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.

SDR 08FDEA01570Cover · damagedR-1 DOOR INTERIOR HINGE MECHANISM COVER IS DAMAGED. REMOVED DAMAGE; CLEANED & PREPPED FOR WET LAY UP. LAYED UP REPAIR PLIES & STARTED CURE, COMPLETED CURE & LIGHTLY SANDED, CLEANED & PREPPED FOR FINISH COAT; APPLIED FINISH COAT IAW SRM 51-77-10 & 51-77-11.Apr 25, 2008 · N661FE · Airbus A300F4605RSDR QXEA200800425Hinge Fitting · corrodedPDX C4 CHECK - MCD LAY SHAFT, AFT HINGE FITTING HAS PITTING AROUND BOLT HOLES. REMOVED MCD LAY SHAFT. SEPARATED LAYSHAFT AND DRILLED OUT AFT HINGE FITTING. DRILLED UP AND INSTALL NEW HINGE FITTING REF SRM 51-40-00. INSTALLED MCD LAY SHAFT.Apr 18, 2008 · N355PH · Dhav DHC8202SDR SWAA082053Hinge Fitting · crackedDURING SCHEDULED HC1 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE FITTING CRACKED. REMOVED AND REPLACED HINGE FITTING PER SRM.Apr 17, 2008 · N605SW · Boeing 7373H4SDR SWAA082054Hinge Fitting · crackedDURING SCHEDULED HC1 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE FITTING CRACKED. REMOVED AND REPLACED HINGE FITTING PER SRM.Apr 17, 2008 · N605SW · Boeing 7373H4SDR A6WA200840342Hinge · crackedCARGO DOOR STEP PLATE ONE HINGE CRACKED (FWD). CARGO DOOR STEP PLATE ONE HINGE (FWD) REPLACED IAW SRM 51-42-06. .Apr 16, 2008 · N443AW · Cndair CL6002B19SDR A6WA200840311Hinge · crackedPAX DOOR UPPER FOLDING STEP BOTTOM HINGE FOUND CRACKED FOUND NEAR FWD END. - - PAX DOOR FLODING STEP BOTTEM HINGE REPLACED IAW SRM 51-41-02. .(A)Apr 7, 2008 · N403AW · Cndair CL6002B19SDR A6WA200840291Hinge · crackedFOUND CARGO DOOR STEP PLATE HINGE CRACKED. REPLACED CARGO DOOR STEP PLATE HINGERS IAW SRM 51-42-06. .Apr 3, 2008 · N403AW · Cndair CL6002B19SDR M7K2008F00091Hinge · crackedDURING ROUTINE INSPECTION, A CRACK WAS FOUND IN THE HINGE MOUNTING FLANGE RADIATING FROM THE OUTERMOST LT ATTACHMENT SCREW BORE. REMOVAL OF ATTACHMENT SCREW REVEALED THE FLANGE CORNER HAD SEPARATED FROM THE REST OF THE HINGE. (K)Mar 24, 2008 · N822MH · Urocop EC130B4SDR M7K2008F00090Hinge · crackedDURING ROUTINE INSPECTION A CRACK WAS FOUND IN THE HINGE MOUNTING FLANGE RADIATING FROM THE OUTERMOST LT ATTACHMENT SCREW BORE. REMOVAL OF ATTACHMENT SCREW REVEALED THE FLANGE CORNER HAD SEPARATED FROM THE REST OF THE HINGE. THIS IS A VERY COMMON FAILURE FORMar 24, 2008 · N821MH · Urocop EC130B4SDR M7K2008F00054Hinge · crackedDURING ROUTINE INSPECTION A CRACK WAS FOUND IN THE HINGE MOUNTING FLANGE RADIATING FROM THE OUTERMOST LT ATTACHMENT SCREW BORE. THIS IS A VERY COMMON FAILURE FOR THIS PART. (K)Mar 24, 2008 · N817MH · Urocop EC130B4SDR YOL2008F00000Hinge · crackedAC CURRENTLY IN FOR INSPECTION. CABIN DOOR WAS FOUND TO HAVE CRACKED HINGE. OUR OFFICE