/17 1V

Main System/Major Assembly

Hose

Annual Requirement 100

14. HOSE END FITTING SET

Details Info

Part No 8AT-6200-160-EF-2

Description Hose End Fitting Set

Wpn Sys Hose

Main System/Major Assembly

MI-17/17 1V

Annual Requirement 100

Page 17: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

15. HOSE END FITTING SET

Details Info

Part No 4830A-Y4-335-EF-74

Description Hose End Fitting Set

Wpn Sys MI-17/17 1V

Main System/Major Assembly

Hose

Annual Requirement 100

16. VALVE ASSY

17. TRIP LINE ASSY

Details Info

Part No BB-390

Description Trip Line Assy

Wpn Sys MI-17 V5

Main System/Major Assembly

Bambi Bucket

Annual Requirement 5

18. BEARING BORE

PHOTO N/A

Details Info

Part No 7823-9050

Description Bearing Bore

Wpn Sys MI17

Main System/Major Assembly

3RD NGV

Annual Requirement 20

Details Info

Part No OU-2-900A

Description Valve Assy

Wpn Sys MI-17/ IV / V5

Main System/Major Assembly

Fire Protection System

Annual Requirement 35

Page 18: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

19. BRANCH PIPE

Details Info

Part No PTS-62-70D

Description Branch Pipe

Wpn Sys MI-17

Main System/Major Assembly

Engine Air Starting Sys

Annual Requirement 16

20. BRANCH PIPE

21. BEARING SLEEVE

PHOTO N/A

Details Info

Part No 7971-0885

Description Bearing Sleeve

Wpn Sys MI-17

Main System/Major Assembly

Main Gear Box

Annual Requirement 12

22. K4PM BEARING

Details Info

Part No 6-42408K4PM

Description Rollar Bearing

Wpn Sys MI-17

Main System/Major Assembly

Main Gear Box

Annual Requirement 745

Details Info

Part No PTS-62-180D

Description Branch Pipe

Wpn Sys MI17

Main System/Major Assembly

Engine Pneumatic Starting Sys

Annual Requirement 48

Page 19: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

23. HYDRAULIC CHAMBER

Details Info

Part No 8MT-9600-22

Description Hydraulic Chamber

Wpn Sys MI-17 ( 3BRD,AF)

Main System/Major Assembly

Weight Measuring Device

Annual Requirement 10

24. CAGE SEPARATOR

Details Info

Part No 148.029

Description Cage Separator

Wpn Sys AN32

Main System/Major Assembly

Starter Generator

Annual Requirement 64

25. IMPEDANCE CORRECTOR CASING

Details Info

Part No YC-1-1

Description Impedance Corrector Casing

Wpn Sys MI-17

Main System/Major Assembly

Self

Annual Requirement 30

Page 20: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

26. CUP REINFORCED

Details Info

Part No 8-1920-085

Description Cup Reinforced

Wpn Sys MI17

Main System/Major Assembly Swash Plate

Annual Requirement 20

27. COLLAR

Details Info

Part No 306-033-04

Description Collar

Wpn Sys MI 17 IV

Main System/Major Assembly Electric Motor

Annual Requirement 40

28. ALKALINE STORAGE BATTERY

Details Info

Part No 10NMGTS2.5

Description IPR Battery(Alkaline Storage Battery)

Wpn Sys MI-17V5

Main System/Major Assembly SELF

Annual Requirement 36

29. LITHIUM BATTERY

Details Info

Part No 452-0133

Description Lithium Battery

Wpn Sys MI 17 V5

Main System/Major Assembly

C-406 NHM

Annual Requirement 27

Page 21: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

30. RELAY

Details Info

Part No TKE-21-PODG

Description Relay

Wpn Sys MI 17 V5

Main System/Major Assembly

Junction Box 2 and 4

Annual Requirement 210

31. PRESSURE WARNING LIGHT

Details Info

Part No ELRP-27-1270

Description Pressure Warning Light

Wpn Sys MI 17 1V

Main System/Major Assembly

Main Rotor Blade

Annual Requirement 40

32. SMART MULTI FUNCTION DISPLAY

Details Info

Part No VIAM.467.846.001

Description Smart Multi-Function Display

Wpn Sys MI 17 V5( 3 BRD,AF)

Main System/Major Assembly

Pilot Instrument Panel Knie-8

Annual Requirement 20

Page 22: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INDIGENISATION REQUIRMENT OF IAF: 4BRD

1. LINER STRUT THIN

Details Info

Part No VJA/303-808-704-0

Description Liner Strut Thin

Wpn Sys M-53

Main System/Major Assembly

Module-7

Annual Requirement 13

2. LEVER ACTUATING

Details Info

Part No VJA/304-141-002-0

Description Lever Actuating

Wpn Sys M-53

Main System/Major Assembly

Module-10

Annual Requirement 06

3. LEVER SYNCHRONISING

Details Info

Part No VJA/303-141-201-0

Description Lever Synchronising

Wpn Sys M-53

Main System/Major Assembly

Module-10

Annual Requirement 05

Page 23: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

4. COLD FLAP OUTER (UN-MODIFIED)

Details Info

Part No VJA/303-030-914-0

Description Cold Flap Outer(Un-Modified)

Wpn Sys M-53

Main System/Major Assembly

Exhaust Nozzle

Annual Requirement 12

5. COLD FLAP OUTER (MODIFIED)

Details Info

Part No VJA/303-030-920-0

Description Cold Flap Outer(Modified)

Wpn Sys M-53

Main System/Major Assembly

Exhaust Nozzle

Annual Requirement 12

6. COLD FLAP INNER (UN-MODIFIED)

Details Info

Part No VJA/303-031-014-0

Description Cold Flap Inner(Un-Modified)

Wpn Sys M-53

Main System/Major Assembly

Exhaust Nozzle

Annual Requirement 12

Page 24: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

7. COLD FLAP INNER (MODIFIED)

Details Info

Part No VJA/303-031-020-0

Description Cold Flap Inner(Modified)

Wpn Sys M-53

Main System/Major Assembly

Exhaust Nozzle

Annual Requirement 12

8. SEAL MECHANICAL

Details Info

Part No VJA/801157

Description Seal Mechanical

Wpn Sys M53-P2 Aero Engine

Main System/Major Assembly

Accessary Gear Box

Annual Requirement 04

9. SEAL MECHANICAL

Details Info

Part No VJA/801159

Description Seal Mechanical/Gasket Mechanical

Wpn Sys M53-P2 Aero Engine

Main System/Major Assembly

Accessary Gear Box & Accessary Transfer Gear Box

Annual Requirement 04

Page 25: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

10. SEAL MECHANICAL

Details Info

Part No VJA/801161

Description Seal Mechanical/Joint Mechanical

Wpn Sys M53-P2 Aero Engine

Main System/Major Assembly

Accessary Transfer Gear Box

Annual Requirement 08

11. RING OIL SEAL

Details Info

Part No 236ST/V103039

Description Ring Oil Seal

Wpn Sys Viper Aero Engine

Main System/Major Assembly

Front Main Bearing

Annual Requirement 10

12. SEAL CARBON FACE

Details Info

Part No 236LL/77561701

Description Seal Carbon Face

Wpn Sys Viper Aero Engine

Main System/Major Assembly

Fuel Pump

Annual Requirement 10

Page 26: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INDIGENISATION REQUIRMENT OF IAF : 5 BRD

1. CABLE ASSY HIGH ENERGY IGNITOR

Details Info

Part No 80237-SHT-43

Description Cable Assy High Energy Igniter

Wpn Sys AVRO

Major Assembly Starting And Ignition

Annual Requirement

08

2. UNIT COUPLING

Details Info

Part No CC 704/S/2

Description Unit Coupling

Wpn Sys AVRO

Major Assembly Bulk Head Arrangement Fire Proof

Annual Requirement

15

3. CODE SCAN CARD ASSY

Details Info

Part No 3716317501

Description Code Scan Assembly

Wpn Sys AVRO

Major Assembly Digital Indicator (PRIMUS-500)

Annual Requirement

04

Page 27: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

4. NAV DISPLAY CIRCUIT CARD

Details Info

Part No 3713607503

Description NAV Display Circuit Card

Wpn Sys AVRO

Major Assembly Digital Indicator (PRIMUS-500)

Annual Requirement

03

5. CONVERTER CARD

Details Info

Part No 3716308-501

Description Converter Card

Wpn Sys AVRO

Major Assembly Digital Indicator (PRIMUS-500)

Annual Requirement

03

6. SWITCH PANEL ASSY

Details Info

Part No 3715130503

Description Switch Panel Assy

Wpn Sys AVRO

Major Assembly Digital Indicator (PRIMUS-500)

Annual Requirement

05

Page 28: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

7. MEMORY CARD

Details Info

Part No 3716305-501

Description Memory Card

Wpn Sys AVRO

Major Assembly Digital Indicator (PRIMUS-500)

Annual Requirement

03

8. TIMING CARD ASSY

Details Info

Part No 3716311501

Description Code Scan Assembly

Wpn Sys AVRO

Major Assembly Digital Indicator (PRIMUS-500)

Annual Requirement

05

9. LOW VOLTAGE POWER ASSY

Details Info

Part No 3713530501

Description Low Voltage Power Assy

Wpn Sys AVRO

Major Assembly Digital Indicator (PRIMUS-500)

Annual Requirement

03

Page 29: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

10. DA CARD ASSY

Details Info

Part No 3713592505

Description DA Card Assy

Wpn Sys AVRO

Major Assembly Digital Indicator (PRIMUS-500)

Annual Requirement

02

11. AD CARD ASSY

Details Info

Part No 3716314-501

Description AD Card Assy

Wpn Sys AVRO

Major Assembly Digital Indicator (PRIMUS-500)

Annual Requirement

05

12. RELAY STC 4190 GD

Details Info

Part No 3716314-501

Description Relay STC 4190 GD

Wpn Sys AVRO

Major Assembly Auto Pilot Amplifier

Annual Requirement

552

Page 30: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INDIGENISATION REQUIRMENT OF IAF: 7 BRD

1. PECHORA GEARS

Details Info

Part No PK4-220-079 SP

Description Pechora Gears

Wpn Sys OSA-AK-M

Main System/Major Assembly

SNR-125 (YHB)

Annual Requirement 08

2. P-18 PANELS

Details Info

Part No 2HZ2.026.003SP

Description P-18 Panels

Wpn Sys P-18

Main System/Major Assembly

P-18 Radar

Annual Requirement 08

Page 31: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

3. LNA (P-19)

Details Info

Part No MSHB-19

Description LNA (P-19)

