Emergencies & Limitations Flashcards

1
Q

Engine Failure During Takeoff

(Below V1 — Takeoff Aborted)

A
  1. Brakes…………………Apply
  2. Thrust…………………Idle
  3. Lift Dump……………Extend
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2
Q

Engine Failure During Takeoff

(Above V1 — Takeoff Continued)

A
  1. Pitch (at VR)……. 8°–10° Noseup
  2. Gear (Positive Rate) … Up
  3. Airspeed …………………….. Maintain V2
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3
Q

**Engine Fire **

A
  1. Thrust (Affected Engine)……………….. Idle
    * If Eng Fire Push Switch Remains Illuminated:*
  2. Thrust Lever (Affected Engine) ….. Cutoff
  3. Illuminated Eng Fire Push Switch .. Push
  4. Fire Ext Push Switch ……………………… Push
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4
Q

**Inadvertent Overspeed **

A
  1. Thrust ……………….. Idle
  2. Speed Brakes … Extend
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5
Q

**Smoke Or Fire **

A
  1. Crew Oxygen Masks……….. Don
  2. Smoke Goggles……………….. Don
  3. Cockpit Door……………………. Open
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6
Q

Cabin Decompression

(Cabin Alt Hi Annunciator Illuminated)

A
  1. Crew Oxygen Masks…………. Don
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7
Q

**Emergency Descent **

A
  1. Thrust…………………… Idle
  2. Speed Brakes……… Extend
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8
Q

Bleed Air Leak

(L Or R Bleed Leak Annunciator Illuminated)

A
  1. Bleed Air ……….. Select Opposite Source
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9
Q

Bleed Air Overheat

(L Or R Bleed Ovht Annunciator Illuminated)

A
  1. Bleed Air……… Select Opposite Source
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10
Q

Wing Anti-Ice Overheat

(L Or R Wing Ovht Annunciator Illuminated)

A
  1. Wing Anti-Ice (Affected Wing) …. Off
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11
Q

Dual Generator Failure

(L And R Gen Off Annunciators Illuminated)

A
  1. GCU Circuit Breakers… Check In
  2. Generators…………………. Reset, Then On
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12
Q

**Trim Malfunctions **

A
  1. Trim Interrupt ………. Push And Hold
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13
Q

**Lift Dump Handle Will Not Move **

A
  1. Lift Dump Lock Release …. Push And Hold To Release
  2. Lift Dump…………………………… Extend
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14
Q

Lift Dump Fails To Extend

(Lift Dump Warning Tone Sounds)

A
  1. Brakes ……. Apply And Maintain Maximum Braking
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15
Q

**Power Brake Failure **

A
  1. Emergency Brakes …… Apply Gradually
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16
Q

**Autopilot Malfunctions **

A
  1. AP/Trim Master Switch …….. Push
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17
Q

EGPWS Warning

(Pull Up Message On ADI and/or

“Pull Up” Or “Terrain, Terrain, Pull Up” Or

“Obstacle, Obstacle, Pull Up” Aural Alert)

A
  1. Go-Around Button …. Depress
  2. Thrust……………………. Take-Off N1
  3. Pitch Attitude……….. Increase And Climb As Required To Avoid Terrain
18
Q

Windshear Warning

(Red Windshear Message On ADI and/or

“Windshear, Windshear, Windshear” Aural Alert)

A
  1. Go-Around Button ……. Depress
  2. Thrust ………………………… Take-Off N1
  3. Pitch Attitude…………….. Increase As Required To Arrest Descent, Allowing Airspeed To Decrease To Intermittent Shaker Activation
19
Q

TCAS II Resolution Alert

Vertical Path Guidance Display and/or

Resolution Alert Aural Warning

A
  1. Pitch Attitude ….. Adjust As Required To Place Airplane Vertical Speed In Green Arc Depicted On The VSI
20
Q

AIRSPEED LIMITATIONS - Airframe

A

VMO (S.L. to 27,600 ft) … 320 KIAS

MMO (above 27,600 ft)… 0.80 Mach

21
Q

AIRSPEED LIMITATIONS - Flaps

A

VFE/VFO (S.L. to 20,000 ft)

(Flaps 10) …… 200 KIAS

(Flaps 20) ….. 200 KIAS

(Flaps DN) ….. 170 KIAS

22
Q

AIRSPEED LIMITATIONS - Landing Gear

A

VLE……………… 200 KIAS

VLO (Extend) … 200 KIAS

VLO (Retract)… 180 KIAS

23
Q

AIRSPEED LIMITATIONS - Speed Brakes

A

MSB………. NO LIMIT

VSB……….. NO LIMIT

24
Q

AIRSPEED LIMITATIONS - Tires

A

VTIRE……. 165Knots (True Ground Speed)

25
Q

AIRSPEED LIMITATIONS - VMCA

A

VMCA

(Flaps Up)………….. 104 KIAS

(Flaps 10) …………… 100 KIAS

(Flaps 20) …………… 96 KIAS

(Flaps DN)……………. 93 KIAS

26
Q

ENGINE LIMITS % RPM

N2 — Takeoff, Max Cont… ___% RPM

N1 — Takeoff, Max Cont… ___% RPM

N1 — Transient………………. ___% RPM

A

N2Takeoff, Max Continuous… 98.8% RPM

N1Takeoff, Max Continuous… 105.2% RPM

N1Transient…………………….. 106.4% RPM

27
Q

ENGINE LIMITS - ITT TEMP (°C)

