BEECH 1900D AIRLINER
Revision 0.2
MEMORY FLASH CARDS
Copyright © 2006, FlightSafety International, Inc.
Unauthorized reproduction or distribution is prohibited. All rights reserved.
INSERT LATEST REVISED CARDS, DESTROY SUPERSEDED CARDS
LIST OF EFFECTIVE CARDS
Dates of issue for original and changed pages are:
Original........ 0......... OCTOBER 2006
Revision....... .01 .............. March 2008
Revision....... 0.2 ............. March 2010
TOTAL NUMBER OF CARDS IN THIS SET IS 74
CONSISTING OF THE FOLLOWING:
Card
*Revision Card
*Revision
No.
No. No.
No.
Title ............................................... 0.2 E-1A .............................................. 0.2
ii .................................................... 0.2 E-2—E-30A................................... .01
E-1 ................................................ .01 L-1—L-44A ................................... .01
*Zero in this column indicates an original card.
ii
Revision 0.2
Emergency
EMERGENCY AIRSPEEDS
(17,120 POUNDS/7765 KILOGRAMS)
Revision .01
BEECH 1900D AIRLINER
E-1
EMERGENCY AIRSPEEDS
(17,120 POUNDS/7765 KILOGRAMS)
1. One-engine-inoperative Best Angle-of-Climb (VXSE) ........... 122 Knots
2. One-engine-inoperative Best Rate-of-Climb (VYSE) ............. 128 Knots
(Decrease 2 Knots per 5000 feet)
3. One-engine-inoperative En Route Climb (VENR) .................. 123 Knots
4. Air Minimum Control Speeds (VMCA)
Flaps Up ..................................................................................... 92 Knots
Flaps 17° .................................................................................... 92 Knots
5. Emergency Descent ................................................................ 180 Knots
6. Maximum Range Glide............................................................ 140 Knots
Revision 0.2
BEECH 1900D AIRLINER
E-1A
Emergency
FAA-Approved Airplane Flight Manual Supplement
Collins FCS-65 Automatic Flight Control System
(P/N 622-9724-005)
ENGINE FAILURE
(AUTOPILOT ENGAGED)
Revision .01
BEECH 1900D AIRLINER
E-2
FAA-Approved Airplane Flight Manual Supplement
Collins FCS-65 Automatic Flight Control System
(P/N 622-9724-005)
ENGINE FAILURE
(AUTOPILOT ENGAGED)
1. Autopilot............................................................................... DISENGAGE
2. Engine Failure Procedures in
Emergency Section of AFM ................................................. COMPLETE
3. Trim Controls ........................................................... RETRIM AIRPLANE
4. Autopilot ........................................................ RE-ENGAGE, IF DESIRED
5. Rudder Trim..................... MANUALLY ADJUST AS REQUIRED AFTER
POWER AND CONFIGURATION CHANGES
Revision .01
BEECH 1900D AIRLINER
E-2A
Emergency
ENGINE FAILURE
ENGINE FIRE OR FAILURE IN FLIGHT
Revision .01
BEECH 1900D AIRLINER
E-3
ENGINE FAILURE
ENGINE FIRE OR FAILURE IN FLIGHT
Affected Engine:
1. Condition Lever ............................................................... FUEL CUTOFF
2. Propeller Lever......................................................................... FEATHER
3. Firewall Fuel Valve .......................................................... PULL CLOSED
4. Fire Extinguisher, if required .................................................. ACTUATE
Revision .01
BEECH 1900D AIRLINER
E-3A
Emergency
ENGINE FAILURE
ENGINE FIRE ON GROUND
Revision .01
BEECH 1900D AIRLINER
E-4
ENGINE FAILURE
ENGINE FIRE ON GROUND
Affected Engine:
1. Condition Lever ............................................................... FUEL CUTOFF
2. Firewall Fuel Valve .......................................................... PULL CLOSED
3. Ignition and Engine Start Switch................................. STARTER ONLY
4. Fire Extinguisher, if required .................................................. ACTUATE
Revision .01
BEECH 1900D AIRLINER
E-4A
Emergency
ENGINE FAILURE
ENGINE FAILURE DURING TAKEOFF
(AT OR BELOW V1—TAKEOFF ABORTED)
Revision .01
BEECH 1900D AIRLINER
E-5
ENGINE FAILURE
ENGINE FAILURE DURING TAKEOFF
(AT OR BELOW V1—TAKEOFF ABORTED)
1. Power Levers ................................................................... GROUND FINE
WARNING
Do not use reverse thrust with one engine inoperative.
Care must be exercised when using single-engine
ground fine on surfaces with reduced friction.
2. Brakes............................................... MAXIMUM (OR AS REQUIRED TO
ACHIEVE STOPPING DISTANCE)
Revision .01
BEECH 1900D AIRLINER
E-5A
Emergency
ENGINE FAILURE
ENGINE FAILURE DURING TAKEOFF
(AT OR ABOVE V1—TAKEOFF CONTINUED)
Revision .01
BEECH 1900D AIRLINER
E-6
ENGINE FAILURE
ENGINE FAILURE DURING TAKEOFF
(AT OR ABOVE V1—TAKEOFF CONTINUED)
1.
2.
3.
4.
VR Speed ............................................ ROTATE TO APPROXIMATELY 8°
Landing Gear (when positive climb established)............................. UP
Airspeed............................................... MAINTAIN V2 TO 400 FEET AGL
Propeller (inoperative engine) ............................. VERIFY FEATHERED
WARNING
Do not retard the failed engine power lever until the autofeather system has completely stopped propeller rotation.
