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 VNAA0802021Fairing · damagedCREW REPORTED THE RIGHT WING STRUCK THE GROUND UPON LANDING. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE RIGHT HAND WINGTIP LOWER SKIN PANEL. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND WINGTIP FAIRING IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAFeb 26, 2008 · N250PS · Cndair CL6002B19SDR HALA0800356Skin · corrodedLEVEL 1 CORROSION RT WING UPPER SURFACE, AROUND FASTENER AT WING STA 865 AND 4 INCHES AFT OF FRONT SPAR. CORROSION REMOVED IAW B767300 SRM 51-10-02 TO THE POINT OF CONFIRMATION WITH 10X MAGNIFING GLASS. NO OTHER DAMAGE EXISTS ON THIS LINE PERPENDICULAR TO REFeb 26, 2008 · N585HA · Boeing 7673G5SDR HALA0800352Skin · corrodedLEVEL 1 CORROSION, WING RT UPPER SKIN FASTENER AT WS 936 ON FWD SPAR CAP. REMOVED CORROSION IAW B767-300 SRM 51-10-02 TO THE POINT OF CONFORMATION WITH 10X MAGNIFYING GLASS. NO OTHER DAMAGE EXIST ON THIS LINE PERPENDICULAR TO REAR SPAR. REF SRM 57-20-01, FIFeb 26, 2008 · N585HA · Boeing 7673G5SDR 08FDEA00609Skin · corrodedCORROSION FOUND ON RT WING BOTTOM SKIN IN RIB 8 AND STRINGER 18 AREA. REPAIR PERFORMED BY BLEND OUT OF CORROSION, NDT FOR CRACK FREE AND OVERSIZING OF FASTENER IAW RAS/BAE/1006317/2008 ISS A, APPROVE DBY EA 6-5720-114868.Feb 26, 2008 · N741FD · Airbus A300B4622RSDR 08FDEA00608Skin · corrodedCORROSION FOUND ON RT WING BOTTOM SKIN RIB 1-2 AND REAR SPAR AND AFT OF REAR SPAR. REPAIR PERFORMED BY REWORK OF CORROSION AND OVERSIZING THE HOLES IAW RAS/BAE/1006320/2008 ISS A, APPROVED BY EA 6-5720-114867.Feb 26, 2008 · N741FD · Airbus A300B4622RSDR 08FDEA00607Skin · corrodedCORROSION ON LT WING BOTTOM SKIN UPPER SURFACE AT RIB 5 AFT OF REAR SPAR. REPAIR PERFORMED BY BLEND OUT THE CORROSION AND NDT FOR CRACK FREE CONDITION, FLAP PEENING IAW RAS/BAE/1006416/2008 ISS A, APPROVED BY EA 6-5720-114931.Feb 26, 2008 · N745FD · Airbus A300B4622RSDR 08FDEA00606Skin · chafedCHAFING MARKS FOUND ON LT OUTER WING BOTTOM SKIN REINFORCING PLATE AT RIB 7. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS AND NDT FOR CRACK FREE IAW RAS/BAE/1006409/2008 ISS A, APPROVED BY EA 6-5720-114930.Feb 26, 2008 · N745FD · Airbus A300B4622RSDR 08FDEA00604Skin · cracked16 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RT WING, LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS 690 AND XORS 700. REPAIR CARRIED OUT AS PER EA 1-5710-118761 PART 1, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 26, 2008 · N608FE · Doug MD11FSDR 08FDEA00603Skin · crackedFOUND SIX FASTENER HOLES CRACK INDICATION DURING HFEC, OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS = 690 AND XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-118760 PART 1, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 26, 2008 · N608FE · Doug MD11FSDR DHL2008805507Skin · crackedLT WING UPPER SKIN CRACK 1" STA XRS 74.000 S-9. PERFORMED MAJOR REPAIR IAW SRM 57-2-1- FIG 17 PG 87-88. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG 17 PG 87-88. