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Amerijet 767 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Runway Slope

A

+/- 2%

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2
Q

Max Operating Altitude

A

43,100

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3
Q

Max T/O and Landing Altitude

A

8,400 PA

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4
Q

Max Tailwind 200/300

A

10 Kts(200) / 15 Kts (300)

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5
Q

Max Demonstrated Crosswind

A

29 kts (not limiting)

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6
Q

Turbulent Air Penetration Speed

A

290 Kts / .78 M

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7
Q

Altimeter Checks

A 
75' of Field Elevation
200' Difference CAP/COP in RVSM
40' Difference CAP/COP @ Sea Level
45' Difference CAP/COP @ 5000
50' Difference CAP/COP @10,000
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8
Q

Max G Loading

A

Flaps up 2.5g to -1.0g
Flaps down +2.0g to 0.0g(max ldg wt)
(1.5g at max T/O weight)

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9
Q

Max Taxi Weight 200/300

A

352,200 / 413,000

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10
Q

Max T/O weight 200/300

A

351,000 / 412,000

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11
Q

Min Inflight Weight 200/300

A

168,000 / 179,000

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12
Q

Max Landing Weight 200/300

A

283,000 / 326,000

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13
Q

Max ZFW 200/300

A

266,000 / 309,000

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14
Q

Cargo Door Wind Limits

A 
Operation 40kts
Door Open (STATIC) 60kts
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15
Q

A/P Min Altitude Use

A

400’ after Takeoff

50’ below MDA/DA unless autoland

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16
Q

Autoland wind limitations

A

25 kts HW
25 kts Xwind
10 kts Tailwind (200/300)

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17
Q

Navigation Limitations

A

1) No IFR or Night 73 degrees N or 60 degrees S
2) VOR Approach - 1 pilot raw data
3) TAAD Override selected when IRS in NAV only mode when within 15 nm of T/O, APP, Lnd when airport has no inst appr or RWY less than 3500 feet.

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18
Q

Aircraft Certification

A

FAR Part 25 and Part 36

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19
Q

Weather Radar operating restriction

A

In hangar or within 50ft of a fuel spill or personnel

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20
Q

How often must we verify flight deck access system

A

Once each flight day

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21
Q

Smoke barrier door

A

Must be closed during taxi, t/o and landing except for access

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22
Q

CONT Ignition

A

Must be on during severe turbulence

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23
Q

EGT LIMITS

A

CF6-80A CF6-80C
Starting 750C 750C
Takeoff(5min) 940C 960C
Continuous 895C 925C

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24
Q

Min Oil Quantity 200/300

A

17 qts

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25
Q

Min Oil Pressure 200/300

A

10 psi

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26
Q

Max Oil Temp 200/300

A

160C continuous

175 for 15 min

27
Q

What circuit breakers cannot be reset

A

1) Fuel Pump

2) Fuel Pump Control

28
Q

Maximum Flaps Altitude

A

20,000ft

29
Q

Flap Limit Speeds (200)

A
  1. …240
  2. …220
  3. …210
  4. …195
  5. …190
  6. …162
30
Q

Flap Limit Speeds (300)

A
  1. …250
  2. …230
  3. …210
  4. …210
  5. …180
  6. …170
31
Q

FAR Transport Category

A

FAR Part 25, FAR Part 36

32
Q

Maneuvering G Limits

A

Flaps up +2.5g to -1.0g
Flaps down +2.0g to 0.0g

*Withs flaps 25 or 30 positive g limit varies linearly from 2.0g at MLW to 1.5g at MTOW

33
Q

If landing weight is 272,000 lbs or less the (200 only)…

A

Wing fuel at landing must be 79,000 lbs or less

34
Q

If landing weight is over 272,000 lbs the (200 only)…

A

Wing fuel at landing must be 43,000 lbs or less

35
Q

Flight Deck security door

A

operational check of the flight deck access system must be accomplished once each FLIGHT DAY

36
Q

Autoflight Limits

A

Do not engage cmd mode below 400ft on T/O
Use of Aileron trim prohibited
Autoland not authorized with flaps 20 or less
Autoland not athorized above MLW

37
Q

When to use CONT IGN

A

Severe Turb

38
Q

Flight crew cannot blank ENG VIB display when?

