Good to Know Numbers Flashcards
1
Q
Gross weight with fuel and two souls
A
12800 lbs
2
Q
One engine thrust MIL/MAX
A
2200/3300 lbs
3
Q
Fuel flow for one engine: MAX at rest, MAX at Mach 1
A
7,300; 11,400 lb/hr
4
Q
Pushing start arms ignition for ___ sec
A
30
5
Q
One engine normal oil capacity and air expansion space
A
4 qt, 1 qt
6
Q
Gravity flow guaranteed up to ___
A
6000 MSL
7
Q
Flameouts while gravity feeding in MAX occurred as low as ___
A
7000 MSL
8
Q
Normally sufficient fuel will flow by gravity to maintain MAX up to ___
A
25,000 MSL
9
Q
Fuel cutoff switches operated by ___ power and cut off fuel in ___ sec
A
DC, 1
10
Q
Fuel low level light comes on after ___ sec below ___ amount
A
7.5 sec, 250 lbs
11
Q
Gearbox shift occurs at ___ range
A
65-75%
12
Q
Voltage of battery is ___V and of DC rectifiers is ___V
A
24, 28
13
Q
AC system provides __/__ V power
A
115/200
14
Q
AC generators cut-in between
A
43-48%
15
Q
Min battery voltage of ___ is required to close batt relay
A
18V
16
Q
Left engine provides ___psi for ___ system
A
3200psi, utility
17
Q
Right engine provides ___ psi for ___ system
A
3200psi, flight control
18
Q
Hyd low press comes on at ___ psi, and goes back out at ___ psi
A
1500, 1800
19
Q
Rudder limited to ___ deg each side when nose gear out 3/4 or less
A
6 deg
20
Q
Landing gear extension/retraction takes approx. ___
A
6 sec
21
Q
Gear horn and warning light come on when gear not down and locked, ___ kts or less, attitude __ or below, and both throttles below ___
A
210 kts, 10,000ft, 96%
22
Q
When accelerating, gear light may not go out until ___
A
240 kts
23
Q
Landing gear alt release pulled out ___ inches, and requires ___ sec
A
10in, 15-35 sec
24
Q
Rear canopy follows front by ___ sec after canopy jettison
A
1 sec
25
Aneroid delays parachute opening until between ___
11,500 to 15,000 ft
26
Seat ejection occurs ___ after canopy jettison
0.3 sec
27
Fuel for left engine is __ gal serviced/usable and lbs usable
293/286 gal, 1916 lbs
28
Fuel for right engine is __ gal serviced/usable and ___ lbs usable
305/297 gal, 1990 lbs
29
Total fuel is ___ gal serviced/usable and ___ lbs usable
598/583 gal, 3906 lbs
30
With singe-engine and less than ___ in either system, leave both boost pumps on and crossfeed on:
250 lbs
31
A minimum of ___ RPM is required to achieve any engine fuel flow
12-14%
32
___% RPM is the heart of the airstart envelope at any altitude
18-20%
33
Ignition must occur before fuel flow reaches ___ lb/hr
360 lb/hr
34
After aborted start, wait ___ min before attempting another start
2 min
35
If EGT doesn't rise within ___ sec of fuel flow indication, abort start
12 sec
36
Flaps should be +/-___ of 60% position
5%
37
Normal rotation speed on initial takeoff is
141 KIAS (this is rounded to 145KIAS)
38
Normal liftoff speed on initial takeoff is
165 KIAS
39
Delay takeoff a minimum o f ___ min behind large and ___ min behind heavy aircraft
2, 4
40
With a crosswind greater than __ kts, spacing behind large/heavy aircraft can be reduced
5 kts
41
Abort takeoff if either afterburner doesn't light within __ sec
5 sec
42
Final turn speed is ___ plus 1 knot per 100 lb over 1000lb fuel
180 KIAS
43
Final approach speed is ___ plus 1 knot per 100 lb over 1000lb fuel
160 KIAS
44
Touchdown speed is ___ plus 1 knot per 100 lb over 1000lb fuel
135 KIAS
45
Minimum hydraulic pressure
1500psi
46
Each generator has __ phases
3
47
The O2 low light comes on at or below ___ liter, and may blink at or below ___ liter
1, 3 liters
48
Below __, the engine anti-ice is always open, regardless of switch position
65% RPM
49
There are __ rotating beacons, located where?
2: tail and lower fuselage
50
There are ___ position lights, located where?