Revision .01
BEECH 1900D AIRLINER
E-6A
Emergency
ENGINE FAILURE
ENGINE FAILURE IN FLIGHT BELOW
AIR MINIMUM CONTROL SPEED (VMCA)
Revision .01
BEECH 1900D AIRLINER
E-7
ENGINE FAILURE
ENGINE FAILURE IN FLIGHT BELOW
AIR MINIMUM CONTROL SPEED (VMCA)
1. Reduce power on operative engine as required to maintain control.
2. Lower nose to accelerate above VMCA.
Revision .01
BEECH 1900D AIRLINER
E-7A
Emergency
OIL PRESSURE LOW
OR
Revision .01
R OIL PRES LO
BEECH 1900D AIRLINER
E-8
OIL PRESSURE LOW
1. Oil Pressure Gage ......................................... CONFIRM BELOW 60 PSI
2. If Confirmed ............... SECURE ENGINE OR LAND AT THE NEAREST
SUITABLE AIRPORT USING THE MINIMUM
POWER REQUIRED TO SUSTAIN FLIGHT
Revision .01
BEECH 1900D AIRLINER
E-8A
Emergency
PROPELLER COLLISIONS DURING
GROUND OPERATION
Revision .01
BEECH 1900D AIRLINER
E-9
PROPELLER COLLISIONS DURING
GROUND OPERATION
WARNING
During collisions, the higher the propeller RPM, the
greater the risk of propeller blades, or portion of blades,
separating from the propeller hub causing damage to the
fuselage and physical harm to the passengers.
If maximum braking and maximum reverse are insufficient and a collision
is imminent:
1. Power Levers ................................................... GROUND FINE OR IDLE
2. Condition Levers ............................................................. FUEL CUTOFF
Revision .01
BEECH 1900D AIRLINER
E-9A
Emergency
FUEL SYSTEM
FUEL PRESSURE LOW
Revision .01
BEECH 1900D AIRLINER
E-10
FUEL SYSTEM
FUEL PRESSURE LOW
1. Standby Pump (failed side) ................................................................ ON
Revision .01
BEECH 1900D AIRLINER
E-10A
Emergency
SMOKE AND FUME ELIMINATION
ELECTRICAL SMOKE OR FIRE
Revision .01
BEECH 1900D AIRLINER
E-11
SMOKE AND FUME ELIMINATION
ELECTRICAL SMOKE OR FIRE
Oxygen:
1. Oxygen Control ................................................................. CONFIRM ON
2. Crew ..................................... DON MASK, AND GOGGLES (if installed)
Mask Selector Switch ............................. EMERG (if installed) or 100%
Purge Valve (if installed) ................................................................ OPEN
3. Headsets............................................................................................ DON
4. MIC Selector Switches .................................................. OXYGEN MASK
Revision .01
BEECH 1900D AIRLINER
E-11A
Emergency
SMOKE AND FUME ELIMINATION
ENVIRONMENTAL SMOKE OR FUMES
Revision .01
BEECH 1900D AIRLINER
E-12
SMOKE AND FUME ELIMINATION
ENVIRONMENTAL SMOKE OR FUMES
Oxygen:
1. Oxygen Control ................................................................. CONFIRM ON
2. Crew ..................................... DON MASK, AND GOGGLES (if installed)
Mask Selector Switch ............................. EMERG (if installed) or 100%
Purge Valve (if installed) ................................................................ OPEN
3. Headsets............................................................................................ DON
4. MIC Selector Switches .................................................. OXYGEN MASK
Revision .01
BEECH 1900D AIRLINER
E-12A
Emergency
CABIN DOOR OR CARGO DOOR UNLOCKED
OR
Revision .01
BEECH 1900D AIRLINER
E-13
CABIN DOOR OR CARGO DOOR UNLOCKED
WARNING
Do not attempt to check the security of the cabin door or
cargo door in flight. Remain as far from the doors as possible with seatbelts securely fastened.
If the Cabin Door or Cargo Door Annunciator Illuminates, or if an
Unlatched Cabin or Cargo Door is Suspected:
1. All Occupants ... SEATED WITH SEAT BELTS SECURELY FASTENED
Revision .01
BEECH 1900D AIRLINER
E-13A
Emergency
EMERGENCY DESCENT
Revision .01
BEECH 1900D AIRLINER
E-14
EMERGENCY DESCENT
1.
2.
3.
4.
5.
Power Levers .................................................................................... IDLE
Propeller Levers .............................................................. SET 1700 RPM
Flaps..................................................................................................... 17°
Landing Gear Control ......................................................................... DN
Airspeed................................................................................. 180 KNOTS
Revision .01
BEECH 1900D AIRLINER
E-14A
Emergency
GLIDE
Revision .01
BEECH 1900D AIRLINER
E-15
GLIDE
1.
2.
3.
4.
Landing Gear Control.......................................................................... UP
Flaps ..................................................................................................... UP
Propellers............................................................................. FEATHERED
Airspeed................................................................................. 140 KNOTS
Revision .01
BEECH 1900D AIRLINER
E-15A
Emergency
ELECTRICAL
SINGLE INVERTER OR AC BUS FAILURE
OR
Revision .01
BEECH 1900D AIRLINER
E-16
ELECTRICAL
SINGLE INVERTER OR AC BUS FAILURE
1. AC BUS Switch (failed side) ........................................... OFF, THEN ON
Revision .01
BEECH 1900D AIRLINER
E-16A
Emergency
ELECTRICAL
SINGLE INVERTER FAILURE FOLLOWED BY A
SECOND INVERTER OR AC BUS FAILURE
OR
Revision .01
BEECH 1900D AIRLINER
E-17
ELECTRICAL
SINGLE INVERTER FAILURE FOLLOWED BY A
SECOND INVERTER OR AC BUS FAILURE
Illumination of Both Annunciators Simultaneously After a Single Inverter
Failure Has Been Remedied (by placing one AC Bus Switch to TRANSFER) Indicates a Failure of the Inverter Selected ON, or a Failure of Either
AC BUS.
