JASC 5730

Service difficulty reports · 27,269

Reports filed under 5730 · Wing, Plate/Skin, 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 = '5730'
  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 07FDEA03521Skin Panel · wornELONGATED HOLES AT PYLON SUPPORT BRACKET AND BOTTOM SKIN OF LT WING. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLING BUSHES IAW EA 6-5720-95870 AND RAS/BAE/1002289/2006 ISSUE A.Sep 11, 2007 · N728FD · Airbus A300B4622RSDR 07FDEA03504Skin · damagedRT WING LWR SURFACE OUTBD FLAP FOUND 30 EA LOOSE RIVETS ON SKIN. REPAIRED AREA IAW SRM 57-20-00 VOL I FIG 11.Sep 10, 2007 · N68052 · Doug DC1010FSDR 07FDEA03498Skin Panel · chafedFOUND TWO CHAFE MARKS AND ONE IMPACT DAMAGE ON FIXED L/E 'D' NOSE SKIN BETWEEN TRACK 3-4 RT WING. REPAIR PERFORMED BY BLEND OUT OF CHAFING MARKS AND DRILLING 1/4INCH DIA HOLE WITH CSK AND INSTALLING A SOLID ALUMINUM RIVET IAW TD/J1/S1/02044/2005 ISSUE B, APPRSep 10, 2007 · N728FD · Airbus A300B4622RSDR 07FDEA03483Skin Panel · corrodedFOUND ON WING BOTTOM SKIN LT, RIB 8 AN OLD CORROSION REPAIR AROUND HOLE 585 (DRAWING R571-401410 ) WITHOUT ANY DOCUMENTATION. REPAIR PERFORMED BY REWORK OF AREA AND FASTENER REPLACEMENT IAW EA 6-5720-106534 AND RAS/BAE/1005114/2007 ISS A.Sep 10, 2007 · N749FD · Airbus A300B4622RSDR 07FDEA03480Skin Panel · wornFOUND ELONGATED HOLES ON BOTTOM SKIN LT OUTER WING RIB 8 REPAIR PERFORMED IAW R571-50532 (REAM UP AND BUSHING INSTALLATION), APPROVED BY EA 6-5720-106531 AND RAS/BAE/1005033/2007 ISS A.Sep 10, 2007 · N749FD · Airbus A300B4622RSDR 07FDEA03473Panel · delaminatedFOUND ON OUTBOARD T/E PANEL, LHS, DELAMINATION REPAIR PERFORMED BY REMOVING THE DELAMINATION AND INSTALLING NEW PLIES IAW EA 6-5751-95858 AND RAS /BAE/1002007/2005 ISS A.Sep 10, 2007 · N728FD · Airbus A300B4622RSDR DLM88071225Skin · crackedFOUND CRACK ON WING FIXED L/E AT STA XRS 214, REPAIRED.Sep 8, 2007 · N951DL · Doug MD88SDR F3LA200700229Access Panel · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FUEL PANEL 640JB ATTACHMENT HOLES. REMOVED AND REPLACED FUEL PANEL 640JB ON RT WING IAW AMM 57-27-11-400-002. PERFORMED LEAK CHECK IAW 57-27-11-400-002, NO LEAKS FOUND.Sep 8, 2007 · N909FR · Airbus A319112SDR 2007UALA03621Skin · damagedLEFT WING CUTOUT FOR FUEL TANK PNL 540KB HAS 2 EA FASTENER HOLES FOR ATTACHMENT OF THE NUT PLATE CHANNEL TO THE WING SKIN ELONGATED BEYOND LIMITS. COLD WORKED FASTENER HOLES AND INSTALLED NEW REPAIR BUSHINGS.Sep 8, 2007 · N842UA · Airbus A319131SDR MWEA070208Skin · corrodedCENTER WING SKIN AND STRINGER HAS CORROSION, 17 XCW, INDICATOR NOTED AT LOWER AFT 9 FOOT SKIN PANEL 53 INCHES FROM CENTER FASTENERS ROW 3. REMOVED CORROSION, FABRICATED AND INSTALLED