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.

SDR WRXR20250117001Hinge · gougedGOUGE ON RH HINGE ARM FITTING PN.CC670-14131-4 AT I/B FLAP WS54.55. MEASURES .250 X .025. ROTO-PEEN REWORKED AREA IAW CRJ 700 SRM 51-24-11. ALODINED AND PRIMED RH HINGE ARM FITTING PN.CC670-14131-4 AT I/B FLAP WS54.55. IAW CRJ700 SRM 51-21-001-001-A01 AND CRJJan 17, 2025 · N540EG · Cndair CL6002C10SDR SWAA2025011686689Skin · crackedRH IB AFT FLAP HAS DENT/CRACK AT 20 IN. FROM IB END AND 11.7 IN. FROM TE RH IB AFT FLAP HAS DENT/CRACK AT 20 IN. FROM IB END AND 11.7 IN. FROM TE. DENT MEASURES 1.6 IN. X 1.5 IN. AND .360 IN. DEEP CRACK IS .5 IN. LONG.<[01] REPAIRED FLAP PER SRM 57-53-01-2R-4 Jan 16, 2025 · N8561Z · Boeing 7378H4SDR IPXA2025022037965Bracket · corrodedSTR - L/H I/B FLAP I/B TRACK FITTINGS HAS 8 HOLES WITH PITTING. ATA 57-55. ACCOMPLISHED REPAIR PER EO-92870-REQ1 AND VT-SAA EA 011-5753-01-B0371 I/R. REVIEWEDJan 16, 2025 · N255UP · Doug MD11FSDR IPXA2025012634796Angle · brokenLEFTO/B FLAP INBD EDGE ANGLE WEB BROKEN DOT# 110-161 JP-110. REMOVED AND REPLACED ANGLE P/N A5796040221400 BATCH # 0004352771. IAW A300-600 SRM 51-40-21. OSD: 1/27/2025Jan 16, 2025 · N171UP · Airbus A300F4622RSDR IPXA2025012634986Angle · brokenLEFT CENTER FLAP IO/B EDGE ANGLE WEB BROKEN DOT# 110-162 JP-110. TECHNICIAN #91195302 (MCCANKIUS HARRIS) REMOVED AND REPLACED ANGLE P/N A5796040221400 BATCH # 0004352771. IAW A300-600 SRM 51-40-21. OSD: 1/27/2025Jan 16, 2025 · N171UP · Airbus A300F4622RSDR IPXA2025012635000Angle · brokenRIGHT CENTER FLAP IO/B EDGE ANGLE WEB BROKEN DOT# 110-163 JP-110. REMOVED AND REPLACED ANGLE P/N A5796040221400 BATCH #004352771 IAW SRM51-40-21.Jan 16, 2025 · N171UP · Airbus A300F4622RSDR DALA2025012300550Bearing · corrodedSHIP 3147 LH WING INNER FLAP EQUIPPED AT FLAP TRACK #2 LEVEL ATTCHT BEARING AT RIB 9 ASSY CORROSION. CORRECTIVE ACTION: REPAIRED PER ER/A 622658-14. (0764439)Jan 16, 2025 · N347NB · Airbus A319114SDR DALA2025011700408Hinge Arm · damagedSHIP 3147 ELONGATED HOLE (0.3119) WAS FOUND IN THE HINGE ARM BR2. CORRECTIVE ACTION: COMPLIED WITH ER/A 622906-14. (764430)Jan 16, 2025 · N347NB · Airbus A319114SDR VNAA20250116039Skin · dentedTHE LEFT WING INBOARD FLAP LOWER SKIN IS DENTED 6 X 6 X .035 JUST AFT OF THE MLG TIRES. CORRECTIVE ACTION: REPAIRED IAW CRJ-700 SRM 57-52-01-201-005-A01.Jan 16, 2025 · N709PS · Cndair CL6002C10SDR UIEA2025011000019Skin · delaminatedLEFT WING, INBOARD FLAP LOWER AREA BTW WS 314 AND WS404 WITH DELAMINATION.