# Service difficulty reports: N804DH, cancelled Sep 26, 2017

A list on [N804DH, cancelled Sep 26, 2017](https://openairdocs.org/deregistered/N804DH-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 14 · 656 reports

- [SDR DHLA201100537](https://openairdocs.org/sdr/DHLA201100537.md): Skin · corroded · Aug 26, 2011 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE HAS CRACK IN SKIN AT STA 100 AT LONGERON 35 & 36R. CRACK IS PROBABLY INDUCED BY CORROSION. COMPLIED WITH STEPS 1-11 OF EVA D853-00412. FABRICATED FILLER, DOUBLER AND INSTALLED REPAIR. MAJOR REPAIR
- [SDR DHLA2011F00187](https://openairdocs.org/sdr/DHLA2011F00187.md): Skin · cracked · Aug 25, 2011 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > WHILE COMPLYING WITH VISUAL WALK AROUND INSP, A CRACK WAS FOUND IN THE LOWER FUSELAGE SKIN AT STA 100.5. UPON FURTHER INVESTIGATION THE CAUSE OF THE CRACK WAS CORROSION. THE CRACK WAS ADJACENT TO ANOTHER REPAIR WHICH WAS REMOVED AND THE NEW REPAIR INCOORPERA
- [SDR DHLA201000139](https://openairdocs.org/sdr/DHLA201000139.md): Wire · broken · Dec 2, 2010 · N804DH · Doug DC873F · Fire Protection System Wiring
  > CLIMBING OUT OF 2000 FT AFE ENG NR 4 FIRE INDICATION. COMPLETED PHASE I'S AND ENG FIRE CHECKLIST FIRED BOTH BOTTLES. EMERGENCY WAS DECLARED. AIR TURN, ACFT WAS GROUNDED. INSPECTED NR4 ENGINE AND FOUND NO EVIDENCE OF FIRE IAW MM71-00-00. R & R NR3 AND NR4 FIR
- [SDR DHLA201000130](https://openairdocs.org/sdr/DHLA201000130.md): Skin · damaged · Sep 14, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > EXISTING REPAIR LOCATED ON LOWER BELLY AT FS 1400.000 L36 IN POOR CONDITION. R & R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-04-10, EVA D853-00378 REV IR DATED 09-22-10. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED AREA AND
- [SDR DHLA201000120](https://openairdocs.org/sdr/DHLA201000120.md): Skin · damaged · Sep 14, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > EXISTING REPAIR LOCATED ON LWR BELLY AT FS 1400.000 L36 IN POOR CONDITION. R & R PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 10-04-10, EVA D853-00378 REV IR DATED 09-22-10. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED AREA + FA
- [SDR DHLA201000129](https://openairdocs.org/sdr/DHLA201000129.md): Intercostal · cracked · Sep 8, 2010 · N804DH · Doug DC873F · Fuselage Miscellaneous Structure
  > NOSE SECTION.- INTERCOSTAL CRACKED 1" APPROX, STA - 2.000 L-30 - 33RT. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0 CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B PERFORMED STOP HOLE + FABRICATED DOUBLER (AL 2024 B 0.050") IAW SRM 53-2-0 FIG 23, SHEET 1 TR
- [SDR DHLA201000098](https://openairdocs.org/sdr/DHLA201000098.md): Intercostal · cracked · Sep 8, 2010 · N804DH · Doug DC873F · Fuselage Miscellaneous Structure
  > NOSE SECTION.- INTERCOSTAL CRACKED 1" APPROX, STA - 2.000 L-30 - 33RT. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0 CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B PERFORMED STOP HOLE + FABRICATED DOUBLER ( AL 2024 B 0.050") IAW SRM 53-2-0 FIG 23 SHEET 1 TR
- [SDR DHLA201000124](https://openairdocs.org/sdr/DHLA201000124.md): Skin · misrepaired · Sep 3, 2010 · N804DH · Doug DC873F · Rudder, Plate/Skin
