Trans States Limitations

Question 1

Max. Altitude (PA)

Answer 1

37,000 ft

Question 2

Max. Operating Temp.

Answer 2

ISA + 35 degrees C

Question 3

TAT in cruise above ______ is limited to ______

Answer 3

25,000 ft.

-45 degrees C

Question 4

VLO (Retraction)

Answer 4

200 KIAS

Question 5

VLO (Extension)

Answer 5

250 KIAS

Question 6

VLE (Extended)

Answer 6

250 KIAS

Question 7

Maximum Operating VMO/MMO

Answer 7

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

Question 8

Maneuvering VA

Answer 8

200 KIAS

Question 9

Flap Extended VFE

Answer 9

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

Question 10

Tailwind

Answer 10

10 Knots Maximum

Question 11

Direct Vision Window

Answer 11

Max to Remove: 140 KIAS (AFM)

Question 12

Windshield Wiper

Answer 12

Max for Operation: 170 KIAS (AFM)

Question 13

Turbulent Air Penetration (AFM)

Answer 13

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

Question 14

Maximum Aft Cargo Weight

Answer 14

2646 lbs.

Question 15

Maximum Useable Quantity each Tank

Answer 15

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

Question 16

Max APU Start Alt.

Answer 16

30,000 ft.

Question 17

Note 1 APU. Max EGT temp

Answer 17

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

Question 18

APU Note 6. Max EGT

Answer 18

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

Question 19

APU Starter Limits

Answer 19

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

Question 20

Engine Starter Limits on Ground:

Answer 20

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

Question 21

Engine Starter Limits in Flight

Answer 21

Maximum Continuous Operation Time…. 5 minutes on

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

Question 22

ATTCS

Answer 22

Must be operative for ALT T/O-1 Mode

Question 23

Reversers

Answer 23

Do not go-around after reverser deployment

Question 24

Oil Pressure

Below 88% N2

Answer 24

Maximum 110 psi (2) (7)

Question 25

Oil pressure At or above 88% N2

Answer 25

Maximum 110 psi (7)

Question 26

Engine Parameter Note 1. Take off thrust

Answer 26

Takeoff Thurst is time limited to 5 minutes

Question 27

Engine Parameter Note 2. Max oil pressure

Answer 27

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.

Question 28

Engine Parameter Note 3. Minimum temp for engine start.

Answer 28

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

Question 29

Engine Parameter Note 4. Vibration

Answer 29

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.

Question 30

Engine Parameter Note 6. Operation limits for high oil pressure

Answer 30

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.

Question 31

Engine Parameter Note 8. Oil pressure on TO

Answer 31

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).

Question 32

Engine Warm-Up

Answer 32

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

Question 33

Engine Cool-Down

Answer 33

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

Question 34

Minimum/Maximum Temp for A/I operation

Answer 34

-40 C | 10 C

Question 35

Holding configuration icing conditions

Answer 35

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

Question 36

Single-engine or single bleed in icing conditions

Answer 36

Max Altitude 15,000 ft.

Question 37

Max. Load on APU generator

Answer 37

300 amps above 30,000 ft. | 300 amps above 30,000 ft.

Question 38

Max. Altitude to Extend Flaps

Answer 38

20,000 ft.

Question 39

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

Answer 39

160 KIAS

Question 40

Integrated Standby Instrument System (ISIS)

Answer 40

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.

Question 41

Autopilot Min Altitude Coupled to ILS

Answer 41

200 ft.

Question 42

Autopilot Min. Engagement Height After Takeoff

Answer 42

500 ft.

Question 43

Autopilot single-engine go-around

Answer 43

prohibited

Question 44

Max Recommended Crosswind (Non-AFM)

Answer 44

``` 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 ```

Question 45

Bleed / Pack Condition

Answer 45

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)