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DELTA > 7ER General Limitations > Flashcards

7ER General Limitations Flashcards

1
Q

Runway Slope

A

+/- 2%

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2
Q

Max Operating Altitude

A

43000 PA (767)
42000 PA (757)

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3
Q

Max T/O and Landing Altitude

A

8400 PA

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4
Q

Max Tailwind

A

10 Kts as permitted per Company pages

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5
Q

Severe Turbulent Air Penetration

A

290 Kts/ .78M

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6
Q

Max Difference CPT/FO/Field Elevation (Altimeter)

A

75 Ft

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7
Q

Max Difference In Flight (RVSM)

A

200 FT

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8
Q

Max Difference CPT/FO @ S.L.

A

40 FT (767)
25 FT (757)

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9
Q

Max Difference CPT/FO @ 5,000 FT

A

45 FT (767)
35 FT (757)

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10
Q

Max Difference CPT/FO @ 10,000 FT

A

50 FT (767)
40 FT (757)

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11
Q

MAX CROSSWIND TO/LDNG

A

40 kts including gusts

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12
Q

Min Alt to Engage CMD

A

After T/O 200 FT

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13
Q

Min Alt for use of A/P **

A

ENROUTE 1000FT AGL

APPROACH 50 FT AGL or 50 blw DDA/MDA

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14
Q 
#Autoland 
  Max Headwind
A

25 Kts

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15
Q 
#Autoland
  Max Crosswind
A

25 Kts By AFM

Delta 15 Kts Cat II/ Cat III
40 kts Cat I

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16
Q 
#Autoland 
  Max Tailwind
A

10 Kts

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17
Q

AUTOPILOT USE FOR LANDING 8400ft or ABOVE

A

Do not use Autopilot below 100 ft RA

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18
Q

Starting MAX EGT

A

757
485C(max 30”) - 545C

767
535C PW
750C GE

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19
Q

MAX EGT TAKE OFF

A

757
645C max 5’ ( ok transient 660 5”)

767
650C PW
960C GE

20
Q

Min Oil Quantity (Dispatch)

A

17 Quarts
Ok up to 8 Qts after engine stabilize .
Below 8 Qts need ok from Maintainance

21
Q

AUTOLAND MAX GROUND SPEED

A

Do not Autoland when GS exceed 165 kts

22
Q

Engine vibration indicator during take off

A

Should not be blanked

23
Q

GROUND PROXIMITY TERRAIN OVERRIDE SWITCH TO OVERRIDE WHEN

A
  • FMS operating IRS in NAV only mode
  • outside of USA and FMS database not referenced to WGS-84 unless FMS found suitable to operate in that airspace
  • prior to TO FMS position update not verified
24
Q

Max Fuel Temp

A

49 C

25
Q

Min Fuel Temp

A

3 C above Freezing
jet A -37C
Jet A1 -44C

26
Q

Max Fuel Imbalance for Dispatch

A

1500 lbs

27
Q

Type of fuel not allowed

A

Use of JP-4 and Jet B fuels prohibited in revenue operations

28
Q

** Fuel Loading
Center tank may contain ___________ of fuel with LESS than full main tanks, provided _____________________________________ dose not exceed ___________________________ limits are observed

A

22050 lbs , center tank fuel weight plus actual ZFW , MAX ZFW and CG

29
Q

Max Flap Altitude

A

20000 FT

30
Q

Ice conditions exist On Ground

A

OAT 10 C or Below and visible moisture vis <1 mile

31
Q

APU Starter Cycle

A

3 in 60 mins (5 min cooling in between)

32
Q

APU pressurization Max Alt

A

17000 FT

33
Q

ENGINE START DUTY CYCLE

A

5 min on

Cool 30” per minute of operation

34
Q

Turn Radius for 180 deg turn

A

120’ (757)
146’ (767)

35
Q

Use of Aileron trim with A/P engaged

A

Prohibited

36
Q

HF radio operation limitation

A

Never use during refueling

37
Q

Descent Policy

A

Fpm should not exceed altitude AGL

38
Q

Weather Radar Operations Limits

A

Never :

  • In hangar(does not apply to radar test)
  • when people close to nose radome
39
Q

Reverse Thrust Limits

A
  • Ground use only

- Backing the aircraft with T/R is prohibited

40
Q

Circuit Breakers never reset

A

Fuel pump or fuel control (fuel and jettinson)

41
Q

Flight Controls Input Limit

A

Avoid rapid and large alternating inputs

42
Q

Max Cabin differential Pressure

A

9.1 psi

T/O and Landing .125psi (236ft blw AFE)

43
Q

MAX TIME IN BETWEEN 2 FULL IRS ALIGNMENT

A

18hrs

44
Q

MASTER CAUTION INHIBIT

A

During take off

Beeper and Master caution between 80kts and 400ft AGL OR 20” after nose gear strut extension

If RTO above 80kts the inhibit will stay until 75kts

45
Q

MASTER WARNING INHIBIT

A

Fire bell and Master Warning light inhibited from nose wheel strut extension until 20” or 400’ RA

46
Q

Turn degrees

A

Tiller 65

Rudder 7

DELTA (8 decks)

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