JASC 5753
Service difficulty reports · 31,506
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 FDEA202411201699Skin · cracked2EA CRACKS (20MM) & (20MM) WERE FOUND AT R/H WING CENTER FLAP RIB11 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RIB11, S-2.7~REAR SPAR AND EXTERNAL PLATE AT RIB11~12,S-2.2~REAR SPAR FOR REPAIR I.A.W FESDR SWIA202504301119Vane · chafedRH WING, OTBD FLAP VANE MOUNT FITTINGS SHOW CHAFFING AND WEAR ALONG THE LOWER EDGE, AT WS 171, 189, 235, 280, 296, (5EA FITTINGS) (C-CHECK RO 04/30/2025) COMPLIED WITH REO 601R-57-53-195 DISPOSITION FOR WEAR DAMAGE ON O/B FLAPS BUJTE DOOR CAMS AND RIB FITTINGSDR CALA2024112002909Skin · dented9B757-57-06-3-0248) DOT 210-18 R/H WING I/B FLAP O/B SIDE HAS MA RK/DENT. REF NR 114209. REPAIRED FLAP LE SKIN IAW SRM 57-53-01-2R-2. VERIFIED INSPECTION PERFORMED RIISDR CALA2024112002908Skin · gouged(B757-57-06-3-0248) R/H WING MAIN FLAP I/B AT MFSTA 153.43 WITH GOUGE. REF NR 114426. REPAIRED FLAP LE SKIN IAW SRM 57-53-01-2R-2. VERIFIED INSPECTION PERFORMED RIISDR LR7A2024111903603Baffle · crackedDURING SCHEDULED C-5 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH OUTBOARD FLAP UPPER BAFFLE SKIN CRACKED AT OWFS0R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001190949.SDR LR7A2024111903602Skin · crackedDURING SCHEDULED C-5 CHECK UNDER JOB CARD HC 5712, FOUND RH OUTBOARD FLAP UPPER LEADING EDGE SKIN CRACKED AT OWFS303R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-11. NR# 1001188008. / PSE# 57-50-16, AD 2012-06-09SDR HNAA202412010144Hinge Fitting · cracked57-2441 RH OB FLAP SHROUD, IB HINGE AFT SECTION LUG CRACKED. RAR HINGE IAW SRM 51-40-02 AND AMM20-10-01SDR SWI2025F00175Vane · dentedDURING AUDIT OF 1C TASK CARD 57-680-302 (EXTERNAL ZONAL INSPECTION OF THE RIGHT-WING INBOARD FLAP, FLAP VANE, AND HINGE ARMS), FOUND DENT ON UNDERSIDE OF RH INBD FLAP APPROXIMATELY 18 INCHES FROM INBOARD SIDE EDGE AND 5 INCHES UP FROM THE TRAILING EDGE. PLOT, SDR IPXA2025011325354Skin · puncturedRH TRAILING EDGE FLAP HAS PUNCTURE 1.5X1.5€? AND .6€? DEEP. HANGAR REQUIRED FOR COMPOSITE REPAIR. L/M 3.0 HRS TO DROP AND LOCKOUT FLAPS. S/M 40.0 HOURS FOR REPAIR. REF. SRM 57-53-01-2R-2, TABLE 205 ZONE 5. 350 DEGREE COOK (51-70-05). BMS8-256,STYLE3K-70-PW SDR SWAA2024112060413Wedge · debondedLH WING IB MAIN FLAP HAS A METAL BOND REPAIR THAT HAS DISBONDED AND DEPARTED THE AIRCRAFT. LOCATED AT THE LOWER OB END TRAILING EDGE SKIN.<[01] REPAIRED PANEL WEDGE PER SRM 57-53-01-2R-7.SDR DALA2024111911045Strut · corrodedSHIP 3136 CORROSION INTERCONNECTING STRUT OB FLAP ON LH WING (1 EA). CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT OB FLAP ON LH WING, THE INSTALLATION IS TO BE ACCOMPLISHED ON AMDS CARD 2750-6010-LT AND 2750-6020-LT. (0663034)SDR DALA2024111911025Vane · dented-AD- DENTS ON RH WING FWD MOVABLE VANE INBD SURFACE. SUMMARY OF NRC 00326: DENTS (3 LOCATIONS) ON LOWER SKIN OF FWD MOVABLE VANE RH WING WERE EVALUATED AND FOUND OUT LIMITS. RH WING FWD MOVABLE VANE WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR SDR SWAA2024112059173Rib · crackedDEFLECTION CLIP FOR RIGHT WING UPPER SKIN FIXED TRAILING EDGE BROKEN<[01] REMOVED AND REPLACED DEFLECTION