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 FDEA201301280205Trunnion · crackedNOSE LANDING GEAR LT TRUNNION ATTACHMENT FITTING FOUND CRACKED. REPAIRED IAW SRM 53-10-14, FIG 202, REPAIR 2, REV 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.SDR USAA2013012800029Support Fitting · crackedC2 CHECK - CRACK ON RIGHT MAIN LANDING GEAR SUPPORT FITTING IN THE NR 2 HOLE AT WL 160. REPLACED RIGHT MAIN LANDING GEAR SUPPORT FITTING IAW EO 5702V054.SDR FDEA201301080038Trunnion · crackedNLG RT TRUNNION FITTING FORWARD SECTION FOUND CRACKED.SDR CA121214007Trunnion · cracked(CAN) DURING ANNUAL INSPECTION, THE ENGINEER VISUALLY INSPECTING THE MAIN LANDING GEAR NOTICED A CRACK MIGRATING OUT OF THE LOWER BOLT HOLE OF LT FWD MLG ATTACH TRUNNION.SDR DALA12014080868Support Fitting · corrodedDURING STEP 6 OF AA WC 5740-01114-01B FOUND INBD BORE DIAMETER OF RT /MLG SUPPORT FITTING. FOUND OUT OF LIMITS IAW AA WC. CW PRI 509165-14AD REV 1. COMPLIED WITH ERA 509165-14AD, REV ORIG.SDR DALA12014090868Attach Fitting · corrodedLEFT MLG ATTACH FITTING BOTTLE PIN BUSHING BORE HAS CORROSION ON INBD FACE AND BORE. MACHINED BUSHING BORE TO REMOVE CORROSION WITHIN LIMITS IAW AA WC 5740-01114-01A, COMPLIED WITH PRI 509165-14AD, REV. COMPLIED WITH ERA 509165-14AD REV ORIG.SDR FDEA201210313791Pin · corrodedRT MLG AFT TRUNNION PIN HAS PITTING CORROSION UNDER PIN HEAD AROUND THE CIRCUMFERANCE. REPLACED RT MLG AFT TRUNION PIN IAW AMM 32-11-11-04, STEPS B-12-D AND D-8-(A- F).SDR CA121029006Trunnion · worn(CAN) DURING A SCHEDULED INSPECTION THE FITTING ASSEMBLY - FORWARD TRUNNION, RIGHT MAIN LANDING GEAR WAS FOUND LOOSE. INVESTIGATION REVEALED LOSS OF TORQUE OF ALL FOUR RETAINING BOLTS. FITTING ASSY WAS REMOVED AND IT APPEARED THAT ALL FOUR PLATE NUTS SEEMED TOSDR SWIA201232120Trunnion · crackedONE HOLE, SEVENTH FROM AFT, LEFT SIDE TRUNNION WAS FOUND TO BE CRACKED. (C-CHECK) REPAIRED ONE HOLE, SEVENTH FROM AFT ON LEFT TRUNNION PLANK IAW REO.SDR CA130128020Lug · cracked(CAN) LT AND RT MLG UPPER MEMBER FORWARD LUG FOUND CRACKED DURING NDI CALLED FOR IN AD CF2011-35.SDR CA121012012Trunnion · gouged(CAN) DURING REPLACEMENT OF THE RT MLG OLEO, THE OTBD GEAR DOOR WAS REMOVED. WHEN REINSTALLING THE DOOR IT WAS NOTICED THAT THE RT MAIN GEAR TRUNNION WAS GOUGED BY THE GEAR DOOR ROD ATTACH POINT BOLT WHEN GEAR IS RETRACTED. CONTACTED FOR DISPOSITION. CARRIESDR IPXA12M76021Trunnion · crackedINSPECTION TYPE: 4C, APPROX 1.4" LONG TYPICAL CRACK AT NLG LT TRUNNION FITTING. REPAIRED NLG LT TRUNNION FITTING REF EA 011-5310-01-A4307 I/R, EO MD11-5310-48930-A.SDR FDEA201209253435Trunnion · crackedNLG WHEEL WELL, RT TRUNNION FITTING LOWER AREA FOUND CRACKED. REPAIRED AS PER SRM 53-10-14 FIGURE 202 REPAIR 2 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201209253434Trunnion · crackedNLG WHEEL WELL LT TRUNNION FITTING LOWER AREA FOUND