IS AWAITING FURTHER INFORMATION AT THIS TIME. (K)Mar 24, 2008 · N604BB · Cndair CL6002B16SDR 08FDEA01096Hinge · wornFWD CARGO DOOR CONTROL PANEL DOOR HINGE HAS EXCESSIVE PLAY. REMOVED FWD CARGO DOOR CONTROL PANEL DOOR TO FOM PER DC/MD-10 SRM 53-31-01; VOL II. RECEIVED NEW HINGE P/N 2999325N, AND P/N ADA 3469-7, PO 544680.1. ALODINED HINGE PER SRM 51-21-01; PARA 31; VOL IMar 21, 2008 · N365FE · Doug MD1010FSDR 08FDEA01047Hinge · wornLOWER FWD CARGO DOOR FWD HINGE SEGMENT LOBES ARE WORN BEYOND LIMITS PER FEDEX WORK CARD 52X3502. MACHINED 3 EACH REPAIR BUSHINGS IAW SRM 52-10-00 PG 23 VOL I. INSTALLED BUSHINGS IAW SRM 51-39-01 VOL II PG 3. MINOR REPAIR.Mar 19, 2008 · N384FE · Doug MD1010FSDR GTIA0800040Bearing · displacedL1 DOOR UPPER HINGE BEARING IS DISPLACED FROM ITS BORE. REPLACED UPPER AND LOWER L1 DOOR HINGE FITTINGS IAW AMM 52-11-00.Mar 17, 2008 · N502NK · Airbus A319132SDR DHL2008763511Hinge · crackedMCD AFT HINGE SEGMENT AFT LOBE CRACKED. REMOVED AND REPLACED HINGE SEGMENT WITH MS 20001-16-7200 MATERIAL PO NR 9002527 PER AEI B727-200 FREIGHTER MM CH 52 FIG 5201A AND SRM 51-30-5.Mar 16, 2008 · N763AT · Boeing 727264SDR ZESA030808001Hinge · crackedPOST FLIGHT, PILOTS COULD NOT CLOSE AND LATCH MAIN CABIN DOOR. FOUND CABIN DOOR HINGE CRACKED THROUGH ON LOWER ARM.Mar 8, 2008 · N400LX · Cessna 560CESSNASDR 08FDEA00692Hinge · corrodedAFT CARGO DOOR, INTERIOR SIDE OF THE HINGE IS RUSTED. AFTER REMOVING THE CORROSION FOUND HINGE P/N AFA3953-525 OUT OF LIMITS IAW SRM 52-10-00 FIG 8 VOL I. REMOVED (TO GAIN ACCESS TO REMOVE THE HINGE) AND REINSTALLED FASTENERS ON PARTIAL INTERNAL SKIN, GUARMar 4, 2008 · N384FE · Doug MD1010FSDR M7K2008F00117Hinge · crackedDURING ROUTINE 100 HR INSPECTION A CRACK WAS FOUND RADIATING HORIZONTALLY FROM THE SECOND HOLE FROM THE ONE END AND ACROSS THE CORNER OF THE FIRST HOLE ON THE OPPOSITE HINGE END WITH A TOTAL SEPARATION OF THE HINGE CORNER METAL. (K)Mar 3, 2008 · N818MH · Urocop EC130B4SDR HALA0800348Hinge · damagedCONTACT DAMAGE ON MED DOOR HINGE, FROM FUSELAGE FRAME.//REPAIR IN WORK.Feb 21, 2008 · N479HA · Boeing 717200SDR A6WA200840116Hinge · crackedCARGO STOW PLATE, FWD, MID AND AFT HINGES ARE CRACKED. CARGO STOW PLATE REPLACED IAW SRM 51-42-06. (M)Feb 16, 2008 · N430AW · Cndair CL6002B19SDR M7K2008F00002Hinge · crackedDURING ROUTINE 100 HOUR INSP, A CRACK IN THE HINGE OF THE ENGINE FAIRING WAS FOUND RADIATING FROM THE 2ND HOLE FROM ONE END OF THE HINGE WITH THE CORNER HAVING SEPARATED FROM THE HINGE FROM CRACKS EMANATING FROM THE 1ST HOLE. THIS IS A COMMON FAILURE FOR THISFeb 4, 2008 · N817MH · Urocop EC130B4SDR DHL2008749010Hinge · gougedMAIN CARGO DOOR UPPER AFT MOST HINGE IS GOUGED IN CENTER OF HINGE