Upload
arif-sattar
View
33
Download
2
Tags:
Embed Size (px)
DESCRIPTION
Safety
Citation preview
Chapter10.3 Page 1
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
10.3 AIRBUS A310
CONTENTS Page #
10.3.1 EMERGENCY EQUIPMENT CHARTS …………………………
10.3.2 SEAT CHARTS……………………………..………………………….
10.3.3 CREW COMPLEMENT & DEPLOYMENT…………………….
10.3.4 EXITS……………………………………………………………………….
10.3.5 OXYGEN SYSTEM…………………………………………………….
10.3.6 EMERGENCY LIGHTS……………………………………………….
10.3.7 EVACUATION COMMAND SYSTEM ………………………..
10.3.8 TOILET DOOR (EMERGENCY OPENING) …………………
10.3.9 WATER SHUT OFF SYSTEM…………………..…………………
10.3.10 TOILET FIRE EXTINGUISHER………………………………….
10.3.11 HEAT DRAIN PANEL...……………………………………………..
10.3.12 SMOKE DETECTION SYSTEM..……………………………
10.3.13 FLAPS/SLATS & LANDING GEAR INDICATIONS……
3
5
10
11
14
14
14
15
15
17
16
17
18
Chapter10.3 Page 2
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
Intentionally left blank
Chapter10.3 Page 3
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
10.3.1 EMERGENCY EQUIPMENT CHART
10.3.1
Chapter10.3 Page 4
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
Intentionally left blank
Chapter10.3 Page 5
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
10.3.2 (a)SEAT CHART
Chapter10.3 Page 6
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
(b) SEAT CHART
Chapter10.3 Page 7
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
(c) SEAT CHART
Chapter10.3 Page 8
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
(d) SEAT CHART
Chapter10.3 Page 9
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
(e) SEAT CHART
Chapter10.3 Page 10
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
10.3.3 CREW COMPLEMENT & DEPLOYMENT A) SAFETY SEATING POSITION/AREA OF RESPONSIBILITY/
EQUIPMENT TO BE CARRIED
R1--------------------------------R2----------------------------------------------------------------------------R3----- A2 (F.A) C2 (F.A) B2 B3 (F.A) B1 (F.A) A3 A4 (ELT) A1 (P.M) C3 C1 (P.M) L1------------------------------- L2--------------------------------------------- -------------------------------L3-----
A4 A2 21-25 A3
B2 41-50 B3
C2 51-58 C3
A-310 NORMAL CREW COMPLEMENT - (10)
A1 - Overall supervision, coordinate with cockpit, B1 & C1. Make all
emergency announcements B1 - Supervise cabin preparation in B-zone and coordinate with C1
and A1. C1 - Supervise cabin preparation in C-zone between and coordinate
with B1 and A1.
B) MANDATORY CABIN CREW RESPONSIBILITIES
A310 series MANDATORY cabin crew complement: 4 (Except AP-BGN,O,P Mandatory cabin crew complement: 5)
EXITS MANNED
L1 R1 L3 R3
Cabin Crew A1 A2 C1 C2 Area of responsibility
Over all supervision
1-25 All
rows
41-58 LHS
41-58 RHS
Equipment to be carried out
PM/ELT FAK PM FAK
a) A1 will be responsible for announcements and over all supervision
b) B1 – (Only APBGN,O,P will supervise EY and coordinate with A1 and also will operate LR2)
c) AP-BGN, A2 1-27 all rows,C1 41-59 LHS & C2 41-59 RHS d) AP-BGQ, P, O, R&S C1 41-60 LHS & C2 41-60 RHS.
Chapter10.3 Page 11
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
10.3.4 EXITS A) MAIN DOORS (LR1 & LR3) – TYPE “A” DOORS
Type “A” Doors can be opened manually and pneumatically in emergency, the 04 doors are equipped with door mounted Slide Rafts.
a) Pre-flight Check
i) Function of door control handle.
ii) Function of Arm/Disarm lever
iii) Availability of safety pin / streamer
iv) Door pneumatic pressure - 1740 PSI (Pressure + Temperature at 21 Degree Decal)
v) Pressure for slide raft Green band
vi) Door locking indicators- Green flag
vii) Function of door warning system
viii) Door barrier strap (located inside door frame) b) Emergency Opening
i) Assess outside conditions.
ii) Check door in armed mode.
iii) Lift door control handle fully up and release.
iv) Door opens PNEUMATICALLY
In the event of a Ditching situation
i) Confirm Slide Raft deploys and inflates.
ii) Command Evacuation.
iii) Board passengers, directly into the slide raft.
iv) Count Number of passengers.
v) Pull accessory Kit into Raft.
vi) Disconnect Slide Raft. (Open Flap and Pull disconnect handle)
vii) Cut re-entry line and Paddle away.
viii) Ensure passengers inflate life jackets before boarding the raft.