Wpn Sys P-19

Main System/Major Assembly

P-19 Radar Receiver System

Annual Requirement 08

4. COAXIAL CIRCULATOR

Details Info

Part No YEI2-238-002

Description Coaxial Circulator

Wpn Sys P-19 Radar

Main System/Major Assembly

P-19 Radar

Annual Requirement 08

5. FLEXIBLE JOINT

Details Info

Part No YE16-647-063

Description Flexible Joint

Wpn Sys P-19

Main System/Major Assembly

P-19 Radar

Annual Requirement

04

Page 32: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

6. ROH-MU DRIVE

Details Info

Part No PB3.128.014-1

Description ROH-MU Drive

Wpn Sys OSA-AK-M

Main System/Major Assembly

TAR Stabilization System

Annual Requirement

06

7. EMBB

Details Info

Part No BK3.254.090

Description EMBB

Wpn Sys Pechora GW

Main System/Major Assembly

LCR 5П73

Annual Requirement 04

8. WATER PUMP

Details Info

Part No 201-130-7010-B2

Description Water Pump

Wpn Sys Pechora GW

Main System/Major Assembly

AD-30

Annual Requirement 10

Page 33: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

9. CPV

PHOTO N/A

Details Info

Part No 06-02-020

Description CPV

Wpn Sys Pechora GW

Main System/Major Assembly

UKS-400B

Annual Requirement 10

10. USDL

Details Info

Part No BA2-066-127 SP

Description USDL

Wpn Sys OSA-AK-M

Main System/Major Assembly

MTI System

Annual Requirement 08

11. SERVO AMPLIFIER

Details Info

Part No TSK2-039-056-01

Description Servo Amplifier

Wpn Sys OSA-AK-M

Main System/Major Assembly

OSA CV

Annual Requirement

04

Page 34: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

12. OPERATIONAL AMPLIFIER

Details Info

Part No TSK3-086-026

Description Operational Amplifier

Wpn Sys OSA-AK-M

Main System/Major Assembly

OSA CV

Annual Requirement 04

13. MAGNETRON MI- 502

Details Info

Part No SHS3-323-018TU

Description Magnetron MI- 502

Wpn Sys P-19 Radar

Main System/Major Assembly

P-19 Radar

Annual Requirement 04

14. TRANSMITTER VALVE (GI-19B)

Details Info

Part No GI- 19 B

Description Transmitter Valve (GI-19B)

Wpn Sys P-18 Radar

Main System/Major Assembly

P-18 Radar

Annual Requirement 04

Page 35: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INDIGENISATION REQUIRMENT OF IAF: 8 BRD

1. VALVE

Details Info

Part No 204C/895

Description Regulating Valve

Wpn Sys BEFAB 6:3 Arrester Barrier

Main System/Major Assembly

Brake Drum

Annual Requirement 12

2. FLOW CHECK VALVE

Details Info

Part No 104C/153

Description Flow Check Valve

Wpn Sys G+W Arrester Barrier

Main System/Major Assembly

Stanchion System

Annual Requirement 06

3. PURCHASE TAPE

Details Info

Part No 204C/44307-65

Description Purchase Tape

Wpn Sys BEFAB 44B-8F Arrester Barrier

Main System/Major Assembly

Purchase Tape Assy

Annual Requirement 12

Page 36: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

4. MAGNETIC STARTER MOTOR

Details Info

Part No 104C/354

Description Magnetic Starter Motor

Wpn Sys G+W Arrester Barrier

Main System/Major Assembly

Energy Absorber

Annual Requirement 09

5. LIMIT SWITCH DOWN

Details Info

Part No 104C/52B6567-100

Description Limit Switch Down

Wpn Sys G+W Arrester Barrier

Main System/Major Assembly

Stanchion System

Annual Requirement

06

Page 37: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INDIGENISATION REQUIRMENT OF IAF :9 BRD

8. MOUNTING STUD WITH NUT

Details Info

Part No 1110 RAFAEL/TA 1W1006C

Description Mounting stud

Wpn Sys Air borne

Main System/Major Assembly

Litening LDP pod

Annual Requirement 04 Each SQN.

2. PHASED LOCK LOOP

Details Info

Part No 310D/N144160

Description Phased lock loop

Wpn Sys MiG-21/ AN-32

Main System/Major Assembly

VUC-201A

Annual Requirement 50

3. BASE BAND ASSEMBLY

Details Info

Part No 310D/101176

Description Base band assembly

Wpn Sys Sarbe-8

Main System/Major Assembly

PRB / ELT

Annual Requirement 100

Page 38: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

4. INERTIAL MEASUREMENT UNIT CCA

Details Info

Part No TAEM6500J

Description Inertial Measurement Unit CCA

Wpn Sys Rear section

Main System/Major Assembly

Litening LDP 2I

Annual Requirement 3

5. CENTRAL PROCESSING UNIT

Details Info

Part No TA1M1000E

Description Central Processing Unit

Wpn Sys Rear section

Main System/Major Assembly

Litening LDP 2I

Annual Requirement 3

6. SERVO CCA

Details Info

Part No TA1M2500F

Description Servo CCA

Wpn Sys Rear Section

Main System/Major Assembly

Litening LDP 2i

Annual Requirement 3

Page 39: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

7. FLY BY WIRE Su-30 MKI TESTER

Details Info

Part No SDU-10 MK

Description Fly- By- Wire Control Sys

Wpn Sys Flying Control Sys/ SSC

Main System/Major Assembly

Self

Annual Requirement 12

8. MC1 & MC4 Su-30 MKI TESTER

Details Info

Part No SUMCS/ 486-1M-03

Description BTseVM-486-1M-03 (MC-1):

SU30MKI

Wpn Sys KPA-BChVM-486-1 / SSC

Main System/Major Assembly

KPA-BChVM-486-1

Annual Requirement 3

9. BP-95-02 P/S UNIT Su-30 MKI TESTER

Details Info

Part No PZP-117

Description BP-95 Tester for voltage

Wpn Sys Voltage checking of FBW sys.

Main System/Major Assembly

Fly-by-wire control system

Annual Requirement 3

Page 40: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

10. CMDS Su-30 MKI TESTER

Details Info

Part No UV30MKI-8700KPA

Description UV30MKI-8700KPA

Wpn Sys Tester Su-30 MKI

Main System/Major Assembly

CMDS

Annual Requirement 3

11. KPA BRZU (115VO-1) Su-30 MKI TESTER

Details Info

Part No KPA-BRZU-115VO-1

Description Tester

Wpn Sys SSC Tester

Main System/Major Assembly

BRZU 115V

Annual Requirement 3

12. (BAKNA-115V) Su-30 MKI TESTER

Details Info

Part No KPA-BKNA-115V

Description Tester

Wpn Sys SSC Tester

Main System/Major Assembly

KPA-BKNA-115V

Annual Requirement 3

Page 41: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

13. EARTH FAULT CARD LOW VOLTAGE

Details Info

Part No 305AMAFSAF/1600002311AA

Description Earth Fault Module Low Voltage

Wpn Sys Air Field Lighting System

Major Assembly

IDM 8000 IDMAN 25 KVA CCR

Annual Requirement

20

14. EARTH FAULT CARD HIGH VOLTAGE

Details Info

Part No 305AMAFSAF/1600002312AA

Description Arth Fault Module High Voltage

Wpn Sys Air Field Lighting System

Major Assembly

IDM 8000 IDMAN 25 KVA CCR

Annual Requirement

20

15. MOTHER BOARD

Details Info

Part No 305AMAFSAF/1600002305AA

Description Thyristor Control Card

Wpn Sys Air Field Lighting System

Major Assembly

Air Field Lighting System

Annual Requirement

20

Page 42: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

16. POWER UNIT FOR CCR

Details Info

Part No 305AMAFSAF/1600002308AA

Description Power Unit For CCR

Wpn Sys Air Field Lighting System

Major Assembly IDM 8000 IDMAN 25 KVA CCR

Annual Requirement

20

17. THYRISTOR CONTROL CARD FOR CCR

Details Info

Part No 305AMAFSAF/1600002310A

Description Thyristor Control Card

Wpn Sys Air Field Lighting System

Major Assembly Air Field Lighting System

Annual Requirement

20

18. DVTR (JAGUAR)

Details Info

Part No 31700000

Description Digital Video Tape Recorder (Jaguar)

Wpn Sys Jaguar/DVRS

Major Assembly DVTR

Annual Requirement

10

Page 43: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INDIGENISATION REQUIRMENT OF IAF : 11 BRD

1. HOSE 5Y6-100

Details Info

Part No 5Y6-100

Description Hose

Wpn Sys MIG-29

Main System/Major Assembly

Self

Annual Requirement 90

2. HOSE 5Y4-120

Details Info

Part No 5Y4-120

Description Hose

Wpn Sys MIG-29

Main System/Major Assembly

Self

Annual Requirement

25

3. NETWORK CENTERIC DATA CARD

Details Info

Part No AD312040-01

Description NCDC 64 GB ASSY

Wpn Sys SU-30 MKI / 2 WG

Main System/Major Assembly

SS DVRS

Annual Requirement 10

Page 44: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

4. PU FOAM

Details Info

Part No -

Description PU Foam

Wpn Sys SU-30 Aircraft

Main System/Major Assembly

Fuel Tank

Annual Requirement 2000 Kg

5. FRL HOSE

Details Info

Part No 43325602

Description 2.00ʺ FRL Hose

Wpn Sys SU-30 Aircraft

Main System/Major Assembly

Air To Air Refueling POD

Annual Requirement 02

6. CASING (EJECTION HANDLE)

Details Info

Part No 903-9208-80

Description Casing Ejection Handle

Wpn Sys SU-30 MKI

Main System/Major Assembly

K-36D-3.5E

Annual Requirement 50

Page 45: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INDIGENISATION REQUIRMENT OF IAF : 12 BRD

1. RAM AIR TEMP SENSOR-ELTA SYSTEM

Details Info

Part No 3041J195-002

Description Ram Air Temp Sensor

Wpn Sys Jaguar

Main System/Major Assembly

ALTA ASPJ

Annual Requirement 05

2. DEVELOPMENT OF CW TWT-ELTA

Details Info

Part No 3046N503

Description CW TWT

Wpn Sys Jaguar

Main System/Major Assembly

ELTA ASPJ

Annual Requirement 05

3. DEVELOPMENT OF PULSE TWT-ELTA

Details Info

Part No 3046J510

Description Pulse TWT

Wpn Sys Jaguar

Main System/Major Assembly

ELTA ASPJ

Annual Requirement 05

Page 46: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

4. DEVELOPMENT OF CW HPRF ADAPTER FWD-ELTA

Details Info

Part No 3045N340-003

Description CW HPRF Adapter Fwd

Wpn Sys ELTA

Main System/Major Assembly

ELTA ASPJ

Annual Requirement 02

5. DEVELOPMENT OF CW HPRF ADAPTER AFT-ELTA

Details Info

Part No 3045N330-003

Description CW HPRF Adapter Fwd

Wpn Sys ELTA

Main System/Major Assembly

ELTA ASPJ

Annual Requirement

02

Page 47: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INDIGENISATION REQUIRMENT OF IAF: 13 BRD

