Aircraft Limitations Flashcards
(207 cards)
1
Q
Types of Operations
A
VFR
IFR
Icing Conditions
CAT I and II
RVSM
RNP
Extended Overwater EOW
2
Q
LR Maximum Ramp Weight (MRW)
A
85,870 lbs
3
Q
LR Maximum Takeoff Weight (MTOW)
A
85,517 lbs
4
Q
LR Maximum Landing Weight (MLW)
A
74,957 lbs
5
Q
LR Maximum Zero Fuel Weight (MZFW)
A
69,886 lbs
6
Q
Minimum Flight Crew
A
Pilot and Copliot
7
Q
Max Takeoff and Landing Tailwind Component
A
10 knots
8
Q
Max Runway Slope
A
+/-2%
9
Q
Runway Surface Type
A
Paved
10
Q
Flap Maneuvering Load Acceleration Limit - Flaps Up
A
-1.0 G to +2.5 G
11
Q
Flap Maneuvering Load Acceleration Limit - Flaps Down
(1, 2, 3, 4, 5 and Full)
A
0.0 G to +2.0 G
12
Q
Max Operating Altitude
A
41,000’
13
Q
Max Takeoff and Landing Altitude
A
10,000’
14
Q
Min Takeoff and Landing Altitude
A
-1,000’
15
Q
Max Ambient Air Temperature for takeoff, landing and ground starts (decreases with altitude)
A
52 degrees C
16
Q
Max Flap Extension Altitude
A
20,000’
17
Q
Max Latitude for Stationary Alignment
A
78.25 degrees North
78.25 degrees South
18
Q
Minimum Takeoff Temperature / Landing Below __ degrees C, you may not takeoff without further maintenance inspection
A
-40 degrees C SAT
19
Q
Minimum Ambient Temperature for Operation on Ground
A
-54 degrees C
20
Q
Temperature Compensation Baro-VNAV Operation Must Be:
A
- Coordinated with ATC
- Used for operation outside the temperature limits published the approach procedure
21
Q
Max Operating Airspeed Abbreviation
A
Vmo
22
Q
Max Operating Mach Number Mmo
A
.82M
23
Q
Maximum Airspeed for RAT Operation
A
Vmo / Mmo
24
Q
Max Windshield Wiper Operation Speed
A
253 KIAS
25
Max Gear Extension Speed Vloe
250 KIAS
26
Max Gear Extended Speed (Vle)
250 KIAS
27
Max Gear Retraction Speed (Vlor)
250 KIAS
28
Flaps 1
230 KIAS
29
Flaps 2
215 KIAS
30
Flaps 3
200 KIAS
31
Flaps 4
180 KIAS
32
Flaps 5
180 KIAS
33
Flaps Full
165 KIAS
34
Max Operating Speed Up to 8,000’
300 KIAS
35
Max Operating Speed 8,000’-10,000’
300 to 320 KIAS Increases Linearly
36
Max Operating Airspeed 10,000’ - FL290
320 KIAS Vmo
37
Max Operating Airspeed FL290 - FL410
.82M Mmo
38
Define Icing Conditions
OAT on the ground or TAT inflight is 10 degrees C or less with visible moisture in any form
39
Maximum Fuel Capacity
20,935 lbs Total
40
Unusable Fuel Quantity per Tank
75 lbs
41
Maximum Fuel Imbalance
794 lbs
42
Minimum Fuel Tank Temperature
-37 degrees C
43
Crossfeed Operation Limitation
Must be OFF for takeoff and landing
44
Max Differential Pressure
8.4 PSI
45
Max Differential Overpressure
8.8 PSI
46
Max Differential Negative Pressure
-0.5 PSI
47
Max Differential Pressure for Takeoff and Landing
0.2 PSI
48
Max Altitude for Single Pack Operation
FL310
49
Brake Temperature Limitation
Do not takeoff with brake temperatures in the amber
50
Thrust Reverser Limitations
DIMPFNG
Do not attempt a go-around (after deployment)
Idle thrust by 30 KIAS (translating cowl closed)
Min reverse thrust by 60 KIAS (translating cowl open)
Power back prohibited
Full Stop Landings
Not Authorized while Taxiing
Ground Use Only
51
Autopilot Minimum Engagement Height (Takeoff) per AFM
400’AGL per AFM (1,000’ per Mesa CFM)
52
Engine Model
CF34-8E5
53
Engine Takeoff/TOGA Thrust Time Limit
Time limited to 5min with all engines operative. This limit is extended to 10min with one engine inoperative for airplanes with Post-Mod 17073-0002 (which we have) or equipped with an equivalent modification factory incorporated.
