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 SWAA050975Skin · peelingRIGHT WING INBOARD T/E FOREFLAP PREVIOUS REPAIR PEELING. TEMP REPAIRED PER SWA EA, THEN LATER AT PHX, REMOVED AND REPLACED FOREFLAP PER MM.Mar 31, 2005 · N396SW · Boeing 7373H4SDR 05FDEA00763Structure · damagedREPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR AND MINOR CLASSIFICATION. RT WING RT I/B T/E LOWER SURFACE AFT OF NR 2 FLAP TRACK BEAM. COMPLIED WITH EA 6-5750-87747 PART 1. NO DEFECTS NOTED PER NTM 51-10-08. REPAIR IS CLASSIFIED AS A MINOR REPAIMar 31, 2005 · N419FE · Airbus A310SDR 05FDEA00756Wedge · damagedREPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION, LT WING COMPOSITE REPAIR LOWER SURFACE INBD T/E FLAP WEDGE 5 INCH FWD OF AFT EDGE AND 28 INCH O/B OF I/B EDGE. COMPLIED WITH EA6-5750-87746 PT1 NO ANOMALIES NOTED AS PER FEDEX GMMar 31, 2005 · N419FE · Airbus A310SDR 05FDEA00708Hinge · corrodedLEFT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT OUTBOARD BORE CORRODED. REMOVED CORROSION FROM BORE IAW DAC CMM 57-52-01. ALODINED AND PRIMED BORE IAW DC10-10 SRM 51-21-01 VOL 2, FABRICATED AND INSTALLED FINAL HONED NEW OVERSIZED BUSHING TO 0.99Mar 30, 2005 · N10060 · Doug DC10*SDR 05FDEA00707Hinge · corrodedLEFT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION FROM BORE IAW DAC CMM 57-52-01, ALODINE AND PRIMED BORE IAW DC19-10 SRM 51-21-01 VOL 2. FABRICATED AND INSTALLED AND FINAL HONED NEW OVERSIZED BUSHING TO 0.Mar 30, 2005 · N10060 · Doug MD1010FSDR 05FDEA00706Skin · damagedRIGHT WING INBOARD FLAP, INCORRECT REPAIR ON UPPER SKIN, INBOARD WEDGE. REMOVED DOUBLER, FABRICATED NEW SKIN, FINGER DOUBLERS AND DOUBLER AND BONDED IAW FEDEX EA 8- 5710-84001 AND TPS 1001 REV E AND DC10 SRM 51-21-01 VOL 2 AND DC10 SRM 51-31-01 VOL 2. REFEMar 30, 2005 · Doug DC10*SDR DHL2005740514Skin · delaminatedCUT OUT DAMAGED AREA LWR SKIN APPROX 5 X 1.5 INCH IAW B727 SRM 51-40-20 FIG 31. FABRICATED ONE FILLER APPROX 5 X 1.5 INCH AND ONE DOUBLER APPROX 8 X 3 INCHES USING .016 2024-T3 PO 9001660 IAW B727 SRM 57-50-2 FIG 4. CLEANED, PREPPED, APPLIED ADHESIVE PRIMERMar 27, 2005 · N740DH · Boeing 7272Q9SDR DHL2005740513Skin · debondedRT WING TE OB AFT FLAP LOWER SKIN DISBONDED AT TE CENTER. CUT OUT DAMAGED AREA LWR SKIN APPROX 5 INCHES BY 1 1/2 INCHES IAW B727 SRM 54-40-20 FIG 31. FABRICATED ONE FILLER APPROX 5 INCHES BY 1 1/2 INCHES AND ONE DOUBLER APPROX 8 INCHES BY 3 INCHES USING .01Mar 27, 2005 · N740 · Boeing 7272Q9SDR DHL2005740505Skin · delaminatedRT WING OUTBD AFT-FLAP TRAILING EDGE INBD CORNER IS DELAMINATED LOWER SURFACE. CUTOUT DAMAGED LWR SURFACE APPROX 3 INCH BY 5 INCH BAGGED FOR MOISTURE REMOVAL IAW B727 SRM 51-40-20 FIG 32. REMOVAL