# Service difficulty reports: N809DH, cancelled Oct 26, 2006

A list on [N809DH, cancelled Oct 26, 2006](https://openairdocs.org/deregistered/N809DH-2006-10-26.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 2 · 67 reports

- [SDR DHL2006809519](https://openairdocs.org/sdr/DHL2006809519.md): Skin · damaged · Aug 17, 2006 · N809DH · Doug DC873F · Wing, Plate/Skin
  > RT WING CTR LE LWR EXTERNAL SKIN HAS AN INTERIM REPAIR AT STA XFS 422.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-12-06, EO NR AST060702 DATED 07-10-06. REMOVED FASTENERS FROM REPAIR AREA AND EXISTING DOUBLER IAW SRM 51-1-20D, SRM
- [SDR DHL2006809522](https://openairdocs.org/sdr/DHL2006809522.md): Skin · worn · Aug 17, 2006 · N809DH · Doug DC873F · Fuselage Main, Plate/Skin
  > FUS EXT SKIN HAS WEAR OF 0.750" AND 0.500" APPROX AT STA 28.000 L-27L TO L-18L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110 DATED 07-14-06, EO AST060705 DATED 07-13-06. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW
- [SDR DHL2006809521](https://openairdocs.org/sdr/DHL2006809521.md): Doubler · cracked · Aug 17, 2006 · N809DH · Doug DC873F · Wing, Plate/Skin
  > RT WING TOP PANEL NR 3 MAIN TANK ACCESS DOOR 505E, CRACK ON PREVIOUSLY REPAIRED DOUBLER CONTINUES 0.375" (STA XRS 107.000 - 139.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-16-06, EO NR AST060707 DATED 07-15-06. REMOVED EXISTING INT
- [SDR DHL2006809520](https://openairdocs.org/sdr/DHL2006809520.md): Pressure Panel · corroded · Aug 17, 2006 · N809DH · Doug DC873F · Fuselage Main, Bulkhead
  > FLT COMPT HORIZ PRESSURE PANEL CORRODED STA -12.000 RBL 30. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-16-06, EO NR AST060706 DATED 07-14-06. REMOVED CORROSION IAW SRM 51-1-8. FOUND OUT OF LIMITS IAW SRM 53-2-0. REMOVED FASTENERS FROM REPAIR AREA I
- [SDR DHL2006809517](https://openairdocs.org/sdr/DHL2006809517.md): Skin · corroded · Aug 17, 2006 · N809DH · Doug DC873F · Wing, Plate/Skin
  > ITEM REF NR 058142: LT OUTER WING OTBD L/E UPPER SKIN CORRODED, STA XFS 742.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-14-06. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF
- [SDR DHL2006809523](https://openairdocs.org/sdr/DHL2006809523.md): Vane · damaged · Aug 17, 2006 · N809DH · Doug DC873F · Trailing Edge Flaps
  > RT INBD VANE SLOT HOLES ELONGATED STA XILD 7095. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-12-06, EO NR AST060701 DATED 07-07-06. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW EO NR AST060701. PERFORMED
- [SDR DHL2006809518](https://openairdocs.org/sdr/DHL2006809518.md): Doubler · cracked · Aug 17, 2006 · N809DH · Doug DC873F · Wing, Plate/Skin
  > RT WING CTR LE INTERNAL SPLICE DOUBLER 1.500" CRACK STA XFS 341.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-14-06, EO NR AST060704 DATED 07-12-06. REMOVED FASTENERS FROM REPAIR AREA IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW E
