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 FDEA202209012136Skin · dentedLW I/B FLAP UPPER PANEL HAS SEVERAL DENTS AFT OF #6 SPOILER. REPAIRED 2 EACH DENTS #5 AND #6 DENTS ON STEP 9 AT THE LEFT WING I/B MAIN FLAP UPPER SKIN BY REMOVING DAMAGE, FABRICATING FILLERS AND DOUBLER, CLEANING AND PREPPING SURFACE, LAYING UP PARTS AND CSDR SWAA2022100365518Retainer · crackedRIGHT WING #6 FLAP FWD FAIRING PANEL 642AB HAS I/B AND O/B PLASTIC RETAINERS CRACKED AT BOLT WHOLE SIDE. / [01] REMOVED AND REPLACED RIGHT WING #6 FLAP FWD FAIRING PANEL 642AB I/B AND O/B PLASTIC RETAINERS <BR>REF: SOPM 20-50-01;[02] VERIFIED STEP 1.SDR SWAA2022100365517Retainer · crackedLEFT WING #1 FORWARD FAIRING PANEL 544AB I/B PLASTIC RETAINER CRACKED. / [01] REPLACED PLASTIC RETAIN AT LEFT WING #1 FORWARD FAIRING PANEL 544AB I/B IAW B737-700 REF: SRN 51-40-02-0G-0..;[02] CORRECTING STEP 1: REPLACED PLASTIC RETAINER AT LEFT WING #1 FORWARSDR SWAA2022100348074Retainer · crackedLEFT WING #1 FORWARD FAIRING PANEL 544AB I/B PLASTIC RETAINER CRACKED. / [01] REPLACED PLASTIC RETAIN AT LEFT WING #1 FORWARD FAIRING PANEL 544AB I/B IAW B737-700 REF: SRN 51-40-02-0G-0..;[02] CORRECTING STEP 1: REPLACED PLASTIC RETAINER AT LEFT WING #1 FORWARSDR SWAA2022100348075Panel · crackedRIGHT WING #6 FLAP FWD FAIRING PANEL 642AB HAS I/B AND O/B PLASTIC RETAINERS CRACKED AT BOLT WHOLE SIDE. / [01] REMOVED AND REPLACED RIGHT WING #6 FLAP FWD FAIRING PANEL 642AB I/B AND O/B PLASTIC RETAINERS <BR>REF: SOPM 20-50-01;[02] VERIFIED STEP 1.SDR SWAA2022092948072Spar · crackedRIGHT OUTBOARD FLAP FRONT SPAR WEB AND LWR CHORD CRACKED / BROKEN FWD OF 2ND FROM I/B AFT TRACK.<[01] REMOVED R/H WING O/B MAIN FLAP ASSY REF AMM27-51-21-000-801;[02] REMOVED REMOVED R/H WING O/B MAIN FLAP O/B CARRIAGE REF AMM 27-51-23-000-801;[03] REMOVED REMSDR SWAA2022092948073Flap Track · crackedCHECK ADJUSTMENT OF RIGHT OB FLAP DUE TO 2ND FROM I/B AFT FLAP TRACK FWD END CONTACTED FRONT SPAR AND CRACKED / BROKE PIECE OUT OF WEB. / [01] REMOVED RIGHT WING OB AFT FLAP AS PER AMM27-51-22-000--801;[02] REMOVED RIGHT OB AFT FLAP TRACK 4 AND 3 AS PER B737 ASDR Y2PA2022090622046Flap · corrodedDISCREPANCY: : DURING C-CHECK AT COMMERCIAL JET IN KDHN, EXFOLIATION CORROSION FOUND ON RH WING INBOARD FLAP AT APPROXIMATELY XRS 69 INNER SURFACE EMANATING FROM UNDER RIB JUST BELOW 3RD FROM INBOARD FLAP VANE MOUNT SDR FDEA202208302115Wedge · delaminatedR/H WING, O/B TRAILING EDGE FLAP. TRAILING EDGE WEDGE HAS LARGE DENT, APPROX. 6" X 9", LOCATED ON LOWER SURFACE STA WS879.2 APPROX. 