JASC 5753
Service difficulty reports · 31,493
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 HNAA2026012200061Cap · corrodedRIGHT INBD FLAP INBD END CAP CORRODED AROUND NUT PATES HOLES. R & R RT INBD FLAP INBD END CAP IAW SRM 51-40-02.SDR DALA2026012700605Hinge Fitting · corrodedCORROSION ON HARWARE AND AROUND OF BORE IN OTBD HINGE. LT WING FLAP. THE OTBD FLAP HINGE WAS REPLACED IAW AMM 57-55-25. (1340373)SDR AALA202512314664Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING, INBOARD FLAP OUTBOARD TRAILING EDGE SKIN DELAMINATED. REPLACED LOWER SKIN PER CMM 57-53-05.SDR VNAA20260203015Hinge Fitting · corrodedCORROSION ON FWD, CTR & AFT HINGES OF FLAP STEP PLATE OF AFT BAGGAGE BAY. FWD, CTR & AFT HINGES OF FLAP STEP PLATE OF AFT BAGGAGE BAY WERE REPLACED PER SRM 51-42-06-001-001-A01SDR SWAA2026011943437Bracket · crackedRIGHT WING T/E ORSS 280 L-ANGLE COMMON TO DEFLECTION CONTROL RIB AND T/E UPPER SURFACE PANEL IS CRACKED. REMOVED AND INSTALLED NEW L ANGLE IAW SRM 51-40-02-0G 2.SDR SWAA2025122343214Support Angle · crackedCRACK ON SUPPORT ANGLE OF ACCESS PANEL 651FB RT WING T/E. REPLACED THE SUPPORT ANGLE LOCATED AT ACCESS PANEL 651FB IAW SRM 51-10-02, ITEM 9, AND DWG 115A2710, SHEET 6, REV B. MEASURE OF CRACK IS: 0.112 INCH.SDR AALA202601143901Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OTBD T/E AFT FLAP LOWER SURFACE HAS A PREVIOUS REPAIR LOCATED AT THE CENTER OF THE FLAP THAT IS DELAMINATED. REPAIRED FLAP IAW SRM 57-53-00-300-093.SDR SWAA2025123042648Seal · crackedLEFT WING OTBD AFT FLAP PLASTIC SEAL 2ND FROM O/B END CRACKED. R & R OTBD AFT FLAP IAW AMM 27-51-22.SDR SWAA2025123042649Seal · crackedRIGHT WING OTBD AFT FLAP PLASTIC SEAL 2ND FROM INBD END CRACKED. REMOVED AND REPLACED WITH SERVICEABLE RT WING OTBD AFT FLAP IAW AMM. 27-51-22.SDR SWAA2025122342977Angle · crackedCRACK ON ANGLE LOCATED AT LEVEL ORSS 272 DEFLECTION CONTROL RIB AREA RT WING T/E. REPLACED THE ANGLE IAW SRM 51-40-02, AND SRM 51-10-02, ITEM 9.SDR SWI2025F01868Flap Track · wornRIGHT WING FLAP TRACK 1A HAS THICKNESS REDUCTION WEAR OF .87MM MAX ALONG FWD SIDE. REMOVED AND REPLACED RT WING FLAP TRACK 1A IAW AMM 57-54-25.SDR SWIA2025122300004Flap Track · wornLEFT WING FLAP TRACK 1A HAS THICKNESS REDUCTION WEAR OF .25MM MAX ALONG FWD SIDE. REMOVED AND REPLACED LH WING FLAP TRACK 1A REF AMM 57-54-25.SDR VNAA202512020008Hinge Arm · gougedLEFT INBD FLAP OTBD HINGE ARM IS GOUGED AT FLAP MOUNTING BOLT.SDR SWIA2025120375762Skin · chafedLEFT INBD FLAP VANE CHAFED ON MID WEAR CAP OF LEADING EDGE AT APPROX. WS. 104. INSTALLED NEW LT INBD FLAP - SKIN, L/E MID REF. SRM 51-42-13 & NEW CAP AT INBOARD FLAP VANE WS105.67 PER SERVICE BULLETIN 601R-57-022 REV. B. COMPLIED WITH SKYWEST TASK