JASC 5344
Service difficulty reports · 2,431
Reports filed under 5344 · Fuselage, Door Hinge, newest first.
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 jasc_code = '5344' 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.
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 jasc_code = '5344' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2009FA0000498Hinge · debondedUPON PRE-FLIGHT, PILOT FOUND FWD HINGE OF LT REAR DOOR ASSY TO BE CRACKED OR DEBONDED WHERE HINGE ENTERS THE DOOR ASSY. DOOR REMOVED FOR REPAIR BY MFG. (K)SDR ASAA0945603Hinge Fitting · crackedFWD ENTRY DOOR UPPER FUSELAGE HINGE FITTING CRACKED. REMOVED AND REPLACED UPPER HINGE FITTING ON FWD ENTRY DOOR.SDR SWAA092922Hinge Fitting · crackedDURING SCHEDULED 20Y CHECK, FOUND R1 DOOR UPPER HINGE CUTOUT CASTING CRACKED. REMOVED AND REPLACED HINGE CASTING PER SRM.SDR USAA20090429EM024Hinge · looseCLT - THE COCKPIT DOOR CAME OFF THE HINGES WHEN THE DOOR WAS OPENED. MAINTENANCE REMOVED AND REPLACED THE COCKPIT DOOR UPPER HINGE AND PERFORMED ADJUSTMENTS OF THE COCKPIT DOOR.SDR FDEA200903301737Hinge Fitting · corrodedAFT CARGO DOOR HINGE FITTING WAS FOUND WITH CORROSION AT FRAME 63. THE FITTING WAS REPAIRED AS PER EA 6-5310-129288.SDR FDEA200903301736Hinge Fitting · corrodedAFT CARGO DOOR HINGE FITTING WAS FOUND WITH CORROSION AT FRAME 62. THE FITTING WAS REPAIRED AS PER FEDEX EA 6-5310-129288.SDR FDEA200903271077Hinge · chafedFOUND ON RT CENTER HINGE FLANGE FOR MLG DOOR CHAFING MARKS OUT OF SRM LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 2009FA0000165Hinge · corrodedREPORTED TO MFG DURING SUPPLEMENTAL INSPECTION FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUPPLEMENTAL INSPECTION NR 52-10-01 CABIN DOOR RETENTION FOUND HARDWARE UNABLE TO REMOVE FROM UPPER CABIN DOOR DUE TO CORROSION. DRILLED OFF UPPER AND LOWER CASDR 2009FA0000164Hinge · corrodedPREVIOUSLY REPORTED TO MFG DURING SUPPLEMENTAL INSPECTION FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUPPLEMENTAL INSPECTION NR 52-10-01 CABIN DOOR RETENTION FOUND HARDWARE UNABLE TO REMOVE FROM UPPER CABIN DOOR DUE TO CORROSION. DRILLED OFF UPPER ASDR 2009FA0000163Hinge · corrodedPREVIOUSLY REPORTED TO MFG DURING SUPPLEMENTAL INSPECTION FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUPPLEMENTAL INSPECTION NR 52-10-01 CABIN DOOR RETENTION FOUND HARDWARE UNABLE TO REMOVE FROM UPPER CABIN DOOR DUE TO CORROSION. DRILLED OFF UPPER ASDR ASAA0944717Hinge Fitting · damagedL1 DOOR LWR HINGE CUTOUT BEARING PLATE FITTING TO HAVE ELONGATED HOLE. REMOVED EXISTING HINGE FITTING AND INSTALLED NEW LOWER L1 DOOR HINGE FITTING IAW B737 400 SRM 51 40 02.SDR FDEA200902190587Hinge · crackedEXTERIOR FUSELAGE MCD AFT HINGE AFT END HAS LARGE CRACK TO ATTACH SCREW HOLE, FROM