JASC 5753
Service difficulty reports · 31,490
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 SWAA2026083113941Flap · crackedLEFT OTBD. AFT FLAP, INBD. CLOSURE RIB, UPPER FLANGE CRACKED BELOW LOWER FASTENER HOLE. REMOVED AND REPLACED LT WING OTBD AFT FLAP ASSY IAW AMM 27-51-22.SDR AALA202608311125Flap Track · excess playAIRCRAFT GROUNDED: HIGH FREQ VIBRATION FELT AFTER BEING AT CRUISE AT 39,000 FT FOR 5 MINS. SIMILAR TO A CELL PHONE VIBE. 0 HZ. COULD FEEL IN SEAT & FLOOR, AFT GALLEY COULD HEAR & FEEL IT. DESCENDED TO 35,000 FT. VIBE SLOWLY DECREASED IN INTENSITY AFTER BESDR AALA202610063512Link · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING FLAP TRACK 2 INBOARD LINK - MAINTENANCE REPLACED LINK PER SRM 51-42-11SDR FDEA202608281247Skin · debondedLEFT WING INBD T/E MAIN FLAP, AFT PANEL, REAR EDGE HAD DEBONDING. APPLIED PERMANENT REPAIR ON THE LT WING FLAP AFT PANEL IAW SRM 57-53-01-2R, REP 1, DETAIL I, FIG 201, SHEET 2, IAW IAW SRM 51-70-10-2R, REP 4.SDR FDEA202608281245Skin · dentedFOUND LT WING, T/E, OTBD FLAP LOWER SURFACE, HAD ONE DENT AT CROSS OTEF, 315 INCHES AND T/E 5 INCHES. REPAIRED LH WING T/E O/B FLAP LOWER SURFACE 01 EA DENT AT CROSS OTEF 315 INCHES AND T/E 5 INCHES AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70SDR UIEA2026082400793Skin · damagedRT WING OTBD FLAP LOWER SKIN DAMAGED BEYOND SRM REPAIR LIMIT. OTEF STA 23.25 - 257.19, CATEGORY A REPAIR PERFORMED ON RT WING OTBD FLAP LOWER SKIN DAMAGE IAW SRM 57-53-01-2R-3, REPAIR 3, REV 53, & SRM 51-70-04-2R-0, REPAIR GENERAL, REV 53. NO FURTHER DEFECTSDR DALA2026083104918Skin · corrodedCORROSION UPPER SURFACE IB AFT FLAP LT WING. PERFORMED PERMANENT REPAIR ON UPPER SURFACE IB AFT FLAP LT WING AS PER B767-300 SRM 57-53-01 (1778910)(AIRCRAFT GROUNDED)SDR SWAA2026083106833Skin · delaminatedL/H O/B AFT FLAP HAS AREA OF DELAMINATION ON UPPER SURFACE, 2" O/B OF I/B EDGE AND 2" FWD OF AFT EDGE. DELAMINATION AREA MEASURES 4.5" WIDE, 5" LONG, L/H O/B AFT FLAP HAS AREA OF DELAMINATION ON UPPER SURFACE 2" O/B OF I/B EDGE AND 2" FWD OF AFT EDGE. DELAMINASDR 1Q2R2026082550044Vane · damagedLEFT INBB FLAP BOLT HOLE FOR 548AB HAS BROKEN BOLT IN NUTPLATE AND HOLE IS ELONGATED.SDR IPXA2026090407154Flap Track · erodedERODED SKIN, LT WING NR 1 FLAP TRACK FWD FAIRING EXTERNAL SKIN. REMOVED THE DAMAGED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200 F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG IAW SRM 57-53-70-2R-1, REFER TO SRM 51-70-17-0G-0 REV. 96SDR IPXA2026090307096Fairing · debondedDISBOND - SKIN, L/H WING NO. 3 FLAP TRACK MID FAIRING INBD T/E SKIN. REMOVE THE DAMAGED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300F SRM 57-53-70-2R-1 REFER TO SRSDR IPXA2026083103528Fairing · debondedDEBONDED PANEL, RT WING T/E FLAP NR 8 AFT FAIRING LOWER SURFACE. REMOVED THE DISBOND MATERIALS AND