JASC 5753

Service difficulty reports · 31,521

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 04FDEA02977Tee Fitting · corrodedRIGHT HAND WING, INBOARD FLAP VANE INBOARD SUPPORT FITTING, INBOARD AFT HOLE CORRODED AND OUTBOARD HOLE (03 OFF) CORRODED. ALL BORES ARE NOT WITHIN EO LIMITS. RIGHT HAND WING, INBOARD FLAP VANE INBOARD SUPPORT FITTING, REMOVED AND REPLACED AS PER AMM 27-50-2Oct 22, 2004 · N602FE · Doug MD11FSDR 04FDEA02982Fitting · wornLT WING FLAP SIDE LOAD ROLLER FITTING LOWER LUG FLAT SPOTTED AND ALL HOLES HAVE EVIDENCE OF PITTING. REMOVED CORROSION AND PITTING FROM LUG AND BORES. FABBED AND INSTALLED 2 EACH REPAIR BUSHINGS IAW SRM57-20-00 VOL.I PAGE 16. INSTALLED BUSHINGS ON NR N01175. Oct 22, 2004 · N392FE · Doug MD1010FSDR 04FDEA02981Roller · wornRT WING FLAP SIDE LOAD ROLLER FITTING LOWER LUG FLAT SPOTTED AND HOLES HAVE EVIDENCE OF PITTING. REMOVED PITTING AND CORROSION FROM LUG AND BORE. FABBED AND INSTALLED 2 EACH REPAIR BUSHINGS IAW SRM 57-20-00 VOL. I PAGE 16. BLENDED FLAT SPOTTED AREA IAW EA8-Oct 22, 2004 · N392FE · Doug MD1010FSDR SWAA043058Skin · debondedRIGHT WING OUTBOARD AFT T/E FLAP DEBONDING. REMOVED AND REPLACED OUTBOARD AFT T/E FLAP PER MM.Oct 21, 2004 · Boeing 7372H4SDR DHL2004755507Skin · delaminatedDURING C-CHECK, LEFT O/B MID FLAP UPPER T/E WBL 297 & 492 HAVE SKINS DELAMINATED. CUT OUT 2EA UPPER T/E DELAM AREAS APPROX 3 X 6.5 INCH & VACUUM BAGGED FOR MOISTURE REMOVAL IAW B727 SRM 51-40-20 FIG 30. FABRICATED 2EA REPLACEMENT SKINS APPROX 3 X 6.5 INCH & Oct 19, 2004 · N755DH · Boeing 727225SDR DHL2004755506Doubler · chafedDURING C-CHECK, LEFT I/B FORE FLAP O/B L/E WBL 240 HAS REPAIR DOUBLER CHAFED THRU. REMOVED PREVIOUS REPAIR AT LEFT, I/B FORE FLAP L/E IAW B727 SRM 51-30-2. FABRICATED DOUBLER REPAIR 2024T3.063 PO 9001276, 6 X 5 INCH IAW B727 SRM 57-50-4 FIG 1, TREATED & PRIMOct 19, 2004 · N755DH · Boeing 727225SDR USAA040829Skin · delaminatedPIT - C4, IB AFT FLAP SKIN, 3 INCHES BY 2.5 INCH AREA, DELAMINATION, IB AFT FLAP OB T/E LEFT WING. REMOVED SKIN AND CORE, INSTALLED REPAIR AND DOUBLER IAW TYP REP 57-53-04 AND SRM 51-70-10.Oct 19, 2004 · N385US · Boeing 7373B7SDR USAA040837Skin · delaminatedPIT - C4, IB AFT FLAP SKIN, 3 INCHES X 2.5 INCHES AREA, DELAMINATION. IB AFT FLAP OB T/E LT WING. REMOVED DELAMINATION, INSTALLED REPAIR CORE, SKIN AND DOUBLER IAW TYP REP 57-53-04 AND SRM 51-70-10.Oct 19, 2004 · N385US · Boeing 7373B7SDR 2004UALA00967Fitting · crackedRIGHT WING INBOARD FLAP CENTER EXTERNAL HINGE FITTING INBOARD AND OUTBOARD FLANGES ARE CRACKED.Oct 19, 2004 · N654UA · Boeing 767322SDR SWAA043031Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LEFT AFT T/E FLAP PER MM.Oct 19, 2004 · N321SW · Boeing 7373H4SDR DHL2004755505Skin · gougedDURING C-CHECK, LEFT I/B MID FLAP UPPER SURF WBL 93 NEAR L/E HAS SKIN GOUGED. GOUGE IN SKIN FOUND TO BE OUT OF LIMITS NDT VERIFY NO FURTHER DAMAGE IAW B727 SRM 57-50-1. REMOVED DAMAGED AREA OF SKIN 1 X 1 INCH IAW B727 SRM 57-50-4. FABRICATED DOUBLER FROM 20Oct 18, 2004 · N755DH · Boeing 727225SDR DHL2004755504Skin · corrodedDURING C-CHECK, LEFT I/B MID FLAP UPPER SURF WBL 124 HAS CORR BULGES AT SKIN BUTT JOINT, MARKED. CUT OUT CORROSION DAMAGED SECTION OF LEFT I/B MID FLAP UPPER SURFACE SKIN AT BUTT JOINT STA 124 SIZE 7.75 X 1.875 INCH IAW B727 SRM 51-10-1. REMOVED & REPLACED UOct 18, 2004 · N755DH · Boeing 727225SDR 04FDEA02947Fitting · corrodedRIGHT HAND WING, INBOARD FLAP VANE OUTBOARD TEE FITTING, ALL (3) BUSHING BORES EXCEEDED LIMIT. RIGHT HAND WING, INBOARD FLAP VANE OUTBOARD TEE FITTING, ALL (3) EXCEEDED LIMIT BORES REPAIRED AS PER EA NR 1-5750-77965, TITLE:WINGS, TRAILING EDGE AND TRAILING Oct 18, 2004 · N612FE · Doug MD11FSDR 04FDEA02946Fitting · corrodedRIGHT WING, INBOARD FLAP VANE INBOARD TEE FITTING, ALL (3) BUSHING BORES EXCEEDED LIMIT. RIGHT WING, INBOARD FLAP VANE INBOARD TEE FITTING, ALL (3) EXCEEDED LIMIT BORES REPAIRED AS PER EA NR 1-5750-77965, TITLE: WINGS, TRAILING EDGE AND TRAILING EDGE DEVICEOct 18, 2004 · N612FE · Doug MD11FSDR 04FDEA02945Tee Fitting · corrodedLEFT HAND WING, INBOARD FLAP VANE OUTBOARD TEE FITTING, ALL (3) BUSHING BORES EXCEEDED LIMIT. LEFT HAND WING INBOARD FLAP VANE OUTBOARD TEE FITTING, ALL (3) EXCEEDED LIMIT. BORES REPAIRED AS PER EA NR 1-5750-77964, TITLE: WINGS-TRAILING EDGE AND TRAILING EDGOct 18, 2004 · N612FE · Doug MD11FSDR 04FDEA02944Tee Fitting · corrodedLEFT HAND WING, INBOARD FLAP VANE INBOARD TEE FITTING, ALL (3) BUSHING BORES EXCEEDED LIMIT. LEFT HAND WING, INBOARD FLAP VANE INBOARD TEE FITTING, ALL (3) EXCEEDED LIMIT. BORES REPAIRED AS PER EA NR 1-5750-77964, WINGS-TRAILING EDGE AND TRAILING EDGE DEVICEOct 18, 2004 · N612FE · Doug MD11FSDR P5CA0401253Flap Track · corrodedNR 6 FLAP TRACK AFT ATTACHMENT IB BLOCK OB HOLE CORRODED ON WING AT STA 353. REMOVED CORROSION, OPEN HOLE HFEC PERFORMED OK, REPAIRED IAW SRM 51-10-01.Oct 18, 2004 · N858FT · Boeing 747123SDR SWAA043001Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT OUTBOARD AFT T/E FLAP PER MM.Oct 16, 2004 · N318SW · Boeing 7373H4SDR SWAA042989Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING AFT FLAP PER MM.Oct 15, 2004 · N648SW · Boeing 7373H4SDR 04FDEA02941Hinge Fitting · corrodedLEFT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT, OUTBOARD BORE PITTED. REMOVED DAMAGE, BORE FOUND OUT OF LIMITS. REPAIRED BORE I/A/W DOUGLAS CMM 57- 52-01 AND FED-EX EA 8-5750-81492 REFERENCE NON-ROUTINE NR N00417.Oct 15, 2004 · N367FE · Doug DC1010SDR 04FDEA02940Hinge