TSA ERJ Limitations Flashcards
(89 cards)
1
Q
Operational Envelope: Take-off and Landing (pressure altitude)
A
-1000 ft. to 8000 ft.
2
Q
Operational Envelope: Take-off and Landing (Temperature)
A
-40 C to ISA+ 35 C
3
Q
Operational Envelope: Max. Altitude (PA)
A
37,000 ft.
4
Q
Operating Envelope: Max. Operating Temp.
A
ISA + 35 C
5
Q
Operational Envelope: Min. Operating Temp.
A
- 54 C to 25,000 ft.
- 65 C at 37,000 ft.
(TAT in cruise above 25,000 ft. is limited to -45 C)
6
Q
Landing Gear Vlo (Retraction)
A
200 KIAS
7
Q
Landing Gear Vlo (Extension)
A
250 KIAS
8
Q
Landing Gear Vle (Extended)
A
250 KIAS
9
Q
Maximum Operating Vmo / Mmo (0 to 8000 ft.)
A
250 KIAS
10
Q
Maximum Operating Vmo / Mmo (10,000 to 26,000 ft.)
A
320 KIAS
11
Q
Maximum Operating Vmo / Mmo (26,000 to 37,000 ft.)
A
0.78 Mach
12
Q
Maneuvering VA
A
200 KIAS
13
Q
Flap Extended Vfe
A
Flaps 9 = 250 KIAS
Flaps 22 = 200 KIAS
Flaps 45 = 145 KIAS
14
Q
Airspeeds: Tailwind
A
10 Knots Maximum for Take-off and Landing
15
Q
Airspeeds: Direct Vision Window
A
Max to Remove: 140 KIAS (AFM)
16
Q
Airspeeds: Windshield Wiper
A
Max for Operation: 170 KIAS (AFM)
17
Q
Turbulent Air Penetration (AFM)
A
At or blw 10,000 ft. = 200 KIAS
Above 10,000 ft. = 250 KIAS / 0.63 M (Whichever is lower)
18
Q
Load Factor Limit
A
Flaps Up = -1.00 G to 2.50 G
Flaps Down (9, 22, 45) = 0 G to 2.00 G
19
Q
Maximum Ramp Weight
A
LR = 48,722 lbs.
20
Q
Maximum Take-off Weight
A
LR = 48,501 lbs.
21
Q
Maximum Landing Weight
A
LR = 42,549 lbs.
22
Q
Maximum Zero Fuel Weight
A
LR = 39,462 lbs.
23
Q
Maximum Aft Cargo Weight
A
LR = 2646 lbs.
24
Q
Fuel: Specification
A
JET A, JET A-1, JP-8
25
Fuel: Tank Temperature
-40 C to 52 C
26
Fuel: Max. Imbalance
800 lbs.
27
Fuel: Maximum Useable Quantity Each Tank
LR = 844.9 US Gal. (5717 lbs.)
28
Fuel: Unusable Quantity each Tank
LR = 5.8 US Gal. (39 lbs).
29
Fuel: Note about unusable fuel
LR = Unusable fuel increases to 365 lbs. in each tank if any of the associated electric pumps is inoperative
30
Fuel: Note for pressure refueling
LR = When performing pressure refueling, the usable fuel quantity in each tank may be reduced by 13.2 US Gal.
31
Fuel: Note on values
LR = The values above have been determined for an adopted fuel density of 6.767 lb/US Gal.
32
APU T-62T-40C11 MIN and MAX Temperature
Min = -54 C
No Max
33
APU T-62T-40C14 MIN and MAX Temperature
None
34
APU T-62T-40C11 MIN and MAX Altitude for start
Max = 30,000 ft.
35
APU T-62T-40C14 MIN and MAX Altitude for start
Max = 30,000 ft.
36
APU T-62T-40C11 Operational altitude
Max = 37000 ft.
37
APU T-62T-40C14 Operational altitude
Max = 37,000 ft.
38
APU T-62T-40C11 Rotor Speed
Max 108%
39
APU T-62T-40C14 Rotor Speed
Max 108%
40
APU T-62T-40C11 EGT Start limits
884 C Max (May be exceeded up to 925 C above 25000 ft during 10 seconds)
41
APU T-62T-40C14 EGT Start limits
884 C Max
42
APU T-62T-40C11 EGT Continuous limits
680 C (The APU EGT may be exceeded up to 717 C for 5 minutes maximum)
43
APU T-62T-40C14 EGT Continuous limits
680 C (The APU EGT may be exceeded up to 717 C for 5 minutes maximum)
44
APU Starter Limits: Cooling period between each starting attempt:
Between 3 Consecutive Attempts... 1 Minute Off
Between 2 Series of 3 Consecutive Attempts... 30 Minutes Off
45
Engine Starting Limits: On Ground - Starting or Dry Motoring
Starting or Dry Motoring ... Up to 5 minutes on, 5 minutes off
46
Engine Starting Limits: On Ground - First to Fourth Cycles
1 Minute On, 1 Minute Off
47
Engine Starting Limits: On Ground - Following Cycles
1 Minute On, 5 Minutes Off
48
Engine Starting Limits: On Ground (List All)
Starting or Dry Motoring ... Up to 5 minutes on, 5 minutes off OR
First to Fourth Cycles... 1 min on, 1 min off
Following Cycles... 1 min on, 5 mins off
49
Engine Starting Limits: In Flight
Maximum Continuous Operation Time ... 5 MINUTES ON
NOTE: No cool down time is required should an in-flight start be reattempted
50
ATTCS
Must be operative for ALT T/O-1 Mode
51
Reversers
Do not go-around after reverser deployment
52
AE3007A1 (LR) N1 MIN/MAX
Max = 100.0%
53
AE3007A1 (LR) N2 MIN/MAX
Max = 102.4%
| For airplanes with Pre-Mod. SB 145-73-0030 the N2 limit is 102.5%
54
AE3007A1 (LR) ITT Start MIN/MAX
Max = 800 C
55
AE3007A1 (LR) ITT Takeoff Modes MIN/MAX
Max = 948 C
| Takeoff Thrust is limited to 5 minutes
56
AE3007A1 (LR) ITT Continuous MIN/MAX
Max = 901 C
57
AE3007A1 (LR) Oil Pressure Below 88% N2 MIN/MAX
Min = 34 psi
Max = 110 psi
(May be exceeded during starts if oil temp. is below 21 C. The engine must remain at IDLE until the pressure is less than 110 psi.) (Operation in oil pressure amber range between 111 and 115 psi is permitted in all operational modes and time limited to 5 mins, or between 116 and 155 psi in all operational modes time limited to 2 minutes. Total time above 110 psi may not exceed 5 mins.)
58
AE3007A1 (LR) Oil Pressure at or above 88% N2 MIN/MAX
Min = 50 psi
(While this is an abnormal condition, operation between 50 and 34 psi is permitted during takeoff and go around phases (for AE 3007A engines only).
Max = 110 psi
(Operation in oil pressure amber range between 111 and 115 psi is permitted in all operational modes and time limited to 5 mins, or between 116 and 155 psi in all operational modes time limited to 2 minutes. Total time above 110 psi may not exceed 5 mins.)
59
AE3007A1 (LR) Oil Temperature MIN/MAX
Min = 21 C
(Minimum oil temperature for starting is -40 C for lubrication oil specified by MIL-L-23699D.)
Max = 126 C
60
AE3007A1 (LR) Fuel Temperature MIN/MAX
Min = -54 C
Max = 52 C
61
AE3007A1 (LR) Vibration LP Spool MIN/MAX
Max = 1.8 IPS
(Vibration in the amber range below 2.5 IPS is time limited to 5 mins during the t/o or go-around phases or 10 seconds during remainder of flight phases. High vibration indicates a malfunction that may worsen and increase vibration severity. Therefore, a continuous engine operation with vibration in amber range is not recommended. According to engine vibration limits, the pilot may not elect to reduce TLA for vibration below vibration 2.5 IPS time limited to 5 mins during t/o or go-around or 10 seconds during remainder flight phases. If vibration returns to the green range within 5 mins, the flight may continue but vibration causes should be investigated before the next flight. Vibration in any phase of flight in the amber range up to 1.5 IPS for less than 30 seconds does not require mx action.)
62
AE3007A1 (LR) Vibration HP Spool MIN/MAX
Max = 1.1 IPS
(Vibration in the amber range below 2.5 IPS is time limited to 5 mins during the t/o or go-around phases or 10 seconds during remainder of flight phases. High vibration indicates a malfunction that may worsen and increase vibration severity. Therefore, a continuous engine operation with vibration in amber range is not recommended. According to engine vibration limits, the pilot may not elect to reduce TLA for vibration below vibration 2.5 IPS time limited to 5 mins during t/o or go-around or 10 seconds during remainder flight phases. If vibration returns to the green range within 5 mins, the flight may continue but vibration causes should be investigated before the next flight. Vibration in any phase of flight in the amber range up to 1.5 IPS for less than 30 seconds does not require mx action.)
63
Icing Conditions: Max. Temp. for A/I Operation
10 C
| SAT on ground or t/o and TAT in flight
64
Icing Conditions: Min. Temp. for Manual A/I Operation
-40 C
| SAT on ground or t/o and TAT in flight
65
Icing Conditions: Holding Configuration
Landing gear - UP
Flaps - UP
Min. Airspeed - 200 KIAS
66
Icing Conditions: Single-engine or single bleed
Max Altitude 15,000 ft.
67
Electrical: Max Load on Main Generator
400 amps
68
Electrical: Max Load on APU Generator
400 amps below 30,000 ft.
300 amps above 30,000 ft.
69
Electrical: Max. Battery Temp.
70 C
70
Pneumatic: Max. Differential Pressure
7.8 psi
71
Pneumatic: Max. Differential Overpressure
8.1 psi
72
Pneumatic: Max. Differential Negative Pressure
-0.3 psi
73
Flight Controls: Max. Altitude to Extend Flaps
20,000 ft.
74
Flight Controls: Maximum Airspeed after Take-off/During Climb without Re-trimming
160 KIAS
75
Maximum duration of ISIS when operating on batteries
40 minutes
76
Note on ISIS
Maximum duration of battery power can be extended to 45 mins if Pitot 3 Sensor Heating Button is turned off when not operating in icing conditions
Airplane must not be moved during power-up initialization. Do not cage attitude in turning flight.
77
Electromechanical Gust Lock
Each time electromechanical gust lock lever is set to unlocked position elevator movement must be checked. This check must be performed at least 10 seconds after positioning the gust lock lever to the unlocked position by moving the control column from the full up stop to the full down stop and back to the full up stop position.
78
Cockpit Security Door
On airplanes equipped with a cockpit security door, two crew members must be in the cockpit during all flight phases. If one of pilots leaves flight deck, he must be replaced in cockpit by another crew member. Positive identification of the person wishing to enter the flight deck must be obtained before opening the door. Security cockpit door must be kept closed and locked at all times during flight except to permit access and egress according to GOM procedures 6-1.2.1 for opening, closing and locking the door. Anytime that cockpit door is opened in flight, a challenge and response closing and locking verification procedure must be used to verify that door is closed and locked.
79
Autopilot: Min. Altitude Coupled to ILS
200 ft.
80
Autopilot: Min. Engagement Height After Takeoff
500 ft.
81
Autopilot: Single-engine Go-around
Prohibited
82
Max. Recommended Crosswind (Non-AFM) Dry Runway
30 Knots
83
Max. Recommended Crosswind (Non-AFM) Wet Runway
30 Knots
84
Max. Recommended Crosswind (Non-AFM) Runway with Compacted Snow
25 Knots
85
Max. Recommended Crosswind (Non-AFM) Runway with Standing Water or Slush
20 Knots
86
Max. Recommended Crosswind (Non-AFM) Runway with Ice (no melting)
10 Knots
87
Bleed / Pack Condition
Maximum operating altitude when one bleed or one pack is closed is 25,000 ft. (AFM).
When operating with APU bleed supplying Pack 1 (Eng. 1 bleed - closed) and engine 2 supplying Pack 2 (crossbleed closed), maximum operating altitude is 37,000 ft. (Non-AFM)
88
Engine Warm-up
Prior to take-off, the engines must be allowed to run at low thrust to stabilize the engine temperatures before take-off thrust is adjusted. After start, the engines must run at idle or taxi thrust during at least 4 minutes for cold engines (shut down for more than 90 minutes) or 2 minutes for warm engines. To increase N2 above 83% the engine oil temperature must be at 40o C minimum. In lieu of this limit, it is acceptable to either run the engine for at least 8 minutes or complete a static run- up to 88% N2, stabilize, and check to ensure that oil pressure is equal to or less than 83 psi.
89
Engine Cool-Down
The engines must run for at least 1 minute at idle or taxi thrust before shut-down.