24" FROM O/B END AND 2.5" FORWARD OF TRAILING EDGE. REF. SEQ 155, WRI 57-50-1079 AND EA H-5750-T0370322 P2 COMPLISDR SWAA2022101178815Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED ORSS 271 TRAILING EDGE RT WING 2022-485737 / [01] REPLACED SUPPORT ANGLE LOCATED ORSS 271 TRAILING EDGE RT WING IAW B737-700 SRM 51-40-02 AND 51-10-02;[02] REPLACED SUPPORT ANGLE LOCATED ORSS 271 TRAILING EDGE RT WING IAW B737-70SDR SWAA2022100647844Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED ORSS 271 TRAILING EDGE RT WING 2022-485737 / [01] REPLACED SUPPORT ANGLE LOCATED ORSS 271 TRAILING EDGE RT WING IAW B737-700 SRM 51-40-02 AND 51-10-02;[02] REPLACED SUPPORT ANGLE LOCATED ORSS 271 TRAILING EDGE RT WING IAW B737-70SDR CALA2022082902208Seal · missingPDA 3 RIGHT WING #6 FLAP CANOE OUTBD SIDE CENTER SEAL PARTIALLY MISSING AND 2 RETAINING RIVETS LOOSE OUT OF 5. INITIATED A DIP TO REINSPECT REPAIR EVERY 500 CYCLES OR MORE FREQUENTLY. REMOVED WORN SEAL, FASTENERS AND RETAINER AND INSTALLED A NEW SEAL AND RETAISDR FDEA202208282088Skin · wornLW IB FLAP UPPER OB REPAIR AREA IS WORN AT OB UPPER SKIN. REPAIRED LW IB FLAP UPPER SKIN WITH PERMENAT REPAIR IAW B757 SRM 57-53-01-2RFIG 201 REPAIR 1 SHEET 1 AND 51-70-10-2R REPAIR 3 AND 4.SDR DALA2022111407322None · noneSHIP 3264 PER AMDS WORKCARD, FORECAST NUMBER 32-0557-8-0333 INSP. 32, AD FLAP TRUNNION DRV/SLIDE PANEL, LT. REP PAGE 10 ITEM/STEP 22 PERFORM A GVI OF THE SLIDING PANEL FOR CRACKED OR DAMAGE. CORRECTIVE ACTION: COMPLIED WITH WORK CARD 5751-01025-01C. (8256699)SDR SWAA2022090647078None · delaminatedR/H WING T/E FLAP #6 CANOE HAS DELAMINATION O/B UPPER EDGE (MARKED) / [01] SEE INDIVIDUAL SIGN OFFS FOR WORK ACCOMPLISHEDSDR IPXA2022082785670Bracket · crackedINSPECTION TYPE:1CLH WING FIXED T/E UPPER FAIRING SUPPORT STRUCTURE CRACKED LOCATED ON RIB 10.REMOVED, FABRICATED AND REPLACED PER SRM 51-40-21 AND SRM 57-51-11.SDR SWIA202266815None · chafedLH OUTBOARD FLAP CENTER HINGE ARM SIDE PLATE HAS CHAFING DAMAGE (C-CHECK RO 11/10/2022) REMOVED AND REPLACED CHAFED LH OTBD FLAP CENTER HINGE ARM SIDE PLATE. REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-15 & DWG 601R14699 REV B. ALL STEPS OF 51-900-1003-SSDR SWAA2022090246537Intercostal · crackedLT WING UPPER T/E PANEL AT FLAP DEFLECTION RIB ATTACH POINT INTERCOSTAL CRACKED ON OUTBOARD END. / [01] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-02;INSTALLED FASTENERS PER SRM 51-40-02.SDR SWIA202266863Vane · out of limitsREPLACE RH I/B FLAP VANE INBOARD CENTER CAP DUE TO OUT OF LIMITS ON JOB 27634101 OP 184 CAMP 25383077. (C-CHECK RO 11/12/2022) REPLACED R/H INBOARD FLAP VANE CENTER CAP WITH NEW UNIT REF CRJ200 SRM 51-42-13 AND DRAWING 601R14302, REV. E. COMPLIED WITH SDR SWIA202266862Vane · out of limitsREPLACE RH I/B FLAP VANE OUTBOARD CAP DUE TO