AND REPLACED HONEYCOMB CORE APPROX 3 INCH BY 4 INCH USING DUR-Mar 27, 2005 · N740DH · Boeing 7272Q9SDR SWAA050938Skin · delaminatedRIGHT WING INBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.Mar 27, 2005 · N327SW · Boeing 7373H4SDR QXEA200500537Skin · chafedPDX - LEFT WING OUTBOARD FLAP, UPPER SURFACE IS CHAFED BETWEEN YW222 AND YW285. REPAIRED IAW HORIZON AIR EA 6-57-325.Mar 25, 2005 · N416QX · Bombdr DHC8401SDR 05FDEA00644Flap Track · corrodedNR 1 FLAP TRACK FWD I/B ATTACH LUG CORRODED. REPLACED PER FED EX W/C 27X5707-03.Mar 25, 2005 · N481FE · Boeing 727200SDR 05FDEA00643Flap Track · corrodedNR 3 FLAP TRACK AFT MOUNTING PAD CORRODED. REPLACED NR 3 FLAP TRACK PER FED EX W/C 27X5705-03.Mar 25, 2005 · N481FE · Boeing 727200SDR QXEA200500633Hinge · chafedYYC - RIGHTHAND INBOARD FLAP LOWER SURFACE INBOARD HINGE AREA HAS CHAFED MARKS FROM FAIRING. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01.Mar 24, 2005 · N612QX · Cndair CL6002C10SDR QXEA200500627Skin · damagedYYC - RIGHTHAND INBOARD FLAP LOWER SURFACE HAS GRAVEL DAMAGE. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, SRM 51-12-00-001-001-A01, SRM 51-25-01-001-001-A01 AND SRM 57-52-01-101-001-A01.Mar 24, 2005 · N612QX · Cndair CL6002C10SDR UIEA200500038Spar · corrodedDURING SCHEDULE INSPECTION, CORROSION WAS FOUND ON THE REAR SPAR ATTACHMENT HOLES OF NR 5 TRAILING EDGE FLAP TRACK. OVERSIZED THE AFFECTED ATTACHMENT HOLES. MAGNETIC PARTICLE INSPECTED THE REWORKED AREA TO ENSURE CRACK AND DEFECT FREE CONDITION. THE REPAIREMar 24, 2005 · N527MC · Boeing 7472D7BSDR UIEA200500039Skin · delaminatedDURING SCHEDULE INSPECTION, DELAMINATION WAS FOUND ON THE OUTBOARD TRAILING EDGE FLAP AFT FLAP LOWER SKIN PANEL. PANELS EXCEEDED 25 PERCENT DAMAGE OF THE TOTAL AREA. TRIMMED OUT THE DELAMINATED SKIN REGIONS. NDT INSPECTED TO ENSURE CRACK AND DEFECT FREE CONMar 24, 2005 · N527MC · Boeing 7472D7BSDR QXEA200500553Skin · damagedYYC - LEFTHAND INBOARD FLAP LOWER SURFACE GRAVEL DAMAGED. REPAIRED IAW CRJ 700 SRM 51-25-01-001-A01.Mar 24, 2005 · N612QX · Cndair CL6002C10SDR SWAA050904Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING INBOARDD MIDFLAP OUTBOARD T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.Mar 24, 2005 · N324SW · Boeing 7373H4SDR DHL2005782561Skin · delaminatedLT WING OB AFT FLAP OB TE CORNER DELAMINATED. REMOVED PREVIOUS REPAIR AND CUT OUT DELAMINATED AREA OF LOWER SKIN APPROX 7" BY 5" AT O/B CORNER AND VACUUM BAGGED FOR MOISTURE REMOVAL IAW B727 SRM 51-40-20 FIG 31. FABRICATED REPLACEMENT SKIN APPROX 7" BY 5" AMar 23, 2005 · N782DH · Boeing 727227SDR SWAA050878Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD AFT FLAP T/E DELAMINATED. REPAIRED