Fitting · corrodedRIGHT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT, OUTBOARD BORE GOUGED. REMOVED DAMAGE I/A/W DOUGLAS CMM 57-52-01, BORE FOUND OUT OF LIMITS. REPAIRED BORE I/A/W DOUGLAS CMM 57-52-01 AND FED-EX EA 8-5750-81491 REFERENCE NON-ROUTINE NR N00412.Oct 15, 2004 · N367FE · Doug DC1010SDR 04FDEA02939Roller · wornRIGHT WING INBOARD FLAP INBOARD MOST FORWARD TOP ROLLER IS WORN. REMOVED AND REPLACED RIGHT WING INBOARD FLAP INBOARD TRACK MOST FORWARD TOP ROLLER I/A/W DC10-10 MAINTENANCE MANUAL 20-50-02-2 AND EA 8-5750-81490. REFERENCE NON-ROUTINE NR N00776.Oct 15, 2004 · N367FE · Doug DC1010SDR 04FDEA02938Hinge Fitting · corrodedLEFT WING INBOARD FLAP OUTBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE GOUGED. REMOVED DAMAGE IAW DOUGLAS CMM 57-52-01, BORE FOUND OUT OF LIMITS. REPAIRED BORE I/A/W DOUGLAS CMM 57-52-01 AND FED-EX EA 8-5750-81492 REFERENCE NON-ROUTINE NR N00416.Oct 15, 2004 · N367FE · Doug DC1010SDR 04FDEA02937Hinge Fitting · corrodedRIGHT HAND INBOARD FLAP PIVOT ATTACH POINT, OUTBOARD LUG FACE, OUTER SURFACE CORRODED. REMOVED CORROSION FROM LUG FACE, FOUND TO BE OUT OF LIMITS IAW DC10 CMM 57-52-01. COMPLIED WITH FEDEX EA 8-5750-81475, WINGS, RIGHT HAND INBOARD FLAP OUTBOARD HINGE PIVOTOct 15, 2004 · N392FE · Doug MD1010FSDR 04FDEA02935Fitting · crackedRIGHT HAND WING FOUND OUTBOARD FLAP INBOARD STOP FITTING CRACKED, DURING DVI. STOP FITTING REMOVED & REPLACED AS PER SRM51-31-01VOL2 & SRM 51-33-01 VOL2.Oct 15, 2004 · N602FE · Doug MD11SDR USAA040830Skin · delaminatedPIT - C2, UPPER AND LOWER SKIN, .5 INCH BY 2.5 ALONG T/E, DELAMINATED, IB T/E OF RT OB AFT FLAP. FABRICATED REPAIR SKIN AND DOUBLER AND NEW IAW TR 57-50-39A AND EO 5796X105.Oct 14, 2004 · N504AU · Boeing 7373B7SDR 04FDEA02930Hinge · corrodedBFM CLOSE R COMPLY WITH EA 8-5750-82054 WINGS, INBD FLAP REWORK OF UPSTOP MOUNT HOLES IN ARC0154 HINGE ASSY ENT BY: 497234 RPT BY: 497234 FACT 14OCT04 05:49. BFM U COMPLIED WITH EA 8-5750-82054 WINGS INBD FLAP REWORK OF UPSTOP MOUNT HOLES IN ARC0154 HINGE AOct 14, 2004 · N371FE · Doug DC1010SDR SWAA042972Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.Oct 13, 2004 · N318SW · Boeing 7373H4SDR 04FDEA02929Fitting · corrodedCOMPLY WITH EA 8-5750-82057. WINGS LT IB FLAP VANE ASSY, REPAIR OF O SIZED HOLES IN CHANNEL FITTINGS CLOSING ACTION ON 10/12/04.ON N/R S00010. COMPLIED WITH EA 8-5750-82059.Oct 13, 2004 · N68052 · Doug DC1010SDR IXXA060055SFitting · crackedDURING ROUTINE C CHECK, FOUND LEFT WING TRAILING EDGE FLAP DRIVE LINK FITTING CRACKED AT STATION XW 97.906. REMOVED DRIVE LINK. REMOVED DAMAGED DRIVE LINK FITTING. RECEIVED NEW DRIVE LINK FITTING AND INSTALLED NEW FITTING AT STATION 97.906. INSTALLED DRIVEOct 12, 2004 · N825BX · Doug