# Service difficulty reports: N68043, cancelled May 31, 2018 A list on [N68043, cancelled May 31, 2018](https://openairdocs.org/deregistered/N68043-2018-05-31.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 3 · 102 reports - [SDR RRXA010011](https://openairdocs.org/sdr/RRXA010011.md): Wire · damaged · Feb 13, 2001 · N68043 · Doug DC1010F · Engine Starting System Wiring > DURING TAKEOFF ROLL, NR 3 ENGINE START LIGHT CAME ON AND STAYED ON AFTER ENGINE SHUT DOWN. REPAIRED WIRING AT PRESSURE FEED THROUGH ON NR 3 ENGINE STARTER VALVE SYSTEM OP CHECKS GOOD IAW DC-10 M/M CHAPTER 74-00-01. - [SDR RRXA001099](https://openairdocs.org/sdr/RRXA001099.md): Valve · failed · Dec 22, 2000 · N68043 · Doug DC1010F · Airfoil Anti/De-ice System > WHEN WING ANTI-ICE IS TURNED ON - RIGHT 1506 VALVE DISAGREE LIGHT COMES ON WITH NO DROP IN PNEU PRESS FEFI CODE 30-11-00. REMOVED AND REPLACED RIGHT WING ANTI-ICE VALVE IAW M/M 30-00-00. OPS OK ON CHECK. - [SDR RRXA000999](https://openairdocs.org/sdr/RRXA000999.md): Computer · failed · Jun 17, 2000 · N68043 · Doug DC1010F · Stall Warning System > ON TAKEOFF STICK SHAKER ACTIVATED AND AUTO SLAT EXTEND ACTIVATED WITH SLAT RESET LIGHT ON. RAN CK LIST, NO HELP. COULD NOT RESET SLATS, RESET STICK SHAKER CB'S, NO HELP. SLATS REMAINED IN AUTO EXTEND POSITION. REMOVED AND REPLACED AT/SC NR 2 COMPUTER STICK - [SDR CALA9900857](https://openairdocs.org/sdr/CALA9900857.md): Skin · delaminated · Jul 23, 1999 · N68043 · Doug DC1010 · Horizontal Stabilizer, Plate/Skin > INSPECTION FOUND THREE AFT T/E PANELS DELAMINATED FROM I/B HINGE POINT TO HORIZONTAL TIP AT LOWER RIGHT HORIZONTAL STABILIZER. THE THREE PANELS WERE REMOVED AND REPLACED IAW MM 51-31-01. - [SDR CALA9900833](https://openairdocs.org/sdr/CALA9900833.md): Panel · corroded · Jul 16, 1999 · N68043 · Doug DC1010 · Vertical Stabilizer, Plate/Skin > INSPECTION FOUND VERTICAL STABILIZER L/E PANEL THIRD FROM THE BOTTOM CORRODED. THE CORROSION WAS REMOVED IAW EA 10-5533-2-A0440 AND ECRA 5533-01001. - [SDR CALA9900832](https://openairdocs.org/sdr/CALA9900832.md): Panel · corroded · Jul 16, 1999 · N68043 · Doug DC1010 · Horizontal Stabilizer, Plate/Skin > INSPECTION FOUND RT HORIZONTAL STABILIZER MOST I/B UPPER L/E AFT SECTION CORRODED UNDER SKIN. REMOVED ACCESS PANEL DOUBLER AND SPLICES. DOUBLERS AND PANEL WERE INSTALLED IAW ECRA 5530-01245 AND SRM 51-31-01. - [SDR CALA9900831](https://openairdocs.org/sdr/CALA9900831.md): Panel · delaminated · Jul 16, 1999 · N68043 · Doug DC1010 · Wing, Plate/Skin > INSPECTION FOUND LT WING UPPER NR 4 PANEL DELAMINATED. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-31-01 AND WO 99-0659. - [SDR CALA9900830](https://openairdocs.org/sdr/CALA9900830.md): Panel · corroded · Jul 16, 1999 · N68043 · Doug DC1010 · Wing, Plate/Skin > INSPECTION FOUND RT WING UPPER NR 6 PANEL CORRODED ON L/E MID PORTION. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-31-01, 51-71-00 AND WO 99-0657. - [SDR CALA9900829](https://openairdocs.org/sdr/CALA9900829.md): Panel · corroded · Jul 16, 1999 · N68043 · Doug DC1010 · Wing, Plate/Skin > INSPECTION FOUND RT WING UPPER NR 4 PANEL CORRODED AT THE CENTER OF THE PANEL. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-31-01 AND WO 99-0660. - [SDR CALA9900828](https://openairdocs.org/sdr/CALA9900828.md): Longeron · corroded · Jul 16, 1999 · N68043 · Doug DC1010 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND PILLOWING CORROSION AT LONGERON 49L JUST FORWARD OF ADF DOUBLER AT STA 959. REPAIRED LONGERON 49L IAW SRM 53-10-00, FIGURE 2. - [SDR CALA9900827](https://openairdocs.org/sdr/CALA9900827.md): Panel · delaminated · Jul 16, 1999 · N68043 · Doug DC1010 · Horizontal Stabilizer, Plate/Skin > INSPECTION FOUND LT HORIZONTAL STABILIZER THIRD T/E PANEL FROM FUSELAGE GOING OUTBOARD ON LOWER SURFACE DELAMINATED. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-31-01AND WO 99-0653. - [SDR CALA9900826](https://openairdocs.org/sdr/CALA9900826.md): Panel · delaminated · Jul 16, 1999 · N68043 · Doug DC1010 · Horizontal Stabilizer, Plate/Skin > INSPECTION FOUND RT UPPER HORIZONTAL STABILIZER 4TH T/E UPPER AFT PANEL FROM FUSELAGE DELAMINATED. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-31-01 AND WO 99-0648. - [SDR CALA9900825](https://openairdocs.org/sdr/CALA9900825.md): Panel · delaminated · Jul 16, 1999 · N68043 · Doug DC1010 · Horizontal Stabilizer, Plate/Skin > INSPECTION FOUND LT HORIZONTAL STABILIZER 4TH T/E PANEL FROM FUSELAGE GOING O/B DELAMINATED. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-31-01 AND WO 99-0651 AND TRAVELER 105996. - [SDR CALA9900824](https://openairdocs.org/sdr/CALA9900824.md): Panel · delaminated · Jul 16, 1999 · N68043 · Doug DC1010 · Wing, Plate/Skin > INSPECTION FOUND LT WING LOWER PANEL NR 2 DELAMINATED. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-31-01 AND WO 99-0643. - [SDR CALA9900823](https://openairdocs.org/sdr/CALA9900823.md): Panel · delaminated · Jul 16, 1999 · N68043 · Doug DC1010 · Wing, Plate/Skin > INSPECTION FOUND RT WING UPPER NR 7 PANEL DELAMINATED AT I/B EDGE. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-31-01 AND WO 99-0644. - [SDR CALA9900822](https://openairdocs.org/sdr/CALA9900822.md): Panel · delaminated · Jul 16, 1999 · N68043 · Doug DC1010 · Wing, Plate/Skin > INSPECTION FOUND RT WING LOWER PANEL NR 1 DELAMINATED AT TRAILING EDGE. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW MM 51-31-01, 51-71-00 AND WO 99-0645. - [SDR CALA9900809](https://openairdocs.org/sdr/CALA9900809.md): Strip · corroded · Jul 8, 1999 · N68043 · Doug DC1010 · Horizontal Stabilizer Structure > INSPECTION FOUND LEFT HORIZONTAL STABILIZER UPPER MOST I/B L/E ACCESS STRIP CORRODED ON O/B EDGE. THE ACCESS STRIP WAS REPAIRED IAW ECRA 5513-01003. - [SDR CALA9900808](https://openairdocs.org/sdr/CALA9900808.md): Spar · corroded · Jul 8, 1999 · N68043 · Doug DC1010 · Wing Spar > INSPECTION FOUND LEFT WING I/B FALSE SPAR UPPER CAP CORRODED O/B OF SPAR INNER MOST END AT XW 158. THE CORROSION WAS REMOVED AND FALSE SPAR WAS REPAIRED IAW ECRA 5722-01004. - [SDR CALA9900807](https://openairdocs.org/sdr/CALA9900807.md): Spar Cap · corroded · Jul 8, 1999 · N68043 · Doug DC1010 · Wing Spar > INSPECTION FOUND LOWER SPAR CAP CORRODED AT RT WING O/B T/E AILERON CAVITY AT STA XW 802.5 TO XW 895.5. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5710-01962. - [SDR CALA9801454](https://openairdocs.org/sdr/CALA9801454.md): Skin · cracked · Aug 14, 1998 · N68043 · Doug DC1010 · Vertical Stabilizer, Plate/Skin > INSPECTION FOUND A 1 CRACK IN LOWER VERTICAL STABILIZER SKIN (NR 2 ENGINE INTAKE DUCT). THE AREA WAS REPAIRED IAW ECRA 5530-01213 AND A DIP WAS ISSUED TO PERFORM A VISUAL INSPECTION OF THE REPAIR IAW PART 2 OF ECRA 5530-01213 AT EVERY C CHECK. - [SDR CALA9801453](https://openairdocs.org/sdr/CALA9801453.md): Floorbeam · cracked · Aug 14, 1998 · N68043 · Doug DC1010 · Fuselage Main, Floor Beam > INSPECTION