LIMITATIONS Flashcards
(79 cards)
1
Q
Minimum runway width approved for takeoff and landing
A
100’
2
Q
Maximum pressure altitude for takeoff and landing
A
8,000’
3
Q
Maximum ambient temperature approved for takeoff and landing
A
ISA +35
Limited to maximum OAT of 51
4
Q
Minimum ambient temperature approved for takeoff
A
-40C
5
Q
Maneuvering limit load factors:
Flaps retracted
Flaps extended
A
-1.0 to +2.5G
0.0 to +2.0G
6
Q
Maximum positive differential pressure
A
8.7psi
7
Q
Maximum negative differential pressure
A
-0.5psi
8
Q
Maximum pressure differential during ground maneuvering
A
0.1psi
9
Q
Maximum differential pressure during initial landing
A
1.0
10
Q
Minimum temperature for cold-soaked APU starting on the ground
A
-40C
11
Q
APU Maximum RPM
A
106%
12
Q
APU Maximum EGT
Normal
All Conditions
A
Ground- 682-789C
Flight - 773-806C
1038C
13
Q
Maximum APU starting altitude
A
37,000’
14
Q
Maximum APU operating altitude
A
41,000’
15
Q
Maximum Starting altitude using APU
A
21,000’
16
Q
APU EGT indications Deg C
Green
Red
A
0-806C
807C
17
Q
APU RPM indications %
Green
Red
A
0-106
107
18
Q
AC Electrical Load
Altitude
Load Limit
A
0-41,000’
40kVA
19
Q
Maximum permissible DC Load on each TRU
A
120 Amps
20
Q
Engine Indications
N1 % rpm
Red
Amber
Green
A
99.5
NA
0-99.4
21
Q
Engine Indications
N2 % rpm
Red
Amber
Green
A
99.4
NA
0-99.3
22
Q
Engine Indications
ITT deg C
Red
Amber
Green
A
Variable
NA
Variable
23
Q
Engine Indications
Oil Temp Deg C
Red
Amber
Green
A
164
156 - 163
-41 to 155
24
Q
Engine Indications
Oil Press psi
Red
Amber
Green
A
0-24
Variable
Variable
25
During all starts do not exceed ? for 2 minutes, or ?
75% N1, until all engine indications are normal - which ever is longer
26
Operate engines at or near ? for ? prior to shutdown
note: ?
idle, for 2 minutes
Taxi time at a stabilized 80% N2 or below may be credited towards the 2 minute cool down
27
Engine Operating Limits - N1
Idle
Max Continuous
Normal TO (TOGA)1
APR (Max Power)2
20-25%
99.5%
TO - 99.5% - 2 engines is limited to 5 minutes
APR - 99.5% - 1 engine is limited to 10 minutes
28
Engine Operating - Limits ITT
Ground Start
Assisted Air Start
Windmill Start
Max Continuous
NORMAL TO (TOGA)
APR (MAX POWER)
815C
815C
927C
960C
963C - 2 minutes, 947C - 5 minutes
1006C - 2 minutes, 990C - 5 minutes
29
Engine Operating Limits - Oil Press
Ground Start
Assisted Air Start
Windmill Start
Idle
Max Continuous
Normal TO (TOGA)
APR (MAX POWER)
182PSI, 95psi after 10 minutes
182psi, 95psi after 10 minutes
182psi, 95psi after 10 minutes
25-60psi, 25-95psi with temp <60C
45-95psi
45-95psi
45-95psi
30
Max transient oil pressure ? when temp ?
156psi when <60C
31
Define cold soaked airplane?
What must we do?
-30C or below for more than 8 hours
Must motor engine for 60 seconds and verify FAN rotation
Must exercise thrust reversers until cycle time is 2 seconds or less
32
Minimum oil temp for starting
-40C
33
Max continuous oil temp
155C
34
Max permissible oil temp
163C 15 minutes maximum
35
Oil pressure Steady State minimum
25psi
36
Takeoff power oil pressure min
45psi
37
Max continuous oil pressure
95psi
38
Max transient oil pressure
156psi when oil temp <60C
39
Max oil pressure transient after cold start
182psi 10 minutes max (or amber dashes)
40
After cold start engine must remain at idle until?
oil pressure returns to normal range
41
Max oil consumption
6.4 ounces per hour - 0.5 gallons
42
When must continuous ignition be on?
