JASC 5753
Service difficulty reports · 31,494
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 UIEA2025080501088Fairing · delaminatedLEFT WING OTBD MID FLAP L/E FAIRING FOUND DELAMINATED. PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.SDR AALA202508279529Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND WING INBOARD MAIN FLAP OUTBOARD WEDGE DELAMED. REMOVAL AND INSTALLED LEFT HAND INBOARD FLAP WEDGE. PER N/R 615.SDR SWIA2025080675194Rivet · looseRIGHT OTBD FLAP OUTER SKIN HAD SMOKING RIVETS. FOUND AT NUMEROUS LOCATIONS ALONG FLAP. REMOVED 10 SMOKING RIVETS AT RT OTBD FLAP OUTER SKIN AT NUMEROUS LOCATIONS ALONG FLAP IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-13-001-001-A01. INSTALLED 10 EACH FASTENESDR DALA2025080705914Support Fitting · corrodedRIGHT WING FLAP TRACK FAIRNG 633CB ROD SUPPORT FITTING WITH CORROSION. REPLACED SUPPORT FITTING IAW A319 SRM 51-72- 11-911-001.SDR VGCA20250805003Flap Track · crackedCRACK FOUND ON LEFT WING OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP TRACK. CRACK WAS IN UPPER FLANGE INBOARD FLANGE.SDR DALA2025081105960Structure · debondedRIGHT WING O/B FLAP INTERNAL STRUCTURE HONEYCOMB DISBONDING AT OTEF STA 190+5 UNDER FLAP PANEL 666MT IB AREA. RT WING O/B FLAP INTERNAL STRUCTURE HONEYCOMB REPAIRED AT OTEF STA 190+5 UNDER FLAP PANEL 666MT IB AREA IAW SRM 57- 53-01-2R-1, SRM51-70-10-2R-4, ANDSDR FDEA202508051370Skin · dentedDENT IN LOWER SURFACE AT OTEF STA 232.69 AND 9" OF LEADING EDGE ON LH OUTBOARD FLAP LEADING EDGE ON LH OUTBOARD FLAP WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 201 REP 1 SHEET 3 REV 92 APR 15.2025 AND SRM 51-70-10-2R REV 92 APR 15.2025SDR IXXA20250805002Skin · gougedLEFT WING INBD FWD FLAP UPPER SURFACE HAS BARE METAL AND A GOUGE IN THE PREVIOUS REPAIR.SDR SWAA2025081998165Plate · crackedLEFT WING T/E INBD WAFFLE PLATE FOR PANEL 551EB CRACKED. REMOVED & REPLACED LT WING T/E INBD WAFFLE PLATE FOR PANEL 551EB IAW SRM 51-40-05-0G-0 & DWG115A2001 & DWG 115A2713.SDR SWAA2025080697636Tail Cone · pulledNUMBER 3 FLAP FAIRING TAIL CONE HAS SIX PULLED RIVETS ON THE OUTBOARD SIDE. REMOVED AND REPLACED NR 3 FLAP TAIL CONE CANOE PER SRM 51-40-02. APPLIED SEALANT PER SRM 51-40-02.SDR SWIA202508050022Vane · dentedREF EAML 1670491 AND 1671344 FOR TIRE BURST DAMAGE, INSP LT INBD FLAP AND FOUND THREE DENTS MEASURING DENT #1: 5.50€? L X 4.25€? W X 0.031€? MAX. DEPTH, REF. (W/D RATIO = 136) DENT #2: 4.00€? L X 2.75€? W X 0.156€? MAX. DEPTH, REF. (W/D RATIO = 18) DENT SDR SWAA2025080597542Skin · delaminatedLEFT WING OB AFT FLAP LOWER FACE SHEET DELAMINATED AT IB TE 19.5' X 10'(PICS ATTACHED)<[01] R/R LEFT WING OUT BOARD AFT FLAP PER AMM 27-51-22SDR UIEA2025071000897Flap · damaged#7 V/C FLAP LSA DAMAGED.(<P>PERFORMED REPAIR AT LSA DAMAGE AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025071000898Flap · damaged#8 V/C FLAP LSA DAMAGED.(<P>PERFORMED REPAIR AT LSA DAMAGE AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025071000899Flap · damaged#19 V/C FLAP LSA DAMAGED.