Limitations Flashcards
1
Q
MTOM?
A
40.600 lbs
2
Q
MLM?
A
34.150 lbs
3
Q
MRM?
A
40.750 lbs
3
Q
MZFM?
A
28.200 lbs
4
Q
MFM?
A
24.800 lbs
5
Q
With what configuration is holding in icing-conditions prohibited?
A
With Flaps extended
6
Q
VMOs/MMO?
A
0-8.000 ft - 300 KIAS
8.001-29.475 ft - 320 KIAS
Above 29.475 ft - 0.83 Mi
7
Q
VFEs?
A
F10 - 210 KIAS
F20 - 210 KIAS
F30 - 175 KIAS
8
Q
VLOs/VLE?
A
VLOret - 200 KIAS
VLOext - 250 KIAS
VLE - 250 KIAS/0.70 Mi
9
Q
VMCA F10/F20
VMCG F10/F20
Minimum V1
A
110/109 KIAS
115/114 KIAS
119 KIAS
10
Q
VRA?
A
265 KIAS/0.75 Mi (whichever is lower)
11
Q
Minimum Clean Speeds below FL100?
A
Below 34.000 lbs - 170 KIAS
Above 34.000 lbs - 180 KIAS
12
Q
Minimum Clean Speed between FL100 and FL300?
A
200 KIAS
13
Q
Minimum Clean Speed above FL300?
A
0.75 Mi
14
Q
Maximum Tire Speed?
A
182 ground speed
15
Q
Maximum Crosswind Components?
A
T/O on a dry or wet runway - 28 kts LDG on dry or wet runway - 24 kts FC 0.36-0.39 (medium-good) - 20 kts FC 0.30-0.35 (medium) - 15 kts FC 0.26-0.29 (medium-poor) - 10 kts LVTO RVR 250-400 m - 10 kts LVTO RVR 125-250 m - 5 kts T/O or LDG with NWS inoperative - 15 kts
16
Q
Maximum Tailwind Component for T/O or LDG?
A
10 kts
17
Q
Maximum Wind/Gust-speed for parking/ground movement?
A
45 kts
18
Q
OEI Speed and maximum distance from adequate aerodrome?
A
383 KIAS
779 NM
19
Q
Maximum Runway Slope?
A
+/- 2%
20
Q
Maximum Certified Altitude?
A
45.000 ft
21
Q
Maximum Altitude with Gear and/or Flaps Extended?
A
18.000 ft
22
Q
Maximum Altitude for T/O and LDG?
A
10.000 ft
23
Q
G-limits:
- Flaps 0
- Flaps >0
A
- 6/-1.0 g
2. 0/-0.0 g
24
Temperature Limit at MSL and below?
-40C to +50C
25
Temperature Limit FL010 to FL135?
-40C to ISA+35
26
Temperature Limit FL135 to FL350?
Decreasing linearly to -70C to ISA+35
27
Temperature Limit FL350 to FL410?
-70C to ISA+35
28
Temperature Limit FL410 to FL450?
Decreasing linearly to -75C to ISA+35
29
WING A/I and Type II, III and IV application - what to consider for T/O?
WING A/I ON just prior setting Takeoff Thrust
30
Which maneuvers are prohibited?
Aerobatics and Spins
31
What has to be considered when using air condition on ground?
Do not select TRIM AIR ONLY
If electrical power (BATT/EXT) is used for more than 30 minutes at +40C (acc. OM-B +30C) or above the pack must be running (ENG/APU On with AIR SOURCE on NORM or PACK ONLY)
32
Altitude Limitations for the use of Oxygen Masks?
Passenger Oxygen Masks not recommended for prolonged use above 25.000 ft;
Crew and Passenger Oxygen Masks not approved above FL400
33
Maximum Differential Pressures:
- Positive
- Negative
- Landing
- Ground (Taxi etc.)
- Maximum Positive 9.4 psi
- Maximum Negative -0.5 psi
- Maximum Landing 1.0 psi
- Maximum Ground (Taxi etc.) 0.1 psi
34
Minimum Autopilot Altitudes:
- CLB/CRS/DSC
- NPA/VIS Approach
- PA Approach below 3.5 deg
- PA Approach 3.5-4.49 deg
- 700 ft
- 200 ft
- 80 ft
- 160 ft
35
Maximum Approach Glidepath Angle?
4.49 deg.
36
Maximum Altitude without YD?
31.000 ft
37
Altitude for automatic 1/2 BANK engagement?
31.600 ft
38
Performance-, Approach- and Firecategory?
A, C, 4
39
Minimum Runway Width; to what surface is the operation restricted?
30 m (Code 3B); limited to paved surfaces
40
Do not use FMS for navigation unless receiving data from:
One VOR/DME
One IRS
Two DME
Two GNSS
41
RNP/RNAV and Datalink capabilities?
RNP 1/4/10, RNAV 1/5/10
| FANS 1/A, Link2000+, ADS-B/C
42
Which areas must be completely free of any deposits?
- Wings
- Control Surfaces
- Horizontal Stabilizer
- Vertical Stabilizer
- Upper Side of Fuselage
- Engine Inlets
43
Which deposits are allowed if CWO according to FCOM 1 are followed?
- Light Frost on Upper Side of Fuselage
| - Up to 3 mm Frost on Wing's Underside due to cold soaked fuel
44
When must ENG A/I be ON on ground and inflight?
Ground:
OAT +10C and below (visible moisture, contaminated surface)
Flight:
TAT +10C to SAT -40C (visible moisture, icing conditions, ICE DETECTED CAS)
45
When must WING A/I be ON on ground and inflight?
