Limitations Flashcards
1
Q
Weights LR/LL
A
MRW 85,870 / 85,450
MTOW 85,517 / 85,098
MLW 74,957 / 74,957
MZFW 69,886 / 69,467
2
Q
MIN FLIGHT CREW
A
2 = pilot and copilot
3
Q
max runway slope
runway surface type
max altitude for flaps extended
max operating altitude
max T&O & landing altitude
min T&O & landing altitude
A
+/- 2%
paved
20,000
41,000*
10,000
-1000
4
Q
Max speed to open direct vision window
A
160
5
Q
max latitude for stationary alignment
A
78.25N-78.25S
6
Q
min ambient temp approved for T&O
max ambient air temp for takeoff and landing
A
-54c
52c
7
Q
VLO RET, VLO EXT, VLE speeds (gear)
A
250
8
Q
Flap speeds
A
flap 1 230
flap 2 215
flap 3 200
flap 4 & 5 180
flap Full 165
9
Q
aircraft max operating speed
A
VMO/MMO
10
Q
max operating mach
A
.82
11
Q
max airspeed for RAT operation
A
VMO/MMO
12
Q
turbulent air below 10,000
turbulent air above 10,000
A
250
270 or 0.76 whichever is lower
13
Q
max tire limit ground speed
max windshield wiper speed
A
195
253
14
Q
max operating speed up to 8,000
8,000 - 10,000
10,000 - FL290
FL290-FL410
A
300
300-320
320
.82
15
Q
Max recommended xwind for landing
A
Max recommended xwind for landing
Dry 28
wet 28
compacted snow 20
standing water/slush/wet snow/dry snow 18
ice 12
16
Q
max static takeoff crosswind
A
25 kts
17
Q
cargo loading weights
A
FWD 3306
AFT 2535
18
Q
icing conditions may exist
A
icing conditions may exist whenever the Outside Air Temperature (OAT) on the
ground or for Takeoff, or Total Air Temperature (TAT) in-flight, is 10°C or below
and visible moisture in any form is present (such as clouds, fog with visibility of
one mile or less, rain, snow, sleet and ice crystals)
19
Q
APU min start temp (outside temp)
APU max alt to start
APU max operating alt
APU max electrical generation
A
-54C
30,000
33,000
33,000
20
Q
APU bleed altitude
A
15,000
21
Q
Altitude for APU to assist engine start
A
21,000
22
Q
APU max rotor speed %
A
108%
23
Q
APU amber range (no time limit)
A
662 - 717C
24
Q
APU EGT start temp
A
1032
25
APU EGT continuous TEMP
717
26
APU start limits times
1 & 2 1 min on/1 min off
3 1 min on/5 mins off
27
CAT II flaps position
flaps 5
28
CAT II demonstrated wind components (not considered limiting)
headwind 25
tailwind 10
crosswind 12
29
CAT II required equipment
2 Air Data System (ADS).
2 Flight Director Systems.
2 Inertial Reference Systems.
2 Primary Flight Displays (PFD).
2 VOR/ILS NAV System.
Autopilot System Channel.
Cat II Engagement Logic.
EGPWS.
Radio Altimeter.
Rudder in Normal Mode.
SPOILER FAULT message not presented.
VHF/COMM System.
Windshield Wipers.
30
max fuel capacity total
max fuel capacity per tank
unusable fuel per tank
20935 lbs
10392.5 lbs
75 lbs
31
min fuel tank temp
max fuel imbalance
-37C in left tank
794 lbs
32
max differential pressure
Maximum differential overpressure
Maximum differential negative pressure
Maximum differential pressure for Takeoff and Landing
8.4 psi
8.8 psi
-.5 psi
.2 psi
33
Single PACK operations limit
FL 310
34
Thrust reversers conditions
Upon Landing, if thrust reversers have been used, reverser should be set to MIN REV at 60 KIAS, and be closed by 30 KIAS.
A Go-Around Maneuver should not be attempted after Thrust Reversers have been deployed
35
autopilot use
min engagement height in AFM - 400
min engagement height in CFM - 1,000'*
min use height - 50'
36
CF 34-8E5 engines with takeoff thrust time limited to ____ minutes OR POSTMOD SB170-73-0002
10 minutes
37
N1 max percentage
N2 min - max percentage
99.5%
58.5% - 99.4%
38
TT max Start
815
39
ITT max take off and go around temp and time limits
ITT max take off and go around temp and time limits
990C
1. Time limited to 5 min with all engines operative. This limit is extended to 10 min with one engine inoperative for airplanes Post- Mod SB 170-73-0002 or equipped with an equivalent modification factory incorporated.
2. Can be exceeded up to 1006°C during the first 2 minutes.
40
ITT max continuous temp
960
41
oil pressure PSI min- max
25-95psi
42
oil temp continuous
155
43
oil temp transient
163 (Transient operation above 155°C limited to 15 minutes.)
44
Engine starter limits attempts
Engine starter limits attempts
1 and 2 - 90 Seconds on/ 10 Seconds off
3 , 4 and 5 - 90 Seconds On/5 Minutes off
120 seconds on In-flight
45
Engine dry motor starter limits attempts
Engine dry motor starter limits attempts
1 - 90 Seconds on/ 5 Minutes off
2 through 5 - 30 Seconds on/5 Minutes off
After five sequential motorings, cycle may be repeated following a 15 minute cool down period.
46
for FLEX - The total thrust reduction must not exceed ____ of the full Takeoff thrust.
FLEX is prohibited on ____ runways
25%
contaminated
47
TAS, TAT and SAT information are only valid above____ KIAS
60
48
While transmitting in ____ the standby magnetic compass indication is not valid.
VHF1
49
Baro altimeter minimums must be used for all ____Approaches.
CAT I
50
Pilots are authorized to deviate from their current Air Traffic Control (ATC) clearance to the extent necessary to comply with an
EGPWS warning.
51
Localiser Back course Approaches using _____ are prohibited.
IESS
52
RSVM required equipment list
RSVM required equipment list
(2) Air Data Computers (ADC) (Two must be operational)
(2) Altitude Reporting Transponders (One must be operational)
(1) Altitude Alerting System (Must be operational)
(1) Autopilot
53
RVSM tolerances
RVSM tolerances
Total Vertical Error +/- 300 ft.
Altimetry System Error +/- 245 ft.
Assigned Altitude Deviation +/- 300 ft.
54
Use of Temperature compensation
Use of Temperature compensation
The use of temperature compensation feature must be coordinated with ATC if Baro-VNAV operation is intended.
The use of temperature compensation feature is required if Baro-VNAV operation outside the temperature limits published on Approach
procedure chart is intended.
55
APU max start temp (outside temp)
52C
56
In the event of a Landing below ___, the airplane may not Takeoff without further maintenance inspection.
-40C
57
Flaps load factor
Flaps Up -1.00g to 2.5 g
Flaps Down 0g to 2 .00g
58
Fuel Specification
JP8
59
Crossfeed Operation
Crossfeed Selector Knob must be set OFF during Takeoff and Landing
60
The maximum N1 percentage with brakes applied is
60%
61
For Flex - reduction must not exceed
The total thrust reduction must not exceed 25% of the full Takeoff thrust.
62
Flex is prohibited on
Flex is prohibited on
Use of reduced Takeoff thrust procedures is not allowed on runways contaminated with standing water, slush, snow or ice and are not allowed on wet runways
unless suitable performance accountability is made for the increased stopping distance on the wet surface.
63
The TO DATASET MENU on the MCDU must be set to ENG in the following cases when OAT is
The TO DATASET MENU on the MCDU must be set to ENG in the following cases when OAT is
between 5°C and 10°C and:
1. If there is any possibility of encountering visible moisture up to 1,700 ft AFE, or
2. When operating on ramps, taxiways or runways where surface snow, ice, standing water or slush may be ingested by the engines or freeze on engines, nacelles or engine sensor probes.
64
The TO DATASET MENU on the MCDU must be set to ALL in the following cases when
The TO DATASET MENU on the MCDU must be set to ALL in the following cases when
OAT is below 5°C and:
1. If there is any possibility of encountering visible moisture up to 1,700 ft AFE, or
2. When operating on ramps, taxiways or runways where surface snow, ice, standing water or slush may be ingested by the engines or freeze on engines, nacelles or engine sensor probes.
65
Steering degrees for steering handle and rudder
Steering degrees for steering handle and rudder
0 - 10kts 76 degrees
11 - 26kts 20 degrees
27 - 100kts 7 degrees (rudder)
66
TOGA pitch bar range in degrees
TOGA pitch bar range in degrees
8 - 18 degrees
67
Fuel low level warning occurs in each tank at what lbs?
Fuel low level warning occurs in each tank at what lbs?