1. PS 2 (TX) (DC/DC CONV 18-40V IN)

Details Info

Part No 1110LLLWR / M7025-15

Description PS2(TX) (DC/DC CONV 18-

40V IN)

Wpn Sys LLLWR

Main System/Major Assembly Trans Receive Unit

Annual Requirement 04

2. PC ASSY 24V-96V

Details Info

Part No 1110LLLWR/ 1015W581

Description PC ASSY 24-96V

Wpn Sys LLLWR

Main System/Major Assembly

Pedestal Control Unit

Annual Requirement 02

3. FILTER COMM. 69

Details Info

Part No 1110LLLWR/ 5208T731-001

Description Filter COMM 6915

Wpn Sys LLLWR

Main System/Major Assembly

Pedestal Control Unit

Annual Requirement 02

Page 48: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

4. CU INTERFACE BOX

Details Info

Part No 110D/ 1019G181-001

Description CU Interface Box

Wpn Sys LLLWR

Main System/Major Assembly Central Unit

Annual Requirement 02

5. FRONT END FINAL ASSY

Details Info

Part No 1110LLLWR/ 1093N660-003

Description Front End Final Assy

Wpn Sys LLLWR

Main System/Major Assembly

Trans Receive Unit

Annual Requirement 02

6. EXC/REC F/A

Details Info

Part No 110D/ 1093K105002

Description EXC/ REC F/A

Wpn Sys LLLWR

Main System/Major Assembly

Trans Receive Unit

Annual Requirement 04

7. ICT ADPC IF MAIN ITA

Details Info

Part No 1110LLLWR/ 2053B061-001

Description ICT ADPC IF Main ITA

Wpn Sys LLLWR

Main System/Major Assembly

LLLWR

Annual Requirement 02

Page 49: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

8. IFF PRCU POWER SUPPLY

PHOTO N/A

Details Info

Part No 1110D/MPR 1023F140-001

Description IFF PRCU PS

Wpn Sys MPR

Main System/Major Assembly

IFF

Annual Requirement 05

9. CU A/C / HEAT EXCHANGER

Details Info

Part No 1110D/MPR 1025M990-001

Description CU A/C /Heat Exchanger

Wpn Sys MPR

Main System/Major Assembly

Receiver

Annual Requirement 05

10. CU PS CONVERTER TO 400 HZ

Details Info

Part No 1110D/MPR 1025M950-001

Description CU PS Converter To 400 HZ

Wpn Sys MPR

Main System/Major Assembly

Central Unit

Annual Requirement 05

11. CU LINEAR PS

Details Info

Part No 1110D/MPR 1015D420-002

Description CU Linear PS

Wpn Sys MPR

Main System/Major Assembly

Central Unit

Annual Requirement 05

Page 50: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

12. PEDESTAL CONTROL UNIT

Details Info

Part No 1110D/MPR 1025M900-001

Description Pedestal Control Unit

Wpn Sys MPR

Main System/Major Assembly

Antenna

Annual Requirement 05

13. POWER DRIVER SWITCH

Details Info

Part No 1110D/MPR 1093W688-001

Description Power Driver Switch

Wpn Sys MPR

Main System/Major Assembly

Antenna System

Annual Requirement 05

14. FIRST ANTENNA DRIVER

Details Info

Part No 1110D/MPR 1093W686-002

Description First antenna driver

Wpn Sys MPR

Main System/Major Assembly

Antenna System

Annual Requirement 05

15. CAL SWITCH 1:4

Details Info

Part No 1110D/MPR 1093W684-001

Description CAL Switch 1:4

Wpn Sys MPR

Main System/Major Assembly

Receiver System

Annual Requirement 05

Page 51: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

16. CAL DIVIDER 1:8

Details Info

Part No 1110D/MPR D-2040-8

Description CAL Divider 1:8

Wpn Sys MPR

Main System/Major Assembly

Receiver System

Annual Requirement 05

17. DOZOR-K

PHOTO N/A

Details Info

Part No "DOZOR-K" KEUR.421946.005

Description Information And Diagnostics Facility For Monitoring And Maintenance of Karat

Wpn Sys MIG-29 UPG

Main System/Major Assembly

Ground System

Annual Requirement 03

18. DOZOR SER 1M

PHOTO N/A

Details Info

Part No IDS "DOZOR SER 1M" KEUR.421946.004

Description Information And Diagnostics Facility For Re-Recording & Online Processing

Wpn Sys MIG-29 UPG

Main System/Major Assembly

Ground System

Annual Requirement 03

Page 52: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

19. ARM TSV

PHOTO N/A

Details Info

Part No "ARM TSV" KEUR.21946.002 "APM TCB"

Description Ground Based Facility For Ground Data Processing Computer Work Station

Wpn Sys MIG-29 UPG

Main System/Major Assembly

Ground System

Annual Requirement 03

20. RUGGEDIZED ROSE ANALYSING UNIT

PHOTO N/A

Details Info

Part No 17TES0060

Description Ruggedized Rose Analysing Unit

Wpn Sys Dornier

Main System/Major Assembly

Ground System

Annual Requirement 02

21. MAIN UNIT ASSEMBLY (AREA- MTI)

Details Info

Part No 310G / 100101746

Description Main Unit Assembly (Area-MTI)

Wpn Sys THD-1955 Radar

Main System/Major Assembly

Receiver

Annual Requirement 02

22. DUAL AMPLIFIER DRIVER

Details Info

Part No 1093W686-001

Description Dual Amplifier Driver

Wpn Sys MPR

Main System/Major Assembly

Antenna

Annual Requirement 02

Page 53: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

23. SYNTHESIZER

Details Info

Part No 1093P162-001

Description Synthesizer

Wpn Sys MPR

Main System/Major Assembly

Central Unit

Annual Requirement

02

24. RECEIVER MODULE

Details Info

Part No 1093P305-002

Description Receiver Module

Wpn Sys MPR

Main System/Major Assembly

Antenna

Annual Requirement 02

25. TX-OSC S BAND

Details Info

Part No 1093P055-002

Description TX-OSC S Band

Wpn Sys MPR

Main System/Major Assembly Antenna

Annual Requirement 02

Page 54: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

26. DCS

Details Info

Part No 1023F240-002

Description DCS

Wpn Sys MPR

Main System/Major Assembly

Antenna

Annual Requirement 03

27. CHANNEL SELECTOR

Details Info

Part No M930-0011025

Description Channel Selector

Wpn Sys MPR

Main System/Major Assembly

Antenna

Annual Requirement 02

28. MOTHER BOARD

Details Info

Part No 1023R400-001

Description Mother Board

Wpn Sys MPR

Main System/Major Assembly

Antenna

Annual Requirement 04

29. RCU CHASSIS WITH MOTHER BOARD

PHOTO N/A

Details Info

Part No 1110D/MPR / 1025M915CH-001

Description RCU Chassis With Mother Board

Wpn Sys Antenna

Main System/Major Assembly

MPR

Annual Requirement 01

Page 55: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

30. TRANSMIT RECEIVE COMBINER

Details Info

Part No 1093W695001

Description Transmit Receive Combiner

Wpn Sys MPR

Main System/Major Assembly

Antenna

Annual Requirement 02

31. TEST JIG FOR ANTENNA POWER SUPPLY

Details Info

Part No 1110D/MPR / 1025M630JIG-001

Description Test Jig For Antenna Power Supply

Wpn Sys MPR

Main System/Major Assembly

Antenna

Annual Requirement 02

32. TEST JIG FOR CU AC TO AC CONVERTER

Details Info

Part No 2053B126-001

Description

Test Jig For CU AC TO AC Converter (115V 400 HZ 3 Phase From 220V 50HZ Single Phase)

Major Assembly CU PS Converter 400HZ

Wpn Sys MPR

Criticality Non-Critical

Material As Per Sample

Annual Requirement 01

Page 56: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

33. ICT SBC5110 ITA

Details Info

Part No 1019W048-001

Description ICT SBC5110 ITA

Wpn Sys LLLWR

Major Assembly Central Unit

Annual Requirement 01

34. FLU MODULE ASSY

Details Info

Part no 1015W575-001

Description FLU Module Assy

Major Assembly DAU

Wpn Sys LLLWR

Criticality Non-Critical

Annual Requirement 01

35. LV POWER SUPPLY

Details Info

Part No 1014C215-001

Description LV Power Supply

Major Assembly Central Unit

Wpn Sys LLLWR

Criticality Non-Critical

Annual Requirement 01

36. RDP F/ASSY

Details Info

Part No 1015W760-001

Description RDP F/Assy

Wpn Sys LLLWR

Major Assembly Central Unit

Annual Requirement 01

Page 57: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

37. A/D F/ASSY

Details Info

Part No 1019C790-002

Description A/D F/Assy

Wpn Sys LLLWR

Major Assembly Central Unit

Annual Requirement

01

38. RSP F/ASSY

Details Info

Part No 1015W820-001

Description RSP F/Assy

Wpn Sys LLLWR

Major Assembly Central Unit

Annual Requirement

01

39. TIMING I/O F/ASSY

Details Info

Part no 1019C780-001

Description Timing I/O F/Assy

Wpn Sys LLLWR

Major Assembly Central Unit

Annual Requirement 01

40. IRDP PROCESSOR CARD

Details Info

Part No 143031015932

Description IRDP Processor Card

Wpn Sys INDRA MK-II

Major Assembly Receiver

Annual Requirement 02

Page 58: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

41. DIF-2

Details Info

Part No 143031017581

Description DIF-2

Wpn Sys INDRA MK-II

Major Assembly Receiver System

Annual Requirement 02

42. RADAR INTERFACE CARD

Details Info

Part No 143031015835

Description Radar Interface Card

Major Assembly Receiver System

Wpn Sys INDRA MK-II

Criticality Non-Critical

Annual Requirement 01

43. 10/100 MBPS ETHERNET SWITCH CARD

Details Info

Part No 480542290116

Description 10/100 MBPS Ethernet Switch Card

Major Assembly Receiver System

Wpn Sys INDRA MK-II

Criticality Non-Critical

Annual Requirement 01

44. DUAL CHANNEL VIDEO EXTRACTOR

PHOTO N/A

Details Info

Part No 100000022014

Description Dual Channel Video Extractor (DCVE)

