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 06FDEA0534Repair · misinstalledFOUND REPAIR LOCATED ON RT OUTBD FLAP, RT WS 935-950. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMPSDR UPS06446215Panel · delaminatedINSPECTION TYPE:C RIGHT WING: O/B AFT FLAP PANEL 688IT UPPER SURFACE FOUND DELAMINATED. DELAMINATED AREA ACCOMPLISHED METAL HOT BOND REPAIR AS PER SRM 51-40-24 FIG 1.SDR 06FDEA0533Repair · misinstalledFOUND REPAIR LOCATED ON RT INBD FLAP, RT WS 347-349. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX E:A: 6-5710-95695 REPAIR EVALUASDR 06FDEA0532Repair · misinstalledFOUND REPAIR LOCATED ON RT INBD FLAP, RT WS 110-119. REPAIR REQUIRES EVALUATION FOR MAJOR OR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX E:A: 6-5710-95695 REPAIR EVALUSDR 06FDEA0528Repair · misinstalledFOUND REPAIR LOCATED ON LT INBD FLAP, LT WS 346-400. REPAIR REQUIRES EVALUATION FOR MAJOR OR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX EA 6-5710-95695 REPAIR EVALUATSDR 06FDEA0527Repair · misinstalledFOUND REPAIR LOCATED ON LT INBD FLAP, LT WS 236-276. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX EA 6-5710-95695 REPAIR EVALUATED SDR 06FDEA0512Skin · crackedLEFT WING O/B FLAP UPPER SKIN CRACKED. PERFORMED HEFC IAW DC10 NDT SPM 06-10-01. 601. REMOVED DAMAGED AREA IAW DC10-10 SRM 57-10-00 VOL I FIG 85. FAB DOUBLER & FILLER IAW DC10-10 SRM 57-10-00 VOLI FIG 85. ALODINED & PRIMED IAW DC10-10 SRM 51-21-01 VOLIISDR SWAA060398Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR ASAA0640102Skin · gougedRT WING OB FOREFLAP IS GOUGED AT THE UPPER SURFACE AT THE IB END. REMOVED DAMAGED AREA OF FORE FLAP UPPER SKIN, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER PER SRM 51-70-10 REPAIR 4.SDR SWAA060384Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR 06FDEA0485Support Fitting · corrodedLEFT WING OUTBOARD FLAP VANE NR 1 SUPPORT FITTING CORRODED. REMOVED AND REPLACED SUPPORT FITTING PART NUMBER ARC1495-505 IAW EO E8-5750-7-5004.SDR SWAA060348Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING OUTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR ASAA0640071Skin · dentedOKC - FOUND RIGHT WING INBOARD T/E FLAP WEDGE NR 7420 LOWER SURFACE HAS DENTS. REMOVED DENTED AREAS OF ALL 6 DENTS, FABRICATED ALL 6 FILLERS AND DOUBLERS AND INSTALLED IAW B737-400 SRM 51-70-10 PAGE 211 PARAGRAPH 7, PAGE 213 PARAGRAPH 8, PAGE 221, PARAGRAPH 1SDR USAA060149Skin · gougedLOCATION: LWR L/B CORNER AT L/E OF LT MID FLAP. REMOVED OLD REPAIR, INSTALLED NEW IAW SRM 57-53-01 DEFECT SIZE: 4 INCHES.SDR 2006FA0000126Flap · excess playFLAP SN SC279 WAS REMOVED FROM SERVICE FOR LOOSE ATTACHMENT INSERTS ON THE IB END RIB. THE FLAP ATTACH CARRIAGE WAS DISCOVERED LOOSE DURING A ROUTINE DAILY PPOST FLIGHT INSPECTION, WHERE PLAY WAS NOTED BETWEEN THE FLAP ATTACH CARRIAGE AND THE IB FLAP END RIB.SDR AWXA200600147Fairing · separatedDURING CLIMB, CREW REPORTED A VIBRATION AND NOISE. DISCOVERED THE LT WING TO FLAP FAIRING CAME OFF IN FLIGHT. CREW DECLARED EMERGENCY AND LANDED IN TPA. MAINTENANCE INSTALLED TEMP. REPLACEMENT PANEL AND MAINTENANCE FERRIED TO PHX. AIRCRAFT IS STILL OTS. SDR SWAA060315Skin · delaminatedRIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR 06FDEA0371Rib · crackedLT WING OUTBOARD FLAP L/E STA 758 ON RIB FOUND CRACK 0.60 INCH LONG. REMOVED, REPAIRED AND REINSTALLED RIB IAW SRM 57-00-01 FIG 0 SHT 1-3-4 VOL 1, SRM 51-35-01 PAR 1-5 VOL 2 AND SRM 51-33-01 