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. NEITHFeb 25, 2008 · N805DH · Doug DC873FSDR UPS08851746Doubler · bulgedINSPECTION TYPE:C2 LT WING O/B UPPER AND LOWER SURFACE TE WEDGE DOUBLER HAS 2 UPPER FASTENERS PULLING THROUGH AND DOUBLER BULGED. REPAIRED L-WING O/B TE IAW SRM 57-02-00 FIG 002A, SRM 51-01-21A.Feb 24, 2008 · N852UP · Doug DC873FSDR ASMF200802007Skin · deformedDURING TAXING, THE AC LT SLATS NR 2 AND 3 STRUCK AGAINST A LAMPPOST OF TAXIWAY. DETAILED INSP WAS PERFORMED ON LT WING DETECTING STRUCTURAL DAMAGE ON SLATS NR 2 AND 3 OF 70 INCHES LENGTH AND 25 INCHES WIDTH, OUT OF LIMITS, LOCATED BETWEEN STATIONS WS1110 AND WFeb 24, 2008 · N774AM · Boeing 777*SDR 08FDEA00577Access Panel · corrodedWING FUEL PANEL 542BB HAS SURFACE/FRETTING CORROSION. REMOVED CORROSION FROM PANEL 542BB, FOUND TO BE OUT OF SRM 57-20-01, SECTION A-A, DETAIL I LIMITS. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-118.Feb 22, 2008 · N903FD · Boeing 7572B7SDR 08FDEA00576Access Panel · corrodedWING FUEL PANEL 541DB HAS SURFACE/FRETTING CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF SRM 57-20-01, SECTION A-A, DETAIL I LIMITS. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-116.Feb 22, 2008 · N903FD · Boeing 7572B7SDR 08FDEA00541Panel · corrodedWING FUEL PANEL 541LB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 541LB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-116, ALTERNATE PN: 112N6101-1.Feb 21, 2008 · N903FD · Boeing 7572B7SDR 2008UALA00983Seal · leakingFUEL LEAK RT WING UNDERSIDE OUTBOARD OF RT ENGINE PYLON. SUSPECT SEAL ON FUEL TANK ACCESS PLATE. REPLACED SEAL. ACFT OK FOR SERVICE. Feb 20, 2008 · N779UA · Boeing 777222SDR 08FDEA00540Panel · corrodedWING FUEL PANEL 641JB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 641JB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-119.Feb 20, 2008 · N903FD · Boeing 7572B7SDR 08FDEA00539Panel · corrodedWING FUEL PANEL 641KB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 641KB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-116.Feb 20, 2008 · N903FD · Boeing 7572B7SDR 08FDEA00537Panel · corrodedWING FUEL PANEL 541EB HAS SURFACE FRETTING CORROSION. WING FUEL PANEL 541EB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-119.Feb 20, 2008 · N903FD · Boeing 7572B7SDR 08FDEA00536Panel · corrodedWING FUEL PANEL 642AB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 642AB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-116.Feb 20, 2008 · N903FD · Boeing 7572B7SDR 08FDEA00535Panel · corrodedWING FUEL PANEL 642CB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 642CB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-117.Feb 20, 2008 · N903FD · Boeing 7572B7SDR 08FDEA00534Panel · corrodedWING FUEL PANEL 642DB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 642DB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-117.Feb 20, 2008 · N903FD · Boeing 7572B7SDR 08FDEA00533Panel · corrodedWING FUEL PANEL 641DB HAS SURFACE CORROSION. WING FUEL PANEL 641DB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-116.Feb 20, 2008 · N903FD · Boeing 7572B7SDR 08FDEA00532Panel · corrodedWING FUEL PANEL 642BB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 642BB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-118.Feb 20, 2008 · N903FD · Boeing 