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 SWAA2023050930095Support · brokenL/W WING STA 220; CLIP ON LOWER REAR SPAR FOR PANEL SUPPORT 551FB IS BROKEN.<[01] REMOVED AND REPLACED L/W WING STA 220; CLIP P/N 115A5552-1 ON LOWER REAR SPAR FOR PANEL SUPPORT 551FB IAW SRM 51-40-02 AND AIPC 57-50-00-23;[02] VERIFIED CORRECTIVE ACTION 1.SDR AALA202304241971Unknown · unknownAIRCRAFT 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 REQUIRED** (OPEN)SDR DALA2023080206253Unknown · unknownSHIP 3126 CORROSION WAS FOUND COMMON TO THE OUTBOARD AND INBOARD LUG FITTING AT RIB5 FLAP TRACK 3. CORRECTIVE ACTION: REPAIRED PER 607038-14. (2729172)SDR IPXA2023050593127Bracket · crackedINSPECTION TYPE:3CR/H O/B FLAP I/B FAIRING FWD O/B BRACKET CLIP IS CRACKED.REMOVED, FABRICATED AND REPLACED CLIP AT THE R/H O/B FLAP FWD SIDE IAW SRM 51-31-01 (MINOR)SDR AALA202306134207Bracket · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD TRAILING EDGE FLAP, INTERCONNECTING STRUT ATTACHMENT FITTING / BRACKET BEARING HAS EXCESSIVE PLAY. REPLACED FITTING / BRACKET PER SRM 51-72-11.SDR VNAA202304270023Skin · dentedSEVERAL NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP FROM FLS 15.00 TO FLS 65.50SDR DALA2023050703549Unknown · unknownAIRCRAFT 3121, CORROSION INTERCONNECTING STRUT IB FLAP ON RH WING (REFER TO AMDS CARD 2751-9202 RII). CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT IB FLAP ON RH WING ON SERVICEABLE CONDITION AS PER A320 FAM AMM 27-51-44-000-001-A AND27-51-44- 400-001-A. (SDR DALA2023042003108Unknown · unknownLT WING FIXED FLAP VANE DELAMINATED ON UPPER SURFACE 30 INCHES FROM I/B END AND 6 INCHES FROM T/E. SUMMARY NRC 001-0292:5750-2001/001 00109: FLAP VANE FOUND TO BE OUT OF LIMITS. REPLACED LH IB FLAP VANE REF B717 AMM 27-50-02. (LP #2726069)SDR AALA202305192360Flap · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING OUTBOARD TRAILING EDGE FLAP INTERNAL SURFACE BETWEEN FLAP TRACKS 3 AND TRACK 4 , BETWEEN RIBS 6 AND 14. REPLACED FLAP ASSEMBLY PER TASK CARD 26L00027009.SDR SWAA2023050928225Panel · pulledPANEL 661BB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PARA 4B( REPAIRED PER SRM 51-70-04-2R-9 AS DIRECTED BY SRM 57-51-01-2R-1 PARA 4C AND TABLE 202. <BR><BR>REMOVED DAMAGE TO ALL FASTENER HOLES OSDR SWAA2023042028184Bracket · crackedL/H WING DEFLECTION CONTROL PANEL FWD SEAL BRACKET CRACK.<[01] CORRECTION FOR STEP #1 TO READ REMOVED LEFT WING DEFLECTION CONTROL PANEL FORWARD SEAL BRACKET AS PER B 737-700 SRM 51-40-02-0G-0;[02] *** ENTRY 1 WAS ENTERED IN ERROR ***;[03] REMOVED AND REPLACEDSDR SWAA2023050927995Support Angle · crackedLT WING T/E STRUCTURE;SHOWS INB FIXED UPPER PANEL SUPPORT ANGLE BRACKET WITH INB ATTACH BRACKET CRACKED.MKD<[01] REMOVED AND REPLACED DAMAGED LT WING T/E STRUCTURE I/B FIXED UPPER PANEL SUPPORT ANGLE BRACKET I/B ATTACH BRACKET IN REF WITH SRM 51-40-02-0G-0.;[0SDR A6WA202304158552Flap · damagedPERFORM PERMANENT REPAIR FOR LH INBOARD FLAP INNER DOUBLER. ********AIRCRAFT REMOVED FROM SERVICE******* REPAIRED L/H INBOARD FLAP UPPER SKIN REF REO 601R-57-52-2482 REV -- DATED 2023-04-12SDR SWAA2023042027239Beam · crackedRIGHT WING - AFT FLAP DEFLECTION BEAM UPPER TAB CRACKED.