FLAP PER SRM.Mar 22, 2005 · N355SW · Boeing 7373H4SDR UIEA200500030Link · migratedDURING SCHEDULE MAINTENANCE, NR 4 T/E FLAP TRACK FAIL/SAFE LINK TOP END BEARING ON THE 'T' CHORD FOUND MIGRATED. THE LEFT FIXED TRAILING EDGE UPPER CHORD HOLE HAS ELONGATED DAMAGED. OVERSIZED HOUSING BORE TO A MAXIMUM OF .8930 INCH DIAMTER. NDT INSPECTED THMar 21, 2005 · N527MC · Boeing 7472D7BSDR DL757050179Spar · crackedDURING SHOP VISIT, IMPACT DAMAGE WAS FOUND ON THE RT INBOARD MAIN FLAP. THE IMPACT CAUSED DAMAGE TO THE REAR SPAR LOWER CHORD, WHICH WAS SPLICE REPAIRED BETWEEN STA 117 AND 127. REPAIRED PER DELTA ERA 097596-14.Mar 21, 2005 · N670DN · Boeing 757232SDR ASAA0540193Wedge · chafedRT WING IB T/E MIF FLAP T/E WEDGE IS CHAFFED. REMOVED DAMAGED WEDGE, ORDERED AND REPLACED WITH A NEW WEDGE IAW SRM. (K)Mar 20, 2005 · N782AS · Boeing 7374Q8SDR UPS05844293Rib · damagedINSPECTION TYPE:C2 RIGHT STA 3 AFT LINK TO FLAP HINGE BOLT FROZEN & NUT PLATE BROKEN. REMOVED DAMAGED RIB, REMOVED AND REPLACED NUT PLATE, AND FABRICATED & INSTALLED REPLACEMENT RIB PER EO DC8-5750-16293-A AND DWG DC8-57-009.Mar 20, 2005 · N819UP · Doug DC873FSDR GAIA05014STSkin · delaminatedDURING A-CHECK, NO FLIGHT, FWA: FOUND LT IB MID-FLAP OB T/E MISSING 6 INCHES OF SKIN. REMOVED AND REPLACED LT IB MID-FLAP AND AFT FLAPS ASSY. OPS CHECKED NORMAL IAW MM 27-51. AIRCRAFT WAS RETURNED TO SERVICE. (SW07200506017) (K)Mar 19, 2005 · N1269Y · Boeing 727243SDR DHL2005782559Skin · debondedLT I/B T/E FOREFLAP DISBONDED AT T/E. CUT OUT DISBONDED AREA AT TE APPROX 4 1/2" BY 1 3/4". REMOVED DAMAGED CORE APPROX 4 1/2" BY 1 3/4" AND VACUUM BAGGED FOR MOISTURE REMOVAL FABRICATED REPLACEMENT SKIN APPROX 4 1/2" BY 1 3/4" EXTERNAL DOUBLER APPROX 3 1/2"Mar 18, 2005 · N782DH · Boeing 727227SDR DHL2005782500Skin · debondedLEFT INBOARD T/E FOREFLAP DISBONDED AT /TE. CUT OUT DISBONDED AREA AT T/E APPROX 4.5 X 1.75 INCH, REMOVED DAMAGED CORE APPROX 4.5 X 1.75 INCH AND VACUUM BAGGED FOR MOISTURE REMOVAL. FABRICATED REPLACEMENT SKIN APPROX 4.5 X 1.75 INCH EXTERNAL DOUBLER 3.5 X 7.Mar 18, 2005 · N782DH · Boeing 727227SDR ASAA0540181Wedge · dentedOKC - FOUND LEFT INBOARD TRAILING EDGE FLAP HAS SEVERAL DENTS. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 SRM 51-70-10 PAGE 8. (M)Mar 16, 2005 · N764AS · Boeing 7374Q8SDR ASAA0540179Wedge · dentedOKC - FOUND RIGHT INBOARD TE MID FLAP WEDGE DENTED WITH A CRACK. REMOVED DAMAGE FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW B737 SRM 51-70-10. (M)Mar 16, 2005 · N764AS · Boeing 7374Q8SDR 05FDEA00579Pad · corrodedPITTING AND CORROSION ON AFT MOUNTING PAD ON RT WING FOR NR 6 FLAP TRACK. REMOVED CORROSION IAW SRM 51-10-6 PG 5 FIG 4, FOUND TO BE WITHIN LIMITS