Limitations Flashcards
1
Q
Max. Take-off (MTOP) (1) Max N(L) % rpm
A
100%
2
Q
Autopilot approaches have been demonstrated in crosswind components up to ___. This is not considered limiting.
A
18 knots.
3
Q
Transient (20 seconds maximum) Max. Torque %
A
135 %
4
Q
Maximum cabin pressure differential limit
A
5.95 psi
5
Q
APU must not be operated during…
A
gravity refueling
6
Q
Serial numbers: 4187 and above Ramp Weight
A
65,400 lbs
7
Q
Oil pressure minimum
A
44 psi
8
Q
Maximum Oil Temperature at ground idle
A
107 C
9
Q
Powerplant Start Cranking Limits
A
START MAX TIME ON FOLLOWED BY 1 70 seconds 2 minutes off 2 70 seconds 2 minutes off 3 70 seconds 30 minutes off
10
Q
Max. Reverse Max. N(L) % rpm
A
100%
11
Q
Maneuvering Limit Load Factors Flap retracted
A
+ 2.5 g - 1. 0 g
12
Q
Route Limitation
A
The route must be within one hour flight time of a suitable airport in still air at normal cruising speed with one engine inoperative. Take-off alternates for the DHC-8-402 must be within 250 nm of the departure airport.
13
Q
Minimum SAT for engine relight is
A
-40C
14
Q
When using previously store flight plans and waypoints, the waypoints must
A
be verified for accuracy, by reference to current publication, prior to their use.
15
Q
For wind speed greater than 8 kts, with the nose of the airplane more than 30 degrees out of wind, the maximum power for ground static operation is as follows
A
WIND SPEED MAXIMUM POWER SETTING (GROUND STATIC) 9 to 20 kts Power levers angle at 60 degrees (approximately midway between FLIGHT IDLE and Take-off power detent) 21 to 35 kts FLIGHT IDLE 36 to 50 kts DISC (gusts to 55kts)
16
Q
APU Starter Cranking Limits
A
START MAX TIME ON… FOLLOWED BY… 1 60 secs 2 mins off 2 60 secs 2 mins off 3 60 secs 30 mins off NOTE: If the APU does not start in the third attempt, maintenance action is required.
17
Q
Maximum torque
A
100%
18
Q
Transient (20 seconds maximum) Max. N(H) % rpm
A
101.2%
19
Q
Max Continuous (MCP) Max. N(L) % rpm
A
100%
20
Q
Maximum fuel imbalance between the main fuel tanks
A
600 lb.
21
Q
Transient (20 seconds maximum) Max N(L) % rpm
A
102.3%
22
Q
Maneuvering Speed (Va)
A
204 KIAS
23
Q
Max. reverse Max. torque %
A
35%
24
Q
Powerplant: Maximum Altitude for Airstart
A
20,000 ft
25
Landing Gear Extended Speed (Vle)
215 KIAS
26
Standby, Auxiliary, and Main Battery Maximum loadmeter reading for takeoff
0.1
27
Transient (20 seconds maximum) Max. N(P) rpm
1173 rpm
28
Instrument approaches must be conducted in the approach mode and for
GSP approaches, RAIM must be available at the final approach fix.
29
Normal Take-off (NTOP) Max ITT C
The Normal Take-off ITT limit for a given ambient air temperature is given in "Variation of ITT with Ambient Air Temperature for NTOP" below.
30
Maximum crosswind component approved for take-off and landing, on a hard, dry or wet runway
32 knots
31
Vmo 20,000 ft
275 KIAS
32
Max. Reverse Max N(H) % rpm
100%
33
Maximum tire speed
182 kts groundspeed
34
Minimum N(H)
64.2%
35
All flaps 35 landings will be done with a maximum flap setting of...
15 during the approach to the final segment
36
Powerplant: Automatic Take-Off Power Uptrim
10% torque (nominal)
37
Maximum tailwind component approved for takeoff with flaps 5 or landing with flaps 10 or 15
10 kts
38
Starting Max ITT C
920 C 20 seconds maximum
39
Flight Compartment Communication Limit
HOT MIC select switches on the pilot and co-pilot ARCDU must be OFF and the INT/RAD switch on the observers Audio Control Panel must be centered, when using the cockpit speakers.
40
Maximum altitude for extending or extended landing gear or wing flap is
15,000 ft
41
Minimum oil temperature above ground idle
0 C (55 C for take-off in icing conditions)
42
Max Continuous (MCP) Oil Press PSID
61 to 72
43
DC Gen, AC Gen, TRU Maximum load air/ground
1.0
44
To ensure uninterrupted operating of the pilot's and co-pilot's PFD, MFD and the ED, electrical power must be cycled on all displays...
once every 24 hours (flying day)
45
Max continuous oil temperature above ground idle
107 C
46
Fuel Heater limit
Continuous operation with fuel heater outlet temperature indication below 0 C or above 71 C is prohibited.
