Challenger 650 Initial > Warnings/Limitations > Flashcards

Warnings/Limitations Flashcards

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1
Q

45 Min IFR Fuel Reserve

A

2,019 lbs

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2
Q

Hot Spare Fuel

A

8,500 lbs

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3
Q

EMER Fuel

A

1,500 lbs

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4
Q

Inclement Weather Fuel

A

6,500-8,500 lbs

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5
Q

Minimum Runway Length

A

4,500 FT (1)

1) Min distance required for release only. May use LPA upon arrival

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6
Q

Min Runway Width

A

75 FT

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7
Q

Max Runway Slope

A

+/- 2%

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8
Q

Ops Review Required

A

When runway is contaminated and less than 5,800 FT

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9
Q

RVSM Operations

A

Requires:
- Autopilot (1)
- Altitude Alerting Device (1)
- AFDs displaying primary altimeters (2)
- ATC altitude reporting transponder (1)
- Air Data Computers (2)
- Pitot probe heaters (2) on ADC in use

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10
Q

Wifi Limitations

A

Prohibited:
- During de-ice ops
- 100 ft or less from a building that is taller than the aircraft

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11
Q

Zero Fuel Weight

A

32,000 lbs

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12
Q

Max Baggage Compartment Weight

A

900 lbs

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13
Q

Max Pressure Altitude Takeoff/Landing

A

10,000 FT

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14
Q

Max Landing Gear Extended Altitude

A

20,000 FT

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15
Q

Minimum Altitude for Spoilers

A

300 FT AGL

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16
Q

Minimum Temp for Takeoff

A

-40C

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17
Q

Maximum Temp for Takeoff/Landing

A

ISA +35

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18
Q

VLO

A

197KTS/0.6M

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19
Q

Maximum Tire Speed

A

182 KTS

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20
Q

Minimum Speed Spoilers Deployed

A

VREF + 10

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21
Q

Maximum Pressure Differential

A

9.2 PSI

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22
Q

Maximum Negative Relief

A

-0.5 PSI

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23
Q

Maximum Pax Count (Incl Children under 2)

A

14*

*Limited by number of oxygen masks

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24
Q

APU Starting (Batteries On Ground/Normal In-Flight)