FASTENERS.Sep 8, 2007 · N803ME · Doug DC981SDR MWEA070207Skin · corrodedCORROSION AT WING CENTER SECTION REAR SPAR LOWER SKIN AT APPROXIMATELY XCW = 50.000 RIGHT SIDE. REMOVED CORROSION, FABRICATED AND INSTALLED FASTENERS.Sep 7, 2007 · N803ME · Doug DC981SDR 07FDEA03463Skin Panel · corrodedHEAVY CORROSION FOUND ON CENTER WING BOX TOP SKIN AT TR5 AND TR6 RT/LT, FRAME 43-46.2. REPAIR PERFORMED IAW SRM 57-10-12/FIG 201 AND RAS/042817/015/2006 ISSUE A, EXCEPT FOR DAMAGES AT FRAME 44, BEAM 5 AND 6 LT AND RT, WHICH WAS REPAIRED BY DOUBLER IAW RAS/042Sep 7, 2007 · N808FD · Airbus A310324SDR 07FDEA03453Skin Panel · corrodedFOUND CORROSION ON LT WING TOP SKIN T/E AREA AT WORX439.75. REPAIR PERFORMED BY BLEND OUT THE CORROSION AND INSTALLING OVERSIZED FASTENERS IAW EA 6-5720-95931 AND RAS/BAE/1002360/2006 ISSUE A.Sep 7, 2007 · N808FD · Airbus A310324SDR 07FDEA03439Panel · mispinnedFOUND WRONG INSTALLED FASTENERS AT CENTER WING BOX, FRAME 40-47. REPAIR PERFORMED BY INSTALLING NEW OVERSIZED BULL NOSE FASTENERS IAW EA 6-5710- 95919 AND RAS/042817/015/2006 ISSUE A.Sep 7, 2007 · N808FD · Airbus A310324SDR 07FDEA03432Panel · delaminatedDELAMINATION FOUND ON OUTER SHROUD BOX ON RT WING, LOWER SKIN NEAR RIB 31 AND CORROSION OF ALUMINIUM EXTRUSION ON RT WING OUTER TRAILING EDGE PANEL. REPAIR PERFORMED BY REMOVING AND REPLACING ALL DAMAGED LAYERS WITH WET LAY UP. REPLACING THE ALUMINUM T/E SECTSep 7, 2007 · N808FD · Airbus A310324SDR C2XA07SH062Panel · corrodedSHV - DURING C-CHECK MAINTENANCE FOUND PNL 193 BONDING STRIPS WITH CORROSION. MAINTENANCE REPAIRED PNL 193 BONDING STRIPS IAW EC 5750-01315 REV D. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Sep 6, 2007 · N14942 · Emb EMB145EPSDR 07FDEA03410Skin Panel · wornELONGATED HOLES CAUSED BY CHAFING OF HYDRAULIC LINES IN WING PYLON AFT SUPPORT BRACKET AND BOTTOM SKIN, RIB 8. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLING ECCENTRIC BUSHES IAW R572- 49184 ISSUE C, APPROVED B EA 6-5720-95912 AND RAS/BAE/1002263/2006 ISSep 6, 2007 · N808FD · Airbus A310324SDR 07FDEA03409Skin Panel · wornELONGATED HOLES CAUSED BY CHAFING OF HYDRAULIC LINES IN WING PYLON AFT SUPPORT BRACKET AND BOTTOM SKIN, RIB 8. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLING ECCENTRIC BUSHES IAW R572- 49184 ISSUE C, APPROVED B EA 6-5720-95912 AND RAS/BAE/1002263/2006 ISSep 6, 2007 · N808FD · Airbus A310324SDR 07FDEA03408Skin · crackedRT WING LWR SURFACE FOUND CRACK ON SKIN. REPAIRED CRACK IAW SRM 57-10-00 FIG 68 SHT 1 VOL I.Sep 6, 2007 · N371FE · Doug DC1010SDR 07FDEA03398Skin · chafedCHAFING MARK (18 BY 17 MM) FOUND AT WING L/E SKIN RT BETWEEN TRACK 3 AND WOFX-48.9. REPAIR PERFORMED BY BLEND OUT TO SMOOTH PROFILE IAW EA 6-5741-112506 