nav 6 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

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!