Chapter10.3 Page 12
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
Slide Raft Capacity
c) If the door fails to open pneumatically
Push to Open Manually Slide Raft deploys and inflates automatically
d) If the Slide Raft fails to Inflate
Inflate manually by pulling “Red Manual Inflation Handle” on girt extension.
e) If the manual operation of door or device fails
Re-direct passengers
LR1 & LR3 67 - 83
B) EMERGENCY DOOR LR-2 (TYPE “III”)
These doors are only used in land landing a) Pre-flight Check
i) Door closed ii) Protective cover on Door Control
Handle iii) Door locking indicators – GREEN
FLAG - iv) Function of Door Warning system
Aural/ visual v) Function of Armed / Disarmed
lever vi) Availability of safety pin /
streamer. vii) Pressure for Ramp slide: Green
band.
b) Emergency Opening
i) Assess outside conditions
ii) Confirm door is in armed mode
iii) Remove protective panel cover.
iv) Lift handle fully up and release
v) Push door out MANUALLY parallel to wing surface.
Chapter10.3 Page 13
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
vi) Ramp Slide deploys and inflates automatically.
vii) Slide ready indicator visible - Green and White.
c) If the Ramp /Slide fails to Inflate Inflate manually by pulling the manual inflation handle at the base of the door.
d) If the door is advertently opened in disarmed mode Pulling “Manual Inflation Handle” at the base of door will inflate ramp slide.
e) Disconnection of Ramp / Slide
i) Disconnect hose assembly from valve assembly ii) Pull up re-entry line iii) Disconnect FWD girt (i.e. walkway and slide from door) iv) Open Flap and Pull disconnect handle. v) Disconnect AFT girt (i.e. ramp rail from door) vi) Open Flap and Pull disconnect handle.
C) COCKPIT SLIDING WINDOWS i) Push control handle downwards and rear-wards, red pin
confirms unlocking ii) Hold lever and slide AFT until
locked. Note: window can be opened only
from inside.
Chapter10.3 Page 14
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
10.3.5 OXYGEN SYSTEM
Cockpit ----gaseous state Cabin ----solid state (have 2/3 mask generator installed
above Pax seats, jump seats and toilets) a) Location of extra Oxygen masks
i) One extra mask on all lateral seats ii) One extra mask on the set of 3 seats in the centre rows iii) One extra mask in Toilet iv) All single Jump Seats have one extra mask. v) No extra mask. vi) Extra masks on all seats In
AP-BGN/OP/Q/R & S Tool Manual Release (TMR)
b) Operation
i) Automatically – once cabin altitude crosses 14000 ft. ii) Manually - from cockpit. iii) Individually - from P.S.U. with T.M.R iv) Pointed end used to open cabin PSU v) Flat end for crew jump seat and toilet units
c) Duration
Duration of Oxygen system is 22 Minutes. Note: O2 flow in all masks in the
PSU’s will start when any mask is pulled, flow can’t be stopped.
10.3.6 EMERGENCY LIGHT
a) Location of Switch
i) In Cockpit: ON / ARM / DISARM position.
ii) At Purser Station: ON/OFF Position
ON/ARM/DISARM Selector
b) Operation i) Automatically: Electric Power Loss. ii) Manually : From Cockpit / Purser Station
Chapter10.3 Page 15
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
c) Duration
i) 12 Minutes for fixed emergency lights 15 Minutes on AP-BGN/O/P/Q/R & S
ii) 10 Minutes for Peepls lights
Note: The cabin switch over rides the cockpit switch. 10.3.7 EVACUATION COMMAND SYSTEM A) LOCATION:
a) COCKPIT i) Captain ii) Captain and Purser iii) Evacuation signal selector ON iv) Evacuation Flashing Light. v) Evacuation Horn Shut OFF
Button. b) PURSER STATION
i) Evacuation Push for ON Button ii) Evacuation Test Button iii) Tone OFF Button.
c) L3 STATION
i) Evacuation Test Button ii) Tone OFF Button.
B) OPERATION
a) Cockpit Activates when the Evacuation Command Switch is pressed to “ON” position.
b) Purser Station c) System can be activated from the cabin when cockpit selector
switch is in “Captain + Purser” Position. Note: In A310 the Evacuation command selector switch is in CAPT position (during flight). Therefore priority to activate the evacuation command remains with the cockpit.
