JASC 5343
Service difficulty reports · 1,946
Reports filed under 5343 · Fuselage, Landing Gear Attach Fittings, 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 = '5343' 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 = '5343' 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 IXXA10SMN47SFitting · corrodedDURING C-CHECK INSP FOUND LT MLG WHEEL WELL JOINT FITTING LOWER PART CORRODED AT STA 940.000 LONGERON 24 LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED SPLICES, DOUBLER AND SHIMS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. SDR IXXA10SMN048SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND LT MLG WHEEL WELL JOINT FITTING LOWER PART CRACKED AT STA 879.000 LONGERON 24 LT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING, SPLICES, DOUBLER, SHIMS. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW FITTING SDR FDEA201003160962Support · crackedCRACK RT FWD STIFFNER NLG TRUNNION SUPPORT. REPLACEMENT OF STIFFENER ACCOMPLISHED ON SNRM NR N00463, WORK ORDER NR 00047694.SDR FDEA201003160961Support · crackedCRACK RT AFT STIFFNER NOSE TRUNNION SUPPORT. NO WORK ACCOMPLISHED ON THIS WORK CARD. REPLACEMENT OF STIFFENER ACCOMPLISHED ON SNRM NR N00463, WORK ORDER NR 00047694, SDR TRACKING NR 10-0807.SDR DLM88100825Fitting · corrodedPITTING CORROSION ON LT GEAR SUPPORT FITTING BUSHING BORE. LT GEAR SUPPORT FITTING BUSHING BORE WAS MACHINED TO CLEAN UP CORROSION IAW ERA 480222-14AD REV ORIG. FINAL SIZE ID 2.535. FLOURESCENT DYE INSP PERFORMED IAW EA 09-093855-03 AD OPN 0104 PAR J NOTE ASDR UHLA2010022200029Beam · crackedMAJOR REPAIR - CRACK FOUND ON NLG I-BEAM ON FWD SIDE OF I-BEAM. REMOVED DAMAGED I-BEAM AND INSTALLED SERVICEABLE UNIT PER EMB IC2008-170/08207 AND SB 170-53-0055.SDR DALA1026241821Beam · crackedMLG LT, BEAM FOUND WITH CRACK IN WEB. BEAM REPAIRED IAW ERA 1-481136-14, REV ORG.SDR CA100119010Attach Fitting · cracked(CAN) DURING C-CHECK, 2 CRACKS FOUND IN LT MLG FWD WEB AT LOCATION OF MLG FWD FITTING GREASE NIPPLE CUT OUT AT FS 438.8.SDR DALA14003353118Hinge Fitting · corrodedLEFT MLG FWD HINGE FITTING CORRODED. REPAIRED IAW ERA 478979-14AD.SDR DALA100249884Support Fitting · corrodedDURING LINE CHECK FOUND CORROSION ON RT MLG SUPPORT FITTING. REPLACED FITTING IAW CMM 57-40-01 AND AMDS 3210-9904M-RT.SDR 2010FA0000099Trunnion · chafedRT MLG TRUNNION WAS FOUND CHAFED AND WORN BEYOND LIMIT BY CONTACT WITH MLG FAIRING PN 2641018-28. WEAR LIMIT IS ESTABLISHED IN CAB05-17 WHICH ADDRESSES THIS CONDITION IN EARLIER SN AIRPLANES BUT DOES NOT COVER THIS AIRPLANE MFG 6/5/08. CONDITION WAS NOT DETESDR WRLA20100105331Fitting · crackedDURING 01C CHECK FOUND NOSE GEAR TRUNNION LT FITTING P/N ACA7017-502 CRACKED.SDR FFKA147Retainer · loosePILOT REPORTED THAT AFTER LANDING THAT THE RT MLG COLLAPSED ON LANDING. AFTER INVESTIGATING IT WAS