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 MASA2010100101066Skin · crackedLWR WING PLANK CRACK WS 148.019 LT & RT SIDE. MX C/W LOWER WING PLANK REPAIR IAW RO CRJ-57-2914.Sep 30, 2010 · N75995 · Cndair CL6002C10SDR FDEA201009303843Access Panel · corrodedRT WING LOWER SKIN, FUEL TANK ACCESS DOOR NR 641DB MATING SURFACE WITH FRETTING CORROSION. CORRODED RT WING TANK ACCESS PANEL NR 641DB. REMOVED AND REPLACED IAW AMM 28-11-01-4 REV. 98. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 30, 2010 · N935FD · Boeing 7572T7SDR FDEA201009303842Access Panel · corrodedRT WING TANK ACCESS PANEL NR 641KB EXTERIOR SURFACE WITH CORROSION. CORRODED RT WING TANK ACCESS PANEL NR 641KB. REMOVED AND REPLACED IAW AMM 28-11-01-4 REV.98. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 30, 2010 · N935FD · Boeing 7572T7SDR FDEA201009303841Access Panel · corrodedRT WING LOWER SKIN, FUEL TANK ACCESS DOOR NR 641EB MATING SURFACE WITH FRETTING CORROSION. CORRODED RT WING TANK ACCESS DOOR NR 641EB. REMOVED AND REPLACED IAW AMM 28-11-01-4. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 30, 2010 · N935FD · Boeing 7572T7SDR FDEA201009303840Access Panel · corrodedRT WING LOWER SKIN FUEL TANK ACCESS DOOR NR 641LB MATING SURFACE WITH FRETTING CORROSION. CORRODED RT WING TANK ACCESS DOOR NR 641LB. REMOVED AND REPLACED IAW AMM 28-11-01-4 REV. 98. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 30, 2010 · N935FD · Boeing 7572T7SDR FDEA201009303839Skin · crackedLT WING - OUTBOARD OF PYLON, SLAT MECHANISM PANEL, INBOARD FORWARD CUTOUT FOUND CRACKED. TRIMMED AND REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 68, VOL I, REV 96. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 111.Sep 30, 2010 · N390FE · Doug MD1010FSDR FDEA201009303838Skin · crackedLT WING NR 4 SLAT, OUTBOARD SLAT TRACK CUTOUT FOUND CRACKED. TRIMMED OFF AND REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 68, REV 96, VOLUME I. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 111.Sep 30, 2010 · N390FE · Doug MD1010FSDR FDEA201009293780Doubler · corrodedLT WING UPPER WING SURFACE MLG SUPPORT UPPER DOUBLER AT XORS 290 FOUND CORROSION. CARRIED OUT RECTIFICATION AS PER EA 1-5710-143434. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.Sep 29, 2010 · N582FE · Doug MD11FSDR FDEA201009293779Doubler · corrodedLT WING UPPER WING SURFACE MLG SUPPORT UPPER DOUBLER AT XORS 288 FOUND CORROSION. CARRIED OUT RECTIFICATION AS PER EA 1-5710-143434. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.Sep 29, 2010 · N582FE · Doug MD11FSDR REXA201000171Skin · corrodedRT LOWER PLANK FUEL ACCESS HOLE AT WS 54.897 HOLE NR 1 HAS CORROSION ON INBOARD EDGE OF CUTOUT MEASURE APPROXIMATELY .002 INCH DEEP NOT IN CRITICAL AREA. REPAIRED RT LOWER FUEL ACCESS HOLE AT WS 54.897 HOLE NR 1 ON INBOARD EDGE OF CUTOUT NOT IN CRITICAL AREA Sep 28, 2010 · N8775A · Cndair CL6002B19SDR REXA201000172Skin · corrodedLT