<[01] REMOVED DAMAGED UPPER TAB FROM DEFLECTION CONTROL RIB; LOCATED AND DRILLED REPAIR PART PER SRM 57-51-02-2R REPAIR 3.;[02] REPAIRED RH WING AFT FLAP DEFLECTION BEAM UPPER TAB IAW SRM 57-51-02-2R-3SDR SWAA2023041927234Bracket · crackedLEFT WING-AFT TRAILING EDGE UPPER PANEL SUPPORT BRACKET CRACKED JUST OUTBOARD OF #3 FLAP TRACK<[01] REMOVED AND REPLACED LEFT WING-AFT TRAILING EDGE UPPER PANEL SUPPORT BRACKET PER SRM 51-40-02.SDR SWAA2023041927237Plate · crackedRIGHT WING - FIXED LOWER TE PANEL WIGGLE PLATE OTB OF #6 FLAP SUPPORT CRACKED.<[01] REMOVED AND REPLACED RIGHT WING T/E PANEL WIGGLE PLATE PER AMM 57-50-02.;[02] REMOVED AND REPLACED RIGHT WING T/E PANEL WIGGLE PLATE PER AMM 57-50-02.SDR SWAA2023041927229Beam · crackedLEFT WING- AFT FLAP DEFLECTION SUPPORT BEAM UPPER BRACKET CRACKED<[01] ACCOMPLISHED OF L/H WING AFT FLAP FIXED TRAILING EDGE DEFLECTION SUPPORT BEAM UPPER TAB PER SRM 57-51-02-2R-3 REPAIR 3.SDR SWAA2023051527168Support Angle · brokenBROKEN ACCESS PANEL 651GB SUPPORT ANGLE AT RT WING 2023-238052<[01] REPLACED SUPPORT ANGLE AT RT WING LOC. ON ACCESS PANEL 651GB IAW B737-700 SRM 51-10-02 ITEM 9;[02] CORRECTED STEP 1 <BR>REPLACED SUPPORT ANGLE AT RT WING LOC. ON ACCESS PANEL 651GB IAW B737-70SDR CALA2023041301109Flap · unknownFLAP OVERSPEED WITH WINDSHEAR EVENT PER CREW FLAPS AT 25 AND 31KT OVERSPEED FOLLOWED AMM 05-51-08/201. ACP'D PHASE I INSPECTION PER AMM TASK 05-51-08-212-001. INSPECTION COMPLETED, NO FINDINGS. PARTIALLY ACP'D PHASE II INSPECTION IAW TASK 05-51-08-212-007, COMSDR AALA202306293846Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING FLAP TRACK #4 RE-ENFORCING DOUBLER PLATE ON THE LOWER SURFACE OF THE OUTBOARD FLAP BETWEEN RIB 14 AND 15, BETWEEN STRINGERS 1 AND 6. REPLACED RE-ENFORCING DOUBLER PLATE PER SRM 57-53-21-300-003.SDR DALA2023041302933Unknown · unknownSHIP 3254 NEED TO ACCOMPLISH VA 99496AD. CORRECTIVE ACTION: COMPLIED WITH. (2716321)SDR DALA2023041302932Unknown · unknownSHIP 3254 NEED TO ACCOMPLISH VA 99496AD. CORRECTIVE ACTION: COMPLIED WITH. (2716320)SDR DALA2023080206254Unknown · unknownSHIP 3126 CORROSION ON TRACK 3 AND TRACK 4 DRIVE FITTINGS ON LOWER SURFACE. CORRECTIVE ACTION: REPAIRED PER ERA 607202-14. (2714922)SDR DALA2023051703933Unknown · unknownSHIP 3254 ER/A 607742-14AD ISSUED FOR REPLACEMENT OF THE LH INBD FLAP TRUNNION SUPPORT. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: COMPLIED WITH ERA. (2715154)SDR DALA2023041202876Unknown · unknownON ARRIVAL FOUNDL/H WING FLAP TRACK FAIRING NBR 2 TAILCONE MISSING. CORRECTIVE ACTION: REPLACED L/H FLAP TRACK FAIRING NBR 3 TAILCONE.SDR SWAA2023050925704Panel · pulledPANEL 561CB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4.B(5).WILL BE REPAIRED IAW SRM 51-70-04-2R-9 PER SRM 57-51-01-2R-1 PARA 2.B(2) AND TABLE 202.