UC35B EP's LMTS Practical Exercise Flashcards
ENGINE FAILURE OR FIRE, MASTER WARNING OR ANY OTHER ABNORMAL EVENT DURING TAKEOFF
* SPEED BELOW V1 – TAKEOFF REJECTED
1. ______________________________
TAKEOFF - ABORT.
ENGINE FAILURE OR FIRE, MASTER WARNING OR ANY OTHER ABNORMAL EVENT DURING TAKEOFF
- SPEED ABOVE V1 – TAKEOFF CONTINUED
1. ___________________________
Climb to safe altitude.
LH OR RH ENGINE FIRE (ENGINE FIRE)
1. ______________________________
* IF ENGINE FIRE REMAINS ILLIMINATED 15 SECONDS (PROBABLE FIRE)
2. ____________________________________________________________
3. ____________________________________________________________
- Throttle (Affected Engine) -
IDLE
* IF ENGINE FIRE REMAINS ILLUMINATED 15 SECONDS
(PROBABLE FIRE) - Illuminated ENGINE FIRE Switchlight (Affected Engine) -
LIFT COVER and PUSH. - Either Illuminated BOTTLE ARMED Switchlight -
PUSH (BOTTLE ARMED switchlight extinguishes).
ENGINE FAILURE DURING FINAL APPROACH
1. ___________________________________________________________
2. ___________________________________________________________
3. ___________________________________________________________
4. ___________________________________________________________
- AP TRIM DISC Button -
PRESS and RELEASE. - Thrust (Operating Engine) - INCREASE as required.
- Airspeed -
VAPP (minimum). - Flaps -
T.O. & APPR (15°).
EMERGENCY RESTART – TWO ENGINES
1. ___________________________________________________________
2. ___________________________________________________________
3. ___________________________________________________________
- IGNITION Switches -
BOTH ON. - FUEL BOOST Switches -
BOTH ON. - Throttles -
IDLE.
THRUST REVERSER INADVERTENT DEPLOYMENT DURING TAKEOFF
- SPEED BELOW V1 – TAKEOFF ABORTED
- ______________________________
TAKEOFF - ABORT.
THRUST REVERSER INADVERTENT DEPLOYMENT DURING TAKEOFF
- SPEED AT OR ABOVE V1 – TAKEOFF CONTINUED
- ______________________________
- ______________________________
- ______________________________
- Emergency STOW Switch (Affected Engine) …………….. EMER.
- Throttle (Affected Engine) -
CHECK IDLE. - Climb to a safe altitude.
THRUST REVERSER INADVERTENT IN-FLIGHT DEPLOYMENT
1. ____________________________________________________________
2. ____________________________________________________________
3. ____________________________________________________________
4. ____________________________________________________________
- Control Wheel/AP TRIM DISC Button ………. GRIP/PRESS and
RELEASE. - Emergency STOW Switch (Affected Engine) ……………. EMER.
- Throttle (Affected Engine) …………………………….. CHECK IDLE.
- Airspeed ………………………….. REDUCE TO 150 KIAS or below.
THRUST REVERSER UNLOCK LIGHT ON IN FLIGHT
1. ____________________________________________________________
- Emergency STOW Switch (Affected Engine) ……………. EMER.
CAB ALT (CABIN DECOMPRESSION)
1. ____________________________________________________________
2. ____________________________________________________________
3. ____________________________________________________________
- Oxygen Masks
DON and 100% OXYGEN. - Microphone Switches -
MIC OXY MASK. - Emergency Descend -
AS REQUIRED.
Refer to Emergency Procedures, EMERGENCY DESCENT.
EMERGENCY DESCENT
1. ___________________________________________________________________________________________________
2. ___________________________________________________________________________________________________
3. ___________________________________________________________________________________________________
4. ___________________________________________________________________________________________________
- AP TRIM DISC Button -
PRESS and RELEASE. - Throttles -
IDLE. - Speed Brakes -
EXTEND. - Airplane Pitch Attitude -
INITIALLY TARGET 20° NOSE DOWN
ATTITUDE.
