NAV 6

1
NAV 6
WIND, WEIGHT BALANCE and MANIFOLD PRESSURE
2
Out of Focus to Protect the Innocent
3
Xwind CRFI
4
Xwind CRFI
5
CRFI MF vs ATF
6
PQ 1
Obstacles, Arcal, ATF Peripheral
7
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

8
(No Transcript)
9
C-150 Average Seat Positioning
10
Weight Balance C-150
11
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.
12
Weight Balance C-150
13
Plotting of loaded weight and arm for
C15055,600 lb.in. divided by 1600 lb. 34.75
in.
14
Non Standard or Different Seating Positions
5850
39x 150
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.
15

• 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 220T 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.

16
STEERING 042 DEGREES
Identifying landmarks for track or drift
determination
17
C-150 CRUISE
18
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 13w 76
contingency 20 fuel
circuit
029
042
114
92
40
3.1
30 2.2
19
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 13w 042 114 76 40 3.1
contingency 20 fuel 1.9
circuit 06 0.5
76 56 7.8
30 2.2
76 126 10.0
20
MAG vs COMPASS HEADING

• FROM PLANNING LOG
• TO FLIGHT LOG
• INCLUDE DEVIATION
• (From the
• magnetic
• meridian)

21
1405
1501
0056
1405
10 1415
67 O/H
CYGK
1414
CYOW
26 92 044 044 114 76 40
1454
5500
CYOW
06
22
CYPQ to CYQA
23
CYPQ to CYQA
24
FLIGHT PLANNING LOG
CYPQ
SLOW
ME
30 MAR 05
CYPQ Start, t/o 67 O/H 11w 08 0.9
CYQA 65
circuit 06 ---
_at_ 5.3 gph

30 2.7
25
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

26
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 11w 323 62 60 58 5.1

circuit ?? N/A
60 58 6.0
30 2.7
60 128 8.7
27
CYPQ to Dunsford spot elevation
28
1507
1405
1619
0112
08
67 O/H
CYPQ
1513
1515
CYQA
28 80 329 323 62 60 58
1611
6500
CYQA
06
1533 323 Dunsford 19nm in 20 (E6B 19/60)
1618 57
19 in 20 is 60 in 105 / 1513 105
1533 to1553 Drift left 06o - 32366335 then 329
29
(No Transcript)
30
VOT - VOR TEST
31
Manifold Pressure and fuel requirements
CESSNA 172
32
INTAKE MANIFOLD C172
33
INTAKE MANIFOLDfrom below
34
Power Settings C172
Note- No manifold pressures provided, only RPM,
percentage brake horsepower and true airspeed
35
(No Transcript)
36
(No Transcript)
37
INTAKE MANIFOLD Be33
38
C 172 Tachometer NO Manifold
Pressure!
39
(No Transcript)
40
Be 33 Tachometer Manifold
Pressure!
41
(No Transcript)
42
(No Transcript)