JASC 5710

Service difficulty reports · 4,462

Reports filed under 5710 · Wing Main, Frame Structure, newest first.

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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 = '5710'
  ORDER BY difficulty_date DESC"

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SDR 08FDEA03978Fitting · damagedFOUND DAMAGED HOLES DURING ACCOMPLISHMENT OF SB A300-57-6086 (HOLE G,T) ON HORIZONTAL FLANGE, C47, RT. REPAIR PERFORMED BY OVERSIZING THE HOLES, NDT FOR DAMAGE FREE CONDITION AND INSTALLING A CONICAL WASHER IN HOLE T IAW RAS/70512903/024/2008 ISS A, APPROVESep 22, 2008 · N744FD · Airbus A300B4622RSDR 08FDEA03977Fitting · damagedFOUND DAMAGED HOLES DURING ACCOMPLISHMENT OF SB A300-57-6086 (HOLE E, F, P) ON HORIZONTAL FLANGE, C 47, LT. REPAIR PERFORMED BY OVERSIZING THE HOLES AND NDT FOR DAMAGE FREE CONDITION IAW RAS/70512903/024/2008 ISS A, APPROVED BY EA 6-5710-123133.Sep 22, 2008 · N744FD · Airbus A300B4622RSDR 08FDEA03976Fitting · damagedFOUND DAMAGED HOLES DURING ACCOMPLISHMENT OF SB A300-57-6049 (HOLE I, L, N, U) ON VERTICAL FLANGE, C 47, RHS. REPAIR PERFORMED BY OVERSIZING THE HOLES, EXTERNAL FITTING CUT OUT AT HOLE I AND NDT FOR DAMAGE FREE CONDITION IAW RAS/70512903/024/2008 ISS A, APPROSep 22, 2008 · N744FD · Airbus A300B4622RSDR 08FDEA03975Fitting · damagedFOUND DAMAGED HOLES DURING ACCOMPLISHMENT OF SB A300-57-6049 (HOLE N, Y, U) ON VERTICAL FLANGE, C 47, LHS. REPAIR PERFORMED BY OVERSIZING THE HOLES OF EXTERNAL FITTING AND INSTALL A CONICAL WASHER AT HOLE U IAW RAS/70512903/024/2008 ISS A, APPROVED BY EA 6-57Sep 22, 2008 · N744FD · Airbus A300B4622RSDR 08FDEA03821Beam · crackedRT WING T/E "J " BEAM IS CRACKED AT WBL 118 REMOVED T/E PANEL FOR ACCESS IAW SRM 51-30-2. REMOVED "J" BEAM AS REQUIRED BY SRM 51-30-2. FABRICATED NEW "J" BEAM IAW DRAWIING NR 65-21655-10 REV "J". TREATED AND PRIMED AFFECTED PARTS IAW SRM 51-10- 2. INSTALLESep 11, 2008 · N492FE · Boeing 727227SDR 08FDEA03732Skin · crackedA CRACK IS PROPAGATING FROM UNDER THE REPAIR DOUBLER AT THE RIGHT WING L/E SLAT DRIVE MECHANISM INBD CORNER. WORK WAS ACCOMPLISHED ON NON-ROUTINE N00802.Sep 5, 2008 · N550FE · Doug MD1010FSDR 08FDEA03714Angle · wornLT WING LOWER T/E PANEL MATING SURFACE IS WORN OUT BY THE OUTBOARD FLAP; INBOARD HINGE FITTING. REMOVED ANGLE & ATTACH ANGLE IAW SRM 51-31-01 VOL II. FABRICATED A NEW ANGLE IAW DWG ARG 0744; REV "J ". ALODINED IAW SRM 51-21-01 VOL II. PRIMED IAW SRM 51-21Sep 3, 2008 · N550FE · Doug MD1010FSDR 08FDEA03711Cap · wornLEFT WING LOWER T/E STRUCTURE IS WORN APPROXIMATELY 48" INBD OF THE OUTBD AILERON ACTUATOR. UPON FURTHER INVESTIGATIONDAC DWG ARC 0824; REV "H" ALLOWS THE TRIMMING OF THE FLANGE IN THE WORN ARE. TRIMMED AREA