Major Assembly ADHS

Wpn Sys THD-1955 RADAR

Criticality Non-Critical

Annual Requirement 03

Page 59: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

45. ANTENNA MOUNT SYSTEM

PHOTO N/A

Details Info

Part No AWACS(MSA)1041464655.053

Description Antenna Mount System

Major Assembly Ground Satcom

Wpn Sys AWACS

Criticality Non-Critical

Annual Requirement 03

46. FRONT END ASSEMBLY

PHOTO N/A

Details Info

Part No AWACS(MSA)104.3.585.009

Description Front End Assembly

Major Assembly Ground Satcom

Wpn Sys AWACS

Criticality Non-Critical

Annual Requirement 03

47. SATCOM DATA PROCESSOR

PHOTO N/A

Details Info

Part No 104.2.131.22

Description Satcom Data Processor

Major Assembly Ground Satcom

Wpn Sys AWACS

Criticality Non-Critical

Annual Requirement 03

48. CONTROL CABLES 04 TYPES MPR

PHOTO N/A

Details Info

Part No ---

Description Control Cables 04 Types of MPR

Major Assembly MPR

Wpn Sys MPR

Criticality Non-Critical

Annual Requirement 03 Set

Page 60: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

49. POWER CABLES 16 TYPES OF MPR

PHOTO N/A

Details Info

Part No ---

Description Power Cables 16 Types of MPR

Major Assembly MPR

Wpn Sys MPR

Criticality Non-Critical

Annual Requirement 03 Set

50. OPTICAL FIBER CABLES 15 TYPES

PHOTO N/A

Details Info

Part No ---

Description Optical Fiber Cables 15 Types of MPR

Major Assembly MPR

Wpn Sys MPR

Criticality Non-Critical

Annual Requirement 03 Set

51. LNA B BAND ASSEMBLY

Details Info

Part No 51044600100

Description LNA B Band Assembly

Major Assembly Receiver

Wpn Sys THD

Criticality Non Critical

Annual Requirement 02

52. SATELLITE ROUTER

Details Info

Part No 9131-0102-0008

Description Satelite Router

Major Assembly Satcom

Wpn Sys Satcom

Criticality Non Critical

Annual Requirement 03

Page 61: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

53. LOGIC CARD

Details Info

Part No 422900

Description Logic Card

Major Assembly ADU 7150 Series

Wpn Sys SATCOM

Criticality Non Critical

Annual Requirement 04

54. CICC/2 CABLE

PHOTO N/A

Details Info

Part No 17TES0070

Description CICC/2 CABLE

Major Assembly Rose Analysis Unit

Wpn Sys Dornier

Criticality Non Critical

Annual Requirement 02

55. INTERFACE CABLE

PHOTO N/A

Details Info

Part No 17TES0071

Description Interface Cable

Wpn Sys Dornier

Major Assembly Rose Analysis Unit

Annual Requirement 02

56. OCTOPACK REPLACEMENT TOOL

Details Info

Part No 62265141

Description Octopack Replacement Tool

Wpn Sys LLTR

Major Assembly LLTR

Annual Requirement 05

Page 62: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

57. AMT-641

Details Info

Part No 143000331825

Description AMT-641

Wpn Sys THD-1955

Major Assembly Receiver

Annual Requirement 01

58. REPAIR OF ANTENNA POWER SUPPLY

Details Info

Part No 1025M630-002

Description Repair Of Antenna Power Supply

Wpn Sys MPR

Major Assembly Antenna System

Annual Requirement 05

59. IFF INTERROGATOR

Details Info

Part No 1015W147-001

Description IFF Interogator

Wpn Sys LLLWR

Major Assembly LLLWR

Annual Requirement 03

60. RC COMPUTER

PHOTO N/A

Details Info

Part No AEROSTAT / 1015L382-001

Description RC Computer

Wpn Sys Aerostat

Major Assembly Aerostat Balloon Complete With Rigging & Hardware

Annual Requirement 02

Page 63: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

61. TWS COMPUTER

PHOTO N/A

Details Info

Part No Aerostat / 1015L381-001

Description TWS Computer

Wpn Sys Aerostat

Major Assembly Aerostat Balloon Complete With Rigging & Hardware

Annual Requirement 02

62. OWS COMPUTER

PHOTO N/A

Details Info

Part No Aerostat / 1015L380-001

Description OWS Computer

Wpn Sys Aerostat/ 13 BRD

Major Assembly Aerostat Balloon Complete With Rigging & Hardware

Annual Requirement 05

63. REPRODUCTION UNIT

PHOTO N/A

Details Info

Part No IL-76/ BVS-I

Description Reproduction Unit

Wpn Sys IL-76

Major Assembly Self

Annual Requirement N/A

64. DUAL RECEIVE MODULE

Details Info

Part No 1110D/MPR 1093W665-002

Description Dual Receive Module

Wpn Sys MPR

Major Assembly Antenna System

Annual Requirement 30

Page 64: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INDIGENISATION REQUIRMENT OF IAF :16 BRD

1. HARNESS ASSEMBLY

Details Info

Part No SUACS/3-17343-00-01

Description Harness Assembly

Wpn Sys SU–30 MKI

Major Assembly Parachute Assembly

Annual Requirement 126

2. METAL COMPONENTS OF SU-30 HARNESS

Details Info

Part No SUACS/3-17343-00-01-AA to AH

Description Metal component of Harness Assembly - Su 30 MKI

Wpn Sys / Unit SU – 30 MKI/16 BRD

Major Assembly Harness Assembly

Annual Requirement 126x23 = 2898

Page 65: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INDIGENISATION

REQUIREMENTS

INDIAN AIR FORCE

Page 66: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PROPOSED ITEMS FOR

INDIGENISATION

1CIMD, AF

E-MAIL- [email protected]

CONTACT- 02550-272233

Page 67: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

CASING

Part No 5.12.6105.1580.00

Description Casing

Major

Assembly

Pipeline inside tank

Wpn Sys MIG-29

Criticality Non – Critical

Function To hold filter inside tank

Operating

Temp

Ambient

Operating

Pressure

Atmospheric

Medium Fuel

Material AL-9 (In lieu for 3 D printing)

Annual

Requirement 04

Page 68: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

RUBBER SLEEVE

Part No RH1-89-26-006-201

Description Rubber Sleeve

Major

Assembly

Surge Suppressor Assembly

Wpn Sys ARP-3 POD

Criticality Non – Critical

Function Absorbs fuel supply line surges

Operating

Temp

Ambient

Operating

Pressure

Atmospheric

Medium Fuel

Material To be analysed

Annual

Requirement 15

Page 69: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

Filter Element

Part no 8D2.966.706

Description Filter element

Major assembly AD-5A

Wpn sys MiG – 29

Criticality Critical

Function To filter air before entry into

anti ‘g’ valve

Operating temp 15-300 c

Operating pressure 1 Kgf/cm2

Medium Air

Material To be analysed

Annual requirement10

Page 70: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

FILAMENT

Part No LFSM 27-1000

Description Lamp landing

Major Assembly Landing light

Wpn Sys Mig-29

Criticality Non-critical

Function To illuminate the taxy track

during night flying.

Operating Temp Ambient

Operating Pressure Ambient

Atmospheric

Medium Air

Material To be analysed

Annual Requirement 216

Page 71: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

GREEN GLASS FILTER

PHOTO NOT AVAILABLE

PART NO A10160

DESCRIPTION Green glass filter

MAJOR ASSEMBLY Forward nav. Light

WPN SYS Mig-29

CRITICALITY Non-critical

FUNCTION It clearly indicates stbd

wing tip during night flying.

OPERATING TEMP Ambient

OPERATING PRESSURE Ambient

MEDIUM Air

MATERIAL To be analysed

ANNUAL REQUIREMENT 08

Page 72: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

HYDRAULIC DISC FILTER

Part no 8D6.270.001-06

Description Hydraulic disc filter

Major assembly Filter assembly

Wpn sys Su-30 MKI

Criticality Critical

Function Filtering hydraulic fluid in

pressure line both system

1 & 2.

Operating temp Ambient

Operating pressure N/K

Medium Hyd oil

Material To be analysed

Annual requirement 6019

Page 73: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

RIGHT BLOCK

Part No KD-E7P.575.03.09.000.0

Description Right block

Major Assembly CMDS ASO

Wpn Sys CMDS ASO

Criticality Critical

Function To extend power supply to

firing pins

Operating Temp -60 to +600 c

Operating Pressure Atmospheric

Medium Air

Material Metallic stroke and bakelite

Annual Requirement 30

Page 74: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

FILAMENT

Part No LFSM 27-250-1

Description Lamp Taxying

Major Assembly Taxy Lamp

Wpn Sys MIG-29

Criticality Non-critical

Function To illuminate the taxy track

during night flying.

Operating Temp Ambient

Operating Pressure Atmospheric

Medium Air

Material To be analysed

Annual Requirement 45

Page 75: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

LEFT BLOCK

Part No KD-E7P.575.03.11.000.0

Description Left block

Major Assembly CMDS ASO

Wpn Sys / Unit CMDS ASO

Criticality Critical

Function To extend power supply to

firing pins

Operating Temp -60 TO +600 C

Operating Pressure NK

Medium Air

Material Metallic stroke and Bakelite

Annual Requirement 20

Page 76: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

FILTER ELEMENT

Part no 8D2.966.706

Description Filter Element

Major assembly AD-5A

Wpn sys MiG - 29

Criticality Critical

Function Filter Air Before Entering To

Anti ‘G’ Valve

Operating temp 15-300 C

Operating pressure 1 Kgf/CM2

Medium Air

Material To be analysed

Annual requirement10

Page 77: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PROPOSED ITEMS FOR

INDIGENISATION

3 BRD, AF

E-MAIL- [email protected]

CONTACT- 0172-2641090

Page 78: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

BEAM ANTENNA CABLE

Part no 8AT-7103-30

Description BEAM ANTENNA CABLE

Major assembly KHF 1050 (HF Communication

system)

Wpn sys MI-17V 5

Criticality Non Critical

Function To receive and transmit the radio

signal for HF Communication

Operating temp -60 TO + 60˚ C

Operating pressure N/K

Medium Air/ ground

Material -60 TO + 60˚ C

Annual requirement50

Page 79: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

POWER SUPPLY MODULE

Part no SGKL.436744.006-10

Description POWER SUPPLY MODULE

Major assembly Multi Functional Display

Wpn sys M-53 P2 Aero engine

Criticality Non Critical

Function convert 27 V power supply and

provide to other sub –assemblies

( Range -15 V to 15 V

Operating temp - 40 TO +55˚ C

Operating pressure N/K

Medium Air/ ground

Material To be analysed

Annual requirement 100

Page 80: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INDICATION MODULE

Part no SGKL.467849.014-10

Description INDICATION MODULE

Major assembly Multi Functional Display

Wpn sys M-53 P2 Aero engine

Criticality Non Critical

Function Recording of real time

parameters and converting into

video signals, To control

switching on/off the fan, and to

control illumination and

brightness.

Operating temp - 40 TO +55˚ C

Operating pressure N/K

Medium Air/ ground

Material To be analysed

Annual requirement 100

Page 81: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

VIDEO PROCESSOR

Part no VIAM.468172.008

Description VIDEO PROCESSOR

Major assembly Multi Functional Display

Wpn sys M-53 P2 Aero engine

Criticality Non Critical

Function To process video signals and

display them as per mode of

selection of pages.