1. Attitude/Heading Control ............................. USE STANDBY ATTITUDE
INDICATOR AND COMPASS
Revision .01
BEECH 1900D AIRLINER
E-17A
Emergency
ELECTRICAL
DUAL INVERTER FAILURE
AND
Revision .01
BEECH 1900D AIRLINER
E-18
ELECTRICAL
DUAL INVERTER FAILURE
Illumination of Both Annunciators Simultaneously (With Neither AC Bus
Switch in Transfer), Indicates that a Failure in One Inverter is Affecting the
Other Inverter.
1. Attitude/Heading Control ............................. USE STANDBY ATTITUDE
INDICATOR AND COMPASS
Revision .01
BEECH 1900D AIRLINER
E-18A
Emergency
ELECTRICAL
DUAL GENERATOR FAILURE
AND
Revision .01
BEECH 1900D AIRLINER
E-19
ELECTRICAL
DUAL GENERATOR FAILURE
1. Instrument Emergency Lights (if required) ...................................... ON
2. Generators ................................................................... RESET, THEN ON
If Either Generator Will Reset:
3. Do not exceed 100% load on operating generator.
If Neither Generator Will Reset:
4. Non-Essential Equipment................................................................. OFF
Revision .01
BEECH 1900D AIRLINER
E-19A
Emergency
FAA-Approved Airplane Flight Manual Supplement
Collins FCS-65 Automatic Flight Control System
(P/N 622-9724-005)
AUTOPILOT MALFUNCTION/
ELEVATOR TRIM RUNWAY
Revision .01
BEECH 1900D AIRLINER
E-20
FAA-Approved Airplane Flight Manual Supplement
Collins FCS-65 Automatic Flight Control System
(P/N 622-9724-005)
AUTOPILOT MALFUNCTION/
ELEVATOR TRIM RUNWAY
1. Control Wheel................... HOLD FIRMLY, BE PREPARED TO ACCEPT
CONTROL WHEEL FORCES
2. AP YD/DISC TRIM Switch ............................................ DEPRESS FULLY
(Pilot’s or Copilot’s Control Wheel)
3. Flight Controls/Power Levers ................................... AS REQUIRED TO
RECOVER THE AIRPLANE
Revision .01
BEECH 1900D AIRLINER
E-20A
Emergency
FAA-Approved Airplane Flight Manual Supplement
Collins FCS-65 Automatic Flight Control System
(P/N 622-9724-005)
OVERSPEED
(OVERSPEED WARNING HORN SOUNDS)
Revision .01
BEECH 1900D AIRLINER
E-21
FAA-Approved Airplane Flight Manual Supplement
Collins FCS-65 Automatic Flight Control System
(P/N 622-9724-005)
OVERSPEED
(OVERSPEED WARNING HORN SOUNDS)
1. Control Wheel ................................................................................. HOLD
2. Autopilot............................................................................... DISENGAGE
3. Airspeed ..................................................................................... REDUCE
Revision .01
BEECH 1900D AIRLINER
E-21A
Emergency
FLIGHT CONTROLS
UNSCHEDULED ELECTRIC ELEVATOR TRIM
(IF INSTALLED)
Revision .01
BEECH 1900D AIRLINER
E-22
FLIGHT CONTROLS
UNSCHEDULED ELECTRIC ELEVATOR TRIM
(IF INSTALLED)
1. Airplane Attitude ............................ MAINTAIN (using elevator control)
2. Control Wheel Disconnect Switch ............................. DEPRESS FULLY
(PITCH TRIM OFF Annunciator–Illuminated)
Revision .01
BEECH 1900D AIRLINER
E-22A
Emergency
FLIGHT CONTROLS
UNSCHEDULED RUDDER BOOST ACTIVATION
Revision .01
BEECH 1900D AIRLINER
E-23
FLIGHT CONTROLS
UNSCHEDULED RUDDER BOOST ACTIVATION
1. Control Wheel Disconnect Switch ... DEPRESS and HOLD (1st Level)
2. Rudder Boost/Yaw Control Test Switch .......................................... OFF
If Condition Persists:
3. Rudder Boost Circuit Breaker........................................................ PULL
Revision .01
BEECH 1900D AIRLINER
E-23A
Emergency
ENVIRONMENTAL SYSTEMS
USE OF OXYGEN
Revision .01
BEECH 1900D AIRLINER
E-24
ENVIRONMENTAL SYSTEMS
USE OF OXYGEN
1.
2.
3.
4.
Oxygen Control ................................................................. CONFIRM ON
Cabin Oxygen Control.............................................................. PULL ON
Crew ....................................................................................... DON MASK
Mask Selector Switch........................................................................ SET
Inflatable Type Harness ............................................................ NORMAL
Strap Type Harness .................................................................. NORMAL
(100% AT CABIN ALTITUDES ABOVE 20,000 FEET)
5. Headsets............................................................................................ DON
6. MIC Selector Switches .................................................. OXYGEN MASK
Revision .01
BEECH 1900D AIRLINER
E-24A
Emergency
ENVIRONMENTAL SYSTEMS
CABIN DECOMPRESSION
Revision .01
BEECH 1900D AIRLINER
E-25
ENVIRONMENTAL SYSTEMS
CABIN DECOMPRESSION
1.
