JASC 5753
Service difficulty reports · 31,515
Reports filed under 5753 · Trailing Edge Flaps, 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 = '5753' 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 = '5753' 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 UPS08M52029Skin · corrodedINSPECTION TYPE:C RT I/B TE FLAP O/B LOWER SEGMENT BOTTOM SKIN TO BE REPLACED DUE TO MULTIPLE DENTS AND CORROSION. NEW SKIN FABRICATED PER BOEING DRAWING ARC2444 USING MATL 2024T3-0.040" NEW SKIN HOLES PICKED UP PER SRM 51-31-01 V.2R40. NEW SKIN PROTECTED PESDR UPS08M52028Skin · corrodedINSPECTION TYPE:C RT I/B TE FLAP LOWER SEGMENT BOTTOM SKIN TO BE REPLACED DUE TO MULTIPLE DENTS AND CORROSION. NEW SKIN FABRICATED PER BOEING DRAWING ARC2736 USING 2024T3-0.040" MATL NEW SKIN HOLE PICKED UP PER SRM 51-31-01 V.2R.40. NEW SKIN PROTECTED PER SRSDR 2008UALA00654Flap · crushedLEFT WING,OUTBOARD FLAP LEADING EDGE IS CRUSHED AND HAS 1 INCH LONG PUNCTURE LOCATED FROM APPROX 24 INCHES FROM OUTBOARD END TO APPROX 48 INCHES FROM OUTBOARD END.SDR SWAA080594Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.SDR UIEA200800025Skin · corrodedLT WING O/B FLAP, AFT FLAP UPPER SKIN ON PANEL, AN AREA OF 5.0 INCH BY 2.0 INCH IS CORRODED AT WBL 625 LT. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 5, SHEETS 7 AND 9, PREPREG LAYUP 250 DEGREES F CURE PER SRM 51-40-12. REF: ATLAS AIR EO SDR F3LA200800068Arm · damagedDURING C3/S1 C CHECK, INSPECTION REPORTED THE LEFT WING, NUMBER 2 FLAP DRIVE LEVER EXTENSION ARM (STRUT) FITTING, ON THE FLAP, IS CHAFING INTO THE FITTING AT THE ATTACH POINT (BOTTOM AND TOP) ON THE FLAP. MAINTENANCE BLENDED AND CHAMFERED THE EDGE OF THE FITTSDR 2008UALA00603Attach Fitting · brokenRIGHT WING OUTBOARD FORE FLAP OUTBOARD ATTACH FITTING BROKEN AT FLAP CONNECTION POINT. REPLACED THE RT WING OUTBOARD FORE FLAP ASSEMBLY.SDR CA080212003Support · worn(CAN) DURING A CAMPAIGN NOTICE OF THE RT FLAP CENTER BRG INSTALLATION, BOTH OF THE AFT FLAP BEARINGS WERE FOUND LOOSE AND WORN DUE TO THE LOCATING PIN ON THE BEARINGS NOT INSTALLED INTO MATING HOLES OF FLAP RIB EXTENSIONS. FLAP ROLLER PN KJS 112603 AND BOTH CSDR IXXA08SMN045SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING FLAP INBOARD UPPER SKIN SHOWS DENTS BETWEEN STATION XW 3.000 - XW 91.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, DOUBLER. CLEANED, TREATED AND PRIMED AREA ASDR DHL2008765015Structure · crackedDURING C CHECK, LEFT INBOARD MID FLAP LOWER TRAILING EDGE WBL 102 AT PUSH-ROD IS CRACKED, INBOARD. REMOVED INBOARD MID FLAP LOWER SKIN AND NR 3 TEAR DROP FOR ACCESS IAW SRM 51-30-2. FABRICATED NEW SECTION DIMENSION 57.5" LONG IAW SRM 53-30-5 AND 57-50-2 FIG SDR IXXA08SMN044SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING RIGHT INBOARD FLAP UPPER SKIN HAS DENTS BETWEEN STATION XW 3.000 AND XW 91.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE PANEL PLATING. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS SDR IXXA08SMN043SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP LOWER SKIN HAS DENTS AT STATION XW 3.000 - 91.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE PANEL PLATING. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSDR 2008UALA00586Panel · puncturedOUTBOARD PANEL, ABOVE T/E FLAP PUNCTURED FROM FLAP GUIDE TRACK. SUSPECT FLAP TRACK SNAPPED. REMOVED PANEL AND ROUTED TO SHOP ON R & R NR R16520. REINSTALLED PANEL. ACFT OK FOR SERVICE.SDR WRLA2008017Skin · crackedDURING A CHECK INSPECTION 9 INCH CRACK FOUND RIGHT WING INBOARD FLAP UPPER SKIN INBOARD AFT SKIN PANEL AT XIFH231.2. REPAIRED PER MD-11 SRM 57-20-00 VOL 1 REF ERA 466462-14.SDR SWAA080603Flap · delaminatedDURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.SDR SWAA080610Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR TRAX200800174Bracket · crackedOUTBOARD FLAP ARM OF RT INBOARD FLAP FOUND WITH 4 OMEGA BRACKET CRACKED.SDR TRAX200800173Bracket · crackedTWO OMEGA BRACKET FOUND CRACKED ON INBOARD FLAP ARM OF LT INBOARD FLAP.SDR TRAX200800172Bracket · crackedTWO OMEGA BRACKETS FOUND CRACKED ON FLAP ARM OUTB FLAP ARM OF LT INBOARD FLAP.