54
Engine Start ITT Limitations (Min and Max)
Min: None, Max: 815deg C
55
EICAS Red Markings
Max and Min Limitations
56
EICAS Amber Markings
Caution Range
57
EICAS Green Markings
Normal Operating Range
58
FLEX Takeoff Reduction Limitaion
Must not exceed 25% full takeoff thrust
59
Can FLEX Takeoff be used on Contaminated Runways?
No. The FAA defines that a runway is contaminated whenever standing water, ice, snow, slush, frost in any form, heavy rubber or other substances are present. So “Good to Medium” reported.
60
ATTCS (Automatic Takeoff Thrust Control System) (selects RSV power for engine failures based on system logic)
Must be ON for all takeoffs and landings
61
Engine Starter Duty Cycle Limits - On Ground
Attempt 1,2: 90 sec ON / 10 sec OFF
Attempt 3,4,5: 90 sec ON / 5min OFF
For ground starts the max cumulative starter run time per start attempt is 90sec
62
Engine Starter Duty Cycle Limits - In Flight
Attempt 1-2: 120 sec ON / 10 sec OFF
Attempt 3-5: 120sec ON / 5min OFF
63
Dry Motoring Duty Cycle Limits (used to remove heat and fuel that was introduced but not ignited - only use for hot starts)
Attempt 1: 90 sec ON / 5 min OFF
Attempt 2-5: 30 sec ON / 5 min OFF
After 5, the cycle can be repeated after 15min
So in a scenario, you would attempt an engine start for 90sec ON, then 10sec OFF after it didn’t start. Then, if it is a hot start, you would dry motor the engine for 90sec ON max (QRH calls for 30sec), followed by 5min off. Then you could try starting the engine again on attempt 2 for 90sec ON, 10sec OFF. If you have to dry motor again, you will be on dry motoring attempt 2 so 30sec ON, 5min off. Then attempt an engine start for the 3rd time so then 90sec ON, 5min off. Maintenance must be called if the third attempt doesn’t work per the CFM.
For HOT Starts, the FADEC commands an automatic abort when ITT is 10°C lower than the engine hot start limit. This will prevent ENG EXCEEDANCE EICAS message to be displayed. In this case, two additional engine starts are allowed without any cause investigation.
If both the following conditions occur, only one additional engine start is allowed:
a. Engine start is manually aborted due to no ITT indication 15 seconds after fuel is reapplied, and
b. “ENG 1(2) NO DISPATCH” or “ENG 1(2) SHORT DISPATCH” EICAS messages are not displayed.
64
APU Starter Duty Cycle Limits
Attempt 1,2: 1min ON / 1min OFF
Attempt 3: 1min ON / 5min OFF
(The 1min ON shutoff function is automatically provided by the APU FADEC)
65
APU Start Min Temperature
-54 degrees C
66
APU Start Max Temperature
APU Temperature matches the Airplane Operational Envelope temperature (52deg C on the ground)
67
APU Start Max Altitude
30,000’
68
APU Operation Min Temperature
APU Temperature matches the Airplane Operational Envelope temperature (-54 deg C on the ground)
69
APU Operational Max Temperature
APU Temperature matches the Airplane Operational Envelope temperature (52deg C)
70
APU Operation Max Altitude
33,000’
71
APU Operation Max Electrical Gen Altitude
33,000’
72
APU Operational Max Bleed Altitude
15,000’
73
APU Operation Max Altitude to Assist Engine Start
21,000’
74
Is there an automatic in-flight shutdown if the APU EGT exceeds limits?