Operating temp - 40 TO +55˚ C

Operating pressure N/K

Medium Air/ ground

Material To be analysed

Annual requirement 100

Page 82: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

TV ADOPTOR

Part no VIAM.467221.002

Description TV ADOPTOR

Major

assembly

Multi Functional Display

Wpn sys M-53 P2 Aero engine

Criticality Non Critical

Function Conversion of analog signal into

digital signals.

Operating

temp

- 40 TO +55˚ C

Operating

pressure

NOT KNOWN

Medium Air/ ground

Material To be analysed

Annual

requirement100

Page 83: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

SYNTHESIZER MODULE ASSY

Part no 716026

Description SYNTHESIZER MODULE ASSEMBLY

Major

assembly

Multi Functional Display

Wpn sys M-53 P2 Aero engine

Criticality Non Critical

Function To provide ACR-500LK with a stable,

low noise, local oscillator signal for

transmit and receipt channel.

Operating

temp

- 40 TO +71 ˚ C

Operating

pressure

NOT KNOWN

Medium Air/ ground

Material To be analysed

Annual

requirement100

Page 84: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

POWER SUPPLY MODULEPart no 716024

Description POWER SUPPLY MODULE

Major assembly ACR-500 LK V/U HF

Wpn sys MI-17V 5

Criticality Non Critical

Function To provide seven different voltage (+12

V,_12V,_7.5 V,+5volt AC,+5volt DC ,+ 75 Volt

and 19 Volts)required for specific function within

the ACR-500LK.

Operating temp - 40 TO +71 ˚ C

Operating

pressure

Not known

Medium AIR/ GROUND

Material To provide seven different voltage (+12

V,_12V,_7.5 V,+5volt AC,+5volt DC ,+ 75 Volt

and 19 Volts)required for specific function within

the ACR-500LK.

Annualrequirement 50

Page 85: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

FILTER MODULE

Part no B81036

Description FILTER MODULE

Major assembly ACR-500 LK V/U HF

Wpn sys MI-17V 5

Criticality Non Critical

Function To provide filtration of unwanted

spurious and noise signal on

transmit channel and protection

against co located signal on the

receipt channel.

Operating temp - 40 TO +71 ˚ C

Operating pressure Not known

Medium Air/ ground

Material To be analysed

Annual requirement50

Page 86: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

POWER AMPLIFIER

Part no 716031

Description POWER AMPLIFIER

Major assembly ACR-500 LK V/U HF

Wpn sys MI-17V 5

Criticality Non Critical

Function To provide amplification of the

signal from the low level

transmit path to the final power

level required to transmit.

Operating temp - 40 TO +71 ˚ C

Operating pressure Not known

Medium Air/ ground

Material To be analysed

Annual requirement50

Page 87: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

ANALOGUE SIGNAL RECEPTION

MODULEPart no MPD-23

Description ANALOGUE SIGNAL RECEPTION

MODULE

Major assembly BPV-6-2

Wpn sys MI-17V 5

Criticality Non Critical

Function BPV-6-2

Operating temp - 60 TO +70 ˚ C

Operating pressure 46.7 K Pa

Medium Ambient

Material To be analysed

Annual requirement100

Page 88: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

EVENT SIGNAL RECEPTION MODULE

Part no MPD-14

Description EVENT SIGNAL RECEPTION

MODULE

Major assembly BPV-6-2

Wpn sys MI-17V 5

Criticality Non Critical

Function On receipt of various events like

hydraulic failure, fuel level warning,

input is provided for further

computing.

Operating temp - 60 TO +70 ˚ C

Operating pressure 46.7 K Pa

Medium Ambient

Material To be analysed

Annual requirement 100

Page 89: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

COMPUTATION AND GENERATION

MODULEPart no MVF-01-05

Description Computation and generation

module

Major assembly BPV-6-2

Wpn sys MI-17V 5

Criticality Non Critical

Function Conversion of various signals

and processing of various

events and to provide output.

Operating temp 46.7 K Pa

Operating

pressure

Not known

Medium Ambient

Material To be analysed

Annual

requirement100

Page 90: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

POWER SUPPLY MODULE

Part no MP-53

Description POWER SUPPLY MODULE

Major assembly BPV-6-2

Wpn sys MI-17V 5

Criticality Non Critical

Function To cater power requirement of

various sub modules.

Operating temp 60 TO +70 ˚ C

Operating

pressure

46.7 K Pa-

Medium Ambient

Material To be analysed

Annual

requirement100

Page 91: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

COVER

Part no 0-8-0062

Description COVER

Major assembly AI-20

Wpn sys AN-32

Criticality Non Critical

Function Covers the blank nut of pipe

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium AIR/GROUND

Material TO BE ANALYSED

Annual

requirement08

Page 92: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

SPRING OUTER

Part no 20-261-031

Description Spring outer

Major assembly AI-20

Wpn sys AN-32

Criticality Critical

Function Provide forward and rear word

movement to the shaft

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement10

Page 93: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

BUSHING

Part no 20-751-236

Description Bushing

Major assembly AI-20

Wpn sys AN-32

Criticality Critical

Function Prevents wear & tear of bearing

during rotation

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement10

Page 94: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

SPRING OUTER

Part no 20-1011-161

Description Spring outer

Major assembly AI-20

Wpn sys AN-32

Criticality Critical

Function Provide forward and rear word

movement to the shaft

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement15

Page 95: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

NT PISTON

Part no 20-11-249

Description NT PISTON

Major assembly AI-20

Wpn sys AN-32

Criticality Critical

Function Used with spring to act as

negative thrust assembly

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement15

Page 96: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

RING DAMPER

Part no 0780230206-02

Description RING DAMPER

Major assembly TV-3

Wpn sys Mi-17 V5

Criticality Critical

Function Prevents damping effect on 3rd

support assembly

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement10

Page 97: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

SHIELD (SCREEN)

Part no 7823-9017

Description SHIELD SCREEN

Major assembly TV-3

Wpn sys Mi-17 V5

Criticality Critical

Function Prevents damping effect on 3rd

support assembly

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement10

Page 98: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

SHIELD

Part no 7857-9082

Description SHIELD

Major assembly TV-3

Wpn sys Mi-17 V5

Criticality Non Critical

Function Prevents ingestion of coke

deposition in 4th & 5th support

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement10

Page 99: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

DAMPER RING

Part no 78230206-01

Description DAMPER RING

Major assembly TV-3

Wpn sys Mi-17 V5

Criticality Critical

Function Prevents damping effect on 3rd

support assembly

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement10

Page 100: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

SHIELD

Part no 7822-0314

Description SHIELD

Major assembly TV-3

Wpn sys Mi-17 V5

Criticality Critical

Function Prevents ingestion of coke

deposition in 2nd & support

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement10

Page 101: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

RING REAR

Part no 08-01-033

Description RING REAR

Major assembly AI-9V

Wpn sys Mi-17 V5

Criticality Critical

Function Used to maintain the gap between

impeller and turbine wheel

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement12

Page 102: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

RESTRICTOR

Part no 90102-118

Description Restrictor

Major assembly AI-9V

Wpn sys AI-9V

Criticality Critical

Function To restrict the flow of air so that

required air can be obtained for

engine starting

Operating temp -60 TO + 60˚ C

Operating pressure Not known

Medium Air/ground

Material To be analysed

Annual

requirement12

Page 103: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

FILTER

Part no 68-054

Description FILTER

Major assembly Prop

Wpn sys Mi-17 V5

Criticality Critical

Function Filter oil entering into propeller

assembly

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement12

Page 104: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

HOUSING REDUCTION GEAR

Part no 0780850620-03

Description Housing reduction gear

Major assembly Air starter

Wpn sys Mi-17 V5

Criticality Critical

Function Accommodate the gears of air

starter

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement12

Page 105: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

FILTER CASING

Part no 780679730

Description Filter casing

Major assembly Oil filter

Wpn sys Mi-17 V5

Criticality Non Critical

Function Accommodate the filter element

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement12

Page 106: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

VALVE PLATE

Part no 7884.0411

Description Valve plate

Major assembly ABOV

Wpn sys Mi-17 V5

Criticality Non Critical

Function Open and close the air path of

ABOV

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement12

Page 107: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

CASING

Part no 7884.405

Description Casing

Major assembly ABOV

Wpn sys Mi-17 V5

Criticality Non Critical

Function Accommodate the valve housing

and spring

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement12

Page 108: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

OPB CASING

Part no 7867.3040-01

Description OPB Casing

Major assembly OPB

Wpn sys Mi-17 V5

Criticality Critical

Function Accommodate the accessories of

OPB

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement12

Page 109: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

GEARS

Part no 7867.0589

Description Gears

Major assembly OPB

Wpn sys MI-17 V5

Criticality Critical

Function Transfer the rotation

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement12

Page 110: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

IGB CASING

Part no 7826.0850

Description IGB Casing

Major assembly IGB

Wpn sys Mi-17 V5

Criticality Critical

Function Accommodate the accessories of

IGB

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement12

Page 111: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INTERNAL SLEEVE

Part no 7826.0353

Description Internal sleeve

Major assembly IGB

Wpn sys Mi-17 V5

Criticality Non Critical

Function To accommodate bearing and

gear of IGB

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement11

Page 112: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

UPPER SLEEVE

Part no 7826.9160

Description Upper Sleeve

Major assembly IGB

Wpn sys Mi-17 V5

Criticality Non Critical

Function To accommodate bearing of IGB

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement11

Page 113: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

EGB ADAPTOR

Part no 7862.0990

Description EGB Adapter

Major assembly IGB

Wpn sys Mi-17 V5

Criticality Non Critical

Function To accommodate drive

mechanism for H/C

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement11

Page 114: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

FT ADAPTOR

Part no 7862.1980

Description FT Adapter

Major assembly EGB

Wpn sys Mi-17 V5

Criticality Non Critical

Function To accommodate F/T shaft

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium Air/ground

Material To be analysed

Annual

requirement11

Page 115: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

SGD HOUSING

Part no 7862.2070.02

Description SGD Housing

Major assembly SGD

Wpn sys Mi-17 V5

Criticality Critical

Function Accommodate the SGD gears and

accessories

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium AIR/GROUND

Material TO BE ANALYSED

Annual

requirement11

Page 116: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PUMP BODY

Part no 20-757-833

Description Pump Body

Major assembly COP

Wpn sys Mi-17 V5

Criticality Non Critical

Function To accommodate the accessories of

COP

Operating temp -60 TO + 60˚ C

Operating

pressure

Not known

Medium AIR/GROUND

Material TO BE ANALYSED

Annual

requirement11

Page 117: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

ON BOARD AIRCARFT CLOCK

Weapon platform/systemMI-17V5

Part no

V18-956.22.28.4FK

Major assy Self

Function Indicates flight time and

current time

Material specification N/k

Annual requirement 19

Working medium Air

Working pressure N/k

Working temperature -60 to +60˚c

Page 118: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INDICATOR RADIO ALTIMETER

