Term
|
Definition
|
|
Term
| NP at approximately 30% torque during overspeed gov check |
|
Definition
|
|
Term
| NP limit with PMU off during overspeed gov check |
|
Definition
|
|
Term
|
Definition
|
|
Term
| setting to check engine instruments for T/O check |
|
Definition
|
|
Term
| degrees nose up for rotation |
|
Definition
|
|
Term
|
Definition
| ½ gust factor (up to 10 knots) |
|
|
Term
| climbout speed (160-180 KIAS for better forward visibility in climb) |
|
Definition
|
|
Term
|
Definition
|
|
Term
| pitch and speed for obstacle clearance climb |
|
Definition
| 15 degrees nose high and 140 KIAS |
|
|
Term
|
Definition
|
|
Term
| increase in ITT w/defog on at any PCL setting |
|
Definition
|
|
Term
| ITT limit as controlled by PMU |
|
Definition
|
|
Term
| required pressure differential above 18,000 feet MSL |
|
Definition
|
|
Term
| max fuel imbalance for pre-stall, spinning and aerobatic checks |
|
Definition
|
|
Term
| recommended holding speed |
|
Definition
|
|
Term
| penetration descent parameters |
|
Definition
| 2000–4000 fpm and 200-250 KIAS |
|
|
Term
| gusty wind threshold and touchdown speeds |
|
Definition
| ½ gust factor (up to 10 knots) |
|
|
Term
| subtract from normal approach speed for normal touchdown speed |
|
Definition
|
|
Term
| braking above to be done with great caution |
|
Definition
|
|
Term
| check oil within after landing to be max hot |
|
Definition
|
|
Term
| max slope approved for fueling |
|
Definition
|
|
Term
| time limit for LH and RH single point refueling precheck valves to shut |
|
Definition
|
|
Term
|
Definition
| 28-28.5 VDC /1000 amps for 5 sec/500 amps for 2 min/300 amps continuous |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| wind speed to consider hangaring A/C |
|
Definition
|
|
Term
| max nose wheel deflection while towing |
|
Definition
|
|
Term
|
Definition
|
|
Term
| time for ITT to start rising after fuel flow indication during start |
|
Definition
|
|
Term
| N1 with engine flameout (speeds below 8% not indicated) |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| consider rapid descent above this altitude if using emer O2 to prevent depletion |
|
Definition
|
|
Term
| glide rotates N1 below 8% (indicate 0%) if engine flamed out (oil px = 0 psi) |
|
Definition
|
|
Term
| airstart not recommended below |
|
Definition
|
|
Term
| airstarts are demonstrated below |
|
Definition
|
|
Term
| altitude lost during airstart procedure (at 125 KIAS glide) |
|
Definition
|
|
Term
| time to complete airstart sequence |
|
Definition
|
|
Term
| airstart envelope (above 15,000 feet MSL) |
|
Definition
|
|
Term
| airstart envelope (at or below 15,000 feet MSL) |
|
Definition
|
|
Term
| time for prop to unfeather after N1 reaches approximately 45% |
|
Definition
|
|
Term
| PCL to idle for PMU off airstart (look for ITT rise w/in 10 seconds or abort) |
|
Definition
|
|
Term
| initial fuel flow during airstart |
|
Definition
|
|
Term
| amp reading after airstart |
|
Definition
|
|
Term
| time for starter to drain battery if generator is left in manual |
|
Definition
|
|
Term
| time for prop to come out of feather after prop sys CB is pulled |
|
Definition
|
|
Term
| minimum altitude uncontrolled ejection |
|
Definition
|
|
Term
| 135 KIAS and AOA 18+ indicate a steady state spin |
|
Definition
|
|
Term
| time standby attitude indicator will provide accurate info after loss of power |
|
Definition
|
|
Term
| time aux battery provides stby instruments/lighting, fire 1 and standby UHF |
|
Definition
|
|
Term
| torque max with CHIP or OIL PX lights illuminated |
|
Definition
|
|
Term
| normal sustained oil pressure limits |
|
Definition
|
|
