900 Limitations

Question 1

Max Ramp Weight

Answer 1

85,000 lbs

Question 2

Max Takeoff Weight

Answer 2

84,500 lbs

Question 3

Max Landing Weight

Answer 3

75,100 lbs

Question 4

Max Zero Fuel Weight

Answer 4

70,750 lbs

Question 5

Min Flight Weight

Answer 5

45,000 lbs

Question 6

Forward Cargo - Comp 11

Answer 6

1700 lbs

Question 7

Aft Cargo - Comp 61 (900)

Answer 7

2892 lbs

Question 8

Cabin Wardrobe (900)

Answer 8

385 lbs

Question 9

Aft Cargo - Comp 61 (NG)

Answer 9

3740 lbs

Question 10

Cabin Wardrobe (NG)

Answer 10

215 lbs

Question 11

Flight must be within ___ minutes of a suitable airport if cargo is carried in either cargo compartment

Answer 11

60 min

Question 12

Max Operating Speed

Answer 12

M .84 or 335 KIAS

Question 13

Max Mach in RVSM

Answer 13

M .82

Question 14

Max altitude for single PACK ops

Answer 14

82 cabin occupants or less - 31,000 ft

83 cabin occupants or more - 25,000 ft

*including flight attendants

Question 15

Min autopilot altitude for 1 engine inop precision approach

Answer 15

110 AGL

Question 16

Min autopilot altitude for APV approaches (NG)

Answer 16

80 AGL

Question 17

Operations with an ILS glideslope or APV glidepath that exceeds ___ degrees is prohibited

Answer 17

3.5 degrees

Question 18

Max airspeed at the initial approach fix for an approach with a T-transition (NG)

Answer 18

210 KIAS

Question 19

Max individual AC generator load [Main Genertor]

Answer 19

40 kVA

Question 20

Max Individual AC generator load [APU Generator]

Answer 20

40 kVA

Question 21

Max continuous load on each TRU

Answer 21

120 AMPS

Question 22

Flaps 1

Answer 22

230 KIAS

Question 23

Flaps 8

Answer 23

230 KIAS

Question 24

Flaps 20

Answer 24

220 KIAS

Question 25

Flaps 30

Answer 25

185 KIAS

Question 26

Flaps 45

Answer 26

170 KIAS

Question 27

Max fuel imbalance between main tanks [Takeoff]

Answer 27

300 lbs

Question 28

Max fuel imbalance between main tanks [All phases of flight except for takeoff]

Answer 28

800 lbs

Question 29

Min fuel in each wing tank for go-around

Answer 29

600 lbs

Question 30

Min cool hydraulic fluid quantity required for dispatch [27 C or less]

Answer 30

System No. 1 - 34% System No .2 - 29% System No. 3 - 31%

Question 31

Max airspeed with the windshield wiper operating or in an un-parked position

Answer 31

250 KIAS

Question 32

Max Landing Gear Speed

Answer 32

Extension - 220 KIAS Retraction - 200 KIAS

Question 33

Tire Limit Speed

Answer 33

195 KIAS

Question 34

The starter must not be engaged if indicated N2 RPM exceeds ___

Answer 34

50%

Question 35

Starter Cranking Limits [Ground]

Answer 35

1st and 2nd - 90 sec on, 10 sec off 3rd through 5th - 90 sec on, 5 min off

Question 36

Starter cranking limits [Air]

Answer 36

1st - 2 min on, 10 sec off 2nd through 5th - 1 min on, 5 min off

Question 37

Dry motoring cycle [Ground]

Answer 37

1st - 2 min on, 10 sec off 2nd through 5th - 1 min on, 5 min off

Question 38

Dry motoring cycle [Air]

Answer 38

1st - 90 sec on, 5 min off 2nd through 5th - 30 sec on, 5 min off

Question 39

Max continuous oil pressure

Answer 39

95 PSI

Question 40

Max transient oil pressure after cold start

Answer 40

182 PSI

Question 41

Max APU starting altitude

Answer 41

37,000 ft

Question 42

Max APU starts or start attempts in one hour

Answer 42

3 Must observe 2 minutes before next start attempt

Question 43

Bleed air extraction from the APU is not permitted above ___ ft

Answer 43

25,000 ft

Question 44

APU bleed air extraction for engine start during flight is limited to ___ ft

Answer 44

21,000 ft

Question 45

With the APU DOOR not CLSD or DOOR position unknown the APU must remain in operation OR the airplane must be limited to ___ KIAS

Answer 45

220 KIAS

Question 46

Max ambient temperature for takeoff and landing

Answer 46

ISA +35

Question 47

Normal Takeoff, Go-around and Max thrust are limited to ___ min

Answer 47

5 min

Question 48

APR thrust is limited to ___ min

Answer 48

10 min

Question 49

Do not exceed 75% **N1** for ___ min after start or until all indications are in the normal range

Answer 49

2 min

Question 50

Flight spoilers must not be extended at airspeeds below applicable flap landing speed plus ___ KIAS

Answer 50

10 KIAS

Question 51

To apply the approach ban on an RNAV SCDA, the descent angle from the FAF must be between ___ and ___ degrees

Answer 51

2.9 to 3.5 degrees (inclusive) Otherwise, 2.9 to 4.0 degrees using charted visibility

Question 52

Max pressure altitude for takeoff and landing (900)

Answer 52

8,000 ft

Question 53

Max pressure altitude for takeoff and landing (NG)

Answer 53

10,000 ft