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 CA031205003Skin · damaged(CAN) DURING FTP STALLS, BUFFET WAS EXPERIENCED JUST PRIOR TO PUSHER ACTIVATION FOR BOTH THE CLEAN AND F20 STALLS. ADDITIONALLY A MILD LT WING DROP WAS EXPERIENCED ON THE F20 STALL. AFTER LANDING, SEALANT WAS OBSERVED TO HAVE SPREAD OUT OF THE LT WING LEADINGDec 1, 2003 · Cndair CL6002B19SDR COOSDR030158Skin · corrodedLT WING, LOWER SKIN, LOWER SURFACE, ACCESS DOOR CUTOUT CORRODED. (K)Dec 1, 2003 · N395AJ · Boeing 727233SDR CALA0300676Fairing · damagedTHE RT RED GEAR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION ON TAKEOFF. THE GEAR WAS CYCLED, BUT THE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT WAS DIVERTED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT I/B FLAP FAIRING HANGING BY FORWARNov 27, 2003 · N62631 · Boeing 737524SDR ASAA0380811Skin · crackedOKC - DURING 15K CHECK, FOUND RIGHT WING LEADING EDGE CRACKED. INSTALLED DOUBLER AND FILLER PER SRM 57-06 AND 51-10-3. (M)Nov 26, 2003 · N960AS · Doug DC983SDR 03FDEA01989Skin · crackedRIGHT WING NR 1 SLAT TRACK CUT OUT I/B SKIN FOUND CRACKED DURING I/B SLAT RIGGING CHECK. RT WING NR 1 SLAT TRACK CUT OUT I/B SKIN CRACK REPAIRED AS PER SRM 57-10-00 FIG 15 VOL1.Nov 26, 2003 · N583FE · Doug MD11SDR DHL2003742554Skin · crackedDURING C-CHECK, RT WING UPPER L/E SKIN WS 460 HAS CRACKS FROM RIVET ROW HOLES 3 PLACES. REMOVED FUELING RECEPTACLE MANIFOLD IAW B-727 MM 28-21-11. CUT OUT DAMAGED AREA, FABRICATED FILLER DIM 5.5 X 2.5 INCH FROM 2024 T3 .040 PO 900414 AND DOUBLER DIM 8 X 7 INNov 24, 2003 · N742DH · Boeing 727225SDR 03FDEA01964Panel · corrodedLEFT WING UPPER SURFACE O/B OF FUEL TANK PANEL 533 AT FOUND CORROSION. LT WING UPPER SURFACE O/B OF FUEL TANK PANEL 533 AT CORROSION REPAIRED AS PER FEDEX EA 1-5710-74260.Nov 21, 2003 · N583FE · Doug MD11SDR DHL2003802552Skin · corrodedLT OUTER WING OTBD EXTENDED L/E OUTER PLATING CORROSION DAMAGE AROUND STA XW 761.695 (MAJOR REPAIR). REMOVED FASTENERS. REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA INov 20, 2003 · N802DH · Doug DC873SDR CALA0300654Skin · corrodedINSPECTION FOUND RT WING LOWER T/E SKIN CORRODED AT REAR SPAR STA XRS 399-477. A SKIN DOUBLER WAS INSTALLED IAW ECRA 5731-01037.Nov 20, 2003 · N18835 · Doug DC982SDR TSAA0357211Skin · corrodedBLENDED OUT THE CORROSION, VERIFIED FREE USING 10X VISUAL INSPECTION. FLAT PEEN BLENDOUT AREA. DRILLED AND SPOTFACE FASTENER HOLE. COLD WORKED FASTENER HOLE. ALODINED AND TWO COATS BMS 10-79 TYPE III PRIMER TO BLEND AND SPOT FACE AREA. INSTALLED 1/32 INCHNov 19, 2003 · N818AL · Boeing 737230SDR ASAA0380797Doubler · crackedOKC - DURING 15K CHECK, FOUND LT WING LEADING EDGE SPLICE DOUBLER IS CRACKED AT STATION 120. INSTALLED SPLICE DOUBLER IAW SRM 51-30-2. (M)Nov 19, 2003 · N943AS · Doug DC983SDR TSAA0357216Panel · corrodedBLENDED OUT THE CORROSION TO A 20:1 RATIO. VERIFIED CORROSION FREE USING 10X VISUAL INSPECTION. REMOVED FASTENERS IN REPAIR AREA. FLAT PEEN BLENDOUT AREA. ALODINED AND TWO COATS BMS 10-20 TYPE II PRIMER TO BLEND AND SPOT FACE