Limitations Flashcards
Max. Take-off (MTOP) (1) Max N(L) % rpm
100%
Autopilot approaches have been demonstrated in crosswind components up to ___. This is not considered limiting.
18 knots.
Transient (20 seconds maximum) Max. Torque %
135 %
Maximum cabin pressure differential limit
5.95 psi
APU must not be operated during…
gravity refueling
Serial numbers: 4187 and above Ramp Weight
65,400 lbs
Oil pressure minimum
44 psi
Maximum Oil Temperature at ground idle
107 C
Powerplant Start Cranking Limits
START MAX TIME ON FOLLOWED BY 1 70 seconds 2 minutes off 2 70 seconds 2 minutes off 3 70 seconds 30 minutes off
Max. Reverse Max. N(L) % rpm
100%
Maneuvering Limit Load Factors Flap retracted
+ 2.5 g - 1. 0 g
Route Limitation
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.
Minimum SAT for engine relight is
-40C
When using previously store flight plans and waypoints, the waypoints must
be verified for accuracy, by reference to current publication, prior to their use.
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
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)
APU Starter Cranking Limits
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.
Maximum torque
100%
Transient (20 seconds maximum) Max. N(H) % rpm
101.2%
Max Continuous (MCP) Max. N(L) % rpm
100%
Maximum fuel imbalance between the main fuel tanks
600 lb.
Transient (20 seconds maximum) Max N(L) % rpm
102.3%
Maneuvering Speed (Va)
204 KIAS
Max. reverse Max. torque %
35%
Powerplant: Maximum Altitude for Airstart
20,000 ft
Landing Gear Extended Speed (Vle)
215 KIAS
Standby, Auxiliary, and Main Battery Maximum loadmeter reading for takeoff
0.1
Transient (20 seconds maximum) Max. N(P) rpm
1173 rpm
Instrument approaches must be conducted in the approach mode and for
GSP approaches, RAIM must be available at the final approach fix.
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.
Maximum crosswind component approved for take-off and landing, on a hard, dry or wet runway
32 knots
Vmo 20,000 ft
275 KIAS
Max. Reverse Max N(H) % rpm
100%
Maximum tire speed
182 kts groundspeed
Minimum N(H)
64.2%
All flaps 35 landings will be done with a maximum flap setting of…
15 during the approach to the final segment
Powerplant: Automatic Take-Off Power Uptrim
10% torque (nominal)
Maximum tailwind component approved for takeoff with flaps 5 or landing with flaps 10 or 15
10 kts
Starting Max ITT C
920 C 20 seconds maximum
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.
Maximum altitude for extending or extended landing gear or wing flap is
15,000 ft
Minimum oil temperature above ground idle
0 C (55 C for take-off in icing conditions)
Max Continuous (MCP) Oil Press PSID
61 to 72
DC Gen, AC Gen, TRU Maximum load air/ground
1.0
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)
Max continuous oil temperature above ground idle
107 C
Fuel Heater limit
Continuous operation with fuel heater outlet temperature indication below 0 C or above 71 C is prohibited.
Flight in conditions of _______ ________ _______ with autopilot engaged is _________.
severe atmospheric turbulence prohibited
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
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.
Usable fuel tank capacities per tank
5,862 lb per tank
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.
Max. Take-off (MTOP) (1) Max ITT C
880 C
Transient minimum oil pressure
44 to 61 psi
Serial numbers: 4168, 4181, 4182, 4186 Maximum Take-off Weight
64,500 lbs
Normal cabin pressure differential limit
5.46 +/- 0.1 psi
Max. Take-off (MTOP) (1) Oil press PSID
61 to 72
Serial numbers: 4187 and above Maximum Zero Fuel Weight
58,000 lbs
Minimum Runway Width
100 feet
Maximum crosswind component Runway with standing water, slush or wet snow
14 kts
Transient (20 seconds maximum) Oil Temp C
125 C Max. (5 seconds maximum for torque values above flight idle and less than 55%)
Rough Air Speed
210 KIAS
P-RNAV operations may
only be conducted with the FMS in terminal mode.
