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 S9BA200700018Attach Bracket · corrodedNOSE LANDING GEAR LOWER MOUNTING FITTING CORRODED.SDR 2007UALA03911Trunnion · gougedNLG TRUNNION IS CREAKING AND GROANING. AFTER FURTHER ANALYSIS, IT HAS BEEN DETERMINED THIS IS NOT AN SDR REPORTABLE EVENT.
SDR 07FDEA03802Trunnion · corrodedCENTER LANDING GEAR RIGHT MOUNTING. TRUNNION FITTING FORWARD AND AFT HOLE FOUND WITH CORROSION. 10-01-07 COMPLIED WITH FEDEX E.A. 1-5310-115190. CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA03801Trunnion · corrodedCENTER LANDING GEAR LEFT MOUNTING. TRUNNION FITTING FORWARD AND AFT HOLE FOUND WITH CORROSION. 10-01-07 COMPLIED WITH FEDEX E.A. 1-5310-115189. CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR CA071011007Attach Fitting · cracked(CAN) AFTER REPAINT OF A/C INSPECTION REVEALED A CRACK ON SIDE OF ATTACH POINT. LDG WAS PULLED TO REPLACE ATTACH POINT BRACKET AND ATTACH POINT BRACKET BOLTS. THESE BOLTS WERE SHOWING WEAR MARKS ON THE SHANK, SUGGESTING THE NUTS WERE THREAD BOUND, INDICATING NSDR 07FDEA03794Trunnion · crackedFASTENER HOLE FOUND CRACK AT 9 AND 3 O'CLOCK POSITION ON LONGERON AT RIGHT SIDE NOSE LANDING GEAR TRUNNION. 09-28-07 REPAIR CARRIED OUT AT FASTENER HOLE, 9 AND 3 O'CLOCK POSITION ON LONGERON AT RT NLG TRUNNION AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFISDR 07FDEA03553Trunnion · crackedRIGHT NOSE LANDING GEAR TRUNNION FITTING SUSPECT WITH CRACK. 09-28-07 REPAIR CARRIED OUT AT RT NLG TRUNNION FITTING AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA03552Trunnion · crackedLEFT NOSE LANDING GEAR TRUNNION FITTING SUSPECT WITH CRACK. 09-28-07 REPAIR CARRIED OUT AT LT HAND NOSE LANDING GEAR TRUNNION FITTING AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR DHL2007746528Trunnion · corrodedRIGHT NOSE LANDING GEAR TRUNNION BORE HAS CORROSION. REMOVED CORROSION AND REPAIRED NOSE LANDING GEAR TRUNNION SUPPORT FITTING IAW B727 SRM 51-10-6 AND 53-40-01. NOSE LANDING GEAR OPS/CHECK GOOD IAW B727 MM 32-33-00.SDR DHL2007746525Trunnion · corrodedLEFT NOSE LANDING GEAR TRUNNION BORE HAS CORROSION. REMOVED CORROSION AND REPAIRED NOSE LANDING GEAR TRUNNION SUPPORT FITTING IAW B727 SRM 51-10-6 AND 53-40-01. NOSE LANDING GEAR, OPS/CHECK GOOD IAW B727 MM 32-33-00.SDR CA070904003Trunnion · cracked(CAN) DURING THE A-CHECK INSPECTION, MAINTENANCE DETECTED A CRACKED RT NOSE LANDING GEAR TRUNNION FITTING. THE AIRCRAFT WAS RE- POSITIONED FOR PART REPLACEMENT. (TC NR 20070904003)SDR 2007FA0000824Fitting · crackedAC WAS BEING TAXIED FROM THE RAMP TO THE TAXIWAY, AND DURING TAXI, THE PILOTS REPORTED THAT THE NOSE GEAR STEERING SEEMED TO BE MALFUNCTIONING. UPON INSPECTION, THE NOSE GEAR STRUT APPEARED TO BE PRESSED UP AGAINST THE REAR HALF OF THE LOWER COWLING. THE LOWSDR 07FDEA03128Trunnion · crackedNOSE LANDING GEAR RIGHT TRUNNION FITTING SUSPECT CRACKED. 09-11-07 NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING REPAIR CARRIED OUT AS PER SRM 53- 40-00 FIG. 23 VOL I. REPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVASDR 07FDEA03127Trunnion · crackedNOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. 