JASC 5753
Service difficulty reports · 31,496
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 FDEA202507031103Skin · dentedDENT ON OUTBOARD LOWER SKIN, BETWEEN WS 720 AND 746 LH WING LH WING, OUTBOARD FLAP LOWER SKIN WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 201 SHEET 3 DETAIL II AND SRM 51-70-10-2R REPAIR 4 REV 92 15/2025SDR IXXA20250703003Fairing · chafedLT O/B FLAP FAIRING 573BB SEAL RETAINER AND SEAL ARE CHAFEDSDR IXXA20250703001Skin · chafedLEFT WING AFT FLAP L\E CHAFED BEYOND LIMITSSDR REXA2026072901298Skin · wornSEVERAL NICKS AND WEAR ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.00 LOWER SKIN OF RH INBOARD FLAP FLS 48.00 TO FLS 65.00 WING WAS BLENDED OUT PER CRJ 900 SRM 51-12-00-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 57-52-01-101-001-A01 AND LSDR SWIA202512090702Hinge Fitting · gougedLEFT OTBD FLAP, MID. HINGE AFT FLAP ATTACH FITTING, INBD LUG GOUGED. REMOVED DAMAGE FROM LT OTBD FLAP MID HINGE FLAP ATTACH FITTING IAW SRM 51-12-00-001-001-A01. PERFORMED HFEC OF LT OTBD FLAP ATTACH FITTING INBD LUG REWORKED AREA IAW PART 1 51-20-006-250-A01SDR IPXA2025072237941Skin · crackedMAJOR REPAIR, LH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 27. CIRCLED IN RED. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-94346-REQ1 AND VT-MAE EA 300-5750-27-A4023, REV. -. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVESDR IPXA2025071524693Shaft · corrodedCORROSION AT LH SIDE NO.4 FLAP SUPPORT MECHANISM 6-6 OUTER SHAFT, STEP 3. PERFORM OK TO INSTASLL CHECK SATISFIED & INSTALL NEW LH WING NO.4 FLAP SUPPORT MECHANISM 6-6 OUTER SHAFT & CONDITION CHECK NORMAL. (RII ITEM) CHECKED COMPLETED.SDR FDEA202507021099Wedge · delaminatedLH WING INB MAIN FLAP OUTB T/E WEDGE CUT OUT DELAMINATED PERFORMED TAP TEST ON LH WING I/B MAIN FLAP DELAMINATION FOUND DIM = WIDTH .7" LONG 1.3" OUT OF LIMITS IAW B757 SRM 57-53-01-1A DETAIL I, FIG 101, SHEET 5, NOTE "L" AND IAW B757 SRM 51-10-06-2R, APPSDR IXXA20250702003Retainer · chafedRT I/B FLAP FAIRING 671DB I/B SEAL RETAINER AND SEAL ARE CHAFEDSDR SWI2025F01473Rod · dentedRH INBOARD FLAP, INBOARD VANE ACTUATOR ROD HAS INDENT. (C-CHECK RO 11/01/2025)REMOVED DAMAGE ON RH IB FLAP -IB VANE ACTUATOR ROD TO SMOOTH CONTOUR PER REO 670-57-52-257 REV B DATED 2024-10-17 AND DWG CC670-14303 REV B. ALL STEPS OF REO COMPLIED WITH. ALL CHSDR SWI2025F01472Rod · dentedRH INBOARD FLAP, SECOND TO INBOARD VANE ACTUATOR ROD HAS INDENT. (C-CHECK RO 11/01/2025)REMOVED DAMAGE FROM RH INBOARD FLAP, SECOND TO INBOARD VANE ACTUATOR ROD, REF, CRJ-900, SRM 51-12-00-001-001-A01, AND PERFORMED REPAIRS PER REO 670-57-52-257 REV -B DATED SDR SWI2025F01499Rod · dentedRH INBOARD FLAP, OUTBOARD VANE ACTUATOR ROD HAS INDENT. (C-CHECK RO 11/01/2025) REMOVED INDENT ON RH INBOARD FLAP, OUTBOARD VANE ACTUATOR ROD IAW CRJ900 SRM 51-12-00-001-001-A01 AND PERFORMED REPAIR PER REO 670-57-52-257 REV B DATED 2024-10-17. ALL CHECKS GOSDR SWAA2025073086808Support Bracket · crackedCRACK SUPPORT BRACKET LOCATED ON TRAILING EDGE ORSS 273 LT WING/ REPLACED SUPPORT BRACKET LOCATED ON TRAILING EDGE ORSS 273 LT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2930, SHEET 7, REV-.SDR SWAA2025071786982Skin · delaminatedLH OTBD. AFT FLAP IS DELAMINATED