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Primary Flight School > Emergency Procedures/Limits > Flashcards

Emergency Procedures/Limits Flashcards

0
Q

Emergency Engine Shutdown on the Ground

A
  1. PCL-OFF
  2. FIREWALL SHUTOFF HANDLE-PULL
  3. EMERGENCY GROUNG EGRESS-AS REQUIRED
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1
Q

Abort Start Procedure

A
  1. PCL-OFF OR STARTER SWITCH-AUTO/RESET
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2
Q

EMERGENCY GROUND EGRESS

A
  1. ISS MODE SELECTOR-SOLO
  2. SEAT SAFETY PIN-INSTALL (BOTH)
  3. PARKING BRAKE-AS REQUIRED
  4. CANOPY-OPEN

IF CANOPY CANNOT BE OPENED OR SITUATION REQUIRES RIGHT SIDE EGRESS

  1. CFS HANDLE-ROTATE AND PULL ( BOTH)
  2. UPPER FITTINGS, LOWER FITTINGS AND LEG RESTRAINT GARTERS-RELEASE ( BOTH)
  3. BAT, GEN AND AUX BAT SWITCHES-OFF
  4. EVACUATE AIRCRAFT
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3
Q

Abort

A
  1. PCL-IDLE

2. BRAKES-AS REQUIRED

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4
Q

Engine Failure Immediately After Takeoff

Sufficient Runway Remaining Straight Ahead

A
  1. AIRSPEED-110 KNOTS (MINIMUM)
  2. PCL-AS REQUIRED
  3. EMER LDG GR HANDLE-PULL (AS REQUIRED)
  4. FLAPS-AS REQUIRED
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5
Q

Engine Failure During Flight

A
  1. ZOOM/GLIDE-125 KNOTS (MINIMUM)
  2. PCL-OFF
  3. INTERCEPT ELP
  4. AIRSTART-ATTEMPT IF WARRENTED

IF CONDITIONS DO NOT WARRENT AN AIRSTART

  1. FIREWALL SHUTOFF HANDLE-PULL
  2. EXECUTE FORCED LANDING OR EJECT
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6
Q

Immediate Airstart (PMU NORM)

A
  1. PCL-OFF
  2. STARTER SWITCH-AUTO/RESET
  3. PCL-IDLE, ABOVE 13% N1
  4. ENGINE INSTRUMENTS-MONITOR ITT, N1, AND OIL PRESSURE

IF AIRSTART IS UNSUCCESSFUL

  1. PCL-OFF
  2. FIREWALL SHUTOFF HANDLE-PULL
  3. EXECUTE FORCED LANDING OR EJECT

IF AIR START IS SUCCESSFUL

  1. PCL-AS REQUIRED AFTER N1 REACHES IDLE RPM (APPROXIMATELY 67% N1)
  2. PEL-EXECUTE
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7
Q

Uncommanded Power Changes/
Loss of Power/
Uncommanded Propeller Feather

A
  1. PCL-OFF
  2. PMU SWITCH-OFF
  3. PROP SYS CIRCUIT BREAKER (Left Front Console) -Pull, IF NP STABLE BELOW 40%
  4. PCL-AS REQUIRED

IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT:

  1. PEL-EXECUTE

IF POWER IS INSUFFICIENT TO COMPLETE PEL

  1. PROP SYS CIRCUIT BREAKER-RESET, AS REQUIRED
  2. PCL-OFF
  3. FIREWALL SHUTOFF HANDLE-PULL
  4. EXECUTE FORCED LANDING OR EJECT
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8
Q

Compressor Stalls

A
  1. PCL-SLOWLY RETARD BELOW STALL THRESHOLD
  2. DEFOG-ON
  3. PCL-SLOWLY ADVANCE (AS REQUIRED)

IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT

  1. PEL-EXECUTE

IF POWER IS INSUFFICIENT TO COMPLETE PEL

  1. PCL-OFF
  2. FIREWALL SHUTOFF HANDLE-PULL
  3. EXECUTE FORCED LANDING OR EJECT
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9
Q

Inadvertent Departure from Controlled Flight

A
  1. PCL-IDLE
  2. CONTROLS-NEUTRAL
  3. ALTITUDE-CHECK
  4. RECOVER FROM UNUSUAL ATTITUDE
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10
Q

Fire in Flight

A

IF FIRE IS CONFIRMED

  1. PCL-OFF
  2. FIREWALL SHUTOFF HANDLE-PULL

IF FIRE IS EXTINGUISHED

  1. FORCED LANDING-EXECUTE

IF FIRE IS NOT EXTINGUISHED

  1. EJECT (BOTH)

IF FIRE IS NOT CONFIRMED

  1. PEL-EXECUTE
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11
Q

Chip Detector Warning

A
  1. PCL-MINIMUM NECESSARY TO INTERCEPT ELP; AVOID UNNECESSARY PCL MOVEMENTS
  2. PEL-EXECUTE
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12
Q

Oil System Malfunction or Low Oil Pressure

A

IF ONLY AMBER OIL PX CAUTION ILLUMINATES

  1. TERMINATE MANEUVER
  2. CHECK OIL PRESSURE; IF PRESSURE IS NORMAL, CONTINUE OPERATIONS

IF RED OIL PX ILLUMINATES AND/OR AMBER OIL PX CAUTION REMAINS ILLUMINATED FOR 5 SECONDS:

  1. PCL-MINIMUM NECESSARY TO INTERCEPT ELP; AVOID UNNECESSARY PCL MOVEMENTS
  2. PEL-EXECUTE
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13
Q

Low Fuel Pressure

A
  1. PEL-EXECUTE
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14
Q

OBOGS System Malfunction

A
  1. PCL-ADVANCE
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15
Q

OBOGS INOPERATIVE

A
  1. GREEN RING-PULL (AS REQUIRED)
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16
Q

EJECT

A
  1. EJECTION HANDLE- PULL (BOTH)
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17
Q

Forced Landing

A
  1. AIRSPEED-125 KNOTS PRIOR TO EXTENDING EMERGENCY LANDING GEAR
  2. EMERGENCY LDG GR HANDLE-PULL ( AS REQUIRED)
  3. AIRSPEED-120 KIAS MINIMUM UNTIL INTERCEPTING FINAL; 110 KIAS MINIMUM ON FINAL
  4. FLAPS-AS REQUIRED
18
Q

Precautionary Emergency Landing

A
  1. TURN TO NEAREST SUITABLE FIELD
  2. CLIMB OR ACCELERATE TO INTERCEPT ELP
  3. GEAR, FLAPS, SPEED BREAK-UP
19
Q

Takeoff/Max

A 
Torque                100%
ITT Max               820
N1                       104%
NP (2)                  100%
Oil Pressure (6)    90 to 120psi 
Oil Temp              10 to 105
20
Q

Idle

A 
Torque (9)            3-8% 
ITT Max               750
N1                       60-61% Ground
                            67% Flight
NP                       46-50% Ground
Oil Pressure        90 psi min
Oil Temp             -40-105 Ground
                           10-105 Flight
                           106-110 (7)
21
Q

Start

A

ITT Max 1000 for 5 sec
Oil PX. 200 psi max
Oil Temp -40 min

22
Q

Transient

A 
Torque (8)            131%for 20 sec
ITT Max               870 for 20 sec
N1                       104%
NP                       102% for 20 sec
                            110% (3)
Oil Pressure (5)    40-130psi 
Oil Temp              106-110 for 10 minutes
23
Q

(1)

A

N1 values presented for PMU ON. With PMU OFF, N1 may vary from these values

24
Q

(2)

A

With PMU OFF, permissible maximum NP is 100+/-2%

25
Q

(3)

A

Permissible at all powers for completion of flight in emergency

26
Q

(4)

A

Avoid stabilized ground operations from 62-80% NP

27
Q

(5)

A

Operations in this range permitted only during aerobatics or spins, and 15-40 psi for 5 seconds with PCL at IDLE.

28
Q

(6)

A

Normal oil pressure during stead state conditions is 90-120 psi. Operation at oil pressure less than 90 psi at flight idle or adove is indicative of oil system malfunction.

29
Q

(7)

A

Acceptable for ground operations at or below 20% torque.

30
Q

(8)

A

Torque at 131% is a materials limit above which damage to the engine may occur. Torque above 102% is indicative of a system malfunction.

31
Q

(9)

A

Allowable torque range with NP stabilized and PCL at IDLE

32
Q

Starter Cycle Limits

A

20 sec cycles

1st 30 sec
2nd 2 min
3rd 5 min
4th 30 min

33
Q

Flight Maneuver Limits

A

Inverted Flight 15 sec

Zero G Flight. 5 sec

34
Q

Acceleration Limits

A

Symmetric Clean +7 to -3.5
Symmetric Gear & Flaps +2.5 to 0
Asymmetric Clean +4.7 to -1.0
Asymmetric Gear &Flaps +2 to 0

For uncoordinated rolling maneuvers initiated at -1G, the max AOB is 180 degrees.

35
Q

Other Limitations

A

MIN VOLTAGE FOR BAT START 23.5 volts
MAX CX FOR DRY RWY 25 knots
MAX CX FOR WET RWY 10 knots
MAX CX FOR ICY RWY 5 knots
MAX TW COMPONENT FOR TAKEOFF 10 knots

36
Q

Airspeed Limits

A

VLE & VFE 150
VMO 316
MMO .67
PENETRATION AIRSPEED 207

37
Q

Prohibited Maneuvers

A 
Inverted stalls
Inverted spins
Spins with PCL above idle
Spin with LDG GR, Flaps or Speed Break extended
Spins with the PMU OFF
Aggravated spins past two turns
Spins below 10000 feet pressure altitude
Spins above 22000 feet pressure altitude
Abrupt Cross-Controlled (Snap) Maneuvers
Aerobatic maneuvers, spins, or stalls with a fuel imbalance greater than 50 pound between wings
Tailslides
38
Q

The aircraft has been approved only for transit through _____ feet of ______ ice.

A

5000ft of Rime Ice

39
Q

Mini Battery Voltage

A

22 volts

40
Q

Hydraulic Caution

A

3500 psi

41
Q

Fuel Caution Light

A

< 110 pounds in respective tank

42
Q

Cockpit Pressurization schedule Limits:

A

3.6+/-0.2 psi

Primary Flight School (5 decks)

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