No
75
At what speed are the TAS, TAT, and SAT valid?
Above 60 KIAS
76
When is the standby magnetic compass not valid?
While transmitting on VHF #1
77
What kind of minimums must be used for all CAT I approaches?
Baro Minimums
78
Are pilots advised to deviate from their current ATC clearance to the extent necessary to comply with a RA?
Yes
79
Can you fly a LOC Back Course approach using IESS?
No
80
How many lbs of fuel are used for taxi?
About how many gallons is this?
353 lbs
~52 Gallons
81
How many lbs are a Gallon of Jet Fuel
6.8 lbs per Gallon
82
Is unusable fuel included in the Maximum Zero Fuel Weight?
Yes
83
What is the purpose of the MZFW Maximum Zero Fuel Weight?
Structural Limitation
Wings are subjected to upward bending stress that is counteracted by the weight of the fuel
If the fuel level becomes low and the aircraft weight is high, the wings may be subject to too much lift production
This could result in the wings becoming over-stressed in flight
84
Max Fuel Capacity Per Tank
10,392.5 lbs per Tank (doesn’t include unusable fuel)
85
Minimum Engagement Height (Takeoff) per GOM
1,000’AGL per GOM
86
Minimum Use Height (Coupled ILS Approach)
50’AGL
87
Fwd baggage compartment capacity
3,306lbs
88
AFT baggage compartment capacity
2,535 lbs
89
Max alt for flaps extended
20,000’
90
Max speed to open the direct vision window
160KIAS
91
Max crosswind takeoff on dry runway
38kts
92
Max crosswind takeoff on wet runway
31kts
93
Max crosswind takeoff on rwy with compacted snow
20kts
94
Max crosswind takeoff on rwy with standing water/slush/wet snow/dry snow
18kts
95
Max crosswind takeoff on rwy with ice/wet ice
12kts
96
Due to compressor stall possibility, static takeoff is not recommended with crosswinds greater than
25kts
97
What fuel weight was used for the fuel capacity info in the CFM
6.767 lbs/gal
98
What is the maximum thrust with brakes applied?
60% N1
99
What is the N1 limit?
99.5%
100
What is the N2 min and max limit?
58.5 - 99.4% N2
101
What is the max ITT for TOGA thrust? Is there a time limit?
990 deg C limited to 5min
or 10min with one engine inop (we have the Postmod)
can be exceeded up to 1006 deg C during first 2 min
102
Max Continuous Thrust (CON) ITT limit
960deg C
(Max Continuous Thrust CON is the highest thrust that does not require maintenance to inspect the engine earlier than planned. It is used in emergency situations and is 12,800lbs. The highest possible thrust is TO-1 RSV or GA RSV, RSV meaning that ATTCS is activated. TO-1 RSV and GA RSV produce 14,200lbs of thrust or 13,000lbs SE)
103
Engine Oil Pressure Min and Max Limits
25psi - 95psi
104
Max Continuous (engine) Oil Temperature
155deg C
(Max Continuous Thrust CON is the highest thrust that does not require maintenance to inspect the engine earlier than planned. (Up to the red line) It is used in emergency situations and is 12,800lbs. The highest possible thrust is TO-1 RSV or GA RSV, RSV meaning that ATTCS is activated. TO-1 RSV and GA RSV produce 14,200lbs of thrust or 13,000lbs SE)
105
Max Transient Oil Temperature
above 155deg C (max continuous) is limited to 15min up to 163deg C (max transient oil temp)
(Max Continuous Thrust CON is the highest thrust that does not require maintenance to inspect the engine earlier than planned. (N1 to the red line) It is used in emergency situations and is 12,800lbs. The highest possible thrust is TO-1 RSV or GA RSV, RSV meaning that ATTCS is activated. TO-1 RSV and GA RSV produce 14,200lbs of thrust or 13,000lbs SE) So Max Transient must be RSV thrust.