Max Continuous… ___°C

Takeoff……………….. ___°C ( __ Minutes)

Transient…………….. ___°C ( __ sec)

Start……………………. ____°C ( __ sec)

A

Max Cont … 805°C

Takeoff……… 820°C (5 Minutes)

Transient….. 835°C (10 sec)

Start………….. 1000°C (15 sec)

28
Q

ENGINE LIMITS OIL (°C/PSI)

Oil Temp for Starting ………………. –_ to __°C

Oil Temp takeoff and max cont thrust … __–__°C

Oil Press at Idle RPM……………………… __–___ psi

Oil Press takeoff and max cont thrust….. __–__ psi

A

Oil Temp

Starting ................... –40 to 135°C

Takeoff and max cont thrust ... +10 to 135°C

**Oil Press **

at Idle RPM ..................... 35 to 100 psi

takeoff and max cont thrust<sub></sub>...  45 to 90 psi
29
Q

WIND LIMITS FOR ENGINE STARTS

A

Tailwind Max…………. 15 KIAS

Crosswind Max……… 25 KIAS

30
Q

STARTER LIMITS

(Battery or External Power Assisted Start)

A

Motoring of engine is limited to TWO Start Attempts, with engine clearing after the first Attempt as follows.

20seconds…………….. ON

30 seconds …………… OFF

20 seconds……………. ON for engine clearing

30 seconds …………… OFF

20seconds…………….. ON

2 hours…………………… OFF

31
Q

EXTERNAL POWER LIMITS

A

Volts …. 28.0–28.4

Amps … 400 Amps (Continuous)

        / 1000 Amps (Momentary)
32
Q

GENERATOR LIMITS

Ground Operation (Each Generator)

A

Maximum Amps… 325 Amps

33
Q

GENERATOR LIMITS

In-Flight Operation

A

One or Both Generators (to FL410)

Max Amps................. 325 Amps

One Generator (to FL290 in Icing Cond)

Max Amps ................ 400 Amps
34
Q

STRUCTURAL LIMITATIONS

Ramp

Takeoff

Landing

Zero Fuel

A

Maximum Weights:

Ramp ……….. 12,591 lbs

Takeoff………. 12,500 lbs

Landing …….. 11,600lbs

Zero Fuel …. 10,000 lbs

35
Q

FUEL LIMITS

Approved Fuels

Temps

A

Approved Engine Fuels (unlimited use)

Jet A, Jet A-1, JP-8

Fuel Temperature (°C)

Minimum….. –40°C

Maximum….. 43°C

36
Q

ICING LIMITATIONS - Must be ON below ____ ˚C

A

Temp (°C) ……… When operating in visibile moisture and 5°C or Colder (engines / wings)

Max 30sec Wing anti-ice ON, at Take-off Thrust, prior to Brake Release.

37
Q

ICING LIMITATIONS - Holding Min Speed. Flaps

A

Holding in Icing Conditions

Is prohibited below 160 KIAS.

Must have flaps UP

38
Q

AUTO PILOT LIMITATIONS

A
  1. Coupled VOR approaches; using a VOR as the NAV source, are prohibited.
  2. Do not use the auto pilot below 200 ft. above terrain during approach operations or below 500 ft. above the terrain during all other operations.
  3. Maximum angle for NAV capture is 90°.
39
Q

EFIS LIMITATIONS - How many Adaptive Flight Displays must be operated in normal mode for takeoff?

A

All Adaptive Flight Displays must be operated in normal mode for takeoff

40
Q

VNAV LIMITATIONS

A
  1. VNAV altitudes must be displayed on the MFD or CDU when utilizing VNAV for flight guidance.
  2. Use of VNAV while conducting a missed approach procedure is prohibited.
41
Q

TAKEOFF AND LANDING OPERATIONS

Max. Airfield Elevation (Pressure Altitude) …. ____ ft

Ambient Temperature (°C) ……………… –__°C to ____°C

Maximum Tailwind (Component)
for Takeoff and Landing......................... \_\_ Kts

Maximum Fuel Imbalance

for Takeoff/Landing… ___ lbs

A

Max. Airfield Elevation (Pressure Altitude) …. 9,400 ft

Ambient Temperature (°C) … –40°C to ISA +37°C

Maximum Tailwind (Component)
for Takeoff and Landing.......... 10 Kts

Maximum Fuel Imbalance

for Takeoff/Landing… 200 lbs

42
Q

ENROUTE OPERATIONS

Maximum Operating Altitude… _____ ft

Ambient Air Temperature (°C)… –__°C to _____°C

Maximum Fuel Imbalance ……… ___ lbs

Yaw Damper ……………………………. _______

A

Max Operating Altitude … 41,000 ft

Ambient Air Temp (°C) … –65°C to ISA +37°C

Max Fuel Imbalance ……… 200 lbs

Yaw Damper ………………….. Operable and On