FOUND A 2 CRACK IN FLOORBEAM AT STA 1289 ADJACENT TO L-3 DOOR THRESHOLD. THE CRACKED AREA WAS TRIMMED OUT. A NEW FLOORBEAM SECTION WITH SPLICE CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01. - [SDR CALA9801432](https://openairdocs.org/sdr/CALA9801432.md): Axle Sleeve · broken · Aug 9, 1998 · N68043 · Doug DC1010 · Main Landing Gear Strut/Axle/Truck > INSPECTION FOUND LT MLG NR 2 AXLE SLEEVE LOCK KEY BROKEN. THE NR 2 AXLE SLEEVE WAS REMOVED AND REPLACED IAW CMM 32-12-01. - [SDR CALA9801431](https://openairdocs.org/sdr/CALA9801431.md): Seat Track · corroded · Aug 9, 1998 · N68043 · Doug DC1010 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND SEAT TRACK CORRODED AT STA 824, RBL 70. THE CORRODED AREA WAS TRIMMED AND BLENDED OUT. STRAP AND FILLER WERE USED TO REINFORCE THE AREA IAW SRM 53-70-00, FIGURE 18. - [SDR CALA9801387](https://openairdocs.org/sdr/CALA9801387.md): Web · cracked · Aug 5, 1998 · N68043 · Doug DC1010 · Wing Miscellaneous Structure > INSPECTION FOUND CRACKS IN CENTER WING BOX WEBS AT STA XCWR46, XCWL46, XCWR17, AND XCWL18. ALL CRACKS WERE TRIMMED AND BLENDED OUT. REWORKED AREAS AND REINFORCED WITH DOUBLERS AND FILLERS IAW SRM 57-00-01, FIGURE 1, 51-21-03, AND 51-30-02. - [SDR CALA9801386](https://openairdocs.org/sdr/CALA9801386.md): Flange · corroded · Aug 4, 1998 · N68043 · Doug DC1010 · Fuselage Miscellaneous Structure > INSPECTION FOUND CORROSION ON CAC LOWER FLANGE AT STA 1129 BETWEEN LONGERON 50L AND 50R. THE CORRODED AREA WAS CLEANED. THE AREA WAS REWORKED AND REINFORCED WITH TWO FRAME SPLICES IAW SRM 53-30-00, FIGURE 5, 51-21-01, AND 51-31-01. - [SDR CALA9800905](https://openairdocs.org/sdr/CALA9800905.md): Sensor · inoperative · May 21, 1998 · N68043 · Doug DC1010 · Autopilot System > THE AIRCRAFT PITCHED UP RAPIDLY WITH NR 1 AUTOPILOT ENGAGED WHILE IN CLIMB AT APPROXIMATELY 31,000 FEET AFTER DEPARTURE. THE CAPTAIN COUNTERED THE AFT YOKE MOTION AND DISENGAGED AUTOPILOT. THE AIRCRAFT WAS IN TRIM WITH AUTOTHROTTLES STABLE IN N1 AND CLIMB PO - [SDR CALA9701298](https://openairdocs.org/sdr/CALA9701298.md): Wedge · cracked · Aug 19, 1997 · N68043 · Doug DC1010 · Elevator Structure > INSPECTION FOUND A 12 INCH CRACK ON INBOARD END OF LT OUTBOARD ELEVATOR TRAILING EDGE WEDGE. THE TRAILING EDGE SECTION WAS REMOVED. A Z ANGLE SPLICE WAS FABRICATED. THE NEW WEDGE SECTION AND SPLICE WERE INSTALLED. THE WORK WAS PERFORMED IAW SRM 55-30-00 AND - [SDR CALA9701224](https://openairdocs.org/sdr/CALA9701224.md): Charger · inoperative · Aug 15, 1997 · N68043 · Doug DC1010 · Emergency Lighting > THE L-3 AND R-3 EMERGENCY EXIT SIGNS WOULD NOT ILLUMINATE. MAINTENANCE CHANGED BATTERY PACK, BUT EXIT SIGNS WERE STILL INOPERATIVE. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERATION OF THE LIGHTS CHECKED GOOD. - [SDR CALA9701309](https://openairdocs.org/sdr/CALA9701309.md): Spar · corroded · Aug 9, 1997 · N68043 · Doug DC1010 · Wing Spar > INSPECTION FOUND RT WING LOWER LEADING EDGE SPAR CORRODED AT STA 429.44 AND 484.51. THE AREAS WERE REPAIRED IAW ECRA 5710-01829. - [SDR CALA9701301](https://openairdocs.org/sdr/CALA9701301.md): Spar · gouged · Aug 5, 1997 · N68043 · Doug DC1010 · Wing Spar > INSPECTION FOUND A GOUGE IN THE NR 2 ENGINE FORWARD SPAR. THE GOUGE WAS BLENDED OUT. REPAIR STRAP AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-21-01 AND ECRA 5410-01451. - [SDR CALA9701297](https://openairdocs.org/sdr/CALA9701297.md): Stiffener · corroded · Aug 5, 1997 · N68043 · Doug DC1010 · Fuselage Miscellaneous Structure > INSPECTION HORIZONTAL STIFFENER AT BS 1521 CORRODED. THE CORRODED AREA WAS CUT OUT. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-21-01 AND ECRA 5300-01176. - [SDR CALA9701296](https://openairdocs.org/sdr/CALA9701296.md): Rib · cracked · Aug 5, 1997 · N68043 · Doug DC1010 · Wing, Rib/Bulkhead > INSPECTION FOUND SIX INCH CRACK IN WEBS OF CENTER WING BOX INTERNAL RIBS AT STATIONS XCW 17R AND XCW 17L. THE CRACKED AREAS WERE REMOVED. DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-33-01, 51-21-01, 57-00-21, AND ECRA 5710-01828. - [SDR CALA9701291](https://openairdocs.org/sdr/CALA9701291.md): Frame · corroded · Aug 4, 1997 · N68043 · Doug DC1010 · Fuselage Miscellaneous Structure > INSPECTION FOUND CENTER CARGO FORWARD CUTOUT FRAME AND SKIN CORRODED. THE CORRODED SKIN AND FRAME WERE REMOVED, REPAIR FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03539. - [SDR CALA9701288](https://openairdocs.org/sdr/CALA9701288.md): Web · cracked · Aug 4, 1997 · N68043 · Doug DC1010 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 2.5 INCH CRACK IN LT MAIN WHEEL WELL WEB AT STA 1505. A REPAIR WAS ACCOMPLISHED IAW ECRA 5350-01341. - [SDR CALA9701295](https://openairdocs.org/sdr/CALA9701295.md): Longeron · corroded · Aug 2, 1997 · N68043 · Doug DC1010 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND CORROSION ON VERTICAL AND UPPER HORIZONTAL FLANGE OF LONGERON 52 AT STA 1267 TO 1288. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW ECRA 5310-03538. - [SDR CALA9701294](https://openairdocs.org/sdr/CALA9701294.md): Beam · corroded · Aug 2, 1997 · N68043 · Doug DC1010 · Fuselage Miscellaneous Structure > INSPECTION FOUND CENTER CARGO DOOR SILL BEAM CORRODED. A REPAIR WAS ACCOMPLISHED IAW ECRA 5310-03530. - [SDR CALA9701285](https://openairdocs.org/sdr/CALA9701285.md): Skin · corroded · Aug 2, 1997 · N68043 · Doug DC1010 · Fuselage Main, Plate/Skin > INSPECTION FOUND LT FORWARD EXHAUST CUTOUT CORRODED AT STA 561. A DOUBLER AND TRIPLER WERE FABRICATED AND INSTALLED IAW ECRA 5300-01171. - [SDR CALA9701302](https://openairdocs.org/sdr/CALA9701302.md): Spar · corroded · Jul 31, 1997 · N68043 · Doug DC1010 · Wing Spar > INSPECTION FOUND LEFT WING SPAR CORRODED AT STA XORS 264 TO XORS 272. THE CORROSION WAS REMOVED IAW SRM 51-21-01. A REPAIR WAS INSTALLED IAW SRM 57-20-00 AND ECRA 5311-01033. - [SDR CALA9701287](https://openairdocs.org/sdr/CALA9701287.md): Longeron · corroded · Jul 30, 1997 · N68043 · Doug DC1010 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND LONGERON 45L CORRODED ON HORIZONTAL FLANGE AT STA 565. THE CORRODED SECTION OF LONGERON WAS REMOVED, LONGERON, FILLER, AND SPLICE ANGLES WERE FABRICATED AND INSTALLED IAW ECRA 5300-01177. - [SDR CALA9701315](https://openairdocs.org/sdr/CALA9701315.md): Longeron · corroded · Jul 28, 1997 · N68043 · Doug DC1010 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND LONGERON 48L CORRODED AT STA 1711-1857. THE LONGERON WAS REMOVED AND A NEW LONGERON AND SPLICE ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-00, 51-21-01, 51-33-01, AND 51-41-01. - [SDR CALA9701312](https://openairdocs.org/sdr/CALA9701312.md): Skin · corroded · Jul 28, 1997 · N68043 · Doug DC1010 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1741-1781, LONGERON 45L TO 48L. THE CORRODED SKIN WAS CUT OUT. SKIN, DOUBLER, TRIPLER, AND FINGER DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-20-00, 