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 RU3A0917Flap Track · corrodedFLAP TRACK EXFOLIATION CORROSION: LT WING, INBOARD FLAP, INBOARD TRACK (P/N 101-120056-1; OUTBOARD FLAP, INBOARD (P/N 101-110017-1) AND OUTBOARD (P/N 101-110016-3). RT WING, INBOARD FLAP, INBOARD TRACK (P/N 101-120056-1); OUTBOARD FLAP, OUTBOARD TRACK (P/N 1SDR SWAA095844Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR IPXA09M57406Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQUENCE, 284-W3-01 LT WING I/B FLAP EXISTING REPAIR DOES NOT CORRELATE WITH SRM. REMOVED DOUBLER, CUTOUT SKIN, FABRICATED AND INSTALLED REPLACEMENT SKIN AND DOUBLER IAW MD-11 SRM 57-50-01 REPAIR 1 FIG 201.SDR SWAA095826Flap · delaminatedDURING SCHEDULED 14Y CHECK, FOUND RT WING LOWER SURFACE I/B TRAILING EDGE FLAP O/B EDGE DELAMINATED. REPAIRED FLAP PER SRM.SDR SWAA095825Flap · puncturedDURING SCHEDULED MV2 CHECK, FOUND RT WING I/B FORE FLAP PUNCTURED. REMOVED AND REPLACED FORE FLAP PER MM.SDR QXEA2009091100663Panel · chafedRIGHT INBOARD FLAP LEADING EDGE ACCESS PANEL 684ET SHOWS EVIDENCE OF CHAFING. BLENDED CHAFE AREA TO A SMOOTH CONTOUR IAW CRJ 700 SRM 51-21-00 ALL WORK DONE IAW REO 670-57-52-147. PERFORMED LPI ON BLENDED AREA, NO CHAFE OR CRACK FOUND AT THIS TIME. PREPARESDR SWAA095734Flap · delaminatedDURING SCHEDULED 24Y CHECK, FOUND LT WING I/B AFT FLAP T/E DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR IPXA09657321Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.SDR SWAA095757Flap · delaminatedDURING SCHEDULED MV4 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR IPXA09657290Skin · damagedINSPECTION TYPE:N/A LT OTBD FLAP T/E WEDGE LOWER SKIN DAMAGE REF D-406042 LP 300440. REPAIRED IAW EO B767-5750-34485-B / SRM 51-70-17.SDR QXEA2009090900661Skin · gougedDURING INSPECTION FOUND CHAFING ON FLAP INNER SURFACE UNDER INBD FLAP NR 3 VANE ACTUATOR, . BLENDED GOUGE. BLEND MEETS THE CRITERIA STATED IN THE SRM 57-52-01-001-A01 ALLOWABLE DAMAGE LIMITS PG 102. WORK DONE IAW SRM 51-21-11, 51-25-06 AND 51-42-06.SDR QXEA2009090900657Skin · gougedSMALL GOUGE ON LT I/B FLAP UNDER PANEL 584BB. REMOVED 1 SOLID RIVET TO ACCESS GOUGE. BLENDED SMALL GOUGE. BLEND MEASURES .002 AND MEETS THE CRITERIA STATED IN SRM 57-52-01-01-001-A01 ALLOWABLE DAMAGE LIMITS PG 102. ALL WORK DONE IAW SRM 51-21-11, 51-25-06SDR QXEA2009090900656Skin · gougedSMALL GOUGE ON LT I/B FLAP UNDER PANEL 584DB. REMOVED 1 SOLID RIVET TO ACCESS GOUGE. BLENDED SMALL GOUGE. BLEND MEASURES .002 AND MEETS THE CRITERIA STATED IN THE SRM 57-52-01-001-A01 ALLOWABLE DAMAGE LIMITS PG 102. ALL WORK DONE IAW SRM 51-21-11, 51-25-SDR UALA2009090802812Skin · chafedLEFT WING INBOARD FLAP OUTBOARD UPPER EXTERNAL SKIN CHAFED. REPAIRED THE INBOARD FLAP OUTBOARD UPPER EXTERNAL SKIN. GAP CHECKED SPOILER TO FLAP UPPER PANEL. GAP CHECKED GOOD.SDR IPXA09657333Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP TRAILING EDGE WEDGE I/B AREA UPPER SURFACE, THE EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A (1) FIG 9 REV 45.SDR IPXA09657332Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP TRAILING EDGE WEDGE I/B AREA LOWER SURFACE THE EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5G FIG 14 REV 45.SDR