ENVIRONMENTAL SYSTEM SMOKE OR ODOR
1. ____________________________________________________________________________________________________
2. ____________________________________________________________________________________________________
- Oxygen Masks -
DON and EMER. - Microphone Switches -
MIC OXY MASK.
SMOKE REMOVAL
1. ____________________________________________________________________________________________________
2. ____________________________________________________________________________________________________
- Oxygen Masks -
DON and EMER. - Microphone Switches -
MIC OXY MASK.
ELECTRICAL FIRE OR SMOKE
1. ____________________________________________________________________________________________________
2. ____________________________________________________________________________________________________
- Oxygen Masks -
DON and EMER. - Microphone Switches -
MIC OXY MASK.
AUTOPILOT MALFUNCTION
1. ____________________________________________________________________________________________________
- AP TRIM DISC Switch -
PRESS AND RELEASE
ELECTRIC ELEVATOR RUNAWAY TRIM
1. ____________________________________________________________________________________________________
- AP TRIM DISC Switch -
PRESS and HOLD.
STALL RECOVERY – INADVERTENT STALL (BUFFET/ROLL-OFF)
1. ______________________________________
2. ______________________________________
3. ______________________________________
4. ______________________________________
- Autopilot -
DISCONNECT. - Pitch Attitude -
REDUCE. - Roll Attitude -
LEVEL. - Throttles -
MAXIMUM THRUST.
EMERGENCY EVACUATION
1. ______________________________________
2. ______________________________________
3. ______________________________________
4. ______________________________________
5. ______________________________________
6. ______________________________________
- Parking Brake -
SET. - Throttles -
BOTH OFF. - LH/RH ENGINE FIRE Switchlights -
BOTH PRESS. - LH/RH Fire BOTTLE ARMED Switchlights -
BOTH PRESS (if fire suspected). - Passenger Advisory Lights -
PASS SAFETY. - BATT Switch -
OFF.
Maximum Design Ramp Weight - _____________
17.030 lbs.
Maximum Design Takeoff Weight - ___________
16,830 lbs.
Maximum Design Landing Weight - ___________
15,200 lbs.
Maximum Design Zero Fuel Weight - __________
12,850 lbs.
Normal oil pressure is ____ to ____ PSI at N2 speeds above 60%. Oil pressure below ____ PSI is undesirable and should be tolerated only for the completion of the flight, preferably at reduced power setting.
Normal oil pressure is 45 to 140 PSI at N2 speeds above 60%. Oil pressure below 45 PSI is undesirable and should be tolerated only for the completion of the flight, preferably at reduced power setting.
Max observed ITT ° C –
Takeoff _____,
Maximum Continuous _____ ,Starting/Transient ___________
Max observed ITT ° C – Takeoff 700.
Maximum Continuous - 700.
,Starting/Transient 740 (20 sec)
N2%
Takeoff _____,
Maximum Continuous _____,
Ground Idle _________,
Flight Idle _________,
Transient _____
N2%
Takeoff 100%.
Maximum Continuous 100%.
Ground Idle 49.1%.
Flight Idle 52.9%.
Transient 102%.
N1%
Takeoff _____.
Maximum Continuous _____.
Transient _____.
N1%
Takeoff 100%.
Maximum Continuous 100%.
Transient 102%.
Starter Limitation.
____ engine starts per ____ minutes.
____ cycles of operation with a ____ second rest period between cycles is permitted.
Starter Limitation.
3 engine starts per 30 minutes.
3 cycles of operation with a 90 second rest period between cycles is permitted.
Battery Limitation - ____ engine starts per hour.
Battery Limitation: Three engine starts per hour.
Use of an external power source with voltage in excess of ____ VDC or current in excess of ______ amps may damage the starter. Minimum_____ amps for start.
Use of an external power source with voltage in excess of 28 VDC or current in excess of 1000 amps may damage the starter. Minimum 800 amps for start.
Limit ground operation of pitot static heat to ___ minutes ON with ___ minutes OFF between cycles to preclude system damage.