ORIGINAL DRWG SPECS IAW DWG 66-14734. TREATED & PRIMED IAW SRM 51-10-2, ORIGINAL MAT THICKNESS .600, REMOVED .00Mar 16, 2005 · N480FE · Boeing 727200SDR 05FDEA00578Skin · damagedREPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. RT WING RT INBOARD TRAILING EDGE FLAP LOWER SURFACE AFT AND INBOARD OF NR 2 TRACK BEAM, ITEM 43 OF LIST. RT WING RT INBOARD TRAILING EDGE FLAP LOWER SUFACE AFT AND I/B OF NR 2 FMar 16, 2005 · N419FE · Airbus A310222SDR 05FDEA00577Wedge · damagedREPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. LT WING REPAIR LOWER SURFACE I/B TRAILING EDGE FLAP FWD OF THE TRAILING EDGE WEDGE AND AFT OF NR 2 FLAP TRACK BEAM, ITEM 57 OF LIST. LT WING I/B FLAP LOWER SURFACE, AND AFT OF NMar 16, 2005 · N419FE · Airbus A310222SDR 05FDEA00532Skin · misrepairedCOMPLY WITH AGING 9 - AGING INSPECTION, LT WING - REPAIR AT LT INBOARD FLAP TRAILING EDGE, UPPER SURFACE (PLEASE EVALUATE). REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX ENGINEERING AUTHMar 15, 2005 · N451FE · Airbus A310222SDR 05FDEA00527Skin · misrepairedCOMPLY WITH AGING 9 - AGING INSPECTION, RT WING - REPAIR AT RT INBOARD FLAP LOWER TRAILING EDGE. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-52-12.Mar 15, 2005 · N451FE · Airbus A310222SDR SWAA050795Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED ON OUTBOARD EDGE LOWER SKIN. REMOVED AND REPLACED FLAP ASSY PER MM.Mar 15, 2005 · N674AA · Boeing 7373A4SDR DHL2005805635Plate · crackedLT INBD FLAP LWR PLATING (2EA) DENTS AND 0.250 CRACK (STA XF 30.000- 40.000) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-28-05 EO NR AST 050209 DATED 02-25-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SKIN SEGMENT IAW Mar 14, 2005 · N805DH · Doug DC873FSDR UIEA200500019Link · gougedDURING D-CHECK, DEEP GOUGE FOUND ON THE EDGE OF THE INBOARD LINK ON THE NR 18 VARIABLE CAMBER FLAP. BLENDED OUT DAMAGE FROM SURFACE OF LINK. NDT INSPECTED TO ENSURE CRACK AND DEFECT CONDITION. SHOP PREENED PER SOPM 20-10-03, INTENSITY .006A2. REFINISHED LIMar 14, 2005 · N527MC · Boeing 7472D7BSDR DHL2005782536Skin · chafedRT IB FOREFLAP LOWER OB END CHAFFED THROUGH REPAIR PATCH. REMOVED FASTENERS AND PREVIOUS REPAIR FOR ACCESS IAW 727 SRM 51-30-2. HFEC INSPECTED AREA WITH NO CRACKS NOTED IAW B727 NDT MAN. PT. 6 51-00-00 FIG 23. FABRICATED REPAIR DOUBLER FROM 2024T3 .071 PO NMar 12, 2005 · N782DH · Boeing 727227SDR DHL2005782531Skin · delaminatedRT IB T/E FLAP IS DELAMINATED ON THE UPPER SURFACE OF THE AFT FLAP INBOARD EDGE CORRECTIVE ACTION: CUT OUT DELAM AREAS 3 APPROX 3 INCH DIAM, 2 INCH DIAM AND 2 INCH BY 4 1/4 AND CUT OUT PUNCTURED SKIN APPROX 2 INCH IAW B727 SRM 51-40-20 FIG 30. FABBED 2 FILLERMar 12, 2005 · N782DH · Boeing 727227SDR DHL2005782569Strip · missingLEFT I/B FORE FLAP WBL 70 UPPER SURFACE HAS CHAFE STRIP MISSING. REMOVED AND INSTALLED LEFT I/B FORE FLAP AFTER SHEET METAL REPAIR IAW B727 MM 27-51-1, OP CHECK GOOD IAW B727 27-51-0. CUT OUT DAMAGE SKIN, FABBED FILLER 3.5 X 2.5 INCH & DOUBLER 5 X 4 INCH FROMar 11, 2005 · N782DH · Boeing 727227SDR DHL2005782532Skin · debondedLT OB AFT FLAP IB UPPER SURFACE WBL 300 HAS DISBOND AT EDGE OF EXISTING REPAIR. FOUND 2 EACH DISBONDED AREA OF LOWER SKIN, ALSO REMOVED PREVIOUS REPAIR FROM LOWER SKIN AND CUTOUT DAMAGED AREA APPROX 48 SQ IN IAW B727 SRM 51-40-20 FIG 31. FABRICATED ON FILLERMar 11, 2005 · N782DH · Boeing 727227SDR DHL2005782526Skin · gougedLT OB FORE FLAP L/E IB AT WBL 314 HAS GOUGES IN REPAIR DOUBLER SURFACE. REMOVED DOUBLER IAW B727 SRM 51-30-2. FABRICATED NEW DOUBLER USING 2024T3 .063 PO# 9001978 DIM. 7 1/2" BY 3 1/2" IAW B727 SRM 57-50-2 FIG 3 AND 57-30-4 FIG 1. ALODINE AND PRIMED PART ANMar 11, 2005 · N782DH · Boeing 727227SDR DHL200578228Skin · gougedLT OB FORE FLAP L/E IB AT WBL 314 HAS 2 GOUGES IN REPAIR DOUBLER SURFACE. REMOVED DOUBLER IAW B727 SRM 51-30-2 FABRICATED NEW DOUBLER USING 2024T3 .063 PO NR 9001978 DIM 7 1/2" BY 3 1/2" IAW B727 SRM 57-50-2 FIG 3 AND 57-30-4 FIG 1. ALODINE AND PRIMED PART AMar 11, 2005 · N782DH · Boeing 727227SDR UPS05244172Fitting · corrodedINSPECTION TYPE:C NR 5 FLAP TRACK FWD SUPPORT FITTING P/N 65-21651 HAS PITTING CORROSION ON HOLE FOR SPECIAL STUD. REPAIR CARRIED OUT IAW AAAE EO 2005-021-003.Mar 10, 2005 · N942UP · Boeing 72722CSDR 05FDEA00484Support · corrodedCOMPLY WITH EA 8-5750-55451, RT OB FLAP FLAP VANE SUPPORT CORROSION REWORK. CLOSING ACTION ON 03/08/05. ON N/R S00013. COMPLIED WITH EA 8-5750-55451.Mar 10, 2005 · N369FE · Doug DC1010SDR 05FDEA00460Vane · wornRIGHT HAND WING, INBOARD FLAP VANE, LEADING EDGE, ABOUT 25 INCHES (FROM OUTBOARD TO INBOARD). FOUND WITH CHAFFING DAMAGE OF 3 INCHES DIAMETER. REMOVED AND REPLACED PER AMM 27-50-22-02. ADJUSTMENT AND TEST CARRIED OUT PER AMM 27-50-22-05.Mar 8, 2005 · N614FE · Doug MD11SDR 05FDEA00443Flap Track · corrodedRT WING FLAP O/B UPPER SURFACE AT NR 3 FLAP TRACK AND NR 4 FLAP TRACK HAS 2 EA AREAS OF NOTED CORROSION REF N00771. REMOVED CORR IAW SRM 51-74-10, FOUND IN LIMITS IAW SRM 57-53-12.Mar 8, 2005 · N446FE · Airbus A310SDR 05FDEA00442Skin · puncturedRT WING I/B FLAP UPPER SURFACE 3.9 IN FROM T/E AND 30 IN FROM I/B END SKIN PUNCTURED REF N00914. REPAIRED FLAP IAW SRM 57-52-12 FIG 4D.Mar 8, 2005 · N446FE · Airbus A310SDR ASAA0580172Vane · wornHV-CHECK - LT IB FLAP IB VANE IS WORN AT LEADING EDGE. INSTALLED REPAIR DOUBLER. (K)Mar 7, 2005 · N965AS · Doug DC983
Back to JASC 5753