Beech 1900C

Service difficulty reports · 1,841

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Query with SQL
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 = '1900C'
  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 95ZZZX3383End Cap · crackedDURING SCHEDULED MAINTENANCE, A CRACK OF 1.5 INCHES WAS FOUND 4 INCHES INBOARD OF OUTBOARD END CAP 3 INCHES FROM TRAILING EDGE. STOPPED DRILLED AND INSTALLED DOUBLER.Jun 13, 1995 · N119YV · Beech 1900C · Trailing Edge FlapsSDR 95ZZZX3382End Cap · crackedDURING SCHEDULED MAINTENANCE, A CRACK OF .5 INCH WAS FOUND 30 INCHES INBOARD OF END CAP ON BOTTOM SIDE .5 INCHES FROM TRAILING EDGE AND A .375 INCH CRACK ON BOTTOM SIDE 46 INCHES FROM INBOARD END .5 INCH AFT OF LEADING EDGE. STOPPED DRILLED AND INSTALLED PATCJun 13, 1995 · N106YV · Beech 1900C · Trailing Edge FlapsSDR SW019514Downlock Switch · failedDURING APPROACH INTO CLARKSBURG, WV, PILOT SELECTED LANDING GEAR DOWN AND DID NOT GET A NOSE DOWN AND LOCK INDICATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE DOWNLOCK SWITCH AND RETURNED TO SERVICE. (X)Jun 9, 1995 · N158YV · Beech 1900C · Landing Gear Position and WarningSDR 95ZZZM210Dnlock Switch · failedDURING APPROACH INTO CLARKSBURG, WV, PILOT SELECTED LANDING GEAR DOWN AND DID NOT GET A NOSE DOWN AND LOCK INDICATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE DOWNLOCK SWITCH AND RETURNED TO SERVICE.Jun 9, 1995 · N158YV · Beech 1900C · Landing Gear Position and WarningSDR 95ZZZM209Seal · out of positionEN ROUTE TO UTICA, NY, AIRCRAFT WAS 17,000 FEET WHEN DOOR SEAL STARTED LEAKING (APPROX 2000 TO 3000 FEET CABIN ASCENT). AIRCRAFT DESENDED TO 10,000 FEET AND WAS ABLE TO MAINTAIN A 3000 FT CABIN ALTITUDE. AFTER LANDING, INSPECTION SHOWED DOOR SEAL WAS DISLODGJun 9, 1995 · N90YV · Beech 1900C · Passenger/Crew DoorsSDR 95ZZZM198Te Skin · crackedDURING SCHEDULED MAINTENANCE, A 1 INCH CRACK 3 INCHES FROM INBOARD EDGE AND .625 INCH FROM TRAILING EDGE. STOPPED DRILLED AND INSTALLED PATCH.Jun 9, 1995 · N85YV · Beech 1900C · Trailing Edge FlapsSDR 95ZZZM180Door Seal · dislodgedEN ROUTE TO UTICA, NY, AIRCRAFT WAS 17,000 FT WHEN DOOR SEAL STARTED LEAKING (APPROX 2000 TO 3000 FEET CABIN ASCENT). AIRCRAFT DESCENDED TO 10,000 FEET AND WAS ABLE TO MAINTAIN 3000 FEET CABIN ALTITUDE. AFTER LANDING INSPECTION SHOWED DOOR SEAL WAS DISLODGEDJun 9, 1995 · N90YV · Beech 1900C · Passenger/Crew DoorsSDR PLGA68951Altimeter · failedBOS - FLT NR 4864 - AFTER TAKEOFF THE CAPTAIN'S ALTIMETER FAILED, THE AIRCRAFT RETURNED TO BOS LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS ALTIMETER AND RETURNED THE