SDR 2008UALA00585Hinge Fitting · crackedRIGHT I/B AFT FLAP CENTER HINGE FITTING CRACKED ON I/B AND O/B SIDES. ACCOMPLISHED INSPECTION OF THE OUTBOARD HINGE FITTINGS ON LEFT AND RIGHT WING INBOARD TRAILING EDGE MAIN FLAPS. MANDATED BY AD 2003-13-01 AND NOT EXTENDABLE. REMOVED, REPLACED AND INSTALLEDSDR SWAA080581Flap Track · wornDURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 7 T/E AFT FLAP TRACK WORN. REMOVED AND REPLACED FLAP TRACK PER MM.SDR WRLA2008016Skin · debondedDURING C-CHECK MECHANIC FOUND LEFT WING INBOARD FLAP VANE LOWER SKIN DISBONDED 2 PLACES. REPAIRED PER ENGINEERING INSTRUCTION W2008A57B-082 REV.00. REF NRC U01041.SDR QXEA200800192Flap Track · damagedPDX - C5 CHECK - THERE IS ONE DIVOT ON THE UPPER SIDE OF THE OUTBOARD LOWER FLANGE OF THE RIGHT NR 4 FLAP TRACK. REPAIRED IAW DHC8 200 RD8-57-988, NDTM PT-6 51-00-01.SDR QXEA200800189Flap Track · corrodedPDX - C5 CHECK - LEFT NR 5 FLAP TRACK HAS PITTING ON THE LOWER SURFACE OF THE UPPER INBOARD FLANGE AT THE ROLLERS ZERO DEGREE POSITION. REPAIRED IAW DHC 8 200 RD8-57-989, NDTM PT-6 51-00-01.SDR QXEA200800188Flap Track · corrodedPDX - C5 CHECK - LEFT NR 5 FLAP TRACK HAS PITTING ON UPPER SURFACE OF THE LOWER OUTBOARD FLANGE AT THE ROLLERS ZERO DEGREE POSITION. REPAIRED IAW DHC 8 200 RD8-57-989, AND NDTM PT-6 51-00-01.SDR 08FDEA00388Bushing · corrodedLT WING OUTB FLAP, FITTING WITH UPPER BUSHING ATTACHMENT TO NR 3 TRUNNION WITH SPOTS OF CORROSION. REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5710-117224.SDR 08FDEA00328Skin · misrepairedFOUND REPAIR DOUBLER R/W O/B FLAP LOWER SKIN STA XOF 458. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED REPAIR AND FOUND NOT TO BE WITHIN THE LIMITS OF DC/MD10 SRM 57-10-00 FIG9 VSDR 2008UALA00526Skin · delaminatedLEFT INBOARD MID FLAP DELAMINATED OUT OF LIMITS. REPAIRED DELAMINATION.SDR 2008UALA00507Skin · nickedRIGHT I/B MAIN FLAP UPPER PANEL HAS A NICK AROUND A FASTENER HOLE, APPROX 1.8 INCHES FROM O/B END AND 36.10 FROM AFT END. SUSPECT FOREIGN OBJECT DAMAGE
REPAIRED PER SRM 51-00-04, OK TO CF PER EVA-71089. ACFT OK FOR SERVICE.SDR 08FDEA00329Skin · failedLT I/B FLAP LOWER EXTERNAL SURFACE HAS ERRODED DENT FILLER. REMOVED FILLER,FABRICATED AND INSTALLED NEW REPAIR IAW MD/DC10 SRM 57-10-00 FIG 85 VOLI , 51-21-01 VOLII.SDR DHL2008780002Flap · cracked1 INCH CRACK ON I/B LOWER SIDE OF NR 3 K FLAP JUST ABOVE BULL NOSE.SDR SWAA080518Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR DHL2008780001Flap · delaminatedLT WING I/B FORE FLAP DELAMINATED BEHIND I/B FLAP TRACK AREA 7 INCH BY 3 INCH.SDR USAA920080334Skin · delaminatedCLT - MAJOR REPAIR - C2 CHECK - NR 6005796/JK-15-2725C/1, LEFT WING OUTBOARD TRAILING EDGE FLAP HAS AREA OF DELAMINATION. REPLACED LEFT WING OUTBOARD TRAILING EDGE FLAP IAW B737 AMM 27-51-39.SDR MALA080014Skin · dentedSEVERAL DENTS IN RT FLAP UPPER SURFACE INCLUDING DENTS PARTIALLY COVERED BY 3 MOST OB CHAFE STRIPS REQUIRE MAPPING. REPAIRED DENT NR 12 IAW EO NR S51031. DENTS 1-11, 13-23 ACCEPTED AS IS IAW EO NR 57174. ENTERED INTO SCRATCH AND DENT LOG FROM CONTINUATION CSDR ASAA0842676Skin · dentedLEFT WING AFT FLAPS I/B FORE FLAP LOWER SURFACE HAS MULTIPLE DENTS. PREPARED DAMAGED AREA, FABRICATED FILLERS AND 3 EA DOUBLERS AND BONDED IAW B737 400 SRM 51 70 10 PGS 212 241 214 AND 254 3 EA REPAIR DOUBLERS LOCATED AT WBL 90 115 AND 121.SDR ASAA0842675Skin · dentedRIGHT I/B FOREFLAP HAS MULTIPLE DENTS ON LOWER SURFACE 32" FRM I/B AND 34" FRM O/B SIDES. PREPARED DAMAGED AREA, FABRICATED FILLERS AND DOUBLERS AND BONDED IAW B737 400 SRM 51 70 10 PGS 212 241 214 AND 254.SDR ASAA0842661Skin · dentedLEFT WING O/B AFT FLAP LOWER SURFACE HAS MULTIPLE DENTS AT MID SECTION. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.SDR USAA920080305Skin · debondedMCN - MAJOR REPAIR - C18 CHECK, LEFT WING OUTBOARD FORE FLAP, UPPER SURFACE HAS AREA OF DISBOND, WS 289 - WS 295. REPAIRED LEFT WING OUTBOARD FORE FLAP, UPPER SURFACE, WS 289 - WS 295 IAW B737 SRM 51-70-10-2R3.SDR ASAA0842503Door · brokenCOULD NOT LOWER T/E FLAPS BEYOND 10 DEGS ON APPROACH INTO KTN. REMOVED DAMAGED RIGHTHAND INBOARD FLAP MID FLAP TORQUE DOOR WHICH WAS IMPEDING FLAP TRANSLATION. DOOR REPLACEMENT DEFERRED PER CDL.SDR SWAA080452Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT WING INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR 08FDEA00255Hinge · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD HINGE AFT FAIRING STRUT AFT FASTENER HOLE FOUND CORRODED. CORROSION AT LEFT WING OUTBOARD FLAP OUTBOARD HINGE AFT STRUT AFT HOLE REPAIRED AS PER FEDEX EA NR 1-5750-117303, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR SWAA080439Wedge · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING INBOARD MID FLAP T/E WEDGE DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.SDR USAA920080270Wedge · corrodedMCN - MAJOR REPAIR - C11 CHECK - CORROSION ON LEFT WING INBOARD FLAP WEDGE, FLAP STATION 224.86 - 228.86. REPAIRED LEFT WING INBOARD FLAP WEDGE, FLAP STATION 224.86 - 228.86 IAW B757 SRM 51-70-10-2R.SDR USAA920080251Skin · delaminatedMCN - MAJOR REPAIR - C18 CHECK - LEFT WING INBOARD FORE FLAP LOWER SURFACE HAS DELAMINATION, WBL 125 - WBL 127. REPAIRED LEFT WING INBOARD FORE FLAP LOWER SURFACE, WBL 125 - WBL 127 IAW B737 SRM 51-70-10-2R4.SDR 08FDEA00256Support Bracket · corrodedFOUND CORROSION, LT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT INBOARD CENTER FASTENER HOLE. CORROSION REPAIRED AS PER EA 1-5750-117305, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 08FDEA00253Skin · dentedRT WING, INBOARD FLAP LOWER SURFACE FOUND DENTS AT XIFH 192. REPAIR CARRIED OUT AT RT WING INBOARD FLAP LOWER SURFACE DENT AREA AT XIFH 192 AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR CA080124015Bearing · missing(CAN) ACFT ARRIVED AT OUR FACILITY FOR PAINT. UPON DISASSEMBLY MX NOTED THE BOLT SECURING THE RT FLAP CENTRE AFT ROLLER WAS LOOSE. FURTHER INVESTIGATION AND REMOVAL DETERMINED THAT THE BEARING AND SHIM REQUIRED TO BE UNDER THE HEAD OF BOLT WAS MISSING AND PRSDR 08FDEA00549Trunnion · corrodedLT WING, INBD FLAP NR 1 TRUNNION WITH CORRODED AREA AND EXCESSIVE WEAR. TRUNNION NR 1 LT WAS REPAIRED IN ACCORDANCE WITH CMM 57-52-15.SDR 08FDEA00424Skin · damagedPREVIOUS REPAIR FOUND LOCATED ON LT (FLAP INBD UPPER SKIN) RIB 2/4 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUS REPAIR WAS FOUND DAMAGED AND IT WAS REMOVED. NEW REPAIR WAS DONE PER SRM 57-
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