Weapon platform/systemMI-17V5

Part noA-052-4A

Major assy A-037-28

Function Displaying of altitude of a/c

from immediate terrain

Material specification N/k

Annual requirement 10

Working medium Air

Working pressure N/k

Working temperature -60 to +60˚c

Page 119: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PROPOSED ITEMS FOR

INDIGENISATION

4 BRD, AF

E-MAIL- [email protected]

CONTACT- 0512-2457668

Page 120: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

344 MM CORE BURNER RING

Part no VJA/303-093-803-0

Description Burner ring 344 mm diameter

Major assembly Fan burner ring 344 mm

diameter

Wpn sys M-53 P2 Aero engine

Criticality Critical

Function Hold 344 mm Dia spray ring

with heat shield

Operating temp 800-10000c

Operating pressure 03 bar

Medium Hot air

Material KC25NW

Annual

requirement06

Page 121: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

610 MM CORE BURNER RING

Part no VJA/303-093-320-0

Description Burner ring 610 mm diameter

Major assembly Fan burner ring

Wpn sys M-53-P2 Aero engine

Criticality Critical

Function Hold 610 mm Dia spray ring

with heat shield

Operating temp 800-10000c

Operating

pressure

03 bar

Medium Hot air

Material KCN22W

Annual

requirement06

Page 122: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

866 MM CORE BURNER RING

Part no VJA/303-094-601-0

Description Burner ring 866 mm diameter

Major assembly Fan burner ring

Wpn sys M-53-P2 Aero engine

Criticality Critical

Function Hold spray segment with heat

shield

Operating temp 800-10000c

Operating pressure 03 bar

Medium Hot air

Material KCN22W

Annual requirement06

Page 123: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

LEVER SYNCHRONISING

Part no VJA/303-141-201-0

Description Lever synchronizing

Major assembly Exhaust nozzle

Wpn sys M-53-P2 Aero engine

Criticality Critical

Function To synchronise the

displacement of hot flap (inner

flap) and cold flap (outer flap)

with the help of link.

Operating temp 4000c

Operating pressure Ambient

Medium Air

Material KC25NW

Annual requirement06

Page 124: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

LEVER ACTUATING

Part no VJA/303-141-002-0

Description Lever Actuating

Major assembly Exhaust nozzle

Wpn sys M-53-P2 Aero engine

Criticality Critical

Function To synchronise the

displacement of hot flap (inner

flap) and cold flap (outer flap)

with the help of link.

Operating temp 3000c

Operating pressure Ambient

Medium Air

Material KC25NW

Annual requirement 80

Page 125: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

COLD FLAPS(MODIFIED & UNMODIFIED FOR INNER AND OUTER)

Part no 303-030-920-0, 303-030-914-0,

303-031-014-0, 303-031-020-0

Description Cold flap

Major assembly Exhaust nozzle

Wpn sys M-53-P2 Aero engine

Criticality Critical

Function Cooling of nozzle equipment

Operating temp 3000c

Operating pressure 1.5 bar

Medium Air

Material NC22FED & Z12CNKDW20

Annual requirement 13

Page 126: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

SUPPORT SEAL

Part no VJA/979322

.

Description Support seal

Major assembly Exhaust nozzle control pump

Wpn sys M-53-P2 Aero engine

Criticality Critical

Function To prevent leakage of fuel into

the case assembly under the

pressure of 120 bar.

Operating temp 15-350c

Operating pressure 10-180 bar

Medium Fuel

Material Carbon graphite/C-G Aero II

Annual requirement 40

Page 127: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

LINER STRUT THIN

Part no VJA/303-808-704-0

Description Liner strut thin

Major assembly Turbine frame

Wpn sys M-53 aero engine

Criticality Critical

Function To give streamline flow to air

coming from turbine.

Operating temp 9000c

Operating pressure 30 bar

Medium Hot air

Material KC20WNX

Annual requirement78

Page 128: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

LINER STRUT THICK

Part no VJA/303-808-904-0

Description Liner strut thick

Major assembly Turbine frame

Wpn sys M-53 aero engine

Criticality Critical

Function To give streamline flow to air

coming from turbine.

Operating temp 9000c

Operating

pressure

30 bar

Medium Hot air

Material KC20WNX

Annual

requirement 39

Page 129: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

SEAL MECHANICAL

Part no VJA/801157, VJA/801159, VJA/801161

236 ST/V 103039 , 236ll/77561701

Description Seal mechanical/ring oil seal

Major assembly Accessory gear box/front main bearing

Wpn sys M53-p2 aero engine/viper a/e

Criticality Critical

Function To prevent air /oil leak from various

rotating bearings and gears of

Accessory gear box.

Operating temp -10 to 120 deg c

Operating press 4 bar

Medium Lubricating oils-turbo NV coil 13 b, ox-

38

Material Graphite base material aero-ii

Annual requirement 02 for item 1 to 3, 33 for item 3 08 for

item 5

Page 130: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

LIFE EXTENSION STUDY OF

ASL ITEMS(07 ITEMS)

Description Total 07 types of components

Major assembly M-53 P2 Aero engine

Wpn sys M-53 Aero engine

Criticality Critical

Function All the items are for life

extension of their authorized

service life

Operating temp Up to 1300 deg c

Operating pressure 09 bar

Medium Hot gases

Material NC19FENB, Z8NCDT42,

NC20K14

Page 131: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

REPLACMENT OF VANES OF

6-7 STAGE STATOR ASSY(MOD-3)

Part no 303-007-720-0, 303-008-223-0

303-008-620-0, 303-210-710-0

303-022-017-0

Description Stator vanes of 4-7 stage of

MOD-3

Major assembly HP Compressor MOD-3

Wpn sys M-53 Aero engine

Criticality Critical

Function To assist in converting the

kinetic energy into pressure

energy.

Operating temp 950 º C

Operating pres. 3.2 bar

Medium Hot gas

Material Z12C13

Page 132: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

REPLACMENT OF LIP OF CBR BY

DIFFUSIOIN BRAZING ON

344 & 610 MM BURNER RINGS

Part no VJA/303-093-803-0 , VJA/303-093-

803-0

.

Description BURNER RING 344 MM & 610MM

Major assembly MODULE-8

Wpn sys M-53 Aero Engine

Criticality CRITICAL

Function The purpose of the 344 mm Dia

and 610 mm Dia burner ring is to

supply the fuel throughout the A/B

operation of engine.

Operating temp 800-10000c

Operating pressure 03 bar

Medium Hot air

Material KC25NW

Page 133: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INIDGENISATION OF HARNESS M-53 AERO-

ENGINE INCLUDING TT-7 HARNESS

Part no ------

Description TT-7 harness(including modified

harness)

Major assembly M-53 Aero engine

Wpn sys M-53 Aero engine

Criticality Critical

Function It send and receive electrical

signals to various sensors and

actuators install on aero engine.

Operating temp Not known

Operating pressure Ambient pressure

Medium Air

Material N/k

.

Page 134: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

SPECIAL CONTAINERS FOR

TRANSPORTING CRITICAL

COMPONENT OF M-53 AERO ENGINE

Part no 399-0025-584-0,399-005-026-0,

399-005-025-0, 399-002-726-0

Description CONTAINERS FOR MFCU,

ABFCU, EFCU, AB PUMP

Major assembly N/A

Wpn sys M-53 G/E

Criticality Non-critical

Function

The container is used for

transporting the critical

components /accessories.

Operating temp Ambient

Operating pres. Atmospheric pressure

Medium Air

Material N/k

Page 135: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

DIFFUSION BRAZING OF MODULE-4

COMBUSTION CHAMBER OF M-53

Part no 303-016-924/927/941/944-0

Description Diffusion brazing on cc of

mod-4

Major assembly N/a

Wpn sys M-53 aero engine

Criticality Critical

Function Air fuel mixture is supplied

in pre atomised form to the

combustion chamber .

Operating temp Up to 1300ºC

Operating pres. N/A

Medium Air/fuel

Material NC22FED

Annual requirement 10-20 repairs

Page 136: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

REPAIR OF NOZZLE GUIDE VANES

MODULE-5 OF M-53 A/E

Part no 303-180-014-0

Description Stage-1 nozzle guide vane

Major assembly M53-P2 Aero engine.

Wpn sys M53-P2 Aero engine

Criticality Critical

Function The nozzle directs hot gas flow

coming from the combustion

chamber to the turbines.

Operating temp Up to 1500º C

Operating pres. N/A

Medium Hot air

Material Heat resistant alloy

(KC24NWTA)

Annual

requirement

10-20 repairs

Page 137: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

BELLOWS ASSEMBLY

Part no VJA/1231-00

Description Bellows assembly

Major assembly ABFCU

Wpn sys Mirage-2000

Criticality Critical

Function Regulates fuel flow of

metering valve

Operating temp 100⁰c

Operating

pressure

80 bar

Medium Fuel

Material N/k

Annual

requirement03

Page 138: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

FILTER

Part no VJA/978792-100

Description Filter

Major assembly ENCP

Wpn sys Mirage-2000

Criticality Critical

Function To supply filtered fuel to servo

and hp piston

Operating temp Below 30⁰c

Operating

pressure

120 bar

Medium Fuel

Material N/k

Annual

requirement07

Page 139: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

ELEMENT FILTERING

Part no GA70962

Description Element filtering

Major assembly Oil failure solenoid valve

Wpn sys Mirage-2000

Criticality Critical

Function Filter the air

Operating temp Ambient

Operating pressure Atmospheric

Medium Air/Oil

Material N/k

Annual requirement01

Page 140: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

BELLOWS BALL JOINT VALVE ASSY

Part no VJA/303-940-903-0

Description Bellows ball joint valve assy

Major assembly Pressurizing valve assembly

Wpn sys / unit Mirage-2000

Criticality Critical

Function It operates in oil failure control

mode at a given altitude

Operating temp (10-50) ⁰c ± 2⁰c

Operating press 1-2 bar

Medium Air

Material N/k

Annual

requirement01

Page 141: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PROPOSED ITEMS FOR

INDIGENISATION

5BRD, AF

E-MAIL- [email protected]

CONTACT- 0422-2683381

Page 142: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

OBOGS CONCENTRATOR

Part no 9571210619

Description OBOGS Concentrator

Major assembly OBOGS Concentrator

Wpn sys PC-7 MK-II

Criticality Non critical

Function Separates the oxygen from the

other constituents of air

Operating temp Ambient

Operating pressure Ambient

Medium Air

Material To be analysed

Annual requirement15

Page 143: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

BRAKE FLUID RESERVOIR

Part no 9594751112

Description Brake fluid reservoir

Major assembly Brake fluid reservoir

Wpn sys PC-7 MK-II

Criticality Non critical

Function To fill and service the system are

installed on the power package

Operating temp Not specified

Operating

pressure

Not specified

Medium Hydraulic

Material To be analysed

Annual

requirement06

Page 144: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

CYLINDER DOOR

Part no 5323009275

Description Cylinder door

Major assembly Cylinder door

Wpn sys PC-7 MK-II

Criticality Non critical

Function It operates hydraulically

provides open and closing of

landing gear doors

Operating temp Not specified

Operating pressure 1800-3000 psi

Medium Hydraulic

Material To be analysed

Annual requirement 02

Page 145: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

CYLINDER BRAKE

Part no 9594751131

Description Cylinder brake

Major assembly Cylinder brake

Wpn sys PC-7 MK-II

Criticality Non critical

Function Operated from the associated

interconnected toe pedals

Operating temp Not specified

Operating pressure Not specified

Medium Hydraulic

Material To be analysed

Annual requirement08

Page 146: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PROPELLER GOVERNOR

Part no 9682914802

Description Propeller governor

Major assembly Reduction gear box

Wpn sys PC-7 MK-II

Criticality Non critical

Function To keep the propeller at a speed

of 2000 rpm

Operating temp Not specified

Operating pressure Not specified

Medium Engine

Material To be analysed

Annual requirement05

.

