# Service difficulty reports: N801DH, cancelled Sep 26, 2017

A list on [N801DH, cancelled Sep 26, 2017](https://openairdocs.org/deregistered/N801DH-2017-09-26.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 16 · 758 reports

- [SDR DHLA20120519801](https://openairdocs.org/sdr/DHLA20120519801.md): Skin · corroded · May 19, 2012 · N801DH · Doug DC872F · Fuselage Main, Plate/Skin
  > POSSIBLE CORROSION FOUND AT FS 102 AND LONGERON 36.
- [SDR DHLA201000152](https://openairdocs.org/sdr/DHLA201000152.md): Access Door · corroded · Dec 12, 2010 · N801DH · Doug DC873F · Service Doors
  > ACCESS DOOR HAS CORROSION AT FUSELAGE STA FS 650.000 L32R - L36. PERFORMED MAJOR REPAIR IAW ASTAR EC-02354-001 AND DWG 5800471 AND WO 9735. REMOVED CORRODED ACCESS DOOR IAW DPS 3.67 AND SRM 51-3-0. REMOVED CORROSION IAW SRM 51-1-8. FOUND OUT OF LIMITS IAW
- [SDR DHLA201000150](https://openairdocs.org/sdr/DHLA201000150.md): Skin · damaged · Dec 12, 2010 · N801DH · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTED EXISTING REPAIR LOCATED AT FS 1890.000, L36 FOR CONDITION, SECURITY AND CONFORMITY. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 12-09-10 AND EVA D853-00384 REV "IR" DATED 11-18-10. REMOVED EXISTING REPAIR IAW SRM 51-1-21. TRIMMED OUT DAMAGED A
- [SDR DHLA201000151](https://openairdocs.org/sdr/DHLA201000151.md): Spar Cap · cracked · Dec 5, 2010 · N801DH · Doug DC873F · Wing Spar
  > NR 1 ALT TANK FRONT SPAR LWR CAP SPLICE CRACKED 1" STA XFS 532.000 S-64 PERFORMED MAJOR REPAIR IAW EC-02340-001, WO 9735, MESSAGE SEU-SEU-10-0074-028, DATED 11-17-10. REMOVED CRACKED SPLICE FITTING IAW JC EC-02340-001, MESSAGE SEU-10-0074-028 AND DWG 3644046.
- [SDR DHLA201000133](https://openairdocs.org/sdr/DHLA201000133.md): Finger Doubler · corroded · Nov 1, 2010 · N801DH · Doug DC873F · Fuselage Main, Plate/Skin
  > MAIN CARGO COMPT- FINGER DOUBLER CORRODED, STA 879.000 RB 1. 65" REMOVED CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0, PG 2P. REMOVED FINGER DOUBLER IAW SRM 51-1-21, FABRICATED FINGER DOUBLER (AL7075T6 0.050") IAW SRM 53-7-3 FIG 4,
- [SDR DHLA201000148](https://openairdocs.org/sdr/DHLA201000148.md): Skin · corroded · Oct 29, 2010 · N801DH · Doug DC873F · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN CORRODED, STA 1690.000 L28L AND CRACKED.5" ALSO PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9, DATED 11-19-10, AD2008-06-23, S/B 53A080, EVA D853-00383, REV IR DATED 11-18-10. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. REMOVED CORR
- [SDR DHLA201000145](https://openairdocs.org/sdr/DHLA201000145.md): Rib · cracked · Oct 27, 2010 · N801DH · Doug DC873F · Trailing Edge Flaps
  > LT INBD FLAP.- RIB CRACKED AND WITH IMPROPER REPAIR, STA XW 125.000. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 2, SHEET 4, ITEM "Q". REMOVED DAMAGED RIB IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA + NEW RIB IA
- [SDR DHLA2010000149](https://openairdocs.org/sdr/DHLA2010000149.md): Frame · worn · Oct 26, 2010 · N801DH · Doug DC873F · Engine Thrust Reverser
  > NR2 ENG LT T/R STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE AT STA YN 202.000, BETWEEN 7 AND 8 O'CLOCK POS. C/A PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-29-10, EVA D878-00380, REV IR DATED 11-09-10. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED
- [SDR DHLA201000147](https://openairdocs.org/sdr/DHLA201000147.md): Frame · worn · Oct 26, 2010 · N801DH · Doug DC873F · Engine Thrust Reverser
  > NR1 ENG LT T/R STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE AT STA YN 202.000, BETWEEN 7 AND 8 O'CLOCK PERFORMED MAJOR REPAIR IAW FAA, FORM 8110-3, DATED 11-29-10, EVA D878-00382 REV IR DATED 11-09-10. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED AREA. F
- [SDR DHLA201000146](https://openairdocs.org/sdr/DHLA201000146.md): Vane · delaminated · Oct 26, 2010 · N801DH · Doug DC873F · Trailing Edge Flaps
  > NR 2 RT FLAP VANE DELAMINATED. R & R NEW FLAP VANE NR2 RT IAW MM 27-51-14, PG 201-203. REFER TO NR 239348 FOR OPS CHECK.
