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Ifs OPS limits

QuestionAnswer
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