A

Takeoff

39
Q

Max fuel temp Jet A

A

49C

40
Q

Minimum Fuel temp above freezing

A

Freezing temp +3C

41
Q

Fuel imbalance

A

2000 +- 500

42
Q

Fuel Loading

A

Center Tank may contain up to 22,050 lbs with less than full wing tanks provided center furl plus ZFW does not exceed MAX ZFW and CG is within limits. In this case FUEL USAGE II must be utilized

43
Q

Prohibited Fuel on revenue

A

JP4 and JP8

44
Q

FUEL USAGE I

A

Tank to engine fuel for T/O and LDG with all operable pumps on and crossfeed closed.

Open crossfeed for minimum fuel operations or to correct / prevent imbalance

45
Q

FUEL USAGE II

A

Use center tank fuel for all operations until depleted.

Open crossfeed for minimum fuel operations.

Intentional dry running of center tank (CENTER L FUEL PUMP, CENTER R FUEL PUMP) is prohibited

46
Q

If center fuel pump fails with fuel in the center tank, what checklist

A

FUEL PUMP

47
Q

With engines off on the ground and fuel in the center tank verify…

A

CTR L FUEL PUMP and CTR R FUEL PUMP are displayed

48
Q

Prior to transferring fuel or defueling verify conduct..

A

a lamp test of the respective fuel pump low pressure light

49
Q

Which circuit breakers may we NOT reset

A

FUEL PUMP and/or FUEL PUMP CONTROL circuit breakers

50
Q

Prior to ETOPS flight you must check

A

Fuel crossfeed in aircraft with a single crossfeed valve.

This may not be done earlier that 1 hour prior to he flight crew boarding for departure

51
Q

Max Fuel Imbalance

A

2500 - 48,000 or less
Linear reduction 48,000 to 79,000
1500 - Greater than 79,800

52
Q

Reverse Backing

A

prohibited

53
Q

Max Flaps altitude

A

20,000

54
Q

IRS will provide valid MAG HDG and TRACK when

A

82 N except from 80 W to 130 W the boundary is restricted to 70 N

The southern boundary is 82 S except from 120 E to 160 E the boundary is restricted to 60 S

55
Q

Do not operate IFR or at NIGHT when

A

North of 73N or south of 60S when those are in reference to magnetic N

56
Q

When must TERR OVD be selected

A

1) FMS in IRS NAV ONLY mode
2) Within 15nm of a takeoff or approach or landing to an airport of which ANY of the following conditions apply

  • The airport has no approved approach
  • Longest rwy is less than 3500 feet

1) Also inhibit when dispatching with both FMCs inop
2) BOTH FMCs fail in flight
3) when doing QFE ops

57
Q

FMC may be used during approach provided

A

Raw data is being monitored

58
Q

When to use VOR on HSI

A

One pilot must monitor during VOR Appr

59
Q

What is approved to be transmitted via ACARS

A 
PDC
D-ATIS
Oceanic Clearance
Weight and Balance
Takeoff Data

*If they are verified

60
Q

Icing Conditions

A

GROUND:
AT OR BELOW 10C
Visible Moisture Present

FLIGHT:
ENG A/I when TAT AT OR BELOW 10C except -40C
Visible Moisture
Prior to reducing thrust for descent below 10C ENG A/I must be on and Wing below 22,000ft

61
Q

Starter Duty Cycle Limits

A

Normal - 1 min on 1 minute off indefinitely

Extended - 2 min on, 1 minute off
5 min on 2.5 min off
Two consecutive 5 min on cycles require a 10
min cooling period before addition 5 min cycle

Re-engagement - 0-20%N2 recommended
20-30%N2 Permissible
Above 30% permissible for purging or to clear a fire, may result in gearbox damage (logbook entry required above 20% N2

62
Q

When EGPWS display is desired do not

A

operate HSI in CTR mode

63
Q

Polarized Sunglasses

A

Prohibited

64
Q

If flight crew is asked by ATC to disable altitude reporting

A

200 - XPDR switch to OFF on the ALT switch

300 - Select ALT OFF

Amerijet 767 (2 decks)

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