JASC 5753
Service difficulty reports · 31,513
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 FDEA201709122509Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (FLAP SIDE) PIVOT INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-04. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335333, PART 1, STEP 3A, AND 3C.SDR FDEA201709112477Support Fitting · corrodedRIGHT WING OUTBOARD FLAP VANE NR 1 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R, FIG 201. AN OVERSIZED WAS FABRICATED IAW EA 1-5750-T0335352, PART 1, STEP 3, TEST CARRIED OUT IAW AMM 27- 50-32SDR FDEA201709112476Support Fitting · corrodedLEFT WING OUTBOARD FLAP VANE NR 5 SUPPORT FITTING BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R, FIG 201. AN OVERSIZED BUSHING WAS FABRICATED IAW EA1-5750-T0335345, PART 1, STEP 1A. INSTALLED IAW AMM 27-50-32-4. LT WING FLAPSDR CALA2017091103129Skin · dentedRH WING I/B FLAP LOWER SURFACE SKIN HAS DENT AT BEHIND NO 6 FLAP TRACK. ACCOMPLISHED A PERMANENT REPAIR ON R/H WING I/B FLAP LOWER SURFACE IAW B757-200 SRM 51-70-10 REPAIR 3 PARA 4 B(2)(B) AND B757-200 SRM 51-70-10SDR CALA2017091103128Skin · dentedLH WING INBD FLAP LOWER SURFACE HAS DENT. ACCOMPLISHED PERMENANT REPAIR DOUBLER OVER DENT ON LH WING INBD FLAP LOWER SURFACE IAW B757-200 SRM 57-53-01 ALLOWABLE DAMAGE 1 FIGURE 101 AND B757-200 SRM 51-70-10, MAJOR REPAIR.SDR IXXA20171109340Skin · corrodedCORRODED AREA NEXT TO FASTENER ON THE LT WING OTBD FLAP SKIN LOWER SURFACE JUST INBD OF THE OTBD FLAP HINGE AT WBL 468. REMOVED, FABRICATED A NEW PANEL IAW DWG 11N3600. INSTALLED THE PANEL IAW SRM 51-40-02, PAR 6.SDR SCNA20170909163Structure · missingLEFT OTBD FLAP PHENOLIC CHAFE MATERIAL MISSING FROM T/E OF FORE FLAP. REMOVED ALL OLD PHENOLIC AND ADHESIVE. CLEANED BOTTOM SIDE OF THE O/B FLAP. REPAIRED.SDR SCNA20170909162Structure · missingRIGHT OTBD FLAP PHENOLIC CHAFE MATERIAL MISSING FROM T/E OF FORE FLAP. REPAIRED.SDR DALA2017090700005Vane · wornWEAR ON LEADING EDGE AT LT INBOARD VANE OUTBOARD FLAP. REPAIRED IAW 2000-8149-04.SDR DALA2017090606642Vane · damagedCRACK AND DENT ON THE LT AFT MOVABLE FLAP VANE LOWER SURFACE APROX 24.75 INCHS FROM INBD SIDE AND 3.25 INCHS FROM THE LE. THE FLAP VANE WAS REPAIRED IAW SRM 57-53-01-2R-1.SDR DALA2017090606641Vane · puncturedPUNCTURE ON INBD FACE AT AFT MOVABLE FLAP VANE, LT WING. THE FLAP VANE WAS REPAIRED IAW SRM 57-53-01-2R-1.SDR IPXA2017090521329Wedge · dentedRT WING INBD AFT FLAP T/E WEDGE LOWER SKIN DENTED. REPAIRED THE FLAP IAW B767-5750-64932-BSDR DALA2017092807160Hinge Fitting · corrodedCORROSION ON THE LT WING FWD FLAP HINGE FITTING AND LOWER STUDS, XW 251.383. THE HINGE FITTINGS WERE REPLACED IAW AMM 57-40-01.SDR FDEA201709022451Hinge Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135692F, PART 5, STEP 2 AND 3. REPAIR CSDR FDEA201709022450Hinge Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135692F, PART 5, STEP 2 AND 3. REPAIR CLASSDR FDEA201709022449Hinge Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135691F, PART 