  > R & R EXISTING REPAIR ON RT RUDDER PLATING AT ZR 61.156 UTILIZING APPROVED DATA. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG. 1. REMOVED PLATING AND EXISTING NON STANDARD REPAIR IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING IAW SRM 55-6-1 FIG 1 ITEM "
- [SDR DHLA201000115](https://openairdocs.org/sdr/DHLA201000115.md): Skin · misrepaired · Sep 3, 2010 · N804DH · Doug DC873F · Wing, Plate/Skin
  > R & R EXISTING REPAIR ON RT WING LOWER SURFACE AT XFS 566.250 UTILIZING APPROVED DATA. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 09-30-10, EVA D857-00373 REV IR DATED 09-17-10. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED AREA
- [SDR DHLA201000111](https://openairdocs.org/sdr/DHLA201000111.md): Skin · misrepaired · Sep 3, 2010 · N804DH · Doug DC873F · Wing, Plate/Skin
  > EXISTING REPAIR ON RT WING L/E LOWER SURFACE AT XW257.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 ATED 09-21-10, EVA D857-00367 REV IR DATED 09-14-10. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED AREA & FABRICATED FILLER & REPAIR
- [SDR DHLA201000107](https://openairdocs.org/sdr/DHLA201000107.md): Skin · cracked · Sep 3, 2010 · N804DH · Doug DC873F · Ailerons
  > R & R EXISTING REPAIR LOCATED ON RT AILERON UPPER PLATING SURFACE UTILIZING APPROVED DATA, PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 2X PAR 16D-3. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21. CUT OUT DAMAGED AREA + FABRICATED INTERNAL REPAIR DOUBLER
- [SDR DHLA201000102](https://openairdocs.org/sdr/DHLA201000102.md): Skin · misrepaired · Sep 3, 2010 · N804DH · Doug DC873F · Rudder, Plate/Skin
  > R & R EXISTING REPAIR ON RT RUDDER PLATING AT ZR 61.156 (REF REPAIR REPORT VS002) UTILIZING APPROVED DATA. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1. REMOVED PLATING AND EXISTING NON STANDARD REPAIR IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING
- [SDR DHLA201000126](https://openairdocs.org/sdr/DHLA201000126.md): Skin · deformed · Sep 2, 2010 · N804DH · Doug DC873F · Ailerons
  > LEFT OTBD AILERON LOWER PLATING DEFORMED STA XA 741.000. PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 4. REMOVED DEFORMED NOSE PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-3-0. FABRICATED NEW NOSE PLATING IAW SRM 57-8-1 FIG. 4 ITEM "H". CLEANED, TREATED AND P
- [SDR DHLA201000096](https://openairdocs.org/sdr/DHLA201000096.md): Skin · deformed · Sep 2, 2010 · N804DH · Doug DC873F · Ailerons
  > LT OTBD AIL LWR PLATING DEFORMED STA XA 741.000 PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 4. REMOVED DEFORMED NOSE PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-3-0. FABRICATED NEW NOSE PLATING (AL2024T3 0.032") IAW SRM 57-8-1 FIG. 4 ITEM "H". CLEANED, TRE
- [SDR DHLA201000128](https://openairdocs.org/sdr/DHLA201000128.md): Cargo Track · worn · Sep 1, 2010 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO COMPT.-NR3 TRACK LUGS WORN (STA 1670.000 - 1702.000). PERFORMED MAJOR REPAIR IAW SRM 53-2-3, FIG 12, 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 TRACK SEGMENT EXTRUSION PN S277
- [SDR DHLA201000127](https://openairdocs.org/sdr/DHLA201000127.md): Cargo Track · worn · Sep 1, 2010 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO COMPT.- NR4 TRACK LUG WORN (STA 57.000 - 110.000). PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG 12, 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 TRACK SEGMENT EXTRUSION PN S2772660
