Chapter 4 Flashcards

1
Q

Maximum altitude

A

41000 MSL

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2
Q

Icing limits

A
  • prolonged flight in icing conditions shall be avoided

- when airframe icing is visible, intentional stalls or use of full flaps is not authorized

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3
Q

Engine handling limits

A
  • Throttle at idle for:
      • abrupt (0.5 sec or less from neutral to full back stick) pulls to full back stick
      • abrupt full lateral stick inputs at full back stick
      • airspeeds less than 85 KIAS at altitudes above 15000 MSL
  • A/S 85-150 KIAS above 35k MSL: slow throttle movements
  • except in emer, engine stabilized at idle for 30 sec prior to shutdown
  • sustained eng operation <70% N2 above 30k’ MSL may result in a sub-idle condition leading to flameout
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4
Q

Start ____ with throttle _____.

A

prohibited / above ground idle detent

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5
Q

Minimum RPM required for start

A

15% N2

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6
Q

Engine light-off must occur within ____ of throttle ___.

A

15 seconds / moving to idle

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7
Q

Minimum voltage for each battery

A

24V

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8
Q

_____ start in manual fuel is _____.

A

ground / prohibited

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9
Q

Manual fuel RPM limit above/below ___K’ MSL.

A

90% N2 above 20k’ MSL

95% N2 at or below 20k’ MSL

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10
Q

T/F: GTS start with external power is prohibited.

A

True

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11
Q

GTS start attempt interval

A

3 minutes between attempts, following 3rd attempt 30 minute cool down period is required

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12
Q

Following unsucessful GTS start attempt…

A

…further attempts prohibited until GTS exhaust duct and combustor section are inspected and any residual fuel is removed, and the RAT doors are inspected for discoloration/warpage.

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13
Q

GTS starts not reliable above _____.

A

15K’ MSL

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14
Q

MRT (max RPM/EGT, limit)

A

104% N2, 610 C, 30 mins per flight hour

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15
Q

Transient/acceleration engine limit

A

106% N2, 645 C, less than 20 seconds

may reach 645 C during or immediately following accel, but must decrease to 610 C within 20 seconds

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16
Q

Max continuous engine limit

A

100% N2, 550 C

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17
Q

Idle engine limit

A

55% N2 +/- 2%, 450 C

  • with airflow knob off, idle RPM approx 2% higher
  • idle rpm increases ~1% for each 1500’ altitude and 10 C in ambient temperature
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18
Q

Ground start engine limit

A

550 C

max overshoot 20 C for 10 seconds

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19
Q

Airstart engine limit

A

600 C

max overshoot 50 C for 10 seconds

(EGT/RPM light operates at 650 +/- 8 C)

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20
Q

Jet A, A++, A++ 100 freeze point / limit

A

freeze point -40 C

maintain TAT above freeze point +3 C (-37 C)

21
Q

To be used as primary fuel, commercial fuels require…

A

Fuel System Icing Inhibitor (FSII) and Corrosion Inhibitor/Lubricity Improver (CI/LI).

(use of aerosol FSII prohibited)

22
Q

Max AOA with flaps full/half and slats up (emer flaps DOWN)

A

AOA for pedal shaker / stall warning tone

23
Q

To prevent damage to ___ and ___, minimize ____ with gear in transition or extended above ___.

A

nose gear doors
NLG strut door
sideslip
150 knots

24
Q

Landing gear A/S limit

A

<= 200 KIAS

25
Q

Flaps/Slats A/S limit

A

<= 200 KIAS

26
Q

Arresting hook A/S limit

A

<= 450 KIAS

27
Q

Canopy wind limit

A

Stationary/towing full open: <= 32 knots

Locked in intermediate position: ingress/egress only, towing/taxi not permitted

Taxi with canopy full open: <= 20 knots

28
Q

Tire speed limit

A

<= 176 knots groundspeed

29
Q

Nose wheel steering speed limit

High gain limit

A

<= 176 knots groundspeed

< 10 knots groundspeed

30
Q

Fuel system hot refueling limit

A

<= 2800# if PRECHECK unsuccessful

31
Q

Crosswind component limits

  • single a/c dry runway
  • single a/c wet runway
  • section takeoff
  • banner tow
  • NWS off/failed
  • with baggage pod
A
  • 20 knots
  • 15 knots
  • 10 knots
  • 10 knots
  • 15 knots
  • 15 knots
32
Q