Flap Extended Speed (Vfe) Flap 35
158 KIAS
Powerplant Ambient temperature limitations
-54 C to +50 C or ISA +35 C, whichever is lower
Normal operating range (oil pressure)
61 to 72 psi
Minimum oil temperature required to ensure engine air inlet ice protection, in flight and within 3 minutes of setting take-off power
65 C
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
Minimum oil temperature required to ensure engine air inlet ice protection, prior to take-off
55 C
Transient (20 seconds maximum) Oil Press PSID
44 to 61 72 to 100
Serial numbers: 4168, 4181, 4182, 4186 Maximum Zero Fuel Weight
57,000 lbs
Max. Reverse Max. ITT C
880 C
Instrument approaches must be accomplished in accordance with instrument approach procedures that
are retrieved from the FMS database.
An autopilot approach must be continued past the ______ _______ ___ or ____ feet AGL, whichever is lower, with an _______ ______.
final approach fix 1000 inoperative engine
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.
Normal Take-off (NTOP) Oil Temp C
0 to 107 C
Max Take-off (MTOP) (1) Max Torque %
106%
Vmo 10,000 ft
282 KIAS
Navigation by means of Pilot-defined,
non published approaches under instrument meteorological conditions is prohibited.
Serial number: 4187 and above Forward limit (all weights up to 53,000 lbs.):
13.8% MAC
Max. Reverse Oil Temp C
0 to 107 C
Serial numbers: 4187 and above Maximum Take-off Weight
65,200 lbs
Flap Extended Speed (Vfe) Flap 5
200 KIAS
Minimum oil temperature for start up
-40 C
Landing Gear Operating Speed (Vlo)
200 KIAS
Maximum cabin pressure differential limit during taxiing, take-off and landing
0.5 psi
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.
Serial numbers: 4168, 4181, 4182, 4186 Maximum Landing Weight
61,750 lbs
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.
Transient (20 seconds maximum) Max ITT C
920 C
Maximum tailwind component approved for take-off with flaps 10 or 15 or landing with flaps 35
20 kts
Max Continuous (MCP) Max Torque %
100%
Serial Numbers: 4168, 4181, 4182, 4186 Forward limit (all weights up to 53,000 lbs.):
13.8% MAC
APU ambient temperature (lower)
-35 C
Starting Oil Temp C
-40 C min.
Flap Extended Speed (Vfe) Flap 10
181 KIAS
Normal Take-off (NTOP) Oil Press PSID
61 to 72
Maximum wind speed for ground operation, with nose of the airplane more than 30 degrees out of the wind
50 kts
Airplane minimum operating ambient temperature limit
-54 C
APU must be shutdown…
prior to take-off
Maximum operating altitude
25,000 ft
Taxi Limitations
Single Engine Taxi is not authorized. Reverse Taxi is no authorized. Note: Exiting the runway after a single engine landing is acceptable.
Max. Reverse Oil Press PSID
61 to 72
Powerplant Manufacturer and Model
Pratt & Whitney, PW 150A
Fuel display parameter is advisory only and
must not be used as the primary means for computing fuel load and range.
FMS based ILS and MLS approaches
are prohibited.
Standby, Auxiliary, and Main Battery Minimum battery temperature for takeoff
-20C
Starting Oil Press PSID
100 max. 165 (Maximum oil pressure at discing with OAT below 0 C)
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)
Normal Take-off (NTOP) Max Torque %
90.3% (NTOP torque indication will be 90% or 91%)
Use of ___ without associated ___ is prohibited in ___ mode.