(<P>PERFORMED REPAIR AT LSA DAMAGE AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025071000900Flap · damaged#20 V/C FLAP LSA DAMAGED. PERFORMED REPAIR AT LSA DAMAGE AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.SDR UIEA2025073001064Skin · dentedAIRCRAFT DAMAGE LOG 8337 - DENT RH WE 724.5 L/E CAMBER FLAP #17 WITHIN LIMITS PER SRM 57-41-01A-01 DETAIL VIII. W: 24. D" Y: 0.120" W/Y 33(<P>AIRCRAFT DAMAGE LOG 8337 - DENT RH WE 724.5 L/E NOSE SKIN REPAIRED I.A.W RI-57-40-17783 REV.A DATE: 22 JUL 2025. NO FUSDR SWAA2025081197274Skin · debondedRIGHT WING INBD AFT FLAP OUTER SURFACE IS DISBONDED 4' FROM I/B SIDE AND 8' FROM T/E. INBOARD AFT FLAP INSTALLATION COMPLETE IAW AMM 27-51-12-400-801. REMOVED AND REPLACED R/W I/B AFT FLAP AND ADJUSTMENTS ACCOMPLISHED SATISFACTORY IAW AMM 27-51-12-000-801 AND SDR AALA202508063158Support Bracket · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND FLAP INTERCONNECT STRUT HAS EVIDENCE OF CORROSION AND GOUGING ON AFT SIDE OF INNER CYLINDER ALONG WITH WITH EXCESSIVE PLAY DUE TO THE ATTACHMENT / SUPPORT BRACKET BEING WORN FOR THE INTERCONNECTING STRUT. REPLACED INTESDR AALA202508065348Strut · corrodedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND FLAP INTERCONNECT STRUT HAS EVIDENCE OF CORROSION AND GOUGING ON AFT SIDE OF INNER CYLINDER ALONG WITH WITH EXCESSIVE PLAY DUE TO THE ATTACHMENT / SUPPORT BRACKET BEING WORN FOR THE INTERCONNECTING STRUT. REPLACED INTESDR FDEA202507301551Flap · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON LH INBD FLAP LWR SKIN BTW RIB12A~14A, T/E-21" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF DOUBLER REPAIR WITHOUT REPAIR RECORD AND DETERMINED IT NOT CONFORMITY ANY FAASDR HALA20250731042Vane · dentedDENT ON LH WING FLAP FIXED VANE INBOARD DENETIONS 5" X 1 ". REPLACED LT WING INBRD FLAP FIXED VANE PER AMM 27-50-02 OPS CHECK GOOD.SDR UIEA2025072501022Skin · damagedRH INBD FLAP T/E FORE FLAP MIDSECTION UPPER SURFACE HAS A SMALL HOLE 0.250 DIAMETER. ACCOMPLISHED REINFORCING REPAIR ON RH INBD FLAP T/E FORE FLAP UPPER SURFACE PER SRM 51-70-03-0G-0. NO FURTHER DEFECTS NOTED.SDR UIEA2025072501024Skin · damagedRH INBD FLAP T/E FORE FLAP HAS DAMAGE NEAR THE INBD TOGGLE HOOK L/E LOWER SKIN. ACCOMPLISHED REINFORCING REPAIR ON RH INBD FLAP T/E FORE FLAP PER SRM 51-70-07-0G-0 PARG 5A, 4C, 4E & 4G. NO FURTHER DEFECTS NOTED.SDR CALA2025080107203Wedge · delaminatedRIGHT INBD MAIN FLAP OTBD AFT WEDGE WITH EVIDENCE OF DISBONDED. REMOVED AND REPLACED RT INBD MAIN FLAP T/E WEDGE IAW SRM 51-40-02-0G-0, AND DWG 113A2100.SDR CALA2025080107202Wedge · corrodedLEFT INBD FLAP OTBD AFT WEDGE WITH EVIDENCE OF A DISBONDED AREA AT TE. REMOVED AND REPLACED LT INBD MAIN FLAP T/E WEDGE IAW SRM 51-40-02-0G-0, AND DWG 113A2100.SDR AALA202509293730Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: DEBONDED IB FLAP EXISTING REPAIR ON LH WING MEASURE OF DISBOND IS L=18.0IN W=12.0IN. MAINTENANCE