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

25
Min Fuel Temp
3 C above Freezing jet A -37C Jet A1 -44C
26
Max Fuel Imbalance for Dispatch
1500 lbs
27
Type of fuel not allowed
Use of JP-4 and Jet B fuels prohibited in revenue operations
28
** Fuel Loading Center tank may contain ___________ of fuel with LESS than full main tanks, provided _____________________________________ dose not exceed ___________________________ limits are observed
22050 lbs , center tank fuel weight plus actual ZFW , MAX ZFW and CG
29
#Max Flap Altitude
20000 FT
30
Ice conditions exist On Ground
OAT 10 C or Below and visible moisture vis <1 mile
31
APU Starter Cycle
3 in 60 mins (5 min cooling in between)
32
APU pressurization Max Alt
17000 FT
33
ENGINE START DUTY CYCLE
5 min on Cool 30” per minute of operation
34
Turn Radius for 180 deg turn
120’ (757) 146’ (767)
35
#Use of Aileron trim with A/P engaged
Prohibited
36
#HF radio operation limitation
Never use during refueling
37
Descent Policy
Fpm should not exceed altitude AGL
38
#Weather Radar Operations Limits
Never : - In hangar(does not apply to radar test) - when people close to nose radome
39
#Reverse Thrust Limits
- Ground use only | - Backing the aircraft with T/R is prohibited
40
Circuit Breakers never reset
Fuel pump or fuel control (fuel and jettinson)
41
#Flight Controls Input Limit
Avoid rapid and large alternating inputs
42
Max Cabin differential Pressure
9.1 psi | T/O and Landing .125psi (236ft blw AFE)
43
MAX TIME IN BETWEEN 2 FULL IRS ALIGNMENT
18hrs
44
MASTER CAUTION INHIBIT
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
MASTER WARNING INHIBIT
Fire bell and Master Warning light inhibited from nose wheel strut extension until 20” or 400’ RA
46
Turn degrees
Tiller 65 | Rudder 7