CLIP FOR RIGHT WING UPPER SKIN FIXED TRAILING EDGE PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]SDR SWAA2024111859818Flap · crackedDURING HFEC INSPECTION OF R/H WING TE; O/B AFT FLAP LEADING EDGE DENT PER EA 24-127-03162; FOUND CRACK INDICATION MEASURING 1' IN LENGTH. (SEE ATTACHED PICTURE)<[01] VERIFIED CRACK INDICATION USING FLUORESCENT PENETRANT INSPECTION IAW B737 AMM 70-40-01.;[02] RSDR DALA2024111510978Skin · delaminatedSHIP 1808 L/H WING I/B AFT FLAP UPPER SURFACE FOUND DELAMINATION 2IN TO LOWER EDGE AND 30IN TO O/B EDGE. CORRECTIVE ACTION: REPAIRED L/H WING I/B AFT FLAP UPPER SURFACE DELAMINATION AS PER B767-400 SRM 57-53-01-2R-1, SRM 51-70-10-2R-4 AND SRM 51-70-10 (0657525SDR IXXA20241113003Retainer · brokenLEFT IB TRAILING EDGE FLAP SEAL RETAINER FOUND CRACKED. 8110-3 USED TO REPAIR AFTER FABRICATION AND CHEMICAL CONVERSION COATING, SINCE CHROME ACID ANODIZE CANNOT BE ACCOMPLISED.SDR DALA2024111310926Skin · wornSHIP 1808 FOUND RH WING I/B FLAP AFT FLAP UPPER SURFACE WORN AT I /B AREA. CORRECTIVE ACTION: REPAIRED RH WING I/B FLAP AFT FLAP UPPER SURFACE WORN AT I/B AREA AS PER B767-400 SRM 57-53-01 (0657514)SDR FDEA202411121671Skin · dentedRH WING, DENT ON LOWER SKIN FLAP OUTBOARD, 23 TO LOWER EDGE AND 12 TO FAIRING. RH WING, LOWER SKIN FLAP OUTBOARD, 23 TO LOWER EDGE AND 12 TO FAIRING WAS REPAIRED IAW B767 SRM 51-70-10-2R REP 4 FIG 202 (SHEET 3) AND SRM 57-53-01-2R FIG 201 REP 1 (SHEESDR FDEA202411121670Skin · dentedRIGHT WING, INBOARD TRAILING EDGE FLAP (ZONE 655) WITH DENT. RIGHT WING, INBOARD TRAILING EDGE FLAP (ZONE 655) WAS REPAIRED IAW B767 SRM 57-53-01- 2R REP 1 FIG 201 (SHEET 4) AND SRM 51-70-10-2R REP 4 FIG 201 (SHEET 1) REV 90 AUG 15/2024SDR DALA2024111310922Bonding Plate · corrodedSHIP 3160 CORROSION BONDING PLATE FLAP TRACK FAIRING 3 (532CB) ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620610-14. (0657078)SDR DALA2024111310921Bonding Plate · corrodedSHIP 3160 CORROSION FLAP TRACK FAIRING 632CB BONDING PLATE ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620610-14. (0657071)SDR DALA2024111210888Vane · dentedDENT ON LWR SURFACE AT FWD MOVABLE FLAP VANE OF LEFT WING WAS FOUND OUT OF LIMITS DUE TO DISTANCE. SUMMARY OF NRC 00674: AREA BTW XF 85 TO XF 95 ON LWR SURFACE AT FWD MOVABLE FLAP VANE OF LEFT WING WAS REPAIRED PER B717-200 SRM 51-70-02-0G PROCEDURE GENERAL INSDR DALA2024111210873Fitting · corrodedSHIP 3160 CORROSION ON BORE I/B FITTING OF O/B FLAP LH. CORRECTIVE ACTION: COMPLIED WITH ER/A 620919-14. (0655751)SDR DALA2024111210886Vane · dentedDENTS: 2, 3, 4, 5, AND 6 BTW XF89 AND XF95 (10 TO 13.5 INCHES FROM T.E.) ON RH AFT MOVABLE FLAP VANE WERE FOUND OUT OF LIMITS BY DISTANCE BTWN OTHER DAMAGES. SUMMARY OF NRC 00628: DENTS: 2, 3, 4, 5, AND 6 BTW XF89 AND XF95 (10 TO 13.5 INCHES FROM T.E.) ON RH ASDR DALA2024111210879Flap Track · damagedSHIP 3126 DMG FOUND ON #3 RH FWD FIXED FLAP TRACK FAIRING. CORRECTIVE ACTION: COMPLIED WITH ER/A 622279-14. (6527417)SDR DALA2024111210877Flap Track · corrodedSHIP 3160 CORROSION BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620610-14. (0655121)SDR DALA2024111210876Flap Track · corrodedSHIP 3160 CORROSION FLAP TRACK