PAGE 34-47 VOL 2. FABRICATED PART IAW DETAIL PART TRAVELER N00402 ASDR WRNA200600023Doubler · debondedDURING INSPECTION, TWO DIS-BONDED DOUBLERS WERE FOUND ON LEFT WING OUTBOARD FLAP SKIN UPPER SURFACE ON RIB 4 AND 15 TRAILING EDGE AREA. AFTER DOUBLERS WERE REMOVED, CORROSION WAS FOUND. REPAIRED PER AVBORNE REPAIR REFERENCE 25599-9-01-24-06 (AIRBUS TECHNICALSDR SWAA060288Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E FOREFLAP UPPER SKIN DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR SWAA060286Skin · delaminatedDURING SCHEDULED A1 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR USAA060135Skin · wornLEADING EDGE SKIN OF MID FLAP 13 TO 20 INCHES FROM OUTBOARD END WORN. FABRICATED AND INSTALLED DOUBLER IAW SRM 57-53-01 REPAIR 8, DEFECT SIZE: 7 X 4 INCHES.SDR QXEA200600349Skin · chippedYYC - C3 LEFT WING INBOARD FLAP NUMEROUS ROCK CHIPS INPAINT AFT OF MAIN LANDING GEAR AREA. REPAIRED IAW CRJ700 SRM 51-21-26-00-001-001-A01 AND SRM 51-25-01-001-001-A01.SDR QXEA200600324Skin · damagedYYC - C3 RIGHT HAND INBOARD FLAP LOWER SURFACE HAS GRAVEL DAMAGE. REPAIRED IAW CRJ700 SRM 51-21-26-00-001-001-A01, SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-A01.SDR DHL2006763517Skin · puncturedS/O 284007 N/R 032223 - RT INBD FORE FLAP PUNCTURED APPROX 4 FEET FROM INBD END. CUT OUT PUNCTURED AREA 1" X 3". FABRICATED AND INSTALLED REPAIR DOUBLER 3 X 6" FROM 2024-T3 .016" IAW SRM 51-40-20 FIG 8.SDR AWXA200600130Skin · debondedPHX - MAJOR REPAIR - MAINTENANCE REPORTED TWO DISBONDED AREAS FOUND ON LEADING EDGE OF LOWER SKIN ON THE TRAILING EDGE WEDGE ON THE LEFT HAND WING APPROX. 2" BY 0.5" AND 1" BY 0.3" ON THE INBOARD FLAP. MAINTENANCE CUT OUT AND REMOVED DAMAGED CORE ON THE INBOASDR SWAA060299Skin · delaminatedDURING SCHEDULED HC1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP LOWER SKIN DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.SDR DHL2006763515Skin · chafedS/O 284007 N/R 032201 - RT INBD T/E FORE FLAP L/E SKIN CHAFED BEYOND LIMITS AT WBL 72 AND 166, 1.5" AND 96" INBD END. REMOVED 2 EA L/E PANELS THAT WERE OUT OF LIMITS. FABRICATED AND INSTALLED NEW PANELS 7" X 7-5/8" AND 15" X 15" FROM 2024-T3 .040 IAW B727 BOESDR DHL2006763516Skin · crackedS/O 284007 N/R 032203 - RT INBD T/E FORE FLAP L/E SKIN CRACKED ON LOWER SURFACE 53.5" FROM INBD END WBL 124. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER 8" X 6.375 FROM 2024-T3 .063" IAW SRM 57-50-4 FIG 1.SDR DHL2006763514Skin · chafedS/O 284007 N/R 032199 - LTOUTBD T/E FORE FLAP L/E SURFACE CHAFED BETWEEN IND AND CENTER HINGES WBL 367. TRIMMED OUT CHAFED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER 6" X 4" FROM 2024-T3 .063" IAW B727 SRM 57-50-4 FIG 1.SDR 06FDEA0304Flap Track · corrodedCORROSION ON NR 2 FLAP TRACK, AFT O/B MOUNTING HOLE. NEW NR 2 FLAP TRACK WAS INSTALLED ON FED-EX W/C 27X5706-03.SDR ASAA0640048Skin · dentedOKC - RIGHT INBOARD FORE FLAP DENTED ON LOWER SIDE 14 INCHES FROM INBOARD SIDE 7 INCHES FROM TRAILING EDGE. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737-400 SRM 51-70-10 REPAIR 2. (M)SDR ASAA0640047Skin · dentedOKC - FOUND RIGHT INBOARD AFT FLAP DENTED ON LOWER SIDE 1 INCH FROM TRAILING EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW B737-400 SRM 51-70-10. (M)SDR ASAA0640046Wedge · dentedOKC - RIGHT INBOARD MID FLAP T/E WEDGE DENTED IN SEVERAL AREAS. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW B737-400 SRM 51-70-10. (M)SDR IXXA06SMN053SSupport · crackedDURING ROUTINE C-CHECK INSPECTION, LT FLAP SUPPORT, STA 3.000 CRACKED 4. REMOVED AND REPLACED SUPPORT ASSY AT STA 3.000 (LT FLAP) IAW DC-8 SRM 51-1-21, DC-8 SRM 51-1-20D, DC-8 SRM 51-3-1, OPS CHECK.SDR DHL2006763513Nut Plate · missingS/O 284007 N/R 032195 - LT OUTBD FLAP OUTBD ATTACH FITTING ATTACH POINT HAS MISSING NUTPLATE. REMOVED EXISTING REPAIR DOUBLER, CUT OUT SKIN FOR ACCESS, REMOVED AND REPLACED NUTPLATE. FABRICATED AND INSTALLED REPAIR DOUBLER 10.25" X 4" FROM 2024-T3 .063" IAW ISDR 06FDEA0272Repair · unknownFOUND REPAIR LOCATED RT WS 1574-1604. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUS REPAIR EVALUATED AND FOUND NOT TO CONFORM TO EXISTING SRM REPAIR RT FLAP OUTBOARD REPAIRED PER SRMSDR 06FDEA0271Repair · unknownFOUND REPAIR LOCATED RT WS 1372-1372. REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO EXISTING SRM REPAIR RIGHT WING OUTBOARD FLAP LOWER T/E WSDR SWAA060256Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA060226Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SWA EA.SDR 06FDEA0266Wedge · damagedLEFT OUTBOARD FLAP WEDGE STA XOFH 681 TO STA 747 HAS SEVERAL SKIN REPAIRS WITH LEAKING FASTENERS, AND LARGE AREA OF LEAKING FASTENERS ON TOP SKIN. REMOVED DAMAGED SKIN IAW DC 10 SRM 51-31-01 VOL II. FABRICATED NEW SKIN ASSEMBLY IAW DAC DRAWING ARC1953. INSTSDR 06FDEA0248Skin · unknownLEFT WING OUTBOARD FLAP UPPER SKIN AT STA XOF 563 TO STA XOF 569 FOUND TWO EXTERNAL DOUBLERS. PERFORMED INSPECTION ON REPAIR IAW SRM 57-10-00 FIG 85 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR USAA060096Skin · chafedFOUND RT FLAP IB END L/E CHAFFED. FABRICATED INTERNAL DOUBLER, SKIN PER EA 97228, DEFECT SIZE: 1" BY 1".SDR AWXA200600267Skin · debondedMCN - DURING C19 CHECK DISCOVERED LT INBOARD AFT FLAP, OUTBOARD AFT CORNER SEPARATED FROM WS 170L TO WS 173L. MAINTENANCE REMOVED DAMAGED SKIN ON THE LT INBOARD AFT FLAP OUTBOARD UPPER AFT CORNER IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 202. FABRICATED REPAIRSDR AWXA200600246Skin · delaminatedGYR - DURING C10 DISCOVERED LT TRAILING EDGE FLAP, AFT FLAP AREA, DISBOND AT THE INBOARD END, UPPER SURFACE AT WBL 71.0L. MAINTENANCE REMOVED DELAMINATED PREVIOUS REPAIR PLY, CLEANED AND PREPPED AREA FOR BONDING OF REPLACEMENT REPAIR PLIES IAW BOEING 757-200 SDR AMTA200600032Skin · crackedLEFT WING NR 3 FLAP LEADING EDGE MID AREA FOUND WITH 1 INCH CRACK. REPAIR CARRIED OUT ON LEFT WING NR 3 FLAP LEADING EDGE IAW L1011 SRM 57-54-00 PAGE 804 FIG 802.SDR SWAA060235Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RIGHT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR IXXA06SMN035SSkin · dentedDURING ROUTINE CORRECTIVE ACTION, PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 2Q. REMOVED FASTENERS IAW DC8 SRM 51-1-21. TRIMMED OUT DAMAGED AREA. FABRICATED EXTERNAL REPAIR DOUBLER (AL 2024 T3 0.040) IAW DC-8 SRM 57-2-1 FIG 2Q, DC-8 SRM 57-7-1 FIG 4, TR SDR DHL2006804504Skin · delaminatedLT WING NR 6 FLAP VANE LWR SKIN DELAMINATED. REMOVED AND REPLACED NR 6 LT FLAP VANE IAW MM 27-51-14 PG 201-202. REFER TO NR 044174 FOR OPS CHECK.SDR IXXA06SMN045SSkin · dentedDURING ROUTINE C CHECK INSPECTION, RT WING OUTBOARD FLAP SKIN LWR PART DENTED 1 STA XF 390.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 3), TR NR 57-91 DATED 09-30-01. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED DAMAGED SECTION. FABRICAT
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