(<P>LEFT WING INBOARD FLAP LOWER AREA WAS REPAIRED IAW SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED</P>)Jan 15, 2025 · N641GT · Boeing 76738ESDR DALA2025011600399Track · corrodedSHIP 3147 CORROSIONS WERE FOUND IN TRACK 3 SUB-ASSY. CORRECTIVE ACTION: COMPLIED WITH ER/A 623039-14. (0762470)Jan 15, 2025 · N347NB · Airbus A319114SDR SWAA2025022885827Flap · delaminatedRIGHT WING OUTBOARD AFT FLAP INBOARD LOWER CORNER IS DELAMINATED <[01]. REMOVED AND REPLACED RIGHT WING OUTBOARD AFT FLAP IAW B737-800 AMM 27-51-22-401-NG.; [02] VERIFIED REMOVED AND REPLACED RIGHT WING OUTBOARD AFT FLAP IAW B737-800 AMM 27-51-22-401-NG.; [03Jan 14, 2025 · N8608N · Boeing 7378H4SDR UIEA2025011300051Skin · dentedRH WING, AFT FLAP LOWER SKIN OUTER PLIES WITH DENT BETWEEN IFS 230 AND IFS 280.(<P>DENT WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 4 PAGE 1-5. NO FURTHER DEFECTS NOTED</P>)Jan 14, 2025 · N664GT · Boeing 76731BSDR UIEA2025010900006Skin · dentedLH WING INBOARD AFT FLAP, DENTS ON LOWER SKIN. LH WING INBOARD AFT FLAP, DENT'S ON LOWER SKIN WERE REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 4 NOTE A PAG 1-5 AND SRM 51-70-03-OG-O PAR 5L FIG 16 PAG 15, -41 REV 127 15/DEC/24. NO FURTHER DEFECTS NOTED/Jan 14, 2025 · N664GT · Boeing 76731BSDR UIEA2025010900005Skin · dentedRH WING, AFT FLAP UPPER SKIN WITH DENT BETWEEN IFS 230. RH WING AFT FLAP UPPER SKIN WITH DENT BETWEEN IFS 230 WAS REPAIRED IAW SRM 57-53-01-2R-1 PAG 1-7 FIG 201 AND SRM 51-70-10-2R-4 PAG 8-22 FIG 202 SHEET 1 REV 127 15/DEC/24. NO FURTHER DEFECTS NOTED.Jan 14, 2025 · N664GT · Boeing 76731BSDR WRXR20250113002Skin · chafedRH WS54.55 AFT HINGE WAS CHAFFING ON FLAP LOWER SKIN COMMON TO FAIRING SEAL. BLENDED CHAFE DAMAGE TO RH INBD FLAP LOWER SKIN, (DWG: CC670-14061, AL ALY ALCD 2024-T3, 0.063” NOMINAL STOCK THICKNESS, 0.052” ± 0.003” & 0.040” ± 0.003” CHEM. MILL POCKET THICKNESSJan 13, 2025 · N540EG · Cndair CL6002C10SDR IPXA2025030442568Hinge Bracket · corrodedHINGE 3 LH/ I/B FLAP O/B FWD HINGE LUG #3 BORE HAS CORROSION BR-097 57-55. ACCOMPLISHED REPAIR PER UPS EO-92718-REQ1 AND VT-SAA EA 011-5740-01-B0370 I/R.Jan 11, 2025 · N255UP · Doug MD11FSDR IPXA2025030442543Hinge Bracket · corrodedHINGE 3 L/H I/B FLAP O/B FWD HINGE LUG #3 O/B FACE HAS CORROSION BR-096 57-55. ACCOMPLISHED REPAIR PER UPS EO-92718-REQ1 AND VT-SAA EA 011-5740-01-B0370 I/R.Jan 11, 2025 · N255UP · Doug MD11FSDR IPXA2025030442447Hinge Bracket · corrodedHINGE 3 L/H I/B FLAP O/B FWD HINGE LUG#3 I/B FACE HAS CORROSION BR-095 57-55. ACCOMPLISHED REPAIR PER UPS EO-92718-REQ1 AND VT-SAA EA 011-5740-01-B0370 I/R.Jan 11, 2025 · N255UP · Doug MD11FSDR IPXA2025022742742Hinge Bracket · corrodedSTR-HINGE 4 R/H I/B FLAP O/B FWD HINGE LUG #3 BORE HAS CORROSION BR-102 57-55. ACCOMPLISHED REPAIR PER EO-92720-REQ1 AND VT-SAA EA 011-5740-01-B0327 I/R. REVIEWEDJan 11, 2025 · N255UP · Doug MD11FSDR SWAA2025012885196Flap · delaminatedLEFT OUTBOARD AFT FLAP HAS AN AREA OF DELAMINATION ON THE INBOARD BOTTOM SURFACE. REMOVED LEFT HAND OUTBOARD AFT FLAP PER AMM 27-51-22. INSTALLED NEW LEFT AFT OUTBOARD FLAP PER AMM 27-51-22. VERIFIED ATTACHMENT FASTENER'S SAFETIES AND TORQUES. REMOVED ANJan 11, 2025 · N8679A · Boeing 7378H4SDR SWIA2025040400110Vane · gougedRIGHT WING OUTBOARD FLAP VANE MULTIPLE BUTTE DOOR CAMS GOUGED AS MARKED (C-CHECK RO 04/04/2025)INSTALLED NEW BUTE DOOR CAM FITTING AT FLS296.07 AND APPLIED AERODYNAMIC SEALANT REF CRJ 700 SRM 57-53-02-201-002-A01 REPAIR TYPE 1 AND REPAIRED ALL OTHER LOCATIONJan 10, 2025 · N707SK · Cndair CL6002C10SDR IPXA2025030424694Hinge Bracket · corrodedSTR- HINGE 2 L/H O/B FLAP I/B FWD HINHE O/B LUG #8 BORE HAS CORROSION. BR-066. ACCOMPLISHED REPAIR PER EO-92719-REQ1 AND EA 011-5740-01-B0364 IR. PRODUCTION AUDIT C/WJan 10, 2025 · N255UP · Doug MD11FSDR IPXA2025030424543Hinge Bracket · corrodedSTR- HINGE 2 L/H O/B FLAP I/B FWD HINGE I/B LUG #8 BORE HAS CORROSION. BR-063. ACCOMPLISHED REPAIR PER EO-92719-REQ1 AND EA 011-5740-01-B0364 IR. REVIEW COMPLETEJan 10, 2025 · N255UP · Doug MD11FSDR IPXA2025030425395Hinge Bracket · corrodedHINGE 6 R/H O/B FLAP O/B FWD HINGE I/B LUG #8 BORE HAS CORROSION. BR-051. ACCOMPLISHED REPAIR PER EO-92922-REQ1 AND EA 011-5740-01-B0372 IR. PRODUCTION AUDIT C/WJan 10, 2025 · N255UP · Doug MD11FSDR IPXA2025030424321Hinge Bracket · corrodedHINGE 1 L/H O/B FLAP O/B FWD HINGE O/B LUG #8 BORE HAS CORROSION. BR-060. ACCOMPLISHED REPAIR PER EO-92860-REQ1 AND EA 011-5740-01-B0362 IR.Jan 10, 2025 · N255UP · Doug MD11FSDR IPXA2025030430416Hinge · corrodedINGE 8 L/H O/B FLAP I/B AFT HINGE LUG #11 BORE HAS CORROSION. BR-078. ACCOMPLISH REPAIR PER CMM 57-52-04. L/H O/B FLAP I/B AFT HINGE WAS REPLACED DUE TO CORROSION AND INCOMING REPAIRS EXCEEDING REPAIR LIMITS IAW BOEING CMM 57-52-04. REVIEWEDJan 10, 2025 · N255UP · Doug MD11FSDR IPXA2025030429920Hinge · corrodedSTR- HINGE 7 L/H O/B FLAP O/B AFT HINGE LUG #11 BORE HAS CORROSION. BR-069. REMOVE AND REPLACE OUTBOARD SUPPORT HINGE ASSEMBLY P/N ARC1991-501 PER CMM 57-52-04. REVIEWEDJan 10, 2025 · N255UP · Doug MD11FSDR IPXA2025022824162Hinge · corrodedHINGE 1 L/H O/B FLAP O/B FWD HINGE I/B LUG #8 BORE HAS CORROSION. BR-057. ACCOMPLISHED REPAIR PER EO-92860-REQ1 AND EA 011-5740-01-B0362 IR.Jan 10, 2025 · N255UP · Doug MD11FSDR REXA2025012900099Bumper · wornLH AND RH FLAP VANE BUMPERS WORN NBUMPERS ON FLAP VANE LH (1EA) AND RH (2EAS) WERE REPLACED PER CRJ 900 SRM 51-42-10-001-001-A01 PAR 8.C AND SRM 51-41-02-001-001-A01Jan 10, 2025 · N349PQ · Cndair CL6002D24SDR DALA2025011300247Flap Track · corrodedSHIP 3147 CORROSION FOUND ON INB'D AND OUTB'D AL PLATES AT TRACK #3, INNER AND OUTER RIB 5, ECCENTRIC BEARING, BORES. CORRECTIVE ACTION: REPAIRED WITH ER/A 623009-14. (0755439)Jan 10, 2025 · N347NB · Airbus A319114SDR FDEA202501100055Hinge Bracket · corrodedRIGHT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE FOUND CORROSION. CORROSION AT RIGHT HAND, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACJan 10, 2025 · N607FE · Doug MD11FSDR FDEA202501100054Skin · dentedFOUND RHW T/E O/B FLAP LOWER SURFACE DENT 1EA AT THE CROSS OTEF 249 AND T/E 11 INCHS. REPAIRED RH WING T/E O/B FLAP LOWER SURFACE DENT AT OTEF STA 249 AS PER B777 SRM 57- 53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1 REV 47.2 AND EA: G-5750-T0381784 P1. TJan 10, 2025 · N866FD · Boeing 777FSDR FDEA202501100053Hinge Bracket · corrodedLEFT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATEDJan 10, 2025 · N607FE · Doug MD11FSDR IPXA2025022605227Hinge · corrodedSTR-HINGE 11 R/H O/B FLAP I/B AFT HINGE LUG #13 I/B FACE HAS INCOMING REPAIR AND CORROSION BR-020. REMOVE AND REPLACE SUPPORT HINGE ASSY P/N=ARC1984-502 IAW BOEING CMM 57-52-04. REVIEWEDJan 9, 2025 · N255UP · Doug MD11FSDR IPXA2025022605426Hinge · corrodedSTR- HINGE 12 R/H O/B FLAP O/B AFT HINGE LUG #13 I/B FACE HAS INCOMING REPAIR BR-023. REMOVE AND REPLACE RIGHT-HAND OUTBOARD FLAP OUTBOARD AFT HINGE PER BOEING CMM 57-52-04. REVIEWEDJan 9, 2025 · N255UP · Doug MD11FSDR DXTA2025011401902Skin · dentedDENT DISCOVERED ON TOP OF LEFT WING.2). FLAP: RIGHT FLAP HAS A NOTICEABLE DENT ON THE TOP DISCOVERED DURING PREFLIGHT INSPECTION. PERFORMED PERMANENT REPAIR IAW RFTS-112809 AND SPM 20-50-00.Jan 9, 2025 · N627QS · Cessna 680ASDR DALA2025011300274Skin · dentedDENT #4, XF=89.250" DAE=13.500"; DENT #5, XF=86.500" DAE=11.500"; DENT#6. XF=88.375" DAE=14"; AND DENT#26, XF=81.250" DAE=4.500" WERE FOUND OUT OF LIMITS ON LOWER SURFACE ON AFT MOVABLE FLAP VANE AT RH WING. SUMMARY OF NRC 00592: RIGHT WING AFT MOVABLE FLAP VAJan 9, 2025 · N995AT · Boeing 717200SDR DALA2025011000224Roller · excess playSHIP 3421 R/H WING, O/B FLAP UPLOCK ROLLER HAS PLAY. CORRECTIVE ACTION: REPLACED ROLLER ASSYS PER A330 AMM 27-54-73. (0753315)Jan 9, 2025 · N421DX · Airbus A330941SDR DALA2025011000223Roller · excess playSHIP 3421 L/H WING, O/B FLAP UPLOCK ROLLER HAS PLAY. CORRECTIVE ACTION: REPLACED ROLLER ASSYS PER A330 AMM 27-54-73. (0753314)Jan 9, 2025 · N421DX · Airbus A330941SDR IPXA2025030585017Hinge · corrodedHINGE 10 R/H I/B FLAP O/B AFT HINGE LUG #13 BORE HAS CORROSION BR-008. INSTALLED REPAIR BUSHING AT R/H I/B FLAP O/B AFT HINGE AT LUG BORE #13 IAW BOEING CMM 57-52-03 AND E.A. 011-5740-01-B0361 