FAIRING 631CB BONDING PLATE ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620610-14. (0655117)SDR AALA202411203711Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD FLAP DELAMINATED ON THE INBOARD TRAILING EDGE. REPLACED FLAP PER TASK CARD 26L00027009.SDR SWIA202503171109Skin · gougedR/H OTBD FLAP HAS GOUGE ON LWR SURFACE INBD OF CENTER FARING @ 41/2" FROM T/E (C-CHECK RO 3/14/2025) CUT OUT DAMAGE AND PERFORMED SKINS AND PLATINGS, METALLIC OUTBOARD FLAP REPAIR TYPE III. REF. CRJ700 SRM 57-53-01-201-001-A01 REPAIR TYPE III.COMPLIED WSDR SWAA2024120658117Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED TRAILING EDGE ORSS322 AT LT WING 2024-686314<[01] REPLACED SUPPORT ANGLE LOCATED TRAILING EDGE BTW ORSS279 TO ORSS330 AT LT WING IAW. B737-800 SRM 51-10-02-0G-0 ITEM 9 ; SRM 51-40-02-0G-0 AND DWG 115A3700 SHEET: 71 REV: -. MEASURSDR DALA2024111110803Vane · dentedDENTS OUT OF LIMITS: 8, 12, 19, 22, AND 24 BTW STA XF95 AND XF103 (4 TO 7 INCHES FROM T.E.) ON UPPER SURFACE AT LH AFT MOVABLE VANE AT LH WING. SUMMARY OF NRC 00618: IN REFERENCE TO NRC 00501 DENTS OUT OF LIMITS: 8, 12, 19, 22, AND 24 BTW STA XF95 AND XF103 (4SDR DALA2024111110802Vane · dentedDENT #1 (1EA) OUT OF LIMITS UPPER SURFACE RH FWD MOVEABLE FLAP VANE. DISTANCE TO AFT EDGE 6.650, DISTANCE OF OUTER EDGE 34.900 RH WING. SUMMARY OF NRC 00620: ON REF NRC 00503 DENT #1 (1EA) OUT OF LIMITS UPPER SURFACE RH FWD MOVEABLE FLAP VANE DISTANCE TO AFT ESDR SWAA2024111258016Skin · crackedRIGHT INBOARD AFT FLAP HAS A 3' HORIZONTAL CRACK AND HAS A DENT 40' FROM INBOARD EDGE AND 1/2' FROM LEADING EDGE.<[01] REMOVED AND REPLACED RIGHT HAND INBOARD AFTFLAP; RIG AND OPS CHECK GOOD IAW AMM 27-51-12;[02] C/W INSPECTION OF RIG AND OPS CHECK GOOD IAW AMSDR DALA2024111110811Flap Track · corrodedSHIP 3160 CORROSION WAS FOUND AFFECTING THE INB'D AND OUTB'D AL PLATES AT TRACK #3. CORRECTIVE ACTION: COMPLIED WITH ER/A 31-620919. (0650452)SDR SWAA2024120257643Flap · delaminatedL/H WING O/B T/E FLAP HAS LARGE AREA OF DELAMINATION ON LOWER SKIN AT I/B END (MKD).<[01] REMOVED ' L/H WING OUTBOARD AFT FLAP ' IAW AMM 27-51-22.;[02] REMOVED AND REPLACED L/H WING; O/B FLAP; 'AFT FLAP' IAW AMM 27-51-26.;[03] STEP 2 OF CORRECTIVE ACTIONS HAS SDR SWAA2024120257644Wedge · delaminatedLEFT HAND WING I/B MAIN FLAP T/E WEDGE IS DELAMINATED.<[01] REMOVED TRAILING EDGE WEDGE PER SRM 51-40-02.;[02] PARTIALLY DRILLED NEW LH WING IB MAIN FLAP T/E WEDGE; BOTTOM SIDE ONLY.;[03] DRILLED NEW WEDGE ASSY; INTALLED NUT PLATES AND APPLIED DECORATIVE PAINTSDR SWAA2024120257846Flap · delaminatedRIGHT HAND WING O/B T/E FLAP HAS AN AREA OF DELAMINATING AT I/B END.<[01] REMOVED AND INSTALLED ' R/H WING OUTBOARD AFT FLAP ' IAW AMM 27-51-22.;[02] RII INSPECTION C/WSDR SWAA2024120257847Wedge · delaminatedR/H I/B MAIN FLAP TRAILING EDGE WEDGE IS DELAMINATED.