# Service difficulty reports: N803DH

A list on [N803DH](https://openairdocs.org/aircraft/N803DH.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 12 · 573 reports

- [SDR DHLA201200003](https://openairdocs.org/sdr/DHLA201200003.md): Blade · missing · Jan 31, 2012 · N803DH · Doug DC873F · Turbine Section
  > NR 1 ENGINE FAILED WHEN ENCOUNTER OF CAT AT FL 370 OCCURED. PERFORMED ENGINE FAILURE CHECKLIST AND INFLIGHT AIRSTART ABNORMAL PROCEDURE AND ENGINE SHUTDOWN PROCEDURE. ENGINE MOTORED FROM 0406 TO 0629. OIL PRESSURE AT FAILURE NORMAL, IN CRUISE 10 PSI. FUEL A
- [SDR DHLA2012010600001](https://openairdocs.org/sdr/DHLA2012010600001.md): Fire Detector · malfunctioned · Jan 6, 2012 · N803DH · Doug DC873F · Fire Detection
  > NR 3 ENGINE FIRE WARNING, PHASE ONES COMPLETED & ENGINE CHECKLIST, FIRED BOTTLE, LIGHT WENT OUT. OIL PRESSURE WAS POSITIVE. ACFT DIVERTED, ACFT WAS GROUNDED. INSPECTED ENGINE IAW MM 72-00-00. NO DEFECTS NOTED. INSPECTED ENGINE FOR EVIDENCE OF POSSIBLE FIRE
- [SDR DHLA201000143](https://openairdocs.org/sdr/DHLA201000143.md): Seat Track · worn · Oct 29, 2010 · N803DH · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > COCKPIT.- F/E'S FWD SEAT TRACK HOLES ELONGATED. CORRECTIVE ACTION: REMOVED F/E'S FWD SEAT TRACK IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SEAT TRACK IAW SRM 51-3-0, SRM 51-3-1. OPS CHECKED GOOD IAW MMS 25-11-02 PG 501.
- [SDR DHLA201000144](https://openairdocs.org/sdr/DHLA201000144.md): Frame · worn · Oct 26, 2010 · N803DH · Doug DC873F · Engine Thrust Reverser
  > NR 4 ENG LT T/R STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE AT STA YN 202.000, BETWEEN 7 AND 8 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW FORM 8110-3. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED AREA + FABRICATED FRAME SEGMENT (AL6061T6 0.071") IAW DWG E
- [SDR DHLA201000090](https://openairdocs.org/sdr/DHLA201000090.md): Battery Pack · failed · Sep 12, 2010 · N803DH · Doug DC873F · Emergency Lighting
  > EMERGENCY BATTERY WILL NOT TEST EXIT LIGHTS. ACFT WAS GROUNDED. R & R EMERGENCY EXIT LIGHT RACK ASSY. OPS CHECKS GOOD IAW MM 33-50-01.
