Beech 1900D

Service difficulty reports · 7,152

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '1900D'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 29GA2014072900001Line · inoperativeDURING APPROACH, WHEN LANDING GEAR WAS SELECTED TO THE DOWN POSITION, RED LIGHT IN GEAR HANDLE DID NOT EXTINGUISH AND NO 3 GREENS WERE OBSERVED. QRH WAS COMPLETED AND A MANUAL EXTENSION PERFORMED LANDING GEAR DOWN AND 3 GREEN LIGHTS WAS CONFIRMED ON AND SAFE Jul 24, 2014 · N81556 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA2014071800422Spar Cap · mechanic errorMAJOR REPAIR DURING A SCHEDULED INSPECTION FOUND THE LT WING SPAR AFT CAP AT WS 12325 FASTENER HOLE MISSED DRILLED THROUGH THE WING SKIN & WING SPAR CAP. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-57-003. MATERIALS UTIJul 16, 2014 · N247GL · Beech 1900D · Wing SparSDR CA140811002Pitot Tube · malfunctioned(CAN) DURING DEPARTURE, ADVISED OF A PITOT TUBE ISSUE AND REQUESTED TO RETURN TO THE AIRPORT, RETURNED AND LANDED SAFELY. UPON ARRIVAL MAINTENANCE CARRIED OUT AN INSPECTION AND FOUND THE LEFT HAND (LH) PITOT TUBE ELEMENT TO BE AT FAULT. THE PITOT TUBE WAS REPJul 14, 2014 · Beech 1900D · Pitot/Static SystemSDR GLBA2014071400420Tire · failedPILOT STATED THAT THE TOWER CALLED & SAID THEY SAW DEBRIS AFTER TAKEOFF. GROUND OPS CONFIRMED PIECES OF A TIRE ON THE RUNWAY. DECLARED AN EMERGENCY & RETURNED TO THE FIELD, RT INBD TIRE HAD SEPARATED. MAINTENANCE REPLACED BOTH RT TIRES.Jul 13, 2014 · N100UX · Beech 1900D · TireSDR GLBA2014071400421Uplock Switch · faultyPILOT REPORTED THAT ON MLG EXTENSION THE CREW HEARD THE MOTOR RUN FOR APPROX 15 SECONDS THEN THE CB NEXT TO THE GEAR HANDLE POPPED. RAN CHECKLIST & MANUALLY EXTENDED GEAR, ALL INDICATIONS WERE NORMAL. REPLACED THE RT MLG UPLOCK SWITCH & RIGGED IAW TC 1900-32Jul 12, 2014 · N245GL · Beech 1900D · Landing Gear Position and WarningSDR 8EKA20140723001Relay · stuckCREW PUT THE LG UP WITH NO ISSUES. WHEN THEY PUT THE GEAR HANDLE DOWN, THE GEAR DID NOT GO DOWN. THEY NOTICED THAT THE LG CONTROL CB WAS POPPED & ATTEMPTED TO PUSH IT IN. WHEN THEY DID THIS THE GEAR UNLOCKED & STARTED TO DROP & THE GEAR CONTROL BREAKER POPPJul 9, 2014 · N104EV · Beech 1900D · Hydraulic Pump (Electric/Engine), MainSDR CA140707012Control Cable · damaged(CAN) FLIGHT CREW HAD EXPERIENCED LOSS OF ELEVATOR TRIM TAB CONTROL. UPON INVESTIGATION BY MAINTENANCE, IT WAS FOUND THAT THE PRIMARY TAB CONTROL CABLE HAD WORN AND SEPARATED WHERE IT IS ROUTED THROUGH THE ELEVATOR TRIM TAB SERVO, A PART OF THE INSTALLED AUTOJul 4, 2014 · Beech 1900D · Elevator Tab Control SystemSDR GLBA2014070300419Line · rupturedLANDING GEAR FAILED TO EXTEND NORMALLY, GEAR INTRANSIT LIGHT ILLUMINATED, WITH GEAR SELECTED DOWN. TRANSIT LIGHT FAILED TO EXTINGUISH NORMALLY, HYD FLUID LOW ANNUNCIATOR ILLUMINATED. PERFORMED MANUAL GEAR EXTENSION, GEAR IND WERE NORMAL. ON LANDING, FOUND Jul 2, 2014 · N261GL · Beech 1900D · Hydraulic System, MainSDR GLBA2014070100418Uplock Switch · malfunctionedPILOT REPORTED THAT THE CIRCUIT BREAKER TRIPPED ON THE LANDING GEAR CONTROL, RAN CHECKLIST, PROCEEDED TO DESTINATION & USED