LOWER PLANK FUEL ACCESS HOLE AT WS 12.245 HOLE NR 2 HAS CORROSION ON INBOARD EDGE OF CUTOUT MEASURE APPROXIMATELY .003 INCH DEEP NOT IN CRITICAL AREA. REPAIRED LT LOWER FUEL ACCESS HOLE AT WS 12.245 HOLE NR 2 ON INBOARD EDGE OF CUTOUT NOT IN CRITICAL AREA Sep 28, 2010 · N8775A · Cndair CL6002B19SDR ASMF20101001Access Panel · crackedDURING TRANSIT CHECK, TECH DETECTED A FUEL LEAK IN LT WING MAIN TANK DUE TO A CRACK IN THE FUEL TANK ACCESS DOOR PANEL NR 532DB; SO IT WAS REPLACED AND LEAK TEST WAS PERFORMED IAW MM 28-11-11, ALL CORRECT. AFTER DURING OVERNIGHT CHECK WAS DETECTED A FUEL LEAKSep 28, 2010 · N904AM · Boeing 737705SDR FDEA201009273734Skin · crackedLEFT WING LEADING EDGE LOWER ACCESS PANEL 519CB CUT OUT, INBOARD CORNER SKIN FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 57-40-02 FIGURE 201, REPAIR 7, REVISION 44. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.Sep 27, 2010 · N582FE · Doug MD11FSDR FDEA201009273732Skin · crackedRIGHT WING LOWER SKIN PANEL OUTER WING ACCESS DOOR CUT OUT AT APPROXIMATELY BETWEEN XORS 683.400 AND XORS 713.600, 01 EACH FASTENER HOLE FOUND WITH CRACKED INDICATION DURING HFEC OPEN HOLE INSPECTION. CARRIED OUT REPAIR BY INSTALLATION OF BUSHING IN REWORK FASep 27, 2010 · N582FE · Doug MD11FSDR FDEA201009273731Skin · crackedLEFT WING LOWER SKIN PANEL, OUTER WING ACCESS DOOR CUT OUT AT APPROXIMATELY BETWEEN XORS 683.400 AND XORS 713.600, 03 EACH FASTENER HOLE FOUND WITH CRACKED INDICATION DURING HFEC OPEN HOLE INSPECTION. 03 EACH FASTENER HOLE AT LEFT HAND WING LOWER SKIN FUEL TANSep 27, 2010 · N582FE · Doug MD11FSDR FDEA201009273754Skin · crackedRT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACKED. CARRIED OUT IAW EA NR8-5710-143754, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.Sep 27, 2010 · N390FE · Doug MD1010FSDR FDEA201009273753Skin · crackedLT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACK AT 2 LOCATIONS. TRIMMED AND REPAIR CARRIED OUT IAW EA 8-5710-143751, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.Sep 27, 2010 · N390FE · Doug MD1010FSDR CA101109009Fastener · loose(CAN) WING CENTER SECTION - P/N 101-120140-5 SKIN P/N 101-120116-53 HAD LOOSE FASTENERS AT AFT EDGE AT SPAR.Sep 26, 2010 · Beech B200SDR IPXA10M62945Doubler · crackedINSPECTION TYPE:1C, WHILE PERFORMING DVI OF THE REPAIRED AREA REF EA 011-5720-01-A2697 STEP E, FOUND 3 CRACKS ON BEADED DOUBLER AT INBD OF FORMER XOS 789.6. REMOVED DAMAGE ON RT WING FIXED L/E BEADED DOUBLER BETWEEN STA XOS 783. 2 TO XOS 789.6. FABRICATED Sep 26, 2010 · N257UP · Doug MD11FSDR IXXA10SMN094SSkin · crackedDURING ROUTINE C-CHECK INSP, FOUND LT WING OUTER WING OTBD L/E LOWER SKIN CRACKED AT STA XFS 847.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. FABRICATED NEW SKIN, FILLERS AND DOUBSep 25, 2010 · N606AL · Doug DC873FSDR FDEA201009243700Rib · crackedRIGHT WING NR 1 LEADING EDGE SLAT INBOARD PERFORMANCE FILLET OUTBOARD EDGE RIB FOUND CRACKED AROUND AFT FASTENER HOLE. CARRIED OUT REPAIR AS PER SRM 57-40-71 FIGURE 201, REPAIR 1, REVISION 44. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 111.Sep 24, 2010 · N582FE · Doug MD11FSDR FDEA201009243698Skin · corrodedRIGHT WING UPPER SURFACE, MAIN LANDING GEAR SUPPORT UPPER DOUBLER AT XORS 277 FOUND CORROSION. CARRIED OUT RECTIFICATION AS PER E.A. 1-5730-143750. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 111.Sep 24, 2010 · N582FE · Doug MD11FSDR ABXA201010010125Panel · corrodedUPPER AND LOWER SURFACE OF REFUELING PANEL HAS AREAS OF CORROSION. REMOVED WIRE HARNESS TO FOM REMOVED CORROSION. TREATED PRIMED AND PAINTED. RE-INSTALLED WIRE HARNESS CONTINUITY CHECKED GOOD. OPS CHECK OF FUELING PANEL GOOD IAW B767 AMM 28-21-00-5 AND 28-Sep 24, 2010 · N790AX · Boeing 767281SDR CA101109008Skin · cracked(CAN) ON WING CENTER SECTION P/N 99-120000-603 SKINS 50-120068-96 LT AND 97 RT WERE CRACKED AT UPPER FEW WING ATTACH FITTINGS.Sep 23, 2010 · Beech A100SDR ABXA201010010130Skin Panel · damagedDURING TRIM OUT OF RIGHT SIDE FAIL-SAFE STRAP PER REA B653-58935-SB STEP 6 RT WING SKIN PANEL DAMAGED DURING CUTOUT PROCESS. POSSIBLE DAMAGE TO LONGERON SPLICE. RIGHT WING SKIN PANEL REPAIRED IAW REA B653-58942-MR & B653-58947-MR.Sep 23, 2010 · N790AX · Boeing 767281SDR DALA1023817101Skin · damagedPERFORMED HFEC, NO DISCREPENCIES FOUND. REWORKED TO 3 IN DIA RADIUS. HFEC NO CRACKS FOUND C/W INSURANCE CUT. BROKE ALL SHARP EDGES, AND ROTO PEENED. TREATED AND PAINTED AERA. REF EO CARD 20-22.Sep 23, 2010 · N701DN · Boeing 777232LRSDR DALA1023807101Skin · damagedC/W EA 11-479059-12AD ME01 REV ORIG OPN 0101. PERFORMED HFEC, NO DISCREPENCIES FOUND. REWORKED TO 3 INCH DIA RADIUS. HFEC NO CRACKS FOUND C/W INSURANCE CUT. BROKE ALL SHARP EDGES, AND ROTO PEENED. TREATED AND PAINTED AERA. REF EO CARD 17-19.Sep 23, 2010 · N701DN · Boeing 777232LRSDR IXXA10SMN092SSkin · damagedDURING ROUTINE C-CHECK INSP, FOUND LT WING NR 2 STUB WING LOWER SKIN ELONGATED HOLES AT STA XFS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED SPLICE DOUBLER AND NEW SKIN. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTSep 22, 2010 · N606AL · Doug DC873FSDR GUUA93857092210ASkin · damagedFLIGHT 5401 PILOT REPORTED BIRD STRIKE ON RIGHT WING. REMOVED DAMAGED SECTION OF SKIN AT RIGHT WING OUTBOARD LEADING WS 189.0 AND INSTALLED A DOUBLER REPAIR AND SKIN FILLER.Sep 22, 2010 · N81538 · Beech 1900DSDR REXA201000154Skin · dentedDENT (6.5" LX 5.5" W X 0.380" DEEP) TO RT WING FIXED LEADING EDGE (PIN: 601R120161-4 REF) BETWEEN WS 131.80-WS 139.54 DUE TO A BIRD STRIKE. NO DAMAGE TO FASTENERS OR UNDERLYING STRUCTURE. TEMPORARY REPAIR IAW SRM 57-41-31 AND SRM 51-12-00. GOOD TO NEXT C CHSep 22, 2010 · N8694A · Cndair CL6002B19SDR IXXA10SMN091SSkin · crackedDURING ROUTINE C-CHECK INSP FOUND LT WING NR 2 STUB WING LOWER SKIN CRACKED AT STA XFS 200.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED SPLICE DOUBLER AND NEW SKIN. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. Sep 21, 2010 · N606AL · Doug DC873FSDR IPXA10M63019Skin · chafedINSPECTION TYPE:1C, LT WING FIXED L/E AT NR 3 SLAT ANTI-ICE DUCT CUT OUT DOUBLER HAS CHAFE DAMAGE 2 PLACES (INBD AND OTBD OF ANTI-ICE DUCT). REMOVED EXISTING REPAIR FROM LT WING FIXED L/E AT ANTI-ICE DUCT BETWEEN XOS464-XOS470, CUT OUT DAMAGE AT STA XOS470 WSep 21, 2010 · N257UP · Doug MD11FSDR ABXA201009200122Panel · missingAIRCRAFT EXPERIENCED A PART DEPARTING THE AIRCRAFT EVENT. CREW REPORTED HEARING A LOUD BANG AT 12,000 FT. COMPOSITE PANEL P/N 561QB TRAILING EDGE PANEL JUST FORWARD OF LT AILERON HAD 75 SCREWS MISSING OF 104. PANEL MEASURES 14 X 46 AND IS COMPLETELY MISSINGSep 20, 2010 · N798AX · Boeing 767281SDR IPXA10M62925Skin · crackedINSPECTION TYPE:1C, RT WING FIXED L/E SLAT TRACK NR 14 DOOR WING CUT OUT FOUND WITH SUSPECTED CRACK AS MARKED. REMOVED DAMAGE ON RT WING FIXED L/E AT SLAT TRACK NR 14. FABRICATED DOUBLER AND FILLER AND INSTALLED REF SRM 57-40-02, FIG 201, REPAIR 7.Sep 19, 2010 · N257UP · Doug MD11FSDR DALA1023269886Panel · chafedDURING H-CHECK, FOUND CHAFING IN LT WING T/E PANEL 1523A LOWER SURFACE. REPAIRED IAW SRM 51-10-2, SRM 51-10-3 TABLE 1.Sep 17, 2010 · N600TR · Doug DC951SDR FDEA201009173529Skin · corrodedRT WING TOP SKIN SURFACE FRONT SPAR AREA SKIN IS CORRODED FROM RIB 17 - RIB 18. REMOVED 5 EA FASTENERS RT WING TOP SKIN UPPER SURFACE FRONT SPAR BETWEEN RIB 17 AND RIB 18. BLENDED CORROSION IAW SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PGS 13Sep 17, 2010 · N803FD · Airbus A310324SDR FDEA201009173528Skin · corrodedLT WING TOP SKIN SURFACE IS CORRODED AT THE REAR SPAR AREA FROM RIB 4 - RIB 5. REMOVED 2 EA FASTENERS LT WING TOP SKIN UPPER SURFACE REAR SPAR BETWEEN RIB 17 AND RIB 18 IAW SRM 51-40-21. BLENDED CORROSION IAW SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM Sep 17, 2010 · N803FD · Airbus A310324SDR FDEA201009173527Skin · corrodedLT WING TOP SKIN SURFACE IS CORRODED 2 EA PLACES AT THE REAR SPAR AREA FROM RIB 12 - RIB 13. REMOVED CORROSION IAW SRM 57-00-00, PG 212 AT THE LT WING TOP SKIN UPPER SURFACE T/E BETWEEN RIBS 12-13. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PGS 9 & 111. Sep 17, 2010 · N803FD · Airbus A310324SDR FDEA201009173525Skin · corrodedLT WING TOP SKIN SURFACE IS CORRODED AT THE REAR SPAR AREA FROM RIB 15-RIB 16. REMOVED CORROSION ; LT WING TOP SKIN T/E AREA BETWEEN RIBS 15-16 IAW SRM 57-20-12, PG 9. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PGS 9 & 111. TOOL T8285D. FLAP PEENED AREA IASep 17, 2010 · N803FD · Airbus A310324SDR IXXA10SMN086SDoubler · crackedDURING ROUTINE C-CHECK INSP FOUND LT WING NR 2 STUB WING EXTERNAL LOWER REPAIR DOUBLER CRACKED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED DOUBLER. FABRICATED EXTERNAL AND INTERNAL DOUBLERS. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMESep 16, 2010 · N606AL · Doug DC873FSDR ZZDA2010425Skin · damagedLEFT WING INBOARD LEADING EDGE, DAMAGED. ACCOMPLISHED LEADING EDGE DOUBLER AND FILLER REPAIR PER EA 37-57-02795IR. SEE NR 1634098-1.Sep 16, 2010 · N276AT · Boeing 73776NSDR FDEA201009163505Skin · corrodedRT WING TOP SKIN UPPER SURFACE, SKIN IS CORRODED FROM RIB 10 TO RIB 11. REMOVED FASTENER RT WING TOP SKIN UPPER SURFACE REAR SPAR BETWEEN RIB 10 AND RIB 11. BLENDED CORROSION IAW SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PGS 13 & 110. FLAP Sep 16, 2010 · N803FD · Airbus A310324SDR FDEA201009163504Skin · corrodedRT WING TOP SKIN UPPER SURFACE, REAR SPAR AREA SKIN IS CORRODED FROM RIB 4 TO RIB 5. REMOVED 2 EA FASTENERS RT WING TOP SKIN UPPER SURFACE AT REAR SPAR IAW SRM 51-40-21. BLENDED CORROSION IA SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PGS 13 &Sep 16, 2010 · N803FD · Airbus A310324SDR FDEA201009163503Skin · corrodedRT WING TOP SKIN UPPER SURFACE, REAR SPAR AREA SKIN IS CORRODED FROM RIB 23 TO RIB 24. REMOVED FASTENER RIGHT WING TOP SKIN UPPER SURFACE REAR SPAR BETWEEN RIB 23 AND RIB 24. BLENDED CORROSION IAW A310-300 SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM 5Sep 16, 2010 · N803FD · Airbus A310324SDR FDEA201009163502Skin · crackedLT WING BOTTOM SKIN LOWER SURFACE T/E AREA SKIN IS CRACKED FROM RIB 11 TO RIB 12. COMPLIED WITH EA 6-5730-136705.Sep 16, 2010 · N803FD · Airbus A310324SDR ASOA201001816Panel · chafedPANEL 622CB CHAFED ON L/E (MARKED) RESOLVED ON W/O: 173017 TASKCARD: N/R-00312. BLENDED OUT CHAFING ON L/E PANEL 622CB ALL WORK DONE IAW CRJ700 SRM 57-12-00-001-001-A01. BLENDED AREA REQUIRE NDT. RECEIVED NEW PANEL, LOCATED HOLES AND TRIMMED IAW CRJ700 SRMSep 15, 2010 · N710EV · Cndair CL6002C10SDR IPXA10M62870Doubler · crackedINSPECTION TYPE:2C, RT WING L/E WEB HAS CRACK AT 3 EA RIVET MOUNTING HOLE ACCESS THROUGH PANEL 619DB. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW MD-11 SRM 57-40-02, REPAIR 9 FIG. 203Sep 15, 2010 · N273UP · Doug MD11FSDR IPXA10M62869Doubler · crackedINSPECTION TYPE:2C, LT WING L/E COMPARTMENT HAS A CRACK AT FASTENER ON CEILING DOUBLER AT XOS 627. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW SRM 57-40-02, REPAIR 9, FIG 203.Sep 15, 2010 · N273UP · Doug MD11FSDR VNAA2010092200006Skin · dentedAT CLT, CREW REPORTED A BIRD STRIKE ON THE LEFT WING LEADING EDGE. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE LEFT WING MIDDLE LEADING EDGE AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Sep 15, 2010 · N213PS · Cndair CL6002B19SDR QXEA2010092000544Panel · leakingWHILE REFUELING TO AN ALMOST FULL FUEL LOAD FOR TANKERING (10,500 LBS), FUEL BEGAN LEAKING FROM THE RT WING (ON TOP) SPILLING DOWN THE FRONT, INBD OF THE NR2 ENG NACELLE. INSPECTED AND FOUND FUEL PANEL 622BT LEAKING FUEL ONLY DURING PRESSURE REFUELING OPERATIOSep 15, 2010 · N424QX · Bombdr DHC8402
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