Good to Know Numbers Flashcards
Gross weight with fuel and two souls
12800 lbs
One engine thrust MIL/MAX
2200/3300 lbs
Fuel flow for one engine: MAX at rest, MAX at Mach 1
7,300; 11,400 lb/hr
Pushing start arms ignition for ___ sec
30
One engine normal oil capacity and air expansion space
4 qt, 1 qt
Gravity flow guaranteed up to ___
6000 MSL
Flameouts while gravity feeding in MAX occurred as low as ___
7000 MSL
Normally sufficient fuel will flow by gravity to maintain MAX up to ___
25,000 MSL
Fuel cutoff switches operated by ___ power and cut off fuel in ___ sec
DC, 1
Fuel low level light comes on after ___ sec below ___ amount
7.5 sec, 250 lbs
Gearbox shift occurs at ___ range
65-75%
Voltage of battery is ___V and of DC rectifiers is ___V
24, 28
AC system provides __/__ V power
115/200
AC generators cut-in between
43-48%
Min battery voltage of ___ is required to close batt relay
18V
Left engine provides ___psi for ___ system
3200psi, utility
Right engine provides ___ psi for ___ system
3200psi, flight control
Hyd low press comes on at ___ psi, and goes back out at ___ psi
1500, 1800
Rudder limited to ___ deg each side when nose gear out 3/4 or less
6 deg
Landing gear extension/retraction takes approx. ___
6 sec
Gear horn and warning light come on when gear not down and locked, ___ kts or less, attitude __ or below, and both throttles below ___
210 kts, 10,000ft, 96%
When accelerating, gear light may not go out until ___
240 kts
Landing gear alt release pulled out ___ inches, and requires ___ sec
10in, 15-35 sec
Rear canopy follows front by ___ sec after canopy jettison
1 sec
Aneroid delays parachute opening until between ___
11,500 to 15,000 ft
Seat ejection occurs ___ after canopy jettison
0.3 sec
Fuel for left engine is __ gal serviced/usable and lbs usable
293/286 gal, 1916 lbs
Fuel for right engine is __ gal serviced/usable and ___ lbs usable
305/297 gal, 1990 lbs
Total fuel is ___ gal serviced/usable and ___ lbs usable
598/583 gal, 3906 lbs
With singe-engine and less than ___ in either system, leave both boost pumps on and crossfeed on:
250 lbs
A minimum of ___ RPM is required to achieve any engine fuel flow
12-14%
___% RPM is the heart of the airstart envelope at any altitude
18-20%
Ignition must occur before fuel flow reaches ___ lb/hr
360 lb/hr
After aborted start, wait ___ min before attempting another start
2 min
If EGT doesn’t rise within ___ sec of fuel flow indication, abort start
12 sec
Flaps should be +/-___ of 60% position
5%
Normal rotation speed on initial takeoff is
141 KIAS (this is rounded to 145KIAS)
Normal liftoff speed on initial takeoff is
165 KIAS
Delay takeoff a minimum o f ___ min behind large and ___ min behind heavy aircraft
2, 4
With a crosswind greater than __ kts, spacing behind large/heavy aircraft can be reduced
5 kts
Abort takeoff if either afterburner doesn’t light within __ sec
5 sec
Final turn speed is ___ plus 1 knot per 100 lb over 1000lb fuel
180 KIAS
Final approach speed is ___ plus 1 knot per 100 lb over 1000lb fuel
160 KIAS
Touchdown speed is ___ plus 1 knot per 100 lb over 1000lb fuel
135 KIAS
Minimum hydraulic pressure
1500psi
Each generator has __ phases
3
The O2 low light comes on at or below ___ liter, and may blink at or below ___ liter
1, 3 liters
Below __, the engine anti-ice is always open, regardless of switch position
65% RPM
There are __ rotating beacons, located where?
2: tail and lower fuselage
There are ___ position lights, located where?
