JASC 5753
Service difficulty reports · 31,484
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 FDEA202610191605Attach Angle · damagedR/H WING INBD T/E FLAP, OUTBD TRACK FAIRING 672HB ATTACH ANGLE HAS ELONGATED HOLES. PERFORMED REPAIR IAW B757-200 SRM 57-53-02-2R FIG 202 REPAIR 3 SHEET 1 AND 2. REMOVED AND REPLACED FITTINGS P/N 113N2304-10 AND 113N2306-1 IAW SRM 51-40-02. THIS CATAGORY B SDR FDEA202610191603Skin · gougedRH WING INNER FLAP UPPER SKIN FOUND 1EA GOUGE BTW RIB4-5SDR SWAA2026101901367Support Bracket · delaminatedRIGHT WING NR 8 FLAP FWD CANOE FAIRING FWD SUPPORT BRACKET RUBBER BOLT ISOLATOR IS DELAMINATED. REMOVED AND REPLACED R/H WING #8FLAP FWD CANOE FAIRING FITTING ASSY IAW AMM 20-50-11.SDR DALA2026101505668Roller · wornRIGHT WING OUTBRD FLAP, OUTBRD UPLOCK ROLLER WORN. REPLACED ROLLER PER A330 AMM 27-54-73. OK FOR SERVICE. (1865718) AIRCRAFT WAS GROUNDED.SDR DALA2026101505667Roller · wornSHIP 3420 LEFT WING FLAP. O/B FLAP, O/B END FLAP GUIDE ROLLER IS WORN. CORRECTIVE ACTION: REPLACED ROLLER PER A330 AMM 57-52. (1865714) AIRCRAFT WAS GROUNDED.SDR FDEA202610141573Skin · dentedLEFT WING OTBD FLAP LWR SURFACE FOUND DENTED AT 3" TO AFT EDGE AND 195" TO IB EDGE. REPAIRED LH WING OB FLAP LWR SURFACE DENT AT OTEF STA 218 AS PER B777 SRM 57-53-01-2R- 2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4G FIGURE 210 REV 54.1 AND EA: G-5750-T03SDR IPXA2026101442976Flap System · faultedAIR TURN BACK, EMERGENCY DECLARED. AFTER TAKEOFF ON FLAP RETRACTION EICAS MESSAGE LE SLAT ASYMMETRY. FOLLOWED QRH PROCEDURE COULD NOT RETRACT SLAT. RETURNED SDF.SDR YENA2026101600981Skin · corrodedDURING HEAVY MAINTENACE, DENTS ON LOWER SURFACE OB FLAP TAB EXTERNAL SKIN ON RH WING; (RESOLVED ON W/O: 1492823 TASKCARD: NR-00015 ) REF: ARM W/O 2026 284/1 N/R 2026-598382 REPAIRED LOWER SURFACE OB FLAP TAB EXTERNAL SKIN ON RH WING IAW EC NO. A26-897-01, EA-5SDR FDEA202610121559Skin · corrodedLEFT WING INBD FLAP UPPER SURFACE O/B SIDE EXTERNAL SKIN SOME AREA WITH CORROSION. LT WING I/B FLAP UPPER SURFACE O/B SIDE WAS REPAIRED IAW B757 SRM 57-53-01-2R REPAIR 1 FIGURE 201 DETAIL I (SHEET 2) AND SRM 51-70-10-2RSDR FDEA202610111552Skin · dentedLEFT WING OTBD FLAP LWR SURFACE FOUND DENT AT 33" AWAY TO IB EDGE AND 19" TO AFT EDGE. REPAIRED LH WING OB FLAP LWR SURFACE DENT AT OTEF STA 56 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4G FIGURE 210 REV 54.1 AND EA: G-5750-T03SDR FDEA202610111551Skin · dentedLH WING OB FLAP LWR SURFACE FOUND DENT AT 37" AWAY TO IB EDGE AND 16" TO AFT EDGE. REPAIRED LH WING OB FLAP LWR SURFACE DENT AT OTEF STA 60 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4G FIGURE 210 REV 54.1 AND EA: G-5750-T038904SDR JR2R20261011638Fitting · corrodedLEFT WING NR 1 FLAP INSIDE TORQUE TUBE ACCESS PANEL 561ET INBD FITTING CORRODED AFT OF NUTPLATE. REPAIRED.SDR JR2R20261011673Fitting · corrodedRIGHT WING NR 1 MAIN FLAP INSIDE TORQUE TUBE ACCESS PANEL 661ET, INBD FITTING