T6 LIMITS EKQ Flashcards

1
Q

Max Vmo
(M?)

A

316kts
M0.67

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2
Q

Manoeuvre Vo

A

227kts

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3
Q

Turb Air Vg

A

207kts

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4
Q

Gear Op Vle

A

150kts

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5
Q

Flaps Ext Vfe

A

150kts

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6
Q

Max Full Rudder Deflection Speed

A

150kts

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7
Q

Recommended Turb Pen Speed

A

180kts

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8
Q

Starter duty cycle limits

A

1st: 20sec on, 30sec cool
2nd: 20sec on, 2min cool
3rd: 20sec on, 5min cool
4th: 20sec on, 30min cool

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9
Q

Max ZFW

A

5850lbs

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10
Q

Max Ramp weight

A

6950lbs

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11
Q

Max T/O & LDG weight

A

6900lbs

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12
Q

Max TQ for Takeoff
(note x2)

A

100%

  • The PMU will govern Max TQ at 100, +/- 2%
  • TQ above 102% at a constant PCL setting & steady state flight is indicative of a governing system malfunction
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13
Q

TQ: Idle
(Note)

A

1-10%

Allowable TQ range with N1 stable and PCL at idle

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14
Q

TQ: Transient
(Note)

A

101-107% for 5sec

With the PMU on, TQ between 102-107% is possible following rapid PCL movement or aerobatic maneuvers.
TQ above 107% is a limiting system malfunction

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15
Q

Max ITT: Takeoff

A

820 deg C

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16
Q

Max ITT: Idle

A

750 deg C

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17
Q

Max ITT: Start

A

871-1000 deg C
5 sec

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18
Q

Max ITT: Transient

A

821-870 deg C
20 sec

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19
Q

Note wrt N1 limits

A

N1 values are presented for PMU on. With PMU off, N1 may vary from these values

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20
Q

Max N1: Take off

A

104%

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21
Q

N1: Idle (Ground & Air)

A

Ground: 60-61%
Flight: 67%

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22
Q

Max N1: Transient

A

104%

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23
Q

Note wrt Np limits

A

Avoid stabilised ground operation from 62-80% Np (to avoid ground resonance)

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24
Q

Np: Max Takeoff
(Note)

A

100%

With PMU off, the mechanical overspeed governor may allow Np to range from 98% to 102%.
A 20sec transient limit applies at 102%

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25
Np: Idle
46-50% (GND)
26
Np: Transient (Note)
110% to 20sec Permissible at any power setting for completion of inflight emergency.
27
Oil px: Takeoff Max (Note)
90-120psi Operation at oil px less than 90psi at idle or above is indicative of an oil system malfunction
28
MIN Oil px: Idle
90psi
29
MAX Oil px: Start
200psi
30
Oil px: transient (Note)
40-130 psi Operation in this range is only permitted during aeros or spins, and; 15-40psi for 5sec with PCL at idle.
31
Oil Temp: Max takeoff
10-105 deg C
32
Oil temp: Idle (Ground, Air, other (Note))
Ground: -40 to 105 deg C Air: 10 to 105 deg C 106 to 110 deg C acceptable for ground operation at and below 20% TQ
33
MIN Oil temp: Start
-40 deg C
34
Oil temp: Transient
106-110 Deg C for 10 mins
35
Max G: symmetric, clean
-3.5 to +7.0G
36
Max G: symmetric, gear/flap ext
0 to +2G
37
Max G: asymmetric, clean
-1 to +4.7G
38
Max G: asymmetric, gear/flap ext
0 to +2G
39
When are spins prohibited (6)
- Inverted Spins - Aggravated spins past 2 turns - Spins with the PCL > idle - Spins with gear/flap/ speedbrake extended - Spins below 10,000ft PA or >FL220 PA - Spins with PMU OFF
40
When are stalls prohibited
Inverted stalls
41
When are tail slides or abrupt snap maneuvers allowed?
Never, they are prohibited.
42
Aerobatic man. fuel imbalance limits
>50lbs fuel imbalance <150lbs fuel on lowest side Aeros prohibited
43
Intentional zero G is limited to?
5 sec
44
Max XWC: Wet Icy Dry
Dry: 25kts Wet: 10kts Icy: 5kts
45
Max T/O TWC
10kts
46
Max SFC wind, canopy open
40kts
47
Gen Load inflight (Note)
+50 to -2 Amps When checking Gen Voltage, whether on the ground or in flight, the PCL should be at least 80% N1 or greater
48
In flight Voltage
28 to 28.5V
49
Min Battery voltage to connect ext power
22V
50
Min Battery voltage for start
23.5V
51
Flight temp range
Min -54 to Max 43 deg C
52
Ground temp range
Min -23 to Max 43 deg C
53
Min/Max pilot weight
138 to 265.4lbs
54
Max time for inverted flight
60sec
55
Max weight baggage compartment
80lbs
56
Max lateral fuel imbalance
50lbs
57
Hydraulic normal operating range
3000psi, +/- 120psi
58
Engine oil level must be checked within ? mins of shutdown
30mins
59
Max IOAT for start
80 deg C
60
Note wrt checking Generator Voltage
When checking the voltage, both on the ground and in flight, PCL must be at least >80% N1 (or greater)