# Service difficulty reports: N802DH

A list on [N802DH](https://openairdocs.org/aircraft/N802DH.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 11 · 511 reports

- [SDR DHLA201100536](https://openairdocs.org/sdr/DHLA201100536.md): Battery Pack · inoperative · Aug 15, 2011 · N802DH · Doug DC873F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS INOPERATIVE. ACFT GROUNDED. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK AND OPS CHECKED GOOD IAW MM 33-50-1.
- [SDR 2010FA0000325](https://openairdocs.org/sdr/2010FA0000325.md): Frame · worn · Mar 26, 2010 · N802DH · Doug DC873 · Engine Thrust Reverser
  > (SPUY) DURING ROUTINE C-CHECK INSPECTION, NR 3 ENG LT T/R FIXED STRUCTURE FRAME WORN, STA YN 203.000 AT 7 O`CLOCK POS.
- [SDR 2010FA0000324](https://openairdocs.org/sdr/2010FA0000324.md): Frame · worn · Mar 26, 2010 · N802DH · Doug DC873 · Engine Thrust Reverser
  > (SPUY) DURING ROUTINE C-CHECK INSPECTION, NR 2 ENGINE. T/R FIXED STRUCTURE FRAME WORN, STA YN 203.000 AT 5 O`CLOCK POSITION RT.
- [SDR 2010FA0000316](https://openairdocs.org/sdr/2010FA0000316.md): Unknown · unknown · Mar 26, 2010 · N802DH · Doug DC873 · Standard Practices/Structures
  > (SPUY) DURING ROUTINE C-CHECK INSPECTION, R & R EXISTING REPAIR LOCATED FS 1180.000- 1200.000, L36 WITH A REPAIR IAW APPROVED DATA (SRM) LIST ANY AND ALL REINSPECTIONS ON THE NON-ROUTINE.
- [SDR 2010FA0000312](https://openairdocs.org/sdr/2010FA0000312.md): Skin · corroded · Mar 26, 2010 · N802DH · Doug DC873 · Vertical Stabilizer, Plate/Skin
  > (SPUY) DURING ROUTINE C-CHECK INSPECTION, VERT STAB - CORROSION BETWEEN SKIN AND BEADED DOUBLER (STA ZR 153.000 - 281.963).
- [SDR DHLA201000040](https://openairdocs.org/sdr/DHLA201000040.md): Frame · corroded · Mar 18, 2010 · N802DH · Doug DC873 · Fuselage Main, Frame
  > AFT CARGO BAY FRAME CAP SHOWS MISDRILLED HOLES & CORROSION DAMAGE BS 1180.000 L32L-32R. PERFORMED MAJOR REPAIR IAW FORM 8110-3, DATED 04-23-10, EVA D853-00325, REV 01, DATED 04-15-10. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2
- [SDR 2010FA0000230](https://openairdocs.org/sdr/2010FA0000230.md): Cable · broken · Mar 16, 2010 · N802DH · Doug DC873 · Aileron Control System
  > RT AILERON BUS CABLE PN 3763151-501 BROKEN JUST OTBD OF THE RT INBD AILERON. FOUND LT AILERON WAS INOPERATIVE; THEREFORE PLACING HIGH TENSION ON THE BUS CABLE. WE ARE QUARANTINING THE ACTUATOR AND CABLE ASSY UNTIL FURTHER INVESTIGATION.