AIRCRAFT TO SERVICE.Jun 8, 1995 · N820BE · Beech 1900C · Altimeter, Barometric/EncoderSDR 95ZZZX3038Blade · tip missingTHE POWER SECTION WAS RECEIVED FROM ARIZONA AIRWAYS WITH 35 PERCENT OF A FIRST STAGE PT BLADE TIP PLATFORM MISSING. AFTER THE PT BLADE AND DISK WERE DISASSEMBLED AND INSPECTED, A TOTAL OF (2) 1ST STAGE AND (11) 2ND STAGE BLADES WERE REPLACED.Jun 6, 1995 · N259AF · Beech 1900C · Turbine SectionSDR PLGA64951Keel Web · crackedDURING PERFORMANCE OF A NR 1 DETAIL WING INSPECTION THE LEFT NACELLE OUTBOARD KEEL WEB (P/N 114-980022-1) WAS FOUND TO HAVE A CRACK APPROXIMATELY 3 INCHES IN LENGTH. THE CRACK WAS ON THE FORWARD FLANGE THAT RIVETS TO THE ENGINE BAY AFT FIREWALL, ON THE LOWER Jun 4, 1995 · N807BE · Beech 1900C · Nacelle/Pylon StructureSDR PLGA63951Itt Indicator · malfunctionedAFTER TAKEOFF OF FLIGHT NR 4354, THE CREW NOTICED THE RIGHT HAND ITT INDICATOR WAS READING VERY HIGH. AIRCRAFT RETURNED TO ALB MAINTENANCE WHICH FOUND THE ITT INDICATOR OUT OF CAL. MAINTENANCE RECALIBRATED INDICATOR. OPERATIONS CHECKED GOOD. AIRCRAFT RETURJun 3, 1995 · N15553 · Beech 1900C · Engine EGT/TIT Indicating SystemSDR 95ZZZM202Truss · crackedDURING AD 95-02-18 AREA 'A' INSPECTION A .5 INCH CRACK WAS FOUND JUST AFT OF INBOARD UPPER BOSS ON RIGHT TRUSS. WELDED TRUSS AND RETURNED TO SERVICE.May 31, 1995 · N134YV · Beech 1900C · Engine Mount SectionSDR 95ZZZM201Skin · crackedDURING SCHEDULED MAINTENANCE, A .875 INCH CRACK WAS FOUND 15 INCHES FROM OUTBOARD EDGE AND 6 INCHES FROM TRAILING EDGE OF RIGHT INBOARD FLAP. STOPPED DRILLED AND INSTALLED DOUBLER.May 24, 1995 · N160AM · Beech 1900C · Trailing Edge FlapsSDR PLGA523951Keel · crackedDURING NR 1 DETAIL (WING) INSPECTION, THE LEFT NACELLE UPPER FORWARD KEEL (OUTBOARD) WAS FOUND TO HAVE 4 CRACKS ON FORWARD EDGE FLANGE. THESE CRACKS WERE FROM .375 INCH TO 1 INCH IN LENGTH BETWEEN RIVETS ON FORWARD EDGE FLANGE. AN APPROVED REPAIR IS BEING DEMay 23, 1995 · N817BE · Beech 1900C · Nacelle/Pylon StructureSDR 95ZZZM104Truss Assy · crackedWHILE COMPLYING WITH AD 95-02-18, AREA A, GP EXPRESS MAINTENANCE FOUND THE RT ENGINE TRUSS CRACKED IN THE FORWARD UPPER OUTBOARD POSITION. TRUSS WAS REPLACED WITH NEW P/N 114-910032-79 TRUSS ASSEMBLY. AIRCRAFT WAS RETURNED TO SERVICE. (M)May 22, 1995 · N319BH · Beech 1900C · Engine Mount SectionSDR 95ZZZM102Uplock Switch · shortedAFTER DEPARTURE FROM GJT, FLIGHT NR 2259 RETURNED TO GJT WHEN THE GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH. GP EXPRESS MAINTENANCE FOUND A DEFECTIVE RT MLG UPLOCK SWITCH. SWITCH WAS REPLACED WITH A NEW UNIT AND GEAR WAS CYCLED SEVERAL TIMES WITH NO