Help
Options
Didn't know it?
click below
click below
Knew it?
click below
click below
Don't Know
Remaining cards (0)
Know
retry
shuffle
restart
0:00
Embed Code - If you would like this activity on your web page, copy the script below and paste it into your web page.
Normal Size Small Size show me how
Normal Size Small Size show me how
Ifs OPS limits
| Question | Answer |
|---|---|
| ENGINE FIRE ON THE GROUND | FUEL SHUTOFF VALVE - OFF CABIN HEAT - OFF |
| ELECTRICAL FIRE ON THE GROUND | GEN/BAT MASTER SWITCH - OFF |
| ABORT | THROTTLE - IDLE BRAKES - AS REQUIRED FLAPS - CRUISE |
| ENGINE MALFUNCTION IN FLIGHT (SUFFICIENT RUNWAY REMAINING TO LAND) | AIRSPEED - 60 KIAS FLAPS - LDG |
| ENGINE FIRE DURING FLIGHT | FUEL SHUTOFF VALVE - OFF CABIN HEAT - OFF |
| ELECTRICAL FIRE DURING FLIGHT | GEN/BAT MASTER SWITCH - OFF AIR VENTS AND WINDOWS - OPEN |
| CABIN FIRE IN FLIGHT | GEN/BAT MASTER SWITCH - OFF AIR VENTS AND WINDOWS - OPEN CABIN HEAT - OFF |
| Vs0 (Stall speed in LDG configuration, kts) | 34 |
| Vs1 (stall speed in CRUISE configuration, kts) | 42 |
| Vr (Rotate Speed, kts) | 44 |
| Lift-off airspeed (kts) | 52 |
| Forced landing final approach airspeed (flaps LDG, kts) | 55 |
| Min. engine-out airspeed to sustain windmilling prop (kts) | 60 |
| Forced landing final approach airspeed (flaps T/O kts) | 60 |
| Forced landing final approach airspeed (flaps CRUISE. kts) | 64 |
| Normal landing final approach airspeed (kts) | 60 |
| No-Flap landing final approach airspeed (kts) | 65 |
| Vx (flaps T/O, kts) (Best angle of climb) | 60 |
| Vx (flaps CRUISE, kts) (Best angle of climb) | 65 |
| Vy (flaps T/O, kts) (Best rate of climb) | 66 |
| Vy (flaps CRUISE, kts) (Best rate of limb) | 70 |
| Best glide airspeed (1764 lbs) (L/D max) | 73 |
| Vfe (flaps LDG, kts) (Max. Airspeed with flaps extended) | 78 |
| Vfe (flaps T/O, kts) (Max. Airspeed with flaps extended) | 100 |
| Va (kts, 1764lbs) | 106 |
| Vno (Max. structural cruising speed, kts) | 118 |
| Force propeller to windmill if stopped, starter inop (kts) | 137 |
| Vne (Never exceed airspeed, kts) | 164 |
| Positive limit load factor (flaps CRUISE) | +4.4 |
| Negative limit load factor (flaps CRUISE) | -2.2 |
| Positive limit load factor (flaps T/O or LDG) | +2.0 |
| Negative limit load factor (flaps T/O or LDG) | 0 |
| Max. permissible bank angle for steep turns (in degrees) | 60 |
| Voltmeter lower limit red arc (volts) | 8-11 |
| Voltmeter caution range yellow arc (volts) | 11-12.5 |
| Voltmeter green arc (volts) | 12.5-16 |
| Voltmeter upper limit red line (volts) | 16.1 |
| Approved fuel grade | 100LL |
| Usable fuel (US gal.) | 24.0 |
| Fuel tank capacity (US gal.) | 24.5 |
| Max. ramp weight (lbs) | 1770 |
| Max. takeoff weight (lbs) | 1764 |
| Max. landing weight (lbs) | 1764 |
| Forward CG limit (at or below 1653 lbs) | 7.95 |
| Forward CG limit (1764 lbs) | 8.07 |
| Aft CG limit (1764 lbs) | 12.16 |
| AFT CG limit (at or below 1653 lbs) | 12.48 |
| Max. weight in baggage compartment (lbs) | 44 |
| Min. rpm during engine runup idle check | 975 |
| Min. rpm during flight if beyond gliding range of a runway (area idle) | 1400 |
| Min. rpm operations iwth fuel pump off | 1400 |
| Min. permissible static rpm (full throttle runup) | 2000 |
| Tachometer normal operating range (rpm) | 700-2800 |
| Max. permissible continuous rpm | 2800 |
| Min. rpm drop during magneto check | 25 |
| Max. rpm drop during magneto check | 150 |
| Max. rpm drop difference between magnetos | 50 |
| Max permissible continuous bhp | 125 |
| Min. oil pressure (psi) | 10 |
| Oil pressure normal operating range (psi) | 30-60 |
| Max. time for oil pressure to reach 10 psi after start (secs.) | 30 |
| Max. oil pressure for full power operation if OAT <0C (psi) | 70 |
| Max. oil pressure (psi) | 100 |
| Min. oil temperature (F) | 75 |
| Max. rpm after start until oil temp indication registers | 1000 |
| Oil temperature normal operating range (F) | 170-220 |
| Min oil temp. to begin an area SFL at Area Idle (F) | 170 |
| Min. oil temp for full power operation if oil pressure norm (F) | 100 |
| Max. oil temp (F) | 240 |
| Min oil quantity (US qts) | 4 |
| Max oil quantity (US qts) | 6 |
| Fuel pressure lower limit red line (psi) | 3.5 |
| Fuel pressure upper limit red line (psi) | 16.5 |
| Max. continuous start operation (secs) | 10 |
| Max. cumulative starter op. before cooling 3-5 min. (secs.) | 30 |
| Max. time for CHT below 300F in descent (minutes) | 5 |
| Min. CHT (F) takeoff & descent | 240 |
| CHT normal operating range (F) | 300-420 |
| CHT caution range (F) | 420-460 |
| Max. CHT (F) | 460 |
| Max OAT(C) operation w/full winterization kit | 0 |
| Max. OAT (C) operation w/ partial winterization kit | 12.5 |
| Max. total wind student dual (kts) | 25 |
| Max. total wind student solo (kts) | 20 |
| DA20 max. demosntrated crosswind component (kts) | 20 |
| Max. crosswind component student dual (kts) | 15 |
| Max. crosswind component student solo (kts) | 10 |
| Max. tailwind component (kts) | 5 |
| Maximum airplane structural temperature (C) | 55 |
| Propeller approx. minimum ground clearance (inches) | 10 |
| Main landing gear tire pressure (psi) | 33 |
| Nose gear tire pressure (psi) | 26 |
| Min. OAT (C) cabin heat not req for 10 min. before T/O | -20 |
Created by:
100001402898851
Popular Aviation sets