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 GLBA2012041201Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS IN THE FUSELAGE FRAME AT FS 509 AND BETWEEN STRINGERS 4L & 5L AT THE CARGO DOOR STRUT MOUNT, UPPER INBD NUTPLATE MOUNT, 1.8" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EApr 12, 2012 · N254GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2012041002Spar · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS IN THE HORIZONTAL STAB REAR SPAR WEB AT 10, 2, 5, & 7 O`CLOCK POSITION VIEWING FWD, TOTAL LENGTH 1". REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-55Apr 10, 2012 · N254GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012041001Door Frame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE AIR STAIR DOOR ENTRANCE LWR FRAME AT THE LWR AFT CORNER, FS 173, 1.3" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 12-1900-53-020. MAJOR REPAIR.Apr 10, 2012 · N254GL · Beech 1900D · Fuselage Main, StructureSDR 29GA93832040912Switch · out of adjustFLIGHT 4009, PILOT REPORTED LANDING GEAR WARNING HORN COMES OFF AT 91% N1. ADJUSTED POWER LEVERS SWITCHES, TEST FLIGHT SATISFACTORY.Apr 9, 2012 · N81538 · Beech 1900D · Power LeverSDR 29GA201204110001Switch · dirtyIN FLIGHT, REDUCED POWER TO IDLE NO HORN NO GEAR LIGHTS. PERFORMED INSP OF LANDING GEAR HORN SYS AND INTRANSIT LIGHT SYS CLEANED DEBRIS FROM LANDING GEAR SWITCHES OPS CHECKED GOOD.Apr 7, 2012 · N16540 · Beech 1900D · Landing Gear Position and WarningSDR GLBA2012040501Spar · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A SMALL CRACK ON THE HORIZONTAL STAB AFT SPAR CENTER WEB AT 2-OCLOCK POSITION AS VIEWED FROM REAR, .125" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW FR EO 02Apr 5, 2012 · N178YV · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR ERAA20120036Pressure Switch · defectiveAFX DISABLE LIGHT - RIGHT AUTO FX DIDN'T ARM. REMOVED AND REPLACED NR 1 AUTO FEATHER HIGH PRESSURE SWITCH IAW MM 61-21-00. OPS CHECKED GOOD IAW MM 61-21-00. LEAK CHECKED GOOD. OK FOR CONTINUED SERVICE AT THIS TIME.Apr 4, 2012 · N973EA · Beech 1900D · Propeller Feathering/ReversingSDR 29GA95532040312ACircuit Board · looseFLIGHT 3994, GEAR HANDLE LIGHTS DO NOT ILLUMINATE IN FLIGHT WHEN POWER LEVERS REDUCED BELOW 85% GEAR WARNING HORN WORKS NORMAL. SECURED LANDING GEAR CONTROL RELAY BOARD. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK GOOD.Apr 3, 2012 · N87555 · Beech 1900D · Landing Gear System WiringSDR GLBA2012040203Skin · damagedDURING A SCHEDULED ROUTINE INSPECTION, FOUND THE RT FUSELAGE FS 288 HAS ELONGATED HOLES FROM ATTACHING FAIRING PANEL TO FS 327. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-019. MATERIALS UTILIZED ARE INCLUDED IN TApr 2, 2012 · N210GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012040202Fairing · damagedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A HOLE IN THE FUSELAGE FARING, RT SIDE UNDER AFT WING, AFT OF FS 363.250, 2.25 INCHES JUST ABOVE STRINGER 1R, .687 BY .25. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-01Apr 2, 2012 · N210GL · Beech 1900D · Aerodynamic FairingsSDR CA120411005Gear · failed(CAN) DURING CLIMB NR 1 ENGINE LOST POWER, FOLLOWED BY A TORQUE DECREASE AND FLUCTUATING, THIS WAS ALSO ACCOMPANIED BY AN OIL PRESSURE LIGHT. THE CREW ELECTED TO SHUTDOWN THE ENGINE AND RETURNED TO DEPARTURE. FIRST ATTEMPT TO START THE ENGINE WAS SUCCESSFUL.Apr 1, 2012 · Beech 1900D · Turbine Engine Reduction GearSDR GLBA2012040201Engine · failedPILOT REPORTED THAT AFTER TAKEOFF AT 5000 FT, NR 1 ENGINE SHUTDOWN, RAN CHECKLIST, DECLARED EMERGENCY, RETURNED TO DEPARTURE, MANUALLY FEATHER NR 1 PROP. MX R & R LT ENGINE, PWR SEC AND GAS GENERATOR, IAW TC 1900-7100-00, OPS CHECKED GOOD.Apr 1, 2012 · N153GL · Beech 1900D · Engine (Turbine/Turboprop)SDR 