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 2011FA0000683Skin · crackedA CRACK OF APPROX 8-9 INCHES WAS FOUND IN UPPER INBD RT WING SKIN AND A 6-7 INCH CRACK FOUND IN UPPER INBD OF LT WING SKIN. THIS CRACK WAS LOCATED ON INTERIOR SIDE OF BOTH WING NACELLE LOCKERS, UNDERNEATH THE CARPET, AT INBD SIDE OF RIB WHICH SUPPORTS UPPER MOct 14, 2011 · N87397 · Cessna 310RSDR SWAA2013021312633Fairing · crackedNR 3 FLAP TRACK FIXED FIXED FAIRING I/B SIDE HAS CRACK MOD. NR 3 FLAP TRACK FAIRING CRACKED ON INBOARD SIDE, REPAIRED IN ACCORDANCE WITH EA 1-A57-0553. REMOVED AND RE-INSTALLED ACCESS PANEL FWD OF NR 3 FLAP TRACK FAIRING IAW IAW SRM 51-40-02.Oct 13, 2011 · N660SW · Boeing 737301SDR A6WA201141089Panel · chafedPANEL 699AB IS CHAFED. BLENDED DAMAGE ON PANEL 699AB IAW SRM 51-12-00, MAX DAMAGE LOSS .015 MAT REMAINING .046 WITHIN SERVICEABLE LIMITS IAW REO 601R-57-60-020.Oct 13, 2011 · N467AW · Cndair CL6002B19SDR A6WA2011741088Panel · chafedPANEL 699BB CHAFED, BLENDED DAMAGED ON PANEL 699BB IAW 51-12-00, MAX DAMAGE LOSS .010 MAX REMAINING .045 WITHIN LIMITS IAW REO 601R-57-60-020.Oct 13, 2011 · N467AW · Cndair CL6002B19SDR DALA1164485653Skin · dentedGOUGES LT WING LOWER SKIN BETWEEN STRINGERS 9 AND 10 AT WING STA 210 MARKED GOUGE-B. DAMAGE REPAIRED PER ERA 497012-14 REV ORIG.Oct 13, 2011 · N553NW · Boeing 757251SDR DALA1164475653Skin · dentedGOUGES - LT WING LOWER SKIN BETWEEN STRINGERS 10 AND 11 O/B OFWING STA 204.5. MARKED GOUGE-A. DAMAGE REPAIRED PER ERA 497012-14 REV ORIG.Oct 13, 2011 · N553NW · Boeing 757251SDR DALA1164465653Skin · dentedDENT- LT WING LOWER SKIN AT STRINGER 11 WING STA 200. MARKED DENT-A DAMAGE REPAIRED PER ERA 497012-14 REV ORIG.Oct 13, 2011 · N553NW · Boeing 757251SDR DALA1164455653Skin · dentedDENT - LT WING LOWER SKIN FWD OF STRINGER 10 WING ATA 207. MARKED DENT-B DAMAGE REPAIRED PER ERA 497012-14 REV ORIG.Oct 13, 2011 · N553NW · Boeing 757251SDR DALA1164445653Skin · dentedLOWER LT WING SKIN GOUGED WS 200 FWD OF STR 9. MARKED GOUGE-F DAMAGE REPAIRED PER ERA 497012-14 REV ORIG.Oct 13, 2011 · N553NW · Boeing 757251SDR DALA1164425653Skin · gougedLOWER LT WING SKIN GOUGED JUST AFT OF STR 13 AR WS 234. MARKED GOUGE C DAMAGE REPAIRED PER ERA 497012-14 REV ORIG.Oct 13, 2011 · N553NW · Boeing 757251SDR DALA1164415653Skin · gougedLOWER LT WING SKIN IS GOUGED FWD OF STR 13 AT WS 239. MARKED GOUGED DAMAGE REPAIRED PER ERA 497012-14 REV ORIG.Oct 13, 2011 · N553NW · Boeing 757251SDR DALA1164405653Skin · gougedLOWER WING SKIN IS GOUGED JUST FWD OF STR 12 AT WS 241. MARKED GOUGE-E DAMAGE REPAIRED PER ERA 497012-14 REV ORIG.Oct 13, 2011 · N553NW · Boeing 757251SDR DALA1164395653Skin · dentedDENT - LT WING LOWER SKIN AFT OF STRINGER 11 AT WING STA 218 MARKED DENT. DAMAGE REPAIRED PER ERA 497012-14 REV ORIG.Oct 13, 2011 · N553NW · Boeing 757251SDR IPXA11M70152Skin · crackedINSPECTION TYPE:2C LT WING FIXED L/E SKIN CRACKED AT INBD CORNER OF FUEL PANEL ACCESS DOOR. REPAIRED LT