AREAS. INSTALLED 1/32 INCH OVNov 17, 2003 · N818AL · Boeing 737230SDR FE5F200300004Skin · crackedDURING SC12 CHECK, A 4.6250 INCHES LONG SPAN WISE CRACK IS REVEALED BETWEEN OSS 831.5 AND OSS 836 ON LT WING LEADING EDGE LOWER SURFACE SKIN. ACTION: REQUEST MFG ASSISTANCE AND IAW MFG'S RESPONSE, REPAIR THE CRACK.Nov 17, 2003 · Boeing 75729JSDR ASAA0380743Skin · crackedOKC - DURING 15K CHECK, FOUND RIGHT WING LEADING EDGE BETWEEN STATION XCW 121.688 AND XCW 104.500 CRACKED. REPAIRED PER SRM. (M)Nov 14, 2003 · N960AS · Doug DC983SDR UPS03841596Skin · crackedINSPECTION TYPE: C1, RT WING LE UPPER SKIN IS CRACKED AT XFS 304. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER I.A.W. SRM.57-2-1 FIG. 38Nov 13, 2003 · N718UP · Doug DC871FSDR DHL2003802507Skin · delaminatedLEFT WING T/E LOWER PANEL LOWER SKIN DELAMINATED STA XW 97.000 - XRS 162.000. REMOVED AND REPLACED LOWER PANEL ASSY ON LEFT WING T/E STA XW 97.000 XRS 162.000 IAW SRM 51-3-0 PG 1.Nov 13, 2003 · N802DH · Doug DC873SDR GTIA031055Panel · corrodedFTW - FOUND RIGHT WING PANEL 1242C HAS CORROSION 3 PLACES. FABRICATED NEW WING PANEL EA 5730-0311. (M)Nov 12, 2003 · N818NK · Doug DC981SDR AWXA200301433Skin · crackedMCN - MINOR REPAIR - DURING C-13 CHECK A .5 INCH CRACK WAS FOUND ON RT WING LEADING EDGE SKIN PANEL WS 0 TO WS 12. MAINTENANCE REMOVED CRACKED RT WING LEADING EDGE SKIN PANEL WS 0 TO WS 12; FABRICATED NEW REPLACEMENT SKIN PER DWG 65C26701; INSTALLED REPAIR PANov 9, 2003 · N307AW · Boeing 7373G7SDR HYI2003F00019Seal · unserviceableDURING FLIGHT, CREW NOTICED FUEL ESCAPING FROM RT UPPER ACCESS PANEL. ENGINES RUNNING NORMAL, EMERGENCY WAS DECLARED, LANDED WITHOUT INCIDENT. MECHANIC REMOVED AND REPLACED PANEL SEALS AND RELEASED AIRCRAFT BACK TO SERVICE.Nov 7, 2003 · N402VN · Cessna 402CSDR CALA0300624Skin · crackedINSPECTION FOUND A 6 INCH CRACK IN RT WING L/E SKIN PANEL AT WS 421.5. THE SKIN PANEL WAS REMOVED AND REPLACED IAW EA 5731-01010, OP 3.Nov 7, 2003 · N34131 · Boeing 757224SDR GTIA031030Panel · delaminatedFOUND RT WING INBOARD LOWER T/E PANEL CRACKED/DELAMINATED AT BOTTOM SIDE ABOVE RIGHT MLG. REMOVED RT WING INBOARD LOWER TRAP PANEL. REPAIRED CRACKED, DELAMINATED AREA. INSTALLED RT WING INBOARD LOWER T/E PANEL. (M)Nov 6, 2003 · N831NK · Doug DC983SDR DHL2003802519Skin · corrodedRIGHT WING CTR L/E UPPER SKIN CORRODED, STA XFS 330.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. TRIMMED OUT DAMAGED AREA IAW SRM 5Nov 6, 2003 · N802DH · Doug DC873SDR GTIA031029Skin · erodedFTW - FOUND RIGHT WING INBOARD FLAP LOWER SKIN BEHIND TIRES HAS LIGHT EROSION. REMOVED DAMAGED SKIN AT INBOARD FLAP REMOVAL PANEL. REMOVED CORRODED SKIN AT OUTBOARD FLAP REMOVAL PANEL. FABRICATED NEW SKIN PANELS. INSTALLED NEW SKIN ON INBOARD FLAP PANEL ATNov 5, 2003 · N831NK · Doug DC983SDR ZIAA03005Panel · corrodedYIP - PLANK NR 3 JUST AFT OF 2-3 PLANK SEAM CORROSION BETWEEN RISERS AT BL61R, CENTER DRY BAY, LOWER SURFACE. REMOVED CORROSION AND TREATED AREA. REPAIRED PER LOCKHEED S/B 678 DWG 841795. (M)Nov 3, 2003 · N346HA · Lkheed 188ASDR ZIAA03004Panel · crackedCRACK NOTED IN CENTER DRY BAY RIGHT WING AT PLANK SEAM 5-6 AT BL37R. ROUTED OUT CRACK AND INSTALLED FILLET PER L-188 SRM 51-2-7. REPAIRED PER L-188 SRM 57-2-1 FIG 3 SHEET 15. (M)Nov 3, 2003 · N346HA · Lkheed 188ASDR TSAA0353219Skin · corrodedFOUND LT UPPER WING SURFACE CORRODED BETWEEN FRONT & REAR SPAR IDENTIFIED ON FIGURES 1 THROUGH 6 AS NR 1 - 19 AT LOCATIONS, NR 1, 2, & 3 AT WBL 227, NR 4 AT WLB 228, NR 5 AT WBL 254, NR 6 AT WBL 264, NR 7 AT WBL 268, NR 8 AT WBL 234, NR 9 AT WBL 236, NR 10 AT Nov 2, 2003 · N824AL · Boeing 737282SDR TSAA0353218Skin · corrodedFOUND RIGHT UPPER WING SURFACE CORROSION BETWEEN THE FRONT AND REAR SPAR IDENTIFIED ON FIGURES 1 THROUGH 5 AS NR 1 TO NR 15 AT THE FOLLOWING LOCATIONS, NR 1 AT WBL 92.5, NR 2, 3, 4, 5 AND 6 BETWEEN WBL 198.6 AND WBL 227.0, NR 7 AND 8 AT WBL 157, NR 9 AND 10 BENov 2, 2003 · N824AL · Boeing 737282SDR GKZR200479904Skin · corrodedRIGHT WING UPPER SURFACE FROM WING ROOT TO STA 624 HAS NUMEROUS LOCATIONS OF EXFOLIATION RUNS FROM FRONT SPAR TO AFT SPAR. REMOVED CORROSION IAW DC8 SRM 51-1-8, NDT VERIFIED ALL WITHIN LIMITS. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FASTENERS IAW DNov 1, 2003 · N799AL · Doug DC862SDR AMWA115Plate · chafedWHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, THE RIGHT WING ROOT PRESSURE PLATE WAS FOUND TO HAVE A RIVET HEAD CHAFE.Oct 30, 2003 · N23YV · Beech 1900DSDR ABXA030441Skin · corrodedRIGHT WING UPPER SKIN CORRODED AND PULLED RIVETS JUST INBOARD OF SPOILER ACTUATOR. REPLACED SECTION OF STRINGER AND SPLICE IAW DC-9 SRM 51-70-5 AND 51-30-5.Oct 30, 2003 · N925AX · Doug DC914SDR A6WA200340152Skin · gougedRIGHT WING UNDERSIDE SKIN HAD NUMEROUS SCRATCHES AND GOUGES OUTBOARD OF WS 178 BETWEEN X163-X199. BLENDED AND SMOOTHED OUT DAMAGED AREAS, PERFORMED EDDY CURRENT INSPECTION OF AREAS, ALODINED PRIMED AND TOP COATED ALL BARE METAL IAW WVAC EO 601R-57-4317. (M)Oct 28, 2003 · N415AW · Cndair CL6002B19SDR AWXA200301410Doubler · crackedMCN - MINOR REPAIR - DURING C-13 CHECK A 1.3125 INCH CRACK WAS FOUND ON NR 6 FLAP TRACK FAIRING INNER DOUBLER AT AFT END WBL 191 RT. MAINTENANCE REMOVED CRACKED INNER DOUBLER AT WBL 191 RT; FABRICATED A NEW REPLACEMENT INNER DOUBLER; INSTALLED REPAIR PART IAWOct 28, 2003 · N307AW · Boeing 7373G7SDR AUS20031086Panel · debonded(AUS) LT WING LOWER SKIN PANEL DISBONDED.Oct 28, 2003 · Cessna 402CSDR AUS20031082Panel · debonded(AUS) RT UPPER WING PANEL SKIN DISBONDED.Oct 28, 2003 · Cessna 402CSDR AUS20031081Panel · debonded(AUS) LT WING UPPER SKIN PANEL DISBONDED.Oct 28, 2003 · Cessna 402CSDR AUS20031080Skin · debonded(AUS) LT WING LEADING EDGE SKIN DISBONDED.Oct 28, 2003 · Cessna 402CSDR AUS20031079Panel · debonded(AUS) RT LOWER WING PANEL DISBONDED.Oct 28, 2003 · Cessna 402CSDR AWXA200301413Skin · crackedMCN - MAJOR REPAIR - DURING C-13 CHECK .3125 INCH CRACK WAS FOUND ON LT WING LEADING EDGE SKIN ABOVE NR 2 SLAT OUTBOARD AUXILIARY TRACK. MAINTENANCE PERFORMED BOND REPAIR ON LT WING LEADING EDGE SKIN ABOVE NR 2 SLAT OUTBOARD AUXILIARY TRACK IAW B737-300 SRM 5Oct 26, 