106
When must the TO DATSET MENU on the MCDU be set to ENG
when OAT is 5-10deg C and there is a possibility of encountering moisture up to 1,700’ AFE or water/snow/ice on airport surfaces
107
When must the TO DATASET MENU on the MCDU be set to ALL?
when OAT is below 5deg C and there is a possibility of encountering moisture up to 1,700’ AFE or water/snow/ice on airport surfaces
108
Autopilot minimum use height per AFM
50’
109
What flap setting must be used for a CAT II approach?
flaps 5
110
What is the demonstrated headwind component for CAT II?
25kts
111
What is the demonstrated tailwind component for CAT II?
10kts
112
What is the demonstrated crosswind component for CAT II?
12kts
113
What kind of FMS do we have?
Honeywell Primus Epic II
114
What equipment is required for RVSM operations?
1 autopilot, altitude alerting system, 2 transponders (1 must be operational), 2 ADCs (both operational)
115
Aircraft Wingspan
93’ 11”
116
Tail Height
32’ 4”
117
Aircraft Length
103’ 11”
118
Max Ambient Air Temp for Takeoff and Landing
52 deg C
119
What is the minimum oxygen required for dispatch? Max, Green, Blue, Amber
Max - 1664psi
Green for 3 - 1150psi
Blue for 2 - 842psi
Amber - No Dispatch
120
Fuel Tanks Red
660lbs
121
Fuel Tanks Amber
1320lbs
122
180 Degree Turn Radius (Wheel to Wingtip)
57’ 10”
123
180 Degree Turn Tail Clearance (Wheel to Tail)
57’ 3”
124
Pavement Required for 180 Degree Turn (Min Rwy Length)
59’ 2”
125
Max Fuel Capacity
20,935lbs
126
Useable fuel per side
10392.5lbs
127
Unusable Fuel per side
75lbs
128
What is max thrust limited to?
14,200lbs for SE or 13,000 with both engines
129
LL MRW, MTOW, MLW, MZFW
MRW 85,450 (420lbs less)
MTOW 85,098 (419lbs less)
MLW 74,957 (same)
MZFW 69,467 (419lbs less)
130
APU Amber range (no time operating limit in amber in flight or on the ground)
662-717deg C
131
5G Limitation - autothrottles
For all approaches in VMC or IMC, the Auto -Throttles will be turned off by 500ft AGL
132
5G Abnormal EICAS Messages on Takeoff
On takeoff above 80 knots or on landing below 60 knots, messages may appear that are normally inhibited. Some of these messages are related to hydraulic and brakes failure.
If Caution and/or Advisory messages are displayed above 80 KIAS, continue the takeoff, except for ENG 1 (2) FAIL Caution messages up to V1.
133
How could 5G affect TCAS?
During normal operation, TCAS will switch to TA only mode below 900ft during descent and 1000ft during climb. This operation could be affected by 5G interference where an RA descent could occur below 900ft.
134
What is the APU oil capacity?
4.12 Quarts
135
Maximum Tire Ground Speed
195
136
What fuel weight are the fuel limits based on?
6.75lbs/gal
137
Max N1 with brakes applied
60%
138
Is there a temperature limitation for anti-icing system AUTO operation?
No
139
Can the aircraft be operated within the north and south magnetic polar cut-out regions?
Yes. The airplanes may be operated within the North and South magnetic polar cut- out regions specified in the "North and South Magnetic Polar Cut-Out Regions" table below, but IRS magnetic Heading and track angle magnetic data will not be available.
Whenever operating within North or South magnetic polar cut-out regions, current airplane Heading must be referenced to true Heading, if not already selected. Otherwise, the Heading Failure Indication flag will be displayed.
See table for latitude longitude coordinates.