STEP 9. ACCOMPLISHED REPAIR PER EO-92858-REQ1 AND VT-SAA EA 011-5Jan 8, 2025 · N255UP · Doug MD11FSDR IPXA2025030585432Hinge · corrodedHINGE 10 R/H I/B FLAP O/B AFT HINGE LUG #14 BORE HAS CORROSION BR-011. INSTALLED REPAIR BUSHING AT R/H I/B FLAP O/B AFT HINGE AT LUG BORE#14 IAW BOEING CMM 57-52-03 AND E.A. 011-5740-01-B0360. ACCOMPLISHED REPAIR PER EO-92858-REQ1 AND VT-SAA EA 011-5740-01-B0Jan 8, 2025 · N255UP · Doug MD11FSDR IPXA2025022286041Hinge · corrodedSTR- HINGE 9 L/H I/B FLAP O/B AFT HINGE LUG #14 BORE HAS CORROSION BR-005. ACCOMPLISHED REPAIR PER EO-92848-REQ1 AND VT-SAA EA 011-5740-01-B0343 I/R. REVIEWEDJan 8, 2025 · N255UP · Doug MD11FSDR SWAA2025010884121Skin · delaminatedLH INBOARD MAIN FLAP LOWER SKIN DELAMINATION AT AFT OUTBOARD. REMOVED AND REPLACED L/H I/B AFT FLAP O/B WEDGE PANEL PER AMM 27-51-11.Jan 8, 2025 · N428WN · Boeing 7377H4SDR SWAA2025010884119Skin · delaminatedRIGHT INBD MAIN FLAP LOWER SKIN O/B END OF TRAILING EDGE, AREA OF DELAMINATION. REMOVED SECTION OF DISBONDED LOWER SKIN; PREPPED AREA; APPLIED BOEGEL; BOND PRIMER; LAYED UP REPAIR PARTS AND STARTED CURE PER SRM 57-53-01-2R-7. PERMANENT REPAIR ACCOMPLISHED PJan 8, 2025 · N428WN · Boeing 7377H4SDR IXXA20250130001Skin · dentedRIGHT WING I/B AFR FLAP UPPER SKIN HAS A DENT 35.7" FROM I/B END. REF HAECO WO 320010 NON ROUTINE 30313Jan 7, 2025 · N571AZ · Boeing 767323SDR AALA202501105352Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND WING OUTBOARD FLAP INBOARD UPPER AFT CORNER HAS POSSIBLE DELAMINATION. APPLIED PERMANENT REPAIR ON LEFT HAND WING OUTBOARD FLAP INBOARD UPPER AFT CORNER. PER B737-NG SRM 57-53-01-2R-4 B737-NG SRM 51-70-10-2R-4AND B737-NJan 7, 2025 · N981NN · Boeing 737823SDR SWI2025F00812Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA85681-670-57-53-141 MXCODEID69288-PR - DENT TO LH OUTBOARD FLAP LOWER SKIN AFT OF INTERCOSTAL SPAR DATUM BETWEEN FS171.963-FS179.965. THIS TEMPORARY DISPOSITION IS VALID FOR 4300 FLIGHT HOURS FROM THE TIME OF INCORPORAJan 6, 2025 · N800SK · Cndair CL6002D24SDR SWAA2025010683384Wedge · delaminatedINBOARD MAIN FLAP TRAILING EDGE WEDGE ASSEMBLY DELAMINATED.<[01] REMOVED DAMAGED OTBBOARD T/E WEDGE FROM RT MAIN FLAP; LOCATED AND DRILLED NEW WEDGE PER SRM 51-40-06;[02] REMOVED AND REPLACED WEDGE PER M/M 27-51-00Jan 6, 2025 · N7821L · Boeing 7377CTSDR DALA2025010600082Bearing · corrodedSHIP 3147 CORROSION I/B SPHERICAL BEARING ON O/B LH FLAP. CORRECTIVE ACTION: REPLACED I/B SPHERICAL BEARING ON O/B LH FLAP AS PER A320 AMM 57-53-21-000-001-A AND AS PER A320 AMM 57-53-21-400-001-A. (0746501)Jan 5, 2025 · N347NB · Airbus A319114
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