2.
3.
4.
Oxygen Control ................................................................. CONFIRM ON
Cabin Oxygen Control.............................................................. PULL ON
Crew ....................................................................................... DON MASK
Mask Selector Switch........................................................................ SET
Inflatable Type Harness ............................................................ NORMAL
Strap Type Harness .................................................................. NORMAL
(100% AT CABIN ALTITUDES ABOVE 20,000 FEET)
5. Headsets............................................................................................ DON
6. MIC Selector Switches .................................................. OXYGEN MASK
Revision .01
BEECH 1900D AIRLINER
E-25A
Emergency
ENVIRONMENTAL SYSTEMS
HIGH DIFFERENTIAL PRESSURE
Revision .01
BEECH 1900D AIRLINER
E-26
ENVIRONMENTAL SYSTEMS
HIGH DIFFERENTIAL PRESSURE
1. Bleed Air Valves .................................................................... ENVIR OFF
Revision .01
BEECH 1900D AIRLINER
E-26A
Emergency
ENVIRONMENTAL SYSTEMS
BLEED AIR LINE FAILURE
OR
Revision .01
BEECH 1900D AIRLINER
E-27
ENVIRONMENTAL SYSTEMS
BLEED AIR LINE FAILURE
1. Bleed Air Valve (affected engine)............................ INST & ENVIR OFF
Revision .01
BEECH 1900D AIRLINER
E-27A
Emergency
ENVIRONMENTAL SYSTEMS
ENVIRONMENTAL FAILURE
OR
Revision .01
BEECH 1900D AIRLINER
E-28
ENVIRONMENTAL SYSTEMS
ENVIRONMENTAL FAILURE
1. Bleed Air Valve (affected side) .......................... CYCLE TO ENVIR OFF
AND BACK TO OPEN
If ENVIR FAIL Annunciator Extinguishes, Continue Operation. If
Annunciator Remains Illuminated:
2. Bleed Air Valve (affected side) ............................................. ENVIR OFF
Revision .01
BEECH 1900D AIRLINER
E-28A
Emergency
MARK-VI GROUND PROXIMITY
WARNING SYSTEM (IF INSTALLED)
IN-FLIGHT ACTIVATION OF GPWS WARNING
Continuous “PULL UP, PULL UP” Voice Warning
Or
“TERRAIN, TERRAIN, PULL UP, PULL UP” or “OBSTACLE,
OBSTACLE, PULL UP, PULL UP” Voice Warning
Revision .01
BEECH 1900D AIRLINER
E-29
MARK-VI GROUND PROXIMITY
WARNING SYSTEM (IF INSTALLED)
IN-FLIGHT ACTIVATION OF GPWS WARNING
IN IMC OR AT NIGHT:
1. Wings ............................................................................................. LEVEL
2. Airspeed..................................................................................... 122 KIAS
3. Power ......................................................................... MAX ALLOWABLE
4. Gear and Flaps ........................................................................ RETRACT
5. Continue Climb at 122 KIAS Until all Visual and Aural Warnings Cease
IN DAY VMC:
1. Evaluate Flight Path With Respect to Terrain
2. Take Action As Necessary To Recover Safe Terrain Clearance
Revision .01
BEECH 1900D AIRLINER
E-29A
Emergency
SPINS
Revision .01
BEECH 1900D AIRLINER
E-30
SPINS
Intentional spins are prohibited. If an unintentional spin is encountered,
perform the following procedure IMMEDIATELY–THE LONGER THE DELAY,
THE MORE DIFFICULT RECOVERY WILL BECOME. Steps 1 through 3
should be done AGGRESSIVELY and SIMULTANEOUSLY. The full forward
position of the control column may be reduced slightly, if required, to prevent the airplane from exceeding a 90° nose down (inverted) attitude.
1.
2.
3.
4.
5.
Control Column ..................... FULL FORWARD, AILERONS NEUTRAL
Full Rudder ................................. OPPOSITE THE DIRECTION OF SPIN
Power Levers .................................................................................... IDLE
Rudder..................................... NEUTRALIZE WHEN ROTATION STOPS
Execute a smooth pullout.
Revision .01
BEECH 1900D AIRLINER
E-30A
Limitations
AIRSPEED LIMITATIONS
Maneuvering Speed VA
(17,120 lbs/7765 kg)
Revision .01
BEECH 1900D AIRLINER
L-1
AIRSPEED LIMITATIONS
Maneuvering Speed VA
(17,120 lbs/7765 kg)
178 KIAS
Revision .01
BEECH 1900D AIRLINER
L-1A
Limitations
AIRSPEED LIMITATIONS
Maximum Flap Extension/Extended Speed (VFE)
Flaps 17°............................................................................................... ?
Flaps 35°
(UE-1 thru UE-78 not in compliance with S.B. 2512) .............................?
Flaps 35°
(UE-79 and after, and earlier airplanes in compliance with S.B. 2512)... ?
Revision .01
BEECH 1900D AIRLINER
L-2
AIRSPEED LIMITATIONS
Maximum Flap Extension/Extended Speed ( VFE)
Flaps 17° ................................................................................. 188 KIAS
Flaps 35°
(UE-1 thru UE-78 not in compliance with S.B. 2512).............. 143 KIAS
Flaps 35°
(UE-79 and after, and earlier airplanes
in compliance with S.B. 2512)..................................................... 154 KIAS
Revision .01
BEECH 1900D AIRLINER
L-2A
Limitations
AIRSPEED LIMITATIONS
Maximum Landing Gear Operating Speed (VLO)
Extension ........................................................................... ?