- [SDR DHLA201000114](https://openairdocs.org/sdr/DHLA201000114.md): Rib · damaged · Sep 1, 2010 · N804DH · Doug DC873F · Trailing Edge Flaps
  > REMOVE DAMAGED RIB IN RT FLAP WELL STA XW 90 AND REPAIR IAW APPROVED DATA PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 10-06-10, EVA D857-00357 REV IR DATED 09-01-10. REMOVED DAMAGED RIB & EXISTING REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED WEB
- [SDR DHLA201000109](https://openairdocs.org/sdr/DHLA201000109.md): Skin · nicked · Sep 1, 2010 · N804DH · Doug DC873F · Trailing Edge Flaps
  > RT OTBD FLAP UPPER SKIN NICK, STA XF 227.000 PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-04-10 EVA D857-00377 REV IR DATED 09-22-10. REMOVED DAMAGED PLATING AND EXISTING SPLICE IAW SRM 51-1-21, SRM 51-3-0. FABRICATED NEW PLATING SEGMENT (AL2024T3 0.071
- [SDR DHLA201000097](https://openairdocs.org/sdr/DHLA201000097.md): Seat Track · worn · Sep 1, 2010 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO COMPT.- NR3 TRACK LUGS WORN STA 1670.000 - 1702.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-3, FIG 12, 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 TRACK SEGMENT EXTRUSION IAW SRM
- [SDR DHLA201000095](https://openairdocs.org/sdr/DHLA201000095.md): Seat Track · worn · Sep 1, 2010 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO COMPT.- NR 4 TRACK LUG WORN STA 57.000 - 110.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG. 12 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 TRACK SEGMENT EXTRUSION IAW SRM 53-2-3
- [SDR DHLA201000131](https://openairdocs.org/sdr/DHLA201000131.md): Skin · corroded · Aug 31, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > FUS LWR SKIN CORRODED, STA 160.000 L-35R - L-36 PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7, SHEET 25,23,24 TR 53-203, DATED JAN 21-2008. REMOVED CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0, PG 2P. REMOVED EXISTING REPAIR NEAR CORRO
- [SDR DHLA201000118](https://openairdocs.org/sdr/DHLA201000118.md): Skin · cracked · Aug 31, 2010 · N804DH · Doug DC873F · Trailing Edge Flaps
  > RT INBD FLAP WELL.- WEB CRACKED 1" STA XF 75.000 PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 10-04-10, EVA D857-00375 REV IR DATED 09-21-10. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER REPAIR STRAP IAW DWG ES-D85700375-001-D REV IR DATED 9-21-10.
- [SDR DHLA201000110](https://openairdocs.org/sdr/DHLA201000110.md): Skin · misrepaired · Aug 31, 2010 · N804DH · Doug DC873F · Horizontal Stabilizer, Plate/Skin
  > PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-11-10, EVA D85500374 REV IR DATED 09-28-10. REMOVED RUB PLATE IAW SRM 51-1-21. CUT OUT DAMAGED AREA + FABRICATED (3EA) FILLERS & INTERNAL REPAIR DOUBLER IAW DWG ES D85500374-001-D REV IR DATED 09-28-10. HEAT
- [SDR DHLA201000106](https://openairdocs.org/sdr/DHLA201000106.md): Skin · cracked · Aug 31, 2010 · N804DH · Doug DC873F · Wing, Plate/Skin
  > REMOVED & REPLACED EXISTING REPAIR ON LT WING T/E AT STA XW 47.000 UTILIZING APPROVED DATA. (REF REPAIR REPORT LW011) REMOVED EXISTING REPAIR AND CUT OUT DAMAGED AREA IAW SRM 57-2-3 PAR 5. FABRICATED DOUBLER (AL7075T6 0.020") IAW SRM 57-3-3 PG 36. BONDED DOUBL
- [SDR DHLA201000103](https://openairdocs.org/sdr/DHLA201000103.md): Skin · damaged · Aug 31, 2010 · N804DH · Doug DC873F · Horizontal Stabilizer, Plate/Skin