FLANGE IAW DWG ARC 0724; REV "H"; E.O. SHEESep 2, 2008 · N550FE · Doug MD1010FSDR UPS08653110Beam · crackedINSPECTION TYPE:C LT WING LES 674 'D' NOSE SUPPORT WEB LOWER FLANGE FOUND CRACKED. CRACK LENGTH 1.125 INCH. LT WING LES 674 'D' NOSE SUPPORT WEB LOWER FLANGE REPAIRED AS PER SRM 57-41-13-2R REPAIR 3 FIG 201.Aug 8, 2008 · N334UP · Boeing 76734AFSDR 08FDEA03314Support Beam · crackedLT WING TRAILING EDGE SUPPORT BEAM CUT OUT ON SPOILER NR 7 IS CRACKED AT WBL 122 REMOVED "J" BEAM IAW B727 SRM 51-30-2. FABRICATED NEW "J" BEAM FROM BAC 1506 860 7075 T6 (DIM 81 INCHES IN LENGTH) AND TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED "J" BEAAug 8, 2008 · N275FE · Boeing 727233SDR 08FDEA03313Support Beam · crackedRT WING TRAILING EDGE SUPPORT BEAM CUT OUT ON SPOILER NR 8 IS CRACKED AT WBL 123 REMOVED "J" BEAM IAW B727 SRM 51-30-2 AND FABRICATED NEW "J" BEAM FROM BAC1506-860 7075-T6. APPROX DIM 81 INCHES IN LENGTH IAW B727 SRM 51-30-5 AND SRM 57-20-2 FIG 2. TREATED ANAug 8, 2008 · N275FE · Boeing 727233SDR UPS08M53096Structure · crackedINSPECTION TYPE:2C LT WING FIXED L/E TELESCOPIC DOOR CUTOUT FOUND CRACKED ON ONE SIDE. REMOVED CRACK, FABRICATED, AND INSTALLED FILLER AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 43, 51-21-01, 51-35-01, 51-33-01.Aug 5, 2008 · N281UP · Doug MD11FSDR 08FDEA02308Panel · damagedCENTER WING TANK LT BOOST PUMP AREA HAS 4 FASTENERS DAMAGED AT REINFORCEMENT BETWEEN FR 46 AND FR 47 REPAIRED DAMAGED FASTENER HOLES AT CENTER TANK LT BOOST PUMP INNER REINFORCEMENT PANEL BETWEEN FR 46 AND FR 47 IAW FEDEX EA 6-5710-121292, RELEASE DATE 6 JUNJun 18, 2008 · N443FE · Airbus A310203SDR VNAA0806008Structure · damagedCREW REPORTED A LIGHTNING STRIKE. MAINTENANCE COMPLIED WITH AN EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE LT AND RT WINGTIPS. MAINTENANCE REPAIRED THE DAMAGE UNDER REO 601R-57-30-001 AND THE STRUCTURAL REPAIR MANUALJun 13, 2008 · N226JS · Cndair CL6002B19SDR UPS08M52641Structure · crackedINSPECTION TYPE-C, RT WING ANTI-ICE TELESCOPIC DUCT, L/E CUT OUT AREA SUSPECT CRACK AT IB AND OB SIDE AS MARKED. HFEC INSP CARRIED OUT IAW DAC NDT SPM R.13,06-10-01.001 & FOUND CRACK AS MARKED. FASTENERS AT CRACKED AREA REMOVED IAW SRM57-31-01V.2 & SRM 57-33-Jun 13, 2008 · N271UP · Doug MD11FSDR 08FDEA02230Cap · crackedLOWER BULKHEAD CAP LUG IS CRACKED FWD SIDE. REPAIRED AREA IAW SRM 57-20-00 FIG 27 SHEET 2-3-4 VOL I.Jun 12, 2008 · N40061 · Doug DC1010SDR 08FDEA02229Cap · crackedTHE LOWER BULKHEAD CAP IS CRACKED IN 3 PLACES. LOWER LUG AT STR NR 43 FWD AND AFT, STR NR 44 AFT RT WING. REPAIRED AREA IAW SRM 57-20-00 FIG 27 SHT 3 VOL I.Jun 12, 2008 · N40061 · Doug DC1010SDR 08FDEA02149Rub Strip · failedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING OUTBD FLAP MAIN SKIN UNDER RUB STRIP BETWEEN RIB NR 2 AND RIB NR 3, 4.4 IN FWD OF REAR SPAR MEASURING 13 IN BY 11.8 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT OUTER SJun 4, 2008 · N443FE · Airbus A310203SDR 08FDEA02060Beam · crackedRT WING UPPER TRAILING EDGE "J " BEAM IS CRACKED AT WBL 118, WS 155 - WS 160 REMOVED NR 8 SPOILER FITTING FOR ACCESS IAW B727 SRM 51-30-2. TRIMMED OUT CRACK (DIMENSION 0.280 INCH IN LENGTH ) IAW B727 SRM 51-10-1 AND FEDEX DRAWING SR 27-57-025 REV A. TREATED May 30, 2008 · N490FE · Boeing 727227SDR IPXA09M55955Winglet · damagedRT UPPER WINGLET ASSY HAS 3 DAMAGED AREAS ALONG T/E. REPAIRED PER EO C-5720-33537-A.May 19, 2008 · N296UP · Doug MD11FSDR HALA0800594Structure · crackedLT WING HAS CRACKED STRUCTURE ON FIXED L/E ABOVE FUELING PANEL. REPAIRED PER SRM 57-41-13 FIG 201 REPAIR 3.May 8, 2008 · N590HA · Boeing 7673CBSDR UPS08452200Wing · damagedLT WING DAMAGE ON CONTACT WITH POLE ON TAXI IN.May 8, 2008 · N520UP · Boeing 747212BSDR A6WA200840384Piccolo Tube · dentedRT WING INTERNAL OUTBOARD LEADING EDGE AT W/S 252, PICCOLLO TUBE DENTED (.300 X .200 X .040 DEEP). PICCOLLO TUBE REPLACED IAW AMM TASK 30-11-41-400-801. (A)May 6, 2008 · N437AW · Cndair CL6002B19SDR 08FDEA01759Fairing · chafedRIGHT WING INBD FLAP TRACK FAIRING NR 641 DL AFT EDGE IS CHAFED. BLENDED AREA; PERFORMED D.P.I. AODINED & PRIMED IN REF TO FEDEX E.A. 8-5720-116982" REMOVED & INSTALLED FAIRING IN REF TO SRM 51-31-01; VOL II.May 5, 2008 · N567FE · Doug MD1010FSDR 08FDEA01556Structure · corrodedCORROSION AND LIGHTNING STRIKE FOUND ON RT WING TIP. REPAIR PERFORMED BY BLEND OUT AREA IAW RAS/FOK/037/2008 ISS A, APPROVED BY EA 6-5730-115275.Apr 25, 2008 · N745FD · Airbus A300B4622RSDR 08FDEA01555Structure · corrodedCORROSION AND LIGHTNING STRIKE FOUND ON LT WING TIP (4 AREAS) REPAIR PERFORMED BY CUT OUT DAMAGED AREA 1 AND 4 AND INSTALLING AN EXTERNAL PATCH WITH SHIM, BLEND OUT AREA 2 AND 3 AND INSTALLING EXTERNAL PATCH UNDER STATIC DISCHARGER , APPROVED BY RAS/FOK/037/Apr 25, 2008 · N745FD · Airbus A300B4622RSDR HALA0800535Structure · damagedLIGHTNING STRIKE DAMAGE, RIGHT WING TIP TRAIL EDGE. REMOVED RT WING TIP. INSTALLED WING TIP ASSY PER AMM 57-30-01. SECURITY CK AND OPS CK OK.Apr 17, 2008 · N486HA · Boeing 717200SDR IXXA08SMN151SStructure · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT XRS 74 EXTERNAL DOUBLER LEFT WHEEL WELL AFT OF MAIN LANDING GEAR TRUNNION. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED EXTERNAL DOUBLERApr 15, 2008 · N821BX · Doug DC871FSDR 2008UALA02177Structure · damagedBIRD STRIKE LEFT WING. DAMAGE TO THE LEFT HAND WING OUTBOARD FIXED FLAP FAIRING ACCOMPLISHED.Apr 15, 2008 · N202UA · Boeing 737322SDR A6WA200840607Fairing · crackedLOG 196188/1 REQUEST INSPECTION OF LT WINGLET TRAILING EDGE FOR CRACK. REMOVED LT WINGLET T/E ASSY PER AMM 57-30092 REF LOG PAGE 196188/4 FOR INSTALLATION. INSTALLED NEW LT WINGLET T/E FAIRING ASSY PER AMM 57-30-02.Apr 14, 2008 · N446AW · Cndair CL6002B19SDR 2008UALA02164Structure · crackedCRACK INDICATION UNDER FLAKING TEFLON PAINT ON UPPER SURFACE OF THE RT WING FIXED LEADING EDGE BELOW NR 10 SLAT. REMOVED DAMAGED AREA APPLIED A PRE-PREG FIBERGLASS REPAIR IAW SRM 57-41-01 AND 51-70-07Apr 14, 2008 · N536UA · Boeing 757222SDR UIEA200800123Beam · crackedRIGHT WING LEADING EDGE CAVITY INBOARD OF NR 4 PYLON AT ABOUT WBL 830 FOUND WEB OF D-BEAM CRACKED. DAMAGED WEB REPLACED IAW SRM 57-20-03.Apr 4, 2008 · N517MC · Boeing 747243BSDR HALA0800531Structure · crackedCRACK ON RT WING CAVITY AT WS 671, CRACK IN L/E STRUCTUE. REPLACED L/E STRUCTURE.Apr 2, 2008 · N587HA · Boeing 76733ASDR 08FDEA00917Tee Fitting · crackedRT WING INT ZONE L/E FOUND CRACK ON FIXED TEE CAP. REPAIRED TEE CAP IAW SRM 57-10-00 VOL I FIG 49.Mar 13, 2008 · N307FE · Doug DC1030FSDR 08FDEA00918Tee Fitting · crackedRT WING L/E INT ZONE FOUND CRACK ON FIXED TEE CAP. REPAIRED TEE CAP IAW SRM 57-10-00 VOL I FIG 49.Mar 13, 2008 · N307FE · Doug DC1030FSDR 08FDEA00799Skin · crackedRING WING, LEADING EDGE TELESCOPIC DUCT CUTOUT DOOR OUTBOARD CORNER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 43 VOLUME I AND EA 1-5710-115329. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Mar 9, 2008 · N521FE · Doug MD11FSDR A6WA200840174Structure · damagedWINDSHEAR DURING LANDING LEFT WING PUSHED UP AND RIGHT WINGSTRIP SCRAPED RUNWAY. (M)Mar 8, 2008 · N462AW · Cndair CL6002B19SDR 08FDEA00644Skin · crackedHFEC OPEN HOLE INSPECTION CARRIED OUT AND FOUND 10 HOLES WITH CRACK INDICATION AT RIGHT WING ACCESS DOOR 636AB CUT OUT. (BETWEEN STATION XORS 683.4 AND XORS 713.6). REPAIR CARRIED OUT AS PER EA 1-5710-109926, PART 1 REPAIR CLASSIFIED AS MAJOR AS PER PER Feb 28, 2008 · N604FE · Doug MD11FSDR 08FDEA00520Frame · crackedLEFT WING OUTBOARD T/E NR 1 TRACK CENTER FAIRING INTERNAL AFT FORMER FRAME IS CRACKED IN CENTER. REMOVED AFT FORMER FRAME, LOCATED AND DRILLED NEW AFT FORMER FRAME AND INSTALLED REF SRM 51-30-2 PG 1, THIS IS CLASSIFIED AS A MINOR REPAIR.Feb 20, 2008 · N486FE · Boeing 727227SDR DHL2008765022Beam · damagedDURING C CHECK, REJECTED NR 105146 BECAUSE ORIGINAL FABRICATED 'J' BEAM WAS DAMAGED UPON INSTALLATION. RT WING TRAILING EDGE UPPER 'J' BEAM IS CRACKED AT WBL 118. REMOVED TRAILING EDGE PANEL FOR ACCESS AT RT WING IAW SRM 51-30-2. REMOVED 'J' BEAM AT RT SIDEJan 27, 2008 · N765AT · Boeing 727264SDR DHL2008765016Beam · crackedDURING C CHECK, LT WING UPPER TRAILING EDGE PANEL SUPPORT 'J' BEAM WBL 124 IS CRACKED IN CUT