Retraction .......................................................................... ?
Revision .01
BEECH 1900D AIRLINER
L-3
AIRSPEED LIMITATIONS
Maximum Landing Gear Operating Speed (VLO)
Extension ............................................................. 180 KIAS
Retraction ............................................................. 180 KIAS
Revision .01
BEECH 1900D AIRLINER
L-3A
Limitations
AIRSPEED LIMITATIONS
Maximum Landing Gear Extended Speed (VLE)
Revision .01
BEECH 1900D AIRLINER
L-4
AIRSPEED LIMITATIONS
Maximum Landing Gear Extended Speed (VLE)
180 KIAS
Revision .01
BEECH 1900D AIRLINER
L-4A
Limitations
AIRSPEED LIMITATIONS
Air Minimum Control Speed (VMCA)
Flaps 0°................................................................................?
Flaps 17° ........................................................................... ?
Revision .01
BEECH 1900D AIRLINER
L-5
AIRSPEED LIMITATIONS
Air Minimum Control Speed (VMCA)
Flaps 0° .................................................................. 92 KIAS
Flaps 17° ................................................................ 92 KIAS
Revision .01
BEECH 1900D AIRLINER
L-5A
Limitations
AIRSPEED LIMITATIONS
Maximum Operating Speed (VMO)
Sea Level to 13,200 feet.................................................... ?
13,200 feet to 25,000 feet.................................................. ?
Revision .01
BEECH 1900D AIRLINER
L-6
AIRSPEED LIMITATIONS
Maximum Operating Speed (VMO)
Sea Level to 13,200 feet ................................................ 248
13,200 feet to 25,000 feet .................................... 248–195*
(*.48 Mach)
Revision .01
BEECH 1900D AIRLINER
L-6A
Limitations
STALLING SPEED (VSO)
Revision .01
BEECH 1900D AIRLINER
L-7
STALLING SPEED (VSO)
84 KIAS
Revision .01
BEECH 1900D AIRLINER
L-7A
Limitations
ENGINE EXHAUST HEATING OF CABIN
WINDOWS AND AIRFRAME
Revision .01
BEECH 1900D AIRLINER
L-8
ENGINE EXHAUST HEATING OF CABIN
WINDOWS AND AIRFRAME
1. Do not operate the engines with the propellers feathered except during
external power starts and propeller feather checks, except that the propellers may be operated in feather at temperatures not to exceed +5°C
for a maximum of 3 minutes for purposes of airframe deiceing.
2. Do not conduct static operations in ground fine when the OAT exceeds
38°C.
3. Do not back the airplane using reverse thrust for periods longer than 10
seconds.
Revision .01
BEECH 1900D AIRLINER
L-8A
Limitations
REDUCED POWER TAKEOFFS
Revision .01
BEECH 1900D AIRLINER
L-9
REDUCED POWER TAKEOFFS
1. The runways must not be wet or contaminated with
snow, slush, or ice.
2. Flaps must be set at 17° for takeoff
3. Periodically check the availability of Static Take-Off
Power. Use Static Take-off Power at least once during
each 25 hours of operation or 25 takeoffs, whichever
occurs first.
Revision .01
BEECH 1900D AIRLINER
L-9A
Limitations
POWER LEVERS
Revision .01
BEECH 1900D AIRLINER
L-10
POWER LEVERS
Do not lift power levers in flight. Lifting the power levers
in flight, or moving the power levers in flight below the
flight idle position, could result in a nose-down pitch and
a descent rate leading to aircraft damage and injury to
personnel.
Revision .01
BEECH 1900D AIRLINER
L-10A
Limitations
ENGINE OPERATING LIMITS
Torque FT–LBS
Takeoff ............................................................................... ?
Max Continuous................................................................. ?
Transient ............................................................................ ?
Revision .01
BEECH 1900D AIRLINER
L-11
ENGINE OPERATING LIMITS
Torque FT–LBS
Takeoff ......................................................................... 3950
Max Continuous ........................................................... 3750
Transient...................................... 5000 FOR 20 SECONDS
Revision .01
BEECH 1900D AIRLINER
L-11A
Limitations
ENGINE OPERATING LIMITS
Maximum ITT (°C)
Starting .............................................................................. ?
Idle ..................................................................................... ?
Takeoff ............................................................................... ?
Max Continuous................................................................. ?
Transient ............................................................................ ?
Revision .01
BEECH 1900D AIRLINER
L-12
ENGINE OPERATING LIMITS
Maximum ITT (°C)
Starting...................................... 1000°C FOR 5 SECONDS
Idle ............................................................................. 750°C
Takeoff ....................................................................... 800°C
Max Continuous ......................................................... 780°C
Transient.................................... 870°C FOR 20 SECONDS
Revision .01
BEECH 1900D AIRLINER
L-12A
Limitations
ENGINE OPERATING LIMITS
Gas Generator RPM (% N1)
Idle ..................................................................................... ?
Takeoff ............................................................................... ?
Max Continuous................................................................. ?
Transient ............................................................................ ?
Revision .01
BEECH 1900D AIRLINER
L-13
ENGINE OPERATING LIMITS
Gas Generator RPM (% N1)
Idle ...................................................................... 65% (min)
Takeoff ........................................................................ 104%
Max Continuous.......................................................... 104%
Transient ..................................................................... 104%
Revision .01
BEECH 1900D AIRLINER
L-13A
Limitations
ENGINE OPERATING LIMITS
Propeller RPM (N2)
Idle ..................................................................................... ?
Takeoff ............................................................................... ?