29GA94332033112AWire · shortedFLIGHT 4026, LANDING GEAR HAS TO BE MANUALLY PUMPED, THREE GREEN AFTER MANUAL EXTENSION. RECONNECTED HYDRAULIC POWER PACK SELECT VALVE WIRING AT LEFT STUB WING INBOARD OF FUSELAGE, LANDING GEAR EXTENSION AND RETRACTION. OPS CHECKED GOOD.Mar 31, 2012 · N49543 · Beech 1900D · Landing Gear System WiringSDR 29GA20120331943Wire · shortedFLIGHT4026, LANDING GEAR HAS TO BE MANUALLY PUMPED, THREE GREEN AFTER MANUAL EXTENSION. RECONNECTED HYDRAULIC POWER PACK SELECT VALVE WIRING AT LEFT STUB WING INBOARD OF FUSELAGE, LANDING GEAR EXTENSION AND RETRACTION, OPS CHECKED GOOD.Mar 31, 2012 · N49543 · Beech 1900D · Landing Gear System WiringSDR GLBA2012033002Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 5 TO 7 CRACKS RADIATING FROM THE CENTER LIGHTNING HOLE ON THE STAB REAR SPAR CENTER WEB, 2.5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-55-009. MATERIALMar 30, 2012 · N247GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012033001Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS ON MAIN SPAR WEB AT HSS 3.0L AND 3.0R, 1 INCH IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-55-010. MATERIALS UTILIZED ARE INCLUDED IN THE EO. MAJOR REPAIMar 30, 2012 · N247GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR 29GA94252033012Handle · stiffDURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT EMERGENCY EXIT OUTER HANDLE STIFF TO OPERATE. CLEANED AND LUBRICATED LEFT EMERGENCY EXIT OUTER HANDLE.Mar 30, 2012 · N47542 · Beech 1900D · Emergency ExitsSDR EHAA20120329004Relay · defectivePIC NOTICED LANDING GEAR CB POPPED. FOLLOWED CHECKLIST AND CB RESET AND IT POPPED AGAIN. AIRCRAFT RETURNED TO BASE. CREW MANUALLY EXTENDED LANDING GEAR. AIRCRAFT LANDED WITH NO ISSUE.Mar 29, 2012 · N171CJ · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 29GA93852032312AHandle · lack of lubeREPORT: DURING SCHEDULED ROUTINE INSPECTION DICOVERED RIGHT AFT EMERGENCY EXIT OUTER LATCH HANDLE CATCH WILL NOT SPRING OPEN. LUBRICATED RIGHT AFT EXIT OUTER DOOR HANDLE AND LATCH MECHANISM.Mar 23, 2012 · N81538 · Beech 1900D · Emergency ExitsSDR 29GA95532032312AWarning System · malfunctionedFLIGHT: 4022 TCB/FLL GEAR WARNING HORN DOES NOT GO OFF WHEN POWER LEVERS ARE BROUGHT TO IDLE AND NO GEAR LIGHTS. PERFORMED LANDING GEAR OPERATIONAL CHECKS. OPERATIONAL CHECKS NORMAL.Mar 23, 2012 · N87555 · Beech 1900D · Landing Gear Position and WarningSDR GLBA2012032300001Damper · wornEXPERIENCED VIOLENT NOSE WHEEL SHIMMY DURING TO AT APPX V1. CONTINUED UNTIL SHORTLY AFTER GEAR RETRACTION. MX REPLACED THE NLG TIRE IAW TC 1900-3240.00 AND REPLACED SHIMMY DAMPER IAW MM 32-20-03.Mar 22, 2012 · N170GL · Beech 1900D · Nose/Tail Landing GearSDR 29GA93532032212AWarning Light · intermittentFLIGHT: 4070 FKL/DUJ WHEN LANDING GEAR HANDLE MOVED GEAR INTRANSIT LIGHT IS INTERMITTENT. CLEANED LAMP CONTACTS AND LANDING GEAR HANDLE ASSEMBLY OPERATIONAL CHECKS GOOD.Mar 22, 2012 · N81535 · Beech 1900D · Landing Gear Position and WarningSDR GLBA2012032301Spar · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS AT A MACHINED HOLE AT 2, 8, 10, & 4 O'CLOCK POSITIONS AT THE HORIZONTAL STAB AFT SPAR WEB AT HSS 0.0, .73" IN LENGTH.Mar 22, 2012 · N170GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012032101Spar · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS AT A MACHINED HOLE AT 2, 8, 10, & 4 O'CLOCK POSITIONS AT THE HORIZONTAL STAB AFT SPAR WEB AT HSS 0.0, .73" IN LENGTH. ED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-55-008. MATERIALS UTILMar 20, 2012 · N210GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR CA120321002Hose · cracked(CAN) CRACK EXTENDING APPROX .7500 OF THE CIRCUMFERENCE AT THE MOUNTING FLANGE ON THE LT INBD BLEED AIRHOSE LT ENGINE.Mar 19, 2012 · Beech 1900D · Engine Bleed Air SystemSDR GLBA201203191205Skin · chafedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 RIVET HEADS CHAFING ON A PREVIOUS REPAIR OF THE LOWER RT WING WHERE THE FUSELAGE MEETS THE WING. REPAIRED IAW EO 12-1900-53-014. MAJOR REPAIR.Mar 19, 2012 · N210GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012031904Attach Fitting · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT THE NUTPLATE, FWD CARGO DOOR SNUBBER FUSELAGE ATTACH POINT, UPPER IB NUTPLATE FS 456, .35" IN LENGTH. REPAIRED IAW EO 12-1900-53-014. MAJOR REPAIRMar 19, 2012 · N210GL · Beech 1900D · Cargo/Baggage DoorsSDR GLBA2012031903Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE SKIN, LT BELLY AT FS 303.25 WHERE THE FUSELAGE MEETS THE WING, 5" IN LENGTH. REPAIRED IAW EO 12-1900-53-015. MAJOR REPAIRMar 19, 2012 · N210GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012031902Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FRAME AT FS 150.6 BETWEEN STRINGERS 2R AND 3R, .9" IN LENGTH. REPAIRED IAW EO 12-1900-53-016. MAJOR REPAIRMar 19, 2012 · N210GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2012031901Doubler · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT DOUBLER, FWD END, FS 288, 1.2" IN LENGTH. REPAIRED IAW EO 12-1900-53-017.Mar 19, 2012 · N210GL · Beech 1900D · Fuselage Main, StructureSDR 29GA94632031812AWarning Switch · out of adjustFLIGHT: 4069 CLE/DUJ DURING APPROACH LANDING GEAR WARNING HORN ACTIVATES AT 1600 FTLB WHEN RETARDING PROP LEVERS TURBINE SPEED WAS 88.8%. ADJUSTED LEFT AND RIGHT PEDESTAL HORN SWITCHES, TEST FLIGHT SATISFACTORY.Mar 18, 2012 · N81546 · Beech 1900D · Landing Gear Position and WarningSDR CA120319012Terminal · loose(CAN) ITERMITTENT BUZZING AUDIO SOUND THROUGH INTERCOM WITH ASSOCIATED AUTO PILOT. PITCHING ON RT AUTOPILOT COMPUTER.FAULT CONFIRMED BY MAINTENANCE,WIRING AT GS 10 FOUND TO BE LOOSE AT GROUND TERMINALS AND SPARKING WHEN MOVED. RETERMINATED AND RE-SECURED. FUNMar 15, 2012 · Beech 1900D · Auto Flight System WiringSDR GLBA2012031601Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK EXTENDING FROM THE 2 O'CLOCK POSITION ON THE AFT HORIZONTAL STAB SPAR CENTER WEB, .281" IN LENGTH. REPAIRED IAW FR-EO-02386. MAJOR REPAIRMar 15, 2012 · N211GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR 29GA2012030995132Pressure Switch · brokenFLIGHT: 3981 TPA/PNS PILOT REPORTED LANDING GEAR CONTROL 2 AMP BREAKER POPPED IN FLIGHT. REPLACED POWER PACK PRESSURE SWITCH. LANDING GEAR OPERATIONAL CHECK GOOD.Mar 8, 2012 · N87551 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 29GA2012030994632Bracket · looseFLIGHT: 4037 BIM/FLL PILOT REPORTED AFTER EXTENDING GEAR ON FINAL HEARD REPETITIVE VIBRATING/BANGING NOISE COMING FROM NOSE WHEEL AREA. RE-SECURED BRACKET FOR ANTISKID COVER IN NOSE WHEEL WELL. LANDING GEAR OPERATIONAL CHECK NORMAL.Mar 8, 2012 · N81546 · Beech 1900D · Brake Anti-Skid SectionSDR GLBA2012030901Rib · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT THE LT CENTER WING L/E INBD RIB AND REINFORCEMENT STRAP 1.5" FWD OF SPAR, 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-57-002. MAJOR REPAIR.Mar 8, 2012 · N231YV · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2012030500011Spar · cracked"SUP" - MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP FOUND A CRACK AT IN THE CENTER WEB OF THE REAR SPAR OF HORZ STAB, CRACK RADIATES FROM THE UPPER RT OF THE LIGHTNING HOLE UPWARD AND OB, .375" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIREMar 5, 2012 · N220GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012030502Structure · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT THE LIGHTNING HOLE EXTENDING BACK AND TO THE LT, AT LT SIDE VERTICAL STAB AT 39.5 PERCENT CHORD AND CSS 69.184, 1.375" IN LENGTH. REPAIRED IAW EO 12-1900-55-006. MAJOR REPAIRMar 5, 2012 · N122UX · Beech 1900D · Vertical StabilizerSDR GLBA2012030501Skin · dentedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION FOUND A DENT IN THE LT WING L/E AT WS 236 MEASURING 4.2" LONG AND 1.5" DEEP.Mar 5, 2012 · N220GL · Beech 1900D · Wing, Plate/SkinSDR CA120309003Switch · out of adjust(CAN) THROUGH APPROX. 