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 07FDEA04253Skin · wornFOUND ELONGATED HOLES ON RT WING BOTTOM SKIN AFT OF REAR SPAR. REPAIR PERFORMED BY OVERSIZING AND BUSH INSTALLATION IAW DRAWING R571-50532 AND SB 29-6058, APPROVED BY EA 6-2910-112501 AND RAS/BAE/1005314/2007 ISS A.Sep 24, 2007 · N733FD · Airbus A300B4605RSDR 07FDEA04252Skin · wornFOUND ELONGATED HOLES ON LT WING BOTTOM SKIN AFT OF REAR SPAR REPAIR PERFORMED BY OVERSIZING AND BUSH INSTALLATION IAW DRAWING R571-50532 AND SB 29-6058, APPROVED BY EA 6-2910-112501 AND RAS/BAE/1005314/2007 ISS A.Sep 24, 2007 · N733FD · Airbus A300B4605RSDR 07FDEA04246Skin Panel · wornELONGATED HOLES OF HYDRAULIC PIPE SUPPORT BRACKET AND LOWER SKIN PANEL NR 2, BOTH WINGS. REPAIR PERFORMED BY OVERSIZING HOLES, SPOTFACING AND BUSHING USING THE PRINCIPLES OF REPAIR INSTRUCTION R571-50532 IAW EA 6-5720-82902 AND RAS/BAE/1000997/2005 ISSUE A.Sep 24, 2007 · N724FD · Airbus A300B4622SDR UIEA200700384Panel · delaminatedLT WING, UPPER LEADING EDGE FIXED PANEL AT WING STATION 766 HAS AN AREA OF 12.0 INCH BY 12.0 INCH OF DELAMINATION. PERMANENT REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18, SHEETS 1, 3 AND 5, AND SRM 51-40-12. ALSO, REFERENCE ATLAS AIR XEO NR 57Sep 21, 2007 · N522MC · Boeing 7472D7BSDR 07FDEA04169Skin · corrodedLT WING INBD AILERON CORROSION BOTTOM UPPER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 86 VOL I.Sep 21, 2007 · N369FE · Doug DC1010FSDR 07FDEA04161Skin · looseRT WING UPPER SURFACE OUTBD FLAP FOUND 180 EA LOOSE RIVETS ON SKIN. REPAIRED EFFECTED AREAS IAW SRM 57-20-00 VOL I FIG 11 AND WORK IN CONJUNCTION OF NRC N00468.Sep 21, 2007 · N68052 · Doug DC1010FSDR 07FDEA04152Skin · chafedFOUND CHAFING MARKS ON LEADING EDGE SKIN BETWEEN SLAT TRACK 7-8 OF RT WING. NOSE SKIN REPAIR PERFORMED IAW SRM 57-41-12/FIG 203, 204.Sep 21, 2007 · N803FD · Airbus A310324SDR 07FDEA04099Skin · chafedFOUND CHAFING MARKS ON LEADING EDGE SKIN BETWEEN SLAT TRACK NR 5 AND 6 LT WING. REPLACEMENT OF DAMAGED NOSE SKIN IAW SRM 51-72-10.Sep 20, 2007 · N803FD · Airbus A310324SDR 07FDEA04067Skin Panel · wornELONGATED HYDRAULIC FITTING HOLES ON PYLON NR 1 SUPPORT BRACKET, BOTTOM WING SKIN PANEL 2. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLING BUSHINGS IAW EA 6-5720-82887 AND RAS/BAE/1000947/2005 ISSUE A.Sep 20, 2007 · N803FD · Airbus A310324SDR 07FDEA04065Skin Panel · wornELONGATED HYDRAULIC FITTING HOLES ON PYLON NR 2 SUPPORT BRACKET, BOTTOM WING SKIN PANEL 2. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLING BUSHINGS IAW EA 6-5720-82887 AND RAS/BAE/1000947/2005 ISSUE A.Sep 20, 2007 · N803FD · Airbus A310324SDR 07FDEA04046Skin Panel · chafedFRETTING DAMAGE ON LT BOTTOM SKIN PANEL NR 2, RIB 8-9 REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5720-81068 AND RAS/BAE/1126/2004 ISS A.Sep 19, 2007 · N434FE · Airbus A310203SDR 07FDEA04045Skin · damagedFOUND ON RT WING UPPER SKIN PANEL RIB 15 T/E WAS CUT OUT AND A SEALING STRIP HAD COME A DRIFT. REPAIR PERFORMED BY REMOVING THE SEALING STRIP, ENSURE CUT OUT TO SMOOTH PROFILE AND INSTALL A NEW REPAIR STRIP ON UPPER SURFACE IAW EA 6-5720-81075 AND RAS/BAE/110Sep 19, 2007 · N434FE · Airbus A310203SDR 07FDEA04043Skin · wornFOUND ELONGATED HOLES AT PYLON TO WING HYDRAULIC FITTING HOLES, LT WING BOTTOM SKIN. REPAIR PERFORMED IAW DRAWING R572-59184 (BUSHING REPAIR), APPROVED BY EA 6-5720-81069 AND RAS/BAE/1026/2004 ISS A.Sep 19, 2007 · N434FE · Airbus A310203SDR 07FDEA04042Skin · wornFOUND ELONGATED HOLES AT PYLON TO WING HYDRAULIC FITTING HOLES, RT WING BOTTOM SKIN REPAIR PERFORMED IAW DRAWING R572-59184 (BUSHING REPAIR), APPROVED BY EA 6-5720-81069 AND RAS/BAE/1026/2004 ISS A.Sep 19, 2007 · N434FE · Airbus A310203SDR 07FDEA04027Skin · corrodedFOUND CORROSION ON CENTER TANK TOP SKIN C 45-46 LT, C 41-46 RT REPAIR PERFORMED IAW SRM 57-10-12 FIG 201 AND IN ADDITION THE HOLES OVERSIZED IAW EA 6-5710-81049 AND RAS//AS/0256/2004 ISS A.Sep 19, 2007 · N434FE · Airbus A310203SDR 07FDEA03995Skin Panel · crackedCRACK IN TRAILING EDGE OF BOTTOM SKIN PANEL NR 2, ON RT ZONE 675CB ONE HOLE WITH CRACK IN SKIN. FOR LOCATION SEE EA 6-5710-81091/PG 4 (CRACK LENGTH IN HOLE ABOUT 3MM). DOUBLER PLATE INSTALLED, REPAIR PERFORMED IAW DRW R573-49237 AND EA 6-5710-81091.Sep 19, 2007 · N807FD · Airbus A310324SDR 07FDEA03993Skin Panel · crackedCRACK IN TRAILING EDGE OF BOTTOM SKIN PANEL NR 2, ON LT ZONE 575CB TWO HOLES WITH CRACKS IN SKIN. FOR LOCATION SEE EA 6-5710-81091/PG 3 CRACK LENGTH IN HOLES ABOUT 2 AND 4MM. DOUBLER PLATE INSTALLED, REPAIR PERFORMED IAW. DRW. R573-49237 AND EA 6-5710- 8109Sep 19, 2007 · N807FD · Airbus A310324SDR 07FDEA03962Skin Panel · wornELONGATED HYDRAULIC FITTING HOLES ( 2 AND 4 ) AT PYLON SUPPORT BRACKET, BOTTOM WING SKIN LT, RIB 8. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF BUSHINGS IAW EA 6-5720-81089 AND RAS/BAE/100174/2005 ISSUE A.Sep 19, 2007 · N807FD · Airbus A310324SDR 07FDEA03906Skin Panel · wornELONGATED WING TO PYLON HYDRAULIC FITTING HOLES IN LOWER WING SKIN PANEL NR 2 RT WING. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLING BUSHES IAW R572-49184 ISSUE C, APPROVED BY EA 6-5720-81095 AND RAS/BAE/1000166/2005 ISSUE A.Sep 18, 2007 · N804FD · Airbus A310324SDR 07FDEA03905Skin Panel · wornELONGATED WING TO PYLON HYDRAULIC FITTING HOLES IN LOWER WING SKIN PANEL NR 2. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLING BUSHES IAW R572-49184 ISSUE C, APPROVED BY EA 6-5720-81095 AND RAS/BAE/1000166/2005 ISSUE A.Sep 18, 2007 · N804FD · Airbus A310324SDR 07FDEA03901Skin Panel · corrodedFOUND OLD BLEND OUT REPAIRS WITH NEW CORROSION SIGNS ON LT WING UPPER SKIN BETWEEN RIB 3 TO 5 NEAR THE REAR SPAR AND BETWEEN RIB 7 TO 8 AND RIB 10 TO 11 AT THE FRONT SPAR. THE CORRODED AREAS HAVE BEEN REPAIRED IAW WITH SRM 57-00-00/PG 201/PARA 4C PART B AND TSep 18, 2007 · N804FD · Airbus A310324SDR 07FDEA03894Skin Panel · corrodedFOUND SEVERAL OLD REPAIRS OF THE WING TOP SKIN PANEL BETWEEN RIB 9-23 RT WITH NEW CORROSIONS SPOTS. REPAIR PERFORMED BY BLEND OUT CORROSION, FLAP PEENING REWORKED AREAS IAW EA 6-5720-81120, RAS/BAE/0203/2000 ISSUE A AND RAS/BAE/1409/2004 ISSUE A.Sep 18, 2007 · N804FD · Airbus A310324SDR EIA2007161Skin · damagedRIGHT WING LANDING LIGHT SKIN PANEL OUTBOARD HAS NUMEROUS RIVETS PULLED/WORN THRU SKIN AND FASTENERS DISTRESSED. REPAIRED RT LEADING EDGE LANDING LIGHT SKIN PANEL PER ECRA NR 486-57-057-2.Sep 17, 2007 · N486EV · Boeing 747212BSDR 07FDEA03822Skin · unknownRT WING L/E SKIN EXISTING DOUBLER. REPLACED DOUBLER IAW SRM 51-30-00 VOL II.Sep 17, 2007 · N68052 · Doug DC1010FSDR CA070918002Panel · cracked(CAN) AFTER A (WATER - FIRE SUPPRESSION) BOMBING MISSION, FUEL WAS FOUND LEAKING FROM A CRACK THAT WAS COMING FROM AN OLD REPAIR. THE A/C WAS DOWN LOADED WITH WEIGHT AND THE A/C WAS FERRIED TO THE COMPANY MAINTENANCE STATION. (TC NR 20070918002)Sep 16, 2007 · Lkheed 188ASDR F3LA200700247Skin · damagedINSPECTION REPORTED LIGHTNING DAMAGE TO LEFT WING UPPER SURFACE RIB 17, APPROX 12 INCHES AFT OF MIDSPAR AT FASTENER LOCATION. REMOVED FASTENER, BLENDED DAMAGE TO COUNTERSINK IAW SRM 51-11-13. REPLACED FASTENER IAW EA A9-574-12145.Sep 16, 2007 · N918FR · Airbus A319111SDR F3LA200700246Fastener · damagedINSPECTION REPORTED LIGHTNING DAMAGE TO LEFT WING UPPER SURFACE AFT OF NR 3 SLAT, OUTBOARD SLAT TRACK, INBOARD OF RIB 17. REMOVED AND REPLACED DAMAGED FASTENER IAW EA A9-57R-12145.Sep 15, 2007 · N5730 · Airbus A319111SDR F3LA200700245Fastener · damagedINSPECTION REPORTED LIGHTNING DAMAGE TO LEFT WING UPPER SURFACE AT FASTENER INBOARD OF RIB 17 AT MID SPAR. REMOVED DAMAGED FASTENER, BLENDED DAMAGED AREA, PERFORMED REQUIRED NDT PROCESS, AND INSTALLED NEW FASTENER IAW EA A9-57R-12145.Sep 15, 2007 · N918FR · Airbus A319111SDR F3LA200700244Fastener · damagedINSPECTION REPORTED LIGHTNING DAMAGE TO LEFT WING UPPER SURFACE AT FASTENER RIB 17, JUST FWD OF NR 4 SPOILER. REMOVED DAMAGED FASTENER, PERFORMED REQUIRED NDT PROCESS, AND INSTALLED NEW FASTENER IAW EA A9-57R-12145.Sep 15, 2007 · N918FR · Airbus A319111SDR F3LA200700243Fastener · damagedINSPECTION REPORTED LIGHTNING DAMAGE TO LEFT WING UPPER SURFACE AT FASTENER RIB 17, 12 INCHES FWD OF AFT SPAR. REMOVED DAMAGED FASTENER, BLENDED DAMAGED AREA, PERFORMED REQUIRED NDT PROCESS AND INSTALLED NEW FASTENER IAW EA A9-57R-12145.Sep 15, 2007 · N918FR · Airbus A319111SDR 07FDEA03774Skin · chafedCHAFING DAMAGE AT ONE POSITION AND CRACK WITH DEFORMATION AT ANOTHER LOCATION ON FIXED LEADING EDGE D-NOSE SKIN RT, BETWEEN TRACK 3 AND TRACK 4. REPAIR PERFORMED BY BLENDING OUT DAMAGES AT BOTH POSITIONS, REMOVING FASTENER OF HOLE IN AREA OF CRACK WITH ROTOTESep 14, 2007 · N815FD · Airbus A310324SDR QXEA200701433Skin · damagedC5 PDX - TOP SURFACE OF BOTTOM PANEL OF LEFT WING IS SCRATCHED IN MULTIPLE PLACES BETWEEN YW 155 AND YW 139 FORWARD REAR SPAR. REPAIRED IAW SRM 51-20-11, 51-20-16, AND 51-20-41.Sep 13, 2007 · N345PH · Dhav DHC8202SDR QXEA200701431Skin · damagedC5 PDX -TOP SURFACE OF BOTTOM PANEL OF RIGHT WING IS SCRATCHED IN MULTIPLE PLACES BETWEEN YW 171 AND YW 139 AFT OF FRONT SPAR. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-41.Sep 13, 2007 · N345PH · Dhav DHC8202SDR 07FDEA03690Skin Panel · wornELONGATED HOLES FOUND ON RT WING TO PYLON HYDRAULIC FITTING RIB 8 REPAIR PERFORMED BY REAM UP AND BUSH INSTALLATION IAW DRAWING R572-49184, APPROVED BY EA 6-5720-79595 AND RAS/BAE/0931/2004 ISS A.Sep 13, 2007 · N432FE · Airbus A310203SDR 07FDEA03688Skin Panel · wornFOUND ELONGATED HOLES ON LT WING TO PYLON HYDRAULIC FITTING HOLES RIB 8 REPAIR PERFORMED BY REAM UP AND INSTALL BUSHINGS IAW DRAWING R572-49184 , APPROVED BY EA 6-5720-79594 AND RAS/BAE/0931/2004 ISS A.Sep 13, 2007 · N432FE · Airbus A310203SDR 07FDEA03681Skin · corrodedDURING REMOVAL OF BOLT 642, NOTED IN SB A310-57-2028 FOUND CORROSION INSIDE THE FITTING BORE, LT WING AREA OF RIB 5 REPAIR PERFORMED BY OVERSIZING THE HOLE IAW EA 6-5721-81050 AND RAS/BAE/0928/2004 ISS A.Sep 13, 2007 · N432FE · Airbus A310203SDR 07FDEA03631Skin Panel · chafedCHAFING MARKS FOUND AROUND MANHOLE 9 APERTURE ON THE UPPER SURFACE OF THE BOTTOM WING SKIN PANEL NR 2 BETWEEN RIB 14-15, BOTH WINGS. REPAIR PERFORMED BY SMOOTH BLEND OUT, NDT INSPECTION FOR CRACK FREE AND FILLING BLEND LEVEL RESIN IAW EA 6-5720-92205 AND RAS/Sep 13, 2007 · N812FD · Airbus A310324SDR MALA070157Skin Panel · puncturedLT WING TRAILING EDGE UPPER SKIN PANEL PUNCTURE 3.0" FWD OF T/E ST WS 52. REPAIRED PER EOS51031.Sep 12, 2007 · N415XJ · Saab 340BSDR UIEA200700372Skin · corrodedRHW UPP SKIN PNL: WS1141-WS1337, FRONT SPAR TO REAR SPAR SEVERAL AREAS OF CORROSION EVIDENCED. SURF CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND SOPM 20-43-03.Sep 12, 2007 · N512MC · Boeing 747230BSDR UIEA200700370Skin · corrodedSURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 724.50 TO WS 917.00 BETWEEN FRONT SPAR AND MID SPAR. SURF CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.Sep 12, 2007 · N512MC · Boeing 747230BSDR UIEA200700369Skin · corrodedSURF CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 528 TO SIDE OF FUS BODY BETWEEN FRONT SPAR AND MID SPAR. SURF CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.Sep 12, 2007 · N512MC · Boeing 747230BSDR UIEA200700368Skin · corrodedSURF CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 528 TO WS 724.5 BETWEEN FRONT SPAR AND MID SPAR. SURF CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.Sep 12, 2007 · N512MC · Boeing 747230BSDR UIEA200700367Skin · corrodedSURF CORROSION EVIDENT AROUND FASTENER HEAD FROM SIDE OF BODY TO WS 528 BETWEEN MID SPAR AND REAR SPAR. SURF CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.Sep 12, 2007 · N512MC · Boeing 747230BSDR 07FDEA03616Skin · corrodedFOUND SKIN BULGE (CORROSION) ON LEADING EDGE OF RT WING INBOARD FLAP, NEAR TO TRACK 1. REPLACEMENT OF L/E SKIN AT FLAP IAW SRM 51-72-10.Sep 12, 2007 · N812FD · Airbus A310324SDR 07FDEA03589Skin · crackedLT WING FOUND CRACK ON LOWER EXT SKIN L/E. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 1 VOL I.Sep 12, 2007 · N371FE · Doug DC1010SDR 07FDEA03576Skin · chafedFOUND THREE CHAFING MARKS ON LEADING EDGE D-NOSE SKIN BETWEEN SLAT TRACK 6 AND JACK 4 RT WING. NOSE SKIN REPAIR PERFORMED IAW SRM 57-41-12/ FIG 204 WITH ALTERNATIVE MATERIAL, APPROVED BY EA 6-5741-92200 AND RAS/BAE/1001636/2005 ISSUE B.Sep 11, 2007 · N812FD · Airbus A310324SDR 07FDEA03574Skin · chafedFOUND SEVERAL CHAFING MARKS ON LEADING EDGE D-NOSE SKIN RT BETWEEN SLAT TRACK 2 AND JACK 2. REPLACEMENT OF D-NOSE SKIN IAW SRM 51-72-10.Sep 11, 2007 · N812FD · Airbus A310324SDR 07FDEA03573Skin · chafedFOUND SEVERAL CHAFING MARKS ON LEADING EDGE D-NOSE SKIN RT BETWEEN TRACK 5 AND 6. REPLACEMENT OF D-NOSE SKIN IAW SRM 51-72-10.Sep 11, 2007 · N812FD · Airbus A310203SDR 07FDEA03568Skin Panel · wornELONGATED HYDRAULIC FITTING HOLES AT PYLON SUPPORT BRACKET AND BOTTOM OF LT WING, RIB 8. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLING BUSHES IAW R572-49184 ISSUE C, APPROVED BY EA 6-5720-92194 AND RAS/BAE/1001639/2005 ISSUE A.Sep 11, 2007 · N812FD · Airbus A310203SDR 07FDEA03567Skin Panel · wornELONGATED HYDRAULIC FITTING HOLES AT PYLON SUPPORT BRACKET AND BOTTOM OF RT WING, RIB 8. REPAIR PERFORMED BY OVERSIZING AND INSTALLING BUSHES IAW R572-49184 ISSUE C, APPROVED BY EA 6-5720-92194 AND RAS/BAE/1001639/2005 ISSUE A.Sep 11, 2007 · N812FD · Airbus A310324
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