1
Q
Vo @ 3000lbs
Vo @ 2600lbs
Vo @ 2300lbs
Vo @ 2200lbs
A
3,000 = 131 2,600 = 122 2,300 = 114 2,200 = 111
2
Q
Vfe
A
50% Flaps - 120
100% Flaps - 100
3
Q
Vpd
A
135
4
Q
Vno
A
165
5
Q
Vne
A
200
6
Q
Normal Oil Temperature Range
A
100 - 240 deg F
7
Q
Max Oil PRESSURE
A
100psi
8
Q
CHT Normal Range
A
240 - 420 deg F
9
Q
CHT Caution Range
A
420 - 460 deg F
10
Q
MAP Normal Range
A
15 - 29.5”Hg
11
Q
Normal Fuel Flow Range (GPH)
A
7 - 13 GPH
12
Q
MAX Oil TEMP (do not confuse with CHT)
A
240 deg F
13
Q
Oil Pressure Normal Range
A
30 - 60 psi
14
Q
Voltmeter Normal Range
A
24 - 30V
32V is MAX
15
Q
Total Fuel Each Tanks
A
30.3 gal (28 usable each side)
16
Q
Max Operating Altitude is
A
17,500’
17
Q
PFD coupled Autopilot System Limitations (VFR): (there are 7)
A
- AP ops prohibited above 185 KIAS (system 55) or 180 KIAS (ssytem 55SR) and below 1.2Vs for given config.
- Not engaged for TO/LD
- Must be disengaged for Missed Approach, Go-Around, and Balked Landing
- Flaps must be set to 50% for AP Ops in ‘Altitude Hold’ at ASI below 95
- Flap deflection limited to 50% during AP ops
- AP must be disconnected in MOD-SEV TURB
- Min AP engage height is 400’ AGL
18
Q
PFD coupled Autopilot System Limitations (IFR): (there are 10)
A
- AP must be disengaged no later than 100’ below the MDA
- AP must be disconnected during APRCH if course deviation exceeds 50%, hand fly remaineder
- AP must be disengaged at the DA
- 12 knot max XC component between MAP and OM
- Intercept of LOC shall occur at least 5nm outside the OM
- XC component between 12-17 knots, intercept shall occur at least 10nm outside the OM
- Intercept angle no greater than 45 deg
- ILS is flown at ‘normal’ approach speeds
- Flaps extended to approach config prior to OM
- Approach GS to allow automatic Arming (no more than 15% above if manual arming)w
19
Q
Vg @ 3000
Vg @ 2500
A
3,000 = 96 KIAS 2,500 = 87 KIAS
20
Q
Vso
A
56
21
Q
Vs1
A
65
22
Q
Vx
A
81
23
Q
Vy
A
96
24
Q
Vr
A
67
25
Cruise Climb
105
