Question | Answer |
ITT Normal idle range | 400-660 |
ITT Normal operating range | 400-695 |
ITT Max at shutdown | 610 |
ITT Max continuous | 695 |
ITT Max acceleration | 825 |
ITT Hot Start | 925 for 2 seconds |
ITT Max during start | 1090 |
What measures ITT? | 8 thermocouples |
Prop RPM Idle range | <1800 |
Prop RPM normal range | 2200 +- 25 |
Prop RPM overspeed governor | 2332 +- 40 |
Prop RPM Fuel topping governer | 2398 |
N1 Introduce fuel | 12 % |
N1 Flameout | 10-12% |
N1 Rollback | 40-60% |
N1 Minimum for flight (griped) | 60% |
N1 Idle range | 62-65% |
N1 Normal range | 89-93% |
N1 Max | 101.5% |
N1 max acceleration | 102.6% |
Airspeed Max clean | 280 (surface-20,000)
245 (20,000-25,000) |
Airspeed Max canopy emergency open | 250 |
Airspeed Max canopy open | 240 |
Airspeed Max turbulent air penetration | 195 |
Airspeed Max gear extension | 150 |
Airspeed Max flap extension | 120 |
Airpseed Max gear retraction | 120 |
Airspeed Max flap retraction | 120 |
Airspeed Min flap retraction | 90 |
Airspeed for downwind | 100 |
VFR overhead break airspeed | 170 |
Airspeed full flap landing | 85 |
Airspeed no flap landing | 95 |
Airspeed best angle of climb (Vx) | 75 |
Airspeed best rate of climb (Vy) | 100 |
Airspeed Best maneuvering speed (Va) | 135 |
Airspeed recommended bailout | 90-120 |
Torque Max range | 580 |
Torque Max endurance | 420 |
Torque Idle range | 150 |
Torgue Autoignition range | 180-300 |
Torque descent | 300 |
Torque overspeed test | 400-500 |
Torque Normal operating range | 400-1015 |
Torque Climb | 1015 |
Torque Max allowable | 1015 |
Torque max | 1315 |
Torque max for oil malfunction | 850 |
Fuel flow idle | 125 |
Fuel flow normal operation | 335 |
Fuel type primary | JP5 |
Fuel type alternates | JP4 and JP8 |
Oil temp min start | -40 |
Oil temp normal range | 10-99 |
Oil temp max | 100 |
Oil pressure idle range | 40 min |
Oil pressure Normal range | 65-85 |
Oil pressure max fluctuation | +-5 psi within limits |
Max oil pressure | 100 |
Oil pressure dynamic maneuvers | 10 psi for 5 secs |
Oil pressure cold days | 80-100 psi |
G limits up to 280 kts | +4.5/ -1.0 |
G limits up to 220 kts | +4.5/ -2.3 |
G limits flaps down | +2.0/ -1.0 |
G limits gear down | +1.5/ -1.0 |
Max time inverted | 15 sec |
Max time vertical nose up | 15 sec |
Max time vertical nose down | 3 sec |
Max time wings vertical | 3 sec |
Max time zero G | transient |
Starter time limitations | 40s/60s/40s/60s/40s/30min |
Wing span | 33 feet 4 inches |
Length | 28 feet 6 inches |
prop arc clearance | 11 inches |
max ramp weight | 4425 |
max takeoff/landing weight | 4400 |
max aerobatic weight | 4300 |
max zero fuel weight | 3650 |
max weight crew and luggage | 425 |
max sink rate at touch down | 600 fpm |
max total winds | 25 |
max crosswind component | 22 NF, 15 FF |
max operating altitude | 25000 |
airstart envelope (sea level to 20000) | 80-280 kts |
Engine flat rated horsepower | 550 (1315 torque) |
Engine normal rated horsepower | 425 (1015 torque) |
Engine how many stages? | 3 axial, 1 centrifugal |
Engine compression ratio | 7:1 |
Engine reduction ratio | 15:1 |
Engine compressor turbine RPM (N1) | 37000 |
Engine power turbine (N2) | 33000 |
Landing gear nose gear turn limits | +-30 deg |
Main gear tire pressure | 90 psi +-2 |
nose wheel tire pressure | 70 psi +-2 |
Main oleo height | 3 inches |
nose gear oleo height | 3-5 inches |
red tire mark max slip | 1/4 inch |
aldis steady green | Ground: takeoff
Air: Land |
aldis flashing green | Ground: taxi
Air: return to land |
aldis steady red | Ground: stop
Air: give way, circle |
aldis flashing red | Ground: taxi clear
Air: Do not land |
aldis flashing white | return to start |
aldis flashing red/green | Use extreme caution |
aldis pyrotechnic | waveoff |
Oil system capacity | 4.4 gal |
oil tank capacity | 2.8 gal |
usable oil | 1.4 upright
.25 inverted |
GPU output needed for start | 28V 600 amps |
battery rated at... | 24V 24A |
generator rated at... | 30V 200A |
starter rated at... | 28V 800A |
generator control panel | 27-29.5V |
overvoltage protection | 34V |
undervolt protection | 25V |
annunciator light | 25-27.5V |
battery voltage for start | min 22V |
min battery voltage during start | 10V |
replace battery below... | 18V |
voltage for GPU start | 18-22V |
ammeter shows __ during GPU | discharging |
6 Prohibited maneuvers (anytime) | Night forms
inverted stall
inverted above 220 kts
intentional dirty spin
intentional inverted spin
intentional feathered spin |
Prohibited maneuvers (solo) | EPs
PPEL
spins
stalls
(only previously introduced maneuvers) |
