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 DALA2024032603801Support Rib · damagedSHIP 1708 T/E FLAP SUPPORT RIB ASSY POSITION #1-REACTION RING DAMAGED. CORRECTIVE ACTION: REMOVED AND REPLACED #1 REACTION RING REF WC 2751-01046-02A (0260251)SDR DALA2024032503737Skin · debondedTWO DISBONDS FOUND ON LH AFT MOVABLE FLAP VANE LOWER SKIN: 1) LENGTH=1.700IN, WIDTH=1.500IN AND 2) LENGTH=2.100IN, WIDTH= 1.000IN (IN REF MON/9541/0138992 JOB # 005-0001). SUMMARY OF NRC 00037: LH AFT MOVABLE FLAP VANE LOWER SKIN WAS REPAIRED PER ERA 595913-14SDR DALA2024032503736Skin · debondedTWO DISBONDS WERE FOUND OF: 0.500 IN LENGTH .X 0.500 IN. WIDTH. ON DENTS LOWER SKIN AT LH CENTER FLAP VANE 26.500 IN. INBOARD EDGE, 12.500 IN. TRAILING EDGE AND 28.000 IN. INBOARD EDGE, 12.500 IN. TRAILING EDGE. (IN REFERENCE JOB# 020-0001) SUMMARY OF NRC 0065SDR 2026FA0000356Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKEDSDR AALA202403271155Skin · delaminatedAIRCRAFT WAS GROUNDED: RIGHT WING TRAILING EDGE FLAP DELAMINATED AND DISBONDED. INSTALLED SERVICEABLE INBOARD FLAP WEDGE PER SRM 57-53-01.SDR AALA202403277222Skin · delaminatedAIRCRAFT WAS GROUNDED: LEFT WING INBOARD FLAP LOWER SKIN DELAMINATED. INSTALLED SERVICEABLE INBOARD FLAP WEDGE PER SRM 57-53-01.SDR AALA202403264249Skin · delaminatedAIRCRAFT WAS GROUNDED: RIGHT HAND OUTBOARD T/E FLAP END LOWER SKIN HAS A 1O BY 9 INCH AREA OF DELAMINATION. REMOVED AND REPLACED RIGHT HAND OUTBOARD T/E FLAP. PER AMM 27-51-22.SDR DALA2024032203645Skin · damagedSHIP 3144 DAMAGE TO RIGHT HAND OUTBRD FLAP TRAILING EDGE. CORRECTIVE ACTION: RIGHT HAND OUTBOARD FLAP TRAILING EDGE REPAIRED PER A319 SRM 57- 53-00-300-120. (5544854)SDR DALA2024032103593Guide Vane · puncturedPUNCTURE ON AFT MOVABLE GUIDE VANE AT RH WING. SUMMARY OF NRC 00042: AFT MOVABLE GUIDE VANE AT RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 AND 51-70-02-0G PROCEDURE GENERAL. (LP #0254635)SDR SWAA2024041766042Skin · delaminatedLEFT HAND WING OUTBOARD TRAILING EDGE FLAP HAS AN AREA OF DELAMINATION AT IB END LOWER SURFACE (MKD).<[01] REMOVED DAMAGE SKIN PER SRM 57-53-01-2R-14;[02] INSPECTED WORK PERFORMED ON C/A #1;[03] REPAIRED DAMAGED AREA PER SRM 57-53-01-2R-14.;[04] RII- INSPECTEDSDR DALA2024032603809Skin · damagedMTC TASK - RH WING I/B FLAP ASSEMBLY. O/B LOWER SURFACE FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT RH WING I/B FLAP ASSEMBLY O/B LOWER SURFACE REMOVED AS PER ASR A350-A-51-27-21-01001-667A-A. REPAIR CARRIED OUT AT RH WING I/B FLAP ASSEMBLY O/B LOWER SURFACSDR DALA2024032203644Flap Track · corrodedSHIP 3117 CORROSION RH WING INB FLAP TRACK 2 BEARING AT RIB 9 LEVEL INB & OUTB PLATES. CORRECTIVE ACTION: REPAIRED PER ERA 612080-14. (0254037)SDR DALA2024032003557Lug · corrodedSHIP 3311 RH RIB 6 FITTING FWD LUG WAS FOUND CORRODED. CORRECTIVE ACTION: COMPLIED WITH ERA 616142-33. (0253324)SDR DALA2024032003556Lug · corrodedSHIP 3311 LH RIB 6 FWD LUG WAS FOUND CORRODED. CORRECTIVE ACTION: COMPLIED WITH ERA 616141-33. (0253273)SDR FDEA202403190293Rib · cracked1EA CRACK WAS FOUND AT LH WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.26 S-2.7~S-2.8, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR I.A.W FEDEX EA NO:T6-5750- T0SDR FDEA202403190292Rib · cracked1EA CRACK WAS FOUND AT LH WING CENTER FLAP RIB18 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.18 S-2.8~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W SDR FDEA202403190290Rib · cracked2EA CRACKS WERE FOUND AT LH WING CENTER FLAP RIB12 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT LH CENTER FLAP RIB.12 S-2.7~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-T0378613 SDR FDEA202403190289Rib · cracked1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB27 FWD AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE CAT.A MAJOR FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT RH CENTER FLAP RIB27 I.A.W FEDEX EA NO:T6-5750-T0378627 A P1, SEQ NO:1171, TITLE:WINGS- FLIGHT SSDR FDEA202403190288Rib · cracked2EA CRACKS WERE FOUND AT LH WING CENTER FLAP RIB11 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGES REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.11 S-2.7~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W SDR FDEA202403190287Rib · cracked2EA CRACKS WERE FOUND AT RH WING CENTER FLAP RIB26 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE CAT.A MAJOR FLANGES REPAIR AT RH CENTER FLAP RIB26 I.A.W FEDEX EA NO:T6-5750-T0378627 A P1, SEQ NO:1171, TITLE: WINGS-FLIGHT SURFACES-RH CENTER FLAP; CSDR SWAA2024042565754Skin · debonded(CUSTOMER REQUEST) DEBONDED OB AFT FLAP AT LT WING. PERFORMED INTERIM REPAIR OF OB AFT FLAP AT LT WING IAW B737-700 SRM 57-53-01-2R-16. REPAIR 16; AN REPAIR REQUIERES TAP TEST INSPECTION EVERY 6875 FLIGHT CYCLES OR 30 MONTHS;WHICHEVER COMES FIRST SEE INDIVIDSDR FDEA202403190481Skin · cracked2EA CRACKS WERE FOUND AT RH WING CENTER FLAP RIB26 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE CAT.A MAJOR FLANGES REPAIR AT RH CENTER FLAP RIB26 I.A.W FEDEX EA NO:T6-5750-T0378627 A P1, SEQ NO:1171, TITLE:WINGS-FLIGHT SURFACES-RH CENTER FLAP; SDR FDEA202403190480Skin · cracked1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB27 FWD AREA OF TOP SURFACE RIB FLANGE ACCOMPLISHED THE CAT.A MAJOR FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT RH CENTER FLAP RIB27 I.A.W FEDEX EA NO:T6-5750-T0378627 A P1, SEQ NO:1171, TITLE:WINGS- FLIGHT SUSDR FDEA202403190478Skin · cracked1EA CRACK WAS FOUND AT LH WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.26 S-2.7~S-2.8, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR I.A.W FEDEX EA NO:T6-5750- T0SDR FDEA202403190477Skin · cracked1EA CRACK WAS FOUND AT LH WING CENTER FLAP RIB18 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.18 S-2.8~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FSDR FDEA202403190476Skin · cracked2EA CRACKS WERE FOUND AT LH WING CENTER FLAP RIB12 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGES REPAIR AT LH CENTER FLAP RIB.12 S-2.7~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-T0378613SDR FDEA202403190475Skin · cracked2EA CRACKS WERE FOUND AT LH WING CENTER FLAP RIB11 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGES REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.11 S-2.7~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W SDR SWAA2024041165840Skin · delaminatedRH O/B AFT FLAP I/B LOWER CORNER DELAMINATED ON LOWER AND UPPER SURFACE.