Number to Memorize Flashcards
1
Q
Height
high skid gear
A
10.91 feet
2
Q
Length
A
41.4 feet
3
Q
Baggage Max Weight
A
250 lbs
4
Q
Baggage Max Volume
A
16 cubic feet
5
Q
Number of Skid Shoes
A
7/Skid
14 Total
6
Q
Engine Type
A
RR 250 C47B
7
Q
Engine Horsepower
Thermodynamic Rating
A
813 SHP
8
Q
Engine Takeoff Horsepower Rating
and Q
A
674 SHP @ 93.5-100% Q
9
Q
Engine Continuous Horesepower Rating
and Q
A
630 SHP
10
Q
RR Rating on Engine Plate
A
650 SHP
11
Q
Compressor RPM
A
51,000 RPM @ 100% Q
12
Q
Compression Ratio
A
9.2:1
13
Q
Compressor Temperature Increase
A
291C/555F
14
Q
Combustion Air Use
A
75-80% for cooling of internal parts
20-25% for fuel burn
~2% for sealing oil passages
15
Q
Ng Speed
A
51,000 RPM @ 100% Ng
16
Q
Np Speed
A
32,183 RPM @ 100% Np
17
Q
Torquemeter Gear Speed
A
10,528 RPM @ 100% Np
18
Q
Output Drive Gear Speed
A
6,317 RPM @ 100% Np
19
Q
Transmission Speed Ratio
A
15.29:1 Reducing
20
Q
Main Rotor RPM
A
413 RPM @ 100% Np
21
Q
Tail Rotor Gearbox Ratio
A
2.53:1 Reducing
22
Q
Tail Rotor RPM
A
~2,497 RPM @ 100% Np
23
Q
Engine Anti-Ice/Pitot Heat - ON
OAT
A
Less than 5C/40F ambient air temperature and in visible moisture
24
Q
CEFA Fuel Filter LRB pop
A
2.5 +/- 0.5 PSID
25
CEFA Fuel Filter bypas
3.4 PSID
26
CEFA Engine Oil Bypass
8.8-10.8 PSID
| LRB shows indication of bypass
27
Engine Oil Tank Capacity
6 quarts
28
Minimum Engine Oil Pressure
| Cruise
115 PSI
29
Maximum Engine Oil Pressure
| Cruise
130 PSI
30
Maximum Engine Oil Pressure
| Cold Start
200 PSI
31
Maximum Engine Oil Temp
| Cruise
107C
32
Fuel System Capacity
Total/usable gallons
Total Pounds
130 total/ 127.8 usable gallons
| 869 lbs total
33
Fuel Forward Cell Capacity
| gallons/pounds
37.6 gal
| 256 lbs
34
Main Fuel Cell Capacity
| gallons/pounds
90.2 gal
| 626 lbs
35
Full Fuel Capacity
| pounds
869 lbs
36
Fuel in pounds at which transfer from forward to main fuel cell begins and CG is moving forward.
770 lbs
37
Fuel in pounds at which both cells are drained equally and CG is at its max forward point.
508.6 lbs
38
Fuel in pounds at which only the forward cell is being drained and CG is moving aft.
344.1 lbs
39
Fuel in pounds at which the forward cell empties and CG is at is max aft point.
193.1 lbs
40
LOW FUEL CAS
100 +/- 10 lbs
41
FADEC Hot Start Abort
1. MGT > 885C <10,000 feet
2. MGT > 912C >10,000 feet
3. Volt drops <10vDC
42
Max Start MGT
10 seconds > 843C
| 1 second > 927C
43
Transmission Oil Capacity
5 quarts
44
Transmission Oil Pump Volume
6-6.7 gal/min
45
Temperatures at which transmission oil is NOT sent to the cooler
Less than 66C
46
Temperatures at which transmission oil is gradually sent to the cooler
66-81C
47
Temperatures at which ALL transmission oil is sent to the cooler
Greater than 81C
48
At what pressure differential does the transmission oil filter LRB pop?
14 +/- 2 PSID
49
At what pressure differential does the transmission oil filter bypass?
17 PSID
50
Maximum Transmission Oil Temp
110C
51
Minimum Transmission Oil Temp
30C @ Idle
| 40c @ Continuous speeds
52
Number of MR Blades
4
53
Diameter of MR
35 feet
54
MR Blade Chord
10.75 inches
55
MR Blade Twist
-13 degrees
56
Weight of a single MR Blade
~58 lbs
57
MR Rigging
1 degree left - translating tendency
| 5 degrees forward - level ship in forward flight
58
Max MR Tie Down Load
60 lbs
59
Max MR Tie Down Deflection
50 inches
60
Minimum wind velocity required for MR tiedown
30 knots
61
Number of TR Blades
2
62
Diameter of TR
65 inches or 5.42 feet
63
TR Blade Chord
6.4 inches
64
TR Blade Twist
0 inches
65
TR Gearbox Oil Capacity
.33 quarts
66
TR Gearbox Attachment
4 studs and 2 alignment pins
67
Tailboom Attachment
4 bolts
68
Number of Hanger Bearings
6
69
Number of Thomas Couplings
8
70
Number of Plates in each Thomas Coupling
9-12
71
Max force on Stinger
400 lbs
72
Auxiliary Fin Offset
5 degrees outward
73
Vertical Stabilizer Offset
9 degrees outward
74
Number of Hydraulic Servo Actuators
4
75
Hydraulic System Pressure
1000 +/- 25 PSI
76
Hydraulic Reservoir Capacity
1.3 US Pints
77
Total Hydraulic System Capacity
1.68 US Quarts
78
At what differential pressure do the hydraulic pump LRBs pop?
70 +/- 10 PSID
79
At what temperatures will the hydraulic pumps LRBs NOT work?
Less than 2C
80
At what pressures will the hydraulic relief valve open?
1075-1375 PSI
81
MR Brake limit
Below 40% Nr
82
Vertical Speed Limit
2000 fpm
83
Max number of CAS displayed in the Crew Alert Window?
12
84
Max weight
5250 lbs
85
Minimum weight at fuselage station 65.0 (pilot/copilot)
170 lbs
86
Vne in 5 min range of 93.5-100% torque?
100 knots
87
Vne with doors removed
100 knots
88
Max allowable airspeed for sideward/rearward flight or crosswind hover
35 KTAS
89
Max operating altitude
20,000 feet Hd or Hp, whichever is lower
90
Slope landing limitations
10 degrees side slopes
10 degrees nose up slopes
5 degrees nose down slopes
91
Max sea level ambient temp for operation
51.7C/125F
| Decreasing 2C/1000ft Hp
92
Minimum ambient temp for operation at all altitudes
-40C/-40F
93
% Np for Engine Overspeed
102. 1% for 2.5 seconds
| 107. 3% Immediately
94
MGT start limits
843C for 10 seconds
| 927C for 1 second
95
Max continuous MGT
| Max takeoff MGT
727C
| 779C
96
Engine torque ranges
Continuous 0-93.5%
| Takeoff, 5min 93.5-100%
97
Fuel pressure ranges
Min 8PSI
Continuous 8-25PSI
Max 25 PSI
98
Nr power off limits
85-107%
99
Best rate of climb airspeed
60 knots
100
What supplement number do we use in the POH?
FMS 28
