# Service difficulty reports: N14075, cancelled May 21, 2013 A list on [N14075, cancelled May 21, 2013](https://openairdocs.org/deregistered/N14075-2013-05-21.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 · 108 reports - [SDR WRLA2009062](https://openairdocs.org/sdr/WRLA2009062.md): Slide · malfunctioned · Feb 23, 2009 · N14075 · Doug DC1030 · Escape Slide > DURING LINE MAINTENANCE, R1 SLIDE WAS INADVERTENTLY DEPLOYED. SLIDE DID NOT DEPLOY CORRECTLY. - [SDR WRLA2009012](https://openairdocs.org/sdr/WRLA2009012.md): Unknown · fumes · Jan 17, 2009 · N14075 · Doug DC1030 · Air Distribution System > N3 PACKS PRODUCED FUMES IN CABIN. INSPECTED NR 3 ENG INLET AND EXHAUST, CHECKS OK. INSPECTED BREATHERS, CHECKS OK. CHECKED CHIP DETECTOR AND RAN ENG, CHECKS OK. - [SDR WRLA2008090](https://openairdocs.org/sdr/WRLA2008090.md): Cable · misrigged · Oct 22, 2008 · N14075 · Doug DC1030 · Passenger/Crew Doors > DURING MAINTENANCE L4 DOOR FAILED TO OPEN WITH DOOR ARMED, EMERGENCY MODE. REMOVED LININGS, RIGGED AIR RELEASE CABLE AND ARMING ROD IAW DC10 MM 52-12-00. OPS CHECK GOOD. SERVICED DOOR OPENING RESERVOIR IAW DC10 MM 52-12-00. REPLACED L4 DOOR AND SURROUND LI - [SDR WRLA2008106](https://openairdocs.org/sdr/WRLA2008106.md): Fairing · punctured · Sep 6, 2008 · N14075 · Doug DC1030 · Aerodynamic Fairings > FLIGHT 8010 09/06/08 KBWI/ETAR - DURING FLIGHT A THUMP WAS HEARD AND FELT 5 HOURS INTO FLIGHT AT FL310, NO ABNORMAL INDICATIONS OR HANDLING FOLLOWED. DURING POST FLIGHT INSPECTION, MAINTENANCE FOUND LT WING LDG EDGE WING/BODY FAIRING PUNCTURED AND CRACKED. R - [SDR WRLA2008051](https://openairdocs.org/sdr/WRLA2008051.md): Fitting · cracked · Jun 7, 2008 · N14075 · Doug DC1030 · Wing, Attach Fittings > DURING INSPECTION, MAINTENANCE FOUND FITTING CRACKED IN CENTER FUEL TANK I/B CORNER ABOVE ACCESS DOOR 141AZ. REMOVED AND REPLACED FITTING. (S) - [SDR WRLA2008052](https://openairdocs.org/sdr/WRLA2008052.md): Frame · corroded · Jun 6, 2008 · N14075 · Doug DC1030 · Fuselage Main, Frame > DURING INSPECTION, MAINTENANCE FOUND AFT FUSELAGE WASTE TANK COMPARTMENT CORROSION ON FRAME LOWER LEG 1967 LBL 6-10. REPAIRED IAW SRM 63-30-00 FIG 9 & 10 VOL 1. (S) - [SDR WRLA2008044](https://openairdocs.org/sdr/WRLA2008044.md): Slide · dislodged · Apr 14, 2008 · N14075 · Doug DC1030 · Escape Slide > L1 DOOR SLIDE DROPPED OUT WHEN DOOR OPENED PNEUMATICALLY, SLIDE DID NOT DEPLOY CORRECTLY. REMOVED AND REPLACED SLIDE ASSY IAW MM 25-61-01. SERVICED PNEUMATIC DOOR ASSIST. - [SDR WRLA2008043](https://openairdocs.org/sdr/WRLA2008043.md): Oven · malfunctioned · Apr 6, 2008 · N14075 · Doug DC1030 · Buffet/Galleys > EDDP/KBGR OVEN 609 AFT GALLEY ON FOR 5 MIN. THEN GRAY AND WHITE SMOKE BILLOWED OUT, SHUT OFF OVEN. ITEM PLACED ON DMI PER MEL 25-29-01 CAT C DUE 04/17/08. REMOVED AND REPLACED OVEN 609, DMI CLEARED 04/10/08. - [SDR WRLA2001129](https://openairdocs.org/sdr/WRLA2001129.md): Cable Assy · misrigged · Dec 1, 2007 · N14075 · Doug DC1030 · Passenger/Crew Doors > DURING MAINTENANCE INSPECTION L4 PASSENGER DOOR FAILED PNEUMATIC TEST. RIGGED AIR RESERVOIR AIR RELEASE CABLE PER DC10 AMM 52-12-00 PAGE 534. ADJUSTED L4 DOOR EMERGENCY BACKLOCK PER DC10 AMM 52-12-00 PAGE 530A. PERFORMED PNEUMATIC TEST OF THE L4 DOOR PER DC - [SDR WRLA2007078](https://openairdocs.org/sdr/WRLA2007078.md): Switch · locked · Jul 1, 2007 · N14075 · Doug DC1030 · Landing Gear Retraction/Extension System > RME/BWI CENTER GEAR TOOK 30 SEC TO RETRACT DID