7572B7SDR 08FDEA00531Access Panel · corrodedWING FUEL PANEL 641MB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 641MB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 112N6101-5.Feb 20, 2008 · N903FD · Boeing 7572B7SDR HALA0800311Skin · corrodedLEVEL 1 CORROSION AROUND FASTENER TAILS LEFT WING BELOW CENTER SECTION. REPAIR IN WORK.Feb 18, 2008 · N479HA · Boeing 717200SDR 08FDEA00501Skin · damagedRT WING LOWER O/B PANEL 590 BB HAS SCRATCHES ON THE SKIN AROUND THE CUTOUT, AND ON THE ANGLES INSIDE THE CUTOUT.Feb 18, 2008 · N684FE · Airbus A300F4605RSDR KCSA081080Skin · corrodedAIR CONDITIONING BAY CENTER WING LOWER SKIN MATERIAL LOSS FOUND OUT OF LIMITS AT STA 1067, CENTER WING LBL 116 BETWEEN WING STRINGERS 17 AND 18 AREA MAPPED.Feb 16, 2008 · N715CK · Boeing 747209BSDR IXXA08SMN088SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP LOWER FORWARD PANEL PLATING DENTED AT STATION XW 2.000 - STA XW 91.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, AND BONDED DOUBLER. BONDED PARTS AS Feb 15, 2008 · N822BX · Doug DC871FSDR IXXA08SMN087SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER INNER SKIN INBOARD SPLICE CRACKED AT STATION XFS 341.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. Feb 15, 2008 · N822BX · Doug DC871FSDR IXXA08SMN089SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING LEADING CENTER LEADING EDGE OUTER SKIN LOWER SHOWS IMPROPER REPAIR AT STATION XFS 385.200. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPEFeb 15, 2008 · N822BX · Doug DC871FSDR IXXA08SMN079SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD AFT LOWER FLAP SKIN SHOWS DENTS AT STATION XE 2.000 TO STA XE 91.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS AS NEEDED WIFeb 15, 2008 · N822BX · Doug DC871FSDR 08FDEA00451Skin · corrodedRIGHT WING UPPER TRAILING EDGE PANEL HAS CORROSION ON THE UPPER SURFACE, APPROXIMATELY XORS 345. REMOVED CORROSION; OUT OF LIMITS IAW 10 SRM 51-21-01, VOL II & 57-31-01 FIG A, VOL III & 57-00-01 FIG A, VOL I. REMOVED PANEL IAW SRM 51-33-01, VOL II, 51-3Feb 15, 2008 · N374FE · Doug MD1010FSDR IXXA08SMN075SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER OUTER SKIN SHOWS IMPROPER REPAIR AT STATION XOLDI 6.2246. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. Feb 14, 2008 · N822BX · Doug DC871FSDR IXXA08SMN074SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER OUTER SKIN SHOWS IMPROPER REPAIR AT STATION XFS 304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRAFeb 14, 2008 · N822BX · Doug DC871FSDR UPS08M52030Skin · damagedINSPECTION TYPE:C LT WING FIXED L/E LOWER SURFACE ABOVE NR 1 ENGINE PYLON O/B SIDE AT APPROXIMATELY STA XORS 299 FOUND SCRATCH MARKS AS MARKED. DAMAGE SKIN REMOVED PER SRM 51-31-01V.2R.40. NEW SKIN FAB PER BOEING DRAWING ARB2363 USING MATL 7075T6-0.090". NEFeb 12, 2008 · N294UP · Doug MD11SDR UPS08M51738Skin · crackedINSPECTION TYPE:1C RIGHT LE NR 14 SLAT TRACK CUT OUT CRACKED ON LWR O/B CORNER, CUTOUT DAMAGE. FABRICATED DOUBLER AND INSTALLED DOUBLER IAW MD-11 SRM 57-10-00 FIG 21.Feb 12, 2008 · N259UP · Doug MD11FSDR WRLA2008023Skin · corrodedDURING MAINTENANCE INSPECTION AT SAA, CORROSION FOUND ON CENTER