09-11-07 NOSE LANDING GEAR LEFT HAND TRUNNION FITTING REPAIR CARRIED OUT AS PER SRM 53-40- 00 FIG. 23 VOL I. REPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS. RESDR SROM200700017Support Beam · crackedNR419 - CRACK ON NLG ACTUATOR SUPPORT BEAM AT BS 227-0 UPPER RIGHT SIDE. REPLACED NLG ACTUATOR UPPER RIGHT SIDE SUPPORT BEAM IN ACCORDANCE WITH BOEING 737 SRM 51-10-1, 53-10-2 AND 51-30-2.SDR 2007FA0000801Support · corrodedLT MLG DOOR IB AFT SUPPORT REMOVED FOR OTHER MAINTENANCE AND SEVERE INTERGRANULAR CORRODION DISCOVERED FROM LAVATORY LEAKAGE AS INDICATED BY STAINING ON PART LOCATION WHERE BONDING STRAP ATTACHES. CORROSION SEVERE AND IS ENOUGH TO CAUSE PART TO FAIL. (K)SDR SROM200700012Trunnion · wornWEAR DAMAGE, LT MLG FUSELAGE TO TRUNNION SUPPORT BEAM ATTACH FITTING. BLEND REPAIRED IAW MFG, FORM 8100-9, MESSAGE NR 1-515849678-6, DATED AUGUST 23, 2007.SDR DLM88071038Fitting · bentNLG SUPPORT BEAM FITTING BENT AND WHEELWELL WEB CRACKED. REPLACED SUPPORT BEAM FITTING AND REPAIRED WEB.SDR DHL2007741535Fitting · corrodedRT SIDE NLG TRUNNION SUPPORT FITTING SHOWS SIGNS OF CORROSION ON UPPER CAP, BS 304. CORROSION CLEAN UP WOULD EXCEED TRUNNION BORE DIA LIMITATIONS. REMOVED, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW TRUNNION SPT FITTING, P/N 65-17676-40, PER B727 SSDR DHL2007741529Stiffener · corrodedNOSE LANDING GEAR RT TRUNNION AFT STIFFENER CORRODED OUT OF LIMITS. LOCATED AND DRILLED NEW STIFFENER, TREATED, PRIMED, AND INSTALLED NEW STIFFENER PER B727 SRM 51-10-2, 51-30-5, AND 51-30-2.SDR DHL2007741523Support · corrodedCORROSION ON APU INLET SCREEN LWR FWD SUPPORT FRAME IN LMLG W/WELL, AT BS 910. REMOVED FRAME SECTION, FABRICATED NEW FRAME SECTION FROM BAC1520-1247 EXTRUSION, 33" IN LENGTH, PO NR 994061, PER B727 SRM 53-10-2 FIG 4 AND 51-20-1. TREATED, PRIMED, AND INSTALLESDR DHL2007741520Support Fitting · corrodedLT NLG TRUNNION SUPPORT FITTING HAS CORROSION ON UPPER CAP SURFACE. REMOVED AND REPLACED LT NLG TRUNNION SUPPORT FITTING DUE TO CORROSION REMOVAL WOULD HAVE EXCEEDED BORE DIAMETER LIMITS. REMOVED AND REPLACED COMPLIED WITH PER B727 SRM 51-330-5 AND 51-30-2.SDR DHL2007741521Support Beam · corrodedNLG LT TRUNNION VERTICAL SUPPORT BEAM AT BS 312.0 HAS CORROSION. CORROSION REMOVAL EXCEEDED LIMITS PER B727 SRM 53-10-1 FIG 1. REMOVED AND REPLACED VERTICAL SUPPORT BEAM PER B727 SRM 51-30-2 AND 51-30-5.SDR 07FDEA02694Trunnion · crackedNOSE LANDING GEAR RT TRUNNION FITTING CRACKED. [08-20-07] REPAIRED AS PER SRM 53- 40-00 FIGURE 23 VOLUME I. REPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS AS REQUIRED IN SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSSDR 07FDEA02678Fitting · crackedNOSE LANDING GEAR LT TRUNNION FITTING FOUND CRACKED. [08-20-07] REPAIRED AS PER SRM 53-40- 00 FIGURE 23 VOLUME I. REPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS REQUIRED IN SRM 53-40-00 FIGURE 23 VOLUME I. REPASDR UIEA200700304Trunnion · corrodedLEFT BODY GEAR INBOARD TRUNNION FITTING HAS CORROSION AROUND THE UPPER