CRACKED. REPAIRED AS PER SRM 53-10-14 FIGURE 202 REPAIR 2 REVISION 50 AND REPAIR PARTS INSTALLED AS PER SRM 53-10-14 FIGURE 202 REPAIR 2 AND SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6SDR IPXA2M75770Trunnion · crackedINSPECTION TYPE: 3C, NLG RT TRUNION FITTING CRACKED. REPAIRED NLG RT TRUNION IAW EA 011-5310-01-A4305 REV.IR AND UPS EO 5310-48760-A. MAJOR.SDR FDEA201209213388Attach Bracket · failedUNSAFE NOSE GEAR INDICATION UPON EXTENSION. EXTENDED GEAR WITH ALTERNATE EXTENSION HANDLE. HEARD LOUD BANG ON RT SIDE ON TAKEOFF. NOTE: UPON CREW DEBRIEF. CAPT STATED THEY DID NOT FEEL THE NOSE GEAR EXTEND (AS THEY NORMALLY WOULD) WHEN SELECTED DOWN. RSDR FDEA201209203366Mount · brokenUNSAFE NOSE GEAR INDICATION ON EXTENSION. EXTENDED GEAR WITH ALTERNATE EXTENSION HANDLE. HEARD LOUD BANG ON RT SIDE AFTER TAKEOFF. CAPTAIN STATED THEY DID NOT FEEL THE NOSE GEAR EXTEND WHEN SELECTED DOWN. RT PSEU SHOWED NO NOSE GEAR CURRENT OR PREVIOUS FSDR IPXA12M75379Trunnion · crackedINSPECTION TYPE:3C, NLG TRUNNION FITTING CRACKED, LT SIDE NEAR TRUNNION PIN. REPAIRED NLG LT TRUNION FITTING IAW SRM 53-10-14, REPAIR 2, FIG 202. (MAJOR)SDR CA120824004Crossbeam · cracked(CAN) CRACK FOUND ON CROSSBEAM, HOLDING THE NLG UPLOCK.SDR FDEA201208092925Hinge Fitting · gougedRIGHT NLG AFT DOOR UPPER FWD HINGE FITTING HAS .2500" X .5" GOUGE FROM CONTACT WITH DOOR CONTROL ROD (ON AFT FACE OF HINGE FITTING) R & R RT NLG AFT DOOR UPPER FWD HINGE FITTING IAW SRM 51-72-10. REMOVED AND REINSTALLED FLOOR PANEL 122 PF IAW AMM 53-10-27-04.SDR FDEA201208092923Hinge Fitting · gougedLT NLG AFT DOOR UPPER FWD HINGE FITTING HAS .2500" X .5" GOUGE FROM CONTACT WITH DOOR CONTROL ROD (ON AFT FACE OF HINGE FITTING) R & R LT NLG AFT DOOR UPPER FWD HINGE FITTING IAW A310 SRM 51-72-10. REMOVED AND REINSTALLED FLOOR PANEL 121PF IAW A310-200 AMM 53SDR 2012FA0000522Attach Fitting · crackedDURING AN ANNNUAL INSPECTION, FOUND A .7500" CRACK IN THE LT MAIN LANDING GEAR OUTBOARD ATTACH FITTING AS VIEWED THROUGH A FLOOR ACCESS PANEL. THE CRACK IS IN THE RADIUS OF THE FITTING AFT AND BELOW THE MLG SPRING. FOUND NO HISTORY OF A HARD LANDING.SDR FDEA201207262693Trunnion · crackedNLG RT TRUNNION FITTING CRACKED. REPAIR CARRIED OUT AS PER SRM 53-10-14, FIGURE 202, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115SDR FDEA201207262692Trunnion · crackedNOSE LANDING GEAR LT TRUNNION FITTING CRACKED. REPAIR CARRIED OUT AS PER SRM 53-10-14, FIGURE 202, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115SDR IPXA12M74774Trunnion · crackedINSPECTION TYPE: 4C, APPROX 1 INCH CRACK AT TYPICAL CRACK LOCATION ON LT NLG TRUNNION FITTING. REPAIRED LT NLG TRUNNION FITTING REF SRM 53-10-14, REPAIR 2, FIG 202, REV 49.SDR SIMA20120718009Trunnion · damagedDURING MAINTENANCE INSPECTION, FOUND THE LEFT NOSE LANDING GEAR TRUNNION FITTING DAMAGED. AIRCRAFT REMOVED