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 SWAA2022042686723Wedge · delaminatedLEFT HAND I/B MAIN FLAP TRAILING EDGE WEDGE HAS AREA OF DELAM. (MARKED). / [01] OK TO INSTALL WEDGE;[02] REMOVED DAMAGE PER SRM 57-53-01-2R-7;[03] VERIFIED REMOVED DAMAGE PER SRM 57-53-01-2R-7;[04] C/A #1 ENTERED IN ERROR;[05] REMOVED AND REPLACED R/H WING ; ISDR SWAA2022042687038Angle · crackedCRACK ANGLE TRAILING EDGE REAR SPAR LOCATED ON ORSS 274 AT LT WING 2022-158323 / [01] REPLACED ANGLE TRAILING EDGE REAR SPAR LOCATED ON ORSS 274 AT LT WING IAW B737-700 SRM-51-10-02 ITEM 9 AND DWG-115A2930 REV: - SEE INDIVIDUAL SIGN-OFF BELOW;[02] TASK CARD COSDR SWAA2022042687039None · crackedCRACK CORRUGATED PLATE TRAILING EDGE REAR SPAR LOCATED ON ORSS 261 AT LT WING 2022-158331 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE REAR SPAR LOCATED ON ORSS 261 AT LT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 115A2001 SHEET 29 REV -. SEE INDIVSDR SWAA2022042086724Flap · delaminatedRIGHT HAND INBOARD MAIN FLAP T/E WEDGE HAS AREA OF DELAM. (MARKED) / [01] REMOVED AND REPLACED R/H WING ; I/B TRAILING EDGE FLAP WEDGE IAW SRM 51-40-02 AND 51-40-04.;[02] INSPECTED WORK PERFORMED IN CORRECTIVE ACTION #1. WADE MOREY (TECHNICIAN); 02-APR-2022 17SDR FDEA202203230764Flap · dentedL/H WING OUTBD AFT FLAP FOUND SMALL DENT ON LOWER SURFACE CLOSE TO OUTBD END WITH ON DELAMINATION SIGHN PERFORMED WET LAYER REPAIR FOR MENTIONED AREA PER SRM 51-70-03, PAR. 5L REF. SRM 57-53-01-2R-1 REPAIR 1 FIG. 201 DETAIL 4, TABLE 2. REP. DIM. : 4" REPSDR FDEA202203230654Skin · damagedLEFT HAND WING - INBOARD FLAP ASSEMBLY INBOARD LOWER SEGMENT EXISTING REPAIR INTERNAL DAMAGED. DAMAGE EXISTING REPAIR AT LEFT HAND WING INBOARD FLAP ASSEMBLY INBOARD LOWER SEGMENT BETWEEN XIFH 133.9 AND XIFH 195.3 REMOVED AS PER SRM 51-31-01-0G. REPAIR SDR SWAA2022042687026Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ON IRSS 226 AT RT WING 2022-158245 / [01] REPLACED CORRUGATED PLATE AND FASTENERS LOCATED ORSS 256 AT RT WING TRAILING EDGE IAW B737-700 SRM 51- 10-02 ITEM 9 AND DWG 115A2001 SHEET 30 REV A;[02] REPLACED CORRUGATED SDR SWAA2022042687028Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 256 AT RT WING 2022-158246 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 256 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 29 REV -.;[02] REPLACED CORRUGATED PLATE TRAILING EDSDR SWAA2022042087054Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED WS228.25 AND WS253 AFT POSITION RT WING 2022-148189 / [01] REPLACED ANGLE TRAILING EDGE LOCATED WS228.25 AND WS253 AFT POSITION RT WING IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 P/N USED 115A2982-10 PO 