AND RAS/BAE/1005353/2007 ISSUE A.Sep 6, 2007 · N733FD · Airbus A300B4605RSDR EPUA092007ASkin · crackedDURING ROUTINE INSPECTION, DISCOVERED 4" CRACK ON UPPER RT AFT WING SKIN 18" FROM WING ROOT AT WS 53.00. DAMAGE WAS REPAIRED IAW CESNNA MM 51-75-00. AIRCRAFT WAS RETURNED TO SERVICE.Sep 5, 2007 · N407GV · Cessna 208BSDR 07FDEA03381Skin Panel · damagedFOUND ON CENTER WING BOX UPPER PANEL, UPPER SURFACE A NOTCH AT FRAME 47, BETWEEN TRACK 3-4 RT. REPAIR PERFORMED BY BLEND OUT DAMAGE IAW EA 6-5710-95852 AND RAS/AS/0003/2006 ISSUE A.Sep 5, 2007 · N727FD · Airbus A300B4622RSDR 07FDEA03359Skin Panel · wornELONGATED HOLES IN LT PYLON SUPPORT BRACKET AND BOTTOM WING SKIN, RIB 8. REPAIR PERFORMED BY REAM UP THE HOLES AND INSTALLING BUSHES IAW DRW, R571- 50532, APPROVED BY EA 6-5720-95853 AND RAS/BAE/1002114/2006 ISSUE A.Sep 5, 2007 · N727FD · Airbus A300B4622RSDR 07FDEA03343Skin Panel · chafedFOUND CHAFING MARK ON INTERNAL SURFACE OF RT WING TOP SKIN PANEL NR 3 BETWEEN RIB 27-28 NEAR FRONT SPAR. REPAIR PERFORMED BY BLEND OUT, HFEC INSPECTION FOR CRACK FREE AND FLAP PEENING IAW EA 6-5720-95843 AND RAS/BAE/1001878/2005 ISSUE A.Sep 4, 2007 · N727FD · Airbus A300B4622RSDR 07FDEA03342Skin Panel · corrodedFOUND CORROSION ON TOP SKIN PANEL NR 3 LT, NEAR RIB 25-28 AT T/E, OUT OF SRM LIMIT. REPAIR PERFORMED BY BLEND OUT, REPLACEMENT OF AFFECTED FASTENERS AND FLAP PEENING IAW EA 6-5720-92224 AND RAS/BAE/1001906/2005 ISSUE A.Sep 4, 2007 · N727FD · Airbus A300B4622RSDR 07FDEA03330Skin · crackedRT WING UPPER SURFACE FOUND 1 CRACK REPAIR SKIN IAW SRM 57-10-00 VOL1 FIG 68 SHT 1, 2.Sep 3, 2007 · N371FE · Doug DC1010SDR UPS07M50968Access Panel · crackedINSPECTION TYPE:C LEFT WING ACCESS PANEL 536AB CUTOUT AREA FOUND CRACK INDICATION DURING NDT INSPECTION. HOLES REAMED FOR LEFT WING ACCESS PANEL 536AB CUTOUT AREA AS PER EN1639-07. HFEC OPEN HOLE INSPEC C/OUT ON REWORKED HOLE FOUND NO CRACK. BUSHINGS 17EA FSep 2, 2007 · N290UP · Doug MD11FSDR P3MB0709001Skin · dentedDURING POST FLIGHT INSPECTION, FOUND BIRD STRIKE DAMAGE ON LT WING LEADING EDGE, DAMAGE WAS A DENT APROX 8 INCHES LONG, 4 INCHES WIDE AND 1 INCH DEEP, WITH A TEAR IN THE FORM OF A "T" 5 INCHES VERTICAL BY 4 INCHES HORIZONTAL, SECTION OF LEADING EDGE WAS REMOVESep 1, 2007 · N305PA · Doug DC915SDR 2007FA0000794Skin · damagedBIRD STRIKE ON LT LEADING EDGE, CAUSING DEEP DENT AMD A TEAR 5 INCHES VERTICAL AND 4 INCHES HORIZONTAL, FOUND ON POST FLIGHT INSPECTION. REPAIRED IAW SRM CHAPTER 57-06.Sep 1, 2007 · N305PA · Doug DC915SDR CO1Y200700003Skin · corrodedLT WING UPPER SURFACE ON SKIN FROM XORS 130 TO XORS 738 FOUND EXFOLIATION CORROSION.Sep 1, 2007 · N702BC · Doug MD11SDR CO1Y200700004Skin · corrodedRT WING