LOBE. REPLACED HINGE SEGMENT IAW SRM 51-30-5, 51-30-2 & IAW DWG 52FX1433 REV E & INSTALLED NEW HINGE PIN IAW SRM 51-30-2 & DRAWING 52FX1433 REV E. OPS CHECK GOOD IAW MM 52-34-0SDR ASAA0944546Hinge Fitting · crackedL1 DOOR UPPER HINGE FITTING CRACKED. REMOVED CRACKED FITTING INSTALLED NEW HINGE FITTING B737 400 SRM 51 40 02.SDR ASAA0944687Hinge Fitting · damagedL1 DOOR LWR HINGE CUTOUT BEARING PLATE FITTING HAS ELONGATED HOLE. REMOVED EXISTING HINGE FITTING AND INSTALLED NEW LOWER L1 DOOR HINGE FITTING IAW B737 400 SRM 51 40 02.SDR SWAA090976Hinge Fitting · crackedDURING SCHEDULED 14Y CHECK, FOUND L1 DOOR UPPER HINGE FITTING CRACKED AT BS 304. REMOVED AND REPLACED FITTING PER SWA EA.SDR WRLA2009041Hinge Bracket · brokenDURING C-CHECK IN TPE INSPECTION FOUND LT O/B FLAP INBOARD FORWARD HINGE BRACKET BROKEN. REPLACED WITH NEW BRACKET IAW SRM VOL 2 51-31-01 REV 40.SDR CA090210008Hinge · looseON FEBRUARY 8, 2009 LEAVING TORONTO THE AIRCRAFT FAILED TO PRESSURIZE AFTER TAKEOFF THEN RETURNED TO GATE. MAINTENANCE ACTION CONFIRMED THE L1 ENTRY DOOR GUIDE ARM JAM NUT WAS LOOSE CAUSING THE DOOR TO MIGRATE OUT OF RIG. THE GUIDE ARM WAS RE-ADJUSTED. WESTSDR C8GA20090053Hinge · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE MAIN CARGO DOOR AFT HINGE SEGMENT IS CRACKED SEVERAL PLACES BS 680. REMOVED AFT HINGE SEGMENT, INSTALLED NEW HINGE. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.SDR C8GA20090034Hinge · misrepairedWHILE IN HEAVY MAINTENANCE PERFORMING DTA EVALUATION IT WAS NOTED THAT THE L1 DOOR LOWER HINGE REPAIR FASTENERS DID NOT COMPLY WITH SB 727-53A0198. FASTENERS WERE REMOVED, HOLES NDT AND OVER SIZED. INSTALLED NEW FASTENERS IAW 727-53A0198. NO OTHER DEFECTS WSDR FDEA200902030436Hinge · crackedMCD AFT HINGE LAST LUG CRACKED FROM EDGE TO FASTENER HOLE. REMOVED MCD AFT UPPER HINGE IAW FX DWG 52FX1433 REV E AND B727 SRM 51-30-2. LOCATED SHAPED AND DRILLED NEW HINGES SEGMENT 48 INCH BY 4 INCH IAW B727 SRM 51-30-5. TREATED AND PRIMED NEW PART IAW B7SDR SWAA090379Casting · crackedDURING SCHEDULED 16Y CHECK, FOUND L1 DOOR LOWER HINGE CASTING CRACKED. REMOVED AND REPLACED HINGE CASTING PER SRM.SDR FDEA200901150210Hinge · shearedFWD MAIN CARGO DOOR MAIN HINGE, 2ND FROM THE AFT, HINGE HAS 6 ATTACHMENT BOLTS SHEARED. REMOVED AND REPLACED HINGE HASP IN REF TO AMM SUPPLEMENT 52-36-12; PG 401.SDR ASAA0944180Hinge Fitting · crackedFORWARD ENTRY DOOR UPPER HINGE FITTING CRACKED. R&R HINGE FITTING.SDR ASAA0944169Hinge Fitting · crackedFWD ENTRY DOOR UPPER HINGE FITTING CRACKED. R&R HINGE FITTING.SDR AALA2009012200016Hinge · wornMAIN LANDING GEAR DOOR STRUT HINGE WORN. REPLACED HINGE ON MAIN LANDING GEAR DOOR STRUT PER ESO 80029.SDR SWAA090072Hinge Fitting · crackedDURING SCHEDULED 16Y CHECK, FOUND FUSELAGE