FACE OF 3 BOLT HOLES (INBOARD FWD, OUTBOARD FWD, AND OUTBOARD AFT). LOCALLY BLENDED OUT ALL PITTING CORROSION AREAS. HFEC AND 10X VISUAL INSPECTION PLUS DYE PENETRANT INSPECTION ACCOMPLISSDR UIEA200700282Trunnion · corrodedCORROSION ON UPPER SURFACE OF RIGHT BODY GEAR OUTBOARD TRUNNION UPPER CAP AROUND THE FORWARD BOLT HOLE. LOCALLY BLENDED PITTING CORRODED AREA. HFEC AND 10X VISUAL INSPECTION PLUS DYE PENETRANT INSPECTED. SPOT FACED WASHER BEARING SURFACE AREA SHOT PEENED BLSDR UIEA200700279Trunnion · damagedNOSE GEAR LEFT TRUNNION BEARING LOWER CAP TOOLING DAMAGE ON BOTTOM MATING SURFACE. BLENDED OUT DAMAGE MIN .250"R , HFEC AND 10X VISUAL INSPECTION TREATED AND PRIMED. REF BOEING 8100-9 MESSAGE 1-384920112-1.SDR UIEA200700278Trunnion · corrodedLT BODY GEAR OUTBOARD TRUNNION BEARING SUPPORT FITTING FACE HAS PITTING. BORE FACE AND SIDE FACES WERE MACHINED TO REMOVE DAMAGED AREAS ID= 10.826", IB SIDE FACE = 0.017 REMOVED. OB SIDE FACE = 0.025 REMOVED. REPAIR REF B747 SRM 53-10-08 FIG 2.SDR UIEA200700277Trunnion · corrodedLT BODY GEAR OUTBOARD TRUNNION FITTING HAS CORROSION AROUND THE UPPER FACE OF THE FWD BOLT HOLE. LOCALLY BLENDED CORROSION AREAS AND THEN SPOT FACING AROUND THE FORWARD BOLT HOLE REMOVE ALL BLEND OUTS WITHIN THE BEARING SURFACE. REF BOEING 8100-9.SDR USAA070580Beam · crackedSTA 259.5 AT NOSE W/W CEILING WL 192.5, BL 0, RADIUS OF NOSE GEAR ACT BEAM. REPLACED GUSSET PER SRM 51-10-02, DEFECT SIZE: .75 INCH.SDR 07FDEA02580Trunnion · chafedCENTER LANDING GEAR LEFT MOUNTING TRUNNION FITTING BOTTOM SURFACE FOUND WITH CHAFED MARK. [08-03-07] REPAIR CARRIED OUT AT CENTER LANDING GEAR LEFT HAND MOUNTING TRUNNION FITTING BOTTOM SURFACE AS PER SRM 53-40-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS SDR 07FDEA02579Trunnion · corrodedCENTER LANDING GEAR MOUNTING LEFT TRUNNION FITTING FOUND WITH CORROSION. [08-03-07] REPAIR CARRIED OUT AT CENTER LANDING GEAR MOUNTING LEFT HAND TRUNNION FITTING AS PER SRM 53-40-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 07FDEA02578Trunnion · corrodedCENTER LANDING GEAR RIGHT TRUNNION FITTING FOUND WITH CORROSION. [08-03-07] REPAIR CARRIED OUT AT CENTER LANDING GEAR RIGHT HAND TRUNNION FITTING AS PER SRM 53-40-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 07FDEA02528Trunnion · corrodedCENTER LANDING GEAR LEFT MOUNTING TRUNNION FITTING CENTER GUIDE HOLE FOUND WITH CORROSION. [08-06-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-112364, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA02497Trunnion · crackedNOSE LANDING GEAR RIGHT TRUNNION FITTING FOUND CRACKED. [08-03-07] CARRIED OUT REPAIR AS PER SRM 53-40 -00 FIGURE 23 VOLUME I. REPETITIVE INSPECTION TO BE CARRIED OUT NOT EXCEEDING 1,500 LANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA02496Trunnion · crackedNOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. [08-03-07] CARRIED OUT REPAIR AS PER SRM 53-40- 00 FIGURE 23 VOLUME I. REPETITIVE INSPECTION TO BE CARRIED OUT NOT EXCEEDING 1,500 LANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR KCSA071232Fitting · corrodedCORROSION ON LT BODY LANDING GEAR TRUNNION SUPPORT FITTING IN BEARING BORE AND ON SIDE FACES BS 1470.SDR CA070716001Mount · damaged(CAN) AFTER TAKEOFF, THE LANDING GEAR WAS RETRACTED AND THE RT/MAIN GEAR DID NOT INDICATE UP AND LOCKED. THE GEAR WAS SELECTED DOWN AND ALL (3) GEAR INDICTED DOWN AND LOCKED. MAINTENANCE HAS FOUND THE RT MAIN GEAR ACTUATOR MOUNTING DAMAGED. PARTS 215-34071-1,2SDR 07FDEA02389Trunnion · crackedNOSE LANDING GEAR LT TRUNNION FOUND CRACKED. [07-24-07] REPAIR CARRIED OUT AS PER SRM 53-40-00 VOL.I. FIG. 23. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR WRNA200700052Trunnion · corrodedDURING M-96 CHECK, CORROSION WAS FOUND IN LT MAIN LANDING GEAR AFT TRUNNION FORWARD LUG FITTING BORE AND FACE. REMOVED CORROSION BY OVERSIZING BORE AND SPOT FACING THE LUG FACE AND INSTALLED NEW BUSHING IAW REPAIR DESIGN APPROVAL SHEET RAS/BAE/1005347/2007.SDR 07FDEA02322Trunnion · corrodedCTR LANDING GEAR, RT TRUNNION FITTING FWD HOLE FOUND CORRODED. [07-10-07] COMPLIED WITH FEDEX E.A. 1-5310-112350, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA02321Trunnion · corrodedCTR LANDING GEAR, RT TRUNNION FITTING AFT HOLE FOUND CORRODED. [07-10-07] COMPLIED WITH FEDEX E.A. 1-5310-112350, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA02320Trunnion · corrodedCTR LANDING GEAR, RT TRUNNION FITTING ALIGNMENT HOLE FOUND CORRODED. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL.I. ORIGINAL HOLE DIAMETER: 1.500"; REWORKED HOLE TO 1.6664". MAXIMUM HOLE DIAMETER: 1.680". BUSHING FABRISDR 07FDEA02319Trunnion · corrodedCTR LANDING GEAR, RT TRUNNION FITTING MATING SURFACE FOUND CORRODED. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL.I. FWD LUG - ORIGINAL THICKNESS: 2.505"; MATERIAL REMOVED: 0.040" REMAINING THICKNESS: 2.465"; MIN. ALLOWABSDR 07FDEA02318Trunnion · corrodedCTR LANDING GEAR, LT TRUNNION FITTING ALIGNMENT HOLE FOUND CORRODED AFTER PILLOW BLOCK REMOVAL. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL I. ORIGINAL HOLE DIAMETER: 1.500"; REWORKED HOLE TO 1.666". MAXIMUM HOLE DIAMETERSDR 07FDEA02317Trunnion · corrodedCTR LANDING GEAR, LT TRUNNION FITTING MATING SURFACE FOUND CORRODED AFTER PILLOW BLOCK REMOVAL. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL.I. FWD SIDE - ORIGINAL THICKNESS: 2.536"; MATERIAL REMOVED: 0.044" REMAINING THICSDR 07FDEA02316Trunnion · corrodedCTR LANDING GEAR, LT TRUNNION FITTING FWD HOLE FOUND CORRODED. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL.I. ORIGINAL HOLE DIAMETER: 1.341"; REWORKED HOLE TO 1.379". MAXIMUM HOLE DIAMETER: 1.385". BUSHING FABRICATED AND INSTSDR 07FDEA02315Trunnion · corrodedCTR LANDING GEAR, LT TRUNNION FITTING AFT HOLE FOUND CORRODED. [07-10-07] COMPLIED WITH FEDEX E.A. 1-5310-112351. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA02267Trunnion · crackedLANDING GEAR, NOSE GEAR LT TRUNNION FITTING FOUND CRACKED. [07-06-07] REPAIR CARRIED OUT AT NOSE LANDING GEAR LT TRUNNION FITTING AS PER SRM 53- 40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
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