OUT OF LIMITS ON JOB 27634101 OP 184 CAMP 25383077. (C-CHECK RO 11/12/2022) REMOVED AND REPLACED R/H INBOARD FLAP VANE, OUTBOARD CAP P/N: 601R14303-44 REF. CRJ-200 SRM 51-42-13 AND DWG# 601R14302 REV E. C/W 5SDR SWIA202266861Vane · out of limitsREPLACE RH I/B FLAP VANE INBOARD CAP DUE TO OUT OF LIMITS ON JOB 27634101 OP 184 CAMP 25383077. (C-CHECK RO 11/12/2022) REMOVED AND REPLACED WITH NEW RH IB FLAP VANE IB CAP REF. CRJ-200 SRM, 51-42-10 AND DWG PL601R14302 REV E. COMPLIED WITH TASK CARD 5SDR AALA202211152200Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING OUTBOARD TRAILING EDGE FLAP INTERNAL ATTACH FITTING TRACK 4, BETWEEN RIB 14 AND RIB 15. MAINTENANCE REPLACED FLAP PER AMM 27-54-62.SDR SWAA2022092246101None · corrodedCORROSION ON R/W #2 FUEL TANK AFT BOOST PUMP UPPER ATTACH CLIP COMMON TO BONDING JUMPER ATTACH POINT / [01] REMOVED AND REPLACED CORRODED CLIP ON R/W #2 FUEL TANK AFT BOOST PUMP UPPER ATTACH CLIP COMMON TO BONDING JUMPER ATTACH POINT IAW AMM 20-50-11-910-801 TSDR WX0A1900010074233None · noneDURING MASKING A/C FOR PRIMER FOUND DAMAGE TO LEFT HAND INBOARD FLAP. APPROX 12"" AFT OF WALKWAY APPROX 30"" OUTBOARD OF FUSELAGE/RECEIVED FINAL ERFTS #60003 AND ALLEGIANT REO NO R5752-0013 REV 00. REPAIRED PUNCTURED AREA ON LH FLAP ZONE 2 I/B FLAP APPROX 12 ISDR SWAA2022092965480Skin · delaminatedLEFT O/B AFT FLAP INBOARD AFT CORNER DELAMINATED. 8-56 / [01] MEASUREMENTS;[02] PERFORMED VISUAL INSPECTION AND PERFORMED TAP TEST FOUND DELAMINATION SIZE 0.500 AS PER B737 NDT 51-05-01 SECTION (3) AND (5).;[03] CLEANED AND PREPARED DAMAGE AREA FOR REPAIR ;FOUSDR SWAA2022092844977Skin · delaminatedLEFT O/B AFT FLAP INBOARD AFT CORNER DELAMINATED. 8-56 / [01] MEASUREMENTS;[02] PERFORMED VISUAL INSPECTION AND PERFORMED TAP TEST FOUND DELAMINATION SIZE 0.500 AS PER B737 NDT 51-05-01 SECTION (3) AND (5).;[03] CLEANED AND PREPARED DAMAGE AREA FOR REPAIR ;FOUSDR SWAA2022082644563Flap · delaminatedLEFT WING O/B AFT FLAP DELAMINATED ON I/B LOWER SURFACE. / [01] PERFORMED SRM 57-53-01-1A-4. NUMBER 4; (8)(A) 1) A-H)SDR FDEA202208232032Skin · gougedRIGHT WING OUTBOARD FWD FLAP OUTBOARD LEADING EDGE HAS GOUGESDR SWAA2022092765235None · delaminatedRIGHT WING O/B AFT FLAP HAS A DELAM ON I/B LOWER CORNER / [01] REMOVED RIGHT WING O/B AFT FLAP PER AMM 27-51-22-000-801[08] FABRICATED THE REPAIR DOUBLER AND FILLER FROM PRE-PRIMED 0.16' 7075 T6 ALUMINUM (LOT# 1351319-2) ACCORDING TO SRM 51-70-10-2R-0; PARA'S SDR CALA2022082402169Skin · dentedSUPPORT TASK LEFT WING OB FWD FLAP UPPER SKIN HAS DENTS AS MARK TRANSCRIBED FROM HAECO GSO NR 9286084 EVALUATED, REMOVED DAMAGE AND REPAIRED AND RESTORED FINSIH OF L /H WING O/B FWD FLAP UPPER