CORRODED AT SECOND NUTPLATE. REPAIRED.SDR UIEA2026100900975Skin · corrodedCORROSION FOUND ON R/H INBOARD MAIN FLAP LOWER SKIN (DAMAGE SIZE: L=11.2", W=1.7")(<P>REPAIRED THE R/H INBD MAIN FLAP LOWER PANEL (P/N 113T2243-2) SKIN IN ACCORDANCE WITH BMN SP1-TLS-26-0036, WHICH WAS APPROVED BY FAA FORM 8100-9 DATED 08OCT2026. NO FURTHER DESDR UIEA2026100900976Structure · corrodedCORROSION FOUND ON L/H INBOARD MAIN FLAP LOWER CHORD (DAMAGE SIZE: L=19")(<P>PER BOEING RDR SP1-TLS-26-0037-05B, INSTALLATION OF CHORD (P/N 113T2225-401) ON THE FLAP (P/N 113T2201-23A) FOR AIRCRAFT N649GT HAS BEEN APPROVED AS STRUCTURALLY ACCEPTABLE. REMOVED LSDR UIEA2026100900977Flap · damagedCORROSION FOUND ON RT INBD MAIN FLAP LOWER CHORD (DAMAGE SIZE: L=12") REMOVED RT INBD MAIN FLAP LOWER CHORD AND REPLACED WITH NEW CHORD PER SRM 51-40-02. HOLE COPIED PER SRM 51-40-05. NUT-PLATES INSTALLED PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.SDR SWAA2026101218078Skin · delaminatedLEFT WING INBD AFT FLAP HAS DELAMINATED 20 INCH FROM INBD EDGE AND 4" FROM T/E ON THE LOWER SIDE. 4.1" X 3.8". 01. REMOVED AND REPLACED IAW AMM 27-51-12-401.SDR SWAA2026101239768Skin · delaminatedRIGHT OTBD T/E FLAP LOWER SKIN DELAMINATED, APPROX 26 1/4 INBD FROM INBD EDGE & 7 1/4 FROM T/E. R & R IAW AMM 27-51-22-401.SDR UIEA2026100500953Bearing · migratedRT WING T/E FLAP TRACK #6 FITTING SUSPECT MIGRATION. RT WING T/E FLAP TRACK #6 FWD FITTING BEARING REMOVED AND INSTALLED OVERSIZED BEARING AS PER EN 3687-26 REV. 0.NO FURTHER DEFECTS NOTED.SDR DALA2026100705545Flap · damagedFOUND DAMAGE ON LEFT TRAILING EDGE FLAP, INSTALLED PERMANENT REPAIR PER B717 SRM 57-00-01-02A. (9483579) (AIRCRAFT GROUNDED).SDR DALA2026100605530Skin · dentedSEVERAL DENTS ON LOWER SKIN OF RT AFT MOVABLE VANE WAS FOUND AT RT WING. AREA AT RT AFT MOVABLE VANE RT WING WAS REPAIRED IAW ER/A 637238-14. (1850252) AIRCRAFT WAS GROUNDED.SDR FDEA202610031471Skin · damagedR/H WING, INBD AFT FLAP LOWER SURFCE HAS IMPACT DAMAGE LOCATED APPOX. 42" FROMINBD EDGE AND APPROX. 6" FROM AFT EDGE. REPAIRED R/H WING INBD AFT FLAP TRAILING EDGE WEDGE LWR SURFACE APPROX. 42" FROM INBD EDGE AND APPROX. 6" FROM AFT EDGE AN AREA OF .3 X .SDR HNAA2026100500945Shroud · unsecureFLAP FAIL AT 11 DEGREES DURING GO-AROUND. INSP'D FLAPS & FOUND L/H INBD FLAP SHROUD OTBD ROLLER MISSING & FLAP JAMMED INTO SHROUD, REMOVED L/H INBD FLAP, INSTALED SHROUD BEARING, INSTALLED FLAP IAW AMM 27-50-00-405-801A. RIGGED IAW AMM 27-53-04. OPS CHECK SDR IPXA2026100856727Skin · debondedFAULT - DISBOND - END CAP, R/H WING T/E OUTBD FLAP INBD. MEASURE THE DAMAGE AREA (L:1.5", W:0.1", D:2PLIES, 7" FROM AFT EDGE, AT INBD EDGE). BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W UPS SREO-70175-RSDR IPXA2026100857298Skin · crackedFAULT - CRACK - SKIN, R/H WING T/E INBD MAIN FLAP INBD UPPER. (REPAIR). MEASURE THE DAMAGE AREA (DIA:1", 16.5" FROM INBD EDGE, 3.5" FROM AFT EDGE). BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300FSDR SWIA2026100277469Rod · bentDURING PHASE 1 INSPECTION FOR FLAP 3 OVERSPEED, FOUND UPPER INBD FLAP ROD ON LT INBD FLAP ASSY TO BE BENT. REMOVED AND REPLACED THE FLAP ROD IAW AMM 57-54-30, OPS CHECK GOODSDR 4T1R20261005001Spigot · corrodedDURING THE BORESCOPE INSPECTION OF THE INBOARD FLAP INTERNAL STRUCTURE PER AMM 57-51-00-290-801, STEP F.