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 03FDEA01068Skin · corrodedMAIN DECK - BETWEEN BS 1215-1235, RIGHT XCW 50-115, CENTER WING UPPER PANEL STRUCTURE FOUND CORROSION. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5720-69361 WINGS - CENTER WING / UPPER FWD AND UPPER CENTER WING SKIN PANEL - CORROSION REWORK.Jun 25, 2003 · N582FE · Doug MD11SDR 03FDEA01069Skin · corrodedMAIN DECK - BETWEEN BS 1160-1170, RIGHT XCW 80-100, CENTER WING UPPER PANEL STRUCTURE FOUND CORROSION. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5720-69361 WINGS - CENTER WING / UPPER FWD AND UPPER CENTER WING SKIN PANEL - CORROSION REWORKJun 25, 2003 · N582FE · Doug MD11SDR 2003FA0000779Fabric · rottedWING FABRIC WAS FOUND TO BE ROTTED ALONG THE EDGE OF THE STRAIGHT EDGED FIBREGLASS SURFACE TAPE ON A TWO YEAR OLD FACTORY COVERED WING. THE PAINT PPG SYSTEM DELTA, SHOWS CRACKS ALONG THE EDGES OF ALL SURFACE TAPES ON THE TOP OF BOTH WINGS IN THE PROP ARC. THJun 24, 2003 · N8642V · Bbavia 7GCAASDR DHL2003873523Plate · corrodedRT OUTER WING OUTBD L/E PLATING CORRODED, XFS 710.000 - XFS 741.500 (UPPER SURFACE) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION FROM RT WING OUTBD L/E UPPER PLATING (STA XFS 710.000 -Jun 24, 2003 · N873SJ · Doug DC873FSDR DHL2003604603Fairing · delaminatedLT OTBD FAIRING ASSY WITH EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED OB FAIRING ASSY ON LT WING IAW SRM 51-3-0 PG 1, SRM 51-3-1 PG 2A. FOR OPS CHECK SEE NR 0531.Jun 22, 2003 · N604AL · Doug DC873FSDR UPS03840885Skin · crackedINSPECTION TYPE:C3 LEFT WING CENTER LE. LOWER SKIN IS CRACKED AT FASTENER HOLES AT XOLDI 6.225 STOP DRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087-B APPX. CJun 22, 2003 · N807UP · Doug DC873FSDR DHL2003604741Skin · corrodedLT WING INBD. L/E SLANT PANEL UPPER CAP SHOWS CORROSION FROM XFS.63.750 TO XFS.82.500 AND REPAIR DOUBLER FROM XFS.201.000 TO XFS.207.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-2-1 FIG.37, SRM 57-3-3 FIG.2. REMOVED CORROSION ON UPPER CAP IAW SRM 5Jun 20, 2003 · N604AL · Doug DC873FSDR DHL2003604724Skin · corrodedRT INNER WING LE SLANT PANEL UPPER CAP SHOWS CORROSION BETWEEN XFS.93.000 AND XFS.107.500, REPAIR DOUBLERS. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-2-1 FIG.37, SRM 57-3-3 FIG.2. REMOVED CORROSION ON UPPER CAP IAW SRM 51-1-8 PG.17-18. FOUND OUT OF LJun 20, 2003 · N604AL · Doug DC873FSDR DHL2003873517Panel · delaminatedLT WING T/E PANEL SHOWS INNER SKIN DELAMINATED 4.000, (XW0.000-XW97.000). REMOVED AND REPLACED LT WING T/E PANEL (XW0.000-XW97.000) IAW SRM 51-3-0 PG 1.Jun 19, 2003 · N873SJ · Doug DC873FSDR DHL2003873526Skin · corrodedLT WING CTR LE UPPER PLATING CORRODED, XS.466.651 - XS.442.115. PERFORMED MAJOR REPAIR IAW SRM 567-1-0 PG 1, SRM 57-3-30 PG 14, FIG 5. REMOVED CORROSION FROM CTR LE UPPER PLATING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. REMOVED CORJun 17, 2003 · N873SJ · Doug DC873FSDR DHL2003873520Skin · corrodedLT WING CENTER LE UPPER PLATING CORRODED AT XS.478.897 XW. 408.343. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 12, FIG 4. REMOVED CORROSION FROM CENTER LE UPPER PLATING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. REMOVJun 17, 2003 · N873SJ · Doug DC873FSDR DHL2003873518Skin · corrodedLT OUTER WING INBD L/E UPPER PART PLATING SHOWS CORROSION IN MANY POINTS BETWEEN XFS 560 AND XFS 710 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED INTERIM REPAIR. REMOVED CORROSION FROM INBD L/E UPPER PART PLATING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIJun 17, 2003 · N873SJ · Doug DC873FSDR UPS03840890Skin · crackedINSPECTION TYPE:C3 RIGHT WING OB. LE. LOWER SKIN IS CRACKED AT XFS 628 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER I.A.W. DC8-5720-4087-BJun 17, 2003 · N807UP · Doug DC873FSDR UPS03840889Skin · crackedINSPECTION TYPE:C3 RIGHT WING LE. LOWER SKIN IS CRACKED AT SCREWHOLE AT XFS 834 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED DOUBLER I.A.W. DC8-5720-4087-BJun 17, 2003 · N807UP · Doug DC873FSDR UPS03840887Doubler · crackedINSPECTION TYPE:C3 PRODUCTION SPLICE DOUBLER CRACKED AT XFS 710 ON RH WING LE. REMOVED,FABRICATED AND REPLACED DOUBLER I.A.W. DWG. 5769572,AND SRM. 51-1-21Jun 17, 2003 · N807UP · Doug DC873FSDR UPS03840891Access Panel · crackedINSPECTION TYPE: C3, RIGHT WING IB. AILERON LOWER ACCESS PANEL NR 541 CUTOUT IS CRACKED. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED DOUBLER IAW SRM. 57-2-0 FIG. 2H.Jun 16, 2003 · N807UP · Doug DC873FSDR DHL2003604734Plate · damagedLT INNER WING L/E AUX TANK UPPER PLATING SHOW HOLES FOR DOUBLER REMOVAL. PERFORMED MAJOR REPAIR IAW EODHL-030577, ED-3426. REMOVED ALL EVIDENCE OF CORROSION FROM REPAIRED AREA IAW SRM 51-1-8 PG 17-18. PLUGGED EXISTING HOLES WITH RIVETS IAW EODHL-030577, ED-Jun 15, 2003 · N604AL · Doug DC873FSDR QXEA200300743Skin · chafedPDX - RIGHT HAND WING BOTTOM TRAILING EDGE CHAFED. REPAIRED IAW MFG EA R-57-38 AND REO 670-57-51-012.Jun 14, 2003 · N608QX · Cndair CL6002C10SDR CALA0300314Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 4 SLAT ACTUATOR CUTOUT ON RT FIXED LEADING EDGE SKIN AT WBL 325. A DOUBLER WAS INSTALLED IAW SRM 57-41-01.Jun 14, 2003 · N70352 · Boeing 7373T0SDR DHL2003873500Skin · corrodedRT WING CTR L/E UPPER PLATING CORRODED STA XFS.460.