Term
| time battery will last with bus tie open |
|
Definition
|
|
Term
| generator is considered inoperative |
|
Definition
| 25 volts and ammeter discharging |
|
|
Term
| reading if battery bus fails |
|
Definition
|
|
Term
| engine feed fuel pressure below causes boost pump to automatically engage |
|
Definition
|
|
Term
| max engine time with high pressure fuel pump suction feeding |
|
Definition
|
|
Term
| auto fuel balancing keeps fuel balance within |
|
Definition
|
|
Term
| fuel imbalance for two minutes triggers FUEL BAL light (fault in auto system) |
|
Definition
|
|
Term
| level of fuel that triggers L or R FUEL LO annunciator |
|
Definition
|
|
Term
| EHYD PX LO light illuminates below |
|
Definition
|
|
Term
| HYDR FL LO light illuminates below |
|
Definition
|
|
Term
| hydraulic pressure w/in green arc |
|
Definition
|
|
Term
| minimum altitude for controllability check |
|
Definition
|
|
Term
| minimum speed during controllability check (or stick shaker or max deflection) |
|
Definition
|
|
Term
| add to minimum controllable speed on final with structural damage |
|
Definition
|
|
Term
| touchdowns in landing configuration have been accomplished up to this |
|
Definition
|
|
Term
| – touchdowns above this cause increased directional sensitivity & longer landing |
|
Definition
|
|
Term
| in environmental systems or defog duct triggers the DUCT TEMP light |
|
Definition
|
|
Term
| descend below with environmental system/pressurization failure |
|
Definition
|
|
Term
| speed to attain with runaway trim |
|
Definition
|
|
Term
| stick pressure at approach speed with elevator trim failure at high speed cruise |
|
Definition
|
|
Term
| stick pressure at approach speed with aileron trim failure at high speed cruise |
|
Definition
|
|
Term
| stick pressure at approach speed with rudder trim failure at high speed cruise |
|
Definition
|
|
Term
| – max speed with canopy shattered/damaged/gone or CANOPY light on |
|
Definition
|
|
Term
| – CKPT PX light illuminates with this pressure differential |
|
Definition
|
|
Term
| – cabin alt triggers CKPT ALT annunciator |
|
Definition
|
|
Term
| decompression above may trigger OBOGS light due to mode compensation |
|
Definition
|
|
Term
| – recommended minimum ejection altitude (controlled) |
|
Definition
|
|
Term
| recommended minimum ejection altitude (uncontrolled) |
|
Definition
|
|
Term
| Use MOR handle to deploy parachute & separate from seat in mtns. |
|
Definition
|
|
Term
| speed range for controlled ejection |
|
Definition
|
|
Term
Ejection seat time to full chute
(based on ISS BOTH, 271 pound pilots, 250 KIAS) |
|
Definition
| 4.37 sec (FRONT)/4.00 sec (REAR) |
|
|
Term
| min altitude/airspeed for successful ejection with up to a 10,000 fpm sink rate |
|
Definition
|
|
Term
| min ejection altitude with 90 degree dive and 250 KIAS |
|
Definition
|
|
Term
| min ejection altitude inverted (level flight) with 250 KIAS |
|
Definition
|
|
Term
| additional terrain clearance to above numbers for each 1000 ft MSL of altitude |
|
Definition
|
|
Term
| – ejection seat chart not accurate above |
|
Definition
|
|
Term
|
Definition
|
|
Term
| min speed until intercepting final on ELP |
|
Definition
|
|
Term
| min speed on final during ELP |
|
Definition
|
|
Term
| ditch into the wind instead of parallel the swells |
|
Definition
|
|
Term
| – add to high, low, and base key with engine in idle due to no feathering |
|
Definition
|
|
Term
| max descent rate for 125 KIAS glide, 4-6% torque, clean. |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| – torque to set for ELP, PEL, or to simulate zero thrust |
|
Definition
|
|
Term
