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 SWAA101056Flap · puncturedDURING SCHEDULED MV2 CHECK, FOUND RT WING I/B AFT FLAP PUNCTURED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA101053Skin · puncturedDURING SCHEDULED MV2 CHECK, FOUND LT WING O/B FORE FLAP UPPER SURFACED PUNCTURED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA101057Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA101001Flap · puncturedLEFT WING I/B TRAILING EDGE FLAP PUNCTURED. REMOVED AND REPLACED FLAP PER SRM.SDR SWAA101021Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING I/B AFT FLAP LOWER SKIN DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR ASAA1047518Skin · dentedRIGHT I/B AFT FLAP LWR SURFACE DENTED OUT OF LIMITS. REPAIRED RIGHT I/B AFT FLAP LWR SURFACE.SDR IPXA10B58620Skin · dentedLT INBD MID FLAP HAS DENT IN LOWER SURFACE. REPAIRED IAW EO B747-5750-36126-C.SDR SWAA100958Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR USAA2010022290420Skin · debondedPHX - MAJOR REPAIR - B CHECK - LEFT WING INBOARD FOREFLAP UPPER SURFACE DISBONDED AT WBL 117. REPLACED THE LEFT WING INBOARD FORE FLAP IAW TASK CARD R3M27008.SDR ASAA1047594Skin · damagedLEFT WING I/B FOREFLAP LWR SURFACE HAS SEVERAL CLUSTER OF DENTS SOME OF WHICH ARE CREASED AND PUNCTURED. REPAIRED THE LEFT I/B FOREFLAP.SDR SWAA101002Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR IPXA10558602Wedge · damagedINSP TYPE:C2, RT WING INBD MAIN FLAP DAMAGE ON UPPER AND LOWER SURFACE AT INBD T/E WEDGE BOND ASSY. REMOVED DAMAGED SKINS IS APPROX .120" X .7" OF 2024T3 0.020", THICK SKIN ON UPPER SURFACE AND LOWER SURFACE. REPAIR T/E WEDGE IAW SRM 51-70-10-2R.SDR CALA2010022600038Fastener · shearedLEFT WING I/B FLAP, O/B TRACK, AFT FAIRING (572HB), FWD I/B MOUNT BRACKET HAS SHEARED FASTENERS FOR ATTACHMENT TO LOWER SURFACE OF FLAP. REMOVED FITTING, CUTOUT DAMAGE, INSTALLED FREEZE PLUGS, REPAIR STRAPS AND FILLERS REF ECRA 5750-04299.SDR DALA104006314Skin · delaminatedDURING "L" CHECK FOUND DELAMINATION ON RT WING OTBD T/E FLAP LOWER SURFACE. REPAIRED IAW SRM 51-70-07.SDR FDEA201002190455Strap · crackedRT WING OTBD FLAP INBD HINGE TENSION STRAP FOUND CRACKED. RT WING OTBD FLAP INBD HINGE CRACKED TENSION STRAP. R & R WITH A NEW TENSION STRAP IAW EO NR 1-5750-7-5004, REV 3, PART 2. REPAIR CLASSIFIED MINOR REPAIR IAW GMM 6-2-100, REVISION 109.SDR SWAA100932Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP I/B END DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA100930Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWIA201023690Skin · dirtyUNCOMMANDED RIGHT ROLL WITH FLAPS AT 45°. (FLT 1001) RIGGING VERIFIED AND FLAP SURFACES CLEANED.SDR SWAA100904Flap · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR ABXA201003260014Flap · damagedRIGHT I/B FLAT BOTTOM OF TRAILING EDGE HAS 3 FASTENERS PULLED THRU. REMOVED AND REPLACED RIGHT I/B MAIN FLAP IAW 767 AMM 27-51-03-4.SDR SWAA100889Wedge · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING I/B MID FLAP WEDGE DELAMINATED. REPAIRED WEDGE PER AAR EA.SDR SWAA100884Flap · corrodedDURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD FLAP