<BR>REMOVED ALL DAMAGE AT FASTENER HOLES TO .5' DISDR SWAA2023050925703Panel · pulledPANEL 561AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4.B(5).REPAIRED IAW SRM 51-70-04-2R-9 PER SRM 57-51-01-2R-1 PARA 2.B(2) AND TABLE 202.REMOVED ALL DAMAGE AT FASTENER HOLES TO .5' DIAMETER; CLEASDR IPXA2023042793013Fitting · corrodedINSPECTION TYPE:3CL/H I/B FLAP VANE O/B FITTING 1ST LUG BORE HAS CORROSION.REPLACED CORRODED FITTING ON L/H I/B FLAP VANE O/B SIDE IAW CMM 57-52-03 (MINOR)SDR SWIA2023052212Panel · chafedLH WING FLAP PANEL 584HT CHAFE (C-CHECK RO 5/18/2023) REMOVED AND REPLACED LH WING FLAP PNL 584HT REF-CRJ-700 SRM 51-40-11-001-001 A01 AND PANEL INSTALLED ON CAMP # 26307786 M-212 FORM, JOB 0 OP 7005SDR DALA2023041202892Unknown · unknownSHIP 665 AWR. SECONDARY NRC IN REF NRC.00370, HIDDEN CORROSION WAS FOUND AFTER FIBERGLASS SKIN REMOVAL ON L/E OF INBD MAIN FLAP AT RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00629. SKIN ON L/E OF INBD MAIN FLAP AT RH WING WAS REPAIRED PER B757-200 SRM. (271141SDR IPXA2023050293081Flap · corrodedINSPECTION TYPE:C3R/H O/B FLAP I/B AFT HINGE #7 LUG BORE HAS CORROSION AT STA XW=-486.403, YW=589.366.REPAIRED CORRODED HINGE AT THE R/H O/B FLAP I/B AFT #7 LUG BORE AT STA XW=-486.403, YW=589.366 IAW VTSAA EA 011-5740-01-A9932 I/R AND UPS EO MD11-5750-86681-ASDR IPXA2023042993038Flap · corrodedINSPECTION TYPE:3CR/H I/B FLAP O/B AFT HINGE #7 LUG BORE HAS CORROSION AT STA XW=-254, YX=495.96.REPAIRED CORRODED HINGE #7 LUG BORE AT R/H I/B FLAP O/B AFT HINGE AT STA XW=-254, YX=495.96 IAW VTSAA EA 011-5752-01-A9924 I/R , UPS EO MD11-5750-86671-A DATED 04/SDR IPXA2023042893026Bracket · corrodedINSPECTION TYPE:3CR/H O/B FLAP O/B FWD HINGE #1 LUG BORE HAS CORROSION AT STA XW=-638.305, YW=670.239.REPAIRED CORRODED HINGE BRACKET ASSY AT STA XW=-638.305, YW=670.239 IAW VTSAA EA 011-5740-01-A9929 IR AND UPS EO MD11-5740-86679-A DATED 4/27/23 AND FAA FORM SDR IPXA2023042893025Bracket · corrodedINSPECTION TYPE:C3R/H O/B FLAP O/B FWD HINGE #3 LUG BORE HAS CORROSION AT STA XW=-638.305.REPARIED HINGE BRACKET ASSY AT THE R/H O/B FLAP O/B FWD SIDE AT STA XW=-638.305 IAW VTSAA EA 011-5740-01-A9929 IR AND UPS EO MD11-5740-86679-A DATED 4/27/23 AND FAA FORM SDR IPXA2023042893024Bracket · corrodedINSPECTION TYPE:3CR/H O/B FLAP O/B FWD HINGE #2 LUG BORE HAS CORROSION AT STA XW=-638.305 .REPAIRED CORRODED HINGE BRACKET ASSY AT THE R/H O/B FLAP O/B FWD SIDE AT STA XW=-638.305 IAW VTSAA EA 011-5740-01-A9929 IR AND UPS EO MD11-5740-86679-A DATED 4/27/23 (MISDR IPXA2023042793014Fitting · corrodedINSPECTION TYPE:3CR/H I/B FLAP VANE O/B TRACK FITTING HAS CORROSION.REPLACED CORRODED FITTING AT THE R/H I/B FLAP VANE O/B SIDE IAW CMM 57-52-03. (MINOR)SDR IPXA2023060836746Flap · puncturedRH INBD MAIN FLAP HAS HOLE AND PUNCTURE IN L/E 48' OUTBD OF #5 BALLSCREW ATTACHMENT.***SM30*** **LMX36** INSTALLED RH INBOARD FLAP LEADING EDGE MIDDLE PANEL PER B747 AMM 20-51-01SDR SWAA2023051524626Angle · crackedCRACK ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 272 LT WING 2023-237685<[01] REPLACED ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 272 LT WING AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 115A2930 REV. ?