Chapter 1 Limitations

Question 1

Maximum Relief Valve Diff Pressure

Answer 1

9.1 PSI

Question 2

Max Diff Pressure at T/O and Land

Answer 2

0.5 PSI

Question 3

Unpressurized flight must be conducted with the cabin pressure control in ______ and the outflow valve between ___ and ___ open.

Answer 3

MANUAL, 1/2, 2/3

Question 4

Max recommended operation for any one engine pneumatic supply is:

Answer 4

• 2 A/C Packs
• One pack + eng x-bleed start
• One pack + wg anti-ice (both wgs)
• One pack + wg anti-ice (one wg) & tail anti-ice

Question 5

Automatic landings are prohibited above _____ MSL.

Answer 5

8000

Question 6

Automatic landings are prohibited on runways less than ____ in width.

Answer 6

145 ft

Question 7

Min runway width for landing:

Answer 7

148 feet or 45 meters

Question 8

Do not exceed _____ kts with single land or dual land modes of the autopilot engaged.

Answer 8

200

Question 9

Do not enter more than ____ waypoints in the FMS ACT F-PLN

Answer 9

100

Question 10

NDB approaches are prohibited at airports where the IRU mag heading error exceeds ______ deg

Answer 10

6.28

Question 11

___ LSAS channels must be operative for T/O and must originate from a common FCC.

Answer 11

2

Question 12

During banks greater than ____ deg the WSS is desensitized and alerts will be delayed.

Answer 12

15

Question 13

___ yaw damper channels must be operative for takeoff and must originate from the FCC.

Answer 13

2

Question 14

The carrying of ballast fuel limits the MTOGW to _______ and requires appropriate fuel loading and CG envelope.

Answer 14

625,500 lbs

Question 15

Ballast fuel may only be loaded into ____, ______ or ______. It may not be loaded in more than _____ tank(s) at a time. Tank 2 is limited to _____ lbs of ballast fuel.

Answer 15

• main tank 2, upper aux tank, tail tank
• one
• 25,000 lbs

Question 16

The tail tank cannot contain _____ fuel AND _____ fuel at the same time.

Answer 16

Ballast and usable

Question 17

When the tail tank contains ballast fuel, the ______ switches on the cockpit MX panel must be set to _______.

Answer 17

• 2 TAIL TANK BALLAST

- TRANS OFF

Question 18

Fuel density must be between ____ and _____. Allowable fuel temperature at takeoff ranges from ____ to ____.

Answer 18

• 6.0 to 7.1

- -40F to 122F

Question 19

When tank 3 has less than _____ lbs of fuel, the temp reflects _________, not fuel temp.

Answer 19

• 13,500

- Air temperature

Question 20

Fuel Use Schedule:

1. Fuel will be transferred from ______ to _______, keeping them full. Simultaneously, fuel will be transferred from _______, keeping the _________ full until the _______ is empty.
2. When the ____ is empty, fuel will be x’d from ____ to _____ until _________. The fuel quantity in the _____ is controlled automatically by the _____.

Answer 20

1. UAT/Each MT/LAT/UAT/LAT

2. UAT / 2 / 1 and 3 / All tanks are even / Tail tank / FSC

Question 21

Which fuel pumps must be off for T/O and Land?

Answer 21

LAT and Tail tank

Question 22

Do not operate the wx radar in a _____ or within’ ____ of any personnel or spill (except for wx test mode).

Answer 22

Hangar / 50 ft

Question 23

MX should service Sys 1/2 hydraulics if less than ___ and ____ for Sys 3.

Answer 23

4.75 / 6.0

Question 24

Anti-Ice should be on if air temp is below ____ and moisture is present or spread is within ____.

Answer 24

42 deg F (6 TAT)

5 deg F

Question 25

Prior to reducing thrust for descent in icing conditions, the ____ and _____ must be ON. (GE ENGINES)

Answer 25

EGN IGN OVRD

ENG, WING and TAIL AI

Question 26

Select engine ignition OVRD ON whenever conditions call the use of ________. (GE ENGINES)

Answer 26

Engine or Engine airframe Anti-Ice

Question 27

Do not operate windshield wipers at high speed for more than _____.

Answer 27

30 sec

Question 28

APU starter duty cycle is limited to ____ consecutive start attempts. After ___ min of req cooling time, ____ additional starts may be attempted followed by a cooling period of _____.

Answer 28

2
10
2
1 hours

Question 29

Ignition OVRD should be used to flameout protection during ____ (GE) and _________ for (PW).

Answer 29

Sev

Mod to Sev

Question 30

GE Engines:

• A logbook entry is req whenever EGT of ___ is exceeded.
• If EGT is between ____ and ____ for less than 40 secs, MX action must be taken before the next start. One start is allowed in that range. Request MX inspection delay till next flight.
• Repetitive starts where EGT exceeds ____ but does not exceed ___ for ____ are cause for corrective action.

Answer 30

• 750 C
• 820 C and 870 C
• 750 C / 820 C / 40 sec

Question 31

Engine starter motor may be operated continuously for ____. It must be cooled for at least ___ for each minute of operation before a subsequent start.

Answer 31

5 min / 30 sec

See AOM for Engine Specific Limitations