CARD 51SDR SWAA2025120442178Wedge · delaminatedRIGHT MAIN FLAP TE WEDGE DELAMINATED. REMOVED DAMAGED T/E WEDGE, LOCATED AND DRILLED NEW WEDGE IAW SRM 51-40-06. INSTALLED NUTPLATES AS REQUIRED IAW SRM 51-40-02; APPLIED TOP COAT PER AMM 51-21-99.SDR SWAA2025120442179Skin · delaminatedT/E MAIN FLAP, LT INBD FOUND DELAMINATED. REMOVED THE LT INBD FLAP WEDGE IAW SOPM 20-50-01. LOCATED AND DRILLED ALL FASTENER HOLES EXCEPT HOLES COMMON TO OTBD SEAL IAW SRM 51-40-05, AND SRM 51-40-08. APPLIED DECORATIVE FINISH TO LT INBD FLAP WEDGE IAW AMM SDR DALA2025120408863Roller · wornRIGHT WING OTBD FLAP OTBD UPLOCK ROLLER FOUND WORN. REMOVED AND REPLACED RH WING O/B FLAP O/B UPLOCK ROLLER IAW AMM 27-54-73. (1333153)SDR DALA2025120408854Strut · wornWEAR INTERCONNECTING STRUT INBD FLAP ON RT WING (1EA). REPLACED INTERCONNECTING STRUT INBD FLAP ON RT WING (1 EA) AS PER FAM AMM 27-51-44-000-001-A. (1333800).SDR SWIA20251224102Flap Track · wornLH #1 FLAP TRACK 1A HAS A THICKNESS REDUCTION OF .037 CALIPER S/N:1279 CAL DUE 9/17/26 (C-CHECK RO 12/23/2025)REMOVED AND REPLACED THE LH FLAP TRACK 1A. REF AMM 57-54-25. TQ TC1-601 CAL 7-17-26.SDR DALA2025120308817Bearing · damagedFOUND RT WING OTBD FLAP INBD FLAP TRACK NR 3 ECCENTRIC WITH BEARING DAMAGED. COMPLIED WITH ER/A 630238-14. (1332112).SDR DALA2025120308816Bearing · damagedLEFT WING OTBD FLAP INBD SECTION TRACK NUMBER 3 ECCENTRICAL BEARING DAMAGED. CORRECTIVE ACTION: COMPLIED WITH ER/A 630235-14. (1332071).SDR CALA2025120811841Skin · delaminatedRIGHT WING, OTBD FLAP, AFT FLAP, INBD END, LOWER SKIN DEBONDED, L=2 X W 1.5 INCHES. CLEANED, PREPPED, PERFORMED PERMANENT REPAIR, & RESTORED FINISH ON RT WING OTBD AFT FLAP LWR SKIN IAW SRM 57-53-01-2R-16, SRM 51-70-10-2R-0, AND AMM 51-21-99-300-801.SDR CALA2025120811839Skin · delaminatedRIGHT WING, OTBD FLAP, AFT FLAP, INBD END, UPPER SKIN WITH DISBONDED AREA, L=1 X W=1 INCHES. CLEANED, PREPPED, PERFORMED PERMANENT REPAIR AND RESTORED FINISH ON RT WING OTBD AFT FLAP UPPER SKIN IAW SRM 5 7-53-01-2R-16, SRM 51-70-10-2R-0, AND AMM 51-21-99-300-SDR SWAA2026011341133Skin · debondedDEBONDED EXTERNAL SKIN ON LT WING OTBD AFT FLAP. REPLACED LT WING OTBD AFT FLAP IAW AMM 27-51-22. REMOVAL AND INSTALATION SEE TTG8Q0197FMU.SDR SWAA2026011341134Skin · debondedDEBONDED EXTERNAL SKIN ON OTBD AFT FLAP, LOCATED INBD END AT RT WING. REPLACED THE RT WING OTBD AFT FLAP IAW AMM 27-51-22. FOR REMOVAL AND INSTALLATION SEE TTG8Q0197FS0.SDR SWIA2026011209Vane · gougedLEFT INBD FLAP, FLAP VANE LEADING EDGE SKIN PANEL IS GOUGED. REPLACED LT INBD FLAP VANE MID LE IAW CRJ 200 SRM 51-42-13. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NOW WEIGHT CHANGE NOTEDSDR SWAA2025123140466Wedge · delaminatedLEFT WING MAIN FLAP, OTBD AFT WEDGE HAS A LARGE AREA OF DELAMINATION. REMOVED DELAMINATED FLAP WEDGE PER SRM 51-40-02. LOCATED AND MATCH DRILLED REPLACEMENT WEDGE IAW SRM 51-40-02. INSTALLED NUT PLATES IAW SRM 51-40-02.SDR DALA2025120108767Flap Track · corrodedCORROSION LH WING OUTBD FLAP TRACK #3 IINER AND OUTER RIB 5, AT ECCENTRIC BEARING AREA. CORRECTIVE ACTION: REPAIRED PER ERA 630235-14. (1325811)SDR AALA202512155321Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT WING TRAILING EDGE AFT FLAP INBOARD BOTTOM SURFACE DELAMINATED. REPAIRED FLAP PER SRM 57-52-00-300-113.SDR CALA2025112711522Skin · debondedRIGHT WING, OTBD FLAP, AFT FLAP, INBD END, UPPER SKIN DEBONDED SIGNAL NOTED, AREA L=1X1.25 INCHES. CLEANED, PREPPED, REPAIRED & RESTORED PAINT AT RT WING, OTBD FLAP, AFT FLAP, INBD END, UPPER SKIN IAW SRM 57-5 3-01-2R-16, SRM 51-70-10-2R-0, AMM 51-21-41-370SDR DALA2025112708673Flap Track · corrodedRIGHT WING OTBD FLAP TRACK NR 3, OUTER RIB 5, AT ECCENTRIC BEARING AREA, CORRODED. REPAIRED IAW ER/A 630238-14. (1323092)SDR SWAA2025120339614Skin · damagedFOUND RT WING TRAILING EDGE OTBD MAIN FLAP LOWER TRAILING EDGE COVE SKIN CREASED OVER FASTENER. IAW SRM 57-53-01-0I-3, TABLE 2, ITEM 5 FOR CLARIFICATION. RT WING TRAILING EDGE OTBD MAIN FLAP LOWER TRAILING EDGE COVE SKIN DAMAGE FOUND TO BE OUT OF LIMITS IAW SSDR SWAA2025120139571Tail Cone · damagedNUMBER 3 FLAP TRACK TAIL ONE HAS FOUR PULLED FASTENERS AND ONE MISSING FASTENER. R & R NR 3 TAIL CONE IAW AMM 27-51-18.SDR SWIA2025112476592Vane · wornRIGHT INBD FLAP VANE ACTUATOR BEAM WORN AT FLAP STATION 140.4. REPAIRED RIGHT INBD FLAP VANE ACTUATOR BEAM (OUTER TUBE) AT FLAP IAW REO 670-57-52-257, REV -B. COMPLIED WITH ALL STEPS OF REO 670-57-52-257 REV -B. OPS CHECK GOOD. COMPLIED WITH TASK CARD 51-9SDR SWIA2025112476468Tube · wornRIGHT INBD FLAP VANE ACTUATOR BEAM (OUTER TUBE) HAS WEAR DAMAGE AT FLAP STATION 65.5. REPAIRED RIGHT HAND INBOARD FLAP VANE ACTUATOR BEAM (OUTER TUBE) AT FLAP STATION 65.5 IAW REO 670-57-52-257 REV -B. COMPLIED WITH ALL STEPS OF REO 670-57-52-257 REV -B, COSDR SWAA2025112639059Skin · delaminatedRIGHT HAND MAIN FLAP TRAILING EDGE DELAMINATED. C/W TEMPORARY REPAIR PER SRM 57-53-01-1A-1. REFER TO TSR 2025009642. AFTER REVIEW; ENGINEERING CONCURS WITH SRM DEFERRAL FOR FAULT TTG8Q0190VFG.SDR SWAA2025112539058Wedge · delaminatedLEFT HAND INBOARD MAIN FLAP WEDGE DELAMINATED, COMPLIED WITH EA-25-127-03229.SDR SWI2025F01830Flap Track · wornRIGHT WING INBD FLAP TRACK NR 6 HAS THICKNESS REDUCTION OF .024". REMOVED AND REPLACED THE RT WING INBD FLAP TRACK NR 6 IAW AMM 27-51-08HG2-695.SDR SWIA2025121700121Flap Track · wornR/H WING I/B FLAP TRACK #5 HAS THICKNESS REDUCTION OF .020". REMOVED AND REPLACED