FOUND THAT PN 401-335 (AN4-40A) BOLT AND PN 67502-00 RETAINER ASSY HAD BACKED OUT OF THE TRUNNION ASSY (PN 96766-17). THIS CAUSED PN 67040-15 (FITTING ASSY- FWSDR SWAA098086Stringer Clip · crackedDURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10R. REMOVED AND REPLACED CLIP PER SI.SDR SWAA097961Trunnion · corrodedDURING SCHEDULED MV3 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.SDR SWAA097960Trunnion · corrodedDURING SCHEDULED MV3 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.SDR 2009F00123Trunnion · crackedCRACKS IN NLG TRUNNION BELOW ACTUATOR ATTACH POINT. PART WAS REPLACED ON ACFT AND SENT TO MFG FOR EVALUATION.SDR CA091125007Trunnion · corroded(CAN) FOUND CORROSION PITTING IN TRUNNION BORES ON BOTH SIDES OF NLG TRUNNION, WHICH HOUSE THE DRAG BRACE PINS. PITTING IS 0.030 INCHES DEEP LONGITUDINALLY IN END OF BORE AND 0.045 INCHES DEEP LATERALLY AT END OF BORE, AROUND THE BORE RADIUS FOR APPROXIMATELYSDR 2009FA0000964Bolt · undertorquedDURING SCHEDULED INSP, THE STARBOARD MLG FITTING ATTACH BOLTS WERE FOUND UNDER-TORQUED. UPON REMOVAL OF FITTING FOR HIDDEN DAMAGE INSP THE WING SPAR WEB AND THE MATING FACE OF THE GEAR FITTING SHOWED EVIDENCE OF FRETTING CORROSION AROUND MOUNTING HOLES. CORROSSDR WRLA20091023261AFitting · crackedCRACK - FITTING NLG TRUNNION FITTING, LT SIDE STA Y= 595 L= 2. IAW AMM 32-21-01-000-801 REV 65 RMV NOSE LANDING GEAR. REPAIRED CRACK AREA IAW MD11 SRM 53-10-14 REV 41 FIG 202 REPAIR 2. RE-INSTALLED NOSE LANDING GEAR ASSY REF EGAT NRC U05011.SDR FDEA200910053474Trunnion · crackedNLG WW, LT NLG TRUNNION FITTING FOUND CRACKED. REPAIRED AS PER SRM 53-10-14 FIGURE 202 REPAIR 2, REVISION 41. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, REVISION 108. INITIAL INSPECTION TO BE CARRIED OUT AT 1500 CYCLE AND REPETITIVE INSPECTION TO CARRY OUT SDR ABXR20091005033Trunnion · corrodedDURING A HEAVY MX INSP, THE NOSE LANDING GEAR DRAG BRACE/ACTUATOR TRUNNION FITTING HAD CORROSION UNDER THE BEARING SURFACE. THE NOSE LANDING GEAR DRAG BRACE/ACTUATOR TRUNNION FITTING WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.SDR CA091005013Bolt · corroded(CAN) DURING A SCHEDULED REBUILD OF THE LANDING GEAR, THE LT GEAR TRUNNION WAS REMOVED FROM THE ACFT. THE RETAINING BOLT HOLDING THE AFT PIN INTO THE TRUNNION WAS FOUND TO BE CORRODED AND TWISTED. BOLT IS MISSING MATERIAL FROM THE HEAD FOR ABOUT A 1/4 INCH DOSDR 2009FA0000799Trunnion · crackedFOUND NLG TRUNNION TO BE CRACKED AT 2 WELDS, 1 CRACK .2500" THE OTHER .0625". THESE CRACKS ARE IN THE AREA TO BE INSPECTED IAW AD 2005-13-16 AT 1000 HOUR INTERVALS. TIME SINCE LAST INSPECTION WAS 464.2. LARGER CRACK WAS FOUND BY SIMPLE VISUAL INSPECTION DURINGSDR WRLA20090917204Fitting · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON NLG TRUNNION SUPPORT FITTING, Y=582, X=24. CRACK