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PRE-SOLO BAC36 > [Section 1] Performance&Limitations > Flashcards

[Section 1] Performance&Limitations Flashcards

1
Q

Service celing

A

13000 ft

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2
Q

Take off ground roll

A

890 ft

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3
Q

take off total distance over 50ft. obstacle

A

1625 ft

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4
Q

Landing ground roll

A

540 ft

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5
Q

Landing total distance over 50 ft. obstacle

A

1280 ft

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6
Q

Maximum ramp weight

A

2407 lbs

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7
Q

maximum take off weight

A

2400 lbs

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8
Q

maximum landing weight

A

2400 lbs

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9
Q

engine manufacturing and model

A

AVCO LYCOMING O-320-D2J

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10
Q

what does POH stand for

A

Pilot’s Operating Handbook

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11
Q

Vso

A

Stalling speed with Landing configuration

33 KIAS

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12
Q

Vs

A

Stalling speed clean configuration

44 KIAS

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13
Q

Vfe

A

Maximum flaps extended speed

10 degree = 110 KIAS
10-30 degree = 85 KIAS

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14
Q

Fuel capacity: standard tank

A

total capacity 43 gallons
each tank 21.5 gallons
useable fuel 40 gallons
unusable fuel 3 gallons

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15
Q

fuel capacity : long range tasks

A

total capacity 54 gallons
each tank 27 gallons
useable fuel 50 gallons
unusable fuel 4 gallons

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16
Q

fuel capacity: integral tanks

A

total capacity 68 gallons
each tank 34 gallons
useable fuel 62 gallons
unusable fuel 6 gallons

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17
Q

maximum combine weight capacity for baggage area 1 and 2

A

120 lbs

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18
Q

Vy

A

Best rate of climbing speed

76 KIAS

19
Q

Va

A

Maneuvering speed for
2400 lbs = 99 KIAS
2000 lbs = 92 KIAS
1600 lbs = 82 KIAS

20
Q

Vno

A

Maximum structural cruising speed

127 KIAS

21
Q

Vne

A

Never exceed speed

158 KIAS

22
Q

what is KIAS stand for

A

Knots Indicated Airspeed

23
Q

Vx

A

Best angle of climbing speed

60 KIAS

24
Q

Maximum performance

A

160 BHP at 2700 RPM

25
Propeller diameter
max 75" | min 74"
26
Approved fuel grades and colors
100LL blue | 100 green
27
White arc is indicated?
Full flap operating range 33-85 KIAS
28
Green arc indicated?
Normal operating range 44-127 KIAS
29
Yellow arc is indicated?
Caution operating range | 127-158 KIAS
30
Red arc is indicated?
Maximum speed for all operations 158 KIAS
31
What is pressure altitude means
The altitude read from an altimeter when the altimeter's barometric scale has been set to 29.92 inHg (1013mb)
32
What is reference datum of Cessna172 located?
Lower portion of front face of firewall
33
Flight load factors (MTOW 2400lbs.)
Flaps up +3.8g, -1.52g | Flaps down +3.0g
34
Which section in POH can you find Emergency procedures?
Section 3
35
Maximum cross wind velocity
15 knots
36
While you taxi you should set throttle to which rpm instead of idle and why?
1000 rpm In order to prevent spark plug become fault
37
Refer to BEFORE TAKEOFF procedure while set the throttle to 1700 rpm for magnetos check the RPM drop should not exceed ____ rpm on either magnetos and _____ rpm differential between magnetos.
125 rpm | 50 rpm
38
Which badge should we use for BAC36
Kumamon Squadon!!
39
Please describe the Pitot-Static system
The system received ram pressure and static pressure then send to Pitot-static instrument. These instruments convert pressure and send to 3 indicators. 1.Airspeed indicator measuring differential pressure between dynamic pressure from pitot tube and static pressure from static port. 2 and 3. For Altimeter and Vertical speed indicator use only static pressure to measure changed pressure varies by altitude in Aneroid wafers and Diaphragm respectively.
40
Please describe the Pitot tube's malfunctions
Malfunction may occur by blockage of ice, dirt or insect. Pitot tube malfunction 1. Pitot tube clear but drain hole blocked: A/S will read more than actual speed 2. Pitot tube blocked but drain hole clear. A/S will slowly drop to "0" 3. Pitot tube and drain hole blocked: A/S will related to changing in altitude High altitude -> A/S increase Low altitude -> A/S decrease Correction by turn on Pitot heat switch
41
Please describe the static port's malfunction
Malfunction may occur by blockage of ice, dirt or insect. Static port malfunction 1.Blocked static port: Inaccurate Airspeed, Freeze Altimeter and Freeze Vertical speed indicator. Correction by use alternate static port if cannot or didn't equip try to break Vertical speed indicator gauge
42
Visual flight rules condition (VFR)
1. Operate sunrise to sunset / Ceiling more than 1,500 ft. 2. Visibility 5-8 km. When operate at altitude below 10,000 ft. 3. Visibility 8-10 km. When operate at altitude between 10,000-20,000 ft. 4. Operate altitude not more than 20,000 ft. 5. Do not operate in transonic (0.5M-1.2M) or supersonic (1.2M-3M) 6. East round route (0-179 degree) operating altitude odd thousand +500 ft. When altitude more than 3000 ft. (3500, 5500, 7500, ...) 7. West round route (180-359 degree) operating altitude even thousand +500 ft. When altitude more than 3000 ft. (4500, 6500, 8500, ...) 8. Maintain clear of cloud 2,000 ft. Horizontal, 1,000 ft. above and 500 ft. below 9. Operating altitude above congested area more than 1,000 ft. 10. Operating altitude above uncongested area more than 500 ft.
43
Please describe the Gyroscopic system
This system base on 2 fundamental concepts 1. Rigidity in space 2. Precession Gyroscope is able to remain in fixed position on plane in which it originally spinning. There are 3 types of gyroscope instruments 1. Attitude indicator 2. Heading indicator 3. Turn coordinator Attitude and Heading indicator received power from vacuum pump system and normally operate when suction gauge is on green (4.5 - 5.4) It will malfunction if suction gauge is out of range. If vacuum system failed these 2 instruments won't work and use magnetic compass instead of Heading indicator Turn coordinator powered by an electrical system.

PRE-SOLO BAC36 (2 decks)

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