DISCREPAMay 22, 1995 · N317BH · Beech 1900C · Landing Gear Position and WarningSDR 95ZZZM200Le Skin · dentedINBOUND TO DSM THE LEFT WING TOOK A BIRD STRIKE 3 FEET INBOARD OF WING TIP. REPAIRED WITH 14 INCH FILLER PATCH.May 14, 1995 · N97YV · Beech 1900C · Wing, Plate/SkinSDR 95ZZZM107Keel · crackedDURING LT ENG & TRUSS REPLACEMENT, LT NACELLE INBD & OTBD UPPER KEEL WEBS FND CRACKED. TWO CRACKS FND ON OTBD KEEL, P/N 114-98002201. ONE CRACK, APPROX 1.25 INCH LONG, LOCATED BETWEEN UPPER 2 RIVETS ON FWD SIDE OF KEEL WEB JUST BELOW UPPER OTBD TRUSS ATTACH May 13, 1995 · N812BE · Beech 1900C · Nacelle/Pylon StructureSDR 95ZZZM106Keel · crackedDURING LEFT ENGINE AND TRUSS REPLACEMENT THE LEFT NACELLE INBOARD AND OUTBOARD UPPER KEEL WEBS WERE FOUND TO BE CRACKED. TWO CRACKS WERE FOUND ON THE OUTBOARD KEEL, P/N 114-98002201. ONE CRACK, APPROXIMATELY 1.25 INCH LONG, WAS LOCATED BETWEEN THE UPPER 2 RIMay 13, 1995 · N812BE · Beech 1900C · Nacelle/Pylon StructureSDR 95ZZZM141Pwr Pack Motor · inopESC - THE CREW ELECTED AN AIR TURN BACK WHEN THEY WERE UNABLE TO RETRACT THE LANDING GEAR. AFTER AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE LANDING GEAR POWER PACK MOTOR. BOTH THE GEAR SWING AND THE TEST FLIGHT WERE SATISFACTORY.May 12, 1995 · N79GL · Beech 1900C · Landing Gear Retraction/Extension SystemSDR 95ZZZM199Skin · crackedDURING SCHEDULED MAINTENANCE, A 1.5 INCH CRACK WAS FOUND ON RIGHT OUTBOARD FLAP, 16 INCHES INBOARD OF END CAP AND 5 INCHES AFT OF LEADING EDGE. REPAIRED BY STOP DRILLED CRACK AND INSTALLED DOUBLER. (M)May 10, 1995 · N137YV · Beech 1900C · Trailing Edge FlapsSDR 95ZZZM103Engine · failedFLT NR 2094 - ON APPROACH TO BFF EXPERIENCED A SLIGHT VIBRATION FOLLOWED BY LEFT ENGINE SHUTDOWN, SHORTLY AFTER REDUCING POWER FOR APPROACH. AIRCRAFT LANDED SAFELY IN BFF WHERE GP EXPRESS MAINTENANCE FOUND THE ENGINE COMPLETELY SEIZED. ENGINE WAS REPLACED WIMay 9, 1995 · N318BH · Beech 1900C · Engine (Turbine/Turboprop)SDR 95ZZZW732Breaker · trippedFLT 487A - MCO-MIA - LANDING GEAR CIRCUIT BREAKER POPPED ON RETRACT OUT OF MCO. TROUBLE SHOT SYSTEM WIRING. PERFORMED SEVERAL GEAR SWINGS. OPS CHECK GOOD, COULD NOT DUPLICATE.May 8, 1995 · N198GA · Beech 1900C · Landing Gear Retraction/Extension SystemSDR 95ZZZM13Te Skin · crackedDURING SCHEDULED MAINTENANCE AND INSPECTION OF RIGHT OUTBOARD TE FLAP (P/N 35165050259) REVEALED A 1.5 INCH CRACK, LOCATED AT TRAILING EDGE APPROXIMATELY 10 INCHES INBOARD OF END CAP. STOP DRILLED CRACK AND INSTALLED DOUBLER.May 6, 1995 · N134YV · Beech 1900C · Trailing Edge FlapsSDR 95ZZZM19Eng Mount · crackedDURING SCHEDULED MAINTENANCE, AN