<[01] 05 - OK TO CONTINUE AND INSTALL RH O/B TE FLAP PER MM 27-51-21;[02] 01 - REMOVED AND REPLACED PER [AMM 27-51-22-401-NG (OUTBOARD AFT FLAP - REMOVAL/INSTALLATION - PERMANENT)];[03] RISDR ENHA04032024Flap Track · corrodedDURING ANNUAL INSPECTION IT WAS NOTED THAT ALL FLAP TRACKS SHOWED SIGNS OF CORROSION. WITH THE DEGREE OF CORROSION IT WAS DECIDED TO REPLACE ALL FLAP TRACKS.FLAP TRACK PNS: 2622075-4 , 2622075-5,2622075-6SDR SWAA2024040365610Skin · delaminatedRH OTBD AFT FLAP INBD LOWER SURFACE HAS DELAMINATION.<[01] REMOVED RIGHT WING O/B T/E FLAP ASSY PER AMM 27-51-22;[02] OK TO INSTALL AFT FLAP.;[03] INSTALLED NEW AFT FLAP IN REF TO AMM 27-51-22;[04] INSPECTION C/W FOR CA #3;[05] DUE TO FAILED RIG CHECK REMOVED SDR CALA2024032200847Limiter · trippedFLIGHT CREW REPORTS FLAPS OVERSPEED DUE TO GO AROUND FLAPS 3 , HEARD AUDIBLE CHIME 3 TIMES, CREW STATED THEY DID NOT OBSERVE THE DURATION OR HOW MUCH OF AN OVERSPEED THE AIRCRAFT REACHED. VARGAS TOMC REQUIRES TASK 05-51-13-200-001 INSPECTION AFTER FLAP/SLAT EXSDR SWAA2024031965467Skin · delaminatedL/H O/B TRAILING EDGE FLAP REQUIRES REPLACEMENT. REMOVED LH OTBD AFT FLAP IAW AMM 27-51-22. REMOVED AND REPLACED LH OB AFT FLAP PER AMM 27-51-26.SDR SWAA2024031965191Skin · delaminatedL/H WING OUTBD AFT FLAP IS DELAMINATED ON LOWER INBOARD TRAILING EDGE SURFACE. DELAMINATION MEASURES 1.85 IN FORWARD DIRECTION AND 5.35 IN SIDE DIRECTION. CONTINUED IN FAULT DESCRIPTION BOX. L/H WING OUTBD AFT FLAP IS DELAMINATED ON LOWER INBOARD TRAILING EDGESDR DALA2024032003534Skin · puncturedSHIP 1813 R/H WING O/B FLAP UPPER SURFACE FOUND PUNCTURE 29IN FROM I/B 23 FROM T/E. CORRECTIVE ACTION: R/H WING O/B FLAP UPPER SURFACE REPAIRED AT 29IN FROM I/B ,23IN FROM T/E AS PER B767-400 SRM 57-53 -01-2R-1 & SRM 51-70-10-2R-4 FIG201-SHEET3 & SRM 51-70-10-SDR FDEA202403180308Skin · dentedTWO DENTS ON LH WING, INBD AFT FLAP UPPER SURFACE BTWN IFS 153/158. LH WING, INBD AFT FLAP UPPER SURFACE BTW IFS 153/158 WAS REPAIRED IAW B767 SRM 57-53- 01-2R REP 1 AND SRM 51-70-10-2R REP 4 FIG 201 (SHEET 1) REV 88 DEC 15/2023.SDR DALA2024032103578Skin · dentedDENTS OUT LIMITS WERE FOUND ON REVALUATION DENTS OF LOWER SKIN FWR MOVABLE VANE FLAP AT LH WING. SUMMARY OF NRC 00659: PERMANENT REPAIR WAS PERFORMED ON FWD MOVABLE FLAP VANE (LOWER SKIN) OF LH WING PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PAR 4. (LP SDR SWAA2024031864684Skin · delaminatedLH WING OUTBD TRAILING EDGE FLAP IS DELAMINATED AT LOWER INBD END. 17IN X 9IN<[01] CW EA 24-127-00702;[02] CWSDR AALA202405226608Skin · debondedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD TRAILING EDGE FLAP LOWER SURFACE EXISTING REPAIR HAS BECOME DEBONDED BETWEEN FLAP RIBS 1 AND 2, 2.09 INCHES FROM THE INBOARD EDGE OF THE FLAP. REPAIRED FLAP LOWER SURFACE PER EA 353431.SDR SWAA2024040564489Fairing · damagedL WING #2 MAIN FLAP TRACK FAIRING TAILCONE HAS ELONGATED FASTENERS HOLES.<[01] ADDED STEP 1.;[02] REMOVED AND REPLACED #2 FLAP TRACK TAIL CONE FARING PER SOPM 20-50-01<BR>01 - REMOVED AND REPLACED PER [SOPM SOPM REPREF NOT FOUND (SOPM REPAIR REFERENCE NOT FOUNSDR SWAA2024040564485Skin · delaminatedLH OTBD AFT FLAP HAS DELAMINATION ON INBD LOWER SURFACE.