SKIN IAW B757-300 SRM 51-70-07, SRM 5 7-53-01 B757-300 AMM 51-21-0SDR SWIA202266860Skin · chafed* L/H INB FLAP VANE SKIN HAS THREE CHAFES AT LEADING EDGE. (C-CHECK RO 11/12/2022) REPAIRED DAMAGE TO LH INBD FLAP VANE SKIN INBD AND OTBD CHAFES PER REO 601R-57-52-004 REV-D DATED 2012-12-19. REPLACED LH INBD FLAP VANE SKIN CHAFED MIDDLE SKIN PANEL PESDR SWAA2022092743887None · debondedDEBONDED O/B AFT FLAP LOWER SURFACE AT LT WING. PERFORMED INTERIM REPAIR ON O/B AFT FLAP LOWER SURFACE AT LT WING IAW SRM SRM 57-53-01-2R-16 REPAIR 16.SDR SWAA2022091344229None · delaminatedLEFT WING OB AFT FLAP HAS LARGE AREA OF DELAMINATION ON LOWER SKIN IB END. / [01] REMOVED LEFT OUTBD AFT FLAP TO F.O.M;[02] INSTALLED LH TRAILING EDGE OUTBD AFT FLAP IAW AMM 27-51-22;[03] INSPECTED C/A 2. LH TRAILING EDGE OUTBD AFT FLAP IAW AMM 27-51-22;[04] RSDR SWAA2022091244105Flap Track · wornWEAR ON FLAP TRACK 3 UPPER AND LOWER TRACK FLANGE ROLLER CONTAC INBOARD AT LT WING 2022-447246 / [01] REPAIRED FLAP TRACK 3 UPPER AND LOWER TRACK FLANGE ROLLER CONTAC INBOARD AT LT WING IAW B737-700 SRM 57-53-02-2R-10 REPAIR 10 PARAGRAPH 4;PERFORMED FLUORESCENSDR SWAA2022091244111None · wornWEAR ON FLAP TRACK 6 LOWER TRACK FLANGE ROLLER CONTAC INBOARD AT RT WING 2022-447262 / [01] REPAIRED FLAP TRACK 6 LOWER TRACK FLANGE ROLLER CONTAC INBOARD AT RT WING IAW B737-700 SRM 57-53-02-2R-10 REPAIR 10 PARAGRAPH 4;PERFORMED FLUORESCENT PENETRANT INSPECTISDR CALA2022081902122Skin · puncturedLEFT OUTBOARD AFT FLAP HAS SIX PUNCTURES DUE TO HAIL 1. 103 INCHES INBOARD FROM OUTBOARD EDGE 9 INCHES FROM TRAILING EDGE .25 INCH DIAMETER 2. 129.25 INCHES INBOARD 6.25 INCHES FROM TRAILING .5 INCH DIAMETER 3. 75.25 INCHES OUTBOARD 3.5 INCHES FROM TRAILING .7SDR SWAA2022090842601None · delaminatedLH O/B AFT FLAP LOWER SURFACE HAS DELAMINATION AT LOWER INBD CORNER . / [01] REMOVED AND REPLACED WITH NEW L/H OUTBOARD AFT FLAP PER A.M.M. 27-51-22.;[02] VERIFIED L/H O/B AFT FLAP REMOVED AND REPLACED.SDR SWAA2022090842603None · delaminatedRH O/B AFT FLAP LOWER SURFACE HAS DELAMINATION AT LOWER INBD CORNER . / [01] OK TO INSTALL R/H O/B AFT FLAP;[02] REMOVED AND REPLACED R/H OUTBOARD AFT FLAP PER AMM 27-51-22. REFERENCE ALL STEPS FOR INDIVIDUAL WORK PERFORMED.;[03] VERIFIED R/H O/B AFT FLAP REMOSDR SWAA2022082545974Flap · delaminatedRIGHT WING O/B AFT FLAP LOWER SURFACE I/B T/E CORNER IS DELAMINATED. MEASURES 1 X 1 / [01] R&R RIGHT WING O/B AFT FLAP PER AMM 27-51-22. REQUIRES RIG CHECK.;[02] WITNESSED R AND R OF RIGHT O/B AFT FLAP PER 27-51-22 UP TO SECTION (G) OUTBOARD AFT FLAP ADJUSTMENSDR SWAA2022081942121Support Bracket · crackedRIGHT WING LOWER WEB SUPPORT BRACKET UNDER FIXED PANEL HAS 