*This is not the same as maximum latitude for stationary alignment.*
140
Minimum Equipment Required for CAT II
1. Two Inertial Reference Systems.
2. Two Flight Director Systems.
3. Two Primary Flight Displays (PFD).
4. Windshield Wipers.
5. Two VOR/ILS NAV System.
6. One VHF/COMM System.
7. Cat II Engagement Logic.
8. One Radio Altimeter.
9. One Ground Proximity Warning System (EGPWS).
10. Two Air Data System (ADS).
11. One Autopilot System Channel.
12. Rudder in Normal Mode.
13. SPOILER FAULT message not presented.
141
What flap setting must be used with CAT II?
Flap 5 Only
142
What is the maximum ozone criteria?
The Maximum Ozone Criteria is the limiting altitude for every flight and does not depend on flight time.
143
What is the Time weighted average TWA ozone criteria?
The Time Weighted Average (TWA) Ozone Criteria tables do not represent the ceiling altitude, but the altitude above which the airplane should not fly for more than three continuous hours (14 CFR 25.832 (a)(2)). This means that the TWA ozone chart shall only be considered if both of the following conditions are met:
a. The airplane is flying in a latitude range at or above the minimum indicated in the table with an actual limitation (not a dash).
b. The flight will be conducted at or above FL270 in that latitude range for three or more hours.
C. If the latitude considered is in between the ones presented in the table, the altitude value may be interpolated. For calculation purposes, the dashes in the table should be considered the maximum altitude presented in the approved operational envelope (FL410).
D. For example, during flight on the west side of the longitude reference line (100°W) at any latitude above 45°N up to 50°N in January, the maximum flight level shall be limited to 407 (Maximum Ozone Criteria), but the airplane shall not be above flight level 338 for more than three hours (TWA Ozone Criteria).
The tables show altitude limitations calculated for constant ozone concentration and cabin stabilized at 8,000 ft. However, ozone tables shall still be considered regardless of the actual cabin altitude attained during a given flight.
144
What types of non-precision approaches does the FMS support?
a. GPS only (type III FAA overlay definition);
b. RNAV (including type II or type III FAA overlay definition);
c. VOR; VOR-based Approaches include FAA type II GPS overlays.
d. VOR-DME;
145
What non-precision GPS approach minima are supported by the FMS?
LNAV.
LNAV/VNAV.
RNP-APCH.
146
Can pilots conduct RNP AR or RNP RF Legs?
Mesa Airlines, Inc. does not have Operations Specifications authorization to conduct RNP AR or RNP RF Legs operations. Flight crews shall not conduct RNP AR operations until Operations Specifications approval is authorized.
147
When must an IRS be operational?
Operation above 72° 30.0’ north latitude and below 59° 30.0’ south latitude is prohibited due to unreliable magnetic Heading, unless at least one Inertial Reference System (IRS) is verified operational as a sensor to the FMS. In this case, the system will automatically switch to TRUE.
148
Can FMS Performance Management calculations be used for load planning or airplane range predictions?
*** FMS performance management calculations have not been certified by the Airworthiness Authority. FMS performance management information is advisory information only, and may not be used as a basis for fuel load planning or airplane range predictions.***
149
What is required when inserting a hold on a waypoint through the FMS?
The use of the FMS default option (if presented) is required when inserting a hold on a waypoint.
The selection of a database defined hold option on the FMS select hold page is prohibited.
150
RVSM Tolerances
A. Total Vertical Error
Equal to, or greater than, +/- 300 ft. Vertical geometric difference between the actual pressure altitude flown by an aircraft and its assigned pressure altitudes.
B. Altimetry System Error
Equal to, or greater than, +/- 245 ft. Any system which is designed to automatically control the aircraft to a referenced pressure altitude.
C. Assigned Altitude Deviation
Equal to, or greater than, +/- 300 ft. Difference between the transponder Mode C altimeter and the assigned altitude/flight level.
151
RVSM Required Equipment
(1) Autopilot - Must be operational
Altitude Alerting System - Must be operational
(2) Altitude Reporting Transponders - One must be operational
(2) Air Data Computers (ADC) - Two must be operational
152
Flaps 1 Pitch
11deg
153
Flaps 2 pitch
10deg
154
Flaps 4 pitch
12deg
155
What is the demonstrated crosswind for takeoff and for landing? Is this considered limiting?