THE MANUAL EXTENSION. MAINTENANCE R & R RT UPLOCK SWITCH IAW TC 1900-3260.00 REV 2.Jul 1, 2014 · N245GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA2014062300417Connector · unsecureSIG EVENT PILOT REPORTED THAT AN UNSCHEDULED AUTO FEATHER ACTIVATION ON THE RT ENG, ON APPROACH SEVERAL TIMES UNTIL THE SYS WAS TURNED OFF. SECURED THE RT LP AFX SWITCH CONNECTOR, OPERATIONS CHECKED GOOD.Jun 21, 2014 · N220GL · Beech 1900D · Propeller/Propulsor System WiringSDR CA140623001Connector · damagedCREW REPORTED, UNABLE TO DISCONNECT PITCH TRIM USING BOTH CONTROL WHEEL DISCONNECT BUTTONS. PROBLEM DETERMINED TO BE LOW VOLTAGE (22V) AT PIN -K-, CONNECTOR P312, THUS PREVENTING K1 TO REMAIN ENERGIZED ONCE PITCH/TRIM DISCONNECT SWITCH WAS RELEASED. CAUSE OFJun 19, 2014 · Beech 1900D · Flight Control System WiringSDR CA140619006Terminal · damaged(CAN) AFTER DEPARTURE THE RH AC BUS ANNUNCIATOR ILLUMINATED. TROUBLE SHOOTING CARRIED OUT BY THE CREW WAS UNSUCCESSFUL. THE AIRCRAFT RETURNED TO THE POINT OF DEPARTURE AS THIS WAS A MAINTENANCE BASE. UPON ARRIVAL A SYSTEM INSPECTION WAS COMPLETED AND MAINTENANJun 19, 2014 · Beech 1900D · Electrical Power System WiringSDR CA141014003Rib · worn(CAN) LEFT HAND INBOARD RIB FLANGE WORN AWAY AT UPPER TWO FASTENERS OF FENDER SUPPORT STIFFENER. REPAIR CARRIED OUT IAW 3 POINTS MACHINING & AEROSPACE A-RA14-012/D. DAMAGE KEEL WEB AT THE TWO LOOSE FASTENERS REMOVED. REPAIR ANGLE MADE AND INSERTION REPAIR SHIJun 11, 2014 · Beech 1900D · Wing, Rib/BulkheadSDR CA141014002Spar Cap · chafed(CAN) MINOR CHAFING ON LOWER AFT WING SPAR CAP SURFACE FROM LOOSE FENDER BRACKET (BOTH LH AND RH SIDES). RECTIFICATION: REPAIR CARRIED OUT IAW FR-CO-102496 REV 2. CHAFING REMOVED. NDT CARRIED OUT TO ENSURE NO FURTHER DAMAGE EVIDENT. SHIM FILLER PLATES INSTAJun 10, 2014 · Beech 1900D · Wing SparSDR CA140620005Engine · power loss(CAN) AT TAKE OFF POWER, THE PILOT OBSERVED PROPELLER SPEED AND TORQUE FLUCTUATIONS. DURING THE TROUBLESHOOTING, THE OVERSPEED GOVERNOR WAS CHANGED AND FLUCTUATIONS PERSISTED. TROUBLESHOOTING IS ONGOING.Jun 8, 2014 · Beech 1900D · Engine (Turbine/Turboprop)SDR CA141014001Spar Cap · cracked(CAN) VERTICAL FWD PORT & STARBOARD CAPS FOUND CRACKED AT UPPER ATTACH POINT FASTENERS. IAW RDO FR-CO-102431. UPPER DAMAGED PORTIONS OF SPAR CAPS CUT AWAY. INSERTION PIECES OF SPAR CAPS AND DOUBLER REPAIR ANGLES CUT FROM NEW SPAR CAPS WITH SPLICE CARRIED OUT Jun 2, 2014 · Beech 1900D · Wing SparSDR CA140813005Motor · malfunctioned(CAN) LANDING AT THE AIRPORT, THE CREW COMPLETED THE AFTER LANDING CHECKLIST AND STARTED TO SMELL SMOKE. THE CREW CONTINUED TO TAXI TO THE GATE AND DE-PLANED THE PASSENGERS NORMALLY. THE CREW THEN SAW SMOKE IN THE CABIN, ADVISED THE AIRPORT, AND TURNED OFF THMay 28, 2014 · Beech 1900D · Trailing Edge Flap ActuatorSDR GLBA2014052800416Door Frame · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK AT THE LOWER AIR STAIR DOOR FRAME, AIRFRAME SIDE, LOWER AFT CORNER, BS 173.35, VISIBLE PORTION OF CRACK 1.75 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-026.May 28, 2014 · N192GL · Beech 1900D · Fuselage Main, StructureSDR