INSPECTION OF LEFT TRUSS REVEALED A .375 INCH CRACK AT OUTBOARD UPPER MOUNT BOLT. CRACK AT LOWER OUTBOARD GUSSETT .5 INCH CRACK AT TOP INBOARD GUSSETT .5 INCH. CRACK AT TOP AFT, GUSSETT .375 INCH. REPAIRED BY WELDING ALL CRAMay 5, 1995 · N80ZR · Beech 1900C · Engine Mount SectionSDR 95ZZZM20Te Skin · crackedDURING ROUTINE MAINTENANCE A CRACK 1 INCH WAS FOUND ON TRAILING EDGE SKIN APPROXIMATELY 1 FOOT INBOARD OF END CAP. ON TE FLAP (P/N 3516505259). STOP DRILLED AND INSTALLED DOUBLER. (M)May 3, 1995 · N160AM · Beech 1900C · Trailing Edge FlapsSDR 95ZZZM143Bleed Valve · malfunctionedMHE - DURING APPROACH THE CREW REPORTED THAT THE LEFT ENGINE WAS COMPRESSOR STALLING. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE LEFT BLEED VALVE AND SEAT. A TEST FLIGHT WAS SUCCESSFUL.May 3, 1995 · N123UE · Beech 1900C · Compressor Bleed ValveSDR 95ZZZX2629Pad Rivet · crackedDURING RE-PADDING OF BRAKE STATIONARY DISC, RIVETS WERE FOUND TO HAVE MULTIPLE CRACKS IN THE SHOP HEAD AND NOT SECURELY HOLDING PAD IN POSITION.May 2, 1995 · Beech 1900C · BrakeSDR 95ZZZM15Le Skin · dentedINBOUND TO MCI A BIRD STRUCK THE RIGHT WING DENTING RIGHT WINGS LEADING EDGE. REPAIRED WITH FLUSH PATCH APPROXIMATLELY, 12 INCHES BY 10 INCHES ON LEADING EDGE. (M)May 2, 1995 · N69ZR · Beech 1900C · Wing, Plate/SkinSDR 95ZZZM147Hyd Pwr Pack · inopLAN - AFTER LIFTOFF, THE CREW ELECTED AN AIR TURN BACK WHEN THE GEAR WOULD NOT RETRACT. THEY REPORTED THAT THE MOTOR RUNS AND POPS CIRCUIT BREAKER. AFTER AN UNEVENTFUL LANDING, MAINTENANCE REPLACED THE HYDRAULIC POWER PACK AND MOTOR P/N 571302. ALL TESTS WEMay 2, 1995 · N87GL · Beech 1900C · Landing Gear Retraction/Extension SystemSDR 95ZZZX2511Engine Truss · chafedSPW - DURING ROUTINE MAINTENANCE, THE RT ENGINE TRUSS WAS FOUND CHAFED IN AREA 'C' AS DESCRIBED IN AD 95-02-18 AND BEECH SB 2255, REV 6. REPLACED TRUSS AND OPS CHECKED.Apr 30, 1995 · N159GL · Beech 1900C · Engine Mount SectionSDR 95ZZZM21Hot Section · failedFLT 5657 - ON INBOUND FLIGHT TO ICT CREW REPORTED SMOKE IN BLEED AIR SYSTEM. REMOVED POWER SECTION AND FOUND OIL IN GAS GENERATOR, HOT SECTION. REPLACED GAS GENERATOR SECTION. (M)Apr 29, 1995 · N134YV · Beech 1900C · Turbine Engine Combustion SectionSDR 95ZZZX3959Air Distr · odorPIT - AFTER TAKEOFF, CREW NOTICED AN ODOR AND HAZE IN THE CABIN AND COCKPIT. AFTER SHUTTING OFF BLEEDS, ODOR SUBSIDED. AIRCRAFT RETURNED TO GATE IN PIT. MAINTENANCE INSPECTED ENVIRONMENTAL SYSTEM AND RAN A.C. WITH BLEEDS ON AND PRESSURIZED. NO DEFECTS NOTEApr 28, 1995 · N140YV · Beech 1900C · Air Distribution SystemSDR 95ZZZM14Le Skin · crackedAN .625 INCH