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T-34 Limits

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Question
Answer
ITT Normal idle range   400-660  
🗑
ITT Normal operating range   400-695  
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ITT Max at shutdown   610  
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ITT Max continuous   695  
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ITT Max acceleration   825  
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ITT Hot Start   925 for 2 seconds  
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ITT Max during start   1090  
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What measures ITT?   8 thermocouples  
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Prop RPM Idle range   <1800  
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Prop RPM normal range   2200 +- 25  
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Prop RPM overspeed governor   2332 +- 40  
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Prop RPM Fuel topping governer   2398  
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N1 Introduce fuel   12 %  
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N1 Flameout   10-12%  
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N1 Rollback   40-60%  
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N1 Minimum for flight (griped)   60%  
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N1 Idle range   62-65%  
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N1 Normal range   89-93%  
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N1 Max   101.5%  
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N1 max acceleration   102.6%  
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Airspeed Max clean   280 (surface-20,000) 245 (20,000-25,000)  
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Airspeed Max canopy emergency open   250  
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Airspeed Max canopy open   240  
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Airspeed Max turbulent air penetration   195  
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Airspeed Max gear extension   150  
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Airspeed Max flap extension   120  
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Airpseed Max gear retraction   120  
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Airspeed Max flap retraction   120  
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Airspeed Min flap retraction   90  
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Airspeed for downwind   100  
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VFR overhead break airspeed   170  
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Airspeed full flap landing   85  
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Airspeed no flap landing   95  
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Airspeed best angle of climb (Vx)   75  
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Airspeed best rate of climb (Vy)   100  
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Airspeed Best maneuvering speed (Va)   135  
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Airspeed recommended bailout   90-120  
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Torque Max range   580  
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Torque Max endurance   420  
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Torque Idle range   150  
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Torgue Autoignition range   180-300  
🗑
Torque descent   300  
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Torque overspeed test   400-500  
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Torque Normal operating range   400-1015  
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Torque Climb   1015  
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Torque Max allowable   1015  
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Torque max   1315  
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Torque max for oil malfunction   850  
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Fuel flow idle   125  
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Fuel flow normal operation   335  
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Fuel type primary   JP5  
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Fuel type alternates   JP4 and JP8  
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Oil temp min start   -40  
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Oil temp normal range   10-99  
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Oil temp max   100  
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Oil pressure idle range   40 min  
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Oil pressure Normal range   65-85  
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Oil pressure max fluctuation   +-5 psi within limits  
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Max oil pressure   100  
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Oil pressure dynamic maneuvers   10 psi for 5 secs  
🗑
Oil pressure cold days   80-100 psi  
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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  
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G limits gear down   +1.5/ -1.0  
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Max time inverted   15 sec  
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Max time vertical nose up   15 sec  
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Max time vertical nose down   3 sec  
🗑
Max time wings vertical   3 sec  
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Max time zero G   transient  
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Starter time limitations   40s/60s/40s/60s/40s/30min  
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Wing span   33 feet 4 inches  
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Length   28 feet 6 inches  
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prop arc clearance   11 inches  
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max ramp weight   4425  
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max takeoff/landing weight   4400  
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max aerobatic weight   4300  
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max zero fuel weight   3650  
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max weight crew and luggage   425  
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max sink rate at touch down   600 fpm  
🗑
max total winds   25  
🗑
max crosswind component   22 NF, 15 FF  
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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  
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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  
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Main gear tire pressure   90 psi +-2  
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nose wheel tire pressure   70 psi +-2  
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Main oleo height   3 inches  
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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  
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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  
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torque sensing failure 205 ft lb   N1 = 77-80 FF = 150-170  
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torque sensing failure 650 ft lb   N1 = 85-87 FF = 200-220  
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torque sensing failure 850 ft lb   N1 = 90 FF = 250-270  
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glide characteristics clean/feathered   800 fpm 12:1  
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glide characteristics gear down/feathered   1200 fpm 8:1  
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glide characteristics flaps down/feathered   1250 fpm 8:1  
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glide characteristics dirty/feathered   1650 fpm 6:1  
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glide characteristics clean/feathered   2400 fpm 3:1  
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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  
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what are pitch change parts   feather spring, counter weights, servo piston, beta ring, high pressure oil  
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open canopy increases rate of descent by ___   300 fpm  
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flux detector is where?   in left wing  
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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  
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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  
🗑


   

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