| – minimum fuel to burn down to for landing with gear malfunction |
|
Definition
|
|
Term
| set PCL to fuel flow indication (expect 70-80 pph) for PMU off ground start |
|
Definition
|
|
Term
| – if no rise in ITT, place PCL off and abort start |
|
Definition
| 10 seconds after fuel flow indications |
|
|
Term
| approximate idle for PMU off ground start |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| red oil px annunciator with pcl above idle |
|
Definition
|
|
Term
| red oil px with pcl at idle |
|
Definition
|
|
Term
| amber oil px annunciator at idle |
|
Definition
|
|
Term
|
Definition
|
|
Term
| amber and red oil px at idle |
|
Definition
|
|
Term
| after shutdown, check oil for best results |
|
Definition
|
|
Term
| turbine output shaft speed |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| pmu managed minimum above 10k |
|
Definition
|
|
Term
| pmu off overspeed governor Np range |
|
Definition
|
|
Term
| ignition and boost pump deactivated during auto start |
|
Definition
|
|
Term
| fuel pressure switch limit, turns on boost pump |
|
Definition
|
|
Term
| manual motor after aborted at start |
|
Definition
|
|
Term
| normal wing tank capacity |
|
Definition
|
|
Term
|
Definition
|
|
Term
| full fuel load- single point refueling |
|
Definition
|
|
Term
| over wing refueled full fuel load |
|
Definition
|
|
Term
| imbalance where FUEL BAL annunciator illuminated (2 min) |
|
Definition
|
|
Term
| fuel probes: 3 in each wing, 1 collector tank |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| collector tank pressurized by transfer jet pumps |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| min voltage to charge battery |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| hydraulic system total capacity |
|
Definition
|
|
Term
| hydraulic reservoir capacity |
|
Definition
|
|
Term
| min hydraulic pressure necessary to operate nw steering, gear, Flaps, speed brake |
|
Definition
|
|
Term
| fuel pressure supplied by engine driven low pressure fuel pump |
|
Definition
|
|
Term
| fuel pressure supplied by engine driven high pressure fuel pump |
|
Definition
|
|
Term
| max hydraulic volume allowed past hydraulic fuse |
|
Definition
|
|
Term
| hydraulic pressure relief valve opens |
|
Definition
|
|
Term
| EHYD PX LO annunciator illuminates |
|
Definition
|
|
Term
|
Definition
|
|
Term
| normal gear extension/retraction time |
|
Definition
|
|
Term
| gear warning horn sounds if airspeed if airspeed below 120 |
|
Definition
|
|
Term
|
Definition
|
|
Term
| flap deflection in landing |
|
Definition
|
|
Term
| speed brake deflection when deployed |
|
Definition
|
|
Term
| TAD active with no weight on wheels |
|
Definition
|
|
Term
| below this number mach is blank |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| optimum approach speed decrease rate |
|
Definition
|
|
Term
| optimum max range AOA altitude |
|
Definition
|
|
Term
|
Definition
| 5-10 kts before stall, 15.5 units |
|
|
Term
|
Definition
|
|
Term
| automatic seat man separation |
|
Definition
|
|
Term
| IAS both rear ejection delay |
|
Definition
|
|
Term
| bleed air inflow prevented with ac clutch engaged |
|
Definition
|
|
Term
| automatically maintained until 18,069 msl |
|
Definition
| 8000' cockpit pressure altitude |
|
|
Term
|
Definition
|
|
Term
| CKPT PX annunciatorannunciator |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| AUX BAT test light will not illuminate |
|
Definition
|
|
Term
|
Definition
|
|
Term
| normal O2 concentration, sea level-15k feet |
|
Definition
|
|
Term
| normal O2 concentration, 15-31 k feet |
|
Definition
|
|
Term
|
Definition
|
|
Term
| OBOGS warm up time after engine start |
|
Definition
|
|
Term
| OBOGS fail annunciator extinguishes during BIT test |
|
Definition
|
|
Term
| baggage compartment weight limit |
|
Definition
|
|
Term
|
Definition
|
|
Term
| external power requirements |
|
Definition
| 28-28.5 V, 1000-1500 amps |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| thrust available at sea level |
|
Definition
|
|
Term
| 100% torque available up to this altititude |
|
Definition
|
|
Term
| torque produced at prop shaft |
|
Definition
|
|
Term
| emergency o2 bottle min at 70f |
|
Definition
|
|
Term
| sufficient battery voltage for start |
|
Definition
|
|
Term
| mminimum main gear strut extension |
|
Definition
|
|
Term
| minimum nose gear strut extension |
|
Definition
|
|
Term
| delay between ejections with ISS both |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| use HIGH IOAT start procedure |
|
Definition
|
|
Term
| time for STARTER switch manual to cool IOAT or residual fuel |
|
Definition
|
|
Term
|
Definition
|
|
Term
| prohibited range stable prop speed on ground |
|
Definition
|
|
Term
| idle with PMU off during overspeed gov checklist |
|
Definition
|
|
Term
Placing PCL in idle before during manual start may cause eng damage/overtemp |
|
Definition
|
|
Term
| FUEL PX light illuminates |
|
Definition
|
|
Term
|
Definition
| <40 psi above idle or 15 psi at idle |
|
|
Term
| OBOGS TEMP light illuminates |
|
Definition
|
|
Term
fuel level which triggers L/R FUEL LO |
|
Definition
| 110 lbs or 16 gallons (respective tank) |
|
|
Term
| MAINT FDR light illuminates |
|
Definition
|
|
Term
| Maximum allowable airspeed |
|
Definition
|
|
Term
|
Definition
|
|
Term
| Maximum torque transient for 20 seconds |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
Max ITT for start (5 seconds) |
|
Definition
|
|
Term
Max transient ITT (20 seconds) |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
Normal oil pressure range |
|
Definition
|
|
Term
Max oil pressure during start |
|
Definition
|
|
Term
| Transient oil pressure range, aerobatics and spins only |
|
Definition
|
|
Term
| Minimum oil pressure, at t idle, aerobatics and spins only (5 seconds max) |
|
Definition
|
|
Term
Normal oil temperature range |
|
Definition
|
|
Term
Min oil temperature for start |
|
Definition
|
|
Term
Acceptable oil temperature, transient power, 10 minutes max |
|
Definition
|
|
Term
| Normal hydraulic pressure |
|
Definition
|
|
Term
|
Definition
|
|
Term
cooling period before second start attempt |
|
Definition
|
|
Term
| cooling period before third start attempt |
|
Definition
|
|
Term
cooling period before fourth start attempt |
|
Definition
|
|
Term
| cooling period before fifth start attempt |
|
Definition
|
|
Term
| gear/flap extension limit |
|
Definition
|
|
Term
| Max turbulence penetration A/S (both mentioned) |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| Symmetric, gear/flaps extended |
|
Definition
|
|
Term
|
Definition
|
|
Term
Asymmetric, gear/flaps extended |
|
Definition
|
|
Term
Spins prohibited at altitudes of |
|
Definition
>22,000’ MSL , <10,000’ MSL
|
|
|
Term
|
Definition
1) Rear pilot exceeds 260 lbs, 2) Combined crew weight exceeds 500 lbs,
3) Fuel exceeds 1100 lbs, 4) Baggage compartment is used |
|
|
Term
|
Definition
|
|
Term
Max takeoff/landing weight |
|
Definition
|
|
Term
|
Definition
|
|
Term
Max descent rate at touchdown |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| High pressure fuel pump only limit |
|
Definition
|
|
Term
| Ground ops temperature limits |
|
Definition
| -23° C (-9.4° F) to +43° C (109.4° F) |
|
|
Term
| Apply equipment cooling chart |
|
Definition
|
|
Term
Pressurization Safety valve opens |