Max Continuous................................................................. ?
Transient ............................................................................ ?
Revision .01
BEECH 1900D AIRLINER
L-14
ENGINE OPERATING LIMITS
Propeller RPM (N2)
Idle ........................................................................ 950 RPM
Takeoff ................................................................ 1700 RPM
Max Continuous.................................................. 1700 RPM
Transient............................. 1870 RPM FOR 20 SECONDS
Revision .01
BEECH 1900D AIRLINER
L-14A
Limitations
ENGINE OPERATING LIMITS
Oil Pressure (PSI)
Starting .............................................................................. ?
Idle ..................................................................................... ?
Takeoff ............................................................................... ?
Max Continuous................................................................. ?
Transient ............................................................................ ?
Revision .01
BEECH 1900D AIRLINER
L-15
ENGINE OPERATING LIMITS
Oil Pressure (PSI)
Starting ............................................................ 0 to 200 PSI
Idle .................................................................. 60 PSI (min)
Takeoff ........................................................... 90 to 135 PSI
Max Continuous ............................................ 90 to 135 PSI
Transient ........................................................ 40 to 200 PSI
Revision .01
BEECH 1900D AIRLINER
L-15A
Limitations
ENGINE OPERATING LIMITS
Oil Temperature (°C)
Starting .............................................................................. ?
Idle ..................................................................................... ?
Takeoff ............................................................................... ?
Max Continuous................................................................. ?
Transient ............................................................................ ?
Revision .01
BEECH 1900D AIRLINER
L-16
ENGINE OPERATING LIMITS
Oil Temperature (°C)
Starting............................................................. –40°C (min)
Idle.................................................................. –40 to 110°C
Takeoff.............................................................. 10 to 110°C
Max Continuous ............................................... 10 to 105°C
Transient......................................................... –40 to 110°C
Revision .01
BEECH 1900D AIRLINER
L-16A
Limitations
EXTERNAL POWER LIMITS
Volts ................................................................................... ?
Amps.................................................................................. ?
Revision .01
BEECH 1900D AIRLINER
L-17
EXTERNAL POWER LIMITS
Volts ............................................................ 28.0–28.4 Volts
Amps ......................................... 1000 Amps (Momentary)/
300 Amps (Continuous)
Revision .01
BEECH 1900D AIRLINER
L-17A
Limitations
STARTER LIMITS
Revision .01
BEECH 1900D AIRLINER
L-18
STARTER LIMITS
For restarts following a normal start:
3 minute cool-down, beginning when the starter is turned off.
For an aborted start (no ignition) followed by an attempted restart:
Starter is limited to 20 seconds on (aborted start), 30 seconds off, 20
seconds on (second start attempt), 60 seconds off, 20 seconds on
(third start attempt), 5 minutes off.
For continuous motoring without attempting to start the engine:
Starter is limited to 20 seconds on, 5 minutes off. Repeat as required.
Revision .01
BEECH 1900D AIRLINER
L-18A
Limitations
GENERATOR LIMITS
MINIMUM N1 REQUIREMENTS VS
ELECTRICAL LOAD LIMITS
Minimum Gas Generator RPM (% N1)
0–75%................................................................................ ?
75–100%............................................................................ ?
Revision .01
BEECH 1900D AIRLINER
L-19
GENERATOR LIMITS
MINIMUM N1 REQUIREMENTS VS
ELECTRICAL LOAD LIMITS
Minimum Gas Generator RPM (% N1)
0–75% ..................................................................... 65% N1
75–100% ................................................................. 72% N1
Revision .01
BEECH 1900D AIRLINER
L-19A
Limitations
FUEL LIMITS
Approved Engine Fuels ..................................................... ?
Revision .01
BEECH 1900D AIRLINER
L-20
FUEL LIMITS
Approved Engine Fuels..........................................................
COMMERCIAL GRADES...............................................
Jet A, Jet A-1, Jet B (Operation is prohibited above
8000 feet if either standby pump is inoperative)
MILITARY GRADES .......................................................
JP-4 (Operation is prohibited above 8000 feet if
either standby pump is inoperative), JP-5, JP-8
Revision .01
BEECH 1900D AIRLINER
L-20A
Limitations
FUEL LIMITS
Emergency Engine Fuels .................................................. ?
Revision .01
BEECH 1900D AIRLINER
L-21
FUEL LIMITS
Emergency Engine Fuels............ 80 Red (Formerly 80/87)
91/96
100 Green (Formerly 100/130)
100LL Blue
115/145 Purple
Revision .01
BEECH 1900D AIRLINER
L-21A
Limitations
EMERGENCY ENGINE FUEL LIMITS
Limitations on the use of Aviation Gasoline
Revision .01
BEECH 1900D AIRLINER
L-22
EMERGENCY ENGINE FUEL LIMITS
1. Operation is limited to 150 hours between engine
overhauls.
2. Operation is prohibited if either standby pump is
inoperative.
3. Operation in prohibited above 18,000 feet.
4. Standby pumps must be ON for takeoff and landing.
Revision .01
BEECH 1900D AIRLINER
L-22A
Limitations
FUEL MANAGEMENT
Usable Fuel (Gallons x 6.74=lbs)
Maximum Usable Fuel Quantity ........................................ ?
Each Main Fuel Tank System ............................................ ?
Each Auxiliary Fuel Tank ................................................... ?