2022-102850.SDR SWAA2022042087061Access Panel · crackedCRACK ACCESS PANEL 561CB TRAILING EDGE AROUND HOLES LT WING 2022-148237 / [01] TOOL USED CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 01-OCT-22.;[02] TOOL USED MULTIMETER P/N: FLUKE 87 ; S/N: 43050123 ; DUE DATE: 03-FEB-23;[03] REPAIRED ACCESS PANEL 561CB LT SDR SWAA2022042087072Plate · elongatedELONGATED HOLE PLATE ASSY TRAILING EDGE LOCATED WS204.25 TO WS228.25 RT WING 2022-148246 / [01] REPLACED PLATE ASSY TRAILING EDGE LOCATED WS204.25 TO WS228.25 RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001 SHEET 29 REV-.;[02] REPLACED PLATE ASSY TRAILING ESDR DALA2022033102162None · noneSHIP 3269 CORROSION OB FLAP EXCENTRICAL BEARING ON TRACK 3 AND TRACK 4 ON LH WING REFERENCE AMDS CARD 2750-6020-LT. CORRECTIVE ACTION: REPLACED BEARINGS PER DELTA WORK CARD AMDS 2750-6020-LT. (2166726)SDR SWAA2022032886195Fitting · crackedRT WING FIXED TRAILING EDGE FITTING AT APPR. WING STATION 278.5 CRACKED / [01] REMOVED AND REPLACED FITTING PER SRM 51-40-02SDR SWAA2022042086142Plate · crackedCRACK PLATE ASSY TRAILING EDGE LOCATED WS204.25 TO WS228.25 LT WING 2022-148117 / [01] REPLACED PLATE ASSY AND FASTENERS ON TRAILING EDGE LOCATED WS204.25 TO WS228.25 LT WING I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG:115A2001 SHEET:30 REV:A;[SDR SWAA2022042086145Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED WS228.25 TO WS253 FWD POSITION LT WING 2022-148112 / [01] REPLACED ANGLE TRAILING EDGE LOCATED WS228.25 TO WS253 FWD POSITION LT WING IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A2930 ;SHEET 7 ;REV -.;[02] REPLACED ANGSDR SWAA2022042086143Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED WS228.25 TO WS253 AFT POSITION LT WING 2022-148115 / [01] REPLACED ANGLE TRAILING EDGE LOCATED WS228.25 TO WS253 AFT POSITION LT WING IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02; SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CORRECTED STESDR SWAA2022040486010Skin · delaminatedRH O/B AFT FLAP I/B CORNER HAS SIGNS OF DELAME. EVALUATED AND FOUND UPPER SKIN ON EXISTING REPAIR DOUBLER DISBONDED. FOUND TO BE REPAIRABLE IAW SRM 57-53-01-2R-4 STEP 3 AND SRM 51-70-10-2R-4. REMOVED EXISTING DOUBLER IAW SRM 51-70-10-2R-0 REPAIR GENERAL PARSDR DALA2022032201862Not Reported · not reportedSECONDARY DAMAGE AREAS WERE FOUND AT DENTS #8 & #10 ON INNER FACE OF REAR MOVABLE VANE AT LH WING. AREAS WERE FOUND DEBONDED (IN REF NRC 00060). SUMMARY OF NRC 00238: INNER FACE OF REAR MOVABLE VANE AT LH WING WAS REPAIRED PER B717 SRM 51-70-02-0G AND IN REFERSDR SWAA2022041886027Bracket · brokenFOUND CLIP BROKEN AT RT WING INBOARD LOWER T/E BEAM ASSY TO ATTACH PANEL #651EB TO