- [SDR DHL2006809515](https://openairdocs.org/sdr/DHL2006809515.md): Angle · cracked · Aug 14, 2006 · N809DH · Doug DC873F · Rudder Miscellaneous Structure
  > LT RUDDER BASE 2" CRACK AT STA ZR 59.000 CANT OF ANGLE. REMOVED CRACKED ANGLE IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE IAW SRM 51-3-0, SRM 51-3-1 (TORQUE). REFER TO JC EA27200004-001-D (WO 600016595) FOR FABRICATION OF A
- [SDR DHL2006809516](https://openairdocs.org/sdr/DHL2006809516.md): Doubler · broken · Aug 9, 2006 · N809DH · Doug DC873F · Fuselage Miscellaneous Structure
  > FUS INTERNAL DOUBLER BROKEN AND WITH PATCHES, NEAR ACCESS DOOR (STA -156.000 TO -165.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110 DATED 08-07-06, DWG AB78-53-R01 REV IR DATED 07-11-06. REMOVED INTERNAL REINFORCEMENT REPAIR DOUBLER IAW SRM 51-1
- [SDR DHL2006809514](https://openairdocs.org/sdr/DHL2006809514.md): Skin · damaged · Aug 9, 2006 · N809DH · Doug DC873F · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR INTERIM REPAIR AT HOLD OPEN HOOK AREA STA 14.000 L-15L TO L-16L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 08-07-06, DWG NR AB78-53-R02 REV IR DATED 07-13-06. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D, SRM 51
- [SDR DHL2006809512](https://openairdocs.org/sdr/DHL2006809512.md): Attach Fitting · cracked · Aug 8, 2006 · N809DH · Doug DC873F · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT FITTING CRACKED STA 1240.000 L-35L (INTERCOSTAL ATTACH FITTING). REMOVED CRACKED FITTING IAW SRM 51-1-20D AND INSTALLED A NEW ONE IAW SRM 51-1-20D, SRM 51-3-1.
- [SDR DHL2006809510](https://openairdocs.org/sdr/DHL2006809510.md): Intercostal · cracked · Aug 5, 2006 · N809DH · Doug DC873F · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT INTERCOSTAL 0.500" CRACK (STA 8.000 - 25.000, L-28R TO L-29R). REMOVED CRACKED INTERCOSTAL IAW SRM 51-1-21. CLEANED AREA IAW SRM 51-1-8B. INSTALLED NEW INTERCOSTAL IAW SRM 51-1-21. REFER TO JC EA53000007-001-D (WO 600016595) AND BOEING MESS
- [SDR DHL2006809509](https://openairdocs.org/sdr/DHL2006809509.md): Stiffener · cracked · Aug 5, 2006 · N809DH · Doug DC873F · Fuselage Miscellaneous Structure
  > MAIN CARGO COMPT FLOORBEAM STIFFENER 0.500" CRACK STA 980.000 RBL 25" TO RBL 26". REMOVED AND REPLACED FLOORBEAM STIFFENER AT STA 980.000 RBL 25" TO RBL 26" IAW SRM 51-1-20D, SRM 51-3-1. REFER TO JC EA53000006-001-D W/O NR 600016595 FOR FABRICATION.
- [SDR DHL2006809511](https://openairdocs.org/sdr/DHL2006809511.md): Intercostal · cracked · Aug 2, 2006 · N809DH · Doug DC873F · Fuselage Miscellaneous Structure
  > RT MLG W/W INTERCOSTAL DOUBLER 1" CRACK STA 875.000. REMOVED INTERCOSTAL IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51--1-8B. INSTALLED INTERCOSTAL IAW SRM 51-1-21. REFER TO JC EA52000003-001-D (WO 600016595) FOR FABRICATION.