CRACK LOCATED AT THIRD RIB FROM INBOARD END ON BOTTOM OF FLAP NEAR LEADING EDGE OF TE FLAP (P/N 10116000144). STOP DRILLED AND INSTALLED DOUBLER CRACK WAS FOUND DURING SCHEDULED MAINTENACNE.Apr 28, 1995 · N69ZR · Beech 1900C · Wing, Plate/SkinSDR 95ZZZM18Skin · crackedFLAP IS CRACKED .5 INCH BETWEEN THIRD AND SECOND RIB FROM INBOARD END ON BOTTOM OF FLAP ON SPAR LINE AND A .75 INCH CRACK ON BOTTOM LEADING EDGE THIRD RIB FROM OUTBOARD END OF TE FLAP (P/N 35165050258). STOP DRILLED CRACKS AND INSTALLED DOUBLER CRACKS WERE FOApr 27, 1995 · N137YV · Beech 1900C · Trailing Edge FlapsSDR 95ZZZM17Le Skin · crackedFLAP CRACKED .75 INCH ON BOTTOM LEADING EDGE, 4TH RIB INBOARD. STOP DRILLED AND INSTALLED DOUBLER, ON LT TE FLAP (P/N 35165050258). CRACK WAS FOUND DURING SCHEDULED MAINTENANCE. (M)Apr 27, 1995 · N137YV · Beech 1900C · Trailing Edge FlapsSDR 95ZZZW698Dc Power Panel · open relayBOS - FLT NR 4736 - AFTER TAKEOFF THE RIGHT DC GENERATOR DROPPED OFF LINE AND WOULD NOT RESET. THE AIRCRAFT RETURNED TO BOS, LANDING UNEVENTFULLY. MX WAS DISPATCHED TO THE AIRCRAFT AND REPLACED THE LEFT DC POWER PANEL IAW THE BEECH MM AND RETURNED THE AIRCRAApr 26, 1995 · N31240 · Beech 1900C · DC Generating SystemSDR 95ZZZM22Oil Temp Sensor · fluctuatesFLT 5659 - EN ROUTE LEFT ENGINE OIL TEMP. FLUCTUATED FROM 60 TO 140 CELSIUS. CLEANED AND RESEATED CANNON PLUG, OPS CHECKED NORMAL. (M)Apr 26, 1995 · N85YV · Beech 1900C · Engine Oil TemperatureSDR 95ZZZW650Skin · crackedDURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD FLAP, P/N 35165050259, HAS A 1 INCH CRACK 9.75 INCH FROM INBOARD EDGE ON TRAILING EDGE OF UPPER SKIN. STOP DRILLED AND INSTALLED DOUBLER.Apr 25, 1995 · N143AM · Beech 1900C · Trailing Edge FlapsSDR 95ZZZW649Skin · crackedDURING SCHEDULED MAINTENANCE, A .5 INCH CRACK AT 2ND RIB FROM INBOARD END TOP OF FLAP P/N 10116000143, NEAR LEADING EDGE WAS FOUND. STOP DRILLED CRACKS AND INSTALLED DOUBLER.Apr 25, 1995 · N97YV · Beech 1900C · Trailing Edge FlapsSDR 95ZZZW695Engine Truss · crackedDURING A SCHEDULED INSPECTION, THE ENG TRUSS INSPECTION WAS COMPLIED WITH AS REQUIRED BY AD 95-0218, AND BEECH SB 2255, REV VI. THE TRUSS WAS FOUND BROKEN IN AREA A, ONE OF THE INSPECTION POINTS REQUIRED BY THE AD. THE ENGINE TRUSS WAS LAST INSPECTED ON 4/11Apr 24, 1995 · N11ZR · Beech 1900C · Engine Mount SectionSDR 95ZZZW651Le Skin · crackedDURING SCHEDULED MAINTENANCE, AN INSPECTION OF THE RT OUTBOARD FLAP, P/N 35165050259, REVEALED A .375 INCH CRACK NEAR LEADING EDGE AT 2ND RIB INBOARD AND A CRACK, 2 INCH ON BOTTOM BETWEEN 1ST AND 2ND RIB FROM INBOARD END AT TRAILING EDGE. CRACKS