Page 147: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PARK BRAKE VALVE

Part no 9594751120

Description Park brake valve

Major assembly Park brake valve

Wpn sys PC-7 MK-II

Criticality Non critical

Function Operated by applying toe

brakes and pulling the parking

brake handle

Operating temp Not specified

Operating pressure Not specified

Medium Hydraulic

Material To be analysed

Annual requirement03

.

Page 148: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

CYLINDER NLG

Part no 5323009276

Description Cylinder nlg

Major assembly Cylinder nlg

Wpn sys PC-7 MK-II

Criticality Non critical

Function It operates hydraulically provides

extension and retraction of landing

gear

Operating temp Not specified

Operating pressure 1800-3000 psi

Medium Hydraulic

Material To be analysed

Annual requirement03

Page 149: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

REGULATOR OXYGEN

Part no 9571210623

Description Regulator oxygen

Major assembly Cockpit RH console

Wpn sys PC-7 MK-II

Criticality Non critical

Function Control the OBOGS

concentrator

Operating temp Ambient

Operating pressure Ambient

Medium Air

Material To be analysed

Annual requirement18

.

Page 150: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

TACAN TRC2634 ASSY

Part no 5345209009

Description TACANT RC 2634 assy

Major assembly TACAN TRC 2634 assy

Wpn sys PC-7 MK-II

Criticality Non critical

Function The TACAN Tx-Rx transmits

signals to TACAN/DME ground

stations and receives coded

replies

Operating temp Ambient

Operating pressure Ambient

Medium Air

Material To be analysed

Annual requirement 08

.

Page 151: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

CVFDR

Part no 5313009014

Description CVFDR

Major assembly CVFDR

Wpn sys PC-7 MK-II

Criticality Non critical

Function Automatically records cockpit

audio and flight data when

electrical power is connected to

the system

Operating temp Ambient

Operating pressure Ambient

Medium Air

Material To be analysed

Annual requirement 03

Page 152: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

EID

Part no 5774009013

Description EID

Major assembly EID

Wpn sys PC-7 MK-II

Criticality Non critical

Function Engine indication display (EID) in

each cockpit shows the various

parameters related to engine

Operating temp Ambient

Operating pressure Ambient

Medium Air

Material To be analysed

Annual requirement 14

Page 153: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PFD

Part no 5463009020

Description PFD

Major assembly PFD

Wpn sys PC-7 MK-II

Criticality Non critical

Function Displays data that is supplied

by other systems on the

aircraft

Operating temp Ambient

Operating pressure Ambient

Medium Air

Material To be analysed

Annual requirement08

.

Page 154: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

ECS CONTROL PANEL

Part no 9599001609

Description ECS Control panel

Major assembly Front cockpit ECS control panel

Wpn sys PC-7 MK-II

Criticality Non critical

Function It has a system of ducts and

control levers to distribute the air

Operating temp Ambient

Operating pressure Ambient

Medium Air

Material To be analysed

Annual requirement 03

.

Page 155: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

TRANSCEIVER,UHF

Part no 9859911649

Description Transceiver, UHF

Major assembly Transceiver, UHF

Wpn sys PC-7 MK-II

Criticality Non critical

Function Uhf transceiver operates over

the frequency range 225.000

Mhz to 399.975 Mhz, in

increments of 25khz

Operating temp Ambient

Operating pressure Ambient

Medium Air

Material To be analysed

Annual requirement 01

Page 156: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

SFD

Part no 9759632782

Description SFD

Major assembly SFD

Wpn sys PC-7 MK-II

Criticality Non critical

Function It is a standby system that

supplies attitude, heading and air

data from its own sources and

navigation data from external

sources

Operating temp Ambient

Operating pressure Ambient

Medium Air

Material To be analysed

Annual requirement 03

Page 157: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

AMPLIFIER, FUEL QTY

Part no 9753731132

Description Amplifier, f uel qty

Major assembly Amplifier

Wpn sys PC-7 MK-II

Criticality Non critical

Function Regulation circuitry to maintain

system accuracy

Operating temp Ambient

Operating pressure Ambient

Medium Air

Material To be analysed

Annual requirement03

Page 158: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

AHRU

Part no 9859911891

Description AHRU

Major assembly AHRU

Wpn sys PC-7 MK-II

Criticality Non critical

Function It is a rectangular box that

contains fibre-optic gyros and

accelerometers that are used for

acceleration and rate sensing

Operating temp Ambient

Operating pressure Ambient

Medium Air

Material To be analysed

Annual requirement 02

Page 159: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

TRANSMITTER, AOA

Part no 9754421406

Description Transmitter, AOA

Major assembly Transmitter

Wpn sys PC-7 MK-II

Criticality Non critical

Function To calculate the current AOA

of the aircraft

Operating temp Ambient

Operating pressure Ambient

Medium Air

Material To be analysed

Annual requirement02

Page 160: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

EDCU

Part no 9759632434

Description EDCU

Major assembly EDCU

Wpn sys PC-7 MK-II

Criticality Non critical

Function EDCU is connected to all

engine-related sensors and

most of the warning system

sensors on the aircraft

Operating temp Ambient

Operating pressure Ambient

Medium Air

Material To be analysed

Annual requirement 03

Page 161: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

DIGITAL INDICATOR

Part no Mi-585301-2

Description Digital indicator (DI-5001)

Major assembly Front cockpit digital

indicator

Wpn sys AVRO

Criticality Critical

Function It displays on route weather

information, in the form of

colour code

Operating temp Ambient temperature

Operating pressure Ambient pressure

Medium Air

Material Non corrosive material

Annual requirement45

Page 162: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

RECEIVER TRANSMITTERPart no Mi-585300-1

Description Receiver transmitter

Major assembly Receiver transmitter

Wpn sys AVRO

Criticality Non critical

Function It generates high RF power

output to transmit through

antenna and receives echoes

from target

Operating temp Ambient temperature

Operating pressure Ambient pressure

Medium Air

Material Non corrosive material

Annual requirement45

Page 163: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

AP COUPLING UNITPart no 6TC-1083

Description AP coupling unit

Major assembly Auto pilot system

WpnSys AVRO

Criticality Non critical

Function Couples the radio

error signal from

VOR/LOC and

glide slope receiver for

auto approach

Automatic control of the

aircraft height when height

lock is engaged

Operating temp Ambient temp.

Operating pres. Static pressure

Medium Normal air

Material Non ferrous material

Annual Requirement 30

Page 164: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PROPOSED ITEMS FOR

INDIGENISATION

9 BRD, AF

E-MAIL- [email protected]

CONTACT- 020-26633281

Page 165: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

DVTR (JAGUAR)

Part No 31700000

Description Digital Video Tape Recorder

Major Assembly DVTR

Wpn Sys Jaguar

Criticality Non critical

Function Video Recording Of HUD

Symbiology, SMD VIDEO, LDP

Video And Audio Recording.

Operating Temp Ambient

Operating

Pressure

Atmospheric

Medium Air

Annual

Requirement

10

Page 166: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

DUPLEXER FILTER

Part No 310 MOT/45/MOT/150A

Description Motorola repeater station

Major Assembly Motorola repeater station

Wpn Sys VHF Ground Radio System

Criticality Non critical

Function It allows two radios to operate on

single antenna for transmission &

reception

Operating Temp Ambient

Operating

Pressure

Atmospheric

Medium Ground

Annual

Requirement

20

Page 167: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

RECHARGEABLE (PRB)

BATTERY SARBE 8Part No 310 /101025 BE 586 SARBE-8

Description Rechargeable battery

Major Assembly PRB SARBE-8

Wpn Sys SARBE-8

Criticality Critical

Function Battery Provides Power Supply To

PRB and ELT FO training purpose.

Operating Temp -20o C TO + 55o C

Operating

Pressure

N/K

Medium Air

Annual

Requirement

750

Page 168: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PULL PIN SWITCH

Part No 310D/33287

Description Pull pin switch

Major Assembly PRB / ELT

Wpn Sys SARBE-8

Criticality Non-critical

Function Used in the SARBE equipment for

auto initiation of the emergency

location signals

Operating Temp Ambient

Operating

Pressure

Atmospheric

Medium Air

Annual

Requirement

10

Page 169: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

FLY BY WIRE Su-30 MKI TESTER

Part No SDU-10 MK

Description Fly- by- wire control sys

Major Assembly SELF

Wpn Sys Flying control sys

Criticality Non-critical

Functionoperating system from control &

operate, aircraft control system of

Su-30 MKI

Operating Temp 25 ± 10o C

Operating

Pressure

645 TO 795 MM OF HG

Medium Ground

Page 170: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

BP-95-02 P/S UNIT Su-30 MKI TESTER

Part No PZP-117

Description BP-95 tester for voltage

Major Assembly Fly-by-wire control system

Wpn Sys FBW sys.

Criticality Non critical

Function To Check Various Voltages Of BP-

95 OF FBW system.

Operating Temp 25 ± 10o C

Operating

Pressure

645 TO 795 MM OF HG

Medium Ground

Page 171: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

CMDS Su-30 MKI TESTER

Part No UV30MKI-8700KPA

Description UV30MKI-8700KPA

Major Assembly CMDS

Wpn Sys Su-30 MKI

Criticality Non critical

FunctionFor testing ejection pod,

control panel, controller

Operating Temp 25 ± 10o C

Operatin

g

Pressure

645 TO 795 MM OF HG

Medium Ground

Page 172: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

KPA-BRZU-115VO-1 Su-30 MKI TESTER

Part No KPA-BRZU-115VO-1

Description Tester

Major Assembly BRZU 115V

Wpn Sys SSC TESTER

Criticality Non critical

FunctionTo test voltage regulation ,control

and protection unit .