(3), CORROSION WAS IDENTIFIED INSIDE THE AFT SPIGOT TUBE INNER BORE ON THE LEFT-HAND INBD FLAP.REFERENCE BOMBARDIER REPAIR ENGINEERING ORDER 700-57-51-535SDR FDEA202610021470Skin · dentedLEFT WING OUTBOARD TRAILING EDGE FLAP HAS MULTIPLE AREAS OF DAMAGE. SKIN REPAIR IS BEING DONE WITH TWO SEPERATE REPAIRS, THIS ITEM IS TO DOCUMENT THE SECOND REPAIR. REPAIRED DAMAGED TOPSKIN ON LWR SURFACE OF L/H WING O/B FLAP TRAILING EDGE WEDGE AREA OF SDR FDEA202610021469Skin · dentedLEFT WING OUTBOARD TRAILING EDGE FLAP, UNDERSIDE OF TRAILING EDGE WEDGE, INSIDE OF OUTBOARD FLAP FAIRING, HAS MULTIPLE AREAS OF DELAMINATION. MARKED WITH TAPE. REPAIRED DAMAGED TOPSKIN ON LWR SURFACE OF L/H WING O/B FLAP TRAILING EDGE WEDGE AREA OF 9 X 5 SDR SWAA2026100513123Bracket · crackedLEFT WING ANGLE, BRACKET INBD OF RAY GUN ON TRAILING EDGE SHELF PANEL CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02.SDR AALA202610160128Link · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING FLAP TRACK 2 INBOARD LINK - REPLACED LINK PER AMM 57-55-11SDR SWIA2026092977608Flap Track · damagedRIGHT WING FLAP TRACK 1A, HAD THICKNESS REDUCTION DAMAGE, MAX DEPTH OF DAMAGE IS 032, REQUIRES 200 FC, REINSPECT UNTIL DEPTH OF DAMAGE EXCEED 068, IAW SRM 57-52-03 AD01 TABLE 101. REMOVED & REPLACED, THE RT WING INBD FLAP AFT TRACK 1A IAW AMM 57-54-25.SDR SWIA2026092977607Flap Track · damagedLEFT WING FLAP TRACK 1A HAD THICKNESS REDUCTION DAMAGE, MAX DEPTH OF DAMAGE IS 033, REQUIRES 200 FC RE-INSPECT UNTIL DEPTH OF DAMAGE EXCEED 068, IAW SRM 57-52-03AD01, TABLE 101, REMOVED & REPLACED, THE LT WING INBD FLAP AFT TRACK 1A IAW AMM 57-54-25.SDR SWAA2026092941349Panel · delaminatedDURING WALKAROUND, FOUND THE LEFT WING INBD FLAP, AFT PANEL DELAMINATED. REMOVED AND REPLACED THE LT INBD TRAILING EDGE FLAP WEDGE PANEL IAW CMM 57-53-05.SDR IPXA2026100252112Fairing · puncturedPUNCTURED SKIN, LT WING NR 4 FLAP TRACK AFT FAIRING EXTERNAL SKIN. REMOVE THE PUNCTURED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200F FOR 240 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. IAW SRM 57-53-70-2R-1 REFER TO SRM 51-70-04-2R-1 AND SRSDR IPXA2026100352096Seal · brokenBROKEN-MOLDING SEAL, LT WING NR 1,FLAP EXTERNAL SKIN MOLDING SEAL AREA. REMOVE THE RAIN EROSION SHIELDS AND CLEAN. APPLY THE SEALANT TO REPAIR AREA CURED AT 70F FOR 20 HOURS IAW SRM 57-43-02-2R-4 REV.49 REFER TO SOPM 20-50-12 REV. 160.SDR DALA2026092905410Fitting · corrodedLEFT WING INBOARD FLAP FWD FITTING CORROSION. CORRECTIVE ACTION: REPAIRED PER ER/A 00-637122. (1833480) AIRCRAFT WAS GROUNDED.SDR UIEA2026092300913Skin · dentedRH WING INBOARD AND AFT FLAP LOWER SURFACE HAS A DENT ABOUT WBL 340.