CLEAN. BONDED REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH A MINIMUM VACUUM OF 22 IN/HG.SDR IPXA2026083103549Fairing · debondedDEBONDED RT WING NR 8 AFT FLAP FAIRING LOWER SURFACE. REMOVE THE DISBOND MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH A MINIMUM VACUUM OF 22 IN/HG IAW SRM 57-53-70-2R-1, REF SRM 51-70-05-2R-1, & SRM 51-70-0SDR JR2R20260825350Carriage · gougedRH MAIN FLAP CARRIAGE NR 2 HAS PITTING IN BOLT HOLE FOR O/B UPPER RUB PAD. REPAIRSDR JR2R20260825346Carriage · gougedLH MAIN FLAP CARRIAGE #2 HAS PITTING IN BOLT HOLE FOR I/B LOWER RUB PAD. REPAIRSDR JR2R20260824349Roller Guide · gougedRH O/B FLAP O/B FLAP ROLLER GUIDE RAIL IS GOUGED. REPAIRSDR SWAA2026092974826Access Panel · elongatedELONGATED HOLE ON ACCESS PANEL 542EB, FLAP SUPPORT FAIRING 3, LT WING. REPAIRED THE ACCESS PANEL 542EB ON FLAP SUPPORT FAIRING 3 IAW SRM 51-70-04-2R-9, REPAIR 9.SDR SWAA2026091480621Skin · debondedDEBONDED LOWER SKIN ON OTBD AFT FLAP RT WING. REPAIRED OTBD AFT FLAP RT WING IAW SRM 57-53-01-2R-4, REPAIR 4, & SRM 51-70-10-2R-4, REPAIR 4.SDR SWAA2026091420796Skin · debondedDEBONDED LOWER SKIN ON OTBD AFT FLAP, LT WING. PERFORMED INTERIM REPAIR ON OTBD AFT FLAP AT LT WING IAW SRM 57-53-01-2R-16 REPAIR 16. PERFORMED TAP TEST INSPECTION EVERY 6875 FLIGHT CYCLES OR 30 MONTHS WICHEVER COMES FIRST.SDR SWAA2026091439784Panel · debondedDEBONDED WEDGE PANEL ON RT INBOARD FLAP AT RT WING. PERFORMED INTERIM REPAIR ON WEDGE PANEL ON RT INBD FLAP AT RT WING IAW SRM 57-53-01-2R-18, REPAIR 18. PERFORMED TAP TEST INSPECTION EVERY 6875 FLIGHT CYCLES OR 30 MONTHS WICHEVER COMES FIRST.SDR AALA202609189657Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD FLAP INTERCONNECTING HINGE FITTING BEARING HAS EXCESSIVE PLAY - REPLACED INTERCONNECTING HINGE FITTING PER SRM 51-42-11SDR DALA2026082404788Vane · dentedSEVERAL DENTS ON LOWER SURFACE FWD MOVABLE FLAP VANE AT RT WING, FWD MOVABLE FLAP VANE AT RH WING WAS REPAIRED IAW SRM 57-53-01-2R. (1769283) (AIRCRAFT GROUNDED).SDR SWIA2026082077109Flap Track · wornRH WING FLAP TRACK 2A OUTBOARD HAS WIDTH REDUCTION WEAR OF 1.13MM MAX ALONG ENTIRE LENGTH. REMOVED AND REPLACED RH WING FLAP TRACK 2A OUTBOARD.REF. EMB AMM. 57-54-25.ASSET. TC2-50254 DUE. 9-24-26SDR IPXA2026082877089Skin · debondedDEBONDED LOWER SKIN OF LT WING T/E OTBD FLAP T/E SKIN, WBL 366. IAW SRM 57-53-01-2R-1 REF SRM 51-70-07-0G-0, REV 132. PERFORMED A REPAIR IAW STEP 1. REMOVED THE DISBOND MATERIALS AND CLEANED. MEASURE THE DAMAGE SIZE AND LOCATION(DIA:1", 33.5" FROM INBD EDGE,SDR IPXA2026082577721Skin · debondedDISBOND - SKIN , LOWER SKIN OF L/H WING T/E OUTBD FLAP T/E SKIN WBL 380 (REPAIR) CORRECT THE TYPO IN STEP 1 : 1.I.A.W. 767-300 SRM 57-53-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV.132 PERFORM REPAIR AS BELOW STEP: 1. REMOVE THE DISBOND MATERIALS AND CLEAN. 