- [SDR DHLA201000012](https://openairdocs.org/sdr/DHLA201000012.md): Battery Pack · inoperative · Apr 23, 2010 · N801DH · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHTING SYS WOULD NOT OPERATE DURING PREFLIGHT TEST. R & R BATTERY EMERGENCY RACK ASSY CHECK OPS GOOD IAW MM 33-11-0. ACFT WAS GROUNDED.
- [SDR DHLA201000009](https://openairdocs.org/sdr/DHLA201000009.md): Skin · corroded · Apr 9, 2010 · N801DH · Doug DC873F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CORRODED AT FS 25.25 AND LONGERON 33R. ACCOMPLISHED MAJOR REPAIR TO FUSE SKIN, FS 24.0 TO 70.0, L33R TO L36R IAW EVA D853-00327 & DWG D85300327-001-D. SEE NR 00007 FOR REPAIR DETAILS. REV IR DATED 4/8/10, DWG NO D85300327-001-D REV IR DATED 4/1
- [SDR DHLA201000001](https://openairdocs.org/sdr/DHLA201000001.md): Battery Pack · discharged · Jan 2, 2010 · N801DH · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHTING DIM DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ASSY. OPS CHECK OK IAW MM 33-50-00 & 33-50-1. ACFT WAS GROUNDED.
- [SDR DHLA2009801004](https://openairdocs.org/sdr/DHLA2009801004.md): Heat Exchanger · cracked · Apr 28, 2009 · N801DH · Doug DC873F · Cabin Cooling System
  > FROM N/R 235627- N/R 236921 REF LT PRIMARY HEAT EXCHANGER AFT LOWER CORNER CRACKED 3/4", STA 12. WHILE PERFORMING INSPECTION OF THIS COMPLETED ITEM, QC REP NOTED 1 IN PROCESS INSPECTION NDT C/W 2 HI-LOCKS NOT TORQUED OR WITNESSED BY Q.C + 3 HI LOCK PULLED ON
- [SDR DHLA2009801006](https://openairdocs.org/sdr/DHLA2009801006.md): Angle · corroded · Apr 14, 2009 · N801DH · Doug DC873F · Fuselage Miscellaneous Structure
  > LT MLG WW ANGLE CORRODED, STA XCW 46.000 (NEAR REAR SPAR UPPER PART) PERFORMED MAJOR REPAIR IAW BOEING MSG NR SEU XXX-09-0024-02B DATED 04-20-09, SRM 57-1-0 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG.16. REMOVED C
- [SDR DHLA2009801008](https://openairdocs.org/sdr/DHLA2009801008.md): Skin · corroded · Apr 13, 2009 · N801DH · Doug DC873F · Wing, Plate/Skin
  > NR 4 STUB WING UPPER EXTERNAL SKIN CORRODED, STA.XFS 530.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3,09191 DATED 04-30-09, EVA DB57-00258 REV IR DATED 04-22-09, DWG ED9935 DATED 04-16-09. REMOVED FASTENERS IAW SRM 51-3-0, SRM 51-1-21, SRM 51-1-700. REMO
- [SDR DHLA2009801010](https://openairdocs.org/sdr/DHLA2009801010.md): Skin · damaged · Apr 11, 2009 · N801DH · Doug DC873F · Wing, Plate/Skin
  > RT WING CTR L/E REPAIR DOUBLER HOLES ELONGATED, STA X0LDO 67.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 09175 DATED 04-28-09, EVA DE53-00257 REV IR DATED 04-21-09, DWG ED 4934 DATED 04-15-09. REMOVED DAMAGED REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-1-2
- [SDR DHLA2009801005](https://openairdocs.org/sdr/DHLA2009801005.md): Spar Cap · cracked · Apr 11, 2009 · N801DH · Doug DC873F · Wing Spar