NOT EXTEND NORMALLY, EMERGENCY EXTENSION RELEASED. GEAR EXTENDED IN APPROXIMATLEY 15 SEC. FOUND CENTER GEAR SWITCH ON F/O PANEL LOCKED IN UP POSITION, RETURNED TO NORMAL. DEFLATED CENTER GEAR STRUT, CYCLED CENT - [SDR WRLA2007075](https://openairdocs.org/sdr/WRLA2007075.md): Support Fitting · corroded · May 30, 2007 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > DURING B-CHECK INSPECTION, CORROSION FOUND ON DIAMETER SUPPORT FITTING TIE BRACE ON LOWER INNER SURFACE IN CENTER LANDING GEAR WHEEL WELL RIGHT SIDE FS 1461. REPLACED SPLICE ANGLES AT FS 1461 PER SRM 51-33-01, SRM 53-14-01, SRM 53-00-01, SRM 51-21-01, SRM 51- - [SDR WRLA2007072](https://openairdocs.org/sdr/WRLA2007072.md): Longeron · corroded · May 29, 2007 · N14075 · Doug DC1030 · Fuselage Main, Longeron/Stringer > DURING B-CHECK INSPECTION, CORROSION FOUND ON LOWER END OF LONGERON IN CENTER GEAR W/W RIGHT SIDE AT FS 1461. REMOVED CORRODED LONGERON FROM CENTER GEAR WHEEL WELL. FABRICATED A REPLACEMENT LONGERON FROM 7075-T6 511 AND INSTALLED IAW DC-10 SRM 51-38-01 PG 17 - [SDR WRLA2007073](https://openairdocs.org/sdr/WRLA2007073.md): Stiffener · corroded · May 27, 2007 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > DURING B-CHECK INSPECTION, CORROSION FOUND ON LOWER AFT CORNER OF SUPPORT STRAP IN CENTER W/W RIGHT SIDE ABOVE AFT HINGE ON FWD GEAR DOOR AT FS 1442. REMOVED, FABRICATED, AND INSTALLED TEE STIFFENER IAW DC10 SRM VOL II 51-31-01 & 51-33-01. - [SDR WRLA2007074](https://openairdocs.org/sdr/WRLA2007074.md): Doubler · corroded · May 27, 2007 · N14075 · Doug DC1030 · Fuselage Main, Plate/Skin > DURING B-CHECK INSPECTION, CORROSION FOUND ON FWD LOWER CORNER OF UPPER CUTOUT SUPPORT DOUBLER FOR AFT HINGE ON CENTER GEAR RIGHT FWD DOOR IN CENTER W/W AT FS 1441. REMOVED DOUBLER, FABRICATED DOUBLER AND INSTALLED DOUBLER, TEE STIFFENER AND SUPPORT FITTING I - [SDR WRLA2007070](https://openairdocs.org/sdr/WRLA2007070.md): Angle · corroded · May 23, 2007 · N14075 · Doug DC1030 · Fuselage Main, Attach Fittings > CORROSION FOUND DURING B-CHECK IN LEFT W/W AT FS 1370 BETWEEN TANK AFT PANEL CAP STRUCTURE AND SIDE FORGING AT SPLICE AREA LBL 115, 38 INCHES BWL. [08-07-07] REMOVED AND REPLACED CORRODED ANGLE, P/N ANB7392-1 IN ACCORDANCE WITH DC-10 SRM VOL.2 51-31-01. - [SDR WRLA2007071](https://openairdocs.org/sdr/WRLA2007071.md): Door Frame · corroded · May 23, 2007 · N14075 · Doug DC1030 · Fuselage Main, Structure > DURING B-CHECK INSPECTION, RIGHT HAND OVERWING DOOR R-3, AFT LOWER CORNER (AT FLOOR LEVEL) STA 1305 EVIDENCE OF CORROSION UNDER DOOR SILL PLATE. [08-07-07] SILL PLATE SUPPORT CHANNEL FOUND CORRODED BEYOND LIMITS. REMOVED CHANNEL, FABRICATED NEW SUPPORT CHAN - [SDR WRLA2006097](https://openairdocs.org/sdr/WRLA2006097.md): Door · missing · Oct 1, 2006 · N14075 · Doug DC1030 · Engine Cowling System > DURING WALKAROUND FOUND MISSING PRESSURE RELIEF DOOR FROM NR 1 ENG LT HAND SIDE CORE COWL, DOOR HINGE DAMAGED AND COWLING SKIN CRACKED ABOUT.875 INCH FORWARD OF DOOR HINGE AREA; CHECKED WING FUSELAGE AND TAIL, NO DAMAGE NOTED. REPAIRED AS PE 14-121-379 BOEIN - [SDR WRLA2006079](https://openairdocs.org/sdr/WRLA2006079.md): Pressure Panel · corroded · Sep 5, 2006 · N14075 · Doug DC1030 · Fuselage Main, Bulkhead > DURING C-CHECK IN GSO FOUND LT WHEEL WELL BS1521 LOWER WEB HAS SEVERE INTERGRANUALAR CORROSION. REMOVED AND REPLACED WITH A NEW FABRICATED INTERCOASTAL IAW DAC DWG AEA7163, ALODINED, PRIMED AND PAINTED IAW SRM 51-21-01 