DC871FSDR IXXA0500054SSkin Panel · corrodedDURING A ROUTINE C CHECK INSPECTION, INTERIM REPAIR FOUND ON LOWER SURFACE OF LT OUTBOARD FLAP STA XF 420.000. REPAIR ACCOMPLISHED REMOVAL OF SKIN WITH THE INTERIM REPAIR ON IT. FABRICATED NEW SKIN PLUS FINGER DOUBLER. BONDED FINGER DOUBLER ON SKIN. CLEANEDOct 11, 2004 · N606AL · Doug DC873FSDR C7WA200400061Flap Track · corrodedRT WING IB FLAP OB TRACK AFT MOUNT PAD HAS CORROSION. RT WING IB FLAP OB. TRACK NR 6 PN 65192493, CORROSION ON AFT MOUNT PAD REMOVED. MATERIAL REMOVED WAS 0.020. REPAIR ACOMPLISHED IAW EO.Oct 11, 2004 · N7635U · Boeing 727222SDR MALA040800Bulkhead · crackedDURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND RT FLAP BEAVERTAIL BULKHEAD CRACKED AT REAR SPAR MOUNT. MAINTENANCE REPAIRED IAW SRM 57-20-10. AIRCRAFT RETURNED TO SERVICE 10/12/04.Oct 11, 2004 · N449XJ · Saab 340BSDR 04FDEA02914Hinge · corrodedLT IB FLAP OB HINGE PIVOT BORE FACE PITTED AND GOUGED (AIRFRAME SIDE) LOCATION NR 3. REMOVED BUSHING, REMOVED CORROSION, AND COMPLIED WITH EA 8-5750-81473 REF NR N00295.Oct 11, 2004 · N392FE · Doug MD1010FSDR 04FDEA02916Hinge Fitting · corrodedLEFT WING INBOARD FLAP OUTBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE GOUGED. REMOVED DAMAGE IAW DACCMM 57-52-01, BORE FOUND OUT OF LIMITS, GENERATED RFTS, RECEIVED FEDEX EA8-5750-81492, REPAIRED BORE IAW DACCMM 57-52-01 AND FEDEX EA8-5750-81492. SEE NR N00Oct 11, 2004 · N392FE · Doug MD1010FSDR 04FDEA02915Support · corrodedRIGHT HAND OUTBOARD FLAP INBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE CORRODED (INBOARD SUPPORT). REMOVED CORROSION IAW DACCMM 57-52-02. ETCHED AND PEENED IAW DACCMM PERCENT &-52-02 AND 20-11-02. FABBED BUSHING IAW DACCMM 57-52-02 AND EA8-5750-81472. CAOct 11, 2004 · N392FE · Doug MD1010FSDR 04FDEA02911Support · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUG HAS CORROSION. REMOVED CORROSION IAW DACCMM 57-44-07. FOUND TO BE STRUCTURALLY ACCEPTABLE IAW FEDEX EA8-5750-81474. ALODINED AND PRIMED LUG FACES IAW DC10 SRM 51-21-01 VOLUME IOct 11, 2004 · N392FE · Doug MD1010FSDR 04FDEA02910Support · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 3 HAS CORROSION IN BORE. REMOVED CORROSION IAW DACCMM 57-44-07. BEGINNING BORE 2.5850 INCH FINAL 2.626 INCH MATERIAL. REMOVED .041 INCH. FABRICATED BUSHING IAW DACCMM 57-44-07 AND EA8-5750-81473. ACCOMPOct 11, 2004 · N392FE · Doug MD1010FSDR 04FDEA02908Support · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUGS HAVE CORROSION. REMOVED CORROSION FROM LOCATION NR 1 MOUNTING SURFACE IAW DACCMM 57-44-07 AND FEDEX EA8-5750- 81473. PRIMED LUGS IAW DC10 SRM 57-21-01 VOLUME I, BEGINNING BOREOct 11, 2004 · N392FE · Doug MD1010FSDR 04FDEA02907Hinge Fitting · corrodedRIGHT HAND INBOARD FLAP PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION BEGINNING BORE 1.1875 INCH FINAL 1.2583 INCH MATERIAL REMOVED .0708 INCH IAW DACCMM 57-52-01. FABBED REPAIR BUSHING IAW DACCMM 57-52-01 AND EA8-5750-81475. PERFORMED MPI IAWOct 11, 2004 · N392FE · Doug MD1010FSDR 04FDEA02903Hinge · corrodedLEFT WING OUTBOARD FLAP INBOARD HINGE, LOCATION NR 4 BORE CORRODED. REMOVED CORROSION IAW DACCMM 57-44-08, INSPECTED IAW DACCMM 57-44-08 AND 20-11-02. PEENED IAW DACCMM 57-44-08 AND 20-11-01. PRIMED IAW DC10 SRM 51-21-01 VOL. II. FABBED BUSHING IAW DACCMM Oct 11, 2004 · N392FE · Doug MD1010FSDR 04FDEA02902Fitting · damagedRIGHT HAND INBD FLAP PIVOT POINT OUTBOARD BORE HAS GROOVE MARK. REMOVED CORROSION IAW DAC CMM 57-52-01. BEGINNING DIAMETER 1.1875 INCH FINAL 1.2552 INCH . FABBED REPAIR BUSHING IAW DACCMM 57-52-01 AND EA8-5750-81475 MPI IAW DACCMM 5752-01 AND DPS 4.704 CAD POct 11, 2004 · N392FE · Doug MD1010FSDR 04FDEA02900Stop · corrodedRT WING INBD FLAP REWORK OF UPSTOP MOUNT HOLE IN ARC0154 HINGE ASSY. COMPLIED WITH E.A.8-5750-82056.Oct 11, 2004 · N371FE · Doug DC1010SDR IXXA060021SSkin · delaminatedDURING ROUTINE C-CHECK FOUND LT WING IB FLAP TRAILING EDGE PANEL UPPER SKIN DELAMINATED. REMOVED FASTENEERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN SECTION. FABRICATED FINGER DOUBLERS AND NEW UPPER SKIN SECTION. LOCATED, DRILLED, TRIMMED, TREATED, PROct 10, 2004 · N825BX · Doug DC871FSDR 2004UALA00925Hinge Fitting · crackedLT WING IB FLAP OB HINGE FITTING CRACKED AFT VANE. SUPPLEMENTAL DATA UPDATE REPAIRED FITTING WITH ANGLE AND FILLER REPAIR.Oct 10, 2004 · N655UA · Boeing 767322SDR 04FDEA02897Vane · corrodedWINGS, RT INBD FLAP VANE ASSY, REPAIR OF OVERSIZED HOLES ON CHANNEL FITTINGS. COMPLIED WITH EA 8-5750-82058.Oct 9, 2004 · N68052 · Doug DC1010FSDR SWAA042927Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E FLAP PER MM.Oct 8, 2004 · N612SW · Boeing 7373H4SDR IXXA060089SSkin · puncturedDURING ROUTINE C CHECK FOUND RIGHT HAND WING INBOARD FLAP OUTBOARD VANE UPPER SIDE SKIN PUNCTURED. REMOVED VANE. REMOVED DAMAGED. MANUFACTURED REPAIR PARTS, PERFORMED HOT BOND. INSTALLED VANE. IAW DC8 MM 27-51-14, DC8 SRM 51-1-9A.Oct 7, 2004 · N825BX · Doug DC871FSDR IXXA060088SSkin · delaminatedDURING ROUTINE C-CHECK FOUND RT WING IB FLAP OB VANE UPPER SKIN DELAMINATED. REMOVED FLAP VANE. REMOVED DELAMINATED SKIN, PERFORMED HOT BOND TO DAMAGED AREA. INSTALLED VANE. IAW MM 27-51-14, SRM 51-1-9A.Oct 7, 2004 · N825BX · Doug DC871FSDR MALA040779Skin · damagedDURING C-CHECK INSPECTION IN YYC, LT FLAP TOP SKIN FOUND DAMAGED. MAINTENANCE REPAIRED IAW EO A57079. AIRCRAFT RETURNED TO SERVICE 10/17/04.Oct 7, 2004 · N513XJ · Bac AVRO146RJ85A
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