Revision .01
BEECH 1900D AIRLINER
L-23
FUEL MANAGEMENT
Usable Fuel (Gallons x 6.74=lbs)
Maximum Usable Fuel Quantity ...... 665.4 gal/4484 lbs (2518.8 ltr)
Each Main Fuel Tank System .............. 240.5 gal/1621 lbs (910.4 ltr)
Each Auxiliary Fuel Tank ....................... 92.2 gal/621 lbs (349.0 ltr)
Revision .01
BEECH 1900D AIRLINER
L-23A
Limitations
FUEL MANAGEMENT
Fuel Imbalance
Maximum allowable fuel imbalance
between wing fuel systems................................................ ?
Revision .01
BEECH 1900D AIRLINER
L-24
FUEL MANAGEMENT
Fuel Imbalance
Maximum allowable fuel imbalance
between wing fuel systems ..................................... 200 lbs
Revision .01
BEECH 1900D AIRLINER
L-24A
Limitations
FUEL MANAGEMENT
Fuel Gages in the Yellow Arc
Revision .01
BEECH 1900D AIRLINER
L-25
FUEL MANAGEMENT
Fuel Gages in the Yellow Arc
Do not take off if fuel quantity gages indicate in yellow arc
or indicate less than 363 lbs of fuel in each wing system.
Revision .01
BEECH 1900D AIRLINER
L-25A
Limitations
FUEL MANAGEMENT
Auxiliary Fuel
Revision .01
BEECH 1900D AIRLINER
L-26
FUEL MANAGEMENT
Auxiliary Fuel
Fuel in auxiliary tank must be used prior to main tank fuel
(except in the event of auxiliary fuel transfer failure.)
Revision .01
BEECH 1900D AIRLINER
L-26A
Limitations
FUEL MANAGEMENT
Operating with Low Fuel Pressure
OR
Revision .01
BEECH 1900D AIRLINER
L-27
FUEL MANAGEMENT
Operating with Low Fuel Pressure
Operation of either engine with its corresponding fuel
pressure annunciator (L FUEL PRESS LO or R FUEL
PRESS LO) illuminated is limited to 10 hours before
overhaul or replacement of the engine-driven fuel
pump. Windmilling time need not be charged against
this time limit.
Revision .01
BEECH 1900D AIRLINER
L-27A
Limitations
PROPELLER ROTATIONAL SPEED LIMITS
Transients not exceeding 20 seconds ............................... ?
Transients not exceeding 5 minutes .................................. ?
Reverse.............................................................................. ?
Minimum Idle Speed.......................................................... ?
Red Arc Ground Operation Prohibited Ranges ................. ?
All Other Conditions........................................................... ?
Revision .01
BEECH 1900D AIRLINER
L-28
PROPELLER ROTATIONAL SPEED LIMITS
Transients not exceeding 20 seconds ................ 1870 RPM
Transients not exceeding 5 minutes ................... 1735 RPM
Reverse............................................................... 1650 RPM
Minimum Idle Speed ............................................. 950 RPM
Red Arc Ground Operation
Prohibited Ranges ............ 400–950 RPM/1250–1395 RPM
All other conditions ............................................. 1700 RPM
Revision .01
BEECH 1900D AIRLINER
L-28A
Limitations
PROPELLER ROTATIONAL
OVERSPEED LIMITS
Revision .01
BEECH 1900D AIRLINER
L-29
PROPELLER ROTATIONAL
OVERSPEED LIMITS
The maximum propeller overspeed Limit is 1870 and is timed limited to 20 seconds. Sustained propeller overspeeds faster than
1700 RPM indicate failure of a primary governor. Flight may be
continued at propeller overspeeds up to 1802 RPM provided torque
is limited to 3538 ft-lbs. Sustained propeller overspeeds above
1802 RPM indicate failure of both the primary and the secondary
governor.
Revision .01
BEECH 1900D AIRLINER
L-29A
Limitations
PROPELLER AUTOFEATHER
Revision .01
BEECH 1900D AIRLINER
L-30
PROPELLER AUTOFEATHER
The propeller autofeather system must be operable for
all flights and must be armed for takeoff, climb, approach
and landing.
Revision .01
BEECH 1900D AIRLINER
L-30A
Limitations
WEIGHT LIMITS
Maximum Ramp Weight .................................................... ?
Maximum Takeoff Weight................................................... ?
Maximum Landing Weight ................................................. ?
Maximum Zero Fuel Weight............................................... ?
Revision .01
BEECH 1900D AIRLINER
L-31
WEIGHT LIMITS
Maximum Ramp Weight .................................................... 17,230 lbs (7815 kg)
Maximum Takeoff Weight................................................... 17,120 lbs (7765 kg)
Max Takeoff Weight to Achieve Takeoff Climb Requirements
Max Takeoff Weight as Limited by Brake Energy
Takeoff Field Length
Takeoff Flight Path Requirements to 1500 feet AGL
Climb–One Engine Inoperative–Enroute Net Climb Gradient
Service Ceiling—One Engine Inoperative
Maximum Landing Weight .................................................................. 16,765 lbs
Max Landing Weight to Achieve Climb Requirements
Max Landing Weight as Limited by Brake Energy
Normal Landing Distance—Flaps Down (35°)
Maximum Zero Fuel Weight ............................................................... 15,165 lbs
Revision .01
BEECH 1900D AIRLINER
L-31A
Limitations
WEIGHT LIMITS
Maximum Weight in Baggage Compartments
Forward Cabin Compartment ............................................ ?
Hanger, Forward Cabin Compartment .............................. ?
Aft Baggage Compartment
Forward Section ......................................................... ?
Aft Section .................................................................. ?
Cabin Floor Loading .......................................................... ?