|
Definition
|
|
Term
|
Definition
|
|
Term
| Min / Max Pilot weight (Nude) for ejection seat |
|
Definition
|
|
Term
Min / Max Pilot weight (with equipment) for ejection seat |
|
Definition
|
|
Term
Ejection above this speed will increase injury due to drogue shot opening shock |
|
Definition
|
|
Term
utilize half lateral stick inputs or less performing sustained elevated G rolls |
|
Definition
|
|
Term
|
Definition
|
|
Term
sink rate at best glide, clean |
|
Definition
|
|
Term
best glide, gear down, flaps/SB up
|
|
Definition
|
|
Term
sink rate at best glide w/gear down |
|
Definition
|
|
Term
| zero thrust power setting |
|
Definition
|
|
Term
full right rudder and full right aileron may not prevent a left roll off at stall |
|
Definition
|
|
Term
altitude loss during six turn, steady-state spin |
|
Definition
|
|
Term
| nose high pitch for best spin entry |
|
Definition
|
|
Term
| per turn, stabilized spin |
|
Definition
| 2 - 3 seconds, 400’ to 500’, 120 KIAS, 18 AOA |
|
|
Term
|
Definition
| 70° nose down, 280°/second turn |
|
|
Term
|
Definition
| 500’/turn, 1500’ to 200’ dive recovery |
|
|
Term
spin entry may result in low oil pressure and engine damage |
|
Definition
|
|
Term
| Accelerated stalls sustained can produce damaging loads fuselage/emenage |
|
Definition
|
|
Term
| Max bank angle change for uncoordinated maneuvers at -1g |
|
Definition
|
|
Term
Above stall, natural stall warning occurs during power on stalls |
|
Definition
|
|
Term
| oil pressure may drop this low during a spin |
|
Definition
|
|
Term
| Recommended turbulence/t-storm penetration airspeed |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
Approach/landing speed with ice accumulation on aircraft |
|
Definition
|
|
Term
Operations in visible moisture should be avoided |
|
Definition
|
|
Term
|
Definition
| <0.1 inch of slush or water, MPH ¸ 1.15 = Knots |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
Power-up of the digital instruments may shorten instrument service life |
|
Definition
|
|
Term
Remove battery, preheat engine prior to start |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| Maximum brake energy absorption capability |
|
Definition
|
|
Term
Max abort speed reaction time |
|
Definition
| 6 seconds (3 sec decision/3 sec application) |
|
|
Term
| Airspeed increase during 6 second reaction at max abort speed |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| Takeoff speed in gusty winds |
|
Definition
| T/O speed + 50% of gust (max of 10) |
|
|
Term
| Charted performance climb speed |
|
Definition
|
|
Term
| Climb above this altitude may not be possible except clean configurations 250 |
|
Definition
|
|
Term
| Penetration descent, idle power, clean |
|
Definition
|
|
Term
Rapid descent, idle power, speed brake extended |
|
Definition
|
|
Term
Enroute descent, power as required, clean |
|
Definition
|
|
Term
Max range descent, power as required, clean |
|
Definition
| 180 KIAS/1500 fpm descent |
|
|
Term
Decreased range for each 10 knots of headwind, clean |
|
Definition
|
|
Term
|
Definition
| VAPP/LND + 50% of gust(max of 10) |
|
|
Term
Charted landing distance glidepath |
|
Definition
|
|
Term
Vobs, obstacle speed (and pitch) |
|
Definition
|
|
Term
| Critical Altitude- 100% torque is no longer available |
|
Definition
|
|
Term
| Do not exceed during climbs when above critical alt |
|
Definition
|
|
Term
Subtract from observed ITT at critical alt during climb out |
|
Definition
|
|
Term
Max cruise power- amount of cruise power available above critical alt |
|
Definition
|
|
Term
Subtract from observed ITT at critical alt for max cruise power |
|
Definition
|
|