WING FIXED L/E EXTERIOR SKIN AT XOS610 IAW STA SA EA 011- 5730-01-A3571 REV IR AND EO MD11-5730-44928-A.Oct 13, 2011 · N275UP · Doug MD11FSDR IPXA11M70148Doubler · crackedINSPECTION TYPE:2C, RT WING FIXED L/E BEADED DOUBLER CRACK AROUND FASTENER HOLES AT XOS STA 731. ACCOMPLISHED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-B.Oct 13, 2011 · N275UP · Doug MD11FSDR IPXA11M70147Doubler · crackedINSPECTION TYPE:2C, RH WING FIXED L/E BEADED DOUBLER CRACK AROUND FASTENER HOLES AT XOS STA 701. ACCOMPLISHED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-B.Oct 13, 2011 · N275UP · Doug MD11FSDR IPXA11M70146Doubler · crackedINSPECTION TYPE:2C, RT WING FIXED L/E BEADED DOUBLER CRACKED AROUND FASTENER HOLES AT XOS 646. ACCOMPLISHED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-B.Oct 13, 2011 · N275UP · Doug MD11FSDR IPXA11570033Access Panel · corrodedINSPECTION TYPE:C-CK, RT WING FUEL ACCESS PANEL 642CB CORRODED AT MOUNT FLANGE. REPLACED ACCESS PANEL.Oct 13, 2011 · N448UP · Boeing 75724APFSDR UHLA2011101300339Skin · crackedAN 0.800" LONG CRACK ON RT WING UPPER SKIN AT RIB 10 SPAR II TRAILING EDGE. CUT OUT DAMAGE, HFEC IAW NDTM 51-00-00, FABRICATED FILLER IAW ETD2011-170-106477 USING PRINCIPLES OF ETD2011-170-02998. INSTALLED DOUBLER AND FILLER IAW SRM 51-43-02, SEAM SEALED ANDOct 13, 2011 · N654RW · Emb ERJ170100SESDR FDEA201110134466Skin · corrodedRT WING UPPER SKIN FUEL PORT CORROSION, EA F-5730-152526 PART 2, REV A COMPLIED WITH. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 13, 2011 · N939FD · Boeing 75723ASDR UIEA2011101300569Access Panel · crackedDURING WALK AROUND INSPECTION, MX REPORTED DAMAGE FOUND TO LT WING LOWER L/E PANEL FWD OF INBD FUELING ACCESS DOOR CRACK, MEASURING 3.0" LONG. (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS IAW SRM 51-10-02, INOct 13, 2011 · N419MC · Boeing 74748EFSDR IPXA1570061Access Panel · corrodedINSPECTION TYPE:C-CK, RT WING FUEL ACCESS PANEL 641DB HAS CORROSION ON THE SEALING SURFACE, REPLACED PANEL.Oct 10, 2011 · N448UP · Boeing 75724APFSDR IPXA11570032Access Panel · corrodedINSPECTION TYPE:C-CK, RT WING FUEL ACCESS PANEL 641KB CORRODED ON THE SEALING SURFACE. REPLACED ACCESS PANEL.Oct 10, 2011 · N448UP · Boeing 75724APFSDR IPXA11570010Access Panel · corrodedINSPECTION TYPE:C-CK, RT WING FUEL ACCESS PANEL NR 641MB HAS CORROSION ON THE SEALING SURFACE. R & R CORRODED ACCESS PANEL IAW SRM 57-20-01.Oct 10, 2011 · N448UP · Boeing 75724APFSDR IPXA11570008Access Panel · corrodedINSPECTION TYPE:C-CK. RT WING FUEL ACCESS PANEL 641LB HAS CORROSION ON THE SEALING SURFACE. REPLACED ACCESS PANEL.Oct 10, 2011 · N448UP · Boeing 75724APFSDR QXEA2011102101092Access Panel · corrodedFRETTING CORROSION ON LT WING FUEL TANK ACCESS PANEL 524BT. REMOVED CORROSION IAW RD 8/4/57/442. DETERMINED TO BE CRACK FREE. MIN REMAINING THICKNESS IS 0.121" WITHIN LIMITS. ALODINED PRIMED AND PAINTED AREA.Oct 10, 2011 · N403QX · Bombdr DHC8402SDR UALA2011101105492Skin · damagedSIGNS OF LIGHTNING STRIKE ON LT WING TIP UPPER AND LOWER AFT FAIRING SKIN PANEL ATTACHMENT SCREWS & REAR POSITION LIGHT LENS ASSY. REPAIRED FAIRING HOLES.Oct 10, 2011 · N220UA · Boeing 777222SDR VIB8101420110001Access Panel · corrodedREMOVED LT AND RT AUXILIARY FUEL TANK ACCESS COVERS FOR INSPECTION. FOUND CORROSION ON LT AND RT WING BONDED PANEL DISH FLANGES. RIGHT ACCESS COVER HAD SEVERE CORROSION AND WAS REPLACED WITH NEW. INSTALLED NEW GASKETS IAW RECOMMENDED SB 28-4059.Oct 10, 2011 · N503JM · Beech 200BEECHSDR QXEA2011101201001Skin · corrodedFUEL TANK CUTOUT 524BT LANDING HAS CORROSION. REMOVED CORROSION AND COMPLETED REPAIRS IAW RD 8/4-57-445.Oct 10, 2011 · N428QX · Bombdr DHC8402SDR IPXA1M70236Skin · chafedINSPECTION TYPE:4C, LT WING LOWER SURFACE SKIN L/E APPRX WS XOS 513-545 HAS CHAFE DAMAGE FROM CONTACT WITH SLAT. REPAIRED IAW EA 011-5730-01-A3566, REV IR AND EO MD11-5730-44847-A.Oct 9, 2011 · N286UP · Doug MD11FSDR QXEA2011101801062Access Panel · corrodedFUEL TANK CUTOUT 525AT LANDING HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. RIVETS CHECK GOOD AND AREA IS CRACK FREE. REMAINING THICKNESS IS .078" AND WITHIN LIMITES. PRIMED AREA.Oct 9, 2011 · N428QX · Bombdr DHC8402SDR WRLA20111009522Skin · crackedRT WING SKIN SURFACE L/E CRACKED. REPAIRED CRACK IAW EI W2011A57B-2156, REV 00 AND REV 01.Oct 9, 2011 · N272WA · Doug MD11SDR QXEA2011101200994Skin · corrodedFUEL TANK CUTOUT 524FT LANDING HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-445. COMPLETED REPAIRS IAW RD 8/4-57-445.Oct 9, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101201007Skin · corrodedFUEL TANK CUTOUT 624ET LANDING HAS CORROSION. REMOVED CORROSION AND COMPLETED REPAIRS IAW RD 8/4-57-445.Oct 9, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101201006Skin · corrodedFUEL TANK 624DT LANDING HAS CORROSION. REMOVED CORROSION AND COMPLETED REPAIRS IAW RD 8/4-57-445.Oct 9, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101201005Skin · corrodedFUEL TANK CUTOUT 624CT LANDING HAS CORROSION. REMOVED CORROSION AND COMPLETED REPAIRS IAW RD 8/4-57-445.Oct 9, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101201004Skin · corrodedFUEL TANK CUTOUT 624BT LANDING HAS CORROSION. REMOVED CORROSION AND COMPLETED REPAIRS IAW RD 8/4-57-445.Oct 9, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101201003Skin · corrodedFUEL TANK CUTOUT 624AT LANDING HAS CORROSION. REMOVED CORROSION AND COMPLETED REPAIRS IAW RD 8/4-57-445.Oct 9, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101201002Skin · corrodedFUEL TANK CUTOUT 524AT LANDING HAS CORROSION. REMOVED CORROSION AND COMPLETED REPAIRS IAW RD 8/4-57-445.Oct 9, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101201000Skin · corrodedFUEL TANK CUTOUT 524CT LANDING HAS CORROSION. REMOVED CORROSION AND COMPLETED REPAIRS IAW RD 8/4-57-445.Oct 9, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101200999Skin · corrodedFUEL TANK