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TSA > Trans States Limitations > Flashcards

Trans States Limitations Flashcards

1
Q

Max. Altitude (PA)

A

37,000 ft

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2
Q

Max. Operating Temp.

A

ISA + 35 degrees C

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3
Q

TAT in cruise above ______ is limited to ______

A

25,000 ft.

-45 degrees C

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4
Q

VLO (Retraction)

A

200 KIAS

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5
Q

VLO (Extension)

A

250 KIAS

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6
Q

VLE (Extended)

A

250 KIAS

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7
Q

Maximum Operating VMO/MMO

A

0 to 8000 ft. 250 KIAS
10,000 to 26,000 ft. 320 KIAS
26,000 to 37,000 ft. .78 Mach

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8
Q

Maneuvering VA

A

200 KIAS

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9
Q

Flap Extended VFE

A

Flaps 9 250 KIAS
Flaps 22 200 KIAS
Flaps 45 145 KIAS

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10
Q

Tailwind

A

10 Knots Maximum

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11
Q

Direct Vision Window

A

Max to Remove: 140 KIAS (AFM)

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12
Q

Windshield Wiper

A

Max for Operation: 170 KIAS (AFM)

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13
Q

Turbulent Air Penetration (AFM)

A

At or below 10,000 ft. 200 KIAS
Above 10,000 ft. 250 KIAS/0.63 M
Whichever is lower

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14
Q

Maximum Aft Cargo Weight

A

2646 lbs.

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15
Q

Maximum Useable Quantity each Tank

A

LR: 844.9 US Gal. (5717 lbs.)
EP: 679.8 US Gal (4,600 lb)

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16
Q

Max APU Start Alt.

A

30,000 ft.

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17
Q

Note 1 APU. Max EGT temp

A

May be exceeded up to 925 C above 25,000 ft. during 10 seconds

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18
Q

APU Note 6. Max EGT

A

The APU EGT may be exceeded up to 717 C for 5 minutes maximum

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19
Q

APU Starter Limits

A

Cooling period between each starting attempt:
Between three consecutive attempts…1 minute off
Between two series of three consecutive attempts… 30 minutes off

20
Q

Engine Starter Limits on Ground:

A

Starting or Dry Motoring… Up to 5 minutes on, 5 minutes off OR
First to Fourth Cycles… 1 minute on, 1 minute off
Following Cycles…. 1 minute on, 5 minutes off

21
Q

Engine Starter Limits in Flight

A

Maximum Continuous Operation Time…. 5 minutes on

Note…. No cool down time is required should an in-flight start be reattempted

22
Q

ATTCS

A

Must be operative for ALT T/O-1 Mode

23
Q

Reversers

A

Do not go-around after reverser deployment

24
Q

Oil Pressure

Below 88% N2

A

Maximum 110 psi (2) (7)

25
Q

Oil pressure At or above 88% N2

A

Maximum 110 psi (7)

26
Q

Engine Parameter Note 1. Take off thrust

A

Takeoff Thurst is time limited to 5 minutes

27
Q

Engine Parameter Note 2. Max oil pressure

A

May be exceeded during starts if oil temp. is below 21 C. The engine must remain at IDLE until the pressure is less than 110 psi.

28
Q

Engine Parameter Note 3. Minimum temp for engine start.

A

Minimum oil temperature for starting is -40C for lubrication oil specified by MIL-L-23699D

29
Q

Engine Parameter Note 4. Vibration

A

Vibration in the amber range below 2.5 IPS is time limited to 5 minutes during the takeoff or go-around phases or 10 seconds during the remainder of the flight phases.

30
Q

Engine Parameter Note 6. Operation limits for high oil pressure

A

Operation in oil pressure amber range between 111 and 115 psi is permitted in all operational modes and time limited to 5 minutes, or between 116 and 155 psi in all operational modes time limited to 2 minutes. Total time above 110 psi may not exceed 5 minutes.

31
Q

Engine Parameter Note 8. Oil pressure on TO

A

While this is an abnormal condition, operation between 50 and 34 psi is permitted during takeoff and go around phases (for AE 3007A engines only).

32
Q

Engine Warm-Up

A

Prior to take-off, the engines must be allowed to run at low thrust to stabilize the engine temperatures before take-off thrust is adjusted. After start, the engines must run at idle or taxi thrust during at least 4 minutes for cold engines (shut down for more than 90 minutes) or 2 minutes for warm engines. To increase N2 above 83% the engine oil temperature must be at 40 C minimum. In lieu of this limit, it is acceptable to either run the engine for at least 8 minutes or complete a static run-up to 88% N2, stabilize, and check to ensure that oil pressure is equal to or less than 83 psi

33
Q

Engine Cool-Down

A

The engines must run for at least 1 minute at idle or taxi thrust before shut-down

34
Q

Minimum/Maximum Temp for A/I operation

A

-40 C

10 C

35
Q

Holding configuration icing conditions

A

Landing Gear…..UP
Flaps….. UP
Min. Airspeed….200 KIAS

36
Q

Single-engine or single bleed in icing conditions

A

Max Altitude 15,000 ft.

37
Q

Max. Load on APU generator

A

300 amps above 30,000 ft.

300 amps above 30,000 ft.

38
Q

Max. Altitude to Extend Flaps

A

20,000 ft.

39
Q

Maximum Airpseed after Take-off/During Climb without Re-trimming

A

160 KIAS

40
Q

Integrated Standby Instrument System (ISIS)

A

Maximum duration of ISIS when operating on batteries is only 40 minutes
Note: The maximum duration of battery power can be extended to 45 minutes if the Pitot 3 Sensor Heating Button is turned off when not operating in icing conditions
Airplane must not be moved during power-up initialization. Do not cage attitude in turning flight.

41
Q

Autopilot Min Altitude Coupled to ILS

A

200 ft.

42
Q

Autopilot Min. Engagement Height After Takeoff

A

500 ft.

43
Q

Autopilot single-engine go-around

A

prohibited

44
Q

Max Recommended Crosswind (Non-AFM)

A 
Dry Runway..........30 knots
Wet Runway........30 knots
Runway with compacted snow.... 25 knots
Runway with Standing Water or Slush.... 20 knots
Runway with Ice (no melting) 10 knots
45
Q

Bleed / Pack Condition

A

Maximum operating altitude when one bleed or one pack is closed is 25,000 ft. (AFM).
When operating with APU bleed supplying pack 1 (Eng. 1 bleed - closed) and engine 2 supplying Pack 2 (crossbleed closed), maximum operating altitude is 37,000 ft. (Non-AFM)

TSA (3 decks)

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