BS 640. REMOVED DAMAGE IAW AEI MM CHAPTER 52. LOCATED AND DRILLED IAW AEI MM CHAPTER 52 FIG 5201B AND SRM 51-30-5. PARTS AND AREA TREATED AND PRIMED IAW SRM 51-10-2 FIGURE 1. INSTALLED IAW MMJan 31, 2008 · N749DH · Boeing 7272J0SDR DHL2008765021Hinge · crackedDURING C CHECK, MCD AFT HINGE SECTION IS CRACKED AT BS 612 STRINGER 4L. REMOVED AFT HINGE SECTION AT MAIN CARGO DOOR BS 612 STRINGER 4L IAW MM FIG 5201B REV E. FABRICATED HINGE SECTION IAW MM FIG 5201B REV E. TREATED AND PRIMED PARTS AND AREA IAW SRM 51-10Jan 20, 2008 · N765AT · Boeing 727264SDR 08FDEA00175Hinge · damagedMAIN CARGO DOOR HINGE SEGMENT DAMAGED FOWARD OF DOOR ACTUATOR. ACCOMPLISHED INTERIM REPAIR PER EA 6-5230-116948, PART 1. INSTALLED A STRAP IN PLACE OF HINGE NR 2 - 22 WITH BOLTS. MAIN CARGO DOOR AND ALL HINGES TO BE REPLACED AT A LATER DATE PER PART 2 OF Jan 16, 2008 · N403FE · Airbus A310203SDR FDKA200801025Bushing · damagedFDM FLT 6206 FLL (0907 PHX LCL) MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. MX REMOVED AND REPLACED DOOR HINGE BUSHING AND BOLT, OPS CHECK GOOD.Jan 14, 2008 · N851MJ · Emb EMB145LRSDR UPS08851442Hinge · crackedINSPECTION TYPE:C2 D-PIT DOOR FWD DOOR LINK HINGE WEB CRACKED IN DOUBLER. REMOVED, FABRICATED, AND INSTALLED REPAIR DOUBLER ON D-PIT DOOR FWD LINK HINGE WEB IAW SRM 51-1-21, AND SRM 51-02-00-0, AND DWG 5616673.Dec 30, 2007 · N718UP · Doug DC871FSDR DHL2007793006Hinge · crackedMAIN CARGO DOOR AFT HINGE APPEARS TO BE CRACKED, BS 640 STRINGER 4L. HFEC VERIFIED CRACK IAW B-727 NDTM PT 6-51-00-00 FIGURE 23. REMOVED AT MAIN CARGO DOOR AFT HINGE BS 640 STRINGER 4L AS REQUIRED IAW AEI BOEING 727-200 FREIGHTER M/M FIGURE 5201B REV G. FABDec 8, 2007 · N793DH · Boeing 727247SDR A6WA200740674Hinge · crackedPAX DOOR UPPER FOLDING STEP, LOWER HINGE IS CRACKED. PAX DOOR UPPER FOLDING STEP, LOWER HINGE REPLACED IAW SRM 51-41-00. (K)Dec 6, 2007 · N433AW · Cndair CL6002B19SDR CA071212005Hinge Pin · corroded(CAN) DOOR HINGE PINS APPEAR TO BE WELDING RODS OR STEEL PINS CUT LONG AND BENT OVER TO SERVE FROM FALLING OUT. REPLACED WITH PROPER PARTS. CAUSED DISSIMILAR METAL CORROSION TO HINGE MATERIAL AS BOGUS PINS RUSTED. THE ENTIRE FLEET HAS THESE SAME BOGUS PINS (1Nov 27, 2007 · Cessna 172SSDR DHL2007742042Hinge · crackedMCD AFT HINGE ON FUSELAGE SIDE HAS AFT LOBE CRACKED. REMOVED DAMAGED SECTION OF MCD HINGE AEI CH 52 REV G FIGURE 5201 B/A. LOCATED AND DRILLED NEW SECTION OF MCD HINGE APPROXIMATE DIMENSION 18" BY 1.75" P/N 14520001-16-7200 PO NR 724546 IAW AEI B-727 MM CH 5Nov 26, 2007 · N742DH · Boeing 727225SDR CA071128010Bulkhead · cracked(CAN) WHILE CARRYING OUT THE SEB 97-1 AFT DOORPOST INSPECTION, CRACKS WERE NOTED AT THE SUBJECT AREAS ON