Emergencies & Limitations Flashcards
(42 cards)
1
Q
Engine Failure During Takeoff
(Below V1 — Takeoff Aborted)
A
- Brakes…………………Apply
- Thrust…………………Idle
- Lift Dump……………Extend
2
Q
Engine Failure During Takeoff
(Above V1 — Takeoff Continued)
A
- Pitch (at VR)……. 8°–10° Noseup
- Gear (Positive Rate) … Up
- Airspeed …………………….. Maintain V2
3
Q
**Engine Fire **
A
- Thrust (Affected Engine)……………….. Idle
* If Eng Fire Push Switch Remains Illuminated:* - Thrust Lever (Affected Engine) ….. Cutoff
- Illuminated Eng Fire Push Switch .. Push
- Fire Ext Push Switch ……………………… Push
4
Q
**Inadvertent Overspeed **
A
- Thrust ……………….. Idle
- Speed Brakes … Extend
5
Q
**Smoke Or Fire **
A
- Crew Oxygen Masks……….. Don
- Smoke Goggles……………….. Don
- Cockpit Door……………………. Open
6
Q
Cabin Decompression
(Cabin Alt Hi Annunciator Illuminated)
A
- Crew Oxygen Masks…………. Don
7
Q
**Emergency Descent **
A
- Thrust…………………… Idle
- Speed Brakes……… Extend
8
Q
Bleed Air Leak
(L Or R Bleed Leak Annunciator Illuminated)
A
- Bleed Air ……….. Select Opposite Source
9
Q
Bleed Air Overheat
(L Or R Bleed Ovht Annunciator Illuminated)
A
- Bleed Air……… Select Opposite Source
10
Q
Wing Anti-Ice Overheat
(L Or R Wing Ovht Annunciator Illuminated)
A
- Wing Anti-Ice (Affected Wing) …. Off
11
Q
Dual Generator Failure
(L And R Gen Off Annunciators Illuminated)
A
- GCU Circuit Breakers… Check In
- Generators…………………. Reset, Then On
12
Q
**Trim Malfunctions **
A
- Trim Interrupt ………. Push And Hold
13
Q
**Lift Dump Handle Will Not Move **
A
- Lift Dump Lock Release …. Push And Hold To Release
- Lift Dump…………………………… Extend
14
Q
Lift Dump Fails To Extend
(Lift Dump Warning Tone Sounds)
A
- Brakes ……. Apply And Maintain Maximum Braking
15
Q
**Power Brake Failure **
A
- Emergency Brakes …… Apply Gradually
16
Q
**Autopilot Malfunctions **
A
- AP/Trim Master Switch …….. Push
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
- Go-Around Button …. Depress
- Thrust……………………. Take-Off N1
- 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
- Go-Around Button ……. Depress
- Thrust ………………………… Take-Off N1
- 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
- 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
AIRSPEED LIMITATIONS - VMCA
VMCA
## Footnote
(Flaps Up).............. 104 KIAS
(Flaps 10) ............... 100 KIAS
(Flaps 20) ............... 96 KIAS
(Flaps DN)................ 93 KIAS
26
ENGINE LIMITS % RPM
## Footnote
N2 — Takeoff, Max Cont... \_\_\_% RPM
N1 — Takeoff, Max Cont... \_\_\_% RPM
N1 — Transient................... \_\_\_% RPM
N2 — Takeoff, Max Continuous... 98.8% RPM
N1 — Takeoff, Max Continuous... 105.2% RPM
N1 — Transient.......................... 106.4% RPM
27
ENGINE LIMITS - ITT TEMP (°C)
## Footnote
Max Continuous... \_\_\_°C
Takeoff.................... \_\_\_°C ( \_\_ Minutes)
Transient................. \_\_\_°C ( \_\_ sec)
Start......................... \_\_\_\_°C ( \_\_ sec)
Max Cont ... 805°C
Takeoff......... 820°C (5 Minutes)
Transient..... 835°C (10 sec)
Start.............. 1000°C (15 sec)
28
ENGINE LIMITS OIL (°C/PSI)
## Footnote
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
**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 ... 45 to 90 psi
29
WIND LIMITS FOR ENGINE STARTS
Tailwind Max............. 15 KIAS
Crosswind Max......... 25 KIAS
30
STARTER LIMITS
## Footnote
(Battery or External Power Assisted Start)
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
EXTERNAL POWER LIMITS
Volts .... 28.0–28.4
Amps ... 400 Amps (Continuous)
/ 1000 Amps (Momentary)
32
GENERATOR LIMITS
Ground Operation (Each Generator)
Maximum Amps... 325 Amps
33
GENERATOR LIMITS
In-Flight Operation
One or Both Generators (to FL410)
Max Amps................. 325 Amps
One Generator (to FL290 in Icing Cond)
Max Amps ................ 400 Amps
34
STRUCTURAL LIMITATIONS
Ramp
Takeoff
Landing
Zero Fuel
Maximum Weights:
Ramp ........... 12,591 lbs
Takeoff.......... 12,500 lbs
Landing ........ 11,600lbs
Zero Fuel .... 10,000 lbs
35
FUEL LIMITS
Approved Fuels
Temps
Approved Engine Fuels (unlimited use)
Jet A, Jet A-1, JP-8
Fuel Temperature (°C)
Minimum..... –40°C
Maximum..... 43°C
36
ICING LIMITATIONS - Must be ON below ____ ˚C
Temp (°C) ......... When operating in visibile moisture and 5°C or Colder (engines / wings)
## Footnote
Max 30sec Wing anti-ice ON, at Take-off Thrust, prior to Brake Release.
37
ICING LIMITATIONS - Holding Min Speed. Flaps
Holding in Icing Conditions
Is prohibited below 160 KIAS.
Must have flaps UP
38
AUTO PILOT LIMITATIONS
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
EFIS LIMITATIONS - How many Adaptive Flight Displays must be operated in normal mode for takeoff?
All Adaptive Flight Displays must be operated in normal mode for takeoff
40
VNAV LIMITATIONS
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
TAKEOFF AND LANDING OPERATIONS
## Footnote
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
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
ENROUTE OPERATIONS
## Footnote
Maximum Operating Altitude... _____ ft
Ambient Air Temperature (°C)... –\_\_°C to \_\_\_\_\_°C
Maximum Fuel Imbalance ......... ___ lbs
Yaw Damper .................................. \_\_\_\_\_\_\_
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