  > LT LWR WING FRONT SPAR CAP AT L/E ATTACH HOLE SHOWS A 0.500 INCH LENGTH CRACK, STA XFE 523.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 05-7-09, EVA D857-00261 REV IA DATED 04-27-09, REPAIR SKETCH 200904200125 DWG J060232, JCT04316 REM
- [SDR DHLA2009801003](https://openairdocs.org/sdr/DHLA2009801003.md): Heat Exchanger · cracked · Apr 8, 2009 · N801DH · Doug DC873F · Cabin Cooling System
  > LT PRIMARY HEAT EXCHANGER AFT LWR CORNER CRACKED 3/7 INCH STA-12.000 L-27L TO 28L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 09181 DATED 04-29-09 EVD DB53-00256 REV IR DATED 04-21-09 SEMAN DWG NR ED-4933 DATED 04-13-09. REMOVED FASTENERS IAW SRM 51-1-21
- [SDR DHLA2009801013](https://openairdocs.org/sdr/DHLA2009801013.md): Skin · misrepaired · Apr 7, 2009 · N801DH · Doug DC871F · Trailing Edge Flaps
  > LT INBD FLAP UPPER SKIN REPAIR IMPROPER, STA XW 106.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1 PG 2. REMOVED PLATING WITH IMPROPER REPAIR IAW SRM 57-1-0 PG 1, SRM 51-1-2. FABRICATED NEW PLATING IAW SRM 57-7-1 FIG 1 PG 2 ITEM D. CLEANED
- [SDR DHLA2009801012](https://openairdocs.org/sdr/DHLA2009801012.md): Skin · delaminated · Apr 7, 2009 · N801DH · Doug DC873F · Spoilers
  > NR 3 RT SPOILER PANEL EXTERNAL SKIN DELAMINATED (STA XRS 162.000 - 230.000). CUT OUT DELAMINATED AREA IAW SRM 57-2-3 PG 33 FIG 4D PAR 23. FABRICATED REPAIR PLUG AND CORE IAW SRM 57-1-1 PG 15,SRM 57-2-3 PAR.23.6,SRM 57-2-0 PAR. 4. PERFORMED CLEANING IAW SRM
- [SDR DHLA2009801011](https://openairdocs.org/sdr/DHLA2009801011.md): Cargo Track · worn · Apr 7, 2009 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO COMPARTMENT NR 5 TRACK SEGMENT LUGS WORN STA 1680.000-1700.000. MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG. 14 SHEET 1 PG. 49-50. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES IAW SRM 53-1-0 PG. 1, SRM 51-3-0. FABRICATED NEW TRA
- [SDR DHLA2009801009](https://openairdocs.org/sdr/DHLA2009801009.md): Vane · delaminated · Apr 7, 2009 · N801DH · Doug DC873F · Trailing Edge Flaps
  > NR 3 LT FLAP VANE INTERNAL SKIN DELAMINATED (STA XF 160.000 - 213.000). REMOVED AND REPLACED NR 3 FLAP VANE IAW MM 27-51-14 PG 201-203.
- [SDR DHLA2009801002](https://openairdocs.org/sdr/DHLA2009801002.md): Skin · delaminated · Apr 7, 2009 · N801DH · Doug DC873F · Wing, Plate/Skin
  > RT WING, PANEL NR 577A EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED WING PANEL NR 577A IAW SRM 51-3-0, SRM 51-3-1.
- [SDR DHLA2009801001](https://openairdocs.org/sdr/DHLA2009801001.md): Skin · delaminated · Apr 7, 2009 · N801DH · Doug DC873F · Wing, Plate/Skin
  > LT WING PANEL EXT SKIN DELAMINATED (STA XW 0 - XW 37.000). REMOVED AND REPLACED DELAMINATED LT WING PANEL IAW SRM 51-3-0 SRM 51-3-1.