47
Flight in conditions of _______ \_\_\_\_\_\_\_\_ _______ with autopilot engaged is \_\_\_\_\_\_\_\_\_.
severe atmospheric turbulence prohibited
48
Powerplant: With Bypass Doors Open, take-off, landing and setting MTOP and MCP are limited to a maximum ambient temperature limitation of
ISA +25 C
49
The aircraft must have approved navigation equipment appropriate to the
route of flight installed and operating so as to provide an alternate means of navigation.
50
Usable fuel tank capacities per tank
5,862 lb per tank
51
Flight Compartment Door Limit
The flight compartment door must be closed and locked at all times during flight except to provide access egress as required per the FOM and SOP400.
52
Max. Take-off (MTOP) (1) Max ITT C
880 C
53
Transient minimum oil pressure
44 to 61 psi
54
Serial numbers: 4168, 4181, 4182, 4186 Maximum Take-off Weight
64,500 lbs
55
Normal cabin pressure differential limit
5.46 +/- 0.1 psi
56
Max. Take-off (MTOP) (1) Oil press PSID
61 to 72
57
Serial numbers: 4187 and above Maximum Zero Fuel Weight
58,000 lbs
58
Minimum Runway Width
100 feet
59
Maximum crosswind component Runway with standing water, slush or wet snow
14 kts
60
Transient (20 seconds maximum) Oil Temp C
125 C Max. (5 seconds maximum for torque values above flight idle and less than 55%)
61
Rough Air Speed
210 KIAS
62
P-RNAV operations may
only be conducted with the FMS in terminal mode.
63
Flap Extended Speed (Vfe) Flap 35
158 KIAS
64
Powerplant Ambient temperature limitations
-54 C to +50 C or ISA +35 C, whichever is lower
65
Normal operating range (oil pressure)
61 to 72 psi
66
Minimum oil temperature required to ensure engine air inlet ice protection, in flight and within 3 minutes of setting take-off power
65 C
67
Oxygen Limit
At 70F the minimum Crew oxygen and Portable oxygen pressure for dispatch is as follows: Portable oxygen 1600 psi 3 Crew 1450 psi 2 Crew 1050 psi
68
Minimum oil temperature required to ensure engine air inlet ice protection, prior to take-off
55 C
69
Transient (20 seconds maximum) Oil Press PSID
44 to 61 72 to 100
70
Serial numbers: 4168, 4181, 4182, 4186 Maximum Zero Fuel Weight
57,000 lbs
71
Max. Reverse Max. ITT C
880 C
72
Instrument approaches must be accomplished in accordance with instrument approach procedures that
are retrieved from the FMS database.
73
An autopilot approach must be continued past the ______ \_\_\_\_\_\_\_ ___ or ____ feet AGL, whichever is lower, with an _______ \_\_\_\_\_\_.
final approach fix 1000 inoperative engine
74
When altitudes are manually entered before or after the
temperature compensation function is activated, it may produce VNAV paths with climb segments, and result in a VNAV disconnect.
75
Normal Take-off (NTOP) Oil Temp C
0 to 107 C
76
Max Take-off (MTOP) (1) Max Torque %
106%
77
Vmo 10,000 ft
282 KIAS
78
Navigation by means of Pilot-defined,
non published approaches under instrument meteorological conditions is prohibited.
79
Serial number: 4187 and above Forward limit (all weights up to 53,000 lbs.):
13.8% MAC
80
Max. Reverse Oil Temp C
0 to 107 C
81
Serial numbers: 4187 and above Maximum Take-off Weight
65,200 lbs
82
Flap Extended Speed (Vfe) Flap 5
200 KIAS
83
Minimum oil temperature for start up
-40 C
84
Landing Gear Operating Speed (Vlo)
200 KIAS
85
Maximum cabin pressure differential limit during taxiing, take-off and landing
0.5 psi
86
Wheel Brake Cooling Limits
Brake cooling times must be observed between a landing or a low-energy rejected take-off and a subsequent takeoff, to ensure that sufficient brake energy is available to bring the airplane to a complete stop if the subsequent takeoff is rejected.
87
Serial numbers: 4168, 4181, 4182, 4186 Maximum Landing Weight
61,750 lbs
88
Take-off Power Setting Limitation
Setting take-off power prior to brake release, with the nose of the airplane more than 45 degrees out of wind, is prohibited for wind speeds greater than 8 kts.