-TO or landing on contaminated runways
-TO with XWind 15 knots or greater
-Flight thru mod or higher intensity rain
-Flight thru moderate or higher intensity turbulence
-Flight in vicinity of Thunderstorm
43
Dry Motoring cycles
90 seconds - 5 minutes off
30 seconds - 5 minutes off
44
Engine Relight Limits
Windmilling - Relight Envelope
Starter Assist - Relight Envelope
All Engine-Out - Relight Envelope
0-25,000' - 250KIAS to VMO from 7.2% N2 MINIMUM
0-21,000' - VREF to VMO form 0-45% N2
0-10,000' - FADEC rapid relight capability has been demonstrated at 200 KIAS for up to 15 second fuel interruptions
45
Reverse Thrust is prohibited -
In flight
46
When can we NEVER attempt a go around?
Once the thrust reversers have been deployed
47
During preflight check of the thrust reversers, reverse thrust must be limited to
reverse idle
48
Max Pressure refueling
Left/Right Tank
Center Tank
Total
7492/7492
4610
19594
49
Max Gravity Refueling - 700/900
Left/Right Tank
Center Tank
Total
7290/7290 - 7405/7405
14580 - 14810
50
TO with fuel temp indications below ? is prohibited
5C
51
TO with Bulk Fuel temp below ? is prohibited
Jet A
Jet A1
JP5
JP8
-30C
-37C
-36C
-37C
During flight bulk fuel should remain above these as well
52
When using Jet A with ambient temp of -30C or below, bulk fuel temp prior to flight must be verified to be above ?
-29C
53
Define Ground Contamination
Runways, ramps or taxiways with surface snow, ice, slush or standing water
54
Define Visible moisture
Visible moisture or precipitation in any form (such as fog with visibility of 1 mile or less, mist, rain, snow, sleet, and ice crystals or clouds inflight)
55
When type IV anti-icing fluids have been applied when must the wing anti-ice system be selected and confirmed on?
Just prior to TO
56
TO is permitted with frost adhering to
-The upper surface of the fuselage and/or
-The underside of the wing (Max 1/8") caused by cold soaked fuel
57
Frost on the upper surface is not considered critical if -
It is possible to distinguish surface features (markings and lines)
58
Single engine taxi is prohibited when
Ramps or taxiways are contaminated with snow, slush, or ice, or when snow or other freezing/frozen precipitation is present
59
Tactile check of the ? is required when
Wing leading edge, wing forward upper surface, and wing rear upper surface
-The OAT is 10C or less
-Bulk fuel temp is 0C or less
-The atmospheric conditions have been conducive to frost formation
-Ice and frost may continue to adhere to wing surfaces for some time even at OAT above 10C
60
Supercooled Large Droplet Icing conditions are indicated by?
Ice accretion on the side windows
-Wing and Cowl anti-icing systems must be ON in SLD icing conditions
-LEAVE ICING CONDITIONS WHEN SIDE WINDOW ICING OCCURS
61
Minimum brake cooling time
15 minutes and all BTMS indicators must be green and not increasing
62
Braking action effect on Tailwind and XWind
Good/5
Good-Medium/4
Medium/3
Med to Poor/2
Poor/1
Nil/0
Tailwind <10, Xwind <27
<10, <27
<5, <15
<5, <10
0, <10
See FOM
63
CAT II approaches are prohibited when braking action is reported as
less than "Medium"
64
TO and Landing on contaminated runways
Standing Water
Slush
Wet Snow
Dry Snow
TO - Landing
1/2" - 3/4"
9/16" - 7/8"
9/16" - 7/8"
3" - 3 3/4"
65
Operation with the autopilot engaged prohibited at altitudes below ? except when
600'
-Visual FMS and non-precision approaches 400'
-GS > 3.5deg <4.0 deg airport elevation <4,000' = 120'
-Precision approach PAR/ILS or APV min height on single engine is 110
66
Use of ? Mode with the FD or autopilot during approach is not permitted
Speed Mode (DES or IAS)
67
When conducting an approach with a T-Transition utilizing VNAV indicated airspeed at the initial approach fix must be
210KIAS or less
68
What type of approaches using the FMS are prohibited?
RNAV (RNP), ILS, LOC, LOC/BC/ LDA, and SDF
69
When is the use of VNAV CLB prohibited
When airspeed is displayed in Mach
70
Use of VNAV vertical guidance for a ? approach is prohibited
V-MDA
71
Minimum Flight Weight 700/900
42,000 / 45,000
72
Minimum Operating Weight 700/900
39385 / ---
73
Maximum Weight in FWD Cargo 700/900
1,000 / 1,700
74
Max Weight in AFT Cargo (N547-615, 629-635)
900s
3,740
75
Max Weight Aft Cargo (N616-619, 636-649)
900s
3,300
76
Max Weight Aft Cargo (N500-524)
700s
4,375
77
Max Weight Aft Cargo (N525-546)
700s
3,740
78
Max Weight Aft Cargo (N702-725)
700s
3,300
79