14000, 3.5 DIFF "CABIN DOOR ILLUMINATED". THEN ON APPROACH CABIN DOOR LIGHT EXTINGUISHED, APPROXIMATELY 0.5 DIFF. SYS INVESTIGATED AND ADJUSTED CABIN UPPER DOOR SWITCH. SYS FUNCTION TESTED, ALL PROVED SATISFACTORY.Mar 1, 2012 · Beech 1900D · Door Warning SystemSDR GLBA2012030101Spar Cap · chafedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CHAFE ON THE LT WING FWD LOWER SPAR CAP AT BL 29.5, APPROX 1" BY .312" AT WIDEST POINT, .125" TO .187" DEEP AT DEEPEST POINT. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONSMar 1, 2012 · N231YV · Beech 1900D · Wing SparSDR GLBA2012022901Trim Panel · dislodgedPILOT REPORTED THAT THE MAIN DOOR GETS STUCK CLOSED DUE TO A LOOSE PIECE OF PLASTIC TRIM. MX RESECURED MAIN DOOR TRIM PANEL, TRIM PIECE TIGHTENED, OPS CK GOOD.Feb 28, 2012 · N251GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2012022801Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE HORIZONTAL FWD SPAR WEB JUST INBD OF RT HSS 00.0, APPROX .5" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTION IAW EO 12-1900-55-004. MAJOR REPAIR.Feb 28, 2012 · N184UX · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012022401Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE HORIZONTAL STAB FWD SPAR WEB JUST INBD OF RT HSS 5.000 OTBD UPPER CORNER. REPAIRED IAW EO 12-1900-55-003. MAJOR REPAIR.Feb 24, 2012 · N245GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR 29GA2012022293671Mount · crackedDURING MAGNETIC PARTICLE INSPECTION, DISCOVERED ENGINE TRUSS MOUNT WELD AREA CRACKED AND TRUSS TUBE CHAFED. PERFORMED WELD REPAIR TO ENGINE MOUNT ATTACH POINTS WELD AREAS AND ENGINE TRUSS TUBE IN ACCORDANCE WITH FAA APPROVED DATA.Feb 22, 2012 · N81536 · Beech 1900D · Engine Mount SectionSDR GLBA2012022102Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND 4 CRACKS ON THE HORIZONTAL STAB REAR SPAR WEB AROUND ACCESS HOLE AT HSS. 00.0. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-55-002. MATERIALS UTILIZED ARE INCLUDED IN THE EOFeb 21, 2012 · N261GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR 29GA94621022012AUnknown · odorPILOT REPORTED STRONG BURNING RUBBER ODOR IN FLIGHT, WENT AWAY WITH RIGHT BLEED AIR INSTRUMENT AND ENVIRONMENTAL OFF. PERFORMED VISUAL INSPECTION OF LEFT AND RIGHT BLEED AIR SYSTEMS AND PERFORMED OPERATIONAL CHECK OF BLEED AIR SYSTEMS. OPS CHECKED GOOD, NO DFeb 20, 2012 · N81546 · Beech 1900D · Air Distribution SystemSDR GLBA2012022002Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT A SCREW HOLE ON THE AFT PRESSURE BULKHEAD, BEHIND AFT WALL AT 1 O`CLOCK POSITION, 1" IN LENGTH. REPAIRED IAW EO 12-1900-53-012. MAJOR REPAIRFeb 20, 2012 · N245GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2012022001Stringer · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS AT STRINGER 10L AND FS 165.4 AND WS 236 FROM A SCREW HOLE, EA CRACK .375 EACH. REPAIRED IAW EO 12-1900-55-001. MAJOR REPAIRFeb 20, 2012 · N245GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2012022101Warning Light · false activationPILOT REPORTED THAT THE GEAR INTRANSIT LIGHT ILLUMINATED IN FLIGHT, RAN CHECKLIST, GEAR OPERATED NORMALLY TO THE EXTENDED POSITION, EMERGENCY DECLARED, LANDED SAFELY. MX COULD NOT DUPLICATE, REPLACED THE NLG UPLOCK SWITCH IAW TC 1900-3260.00, OPS CHECKED GOODFeb 18, 2012 · N210GL · Beech 1900D · Landing Gear Position and Warning
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