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 KCSA202305111046Access Panel · corrodedFLAP PANEL 578IT HAS EVIDENCE OF CORROSIONSDR FDEA202305100841Panel · delaminatedL/WING IB FLAP LWR SURFACE OF CLOSE OUT FAIRING IS DELAMINATED. ACCOMPLISHED PERMANENT REPAIR OF DELAMINATION ON LOWER SURFACE OF L/W INBRD MAIN FLAP AFT FLAP CLOSE OUT IAW B757 SRM 57-53-01-2R FIG 201 SHEET 6 AND 51-70-07-0GSDR IPXA2024112473815Skin · dentedR/H WING INBD AFT FLAP HAS A DENT 45€? FROM INBD EDGE AND 3€? UP FROM T/E. REPAIRED REF EO-92162-REQ1. THIS CLEARS DEFERRAL. OK FOR CONTINUED SERVICESDR IPXA2023051993278Skin · damagedINSPECTION TYPE:1C*** MAJOR REPAIR *** L/H I/B FLAP LOWER SKIN IS DAMAGED BETWEEN STA YIFH=7.6 AND YIFH=-6.00, 66-INCH FROM I/B SIDE.REPAIRED DAMAGED SKIN AT THE L/H I/B FLAP BETWEEN STA YIFH=7.6 AND YIFH=-6.00, 66-INCH FROM I/B SIDE IAW SRM 57-00-01-2R-1 REPASDR FDEA202305090835Skin · delaminatedDURING INSPECTION, FOUND EXISTING SKIN REPAIR AND SURROUNDING AREA DELAMINATED ON THE LW O/B AFT FLAP UPPER SKIN, I/B END. ACCOMPLISHED PERMANENT REPAIR OF DELAMINATED SKIN ON THE INBRD UPPER SURFACE OF THE LEFT WING OTBRD AFT FLAP IAW B757 SRM 57-53-01-2SDR SWAA2023052546231Strip · elongated#6 FLAP SUPPORT FAIRING O/B MIDDLE SEAL FASTENER HOLES ARE ELONGATED & REQUIRE PERMANENT REPAIR.<[01] REPAIRED ELONGATED HOLES AND FABRICATED EXTERNAL STRIP PER SRM 57-53-70-2R-2.;[02] VERIFIED REPAIRED ELONGATED HOLES AND FABRICATED EXTERNAL STRIP PER SRM 57-SDR CALA2023050501366Seal · missingPDA 2 LEFT I/B FLAP, O/B BULB SEAL IS MISSING FROM TRACK. SEAL MISSING IS ROUGHLY 24IN LONG. NEEDS LOWER BULB SEAL M&E 42-2751-3-0005, REF IPC 27-51-11-01. ALTERNATE P/N FOR LOWER BULB SEAL IS 113A2100-13 , M&E ITEM # 335. MF PN# 113A2172-603. 29-2751-3-0023. SDR SWAA2023052445612Flap · delaminatedLEFT WING OUTBOARD AFT FLAP HAS A LARGE AREA OF DELIMITATION ON THE INBOARD LOWER SURFACE. (PIC ATTACHED)<[01] REMOVED AND REPLACED OUTBOARD AFT FLAP IAW AMM 27-51-22. SEE STEPS 1-3 FOR INDIVIUAL SIGN OFFS.;[02] INSPECTED WORK PERFORMEDSDR DALA2023050703550Unknown · unknownAIRCRAFT 3121, CORROSION INTERCONNECTING STRUT IB FLAP ON LH WING (REFER TO AMDS CARD 2751-9202 RII). CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT IB FLAP ON LH WING ON SERVICEABLE CONDITION AS PER A320 FAM AMM 27-51-44-000-001-A AND AMM27-51- 44-400-001-SDR FDEA202305040811Flap · dentedDENTS ON INBOARD FLAP UPPER SURFACE NEXT TO INBOARD EDGE. RH WING AFT FLAP-INBOARD TRAILING EDGE FLAP, UPPER SURFACE, DENTS 1,6 WERE FOUND WITHIN ALLOWABLE DAMAGE LIMITS AND DENTS 2,3,4,5 OUT OF LIMITS WERE REPAIRED IAW SRM B767 57-53-01-1A FIG. 101 TABLESDR FDEA202305040810Flap · dentedRIGHT WING OUTBOARD FLAP, LOWER SURFACE WITH DENTS AT 4-3" FROM LOWER EDGE AND 25" FROM INBOARD FAIRING FLAP. RH WING, OUTBOARD FLAP, LOWER SURFACE AT 3-4" FROM LOWER EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REP. 1 FIG. 201 SHEET 1 AND SRM 51-70-17-0G PASDR FDEA202305040808Flap · dentedRIGHT WING OUTBOARD FLAP, LOWER SURFACE WITH DENT AT 12" FROM LOWER EDGE AND 39" FROM INBOARD FAIRING FLAP. RH WING, OUTBOARD FLAP, LOWER SURFACE AT 12" FROM LOWER EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REP. 1 FIG. 201 SHEET 1 AND SRM 51-70-17-0G PAR. SDR FDEA202305040807Flap · dentedRIGHT WING OUTBOARD FLAP, LOWER SURFACE WITH DENT AT 8-10" FROM LOWER EDGE AND 55" FROM INBOARD FAIRING FLAP. RH WING, OUTBOARD FLAP, LOWER SURFACE AT 8-10" FROM LOWER EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REP. 1 FIG. 201 SHEET 1 AND SRM 51-70-17-0G PSDR FDEA202305040806Flap · dentedRIGHT WING OUTBOARD FLAP, LOWER SURFACE WITH DENT AT 7" FROM LOWER EDGE AND 77" FROM INBOARD FAIRING FLAP. RH WING, OUTBOARD FLAP, LOWER SKIN WAS REPAIRED IAW B767 SRM 57-53-01-2R REP. 1 FIG. 201 SHEET 1 AND SRM 51-70-17-0G PAR. 4.A. REV. 85 DEC15/2022SDR FDEA202305040805Flap · dentedRIGHT WING OUTBOARD FLAP LOWER SURFACE WITH DENT AT 11" FROM LOWER EDGE AND 71" FROM OUTBOARD FAIRING FLAP. RH WING, OUTBOARD FLAP, LOWER SKIN AT 11" FROM LOWER EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REP. 1 FIG. 201 SHEET 1 AND SRM 51-70-17-0G PAR. 4.ASDR SWAA2023060245104Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 233 AT LT WING 2023-295510<[01] REPLACED CORRUGATED PLATE LOC. TRAILING EDGE ORSS 233 AT LT WING AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG: 115A3700 SHEET: 39 REV: - SEE INDIVIDUAL SIGN OFF BELLOW;[02] REPLACEDSDR AALA202307180736Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION RIGHT WING OUTBOARD TRAILING EDGE FLAP LOWER SURFACE REINFORCING DOUBLER FOR #4 FLAP TRACK. REPLACED DOUBLER PER SRM 57-53-21-300-003SDR GTIA2023050437156Rib · wornWEAR ON OB FLAP INTERCONNECTING STRUT RIB ON R/H WING. RAF-01 3057626-01 GENERATED-PERFORMED PERMANENT REPAIR ON OB FLAP INTERCONNECTING STRUT RIB ON RH WING IAW EA 57-0145-23 REV 0 THIS REPAIR IS CAT ASDR IPXA2023050293087Hinge · corrodedINSPECTION TYPE:C3L/H I/B FLAP O/B FWD HINGE #3 LUG O/B FACE HAS CORROSIONREPAIRED L/H FLAP O/B HINGE # 3 LUG O/B FACE AT STA XW 254 YW 495.961 AND ZW -28.941 IAW VTSAA EA 011-5740-01A9922 IR, DATED 04/28/2023 AND UPS EO MD11-5740-86661-A. MINORSDR IPXA2023050293085Hinge · corrodedINSPECTION TYPE:C3FLAP L/H I/B FLAP O/B FWD HINGE #3 LUG I/B FACE HAS CORRODIONREPAIRED L/H I/B FLAP O/B FWD HINGE #3 LUG I/B FACE IAW VTSAA EA 011-25740-A9922 IR, DATED 04/28/2023 AND UPS EO MD11-5740-86661-A MINORSDR IPXA2023050293088Hinge · corrodedINSPECTION TYPE:C3R/H I/B FLAP O/B AFT HINGE #6 LUG BORE HAS CORROSIONREPAIRED R/H I/B FLAP O/B HINGE #6 BORE AT STA XW -254 YW 495.96 AND ZW -28.941 IAW VTSAA EA 011-5752-01-A9924 IR DATED 04/28/2023 AND UPS EO MD11-5750-86671-A. MINORSDR SWAA2023053043797Support · crackedBULB SEAL RETAINER SUPPORT IS CRACKED AT LEFT WING FIXED T/E PANEL JUST AFT OF THE PYLON. MARKED<[01] REMOVED CRACKED BULB SEAL RETAINER SUPPORT CRACKED AT LEFT WING FIXED T/E PANEL JUST AFT OF THE PYLON AND INSTALLED NEW RETAINER PART NUMBER 115A2953-1 SAME LSDR CALA2023051201484Fairing · missingRIGHT WING NO. 6 FLAP TRACK AFT FAIRING FWD LH ATTACH PLATE IS MISSING. SEE PIC AFT FLAP TRACK FAIRING REMOVED. FLAP TRACK FAIRING REMOVED PER CDL27C 486,DELIVERED TO LAX STORES RIGHTWING #6 AFT FLAP FAIRING, ADD EMP:U107479,U232924 DISPATCH DESK: 3355 TOMC APSDR SWAA2023053043455Angle · crackedRT WING FIXED TE UPPER PANEL; VERTICAL BULB SEAL RETAINER ANGLE CRACKED; DIRECTLY AFT OF THE PYLON; MARKED.