LOWER INBD. CORNER. REMOVED L/H OUTBOARD AFT FLAP IAW AMM 27-51-22-000-801. REMOVED AND INSTALLED SERVICEABLE REPLACEMENT LT OUTBOARD AFT FLAP IAW AMM 27-51-22-400-801. L/H OTBD AFT FLAP ADJUSTMENT CHECK GOOD IAW AMM 27-51-2SDR 2DYA202506300151Spar · corrodedCORROSION DAMAGE HAS BEEN FOUND ON THE REAR SPAR LOWER CHORD OF THE INBOARD TRAILING EDGE FLAP ON THE RH WING. THE DAMAGE HAS BEEN CUT OUT TO REMOVE THE DAMAGED SECTION OF THE 2024-T3511 EXTRUDED TEE AND REPLACED WITH AN EQUIVALENT 2024-T3 EXTRUSION. THE REPAISDR VNAA20250629010Vane · chafedFLAP VANE ACTUATOR SHAFT IS CHAFED UNDER PANEL 684CB. COMPLIED WITH MHIRJ GREO 670-57-52-257 REV-A DATED 2024-08-20SDR SWI2025F01503Skin · damagedS/N 0153LH OUTBD FLAP, BACKSIDE/TOP HAS SMOKING RIVETS. CIRCLED WITH GREASE PENCIL. (C-CHECK RO 11/01/2025)REPLACED SMOKING RIVETS ON LH OUTBD FLAP, BACKSIDE/TOP IAW REO#690-57-53-183, REV --, DATE: 2025-07-30. COMPLIED WITH TASK CARD 51-900-1002-SKY AND M-33SDR UIEA2025062500802Skin · debondedSKIN, LOWER SURFACE OF L/H WING INBD AFT FLAP INBD SIDE. PERFORM PERMANENT REPAIR - UPGRADE THE EXISTING REPAIR ON LOWER PANEL OF LT WING INBD AFT FLAP IAW EGAT EI NR: T2025A57M-1065 REV 1. CONDITION CHECK IS SATISFACTORY.SDR SWAA2025072993051Flap Track · wornRIGHT WING I/B AFT FLAP O/B TRACK WORN ON LOWER FLANGE. REMOVED AND RE-INSTALLED RIGHT WING I/B AFT FLAP TO REPLACE WORN O/B TRACK IAW AMM 27-51-12-000-801; AMM 27-51-16-400-801 AND AMM 27-51-12-400-801.SDR COEA2025103003919Deflector · puncturedWO 264878 NR 500052 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: L/H OUTBOARD FLAP DEFLECTOR LEADING EDGE HAS PUNCTURE JUST INBOARD OF THE OUTBOARD MOST CAM GUIDE. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00266312_01...26012 ISSUE A, DATED 9/5/2025.SDR SWAA2025071585370Angle · crackedCRACK ON ANGLE LOCATED ACCESS PANEL 651FB TRAILING EDGE AT RT WING 2025-390049 <[01]. REPLACED ANGLE LOCATED ON ACCESS PANEL 651FB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2710; SHEET 6 REV: B. LENGTH OF CRACK IS: 0.371? TOOL USED CALIPERSDR SWAA2025071585570Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING 2025-390051<[01]. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING IAW SRM B737-700 51-10-02; SRM B737-700 51-40-02 AND DRAWING # 115A 2001; SHEET 29; REV.-. MEASURE OF CRACK ISSDR DALA2025062604804Rib · gougedSHIP 3135 GOUGE OB FLAP ON INBOARD RIB LOWER AREA AT INTERCONNECTING STRUT ARE ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 626573-14. (1045570).SDR FDEA202506251047Skin · corrodedDOT 86-84 RH WING IB MAIN FLAP, CORROSION ON UPPER SURFACE EDGE, AT OB JUNCTION OF AFT FLAP. REMOVED, REPAIRED AND REINSTALLED RH WING MAIN FLAP UPPER SURFACE EDGE (WEDGE) AT O/B JUNCTION AT AFT FLAP IAW SRM 51-40-02, SRM 51-70-10-2R REPAIR 4 & SRM 57-53-0SDR COEA2025103007919Panel · chafedWO 264878 NR 500013 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: L/H OUTBOARD FLAP, OUTBOARD DEFLECTOR LEADING EDGE REPAIR DOUBLER AT THE THIRD FROM OUTBOARD CAM GUIDE IS CHAFED. CORRECTIVE ACTION: REPAIRED PER ATR42 SRM 575320-200-801-A01.SDR SWIA2025081401082Skin · nickedR/H I/B FLAP LOWER SKIN HAS A NICK BETWEEN W.S. 56.30 TO W.S. 75.27. (C-CHECK RO 08/13/2025)REPAIRED RH IB