LENGTH MEASURED 1 INCH. REPAIR THE NLG TRUNNION SUPPORT FITTING IAW MD-11 SRM 53-10-14 FIGURE 202, REPAIR 2, REV 41.SDR HYIA4652NRMLGTrunnion · shearedCREW REPORTED, RT MLG SHEERED OFF ON LANDING ROLL. MX FOUND RT MLG UPPER BARREL AND TRUNNION ASSY SHEARED JUST BELOW MLG ACTUATOR ATTACH POINT. MX REMOVED AND REPLACED RT MLG ASSY, RT PROPELLER, RT ENG, RT SIDE INBD AND OTBD FLAP PANEL ASSEMBIES, AND RT LANSDR 2009FA0000774Trunnion · crackedPERFORMING PIPER EVENT NR 2, NOSE LANDING GEAR TRUNNION FOUND UNSERVICEABLE. EIGHT INCH CRACK NOTED IN CASTING. CRACK STARTING IN UPPER STEERING BEARING BOSS AT THE FIVE O'CLOCK POSITION LOOKING DOWN AT CASTING. CRACK EXTENDS STRAIGHT DOWN THE REAR RIGHT SIDE SDR CA100216017Frame · cracked(CAN) DVI OF NLG BAY APPROX BS 328 FOUND RT TRUNNION SUPPORT FITTING A FRAME CRACKED ABOUT 3 INCHES LONG IN THE UPPER PORTION OF THE A FRAME. REPAIR WAS COMPLIED IAW SRM. (TC 20100216017)SDR ABXR200908240011Trunnion · corrodedDURING ROUTINE C-CK MX, THE LT TRUNNION FITTING WAS FOUND CORRODED OUTSIDE OF MM LIMITS INSIDE THE INNER BORE. THE LT AND RT TRUNNION FITTINGS WERE REMOVED AND REPLACED WITH NEW TRUNNIONS. NO OTHER DAMAGE OR CORROSION NOTED THE ITEM WAS RETURNED TO SERVICE.SDR CA090811006Bolt · shearedWHILE PERFORMING A GENERAL VISUAL INSP OF THE MAIN GEAR WELLS, FOUND SHEARED BOLT IN THE RT WHEEL WELL FWD BULKHEAD OTBD DOOR SUPPORT CASTING. BOLT WAS REPLACED AND RETURNED TO SERVICE.SDR ATJ2009F00000Trunnion · brokenLT MAIN LANDING GEAR WOULD NOT COME DOWN AND LOCIN IN FLIGHT. EMERGENCY PROCEDURES USED TO EXTEND GEAR. AFTER LANDING ACFT WAS MOVED BY GROUND PERSONELL AND LT GEAR COLLAPSED. FWD LT GEAR FITTING WAS FOUND TO BE PARTIALLY MISSING. SB HAD BEEN COMPLIED WITHSDR 2009FA0000613Mount · brokenUPON REMOVAL OF THE ENGINE FOR OVERHAUL, DISCOVERED THAT THE NOSE GEAR DRAG LINK ATTACH POINT WAS BROKEN. DISCOVERED THAT THE LWR RT ENGINE MOUNT MOUNTING BOLT WAS BENT. AFTER RESEARCHING THE LOG BOOKS, FOUND THAT SB 955 PATS I, II, AND III WHERE COMPLIED WISDR FDEA200906302417Trunnion · crackedNLG SUSPECT CRACKED RT TRUNNION FITTING. REPAIRED AS PER SRM 53-40-00 FIG 23 VOL 1 REV 40 (MAJOR CAT B REPAIR).SDR FDEA200906302416Trunnion · crackedNLG SUSPECT CRACKED ON LT TRUNNION FITTING. REPAIRED AS PER SRM 53-40-00 FIG 23 VOL 1 REV 40 (MAJOR CAT B REPAIR).SDR TRBA2009072Pin · looseDURING POST FLIGHT INSP F/O SAW RT MLG TRUNION PIN COMING LOOSE AND DAMAGING TIRE. AWAITNG AML PAGE FOR FURTHER DETAILS.SDR FDEA200906272348Trunnion · crackedCRACK-LOWER FASTENER HOLE AT 5:00 POS ON LONGERON APPROX .1250 INCH UPON CRACK AREA REMOVAL FROM NLG TRUNNION FITTING. NOSE LANDING GEAR TRUNNION FITTING LT LOWER LONGERON FABRICATED IAW DWG ACA3796 REVISION A. LONGERON REMOVED AND REPLACED IAW SRM 51-31-01, SDR FDEA200906192176Trunnion · crackedNLG LT WEB TRUNNION