<[01] THERE IS NO SRM ALLOWABLE DAMAGE FOR RT WING FIXED TE UPPER PANEL; VERTICAL BULB SEAL RETAINER ANGLE CRACK. PART TO BE REPAIRED BY REPLACEMENT IAW SDR SWAA2023061343153Plate · elongatedLEFT WING REAR SPAR WIGGLE PLATE LOOSE WITH ELONGATED HOLES AT RSS 261.(51-001)<[01] REMOVED AND REPLACED WIGGLE PLATE AT LEFT WING REAR SPAR RSS 261 REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2023061342526Panel · crackedL/H WING T/E ACCESS PANEL 561AB INTERNAL SKIN SURFACE HAS CRACKS AROUND MULTIPLE FASTENER HOLES.<[01] MEASUREMENT;[02] CLEANED AND PREPARED AREA AT L/H WING ACCESS PANEL 561AB; REPAIRED DAMAGE AREAS AT L/W ACCESS PANEL #561AB AS PER SRM 51-70-04-2R-9 .MATERIALSDR SWAA2023061342527Panel · crackedL/H WING T/E ACCESS PANEL 561CB INTERNAL SKIN SURFACE HAS CRACKS AROUND MULTIPLE FASTENER HOLES.<[01] APPLIED REPAIR ON DAMAGED AREA AT ACCESS PANEL #561CB AS PER B737 SRM 51-70-04-2R-9; MATERIAL USED CAB PO# 1776837 AND RESIN PO#1800550 AND CLOTH PO#1738579.;SDR SWAA2023061343149Panel · crackedL/H WING T/E ACCESS PANEL 561BB INTERNAL SKIN SURFACE HAS CRACKS AT MULTIPLE FASTENER HOLES.<[01] REPARED ACCESS PANEL #561BB AS PER B737 SRM 51-70-04-2R-9; MATERIAL USED RESIN PO#1800550 AND CLOTH PO#1738579.;[02] VERIFIED STEP 1SDR SWAA2023053042204Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE IRSS 230 RT WING 2023-282698<[01] REPLACED CORRUGATED PLATE LOC. TRAILING EDGE IRSS 230 RT WING I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG 115A2001; SHEET 30; REV. A. SEE INDIVIDUAL SIGN-OFF BELOW.;[02] JOB COMPLETED.SDR SWAA2023053042205Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 272 RT WING 2023-282699<[01] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 272 RT WING IAW B737-700 SRM 51-40-02 AND DWG 115D2001; SHEET 1; REV B. SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] STEP 1 CORRECTED<BR>REPLACED CORRUGSDR SWAA2023053042206Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 272 LT WING 2023-282701<[01] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 272 RT WING IAW B737-700 SRM 51-40-02 AND DWG 115D2001; SHEET 32; REV -. SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] CORRECTED STEP 1: REPLACED CORRUGASDR SWAA2023053042207Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE IRSS 216 LT WING 2023-282700<[01] REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 216 LT WING IAW B737-700 SRM 51-40-02 AND DWG 115D2001; SHEET 1; REV B. SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] STEP 1 CORRECTED<BR>REPLACED CORRUGSDR SWAA2023050141387Flap · delaminatedLH WING OB AFT FLAP IB LOWER SURFACE DELAMINATED.