Operating Temp 25 ± 10o C

Operating

Pressure

645 TO 795 MM OF HG

Medium Ground

Page 173: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

BAKNA-115V Su-30 MKI TESTER

Part No KPA-BKNA-115V

Description Tester

Major Assembly KPA-BKNA-115V

Wpn Sys SSC Tester

Criticality Non critical

Function To Test External Power Control

Unit.

Operating Temp 25 ± 10o C

Operating

Pressure

645 TO 795 MM OF HG

Medium Ground

Page 174: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

DIGITAL VIDEO RECORDER

Part No 0535242007

Description Digital video recorder

Major Assembly MIRAGE-2000

Wpn Sys MIRAGE-2000

Criticality Critical

Function To record audio & video operational

information of lightening pod

Operating Temp Ambient

Operating

Pressure

Atmospheric

Page 175: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

ARTEX ELT BATTERY PACK

Part No STA/452-0133

Description ARTEX battery pack

Major Assembly ARTEX C-406-1 ELT

Wpn Sys AN-32

Criticality Critical

Function ARTEX ELT battery is required for operation of

ARTEX C-406-1 ELT system

Operating Temp -20o to +55o C

Operating Pressure N/K

Medium AIR

Annual Requirement 20

Page 176: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

BATTERY PACK

Part No STA/S1820516-99

Description BATTERY PACK

Major Assembly KANNAD ELT

Wpn Sys AN-32

Criticality Critical

Function KANNAD ELT battery is required for operation of

KANNAD ELT system

Operating Temp -20o to +55oC

Operating Pressure N/K

Medium AIR

Annual Requirement 20

Page 177: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PROPOSED ITEMS FOR

INDIGENISATION

11 BRD, AF

E-MAIL- [email protected]

CONTACT- 02550-276641/46

Page 178: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

NCDC 64 GB ASSY

Part no AD312040-01

Description Network centric data card

Major assembly SS DVRS

Wpn sys / unit SU-30 MKI

Criticality Non-critical

Function To record 01 Ch audio & 04 Ch

video

Operating temp -54 to +95°c

Operating pressure 1.04 psi

Medium Air

Material To be analysed

Annual requirement50

Page 179: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

TEMPERATURE SENSOR

Part no DT-211

Description Temperature sensor

Major assembly DT-211

Wpn sys / unit Mig-29

Criticality Critical

Function It feeds electrical signal to air

intake system

Operating temp -60 to +300°c

Operating

pressure

Ambient

Medium Air

Material To be analysed

Annual

requirement14

Page 180: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

SEAT POSITION SENSOR

Part no 032001A-00/ 032001A-01

Description Seat position sensor

Major assembly Ejection seat

Wpn sys Su-30 MKI

Criticality Critical

Function To measure the height of the

ejection seat inside the cockpit

Operating temp Ambient

Operating pressure Atmospheric

Medium Air

Material To be analysed

Annual

requirement10

Page 181: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PRESS TO TALK SWITCH

Part no 83-452-519

Description Press to talk switch

Major assembly V/UHF communication trans

receiver

Wpn sys MiG-29

Criticality

Function To act as 2 way switch for

selection between rt set 1 and rt

set 2 of the MiG-29 UPG ac

Operating temp Ambient

Operating pressure Atmospheric

Medium Air

Material To be analysed

Annual requirement 20

Page 182: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

AUTONOMOUS POWER SUPPLY UNIT

Part no 903.7200.1400.02

Description Autonomous power supply unit

Major assembly Ejection seat

Wpn sys Su-30 MKI

Criticality Critical

Function To act as main source of power

for ejection control system

during ejection

Operating temp Ambient

Operating pressure Atmospheric

Medium Air

Material To be analysed

Annual requirement30

Page 183: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

INSERT

Part no 170.8740.147

Description Insert

Major assembly Launcher device

Wpn sys Su-30 MKI

Criticality Non-critical

Function Cover of radar APM-90 antenna

Operating temp Ambient

Operating pressure Ambient

Medium Air

Material Aluminium silicate ceramic

Annual requirement10

Page 184: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

BRACKET FOR FIRING HANDLE

Part no 903.9220.1330.04A

Description Bracket for firing handle

Major assembly Ejection seat oxygen system

Wpn sys Su-30 MKI

Criticality Non-critical

Function To secure the red lever of

ejection control mechanism

Operating temp 200 0 to 5000c

Operating pressure 20 Kgf

Medium Air

Material To be analysed

Annual requirement10

Page 185: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

CASING

Part no 5.12.6105.1580.00

Description Casing

Major assembly Pipeline

Wpn sys MIG-29

Criticality Non-critical

Function To hold pipeline inside tank no

1,2 and 3

Operating temp Atmospheric

Operating pressure Ambient

Medium Air

Material Al-9

Annual requirement04

Page 186: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

TX BUTTON(PTT SWITCH)

PART NO 83-452-519

DESCRIPTION TX Button (PTT Switch)

MAJOR ASSEMBLY Communication Set R-833B

WPN SYS / UNIT R-833B

CRITICALITY Critical

FUNCTION It is a spring loaded two way switch, for

selection between COM 1 and COM 2 of

MiG-29UPG aircraft.

OPERATING TEMP -40° C to +71° C

OPERATING

PRESSURE

N/K

MEDIUM Airborne ( fitted in aircraft)

MATERIAL To be analysed

ANNUAL

REQUIREMENT20

Page 187: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PROPOSED ITEMS FOR

INDIGENISATION

12 BRD, AF

E-MAIL- [email protected]

CONTACT- 011-25318704

Page 188: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PULSE TWT

PHOTO

Part no 304B628002

Description Pulse TWT

Major assembly ELTA ASPJ POD

Wpn sys ELTA ASPJ

Criticality Critical

Function The TWT amplifies RF signal to

provide a typical saturation

output RF power of 63 DBM.

Operating temp - 550 c to +850 c

Operating pressure Atmospheric

Medium Air

Material Electronic components

Annual requirement 10

Page 189: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

CW TWT

PHOTO

Part no 3046N503

Description CW TWT

Major assembly ELTA SPJ POD

Wpn sys ELTA ASPJ

Criticality Critical

Function it is used to amplify the RF signal

to provide a typical saturation o/p

RF power of 53 DBM.

Operating temp - 550 c to +850 c

Operating pressure Atmospheric

Medium Air

Material Electronic components

Annual requirement 10

Page 190: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

CW HVPS

PHOTO

Part no 3046N510-005

Description CW HVPS

Major assembly ELTA SPJ POD

Wpn sys ELTA ASPJ

Criticality Critical

Function Generates high voltage ranging

from +/- 15 v, 6.3 v, 750 v, 270 v,

5 kv dc, 2.5 kv dc power supply

Operating temp - 550 c to +850 c

Operating pressure Atmospheric

Medium Air

Material Electronic components

Annual requirement 05

Page 191: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PULSE HVPS

PHOTO

Part no 3046J511

Description Pulse HVPS

Major assembly ELTA SPJ POD

Wpn sys ELTA ASPJ

Criticality Critical

Function Specialized power supply which deals

with high voltage transitions i.e

6.3 v-10.7 kv

Operating temp - 550 c to +850 c

Operating pressure Atmospheric

Medium Air

Material Electronic components

Annual requirement 05

Page 192: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PROPOSED ITEMS FOR

INDIGENISATION

16 BRD, AF

[email protected]

CONTACT-011-25672972

Page 193: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

METAL COMPONENT- SU-30 HARNESS

PHOTO

Part no a) SUACS/3-17343.00.1-AG

b) SUACS/3-17343.00.1-AC

c) SUACS/3-17343.00.1-AH

d) SUACS/3-17343.00.1-AA

Description a) Adaptor with buckle

b) Buckle small for QRL TP

c) Restraint buckle

d) Split buckle

Major assembly Ejection Seat

Wpn sys Su-30

Criticality Critical

Function For Transferring Loads And

Routing Of Tapes In Harness .

Operating temp Ambient Condition

Operating pressure Atmospheric

Medium AIR

Material 30 KGSHA

Annual requirement 250

Page 194: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

BANDOLIER ASSEMBLY

PHOTO

Part no PC-7 / 9593002026

Description Bandolier Assembly

Major assembly Ejection seat

Wpn sysem PC-7

Criticality Critical

Function It withdraws lowering line and

connects the survival pack

with occupant.

Operating temp Ambient Temperature

Operating pressure Atmospheric

Medium Air

Material NYLON 66

Annual requirement 126

Page 195: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

LEG STRAP LEFT SIDE

Part no 903-9210-290-04

Description Leg Strap Left Side

Major assembly Leg Restraint System

Wpn sys Su-30 MKI

Criticality Critical

PHOTO Function It restrain pilot’s leg during

ejection

Operating temp Ambient

Operating pressure Atmospheric

Medium Air

Material Nylon

Annual requirement 40

Page 196: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

LEG STRAP RIGHT SIDE

PHOTO

Part no 903-9210-290-05

Description Leg strap right side

Major assembly Leg Restraint System

Wpn sys Su-30 MKI

Criticality Critical

Function It restrain pilot’s leg during

ejection

Operating temp Ambient

Operating pressure Atmospheric

Medium Air

Material Nylon

Annual requirement 40

Page 197: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

N0 35 LINEN THREAD 08 LBF

PHOTO

Part no BSF 34 / NO 35 / BLACK /

PCPL

Description NO 35 Linen Thread

Major assembly Ejection Seat

Wpn sys PC-7

Criticality Non-critical

Function To secure canopy withdrawal

line sleeve on shackle.

Operating temp Ambient

Operating pressure Atmospheric

Medium Air

Material Linen

Annual requirement 1000 Mtrs

Page 198: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

METALLIC REEL OF DWL

PHOTO

Part no 15A/MBEU 65581

Description Metallic reel

Major assembly DWL KIRAN

Wpn sys KIRAN

Criticality Non-critical

Function Used to connect DWl to the

drogue gun of ejection seat

Operating temp Ambient

Operating pressure Atmospheric

Medium Air

Material Carbon Steel ( IS : 2073-1970)

Annual requirement 100

Page 199: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

PIN SECURING OF DWL KIRAN

PHOTO

Part no 27L/O/MBEU/117

Description Pin securing

Major assembly DWL KIRAN

Wpn sys KIRAN

Criticality Non- critical

Function Used to connect DWl to the

drogue gun of ejection seat

Operating temp Ambient

Operating pressure Atmospheric

Medium Air

Material Spring steel wire ( Spec BS :

1408-C))

Annual requirement 100

Page 200: INDIGENISATION REQUIRMENT OF IAF : 1CIMD 1. GYRO

HOUSING OF DWL KIRAN

PHOTO

Part no 27L/3502-2

Description Pin securing

Major assembly DWL KIRAN

Wpn sys Kiran

Criticality Non-critical

Function Used to protect the DWL from

sun light

Operating temp Ambient

Operating pressure Atmospheric

Medium Air

Material Stainless steel wire ( Spec IS :

6528-1972) , Grade 4,Cr-18, Ni-

10 in annealed condition

Annual requirement 100