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69 Cards in this Set

  • Front
  • Back
ABORT START PROCEDURE
1. PCL - OFF; or STARTER SWITCH - AUTO/RESET
EMERGENCY ENGINE SHUTDOWN ON THE GROUND
1. PCL - OFF
2. FIREWALL SHUTOFF HANDLE - PULL
3. EMERGENCY GROUND EGRESS - AS REQUIRED
EMERGENCY GROUND EGRESS
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:
5. CFS HANDLE - ROTATE AND PULL (BOTH)
6. SHOULDER STRAPS, LAP BELT, SSK FITTINGS, AND LEG GARTERS - RELEASE (BOTH)
7. BAT, GEN, AND AUX BATT SWITCHES - OFF
8. EVACUATE AIRCRAFT
ABORT
1. PCL - IDLE
2. BRAKES - AS REQUIRED
ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF
(SUFFICIENT RUNWAY REMAINING STRAIGHT AHEAD)
1. AIRSPEED - 110 KNOTS (MINIMUM)
2. PCL - AS REQUIRED
3. EMER LDG GR HANDLE - PULL (AS REQUIRED)
4. FLAPS - AS REQUIRED
ENGINE FAILURE DURING FLIGHT
1. ZOOM/GLIDE - 125 KNOTS (MINIMUM)
2. PCL - OFF
3. INTERCEPT ELP
4. AIRSTART - ATTEMP IF WARRANTED
- IF CONDITIONS DO NOT WARRANT AN AIRSTART:
5. FIREWALL SHUTOFF HANDLE - PULL
6. EXECUTE FORCED LANDING OR EJECT
IMMEDIATE AIRSTART (PMU NORM)
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:
5. PCL - OFF
6. FIREWALL SHUTOFF HANDLE - PULL
7. EXECUTE FORCED LANDING OR EJECT
- IF AIRSTART IS SUCCESSFUL:
8. PCL - AS REQUIRED AFTER N1 REACHES IDLE RPM (APPROXIMATELY 67% N1)
9. PEL - EXECUTE
UNCOMMANDED POWER CHANGES / LOSS OF POWER / UNCOMMANDED PROPELLER FEATHER
1. PCL - MID RANGE
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:
5. PEL - EXECUTE
- IF POWER IS INSUFFICIENT TO COMPLETE PEL:
6. PROP SYS CIRCUIT BREAKER - RESET, AS REQUIRED
7. PCL -OFF
8. FIREWALL SHUTOFF HANDLE - PULL
9. EXECUTE FORCED LANDING OR EJECT
Compressor Stalls
1. PCL - SLOWLY RETARD BELOW STALL THRESHOLD
2. DEFOG SWITCH - ON
3. PCL - SLOWLY ADVANCE (AS REQUIRED)
- IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT:
4. PEL - EXECUTE
IF POWER IS INSUFFICIENT TO COMPLETE PEL:
5. PCL - OFF
6. FIREWALL SHUTOFF HANDLE - PULL
7. EXECUTE FORCED LANDING OR EJECT
Inadvertant Depature from Controlled Flight
1. PCL - IDLE
2. CONTROLS - NEUTRAL
3. ALTITUDE - CHECK
4. RECOVER FROM UNUSUAL ATTITUDE
Fire in Flight (Fire Annunciator Illuminated)
- IF FIRE IS CONFIRMED:
1. PCL - OFF
2. FIREWALL SHUTOFF HANDLE - PULL
- IF FIRE IS EXTINGUISHED:
3. FORCED LANDING - EXECUTE
- IF FIRE DOES NOT EXTINGUISH OR FORCED LANDING IS IMPRACTICAL:
4. EJECT (BOTH)
- IF FIRE IS NOT CONFIRMED:
5. PEL - EXECUTE
Chip Detector Warning
1. PCL - MINIMUM NECESSARY TO INTERCEPT ELP; AVOID UNNECESSARY PCL MOVEMENTS
2. PEL - EXECUTE
Oil System Malfunction or Low Oil Pressure
- IF ONLY AMBER OIL PX ANNUNCIATOR ILLUMINATES:
1. TERMINATE MANEUVER
2. CHECK OIL PRESSURE; IF OIL PRESSURE IS NORMAL, CONTINUE OPERATIONS
- IF RED OIL PX ANNUNCIATOR ILLUMINATES AND/OR AMBER OIL PX ANNUNCIATOR REMAINS ILLUMINATE FOR 5 SECONDS:
3. PCL - MINIMUN NECESSARY TO INTERCEPT ELP; AVOID UNNECESSARY PCL MOVEMENTS
5. PEL - EXECUTE
Low Fuel Pressure
1. PEL - EXECUTE
OBOGS System Malfunction
1. PCL - ADVANCE
OBOGS Inoperative (OBOGS Fail Annunciator Illuminated)
1. GREEN RING - PULL (AS REQUIRED)
Eject
1. EJECTION HANDLE - PULL (BOTH)
Forced Landing
1. AIRSPEED - 125 KIAS PRIOR TO EXTENDING LANDING GEAR
2. EMER LDG GR HANDLE - PULL (AS REQUIRED)
3. AIRSPEED - 120 KIAS MINIMUM UNTIL INTERCEPTING FINAL; 110 KIAS MINIMUM ON FINAL
4. FLAPS - AS REQUIRED
Precautionary Emergency Landing
1. TURN TO NEAREST SUITABLE FIELD
2. CLIMB OR ACCELERATE TO INTERCEPT ELP
3. GEAR, FLAPS, SPEED BRAKE - UP
% TORQUE
TAKEOFF/MAX
100
ITT
TAKEOFF/MAX
820
% N1
TAKEOFF/MAX
104
% Np
TAKEOFF/MAX
100
Note 2: WITH PMU OFF, PERMISSIBLE MAX Np IS 100 +/- 2%
OIL PRESSURE
TAKEOFF/MAX
90 to 120 psi
Note 6: NORMAL OIL PRESSURE DURING STEADY STATE CONDITIONS IS 90-120 psi. OPERATION AT OIL PRESSURE LESS THAN 90 psi IS INDICATIVE OF OIL SYSTEM MALFUNCTION.
OIL TEMP - TAKEOFF/MAX
10 to 105 deg C
ITT
IDLE
750 deg C
% N1
IDLE
60 to 61 (ground)
67 Min (flight)
OIL PRESSURE
IDLE
90 psi (min)
OIL TEMP
IDLE
-40 to 105 deg C (Grnd)
10 to 105 (Flt)
106 to 110 Note 7: ACCEPTABLE FOR GROUND OPERATIONS AT AND BELOW 20% TORQUE.
ITT
START
1000 deg C (5 sec)
OIL PRESSURE
START
200 psi (max)
OIL TEMP
START
-40 (min) deg C
% TORQUE
TRANSIENT
131 (20 sec)
Note 8: Torque at 131% is a materials limit above which damage to the engine may occur. Torque above 102% is indicative of a system malfunction.
ITT (deg C)
TRANSIENT
870 (20 sec)
% N1
TRANSIENT
104
% Np
TRANSIENT
102 (20 sec)
110 Note 3: PERMISSIBLE AT ALL POWERS [SETTINGS] FOR COMPLETION OF FLIGHT IN EMERGENCY.
OIL PRESSURE (psi)
TRANSIENT
40 to 130 psi
Note 5: OPERATION IN THIS RANGE PERMITTED ONLY DURING AEROBATICS OR SPINS. (15-40) psi (5 sec) WITH PCL AT IDLE.