Limit ground operation of pitot-static heat to 2 minutes ON with 2 minutes OFF between cycles to preclude system damage.
Electrical load is limited to____ amps per generator during ground operations at ground idle and _____ amps at high idle. Transients up to _____ amps are permissible for up to ___ minutes.
Electrical load is limited to 125 amps per generator during ground operations at ground idle and 225 amps at high idle. Transients up to 300 amps are permissible for up to 4
minutes.
Maximum Asymmetrical Fuel Differential for Normal Operations is ____ pounds.
200 lbs
Flight characteristics requirements were not demonstrated with unbalanced fuel above _____ pounds.
600
A lateral fuel imbalance of ______ pounds has been demonstrated for emergency return.
600
Maximum Operating Limit Speeds -
1. MMO (Above 28,907 feet) - ______________________
- VMO (Between 8000 – 28,907 feet) - _______________
- VMO (Below 8000 feet) - ________________________
Maximum Operating Limit Speeds -
1. MMO (Above 28,907 feet) - 0.755 Mach
- VMO (Between 8000 – 28,907 feet) - 292 KIAS
- VMO (Below 8000 feet) -
262 KIAS
Maximum Flap Extended Speed – VFE
Full Flaps – LAND Position (35°) - ____________
173 KIAS
Maximum Flap Extended Speed – VFE
Partial Flaps – T.O. (7°) and T.O. & APPR Position (15°) - ___________
200 KIAS
Maximum Landing Gear Extended Speed – VLE - ____________
250 KIAS
Maximum Landing Gear Operating Speed – VLO (Extending) - ____________
250 KIAS
Maximum Landing Gear Operating Speed – VLO (Retracting) - ____________
200 KIAS
Maximum Speed Brake Operation Speed – VSB - ______________
No Limit
MAX SPEED - Autopilot Operation - ____________________
292 KIAS or 0.755 Mach
Minimum Speed Sustained Flight in Icing Conditions (Except Takeoff, Approach and Landing) - ________
160 KIAS
Maximum Tailwind Components - ____________
10 KNOTS
Maximum Water/Slush on Runway - __________
0.5 inches
Takeoff with antiskid inoperative is ___________.
prohibited
The _________ must be in firm contact with the ground prior to deploying the ____________________.
The nosewheel must be in firm contact with the ground
prior to deploying thrust reversers.
The anti-ice switches must be selected ___________________ when operating in visible moisture, and the indicated RAT is _________________or below.
The anti-ice switches must be selected WING/ENGINE ON when operating in visible moisture, and the indicated RAT is +10C (+50F) or below.
Tail deice should be turned on when in ____________________, and the indicated RAT is between ________________________________________________ as applicable.
Tail deice should be turned on when in VISIBLE MOISTURE, and the indicated RAT is between +10 C (+50F) and -35C(-31F)/-40C(-40F).
Crew and passenger oxygen masks are not approved for use above __________ feet cabin altitude
40,000 cabin altitude
Prolonged operation of passenger masks above ________ feet cabin altitudes is not recommended.
25,000
Reverse thrust power must be reduced to the ______________ detent position at
_________ on landing roll.
Reverse thrust power must be reduced to the idle reverse detent position at 60 KIAS on landing roll.
Maximum allowable thrust reverser deployed time is ___ minutes in any ___ minute period.
Maximum allowable thrust reverser deployed time is 3 minutes in any 10-minute period.
Use of thrust reversers is __________ during touch and go landings.
The use of thrust reversers to back the airplane is prohibited.
FUEL BOOST Pumps - ___; when low fuel lights illuminate or
at ______ pounds or less indicated fuel.
FUEL BOOST Pumps - ON; when low fuel lights illuminate or
at 180 ± 20 pounds or less indicated fuel.
The thrust reversers must be checked on _________________ and the first flight after any _________________________ has been performed on the aircraft.
The thrust reversers must be checked on the first flight of the day and the first flight after any maintenance action has been performed on the aircraft.