A
  • 3 30 second attempts of continuous cranking followed by 20 mins of cooling
  • 2 additional 30 sec attempts
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25
APU Starting (Using Ground Power)
- 2, 15 second attempts followed by 20 mins of cooling - 2 additional 15 sec attempts. If unsuccessful, do not attempt again for 35 mins
26
Minimum Temp for APU Start (On Ground)
-40C
27
Maximum Temp during APU Start
974C
28
Single Engine Inflight Restart
APU use prohibited
29
APU Time Limitations
Prior to ETD: 75 mins After Engine Off: 30 mins Turn Time: <120 mins - allowed, >120 mins - shut down PIC may modify for: - Temps <40F and >80F - Training - Sliding departures - Airport restrictions - Oceanic Flights - Cleaning - FOM policies - Customs
30
Autopilot Minimum Engagement Height (After Takeoff)
320 FT AGL
31
AC Gen Load Limit (0-22k FT)
Main: 30kVA APU: 30 kVA
32
AC Gen Load Limit (20,001-35k FT)
Main: 30kVA APU: 0
33
AC Gen Load Limit (>35k)
Main: 25kVA APU: 0
34
DC TRU Load Limit
100 amps
35
Pressure Fueling Limits
Left Main: 4,860 lbs Right Main: 4,860 lbs Auxiliary: 7,168 lbs Tail: 3,112 lbs
36
Max Fuel Imbalance Gravity Fueling
Left and Right Main: 2,500 lbs
37
Gravity Fueling (Aircraft Level)
Reduce pressure fueling by 7%
38
Minimum Go-Around Fuel
500 lbs per tank(1) 1) Bank and pitch must be limited to wings level and 10 degrees nose up
39
Auxiliary Tank Limitations
- If Aux tank <= 500 lbs, takeoff permitted: - Each wing tank contains >= 1,500 lbs - Tail Tank is empty - If Aux tank contains > 500 lbs, reference chart in AOM 12.12.1
40
Fuel Temp Limit
>= 5C - Bulk fuel temp must remain above applicable fuel freezing point
41
Fuel Jettison
Flaps = 0 - Do not jettison in known lighting conditions
42
Fuel Transfer
Determine Aux Quantity If Tail: >1,200 Then Aux: 2.75 x Tail Tank Quantity If Tail: <1,200 Then Aux: 2.2 x Tail Tank - Fuel transfer must be off for takeoff - During normal ops, tail tank transfer must be auto - Do not manually transfer tail tank >7,000 in aux tank
43
Icing Conditions Exist
On Ground: - Contaminated runways or: - SAT <= 10C - Visible moisture In-Flight: - EICAS ICE message or: - TAT <=10C - Visible moisture except SAT <= -40C
44
Probes
On ground, limit probe heat ON to 2 mins when TAT >= 15 C
45
Display Unit Operating Temperature
Do not power display units on ground when temp >40C for >30 minutes: - 1 air cond pack is operating - Pax door is closed
46
Integrated Flight Information System (IFIS)
Use Prohibited: - IFIS CHARTS unless database current - Geopolitical boundaries and controlled and special use airspace on MFD MAP used for nav - Aircraft symbol for electronic approach and taxi charts for in-flight nav or precision man on ground
47
Electronic Flight Information System (EFIS)
- Do not use MAP PLAN display for nav while operating north of 70N or south of 70S - OBSTACLE symbols on MFD map are for situational awareness only
48
VNAV Limit
Do not use VNAV: - When using QFE baro altitudes - After go-around until missed approach procedure is complete
49
Engine Start Limit (N1/N2/ITT/Time)
N1: - N2: 20% ITT: 903C Time: 50 seconds - Left and right N2 must not differ by more than 2% at ground idle - When engine is cold soaked -30C for >8 hours: - Motor engines for 60 seconds and verify rotation - Actuate thrust reversers until stow/deploy cycles are less than 5 secs
50
Engine Acceleration Limit (N1/N2/ITT/Time)
N1: - N2: - ITT: 930C Time: 5 sec
50
Engine Max Continuous Limit (N1/N2/ITT/Time)
N1: 98.6 N2: 99.2 ITT: 899C Time: -
51
Engine Takeoff Limit (N1/N2/ITT)
N1: 96.2 N2: 98.3 ITT: 884C (5 mins/red) 900 C (2/5/red)
52
Engine Max Takeoff OEI with APR operating (N1/N2/ITT)
N1: 98.6 N2: 99.4 ITT: 899C (5 mins) 928C (2/5/red)
53
Autothrottle Restrictions
- During OEI - When manually entering FMS Thrust Target (TGT) - During takeoff when TGT selected on FMS PERF page - When max cont thrust selected on FMS PERF page - During touch and go landings - During go-arounds - When APR selected on FMS PERF
54
Min Oil Temp for Start
-40C
55
Max Oil Temp (Continuous)
155C
56
Max Oil Temp (Permissable)
163C
57
Min Oil Pressure (Idle)
25 PSI
58
Max Continuous Oil Pressure
115 PSI
59
Max Oil Consumption
0.05 gal/hr (0.2 qt/hr)
60
Engine Starter Limit
3 consecutive cycles with 5 mins cooling between additional - limit 60 secs per cycle - ITT must be 120C or less for all ground starts - Do not use starter if N2 > 55%
61
Dry Motor Limit
Start: First Max Time: 90 sec Followed by: 5 mins off Start: Second and subsequent Max Time: 30 sec Followed by: 5 mins off - Performed with ignition off and thrust levers shut off - May be used for engine ground or air start
62
Thrust Reversers
< 60 KT, max N1 = 60% - Ground use only - Nose wheel must be on ground
Challenger 650 Initial
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