<[01] REMOVED L/H OUTBOARD AFT FLAP;[02] INSTALLED REPLACEMENT LH OTB AFT FLAP REF MM 27-51-22SDR DALA2023042903344Unknown · unknownAIRCRAFT 3121, CORROSION FLAP TRACK 3 AND 4 CARRIAGE BOLT ON LH WING (2 EA). CORRECTIVE ACTION: REPLACED FLAP TRACK 3 AND 4 CARRIAGE BOLT ON L/H WING. (LP 2738838)SDR IPXA2023050893151Skin · crackedINSPECTION TYPE:CRH CENTER FLAP HAS A CRACK AT RIB26REPAIRED PER EO A300-5750-86793-ASDR CALA2023042601252Support Beam · damagedLH WING #3 FLAP SUPPORT TENSION BEAM DAMAGE TO THE LH WING #3 FLAP SUPPORT TENSION BEAM ASSY., P/N 113W1360- OF EC/RA 2751-01871 ON OR BEFORE 13 APRIL 2025 OR BEFORE REACHIN 601 S/N 9000, CENTER BEAM, P/N 113W1361-9 PER THE LATEST REV. G 5000 TOTAL FLIGHT CYCLSDR IXXA2023042401Flap · delaminatedRW OB FLAP LOWER SURFACE DELAMSDR DALA2023042903342Unknown · unknownAIRCRAFT 3121, CORROSION FLAP TRACK 2 CARRIAGE BOLT ON RH WING (1 EA). CORRECTIVE ACTION: REPLACED FLAP TRACK 2 CARRIAGE BOLT ON R/H WING AND INSTALLATION. (LP 2733776)SDR FDEA202304230746Flap · delaminatedLH WING OUTBD FLAP LEADING EDGE HAS AREA OF DELAMINATION ON INBD SIDE. REPAIRES LH WING O/B T/E FLAP LE NOTED AREA IAW B767 SRM 57-53-01-0I, 57-53-01-1A,57-53-01- 2R AND 51-70-17-OG.SDR IPXA2023051593226Rib · crackedINSPECTION TYPE:5YR*MAJOR REPAIR* RIB 21 ON RH WING CENTER FLAP HAS 1EA CRACKREPAIRED PER SRM 57-50-00 FIG 201 AND 205SDR IPXA2023051593223Rib · crackedINSPECTION TYPE:5YR*MAJOR REPAIR* RIB 19 ON RH WING CENTER FLAP HAS 1EA CRACKREPAIRED PER SRM 57-50-00 FIG 201 AND 205SDR IPXA2023050293084Hinge Fitting · corrodedINSPECTION TYPE:C3FLAP R/H I/B HINGE #3 LUG I/B FACE HAS CORROSIONREPAIRED R/H I/B FLAP FWD HINGE #3 LUG I/B FACE IAW VTSAA EA 011-5740-01-A9921 IR GATED 04/28/2023 AND UPS EO MD-11-5740-86658-A MINORSDR FDEA202304220772Wedge · corrodedL/H I/B MAIN FLAP HAS CORROSION AT THE TRAILING EDGE UPPER SURFACE FROM THE O/B SIDE TO 24" I/B. REPAIRED CORROSION ON LH IB MAIN FLAP TE WEDGE UPPER SURFACE 2 EA LOCATIONS 6" FROM OB EDGE AND 24" FROM OB EDGE IAW B757 SRM 51-10-02, SRM 57-53-01-1A, SRM 5SDR AALA202306139179Bracket · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILING EDGE FLAP, INTERCONNECTING STRUT ATTACHMENT FITTING / BRACKET BEARING HAS EXCESSIVE PLAY. REPLACED FITTING / BRACKET PER SRM 51-72-11.SDR IPXA2023051593225Rib · crackedINSPECTION TYPE:5YR*MAJOR REPAIR* RIB 26 ON RH CENTER FLAP FOUND CRACKEDREPAIRED RIB 26 PER UPS EO A300-5750-8611-A AND VTMAE FINAL EA 300-5750-27-A-A3213-ASDR IPXA2023051593224Rib · crackedINSPECTION TYPE:5YR*MAJOR REPAIR* RIB 27 ON RH CENTER FLAP FOUND CRACKEDREPAIRED RIB 27 PER UPS EO A300-5750-27-A3213-ASDR IPXA2023051393218Flap · crackedINSPECTION TYPE:5Y*MAJOR REPAIR* RIB 17 ON RH CENTER FLAP FOUND CRACKEDREPAIRED RIB 17 PER UPS EO A300-5750-8611-A AND VTMAE FINAL EA 300-5750-27-A3213-ASDR IPXA2023051393217Flap · crackedINSPECTION TYPE:5Y*MAJOR REPAIR* RIB 18 ON RH CENTER FLAP FOUND CRACKEDREPAIRED RIB 18 PER UPS EO A300-5750-8611-A AND VTMAE FINAL EA 300-5750-27-A3213-ASDR IPXA2023051393215Flap · crackedINSPECTION TYPE:5Y*MAJOR REPAIR* RIB 26 ON CENTER FLAP FOUND CRACKEDREPAIRED RIB 26 PER UPS EO A300-5750-8612-A AND VTMAE FINAL EA 300-5750-27-A3212-ASDR AALA202305101971Flap · delaminatedAIRCRAFT WAS GROUNDED: AFTER FLAP EXTENSION FOR A CHECK PRE DOCKING, FOUND AN ARC SHAPE 35 INCHES BY 5/3 INCH DELAMINATION AT LEFT WING AFT FLAP UPPER SKIN. **SUPPLEMENTAL REPORT FOR AALA202304241971: REMOVED AND REPLACED LEFT INBOARD TRAILING EDGE AFT FLAP**
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