-?. MEASURE OF CRACK IS: L=.0.254?. TOOL USEDSDR SWAA2023051524625Plate · crackedCRACK CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 231 AT LT WING 2023-237690<[01] REPLACED CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 231 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SING-OFF BELOW.;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVISDR SWAA2023051524627Plate · crackedCRACK CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 215 LT WING 2023-237688<[01] REPLACED CORRUGATED PLATE AND FASTENERS INBOARD TRAILING EDGE IRSS 215 LT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG #115A2001 SHETT:34 REV: -.;[02] REPLACED CORRSDR SWAA2023051524628Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 LT WING 2023-237691<[01] REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE ORSS 261 LT WING. IAW B737 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 115A2001 SHEET 32 REV: -;[02] REPLACED CORRUGATED PLATE LOCATED TRAISDR SWAA2023051524622Bracket · crackedCRACK TRAILING EDGE BRACKET DEFLECTION CONTROL RIB ORSS 272 AT LT WING 2023-237686<[01] REPLACED BRACKET DEFLECTION CONTROL RIB ORSS 272 AT LT WING IAW B737-700 SRM: 51-10-02 ITEM 9.;[02] TASK CARD COMPLETEDSDR FDEA202304070587Flap · delaminatedRH WING I/B FLAP AFT FLAP LOWER SKIN HAS A DENT WITH SUBSTRATE BREAK THROUGH. REPAIRED RH I/B AFT FLAP ON THE LOWER SKIN IAW B767 SRM 57-53-01-2R AND 51-70-10-2RSDR SWAA2023050224275Panel · crackedRIGHT WING I/B TRAILING EDGE PANEL 551AT CRACKED AND DENTED ON LOWER SURFACE.<[01] REMOVED AND REPLACED PANEL PER AMM 20-50-11.SDR IPXA2023042793012Hinge · crackedINSPECTION TYPE:3CR/H O/B FLAP I/B HINGE BEAM HAS A CRACK ON THE HINGE CAGE AT LWR SIDE.REPLACED HINGE BEAM R/H O/B FLAP I/B HINGE LWR SIDE IAW SRM 51-31-01. (MINOR)SDR SWAA2023040724408Skin · debondedRH INBD MAIN FLAP OUTBD TRAILING EDGE LOWER SKIN DISBONDED FROM LOWER SURFACE. DAMAGE MEASURES 22.5 ALONG T/E; 13.5 FROM T/E FORWARD; AND 8.5 FROM AFT OUTBD CORNER.<[01] REMOVED AND INSTALLED RH INBD MAIN FLAP OUTBD TRAILING EDGE FLAP WEDGE. REF AMM 27-51-11 &SDR IPXA2023042893021Track · gougedINSPECTION TYPE:3CL/H WING T/E AREA O/B FLAP I/B TRACK FWD AND AFT SIDE HAS A GOUGED AT STA XORS=480.250 .REPAIRED GOUGED TRACKED AT THE L/H WING T/E AREA O/B FLAP I/B FWD AND AFT SIDE AT STA XORS=480.250 IAW EA 011-5753-01-A9928 IR AND UPS EO MD11-5750-86655-SDR DALA2023040602699Unknown · unknownAIRCRAFT 3121, CORROSION SUPPORT BRACKET ON INTERNAL AREA AT RIB6 OUTBOARD FLAP ON LH WING. CORRECTIVE ACTION: REPLACED LEFT OUTBOARD FLAP. (LP 2703895)SDR IPXA2023040392546Flap · chafedINSPECTION TYPE:1C*MAJOR REPAIR* L/H WING INNER FLAP P/N A57960000010 S/N FH1297 O/B EDGE HAS A REPAIR DOUBLER WITH 2 EACH CHAFE DAMAGESWORKED PER UPS EO A300-5750-86183-A AND UPS RCD 269862SDR SWAA2023042622914Plate · crackedTHE R/H T/E WIGGLE PLATE AT IRSS 216 IS CRACKED.<[01] REMOVED R/H TE WIGGLE PLATE AT IRSS 216 IAW SRM 51-40-02-0G-0.;[02] INSTALLED NEW WIGGLE PLATE AT RH TE IRSS 216 IAW SRM 51-40-02-0G-0.;[03] INSTALLED NEW WIGGLE PLATE P/N 7570641 AT RH TE IRSS 216 IAW SRM
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