89
Transient (20 seconds maximum) Max ITT C
920 C
90
Maximum tailwind component approved for take-off with flaps 10 or 15 or landing with flaps 35
20 kts
91
Max Continuous (MCP) Max Torque %
100%
92
Serial Numbers: 4168, 4181, 4182, 4186 Forward limit (all weights up to 53,000 lbs.):
13.8% MAC
93
APU ambient temperature (lower)
-35 C
94
Starting Oil Temp C
-40 C min.
95
Flap Extended Speed (Vfe) Flap 10
181 KIAS
96
Normal Take-off (NTOP) Oil Press PSID
61 to 72
97
Maximum wind speed for ground operation, with nose of the airplane more than 30 degrees out of the wind
50 kts
98
Airplane minimum operating ambient temperature limit
-54 C
99
APU must be shutdown...
prior to take-off
100
Maximum operating altitude
25,000 ft
101
Taxi Limitations
Single Engine Taxi is not authorized. Reverse Taxi is no authorized. Note: Exiting the runway after a single engine landing is acceptable.
102
Max. Reverse Oil Press PSID
61 to 72
103
Powerplant Manufacturer and Model
Pratt & Whitney, PW 150A
104
Fuel display parameter is advisory only and
must not be used as the primary means for computing fuel load and range.
105
FMS based ILS and MLS approaches
are prohibited.
106
Standby, Auxiliary, and Main Battery Minimum battery temperature for takeoff
-20C
107
Starting Oil Press PSID
100 max. 165 (Maximum oil pressure at discing with OAT below 0 C)
108
For wind speed greater than 8 kts, with the nose of the airplane more than 30 degrees out of wind, the maximum power for ground maneuvering is as follows
WIND SPEED MAX POWER SETTING (GROUND) 9 to 20 kts FLIGHT IDLE (power levers may be momentarily increased above flight idle) 21 to 35 kts FLIGHT IDLE 36 to 50 kts FLIGHT IDLE (must be at DISC with airplane static)
109
Normal Take-off (NTOP) Max Torque %
90.3% (NTOP torque indication will be 90% or 91%)
110
Use of ___ without associated ___ is prohibited in ___ mode.
VOR DME APP
111
Autopilot must be ________ in _______ icing.
disengaged severe
112
Maneuvering Limit Load Factors Flap extended
+ 2.0 g 0.0 g
113
Maximum crosswind component Runway with dry loose snow (4.0 inches for take-off, 5.1 inches for landing)
18 kts
114
Propeller Manufacturer and Model
Dowty Aerospace R408
115
Max. Take-off (MTOP) (1) Max N(H) % rpm
100%
116
APP mode, autopilot engaged approaches, is approved for:
a. Flap 0 (minimum altitude: 1,000 AGL) b. Flap 5, 10, 15 and 35
117
During autopilot operation, the pilot must be ________ at the controls with _______ \_\_\_\_\_\_\_\_.
seated harness secured
118
Serial numbers: 4187 and above Maximum Landing Weight
62,000 lbs
119
Alternate Gear Extension Speed
185 KIAS
120
Max. Take-off (MTOP) (1) Max N(P) rpm
1020 (maximum allowable continuous N(P) overspeed is 1071 rpm.)
121
Max Continuous (MCP) Oil Temp C
0 to 107 C
122
In-flight operating of the ______ levers aft of the _____ \_\_\_\_ gate is prohibited.
POWER FLIGHT IDLE
123
Normal Take-off (NTOP) Max. N(P) rpm
1020 rpm Maximum allowable continuous N(P) overspeed is 1071 rpm
124
VNAV vertical path angles greater than
6 degrees in enroute and terminal mode and greater than 4 degrees in approach mode are prohibited.
125
Minimum oil temperature above FLT IDLE
0 C
126
Republic Airlines Imposed Light Limitations
On the ground, operating of landing (APPROACH and FLARE) lights is limited to 5 minutes (This does no preclude continuous operation of the TAXI light).
127
Aircraft Approach Category
Category C
128
Minimum oil temperature at ground idle
-40 C
129
Normal Take-off (NTOP) Max. N(H) % rpm
The Normal Take-off N(H) and N(L) limit for a given ambient air temperature is given in "Variation of N(H) and N(L) with Ambient Air Temperature for NTOP".
130
The FMS may only be used for
navigation guidance if the reference coordinated data system for the intended route is referenced to in WGS-84 and NAD-83.
131
Maximum runway slopes approved for take-off and landing
+ 2% (uphill) - 2% (downhill)
132
Vmo 18,000 ft
286 KIAS
133
Kinds of Operation
1. Day and night VFR 2. IFR 3. Icing Conditions
134
On precision approaches, the autopilot must be disengaged at or above a min altitude of _____ feet AGL.