CORRODED. REPAIRED FLAP PER AEM EO.SDR USAA2010022690451Flap · delaminatedSAL - C22 - MAJOR REPAIR - DELAMINATION ON RIGHT WING INBOARD FORE FLAP BETWEEN WBL 170.52 TO WBL 181.52. REPAIRED RIGHT WING INBOARD FORE FLAP BETWEEN WBL 170.52 TO WBL 181.52 IAW B737 SRM 51-70-10.SDR FDEA201002150433Structure · crackedLT INBD MID FLAP LOWER AFT CLOSE OUT CHORD WBL 106 IS CRACKED AT ACT ROD CUTOUT. CUT OUT DAMAGED SECTION DIM 47 1/4 " LONG IAW SRM 51-40-4 FIG 1. FABRICATED LOWER CHORD AND SPLICE IAW SRM 51-40-4 FIG 4. LOCATED AND DRILLED HOLES IAW SRM 51-30-5. INSTALLED LOWSDR FDEA201002150432Skin · crackedRT INBD FORE FLAP, STA 224, CRACK ON THE SKIN, L/E, FWD OF ATTACH FITTING. CUT OUT DAMAGED AREA IAW SRM 57-50-4 FIG 1. FABRICATED DOUBLER AND FILLER IAW SRM 57-50-4 FIG 1. INSTALLED DOUBLER AND FILLER IAW SRM 51-30-2.SDR FDEA201002150426Skin · crackedLT WING INBD FLAP UPPER SURFACE FOUND CRACK ON SKIN. REPAIRED SKIN IAW SRM 57-10-00, FIG 85, SHT 2 & 4 VOL I.SDR IPXA10658584Fairing · delaminatedINSPECTION TYPE:C, RT WING OTBD T/E FLAP MID L/E FAIRING DELAMINATED AT OTEF STA230.5 COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A (1) FIG 5 REV 46.SDR IPXA10658583Fairing · delaminatedINSPECTION TYPE:C, RT WING OTBD T/E FLAP MID L/E FAIRING DELAMINATED AT OTEF STA210. COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A (1) FIG 5, REV 46.SDR SWAA100813Flap · delaminatedDURING SCHEDULED 18Y CHECK, FOUND LT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER MM.SDR IPXA10558520Skin · misrepairedINSP TYPE:C2 PREVIOUS REPAIR TO RT OTBD AFT FLAP AS DOCUMENTED ON EFN 405LPG 1003 REQUIRES REACCOMPLISHMENT AS CALL OUT BY EO B757-5100-3601 STEP (3) REPAIR IS LOCATED 7.5" FROM INBD END AND 10.5" FWD OF T/E LOWER SURFACE. RT OTBD AFT FLAP WAS REPAIRED AT SDR FOTR20006NR2054Structure · crackedRT WING INBD MID FLAP LOWER T/E CHORD CRACKED WBL 100. REPAIRED ON FASI WO 20006, N/R 02054. REMOVED AND REPLACED RT WING INBD MID-FLAP LOWER T/E CHORD SECTION AT WS 100.0 IAW B727 SRM 51-30-5 AND 57-50-2, FIG 5, REV 102. MATERIAL USED: BAC1503-10046 7075-TSDR IPXA10158591Skin · gougedINSP TYPE:3/C LT WING CTR FLAP UPPER SKIN GOUGED 12IN. FWD OF RUB STRIP ABOVE NR 4 FLAP TRACK. REPAIRED IAW SRM 57-50-00 FIG. 205, PARA 4E.SDR USAA2010021590371Skin · crackedCLT - MAJOR REPAIR - Q1 CHECK - LEFT OUTBOARD FOREFLAP LEADING EDGE SKIN CRACKED AT 66 INCHES FROM INBOARD END. REPLACED LEFT OUTBOARD FOREFLAP IAW TASK CARD 03C30727030.SDR AALA20100211TUL13Skin · damagedRIGHT WING FLAPS NUMBER 3 FLAP VANE HAS WEAR MARK ON LEADING EDGE. HOT BOND METAL DOUBLER PER SRM 51-70-02.SDR USAA2010022690449Flap · delaminatedSAL - C22 - MAJOR REPAIR - DELAMINATION ON RIGHT WING INBOARD FORE FLAP BETWEEN WBL 88.32 TO WBL 91.32. REPAIRED RIGHT WING INBOARD FORE FLAP BETWEEN WBL 88.32 TO WBL 91.32 IAW B737 SRM 51-70-10.SDR IPXA10658536Hinge Fitting · crackedINSPECTION TYPE:6C, LT WING - INBD MAIN FLAP INBD HINGE FTG FOUND CRACKED. LT WING - INBD MAIN FLAP HINGE FTG, REPAIRED IAW SRM 57-53-02-2R1, FIG 201, REF 46, ORIGINAL MATERIAL IS 7075T73 FORGING, CRACK LENGTH AT INBD FLANGE IS 1", OTBD FLANGE IS 0.9", DAMSDR IPXA10658535Hinge