FLAP LOWER SKIN BETWEEN WS 53.60 TO WS 75.27 IAW MHIRJ REO 601R-57-52-2523 REV-- DATED 2025-07-07 COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPSDR SWIA2025081400624Hinge Arm · damagedR/H OUTBOARD FLAP, INBOARD HINGE ARM HAS EXCESSIVE PLAY AT ARM-TO-FITTING MOUNT BOLTS. FURTHER INVESTIGATION REQUIRED TO DETERMINE IF BUSHING/BORE DAMAGE IS PRESENT ON ARM OR FITTINGS. (C-CHECK RO 08/13/2025)REPAIRED RH OUTB FLAP INBD HINGE ARM AT ARM TO FITTSDR SWAA2025071585137Support Angle · crackedCRACK ON SUPPORT ANGLE OF ACCESS PANEL 651GB LOCATED TRAILING EDGE AT RT WING 2025-390033 <[01]. REPLACED SUPPORT ANGLE OF ACCESS PANEL 651GB LOCATED TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9 AND DWG 115A2714 SHEET 6 REV-. MESDR SWAA2025071585133Panel · elongatedELONGATED HOLE FITTING ON ACCESS PANEL 551GB TRAILING EDGE AT LT WING 2025-390023 <[01]. REPLACED BRACKET ON ACCES PANEL 551GB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-10-02-0G; 51-40-02-0G AND DWG: 115A2714; SHEET: 6; REV: -; [02] COMPLETED JOB.SDR DALA2025062504746Guide Vane · wornWEAR ON GUIDE VANE BEHIND HINGUE FLAP 1 AT RH WING. CORRECTIVE ACTION: GUIDE VANE WAS REPAIRED PER B717-200 SRM 57-53-01.SDR AALA202506268867Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT WING, OUTBOARD AFT FLAP, STARTING AT INBOARD TRAILING EDGE,T HE LOWER SKIN SURFACE IS DELAMINATED. REPLACED LEFT WING OUTBOARD AFT TRAILING EDGE FLAP IAW AMM 27-50-00.SDR DALA2025062104660Skin · dentedDENT OUT OF LIMITS, AT LOWER SURFACE ON LH AFT MOVABLE FLAP VANE AT STA XF74 APROX (2 INCHES FROM T.E. AND 12 INCH FROM L.E.): W=WIDTH, Y =DEPTH (NO MORE 0.060 INCH), RATIO W/Y= MUST BE 10 OR MORE, DENT #17: W=2.0 INCH, Y=0.090 INCH AND W/Y= 22.22 PER B717-200SDR SWIA2026020475182Skin · scratchedPERFORMED TEMPORARY REPAIR TO SCRATCH DAMAGE ON RT OTBD FLAP VANE UPPER SKIN BETWEEN FLAP STN. 235.84 - FLAP STN. 254.96. COMPLETE PERMANENT REPAIR 650 HOURS FROM THE TIME OF INCORPERATION. , REPAIRD SCRATCH DAMAGE ON RT OTBD FLAP VANE UPPER SKIN BETWEEN FLAP SDR SWAA2025071583401Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED AFT POSITION AT LEVEL ORSS 270 AT RT WING 2025-389818 <[01]. REPLACED ANGLE TRAILING EDGE LOCATED AFT POSITION AT LEVEL ORSS 270 AT RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 8 REV-.TOOL USEDSDR SWAA2025071583404Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED AFT POSITION AT LEVEL ORSS 270 AT LT WING 2025-389821<[01]. REPLACED ANGLE ON TRAILING EDGE LOCATED AFT POSITION AT LEVEL ORSS 270 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2930 SHEET 7 REV:-. LENGTH OF CRACK IS: 1.056?SDR SWAA2025063083436Skin · delaminatedLT. OUTBD AFT FLAP UPPER SURFACE DELAMINATED ON INBD. END<[01] 01 - REMOVED AND REPLACED PER [AMM 27-51-22-400-801-NG (OUTBOARD AFT FLAP INSTALLATION - PERMANENT)];[02] VERIFIED REMOVED AND REPLACED PER [AMM 27-51-22-400-801-NG (OUTBOARD AFT FLAP INSTALLATION SDR DALA2025062004653Rib · gougedSHIP 3135 GOUGE OB FLAP ON INBOARD RIB LOWER AREA AT INTERCONNECTING. CORRECTIVE ACTION: COMPLIED WITH ER/A 626603-14. (1033780).SDR SWAA2025070182661Skin · delaminatedRIGHT WING O/B AFT FLAP HAS DELAMINATION ON I/B LOWER SIDE<[01] CHANGED STEP STATUS ON STEPS 2 & 3 TO [PARTIAL];[02] REMOVED; REPLACED AND ADJUSTED THE RT WING O/B AFT FLAPS IAW AMM 27-51-22-000-801; AMM 27-51-22-400-801; AMM 27-51-28-000-802; AMM 27-51-28-400SDR SWAA2025070182816Skin · delaminatedLT WING O/B AFT FLAP I/B AFT END IS DELAMINATED. CHANGED STEP STATUS ON STEPS 2 & 3 TO [PARTIAL] REMOVED; REPLACED AND ADJUSTED THE LT WING O/B AFT FLAP IAW AMM 27-51-22-000-801; AMM 27-51-22-400-801; AMM 27-51-28-000-802; AMM 27-51-28-400-802;[03] VERIFIEDSDR FDEA202506141122Skin · dentedRH WING OUTER FLAP D-NOSE SKIN GOT DENT BETWEEN RIB15~17 ,S-1.1~1.2 ACCOMPLISHED THE NOSE SKIN FLUSH REPAIR AT RH WING OUTER FLAP RIB15~17, S-1.1~1.2 I.A.W A300-600F SRM 57-50-00-201, PARA.4H, PAGE.231~236, FIG.208 & SRI:57-50-00-201, IIR:57-50- 00-2-002-00SDR SWAA2025061681339Fairing · damagedL/H WING #3 FLAP FAIRING OUTBOARD SIDE HAS FOUR FASTENERS PULLED THROUGH FOR SEAL ATTACHMENT. THE LARGEST HOLE DIMENSION IS .25 IN. REPLACED SEAL 10-60754-20 & PERFORMED INTERIM REPAIR FOR ALTERNATIVE #1 OF THE #3 FLAP TRACK CANOE FAIRING ON THE OUTBOARD TRAISDR IXXA202506260026Multiple · multiple failPOST FLT, INBOUND CREW REPORTED LE SLAT ASSY ILLUMINATED ON FLAP EXTENSION. FLIGHT CONTINUED UNAFFECTED. LANDED WITHOUT INCIDENT. FOLLOWING VISUAL INSPECTS, MX REPORTED DAMAGE TO NR 8 SLAT. NR 8 SLAT DAMAGED. SLAT ASSY, ROTARY ACT, & OTBD LE SLAT G/B ASSY RSDR SWAA2025061280700Attach Fitting · crackedLEFT WING TRAILING EDGE DEFLECTION CONTROL ATTACH FITTING UPPER TAB IS CRACKED APPROXIMATELY 2.5' IN THE RADIUS. PICTURE ATTACHED.<[01] DAMAGE VERIFIED PER NDT PARTY 6 51-00-00 PROCEDURE 23.;[02] DAMAGE VERIFIED PER NDT PART 6 51-00-00 PROCEDURE 23.SDR IXXA2025061202Flap Track · corrodedLEFT WING O/B FLAP I/B SUPPORT UPPER AND LOWER SURFACES CORRODED MAIN TRACKSDR SWAA2025071580588Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE AT LEVEL ORSS 297 AT LT WING 2025-366177 <[01]. REPLACED CORRUGATED PLATE TRAILING EDGE AT LEVEL ORSS 297 AT LT WING IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG: 115A3700 SHEET 38 REV -; [02] REPLACED CSDR AALA202507026803Support Fitting · wornAIRCRAFT IN BASE MAINTENANCE: NUMBER 3 TRANSMISSION ATTACH FITTING SUPPORT AND TRACK BUSHING ARE LOOSE AND WORN. INSTALL TRANSMISSION ATTACH FITTING SUPPORT TO TRANSMISSION, PER 27-51-31-400-801 STEP F SUBTASK 420-001(1)(A) THRU (E)1.SDR AALA202507024915Support Fitting · wornAIRCRAFT IN BASE MAINTENANCE: NUMBER 7 TRANSMISSION ATTACH FITTING SUPPORT AND TRACK BUSHING ARE LOOSE AND WORN. INSTALL TRANSMISSION ATTACH FITTING SUPPORT TO TRANSMISSION. PER AMM 27-51-41-400-802SDR AALA202507024439Fitting · wornAIRCRAFT IN BASE MAINTENANCE: NUMBER 6 TRANSMISSION ATTACH FITTING SUPPORT AND TRACK BUSHING ARE LOOSE AND WORN. INSTALL TRANSMISSION ATTACH FITTING SUPPORT TO TRACK. PER AMM 27-51-31-400-801.SDR UIEA2025060100708Skin · dentedLHW I/B MID FLAP FAIRING EXTERIOR SURFACE FOUND DENT.(<P>PERFORMED REPAIR AT DENT AREA AS PER SRM 51-70-07 PAR 5.A.(1) REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060100709Skin · delaminatedLHW I/B FORE FLAP EXTERIOR SURFACE FOUND DELAMINATED.(<P>PERFORMED REPAIR AT DELAMINATED AREA AS PER SRM 51-70-07 PAR 5.A.(1) REV 103. NO FURTHER DEFECTS NOTED.</P>)
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