  > REMOVED AND REPLACED EXISTING REPAIR LOCATED ON RT HORZ STABILIZER AT XE 159.000 UTILIZING APPROVED DATA (REF REPAIR REPORT HS002) PERFORMED MAJOR REPAIR IAW SRM 55-3-1, FIG 1, SHEET 1-2. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICA
- [SDR DHLA201000093](https://openairdocs.org/sdr/DHLA201000093.md): Skin · corroded · Aug 31, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > FUSELAGE LOWER SKIN CORRODED STA 160.000 L-35R-L-36. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG. 7 SHEET 25,23,24 TR 53-203 DATED. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED EXISTING REPAIR NEAR CORRODED AREA
- [SDR DHLA201000117](https://openairdocs.org/sdr/DHLA201000117.md): Frame · worn · Aug 30, 2010 · N804DH · Doug DC873F · Engine Thrust Reverser
  > NR 3 ENG LT T/R STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE AT STA YN 203.000 (BETWEEN 6 AND 9 O'CLOCK POS) PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR10502 DATED 10-08-10, EVA D878-00368 REV IR DATED 09-15-10. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAM
- [SDR DHLA2010001416](https://openairdocs.org/sdr/DHLA2010001416.md): Skin · misrepaired · Aug 30, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > R & R 3 EXISTING REPAIRS LOCATED ON AFT LOWER BELLY BETWEEN STA 1300-1370.000 LONGERON 36 UTILIZING APPROVED DATA. REF REPAIR REPORT F039, F040 & F041 PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-05-10, EVA D853-00370 REV IR DATED 09-15-10. REMOVED EXI
- [SDR DHLA201000113](https://openairdocs.org/sdr/DHLA201000113.md): Skin · delaminated · Aug 30, 2010 · N804DH · Doug DC873F · Elevator, Tab Structure
  > LT ELEVATOR GEARED TAB DELAMINATED. R & R LT ELEVATOR GEARED TAB IAW MM 27-30-3 PG 201-204. REFER TO NR 265752 FOR OPS CHECK.
- [SDR DHLA201000108](https://openairdocs.org/sdr/DHLA201000108.md): Frame · worn · Aug 30, 2010 · N804DH · Doug DC873F · Engine Thrust Reverser
  > NR 2 ENG LT THRUST REVERSER STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE AT STA YN 203.000 (BETWEEN 6 AND 9 O'CLOCK POS) PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 10486 DATED 09-29-10, EVA-D878-00372 REV IR DATED 09-16-10. CUT OUT DAMAGED AREA. FABRICATED
- [SDR DHLA201000104](https://openairdocs.org/sdr/DHLA201000104.md): Frame · worn · Aug 30, 2010 · N804DH · Doug DC873F · Engine Thrust Reverser
  > NR 3 ENG RT T/R STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE STA YN 202.000 (BETWEEN 5 AND 6 O'CLOCK POS). PERFORMED MAJOR REPAIR IAW FORM 8110-3 NR 10471 DATED 09-22-10, EVA D878-00371 REV IR DATED 09-15-10. CUT OUT DAMAGED AREA, FABRICATED FRAME SEGMENT IA
- [SDR DHLA201000112](https://openairdocs.org/sdr/DHLA201000112.md): Skin · delaminated · Aug 29, 2010 · N804DH · Doug DC873F · Spoilers
  > NR 3 LEFT SPOILER UPPER SKIN DELAMINATED R & R NR3 LT SPOILER IAW MM 27-61-1 PG 201-204. REFER TO NR 265753FOR, OPS CHECK.
- [SDR DHLA201000125](https://openairdocs.org/sdr/DHLA201000125.md): Skin · dented · Aug 28, 2010 · N804DH · Doug DC873F · Trailing Edge Flaps
  > RT INBD FLAP UPPER PLATING DENTED STA XW 68. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DENTED PANEL PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING (AL2024T3 0.025") & BONDED DOUBLER (AL2024T3 0.020") IAW SRM 57-7-1 FIG 1 ITEM "A" & "L"
- [SDR DHLA2010000122](https://openairdocs.org/sdr/DHLA2010000122.md): Skin · misrepaired · Aug 28, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECT EXISTING REPAIR ON RT FUSELAGE STA FS - 17. PERFORMED MAJOR REPAIR IAW SRM 53-2-0, FIG 1 D, SHEET 3 REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21 FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG 1D, SHEET 3, SRM 53-3-3 FIG 1 ITEM "A", SRM 51-9-0 FIG
- [SDR DHLA201000121](https://openairdocs.org/sdr/DHLA201000121.md): Skin · misrepaired · Aug 28, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECT EXISTING REPAIR ON FUS STA -156 FOR CONFORMITY WITH SRM, CONDITION AND SECURITY. IF REPAIR COMPLIES, NOTE DETAILS ON NON ROUTINE. IF REPAIR DOES NOT CONFORM, R & R UTILIZING APPROVED DATA. REF REPAIR REPORT (F011). STRIPPED REPAIR AREA IAW MM 51-20
- [SDR 2010F00223](https://openairdocs.org/sdr/2010F00223.md): Skin · damaged · Aug 28, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECT EXISTING REPAIR ON FUS STA -156 FOR CONFORMITY WITH SRM, CONDITION AND SECURITY. IF REPAIR COMPLIES, NOTE DETAILS ON NON ROUTINE. IF REPAIR DOES NOT CONFORM, R & R UTILIZING APPROVED DATA. REF REPAIR REPORT (F011). STRIPPED REPAIR AREA IAW MM 51-20-0
- [SDR DHLA201000101](https://openairdocs.org/sdr/DHLA201000101.md): Skin · dented · Aug 28, 2010 · N804DH · Doug DC873F · Trailing Edge Flaps
  > RT INBD FLAP UPPER PLATING DENTED STA XW 68 PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DENTED PANEL PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING & BONDED DOUBLER IAW SRM 57-7-1 FIG 1, ITEM "A" & "L". BONDED BOTH PARTS WITH HYSOL IAW
- [SDR DHLA2010000100](https://openairdocs.org/sdr/DHLA2010000100.md): Skin · misrepaired · Aug 28, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21. FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG. 1D SHEET 3, SRM 53-3-3 FIG. 1 ITEM "A" SRM 51-9-0 FIG 68A. CLEANED, TREATED AND PRIMED AREA & REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR DOUBLER IAW SRM 53-
- [SDR DHLA201000094](https://openairdocs.org/sdr/DHLA201000094.md): Skin · misrepaired · Aug 28, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 1 D, SHEET 3 REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21 FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG 1D SHEET 3, SRM 53-3-3 FIG 1 ITEM "A", SRM 51-9-0 FIG 68 A CLEANED, TREATED AND PRIMED AREA & REPAIR DOUBLE
- [SDR DHLA201000071](https://openairdocs.org/sdr/DHLA201000071.md): Battery Pack · inoperative · Aug 14, 2010 · N804DH · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHT BATTERY DEAD. ACFT WAS GROUNDED. R & R EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-1, OPS CK GOOD.
- [SDR DHLA201000068](https://openairdocs.org/sdr/DHLA201000068.md): Rib · damaged · Aug 8, 2010 · N804DH · Doug DC873F · Wing, Rib/Bulkhead
  > ON LANDING, NR8 MAIN TIRE BLEW CAUSING DAMAGE. ON POST FLIGHT INS FOUND RT WING RIB AT STA XW 90.000 DAMAGED. DEFECT RESOLUTION: REPAIRED RIB IAW EVA 085700356-001-D.
- [SDR DHLA2010804001](https://openairdocs.org/sdr/DHLA2010804001.md): Skin · corroded · Feb 4, 2010 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > CORROSION CRACK DISCOVERED ON FUSELAGE EXTERIOR SKIN AT FS 120, AND LONGERON 36, EMANATING FROM FWD ADF ANTENNA. ACCOMPLISHED FUSELAGE SKIN EXTERNAL DOUBLER AND FILLER REPAIR IAW EVA D853-00319, DWG ES D853-00319-001-D, SRM, AMM, AND NDT MANUAL. REF 8110-3