- [SDR DHLA201000045](https://openairdocs.org/sdr/DHLA201000045.md): Skin · corroded · Mar 10, 2010 · N802DH · Doug DC873 · Vertical Stabilizer, Plate/Skin
  > VERT STAB-CORROSION BETWEEN SKIN AND BEADED DOUBLER STA ZR 253.000-281-963. RESOLUTION PERFORMED MAJOR REPAIR IAW SRM 55-5-1, FIG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-20. FOUND OUT OF LIMITS IAW SRM 55-2-0 FIG 6. REMOVED PLATING BEADED DOUBLER IAW SRM 55
- [SDR DHLA201000044](https://openairdocs.org/sdr/DHLA201000044.md): Support Fitting · cracked · Mar 8, 2010 · N802DH · Doug DC873 · Wing, Control Surface Attach Fittings
  > LT OTBD FLAP HINGE SUPPORT FITTING CRACKED 1" STA 339.000. PERFORMED MAJOR REPAIR IAW SB 27-249 DATED 05-29-74 REV IR JULY 15-93, DWG NR 5894377. REMOVED OTBD FLAP HINGE SUPPORT FITTING IAW SRM 57-1-0, PG 1, SRM 51-1-21, SRM 51-1-20D SRM 51-3-0. CLEANED, TREA
- [SDR DHLA201000043](https://openairdocs.org/sdr/DHLA201000043.md): Pin · cracked · Mar 7, 2010 · N802DH · Doug DC873 · Cargo/Baggage Doors
  > CARGO DOOR FITTING LATCH PIN CRACKED 1". RESOLUTION: PERFORMED MAJOR REPAIR IAW SRM 52-1-0, PG 1. REMOVED FITTING ASSY CORNER IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ASSY CORNER IAW SR
- [SDR DHLA201000047](https://openairdocs.org/sdr/DHLA201000047.md): Doubler · corroded · Mar 6, 2010 · N802DH · Doug DC873 · Fuselage Main, Plate/Skin
  > FWD ASSY COMPT. JACK PAD INTERNAL DOUBLER CORRODED STA 70.000 L-36. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED JACK PAD DOUBLER IAW SRM 51-1-21. CLEANED, T
- [SDR DHLA201000038](https://openairdocs.org/sdr/DHLA201000038.md): Frame · worn · Mar 6, 2010 · N802DH · Doug DC873 · Engine Thrust Reverser
  > NR 4 ENG RT T/R FIXED STRUCTURE FRAME WORN STA YN 206.000 AT 5 O'CLOCK POS PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-16-10, EVA D878-00309 REV IR DATED 03-31-10. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED AREA AND FABRICATED NEW F
- [SDR DHLA201000051](https://openairdocs.org/sdr/DHLA201000051.md): Longeron Fitting · cracked · Mar 4, 2010 · N802DH · Doug DC873 · Fuselage Main, Longeron/Stringer
  > LWR FUSELAGE L-34L END FITTING CRACKED 3" STA 780.000. PERFORMED MAJOR REPAIR IAW SRM 53-1-0, PG 1. REMOVED CRACKED END FITTING IAW SRM 53-1-0 PG 1, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW END FITTING WITH SAME FASTENERS IA
- [SDR DHLA201000046](https://openairdocs.org/sdr/DHLA201000046.md): Longeron Fitting · cracked · Mar 4, 2010 · N802DH · Doug DC873 · Fuselage Main, Longeron/Stringer
  > LWR FUSELAGE L-34R END FITTING CRACKED 3" STA 780.000. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED END FITTING IAW SRM 53-1-0, PG 1. SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW END FITTING WITH SOME FASTENERS
- [SDR DHLA201000042](https://openairdocs.org/sdr/DHLA201000042.md): Frame · worn · Mar 4, 2010 · N802DH · Doug DC873 · Nacelle/Pylon, Frame/Spar/Rib