1.2 MEASDR IPXA2026082577089Skin · debondedDISBOND - SKIN , LOWER OF L/H WING T/E OUTBD FLAP T/E SKIN , WBL 366 (REPAIR) CORRECT THE TYPO IN STEP 1 : 1.I.A.W. 767-300 SRM 57-53-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV.132 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE DISBOND MATERIALS AND CLEAN. 1.2 MEASUSDR IPXA2026082577741Skin · debondedDISBOND - SKIN , INBD EDGE UPPER FACE OF L/H WING T/E OUTBD FLAP T/E SKIN , WBL 355 (REPAIR) PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 6" AROUND HEATED AREA ,PER 767 NDT MANUAL PART 1 51-01-01 REV:144 RESULT: NO DEFECT WAS FOUNDSDR SWAA2026091447653Skin · delaminatedDELAMINATION ON OTBD AFT FLAP, LT WING. APPLIED BONDING PRIMER ON REPAIR LOWER AREA IAW SRM 57-53-01-2R-16, REPAIR 16, PARAGRAPH 4.H(1), SRM 51-70-10-2R-0, REPAIR GENERAL, PARAGRAPH 15. PERFORMED INTERIM REPAIR ON O/B AFT FLAP AT LT WING IAW SRM 57-53-01-2RSDR SWAA2026091091817Beam · cracked#8 CANOE FAIRING PANEL 644BB BEAM ASSY. HAS CRACKED FLANGE BUSHING REPLACED BEAM ASSY IAW AMM 27-51-28-400-802 STEP 5. G. (1) (B). CAL TOOL ID: ATS2632 CAL TOOL DUE: 05/2027 VERIFIED CORRECTIVE ACTION ITEM #1.SDR DALA2026082404804Vane · crackedCRACK WAS FOUND ON AFT MOVABLE VANE IN FWD INBD FITTING AT RT WING, R & R AFT RT MOVABLE FLAP VANE UNDER AMDS 2000-2638. (1765421) (AIRCRFT GROUNDED).SDR FDEA202608191161Skin · delaminatedDELAMINATION IN LEADING EDGE ON OUTBOARD FLAP AT 22" OF INBD END LEADING EDGE ON OTBD FLAP AT 22" OF INBD END WAS REPAIRED IAW SRM 57-53-01-2R, FIGURE 201, (SHEET 5) TABLE I, & SRM 51-70-17-0G PAR 4.A REV 94.SDR AALA202609230715Link · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING FLAP TRACK 2 INBOARD LINK - REPLACED LINK PER AMM 57-55-11SDR FDEA202608181143Skin · dentedLEFT WING INBD FLAP HAS TWO DENTS AT WS 177.50 ZONE 553. REPAIRED LT WING INBD FLAP PANEL IAW SRM 51-70-10-2R. MAJOR REPAIR.SDR DALA2026081804712Carriage · crackedLEFT WING FLAP TRACK 3 OTBD CARRIAGE-BRIDGE CRACKED. REPLACED IAW AMM 27-54-78. OK FOR SERVICE. (1762944) AIRCRAFT WAS GROUNDED.SDR SWAA2026090813201Rib · crackedCRACK FOUND ON RT OTBD AFT FLAP INBD RIB 4TH HOLE APPROX. .060". RT OTBD AFT FLAP WAS REPLACED WITH A SERVICEABLE FLAP ON CARD TTG8Q01BR3TM.,SDR SWAA2026082179206Fairing · pulledNR 3 FLAP SUPPORT FAIRING HAS 2 PULLED RIVETS. HOLES OVERSIZED, REQUIRES FAIRING REPLACEMENT. REMOVED THE NR 3 FLAP TRACK FAIRING IAW AMM 27-51-18, REF WO 128526169. INSTALLED A NEW FAIRING IAW AMM 27-51-18.SDR CALA2026082418857Skin · inflt separationLEFT AFT MAIN FLAP LOWER SKIN DISBONDED & DEPARTED AIRCRAFT. ON ARRIVAL, WALKAROUND FOUND LT INBD TRAILING EDGE MAIN FLAP LOWER AFT SKIN DISBONDED & DEPARTED ACFT. DAMAGED TO ALUMINUM HONEYCOMB STRUCTURE. PERFORMED T/E FLAP SYS DEACTIVATION AND ELOTO IAW AMSDR DALA2026081704696Vane · debondedDISBOND WAS FOUND OF 