(<P>ACCOMPLISHED MAJOR REPAIR OF RH INBOARD AND AFT FLAP LOWER SURFACE. HOT-BONDED METAL-TO-METAL REPAIR IAW SRM 57-53-01-2R-1 REPAIR 1 DETAIL III FIG 201, SHEET 4 TABLE III FIG 201, SHEET 10 SDR AALA202609252387Tab · crackedAIRCRAFT WAS GROUNDED: CRACKED RIGHT WING TRAILING EDGE OUTBOARD FLAP TAB - MAINTENANCE REPAIRED THE FLAP TAB PER EA 379370SDR DALA2026092405332Cone · missingDURING WALKAROUND, FOUND LT FLAP TRACK NR 2 TAILCONE MISSING. PLACED ON A330 CDL 57-00-04B. (8804946) AIRCRAFT WAS GROUNDED.SDR DALA2026092405327Vane · damagedDENT AND DEBONDS WERE FOUND ON SUBJECT RT WING AFT MOVABLE FLAP VANE SKIN AT LOWER SURFACE AFT END LOCATION, COMPLIED WITH ER/A 619367-14. (1828149) (AIRCRAFT GROUNDED).SDR DALA2026092405326Vane · damagedSEVERAL DENTS WITH DEBONDS WERE FOUND AFFECTING THE LOWER LT AFT MOVABLE FLAP VANE SKIN, COMPLIED WITH ER/A 637033-14. (1828236) (AIRCRAFT GROUNDED).SDR SWAA2026092833996Fairing · pulledNR 3 FLAP TRACK AFT FAIRING HAS 7 CONSECUTIVE FASTENERS MISSING OR PULLED THROUGH ALONG OB UPPER EDGE NEAR TAIL CONE REMOVED AND REPLACED THE #3 FLAP TRACK AFT FAIRING IAW AMM 27-51-18-400-802. REMOVED AND REPLACED THE #3 FLAP TRACK AFT FAIRING IAW AMM 27-51-1SDR FDEA202609221403Rib · crackedRIGHT WING CENTER FLAP RIB UPR FLANGE FOUND CRACK AT RIB15 BETWEEN STRINGERS 2.6, 2.7, & 2.8. CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100 I.A.W EA T6-5750-T0378801 P1, SEQ 1119, LT CENTER FLAP WITH OVERSIZED HOLE ON UPPER SKIN AT RIB 11. REPAIRED IAW GMM6-2SDR FDEA202609221402Rib · crackedLEFT WING CENTER FLAP RIB UPPER FLANGE FOUND CRACKED AT RIB 26 BETWEEN STGR2.6 AND STGR2.7. COMPLIED WITH EA 6-5750-T0388894 P1 REPAIR LT WING CENTER FLAP UPR FLANGE CRACK. THIS IS CAT A REPAIR. MAJOR REPAIR IAW GMM6-2-100.SDR UATA5120929265701Flap Track · crackedFOUND CRACK IN OUTBOARD FLAP TRACK ON RH WING., TRACK WAS REMOVED AND REPLACED WITH NEW TRACK (PN: MC2622075-6, SN: J079924-020) AND BACK DRILLED TO PRE-EXISTING RIVET SIZES. TRACK WAS INSTALLED WITH MS20470AD RIVETS, AND HL18PB HI-LOKS OF VARYING LENGTHS. ALLSDR DALA2026092105257Roller · wornRIGHT WING OTBD FLAP GUIDE ROLLER IS WORN. REPLACED ROLLER PER A330 AMM 27-54-73. (1822262) AIRCRAFT WAS GROUNDED.SDR AALA202610130007Link · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FLAP TRACK 2 INBOARD LINK - REPLACED LINK PER AMM 57-55-11SDR SWAA2026101227866Access Panel · damagedELONGATED HOLES ON RT WING ACCESS PANEL 661CB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.SDR SWAA2026092125651Wedge · delaminatedRIGHT INBD FLAP, AFT OTBD TRAILING EDGE SHOWS EVIDENCE OF DELAMINATION. REMOVED THE FLAP WEDGE. LOCATED & INSTALLED NUTPLATES TO NEW WEDGE IAW SRM 51-40-10. INSTALLED A SERVICEABLE FLAP WEDGE IAW SRM 51-40-02. APPLIED FILLET SEAL TO THE RT INBD MAIN FLAP W
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