HINGE FITTING CRACKED AT L1 DOOR UPPER HINGE CUTOUT. R&R FITTING PER BAC DWG.SDR ASAA0944166Hinge Fitting · crackedL1 DOOR UPPER HINGE CUTOUT FASTENER HOLE HAS CRACK INDICATION IN THE FITTING AT BS 304 WL 259. R&R L1 DOOR UPPER HINGE FITTING AT BS 304 WL 259.SDR FDEA200812245276Hinge · crackedEXTERIOR FUSELAGE AFT SEGMENT OF MCD HINGE, FUE SIDE, HAS A LOBE CRACKED STA. 680-720 REMOVED AFT SECTION MAIN CARGO DOOR HINGE IAW SRM 51-30-2. FABRICATED NEW HINGE IAW SRM 51-30-5 AND 51-10-1. TREATED AND PRIMED NEW HINGE IAW SRM 51-10-2. INSTALLED NEW MSDR 2009FA0000161Hinge · corrodedPREVIOUSLY REPORTED TO MFG DURING SUPPLEMENTAL INSP FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUPPLEMENTAL INSPECTION NR 52-10-01 CABIN DOOR RETENTION FOUND HARDWARE UNABLE TO REMOVE FROM UPPER CABIN DOOR DUE TO CORROSION. DRILLED OFF UPPER AND LOWSDR M7KA1109084125Hinge · crackedHINGE ATTACHMENT BORE HAD A 1` LONG CRACK RADIATING.SDR ASAA0873946Hinge · crackedAFT ENTRY DOOR LOWER HINGE PANEL CRACKED. REMOVED AND REPLACED HINGE PANEL.SDR SWIA200820212Hinge · wornFLT 5884 - MAIN CABIN DOOR UNUSUALLY DIFFICULT TO CLOSE, HINGE WORN. REPLACED DOOR HINGE.SDR AALA200802646Support · crackedCRACK FOUND ON LEFT NOSE LANDING GEAR DOOR FORWARD HINGE SUPPORT ARM. CRACK LENGTH IS .025 INCH. REPLACED SUPPORT ARM AND DOOR RIGGED IN ACCORDANCE WITH MM 32 22 01 2.SDR 2008FA0000598Hinge · brokenTHE REAR CABIN DOOR AFT HINGE HAS BROKE AS DECRIBED IN AC 43-16A ALERT 360. PROBABLE CAUSE IS REAR HOLD-OPEN CYLINDER.SDR 2009FA0000162Hinge · corrodedPREVIOUSLY REPORTED DURING SUPPLEMENTAL INSPECTION FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUPPLEMENTAL INSPECTION NR 52-10-01 CABIN DOOR RETENTION FOUND HARDWARE UNABLE TO REMOVE FROM UPPER CABIN DOOR DUE TO CORROSION. DRILLED OFF UPPER AND LOWESDR M7KA0706084131Hinge · crackedDURING ROUTINE INSPECTION CRACKS ON THE HINGE SURFACE RADIATE FROM MOUNTING BORES. THIS IS A VERY COMMON FAILURE FOR THIS PART. SUGGEST PART BE MANUFACTURED FROM A MORE DURABLE MATERIAL SUCH AS STAINLESS STEEL OR TITANIUM. (K)SDR M7KA0702084313Hinge · crackedDURING ROUTINE INSPECTION CRACKS ON THE HINGE SURFACE RADIATE FROM MOUNTING BORES. THIS IS A VERY COMMON FAILURE FOR THIS PART. SUGGEST PART BE MANUFACTURED FROM A MORE DURABLE MATERIAL SUCH AS STAINLESS STEEL OR TITANIUM. (K)SDR USAA920081364Hinge · crackedCLT-C11-MAJOR REPAIR LOG 5030342- CRACK AT LOWER HINGE OF FORWARD SERVICE DOOR BS296. REPAIRED HINGE OF FORWARD SERVICE DOOR BS296 IAW US AIRWAYS EA 100568 (B)SDR 2008UALA03693Hinge · crackedL2 DOOR HAS A CRACK AT UPPER HINGE ARM CUTOUT. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. ACCOMPLISHED HFEC OF CUTOUT PER 757 NDT 6-51-00-19, AND FOUND A CRACK APPROXIMATELY .3750 INCH LONG. REMOVED DAMAGE AND ACP'D INSURANCE CUT, LOCATED, DRILLED AND INSTALLSDR 2008FA0000468Hinge · cracked(2) OF THE HINGE LINKS HAD CRACKED OFF ON ONE END. UPON DISASSEMBLY IT WAS DETERMINED THAT A CRACK HAD FORMED LENGTHWISE BETWEEN THE FASTENERS AND THE HINGE LINKS. POSSIBLE CAUSE MAY HAVE BEEN FATIGUE. (K)SDR 08FDEA02465Hinge · crackedGROUND POWER ACCESS PANEL. TOP HINGE BRACKET CRACKED REMOVED DAMAGED PART PER REF SRM 51-30-02 PG 1-3, FABRICATED NEW PART PER REF DWG NR 66-16849-7. TREATED AND PRIMED NEW PART PER REF SRM 51-10-02. INSTALLED NEW PART PER REF SRM 51-30-02 PG 1-3. THIS IS SDR 08FDEA02464Hinge · crackedGROUND POWER ACCESS PANEL. TOP HINGE BRACKET CRACKED REMOVED DAMAGED PART PER REF SRM 51-30-02 PG 1-3, FABRICATED NEW PART PER REF DWG NR 66-16849-7, TREATED AND PRIMED NEW PART PER REF SRM 51-10-02. INSTALLED NEW PART PER REF SRM 51-30-02 PG 1-3. THIS IS CSDR C8G2008F00004Hinge · damagedDURING CLIMB OPERATION THE FWD ENTRY DOOR EICAS MESSAGE APPEARED WITH THE ASSOCIATED OVERHEAD LIGHT. THE AC RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE FWD ENTRY DOOR WAS NOT CENTERED IN THE DOOR FRAME WHESDR 2008FA0000420Hinge · crackedFOUND CRACKS IN AFT DOOR HINGE. (K)SDR ASAA0843036Hinge · wornFA REPORTS L1 IS DIFFICULT TO MOVE OPEN AND CLOSED OPERATED L 1 DOOR AND HEARD AND FELT GRINDING POPPING EMANATING FROM UPPER END OF FUSE TORQUE TUBE INITIATED MIG 2C 224114. WITH FURTHER TROUBLESHOOTING REMOVED L1 DOOR CAM PLATE AND FOUND WORM AREA ON PLATE.SDR DHL2008F00025Hinge · crackedMAIN CARGO DOOR AFT HINGE SECTION IS CRACKED AT FUSELAGE SIDE BS 650. REMOVED AFT HINGE SECTION AT MAIN CARGO DOOR SIDE BS 650 AND INSTALLED NEW SECTION WITH MS 20001+16-7200 AND PO 9002527 DIMENSION 17 IAW BOEING 727-200 FREIGHTER MAINTENANCE MANUAL FIGURE 5SDR 2008UALA03011Hinge Fitting · crackedCRACK AT FWD UPPER L-1 DOOR CUTOUT AREA, INNER UPPER DOOR HINGE FITTING AT BS 337 AND STR 12L. REMOVED DAMAGED AREA REF R EO G-12344-3 AND SRM 51-20-01. THIS IS A TIME LIMITED REPAIR. FITTING P/N 141N8378-2 MUST BE REPLACED AT NEXT CK, NO LATER THAN 05-16-2SDR M7K2008F00005Hinge · cracked(REF 0429084134) DURING ROUTINE INSPECTION, HINGE WAS FOUND CRACKED THROUGH TO SCREW MOUNTING BORES TO THE METALS EDGE. THIS IS A VERY COMMON FAILURE FOR THIS PART. SUGGEST PART BE MFG OF MORE DURABLE MATERIAL SUCH AS STAINLESS STEEL. (K)SDR M7K2008F00004Hinge · crackedDURING ROUTINE INSPECTION, HINGE WAS FOUND CRACKED THROUGH A SCREW MOUNTING BORE TO THE METALS EDGE. THIS IS A VERY COMMON FAILURE FOR THIS PART. (K)SDR DHL2008760531Hinge · crackedREMOVED AND REPLACED CRACKED AFT HINGE SECTION, BS 620 TO 640, FOR MCD PER B727-200 FREIGHTER MM FIG 5201B AND CH 52 REV G, STOCK HINGE P/N MS20001-16-7200
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