OIL TEMP (deg C)
TRANSIENT
106 to 110
(10 minutes)
MAXIMUM AIRSPEED GEAR DOWN (VLE) AND FLAP DOWN (VFE) ____ KIAS
150
MAX OPERATING (Vmo) ___ KIAS / MAX MACH (Mmo) ___ MACH
316
0.67
TURBULENT AIR (Vg) ___ KIAS
195
MAX OPERATING MANEUVERING (Vo) ____KIAS
MAX WITH FULL RUDDER DEFLECTION ____KIAS
227
150
Prohibited Maneuvers 1 thru 4
1. INVERTED STALLS
2. INVERTED SPINS
3. SPINS WITH THE PCL ABOVE IDLE
4. SPINS WITH THE LANDING GEAR, FLAPS, OR SPEEDBRAKE EXTENDED
Prohibited Maneuvers 5 thru 8
5. SPINS WITH THE PMU OFF
6. AGGRAVATED SPINS PAST TWO TURNS
7. SPINS BELOW 10,000 FEET PRESSURE ALTITUDE
8. SPINS ABOVE 22,000 FEET PRESSURE ALTITUDE
Prohibited Maneuvers 9 thru 11
9. ABRUPT CROSS-CONTROLLED (SNAP) MANEUVERS
10. AEROBATIC MANEUVERS, SPINS, OR STALLS WITH A FUEL IMBALANCE GTEATER THAN 50 POUNDS BETWEEN WINGS
11. TAIL SLIDES
THE AIRCRAFT HAS BEEN APPROVED ONLY FOR TRANSIT THROUGH ______ FEET OF ____________ ICE
5000
LIGHT RIME
MINIMUM BATTERY VOLTAGE
22.0
HYDRAULIC CAUTION: < ______ PSI, > ______ PSI
1800
3500
FUEL CAUTION LIGHT: < ________ POUNDS IN RESPECTIVE WING TANK
110
COCKPIT PRESSURIZATION SCHEDULE LIMIT: _____ +/- _____ PSI
3.6 +/- 0.2
STARTER CYCLE LIMITATIONS
STARTER DUTY CYCLE IS LIMITED TO FOUR ___ CYCLES
20 SEC
STARTER CYCLE LIMITATIONS
COOLING PERIOD AFTER FIRST STARTER CYCLE
30 SEC
STARTER CYCLE LIMITATIONS
COOLING PERIOD AFTER SECOND STARTER CYCLE
2 MIN
STARTER CYCLE LIMITATIONS
COOLING PERIOD AFTER THIRD STARTER CYCLE
5 MIN
STARTER CYCLE LIMITATIONS
COOLING PERIOD AFTER FOURTH STARTER CYCLE
30 MIN
FLIGHT MANEUVERING LIMITATIONS

INVERTED FLIGHT ___ SEC
15 SEC
FLIGHT MANEUVERING LIMITATIONS

INTENTIONAL ZERO G FLIGHT ___ SEC
5 SEC
ACCELERATION LIMITATIONS
SYMMETRIC CLEAN
+7.0 TO -3.5 Gs
ACCELERATION LIMITATIONS
SYMMETRIC GEAR & FLAPS EXTENDED
+2.5 TO 0.0 Gs
ACCELERATION LIMITATIONS
ASYMMETRIC CLEAN
+4.7 TO -1.0 Gs
ACCELERATION LIMITATIONS
ASYMMETRIC GEAR & FLAPS EXTENDED
+2.0 TO 0.0 Gs
FOR UNCOORDINATED ROLLING MANEUVERS INITIATED AT -___ G, THE MAXIMUM BANK ANGLE CHANGE IS ___ DEGREES
1
180
MIN VOLTAGE FOR BATTERY START
23.5 VOLTS
NORMAL VOLTAGE RANGE
22.0 TO 29.5 VOLTS
MAX CROSSWIND FOR DRY RUNWAY
25 KNOTS
MAX CROSSWIND FOR WET RUNWAY
10 KNOTS
SOP LIMIT CROSSWIND, LANDING DRY RUNWAY
20 KNOTS
MAX CROSSWIND FOR ICY RUNWAY
5 KNOTS
MAX TAILWIND COMPONENT FOR TAKEOFF
10 KNOT