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 FDEA202401220094Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED SDR FDEA202401220093Hinge Bracket · corrodedLEFT WING- WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING- WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-07. REPAIR BUSHING FABRICATED BY MACHININSDR ASAA2024012149589Skin · dentedRH FLAP HAS MULTIPLE DENTS BEHIND MAIN WHEELS, MEASURE AND MAP ALL. GROUNDED - YES. PREFORMED PERMANT CAT A REPAIR TO R/H FLAP, MULTIPLE DENTS BEHIND MAIN WHEELS. DAMAGE AREA 1 LOCATED 51.3Ï¿½ FROM I/B END CUT OUT SIZE WAS 10 X 9 UPPER AND 9.9 X 8.8 LOWER. REPSDR AALA202402238899Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING OUTBOARD TRAILING EDGE FLAP EXTERNAL DOUBLER AT FLAP TRACK #4, BETWEEN RIBS 14 AND 15. REPLACED DOUBLER PER SRM 57-53-21-300-003 .SDR IPXA2024012227720Cap · crackedFAULT - CRACK, LH WING OUTBD FLAP END CAP. (REPAIR). PERFORMED NDT/UT FOR REWORKED AREA PLUS 6'' AROUND HEATED AREA I.A.W. 767 NTM PART1 51-01-01 REV:136. RESULT:NO DEFECT FOUND. 1.REMOVE THE DAMAGE MATERIALS (L:0.3", W:0.05", AT LEFT HAND OUTBOARD FLAP INBOARSDR IPXA2024012227663Skin · damagedFAULT - CHIP SKIN, LH WING INBD MAIN FLAP OUTBD UPR SEAL LE AREA. (REPAIR). 1. REMOVE THE UNWANTED MATERIALS AND CLEAN AT LEFT HAND WING INBOARD MAIN FLAP OUTBOARD UPPER SEAL LEADING EDGE AREA. AND TRIM OUT THE DAMAGE AS REQUIRED, KEEP A MINIMUM 0.5 IN CORNER SDR DALA2024012200912Bolt · corrodedSHIP 3124 CORROSION ON NUT FLAP CARRIAGE BOLT OF TRACK 2 AND MISSING PIN INDICA TOR OF FLAP TRACK 1 ON R/H WING. CORRECTIVE ACTION: REPLACED NUT OF FLAP CARRIAGE BOLT OF TRACK #2 AND INSTALLED NEW PIN INDICATOR OF TRACK #1 ON RH WING PER AMDS CARD 2750-6010-RTSDR DALA2024012200911Bolt · corrodedSHIP 3124 CORROSION ON ECCENTRIC BOLT (1 E/A) AND PLAIN BUSHING (1 E/A) LOC. ON DRIVE ARM TRACK 3 O/B FLAP R/H WING. CORRECTIVE ACTION: REPLACED ECCENTRIC BOLT (1 E/A) AND PLAIN BUSHING (1 E/A) LOC. ON DRIVE ARM TRACK #3 O/B FLAP R/H WING AS PER AIRBUS CMM 57-SDR DALA2024011900813Track · corrodedSHIP 3124 CORROSION ON ECCENTRIC BOLT (1 E/A) AND PLAIN BUSHING (1 E/A) LOC. ON DRIVE ARM TRACK 4 O/B FLAP R/H WING. CORRECTIVE ACTION: REPLACED EXCENTRICAL BOLT AND PALIN BUSHING OF DRIVE ARM TRACK #4 OUTBOARD FLAP RH WING AS PER AIRBUS CMM 57-53-21. (0161140SDR CALA2024012200163Skin · crackedR/H OUTBOARD MAIN FLAP OUTBOARD LOWER SKIN CRACK REPAIR ON ST ENGINEERING NON ROUTINE 86900 AS PER SRM 57-53-01-2R-4 REPAIR 4 REQUIRES DIP TO REINSPECT BLIND FASTENERS EVERY 3000 FLIGHT CYCLES. IF ANY EVIDENCE OF PULLED OR LOOSE RIVETS, THE RIVETS MUST BE REPLSDR IXXA2024030602Fairing · gougedRIGHT WING, OUTBOARD FLAP, OUTBOARD FLAP TRACK, MID FAIRING TRAILING EDGE IS IN CONTACT WITH GREASE FITTINGS AND IS GOUGEDSDR REXA2024102901096Panel · chafed"L/H WING FLAP PANELS 584HT AND 584ET HAVE CHAFFING AND PAINT DAMAGE. BLENDED AND GRID CHAFFED AREA ON L/H WING FLAP PANELS 584HT AND 584ET ALLOWABLE DAMAGE 0.015"" IAW CRJ900 SRM 57-53-01-101-001-A02. PANEL 584HT FOUND TO BE IN LIMITS ORG. .050"", REMAINING .SDR IPXA2024022786634Support · damaged*** SUPPLEMENTAL SDR *** (STR) RH WING O/B FLAP I/B FWD HINGE FAIRING SUPPORT STRUCTURE LWR SIDE SUPPORT PLATE HAS ELONGATED HOLES. 