THE RT WING INBD FLAP TRACK NR 5 IAW AMM 27-51-08HG2-695.SDR AALA202511249876Flap Track · lack of lubeAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: FLAP INDICATOR SHOWED FLAPS UP WITH A SLIGHT SPLIT BETWEEN THE TWO NEEDLES AND THE FLAP HANDLE AT 15 DEGREES EXTENSION, FLAPS WERE EXTENDED TO 15 DEGREES VIA THE ALTERNATE FLAP SWITCH. AIRCRAFT EMERGENCYSDR AALA202512037600Bushing · wornAIRCRAFT IN BASE MAINTENANCE: LEFT HAND WING NUMBER 3 FLAP TRACK TRANSMISSION ATTACH FITTING BUSHINGS ARE WORN. REMOVAL AND INSTALLATION OF FLIGHT CONTROL HARDWARE WAS ACCOMPLISHED. PERV NON-ROUTINE S/N 506.SDR SWAA2025112036063Support · delaminatedRIGHT WING OTBD FLAP NR 7 FWD SUPPORT FAIRING HAS MULTIPLE FASTENER HOLES FIBER GLASS DELAMINATED. REPLACED RT WING OTBD FLAP NR 7 FWD SUPPORT FAIRING IAW MM 27-51-28.SDR SWAA2025121835677Skin · delaminatedDELAMINATION ON UPPER & LOWER SKIN INBD EDGE OF LT WING OTBD AFT FLAP. REPAIRED UPPER AND LOWER SKIN INBD EDGE OF LT WING OTBD AFT FLAP IAW EA 25-157-03324.SDR SWI2025F01716Flap Track · wornRIGHT WING FLAP TRACK 2A OTBD HAS WIDTH REDUCTION WEAR OF 1.16MM MAX ALONG ENTIRE LENGTH. REMOVED AND REPLACED RT WING FLAP TRACK 2A OTBD IAW AMM 57-54-25.SDR SWI2025F01715Flap Track · wornLEFT WING FLAP TRACK 1A HAS THICKNESS REDUCTION WEAR OF .98MM MAX ALONG FWD SIDE. REMOVED AND REPLACED THE LT WING FLAP TRACK 1A IAW AMM 57-54-25.SDR AALA202511195255Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT WING OUTBOARD AFT FLAP INBOARD END IS DELAMINATED UPPER EXTERNAL SURFACE. EVALUATED LEFT HAND OUTBOARD AFT FLAP INBOARD END UPPER AND LOWER SKIN AND FOUND DISBOND DAMAGE TO EXCEED SRM REPAIR LIMITS, PER B737-NG SRM 57-53-- 01SDR VNAA202601170011Skin · corrodedCORROSION ON INNER SKIN TRAILING EDGE OF LH WING BTW STA BL45 TO STA WS 38, AND CORROSION ON INTERCOSTAL (2EA) OF LH WING T. EDGE BTW STA BL45 TO STA WS 38. CORROSION ON INNER SKIN TRAILING EDGE OF LH WING BTW STA BL45 TO STA WS 38 WAS REPAIRED PER REO 690-57SDR SWAA2025121835361Access Panel · elongatedELONGATED HOLES ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10 .SDR SWIA2026030275395Hinge Arm · gougedLH WING OB FLAP HINGE ARM AT WS178.00 FWD AND AFT BOTH MOUNTS GOUGED (C-CHECK RO 02/28/2026)REPAIRED DAMAGE TO LH WING OTBD FLAP HINGE ARM AT WS.178.00 IAW BOMBARDIER REO 601R-57-53-002 REV-C DATE 03-04-2008, MHIRJ REO 670-57-53-434 REV-- DATE 2025-11-25, CRSDR DALA2025111408346Skin · dentedRIGHT WING INBD FLAP LOWER SURFACE SKIN PANEL WITH DENTS BETWEEN RIB 7 AND RIB 8. CORRECTIVE ACTION: FILLED DENTS AT R/H WING I/B FLAP LOWER SURFACE SKIN (ZONE 2) BETWEEN RIB 7 AND RIB 8 I.A.W A319 SRM TASK 57-52-00-300-091. (1302533).
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