PERFORMED PERMANENT REPAIR ON IB FLAP TRAILING EDGE LH WING IAW EA NO. 367092.SDR IPXA2025082538528Skin · damagedWHILE PERFORMING WALK AROUND PER PS1 FOUND LT WING #2 FLAP UPPER SURFACE AFT OF L/E PREVIOUS REPAIR HAS PEELED OFF . C/W ALL STEPS OF EO-94534-REQ3. THIS REPAIR IS CONSIDERED PERMANENT. MAJOR REPAIR.SDR IPXA2025072938528Repair · peelingMAJOR REPAIR, WHILE PERFORMIN WALK AROUND PER PS1 FOUND L/H WING #2 FLAP UPPER SURFACE AFT OF L/E PREVIOUS REPAIR HAS PEELED OFF . DEFERRED IAW EO-94534-REQ1.SDR SWAA2025082195339Wedge · delaminatedRIGHT WING INBD MAIN FLAP; OTBD TRAILING EDGE WEDGE HAS LARGE AREA OF DELAMINATION. REMOVED DAMAGED WEDGE. LOCATED & DRILLED NEW WEDGE IAW SRM 51-40-02.; COMPLIED WITH STEP 1. INSTALLED NEW NUT PLATES IAW SRM 51-40-02. PAINTED LOWER TE WEDGE SURFACE IAW AMSDR SWAA2025082795110Skin · debondedDEBONDED EXTERNAL SKIN IB MAIN FLAP TRAILING EDGE WED GE LOWER SURFACE AT LT WING. REPAIRED EXTERNAL SKIN IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT LT WING IAW AEM 25-157-02122.SDR SWAA2025082795111Skin · debondedDEBONDED EXTERNAL SKIN IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT RT WING. REPAIRED IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT RT WING IAW 25-157-02127-WIP1 (COMPONENT - AEM - REPAIR - RH WING - I/B MAIN FLAP - WEDGE ASSY - LOWER SKIN).SDR FDEA202507241312Skin · delaminatedDELAMINATION ON LEADING EDGE OF INBOARD MAIN FLAP AT 33" FROM OUTBOARD EDGE, RIGHT WING. LEADING EDGE OF INBOARD MAIN FLAP RT WING WAS REPAIRED IAW SRM 57-53-01-2R FIG 201 SHEET 5 TABLE I AND SRM 51-70-03-0G PAR 5 FIG 5 SHEET 1 REV 92 APR 15/2025SDR SWAA2025081994462Fitting · crackedA71-40 LEFT WING TRAILING EDGE CAVITY. FIXED TRAILING EDGE SUPPORT BRACKET 10' I/B OF DEFLECTION CONTROL RIB; HAS A CRACK AT BULB SEAL ATTACH BRACKET. REMOVED LT WING T/E SUPPORT BRACKET IAW SRM 51-40-02-0G-0. DRILLED FASTENERS HOLES IAW SRM 51-40-02-0G-0 ASDR FDEA202507231297Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE (#3HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATESDR FDEA202507231296Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATEDSDR SWIA202509250722Skin · damagedLEFT OUTBOARD FLAP UPPER SKIN HAS 3 SMOKING RIVETS NEAR THE FORWARD EDGE IN THE CENTER OF THE FLAP. MARKED (C-CHECK RO 09/24/2025)REMOVED (3EA) SMOKING RIVETS ON LEFT OUTBOARD FLAP UPPER SKIN NEAR THE FORWARD EDGE IN THE CENTER OF THE FLAP, REF CRJ 200 SRM 51SDR REXA2025080600789Skin · cracked"SECONDARY NRC IN REF. TO NRC 00013 : AFTER PAINT STRIPPING ON LOWER SKIN AT LH INBOARD FLAP, CRACK WAS FOUND ON LOWER SKIN BTW FS30.00 / FS36.00 FROM 0.750Ï¿½ TO TRAILING EDGE. LOWER SKIN AT LH INBOARD FLAP BTW FLS 30.00 / FLS 36.00 0.750"" ABOVE OF TRAILING SDR SWIA2025072175119Rivet · damagedRT OTBD FLAP HAS SMOKING RIVETS ON TOP SIDE OF FLAP SKIN FROM APPOX. WS.200.00 TO WS.210.00 (MARKED). (C-CHECK RO 02/01/2026)REMOVED AND REPLACED FASTENERS (7 EA) ON RH OB FLAP TOP SIDE SKIN FROM