BOTH DOORPOSTS (IPC "CHANNEL-BULKHEAD"). SUBMITTER SUSPECTS THAT TAXIING OVER ROUGH SURFACES, OR POSSIBLY HARD OR CRABBED LANDINGS, CONTRIBUTES TO THE FLEXNov 16, 2007 · Cessna 172MSDR USAA920071149Hinge Fitting · wornSAL - MAJOR REPAIR - BC6 CHECK - R2 DOOR LOWER HINGE FITTING WORN ALLOWING THE BEARING TO MIGRATE. REPLACED THE R2 DOOR LOWER HINGE FITTING, BEAM 2-3 IAW A320 SRM 51-72-11.Nov 8, 2007 · N657AW · Airbus A320232SDR TRAX200701569Hinge · brokenFITTING HINGE (AFT) BROKEN ON RT EMERGENCY EXIT (RESOLVED ON W/O: 71093 TASKCARD: N/R-00253 ), FITTING HINGE ON RT EMERGENCY EXIT REPLACED AND INSTALLED IAW SRM 51-25-04. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIOct 22, 2007 · N643AS · Aerosp ATR72212SDR CA071214005Hinge Bracket · cracked(CAN) TOP HINGE BRACKET CRACKED ON FWD FACE OF HINGE. (TC NR 20071214005)Oct 4, 2007 · Dhav DHC2MKISDR M7K2008F00116Hinge · crackedCRACK’S DEVELOP IN HINGE 1ST SEGMENT OF LEADING EDGE DURING NORMAL OPERATIONS, REQUIRING REPAIR OR REPLACEMENT EVERY 100 HOURS. TYPICALLY AT MINIMUM A STOP DRILL IS REQUIRED. HINGE MATERIAL IS THIN ALUMINUM AND PERHAPS A CHANGE TO THICKER GAUGE OR ALTERNATE Sep 19, 2007 · N801MH · Urocop EC130B4SDR 07FDEA04044Hinge Fitting · corrodedNEW CORROSION ON OLD REPAIR, FOUND ON FWD PAX DOOR RT ON DOOR HINGE FITTING (LOWER ARM WEB - BOTTOM SIDE). CORROSION REMOVED (TOTAL OF 53 PERCENT REMOVED), FILLER AND OLD REPAIR DOUBLER INSTALLED IAW EA 6-5211-82884 AND RAS/AS/115/2005 ISSUE A.Sep 19, 2007 · N803FD · Airbus A310324SDR DHL2007746527Hinge · crackedEXTERNAL FUSELAGE BODY STATION 640 WL 299 MCD FUSELAGE SIDE AFT MOST HINGE SEGMENT AFT LOBE IS CRACKED. REMOVED AFT SECTION OF MCD HINGE IAW B727 SRM 51-30-2. FABRICATED NEW HINGE FROM MS20001-16-7200 PO NR 9002527 DIMENSION 17 7/8" BY 4 1/4" IAW AEI BOEING Aug 31, 2007 · N746DH · Boeing 727224SDR AALA20071413Hinge · inoperativeCABIN ALTITUDE CONTROL PROBLEM. OXYGEN MASKS AUTO DEPLOYED. DESCENDED TO 10000 FEET AND THE CABIN PRESSURE KEPT CLIMBING. REPLACED BROKEN DOOR HINGE FOR GROUND AIR CONDITIONING COVER. REPLACED BOTH SAFETY VALVES AND OUT FLOW VALVES. SYSTEM GROUND CHECKED NORAug 5, 2007 · N7082A · Airbus A300B4605RSDR DHL2007740512Hinge · crackedEXT FUSE MCD AFT MOST HINGE SEGMENT BS 650 IS CRACKED ON THE AFT LOBE. REMOVED HINGE SECTION IAW B727-200 AEI MM CHAP 52. FAB`D NEW HINGE SECTION FROM MS20001-16-7200 PO NR 9002527 DIM 17" LONG AN 11" LONG IAW B727 MM AEI CHAP 52 TREATED AN PRIMED AREA AN PAMay 14, 2007 · N740DH · Boeing 7272Q9SDR 07FDEA01256Hinge · damagedLOWER FWD CARGO DOOR DAMAGE FOUND ON DOOR HINGE FWD HINGE LOBE AND AFT HINGE LOBE OVALIZED AND OUT OF LIMIT (DIA. 0.355"). REPAIRED WITH BUSHING IAW SRM 52-10-00 