Embed Size (px)
Citation preview
NAV 6
WIND, WEIGHT & BALANCE and MANIFOLD PRESSURE
Out of Focus to Protect the Innocent
Xwind & CRFI
Xwind & CRFI
CRFI & MF vs ATF
PQ 1
Obstacles, Arcal, ATF & Peripheral
WEIGHT and BALANCE
STANDARD WEIGHTS
Males 12 yr + 200 206
Females 12yr + 165 171
With no carry on baggage reduce 13 lb.
Personal weights add 8 or 14 for clothes
Children 2 – 11 75
Infants 30
C-150 Average Seat Positioning
Weight & Balance C-150
C-150 NOT Average Seat Positioning
41” x 170 lb.
33” x 150 lb.=4950 lb.in.
39” x 150 lb.=5850 lb.in.
41” x 280 lb.
RAC 3.5
Weight & Balance C-150
Plotting of loaded weight and arm for C150
55,600 lb.in. divided by 1600 lb.= 34.75 in.
585039x 150
33x 150 4950
Non Standard or Different Seating Positions
55,600 lb.in. divided by 1600 lb.= 34.75 in.
53,100 lb.in. divided by 1560 lb.= 34.04 in.
1560 53.1
Aircraft:Cessna 150 C-GULP White with Red/Orange trim
Owner:Yourself c/o Kingston Federal Pen, Kingston, ON
Radio equipment:1 NAV/COM, 1 Transponder with Mode C, 1 ADF receiver
ELT:Pointer Sentry Fixed ELT
Route:CYGK (Kingston) Direct CYOW (Ottawa). Set heading point will beoverhead Kingston
Power Setting:Closest to 60% at your cruising altitude of 5,500’ ASL
Weather:Assume Standard temperature, Altimeter setting 29.92” Wind at
5,500ASL forecast to be 220°T at 18 knots
Pilot Licence:PA321123
Allow 6 minutes at cruise power for circuit before landing at Ottawa. For start, run-up, takeoff and climb, allow fuel as indicated on the charts. Proposed departure time is 0200 EDT.Complete a flight log and a flight plan for the proposed flight.
STEERING 042 DEGREES
Identifying landmarks for track or drift determination
C-150 CRUISE
FLIGHT PLANNING Kingston /Ottawa
CYGKStart, t/o
67 NE 13w :10 1.5
0.8
CYOW 55 97 031 220/18 13w 76
contingency 20% fuel
circuit
CYGK GULP ME 22 MAR 01
:30 2.2
029 042 114 :40 3.192
4.5gph
FLIGHT PLANNING Kingston /Ottawa
CYGKStart, t/o
67 NE 13w :10 1.5
0.8
CYOW 55 92 97 031 220/18 029 13w 042 114 76 :40 3.1
contingency 20% fuel 1.9
circuit :06 0.5
CYGK GULP ME 22 MAR 01
76 :56 7.8
76 1:26 10.0
:30 2.2
MAG vs COMPASS HEADING
FROM PLANNING LOG TO FLIGHT LOGINCLUDE DEVIATION(From the magnetic meridian)
26 92 044 044 114 76 40
10 1415
5500CYOW
67 O/H CYGK
1405
1454
1414
1405 0056
1501
CYOW 06
CYPQ to CYQA
CYPQ to CYQA
FLIGHT PLANNING LOG
CYPQStart, t/o
67 O/H 11w :08 0.9
CYQA 65
circuit :06 ---
@
5.3 gph
CYPQ SLOW ME 30 MAR 05
:30 2.7
FDs – Interpolation
FCST BASED ON 251200 DATA VALID 251800 FOR USE 17-21 3000 6000 9000 12000 18000
YAM 0117 3613-19 9900-21 9900-26 2408-35YOW 0720 0814-13 1109-12 1614-15 1934-22YQG 3309 3109-14 2707-16 2313-20 2232-28YVV 0606 0305-15 9900-17 2016-20 2039-28YYB 0406 9900-16 2009-17 2020-20 2043-28YYZ 2710 2918-13 2930-13 2939-17 3037-25
FLIGHT PLANNING Peterborough/Muskoka
CYPQStart, t/o, climb
67 NE 11w :?? 0.9
CYQA 65 80 318 290/20 312 11w 323 62 60 :58 5.1
circuit :?? N/A
CYPQ C-150 Nav 2 asgnmt 22 MAR 04
60 :58+ 6.0
60 1:28 8.7
:30 2.7
Fuel 5.3 gph
CYPQ to Dunsford spot elevation
28 80 329 323 62 60 58
08
6500CYQA
67 O/H CYPQ
1405
1611
1513
1507
01:12
1619
CYQA 06
1533 323 Dunsford 19nm in 20 (E6B 19/60)
1618 57
1533 to1553 Drift left 06o - 323+6+6=335 then 329
19 in :20 is 60 in 1:05 / 15:13 +1:05
1515
VOT - VOR TEST
CESSNA 172
Manifold Pressure and fuel requirements
INTAKE MANIFOLD – C172
INTAKE MANIFOLDfrom below
Power Settings C172
Note- No manifold
pressures provided, only
RPM, percentage
brake horsepower and
true airspeed
INTAKE MANIFOLD
– Be33
C 172 Tachometer & NO Manifold Pressure!
Be 33 Tachometer & Manifold Pressure!