2 EACH CRACKS. / [01] REMOVED AND REPLACED PER SRM 51-40-02SDR FDEA202208121972Skin · delaminatedLEFT WING OUTBOARD FLAP LOWER SKIN WITH DENT AT OTEF STA 333. LH WING OUTBOARD FLAP LOWER SKIN, DENT AT OTEF 333 WAS REPAIRED IAW SRM 57-53-01-2R PAG. 1 TO 9 FIG. 201 SHEET 1 AND SRM 51-70-10-2R REPAIR 2 PAG. 9, 101, 128-134 REV. 82 DEC15/2021SDR SWAA2022090940263None · debondedCUSTOMER REQUEST - DEBONDED EXISTING REPAIR ON OB AFT FLAP UPPER SURFACE I/B EDGE AT RT WING 2022-426805 / [01] TOOL USED: CALIPER P/N:500-193-30 S/N:0000285 DUE DATE: 10-DEC-22;[02] TOOL USED BOND TESTER P/N: S-3; S/N: 064; DUE DATE: 19-JUL-23.;[03] TOOL USEDSDR FDEA202208082051Skin · dentedFOUND A DENT AT RH O/B FLAP UPPER SURFACE I/B T/E. CUT OUT THE DAMAGE AREA AND REPAIR WITH EXTERNAL DOUBLER I.A.W EA NO:6-5750-T0370136 P1, SEQ NO:000767, TITLE:WING - FLIGHT SURFACES - RH OUTER FLAP TRAILING EDGE UPPER SKIN REPAIR BETWEEN RIBS 3A AND 3B &SDR FDEA202208061903Skin · damagedLEFT HAND WING INBOARD FLAP OUTBOARD TRAILING EDGE BETWEEN XIFH 247.32 AND XIFH 251.32 EXISITING REPAIR DOUBLER UNABLE TO COMPLY WITH E.A. # : 1-5750-T0357767 B P2 WORK STEP 1. LEFT HAND WING INBOARD FLAP OUTBOARD TRAILING EDGE BETWEEN XIFH 247.32 AND XIFHSDR IPXA2022102643200Skin · damagedRIGHT WING INBD AFT T/E FLAP OUTBD UPPER SKIN GAUGED/DAMAGED, REF T3F18E000EY8Y COMPLIED WITH EO 84104-REQ7. THIS CLEARS DEFERRALSDR 2022FA0000418Skin · gougedR/H INBOARD FLAP HAS A GOUGE ON THE UPPER SURFACE APPROXIMATELY 14" FROM OUTBOARD EDGE AND 1" FROM TRAILING EDGE, MEASURING .5" IN LENGTH AND .03 IN WIDTH, FROM A TOOL FALLING ON THE FLAP. ACCOMPLISHED TEXTRON AVIATION ENGINEERING ORDER, DQ35433M1, DATED: JULYSDR SWAA2022090636043None · crackedCRACK ON CORRUGATED PLATE LOCATED IRSS 215 OF TRAILING EDGE LT WING 2022-410197 / [01] REPLACED CORRUGATED PLATE LOCATED IRSS 215 OF TRAILING EDGE LT WING I.A.W.B737-700 SRM 51-40-02 AND DRAWING #115A2001 REV ?A?.;[02] TASK COMPLETEDSDR SWAA2022090636046None · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 268 AT RT WING 2022-410204 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 268 AT RT WING I.A.W.B737-700 SRM 51-40-02 AND DRAWING # 116A2781 REV ?B?;[02] COMPLETE TASK CERTIFIEDSDR IPXA2022072884662Bracket · crackedINSPECTION TYPE:1CRH WING TRAILING FLAP, BETWEEN BOTH FLAPS AFT HAS BROKEN BRACKET.REMOVED AND REPLACED IAW SRM 51-40-21.SDR SWAA2022090635600None · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT LT WING 2022-410188 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT LT WING I.A.W.B737-700 SRM 51-40-02 AND DRAWING# 115A2001 REV ?;[02] COMPLETE TASK CERTIFIED
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