Revision .01
BEECH 1900D AIRLINER
L-32
WEIGHT LIMITS
Maximum Weight in Baggage Compartments
Forward Cabin Compartment ................... 250 lbs (113 kg)
Hanger, Forward Cabin Compartment........ 100 lbs (45 kg)
Aft Baggage Compartment
Forward Section............................... 1000 lbs (454 kg)
Aft Section ......................................... 630 lbs (286 kg)
Cabin Floor Loading ............... 100 lbs/sq ft (488 kg/sq m)
Revision .01
BEECH 1900D AIRLINER
L-32A
Limitations
MANEUVER LIMITS
Revision .01
BEECH 1900D AIRLINER
L-33
MANEUVER LIMITS
The Beech 1900D Airliner is a Commuter Category
Airplane. Acrobatic maneuvers, including spins, are
prohibited.
Revision .01
BEECH 1900D AIRLINER
L-33A
Limitations
FLIGHT LOAD FACTOR LIMITS
FLAPS UP
FLAPS 17°
FLAPS 35°
?
?
?
?
?
?
Revision .01
BEECH 1900D AIRLINER
L-34
FLIGHT LOAD FACTOR LIMITS
FLAPS UP
FLAPS 17°
FLAPS 35°
3.00 pos g’s
2.00 pos g’s
2.00 pos g’s
1.20 neg g’s
0.00 g
0.00 g
Revision .01
BEECH 1900D AIRLINER
L-34A
Limitations
MAXIMUM PASSENGER
OCCUPANCY LIMITS
Revision .01
BEECH 1900D AIRLINER
L-35
MAXIMUM PASSENGER
OCCUPANCY LIMITS
19
(18 when optional lavatory is installed)
Revision .01
BEECH 1900D AIRLINER
L-35A
Limitations
MAXIMUM OPERATING PRESSUREALTITUDE LIMIT
Revision .01
BEECH 1900D AIRLINER
L-36
MAXIMUM OPERATING PRESSUREALTITUDE LIMIT
25,000 FEET
Revision .01
BEECH 1900D AIRLINER
L-36A
Limitations
MAXIMUM OUTSIDE AIR
TEMPERATURE LIMIT
Revision .01
BEECH 1900D AIRLINER
L-37
MAXIMUM OUTSIDE AIR
TEMPERATURE LIMIT
ISA +37°C
Revision .01
BEECH 1900D AIRLINER
L-37A
Limitations
CABIN PRESSURIZATION LIMIT
Maximum Cabin Pressure Differential ............................... ?
Revision .01
BEECH 1900D AIRLINER
L-38
CABIN PRESSURIZATION LIMIT
Maximum Cabin Pressure Differential ..................... 5.1 PSI
Revision .01
BEECH 1900D AIRLINER
L-38A
Limitations
ICING LIMITATIONS
Revision .01
BEECH 1900D AIRLINER
L-39
ICING LIMITATIONS
Maximum Airspeed for Effective Windshield Anti-icing .................... 223 KNOTS
Minimum Temperature for Operation of Deicing Boots.............................. –40°C
Minimum Airspeed for Sustained Level Flight in Icing Conditions..... 160 KNOTS
Sustained flight in icing conditions with flaps extended is prohibited except
for approach and landings.
Engine Anti-ice shall be on for operations in ambient temperatures of +5°C
or below when flight free of visible moisture cannot be assured.
Operation of propeller deice is limited to one cycle per propeller at
ambient temperatures above 10°C.
Revision .01
BEECH 1900D AIRLINER
L-39A
Limitations
LANDING GEAR CYCLE LIMIT
Revision .01
BEECH 1900D AIRLINER
L-40
LANDING GEAR CYCLE LIMIT
1. The maximum number of consecutive gear cycles is
three, allowing 2 minutes between cycles.
2. Allow five minutes between each additional landing
gear cycle.
Revision .01
BEECH 1900D AIRLINER
L-40A
Limitations
HEADSETS
Revision .01
BEECH 1900D AIRLINER
L-41
HEADSETS
Pilot and Copilot headsets that can be worn with the oxygen masks must be installed and operational.
Revision .01
BEECH 1900D AIRLINER
L-41A
Limitations
CARGO LIMITATIONS
Revision .01
BEECH 1900D AIRLINER
L-42
CARGO LIMITATIONS
1. All cargo shall be properly secured by an FAAapproved cargo restraint system.
2. Cargo shall be so arranged as to permit crews emergency egress through the right forward emergency
exit.
Revision .01
BEECH 1900D AIRLINER
L-42A
Limitations
COCKPIT VOICE RECORDER
Revision .01
BEECH 1900D AIRLINER
L-43
COCKPIT VOICE RECORDER
The Cockpit Voice Recorder test described in Section 4,
NORMAL PROCEDURES, must be successfully accomplished prior to each flight.
Revision .01
BEECH 1900D AIRLINER
L-43A
Limitations
CRACKED OR SHATTERED WINDSHIELD
Revision .01
BEECH 1900D AIRLINER
L-44
CRACKED OR SHATTERED WINDSHIELD
1. Continued flight with a cracked windshield is limited to 25 flight hours.
2. Windshields which have a shattered inner ply will have numerous cracks
which will obstruct forward vision and may produce small particles or
flakes of glass that can break free of the windshield and interfere with the
crew’s vision. These windshields must be replaced prior to the next flight
unless a special flight permit is obtained from the local FAA Flight
Standards District Office.
3. Crack(s) must not impair visibility.
4. Crack(s) must not interfere with the use of windshield wipers for flights
requiring the use of the wipers.
5. Windshield Anti-ice must be operational for flights in icing conditions.
Revision .01
BEECH 1900D AIRLINER
L-44A