- [SDR DHLA2009801007](https://openairdocs.org/sdr/DHLA2009801007.md): Doubler · broken · Apr 4, 2009 · N801DH · Doug DC873F · Fuselage Miscellaneous Structure
  > FUSELAGE NOSE SECTION, INTERNAL DOUBLER BROKEN AT STA 156.00, L-36 (REF ACCESS NR 2). MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 09218 DATED 05-11-09, EVA DB53-00259 REV IR DATED 04-22-09, SEMAN DWG ED 4932 DATED 04-14-09. CUT DAMAGED SECTI
- [SDR DHLA200800099](https://openairdocs.org/sdr/DHLA200800099.md): Battery · discharged · Sep 23, 2008 · N801DH · Doug DC873F · Emergency Lighting
  > EMERG LTS BATTERY DISCHARGED REPLACED BATTERY PACK FOR EMER LTS PER MM 33-50-01 CHECKS SERV. N/A FLT NR. ACFT WAS GROUNDED
- [SDR DHLA200800098](https://openairdocs.org/sdr/DHLA200800098.md): Battery Pack · discharged · Sep 23, 2008 · N801DH · Doug DC873F · Emergency Lighting
  > EMERG LTS BATTERY DISCHARGED. REPLACED BATTERY PACK FOR EMER LTS PER MM 33-50-01 CHECKS SERV. NO FLT NR. ACFT WAS GROUNDED.
- [SDR DHLA200700070](https://openairdocs.org/sdr/DHLA200700070.md): Engine · shutdown · Nov 29, 2007 · N801DH · Doug DC873 · Engine (Turbine/Turboprop)
  > IN CRUISE FL 360 FELT A/C SHUDDER AND VIBRATION FOUND NR 3 ENGINE SPOOLING DOWN ATTEMPTED RELIGHT EGT 565 ENGINE N1 WOULD NOT ACCELERATE N2 MAX 70. VIBRATION NOTED DURING DECELERATION AND ADVANCE OF THRUST LEVER PRECAUTIONARY SHUTDOWN ACCOMPLISHED A WINDMILLI
- [SDR DHL2007801540](https://openairdocs.org/sdr/DHL2007801540.md): Spar Cap · cracked · Nov 21, 2007 · N801DH · Doug DC873F · Wing Main, Frame Structure
  > LT LWR WING FRONT SPAR CAP CRACKED 1.250" APPROXIMATELY AT STA XFS 520.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 11-20-07, BOEING MSG NR 1-653039342-4 DATED 10-22-07, BOEING SKETCH JO060232, JCT04316, EVA D857-00022 REV IR DATED 10-
- [SDR DHL2007801541](https://openairdocs.org/sdr/DHL2007801541.md): Skin · corroded · Nov 18, 2007 · N801DH · Doug DC873F · Fuselage Main, Plate/Skin
  > AFT CARGO COMPT SKIN CORRODED STA 1200.000 L-36 TO L-35L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-15-07, EVA D853-00021 REV "B" DATED 11-15-07. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P.
- [SDR DHL2007801539](https://openairdocs.org/sdr/DHL2007801539.md): Skin · cracked · Nov 14, 2007 · N801DH · Doug DC873F · Nacelle/Pylon, Plate/Skin
  > NR 4 ENG NACELLE INLET COWL LT EXTERNAL SKIN CRACKED 1" STA YN 132.000 AT 9 O'CLOCK POS. (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-16-07, EVA B271-00015 REV IR DATED 10-12-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-21A, CUT OUT
- [SDR DHL2007801533](https://openairdocs.org/sdr/DHL2007801533.md): Skin · damaged · Nov 14, 2007 · N801DH · Doug DC873F · Wing, Nacelle/Pylon Attach Fittings
  > ITEM REF. NR. 101138: UPPER RUDDER T/E BROKEN AT STA ZR 335.250 (FIBERGLASS) DAMAGE CAUSED BY SEMAN. STAGGERED CUT BACK BY A/2" TO A INCH PER PLY FROM THE CRACK THROUGH ALL DAMAGED PLIES OF THE CLOTH IAW SRM 51-1-19 PG 3. REPLACED THE CUT OUT CLOTH WITH A NE
- [SDR DHL2007801526](https://openairdocs.org/sdr/DHL2007801526.md): Skin · delaminated · Nov 14, 2007 · N801DH · Doug DC873F · Wing, Plate/Skin
  > RT WING LWR T/E PANEL INTERNAL/EXTERNAL SKIN DELAMINATED (STA XF 409.000 - XRS 456.000). REMOVED AND REPLACED RT WING T/E LWR PANEL (STA XF 409.000 - XRS 456.000) IAW SRM 51-3-0, SRM 51-3-1.