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 12. REMOVED CORROSION FROM RT WING CTR L/E UPPER SKIN IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. REMOVED CORRODED SKIN Jun 13, 2003 · N873SJ · Doug DC873FSDR GTIA030547Panel · damagedFTW - FOUND RIGHT WING UPPER TRAPAZOIDAL PANEL HONEYCOMB COMPOSITE DAMGED AND DELAMINATED AT TWO PLACES 34 INCHES OUTBOARD OF FUSELAGE AND 7 INCHES AFT OF PANELS L/E. REMOVED RIGHT WING UPPER TRAPAZOIDAL PANEL. REPAIRED TWO EACH DELAMINATES. INSTALLED RIGHTJun 12, 2003 · N821NK · Doug DC982SDR GTIA030531Paint · crackedFTW - FOUND LEFT WING UPPER TRAILING EDGE TRAP PANEL PAINT CRACKED THROUGH OUT TOP COAT AND VISABLE TO COMPOSITE MATERIAL. REPAIRED DAMAGED AREAS. (M)Jun 12, 2003 · N821NK · Doug DC982SDR GTIA030530Panel · delaminatedFTW - FOUND LEFT WING UPPER FORWARD TRAP PANEL PAINT CRACK THROUGH OUT TOP COAT AND VISABLE TO COMPOSITE MATERIAL. FOUND LEFT WING UPPER FORWARD TRAP PANEL DELAMINATED. REPAIRED TWO DELAMINATES ON LEFT WING UPPER TRAP PANEL. (M)Jun 12, 2003 · N821NK · Doug DC982SDR DHL2003604654Skin · corrodedLT INNER WING CTR L/E LOWER PLATING SHOWS THREE INTERIM REPAIRS AND CORROSION AROUND STA XFS 304.000. REMOVED FASTENERS. REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT THE DAMAGED AREA, PERFORMED EDDY CURRENT INSPECTION. CLEANED, TREATED AND PRIMED ARJun 11, 2003 · N604AL · Doug DC873FSDR DHL2003604661Skin · corrodedRT WING CTR L/E LWR EXTERNAL SKIN SHOWS CORROSION, XFS 341.500. 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 PG 11-12. TRIMMED OUT DAMAGED SKIN SECTION IAW EODHL-030531, ED-3304. PERJun 8, 2003 · N604AL · Doug DC873FSDR DHL2003604573Skin · crackedLT WING OTBD SKIN SEGMENT FLAP PLATING CRACKED 2.00, XW 160.000 - XW 169.000. CUT OUT DAMAGED AREA AND FABRICATED SPLICE AND NEW SKIN SEGMENT IAW SRM 57-2-0 FIG 4. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED SPLICE AND NEW SKIN SEGMENT IAW SJun 6, 2003 · N604AL · Doug DC873FSDR QXEA200300718Doubler · chafedPDX - CHAFING ON DOUBLER AT OUTBOARD FLAP, LEFT HAND WING, INBOARD END, UPPER SIDE. REPAIRED IAW HORIZON AIR EA 6-57-141.Jun 6, 2003 · N408QX · Bombdr DHC8401SDR UPS03240965Skin · corrodedINSPECTION TYPE:C SUSPECT CORROSION ON FIXED L-EDGE SKIN UPPER AFT SURFACE AT 2 LOCATIONS LE STA 345 AND 340 APPROX RT. REPAIR CARRIED OUT IAW SMRO EO 2003-038-007. UPS ENGINEERING FILE NO. 727-57-20106Jun 5, 2003 · N940UP · Boeing 727185CSDR AUS20030555Skin · corroded(AUS) LT AND RT LOWER WING SKINS CORRODED IN AREA OF FUEL PUMP WATER SCAVENGE GUARDS AT RIB 15. FOUND DURING INSPECTION IAW ER BA6-28-10-7 AND ISB 28-028.Jun 4, 2003 · Bag BAE146300ASDR ASAA0310503Skin · chafedOKC - DURING SCHEDULED C-CHECK, FOUND THE LEFT WING LEADING EDGE AT WING STATION 505 CHAFED. REMOVED DAMAGED SECTION OF LEADING EDGE AND REPAIRED PER SRM. (M)Jun 2, 2003 · N746AS · Boeing 7372X6CSDR DHL2003604771Skin · corrodedRT INNER WING CTR EXTENDED L/E UPPER SKIN CORRODED AROUND STA XFS 354.000 - XFS 385.250. REMOVED FASTENERS. REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT THE CORRODED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATEDJun 1, 2003 · N604AL · Doug DC873FSDR QXEA200300699Skin · chafedCKB - RIGHT HAND WING FIXED LEADING EDGE CHAFED AT OUTBOARD END OF SLAT PANEL 1. REPAIRED IAW CRJ 700 SRM 51-25-01.May 31, 2003 · N604QX · Cndair CL6002C10SDR DHL2003604657Plate · dentedLT WING INBD FLAP LOWER PLATING HAS DENTS ON SEVERAL SPOTS BETWEEN STA XW 5.000 AND XW115.250. PERFORMED MAJOR REPAIR IAW EODHL-030568, ED-3293. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED DAMAGED SKIN PANEL IAW EODHL-030568, ED-3293. CLEANED, TREATED AMay 30, 2003 · N604AL · Doug DC873FSDR DHL2003604557Panel · delaminatedRT WING T/E LWR PANEL EXTERNAL SKIN DELAMINATED BETWEEN STA XRS 162.000 AND XF 219.000. REMOVED AND REPLACED RT WING T/E LWR PANEL (STA XRS 162.000 - XF 219.000) IAW SRM 51-3-0 PG 1.May 30, 2003 · N604AL · Doug DC873FSDR DHL2003604555Panel · delaminatedLT WING T/E LWR PANEL EXTERNAL SKIN DELAMINATED AT STA XRS 219.000. REMOVED AND REPLACED LT WING T/E LWR PANEL AT STA XFS 219.000 IAW SRM 51-3-0 PG 1.May 30, 2003 · N604AL · Doug DC873FSDR DHL2003604571Skin · delaminatedRT WING T/E LOWER PANEL EXT. SKIN DELAMINATED (NR 540 ACCESS) REMOVED AND REPLACED LOWER PANEL ON RT WING T/E (NR 540 ACCESS) IAW SRM 51-3-0 PG.1May 29, 2003 · N604AL · Doug DC873FSDR DHL2003604660Skin · corrodedLT WING CTR LE UPPER PLATING HAS CORROSION AND INTERIM REPAIR FROM STA XFS 341.500 TO XW 257.000). REMOVED INTERIM REPAIR AND FASTENERS. REMOVED CORROSION ON LT WING CTR L/E UPPER PLATING. FOUND OUT OF LIMITS. TRIMMED OUT THE CORROSION SKIN AREA IAW EO DHLMay 28, 2003 · N604AL · Doug DC873FSDR DHL2003604721Skin · corrodedLT WING CTR L/E UPPER PLATING HAS CORROSION AND INTERIM REPAIR FROM STA XFS 341.500 TO XW 257.000. REMOVED INTERIM REPAIR AND FASTENERS. REMOVED CORROSION ON LT WING CTR L/E UPPER PLATING, FOUND OUT OF LIMITS. TRIMMED OUT CORROSION SKIN AREA. PERFORMED EDDMay 28, 2003 · N604AL · Doug DC873FSDR DHL2003604556Panel · delaminatedLT WING T/E LOWER PANEL INTERNAL AND EXTERNAL SKIN DELAMINATED (NR 577B ACCESS). REMOVED AND REPLACED DELAMINATED LOWER PANEL ON LT WING T/E (NR 577B ACCESS) IAW SRM 51-3-0 PG 1.May 28, 2003 · N604AL · Doug DC873FSDR DHL2003604586Skin · corrodedLT INNER WING CENTER EXTENDED L/E UPPER SKIN CORRODED AROUND STA. XFS.341.500 TO XODI 6.2245. 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 PG.11-12. TRIMMED OUT CORRODED AREA. CLEANED, TMay 28, 2003 · N604AL · Doug DC873FSDR DHL2003604645Vane · damagedRT WING OB SLOT VANE OUTER PLATING SHOWS ELONGATED HOLES AT STA. XOLDI.6.224. PERFORMED MAJOR REPAIR IAW EODHL-030552, ED-3292. REMOVED FASTENERS. TRIMMED OUT THE ELONGATED HOLES SKIN AREA IAW EODHL-030552, ED-3292. CLEANED, TREATED AND PRIMED AREA IAW SRM 51May 27, 2003 · N604AL · Doug DC873FSDR DHL2003604754Skin · damagedRT WING EXTENDED L/E OTBD VANE HAS SEVERAL ELONGATED HOLES AND INTERIM REPAIR AT STA XOLDI 67.000. REMOVED FASTENERS, REMOVED EXISTING INTERIM REPAIR. TRIMMED OUT ELONGATED HOLES SKIN AREA. PERFORMED EDDY CURRENT INSPECTION. CLEANED, TREATED AND PRIMED AREMay 27, 2003 · N604AL · Doug DC873FSDR DHL2003604706Skin · corrodedLT OUTER WING OTBD L/E SHOWS CORROSION AT STA XW 761.000. REMOVED FASTENERS, REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUT THE DAMAGED SKIN AREA IAW EODHL-030547, ED-3313. PERFORMED NDT INSPECTION, CLEAMay 27, 2003 · N604AL · Doug DC873FSDR DHL2003604755Skin · damagedLT WING EXTENDED L/E INBD. VANE SHOWS ELONGATED HOLES AND INTERIM REPAIR AT STA. XS.247.000. PERFORMED MAJOR REPAIR IAW EODHL-030563, ED-3312. REMOVED FASTENERS AND EXISTING DOUBLER IAW SRM 51-1-21 PG.1. TRIMMED OUT DAMAGED AREA IAW EODHL-030563, ED-3312. PEMay 27, 2003 · N604AL · Doug DC873FSDR DHL2003604594Skin · corrodedLT OUTER WING OB L\E SHOWS CORROSION AT STA. XW.761.000. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. REMOVED CORROSION ON LT OUTER WING OB. L\E IAW SRM 51-1-8 PG.17-18. FOUND OUT OF LIMITS. TRIMMED OUT THE DAMAGED SKIN AREA IAW EODHL-030547, ED-3313. CLEANED, TREMay 27, 2003 · N604AL · Doug DC873FSDR CA030609002Seal · swollen(CAN) WHILE REMOVING FUEL LIDS TO ACCESS FUEL TANKS FOR SNAG RECERTIFICATION FOLLOWING MAJOR INSPECTION, IT WAS NOTICED THAT THE NEW LIGHTNING SEAL P/N CVR 67 THAT WAS INSTALLED IN THE LAST WEEK OR TWO HAD SWOLLEN ALMOST 50 PERCENT LARGER THEN ITS NORMAL SIZE May 27, 2003 · Dhav DHC7102SDR DHL2003604548Panel · delaminatedLT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED AT XRS 436.000. REMOVED AND REPLACED UPPER PANEL ON LT WING T/E AT XRS 436.000 IAW SRM 51-3-0 PG 1.May 26, 2003 · N604AL · Doug DC873FSDR DHL2003604723Skin · corrodedRT INNER WING UPPER SKIN CORRODED AROUND STA XRS 184.000 BETWEEN CTR SPAR AND S-9R. REMOVED FASTENERS, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. BLENDED OUT DAMAGED SKIN AREA IAW EODHL-030534, ED-3356. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-May 25, 2003 · N604AL · Doug DC873FSDR DHL2003604595Skin · corrodedRT INNER WING UPPER SKIN CORRODED AROUND STA XRS 184.000 BETWEEN CTR SPAR AND S-9R (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 57-2-0 PG 16. BLENDED OUT DAMAGED SKIN AREA IAWMay 25, 2003 · N604AL · Doug DC873FSDR DHL2003604598Skin · corrodedLT OUTER WING OTBD EXTENDED L/E OUTER PLATING LOWER SURFACE CORRODED AROUND STA XFS 710.000. REMOVED FASTENERS, REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT DAMAGED SKIN AREA. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREAMay 24, 2003 · N604AL · Doug DC873F
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