FITTING FWD SIDE FOUND WITH CRACK. REPAIRED AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS.SDR K11A2009061872201Sleeve · corrodedRT MAIN LANDING GEAR TRUNNION SLEEVE IN RT MLG SUPPORT BEAM CORRODED.SDR DL764091014Trunnion · corrodedDURING A TRIPLE GEAR CHANGE IN ATLANTA, MAINTENANCE FOUND CORROSION ON THE OTBD WALL OF THE RT NLG TRUNNION FITTING. THE MAXIMUM DEPTH OF THE CORROSION WAS .030 INCH. THE CORROSION WAS REMOVED AND REPAIRED PER ER/A 475224-14.SDR FDEA200906091986Trunnion · crackedCRACK 1 INCH FOUND AT FUSELAGE STA 580 FWD OF NOSE GEAR RT TRUNNION FITTING. REPAIR CARRIED OUT AS PER SRM 53-40-00 FIG 23 VOL I REV 40, (MAJOR CAT B REPAIR)SDR FDEA200906081962Trunnion · crackedNLG LT TRUNNION FITTING FORWARD AREA CRACKED. REPAIR CARRIED OUT IAW SRM 53-40-00 FIG 23 VOL I REV 40, (MAJOR CAT B REPAIR)SDR MJ01709001Trunnion · crackedTHIS CRACK WAS DISCOVERED WHILE PERFORMING MX ON THE RT LANDING GEAR PROXIMITY SWITCH. TRUNNION ASSY - DRAG LINKS- AFT LANDING GEAR RT. (K)SDR PCSA2009060401Flange · corrodedCORROSION FOUND ON RT MAIN WHEEL WELL OTBD AFT FLANGE AT STA 930 RBL 72 ABOVE MANUAL EXTENSION TORQUE TUBE. REMOVED SUPPORT FITTING FOR ACCESS. REMOVED CORROSION IAW SRM 51-30-2. FABRICATED AND INSTALLED REPAIR DOUBLER IAW EO SIE-AJ-N495AJ-05-09 REV 1R. REPLACSDR DLM88091040Support · corrodedBUSHING BORE ON RT MLG SUPPORT WITH OVERSIZED MEASUREMENT. BUSHING BORE FOUND WITHOUT DAMAGE. ID BORE SIZE 2.503. BUSHING BORE TREATED IAW SRM 51-10-3.SDR AALA20090512TUL28Trunnion · corrodedCORROSION ON FOWARD FACE OF FWD/AFT TRUNNION LUG FOR LT GEAR. REPAIRED PER AARD 32-10-00-1.SDR 2009FA0000349Attach Fitting · damagedDURING THE SID INSP, THE NLG WAS REMOVED FOR INSP. THE DRAG BRACE LT AND RT BRG PLATE HOLES WERE ALL FOUND EXCESSIVELY ELONGATED REQUIRING STRUCTURAL REPAIR. SUSPECT DAMAGE WAS CAUSED BY NORMAL TOWING OVER THE LIFE OF THE ACFT. THIS WOULD NOT BE DETECTED UNSDR LR7A2009042800068Beam · crackedDURING SCHEDULED B-1 CHECK PER JOB CARD HB3200, FOUND LT MAIN WHEEL WELL BOW BEAM CRACKED AT FS 557, WL198, LBL62. REPAIRED IAW SMP 583 FIG 53-40-14.SDR LR7A2009042800064Beam · corrodedDURING SCHEDULED B-1 CHECK PER JOB CARD HB3200, FOUND RT MAIN LANDING GEAR BEAM WITH EXFOLIATION CORROSION AT FS577, WL160, RBL67. REPLACED BEAM IAW SMP 583 CHAPTER 51-60, 51-70 AND DWG 388482.SDR LR7A2009042800059Beam · corrodedDURING SCHEDULED B-1 CHECK PER JOB CARD HB3200, FOUND LT MAIN WHEEL WELL BOW BEAM ATTACH BRACKET WITH EXFOLIATION CORROSION AT FS 557, WL 198, LBL62. REPLACED BRACKET IAW SMP 583 CHAPTER 51-60 AND 51-70.SDR LR7A2009042800057Beam · corrodedDURING SCHEDULED B-1 CHECK PER JOB CARD HB3200, FOUND LT MLG BEAM WITH EXFOLIATION CORROSION AT FS 577, WL 160, LBL66. REPLACED BEAM IAW SMP 583 CHAPTER 51-60 AND 51-70.
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