CUTOUT 524DT LANDING HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. COMPLETED REPAIR IAW RD 8/4-57-445.Oct 9, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101801074Access Panel · corrodedFUEL TANK PANEL 524FT HAS CORROSION. REMOVED CORROSION IAW R/D 8/4-57-442. CONFIRMED CRACK FREE. MINIMUM THICKNESS REMAINING IS 0.116" WHICH IS WITHIN LIMITS. ALODINE, PRIMED. INSTALLED INNER AND OUTER SEALS.Oct 8, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101801073Access Panel · corrodedFUEL TANK PANEL 524ET HAS CORROSION. REMOVED CORROSION IAW R/D 8/4-57-442. CONFIRMED CRACK FREE. MINIMUM THICKNESS REMAINING IS 0.121" WHICH IS WITHIN LIMITS. APPLIED ALODINE, PRIMED. INSTALLED INNER AND OUTER SEALS.Oct 8, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101801072Access Panel · corrodedFUEL TANK PANEL 524DT HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. CONFIRMED CRACK FREE. MINIMUM THICKNESS REMAINING IS 0.116" WHICH IS WITHIN LIMITS. ALODINE, PRIMED. INSTALLED INNER AND OUTER SEALS.Oct 8, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101801063Access Panel · corrodedFUEL TANK PANEL 525AT HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. CONFIRMED CRACK FREE. MINIMUM THICKNESS REMAINING IS 0.116" WHICH IS WITHIN LIMITS. APPLIED ALODINE, PRIMED. INSTALLED INNER AND OUTER SEALS.Oct 8, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101801071Access Panel · corrodedFUEL TANK PANEL 524CT HAS CORROSION. REMOVED CORROSION IAW Q400 RD 8/4-57-442. CONFIRMED CRACK FREE. MINIMUM THICKNESS REMAINING IS 0.225" WHICH IS WITHIN LIMITS. ALODINE, PRIMED. INSTALLED INNER AND OUTER SEALS.Oct 8, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101801070Access Panel · corrodedFUEL TANK PANEL 524BT HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. CONFIRMED CRACK FREE. REMAINING THICKNESS MIN 0.116" WHICH IS WITHIN LIMITS. ALODINE, PRIMED. INSTALLED INNER AND OUTER SEALS.Oct 8, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101801069Access Panel · corrodedFUEL TANK PANEL 524AT HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. CONFIRMED CRACK FREE. MINIMUM THICKNESS REMAINING 0.123" WHICH IS WITHIN TOLERANCE. ALODINE, PRIMED. INSTALLED INNER AND OUTER SEALS.Oct 8, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101801068Access Panel · corrodedFUEL TANK PANEL 624AT HAS CORROSION. REMOVED CORROSION IAW R/D 8/4-57-442. CONFIRMED CRACK FREE. MINIMUM THICKNESS REMAINING IS 0.118" WHICH IS WITHIN TOLERANCE. APPLIED ALODINE, PRIMER AND INSTALLED INNER AND OUTER SEALS.Oct 8, 2011 · N428QX · Bombdr DHC8402SDR QXEA2011101801064Access Panel · corrodedFUEL TANK PANEL 624ET HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. CONFIRMED CRACK FREE. MINIMUM THICKNESS REMAINING IS 0.117" WITH IS WITHIN LIMITS. APPLIED ALODINE, PRIMER AND INSTALLED INNER AND OUTER SEALS.Oct 8, 2011 · N428QX · Bombdr DHC8402
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