<[01] REMOVED TRAILING EDGE WEDGE PER SRM 51-40-02.;[02] DRILLED UP AND COUNTERSUNK NEW WEDGE IAW SRM 51-40-02.;[03] REMOVED AND INSTALLED NEW PROGRAMMING TRACK PER. SOPM 20-50-01 C/W INSPECTION;[04] DRILL USDR DALA2024110810759Roller · excess playSHIP 3160 EXCESSIVE PLAY CRUISE ROLLER OB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER AS PER AIRBUS CMM 57- 53-21 TASK 57-53-21-000-810-B01 AND CMM 57-53-21 TASK 57-53-21-400-810-B01. (0648983)SDR DALA2024110810726Vane · dentedDENTS (2 EA) ON UPPER SURFACE AFT MOVABLE VANE APPROX BTW STA XRS=69 AND XRS=91 AT RH WING. SUMMARY OF NRC 00143: UPPER SURFACE AFT MOVABLE VANE APPROX BTW STA XRS=69 AND XRS=76 OF RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. (LP #06SDR SWI2025F00104Skin · dentedRH INBD FLAP, THE BOTTOM INBD SKIN HAS SEVERAL DENTS (MARKED) (C-CHECK RO 1/29/2025) RH I/B FLAP BOTTOM I/B SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01, FIG. 57-52-01-995-802, SHEET 1 AND 2. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED FSDR SWI2025F00103Skin · dentedLH INBD FLAP, THE BOTTOM INBD SKIN HAS SEVERAL DENTS (MARKED) (C-CHECK RO 1/29/2025) L/H I/B FLAP, BOTTOM I/B SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01, FIG 57-52-01-995-802, SHEET 1 AND 2. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED SDR SWAA2024120257137Bracket · crackedRIGHT WING TRAILING EDGE; OUTBOARD FIXED TRAILING EDGE PANEL HAS CRACKED BRACKET ON THE R/H SIDE.<[01] REMOVED AND REPLACED BRACKET PER SRM 51-40-02;[02] REMOVED AND REPLACED BRACKET PER SRM 51-40-02;[03] REMOVED AND REPLACED BRACKET PER SRM 51-40-02;[04] CWSDR SWAA2024112757136Web · crackedRIGHT WING TRAILING EDGE HAS A CRACKED WEB ATTACHED TO THE LOWER SURFACE OF THE OUTBOARD TRAILING EDGE FIXED PANEL JUST INBOARD OF THE DEFLECTION RIB.<[01] DRILLED OUT FASTENERS AND REMOVED CRACKED WEB PER SRM 51-40-02.;[02] DRILLED UP NEW WEB PER SRM 51-40-05SDR SWAA2024112657022Flap · delaminatedR/H O/B AFT FLAP HAS SIGN OF DELAMINATION AT THE I/B AFT CORNER AREA. R/H O/B AFT FLAP HAS SIGNS OF DEMLAMINTION AT THE I/B AFT CORNER AREA.<[01] R/H O/B AFT FLAP REMOVED AND REPLACED IAW B737-800 AMM 27-51-22;[02] VERIFIED R/H O/B AFT FLAP REMOVED AND REPLACESDR SWAA2024111157217Skin · crackedRIGHT INBOARD AFT FLAP HAS A 3' HORIZONTAL CRACK AND HAS A DENT 40' FROM INBOARD EDGE AND 1/2' FROM LEADING EDGE<[01] CW EA 24-127-03094SDR DALA2024110710717Plate · corrodedSHIP 3132 CORROSION WAS FOUND AFFECTING THE IB AND OB AL PLATES (FACES AND BORES) AT TRACK #3 LEVEL SPECIFICALLY IN THE INNER AND OUTER RIB 5, ECCENTRIC BEARING AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 618088-14. (0647267)SDR SWAA2025010656626Skin · delaminatedL/H I/B MAIN FLAP LOWER SKIN IS DELAMINATED AT O/B AFT CORNER. (MARKED)<[01] REMOVED; REPLACED; AND INSTALLED A NEW WEDGE AT L/H INBOARD MAIN FLAP IAW SOPM 20-50-01.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWIA2024122301379Vane · chafedRIGHT INBOARD FLAP, NUMBER TWO VANE ACTUATOR SHAFT IS CHAFED, HN00198352 (C-CHECK RO 12/20/2024) REPAIRED RH INBD FLAP VANE ACTUATOR NO. 2 PER MHIRJ REO# 670-57-52-257, REV -A, 2024-08-20. PERFORMED ELECTRICAL RETRACTION & EXTENSION OF THE FLAPS SDR SWIA202412231105Vane · chafedRIGHT INBOARD FLAP, NUMBER ONE VANE ACTUATOR SHAFT IS CHAFED, HN00198345 (C-CHECK RO 12/20/2024) REPAIRED INBOARD FLAP NUMBER ONE VANE ACTUATOR SHAFT, COMPLIED WITH REO 670-57-52-257 REV A DATED 2024-08-20. STEP 5, PERFORMED ELECTRICAL EXTENSION AND
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