- [SDR DHLA201000083](https://openairdocs.org/sdr/DHLA201000083.md): Skin · corroded · Jul 20, 2010 · N803DH · Doug DC873F · Fuselage Main, Plate/Skin
  > NOSE SECTION LWR PLATING SHOWS CORROSION FS 12.000 L-36 PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 3,4,23,24. TR 53-203 DATED 01-21-08. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED AREA + FABRICATE
- [SDR DHLA201000087](https://openairdocs.org/sdr/DHLA201000087.md): Skin · corroded · Jul 8, 2010 · N803DH · Doug DC873F · Fuselage Main, Plate/Skin
  > SKIN CORRODED STA 520.000 L34R PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 07-16-10, EVA D853-00356 REV IR DATED 07-27-10. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT CORRODED AREA AND FABRICATED REPAIR DOU
- [SDR DHLA201000080](https://openairdocs.org/sdr/DHLA201000080.md): Longeron Fitting · cracked · Jul 8, 2010 · N803DH · Doug DC873F · Fuselage Main, Longeron/Stringer
  > LONGERON END FITTING BATHTUB FITTING CRACK 3.5" STA 902.125, L-4L PERFORMED MAJOR REPAIR IAW SRM 53-1-0, PG 1. REMOVED CRACKED BATHTUB FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW BATHTUB FITTING I
- [SDR DHLA201000079](https://openairdocs.org/sdr/DHLA201000079.md): Longeron Fitting · cracked · Jul 8, 2010 · N803DH · Doug DC873F · Fuselage Main, Longeron/Stringer
  > LONGERON END FITTING BATHTUB FITTING CRACK 2.5" STA 902.125, L-5L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0, PG 1. REMOVED CRACKED BATHTUB FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW BATHTUB FITTING
- [SDR DHLA201000076](https://openairdocs.org/sdr/DHLA201000076.md): Skin · worn · Jul 8, 2010 · N803DH · Doug DC873F · Ailerons
  > RIGHT INBD AILERON UPPER PLATING WORN STA XA 474.000 PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 1. REMOVED WORN PLATING IAW SRM 57-1-0, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040") IAW SRM 57-8-1 FIG. 1 ITEM "E". CLEANED, TREATED AND PRIMED AREA + NEW
- [SDR DHLA201000075](https://openairdocs.org/sdr/DHLA201000075.md): Doubler · cracked · Jul 8, 2010 · N803DH · Doug DC873F · Fuselage Miscellaneous Structure
  > NOSE SECTION ACCESS DOOR 2 INTERNAL DOUBLER CRACKED STA-156.0000. PERFORMED MAJOR REPAIR IAW EVA D853-00350, REV IR DATED 07-15-10. REMOVED EXISTING REPAIR IAW SRM 51-1-20D, SRM 51-1-21. VISUALLY INSPECTED REWORKED AREA. NO CRACK, NO CORROSION FOUND. FABRICAT
- [SDR DHLA201000072](https://openairdocs.org/sdr/DHLA201000072.md): Splice · cracked · Jul 8, 2010 · N803DH · Doug DC873F · Fuselage Main, Structure
  > FUS TAIL SECTION.- SPLICE FITTING CRACKED 1" STA 1766.00 L-17L PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED END FITTING IAW SRM 51-3-0 PG 1, SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW END FITTING IAW SRM 51-1-11
- [SDR DHLA201000084](https://openairdocs.org/sdr/DHLA201000084.md): Splice · cracked · Jul 6, 2010 · N803DH · Doug DC873F · Fuselage Main, Structure
  > AFT CARGO COMPT.- SPLICE FITTING CRACKED 6" (STA 1140.000 - 1160.000 L36) PERFORMED MAJOR REPAIR IAW JC EC-02172-001 W/O 9440. REMOVED SPLICE FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED, PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING
- [SDR DHLA201000082](https://openairdocs.org/sdr/DHLA201000082.md): Skin · corroded · Jul 6, 2010 · N803DH · Doug DC873F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN CORRODED STA 670.000 - 680.000, L36 - L35L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR10380 DATED 08-09-10, EVA D853-00355 REV IR DATED 07-19-10. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMO
- [SDR DHLA201000078](https://openairdocs.org/sdr/DHLA201000078.md): Cargo Track · worn · Jul 6, 2010 · N803DH · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO COMPT.- NR 6 TRACK LUGS WORN (STA 560.000 - 610.000) PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG 14, SHEET 1, PG 49-50. REMOVED EXISTING SPLICES AND CUT OUT TRACK DAMAGED SEGMENT IAW SRM 53-2-3 FIG. 14 SHEET 1, SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATED
- [SDR DHLA201000073](https://openairdocs.org/sdr/DHLA201000073.md): Rib · cracked · Jul 6, 2010 · N803DH · Doug DC873F · Trailing Edge Flaps
  > RIGHT INBD FLAP T/E RIB CRACKED 1", STA XW -5.000 REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOPHOLE AND FABRICATED REPAIR ANGLE (AL2024T3 0.071") IAW SRM 57-2-0 PG 9-10, SRM 57-5-2 FIG. 5 SHEET 1, SRM 51-9-0 FIG 68A. CLEANED, TREATED AND PRIMED AREA + REPA
- [SDR DHLA201000081](https://openairdocs.org/sdr/DHLA201000081.md): Skin · damaged · Jul 2, 2010 · N803DH · Doug DC873F · Trailing Edge Flaps
  > RT OTBD FLAP UPPER SKIN HOLE ELONGATED AND WORN STA XF 203.000 - 213.000 PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4, TR 57-94 DATED 10-01-02. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING IAW SRM 57-7-1 FIG 4, TR 57-94 ITEM
- [SDR DHLA201000077](https://openairdocs.org/sdr/DHLA201000077.md): Longeron · cracked · Jul 1, 2010 · N803DH · Doug DC873F · Fuselage Main, Longeron/Stringer
  > LONGERON 24R CRACKED 1.5" STA FS 900.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG 5, SHEET 1, 13, 14, 15, 16, 25, 26, 27 TR 53-123 DATED 05-15-01. REMOVED FASTENERS IAW SRM 51-1-20D. PERFORMED STOP HOLE AND FABRICATED 2 REPAIR ANGLES, & 2 SHIMS IAW SRM 53-
- [SDR DHLA201000088](https://openairdocs.org/sdr/DHLA201000088.md): Frame · worn · Jun 30, 2010 · N803DH · Doug DC873F · Engine Thrust Reverser
  > NR3 ENG LT T/R FRAME WORN AT 6.30 AND 7.30 O'CLOCK POS STA YN 203.000 PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 08-04-10, EVA D878-00353 REV IR DATED 07-15-10. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED AREA AND FABRICATED FRAME SEGM
- [SDR DHLA201000085](https://openairdocs.org/sdr/DHLA201000085.md): Skin · cracked · Jun 30, 2010 · N803DH · Doug DC873F · Wing, Plate/Skin
  > RT WING TOP AFT PANEL PLATING CRACKED 4" STA XCW 69.500 PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 20, SHEET 1. REMOVED FASTENERS IAW SRM 51-3-0, SRM 51-1-20D. CUT OUT DAMAGED AREA + FABRICATED (-5) DOUBLER (7075"0" 0.160") + (-7) TRIPLER (7075"0" 0.125") + FI
- [SDR DHLA201000010](https://openairdocs.org/sdr/DHLA201000010.md): Fire Warning · activated · Apr 15, 2010 · N803DH · Doug DC873F · Fire Detection
  > AFTER TAKEOFF, NR 1 ENGINE FIRE WARNING. (USING "A" LOOP) PERFORMED EMERGENCY PROCEDURES, FIRED BOTH BOTTLES. WARNING CONTINUED AFTER LANDING, PENDING; ACFT IS GROUNDED.
- [SDR DHLA201000008](https://openairdocs.org/sdr/DHLA201000008.md): Pump · low pressure · Mar 18, 2010 · N803DH · Doug DC873 · Engine Fuel Pump
  > NR 3 ENGINE AT FLT LEVEL 330 STARTED TO VIBRATE THEN DROPPED TO 70 PERCENT N1. MOVING THRUST LEVER HAD NO EFFECT. AFTER APPROX 1 MINUTE OIL PRESSURE LIGHT ILLUMINATED AND OIL PRESS INDICATES 3 PSI. ENG SHUTDOWN PROCEDURE ACCOMPLISHED. T/S IAW MM 71-00-00 NO
- [SDR DHLA201000002](https://openairdocs.org/sdr/DHLA201000002.md): Strut · leaking · Jan 7, 2010 · N803DH · Doug DC873 · Nose/Tail Landing Gear Strut/Axle
  > AFTER PUSH BACK, MX REPORTED LEAK FROM NOSE GEAR. RII ITEM. ACFT IS GROUNDED- REPLACING NOSE GEAR ASSY.
- [SDR DHLA200800105](https://openairdocs.org/sdr/DHLA200800105.md): Battery Pack · inoperative · Sep 30, 2008 · N803DH · Doug DC873 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT TEST ON PREFLT, ACFT GROUNDED. R&R BATTERY PACK ASSY, OPS CHECKED GOOD IAW 33-50-1.