CA140811001Selector · failed(CAN) UPON DEPARTURE THE CREW SELECTED GEAR UP AND IT REMAINED DOWN AND LOCKED. THE GEAR WAS CYCLED ONCE WITH SAME RESULTS. CREW CARRIED OUT APPLICABLE CHECKLIST PROCEDURES. GEAR WAS CONFIRMED DOWN AND LOCKED. ATC WAS ADVISED. CREW THEN DIVERTED TO MAINTENANCEMay 27, 2014 · Beech 1900D · Landing Gear SelectorSDR 29GA2014052700001Spar Cap · crackedLEFT SPAR CAP CRACKED ON VERTICAL STABILIZER. REPAIRED LEFT SPAR CAP IAW FR-CO-102455 REV 1.May 27, 2014 · N81536 · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2014052700415Actuator · failedPILOT REPORTED THAT WHILE COMING IN ON FINAL SELECTED THE GEAR DOWN & AFTER THE LG CYCLED, THE LT GEAR FAILED TO ILLUMINATE DOWN & LOCKED, RAN CHECKLIST, FAILED TO RESOLVE SITUATION, CONTACTED DISPATCH & TOWER DECLARED EMERGENCY, PUMPED GEAR DOWN. MAINTENANCEMay 25, 2014 · N202UX · Beech 1900D · Landing Gear ActuatorSDR CA140526007Wire Harness · burned(CAN) CREW REPORTED THAT THE GENERATORS WERE NOT SHARING LOADS DURING RUN UP PROCEDURES. RT GENERATOR WAS AT 5 PERCENT, LT GENERATOR WAS AT 25 PERCENT. ACFT WAS EVALUATED BY MAINTENANCE AND IT WAS FOUND THAT THE RING TERMINALS WERE BURNED AND CORRODED. MAINMay 23, 2014 · Beech 1900D · Electrical Power System WiringSDR GLBA2014050600412Skin · crackedDURING A SCHEDULED INSPECTION, MX FOUND A CRACK AT THE EMERGENCY EXIT, RT FWD, BONDED SKIN AT THE LWR AFT CORNER, 1.3" IN LENGTH. REPAIRED IAW EO 14-1900-52-004.May 5, 2014 · N255GL · Beech 1900D · Fuselage Main, Plate/SkinSDR CA140501004Motor · failed(CAN) UPON LANDING, THE CREW REPORTED TO MAINTENANCE THAT THE FLAPS WERE UNSERVICEABLE. AFTER CONSULTATION WITH MAINTENANCE, THE AIRCRAFT CONTINUED OPERATION UNDER THE COMPANY`S MEL PROTOCOL. ONCE THE AIRCRAFT RETURNED TO THE MAINTENANCE BASE, AN INSPECTION WAApr 29, 2014 · Beech 1900D · Trailing Edge Flap ActuatorSDR GLBA2014042800411Rib · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE LT WING INBD RIB FLANGE & DOUBLER FLANGE AT FS 288 & BL 29.06, FROM OTBD EDGES INWARD TO BEND RADIUS OF THE RIB FLANGE & DOUBLER FLANGE, 1 INCH IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIApr 28, 2014 · N255GL · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2014042400410Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE FRAME AT FS 183.25 BETWEEN STRINGER 2R & 3R AT THE INBD LOWER CORNER AT AIR DUCT CUTOUT FROM A FASTENER TO THE BEND RADIUS, .2 INCHES IN LENGTH. MAJOR REPAIR, REPAIRED THE AFFECTED AREA AND PERFORApr 24, 2014 · N255GL · Beech 1900D · Fuselage Main, FrameSDR ERAA20140022Indicator · inoperativeLEFT PROP GAUGE INOPERATIVE ON TAKEOFF ROLL. R & R PROP INDICATOR, OPERATIONS CHECKED GOOD IAW MM 31-10-00.Apr 18, 2014 · N972EA · Beech 1900D · Propeller Indication SystemSDR CA140417008Valve · failed(CAN) AFTER OPERATING A SINGLE SURFACE DE-ICE CYCLE THE OTBD WING DE-ICE BOOTS WOULD NOT DEFLATE. TROUBLESHOT SYS AND FOUND DISTRIBUTOR VALVE UNSERVICEABLE. DISTRIBUTOR VALVE REPLACED WITH O/H UNIT. OPS CHECK COMPLETED, SYS FUNCTION NORMAL.Apr 16, 2014 · Beech 1900D · Airfoil Anti/De-ice SystemSDR GLBA2014041500408Skin · crackedDURING A SCHEDULED