- [SDR DHL2007801538](https://openairdocs.org/sdr/DHL2007801538.md): Skin · cracked · Nov 14, 2007 · N801DH · Doug DC873F · Wing, Plate/Skin
  > LT WING MAIN TANK NR 1 LWR SIDE CRACKED 1" STA XRS 84.000 S-59. PERFORMED MAJOR REPAIR IAW MSG NR 1-654248500-2 DATED 10-19-07, SRM 57-2-2 FIG 3D SHEET 1, 2, 3, TR NR 57-86 DATED 05-15-01. REMOVED EXISTING CLIPS AND CUT OUT DAMAGED STRINGER SEGMENT IAW MSG N
- [SDR DHL2007801535](https://openairdocs.org/sdr/DHL2007801535.md): Frame · cracked · Nov 14, 2007 · N801DH · Doug DC873F · Fuselage Main, Frame
  > MAIN CARGO COMPT FRAME SEGMENT CRACKED 5" STA 240.000 L20R TO L21R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 2 SHEET 2.6. REMOVED DAMAGED FRAME SEGMENT, SPLICES AND EXISTING ANGLES IAW SRM 51-1-20D. FABRICATED NEW FRAME SEGMENT P/N S2537716 IAW SRM 53-2-0
- [SDR DHL2007801536](https://openairdocs.org/sdr/DHL2007801536.md): Skin · corroded · Nov 13, 2007 · N801DH · Doug DC873F · Fuselage Main, Plate/Skin
  > AFT ACCY COMPT SKIN CORRODED STA 1690.000 - 1700.000 L-30L TO L-32R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-13-07, ENGINEERING VARIATION AUTHORIZATION NR D853-00024 REV IR DATED 11-06-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. REMOVED
- [SDR DHL2007801534](https://openairdocs.org/sdr/DHL2007801534.md): Structure · damaged · Nov 12, 2007 · N801DH · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECT REPAIR AT FUSELAGE STA 280 LONGERON 29R PER INSPECTION REQUIREMENTS OF DC8 SRM 53-2-1 CLASS II TYPE REPAIR. REPAIR ACCOMPLISHED AUG 94. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-12-07, ENGINEERING VARIATION AUTHORIZATION NR D853-00023 REV
- [SDR DHL2007801528](https://openairdocs.org/sdr/DHL2007801528.md): Structure · damaged · Nov 11, 2007 · N801DH · Doug DC873F · Leading Edge Devices
  > LT INNER WING OUTBD EXTENDED LEADING EDGE SLOT LWR PLATING ELONGATED HOLES AT STA XILD 42.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-12-07, ENGINEERING VARIATION AUTHORIZATION NR D857-00020 REV IR DATED 10-20-07. REMOVED FASTENERS
- [SDR DHL2007801523](https://openairdocs.org/sdr/DHL2007801523.md): Skin · cracked · Nov 9, 2007 · N801DH · Doug DC873F · Rudder, Plate/Skin
  > LT RUDDER SKIN CRACKED 5" AT STA ZR 335.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1 PG 2. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21, SRM 51-1-21A. FABRICATED PLATING AND BONDED DOUBLER BOTH FROM AL 2024T3 0.016" IAW SR
- [SDR DHL2007801522](https://openairdocs.org/sdr/DHL2007801522.md): Skin · deformed · Nov 9, 2007 · N801DH · Doug DC873F · Rudder, Plate/Skin
  > RT RUDDER SKIN DEFORMED AT STA ZR 335.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1 PG 2. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21, SRM 51-1-21A. FABRICATED PLATING AND BONDED DOUBLER BOTH FROM IAW SRM 55-6-1 FIG 1 PG 2
- [SDR DHL2007801532](https://openairdocs.org/sdr/DHL2007801532.md): Skin · damaged · Nov 9, 2007 · N801DH · Doug DC873F · Rudder, Plate/Skin
