WIND, WEIGHT & BALANCE and MANIFOLD PRESSURE

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Presentation transcript:

WIND, WEIGHT & BALANCE and MANIFOLD PRESSURE NAV 6 WIND, WEIGHT & BALANCE and MANIFOLD PRESSURE

Out of Focus to Protect the Innocent

Xwind & CRFI

Xwind & CRFI

CRFI & MF vs ATF

Obstacles, Arcal, ATF & Peripheral PQ 1

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. 41” x 280 lb. RAC 3.5 39” x 150 lb. =5850 lb.in. 33” x 150 lb. =4950 lb.in.

Weight & Balance C-150

Plotting of loaded weight and arm for C150 55,600 lb. in Plotting of loaded weight and arm for C150 55,600 lb.in. divided by 1600 lb. = 34.75 in.

Non Standard or Different Seating Positions 39x 150 5850 33x 150 4950 1560 53.1 53,100 lb.in. divided by 1560 lb.= 34.04 in. 55,600 lb.in. divided by 1600 lb.= 34.75 in.

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.

Identifying landmarks for track or drift determination STEERING 042 DEGREES Identifying landmarks for track or drift determination

C-150 CRUISE

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 :30 2.2

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 :56 7.8 :30 2.2 76 1:26 10.0

MAG vs COMPASS HEADING FROM PLANNING LOG TO FLIGHT LOG INCLUDE DEVIATION (From the magnetic meridian)

1405 1501 0056 1405 CYGK 67 O/H 10 1415 1414 CYOW 26 92 044 044 114 76 40 1454 5500 CYOW 06

CYPQ to CYQA

CYPQ to CYQA

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 :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 2408-35 YOW 0720 0814-13 1109-12 1614-15 1934-22 YQG 3309 3109-14 2707-16 2313-20 2232-28 YVV 0606 0305-15 9900-17 2016-20 2039-28 YYB 0406 9900-16 2009-17 2020-20 2043-28 YYZ 2710 2918-13 2930-13 2939-17 3037-25

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 :58+ 6.0 :30 2.7 60 1:28 8.7

CYPQ to Dunsford spot elevation

1507 1619 1405 01:12 CYPQ 67 O/H 08 1515 1513 CYQA 28 80 329 323 62 60 58 1611 6500 CYQA 06 1533 323 Dunsford 19nm in 20 (E6B 19/60) 19 in :20 is 60 in 1:05 / 15:13 +1:05 1618 57 1533 to1553 Drift left 06o - 323+6+6=335 then 329

VOT - VOR TEST

Manifold Pressure and fuel requirements CESSNA 172

INTAKE MANIFOLD – C172

INTAKE MANIFOLD from 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!