- [SDR DHL2006809513](https://openairdocs.org/sdr/DHL2006809513.md): Doubler · cracked · Aug 1, 2006 · N809DH · Doug DC873F · Fuselage Main, Plate/Skin
  > FUS EXTERIOR EXTERNAL POWER RECEPTACLE DOOR, INTERNAL DOUBLER CRACKED 0.500" STA -32.000 STA -40.000 L-31.5R. PERFORMED MAJOR REPAIR IAW SRM 53-3-3 FIG 1. REMOVED EXISTING INTERNAL DOUBLER IAW SRM 53-1-0, SRM 51-1-21, SRM 51-1-20D. FABRICATED INTERNAL DOUBL
- [SDR DHL2006809506](https://openairdocs.org/sdr/DHL2006809506.md): Floorbeam · corroded · Jul 20, 2006 · N809DH · Doug DC873F · Fuselage Main, Floor Beam
  > AFT ACCY COMPT FLOORBEAM CORRODED STA 1620.000 LBL 10". PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1 SHEET 9, 12, TR NR 51-130 DATE 06-26-04. REMOVED FASTENERS IAW SRM 51-1-20D. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 P
- [SDR DHL2006809507](https://openairdocs.org/sdr/DHL2006809507.md): Panel · cracked · Jul 18, 2006 · N809DH · Doug DC873F · Nacelle/Pylon Miscellaneous Structure
  > NR 4 PYLON INBD ADAPTER PANEL 1" CRACK STA YN 323.000 LT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 70 SB 54-93 CONDITION V. REMOVED FASTENERS FROM REPAIR AREA AND ATTACH PARTS IAW DC8 70 SB 54-93, SRM 51-1-21, SRM 51-3-0. FABRICATED DOUBLERS (4) (AL707
- [SDR DHL2006809508](https://openairdocs.org/sdr/DHL2006809508.md): Skin · delaminated · Jul 17, 2006 · N809DH · Doug DC873F · Trailing Edge Flaps
  > LT WING NR 4 FLAP VANE INTERNAL SKIN DELAMINATED. REMOVED AND REPLACED NR 4 LT FLAP VANE IAW MM 27-51-14 PG 201-202. REFER TO NR 058548 FOR OPS CHECK.
- [SDR DHL2006809505](https://openairdocs.org/sdr/DHL2006809505.md): Skin · damaged · Jul 17, 2006 · N809DH · Doug DC873F · Trailing Edge Flaps
  > LT INBD FLAP UPPER SKIN HAS AN INTERIM REPAIR (STA XW 104.000 - 106.000). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED PANEL PLATING WITH EXISTING INTERIM REPAIR IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PANEL PLATING WITH PLATING (AL2024T3 0
- [SDR DHL2006809504](https://openairdocs.org/sdr/DHL2006809504.md): Fitting · cracked · Jul 17, 2006 · N809DH · Doug DC873F · Wing Miscellaneous Structure
  > NR 1 LT STUB WING FITTING 3" CRACK STA XW 454.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0. REMOVED CRACKED FITTING IAW SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-
- [SDR DHL2006809500](https://openairdocs.org/sdr/DHL2006809500.md): Doubler · cracked · Jul 12, 2006 · N809DH · Doug DC873F · Wing Miscellaneous Structure
  > NR 4 RT STUB WING L/E LWR REPAIR FASTENERS IMPROPER STA XFS 562.500 AND CRACK. PERFORMED MAJOR REPAIR IAW SRM 57-2-1A FIG 2. REMOVED FASTENERS, REPAIR DOUBLER, INTERNAL DOUBLER AND EXISTING RIM IAW SRM 51-1-20D. FABRICATED EXTERNAL REPAIR DOUBLER (AL7075T6
- [SDR DHL2006809002](https://openairdocs.org/sdr/DHL2006809002.md): Uplock Switch · dirty · Jun 24, 2006 · N809DH · Doug DC873F · Landing Gear Position and Warning
  > DURING GEAR UPLATCH CHECK, GEAR UNLOCK LIGHT ILLUMINATED. ABNORMAL PROCEDURE COMPLETED. CONTINUED FLIGHT WITH GEAR HANDLE UP. LUBED LEFT AND RIGHT UPLOCK ACTUATOR, CLEANED UPLOCK SWITCHES, PERFORMED A/C JACKING AND PERFORMED 3 GEAR SWINGS IAW 32-31-3. OPS
- [SDR DHL2006809001](https://openairdocs.org/sdr/DHL2006809001.md): Control Panel · smoke · Mar 29, 2006 · N809DH · Doug DC873F · Flight Compartment Lighting
  > SMOKE SEEN COMING FROM LONG TRIM IND AREA OR CENTER PEDESTAL. SMOKE CLEARED IMMEDIATELY WHEN PEDESTAL LIGHTS SWITCH WAS PLACED IN OFF. FOUND CRACKED LONG TRIM PANEL PULLED & COLLARD PED & OVERHEAD SW PANEL C/B FOR LIGHTS DEFERRED IAW DC8 MEL 33-1 DMI 24805.