74-076 INSTALLED ON R/H WING O/B FLAP I/B FWD HINGE FAIRING SUPPORT STRUCTURE LWR SIDE SUPPORT PLATE IN REF MD-11 SRM 51-35 01SDR IPXA2024021686641Support · cracked(STR) RH WING O/B FLAP I/B FWD HINGE FAIRING SUPPORT STRUCTURE FWD SIDE SUPPORT PLATE HAS CRACKED. 74-077 INSTALED ON R/H WING O/B FLAP I/B FWD HINGE FAIRING SUPPORT STRUCTURE FWD SIDE SUPPORT PLATE IAW MD-11 SRM 51-33-01-0G-0 AND 51-35-01-0G-0.SDR DALA2024011700737Bearing · unknownSHIP 3361 RIGHT FLAP TRACK NO.2 REAR LINK - REPLACE BOTH UPPER AND LOWER SPHERICAL BEARINGS PER EO 2754-01029-01-2R. CORRECTIVE ACTION: REMOVED AND REPLACED BOTH UPPER AND LOWER SPHERICAL BEARINGS PER EO2754- 01029-01-2R. (0157626)SDR IPXA2024011747664Skin · cracked*** SDR FILED OPEN *** FAULT - CRACK - SKIN, LH WING NO.1E VC FLAP PANEL OUTER SURFACE (REPAIR) I.A.W AMM 27-81-02-004-001 REV 109 REMOVE #1E V.C FLAPSDR IPXA2024011786634Support · damaged*** SDR FILED OPEN *** (STR) RH WING O/B FLAP I/B FWD HINGE FAIRING SUPPORT STRUCTURE LWR SIDE SUPPORT PLATE HAS ELONGATED HOLES. 74-076 APPROVEDSDR IPXA2024011786641Support · cracked*** SDR FILED OPEN *** (STR) RH WING O/B FLAP I/B FWD HINGE FAIRING SUPPORT STRUCTURE FWD SIDE SUPPORT PLATE HAS CRACKED. 74-077 APPROVEDSDR SWAA2024022741361Skin · debondedCUSTOMER REQUEST- DEBONDED OB AFT FLAP IB SIDE AT LT WING 2024-68634<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:15120589 DUE DATE:13-FEB-24;[02] REPLACED SERVICEABLE O/B AFT FLAP AT LT WING AND WILL BE INSTALLED IN TTG8Q00QXWHA;[03] REPLACED SERVICEABLE O/B AFSDR K11A2024012400252Skin · delaminatedLH WING IB AFT FLAP IB SECTION HAS DELAMINATION.SDR SWAA2024011741470Skin · damagedLEFT WING; AFT FLAP; INBOARD SIDE HONEYCOMB EXPOSED. REPLACED LT OUTBOARD AFT FLAP REF AMM 27-51-22-400-801.SDR SWAA2024022340914Skin · delaminatedL/W OUB AFT FLAP INB LOWER T/E SPOT DELAMINATE 7INC FROM I/B EDGE AND 3INC. FROM TRAILING EDGE MKD DOT<[01] REPLACED L/W OUB AFT FLAP IN REF B737 AMM 27-51-22-400-801 AND ACCOMPLISHED L/W OUTBOARD AFT FLAP ADJUSTMENT /CHECK PER B737 AMM 27-51-22-400-801-NG CALSDR GTIA2024011537777Flap · damagedBROKEN COMPOUND ON TRAILING EDGE INBOARD FLAP RH WING. RAF 3337355-01 GENERATED. SDR GENERATED. -REPAIRED TRAILING EDGE IB FLAP RH WING IAW EA #57-0002-24 PART 1 PART A AND EC EA #5752-2405SDR REXA2024102901095Panel · chafed"L/H WING FLAP PANELS 584LB, 584JB, 584EB, AND 584GB HAVE CHAFFING AND PAINT DAMAGE. BLENDED AND GRIDDED CHAFED AREA ON 4EA L/H WING FLAP ACCESS PANELS 584LB, 584JB, 584EB, AND 584GB IAW CRJ900SRM 51-12-00-001-001-A01. PANELS 584LB, 584EB AND 584GB FOUND TO BESDR FDEA202401120072Skin · delaminatedLH WING OUTBOARD FLAP LEADING EDGE WITH DELAMINATION AT OTEF STA 72 LH WING OUTBOARD FLAP LEADING EDGE AT OTEF STA 72 WAS REPAIRED IAW B767 SRM 57-53-01- 2R REP 1 FIG 201 SHEET 1-3-5-6 PAGE 1-6 AND SRM 51-70-03-0G PAR 5A FIG 5 PAGE 19-36. REV 88 DEC 15/ 202SDR SWAA2024030540163Attach Fitting · crackedLT WING IB FLAP OB ATTACH FITTING WITH CRACKED AFT IB RUB PLATE.