UPPER SURFACE FROM XORS 345 TO XORS 828 FOUND 15EA EXFOLIATION CORROSION POINTS.Sep 1, 2007 · N702BC · Doug MD11SDR 07FDEA03288Skin Panel · failedOLD REPAIR DOUBLER PLATES ON BOTTOM WING SKIN PANEL NR 1 BOTH RHS AND LHS, BETWEEN RIB 8 AND TRACK 4 FWD OF FRONT SPAR ARE NOT PERFORMED IAW DRW R572- 40179/PG 9 (SB A300-57-6019). IN ADDITION THE INSTALLED HI-LOCKS ARE IN BAD CONDITION. REPAIR RENEWED BY IAug 31, 2007 · N725FD · Airbus A300B4622RSDR 07FDEA03286Skin Panel · wornELONGATED HOLES ON PYLON NR 1 SUPPORT BRACKET AND LOWER WING SKIN, RIB 7-8 LT. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF FREEZE PLUGS IAW EA 6-2900-106507 AND RAS/BAE/1005210/2007 ISSUE A.Aug 31, 2007 · N732FD · Airbus A300B4605RSDR 07FDEA03285Skin Panel · wornELONGATED HOLES ON PYLON NR 2 SUPPORT BRACKET AND LOWER WING SKIN, RIB 7-8 RT. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF FREEZE PLUGS IAW EA 6-2900-106507 AND RAS/BAE/1005210/2007 ISSUE A.Aug 31, 2007 · N732FD · Airbus A300B4605RSDR 07FDEA03284Skin Panel · wornELONGATED HOLES ON PYLON NR 2 SUPPORT BRACKET AND LOWER WING SKIN, RIB 7-8 RT. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF FREEZE PLUGS IAW EA 6-2900-106507 AND RAS/BAE/1005210/2007 ISSUE A.Aug 31, 2007 · N732FD · Airbus A300B4605RSDR 07FDEA03261Skin Panel · damagedFOUND THE HYDRAULIC FITTING HOLES IN PYLON SUPPORT BRACKET IN LOWER SKIN PANEL OF THE RT WING ELONGATED. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF REPAIR BUSHES IAW R571-50532 ISSUE: A APPROVED BY EA 6-5720-99183 AND RAS/BAE/1002415/2006 ISSUE:Aug 31, 2007 · N725FD · Airbus A300B4622RSDR CA070911009Skin · corroded(CAN) DE-ICE BOOT REPLACEMENT AT MFG. AFTER REMOVAL OF DE-ICE BOOT NOTED AREA OF FUEL STAINING, CORROSION NOTED. DISCONTINUED BOOT REPLACEMENT, OBTAINED FERRY PERMIT AND RELOCATED AIRCRAFT. FURTHER INVESTIGATION SHOWS: SEVERAL LOCATIONS OF CORROSION DAMAGE WEAug 30, 2007 · Cessna 550SDR AWXA200701050Skin · delaminatedPIT - MAJOR REPAIR, TEAR AND DELAMINATION ON RIGHT WING LEADING EDGE SKIN, WS 538. REPAIRED RIGHT WING LEADING EDGE SKIN, WS 538 PER US AIRWAYS EA (ENGINEERING AUTHORIZATION).Aug 30, 2007 · N158AW · Boeing 7373G7SDR 07FDEA03248Skin · chafedCHAFING MARK IN SKIN OF LEADING EDGE RT WING, BETWEEN TRACK 3 AND 4. REPAIR PERFORMED BY REPLACEMENT OF SKIN PANEL IAW SRM 51-72-10 (SRM 57-41-12/ FIG 6/ITEM 5).Aug 30, 2007 · N725FD · Airbus A300B4622RSDR 07FDEA03237Skin · damagedAFTER LEFT WING UPPER FUELTANK PANEL NR 531AT CUTOUT RUBSTRIP REMOVED. FOUND SKIN CUTOUT WITH 02 EACH DOUBLE HOLES. 09-11-07 COMPLIED WITH FEDEX E.A. 1-5710-115177, CLASSIFIED AS A MINOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 30, 2007 · N585FE · Doug MD11FSDR 07FDEA03236Skin Panel · damagedFOUND THE HYDRAULIC FITTING HOLES IN PYLON SUPPORT BRACKET IN LOWER SKIN PANEL OF THE LT AND RT WING ELONGATED. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF REPAIR BUSHES IAW R571-50532 ISSUE: A APPROVED BY EA 6-5720-99183 AND RAS/BAE/1002415/2006Aug 30, 2007 · N725FD · Airbus A300B4622RSDR 07FDEA03230Skin · crackedRT WING LWR SURFACE FOUND 1 CRACK 2" LONG ON SKIN. REPAIRED CRACK IAW SRM 57-10-00 FIG 68 SHT 1 VOL 1.Aug 29, 2007 · N371FE · Doug DC1010SDR 07FDEA03229Doubler · crackedLT WING L/E CRACK 1" ON TEE ANGLE FIXED PANEL REPAIRED WING LOWER L/E STRINGER DOUBLER IAW SRM 57-10-00 FIG 49.Aug 29, 2007 · N371FE · Doug MD1010FSDR UG8A2007GM05SSkin · chafedDURING COMPLIANCE WITH POST FLIGHT INSPECTION IT WAS NOTED THAT THE LT AND RT WING A FLAP TRACK ISLAND HAT PANELS WERE CHAFING THROUGH THE WING TRAILING EDGE FIXED COVE PANEL. MFG ENGINEERING DISPOSITION NR CS117877 RELEASED OUTLINING REPAIR FOR CONDITION. RAug 29, 2007 · N5101 · Gulstm GULFSTREAMGVSDR UG8A2007GM07SSkin · chafedDURING COMPLIANCE WITH POST FLIGHT INSPECTION IT WAS NOTED THAT THE LT AND RT WING A FLAP TRACK ISLAND HAT PANELS WERE CHAFING THROUGH THE WING TRAILING EDGE FIXED COVE PANEL. MFG ENGINEERING DISPOSITION NR CS117877 RELEASED OUTLINING REPAIR FOR CONDITION. RAug 29, 2007 · N5101 · Gulstm GULFSTREAMGVSDR F3LA200700209Panel · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON ATTACHMENT HOLES ON PANEL 540JB. REPLACED PANEL IAW A319 WORKCARD CP757-2Aug 29, 2007 · N909FR · Airbus A319112SDR USAA070688Skin · damagedWS 72, RIGHT WING, LOWER SURF, Z-ANGLE 3 FWD ATTACH FASTENERS ELONGATED. REMOVED FASTENERS, OVERSIZE & COLD WORK HOLES, & INSTALLED FIRST-OVER FASTENERS PER SRM 51-40-02, 51-40, DEFECT SIZE: .125 INCHES.Aug 28, 2007 · N512AU · Boeing 7373B7SDR USAA070687Skin · damagedTHREE WORKING FASTENER RIGHT WING TO CENTER SECTION Z-ANGLE AT WS 72, AFT 3 FASTENERS ELONGATED. OVERSIZED FIRST OVER, COLD WORKED HOLES & INSTALLED NEW FASTENERS PER SRM 51-40-02, 51-40-03, 51-40-, DEFECT SIZE: .125 INCHAug 28, 2007 · N512AU · Boeing 7373B7SDR USAA070678Skin · crackedLEFT WING FIXED LEADING EDGE LOWER SKIN PANEL AT SLAT STA 3.25 HAS CRACK. REMOVED DAMAGE, FAB'D & INSTALLED REPAIR PARTS PER BOEING TR 57-41-02, DEFECT SIZE: .75 INCH.Aug 28, 2007 · N512AU · Boeing 7373B7SDR A6WA200740535Skin · corrodedRT LOWER WING PLANK ACCESS HOLE 650AB HAS MINOR PITTING CORROSION IN NON-CRITICAL AREA OUTBOARD SIDE OF CUTOUT ON LANDING. CORROSION AREA IS APPROX 2.5 INCHES IN LENGTH AND .2 INCHES WIDE CORROSION PITTING IS APPROX .004 INCH BY .006 INCH BY .008 INCH DEEP. Aug 27, 2007 · N424AW · Cndair CL6002B19
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