4: tail, lower fuselage, one on each wing
Battery energizes DC bus for __ min at __% power
15 at 80%
If oil pressure is high in cold weather, should be in limits within ___
6 min
The radio attenuation switch reduces UHF and VHF volume by ___
66%
IDENT sends a pulse with transponder replies for ___ sec
15 sec
Standby ADI provides ___ deg climb, ___ deg dive, ___ deg roll capacity
92 climb, 78 dive, 360 roll
Standby ADI provides ___ minutes of useful info within +/- ___ deg after DC failure
9 min, 6 deg
Maintain a minimum of __%RPM to ensure effective anti-ice operation
80%
Due to oil supply restriction, zero-G flight is restricted to ___ sec
10 sec
Due to oil supply restriction, negative G flight is restricted to ___ sec
30 sec
Rudder system failure may push rudder to __ deg
30 deg
Stab aug system failure may push rudder to ___ deg
2 deg
Touchdowns greater than ___ KCAS should not be attempted
200 kts
With asymmetric flaps, maintain ___ kts above final appr/touchdown speed
20 kts
Do not touchdown at less than ___ kts with asymmetric flaps
165 kts
On SE go-around, climb only as necessary until reaching ___ kts
200 kts
When landing with all gear up, touch down ___ kts faster than normal
10 kts
Estimation for landing roll is ___ ft + fuel (not including 1000ft down):
2500 ft
Landing roll will approximately ___ for a no flap landing
double
Anti-ice will cause a loss of ___% thrust in MIL and ___ in MAX
8.5%, 5.5%
If flab-slab interconnect fails and flaps needed for landing, ___% flaps provides adequate control authority and controllable stick forces
30-45%
Pressure reg maintain cabin alt of ___ +/- ___ from ___ MSL to ___MSL
8000ft +/- 2000ft, from 8000MSL to 23000MSL
Avoid MAX thrust dives when below ___ lb in either fuel tank
650 lb
Use ___ kts as go/no-go for simple tire failure
100 kts
Increase final approach speed and touchdown speed by __ the gust factor
half
Increase final turn, approach and touchdown by ___ kts for no flap
15 kts
How many seconds until full parachute deployment?
3.42 sec
Landing light retraction takes ___ sec
10 sec
Max allowable sink rates for landing: (fpm) normal landing (>1700lbs) \_\_\_ crab landing (>1700lbs) \_\_\_ normal landing (<1700lbs) \_\_\_ crab landing (<1700lbs) \_\_\_
340
200
590
395
AOA max range ___
AOA max endurance/best angle of climb ___
0.18, 0.3
First 4.5in (out of 6in) of stick travel provides ___ aileron deflection
50%
Last 1.5in (out of 6in) of stick travel provides ___ aileron deflection
Full
Crossfeed recommended with fuel imbalance of __ or greater
200lbs
Holding airspeed
250-265kts
A radar pattern typically burns ___ fuel
325 lbs
Turbulent air/thunderstorm penetration speed
280kts
Climb possible at SETOS is ___ fpm
100 fpm
Climb increased by ___ fpm for each between SETOS and SETOS+10
8-50 fpm
Gear retraction may take ___ when retracted between SETOS+10 and 200 kts
1 min
If unable to retract gear, best climb at ___ for 60% flaps, ___ for 0% flaps
200kts, 220kts
Optimum pitch for ejection zoom
20 deg NH
With loss of canopy, slow to ___ kits; min drag occurs at ___ kts
300 kts, 225kts
If one hydr system reads zero, hydr system transfer may occur, and flight time could be limited to ___ min
35 min
Controllability check should be accomplished at ___ AGL or higher
6000 AGL
Maintain ___kts above min controllable airspeed in descent/landing approach after a controllability check
20kts
Best glide speed is ___kts + 1kt/100lbs fuel
230
Multiply altitude in thousands of feet by ___ for glide distance in NM
1.7
Max crosswind, dry runway
30 kts
Max crosswind, wet runway
20 kts
Max crosswind, icy/standing water
10 kts
Max crosswind, dry runway, single ship TnG
25 kts
Max crosswind for solo students (dry/wet)
15kts/10kts
Minimum runway length for takeoff/landing
8000ft
No flap landings are not accomplished with ___ lbs or greater of fuel
2500lbs
Low level min and max airspeed
300kts min, 420kts max
Simulated single-engine go around must be initiated by ___ (___ full flap)
100ft (300ft full flap) AGL
Perform all aerobatic maneuvers above
8000AGL (?)
Stall and slow flight must be performed between
8000AGL and FL200
Minimum power setting for stalls and slow flight
80%
Nose high recoveries must be accomplished below ___
FL240
Do not perform supersonic flight below ___ unless in an authorized airspeed
FL300
Solo students will not perform patterns and landings with ___ fuel or more
2500lbs
Normal minimum fuel for solo students
800lbs
Minimum Fuel
600lbs
Emergency Fuel
400lbs
Min taxi interval is ___ staggered, ___ in trail
150ft, 300ft
Restricted low approach must be initiated by ___ AGL unless otherwise directed
500 AGL
Chase aircraft in emergency can low approach down to ___ AGL
300ft
For practice single engine approach, set the simulated bad engine to ___% RPM
60%
Begin closed pull up with a minimum of ___ kts, and maintain ___kts during the maneuver
240, 200
RPM of ___ should be sufficient for taxi
80%
Rolling takeoffs may increase takeoff distance by ___
150-300ft
