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 FDEA200904091253Support Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 3 SUPPORT FITTING LOWER AFT HOLE. REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091252Support Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 3 SUPPORT FITTING LOWER FWD HOLE. REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091251Support Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 3 SUPPORT FITTING UPP AFT HOLE. REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091250Support Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 3 SUPPORT FITTING UPP FWD HOLE. CORROSION REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091249Support Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 2 SUPPORT FITTING LOWER FWD HOLE. SUPPORT FITTING LOWER REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR AALA20090423TUL31Wedge · damagedRIGHT INBOARD FLAP INBOARD WEDGE HAS A TEMPORARY DOUBLER INSTALLED ON LOWER SIDE. REMOVED TEMPORARY DOUBLER AND INSTALLED A FLUSH DOUBLER PER SRM 57-01-00 FIGURE 5.SDR IPXA09555594Wedge · dentedINSPECTION TYPE:C2 R/W OTBD AFT FLAP UPPER T/E WEDGE HAS A DENT 28 INCH OTBD OF INBD END (SRM 57-53-01-01 REFERS TO TREAT AS A HOLE OR PUNCTURE) AFT FLAP WAS REPAIRED PER SRM51-70-04.SDR IPXA09155582Skin · gougedINSPECTION TYPE:4C, RT WING INBD FLAP UPPER SKIN GOUGED 7 PLACES APPROX 18 TO 24 INCHES ABOVE RUB STRIP. CUTOUT DAMAGED AREA OF SKIN PER A300 SRM 57-50-00. PERFORMED HFEC . FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300 SRM 57-50-00.SDR FDEA200904081219Rib · damagedFOUND SEVERAL HOLES DAMAGED ON LT INNER FLAP, RIB 7 TOP AND BOTTOM SKIN. REPAIR PERFORMED BY REPLACEMENT OF RIB 7 AND REPAIR ALL DAMAGED PARTS IAW RAS/FOK/351/2008 ISS A, APPROVED BY EA 6-5750-120184.SDR FDEA200904081218Rib · damagedFOUND SEVERAL HOLES DAMAGED ON RT INNER FLAP, RIB 7 TOP AND BOTTOM SKIN REPAIR PERFORMED BY REPLACEMENT OF RIB 7 AND REPAIR ALL DAMAGED PARTS IAW, RAS/FOK/352/2009 ISS B, APPROVED BY EA 6-5750-120182.SDR FDEA200904081216Skin · chafedRIGHT WING LEADING EDGE UPPER SURFACE FOUND CHAFING MARK AT APPROXIMATELY XIS 247. CARRIED OUT REPAIR AS PER SRM 57-10-00 FIGURE 24 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 107.SDR FDEA200904081215Skin · crackedRIGHT WING INBOARD FLAP UPPER SURFACE SKIN FOUND CRACKED AT 46 INCHES FROM INBOARD END AND 51.5 INCHES FROM TRAILING EDGE, AT APPROXIMATELY XIFH 171.5. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 38 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MINOR AS PSDR DHLA2009801013Skin · misrepairedLT INBD FLAP UPPER SKIN REPAIR IMPROPER, STA XW 106.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1 PG 2. REMOVED PLATING WITH IMPROPER REPAIR IAW SRM 57-1-0 PG 1, SRM 51-1-2. FABRICATED NEW PLATING IAW SRM 57-7-1 FIG 1 PG 2 ITEM D. CLEANEDSDR DHLA2009801009Vane · delaminatedNR 3 LT FLAP VANE INTERNAL SKIN DELAMINATED (STA XF 160.000 - 213.000). REMOVED AND REPLACED NR 3 FLAP VANE IAW MM 27-51-14 PG 201-203.SDR WRLA2009106Angle · crackedDURING C-CHECK IN TPE INSPECTION FOUND A CRACK IN THE ANGLE OF RIGHT O/B TRAILING EDGE FLAP I/B FAIRING HINGE STRUCTURE AT STA XW486.483 (REF EGAT NRC U05029). REPAIRED THE ANGLE OF RIGHT O/B TRAILING EDGE FLAP I/B HINGE FAIRING STRUCTURE IAW MD-11F SRM 57-0SDR WRLA2009105Angle · crackedDURING C-CHECK IN TPE INSPECTION FOUND A CRACK IN THE ANGLE OF RIGHT O/B TRAILING EDGE FLAP I/B FAIRING STRUCTURE AT STA XW486.483 (REF EGAT NRC U05030). REPAIRED THE ANGLE OF RIGHT O/B TRAILING EDGE FLAP I/B FAIRING STRUCTURE IAW MD-11F SRM 57-00-01 VOL 1 FISDR IPXA09M55658Skin · chafedINSPECTION TYPE:1C CHAFED LEFT I/B FLAP VANE TRAILING EDGE AT UPPER SURFACE INBOARD SIDE. REMOVED DAMAGE, PREPPED REPAIR, AND APPLIED REPAIR PLIES PER MD-11 SRM 57-90-00 PARA 16.SDR IPXA09855351Doubler · gougedINSPECTION TYPE:SV SURVEY SEQ 752-W4-20 RT OUTBOARD FLAP STA 213.248 TOP SIDE DOUBLER GOUGED. REPAIR ACCOMPLISHED PER REO-G12587 AND EO DC8-5720-32215.SDR SWAA092258Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER MM.SDR SWAA092165Flap · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR ASAA0946333Skin · dentedLEFT INBOARD FORE FLAP LWR SURFACE HAS 5 DENTS FROM WBL 84.5 123.8. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER BONDED REPAIR.SDR IPXA09855325Flap · damagedINSPECTION TYPE:SVC RT OUTBOARD FLAP XF 227 DAMAGE: PREVIOUS REPAIR. REPLACED REPAIR IAW REO G-12745 AND IPXA EO DC8-5720-32994-A.SDR IPXA09855324Flap · damagedINSPECTION TYPE:SV RT OUTBOARD FLAP STA XF 227 DAMAGE; PREVIOUS REPAIR. REPLACED REPAIR IAW REO G-12745 AND IPXA EO DC8-5720-32994-A.SDR IPXA09855322Flap · damagedINSPECTION TYPE:SV RT OUTBOARD FLAP STA XF 227 DAMAGE; PREVIOUS REPAIR. REPLACE REPAIR IAW REO G-12745 AND IPXA EO DC8-5720-32994-A.SDR FDEA200904031176Skin · chafedFOUND CHAFING MARKS ON RT INNER FLAP LEADING EDGE RIB 10-20. REPAIR PERFORMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION IAW RAS/FOK/027/2009 ISS A, APPROVED BY EA 6-5750-120230.SDR USAA2009040690807Flap · delaminatedCLT - FLT 1291 - MAJOR REPAIR - PRE-FLIGHT FOUND LEFT WING OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED. REPLACED LEFT WING OUTBOARD TRAILING EDGE AFT FLAP IAW B737 AMM 27-51-39-04.SDR FDEA200904021155Skin · chafedFOUND ON LT CENTER FLAP TOP SKIN RIB 13-15 2 AREAS OF CHAFING MARKS. REPAIR PERFORMED BY BLEND OUT THE DAMAGE, NDT FOR CRACK FREE CONDITION IAW AS/FOK/040/2009 ISS A, APPROVED BY EA 6-5750-129134.SDR FDEA200904021152Skin · dentedFOUND ON LT INNER FLAP OLD FILLED REPAIR, AFTER REMOVING OF FILLER, DENT VISIBLE, RIB 16-17 TOP SKIN. REPAIR PERFORMED BY BLEND OUT IAW RAS/FOK/066/2009 ISS A, APPROVED BY EA 6-5750-129131.SDR UIEA201000183Skin · delaminatedRT INBD MID FLAP AT WBL 128.45 AND RT INBD AFT FLAP AT WBL 195.45 DAMAGED WITH DELAMINATION. INBD LOWER SURFACE DAMAGE MEASURES 4.0 IN X 4.0 IN. L/E LOWER SUFACE DAMAGE MEASURES 3.0 IN X 3.0 IN. "PERMANENT REPAIRS PERFORMED IAW THE SRM 51-41-09 FIG 6. TABLE I,SDR FDEA200904011131Skin · misrepairedRIGHT WING INBOARD FLAP ASSEMBLY UNDER-SURFACE, EXISTING DOUBLER REPAIR FOUND AT LOWER SEGMENT AFT EDGE, STA XIFH 270. FOUND NOT CONFORM TO SRM REPAIR. RT INBD FLAP ASSY REMOVED AND REPLACED AS PER AMM 27-50-20-4 REV. 62. ADJUSTMENT AND TEST CARRIED OUT FOUSDR USAA2009040390793Flap · delaminatedPHX - RON - MAJOR REPAIR - RIGHT OUTBOARD TRAILING EDGE FLAP WEDGE DISBONDED AT INBOARD END. REPLACED RIGHT OUTBOARD TRAILING EDGE FLAP IAW US AIRWAYS TASK CARD R3C27034.SDR IPXA09855272Doubler · gougedINSPECTION TYPE:SV RT WING 51BD FLAP STA XF 225.740 REPAIR DOUBLER GOUGED SURVEY SEQ 81 4--W4-03. REPAIR ACCOMPLISHED PER TIMCO REO-G12584 REV IR AND UPS EO DC8-5720-32 210-A.SDR UALA2009040200945Structure · damagedRT OUTBOARD TRAILING EDGE FLAP DAMAGED BY BIRD STRIKE. FOUND RT MOST OUTBOARD LEADING EDGE FLAP WITH ONE QTR IN. PUNCTURE ABOVE 4 IN. CRACK FOLLOWED BY A 2 AND A HALF INCH LONG CRACK. BOTH CRACKS ARE WITHIN HALF AN INCH APART. REMOVED RT O/B FLAP LEADING SDR DLM88090571Vane · delaminatedTHE LT WING INBD FLAP INBD GUIDE VANE EXTERNAL LOWER SKIN WAS FOUND WITH A 10 INCH MAXIMUM DIAMETER DELAMINATED AREA. A PUNCTURE WAS ALSO FOUND NEARBY. DAMAGE WAS BETWEEN XIVIF 35.557 AND 6.2364. THE DAMAGE WAS REMOVED AND AN EXTERNAL REPAIR DOUBLER WAS HOTSDR IXXA09SMN039SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP INTERIOR FITTING CRACKED AT STATION XF 337.000. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-21, ATI REPAIR SSDR IXXA09SMN040SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP INTERIOR HAS FITTING CRACKED AT STATION XF 411.000. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-3-1, SRM 51-1-21.SDR IPXA09655462Hinge Fitting · crackedINSPECTION TYPE:C LT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG FLANGE FOUND CRACKED (CRACK I/B FLANGE 1.125 INCH AND O/B FLANGE 1 INCH). LT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 REV 43. THIS IS CLASSIFIED AS A MAJSDR IPXA09655461Fairing · delaminatedINSPECTION TYPE:C RT WING - O/B FLAP I/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4A FIG 10 REV 43.SDR SWAA092055Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.SDR SWAA092054Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR FDEA200903301105Fitting · corrodedCORROSION, HOLE FOR OTBD FLAP VANE FITTING D ECENTRIC ADJUST RETAINER. COMPLIED WITH EA 1-5750-128674. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200903301104Fitting · corrodedCORROSION, HOLE FOR OTBD FLAP VANE FITTING F ECENTRIC ADJUST RETAINER. COMPLIED WITH EA 1-5750-128673. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200903301100Fitting · corrodedCORROSION-HOLE FOR OUTBD FLAP VANE FITTING E ECENTRIC ADJUST RETAINER. COMPLIED WITH EA 1-5750-128671. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200903301099Fitting · corrodedCORROSION-HOLE FOR OUTBD FLAP VANE FITTING C ECENTRIC ADJUST RETAINER. REPAIR CARRIED OUT AS PER EA 1-5750-128672. THIS REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 107.SDR DL75E090774Skin · chafedRT WING OTBD FORE FLAP AT WS 652.50 LOWER OTBD CORNER HAS CHAFE WEAR AT LEADING EDGE. REPAIRED PER SRM 57-53-01 FIG 201. REPAIR 3 DURING HMV CHECK AT SAA ON NRC 134488.SDR QXEA2009040100209Skin · chafedPDX - C1 RT OTBD FLAP HAS TOP SKIN CHAFE APPROX 47 INCHES FROM THE INBD EDGE 34 INCHES LONG. BLENDED AREA OF CHAFE IAW SRM 57-52-30-02 TO REMOVE DAMAGE AND FOUND BLENDED AREA TO BE OUT OF LIMITS IAW SRM 57-52-30-01. HFEC IAW NDTM PART 6 51-00-01, NO CRACKS NSDR QXEA2009040100207Skin · damagedPDX - C1 - LT OTBD FLAP AT APPROX 30 INCHES FROM INBOARD END AND APPROX 14 INCHES UP FROM TRAILING EDGE ON THE TOP SURFACE HAS A CHAFE FORMING, CHAFE IS APPROX 3 INCHES IN LENGTH AND .100 INCH WIDE IN CENTER OF CHAFED AREA. BLENDED AREA IAW SRM 57-52-30-02 TSDR DL75E090769Skin · dentedLEFT INBD FLAP LWR SURFACE T/E HAS DENT AT STA 224. REPAIRED DURING HMV AT SAA IN SAT ON NR 134448 IN CONJUNCTION WITH JIC OPN 1000 CARD NR 82667990001.SDR IXXA09SMN036SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER SKIN CRACKED AT STATION 104.000 - 122.000. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. INSTALLED REPAIR PART IAW SRM 57-7-1 FIGURE 1 ITEM "D",SDR IPXA09155249Skin · dentedINSPECTION TYPE:N/A RT INBOARD FLAP LOWER SURFACE HAS SEVERAL DENTS. DAMAGE LOCATION BETWEEN RIB 9A THRU 10A AND RIB 14 THRU 15A. REPAIRED PER EO A300-5750-32921-A.
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