<[01] REMOVED AND REPLACED TRANSMISSION #3 INBOARD FLAP AFT RUB PLATE REF SRM 51-40-02-0G-0 AND AMM 27-51-13-400-803. TORQUE 175289; DUE DATE 31/07/24.<BR>OPERATED TRAILING EDGE FLAP SYSTEM WITH PSDR IPXA2024021092062Skin · crackedTHE R/H CENTER FLAP HAS 1 EA CRACK AT RIB 27 AFT SIDE ON STR 2.1. ACCOMPLISH PERMANENT REPAIR PER EA 300-5750-27-A3483 REV. - AND EO-89185-REQ1.SDR IPXA2024012382163Cap · crackedFAULT - CRACK EDGE, LH WING OUTBD FLAP INBD SIDE END CAP (REPAIR). REMOVE THE DAMAGE AREA (L:0.2", W:0.1 , 5" FROM AFTER EDGE AT LOWER EDGE) AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURE AT 200°F FOR 220 MINUTES KEEP A MINIMUM VACUUM OF 22 IN/HG I.A.W. UPSSDR AALA202401120581Bearing · out of adjustAIRCRAFT IN BASE MAINTENANCE: DURING POST CHECK TEST FLIGHT IT WAS REPORTED BY THE FLIGHT CREW THAT THE AIRCRAFT FLYS RIGHT WING LOW WITH 1.8 ROLL. MAINTENANCE ADJUSTED THE LEFT WING FLAP TRACK #4 FORWARD ECCENTRIC BEARING PER AMM 27-51-00-820-008-A.SDR DALA2024011200530Unknown · unknownSHIP 3052 EXCESSIVE PLAY BEARING INTERCONNECTING STRUT OB FLAP ON RH WING. CORRECTIVE ACTION: R/R INTERCONNECTING STRUT OB FLAP ON RH WING MPN: D5757030501600 SN: A22442 PER A321 AMM 27-51-44. DELTA PART NUMBER 30-2751-9-0002. OK FOR SERVICE. (0149282)SDR DALA2024011200529Unknown · unknownSHIP 3052 CORROSION INTERCONNECTING STRUT IB FLAP ON LH WING. CORRECTIVE ACTION: R/R INTERCONNECTING STRUT OB FLAP ON LH WING MPN: D5757030501600 SN: A22849 PER A321 AMM 27-51. DELTA PART NUMBER 30-2751-9-0002. OK FOR SERVICE. (0149285)SDR DALA2024011200521Unknown · unknownSHIP 3124 EXCESSIVE PLAY OB LINK FLAP TRACK 2 AND FLAP TRACK 3 ON RH WING. CORRECTIVE ACTION: INSTALLED NEW WASHER OB LINK FLAP TRACK 2 AND FLAP TRACK 3 ON RH WING AS PER A320 FAM AMM 57-55-11-000-001-A. (0150056)SDR IPXA2024011182163Unknown · unknown*** SDR FILED OPEN *** FAULT - CRACK EDGE, LH WING OUTBD FLAP INBD SIDE END CAP (REPAIR) OK TO WORKSDR ASAA2024011047833Skin · dentedLESSOR REQUEST #732: EXISTING REPAIRED DENTS ( GRID PHOTO) ON RH WING INBOARD FLAP LOWER SKIN T/E. MENTION REPAIR CAT. AND PN/SN OF FLAP GROUNDED - YES. REPAIRED RH WING INBOARD FLAP LOWER SKIN T/E. REPAIR STARTS 47" FROM INBOARD TO OUTBOARD AND STOPS AT 62.5SDR ASAA2024011047512Skin · dentedLESSOR REQUEST #731: EXISTING REPAIRED DENTS REQUIRE GRID & PHOTO ON LH WING INBOARD FLAP LOWER SKIN T/E. MENTION REPAIR CAT. AND PN/SN OF FLAP. GROUNDED - YES. REPAIRED LH WING INBOARD FLAP LOWER SKIN T/E. REPAIR STARTS 46" FROM INBOARD TO OUTBOARD AND SDR DALA2024011000402Unknown · unknownSHIP 3161 