  > NR3 ENG LT T/R FIXED STRUCTURE FRAME WORN STA YN 203.000 AT 7 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW FORM 8110-3, DATED 04-16-10, EVA D878-00307 REV IR DATED 03-30-10. REMOVED FASTENERS IAW SRM 51-1-221, SRM 51-3-0. CUT OUT DAMAGED AREA AND FABRICATED NEW FR
- [SDR DHLA201000041](https://openairdocs.org/sdr/DHLA201000041.md): Frame · worn · Mar 4, 2010 · N802DH · Doug DC873 · Nacelle/Pylon, Frame/Spar/Rib
  > NR3 ENG T/R FIXED STRUCTURE FRAME WORN STA YN 203.000 AT 5 O'CLOCK POS. RT PERFORMED MAJOR REPAIR IAW FORM 8110-3, DATED 04-16-10, EVA D878-00308 REV IR DATED 03-31-10. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED AREA AND FABRICATED NEW FRAM
- [SDR DHLA201000039](https://openairdocs.org/sdr/DHLA201000039.md): Angle · cracked · Mar 4, 2010 · N802DH · Doug DC873 · Nacelle/Pylon Miscellaneous Structure
  > NR3 ENG TO PYLON ANGLE CRACKED 10" AT 12 O'CLOCK POS STA YN 183.000-202.500. PERFORMED MAJOR REPAIR IAW FORM 8110-3 DATED 04-21-10 EVA D854-00305 REV IR DATED 03-23-10. CUT OUT DAMAGED AREA IAW SMN DWG ED-5104 REV 01 DATED 03-18-10. VISUALLY INSPECTED CUT OUT
- [SDR DHLA201000037](https://openairdocs.org/sdr/DHLA201000037.md): Structure · damaged · Mar 4, 2010 · N802DH · Doug DC873 · Engine Thrust Reverser
  > NR 2 ENG T/R TRANSLATING COWL HOLES ELONGATED STA 240.000 BETWEEN 6 AND 7 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW FORM 8110-3 DATED 04-20-10, EVA D878-00324 REV IR DATED 04-02-10. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED AREA AND FABRICATED (2EA) F
- [SDR DHLA201000050](https://openairdocs.org/sdr/DHLA201000050.md): Vane · delaminated · Mar 3, 2010 · N802DH · Doug DC873 · Trailing Edge Flaps
  > NR 4 LT FLAP VANE DELAMINATED. R & R NR 4 LT FLAP VANE IAW MM 27-51-14, PG 201-203. REFER TO NR 225817 FOR OPS CHECK.
- [SDR DHLA201000049](https://openairdocs.org/sdr/DHLA201000049.md): Skin Panel · delaminated · Mar 3, 2010 · N802DH · Doug DC873F · Spoilers
  > NR 1 LT SPOILER EXTERNAL SKIN DELAMINATED 3". R & R NR 1 LT SPOILER PANEL (REPAIR CONDITION) IAW MM 27-61-1, PG 201-206. REFER TONR 225817 FOR OPS CHECK.
- [SDR DHLA201000048](https://openairdocs.org/sdr/DHLA201000048.md): Skin · delaminated · Mar 3, 2010 · N802DH · Doug DC873 · Trailing Edge Flaps
  > RT WING FLAP JOINT DELAMINATED. REMOVED DELAMINATED JOINT FLAP IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED JOINT FLAP (REPAIRED CONDITION) IAW SRM 51-3-0 SRM 51-3-1 (TORQUE) (TORQUE WRENCH: SNAP ON, MODEL: QC1R200, SN 089620045
- [SDR 2010F00054](https://openairdocs.org/sdr/2010F00054.md): Cable · broken · Feb 27, 2010 · N802DH · Doug DC873 · Aileron Control System
  > RT AILERON BUS CABLE PN 3763151-501 BROKEN JUST OTBD OF THE RT INBD AILERON. FOUND LT AILERON ACTUATOR WAS INOPERATIVE THEREFORE PLACING HIGH TENSION ON THE BUS CABLE. QUARANTINED THE ACTUATOR AND CABLE ASSY UNTIL FURTHER INVESTIGATION.