- [SDR DHLA200800077](https://openairdocs.org/sdr/DHLA200800077.md): Engine · failed · Jun 27, 2008 · N803DH · Doug DC873 · Engine (Turbine/Turboprop)
  > AT TOP OF CLIMB NR 3 ENGINE FAILED FOLLOWED APPLICABLE PROCEDURES RELIGHT ATTEMPT UNSUCCESSFUL WIND MILLING OIL PRESSURE 2 PSI WIND MILLING TIME 2.55. PERFORMED T/S IAW DC8-70 M/M 71-00, ADJUSTED MEL SPECIFIC GRAVITY IAW MM 73-20-1. ADJUSTED PMC DROP IAW MM
- [SDR DHL2007803545](https://openairdocs.org/sdr/DHL2007803545.md): Skin · delaminated · Jun 14, 2007 · N803DH · Doug DC873 · Fuselage Main, Plate/Skin
  > LT AFT ADF SENSE ANTENNA SKIN DELAMINATED. REMOVED AND REPLACED LT AFT ADF SENSE ANTENNA IAW SRM 51-3-0.
- [SDR DHL2007803537](https://openairdocs.org/sdr/DHL2007803537.md): Skin · delaminated · Jun 12, 2007 · N803DH · Doug DC873 · Wing, Plate/Skin
  > RT WING T/E UPPER PANEL SKIN DELAMINATED (STA XW 0.000 - 47.000). REMOVED DELAMINATED PANEL IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL IAW SRM 51-3-0, SRM 51-3-1 PG 2A (TORQUE).
- [SDR DHL2007803542](https://openairdocs.org/sdr/DHL2007803542.md): None · none · Jun 10, 2007 · N803DH · Doug DC873 · Standard Practices/Structures
  > REMOVE REPAIR BELOW CARGO DOOR AT STA 176 AND INSPECT AREA. INSTALL A NEW REPAIR IAW SRM (PERMANENT) OR APPROVED DATA. ENTER INFORMATION ON 337 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-07, DWG NR AD42-53-11 REV IR DATED 06-01-0
- [SDR DHL2007803543](https://openairdocs.org/sdr/DHL2007803543.md): Frame · worn · Jun 10, 2007 · N803DH · Doug DC873 · Nacelle/Pylon, Frame/Spar/Rib
  > NR 3 ENG T/R FIXED STRUCTURE AND FWD FRAME WORN STA YN 202.000 AT 5 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3- DATED 06-08-07, DWG NR AD42-78-110 REV IR DATED 05-30-07. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION
- [SDR DHL2007803539](https://openairdocs.org/sdr/DHL2007803539.md): Skin · worn · Jun 10, 2007 · N803DH · Doug DC873 · Nacelle/Pylon, Plate/Skin
  > NR 2 ENG NACELLE INLET COWL UPPER SIDE WORN, STA YN 147.534 AT 12 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND STEEL SPLICE 17.7 P
- [SDR DHL2007803541](https://openairdocs.org/sdr/DHL2007803541.md): Skin · worn · Jun 10, 2007 · N803DH · Doug DC873 · Nacelle/Pylon, Plate/Skin
  > NR 1 ENG NACELLE INLET COWL UPPER SIDE WORN, STA YN 147.534 AT 12 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED AREA AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND STEEL SPLICE 17-7PH 0.