FROM SERVICE. PERFORMED REPAIR. REPLACED LEFT NOSE LANDING GEAR TRUNNION FITTING IAW EO EM-53MR-1623 AND EO EM-53MR-1625. AIRCRAFT RETURNED TO SERVICSDR DALA1241739264Support Fitting · corrodedREMOVED RT MLG SUPPORT FITTING BUSHING AND BEARING. NO CORROSION FOUND ON SUPPORT FITTING BUSHING BUT FOUND SCRATCHES AND CORROSION ON BEARING BORE. GENERATED AAR N/R S/N 1016456 AND REWORKED AREA PER DRAWING SR09570087-7001 AND INSTALLED OVER SIZED BEARING,SDR FDEA201207032466Trunnion · corrodedLEFT MLG STRUT FWD TRUNNION LUG IS CORRODED, MISSING. REMOVED AND REPACED LT MAIN LANDING GEAR.SDR FDEA201207032472Bolt · corrodedRIGHT MLG FWD UPPER TRUNNION BOLT CORRODED. REPLACED RT MLG FWD TRUNNION BOLT PER EO 8-3210-7-5004B PT2, ACCOMPLISHED CHECK.SDR FDEA201207022449Bolt · corrodedRIGHT MLG FWD UPPER TRUNNION BOLT CORRODED. REPLACED RT MLG FWD TRUNNION BOLT PER EO 8-3210-7-5004B PT2, SEQ 207, ACCOMPLISHED CHECK.SDR 2012FA0000437Trunnion · crackedDURING AN ANNUAL INSPECTION, WHILE VISUALLY INSPECTING NOSE GEAR, MECHANIC NOTICED THE CRACK IN THE NOSE GEAR TRUNNION ASSY. THERE WERE NO SIGNS OF HYD FLUID LEAKAGE OR LOSS OF THE NITROGEN CHARGE. ACFT WAS INVOLVED IN AN ACCIDENT ON 09/29/1990 INVOLVING COMSDR U2RA201206260002Bracket · crackedRIGHT WING LANDING GEAR STRUT DOOR LOWWER SECTION FIXED FAIRING MID BRACKET FOUND CRACKED. CRACK LENGTH 1".SDR FDEA201206132225Structure · crackedCENTER LANDING GEAR WHEEL WELL - INTERIOR RT SPLICE BEHIND TRUNNION FITTING, FOUND SUSPECTED CRACK. R & R IAW SRM 51-33-01, REV 49 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.SDR CA120604003Support · cracked(CAN) DURING A PROGRESSIVE CARE INSPECTION, A CRACK WAS FOUND ON THE RT MLG SUPPORT BRACKET. THE CRACK WAS APPROX .7500 LONG. THE CRACK WAS LOCATED WHERE BOLT GOES THROUGH THE BRACKET TO THE ATTACHMENT POINT.SDR DALA1234930650Trunnion · corrodedCORROSION WAS FOUND ON THE NOSE LANDING GEAR INBD AND OTBD TRUNNION FITTINGS. BOTH BORES WERE ENLARGED TO A DIA OF 2.813 INCHES FROM AN ORIGINAL SIZE OF 2.762 INCHES. THE INBD TRUNNION FITTING FACE WAS CORRODED REQUIRING REMOVAL WITH SPOTFACE DIA 3.440 INCHESDR WRLA20120521544Fitting · crackedCRACK - FOUND NOSE LANDING GEAR TRUNNION FITTING ON LEFT SIDE HAD CRACK STA Y=595 L=0.5". IAW AMM 32-21-01-000-801 REV B REMOVED NOSE LANDING GEAR ASSY. REPAIR THE CRACK AREA IAW SRM 53-10-14 FIGURE 202 RE. 49 REPAIR 2 IAW AMM 32-21-01-400 REINSTALLED NOSE LSDR FDEA201205071757Support Fitting · corrodedCENTER LANDING GEAR-LINK ASSY UPPER DRAG BRACE MOUNT RT SUPPORT FITTING AFT UPPER SPLICE FOUND CORRODED. R & R WITH NEW SPLICE IAW SRM 51-33-01 REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205071756Support Fitting · crackedCENTER LANDING GEAR-LINK ASSY UPPER DRAG BRACE MOUNT LT HAND SUPPORT FITTING FORWARD LOWER SPLICE FOUND CRACKED. R & R WITH NEW SPLICE IAW SRM 