<[01] REMOVED LH OTBD AFT FLAP.;[02] REMOVED AND REPLACED L/H O/B AFT FLAP PER AMM 27-51-22.;[03] INSPECTED WORK ACCOMPLISHED IN C/A #2 (RII)SDR SWAA2024040464340Panel · crackedLEFT WING T/E DEFLECTION CONTROL RIB UPPER PANEL ATTACH FLANGE IS CRACKED IN HALF. DISASSEMBLED AND REMOVED DAMAGE PER SRM 57-51-02-2R-3. PERFORMED NDT INSPECTION PER NDT PART 6 51-00-00 PROCEDURE 23. NO DEFECTS NOTED. FLAP PEENED REPAIR AREA AND FABRICATESDR ASAA2024031550036Skin · dentedLESSOR ITEM: MULTIPLE LOWER FLAP DENTS BEHIND RIGHT MAIN WHEEL, MAP AND MEASURE ALL. GROUNDED - YES. PERFORMED CATEGORY A PERMANENT REPAIR IN 2EA AREAS ON R/W I/B FLAP LOWER SURFACE IN ZONE 2.AREA 1 REPAIR MEASURES 55" FROM I/B EDGE, 6" FROM T/E REPAIR DOUBLESDR ASAA2024031550035Skin · dentedLESSOR ITEM: MULTIPLE LOWER FLAP DENTS BEHIND LEFT MAIN WHEEL, MAP AND MEASURE ALL GROUNDED - YES. REPAIRED CLUSTER 1 DENTS ON L/W LOWER FLAP, FINAL MEASUREMENT OF REPAIR IS 14.4" X 11.4" LOCATED 45.25" FROM INBOARD AND STOPS 59.65". CLUSTER 2 IS BEING TRACKSDR CALA2024031900791Rivet · missingLEFT WING #4 FLAP AFT FAIRING OUTBOARD TOTAL 20EA RIVETS MISSING OR LOOSE. RIGHT WING #5 FLAP AFT FAIRING OUTBOARD TOTAL 20EA RIVETS MISSING OR LOOSE. INBOARD TOTAL 10EA RIVETS MISSING OR LOOSE. ABOVE FAIRING POSITION IS LEFT WING #3 FLAP AFT FAIRING. ACPD PERSDR FDEA202403140284Skin · dentedRH WING OB FLAP LWR SURFACE FOUND DENT AT 261 IN AWAY FROM OB EDGE AND 6 IN AWAY FROM AFT EDGE. EVALUATED RH WING OB FLAP LWR SURFACE DENT AT 261 IN AWAY FROM OB EDGE AND 6 IN AWAY FROM AFT EDGE DAMAGE SIZE L X W= 4.2"X 2.4" OUT OF ALLOWABLE LIMIT AS PERSDR FDEA202403140283Skin · dentedRH WING OB FLAP LWR SURFACE FOUND DENT AT 257 IN AWAY FROM OB EDGE AND 14.5 IN AWAY FROM AFT EDGE. EVALUATED RH WING OB FLAP LWR SURFACE DENT AT 257 IN AWAY FROM OB EDGE AND 14.5 IN AWAY FROM AFT EDGE DAMAGE SIZE L X W= 4.0"X 1.2" OUT OF ALLOWABLE LIMIT ASDR CALA2024031800777Panel · damagedDURING ACCOMPLISHMENT OF 2SC FOUND T.E FLAP MECHANISM PANEL 196JR WITH SIGNS OF MISALIGMENT. REMOVED INBOARD FLAP TORQUE TUBE SLOT DOOR PERFORM IAW CDL REF # T.E FLAP MECHANISM PANEL 196JR REMOVED PLACED ON MEL CDL 27B DDP 27B. C/W. ADD EMP:U162722,U399319 DISSDR SWIA2024051000312Vane · chafedRH INBD FLAP VANE CHAFED AT WS104.099 (C-CHECK RO 5/9/2024) REPAIRED R/H I/B FLAP VANE L/E SKIN AT W.S. 104.099 IAW CRJ200 SRM 57-52-00 AND 57-52-00 REPAIR #1. NDT PERFORMED BY BARON NDT LLC CRS#: 5NDR545D REPORT#: S032524-1 DATED 25MAR2024. SEE REPORT FORSDR SWAA2024041060236Fairing · delaminatedLW FWD FLAP FARING 544AB HAS 2EA. AREAS OF DELAMINATION<[01] COMPLETED;[02] COMPLETED REPAIR IAW B737 SRM 51-70-05-2R-0 AND REO-G24951;[03] COMPLETED REPAIR IAW B737 SRM 51-70-05-2R-0 AND <BR>EA 24-157-00654;[04] VERIFIED AND INSPECTED COMPLETED REPAIR PER EA SDR SWIA202404250296Hinge Arm · gougedLEFT INBOARD FLAP INBOARD HINGE ARM AT LOWER LUG TO HINGE BOX GOUGED FROM OLD LOOSE STUCK SCREW IN LUG AREA MX TRANS 27912411 (C-CHECK RO 4/24/2024) BLENDED AND FOUND OUT OF LIMITS REPAIRED PER MHIRJ REO 670-57-52-553 REV -A DATE 2024-03-16. SEE CONTINUAT
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