WING UPPER SKIN LT SIDE, APPROX STA XCW101. REPAIRED PER SAA EA 010-5710-11-A0232 REV A.Feb 11, 2008 · N136WA · Doug DC1030SDR S9BA20080003Skin · corrodedCPCP INSPECTION, LT WING CORRUGATION AT WS 65 TO 125 CORRODED. REPAIRED CORRUGATION BETWEEN WS 65 AND 125 IAW SRM 57-30-00 FIG 4 AND RD6-57-077. EMERGENCY MEASURES EXECUTED? NO. AIRCRAFT GROUNDED? YES.Feb 11, 2008 · N573SA · Dhav DHC6SDR S9BA20080012Skin · corrodedCPCP INSPECTION, RT WING IB FWD SKIN CORRODED WS STA. 35.15 TO 185. REPLACED SKIN IAW SRM CH 57-30-00 FIG 1AND RD 6-57-164. EMERGENCY MEASURES EXECUTED? NO. AIRCRAFT GROUNDED? YES.Feb 11, 2008 · N573SA · Dhav DHC6SDR S9BA20080011Skin · corrodedCPCP INSPECTION; RT WING FWD CORRUGATION AT WS 58 CORRODED. REPAIRED CORRUGATION AT WS 58 WITH FACTORY NEW PART IAW SRM 57-30-00 PAGE 4. EMERGENCY MEASURES EXECUTED? NO AIRCRAFT GROUNDED? YES.Feb 11, 2008 · N573SA · Dhav DHC6SDR S9BA200800001Skin · corrodedCPCP INSPECTION, LT FWD SKIN ON LT WING IS CORRODED AT WS 63.5. REPLACED LOWER SKIN FROM RIB 1 (STA 35.15) TO RIB 10 (STA 147.5) SPLICED SKIN AT RIB 2 (STA 47.5) AIRCRAFT GROUNDED? YESFeb 11, 2008 · N573SA · Dhav DHC6SDR TRAX200800239Skin · damagedAPPEARS TO BE SKIN CRACKING OR DELAMINATION ON UPPER WING TO WINGLET MATING AREA. FLT 4330 DEL 35 MINS. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION.Feb 10, 2008 · N873AS · Cndair CL6002B19SDR IXXA08SMN064SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN DENTS AT STATION XF 169.000 - XF 213.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANFeb 8, 2008 · N822BX · Doug DC871FSDR G60A200800020Skin · crackedLT WING TIP TOP SIDE OUTBD AFT END SKIN CRACKED APPROX 5".Feb 8, 2008 · N607GC · Doug DC1030FSDR DHL2008752605Skin · crackedLT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IS CRACKED FWD. REMOVED FASTENERS AT LT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IAW B727 SRM 51-30-2. STOP DRILLED 0.250" DIA AT END OF CRACK IAW B727 SRM 57-30-4 FIG Feb 6, 2008 · N752DH · Boeing 727223SDR 08FDEA00362Skin · crackedRIGHT WING SLAT NR 6 SCREWJACK CUT OUT, WING STATION 1713, CRACKED. REMOVED FASTENERS AT DAMAGED AREA IAW FEDEX A310-200 SRM 51-40-21 PAGE 22. CUT OUT SKIN DAMAGE AT LEADING EDGE WING STATION 1713 IAW FEDEX A310-200 SRM 57-41-12 PAGE 209 FIGURE 203. INSTALLFeb 6, 2008 · N416FE · Airbus A310222SDR UIEA200800028Panel · delaminatedRT WING FIXED UPPER L/E PANEL DIRECTLY ABOVE NR 3 GROUP L/E PDU HAS AREA OF 23.5 BY 19.0 INCHES OF DELAMINATION. INTERIM REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-16 FIG 1, SRM 51-70-06, SRM 51-30-02, ATLAS AIR EO NR 4757A417 AND FAA FORM 8110-3. REQFeb 5, 2008 · N524MC · Boeing 7472D7BSDR C2XA08TY026Skin · crackedTYS - DURING AN A-CHECK INSPECTION A CRACK IN THE UPPER LT WING SKIN FWD OF THE I/B SPOILER CENTER HINGE POINT. THE SKIN WAS INSPECTED AND PLACED ON DMI FOR 500FC WITH A REINSPECT EVERY 50FC IAW IC2008-145/00965. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 5, 2008 · N15986 · Emb EMB145LRSDR DHL2008752600Slat · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL USED 2024TFeb 4, 2008 · N752DH · Boeing 727223
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