- [SDR DHLA20100005](https://openairdocs.org/sdr/DHLA20100005.md): Transducer · malfunctioned · Feb 19, 2010 · N802DH · Doug DC873 · Stall Warning System
  > FLT NR 981, AT THE START OF THE TO ROLL (A/S <60 KTS) THE STICK SHAKER ACTIVATED. TROUBLESHOT FOUND LIFT TRANSDUCER BAD. R & R LIFT TRANSDUCER IAW MM 34-16-1 PERFORMED ADJUSTMENT TEST OF STALL WARN SYS IAW MMS 34-16-00 & 34-16-01, OPS NORMAL. ACFT WAS GROUND
- [SDR DHLA20100004](https://openairdocs.org/sdr/DHLA20100004.md): Stick Shaker · malfunctioned · Feb 18, 2010 · N802DH · Doug DC873 · Stall Warning System
  > STICK SHAKER ACTIVATED ON TAKEOFF ROLL, AT 60 KTS REJECTED TAKEOFF. PERFORMED STALL WARNING SYS TROUBLESHOOTING IAW MM 34-16-0. NO DEFECTS NOTED. FOUND NOSE STRUT AT 9 INCHES. SERVICED NOSE STRUT IAW MM 32-21-12. W&B NOTED TO BE ON THE AFT SIDE OF THE CG. HAD
- [SDR DHLA200800033](https://openairdocs.org/sdr/DHLA200800033.md): Fire Detector · malfunctioned · Jun 5, 2009 · N802DH · Doug DC873 · Detection System
  > FLT NR 403, NR 1 ENGINE FIRE WARNING FLASHED A COUPLE OF TIMES DURING FINAL APPROACH LOOP A HANDLE AND MASTER LIGHTS. DEFERRED PER MEL 26-2-3 A-LOOP DMI NR 31485 PLACARD INSTALLED CAT C B-LOOP. OPS CK GOOD SP C/W 26-2. T/S SYS IAW MMS 26-10-0. REMOVED AND
- [SDR DHLA200900031](https://openairdocs.org/sdr/DHLA200900031.md): Duct · blown · May 20, 2009 · N802DH · Doug DC873 · Pneumatic Distribution System
  > DURING TAKEOFF ROLL MASTER FIRE WARNING ON GLARESHIELD AND SECOND OFFICERS FIRE WARNING LIGHT AND FIREBELL, REJECTED TAKEOFF AT 100 KTS. NO LIGHT IN HANDLES, LIGHTS AND BELL EXTINGUISHED UPON STOPPING. FOUND 9TH BLEED AIR DUCT BLOWN. REPLACED DUCT ASSY PER
- [SDR DHLA200900019](https://openairdocs.org/sdr/DHLA200900019.md): Bulb · inoperative · Apr 1, 2009 · N802DH · Doug DC873 · Emergency Lighting
  > WHEN EMERGENCY LIGHT SWITCH PLACED TO DISARM, EMERGENCY LIGHTS DISARM LIGHT FAILS TO ILLUMINATE. REMOVED AND REPLACED LIGHT BULB P/N 313. OPS CK GOOD IAW M/M 33-50-0.
- [SDR DHLA200800009A](https://openairdocs.org/sdr/DHLA200800009A.md): Fire Loop · malfunctioned · Feb 3, 2009 · N802DH · Doug DC873 · Fire Detection
  > WHILE TAXIING INTO BLOCKS IN ATLANTA WITH NR 1 AND 4 SHUTDOWN, FIREWARNING ACTIVATED ON NR 1, LOOP B. SWITCHING LOOP A, FIREWARNING WENT AWAY. DEFER PER MEL 26-2-3, CAT C DMI 34495, DDD 02-13-09. PLACARD INSTALLED
- [SDR DHLA200800006A](https://openairdocs.org/sdr/DHLA200800006A.md): Fire Warning · illuminated · Jan 26, 2009 · N802DH · Doug DC873 · Fire Detection
  > ON TAXI IN NR 1 ENGINE FIRE LIGHT ILLUMINATED. ACCOMPLISHED ENGINE FIRE CHECK LIST. TRANSFERRED TO DMI LOG NR 34462, REF MEL 26-2-3 CAT C. PLACARDS INSTALLED.
- [SDR DHLA200800134](https://openairdocs.org/sdr/DHLA200800134.md): Fire Warning · illuminated · Dec 10, 2008 · N802DH · Doug DC873 · Fire Detection
  > FIRE INDICATION NR 1 ENG DURING APPROACH. FIRED BOTTLES INBOARD. NR 1 ENG FIRE LOOP B DEFERRED PER MEL 26-2-3 CT C DMI 34247. INSTALL PLACARD INST SPEC PROC C/W. MX NOTIFIED.
- [SDR DHLA200800123](https://openairdocs.org/sdr/DHLA200800123.md): Connector · loose · Nov 6, 2008 · N802DH · Doug DC873 · Fire Protection System Wiring
  > DURING CRUISE FLT 370 ENG FIRE NR 4 IND/ FOLLOWED EMERGENCY PROCEDURES PER AOM / LANDED AT ATL / A&B LOOPS WERE CHK'D B LOOP STEADY IND / A LOOP INTERMITTENT. DEFERRED PER MEL 26-2-3 DMI 34020 ASSIGNED PLACARD INSTALLED REF: LG PG A02579 ITEM 1. NR 4 ENG FI
- [SDR DHL2007806521](https://openairdocs.org/sdr/DHL2007806521.md): Skin · misrepaired · Apr 2, 2007 · N802DH · Doug DC873 · Cargo/Baggage Doors
  > REPAIR ON FWD UPPER JAMB CORNER OF "D" CARGO DOOR IS NOT IN ACCORDANCE WITH DWG SR08530019 (STA 1400.000 - 1420.000 L-25R TO L-27R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW AD2005-18-07 S/B DC8 53-078, DOUGLAS DWG NR SR08530019, 5750776. REMOVED EXISTING NON
- [SDR DHL2007802539](https://openairdocs.org/sdr/DHL2007802539.md): Bulkhead · corroded · Feb 13, 2007 · N802DH · Doug DC873 · Fuselage Main, Bulkhead
  > FWD ACCY COMPT FWD PRESSURE BULKHEAD CAP SHOWS CORROSION AT STA 8.000 L-29R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR ACG2-53-110 REV IR DATED 01-26-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED
- [SDR DHL2007802536](https://openairdocs.org/sdr/DHL2007802536.md): Access Door · delaminated · Feb 11, 2007 · N802DH · Doug DC873 · Wing, Plate/Skin
  > RT WING T/E UPPER ACCESS DOOR NR 510 DELAMINATED (XA 475.000 - 507.000). REMOVED AND REPLACED DELAMINATED ACCESS DOOR NR 510 RT WING T/E IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).
- [SDR DHL2007802537](https://openairdocs.org/sdr/DHL2007802537.md): Rib · cracked · Feb 8, 2007 · N802DH · Doug DC873 · Wing, Rib/Bulkhead
  > NR 1 LT STUB WING UPPER INTERNAL RIB CRACKED STA XS 530.168 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EA NR 06783 IAW DOUGLAS DWG NR 9753297. REMOVED CRACKED RIB IAW SRM 51-1-21, SRM 51-1-20D. INSTALLED NEW RIB IAW DOUGLAS DWG NR 9753297, SRM 51-1-21, SRM
- [SDR DHL2007802535](https://openairdocs.org/sdr/DHL2007802535.md): Longeron · corroded · Feb 8, 2007 · N802DH · Doug DC873 · Fuselage Main, Longeron/Stringer
  > AFT ACCY COMPT L-30L CORRODED, STA 1746.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG 4A. REMOVED CORROSION IAW SRM 51-1-18 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION AND
- [SDR DHL2007802531](https://openairdocs.org/sdr/DHL2007802531.md): Door Frame · cracked · Feb 8, 2007 · N802DH · Doug DC873 · Fuselage Main, Structure
  > "B" CARGO DOOR AFT LWR JAMB CORNER 0.750" CRACK STA 560.000 L-31R TO L-32R. PERFORMED MAJOR REPAIR IAW AD2005-18-07 S/B 53-078 REV 1 JAN 25-01, FAA FORM 8100-9 DATED 02-05-07, BOEING MSG 1-274569547-4 DATED 02-05-07. REMOVED EXISTING REPAIR DOUBLER IAW SRM 5
- [SDR DHL2007802538](https://openairdocs.org/sdr/DHL2007802538.md): Longeron · corroded · Feb 6, 2007 · N802DH · Doug DC873 · Fuselage Main, Longeron/Stringer
  > AFT ACCY COMPT SHOWS CORROSION AT STA 1660.000 L-24L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG 4A. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SEC
- [SDR DHL2007802530](https://openairdocs.org/sdr/DHL2007802530.md): Panel · delaminated · Feb 6, 2007 · N802DH · Doug DC873 · Wing, Plate/Skin
  > LT WING T/E LWR PANEL DELAMINATED (STA XW 97.000 - XRS 162.000). REMOVED AND REPLACED LT WING T/E LWR PANEL IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).
- [SDR DHL2007802532](https://openairdocs.org/sdr/DHL2007802532.md): Fillet · delaminated · Feb 5, 2007 · N802DH · Doug DC873 · Aerodynamic Fairings
  > FOUND FUSELAGE LWR FILLET PANEL NR 732 DELAMINATED (STA 990.000 - 1050.000). REMOVED AND REPLACED LWR FILLET PANEL NR 732 IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).
