LIMITATIONS / MEMORY ITEMS Flashcards
(84 cards)
1
Q
Vne
A
263kts
2
Q
Vlg
A
186kts
3
Q
Vfe ( approach)
Vfe ( landing)
A
200 kts
161 kts
4
Q
Gear warning-
A
130kts
5
Q
ENGINE TEMP LIMITS:
A
START - 1000
MAX TKO - 820
MAX CONTINUOUS- 796
IDLE - 620
6
Q
Vmcg-
Vmca-
A
95
92
7
Q
Vmo < FL305
Mmo - FL305-FL410
A
263kts
.71 Mach
8
Q
Va
A
180kts
9
Q
Max operational alt ( TKO & LDG )
A
14,000
10
Q
Max ramp:
Max TKO:
Max landing:
Zero fuel:
BEW:
A
10,500
10,400
9,700
8,400
6,500
11
Q
Baggage, nose
Baggage, aft cabin
Baggage, tail
A
400
100
300
12
Q
Max runway contamination:
A
0.75”
13
Q
Max ambient temp ( SL )
Min temp
A
39C
-53C
14
Q
Max tailwind
A
10 kts
15
Q
Starter limitation
Battery limitation
A
3 starts in 30 mins
3 starts per hour
16
Q
Max Gen load
A
300A on ground
250 for 15 min
450 spike for 2 mins
17
Q
Max tire speed
A
165kts
18
Q
Tire pressures
A
Nose-120 +/- 5
Mains-98 +/- 5
19
Q
Wnshld heat ( on ground)
A
2 mins
20
Q
Engine FIRE/ FAIL below V1
A
Brakes- APPLY
Throttles-IDLE
Speedbrakes-EXTEND
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 ( A1)
22
Q
Engine FAIL during coupled approach
A
Increase power on operating engine as required
Airspeed Vapp
Flaps APPROACH
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
24
Q
Emergency restart
A
Ignitions- BOTH ON
Fuel boost- BOTH ON
Throttles- IDLE
Airspeed ( if sufficient altitude exists ) 200 kts
25
Electrical smoke/ fire
O2 mask - DON/ EMER
O2 mic switch - MIC OXY MASK
Checklist ( F1)
26
CABIN ALT ( Cabin alt has exceeded 8500’)
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
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:
185#/side, ( plus or minus 15 )
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?
…Memory items if at high alt?
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, heated w/bleed air.
3.)Windshield alcohol ( backup system )
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?
W/S, Wing, and Engine A/I valves fail OPEN
FCV fail CLOSED
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
In EMER PRESS, which valves fail OPEN -
Which valves fail CLOSED -
W/S and EMER - OPEN
LH, RH BLEED AIR and FCV - CLOSED
57
ANTI-ICE SYSTEMS ARE:
HOTWINGS / ENGINE INLETS / GEN COOLING DUCT
W/S ALCOHOL
ELECTRIC PITOT STATIC / PYLON INLETS
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 SOV VALVES FAIL? ( when DC has failed )
CLOSED
61
HSTAB BOOT LIMITATION:
DO NOT OPERATE AT TEMPS < -35 RAT
62
DURING DC FAIL…
EMER PRESS VALVE FAILS:
LH, RH BLEED AIR SOV 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 CONTINUALLY ILLUMINATE UNTIL SYSTEM RESET
66
WHAT DRIVES THE HYD PUMPS?
THE ACCESSORY GEAR BOX
67
WHAT SUBSYSTEMS ARE OPERATED BY THE HYD PUMPS?
FLAPS
SPEEDBRAKES
LANDING GEAR
ATTENUATORS
68
Engine starting limits: ( Wind )
Max tailwind -10kts
Max Xwind - 12kts
69
Max time for light off during start:
10 sec
70
Min ambient temp for batt start
-18
71
EPU ( APU) settings
28/1100
72
Hydraulic fluid:
Mil- H- 83282
73
Describe an “ open center” hydraulic system:
W/ engines running, hyd pumps generate a circular low pressure flow. When a sub-system is selected, the bypass valve closes, pressurizing the whole system which directs pressure towards the sub-system selected. The load builds, and the pressure moves the physical parts of the selected sub- system.
*This underscores the importance of airspeed limitations WRT Gear and Flaps.*
74
Describe engine start sequence:
Starter- engage
Rotation / “8 over the gate” / Fuel flow / Light off
ITT rise / Oil pressure rise / 45%N2 - Starter cutout / Stabilized.
GOOD START.
75
How many ignitor boxes per engine?
2 primary, 2 redundant.
Engine can run with only one.
76
When does engine ignition come on automatically?
START and ENGINE ANTI-ICE selected ON
77
To abort a start:
THROTTLES OFF
MOTOR ENGINE 15 SECONDS
STARTER DISENGAGE
78
What is a HOT START?
ITT RAPIDLY APPROACHING 1000 DEGREES
79
WHAT IS A FALSE START?
NO ITT or FUEL FLOW WITH IN 10 SECONDS
80
What is a hung start
SLOW or NO ROTATION AFTER IIT INCREASE
81
Max ALT limit valve closes at:
13000
82
Oil resivoir capacity:
2 quarts per engine
83
Thrust Attenuators
Electrically deployed
Hydraulically stowed
Protected against in flight deployment by squat switch
Reduce ground idle thrust by 50%
84
ANTI-DROPS OUT AT:
12 KTS