- [SDR DHL2007803540](https://openairdocs.org/sdr/DHL2007803540.md): Skin · worn · Jun 10, 2007 · N803DH · Doug DC873 · Nacelle/Pylon, Plate/Skin
  > NR 4 ENG NOSE COWL EXT SKIN WORN (STA YN 147.000 - 157.000 AT 12 O'CLOCK POS LT/RT) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND
- [SDR DHL2007803538](https://openairdocs.org/sdr/DHL2007803538.md): Skin · worn · Jun 10, 2007 · N803DH · Doug DC873 · Nacelle/Pylon, Plate/Skin
  > NR 3 ENG NOSE COWL EXTERNAL SKIN WORN (STA YN 147.534, AT 12 O'CLOCK POS) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND STEEL SPLI
- [SDR DHL2007803536](https://openairdocs.org/sdr/DHL2007803536.md): None · none · Jun 10, 2007 · N803DH · Doug DC873 · Standard Practices/Structures
  > REMOVE REPAIR BELOW MAIN CARGO DOOR AT STA 226 AND INSPECT AREA. INSTALL NEW REPAIR IAW SRM (PERMANENT) AND APPROVED DATA. ENTER INFORMATION ON 337 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-08-07, DWG NR AD42-53-112 REV IR DATED 06-
- [SDR DHL2007803535](https://openairdocs.org/sdr/DHL2007803535.md): Channel · worn · Jun 8, 2007 · N803DH · Doug DC873 · Landing Gear Doors
  > RT MLG INBD DOOR ZEE CHANNEL WORN STA 870.000 RBL 50" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-07, DWG NR AD42-52-0108 REV IR DATED 05-22-07. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICAT
- [SDR DHL2007803534](https://openairdocs.org/sdr/DHL2007803534.md): Skin · worn · Jun 8, 2007 · N803DH · Doug DC873 · Wing, Plate/Skin
  > RT OUTBD FLAP UPPER SKIN WORN, STA XF 224.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-07, DWG NR AD42-57-106 REV IR DATED 05-21-07. REMOVED EXISTING REPAIR PLATING AND INNER DOUBLER IAW SRM 51-1-21. FABRICATED NEW PLATING SEGM
- [SDR DHL2007803533](https://openairdocs.org/sdr/DHL2007803533.md): None · none · Jun 8, 2007 · N803DH · Doug DC873 · Standard Practices/Structures
  > RT INBD VANE SLOT HAS AN INTERIM REPAIR AT STA XILD 42 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-2007, DWG NR AD42-57-107 REV IR DATED 05-21-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTIO
- [SDR DHL2007803531](https://openairdocs.org/sdr/DHL2007803531.md): Longeron · damaged · Jun 6, 2007 · N803DH · Doug DC873 · Fuselage Main, Longeron/Stringer
  > FUS NOSE SECTION LONGERON HAS A MISDRILLED HOLE AT STA -32.000 L-17R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-04-07, DWG NR AD42-53-109 REV IR DATED 05-25-07. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED REINFORCEMENT (AL7075T6 5
- [SDR DHL2007803532](https://openairdocs.org/sdr/DHL2007803532.md): Access Door · cracked · Jun 6, 2007 · N803DH · Doug DC873 · Doors
  > LT FUS NOSE SECTION ACS MODIFICATION DOUBLER AT UPPER AFT JAMB CORNER OF HEAT EXCHANGER ACCESS DOOR, CRACKED 0.250" STA -12.000 L-24L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-04-07, DWG NR AD42-53-103 REV IR DATED 05-16-07. REMOVED
- [SDR DHL2007803544](https://openairdocs.org/sdr/DHL2007803544.md): None · none · Jun 5, 2007 · N803DH · Doug DC873 · Standard Practices/Structures
  > PERFORM MODIFICATION REPAIR TO THE L2 DOOR, FWD, LOWER CORNER IAW AD2000-20-08, S/B 53-075 AND SR08530021. MAKE ENTRY IN AIRCRAFT LOGBOOK AND PERMANENT RECORD (337 FORM) MAJOR REPAIR (AMOC). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 05-22-07, BOEING M
- [SDR DHL2007803526](https://openairdocs.org/sdr/DHL2007803526.md): Doubler · cracked · Jun 4, 2007 · N803DH · Doug DC873 · Wing, Plate/Skin
  > RT WING CTR L/E UPPER ANGLE DOUBLER CRACKED STA XFS 428.000. REMOVED CRACKED ANGLE DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED ANGLE DOUBLER (AL7075"0" 0.080") IAW SRM 57-2-0 PG 9-10, SRM 57-3-3. HEAT TREATED ANGLE DOUBLER FROM 7075"0" TO 7075T6 IAW S