- [SDR DHLA200900055](https://openairdocs.org/sdr/DHLA200900055.md): Fire Detector · false activation · Nov 26, 2009 · N804DH · Doug DC873F · Fire Detection
  > NR 2 ENG FIRE WARNING LIGHT AND BELL. COMPLETED ENG FIRE PHASE ONE ITEMS COMPLETED ENG FIRE CHECK LIST FIRE LIGHT OUT. INSPECTED ENG NR 2 INLET AND EXHAUST INCLUDING FAN AND CORE SECTION NO DAMAGE OR EVIDENCE OF FIRE NOTED. T/S IAW MMS 26-10-01 AND W/D 26-01
- [SDR DHLA2009804002](https://openairdocs.org/sdr/DHLA2009804002.md): Skin · corroded · Nov 2, 2009 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > REFERENCE ASTAR N/R 8285-39: DURING "B" CHECK, FOUND CRACK IN FUSE SKIN AT FS 1442, BETWEEN LONGERON 35R AND 36. ACCOMPLISHED CLASS II EXTERNAL DOUBLER REPAIR FOR CORROSION REMOVAL IAW SRM 53-2-1 FIG 7 TEMP REV. 53-203, 53-2-0, AND 51-1-8. THIS IS A LIFE LI
- [SDR DHLA2000900052](https://openairdocs.org/sdr/DHLA2000900052.md): Bleed Valve · malfunctioned · Oct 29, 2009 · N804DH · Doug DC873F · Compressor Bleed Valve
  > DURING CRUISE, AT 360FL, ODOR OF SMOKE IN COCKPIT. PERFORMED SMOKE SOURCE IDENTIFICATION CHECKLIST. HAD DIFFICULT TIME CONTROLLING CABIN PRESSURE IN AUTO AT ALT PRESSURE SWING 2000 FT/M UP AND DOWN EVERY 10. TRANSFERRED NR 1 ENG HP REG VALVE TO DMI NR 3567
- [SDR DHLA200900048](https://openairdocs.org/sdr/DHLA200900048.md): Pump · worn · Sep 4, 2009 · N804DH · Doug DC873F · Engine Fuel Pump
  > NR 4 ENG FLAMOUTED, PASSING FL350 IN CLIMB. ATTEMPTED RESTART AT FL350 UNSUCCESSFUL ATTEMPTED. ATTEMPED 2ND RESTART DURING DECENT TO CVG AT FL220. ATTEMPTED UNSECCESSFUL. OIL PRESSURE 3-5 PSI TIME OF FAILER 0430Z. LAND AT 0613. PERFORMED FAULT ISOL 51 IN MM 71
- [SDR DHLA2008804001](https://openairdocs.org/sdr/DHLA2008804001.md): Skin · corroded · Aug 13, 2009 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > FUSE SKIN HAS CORROSION AT FS 100 AND BS 0. ACCOMPLISHED FUSE SKIN DOUBLER AND FILLER REPAIR IAW ASTAR EVA D853-00268 AND DWG D85300268-001-D. HFEC OF REPAIR PARTS AND DAMAGE CUT OUT AREA ON FUSELAGE ACCOMPLISHED PER STEP 6 OF LISTED EVA. NO CRACKS OR CORRO
- [SDR DHLA200900024](https://openairdocs.org/sdr/DHLA200900024.md): Flashlight · inoperative · Apr 8, 2009 · N804DH · Doug DC873F · Emergency Equipment
  > EMERGENCY FLASHLIGHT IN LAV INOP. REMOVED AND REPLACED FLASHLIGHT IAW DC-8 MMS 25-60-62, OPS CHECKS GOOD P/N 3800.
- [SDR DHLA200800044](https://openairdocs.org/sdr/DHLA200800044.md): Bulb · malfunctioned · Apr 25, 2008 · N804DH · Doug DC873F · Flight Compartment Lighting
  > FLT NR 445, IF LIGHT OVER LIFE RAFT IN GALLEY AREA RIGHT COMP LIGHT SWITCH ILLUMINATED FOR 2 HRS THERE IS A STRONG CHEMICAL ODOR. RELAMPED IAW MM 33-13-0. OPS CHECK GOOD NO ODOR DETECTED P/N 307. A/C WAS GROUNDED
- [SDR DHLA200800043](https://openairdocs.org/sdr/DHLA200800043.md): Light · odor · Apr 10, 2008 · N804DH · Doug DC873 · Passenger Compartment Lighting
  > FLT NR 160 WITH COMP LIGHT SWITCH ON LIGHT OVER GALLEY ON A PHOSPHOROUS ODOR WAS DETECTED WITH GALLEY POWER OFF TURNED OFF COMP LIGHT SWITCH AND ODOR DISSIPATED, NO SMOKE DETECTED. TURNED ON COMP LIGHTS INSPECTED CARGO COMP LIGHTS, NO ODOR NOTED. OPS CK GOOD

Next page: https://openairdocs.org/deregistered/N804DH-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 = 'N804DH' AND deregistration_id = 'N804DH-2017-09-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N804DH-2017-09-26/reports

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