2003 · N307AW · Boeing 7373G7SDR 03FDEA01800Skin · crackedMEM MX REPORTS A 1.9 INCH CRACK IN THE RT LOWER WING SKIN AT RIB 11. ACCOMPLISHED WORK CARD T6-5610-66979 A PT3 AT CWF BY INSTALLING DOUBLER AT RIB 11 PER EA 6-571066979 PT 3 AND EA6-5710-73414A AND NRC S00025.Oct 24, 2003 · N442FE · Airbus A310203SDR 03FDEA01799Skin · crackedMEM MX REPORTS A .8 CRACK IN THE LT LOWER WING SKIN AT RIB 11. COMPLIED WITH WORK CARD T6-5710-66977 WRI 57105494 AT CWF BY INSTALLING NEW DOUBLER PER EA6-5710-66977 PT3 AND AIRBUS DRAWING R57249152 AND EA6-5710-73414A AND NRC S00002.Oct 24, 2003 · N442FE · Airbus A310203SDR EIA2003159Skin · corrodedFS 1050 LBL 119 CORROSION ON UPPER WING CENTER SECTION SKIN AT BUTT JOINT BLEND OUT OF LIMITS. REMOVED DAMAGED, NDT AREA, FABBED AND INSTALLED REPAIR ECRA 479-57-177-2Oct 21, 2003 · N479EV · Boeing 747132SDR A6WA200360057Skin · dentedLEFT AND RIGHT WING DENTED, SPOILERS AND T/E PANEL'S, MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1693-6830005. (M)Oct 20, 2003 · N183US · Bag BAE146200ASDR DHL2003807544Skin · corrodedLEFT WING OTBD INNER L/E EXTERNAL SKIN HAS CORROSION AT STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND REMOVED DAMAGED AREA. Oct 19, 2003 · N807DH · Doug DC873FSDR DHL2003807541Skin · corrodedRIGHT WING CENTER L/E UPPER SKIN CORRODED STA XFS 310.250 - XFS 335.250 XW 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT AND REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. FABRICAOct 19, 2003 · N807DH · Doug DC873FSDR DHL2003807542Skin · corrodedLEFT WING OUTBD L/E EXTERIOR SKIN CORRODED AT STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED AND REMOVED DAMAGEDOct 19, 2003 · N807DH · Doug DC873FSDR DHL2003807552Skin · corrodedLEFT WING OUTBD L/E EXTERIOR SKIN CORRODED AT STA XW 761.695 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF PERMISSIBLE LIMITS. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ASTAR ED EDU21-2, ASTAR DWG U21-R02. PERFOct 18, 2003 · N807DH · Doug DC873FSDR DHL2003807546Skin · corrodedRIGHT OUTBOARD STUB WING UPPER SKIN CORRODED, STA XFS 526.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED AND REMOVED DAMAGED AREA IAW ASTAR ED EDU21-7, ASTAR DWG U21-R07Oct 18, 2003 · N807DH · Doug DC873FSDR DHL2003807545Plate · corrodedRIGHT WING CENTER L/E OUTER PLATING LOWER PART HAS CORROSION AT STA 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ASTAR ED EDU 21-8, ASTAR DWG U21-R08. Oct 18, 2003 · N807DH · Doug DC873FSDR DHL2003807540Skin · corrodedRIGHT OUTER WING INBD L/E UPPER SKIN CORRODED XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED AND REMOVED DAMAGED AREAS IAW ASTAR ED EDU21-10, DWG U21-R10. PERFORMED NDT INSPECTION IAOct 18, 2003 · N807DH · Doug DC873FSDR DHL2003807539Plate · corrodedRT WING CTR L/E OUTER PLATING LOWER PART HAS CORROSION AROUND STA XFS 404.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT AND REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION IAW NDT STANDAOct 18, 2003 · N807DH · Doug DC873F
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