- [SDR DHL2005809005](https://openairdocs.org/sdr/DHL2005809005.md): Handle · unsecure · Dec 23, 2005 · N809DH · Doug DC873F · Cargo/Baggage Doors
  > MASTER WARNING LIGHT CAME ON DURING TAKEOFF ROLL. FOUND "B" PIT HANDLE NOT STOWED, PER M/M 52-31-1, OPS CHECK GOOD.
- [SDR DHL2005809004](https://openairdocs.org/sdr/DHL2005809004.md): Battery Pack · intermittent · May 21, 2005 · N809DH · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHT WORK INTERMITTENLY DURING PREFLIGHT CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ASSY IAW 33-50-1, OPS CK NORMAL.
- [SDR DHL2005809003](https://openairdocs.org/sdr/DHL2005809003.md): O-Ring · leaking · May 4, 2005 · N809DH · Doug DC873F · Turbine Engine Oil System
  > 1+ 12 HR INTO FLT NR 1 ENG LOST OIL QUANTITY WITH RESULT OF LOW OIL PRESS PERFORMED ABNORMAL PROCEDURE AND ENG SHUT DOWN. REPLACED O-RING AT STARTER CASE. PER DC-8 M/M 80-10-02 OPS CHECK NORMAL ON RUNS PER JRH CH 13, P/N M83248-1-160.
- [SDR DHL2005809002](https://openairdocs.org/sdr/DHL2005809002.md): Light · inoperative · Mar 23, 2005 · N809DH · Doug DC873F · Emergency Lighting
  > DEMERGENCY EXIT LIGHTS INOP. PERFORMED OPS CHECKS OF EMERGENCY LIGHTS SYSTEM OPS CKS OK IAW MM 33-50-0
- [SDR DHL2005809001](https://openairdocs.org/sdr/DHL2005809001.md): Connector · disconnected · Mar 22, 2005 · N809DH · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHTS WOULD NOT TEST DURING PREFLIGHT. RESECURED CONNECTOR TO EMERGENCY LIGHT RELAY PAC, OPS NORMAL PER MM 33-50-1.
- [SDR DHL2004809530](https://openairdocs.org/sdr/DHL2004809530.md): Longeron · corroded · Jan 21, 2005 · N809DH · Doug DC873F · Fuselage Main, Longeron/Stringer
  > AFT ACCY COMPT L-34 CORRODED STA 1694. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. TRIMMED OUT CORRODED LONGERON SEGMENT IAW SRM 53-2-2 FIG 8. FABRICATED STANDARD LONGERON SPLICE (AL7075-T6510.100) IAW SRM 53-2-2 FI
- [SDR DHL2004809523](https://openairdocs.org/sdr/DHL2004809523.md): Structure · worn · Jan 20, 2005 · N809DH · Doug DC873F · Trailing Edge Flaps
  > RT WING OUTBOARD FLAP UPPER FWD PLATING WORN, XF 227.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 01-19-05, DWG X32-R04 REV-A DATE 01-19-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. TRIMMED OUT DAMAGED PLATING SEGMENT
- [SDR DHL2004809524](https://openairdocs.org/sdr/DHL2004809524.md): Pressure Panel · cracked · Jan 20, 2005 · N809DH · Doug DC873F · Fuselage Main, Bulkhead
  > MAIN CARGO COMPT MLG PRESSURE PANEL SKIN CRACKED STA 907.000 LBL 41. (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 01-19-05 DWG X32-R05 REV A DATE 01-19-05. REMOVED EXISTING REPAIR IAW DWG X32-R05, SRM 51-1-21 PG.1, SRM 51-3-0 PG.1. TRIMMED
- [SDR DHL2004809528](https://openairdocs.org/sdr/DHL2004809528.md): Skin · corroded · Jan 20, 2005 · N809DH · Doug DC873F · Fuselage Main, Plate/Skin
  > LWR FUSELAGE EXTERIOR SKIN CORRODED AT STA 1690.000 (L-28L TO L-28R). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P.
- [SDR DHL2004809526](https://openairdocs.org/sdr/DHL2004809526.md): Panel · delaminated · Jan 18, 2005 · N809DH · Doug DC873F · Fuselage Miscellaneous Structure
  > AFT FUSELAGE 732 LWR PANEL EDGE UNBONDED AND DELAMINATED, STA 980.000 TO STA 1060.000. REMOVED DELAMINATED PANEL IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL ASSY IAW SRM 51-3-0.