200
135
Maximum oil temp PLA between Disc and FLT IDLE
125 C
136
The use of _____ \_\_\_\_ _____ FUELS is prohibited
WIDE CUT TYPE
137
Serial Numbers: 4168, 4181, 4182, 4186 Aft limit:
36.0% MAC
138
Airplane maximum operating ambient temperature limit
50 C or ISA +35 C whichever is lower
139
The UNS-1E is approved for
VFR/IFR enroute, terminal, and approach LNAV and VNAV operations.
140
APU ambient temperature (upper)
+50 C or ISA +35 C, whichever is lower
141
Serial Numbers: 4187 and above Aft limit:
36.0% MAC
142
Normal Take-off (NTOP) Max. N(L) % rpm
The Normal Take-off N(H) and N(L) limit for a given ambient air temperature is given in "Variation of N(H) and N(L) with Ambient Air Temperature for NTOP".
143
Flight above 73 degrees north latitude or below 60 degrees latitude using the
FMS may be conducted only when magnetic variation is input manually into the system or an alternate true heading source is used and no manual variation has been input.
144
With APU inlet louvres installed, APU operation is limited to
+21 C maximum ambient temperature
145
Vmo 0 to 8,000
245 KIAS
146
FMS Approach Navigation is prohibited with the ___ \_\_\_ ___ \_\_\_. IFR enroute and terminal navigation is prohibited with the ___ \_\_\_ ___ \_\_\_\_ expired unless the Pilot....
FMS Data Base expired FMS Data Base expired verifies the waypoints for accuracy by reference to current publications.
147
NOTE: Ground operations in winds greater than 50 kts must be recorded and...
the maximum wind speed provided to maintenance within 24 hours (flying day)
148
Maximum cabin altitude (pressurized flight)
8,000 ft
149
Max. Take-off (MTOP) (1) Oil temp C
0 C to 107 C
150
APU must not be operated unattended...
...with passengers onboard ...during pressure refueling
151
For non-precision approaches the autopilot must be disengaged at or above
200 ft. AGL.
152
Serial Numbers: 4187 and above Forward limit (53,000 lbs. thru 64,500 lbs.):
13.8% thru 17.7% MAC
153
Max Continuous (MCP) Max N(H) % rpm
100%
154
On RNAV approaches where vertical guidance (VNAV Mode) is used, the Company must bug
MDA plus fifty (50) feet. This is referred to as a Derived Descent Altitude (DDA) and allows for dip during a missed approach without descending below the charted LNAV MDA.
155
Max. Reverse Max N(P) rpm
1020 rpm
156
AFCS is approved for autopilot approaches to ___ \_ _____ \_\_\_\_.
CAT I limits only.
157
APU is approved for what kind of operation?
GROUND OPERATIONS ONLY
158
Max Continuous (MCP) Max N(P) rpm
1020 rpm Maximum allowable continuous N(P) overspeed is 1071 rpm
159
Maximum operation altitude for take-off and landing
10,000 ft
160
Auxiliary Fuel Pumps limitation
Tank 1 or take 2 auxiliary fuel pumps must be on for take-off and landing.
161
Whenever navigation is predicated on the FMS,
the Operator's Manual, Report no. 2423sv801 (or equivalent at current revision) must be available to the Flight Crew.
162
With Integrated Standby Instrument installed the airplane must not be operated further than
1 hour flying time from a suitable airport for landing
163
Cargo Compartment Limit
Unless the forward and aft cargo compartments are empty, the airplane must not be operated further than 1 hour flying time from a suitable airport for landing.
164
Flap Extended Speed (Vfe) Flap 15
172 KIAS
165
After take-off or go-around, the minimum height for autopilot engagement is
1,000 ft. AGL.
166
SCN 802.2, SCN 802.8: Manually entered altitudes will not have an altitude correction applied when
temperature compensation function is activated. All manually entered altitudes must be adjusted with the appropriate temperature correction before they are entered into the FMS, even if the temperature compensation function is not active.
167
Ice Protection Limit
Engine intake bypass doors must be open for engine operating in icing conditions. When ice is detected the AIRFRAME MODE SELECT selector must be positioned at FAST.
168
Vmo 25,000 ft
248 KIAS
169
Serial numbers: 4168, 4181, 4182, 4186 Ramp Weight
64,700 lbs
170
Maximum Oil Temperature above ground idle
107 C
171
Serial Numbers: 4168, 4181, 4182, 4186 Forward limit (53,000 lbs. thru 64,500.):
13.8% thru 17.4% MAC
172
Max Continuous (MCP) Max ITT C
880 C
173
Icing conditions exist when:
the SAT on the ground and for take-off is 10C or below, or SAT in flight is 5C or below, and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet or ice crystals). Icing conditions also exist when the SAT on the ground and for takeoff is 10C or below 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.