WERE STOPPED DApr 22, 1995 · N97YV · Beech 1900C · Trailing Edge FlapsSDR 95ZZZW652Te Skin · crackedDURING SCHEDULED MAINTENANCE, A CRACK .125 INCH WAS FOUND ON RIGHT FLAP, INBOARD TRAILING EDGE, NINTH RIB INBOARD AND WAS REPAIRED WITH A 2 INCH BY 2.5 INCH DOUBLER.Apr 16, 1995 · N143AM · Beech 1900C · Trailing Edge FlapsSDR 95ZZZX2501Altimeter · inopGRI - AFTER TAKEOFF, CREW ELECTED AN AIR TURN-BACK WHEN THE NR 1 ALTIMETER FLAGGED AND THE ALTITUDE ALERT WENT BLANK. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED ALTIMETER WHICH TESTED SATISFACTORILY.Apr 14, 1995 · N125GL · Beech 1900C · Altimeter, Barometric/EncoderSDR 95ZZZX2500Frame · crackedSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND CABIN DOOR FRAME CRACKED AT THE SNUBBER ATTACH BRACKET. THE FRAME WAS INSPECTED AND REPAIRED BY INSTALLING A 2024T3 .063 INCH DOUBLER IAW SRM 51-70-00, PAGES 52-53.Apr 14, 1995 · N87GL · Beech 1900C · Fuselage Miscellaneous StructureSDR PLGA413951Sungear · shearedPVD - ON TAKEOFF ROLL, THE LT ENGINE EXPERIENCED A LOSS OF POWER AND OIL PRESSURE. THE TAKEOFF WAS ABORTED, ENGINE WAS SHUTDOWN AND ACFT RETURNED TO GATE. INITIAL ON SITE INVESTIGATION REVEALED LOSS OF POWER TURBINE BLADES, PUNCTURED EXHAUST DUCTS AND DEBRISApr 13, 1995 · N810BE · Beech 1900C · Turbine SectionSDR 95ZZZM16Beta Cable · looseFLT 5630 - AFTER TAKEOFF LEFT TORQUE AND PROP RPM INDICATION FLUCTUATED. FOUND BETA CABLE LOOSE, TIGHTENED CABLE, RERIGGED LEFT ENGINE. OPS CHECK NORMAL. (M)Apr 13, 1995 · N160AM · Beech 1900C · Propeller Controlling SystemSDR 95ZZZX2499Engine · failedBIS - OUTBOUND FROM BIS, THE CREW EXECUTED AN AIR TURN-BACK AFTER THE RT ENGINE LOST OIL PRESSURE AND WAS SECURED. THE SINGLE ENGINE FLIGHT AND LANDING WERE UNEVENTFUL. MAINTENANCE REPLACED THE ENGINE AND THE TEST FLIGHT WAS SATISFACTORY. FAILURE IS ASSUMEDApr 11, 1995 · N84GL · Beech 1900C · Engine (Turbine/Turboprop)SDR 95ZZZW653Le Skin · chafed holeDURING SCHEDULED MAINTENANCE, A CHAFED HOLE APPROXIMATELY .25 INCH WAS FOUND ON THE LEADING EDGE OF LEFT INBOARD FLAP, P/N 1011600143, LOCATED 3RD RIB INBOARD FROM OUTBOARD END. REPAIRED WITH DOUBLER 2 INCHES BY 2.5 INCHES.Apr 11, 1995 · N97YV · Beech 1900C · Trailing Edge FlapsSDR 95ZZZW648Skin · crackedDURING SCHEDULED MAINTENANCE, AN INSPECTION OF THE RIGHT INBOARD FLAP P/N 10116000144, REVEALED A .75 INCH CRACK IN THE LOWER SKIN ALONG THE FIFTH RIB OUTBOARD FROM THE INBOARD END. THE CRACK WAS REPAIRED BY STOP DRILLING AND INSTALLING A DOUBLER APPROX 1.1 IApr 11, 1995 · N134YV · Beech 1900C · Trailing Edge Flaps
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