6.500IN X 3.500IN (LENGTH / WIDTH) ON RT FWD MOVABLE FLAP VANE AT 20IN OF IB AND 5IN TE, RT FWD MOVABLE FLAP VANE WAS REPAIRED IAW SRM 51-70-02-0G AND SRM 57-53-01-2R-1. (1760027) (AIRCRAFT GROUNDED).SDR DALA2026081704681Fairing · damagedELONGATED HOLE (1EA) WAS FOUND AFFECTING THE AFT FIXED FAIRING PANEL 533BB AT LEVEL OF FLAP TRACK FAIRING #4 ON LH WING, COMPLIED WITH ER/A 635816-14. (1760182) (AIRCRAFT GROUNDED).SDR AALA202609058224Link · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FLAP TRACK POSITION 2 INBOARD LINK - MAINTENANCE REPLACED LINK PER AIRBUS DRAWING D57556566SDR VNAA202608200003Skin · damagedSEVERAL NICKS, EROSION AND WEAR ON LOWER SKIN OF LH INBOARD FLAP FLS 15.5 TO FLS 75.5 WAS REPAIRED PER CRJ900 SRM 57-52-01-201-005-A01SDR FDEA202608141124Skin · dentedDENT ON LOWER SKIN OF OUTBOARD FLAP AT 13" FROM INBD EDGE AND 43" FROM TRAILING EDGE LH WING WING LH ON OUTBOARD FLAP, LOWER SKIN AT 13" FROM INBD EDGE AND 43" FROM TRAILING EDGE WAS REPAIRED IAW B767 SRM 57-53-10-01-1A FIG. 101 SHEET 4 AND SRM 51-70-10-2RSDR FDEA202608141121Skin · dentedDENT ON INBD MAIN FLAP L.E., AT 8'' FROM OUTBD EDGE, RH WING. RH WING, ON INBD MAIN FLAP L.E. AT 8'' FROM OUT BD EDGE, WAS EVALUATED IAW SRM 57-53-01-1A AND REPAIRED IAW SRM 51-70-17-0G FIG.1 AND 2 PARAG 3C (2) REV, 94.SDR SWAA2026081711566Link · wornLEFT WING NR 2 FLAP SUPPORT FAIRING HAD PLAY. R & R LT FLAP FAIRING SUPPORT LINK AT NR 2 IAW AMM 27-51-28.SDR SWAA2026090131028Fairing · crackedNR 6 TRAILING EDGE FLAP SUPPORT FAIRING CANOE HAS CRACK AT UPPER OUTBOARD CORNER SURFACE. REMOVED NR 6 TRAILING FLAP SUPPORT FAIRING IAW AMM 27-51-18 OBTAINED NEW CANOE FAIRING FROM STOCK AND INSTALLED TAIL CONE ASSEMBLY PER AMM 27-51-28SDR SWIA2026081177258Vane · chafedLEFT INBD FLAP VANE, INBD LEADING EDGE CAP REQUIRES REPLACEMENT DUE TO CHAFE DAMAGE OUT OF LIMITS. REPLACED THE CHAFED FLAP VANE IAW SRM 51-42-13, & DWG 601R14302, REV E. COMPLIED WITH SKY CARD 51-900-1003 SKY. MAJOR REPAIRSDR SWIA2026081177257Vane · chafedLEFT INBD FLAP VANE, OTBD LEADING EDGE CAP REQUIRES REPLACEMENT DUE TO CHAFE DAMAGE OUT OF LIMITS. REPLACED THE CHAFED FLAP VANE IAW SRM 51-42-13, & DWG 601R14302, REV E. COMPLIED WITH SKY CARD 51-900-1003 SKY. MAJOR REPAIR.SDR SWAA2026082446338Skin · delaminatedFOUND LEFT OTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED LT OTBD AFT FLAP IAW AMM 27-51-22-401.SDR SWAA2026082456139Skin · delaminatedFOUND RT OTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OTBD AFT FLAP IAW AMM 27-51-22.SDR FDEA202608111112Rivet · looseRIGHT WING INBD FLAP UPPER SKIN, FOUND SEVERAL RIVETS LOOSE AT XIFH 276.36. RT WING INBOARD FLAP UPPER SKIN LOOSE RIVETS AT XIFH 276.36 CARRIED OUT REPAIR AS PER EA 1-5750-T0308240 B P2. REPAIR CLASSIFIED AS MAJOR, IAW GMM 6-2-100.
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