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Cessna C J ( N525MB) > LIMITATIONS / MEMORY ITEMS > Flashcards

LIMITATIONS / MEMORY ITEMS Flashcards

1
Q

Vne

A

263kts

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2
Q

Vlg

A

186kts

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3
Q

Vfe ( approach)
Vfe ( landing)

A

200 kts
161 kts

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4
Q

Vlg-
Gear warning-

A

186kts
130kts

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5
Q

ENGINE TEMP LIMITS:

A

START - 1000
MAX TKO - 820
MAX CONTINUOUS- 796
IDLE - 620

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6
Q

Vmcg-
Vmca-

A

95
92

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7
Q

Vmo < FL305
Mmo - FL305-FL410

A

263kts
.71 Mach

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8
Q

Va

A

180kts

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9
Q

Max operational alt

A

14,000

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10
Q

Max ramp:
Max TKO:
Max landing:
Zero fuel:
BEW:

A

10,500
10,400
9,700
8,400
6,500

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11
Q

Baggage, nose
Baggage, aft cabin
Baggage, tail

A

400
100
300

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12
Q

Max runway contamination:

A

0.75”

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13
Q

Max ambient temp ( SL )
Min temp

A

39C
-53C

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14
Q

Max tailwind

A

10 kts

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15
Q

Starter limitation
Battery limitation

A

3 starts in 30 mins
3 starts per hour

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16
Q

Max Gen load

A

300A on ground
250 for up to15 min
450 for up to 2 mins

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17
Q

Max tire speed

A

165kts

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18
Q

Tire pressures

A

Nose-120 +/- 5
Mains-98 +/- 5

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19
Q

Wnshld heat ( on ground)

A

2 mins

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20
Q

Engine FIRE/ FAIL below V1

A

Brakes- APPLY
Throttles-IDLE
Speedbrakes-EXTEND

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21
Q

Engine FIRE / FAIL above V1

A

Maintain directional control
Vr / Rotate / Positive rate
Gear up, climb V2 to 1500AGL
V2+10- Flaps up
Checklist

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22
Q

Engine FAIL during coupled approach

A

Increase power on operating engine as required
Airspeed Vapp
Flaps APPROACH

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23
Q

Engine FIRE

A

Affected throttle IDLE
If fire light stays on..
Affected throttle CUTOFF
Engine FIRE switch - LIFT COVER and PUSH
Either fire bottle switch - PUSH

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24
Q

Emergency restart

A

Ignitions- BOTH ON
Fuel boost- BOTH ON
Throttles- IDLE
Airspeed ( if sufficient altitude exists ) 200 kts