51-21-01, AND 51-33-01. - [SDR CALA9701311](https://openairdocs.org/sdr/CALA9701311.md): Longeron · corroded · Jul 28, 1997 · N68043 · Doug DC1010 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND LONGERON 43L CORRODED AT STA 1125. THE CORRODED SECTION OF LONGERON WAS REMOVED. A NEW SECTION OF LONGERON AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-00, 51-21-01, 51-33-01, AND 51-35-01. - [SDR CALA9701310](https://openairdocs.org/sdr/CALA9701310.md): Fitting · cracked · Jul 28, 1997 · N68043 · Doug DC1010 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 2 INCH CRACK IN LONGERON 42L END FITTING AT STA 1156. THE FITTING WAS REMOVED AND A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-31-01, 51-33-01, 51-21-01. - [SDR CALA9701293](https://openairdocs.org/sdr/CALA9701293.md): Skin · corroded · Jul 28, 1997 · N68043 · Doug DC1010 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1229 TO 1296, LONGERON 52. THE CORROSION WAS REMOVED AND A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND ECRA 5334-01000. - [SDR CALA9701292](https://openairdocs.org/sdr/CALA9701292.md): Panel · corroded · Jul 28, 1997 · N68043 · Doug DC1010 · Fuselage Miscellaneous Structure > INSPECTION FOUND MID LAV SERVICING PANEL CORRODED. THE LAV PANEL WAS REMOVED AND THE CORROSION WAS REMOVED, A DOUBLER, LONGERON SPLICES, AND SHEAR TIE WERE FABRICATED AND INSTALLED IAW SRM 51-21-01, 51-38-01, 51-31-01, 51-33-01, AND 51-35-01. - [SDR CALA9701270](https://openairdocs.org/sdr/CALA9701270.md): Fitting · corroded · Jul 28, 1997 · N68043 · Doug DC1010 · Fuselage Miscellaneous Structure > INSPECTION FOUND LONGERON END FITTING CORRODED AT STA 1156, LONGERON 47L. THE FITTING WAS REMOVED AND A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-21-01, 51-31-01, AND 51-33-01. - [SDR CALA9701269](https://openairdocs.org/sdr/CALA9701269.md): Fitting · cracked · Jul 28, 1997 · N68043 · Doug DC1010 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1.5 INCH CRACK IN LONGERON END FITTING AT STA 1156, LONGERON 40R. THE FITTING WAS REMOVED AND A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-33-01, 51-35-01, AND 51-21-01. - [SDR CALA9701314](https://openairdocs.org/sdr/CALA9701314.md): Longeron · corroded · Jul 27, 1997 · N68043 · Doug DC1010 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND LONGERON 48L CORRODED AT STA 1701-1721. THE LONGERON WAS REMOVED AND A NEW LONGERON SPLICE WAS FABRICATED AND INSTALLED IAW SRM 51-33-01. - [SDR CALA9701313](https://openairdocs.org/sdr/CALA9701313.md): Longeron · corroded · Jul 27, 1997 · N68043 · Doug DC1010 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND LONGERON 47L CORRODED AT STA 1761 TO 1793. THE LONGERON WAS REMOVED AND A NEW LONGERON WAS FABRICATED AND INSTALLED IAW SRM 51-33-01 AND 51-21-01. - [SDR CALA9701306](https://openairdocs.org/sdr/CALA9701306.md): Skin · corroded · Jul 27, 1997 · N68043 · Doug DC1010 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1811-1880, LONGERON 36L TO 48L. THE CORRODED SKIN WAS CUT OUT AND NEW SKIN WAS INSTALLED USING SPLICE DOUBLER, TRIPLER, AND FINGER DOUBLERS PER SRM 53-20-00, 51-33-01, AND 51-35-01. Next page: https://openairdocs.org/deregistered/N68043-2018-05-31/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 n_number = 'N68043' AND deregistration_id = 'N68043-2018-05-31' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N68043-2018-05-31/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.