VOL II. - [SDR WRLA2006078](https://openairdocs.org/sdr/WRLA2006078.md): Angle · corroded · Sep 5, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > DURING "C" CHECK IN GSO, FOUND LEFT WHEEL WELL BS1521 INBOARD BULKHEAD ANGLE CORRODED. REMOVED AND REPLACED WITH A NEW FABRICATED ANGLE IAW DAC DWG AEA0025, ALODINED, PRIMED AND PAINTED IAW DC10 SRM 51-21-01 VOL II. - [SDR WRLA2006077](https://openairdocs.org/sdr/WRLA2006077.md): Stiffener · corroded · Sep 5, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > DURING C-CHECK IN GSO FOUND LT WHEEL WELL BS1521 OB STIFFNER ANGLE HAS SECTION MISSING DUE TO CORROSION. REMOVED AND REPLACED STIFFNER WITH A NEW FABRICATED STIFFNER IAW DAC DWG AEA0025, ALODINED, PRIMED AND PAINTED IAW SRM 51-21-01 VOL II. - [SDR WRLA2006071](https://openairdocs.org/sdr/WRLA2006071.md): Seat Track · corroded · Aug 16, 2006 · N14075 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings > DURING C-CHECK IN GSO FOUND MAIN CABIN BETWEEN STA 824 TO 899 SEAT TRACK AT APPROX RBL 106 CORRODED. REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 765 TO 910 WITH A NEW SEAT TRACK IAW DC10-30 SRM 53-70-00 VOL I. - [SDR WRLA2006074](https://openairdocs.org/sdr/WRLA2006074.md): Seat Track · corroded · Aug 14, 2006 · N14075 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings > DURING C-CHECK IN GSO FOUND CABIN SEAT TRACK AT LBL 28 BS 1481-1491 CORRODED INSIDE LUGS. REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 1391 TO 1531 WITH A NEW SEAT TRACK IAW DC10-30 SRM 53-70-00 VOL I. - [SDR WRLA2006073](https://openairdocs.org/sdr/WRLA2006073.md): Seat Track · corroded · Aug 14, 2006 · N14075 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings > DURING C-CHECK IN GSO FOUND CABIN SEAT TRACK AT LBL 28, BS 1400 TO 1412 HAS CORROSION INSIDE LUGS AND IN UPPER SURFACE OF TRACK. FABRICATED REPAIR PART AND INSTALLED IAW DC10-30 SRM 51-31-01 VOL II, REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 1391 TO 151 - [SDR WRLA2006072](https://openairdocs.org/sdr/WRLA2006072.md): Mount · cracked · Aug 14, 2006 · N14075 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings > DURING C-CHECK IN GSO FOUND LAV-B OUTBOARD AFT MOUNT CRACKED AND CORRODED. REMOVED AND REPLACED LAV-B OUTBOARD AFT MOUNT IAW DC10 MM 25-00-00. - [SDR WRLA2006054](https://openairdocs.org/sdr/WRLA2006054.md): Channel · corroded · Aug 11, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" IN GSO FOUND HAT CHANNEL HAS SURFACE CORROSION AROUND FASTENER HOLE AT STA 1921 BL0. REMOVED AND REPLACED HAT CHANNEL IAW SRM 51-31-01 VOL II. - [SDR WRLA2006063](https://openairdocs.org/sdr/WRLA2006063.md): Floorbeam · cracked · Aug 10, 2006 · N14075 · Doug DC1030 · Fuselage Main, Floor Beam > DURING C-CK IN GSO FOUND MAIN CABIN FLOORBEAM CRACKED AT STA 1482 B/N LBL 107 AND LBL 80. FABRICATED FLOOR SUPPORT IAW DC 10 DWG. INSTALLED FLOOR SUPPORT. - [SDR WRLA2006056](https://openairdocs.org/sdr/WRLA2006056.md): Seat Track · corroded · Aug 10, 2006 · N14075 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings > ITEM: DURING "C" IN GSO FOUND SEAT TRACK CORRODED AT LBL28 STA 420-457. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-31-01 VOL II. - [SDR WRLA2006053](https://openairdocs.org/sdr/WRLA2006053.md): Floor Support · corroded · Aug 10, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL CORRODED ON UPPER SURFACE APPROX STA 1915. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-31-01 VOL II. - [SDR WRLA2006050](https://openairdocs.org/sdr/WRLA2006050.md): Floor Support · corroded · Aug 10, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL HAS SURFACE CORROSION AT STA 1877 - 2007 RBL26. REMOVED AND REPLACED FLOOR SUPPORT CHANNEL IAW SRM 51-31-01 VOL II. - [SDR WRLA2006064](https://openairdocs.org/sdr/WRLA2006064.md): Web · cracked · Aug 9, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > DURING C-CK IN GSO FOUND WEB AT STA 1960-1986 AT RBL 50 CRACKED AROUND FASTENER HOLES. REMOVED WEB IAW DC10 SRM 51-31-01 COL II. FABRICATED DOUBLER IAW DC10 SRM 53-16-01 VOL III. ALIGNED, PRIMED, AND PAINTED, IAW DC10 SRM 51-21-01 VOL I. INSTALLED DOUBLER - [SDR WRLA2006042](https://openairdocs.org/sdr/WRLA2006042.md): Intercostal · corroded · Aug 9, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" IN GSO FOUND CABIN ZONE 220 UNDER FLOOR AREA STA 475 BL95R CORRODED INTERCOSTAL. FABRICATED INTERCOSTAL IAW DC10 DRWG 7186-502. ALODINED & PRIMED IAW DC10 SRM 51-21-01 VOL II. INSTALLED FLOOR SUPPORT IAW SRM 51-31-01. - [SDR WRLA2006041](https://openairdocs.org/sdr/WRLA2006041.md): Floor Support · corroded · Aug 8, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" CHECK IN GSO FOUND MAIN CABIN AT STA 828 AT BL-0 FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT BEAM IAW DC10 SRM 51-31-01 VOL II. - [SDR WRLA2006048](https://openairdocs.org/sdr/WRLA2006048.md): Floor Support · corroded · Aug 7, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" IN GSO FOUND MAIN CABIN AT STA 832 AT APPROX RBL46 TO LBL46 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW SRM 51-31-01 VOL II. - [SDR WRLA2006043](https://openairdocs.org/sdr/WRLA2006043.md): Floor Support · corroded · Aug 5, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" CHECK IN GSO FOUND CABIN ZONE 220 UNDER FLOOR AREA STA 450 BL35L SCALLOPED BEAM CAP CORRODED. REMOVED AND FABRICATED NEW FLOOR SUPPORT IAW DOUGLAS DWG ABA8306 REV K. INSTALLED FLOOR SUPPORT IAW SRM 51-35-01 VOL II. - [SDR WRLA2006059](https://openairdocs.org/sdr/WRLA2006059.md): Floor Support · corroded · Aug 4, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" IN GSO FOUND FLOOR SUPPORT IN MAIN CABIN HAS CORROSION AT STA 879 RBL60. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-31-01 VOL II. - [SDR WRLA2006047](https://openairdocs.org/sdr/WRLA2006047.md): Floor Support · corroded · Aug 3, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" IN GSO FOUND MAIN CABIN BETWEEN STA 808 TO 899 FLOOR SUPPORT AT APPROX RBL 46 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-31-01 VOL I. - [SDR WRLA2006046](https://openairdocs.org/sdr/WRLA2006046.md): Longeron · corroded · Aug 3, 2006 · N14075 · Doug DC1030 · Fuselage Main, Longeron/Stringer > ITEM: DURING "C" CHECK FOUND AT STA 1521 LONGERON 46L HAS EXFOLIATION AND HEAVY PITTING CORROSION. FABRICATED NEW REPAIR ANGLE AND CHANNEL, INSTALLED PER SRM CHAP 51 VOL II. - [SDR WRLA2006040](https://openairdocs.org/sdr/WRLA2006040.md): Floor Support · corroded · Aug 3, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" CHECK IN GSO FOUND MAIN CABIN FLOOR PANEL NR 224AF SUPPORT CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT IAW WITH SRM 51-31-01 VOL II. - [SDR WRLA2006060](https://openairdocs.org/sdr/WRLA2006060.md): Floor Support · corroded · Aug 2, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" IN GSO FOUND FLOOR SUPPORT IN MAIN CABIN HAS CORROSION AT STA 824 RBL60. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-31-01 VOL II. - [SDR WRLA2006058](https://openairdocs.org/sdr/WRLA2006058.md): Floor Support · corroded · Aug 2, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" IN GSO FOUND FLOOR SUPPORT IN MAIN CABIN HAS SURFACE CORROSION AT STA899 RBL60. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-31-01 VOL II. - [SDR WRLA2006052](https://openairdocs.org/sdr/WRLA2006052.md): Floor Support · corroded · Aug 2, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL HAS SURFACE CORROSION AROUND NUT PLATE CLIP HOLES AT STA 1900 LBL22-RBL22. REMOVED AND REPLACED FLOOR SUPPORT CHANNELS IAW SRM 51-31-01 VOL II. - [SDR WRLA2006051](https://openairdocs.org/sdr/WRLA2006051.md): Floor Support · corroded · Aug 2, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL HAS SURFACE CORROSION AT STA 1900 LBL28-LBL53. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-33-01 VOL II. - [SDR WRLA2006049](https://openairdocs.org/sdr/WRLA2006049.md): Floor Support · corroded · Aug 2, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL HAS SURFACE CORROSION AT STA 1887 RBL50. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-33-01 VOL II. - [SDR WRLA2006045](https://openairdocs.org/sdr/WRLA2006045.md): Frame · corroded · Aug 1, 2006 · N14075 · Doug DC1030 · Fuselage Main, Frame > ITEM: DURING "C" CHECK IN GSO FOUND LEFT WHEEL WELL STA 1510 FRAME CORRODED ON LOWER LEG. FORMED NEW FRAME IAW DAC DWG AEA7165 REV K. INSTALLED NEW FRAME SECTION IAW SRM 53-00-01 VOL I. - [SDR WRLA2006055](https://openairdocs.org/sdr/WRLA2006055.md): Floor Support · corroded · Jul 28, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT ANGLE HAS SURFACE CORROSION AT STA 1986 LBL14. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-31-01 VOL II. - [SDR WRLA2006057](https://openairdocs.org/sdr/WRLA2006057.md): Floor Support · corroded · Jul 26, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > ITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL HAS CORROSION AT STA 1913 - 2007 LBL24. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT CHANNEL IAW SRM 51-31-01 VOL II. - [SDR WRLA2006026](https://openairdocs.org/sdr/WRLA2006026.md): Fitting · corroded · Jul 26, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > DURING C3 CK, FOUND CORROSION ON RT W/W FITTING, STA 1505 B/N LONG 44 AND 45. REPLACE SUPPORT FITTING. - [SDR WRLA2006025](https://openairdocs.org/sdr/WRLA2006025.md): Doubler · corroded · Jul 26, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > DURING C3 CK, FOUND CORROSION ON DOUBLER IN RT WHEEL WELL STA 1520-1500. FAB NEW DOUBLER. - [SDR WRLA2006022](https://openairdocs.org/sdr/WRLA2006022.md): Bulkhead · corroded · Jul 25, 2006 · N14075 · Doug DC1030 · Fuselage Main, Bulkhead > DURING C3 CK, FOUND CORROSION IN MAIN CABIN AFT PRESSURE BULKHEAD UNDER SPLICE ANGLE LOWER CORD. REMOVED AND REPLACED T CHORD DC10 SRM 51-31-01 VOL II. - [SDR WRLA2006021](https://openairdocs.org/sdr/WRLA2006021.md): Support · corroded · Jul 25, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure > DURING C3 CK IN GSO, FOUND CORROSION R MLG MOST AFT ACCESS SUPPORT IS CORRODED. SPLICE NEW EXT ANGLE REPAIR. Next page: https://openairdocs.org/deregistered/N14075-2013-05-21/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 = 'N14075' AND deregistration_id = 'N14075-2013-05-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N14075-2013-05-21/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.