- [SDR DHL2004809527](https://openairdocs.org/sdr/DHL2004809527.md): Skin · delaminated · Jan 17, 2005 · N809DH · Doug DC873F · Wing, Plate/Skin
  > LT WING - REMOVE AND INSTALL NR 1 SPOILER FOR DELAMINATION ON UPPER SKIN, XW 5.000 TO XW 90.000. REMOVED AND REPLACED NR 1 SPOILER (O/H CONDITION) ON LT WING XW 5.000 TO XW 90.000 (LT WING) IAW MM 27-61-1 PG 201-205.
- [SDR DHL2004809529](https://openairdocs.org/sdr/DHL2004809529.md): Fitting · cracked · Jan 17, 2005 · N809DH · Doug DC873F · Fuselage Main, Attach Fittings
  > AFT CARGO COMPT SPLICE FITTING CRACKED 2.000 BETWEEN STA 1060.000 AND STA 1040.000, L-35R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW DC8 SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AR
- [SDR DHL2004809525](https://openairdocs.org/sdr/DHL2004809525.md): Fitting · cracked · Jan 17, 2005 · N809DH · Doug DC873F · Fuselage Main, Attach Fittings
  > AFT CARGO COMPT RT TUNNEL FITTING CRACKED 2.000, STA 1220.000. REMOVED CRACKED FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 1, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1,
- [SDR DHL2004809522](https://openairdocs.org/sdr/DHL2004809522.md): Bracket · broken · Jan 17, 2005 · N809DH · Doug DC873F · Wing, Attach Fittings
  > LEFT OUTBOARD SLOT UPPER DOOR BRACKET BROKEN. REMOVED AND REPLACED BROKEN BRACKET TO OUTBOARD SLOT DOOR UPPER DOOR IAW MM 27-80-2 PG 201-202, MM 20-16-0 PG 201-208.
- [SDR DHL2004809521](https://openairdocs.org/sdr/DHL2004809521.md): Bracket · cracked · Jan 17, 2005 · N809DH · Doug DC873F · Wing, Attach Fittings
  > NR 4 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED AFT BOOSTER PUMP BRACKET (NR 4 ALT TANK) IAW SRM 51-1-20D PG 9, 21 SRM 51-3-1 PG 2A.
- [SDR DHL2004809519](https://openairdocs.org/sdr/DHL2004809519.md): Skin · delaminated · Jan 14, 2005 · N809DH · Doug DC873F · Fuselage Main, Plate/Skin
  > LT FWD ADF SENSE ANTENNA PANEL INTERNAL SKIN DELAMINATED (STA 810.000-855.000). REMOVED LT FWD ADF SENSE ANTENNA PANEL IAW SRM 51-3-0 PG 1. CLEANED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LT FWD ADF SENSE ANTENNA PANEL IAW SRM 51-3-0 PG 1.
- [SDR DHL2004809520](https://openairdocs.org/sdr/DHL2004809520.md): Support · cracked · Jan 14, 2005 · N809DH · Doug DC873F · Cargo/Baggage Doors
  > B-CARGO DOOR RT ROLLER SUPPORT CRACKED. REMOVED B-CARGO DOOR IAW MM 52-32-1 PG 201. REMOVED AND REPLACED RT ROLLER SUPPORT IAW OHM 52-3-5 PG 1-2. REINSTALLED B-CARGO DOOR IAW MM 52-32-1 PG 201-203. OPS CHECKED GOOD IAW MM 52-30-0 PG 7-11.
- [SDR DHL2004809518](https://openairdocs.org/sdr/DHL2004809518.md): Bracket · broken · Jan 14, 2005 · N809DH · Doug DC873F · Wing, Attach Fittings
  > LT WING TRACK ASSY BRACKET BROKEN, XW 104.000. REMOVED AND REPLACED BRACKET ON LT WING TRACK ASSY XW 104.000 IAW SRM 51-3-0 PG 1, SRM 51-1-27A PG 1-4.