FIG 8 VOL 1 AND CMM 52-31-03.Apr 3, 2007 · N554FE · Doug DC1010SDR 07FDEA00850Hinge · misinstalledRT MLG FITTING BUSH, WRONG INSTALLATION. REPAIR WAS PERFORMED IAW EA 6-5281-106381 AND RAS/CASA/5328/2007 ISSUE "A" AND RAS/AS/228/95 ISSUE "A".Mar 15, 2007 · N816FD · Airbus A310304SDR DHL2007786519Hinge · crackedEXT FUSELAGE MCD HINGE AFT SEGMENT AFT MOST LOBE IS CRACKED. REMOVED HINGE AT EXT FUSE MCD AFT SEGMENT IAW AEI B727 FREIGHTER CHAPTER 52 FIG 5201 A REVF. FABRICATED AFT SEGMENT, MATERIAL MS20001-16-7200 PO NR 9002527 DIM 18" IAW B727 FREIGHTER CHAPTER 52 FIGMar 13, 2007 · N786AT · Boeing 727214SDR 20582007TJ001Hinge · crackedDURING A DAILY INSPECTION OF THE AIRCRAFT A CRACK WAS FOUND ON THE UPPER LUG OF THE DOOR HINGE. DURING REPLACEMENT OF THE HINGE THE LUG COMPLETELY BROKE IN (2) PEICES.Mar 13, 2007 · N6763L · Cessna 550SDR CA070802003Hinge · cracked(CAN) ON INSPECTION THE LT DOOR WAS FOUND CRACKED ALONG THE FRONT HINGE. (TC NR 20070802003)Mar 12, 2007 · Beech B200SDR 2007UALA00545Hinge · crackedNR 2 RT MED UPPER HINGE CUTOUT IS CRACKED ON DOOR FRAME. [SUP 4-17-07] REPAIRED DOOR 2R PER A BOEING APPROVED REPAIR SCHEME. BOEING AND UA ENGINEERING STILL EVALUATING THE CAUSE OF FAILURE. INCORPORATED A PLAN OF INSTALLING A PREVENTIVE STEEL DOUBLER AT UPFeb 20, 2007 · N511UA · Boeing 757222SDR SWAA070776Stringer Clip · crackedDURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.Feb 13, 2007 · N664WN · Boeing 7373Y0SDR 07FDEA00344Hinge · corrodedCENTER CARGO DOOR HINGE ASSY FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10- 00 FIG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.040" REMAINING THK 0.300". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLFeb 6, 2007 · N529FE · Doug MD11SDR 07FDEA00343Hinge · corrodedCENTER CARGO DOOR HINGE AT FUSELAGE AREA FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10-00 FIG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.028" REMAINING THK 0.312". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02.Feb 6, 2007 · N529FE · Doug MD11SDR 07FDEA00341Hinge · corrodedAFT CARGO DOOR HINGE ASSY FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10- 00 FIG.14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.035" REMAINING THK 0.305". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLASSIFeb 6, 2007 · N529FE · Doug MD11SDR 07FDEA00340Hinge · corrodedFWD CARGO DOOR HINGE FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10- 00 FIG.14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.025" REMAINING THK 0.315". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLASSIFIED MAJOR Feb 6, 2007 · N529FE · Doug MD11
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