- [SDR DHL2007802529](https://openairdocs.org/sdr/DHL2007802529.md): Skin · cracked · Feb 3, 2007 · N802DH · Doug DC873 · Nacelle/Pylon, Plate/Skin
  > RT NR 3 ENGINE NACELLE INLET COWL SHOWS CRACK 0.500" ON SKIN STA YN 138.000 AT 3 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR AC62-54-105 REV IR DATED 01-19-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D.
- [SDR DHL2007802528](https://openairdocs.org/sdr/DHL2007802528.md): Vane · misrepaired · Feb 3, 2007 · N802DH · Doug DC873 · Trailing Edge Flaps
  > RT OTBD SLOT VANE HAS A NON STANDARD REPAIR STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR AC62-57-106 REV IR DATED 01-22-07. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGE
- [SDR DHL2007802527](https://openairdocs.org/sdr/DHL2007802527.md): Splice · cracked · Feb 3, 2007 · N802DH · Doug DC873 · Wing Main, Frame Structure
  > LT WING CTR L/E INTERNAL SPLICE DOUBLER STA XFS 341.500 CRACKED 1" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG NR AC62-57-109 REV IR DATED 01-23-07. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED INTERNAL DOUBLER SEGM
- [SDR DHL2007802521](https://openairdocs.org/sdr/DHL2007802521.md): Vane · misrepaired · Feb 3, 2007 · N802DH · Doug DC873 · Trailing Edge Flaps
  > LT OTBD SLOT VANE HAS A NON STANDARD REPAIR, STA XS 512.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG AC62-57-108 REV IR DATED 01-23-07. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED S
- [SDR DHL2007802520](https://openairdocs.org/sdr/DHL2007802520.md): Vane · misrepaired · Feb 3, 2007 · N802DH · Doug DC873 · Wing Main, Frame Structure
  > LT OTBD VANE SLOT HAS A NON STANDARD REPAIR, STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG NR AC62-57-107 REV JR DATED 01-23-07. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAM
- [SDR DHL2007802526](https://openairdocs.org/sdr/DHL2007802526.md): Vane · misrepaired · Feb 2, 2007 · N802DH · Doug DC873 · Trailing Edge Flaps
  > RT OTBD SLOT VANE HAS A NON STANDARD REPAIR, STA XS 512.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG NR AC62-57-104 REV A DATED 01-31-07. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CUT OUT DA
- [SDR DHL2007802522](https://openairdocs.org/sdr/DHL2007802522.md): Skin · cracked · Feb 2, 2007 · N802DH · Doug DC873 · Passenger/Crew Doors
  > L1 DOOR CUT OUT WITH 0.600" CRACK APPROX AT STA 25.000 L-15L TO L-16L (FUS SKIN) MAJOR REPAIR. CORR.: PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG# AC62-53-101 REV. IR DATED 01-15-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-
- [SDR DHL2007802534](https://openairdocs.org/sdr/DHL2007802534.md): Hinge Fitting · cracked · Feb 2, 2007 · N802DH · Doug DC873 · Ailerons
  > LT NR 4 AILERON HINGE FITTING IS CRACKED. REMOVED AND REPLACED NR 4 LT AIL HINGE SUPPORT FITTING IAW MM 20-16-0 PG 201-207. REFER TO NR 069055 FOR LT INBD AIL REMOVAL/REINSTALLATION AND NR 071624 FOR OPS CK.
- [SDR DHL2007802533](https://openairdocs.org/sdr/DHL2007802533.md): Floorbeam · cracked · Feb 2, 2007 · N802DH · Doug DC873 · Fuselage Main, Floor Beam
  > AFT ACCY COMPT FLOORBEAM SHOWS CRACK 5" AT STA 1700.000 BL 0 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR AC62-53-102, REV IR DATE 01-15-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTION IAW DWG
- [SDR DHL2007802525](https://openairdocs.org/sdr/DHL2007802525.md): Skin · delaminated · Jan 30, 2007 · N802DH · Doug DC873 · Spoilers
  > NR 2 LT SPOILER PANEL DELAMINATED. REMOVED AND REPLACED NR 2 LT SPOILER PANEL IAW MM 27-61-1 PG 201-206. REFER TO NR 071624 FOR OPS CHECK.

Next page: https://openairdocs.org/aircraft/N802DH/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 = 'N802DH' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N802DH/reports

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