- [SDR DHL2004809531](https://openairdocs.org/sdr/DHL2004809531.md): Skin · damaged · Jan 10, 2005 · N809DH · Doug DC873F · Trailing Edge Flaps
  > LT WING INBD FLAP UPPER SKIN DEFLECTED, XW 2.000 TO XW 91.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED DAMAGED PANEL PLATING IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW PANEL PLATING (AL2024-T3 0.050) IAW BOEING MESSAGE 1-XW84N, DWG SEMAN E
- [SDR DHL2004809517](https://openairdocs.org/sdr/DHL2004809517.md): Longeron · cracked · Jan 6, 2005 · N809DH · Doug DC873F · Fuselage Main, Longeron/Stringer
  > AFT FUSELAGE L-17R CRACKED 3.000, STA 1766.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5 SHEET 1. REMOVED DAMAGED LONGERON IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT TO
- [SDR DHL2004809516](https://openairdocs.org/sdr/DHL2004809516.md): Fitting · cracked · Jan 5, 2005 · N809DH · Doug DC873F · Fuselage Main, Attach Fittings
  > AFT FUSELAGE FITTING CRACKED 1.000, NEXT L-17R STA 1766.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW
- [SDR DHL2004809515](https://openairdocs.org/sdr/DHL2004809515.md): Fitting · cracked · Jan 5, 2005 · N809DH · Doug DC873F · Fuselage Main, Attach Fittings
  > FWD CARGO COMPT SPLICE FITTING CRACKED 3.000, STA 600.000 TO STA 620.000 L-31L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW SPL
- [SDR DHL2004809514](https://openairdocs.org/sdr/DHL2004809514.md): Crossbeam · corroded · Jan 3, 2005 · N809DH · Doug DC873F · Fuselage Main, Structure
  > AFT ACCY COMPT CROSS BEAM CORRODED STA 1680.000 RBL 12 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1 (SHEET 7, 12), TR 51-130. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SECTION IAW SR
- [SDR DHL2004809510](https://openairdocs.org/sdr/DHL2004809510.md): Skin · corroded · Dec 30, 2004 · N809DH · Doug DC873F · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE - EXTERNAL SKIN CORRODED STA 857.000 L-11L (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. PERFORMED
- [SDR DHL2004809513](https://openairdocs.org/sdr/DHL2004809513.md): Skin · damaged · Dec 30, 2004 · N809DH · Doug DC873F · Trailing Edge Flaps
  > RT WING OUTBOARD FLAP FWD UPPER PLATING HAS INTERIM REPAIR, XF 211.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 12-28-04, DWG X32-R03 REV IR DATE 12-21-04. REMOVED PLATING WITH INTERIM REPAIR AND EXISTING INTERNAL SPLICE IAW DWG X32-R03, SR
- [SDR DHL2004809512](https://openairdocs.org/sdr/DHL2004809512.md): Fairing · cracked · Dec 30, 2004 · N809DH · Doug DC873F · Wing Miscellaneous Structure
  > RIGHT WING T/E FAIRING CRACKED 2.000 (STA XW -5.000 TO 5.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 12-22-04, DWG X32-R01, REV IR DATED 12-20-04, DWG 5651221. REMOVED CRACKED FAIRING IAW SRM 51-1-21 PG 1. FABRICATED NEW FAIRING (AL2
- [SDR DHL2004809508](https://openairdocs.org/sdr/DHL2004809508.md): Channel · cracked · Dec 28, 2004 · N809DH · Doug DC873F · Fuselage Miscellaneous Structure
  > MAIN CARGO COMPT CHANNEL CRACKED 1.000 STA 680.000 RBL 24. REMOVED CRACKED CHANNEL IAW SRM 51-1-20D PG 1. FABRICATED NEW CHANNEL (AL7075-0-0.100) IAW DWG 5773275. HEAT TREATED IAW DACO DPS 7.00. PERFORMED NDT INSP IAW DC8 NDT SPM PART 08-00-02/07. CLEANED

Next page: https://openairdocs.org/deregistered/N809DH-2006-10-26/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 = 'N809DH' AND deregistration_id = 'N809DH-2006-10-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N809DH-2006-10-26/reports

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