Limitations Flashcards

(48 cards)

1
Q

Limiting Tailwind Component

A

10 Kts

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2
Q

Maximum take off and Landing altitude

A

8300 Ft

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3
Q

Minimum takeoff and landing landing altitude

A

-1000

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4
Q

Take off and landing temperature limits

A

Minimum -65F(-54C)

Maximum. +120F(+49C)

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5
Q

Maximum Crosswind (takeoff and landing)

A

Crosswind 30kts

Standing slush/water 20 kts

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6
Q

Maximum Operating Altitude

A

37000

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7
Q

Maximum ground operating limits landing lights

A

5 minutes on

5 minutes off

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8
Q

Maximum operating speed

A

VMO 350 Knots

MMO .84 Mach

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9
Q

Landing gear operating

A

Extension 270 knots/ .82M

Retraction 235Knots/ .82

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10
Q

Landing gear extended

A

320 knots /.82M

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11
Q

Flap placard speeds

A

Flap position Limiting speed (VFE)

   1. 230 
   2. 230
   5. 225
   10. 210
   15. 195
   25. 190
   30. 185
   40. 170
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12
Q

Turbulence Penetration

A

Above 10000/280 knots/.70M whichever is slower

Below 10000 250 knots

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13
Q

Mach Trim system inoperative max speed

A

.74M

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14
Q

Pressurization system

A

Maximum system differential pressure (safety relief)
8.65PSI

Normal operating differential pressure

  1. 8 +/- 0.1 PSI FL280 and above
  2. 45 +/-0.1 PSI Below FL280
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15
Q

Max allowable cabin pressure differential for take off and landing

A

0.125 psi

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16
Q

Maximum weights

A
Taxi: 125,000
Takeoff: 124,500
Flaps Up: 124,00
Flaps 30/40: 108,000
Landing: 107,000
ZFW: 95,000
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17
Q

Minimum altitude for use of autopilot

A

Climb and in route do not use autopilot below 500 ft agl

Approach: 50 ft Agl

Do not use autopilot pitch Channels above .81M with hydraulic system A or B depressurized

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18
Q

APU maximum EGT

A

760 C

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19
Q

APU Maximum continuos EGT

A

710

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20
Q

Maximum altitude for APU bleed and electrical

21
Q

Max altitude APU bleed

22
Q

Max altitude APU Electrical

23
Q

APU max operating altitude

24
Q

APU Starting cycles

A

Five minutes cooling requires between the second and third attempt, a one hour wait after the 3rd attempt

25
AC system
Engine driven generators max load 111 amperes
26
APU Generator load
Ground 125amps | Flight. 111amps
27
DC system
TR Voltage 24-30 Volts TR Load 65 amps with cooling TR Load. 50 amps without cooling
28
Battery Voltage
22-30 Volts
29
CSD Temps
Oil temp IN maximum 157C | Oil temp rose maximum 30C
30
Maximum flap extension altitude
20,000
31
Alternate flap duty cycle
Ground One cycle, 10 minutes off | Flight One cycle , 25 minutes off
32
Maximum airspeed alternate flap extension
210 kts
33
Min/Max fuel temperature
Max fuel temperature 49 C | Min fuel temperature-37 C
34
Inflight tank temperature must be maintained within
3 degrees C above the freezing point of the fuel being used.
35
Maximum fuel tank quantities
Wing tanks 20,264 | Center Tank 15,684
36
Minimum fuel for ground operation of electric and engine hydraulic pumps
1675
37
Maximum tire ground speed
191 kts
38
Minimum crew oxygen
2: 800 3: 1000 4: 1350
39
Engine oil pressure
Minimum 40 PSI | Maximum. 55 PSI
40
Oil temperature JT8D-17A
Maximum continuous operation 130 C | Maximum for 15 minutes 135 C to 165C
41
Minimum oil quantity for dispatch
2.5 gallons
42
Engine ignition must be on for
Take-off and landing
43
Ignition duty cycle
FLT 2 min ON, 3 min OFF 2 min ON, 23 min OFF LOW IGN Continuous
44
Started duty cycle
First attempted start 30 seconds ON 1 minute OFF Second attempted start 30 seconds On 1 minute off Third attempted start. 30 seconds ON 5 minutes off
45
Started duty cycle ( slow start )
First attempt. 1 minute ON 1 minute off | Second attempt. 1 minute ON 5 minute off
46
Starter duty cycle no fuel ( motoring only)
2 minutes ON 5 minutes OFF
47
JT8D RPM Limits
N1……….102.4% | N2………..100.0%
48
EGT Limits JT8D-17A
Operation condition. Max temp. Time limit Take off 5 min 650C. 5 min Acceleration rapid Power application 2 minutes 660C. 2 min Max continuous and Normal climb 610C. Continuous Starting ground. 575C. Momentary Inflight. 650C. Momentary