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WIND, WEIGHT & BALANCE and MANIFOLD PRESSURE
NAV 6 WIND, WEIGHT & BALANCE and MANIFOLD PRESSURE
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Out of Focus to Protect the Innocent
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Xwind & CRFI
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Xwind & CRFI
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CRFI & MF vs ATF
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Obstacles, Arcal, ATF & Peripheral
PQ 1
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WEIGHT and BALANCE STANDARD WEIGHTS Males 12 yr + 200 206
Females 12yr With no carry on baggage reduce 13 lb. Personal weights add 8 or 14 for clothes Children 2 – 11 75 Infants 30
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C-150 Average Seat Positioning
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Weight & Balance C-150
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C-150 NOT Average Seat Positioning
41” x 170 lb. 41” x 280 lb. RAC 3.5 39” x 150 lb. =5850 lb.in. 33” x 150 lb. =4950 lb.in.
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Weight & Balance C-150
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Plotting of loaded weight and arm for C150 55,600 lb. in
Plotting of loaded weight and arm for C ,600 lb.in. divided by lb. = in.
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Non Standard or Different Seating Positions
39x 5850 33x 4950 53,100 lb.in. divided by 1560 lb.= in. 55,600 lb.in. divided by 1600 lb.= in.
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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 be overhead Kingston Power Setting: Closest to 60% at your cruising altitude of 5,500’ ASL Weather: Assume Standard temperature, Altimeter setting 29.92” Wind at 5,500 ASL 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.
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Identifying landmarks for track or drift determination
STEERING 042 DEGREES Identifying landmarks for track or drift determination
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C-150 CRUISE
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FLIGHT PLANNING Kingston /Ottawa
CYGK GULP ME 22 MAR 01 4.5gph CYGK Start, t/o 67 NE 13w :10 1.5 0.8 CYOW 55 97 031 220/18 76 contingency 20% fuel circuit 92 029 042 114 :40 3.1 FLIGHT PLANNING Kingston /Ottawa :
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FLIGHT PLANNING Kingston /Ottawa
CYGK GULP ME 22 MAR 01 CYGK Start, t/o 67 NE 13w :10 1.5 0.8 CYOW 55 92 97 031 220/18 029 042 114 76 :40 3.1 contingency 20% fuel 1.9 circuit :06 0.5 FLIGHT PLANNING Kingston /Ottawa 76 : : 76 1:
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MAG vs COMPASS HEADING FROM PLANNING LOG TO FLIGHT LOG
INCLUDE DEVIATION (From the magnetic meridian)
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1405 1501 0056 1405 CYGK 67 O/H 1414 CYOW 1454 5500 CYOW 06
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CYPQ to CYQA
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CYPQ to CYQA
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FLIGHT PLANNING LOG :30 2.7 CYPQ SLOW ME 30 MAR 05 CYPQ 67 11w :08 0.9
Start, t/o 67 O/H 11w :08 0.9 CYQA 65 circuit :06 --- @ 5.3 gph FLIGHT PLANNING LOG :
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FDs – Interpolation FCST BASED ON DATA VALID FOR USE 17-21 YAM YOW YQG YVV YYB YYZ
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FLIGHT PLANNING Peterborough/Muskoka
CYPQ C-150 Nav 2 asgnmt 22 MAR 04 Fuel 5.3 gph CYPQ Start, t/o, climb 67 NE 11w :?? 0.9 CYQA 65 80 318 290/20 312 323 62 60 :58 5.1 circuit N/A FLIGHT PLANNING Peterborough/Muskoka 60 : : :
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CYPQ to Dunsford spot elevation
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1507 1619 1405 01:12 CYPQ 67 O/H 08 1515 1513 CYQA 1611 6500 CYQA 06 Dunsford 19nm in 20 (E6B 19/60) 19 in :20 is 60 in 1:05 / 15:13 +1:05 1533 to1553 Drift left 06o =335 then 329
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VOT - VOR TEST
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Manifold Pressure and fuel requirements
CESSNA 172
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INTAKE MANIFOLD – C172
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INTAKE MANIFOLD from below
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Power Settings C172 Note- No manifold pressures provided, only RPM, percentage brake horsepower and true airspeed
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INTAKE MANIFOLD – Be33
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C 172 Tachometer & NO Manifold Pressure!
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Be 33 Tachometer & Manifold Pressure!
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