174
100%
Max. Take-off (MTOP) (1) Max N(L) % rpm
175
18 knots.
Autopilot approaches have been demonstrated in crosswind components up to \_\_\_. This is not considered limiting.
176
135 %
Transient (20 seconds maximum) Max. Torque %
177
5.95 psi
Maximum cabin pressure differential limit
178
gravity refueling
APU must not be operated during...
179
65,400 lbs
Serial numbers: 4187 and above Ramp Weight
180
44 psi
Oil pressure minimum
181
107 C
Maximum Oil Temperature at ground idle
182
START MAX TIME ON FOLLOWED BY 1 70 seconds 2 minutes off 2 70 seconds 2 minutes off 3 70 seconds 30 minutes off
Powerplant Start Cranking Limits
183
100%
Max. Reverse Max. N(L) % rpm
184
+ 2.5 g - 1. 0 g
Maneuvering Limit Load Factors Flap retracted
185
The route must be within one hour flight time of a suitable airport in still air at normal cruising speed with one engine inoperative. Take-off alternates for the DHC-8-402 must be within 250 nm of the departure airport.
Route Limitation
186
-40C
Minimum SAT for engine relight is
187
be verified for accuracy, by reference to current publication, prior to their use.
When using previously store flight plans and waypoints, the waypoints must
188
WIND SPEED MAXIMUM POWER SETTING (GROUND STATIC) 9 to 20 kts Power levers angle at 60 degrees (approximately midway between FLIGHT IDLE and Take-off power detent) 21 to 35 kts FLIGHT IDLE 36 to 50 kts DISC (gusts to 55kts)
For wind speed greater than 8 kts, with the nose of the airplane more than 30 degrees out of wind, the maximum power for ground static operation is as follows
189
START MAX TIME ON... FOLLOWED BY... 1 60 secs 2 mins off 2 60 secs 2 mins off 3 60 secs 30 mins off NOTE: If the APU does not start in the third attempt, maintenance action is required.
APU Starter Cranking Limits
190
100%
Maximum torque
191
101.2%
Transient (20 seconds maximum) Max. N(H) % rpm
192
100%
Max Continuous (MCP) Max. N(L) % rpm
193
600 lb.
Maximum fuel imbalance between the main fuel tanks
194
102.3%
Transient (20 seconds maximum) Max N(L) % rpm
195
204 KIAS
Maneuvering Speed (Va)
196
35%
Max. reverse Max. torque %
197
20,000 ft
Powerplant: Maximum Altitude for Airstart
198
215 KIAS
Landing Gear Extended Speed (Vle)
199
0.1
Standby, Auxiliary, and Main Battery Maximum loadmeter reading for takeoff
200
1173 rpm
Transient (20 seconds maximum) Max. N(P) rpm
201
GSP approaches, RAIM must be available at the final approach fix.
Instrument approaches must be conducted in the approach mode and for
202
The Normal Take-off ITT limit for a given ambient air temperature is given in "Variation of ITT with Ambient Air Temperature for NTOP" below.
Normal Take-off (NTOP) Max ITT C
203
32 knots
Maximum crosswind component approved for take-off and landing, on a hard, dry or wet runway
204
275 KIAS
Vmo 20,000 ft
205
100%
Max. Reverse Max N(H) % rpm
206
182 kts groundspeed
Maximum tire speed
207
64.2%
Minimum N(H)
208
15 during the approach to the final segment
All flaps 35 landings will be done with a maximum flap setting of...
209
10% torque (nominal)
Powerplant: Automatic Take-Off Power Uptrim
210
10 kts
Maximum tailwind component approved for takeoff with flaps 5 or landing with flaps 10 or 15
211
920 C 20 seconds maximum
Starting Max ITT C
212
HOT MIC select switches on the pilot and co-pilot ARCDU must be OFF and the INT/RAD switch on the observers Audio Control Panel must be centered, when using the cockpit speakers.
Flight Compartment Communication Limit
213
15,000 ft
Maximum altitude for extending or extended landing gear or wing flap is
214
0 C (55 C for take-off in icing conditions)
Minimum oil temperature above ground idle
215
61 to 72
Max Continuous (MCP) Oil Press PSID
216
1.0
Standby, Auxiliary, and Main Battery Maximum load air/ground
217
once every 24 hours (flying day)
To ensure uninterrupted operating of the pilot's and co-pilot's PFD, MFD and the ED, electrical power must be cycled on all displays...
218
107 C
Max continuous oil temperature above ground idle
219
Continuous operation with fuel heater outlet temperature indication below 0 C or above 71 C is prohibited.
Fuel Heater limit
220
severe atmospheric turbulence prohibited
Flight in conditions of _______ \_\_\_\_\_\_\_\_ _______ with autopilot engaged is \_\_\_\_\_\_\_\_\_.
221
ISA +25 C
Powerplant: With Bypass Doors Open, take-off, landing and setting MTOP and MCP are limited to a maximum ambient temperature limitation of
222
route of flight installed and operating so as to provide an alternate means of navigation.
The aircraft must have approved navigation equipment appropriate to the
223
5,862 lb per tank
Usable fuel tank capacities per tank
224
The flight compartment door must be closed and locked at all times during flight except to provide access egress as required per the FOM and SOP400.
Flight Compartment Door Limit
225
880 C
Max. Take-off (MTOP) (1) Max ITT C
226
44 to 61 psi
Transient minimum oil pressure
227
64,500 lbs
Serial numbers: 4168, 4181, 4182, 4186 Maximum Take-off Weight
228
5.46 +/- 0.1 psi
Normal cabin pressure differential limit
229
61 to 72
Max. Take-off (MTOP) (1) Oil press PSID
230
58,000 lbs
Serial numbers: 4187 and above Maximum Zero Fuel Weight
231
100 feet
Minimum Runway Width
232
14 kts
Maximum crosswind component Runway with standing water, slush or wet snow
233
125 C Max. (5 seconds maximum for torque values above flight idle and less than 55%)
Transient (20 seconds maximum) Oil Temp C
234
210 KIAS
Rough Air Speed
235
only be conducted with the FMS in terminal mode.
P-RNAV operations may
236
158 KIAS
Flap Extended Speed (Vfe) Flap 35
237
-54 C to +50 C or ISA +35 C, whichever is lower
Powerplant Ambient temperature limitations
238
61 to 72 psi
Normal operating range (oil pressure)
239
65 C
Minimum oil temperature required to ensure engine air inlet ice protection, in flight and within 3 minutes of setting take-off power
240
At 70F the minimum Crew oxygen and Portable oxygen pressure for dispatch is as follows: Portable oxygen 1600 psi 3 Crew 1450 psi 2 Crew 1050 psi
Oxygen Limit
241
55 C
Minimum oil temperature required to ensure engine air inlet ice protection, prior to take-off
242
44 to 61 72 to 100
Transient (20 seconds maximum) Oil Press PSID
243
57,000 lbs
Serial numbers: 4168, 4181, 4182, 4186 Maximum Zero Fuel Weight
244
880 C
Max. Reverse Max. ITT C
245
are retrieved from the FMS database.
Instrument approaches must be accomplished in accordance with instrument approach procedures that
246
final approach fix 1000 inoperative engine
An autopilot approach must be continued past the ______ \_\_\_\_\_\_\_ ___ or ____ feet AGL, whichever is lower, with an _______ \_\_\_\_\_\_.
247
temperature compensation function is activated, it may produce VNAV paths with climb segments, and result in a VNAV disconnect.
When altitudes are manually entered before or after the
248
0 to 107 C
Normal Take-off (NTOP) Oil Temp C
249
106%
Max Take-off (MTOP) (1) Max Torque %
250
282 KIAS
Vmo 10,000 ft
251
non published approaches under instrument meteorological conditions is prohibited.
Navigation by means of Pilot-defined,
252
13.8% MAC
Serial number: 4187 and above Forward limit (all weights up to 53,000 lbs.):
253
0 to 107 C
Max. Reverse Oil Temp C
254
65,200 lbs
Serial numbers: 4187 and above Maximum Take-off Weight
255
200 KIAS
Flap Extended Speed (Vfe) Flap 5
256
-40 C
Minimum oil temperature for start up
257
200 KIAS
Landing Gear Operating Speed (Vlo)
258
0.5 psi
Maximum cabin pressure differential limit during taxiing, take-off and landing
259
Brake cooling times must be observed between a landing or a low-energy rejected take-off and a subsequent takeoff, to ensure that sufficient brake energy is available to bring the airplane to a complete stop if the subsequent takeoff is rejected.
Wheel Brake Cooling Limits
260
61,750 lbs
Serial numbers: 4168, 4181, 4182, 4186 Maximum Landing Weight
261
Setting take-off power prior to brake release, with the nose of the airplane more than 45 degrees out of wind, is prohibited for wind speeds greater than 8 kts.
Take-off Power Setting Limitation
262
920 C
Transient (20 seconds maximum) Max ITT C
263
20 kts
Maximum tailwind component approved for take-off with flaps 10 or 15 or landing with flaps 35
264
100%
Max Continuous (MCP) Max Torque %
265
13.8% MAC
Serial Numbers: 4168, 4181, 4182, 4186 Forward limit (all weights up to 53,000 lbs.):
266
-35 C
APU ambient temperature (lower)
267
-40 C min.