- [SDR DHL2007803523](https://openairdocs.org/sdr/DHL2007803523.md): Vane · unknown · Jun 3, 2007 · N803DH · Doug DC873 · Leading Edge Devices
  > LT OUTBD VANE SLOT HAS AN INTERIM REPAIR AT STA XOLDO 67 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-01-07, DWG NR AD42-57-105, REV IR DATED 05-17-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTI
- [SDR DHL2007807524](https://openairdocs.org/sdr/DHL2007807524.md): Vane · unknown · Jun 3, 2007 · N803DH · Doug DC873 · Wing Main, Frame Structure
  > RT OUTBD VANE SLOT HAS AN INTERIM REPAIR AT SOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-01-07, DWG NR AD42-57-101 REV IR DATED 05-16-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTION
- [SDR DHL2007803529](https://openairdocs.org/sdr/DHL2007803529.md): Vane · unknown · Jun 3, 2007 · N803DH · Doug DC873 · Wing Main, Frame Structure
  > RT OUTBD VANE SLOT HAS AN INTERIM REPAIR AT STA XOLDO 67 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3- DATED 06-01-07, DWG NR AD42-57-102 REV IR DATED 05-16-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTI
- [SDR DHL2007803527](https://openairdocs.org/sdr/DHL2007803527.md): Fitting · cracked · Jun 3, 2007 · N803DH · Doug DC873 · Wing, Attach Fittings
  > NR 4 ALT TANK INTERIOR FITTING CRACKED 1" STA XW 408.000 S-58 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00363-001, DOUGLAS DWG NR 5644972. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. I
- [SDR DHL2007803528](https://openairdocs.org/sdr/DHL2007803528.md): Rib · cracked · Jun 3, 2007 · N803DH · Doug DC873 · Wing, Rib/Bulkhead
  > NR 4 STUB WING RIB CRACKED STA XOLDO 67.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00364-001, DOUGLAS DWG NR 9753297. REMOVED CRACKED RIB 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
- [SDR DHL2007803530](https://openairdocs.org/sdr/DHL2007803530.md): Vane · unknown · Jun 3, 2007 · N803DH · Doug DC873 · Wing Main, Frame Structure
  > LT OUTBD VANE SLOT HAS AN INTERIM REPAIR AT STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-01-07, DWG NR AD42-57-104 REV IR DATED 05-16-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SEC
- [SDR DHL2007803519](https://openairdocs.org/sdr/DHL2007803519.md): Channel · cracked · Jun 3, 2007 · N803DH · Doug DC873 · Wing Miscellaneous Structure
  > RT WING LWR FAIRING ZEE CHANNEL CRACKED 1" STA XW -3.125. REMOVED CRACKED ZEE CHANNEL IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL IAW SRM 51-1-21. REFER TO JC EC-00360-00 (WO 1028) FOR ZEE FABRICATION.
- [SDR DHL2007803521](https://openairdocs.org/sdr/DHL2007803521.md): Panel · cracked · Jun 3, 2007 · N803DH · Doug DC873 · Wing, Plate/Skin
  > LT WING LWR PANEL CRACKED 1" STA XW -3.125. REMOVED PANEL IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). REFER TO JC EC-00359-001 (WO 1028) FOR PANEL FABRICATION.
- [SDR DHL2007803520](https://openairdocs.org/sdr/DHL2007803520.md): Channel · cracked · Jun 3, 2007 · N803DH · Doug DC873 · Wing Miscellaneous Structure
  > LT WING LWR FAIRING ZEE CHANNEL CRACKED 0.750" STA XW -3.125. REMOVED ZEE CHANNEL IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL IAW SRM 51-1-21. REFER TO JC EC-00361-001 (WO 1028) FOR ZEE FABRICATION.

Next page: https://openairdocs.org/aircraft/N803DH/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 = 'N803DH' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N803DH/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.