VOR DME APP
Autopilot must be ________ in _______ icing.
disengaged severe
Maneuvering Limit Load Factors Flap extended
+ 2.0 g 0.0 g
Maximum crosswind component Runway with dry loose snow (4.0 inches for take-off, 5.1 inches for landing)
18 kts
Propeller Manufacturer and Model
Dowty Aerospace R408
Max. Take-off (MTOP) (1) Max N(H) % rpm
100%
APP mode, autopilot engaged approaches, is approved for:
a. Flap 0 (minimum altitude: 1,000 AGL) b. Flap 5, 10, 15 and 35
During autopilot operation, the pilot must be ________ at the controls with _______ ________.
seated harness secured
Serial numbers: 4187 and above Maximum Landing Weight
62,000 lbs
Alternate Gear Extension Speed
185 KIAS
Max. Take-off (MTOP) (1) Max N(P) rpm
1020 (maximum allowable continuous N(P) overspeed is 1071 rpm.)
Max Continuous (MCP) Oil Temp C
0 to 107 C
In-flight operating of the ______ levers aft of the _____ ____ gate is prohibited.
POWER FLIGHT IDLE
Normal Take-off (NTOP) Max. N(P) rpm
1020 rpm Maximum allowable continuous N(P) overspeed is 1071 rpm
VNAV vertical path angles greater than
6 degrees in enroute and terminal mode and greater than 4 degrees in approach mode are prohibited.
Minimum oil temperature above FLT IDLE
0 C
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).
Aircraft Approach Category
Category C
Minimum oil temperature at ground idle
-40 C
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”.
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.
Maximum runway slopes approved for take-off and landing
+ 2% (uphill) - 2% (downhill)
Vmo 18,000 ft
286 KIAS
Kinds of Operation
- Day and night VFR 2. IFR 3. Icing Conditions
On precision approaches, the autopilot must be disengaged at or above a min altitude of _____ feet AGL.
200
Maximum oil temp PLA between Disc and FLT IDLE
125 C
The use of _____ ____ _____ FUELS is prohibited
WIDE CUT TYPE
Serial Numbers: 4168, 4181, 4182, 4186 Aft limit:
36.0% MAC
Airplane maximum operating ambient temperature limit
50 C or ISA +35 C whichever is lower
The UNS-1E is approved for
VFR/IFR enroute, terminal, and approach LNAV and VNAV operations.
APU ambient temperature (upper)
+50 C or ISA +35 C, whichever is lower
Serial Numbers: 4187 and above Aft limit:
36.0% MAC
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”.
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.
With APU inlet louvres installed, APU operation is limited to
+21 C maximum ambient temperature
Vmo 0 to 8,000
245 KIAS
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.
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)
Maximum cabin altitude (pressurized flight)
8,000 ft
Max. Take-off (MTOP) (1) Oil temp C
0 C to 107 C
APU must not be operated unattended…
…with passengers onboard …during pressure refueling
For non-precision approaches the autopilot must be disengaged at or above
200 ft. AGL.
Serial Numbers: 4187 and above Forward limit (53,000 lbs. thru 64,500 lbs.):
13.8% thru 17.7% MAC
Max Continuous (MCP) Max N(H) % rpm
100%
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.
Max. Reverse Max N(P) rpm
1020 rpm
AFCS is approved for autopilot approaches to ___ _ _____ ____.
CAT I limits only.
APU is approved for what kind of operation?
GROUND OPERATIONS ONLY
Max Continuous (MCP) Max N(P) rpm
1020 rpm Maximum allowable continuous N(P) overspeed is 1071 rpm
Maximum operation altitude for take-off and landing
10,000 ft
Auxiliary Fuel Pumps limitation
Tank 1 or take 2 auxiliary fuel pumps must be on for take-off and landing.
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.
With Integrated Standby Instrument installed the airplane must not be operated further than
1 hour flying time from a suitable airport for landing
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.
Flap Extended Speed (Vfe) Flap 15
172 KIAS
After take-off or go-around, the minimum height for autopilot engagement is
1,000 ft. AGL.
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.
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.
Vmo 25,000 ft
248 KIAS
Serial numbers: 4168, 4181, 4182, 4186 Ramp Weight
64,700 lbs
Maximum Oil Temperature above ground idle
107 C
Serial Numbers: 4168, 4181, 4182, 4186 Forward limit (53,000 lbs. thru 64,500.):
13.8% thru 17.4% MAC
Max Continuous (MCP) Max ITT C
880 C
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.