OUT FORWARD OF NR 7 SPOILER ACTUATOR. REMOVED TRAILING EDGE UPPER PANEL FROM LT WING FOR ACCESS IAW SRM 51-30-2. REMOVED CRACKED 'J' BEAM IAW SRM 51-30-2. FABRICATEJan 25, 2008 · N765AT · Boeing 727264SDR 08FDEA00187Skin · wornRT WING LWR SIDE EXT ZONE FOUND DEEP WEAR ON SKIN. REPAIRED AREA IAW SRM 57-10-00 FIG 36 AND 39 VOL I.Jan 17, 2008 · N306FE · Doug DC1030FSDR UPS08M52011Structure · damagedINSPECTION TYPE:C LT WING OUTBOARD FIXED L/E AT NR 8 SLAT 13 INCHES LONG GROOVE WORN FROM CONTACT WITH SEAL RETAINER, OUT OF LIMITS. GROOVE MARK REWORKED PER SRM 51-21-01V.2R35 ORIG THK:0.040", MAT`L REMVD :0.007", MATL REM:0.033" FOUND EXCEED LIMIT PER SRM 5Jan 15, 2008 · N294UP · Doug MD11SDR 08FDEA00004Support Beam · crackedRT WING INBD UPPER WING PANEL SUPPORT BEAM IS CRACKED JUST FWD OF MLG BEAM 10" O/B OF UPLOCK T/T. REMOVED SUPPORT BEAM FROM A/C REF SRM 51-30-2. STOP DRILLED CRACK REF SRM 51-10-1. FABRICATED AND INSTALLED REPAIR ON SUPPORT REF SRM 51-40-2. REINSTALLED SUPJan 2, 2008 · N268FE · Boeing 727233SDR 07FDEA05011Structure · crackedLEFT WING LEADING EDGE AT STA XOS 774 CAVITY EDGE FOUND CRACKED. REPAIRED AS PER SRM 57-10 -00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Dec 7, 2007 · N524FE · Doug MD11FSDR QXEA200801943Structure · corrodedPDX - C5 CHECK - RIGHT WING INBOARD LEADING EDGE UPPER FLANGE HAS MILD FRETTING CORROSION AROUND SCREW HOLES APPROXIMATELY STATION YW48. REPAIRED IAW RD8-57-1513 AND DASH 8 200 SRM 51-20-36.Dec 4, 2007 · N347PH · Dhav DHC8202SDR DHL2007801540Spar Cap · crackedLT LWR WING FRONT SPAR CAP CRACKED 1.250" APPROXIMATELY AT STA XFS 520.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 11-20-07, BOEING MSG NR 1-653039342-4 DATED 10-22-07, BOEING SKETCH JO060232, JCT04316, EVA D857-00022 REV IR DATED 10-Nov 21, 2007 · N801DH · Doug DC873FSDR IXXA07SMN269SStructure · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING. NUMBER 4 STUB WING LEADING EDGE LOWER PART DOUBLER HAS A CRACK AT STATION XFS 529.000. REMOVED FASTENERS AS NEEDED TP PERFORM REPAIR. REMOVED CRACKED DOUBLER. FABRICATED EXTERNAL, INTERNAL REPAIR DOUBLER.Nov 16, 2007 · N604BX · Doug DC873FSDR SWIA200718828Structure · damagedRIGHT WINGLET UPPER LEADING EDGE IS DAMAGED FROM BIRD STRIKE. INSTALLED NEW UPPER WINGLET LEADING EDGE IAW SRM 51-42-06. Oct 25, 2007 · N455SW · Cndair CL6002B19SDR VNAA0710015Structure · damagedWHILE BEING MARSHALED ON TO GATE E19 DURING TAXI, THE LEFT WING STRUCK A STATIONARY TUG. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE LEADING EDGE OF THE LEFT WING. AIRCRAFT WAS FERRIED TO AIR CENTER FOR REPAIR. MAINTENANCE REMOVED AND REPLACED THE LT OUTBOct 14, 2007 · N220PS · Cndair CL6002B19
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