REAR SPAR (MKD) / [01] REMOVED BROKEN CLIP AT R/W I/B LOWER T/E BEAM TO ATTACHED PANEL #651EB TO REAR SPAR AS PER B- 737-700 SRM # 51-40-02-OG-0;[02] INSTALLED NEW CLIP AT R/W ISDR 2022F00136Flap · delaminatedL/H IB FLAP HAS MULTIPLE AREAS OF DELAMINATION ON BOTTOM SIDE OF FLAPS. PN: 6525130-37 SN: 733. R/H IB FLAP HAS MULTIPLE AREAS OF DELAMINATION ON BOTTOM SIDE OF FLAPS. PN: 6525130-38 SN: 772. MAJOR REPAIR ACCOMPLISHED BY AEROSPACE QUALITY RESEARCH AND DEVELOPMSDR SWAA2022041285554Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING 2022-131823 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING IAW B737-700 DWG # 115A2001 REV.- SRM 51-10-02 ITEM 9 SEE INDIVIDUAL SIGN-OFFS BELOW;[02] SDR SWAA2022041985264Flap · debondedCUSTOMER REQUEST - DEBONDED EXISTING REPAIR ON OB AFT FLAP UPPER SURFACE ON IB EDGE AT RT WING 2022-147848 / [01] TOOL USED: CALIPER PN: 500-464; S/N: 15331926; DUE DATE: 28/SEP/22.;[02] UT TOOL USED PN: S-3; SN: 064. DUE DATE: 12-JUL-22;[03] TOOL USED HOT BONSDR LR7A2022031603095Skin · dentedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB2703, FOUND LH INBOARD FLAP LOWER SKIN DENTED AT CWS171L. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12Z. NR#2703.SDR DALA2022031701779None · noneSHIP 3247 - ATB - DUE TO F/A AND PAX REPORT OF LH UPPER AILERON HINGE CLOSEOUT PANEL DEPARTING THE AIRCRAFT. CORRECTIVE ACTION: FOUND ACCESS PANEL 575AT PARTIALLY MISSING. INBOARD MOUNT BRACKET CRACKED AND PARTIALLY GONE. INBOARD FORWARD SCREWS APPEAR TO BE MISDR CALA2022031700689Seal · missingPDA 3 RIGHT WING INBOARD MAIN FLAP OUTBD END LOWER SEAL COMPLETELY MISSING -- SEE PHOTO PHOTO ADDED INSTALLED NEW SEAL REF IPC 27-51-11-01ASDR U2RA2022031700005Flap · damagedDURING SCHEDULED MAINTENANCE, THE R/H FLAPS, OUTBOARD AFT POSITION, SUSTAINED DAMAGE TO THE T/E FROM GSE IMPACT. APPLIED A TEMPORARY REPAIR UTILIZING POTTING COMPOUND AS NEEDED FOR SMOOTHNESS AND 3 LAYERS OF SPEED TAPE FOR SECURITY. THIS REPAIR IS LIMITED TOSDR SWAA2022041283811Support Bracket · crackedCRACK SUPPORT BRACKET LOCATED AT WS 253.00 TRAILING EGE AT LT WING 2022-131705 / [01] REPLACED SUPPORT BRACKET LOCATED AT WS 253.00 TRAILING EGE AT LT WING IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 P/N USED 115A2982-9 PO 2021-235986 1;[02] CORRECTED STEP 1: RSDR SWAA2022040683834Panel · crackedCRACK ACCESS PANEL 561BB TRAILING EDGE ARAUND HOLES LT WING 2022-129777 / [01] TOOL USED: CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 29-SEP-22.;[02] TOOL USED SCALE P/N: CL5000 S/N: AE-409558 DUE DATE: 19-MAY-22.;[03] TOOL USED HOTBONDER P/N: HCS9200B S/SDR SWAA2022041283372Support Bracket · crackedCRACK TRAILING EDGE SUPPORT BRACKET