FCLP landings authorized configuration

sink rate limit for other configurations

A
  • full flaps and
  • clean loading
    OR
  • pylons alone or pylons w/ empty racks
  • 600 FPM
33
Q

Prohibited maneuvers

A
  1. Intentional spins/tailslides.
  2. Rolling cross-control maneuvers of more than 60 deg bank angle change.
  3. Intentional departures except for:
    a. Erect rolling departure entered with full aft stick / full lateral stick.
    b. Erect rudder-induced departure entered with full aft stick / full rudder.
    c. Nose high departures (70 and 110 deg)
  4. Sustained zero or negative g flight for more than 30 seconds.
  5. Less than 30 seconds between negative g or zero g maneuvers.
  6. Rolls at less than:
    a. Negative 1.0g at less than 260 KIAS
    b. Negative 0.2g at or greater than 260 KIAS, but less than .80M.
    c. Approx positive 1.0g at or greater than .8M.
  7. Lateral/directional inputs below 3 units AOA.
  8. Intentional departures with greater than 1000 foot-pounds assymetry.
  9. Operations with EMER FLAPS selected, when normal HYD 1 power is available, is restricted to 30 seconds with engine RPM less than or equal to 90%. Except in an actual emergency, use of EMER FLAPS is restricted to FCF profiles.
  10. Intentional accelerated stalls with landing gear extended while carrying stores.
34
Q

CG limits

  • forward (gear up/down)
  • aft gear up (+/- __M)
  • aft gear down
A
FORWARD
- 14% mean aerodynamic chord for gross weights up to 12k #
- 15.5% MAC above 12760#@
- linear variation between 12000/12760#
AFT gear up
- 21% MAC above .8M
- 23% MAC <= .8M
AFT gear down
- 25% MAC
35
Q

Pitchup and excessive stick lightening is possible at ___, especially for ___ pilots with ___ fuel. CG may exceed high Mach aft limit by as much as ___. For ___ pilots, CG will move ____. ___ CG condition will cause ____ potential for over-g.

A
  • > .8M, solo, partial
  • .5%
  • lightweight, even further aft
  • aft, increased
36
Q

Weight limits

  • field takeoff
  • catapult
  • field landing
  • FCLP
  • carrier landing
A
  • 14,500 pounds
  • 14,200
  • 13,360
  • 13,360
  • 13,360
37
Q

Acceleration limits (gear/flaps transition or extended/half)

A
  1. 0-2.0g symmetrical

1. 0-1.5g unsymmetrical

38
Q

Acceleration limits symmetrical

A

Below 13,233#:

  • 3.0g below .8M, -1.0 at or above .8M
    6. 5g below 5k’ MSL, 7.33 above 5k’ MSL
39
Q

Acceleration limits assymetrical

A
  • 1.0g <260 kts, -0.2g >=260 kts but =.8M

5. 0g below 5k’ MSL, 5.86g above 5k’ MSL

40
Q

Carrier ops with external stores/pylons are _____.

A

prohibited

41
Q

Landings with BRU-38 and 1 or more bomb shall not exceed ____.

A

600 FPM

42
Q

Carriage of wing-mounted stores and a baggage pod is ____.

A

not authorized

43
Q

Lateral stick and rudder pedal inputs with carrige of baggage pod is limited to ____, except ____.

A

half

as needed for crosswind landings

44
Q

Maximum amount of load in baggage pod (and distribution).

A

60# of soft luggage

  • 30# forward, 30# aft
  • contents shall be secured to prevent shifting
  • CG limits of the loaded pod shall be between 1 and 9 inches aft of the rear suspension lug
45
Q

Jettison of racks is limited to ____.

A

between 290 and 310 KIAS

46
Q

PMBR/BRU airspeed limit

A

525 KIAS / .8M

47
Q

Baggage pod airspeed limit

A

380 KIAS / .8M

48
Q

Baggage pod acceleration limits

  • gear/flaps up
  • gear down
A
  • sym/up 0.0-4.0g, assym/up 1.0-3.0g

- sym/down 0.0-2.0g, assym/down 1.0-1.5g

49
Q

Do not use large lateral inputs at ___ than ____.

A

less than 8 units AOA