Ground:
OAT +5C and below (visible moisture, contaminated surface)
Flight:
TAT +10C to SAT -40C (visible moisture, icing conditions if less than 210 KIAS, ICE DETECTED CAS)
46
How do you know that SLD exist and what are the actions?
Ice accretion on Side Windows; ENG/WING A/I ON, leave icing conditions ASAP.
47
Approved Types of Operation for the CL350?
FAR25, two pilots, VFR, IFR, day, night, known icing (no FZRA, FZDZ), ditching with the relevant equipment on board, MNPS, RVSM, CAT I ILS (max. 4.49 deg.), LVTO 125 m
48
What to consider when using:
- STBY INST
- STBY Compass
- Do not use deviaiton bar when flying a LOC B/C Approach
| - L/R WSHLD/WINDOW OFF while reading the Compass
49
Maximum GEN amps?
Two or three GEN - 400 amp (i.e. normal operation in flight)
One GEN on Ground - 400 amp (i.e. APU operation)
One GEN in Flight - 500 amp (single GEN operation)
Transient for 5 min. - 600 amp
50
Minimum BATT temperature for T/O?
-20C
51
Spoiler Limitations?
- Do not select EMER unless required by procedure or in case of emergency
- Do not extend below 500 ft AGL
- Do not extend below Vapp +8 KIAS
52
Approved Fuels?
- JET A, JET A1, JET B, JP4, JP5, JP8
| - Mixing is permitted
53
Fuel Temperature Limitations for:
- Jet A
- Jet A1/JP5/JP8
- Jet B/JP4
- 30C to +50C (JET A)
- 35C to +50C (JET A1, JP5, JP8)
- 40C to +50C (JET B, JP4)
54
Altitude Limitations for:
- Russian TS1
- Jet B/JP4
- Russian TS1 maximum 37.000 ft if fuel temp. is above +30C
| - JET B/JP4 maximum 16.000 ft
55
Which restriction applies if the fuel temp. is above +45C?
Minimum 2.800 lbs fuel required.
| Minimum 1.000 lbs per side required if engines run more than 30 minutes.
56
Are you allowed to add unblended Prist?
No
57
Maximum Pressure for Re- and Defueling?
+55 psi, -8 psi
58
Restriction for FUEL XFERs during T/O?
GRAVITY XFLOW and XFER must be OFF for T/O
59
Maximum Fuel Capacity per Tank for:
- Gravity Refueling
- Pressure Refueling
- Minimum G/A fuel
- Gravity 6.500 lbs
- Pressure 7.075 lbs
- Minimum 500 lbs per tank
60
Maximum Fuel Imbalances:
- Below 4.700 lbs
- 4.700-10.000 lbs
- 10.000-13.700 lbs
- Above 13.700 lbs
- 600 lbs
- 450 lbs
- 315 lbs
- 250 lbs
61
Minimum Oil Temperatures for:
- Starting
- Above Idle (up to excl. CLB)
- T/O
- T/O without icing inhibitor (not applicable for JET A1)
- -40C
- +5C
- +15C
- +27C
62
Thrust Time Limits for:
- T/O
- APR Auto/Manual
- 5 minutes
| - 10/5 minutes
63
Thrust Reverser Limitations?
- Use only on paved surfaces
- No Touch and Go's
- No Powerback
- Do not attempt to deploy in flight
- No REV above idle below 40 KIAS
- Maximum REV Thrust is automatically reduced below 85 KIAS
64
Engine and APU Consecutive Start Limitations?
Engine:
3 consecutive starts - each followed by 30 seconds cranking.
15 minutes cooling period.
APU:
3 consecutive starts - each followed by 1 minute cooling period.
20 minutes cooling period.
2 more consecutive starts with 1 minutes cooling period.
40 minutes cooling period.
Maximum 6 good starts with 10 minutes intervals - then 60 minutes cooling period.
65
Engine cranking limits?
Maximum 5 minutes followed by 15 minutes cooling
66
Engine and APU model?
- AS907-2-1 (HTF7350)
| - Honeywell 36-150BD
67
APU Altitude Limitations for:
- Operation
- Generator
- Bleed for ECS and ENG Start
- 37.000 ft
- 30.000 ft
- 20.000 ft
68
APU Altitude Limitations for:
- Ground Start
- Air Start
- 14.000 ft
| - 30.000 ft
69
Minimum and Maximum Temperature for Engine Starting?
-40C to +50C
| Every 1.000 ft maximum temperature decreases by 2C
70
APU ON or OFF during de/anti-Icing?
OFF
71
When to abort the APU Start?
If after 30 seconds RPM is not >30%
72
What is prohibited on ground above 9.000 ft - and why?
Starting the LH ENG with the APU.
| Ducting from APU to LH ENG is too long to create enough pressure.
73
Maximum Airspeed for APU Air Start?
285 KIAS
74
If the first APU Air Start is unsuccessful:
No further attempt before landing
75
Maximum APU EGT for:
- Starting
- Normal Operation
- 973C
| - 718C
76
Maximum APU RPM?
108%
77
Are you allowed to use the secondary flightplan?
No
78
CWO have to be followed according to _______.
FCOM 1
79
The effect of landing gear retraction on the CG position is __________.
Negligible
80
Determined Maximum Distance from an Adequate Aerodrome?
120 minutes
81
What is prohibited to use during QFE Operation?
- SVS
| - VNAV
82
What is prohibited while using TAWS and TCAS?
Do not use TAWS for navigation.
| Do not maneuver based on information presented on the TFC map.
83
Approximate dimensions of the CL350?
22 m x 22 m x 7 m
84
Minimum Temperature to start the APU?
-40C
85
Minimum Cabin Temperature for the O2 Mask test?
+15C