100%
Max. Take-off (MTOP) (1) Max N(L) % rpm
18 knots.
Autopilot approaches have been demonstrated in crosswind components up to ___. This is not considered limiting.
135 %
Transient (20 seconds maximum) Max. Torque %
5.95 psi
Maximum cabin pressure differential limit
gravity refueling
APU must not be operated during…
65,400 lbs
Serial numbers: 4187 and above Ramp Weight
44 psi
Oil pressure minimum
107 C
Maximum Oil Temperature at ground idle
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
100%
Max. Reverse Max. N(L) % rpm
+ 2.5 g - 1. 0 g
Maneuvering Limit Load Factors Flap retracted
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
-40C
Minimum SAT for engine relight is
be verified for accuracy, by reference to current publication, prior to their use.
When using previously store flight plans and waypoints, the waypoints must
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
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
100%
Maximum torque
101.2%
Transient (20 seconds maximum) Max. N(H) % rpm
100%
Max Continuous (MCP) Max. N(L) % rpm
600 lb.
Maximum fuel imbalance between the main fuel tanks
102.3%
Transient (20 seconds maximum) Max N(L) % rpm
204 KIAS
Maneuvering Speed (Va)
35%
Max. reverse Max. torque %
20,000 ft
Powerplant: Maximum Altitude for Airstart
215 KIAS
Landing Gear Extended Speed (Vle)
0.1
Standby, Auxiliary, and Main Battery Maximum loadmeter reading for takeoff
1173 rpm
Transient (20 seconds maximum) Max. N(P) rpm
GSP approaches, RAIM must be available at the final approach fix.
Instrument approaches must be conducted in the approach mode and for
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
32 knots
Maximum crosswind component approved for take-off and landing, on a hard, dry or wet runway
275 KIAS
Vmo 20,000 ft
100%
Max. Reverse Max N(H) % rpm
182 kts groundspeed
Maximum tire speed
64.2%
Minimum N(H)
15 during the approach to the final segment
All flaps 35 landings will be done with a maximum flap setting of…
10% torque (nominal)
Powerplant: Automatic Take-Off Power Uptrim
10 kts
Maximum tailwind component approved for takeoff with flaps 5 or landing with flaps 10 or 15
920 C 20 seconds maximum
Starting Max ITT C
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
15,000 ft
Maximum altitude for extending or extended landing gear or wing flap is
0 C (55 C for take-off in icing conditions)
Minimum oil temperature above ground idle
61 to 72
Max Continuous (MCP) Oil Press PSID
1.0
Standby, Auxiliary, and Main Battery Maximum load air/ground
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…
107 C
Max continuous oil temperature above ground idle
Continuous operation with fuel heater outlet temperature indication below 0 C or above 71 C is prohibited.
Fuel Heater limit
severe atmospheric turbulence prohibited
Flight in conditions of _______ ________ _______ with autopilot engaged is _________.
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
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
5,862 lb per tank
Usable fuel tank capacities per tank
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
880 C
Max. Take-off (MTOP) (1) Max ITT C
44 to 61 psi
Transient minimum oil pressure
64,500 lbs
Serial numbers: 4168, 4181, 4182, 4186 Maximum Take-off Weight
5.46 +/- 0.1 psi
Normal cabin pressure differential limit
61 to 72
Max. Take-off (MTOP) (1) Oil press PSID
58,000 lbs
Serial numbers: 4187 and above Maximum Zero Fuel Weight
100 feet
Minimum Runway Width
14 kts
Maximum crosswind component Runway with standing water, slush or wet snow
125 C Max. (5 seconds maximum for torque values above flight idle and less than 55%)
Transient (20 seconds maximum) Oil Temp C
210 KIAS
Rough Air Speed
only be conducted with the FMS in terminal mode.