Starting Oil Temp C
268
181 KIAS
Flap Extended Speed (Vfe) Flap 10
269
61 to 72
Normal Take-off (NTOP) Oil Press PSID
270
50 kts
Maximum wind speed for ground operation, with nose of the airplane more than 30 degrees out of the wind
271
-54 C
Airplane minimum operating ambient temperature limit
272
prior to take-off
APU must be shutdown...
273
25,000 ft
Maximum operating altitude
274
Single Engine Taxi is not authorized. Reverse Taxi is no authorized. Note: Exiting the runway after a single engine landing is acceptable.
Taxi Limitations
275
61 to 72
Max. Reverse Oil Press PSID
276
Pratt & Whitney, PW 150A
Powerplant Manufacturer and Model
277
must not be used as the primary means for computing fuel load and range.
Fuel display parameter is advisory only and
278
are prohibited.
FMS based ILS and MLS approaches
279
-20C
Standby, Auxiliary, and Main Battery Minimum battery temperature for takeoff
280
100 max. 165 (Maximum oil pressure at discing with OAT below 0 C)
Starting Oil Press PSID
281
WIND SPEED MAX POWER SETTING (GROUND) 9 to 20 kts FLIGHT IDLE (power levers may be momentarily increased above flight idle) 21 to 35 kts FLIGHT IDLE 36 to 50 kts FLIGHT IDLE (must be at DISC with airplane static)
For wind speed greater than 8 kts, with the nose of the airplane more than 30 degrees out of wind, the maximum power for ground maneuvering is as follows
282
90.3% (NTOP torque indication will be 90% or 91%)
Normal Take-off (NTOP) Max Torque %
283
VOR DME APP
Use of ___ without associated ___ is prohibited in ___ mode.
284
disengaged severe
Autopilot must be ________ in _______ icing.
285
+ 2.0 g 0.0 g
Maneuvering Limit Load Factors Flap extended
286
18 kts
Maximum crosswind component Runway with dry loose snow (4.0 inches for take-off, 5.1 inches for landing)
287
Dowty Aerospace R408
Propeller Manufacturer and Model
288
100%
Max. Take-off (MTOP) (1) Max N(H) % rpm
289
a. Flap 0 (minimum altitude: 1,000 AGL) b. Flap 5, 10, 15 and 35
APP mode, autopilot engaged approaches, is approved for:
290
seated harness secured
During autopilot operation, the pilot must be ________ at the controls with _______ \_\_\_\_\_\_\_\_.
291
62,000 lbs
Serial numbers: 4187 and above Maximum Landing Weight
292
185 KIAS
Alternate Gear Extension Speed
293
1020 (maximum allowable continuous N(P) overspeed is 1071 rpm.)
Max. Take-off (MTOP) (1) Max N(P) rpm
294
0 to 107 C
Max Continuous (MCP) Oil Temp C
295
POWER FLIGHT IDLE
In-flight operating of the ______ levers aft of the _____ \_\_\_\_ gate is prohibited.
296
1020 rpm Maximum allowable continuous N(P) overspeed is 1071 rpm
Normal Take-off (NTOP) Max. N(P) rpm
297
6 degrees in enroute and terminal mode and greater than 4 degrees in approach mode are prohibited.
VNAV vertical path angles greater than
298
0 C
Minimum oil temperature above FLT IDLE
299
On the ground, operating of landing (APPROACH and FLARE) lights is limited to 5 minutes (This does no preclude continuous operation of the TAXI light).
Republic Airlines Imposed Light Limitations
300
Category C
Aircraft Approach Category
301
-40 C
Minimum oil temperature at ground idle
302
The Normal Take-off N(H) and N(L) limit for a given ambient air temperature is given in "Variation of N(H) and N(L) with Ambient Air Temperature for NTOP".
Normal Take-off (NTOP) Max. N(H) % rpm
303
navigation guidance if the reference coordinated data system for the intended route is referenced to in WGS-84 and NAD-83.
The FMS may only be used for
304
+ 2% (uphill) - 2% (downhill)
Maximum runway slopes approved for take-off and landing
305
286 KIAS
Vmo 18,000 ft
306
1. Day and night VFR 2. IFR 3. Icing Conditions
Kinds of Operation
307
200
On precision approaches, the autopilot must be disengaged at or above a min altitude of _____ feet AGL.
308
125 C
Maximum oil temp PLA between Disc and FLT IDLE
309
WIDE CUT TYPE
The use of _____ \_\_\_\_ _____ FUELS is prohibited
310
36.0% MAC
Serial Numbers: 4168, 4181, 4182, 4186 Aft limit:
311
50 C or ISA +35 C whichever is lower
Airplane maximum operating ambient temperature limit
312
VFR/IFR enroute, terminal, and approach LNAV and VNAV operations.
The UNS-1E is approved for
313
+50 C or ISA +35 C, whichever is lower
APU ambient temperature (upper)
314
36.0% MAC
Serial Numbers: 4187 and above Aft limit:
315
The Normal Take-off N(H) and N(L) limit for a given ambient air temperature is given in "Variation of N(H) and N(L) with Ambient Air Temperature for NTOP".
Normal Take-off (NTOP) Max. N(L) % rpm
316
FMS may be conducted only when magnetic variation is input manually into the system or an alternate true heading source is used and no manual variation has been input.
Flight above 73 degrees north latitude or below 60 degrees latitude using the
317
+21 C maximum ambient temperature
With APU inlet louvres installed, APU operation is limited to
318
245 KIAS
Vmo 0 to 8,000
319
FMS Data Base expired FMS Data Base expired verifies the waypoints for accuracy by reference to current publications.
FMS Approach Navigation is prohibited with the ___ \_\_\_ ___ \_\_\_. IFR enroute and terminal navigation is prohibited with the ___ \_\_\_ ___ \_\_\_\_ expired unless the Pilot....
320
the maximum wind speed provided to maintenance within 24 hours (flying day)
NOTE: Ground operations in winds greater than 50 kts must be recorded and...
321
8,000 ft
Maximum cabin altitude (pressurized flight)
322
0 C to 107 C
Max. Take-off (MTOP) (1) Oil temp C
323
...with passengers onboard ...during pressure refueling
APU must not be operated unattended...
324
200 ft. AGL.
For non-precision approaches the autopilot must be disengaged at or above
325
13.8% thru 17.7% MAC
Serial Numbers: 4187 and above Forward limit (53,000 lbs. thru 64,500 lbs.):
326
100%
Max Continuous (MCP) Max N(H) % rpm
327
MDA plus fifty (50) feet. This is referred to as a Derived Descent Altitude (DDA) and allows for dip during a missed approach without descending below the charted LNAV MDA.
On RNAV approaches where vertical guidance (VNAV Mode) is used, the Company must bug
328
1020 rpm
Max. Reverse Max N(P) rpm
329
CAT I limits only.
AFCS is approved for autopilot approaches to ___ \_ _____ \_\_\_\_.
330
GROUND OPERATIONS ONLY
APU is approved for what kind of operation?
331
1020 rpm Maximum allowable continuous N(P) overspeed is 1071 rpm
Max Continuous (MCP) Max N(P) rpm
332
10,000 ft
Maximum operation altitude for take-off and landing
333
Tank 1 or take 2 auxiliary fuel pumps must be on for take-off and landing.
Auxiliary Fuel Pumps limitation
334
the Operator's Manual, Report no. 2423sv801 (or equivalent at current revision) must be available to the Flight Crew.
Whenever navigation is predicated on the FMS,
335
1 hour flying time from a suitable airport for landing
With Integrated Standby Instrument installed the airplane must not be operated further than
336
Unless the forward and aft cargo compartments are empty, the airplane must not be operated further than 1 hour flying time from a suitable airport for landing.
Cargo Compartment Limit
337
172 KIAS
Flap Extended Speed (Vfe) Flap 15
338
1,000 ft. AGL.
After take-off or go-around, the minimum height for autopilot engagement is
339
temperature compensation function is activated. All manually entered altitudes must be adjusted with the appropriate temperature correction before they are entered into the FMS, even if the temperature compensation function is not active.
SCN 802.2, SCN 802.8: Manually entered altitudes will not have an altitude correction applied when
340
Engine intake bypass doors must be open for engine operating in icing conditions. When ice is detected the AIRFRAME MODE SELECT selector must be positioned at FAST.
Ice Protection Limit
341
248 KIAS
Vmo 25,000 ft
342
64,700 lbs
Serial numbers: 4168, 4181, 4182, 4186 Ramp Weight
343
107 C
Maximum Oil Temperature above ground idle
344
13.8% thru 17.4% MAC
Serial Numbers: 4168, 4181, 4182, 4186 Forward limit (53,000 lbs. thru 64,500.):
345
880 C
Max Continuous (MCP) Max ITT C
346
the SAT on the ground and for take-off is 10C or below, or SAT in flight is 5C or below, and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet or ice crystals). Icing conditions also exist when the SAT on the ground and for takeoff is 10C or below 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.
Icing conditions exist when:
