E175 Limitations/Memory Items Flashcards
Aircraft length
103’ 11” (104’)
Aircraft width
93’ 11” (94’) (Wingspan)
Aircraft height
32’ 4” (33’)
Max PAX
76 (12 First/64 Coach)
Max cargo weights
FWD 3307 lbs
AFT 2535 lbs
Maximum ramp weight
85,800 lbs
Maximum takeoff weight (structural)
85,500 lbs
Maximum landing weight (structural)
74,900 lbs
Maximum zero fuel weight
69,800 lbs
Minimum crew
2 pilots (left/right seat)
Aircraft operations
Day/night
VFR/IFR
Icing conditions
CAT I/CAT II
RVSM
Extended Overwater Operation (when EOW equipped)
Max cabin differential overpressure (safety valve)
8.8 PSI
Max cabin differential pressure above FL 370
8.4 PSI
Max cabin differential pressure for T/O and landing
0.2 PSI
Max cabin Negative differential pressure
-0.5 PSI
Max altitude depressurized
10,000’ or MEA whichever is higher
Max altitude for single pack operation
31,000’
Mmo (above FL280)
.82M
Vmo (above 10,000’ to FL280)
320 KIAS
Vmo (below 10,000’) (FAA and structural)
250 KIAS FAA regulatory
300 KIAS Structural
Va
240 KIAS
Vle
250 KIAS
Vlo
250 KIAS
Vlr
250 KIAS
Vfe1
230 KIAS
Vfe2
215 KIAS
Vfe3
200 KIAS
Vfe4
180 KIAS
Vfe5
180 KIAS
Vfefull
165 KIAS
Max turbulent airspeed (below 10,000’)
250 KIAS
Max turbulent airspeed (10,000’ and above)
270 KIAS or .76M
Max crosswind for takeoff (dry and wet)
Dry 35 kts
Wet 30 kts
Max crosswind for takeoff (RWYCC 4)
20 kts
Max crosswind for takeoff (RWYCC 3)
15 kts
Max crosswind for landing (RWYCC 6)
38 kts
Max crosswind for landing (RWYCC 5)
31 kts
Max crosswind for landing (RWYCC 4)
20 kts
Max crosswind for landing (RWYCC 3)
15 kts
Max crosswind for landing (RWYCC 2)
12 kts
Max crosswind for landing (RWYCC 1)
8 kts
Max crosswind for landing (RWYCC 0)
OPERATIONS PROHIBITED
Unless otherwise required by operational restrictions such as CAT II, MEL, or emergency/abnormal procedures, all landings on runways with an RCC less than 5/5/5 must be at what flap setting?
Flaps FULL
Max tailwind
10 kts
Max headwind for CAT II
25 kts
Max crosswind for landing (RVR less than 4000 or 3/4 mile)
15 kts
Max DV window operation speed
160 KIAS
Max tire speed
195 KIAS
Max windshield wiper speed
250 KIAS
Max operating altitude
41,000’
Max altitude with flaps extended
20,000’
Max altitude for takeoff and landing
10,000’
Minimum altitude for takeoff and landing
- 1,000’
Min SAT for takeoff or landing
- 40 deg C
Max SAT for takeoff or landing
54 deg C
Max altitude display difference in flight for RVSM
180’
In the event of a landing below ____ , takeoff not authorized without further maintenance inspection
- 40 deg C
APU model
Sundstrand APS 2300
APU starter limitations
First and second attempts
Third attempt
START/ON then 60 sec OFF
START/ON then 5 min OFF
Minimum starting temperature for APU
- 54 deg C
Max APU operation temperature
ISA + 39 deg C (supplemental info applicable at ISA + 35 deg C)
Max EGT APU start
1032 deg C
Max EGT APU continuous
is there a time limit ground/inflight between 662-717 deg C (amber range)
717 deg C
No time limit between 662-717 deg C (amber range)
Max APU rotor speed
108%
Max altitude for APU electrical power
33,000’
Max altitude for APU start
30,000’
Max altitude for ENG start assist with APU
21,000’
Max altitude for APU bleed air
15,000’
Minimum altitude for autopilot engagement (takeoff/go around)
Above 400’
Minimum altitude with autopilot engaged during landing
above 50’
Engine model
GE CF34-8E5
Max N1 RPM
99.5%
Max N2 RPM
99.4%
Max start ITT
815 deg C
Max normal T/O ITT
965 deg C (2 min)
949 deg C (3 min) [Total 5 min]
Max T/O & G/A ITT
1006 deg C (2 min)
990 deg C (3 min) [Total 5 min]
Max continuous ITT
960 deg C
Min oil pressure
25 PSI
Max oil pressure
95 PSI
Max continuous oil temp
155 deg C
Max transient Oil temp
163 deg C (15 min limit)
T/O-1 engine thrust
13,000 lbs
ATTCS 14,200 lbs
T/O-2 engine thrust
11,800 lbs
ATTCS 13,000 lbs
Fuel types
Jet A or A1
JP8
QAV1 (Brazilian)
Max fuel capacity
20,934 lbs (10,467 lbs/tank)
Max useable fuel
20,784 lbs (10,392 lbs/tank)
Unusable fuel
150 lbs (75 lbs/tank)
Max fuel imbalance
794 lbs
Minimum fuel temperature
-37 deg C
Can you crossfeed fuel during takeoff or landing?
NO
1st and 2nd engine start limits
on ground-90 sec START/10 sec cool-down
in flight-120 sec START/10 sec cool-down
3rd-5th attempts engine start limits
on ground- 90 sec START/5 min cool-down
in flight-120 sec START/5 min cool-down
Dry motoring limits
1st dry motor-Max 90 sec followed by 5 min cool-down
2nd-5th dry motor-Max 30 sec followed by 5 min cool-down
After __ sequential dry motoring cycles, the sequence may be repeated following a __ min cool-down period.
5, 15 min
CABIN ALTITUDE HI/RAPID Depressurzation
Oxygen masks…..CR…..ON, 100%
Jammed Control Column - Pitch
Elevator Disconnect…..CR…..PRESS and PULL
Jammed Control Wheel - Roll
Aileron Disconnect…..CR…..PRESS and PULL
Pitch Trim Runaway
AP/TRIM Disconnect…..PRESS and HOLD
TRIM PITCH SYS 1 & 2 CUTOUT…..Push IN
(Roll or Yaw) Trim Runaway
AP/TRIM Disconnect…..PRESS and HOLD
Nosewheel Steering Runaway
Steering Disconnect…..PRESS
Aborted Engine Start
Associated Thrust Lever…..IDLE
Associated START/STOP…..STOP
Application of reverse thrust is not permitted at airspeeds below __ KIAS during normal operations.
60 KIAS
Can you single engine taxi with an inoperative APU?
NO
Dry Ice limit
50 lbs in forward compartment only
CAUTION-Not all E170s have forward cargo ventilation fans
dry ice/live animals are prohibited in these aircraft
For operations at or above _____’ pressure altitude OR ISA ___ degrees and above, T/O-1 thrust is required.
8,000’
ISA +35