Chapter10.3 Page 16
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
10.3.8 TOILET DOOR EMERGENCY OPENING The toilet doors can be opened from outside in case a person needs help in an emergency.
A) SINGLE FOLDING DOOR
a) Shift “Occupied” sign to “Vacant” b) Rotate handle c) Pull the door outwards
B) SLIDING DOOR
a) Shift “Occupied” sign to “Vacant” b) Rotate handle c) Slide the door
C) BI-FOLDING DOOR
a) Shift occupied sign to vacant. b) Shift two locking devices.
i) Upper device downwards ii) Lower device upwards
c) Pull the door outward. 10.3.9 WATER SHUT OFF SYSTEM
Water supply from pressurised tanks to toilets & galleys can be shut off from:
a) Purser’s station Pressing will shut off water to FWD/MID toilets & galleys Pressing will shut off water to AFT toilets & galleys
b) Galleys: Individually from each wet galley. The shut off valve in Fwd Galley is located behind the waist bin. Mid and Aft galley, it is located beside LHS trolley stowage area. c) Toilet: Individually in each toilet. The shut off valve is located under the sink area.
FWD
AFT
Chapter10.3 Page 17
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
10.3.10 TOILET FIRE EXTINGUISHERS Toilet fire extinguishers are installed in each of the toilets. The fire extinguisher will automatically discharge in case of fire development, as its nozzles are heat sensitive.
LOCATION a) FWD Toilets: Behind the waste bins b) AFT Toilets: Above the waste bins
OPERATION
Automatic: Once temperature exceeds 71 o C. During the flight in case the fire extinguisher has been discharged
i) Both nozzles will turn to silver from black ii) Temperature indicator placard dots will turn black
from white If the extinguisher has been discharged:
a) Inform cockpit crew, b) Monitor toilet for fire situation c) Make entry in cabin technical log 10.3.11 HEAT DRAIN PANEL
Heat drain panel is located at Pursers panel. When pressed the water service panel is heated. Conditions:
a) Outside temperature less than O0C b) Icing conditions expected. c) Water servicing scheduled.
Operation
a) OFF: During climb b) ON: During descent and
taxiing/ground.
Chapter10.3 Page 18
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
10.3.12 SMOKE DETECTION SYSTEM
Smoke Detector System with built in sensor is installed in all the toilets. a) Master display panel is at the Purser station. b) Red flashing mode light outside each toilet. c) A smoke lavatory indicator at L3 station
PURSER STATION
A) Pre-Flight Check a) Confirm availability of ground power. b) Cabin Attendant to individually press red
light outside the toilet in their area. c) Red light ON: Confirms bulb function and
circuit serviceability. d) Senior Purser can confirm the system
serviceability from his master panel by selecting the respective toilet through selector knob and pressing the smoke lav test P/b.
Senior purser should after checking bring the selector knob to NORM FLT position.
B) Operation In case of smoke development in any of the toilets the following will happen: a) Red light out side the respective toilet will flash. b) Amber light on the respective ACP will flash with continuous
single stroke chime. c) Smoke Lav indicator at Purser station panel will illuminate.
Note: In case of AFT toilets in addition to the above Smoke Lav indication at L3 station will also illuminate.
10.3.13 FLAPS/SLATS & LANDING GEAR INDICATIONS
In case of an abnormality the cabin crew may be required to make a visual check of indications for flaps, slats or landing gear from the cabin. When requested to do so by the Flight Deck crew, the cabin crew will visually check the indications from the following rows:
Chapter10.3 Page 19
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
A/C TYPE SLATS
Viewing Location
FLAPS Viewing Location
LANDING GEARS
Viewing Location
A310
22nd Row
44th / 45th Row 45th Row
Viewing location of flaps, slats and landing gear from cabin
VISUAL CHECKS/ FLAPS / SLATS / LANDING GEAR
a) FLAP / SLATS
To be conducted from cabin through the over wing windows with symbol ∆
b) LANDING GEAR
i) To be conducted from cabin through the windows marked with symbol ⊥
ii) A fluorescent coating on the wing surface is visible when landing gear is down and locked.
Chapter10.3 Page 20
CABIN CREW
SAFETY EQUIPMENT & PROCEDURES MANUAL Doc #: FSD/TRG/SEP/03/II
SEP VOLUME-II Airplane Specific/A-310 Rev: 0 Aug 04, 2006
Intentionally left blank