INSPECTION MX FOUND 3 CRACKS AT FS 163.97 & STRINGER 1, AT FASTENERS ON LT & RT SIDE OF STRINGER 1, .35 INCHES IN TOTAL LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-024.Apr 15, 2014 · N255GL · Beech 1900D · Fuselage Main, Plate/SkinSDR CA140415009Heater · unserviceable(CAN) PILOT REPORTED DEFECT OF NR 2 ENGINE OIL PRESSURE FLUCTUATING, AND HIGH OIL CONSUMPTION. AFTER 45 MINUTES OF FLIGHT OIL PRESSURE WOULD DROP FROM A STABLE 110PSI TO 90PSI AND FLUCTUATE APPROXIMATELY 10 PSI. AFTER LANDING AND CHECKING OIL LEVEL THE ENGINApr 10, 2014 · Beech 1900D · Engine Fuel/Oil CoolerSDR A8OA2014F00087Annunciator · no indicationLT ENGINE AFX, AUTOFEATHER, ANNUNCIATOR DID NOT ILLUMINATE AT TAKEOFF POWER.Apr 9, 2014 · N60MJ · Beech 1900D · Propeller Feathering/ReversingSDR GLBA2014040200407Skin · damagedTRAILING EDGE OF THE RT ELEVATOR FROM 165YV HAS TORN & BENT SKIN, 16 INCHES TO 24 INCHES FROM OTBD TIP & 6.5 INCHES FROM TE FWD, TE RIBS 3 & 4 BENT AT TE. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-27-001.Apr 2, 2014 · N113YV · Beech 1900D · Elevator, Plate/SkinSDR ERAA20140008Blower · malfunctionedON FINAL, BLOWERS WERE SELECTED TO AUTO & ELEC BURNING SMELL WAS DETECTED, BLOWERS TURNED OFF AGAIN & SMELL DISSIPATED. FOUND FWD VENT BLOWER BAD, R & R IAW MM CH21-20-01, OPERATIONS CHECKED GOOD.Mar 19, 2014 · N971EA · Beech 1900D · Air Distribution FanSDR GLBA2014031700404Tire · blownPILOT NOTED THAT BOTH LT MAIN TIRES BLEW ON LANDING. R & R NR 1 & NR 2 MAIN WHEEL ASSEMBLIES IAW TASK CARD 1900-3240-01. PN 5006028-5, NR 1 SN ON 56/917, SN OFF 1601, NR 2 SN ON 561 431, SN OFF 284 1930. PERFORMED VISUAL INSPECTION OF LT MLG HUBS, BRAKES & Mar 16, 2014 · N255GL · Beech 1900D · TireSDR GLBA2014031700403Door Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND LOWER AIRSTAIR DOOR FRAME AFT CRACKED APPROXIMATELY 1/2 INCH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-022.Mar 15, 2014 · N240GL · Beech 1900D · Fuselage Main, StructureSDR GLBA2014031700402Door Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND FWD FRAME AIRSTAIR DOOR CUTOUT AT FS 150.6 BETWEEN STRINGER 10L & 11L CRACKED, CRACK IS APPROXIMATELY 1/2 INCHES. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-023.Mar 15, 2014 · N240GL · Beech 1900D · Fuselage Main, StructureSDR 29GA2014031332936Switch · inoperativeGEAR WARNING HORN NEVER SOUNDED BELOW 86 PERCENT. REPLACED LT GEAR WARNING HORN SWITCH AND RIGGED BOTH SWITCHES. GROUND CHECKED GOOD.Mar 13, 2014 · N81536 · Beech 1900D · Landing Gear Position and WarningSDR GLBA201403140001Connector · looseUPON EXTENDING GEAR ON FINAL, RT GEAR R & H ANNUNCIATORS FAILED TO ILLUMINATE. UPON COMPLETION OF CHECKLIST, ALL OTHER INDICATIONS REVEALED GEAR DOWN & LOCKED. INSTRUCTED BY MX TO RECYCLE GEAR, J HOOK WOULD NOT ALLOW GEAR HANDLE TO BE MOVED UP. ATTEMPTED TO Mar 13, 2014 · N201GL · Beech 1900D · Landing Gear System WiringSDR ERAA20140007Motor · failedAFTER FFRUI PARKED ACFT AT GATE & FOUND SMOKE PRESENT IN CABIN SECTION. THE SMELL WAS ACRID. REPLACED FLAP MOTOR, INSTALLED OVERHAULED FLAP MOTOR ASSEMBLY, SYS RIGGED. OK FOR SERVICE IAW MM 27-50-00.Mar 