IPXA09657322Fairing · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP O/B LEADING EDGE FAIRING DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.SDR SWAA095690Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA095673Skin · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING O/B AFT FLAP SKIN DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR IPXA09557350Fairing · erodedINSPECTION TYPE:C2 RT WING FWD FLAP TRACK FAIRING 674AB FWD END WIND ERODED. REPAIRED RT FWD FLAP TRACK FAIRING 674AB FWD END PER SRM 51-70-17-0G.SDR IPXA09557342Skin · chafedINSPECTION TYPE:C4 RT WING INBOARD FLAP UPPER SURFACE IS CHAFED AFT OF FIXED T/E PANEL. REPAIRED PER SRM 51-70-07.SDR IPXA09M57273Wedge · crackedINSPECTION TYPE:2C LT INBD FLAP COMPOSITE WEDGE CRACKED ON UPPER SIDE LOWER CORNER INBD. REPAIRED LT INBD FLAP INBD TE WEDGE REF MD11 SRM 57-50-02 REPAIR 2.SDR ASAA0946509Support Angle · crackedSUPPORT ANGLE IS CRACKED T/E LEFT WING WBL 204. REPLACED SUPPORT ANGLE.SDR ASAA0946502Skin · chafedRIGHT WING O/B FORE FLAP L/E SKIN I/B EDGE TO 1.25 INCHES AND 7.5 INCHES FROM LWR AFT EDGE OF BULLNOSE THERE IS A CHAFED AREA. REPAIRED RIGHT WING OB FORE FLAP LE SKIN I/B EDGE TO 1.25 INCHES AND 7.5 INCHES FROM LWR AFT EDGE OF BULLNOSE.SDR ASAA0946501Skin · chafedLEFT WING O/B FORE FLAP L/E SKIN I/B EDGE TO 15 INCHES AND 7.5 INCHES FROM LWR AFT EDGE OF BULLNOSE THERE IS A CHAFED AREA. REPAIRED LT WING O/B FORE FLAP L/E SKIN O/B EDGE TO 15 INCHES AND 7.5 INCHES FROM LWR AFT EDGE OF BULLNOSE.SDR ASAA0946500Skin · chafedLEFT WING O/B FORE FLAP L/E SKIN O/B EDGE TO 1.75 AND 3 INCHES FROM LWR AFT EDGE OF BULLNOSE THERE IS A CHAFED AREA. REPAIRED LT WING O/B FORE FLAP L/E SKIN O/B EDGE TO 1.75 AND 3 INCHES FROM LWR AFT EDGE OF BULLNOSE.SDR SWAA095653Flap · delaminatedDURING SCHEDULED 18Y CHECK, FOUND LT WING O/B FORE FLAP I/B END DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA095648Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR IPXA09M57269Wedge · damagedINSPECTION TYPE:2C DURING OK TO INSTALL LT I/B FLAP T/E WEDGE, FOUND T/E CORNER DAMAGED 74 INCHES I/B FROM O/B END. REMOVED DAMAGE, INSTALLED FIBERGLASS DOUBLER IAW MD-11 SRM 57-50-02 REPAIR 2.SDR ASAA0946499Panel · dentedRIGHT WING I/B MAIN FLAP T/E PANEL HAS 2 DENTS THAT ARE OUT OF LIMITS ON THE LOWER SURFACE. REPAIRED DENTS.SDR FDEA200908313149Vane · delaminatedLT WING INBD FLAP VANE LWR MID EXTERIOR SURFACE FOUND DELAMINATION. COMPLIED WITH EA 1-5750-133837. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 107.SDR IPXA09557323Flap · debondedINSPECTION TYPE:C4 LEFT I/B AFT FLAP INBOARD LWR CORNER HAS AN AREA APPROXIMATELY 12 SQUARE INCHES DISBONDED & BROKEN. REPAIR PER SRM 51-70-04.SDR VNAA2009090200012Skin · damagedMAINTENANCE FOUND DAMAGE TO RT LOWER FLAP SKIN INBOARD TRAILING EDGE AFTER A TIRE CHANGE FOR THREADS MISSING. PER THE AIRCRAFT MAINTENANCE MANUAL THE FLAP DAMAGE WAS OUT OF LIMITS AND WAS CHANGED. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL AND THE SDR SWAA095612Wedge · delaminatedDURING SCHEDULED 18Y CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR SWAA095589Flap · delaminatedDURING SCHEDULED 24Y CHECK, FOUND LT WING O/B AFT FLAP T/E DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR FDEA200908293121Skin · chafedRT INBD FLAP UPPER SKIN HAS 2 EA AREAS CHAFED, MAX DEPTH 0.016 INCHES, DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00,FIG 101. CUT OUT DAMAGED AREA ON RT INBD FLAP UPPER SKIN AND INSTALLED FLAP SKIN/STRINGER REPAIR BETWEEN FLAP RIBS NR 11 AND NR 12, STSDR ASAA0956474Flap · chafedCHAFING ON LEFT WING I/B AFT FLAP O/B END. REPAIRED AFT FLAP.SDR UALA2009083102704Skin · bentLEFT WING OUTBOARD TRAILING EDGE FLAP LOWER SKIN IS BENT NEAR THE INBOARD FLAP TRACK. FOUND FLAP SUPPORT TRACK LOOSE WITH MISSING BOLTS. INSTALLED & SECURED MISSING BOLTS AFT FLAP TRACK INBOARD SIDE LT OUTBOARD MID FLAP REF IPC 57-53-10 051 VIEW-N. CYCLED FSDR FDEA200908283119Skin · dentedRT WING CTR FLAP LOWER SKIN HAS DENT, MEASURES 3.250 IN X 2.250 IN X 0.680 IN DEEP AND HAS RIVETS WITHIN THE DENT. DENT IS OUT OF LIMITS IAW SRM 57-50-020, PG BLOCK 101 CUT OUT DAMGED AREA AND INSTALLED FLAP SKIN PATCH REPAIR ON RT WING CTR FLAP LWR SKIN BETSDR AALA20090827TUL04Skin · damagedSTATIC DISCHARGE DAMAGE LOCATED 25 INCHES FROM INBOARD END AND 4.5 INCHES FROM TRAILING EDGE. INSTALLED PERMANENT REPAIR DOUBLER PER SRM 57-01-00 FIGURE 5.SDR AALA20090827TUL03Skin · damagedSTATIC DISCHARGE DAMAGE ON LOWER SKIN 14.5 INCHES FROM TRAILING EDGE. DAMAGE WAS REMOVED AND DOUBLER WAS INSTALLED PER SRM 57-01-00 FIG 5 SHEET 1.SDR AALA20090827TUL01Vane · wornWORN AREA ON OUTBOARD FLAP VANE NEXT TO FLEX JOINT. INSTALLED HOT-BOND DOUBLER PER SRM-51-70-02.SDR IPXA09M57369Skin · dentedINSPECTION TYPE:2C REPAIR SURVEY SEQUENCE 253-W4-01 RT WING I/B FLAP UPPER SKIN APPROX BETWEEN STA XIFH153-177 EXISTING REPAIR DOUBLER NOT CORRELATED WITH MD-11 SRM 57-00-01 FIG 201, WRONG LOCATION. REMOVED DOUBLER AND FILLER, FABRICATED AND INSTALLED REPAIR SDR IPXA09M57367Skin · dentedINSPECTION TYPE:2C SHARP DENT ON LEFT I/B FLAP LOWER SKIN, NEAR STA XIFH 203. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLERS IAW UPS EO MD11-5750-34930-A AND SAA EA 011-5753-01-A2008.SDR IPXA09M57295Skin · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQUENCE NR 253-W3-05. LT WING I/B FLAP UPPER SKIN APPROX BETWEEN STA XIFH 207-225 EXISTING REPAIR DOUBLER NOT CORRELATED WITH MD-11 SR 57-00-01 FIG 201. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM SDR IPXA09M57294Skin · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQUENCE NR 253-W3-03. LT WING I/B FLAP UPPER SKIN APPROX BETWEEN XIFH 153-171 EXISTING REPAIR DOUBLER NOT CORRELATED WITH MD-11 SRM 57-00-01 FIG 201. REMOVE DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-0SDR ASAA0946466Skin · delaminatedLEFT I/B FORE FLAP T/E WEDGE LOWER SKIN IS DENTED AND DELAMINATED 28 INCHES FROM O/B END, 9 INCHES FROM T/E. REPAIRED SKIN.SDR ASAA0946465Skin Panel · chafedLEFT O/B MID FLAP LOWER AFT PANEL UPPER SURFACE ADJACENT TO THE O/B AFT FLAP TRACK IS CHAFED. REPAIRED PER SRM.SDR AALA20090826TUL09Vane · wornWORN AREA ON LEADING EDGE OF INBOARD FLAP VANE AT INBOARD AREA. INSTALLED HOT BOND DOUBLER UNDER SRM-51-70-02.SDR SWAA095542Flap · puncturedDURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP PUNCTURED. REPAIRED FORE FLAP PER SRM.
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