  > RUDDER TIP SKIN BROKEN AT STA ZR 335.250 (DAMAGE CAUSED BY SEMAN). REMOVED BROKEN TIP IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TIP IAW SRM 51-1-21A. REFER TO JC EC-00592-001 (WO 2624) FOR FABRICATION AND NR 101137 FO
- [SDR DHL2007801520](https://openairdocs.org/sdr/DHL2007801520.md): Skin · worn · Nov 8, 2007 · N801DH · Doug DC873F · Nacelle/Pylon, Plate/Skin
  > NR 1 ENG NACELLE INLET COWL UPPER SKIN WORN STA YN 150.000 AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION. FABRICATED NEW SKIN (AL2024T3 0.080") AND SPLIC
- [SDR DHL2007801521](https://openairdocs.org/sdr/DHL2007801521.md): Skin · worn · Nov 8, 2007 · N801DH · Doug DC873F · Nacelle/Pylon, Plate/Skin
  > NR 2 ENG NACELLE INLET COWL UPPER SKIN WORN AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN (AL2024T3 0.080") AND SPLICE (STEEL TYP
- [SDR DHL2007801529](https://openairdocs.org/sdr/DHL2007801529.md): Fitting · cracked · Nov 8, 2007 · N801DH · Doug DC873F · Service Doors
  > MAIN CARGO COMPT SERVICE DOOR JAMB FITTING CRACKED 1" AT STA 1118.528 L11R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1.
- [SDR DHL2007801512](https://openairdocs.org/sdr/DHL2007801512.md): Skin · delaminated · Nov 7, 2007 · N801DH · Doug DC873F · Wing, Plate/Skin
  > RT WING ACCESS DOOR NR 577B INTERNAL SKIN DELAMINATED (STA XA 650.000 - 670.000). REMOVED AND REPLACED DOOR ASSY IAW SRM 51-3-0, SRM 51-3-1.
- [SDR DHL2007801524](https://openairdocs.org/sdr/DHL2007801524.md): Support · cracked · Nov 7, 2007 · N801DH · Doug DC873F · Ailerons
  > NR 7 LT AILERON HINGE SUPPORT CRACKED. REMOVED AND REPLACED NR 7 LT AIL HINGE SUPPORT IAW MM 20-16-0 PG 201-207, OHM 27-2-3A. REFER TO NR 130478 FOR OPS CHECK AND NR 130141 FOR LT OUTBD AIL REMOVAL/REINSTALLATION.
- [SDR DHL2007801510](https://openairdocs.org/sdr/DHL2007801510.md): Skin · delaminated · Nov 6, 2007 · N801DH · Doug DC873F · Wing, Plate/Skin
  > LT WING UPPER PANEL EXTERNAL SKIN DELAMINATED (STA XW 0 - 33.000). REMOVED AND REPLACED LT WING UPPER PANEL ASSY IAW SRM 51-3-0, SRM 51-3-1.
- [SDR DHL2007801513](https://openairdocs.org/sdr/DHL2007801513.md): Fitting · cracked · Nov 6, 2007 · N801DH · Doug DC873F · Wing, Attach Fittings
  > LT WING CTR L/E UPPER INTERNAL SPLICE FITTING CRACKED 3" AT STA XOLDI 6.2246. REMOVED SPLICE FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-21, SRM 51-1-20D
- [SDR DHL2007801515](https://openairdocs.org/sdr/DHL2007801515.md): Skin · damaged · Nov 6, 2007 · N801DH · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECT REPAIR AT FUSELAGE STA 490 L-23R PER INSPECTION REQUIREMENTS OF DC8 SRM 53-2-1 CLASS II TYPE REPAIR. REPAIR ACCOMPLISHED AT AIR CANADA AUG 94. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 2. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21.

Next page: https://openairdocs.org/deregistered/N801DH-2017-09-26/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 = 'N801DH' AND deregistration_id = 'N801DH-2017-09-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N801DH-2017-09-26/reports

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