12, 2014 · N971EA · Beech 1900D · Trailing Edge Flap ActuatorSDR GLBA2014031000400Skin · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE SKIN AT THE RT FWD SPAR CAP AREA, FS 288.0, 1.5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-021.Mar 9, 2014 · N100UX · Beech 1900D · Fuselage Main, Plate/SkinSDR CA140304010Altimeter · malfunctioned(CAN) AFTER TAKEOFF, THE PILOT`S ALTIMETER FLAG WOULD NOT GO AWAY. AT THE SAME TIME, THE ALTITUDE ALERTER KEPT CHIMING AND COULD NOT BE RESET.Mar 3, 2014 · Beech 1900D · Altimeter, Barometric/EncoderSDR GLBA2014030300398Channel · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE LT HAT SECTION OF THE UPPER FLANGE FROM FWD FASTENER TO FLANGE LE, VSS 84.10 & 206 CHORD, .35 INCH IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-55-002.Mar 3, 2014 · N255GL · Beech 1900D · Vertical Stabilizer Miscellaneous StructureSDR GLBA2014022800397Frame · corrodedDURING A SCHEDULED INSPECTION MX FOUND CORROSION AT FS 288.000 ON THE FRAME WHERE THE STRINGERS 16, 15R, 15L, 14R, & 14L ATTACHED, AREA OF 3 INCHES WIDE BY 2 INCHES. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-014.Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, FrameSDR GLBA2014022800396Stringer · corrodedDURING A SCHEDULED INSPECTION MX FOUND CORROSION AT FS 258.250 TO FS 288.000 ON STRINGER 14L AT FAYING SURFACE. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-013.Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2014022800395Stringer · corrodedDURING A SCHEDULED INSPECTION MX FOUND CORROSION AT FS 258.250 TO FS 288.000 ON STRINGER 15L AT FAYING SURFACE. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-015.Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2014022800394Stringer · corrodedDURING A SCHEDULED INSPECTION MX CORROSION AT FS 258.250 TO FS 288.000 AT STRINGER 16 ON FAYING SURFACE. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-016.Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2014022800393Stringer · corrodedDURING A SCHEDULED INSPECTION MX FOUND CORROSION AT FS 258.250 TO FS 288.000 ON STRINGER 15R AT FAYING SURFACE. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-017.Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2014022800392Stringer · corrodedDURING A SCHEDULED INSPECTION MX FOUND CORROSION AT FS 258.250 TO 288.000, STRINGER 14R AT FAYING SURFACE. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-018.Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2014022800390Skin · tornDURING A SCHEDULED INSPECTION MX FOUND THE SKIN TORN ON THE BELLY AT FS 265.750 & STRINGER 14L, APPROXIMATELY 5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-020.Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2014022800389Motor · faultyPILOT REPORTED THAT THERE WAS A STRONG BURNING SMELL COMING FROM THE CABIN & IS IRRITATING TO TO EYES. TROUBLESHOT BURNING SMELL COMING FROM FLAP GEAR BOX MOTOR ASSEMBLY. R & R FLAP GEAR BOX MOTOR ASSEMBLY PN 100-524073-1 SN OFF 5693, IAW BMM 27-50-03 OPERATFeb 26, 2014 · N210GL · Beech 1900D · Trailing Edge Flap Actuator
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