51-33-01, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205071755Support Fitting · crackedCENTER LANDING GEAR-LINK ASSY UPPER DRAG BRACE MOUNT RT SUPPORT FITTING FORWARD LOWER SPLICE FOUND CRACKED. CRACKED SPLICE R & R WITH NEW SPLICE IAW SRM 51-33-01, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205071754Support Fitting · crackedCENTER LANDING GEAR-LINK ASSY UPPER DRAG BRACE MOUNT RT SUPPORT FITTING FORWARD UPPER SPLICE FOUND CRACKED. R & R WITH NEW SPLICE IAW SRM 51-33-01, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2- 100, REV 114.SDR KCSA201205031074Support Fitting · corrodedLEFT STA 1488 LBL 15 TRUNNION SUPPORT FITTING IS CORRODED.SDR CA120417001Fitting · cracked(CAN) DURING SCHEDULED INSPECTION OF THE MLG RETRACT JACK FITTING, A CRACK INDICATION WAS FOUND IN THE SPIGOT RADIUS. A NEW FITTING WAS INSTALLED. ACFT RETURNED TO SERVICE.SDR FDEA201204141399Attach Fitting · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION AROUND STOP DRILL HOLE OF LT NOSE LANDING GEAR TRUNNION FITTING FOUND ONE NEW ADDITIONAL CRACK PROPAGATED FROM THE STOP DRILL HOLE TOWARDS THE LOWER EDGE, APPROX 0.25". REPAIR CARRIED OUT AT LT NLG TRUNNION FITTINSDR CA120329011Gusset · cracked(CAN) CRACK FOUND IN RT AREA OF SL 71 REV D AREA C, HOWEVER THIS IS THE UPDATED FRAME CLUSTER. CRACK WAS ON THE WELD WHERE THE FINGER GUSSET ATTACHED TO THE LOWER FUSELAGE TUBE IS WELDED TO THE AFT FLOAT FITTING ATTACH PLATE.SDR CA120327001Lug · broken(CAN) DURING HEAVY MAINTENANCE, THE NOSE GEAR BELLCRANK HAD BEEN FOUND WITH A BROKEN LUG.SDR CA120323004Doubler · damaged(CAN) FOUND A SINGLE CRACK ON THE UPPER FLANGE OF BOTH THE L/H & R/H NLG SUPPORT DOUBLERS (P/N 6213011-139 L/H, & 6213011-140 R/H) LOCATED AT F.S. 92.70 & W.L. 103.95. CESSNA IS AWARE OF THIS SITUATION, REF CESSNA STRUCTURES REPORT S-650-ATA53/02RD. THERE ISSDR USAA2012041900016Attach Fitting · corroded2S CHECK - CORROSION ON RIGHT MAIN LANDING GEAR ATTACHMENT FITTING AT KEEL BEAM AT FR24, S42R. REPLACED RIGHT MAIN LANDING GEAR ATTACHMENT FITTING IAW SRM A319 51-72-11 & AIRBUS DRAWING D53370600.SDR COEA2012031407911Support Fitting · corrodedHEAVY CHECK / MAJOR REPAIR / LEVEL 2 CORROSION: RT MAIN GEAR TRUNNION SUPPORT FITTING UPPER EDGE HAS CORROSION AROUND SOME FASTENERS. SUBMIT DATA TO ATR AND REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS.SDR IPXA12M72659Trunnion · crackedINSPECTION TYPE: 4C, NLG TRUNNION FITTING CRACKED ON RT SIDEWALL AFT OF RT AFT NLG DOOR AFT HINGE. NLG RT TRUNNION FITTING REPAIRED BY FABRICATION IAW SRM 53-10-14 REPAIR 2, FIG 202, REV 48.SDR IPXA2M72616Trunnion · crackedINSPECTION TYPE:4C, NLG TRUNNION FITTING CRACKED ON LT SIDEWALL AFT OF LT AFT NLG DOOR AFT HINGE. REPAIRED LT NLG TRUNNION FITTING AFT OF NLG AFT DOOR AFT OF AFT HINGE REF SRM 53-10-14, REPAIR 2, FIG 202, REV 48.
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