Fitting · crackedRT WING - INBD MAIN FLAP INBD HINGE FTG FOUND CRACKED. RT WING INBD MAIN FLAP INBD HINGE FTG REPAIRED IAW SRM 57-53-02-2R1, FIG 2 201, REV 46 ORIGINAL MATERIAL IS 7075T73 FORGING, CRACK LENGTH INBD FLANGE IS 1.125" & OTBD FLANGE IS 1.25", DAMAGED CUTOUT SIZE SDR AALA20100210TUL11Skin Panel · corrodedCORROSION AT AFT EDGE FASTENER ROW OF INTERSPAR UPPER SKIN PANEL 52 INCHES FROM INBOARD END OF LEFT HAND MAIN INBOARD FLAP. REPAIRED CENTERBORE HONEYCOMB THAT WAS REMOVED TO SHOOT EXTERNAL DOUBLER POTTED CENTERBORE AND HOT BONDED DOUBLER PER SRM 51-70-10-2R PSDR AALA20100210TUL10Flap · corrodedCORROSION AT TOP SIDE OF INBOARD FLAP. LOCATED AT MID SEAM BETWEEN FASTENERS 2 INCHES FROM TRAILING EDGE AT INBOARD END. REPORTED CENTERBORE HONEYCOMB THAT WAS REMOVED TO SHOOT EXTERNAL DOUBLER POTTED CENTERBORE AND HOT BONDED DOUBLER PER SRM 51-70-10-2R PARASDR TIMA2010000014Skin · crackedLIB FLAP CRACKED.SDR FOTR20006NR2031Skin · debondedLT INBD AFT FLAP LOWER SURFACE HAS DISBONDED AREA AT WBL 135. REPAIRED ON ASI WO 20006, N/R 02031. INSTALLED HOT BONDED REPAIR TO LEFT INBD AFT FLAP LOWER SURFACE AT WBL 135 IAW B727 SRM 51-40-20, PARA 20 AND 51-40-23, REV 102. MATERIAL USED: CORE; 5052-4.4-SDR SWIA201023686Flap · crackedLEFT NACELLE FLAP OUTBOARD EDGE CRACKED. (C CHECK) REPLACED FLAP PER AMM.SDR SWAA100862Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RIGHT WING I/B AFT FLAP O/B TRAILING EDGE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR UALA2010021100517Skin · chafedRT WING INBD FORE FLAP UPPER SKIN CHAFING ON THE NR 8 SPOILER PANEL. REPAIRED RT INBD FORE FLAP UPPER SKIN IAW REO G-13248. THE REPAIR IS A MAJOR REPAIR AND RECEIVED STG 1 APPROVAL FROM BAC VIA FAA FORM 8100-9. THE COMPLIANCE OF 14 CFR 25.571 AND 26.43 HAS NSDR FDEA201002090374Skin · dentedLT WING OTBD FLAP L/E APPROX 24" FROM OTBD EDGE IS DENTED. EVALUATED DENT FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01 FIG 101. REPAIRED LT WING OB FLAP L/E IAW SRM 57-53-01, FIG 201 REPAIR NR 2.SDR AALA20100208TUL09Skin · corrodedSEVERAL AREAS OF CORROSION FOUND ON UPPER SURFACE OF UPPER FLAP SKIN ALONG AFT ROW OF FASTNERS. INSTALLED DOUBLER COUNTER BORED HONEYCOMB FROM INSIDE OF FLAP TO SHOOT RIVETS OF DOUBLER. REPAIRED HONEYCOMB POTTING AND HOT BONDED DOUBLER PER SRM 51-70-10-2R PASDR FOTR20006NR2021Skin · puncturedRT WING OTBD FORE FLAP HAS SEVERAL GOUGES. REPAIRED ON FASI W/0 NR 20006, N/R 02021" INSTALLED REPAIR DOUBLER TO RT WING OTBD FORE FLAP AT WS 465 IAW SRM 57-50-2 FIG 4 AND 57-50-4 FIG 1, REV 102. MATERIAL USED; 2024-T3, DIM.; 3.5" X 3.75" X 0.063".SDR FOTR20006NR2011Skin · delaminatedRT WING OTBD AFT FLAP IS DELAMINATED AT STA WBL 338. REPAIRED ON FASI W/O NR 20006, N/R 2011 INSTALLED HOT BONDED REPAIR TO RT WING OTBD AFT FLAP AT WBL 228 IAW SRM 51-40-20 PARA 7 AND PARA 20 REV 102. MATERIAL USED: 7075-T7, 0.012". DIM ; FILLER; 1" X 4", DOUSDR A6WA201040107Fitting · chafedLT OB FLAP HINGE BOX AFT FITTING CHAFED. REPAIRED LT WING OTBD FLAP OB HINGE BOX AFT HINGE FITTING IAW REO 601R-57-21-1232.SDR SWAA100783Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.
Back to JASC 5753