5 DENTS RH I/B LOWER FLAP. CORRECTIVE ACTION: REPAIRED PER A319 SRM 57-52. (5374493)SDR DALA2024011000399Unknown · unknownSHIP 3124 EXCESSIVE PLAY ON BEARING OF INTERCONNECTING STRUT BRACKET ON I/ B FLAP R/H WING (1 E/A). CORRECTIVE ACTION: REPLACED BEARING (1E/A) ON INTERCONNECTING STRUT BRACKET ON I/B FLAP RH WING AS PER A319 AMM 57-51. (0146902)SDR DALA2024011000398Unknown · unknownSHIP 3124 EXCESSIVE PLAY ON BEARING OF INTERCONNECTING STRUT BRACKET ON I/ B FLAP L/H WING (1 E/A). CORRECTIVE ACTION: REPLACED BEARING (1E/A) ON INTERCONNECTING STRUT BRACKET ON I/B FLAP L/H WING AS PER A319 AMM 57-51. (0146896)SDR IPXA2025030425657Plate · gougedRH WING I/B FLAP O/B STOP PLATE IS GOUGED. REMOVED AND REPLACED RT WING I/B FLAP O/B STOP PLATE IAW SRM 51-31-01 ADJUSTMENT CHECKED ON THE R/H I/B FLAP VANE TRAILING EDGE, TO I/B FLAP TRAILING EDGE CHECKED GOOD IN REF TO MD11 AMM 27-50-22-830-801.SDR IPXA2024021625559Plate · gougedSTR-WING I/B FLAP IB STOP PLATE IS GOUGED MARKED 84-19 REMOVE AND REPLACE STOP PLATE STR-WING I/B IB REF MD 11 SRM 51 -31-01SDR IPXA2024021331952Skin · dentedLH WING INBD FLAP LWR SURFACE SHOWS SOME DENT EVALUATE DOT 146-031 APPLY AERODYNAMIC FILLER ON LOWER SURFACE IAW SRM 57-50-00. TREATED AND PRIMED AREA IAW SRM 51-21-10. APPLIED TOP COAT ON AREA IAW SRM 51-75-10, CUP PAINT #02-012-176.SDR IPXA2024021331737Skin · dentedWING RIGHT I/B FLAP HAS SOME DENTS AT LOWER SURFACE.DOT119-008 APPLY AERODYNAMIC FILLER ON LOWER SURFACE IAW SRM 57-50-00. TREATED AND PRIMED AREA IAW SRM 51-21-10. APPLIED TOP COAT ON AREA IAW SRM 51-75-10, CUP PAINT # 02-012-176SDR IPXA2024010931952Unknown · unknown*SDR FILED OPEN* FAULT-LH WING INBD FLAP LWR SURFACE SHOWS SOME DENT EVALUATE DOT 146-031SDR IPXA2024010931737Unknown · unknown-WING RIGHT I/B FLAP HAS SOME DENTS AT LOWER SURFACE.DOT119-008SDR IPXA2024010925657Unknown · unknown*SDR FILED OPEN* RH WING I/B FLAP O/B STOP PLATE IS GOUGED..MARKED 84-20 APPROVEDSDR IPXA2024010925559Unknown · unknownSTR-WING I/B FLAP IB STOP PLATE IS GOUGED MARKED 84-19 APPROVEDSDR DALA2024010900362Unknown · unknownSHIP 3035 R/H O/B MAIN FLAP I/B GUIDE ROLLER IS DAMAGED. CORRECTIVE ACTION: REPLACED RH O/B MAIN FLAP I/B GUIDE ROLLER PER A321 CMM 57-55-21 AND PER A321 AMM 20-21-11 AND ADJUSTMENT CHECK GOOD PER 321 AMM 27-54-62-400-002-A STEP 4.L(1) THRU (2)(G) OPS CHECK GOSDR R3WA2024010800010Skin · delaminatedRH O/B FLAP TRAILING EDGE OF FLAP FOUND TO HAVE DELAMINATION SEPARATION AFTER POST FLIGHT INSPECTION.SDR VNAA202401220006Skin · nickedSEVERAL NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5. SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5, WERE BLENDED OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND WERE EVALUATE AREA BTW FLS 30.00 TO FLS 65.5 IS WISDR IPXA2024010804105Unknown · unknownGOUGED SKIN, RH WING INBD MID FLAP TE UPR FXD PNL LWR SURFACE, WBL 443 (REPAIR)
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