5, STEP 2 & 3. REPAIR CLASSIFSDR FDEA201709022448Hinge Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE (FLAP) PIVOT INBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135691F, PART 5, STEP 2 & 3. REPAIR CLASSIFIEDSDR SWIA201743752Rib · damagedRIGHT INBD RIB ASSY FOUND WITH FIVE ELONGATED CRACKED, DAMAGED HOLES UNDERNEATH THE INBD FLAP SEAL AT TRAILING EDGE. REPAIRED IAW REO.SDR JR2R20170831362Skin · gougedRIGHT WING OTBD FLAP LEADING EDGE, GOUGED IN SKIN AND DOUBLER. REPAIRED THE FLAP LEADING EDGE IAW EA 45-2017-102.SDR FDEA201708302524Skin · delaminatedLT INBD FLAP ENVELOPE, UPPER SKIN, RT CORNER HAS EDGE SEPARATION. REPAIRED IAW SRM 57-10-00 VOL I FIGURE 86 SHEET 1. CUT OUT DAMAGED SKIN PER SRM 57-10-00 FIG 86 SH 1 VOL I. FABRICATED NEW DOUBLER & SKIN SECTION IAW SRM 57-10-00 FIG 86 VOL I. INSTALLED NEW RSDR FDEA201708302523Rub Strip · debondedLT INBD FLAP, UPPER SKIN INBD RUB STRIP IS DISBONDED. REPAIRED IAW SRM 57-10-00 VOL I FIGURE 86 SHEET 1. REMOVED BONDED RUB STRIP. FABRICATED NEW SKIN AND DOUBLER IAW SRM 57-10-00 FIG 86 VOL I. INSTALLED NEW REPAIR SKIN DOUBLER IAW SRM 57-10-00 VOL I FIG 86.SDR DALA2017090106522Vane · gougedLEFT WING OTBD FLAP INBOARD VANE GOUGED AT INBOARD UPPER SURFACE. REMOVED THE FLAP VANE IAW AMM 27-51-03.SDR SWIA201743839Skin · dentedLEFT INBD FLAP LOWER SKIN HAS 3 DENTS. REPAIRED, THE SKIN SECTION REPLACED. LT INBOARD FLAP, TRAILING EDGE IAW SRM AND REO.SDR AALA201709039002Flap Track · corrodedCORROSION ON LEFT WING OTBD FLAP TRACK NR 4 INNER LUG. REPLACED THE FLAP ASSEMBLY IAW CARD 26L00027009.SDR AALA201708289065Skin · delaminatedSMALL AREA OF DISBOND FOUND ON RIGHT INBOARD FLAP. REPAIRED INBOARD FLAP IAW SRM 57-52-00.SDR AALA201708289066Flap · delaminatedAIRCRAFT WAS NOT GROUNDED. SMALL AREA OF DISBOND FOUND ON LEFT HAND INBOARD FLAP. REPAIRED INBOARD FLAP PER SRM 57-52-00.SDR JJBA20170825020Flap Track · corrodedCORROSION FOUND ON RT NR 4 FLAP TRACK. REPLACE RT NR 4 FLAP TRACK.SDR AALA20170825004Hinge Fitting · corrodedCORROSION ON OUTBOARD LEFT WING FLAP CENTER HINGE FITTING AT THE AFT SPAR LOWER INBOARD BOLT. REMOVED AND REPLACED HINGE FITTING IAW AMM 57-40-01-201.SDR SWAA2022020155965Rib · crackedL/H I/B TRAILING EDGE FLAP HAS 2IN LONG CRACK ON RIB THAT I/B PROGRAMMING TRACK ATTACHES TO. / REMOVED AND INSTALLED NEW L/H I/B TRAILING EDGE FLAP ASSY PER AMM 27-51-11. SEE TASKS AND W.I.P'S FOR INDIVIDUAL SIGN-OFFS TAG NO: 296103 PN ON: 113A2100-57A SN ON: SDR SWIA2017100243804Vane · chafedRIGHT INBOARD FLAP VANE SKIN LEADING EDGE CHAFED. REMOVED AND REPLACED THE RT INBD FLAP LEADING EDGE VANE IAW SRM.SDR SWIA2017100243803Vane · chafedLEFT INBOARD FLAP VANE SKIN LEADING EDGE HAS TWO CHAFED AREAS. REMOVED AND REPLACED THE LT INBD FLAP, OTBD SIDE LEADING EDGE VANES IAW SRM.SDR SWAA2017092016479Fairing · crackedRT WING NR 8 FLAP TRACK FAIRING 644BB, INTERIOR SURFACE CRACKED 42" FROM FORWARD EDGE. REPAIRED FAIRING IAW SRM.SDR SWAA2017091216293Flap · delaminatedLT WING OUTBOARD AFT FLAP INBOARD CORNER LOWER SIDE DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR FDEA201708232305Wedge · delaminatedLEFT WING TRAILING EDGE OTBD FLAP, INBD TRAILING EDGE WEDGE FOUND DELAMINATED AT XOF 460 - 468, TOP SURFACE. REPAIRED AND SMOOTHED IAW SRM 57-50-80-2R, REPAIR 1, PARA 4A (1)(A). PERMANENT REPAIR AND EA 1-5750-T0335176, P1. REPAIR CLASSIFIED AS MAJOR IAW SDR AALA201708289026Flap Track · wornTHICKNESS AND WIDTH REDUCTION ON LEFT WING INBORAD FLAP TRACK RAIL 2A AT -Y3025.80. REPLACED FLAP TRACK IAW AMM 27-51-08 SUB TASK 420-035-A.SDR AALA201709049006Trunnion · damagedWHILE ACCOMPLISHING JOB CARD 26T60057066, MAINTENANCE FOUND RIGHT WING INBOARD FLAP TRUNNION OUT OF ALLOWABLE LIMITS. REPLACED THE TRUNNION IAW JOB CARD 26L00027003.SDR AALA201709049005Trunnion · damagedWHILE ACCOMPLISHING JOB CARD 26T50057066, MAINTENANCE FOUND THE LEFT WING FLAP TRUNNION OUT OF ALLOWABLE LIMITS. REPLACED FLAP TRUNNION IAW 26T50057066.SDR DALA2017083106481Wedge · damagedLEFT WING INBOARD TRAILING FLAP TRAILING EDGE HAS DAMAGE APROX 6 INCHES OUTBOARD OF FUSELAGE. COMPLIED WITH IAW ERA 56-1321-14, REV ORIGINAL, SECTION 2. REPLACED THE TRAILING EDGE WEDGE IAW DRAWING 5935966.SDR SWAA2017082815933Skin · delaminatedRIGHT WING OUTBOARD AFT FLAP DELAMINATED. R & R THE AFT FLAP IAW AMM.SDR IPXA2017082220810Skin · damagedTWO DENTS, RT INBD FLAP UPPER SURFACE 49 INCHES FROM INBD EDGE, AND 12 INCHES FROM FWD EDGE OF UPPER SKIN. SECOND DENT IS 57 INCHES FROM INBD EDGE AND 14 INCHES FROM FWD EDGE OF UPPER SKIN. REPAIRED IAW EO A300-5750-65321-B.SDR GR4D20170821010Panel · gougedLEFT A FLAP TRACK HAS A CHAFED GROOVE INTO SURFACE OF FLAP WELL.SDR GR4D20170821009Panel · gougedRIGHT A FLAP TRACK HAS A CHAFED GROOVE INTO SURFACE OF FLAP WELL.SDR GR4D20170821008Roller · gougedLEFT FLAP A TRACK INBOARD ROLLER FITTING HAS A GOUGE .040 X .010.SDR GR4D20170821007Flap Track · corrodedLEFT C FLAP TRACK CORRODED ON ROLLER SURFACES.SDR GR4D20170821002Flap Track · corrodedRIGHT C FLAP TRACK CORRODED ON THE ROLLER SURFACES. APPROACHING MANUFACTURERS MINIMUM TOLERANCESDR GR4D20170821001Flap Track · corrodedRIGHT B FLAP TRACK CORRODED ON THE ROLLER SURFACES. APPROACHING MANUFACTURERS MINIMUM TOLERANCE.SDR SWAA2022013174499Fairing · crackedFLAP FAIRING 642BB CRACKED ON INNER LOWER SURFACE / REMOVED DAMAGE AND ACCOMPLISHED REPAIR REF EA 1-A57-6168 AND SRM 51-70-05. RESTORED FINISH REF AMM 51-21-99.SDR UIEA2017080101405Flap · chafedRT OUTBD AFT FLAP T/E HAS CHAFING. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-70-01-2R, 51-70-10-2R AND SRM 51-70-10-2R REPAIR 2 FIG 201.SDR UIEA2017081501486Flap · corrodedLT WING I/B MID-FLAP UPPER CENTER SECTION HAS 3EA AREAS OF CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 57-53-01-02-01 DETAIL II AND SRM 51-70-10-2R-2 REPAIR 2.SDR UIEA2017081701498Flap · corrodedLT WING I/B MID-FLAP UPPER CENTER SECTION HAS 3EA AREAS OF CORROSION. REPARED PER SRM 57-53-01-01-1 AND EO1957A317.
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