660lbs
68
turn radius for 180 degrees
turn radius for 180 degrees
59' 2"
69
aircraft dimensions
aircraft dimensions
height 32' 4"
wing span 93' 11"
length 103' 11"
70
IESS alignment time
90 sec
71
GE CF34-8E5 max thrust
GE CF34-8E5 max thrust
13,000 - 14,200
72
hydraulic temp limits
hydraulic temp limits
100C HYD HI TEMP EICAS
125C auto shutoff
145C HYD OVERHEAT EICAS
73
Taxi speeds
Taxi speeds
straight/Dry 20
Turns/dry 10
straight/wet or contaminated 10
turns/wet or contaminated 5
74
two engine out speed
two engine out speed
pitch for 250kts MINIMUM
75
single engine drift down speed
single engine drift down speed
green dot
76
green dot represents
green dot represents
1.3G over stick shaker speed
77
Pitch angles for flap positions
Pitch angles for flap positions
Flaps 1 11 degrees
Flaps 2 10 degrees
Flaps 4 12 degrees
78
radar altimeter comes alive at
radar altimeter comes alive at
2,500 AGL
79
percent of recirculation air
52% fresh
percent of recirculation air
52% fresh
48% rec
80
The APU oil capacity is
The APU oil capacity is
4.12 qt
81
BATT 1 (2) OVERTEMP EICAS message will appear at what temp?
BATT 1 (2) OVERTEMP EICAS message will appear at what temp?
A
70C for 2 seconds
82
Manuals and Documents (15 items)
1. Jumpseat Briefing Card.
2. Passenger Briefing Safety Information Cards.
3. Passenger Count Card.
4. TOLD Cards.
5. 2 CAT II INFORMATION and CALLOUTS Cards.
6. 2 ECS Off Takeoff checklist, Engine Battery Start checklists.
7. 2 EPCs.
8. 2 Icing Conditions, Cold Weather and Cold Soak Operations.
9. 2 Lightning Strike, Turbulent Air Penetration, Hot Weather.
10. 2 Normal Operations Checklist(s).
11. Airworthiness Certificate and Registration.
12. AML
13. QRH
14. Radio Station Certificate.
15. W&B Manifest.
3
83
E-175 aircraft are Group ___ aircraft and require a minimum _____ ft of runway at
Sea Level.
E-175 aircraft are Group ___ aircraft and require a minimum _____ ft of runway at
Sea Level.
7
6,000
84
emergency equipment (7)
Crash Axe (1)
Escape Ropes (2)
Fire Extinguisher (1)
Flashlights (2)
Life Vests (3)
Oxygen Masks (3)
PBE (1)
85
Flight Kit items (12)
Airman Certificate
Extra Pair of Corrective Lenses* Only required if wearing corrective lenses
FCC Restricted Radio
Telephone Operating Permit
Flashlight
Jeppesen Inflight Pubs (EFB or Paper)
Log book
Medical Certificate
Mesa Airlines, Inc. ID Card
Passport
Pen
Required Manuals (EFB or Paper)
Training Folder Only required if in training
86
considered stable approach
Stabilized Approach Criteria
1. Flights will be stabilized by 1,000 feet AFE.
2. An approach is considered to be stable when all of the following conditions are met:
a. All appropriate briefings and checklists have been accomplished.
b. The aircraft is in the planned landing configuration.
NOTE
The planned landing configuration is gear down and locked, final landing flaps, and flight spoilers are retracted.
c. The aircraft is on the correct track.
NOTE
The correct track includes normal maneuvering required to align with the final approach course. In VMC conditions this may include turns below 1,000 feet (AFE) but must be aligned by 500 feet (AFE). However, all of the criteria for stabilized approach must be met by 1,000 feet (AFE).
d. The aircraft is not more than the planned approach speed +10 KIAS, while correcting to the proper speed, and not less than VREF.
NOTE
Adjustments may be made for ground speed when applicable. Momentary excursions (deviations which last only a few seconds with every indication that it will return to a stabilized criteria) are acceptable.
e. The power setting is appropriate for the aircraft configuration.
NOTE
At no point except for rollout and flare should the thrust levers be reduced to idle below 1,000 feet AGL. If this occurs then a goaround is mandatory.
f. The rate of descent is no greater than 1,000 fpm.
NOTE
If an expected rate of descent greater than 1,000 fpm. is planned, a special approach briefing should be performed.
NOTE
If an unexpected sustained rate of descent greater than 1,000 fpm. is encountered during the approach, a missed approach or goaround should be performed.
g. After glidepath intercept, or after the FAF, the pilot flying (PF) requires no more than normal corrections to maintain the correct track and desired profile to landing within the touchdown zone.
NOTE
Normal bracketing corrections relate to bank angle of not more than 30°, rate of descent ±300 fpm. deviation from target, and power management in the range required to maintain a constant rate of descent and speed. Normal bracketing corrections occasionally involve momentary overshoots made necessary by atmospheric conditions. Such overshoots are acceptable. Frequent or sustained overshoots caused by poor pilot technique are not normal bracketing corrections.
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