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25
Electrical smoke/ fire
O2 mask - DON/ EMER O2 mic switch - MIC OXY MASK Checklist ( F1)
26
CABIN ALT
O2 Mask - DON/ EMER O2 mic switch - MIC OXY MASK EMER descent - as required Ensure PAX O2
27
Emergency descent
AP/ TRIM DISCONNECT - PUSH and RELEASE Throttles - IDLE Speedbrakes - EXTEND Roll - <40 Pitch - 20/25 nose down Transponder- 7700
28
AP malfunction
AP/ TRIM DISCONNECT- PRESS AND HOLD
29
Elevator trim runaway
AP/ TRIM DISCONNECT- PRESS and RELEASE THROTTLES - AS REQUIRED SPEED BRAKES - AS REQUIRED PITCH / TRIM CB ( left panel) - PULL
30
EMER Evac
Parking brake - SET Throttles - IDLE Fire switches - BOTH PRESS Battery - OFF ELT - Ensure activated for SAR Egress - Cabin door OR Emergency exit depending on outside conditions
31
Stall/ Missed approach
PICKLE, POWER, PITCH FLAPS 15 POSITIVE RATE - GEAR UP CLIMB V2 V2+10- FLAPS UP MISSED APPROACH CHECKLIST
32
TAMARACK WINGLET FAIL
AIRSPEED - < 140kts WINGLET CBs - ( right side) PULL
33
FUEL QUANTITY
3200# flight planning ( 3220 at collar, 3440 at top)
34
LO FUEL LEVEL: LO FUEL PRESS: MAX IMBALANCE:
170#/side 5 psi 200#
35
MAX CABIN DIFF:
8.5 psi
36
MAX CABIN ALT
8000ft
37
ENGINES:
Williams FJ44-1A 1900# thrust ea.
38
If door seal fails, what keeps cabin pressure in?
Secondary rigid seal. 02 MASK 02 MIC SWITCH Descend below FL310 ASAP CONTINUE DESCENT ( expedited) below 15,000 feet ASAP
39
Ammeters must be paralleled and within:
10% of total load
40
Engine starts above 10,000 MSL:
Must use EPU
41
SELECT XFEED TO:
THE “ HEAVY “ WING
42
BOOST PUMPS ON AUTOMATICITY AT:
START XFEED LOW PRESS
43
UN COMMANDED XFEED
TURN ON BOTH BOOST PUMPS
44
MAX FUEL IMBALANCES:
200# 600# ( emergency)
45
WHAT DOES THE AGB DRIVE?
OIL, FUEL, & HYDRAULIC PUMPS STARTER / GENERATOR
46
OIL TEMP LIMITS:
10 - 121C
47
Describe FIRE DET system:
Helium filled gas inside a stainless steel tube that surrounds the burner can. When there is sufficient heat to expand the gas to a certain point, the pressure sets off the ENGINE FIRE light.
48
What actions occur when ENGINE FIRE switch is pressed?
Fuel, Oil, Hydraulic valves shut Generator field relay open / Generator offline Fire bottles armed
49
BLD AIR O’HEAT
Air leaving the bleed air pre-cooler has exceeded 540F.
50
What are the components of the ANTI-ICE system?
1.)Pitot/static, AOA vane, and engine pylons heated electrically. 2.)Wings, Windshield, engine inlets, bullet nose, and stators heated w/bleed air. 3.)Windshield alcohol 4.)Pneumatic boots for HSTAB
51
Min N2 for ANTI- ICE:
70%
52
Wing heat limit ( on ground)
1 min *( A pre-TKO check - using the “ Clean A/C Concept” at 5 mins before TKO, should eliminate the need for using wing heat on ground.)*
53
IN THE EVENT OF DC FAIL, WHICH VALVES FAIL OPEN? WHICH VALVES FAIL CLOSED?
Wing and engine A/I valves fail OPEN
54
HSTAB BOOTS:
Inflated with 16 psi bleed air Do NOT activate at temps below -35 RAT
55
If HSTAB has become iced or boots have failed:
FLAPS are limited to 15* for LDG.
56
EMER PRESS- ( Respective valve failure position)
W/S anti-ice - OPEN EMER - OPEN LH, RH Bleed air shut off and FCV - CLOSED
57
ANTI-ICE SYSTEMS ARE:
HOTWINGS W/S ALCOHOL ELECTRIC P/S PNEUMATIC BOOTS ON HSTAB
58
WING HEAT ON GRND:
1MIN
59
ICING PRE- TKO CHECK:
Clean aircraft concept within 5 min before TKO
60
WHAT POSITION DO WING & ENGINE VALVES FAIL WHEN DC HAS FAILED?
OPEN
61
HSTAB BOOT LIMITATION:
DO NOT OPERATE AT TEMPS < -35 RAT
62
DURING DC FAIL, EMER PRESS VALVE FAILS: AND FCV FAILS
OPEN CLOSED
63
HOW IS W/S HEATED DURING DC FAIL?
MANUAL BLEED AIR CONTROL KNOBS W/S ALCOHOL
64
AIR DUCT O’HEAT:
TEMP HAS EXCEEDED 300*F ENTERING CABIN
65
IN MANUAL MODE TEMP CONTROL, WHAT SYSTEM FAILS?
AUTOMATIC AIR DUCT OVERHEAT PROTECTION THE ANNUNCIATOR, ( AIR DUCT O’HEAT ), WILL ILLUMINATE HOWEVER
66
WHAT DRIVES THE HYD PUMPS?
THE ACCESSORY GEAR BOX
67
WHAT SUBSYSTEMS ARE OPERATED BY THE HYD PUMPS?
FLAPS SPEEDBRAKES LANDING GEAR ATTENUATORS

Cessna C J ( N525MB) (1 decks)

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