Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
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
|