The maximum 90° crosswind component for which adequate control of the airplane during Takeoff and Landing was actually demonstrated during certification tests. The maximum demonstrated crosswind component for Takeoff (at 33 ft (10 meters) tower height) is 28 knots and is to be considered limiting. The maximum demonstrated crosswind component for Landing (at 33 ft (10 meters) tower height) is 30 knots and is to be considered limiting.
In high crosswind conditions, rudder effectiveness may be limited after Landing with maximum reverse thrust selected.
156
Per GOM can the takeoff, approach and landing wind components published as demonstrated, recommended or limiting be exceeded?
The takeoff, approach and landing wind components published in the appropriate aircraft CFMs and listed as demonstrated, recommended, or limiting will not be exceeded.
157
Do wind gusts affect the crosswind limitations?
No
158
APU Max Rotor Speed
108%
159
APU EGT for start
1032deg C
160
APU EGT for continuous operation
717deg C
161
In flight, will the APU shut down if the EGT limit is exceeded?
No.
162
Is there a time limitation for operating the APU on the ground or in flight in the amber range between 662deg and 717deg C?
No
163
What emergency equipment is located on the flight deck?
1 PBE
1 Halon Fire Extinguisher
2 Flashlights
3 Life Vests
3 Oxygen Masks
1 Crash Axe
2 Escape Ropes
1 Thermal Containment Gloves
164
The originating/receiving checklist requires logbook, forms and manuals to be checked. What are you looking for?
Name the 15 required manuals and docs
165
What emergency equipment is located in the LR cabin and where are they located?
FWD Lav (left):
- Halon Fire Extinguisher (1/5) + 1 on flight deck
FWD FA Station (left):
- Life Vest (1/2)
- Flashlight (1/2)
- MRT Manual Release Tool (1/2)
Wardrobe (right):
- Thermal containment gloves and bag
FWD Galley Bulkhead (right):
- Halon Fire Extinguisher (2/5)
- PBE Portable Breathing Equipment (1/3)
- POB Portable Oxygen Bottle (1/2)
- FAK First Aid Kit (1/2)
Row 1 Overhead Bin (left):
- Demo Equipment
- Seat Belt Extensions
- Extra Passenger Briefing Safety Information Cards
Row 23 Overhead Bin (left):
- Portable ELT
Row 24 Overhead Bin (left):
- AED Automated External Defibrillator
- EEMK Enhanced Emergency Medical Kit
- 8 Infant Life Vests
Doghouse (left):
- Halon Fire Extinguisher (3/5)
- PBE (2/3)
- POB (2/2)
- FAK (2/2)
AFT FA Station (left):
- Life Vest (2/2)
- Flashlight (2/2)
- MRT (2/2)
AFT Lav (left):
- Halon Fire Extinguisher (4/5)
Doghouse (right):
- Halon Fire Extinguisher (5/5)
- PBE (3/3)
- Water Fire Extinguisher
- Megaphone
Behind Galley Carts (right):
- Wheelchair
166
What emergency equipment is in the LL cabin and where is it located? What are the major differences?