how many fuel nozzles? | 10 primary, 4 secondary |
FCU pressure | 800 |
PCL spool time | 5 sec |
solitary primary pump operation | 10 hrs |
how many fuel drains | 5 + 1 firewall |
how many fuel quantity indicators? | 6 capacitance probes |
activates low fuel light? | 2 thermistors |
fuel capacity | 135 gal |
usable fuel capacity | 130 gal |
blade angle feathered | 87.5 |
blade angle low pitch/idle | 17.5 |
blade angle beta | -5 |
torque sensing failure 205 ft lb | N1 = 77-80
FF = 150-170 |
torque sensing failure 650 ft lb | N1 = 85-87
FF = 200-220 |
torque sensing failure 850 ft lb | N1 = 90
FF = 250-270 |
glide characteristics clean/feathered | 800 fpm
12:1 |
glide characteristics gear down/feathered | 1200 fpm
8:1 |
glide characteristics flaps down/feathered | 1250 fpm
8:1 |
glide characteristics dirty/feathered | 1650 fpm
6:1 |
glide characteristics clean/feathered | 2400 fpm
3:1 |
left safety switch | down: gear warning
up: NACWS test |
right safety switch | down: disables gear up
up: AOA |
nose safety switch | down: beta
up: disable rudder shakers |
4 EPL dont's | starts, jam acceleration, beta, advance past point at which fluctuations are min during overspeed condition |
left air intake | acc gear box, oil cooler, cockpit air, starter generator |
oil/fuel heater | regulates b/w 70-90 F |
oil cooler bypass | opens @60 F, closes at 71 F |
what are the 4 gyros? | 2 turn, 1 dir, 1 attitude |
what are the 4 prop governer parts | flyweights, speeder spring, pilot valve, oil type pump |
what are pitch change parts | feather spring, counter weights, servo piston, beta ring, high pressure oil |
open canopy increases rate of descent by ___ | 300 fpm |
flux detector is where? | in left wing |
oxygen system capacity | 1850 psi @ 70 F |
oxygen system volume | 76 cubic feet |
oxygen relief ruptures at ___ | 2775 psi |
engine inlet bypass door can't close above ___ | 150 kts |
engine inlet bypass door opens automatically at ___ | 200 kts |
icing checklist | pitot heat on
cockpit enviro and defog as required
engine bypass door
auto ignition switch on |
weather mins for solo | winds 25 steady, crosswind 10 kts, no tail wind
homefield ceiling 1500/ 3 vis
working area ceiling 3000/ 3 vis
working area PA's ceiling 8000/3 vis |
landing gear warning: gear up flaps down | wheels warning light, horn |
landing gear warning: gear up PCL below 75 | gear light, wheels warning light, horn |
landing gear warning: gear handle up on ground | gear handle light, wheel warning light, horn |
landing hear warning: handle and gear disagree | gear handle light |
AC switches | high pressure (black): 380 psi from condenser
low pressure (copper): 3 psi to compressor |
ADB min discrepancy records | last 10 flights |
ADB: turnaround on A sheet good for how long? | 24 hrs, 1 flight |
ADB: daily on A sheet good for how long? | 72 hours, or 24 hrs since last flight |
ADB: 7 checks | 7 day chute and first aid
7 day lube
14 day wash
56 day corrosion
1st 100 hr
2nd 100 hr
25 hr oil sample |
spin characteristics: erect spin | AOA pegged
airspeed 80-100 stable
turn needle pegged |
spin characteristics: inverted | AOA 3 units
airspeed 0
turn needle pegged |
spin rate of descent | 9000-12000 fpm |
rate of descent per turn | 375-500 fpm |
misc solo requirements | 300 lbs fuel per side
landing min fuel 150 lbs
temp/dew point 4 deg max spread
runway lengths 3000 dry VMC, 4000 wet VMC, 4000 touch and go |
Engine failure Indications: Flameout | Torque: 0
N1: 10-12
ITT: 200
RPM: 200
FF: 50
Oil temp: decreasing
Oil press: various |
Engine failure indications: Rollback | Torque: low
N1: 40-60
ITT:
RPM: <2200
FF: 80-100
Oil temp: normal
Oil press: normal |
Engine failure indications: Compressor stall | Torque: fluctuating
N1: fluctuating
ITT: fluctuating
RPM: surges
FF: fluctuating
Oil temp: normal
Oil pressure: normal |
NACWS: number of aircraft can track and radius? | 50 up to 20 NM |
NACWS: passive mode | uses ground radar tracks up to 20 NM |
NACWS: active mode | uses own interrogations up to 6NM |
NACWS: enroute mode | Proximity zone = 20 NM, +-2700 ft
Protection zone = 1 NM, +-500 ft
aircraft within 20 seconds of zone will wound alarm |
NACWS: landing mode | proximity zone = 1.5 NM, +-500 ft
protection zone = .1 NM, +-500 ft
aircraft within 10 seconds of zone will sound alarm |
NACWS: DME ranges | 20, 10, 5, 3, 1.5 NM |
NACWS: range button does what? | toggles between enroute and landing modes |
PRC 90 frequencies are? | 282.8 SAR T/R
243 Guard T/R
243 beacon
Range = 60 miles |
Smoke flare rings | 1 ring is day
2 rings is night |
pencil flare range | 200 ft |