APPOX. WS.200.00 TO WS.210.00. IAW REO 690-57-53-186 REV -- DASDR SWAA2025082193758Skin · delaminatedRIGHT OUTBOARD AFT FLAP; INBOARD LOWER CORNER DELAMINATED. REMOVED RIGHT OUTBOARD AFT FLAP IAW AMM 27-51-22. REMOVED & INSTALLED SERVICEABLE REPLACEMENT RT OTBD AFT FLAP INSTALLATION IAW AMM 27-51-22-400-801.SDR REXA2025081800817Hinge Arm · crackedBROKEN BONDING SUPPORT WS 54.55 AT LH INBOARD FLAP HINGE ARM BONDING SUPPORT WS 54.55 AT LH INBOARD FLAP HINGE ARM WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01SDR DALA2025073105747Strut · corrodedCORROSION INTERCONNECTING STRUT I/B FLAP ON LH WING. REPLACED INTERCONNECTING STRUT I/B FLAP ON LH WING PER AMDS CARD 2750-6010-LT.SDR DALA2025073105746Strut · corrodedCORROSION INTERCONNECTING STRUT I/B FLAP ON RT WING. REPAIRED INTERCONNECTING STRUT I/B FLAP ON RH WING PER AMDS CARD 2750-6010-RT. (1097731)SDR DALA2025072205516Flap Track · corrodedSHIP 3155 CORROSION ON ECCENTRIC BEARING TRACK 3 OB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED ECCENTRIC BEARING TRACK 3 OB FLAP ON LH WING AS PER A320 FAM AMM 57-53-21-000-001-A AND AS PER A320 FAM AMM 57-53- 21-400-001-A.SDR FDEA202507211286Skin · dentedDENT WITH DIMENSION L=4.0" ,W=2.0" ,D=0.036" IN SURFACE OUTERSIDE OF MAIN FLAP OF INBOARD FLAP LEFT WING IN SURFACE OUTERSIDE OF MAIN FLAP OF INBOARD FLAP LEFT WING WAS REPAIRED IAW B767 SRM 57-53-01-2R TABLE 1 FIG 201 SHEET 5 AND SRM 51-70-03-0G PAR 5A SHSDR SWIA2025071975145Beam · groovedLEFT WING INBOARD FLAP INBOARD FLAP VANE ACTUATOR BEAM HAS A LATERAL GROOVE, FLS140.40. (MARKED & FLAGGED) (C-CHECK RO 02/01/2026)REMOVED DAMAGE FROM THE LEFT WING INBOARD FLAP INBOARD FLAP VANE ACTUATOR BEAM AT FLS140.40 IAW CRJ900 SRM 51-12-00-001-001-A01.SDR SWIA2025071975144Beam · groovedLEFT WING INBOARD FLAP INBOARD FLAP VANE ACTUATOR BEAM HAS A LATERAL GROOVE,FLS65.50. (MARKED & FLAGGED) (C-CHECK RO 02/01/2026)REMOVED DAMAGE FROM THE LEFT WING INBOARD FLAP INBOARD FLAP VANE ACTUATOR BEAM AT FLS65.50 IAW CRJ900 SRM 51-12-00-001-001-A01. COMSDR SWIA2025071975143Beam · groovedLEFT WING INBOARD FLAP INBOARD FLAP VANE ACTUATOR BEAM HAS A LATERAL GROOVE, FLS102.90. (MARKED & FLAGGED) (C-CHECK RO 02/01/2026)COMPLIED WITH REO 670-57-52-257 REV -B DATED 2024-10-17 REPARE OF LH WING IB FLAP IB FLAP VAIN ACTUATOR BEAM GROVE AT FLS 102.90SDR SWIA2025071975127Beam · groovedLEFT WING INBOARD FLAP INBOARD FLAP VANE ACTUATOR BEAM HAS A LATERAL GROOVE, FLS24.00. (MARKED & FLAGGED) (C-CHECK RO 02/01/2026)REMOVED DAMAGE FROM THE LEFT WING INBOARD FLAP INBOARD FLAP VANE ACTUATOR BEAM AT FLS24.00 AS PER CRJ900 SRM 51-12-00-001-001-A01.SDR SWAA2025082292708Skin · delaminatedRIGHT OUTBOARD TRAILING EDGE FLAP HAS DELAM ON INBD TRAILING CORNER AND SHARP BEVEL ON TRAILING EDGE AT FLAP CENTER.<[01] REMOVED R/H O/B AFT FLAP PER MM 27-51-22.;[02] OK TO INSTALL R/H OUTBOARD TRAILING EDGE FLAP (RII);[03] REPLACED R/H O/B AFT FLAP PER MM 2
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