LOCATED AT LEVEL IRSS140 AT LT WING 2022-131679 / [01] REPLACED TRAILING EDGE SUPPORT BRACKET LOCATED AT LEVEL IRSS140 AT LT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9; 51-40-02;[02] REPLACED TRAILING EDGE SUPPORT BRACKET LOCASDR SWAA2022041283303Flap · delaminatedRIGHT WING OUTBOARD AFT FLAP HAS DELAM ON LOWER INBOARD SURFACE / [01] REMOVED RIGHT WING O/B AFT FLAP IAW AMM 27-51-22-000-801;[12] REMOVED FAILED DOUBLER AND PREPPED AREA FOR NEW REPAIR. IAW B737-800 SRM 51-70-10-2R-0 PAR 6&7. CLEAN AND PREP AREA. MADE NEW RSDR SWAA2022041883075Panel · pulledL/W T/E PANEL 561AB HAS SEVERAL PULLED FASTENER HOLES (MARKED) / [01] IDENTIFIED PANEL MATERIAL IAW SRM 57-51-01-0I-1 FIG. 3; TABLE 3; ITEM 5. <BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1; PARA. 4.B.(5). <BR><BR>DAMAGE WILL BE REPAISDR SWAA2022041883076Panel · pulledL/W T/E PANEL 561BB HAS SEVERAL PULLED FASTENER HOLES (MARKED) / [01] IDENTIFIED PANEL MATERIAL IAW SRM 57-51-01-0I-1 FIG. 3; TABLE 3; ITEM 9. <BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1; PARA. 4.B.(5). <BR><BR>DAMAGE WILL BE REPAISDR SWAA2022041883077Panel · pulledL/W T/E PANEL 561CB HAS SEVERAL PULLED FASTENER HOLES (MARKED) / [01] IDENTIFIED PANEL MATERIAL IAW SRM 57-51-01-0I-1 FIG. 3; TABLE 3; ITEM 10. <BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1; PARA. 4.B.(5). <BR><BR>DAMAGE WILL BE REPASDR IPXA2022032380398Rub Strip · wornINSPECTION TYPE:CRH INBD FLAP LEADING EDGE 3 EACH RUB PLATES WORNREMOVED FABRICRATED AND INSTALLED 3 EACH IAW SRM 51-40-21SDR IPXA2022032380397Rub Strip · wornINSPECTION TYPE:CRH FLAP LEADNG EDGE 3 EACH PUB PLATES WORNREMOVED FABRICATED AND INSTALLED 3 EACH IAW SRM 51-40-21SDR IPXA2022032380396Rub Strip · wornINSPECTION TYPE:CRH INBD FLAP LEADING EDGE 3 EACH RUB PLATES WORNREMOVED FABRICATED AND INSTALLED 3 EACH IAW SRM 51-40-21SDR DALA2022031601740None · noneSHIP 179 FOUND OUT DENT RH WING IB AFT FLAP EXTERNAL UPPER SURFACE AT 35 INCHES TO IB EDGE AND 2 INCHES TO AFT EDGE. CORRECTIVE ACTION: SKIN REPAIRED BETWEEN FSS 170 AND FSS 245 AS PER B767-300 SRM 57-53 & SRM 51-70 (2154064)SDR SWAA2022040782792Skin · delaminatedL/H O/B AFT FLAP I/B LWR SKIN DELAMINATED / [01] NEW FAULT RAISED TO REPLACE FLAP FOR COMPANY CONVIENANCE DUE TO FOUND DAMAGE & INBOUND DMI?S<BR>REFERENCE<BR>INBOUND TLD TASK BARCODE# TTG8R008048N LINE# 169 & NEW FAULT BARCODE# TTG8Q00BAM05 LINE# 1676<BR>INBOUSDR SWAA2022032481489Seal · elongated642BB FAIRING INBD MIDDLE SEAL RETAINER HOLES ARE ELONGATED / [01] REMOVED MIDDLE SEAL AND RETAINER FOR REPAIR.;[02] REPAIRED ELONGATED HOLES IN #6 FAIRING MIDDLE SEAL PER SRM 57-53-70-2R-2.;[03] INSPECTED 2. RICKY MINYARD (TECHNICIAN); 16-MAR-2022 14:53 UTC<BSDR AALA202205267429Flap · delaminatedAIRCRAFT WAS GROUNDED: RIGHT WING INBOARD FLAP HAS CARBON FIBER DELAMINATION AT TRAILING EDGE TOP SIDE. **SUPPLEMENTAL REPORT FOR AALA202203097429: REPAIRED PER EA 334600** (CLOSED)SDR AALA202203097429None · noneAIRCRAFT WAS GROUNDED: RIGHT WING INBOARD FLAP HAS CARBON FIBER DELAMINATION AT TRAILING EDGE TOP SIDE. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)SDR DALA2022030801506None · noneSHIP 3305 RIB 6 FWD LUG WAS FOUND CORRODED AND AFT LUG FOUND ECENTRIC. CORRECTIVE ACTION: REPAIRED L/H MLG RIB 6 AS PER ER/A 597417-14AD. (2144045)SDR HALA2022030400076None · noneSHIP 386 LH LOWER LG RIB 6 FWD FOUND WITH HEAVY CORROSION ON LUG BORE, FWD & AFT SPOT FACE BEYOND 5753-01164-08A FIG 1 SHEET 2 OF 4 SPECIFIED REWORK LIMIT. CORRECTIVE ACTION: TASK ACCOMPLISHED AS PER ER/A 594574-14. (2143382)SDR HALA2022030400074None · noneSHIP 386 RH LOWER LG RIB 6 FWD FOUND WITH HEAVY CORROSION ON FWD & AFT SPOT FACE BEYOND SPECIFIED DIMENSIONS UNDER TASK 5753-01164-08B. CORRECTIVE ACTION: TASK ACCOMPLISHED AS PER ER/A 594573-14. NIL FURTHER. (2143379)SDR SWAA2022030779789Rib · crackedSEAL RIB UNDER RIGHT WING INBOARD TRAILING EDGE CRACKED / [01] REMOVED AND INSTALLED SEAL RIB UNDER RIGHT WING INBOARD TRAILING EDGE. REF SRM 51-40-02SDR 2023FA0000233Flap · unknownSMALL CRACK ON EXTERNAL TOP OF THE RH FLAP, THE CRACK IS NOT LONGER THAN 2 INCHES AND THE INTERNAL RIBS AND AC STRUCTURE WERE UNDAMMAHED. THE CRACK DID NOT PROTRUDE TO ANY FASTENERS AND WAS RELATED TO PREVIOUS FLAP DAMAGE. CESSNA WAS CONTACTED AND VIA PHONE SDR IPXA2022030179574Flap · noneINSPECTION TYPE:SEGRH WING I/B FLAP L/E HAS DENTS AND BARE METAL.ACCOMPLISHED REPAIR PER SRM 57-50-00 FIG 208.SDR SWAA2022042798784Skin · delaminatedLH OUTBD AFT FLAP INBD CORNER LOWER SKIN DELAMINATED / [01] REMOVED LH OUTBOARD AFT FLAP ASSEMBLY IAW AMM 27-51-22-000-801.;[02] OK TO INSTALL NEW LH OTBD AFT FLAP;[03] INSTALLED NEW LH OUTBOARD AFT FLAP ASSEMBLY IAW AMM 27-51-22-400-801 STEPS 3.F.(1) THRU 3.FSDR SWAA2022032978892Skin · delaminatedDOT A-24-3. LEFT WING O/B AFT FLAP HAS LARGE AREA OF DELAMINATED SKIN ON LOWER INBOARD CORNER. / [01] REMOVED L/H O/B AFT FLAP IAW AMM 27-51-22-000-801.;[02] BOND TEST IAW B737 NDT PT 4; 51-00-05. NO DEFECTS NOTED. TOOL#40082; DUE 11OCT22;[03] REMOVED FASTENERSDR SWAA2022030978943Flap · delaminatedRH OUTBD AFT FLAP INBD CORNER DELAMINATED / [01] EVALUATED R/H OUTBD AFT FLAP INBD CORNER AND FOUND AREA OF DELAMINATION OF 5'X6'.FOUND TO BE REPAIRABLE. IAW B737-700 SRM 57-53-01-2R-4 PAR1A REV 75. REMOVED DAMAGED SKIN FOR REPAIR. NO DAMAGE TO CORE. CLEAN AND
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