Major Differences:
- 3 MRT instead of 2
- 3 POB instead of 2
- Life vests under each seat
- AFT wardrobe (right) instead of doghouse (right)
- Row 22 Overhead Bin (right) instead of 23 and 24 (left)
- AFT Additional Jumpseat (right)
FWD Lav (left):
- Halon Fire Extinguisher (1/5) + 1 on flight deck
FWD FA Station (left):
- Life Vest (1/3)
- Flashlight (1/2)
- MRT Manual Release Tool (1/3)
Wardrobe (right):
- Thermal containment gloves and bag
FWD Galley Bulkhead (right):
- Halon Fire Extinguisher (2/5)
- PBE Portable Breathing Equipment (1/3)
- POB Portable Oxygen Bottle (1/3)
- FAK First Aid Kit (1/2)
Row 1 Overhead Bin (left):
- Demo Equipment
- Seat Belt Extensions
- Extra Passenger Briefing Safety Information Cards
Life Vest Under Each Passenger Seat
Doghouse (left):
- Halon Fire Extinguisher (3/5)
- PBE (2/3)
- POB (2/3)
- FAK (2/2)
AFT Lav (left):
- Halon Fire Extinguisher (4/5)
AFT FA Station (left):
- Life Vest (2/3)
- Flashlight (2/2)
- MRT (2/3)
AFT Wardrobe (right):
- Halon Fire Extinguisher (5/5)
- PBE (3/3)
- POB (3/3)
Row 22 Overhead Bin (right):
- Portable ELT
- 8 Infant Life Vests
- EEMK
- AED
- Megaphone
AFT Additional Jumpseat (right):
- Life Vest (3/3)
- Flashlight (2/2)
- MRT (3/3)
Behind Galley Carts (right):
- Wheelchair
167
Turbulent Airspeed Below 10,000’
250kts
168
Turbulent Airspeed at or above 10,000’
270kts or .76M, whichever is lower
169
Max Range
2,000NM
170
Min Airspeed for RAT Operation
130kts
171
Certification Category
Transport
172
Headsets must be worn below what altitude?
FL180
173
Max Ambient Air Temperature for Operation at FL410
-21.5deg C
174
Min Ambient Air Temperature for Operation at FL410
-65deg C
175
GOM Recommended Max Taxi Speed - Straight, Dry Pavement
20kts
176
GOM Recommended Max Taxi Speed - Straight, Wet Pavement
10kts
177
GOM Recommended Max Taxi Speed - Turns, Dry Pavement
10kts
178
GOM Recommended Max Taxi Speed - Turns, Wet Pavement
5kts
179
Max Recommended Crosswind for Landing - Dry
38kts
180
Max Recommended Crosswind for Landing - Wet “Good”
31kts
181
Max Recommended Crosswind for Landing - Compacted Snow “Good to Medium”
20kts
182
Max Recommended Crosswind for Landing - Standing Water / Wet/Dry Snow “Medium”
15kts
183
Max Recommended Crosswind for Landing - Water/Slush “Medium to Poor”
12kts
184
Max Recommended Crosswind for Landing - Ice “Poor”
8kts
185
Max Recommended Crosswind for Landing - “Nil”
Not Approved
186
PAX Cabin Door Max Wind Gusts - Partially Open
40kts
187
PAX Cabin Door Max Wind Gusts - Open and Locked
65kts
188
Cargo Door Max Wind Gusts - Partially Open
40kts
189
Cargo Door Max Wind Gusts - Open and Locked
60kts
190
Cabin Alt High Warning Occurs When
Cabin Alt is 9,700’ or higher
OR
Cabin Alt > 500’ above LFE, for LFE above 9,400’
191
When should the Hot Weather Checklist be used?
Above 30deg C or 86deg F
192
AP Coupled Go-Around Height Loss
May be 50’
193
Batt 2 Minimum Temperature for APU Start
-20deg C
194
VDC Required for APU Start
22VDC
195
BATT 1(2) OVERTEMP trigger
70deg C for 2 sec
196
VDC Required to Close the battery contactor during APU start
18VDC
197
What is required to start the APU below -20deg C or below 22VDC
The battery must be charged or the DC GPU can be used.
198
DC GPU Voltage Output Required
24-29 VDC
199
IDG HOT Trigger
> 168deg C
200
IDG LOP Trigger
< 140PSI
201
NiCad Batteries Supply Power for
10min
202
TOGA ITT Can be exceeded up to ___deg for ___min
1006deg C for 2min
203
ITT Limit for engine start logic
120deg C for igniters to come on
204
Hydraulic System Pressure
3,000 PSID
205
HYD 1/2/3 HI TEMP Trigger
100deg C
206
HYD SOV automatically closes for systems 1 and 2, or for system 3 pumps 3A and 3B turn off at ____deg C
125deg C
207
HYD 1/2/3 OVERHEAT Trigger
145deg C