4: tail, lower fuselage, one on each wing
51
Battery energizes DC bus for __ min at __% power
15 at 80%
52
If oil pressure is high in cold weather, should be in limits within ___
6 min
53
The radio attenuation switch reduces UHF and VHF volume by ___
66%
54
IDENT sends a pulse with transponder replies for ___ sec
15 sec
55
Standby ADI provides ___ deg climb, ___ deg dive, ___ deg roll capacity
92 climb, 78 dive, 360 roll
56
Standby ADI provides ___ minutes of useful info within +/- ___ deg after DC failure
9 min, 6 deg
57
Maintain a minimum of __%RPM to ensure effective anti-ice operation
80%
58
Due to oil supply restriction, zero-G flight is restricted to ___ sec
10 sec
59
Due to oil supply restriction, negative G flight is restricted to ___ sec
30 sec
60
Rudder system failure may push rudder to __ deg
30 deg
61
Stab aug system failure may push rudder to ___ deg
2 deg
62
Touchdowns greater than ___ KCAS should not be attempted
200 kts
63
With asymmetric flaps, maintain ___ kts above final appr/touchdown speed
20 kts
64
Do not touchdown at less than ___ kts with asymmetric flaps
165 kts
65
On SE go-around, climb only as necessary until reaching ___ kts
200 kts
66
When landing with all gear up, touch down ___ kts faster than normal
10 kts
67
Estimation for landing roll is ___ ft + fuel (not including 1000ft down):
2500 ft
68
Landing roll will approximately ___ for a no flap landing
double
69
Anti-ice will cause a loss of ___% thrust in MIL and ___ in MAX
8.5%, 5.5%
70
If flab-slab interconnect fails and flaps needed for landing, ___% flaps provides adequate control authority and controllable stick forces
30-45%
71
Pressure reg maintain cabin alt of ___ +/- ___ from ___ MSL to ___MSL
8000ft +/- 2000ft, from 8000MSL to 23000MSL
72
Avoid MAX thrust dives when below ___ lb in either fuel tank
650 lb
73
Use ___ kts as go/no-go for simple tire failure
100 kts
74
Increase final approach speed and touchdown speed by __ the gust factor
half
75
Increase final turn, approach and touchdown by ___ kts for no flap
15 kts
76
How many seconds until full parachute deployment?
3.42 sec
77
Landing light retraction takes ___ sec
10 sec
78
```
Max allowable sink rates for landing: (fpm)
normal landing (>1700lbs) ___
crab landing (>1700lbs) ___
normal landing (<1700lbs) ___
crab landing (<1700lbs) ___
```
340
200
590
395
79
AOA max range ___
| AOA max endurance/best angle of climb ___
0.18, 0.3
80
First 4.5in (out of 6in) of stick travel provides ___ aileron deflection
50%
81
Last 1.5in (out of 6in) of stick travel provides ___ aileron deflection
Full
82
Crossfeed recommended with fuel imbalance of __ or greater
200lbs
83
Holding airspeed
250-265kts
84
A radar pattern typically burns ___ fuel
325 lbs
85
Turbulent air/thunderstorm penetration speed
280kts
86
Climb possible at SETOS is ___ fpm
100 fpm
87
Climb increased by ___ fpm for each between SETOS and SETOS+10
8-50 fpm
88
Gear retraction may take ___ when retracted between SETOS+10 and 200 kts
1 min
89
If unable to retract gear, best climb at ___ for 60% flaps, ___ for 0% flaps
200kts, 220kts
90
Optimum pitch for ejection zoom
20 deg NH
91
With loss of canopy, slow to ___ kits; min drag occurs at ___ kts
300 kts, 225kts
92
If one hydr system reads zero, hydr system transfer may occur, and flight time could be limited to ___ min
35 min
93
Controllability check should be accomplished at ___ AGL or higher
6000 AGL
94
Maintain ___kts above min controllable airspeed in descent/landing approach after a controllability check
20kts
95
Best glide speed is ___kts + 1kt/100lbs fuel
230
96
Multiply altitude in thousands of feet by ___ for glide distance in NM
1.7
97
Max crosswind, dry runway
30 kts
98
Max crosswind, wet runway
20 kts
99
Max crosswind, icy/standing water
10 kts
100
Max crosswind, dry runway, single ship TnG
25 kts
101
Max crosswind for solo students (dry/wet)
15kts/10kts
102
Minimum runway length for takeoff/landing
8000ft
103
No flap landings are not accomplished with ___ lbs or greater of fuel
2500lbs
104
Low level min and max airspeed
300kts min, 420kts max
105
Simulated single-engine go around must be initiated by ___ (___ full flap)
100ft (300ft full flap) AGL
106
Perform all aerobatic maneuvers above
8000AGL (?)
107
Stall and slow flight must be performed between
8000AGL and FL200
108
Minimum power setting for stalls and slow flight
80%
109
Nose high recoveries must be accomplished below ___
FL240
110
Do not perform supersonic flight below ___ unless in an authorized airspeed
FL300
111
Solo students will not perform patterns and landings with ___ fuel or more
2500lbs
112
Normal minimum fuel for solo students
800lbs
113
Minimum Fuel
600lbs
114
Emergency Fuel
400lbs
115
Min taxi interval is ___ staggered, ___ in trail
150ft, 300ft
116
Restricted low approach must be initiated by ___ AGL unless otherwise directed
500 AGL
117
Chase aircraft in emergency can low approach down to ___ AGL
300ft
118
For practice single engine approach, set the simulated bad engine to ___% RPM
60%
119
Begin closed pull up with a minimum of ___ kts, and maintain ___kts during the maneuver
240, 200
120
RPM of ___ should be sufficient for taxi
80%
121
Rolling takeoffs may increase takeoff distance by ___
150-300ft