P-RNAV operations may
158 KIAS
Flap Extended Speed (Vfe) Flap 35
-54 C to +50 C or ISA +35 C, whichever is lower
Powerplant Ambient temperature limitations
61 to 72 psi
Normal operating range (oil pressure)
65 C
Minimum oil temperature required to ensure engine air inlet ice protection, in flight and within 3 minutes of setting take-off power
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
55 C
Minimum oil temperature required to ensure engine air inlet ice protection, prior to take-off
44 to 61 72 to 100
Transient (20 seconds maximum) Oil Press PSID
57,000 lbs
Serial numbers: 4168, 4181, 4182, 4186 Maximum Zero Fuel Weight
880 C
Max. Reverse Max. ITT C
are retrieved from the FMS database.
Instrument approaches must be accomplished in accordance with instrument approach procedures that
final approach fix 1000 inoperative engine
An autopilot approach must be continued past the ______ _______ ___ or ____ feet AGL, whichever is lower, with an _______ ______.
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
0 to 107 C
Normal Take-off (NTOP) Oil Temp C
106%
Max Take-off (MTOP) (1) Max Torque %
282 KIAS
Vmo 10,000 ft
non published approaches under instrument meteorological conditions is prohibited.
Navigation by means of Pilot-defined,
13.8% MAC
Serial number: 4187 and above Forward limit (all weights up to 53,000 lbs.):
0 to 107 C
Max. Reverse Oil Temp C
65,200 lbs
Serial numbers: 4187 and above Maximum Take-off Weight
200 KIAS
Flap Extended Speed (Vfe) Flap 5
-40 C
Minimum oil temperature for start up
200 KIAS
Landing Gear Operating Speed (Vlo)
0.5 psi
Maximum cabin pressure differential limit during taxiing, take-off and landing
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
61,750 lbs
Serial numbers: 4168, 4181, 4182, 4186 Maximum Landing Weight
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
920 C
Transient (20 seconds maximum) Max ITT C
20 kts
Maximum tailwind component approved for take-off with flaps 10 or 15 or landing with flaps 35
100%
Max Continuous (MCP) Max Torque %
13.8% MAC
Serial Numbers: 4168, 4181, 4182, 4186 Forward limit (all weights up to 53,000 lbs.):
-35 C
APU ambient temperature (lower)
-40 C min.
Starting Oil Temp C
181 KIAS
Flap Extended Speed (Vfe) Flap 10
61 to 72
Normal Take-off (NTOP) Oil Press PSID
50 kts
Maximum wind speed for ground operation, with nose of the airplane more than 30 degrees out of the wind
-54 C
Airplane minimum operating ambient temperature limit
prior to take-off
APU must be shutdown…
25,000 ft
Maximum operating altitude
Single Engine Taxi is not authorized. Reverse Taxi is no authorized. Note: Exiting the runway after a single engine landing is acceptable.
Taxi Limitations
61 to 72
Max. Reverse Oil Press PSID
Pratt & Whitney, PW 150A
Powerplant Manufacturer and Model
must not be used as the primary means for computing fuel load and range.
Fuel display parameter is advisory only and
are prohibited.
FMS based ILS and MLS approaches
-20C
Standby, Auxiliary, and Main Battery Minimum battery temperature for takeoff
100 max. 165 (Maximum oil pressure at discing with OAT below 0 C)
Starting Oil Press PSID
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
90.3% (NTOP torque indication will be 90% or 91%)
Normal Take-off (NTOP) Max Torque %
VOR DME APP
Use of ___ without associated ___ is prohibited in ___ mode.
disengaged severe
Autopilot must be ________ in _______ icing.
+ 2.0 g 0.0 g
Maneuvering Limit Load Factors Flap extended
18 kts
Maximum crosswind component Runway with dry loose snow (4.0 inches for take-off, 5.1 inches for landing)
Dowty Aerospace R408
Propeller Manufacturer and Model
100%
Max. Take-off (MTOP) (1) Max N(H) % rpm
a. Flap 0 (minimum altitude: 1,000 AGL) b. Flap 5, 10, 15 and 35
APP mode, autopilot engaged approaches, is approved for:
seated harness secured
During autopilot operation, the pilot must be ________ at the controls with _______ ________.
62,000 lbs
Serial numbers: 4187 and above Maximum Landing Weight
185 KIAS
Alternate Gear Extension Speed
1020 (maximum allowable continuous N(P) overspeed is 1071 rpm.)
Max. Take-off (MTOP) (1) Max N(P) rpm
0 to 107 C
Max Continuous (MCP) Oil Temp C
POWER FLIGHT IDLE
In-flight operating of the ______ levers aft of the _____ ____ gate is prohibited.
1020 rpm Maximum allowable continuous N(P) overspeed is 1071 rpm
Normal Take-off (NTOP) Max. N(P) rpm
6 degrees in enroute and terminal mode and greater than 4 degrees in approach mode are prohibited.
VNAV vertical path angles greater than
0 C
Minimum oil temperature above FLT IDLE
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
Category C
Aircraft Approach Category
-40 C
Minimum oil temperature at ground idle
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
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
+ 2% (uphill) - 2% (downhill)
Maximum runway slopes approved for take-off and landing
286 KIAS
Vmo 18,000 ft
- Day and night VFR 2. IFR 3. Icing Conditions
Kinds of Operation
200
On precision approaches, the autopilot must be disengaged at or above a min altitude of _____ feet AGL.
125 C
Maximum oil temp PLA between Disc and FLT IDLE
WIDE CUT TYPE
The use of _____ ____ _____ FUELS is prohibited
36.0% MAC
Serial Numbers: 4168, 4181, 4182, 4186 Aft limit:
50 C or ISA +35 C whichever is lower
Airplane maximum operating ambient temperature limit
VFR/IFR enroute, terminal, and approach LNAV and VNAV operations.
The UNS-1E is approved for
+50 C or ISA +35 C, whichever is lower
APU ambient temperature (upper)
36.0% MAC
Serial Numbers: 4187 and above Aft limit:
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
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
+21 C maximum ambient temperature
With APU inlet louvres installed, APU operation is limited to
245 KIAS
Vmo 0 to 8,000
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….
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…
8,000 ft
Maximum cabin altitude (pressurized flight)
0 C to 107 C
Max. Take-off (MTOP) (1) Oil temp C
…with passengers onboard …during pressure refueling
APU must not be operated unattended…
200 ft. AGL.
For non-precision approaches the autopilot must be disengaged at or above
13.8% thru 17.7% MAC
Serial Numbers: 4187 and above Forward limit (53,000 lbs. thru 64,500 lbs.):
100%
Max Continuous (MCP) Max N(H) % rpm
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
1020 rpm
Max. Reverse Max N(P) rpm
CAT I limits only.
AFCS is approved for autopilot approaches to ___ _ _____ ____.
GROUND OPERATIONS ONLY
APU is approved for what kind of operation?
1020 rpm Maximum allowable continuous N(P) overspeed is 1071 rpm
Max Continuous (MCP) Max N(P) rpm
10,000 ft
Maximum operation altitude for take-off and landing
Tank 1 or take 2 auxiliary fuel pumps must be on for take-off and landing.
Auxiliary Fuel Pumps limitation
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,
1 hour flying time from a suitable airport for landing
With Integrated Standby Instrument installed the airplane must not be operated further than
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
172 KIAS
Flap Extended Speed (Vfe) Flap 15
1,000 ft. AGL.
After take-off or go-around, the minimum height for autopilot engagement is
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
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
248 KIAS
Vmo 25,000 ft
64,700 lbs
Serial numbers: 4168, 4181, 4182, 4186 Ramp Weight
107 C
Maximum Oil Temperature above ground idle
13.8% thru 17.4% MAC
Serial Numbers: 4168, 4181, 4182, 4186 Forward limit (53,000 lbs. thru 64,500.):
880 C
Max Continuous (MCP) Max ITT C
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:
