# N805DH: Maher James P DYKE DELTA

- Status: Valid registration
- Airframe: [Maher James P DYKE DELTA](https://openairdocs.org/model/maher-james-p-dyke-delta) (registry code 05614DJ, 4 seats)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Serial number: 1406
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Experimental, amateur built
- Airworthiness date: August 30, 2006
- Certificate issued: April 27, 2021
- Expires: April 30, 2028
- Mode S code: AAF4C3
- Registered owner: [Hopson Dillon R](https://openairdocs.org/faa-owner/HOPSON%20DILLON%20R)
- Location: [Midway, TN](https://openairdocs.org/faa-place/TN/Midway)
- Owner type: Individual
- Owner's area on the map: 36.1567° N, 83.0381° W: Placed by OpenAirDocs at the center of ZIP code 37809, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=805DH
- Page: https://openairdocs.org/aircraft/N805DH

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 0 in force

### Matched by airframe (Maher James P DYKE DELTA)

None in force.

### Matched by engine (Amateur-built UNKNOWN ENG)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N805DH.

## FAA accident and incident reports

None matched to N805DH.

## Reports on N805DH not matched to an aircraft (3)

They name N805DH, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20100502033469I](https://openairdocs.org/incident/20100502033469I), May 2, 2010: Douglas DC-8-73F (N805DH), Erlanger, KY, Minor damage. N805DH departed RY18L at kcvg, flight #DHL2963 to kmia. During post flight inspection, bird strike damage/dent was found on left wing leading edge. Crew…
- [Incident 20040406004609I](https://openairdocs.org/incident/20040406004609I), Apr 6, 2004: Doug DC873F (N805DH), San Francisco, CA. (-23) Crew declared emergency prior to landing safely at San Francisco international airport due to a #3 engine failure. The engine flamed out at 35,000 feet…
- [Incident 20001007030219I](https://openairdocs.org/incident/20001007030219I), Oct 7, 2000: Doug DC873F (N805DH), Salt Lake City, UT. (-23)On a flight from cvg to sfo the aircraft was diverted to slc due to a fire indication on the #4 engine. Both fire bottles were discharged, the fire…

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N805DH not matched to an aircraft (760, newest 50)

They name N805DH, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DHLA201100516](https://openairdocs.org/sdr/DHLA201100516), Jun 22, 2011: BATTERY PACK. INOPERATIVE. DURING PDC CK FOUND EMERGENCY LIGHTS INOPERATIVE. ACFT WAS GROUNDED. R & R EMER LIGHTS BATTERY PACK IAW MMS 33-50-10. OPS-CK-GOOD.
- [SDR DHLA201100048](https://openairdocs.org/sdr/DHLA201100048), Apr 11, 2011: SKIN. CRACKED. LT OTBD AIL LWR NOSE PLATING CRACKED 1" STA XA 734.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0, PG 1, SRM 57-8-1, FIG 4. REMOVED DAMAGED NOSE PLATING IAW SRM 57-
- [SDR DHLA201100501](https://openairdocs.org/sdr/DHLA201100501), Apr 8, 2011: SKIN. CORRODED. RUDDER LT SIDE.- SKIN CORRODED (STA ZR 150.000 - 178.000). CA-PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1. REMOVED LEVEL II CORROSION IAW SRM 51-1-8, PG 17-18.
- [SDR DHLA201100046](https://openairdocs.org/sdr/DHLA201100046), Apr 8, 2011: SKIN. CORRODED. RUDDER LT SIDE.- SKIN CORRODED STA ZR 115.000 - 150.000 GALVANIC CORROSION. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1. REMOVED LEVEL II CORROSION IAW SRM 51-1
- [SDR DHLA201100510](https://openairdocs.org/sdr/DHLA201100510), Apr 7, 2011: RIB. CRACKED. RT LWR SLOT DOOR NR 3 RIB CRACKED. REMOVED CRACKED RIB IAW SRM 51-1-21. CLEANED, TREATED & PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21.
- [SDR DHLA201100507](https://openairdocs.org/sdr/DHLA201100507), Apr 7, 2011: RIB. CRACKED. LT LWR SLOT DOOR, NR 3 RIB CRACKED. REMOVED CRACKED RIB IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21. RE
- [SDR DHLA201100050](https://openairdocs.org/sdr/DHLA201100050), Apr 7, 2011: RIB. CRACKED. RT WING L/E- INBD LWR SLOT DOOR NR 4 RIB CRACKED. REMOVED CRACKED NR 4 DOOR RIB IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW RIB 
- [SDR DHLA201100047](https://openairdocs.org/sdr/DHLA201100047), Apr 6, 2011: LONGERON SPLICE. CRACKED. AFT FUS- L17L SPLICE FITTING CRACKED .2500" STA 1766.000. PERFORMED MAJOR REPAIR IAW SRM 53-1-0, PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-21, SRM 51-3-
- [SDR DHLA201100504](https://openairdocs.org/sdr/DHLA201100504), Apr 5, 2011: CRANK ASSY. CRACKED. RT OTBD SLOT CRANK CRACKED. REMOVED CRACKED RT OTBD SLOT CRANK IAW MM 27-80-2, PG 201. INSTALLED NEW RT OTBD SLOT CRANK AND REINSTALLED RT OTBD SLOT IAW MM 27-3
- [SDR DHLA201100054](https://openairdocs.org/sdr/DHLA201100054), Apr 5, 2011: STIFFENER. CRACKED. RUDDER L/E STIFFENER CRACKED 2" STA ZR 105.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21, SRM 51-3-0. FABRICATED STIFFENER IAW SRM 55-6-1 PG 4. HEAT TREATED ST
- [SDR DHLA201100508](https://openairdocs.org/sdr/DHLA201100508), Apr 4, 2011: RIB. CRACKED. LT WING L/E -FORMER "L" ANGLE CRACKED 4" STA, XFS-23.750. REMOVED CRACKED FORMER IAW SRM 51-3-0 CLEANED TREATED & PRIMED AREA IAW SRM 51-1-8B INSTALLED NEW FORM
- [SDR DHLA201100502](https://openairdocs.org/sdr/DHLA201100502), Apr 2, 2011: SKIN. CORRODED. RT RUDDER EXT SKIN CORRODED, STA ZR 140.750 (GALVANIC CORROSION). PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1 REMOVED COROSION IAW SRM 51-1-8 PG 17-18. FOUND O
- [SDR DHLA201100053](https://openairdocs.org/sdr/DHLA201100053), Apr 2, 2011: SKIN. CORRODED. RT RUDDER EXT SKIN CORRODED STA ZR 168.656. PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1. REMOVED LEVEL II CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMIT
- [SDR DHLA201100045](https://openairdocs.org/sdr/DHLA201100045), Apr 2, 2011: SUPPORT ANGLE. CRACKED. RT NOSE WHEEL TUNNEL- SUPPORT ANGLE CRACKED STA -50.000. REMOVED SUPPORT ANGLE IAW SRM 51-3-0. FABRICATED SUPPORT ANGLE (AL2024T3 0.040") IAW SRM 53-2-0 PG 1. C
- [SDR DHLA201100043](https://openairdocs.org/sdr/DHLA201100043), Mar 31, 2011: DOUBLER. CRACKED. RT INBD FLAP.- FLAP JOINT RIB ANGLE DOUBLER SHOWS (2EA) CRACKS 1" AND .5". REMOVED CRACKED ANGLE DOUBLER IAW SRM 51-1-21. FABRICATED NEW ANGLE DOUBLER (AL2024T3
- [SDR DHLA201100506](https://openairdocs.org/sdr/DHLA201100506), Mar 30, 2011: TAB. DELAMINATED. RUDDER TAB DELAMINATED 1", STA ZRT 108.000 LT. CUT OUT DAMAGED AREA IAW SRM 55-2-2 PG 6-4. FABRICATED DOUBLER (AL2024T3 0.016") IAW SRM 55-6-1 PG 8. CLEANED + B
- [SDR DHLA201100503](https://openairdocs.org/sdr/DHLA201100503), Mar 30, 2011: TAB. DELAMINATED. LT ELEV CONTROL TAB DELAMINATED 2" STA XET 35.000. CUT OUT DAMAGED SKIN AREA IAW SRM 55-2-2, PAR 6. FABRICATED DOUBLER (2024T3 0.012") IAW SRM 55-4-0 PG 10. CLE
- [SDR DHLA201100051](https://openairdocs.org/sdr/DHLA201100051), Mar 30, 2011: SKIN. DELAMINATED. NR 5 RT SPOILER DELAMINATED 4". CUT OUT DAMAGED AREA IAW SRM 57-2-3, PAR 23. FABRICATED DOUBLER & CORE IAW SRM 57-7-1, PG 15. CLEANED AND BONDED DOUBLER IAW SRM
- [SDR DHLA201100042](https://openairdocs.org/sdr/DHLA201100042), Mar 30, 2011: SKIN. WORN. NR 4 ENG INLET NACELLE COWL UPPER SKIN WORN STA, YN 147.000 AT 12 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW SRM 71-5-2, FIG 2, SHEET 1,2,3. REMOVED FASTENERS IAW 
- [SDR DHLA201100512](https://openairdocs.org/sdr/DHLA201100512), Mar 29, 2011: FITTING. CORRODED. LEFT MLG WW PRESSURE PANEL AFT SIDE FITTING SHOWS INTERGRANULAR CORROSION AT BS 857.000. REMOVED LEVEL II CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMIT
- [SDR DHLA201100052](https://openairdocs.org/sdr/DHLA201100052), Mar 29, 2011: HINGE FITTING. WORN. VERTICAL STABILIZER REAR SPAR NR 1 HINGE FITTING SHOWS WEAR. STA ZR 103.000. PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1. REMOVED FITTING IAW M 20-16-0 PG 201-20
- [SDR DHLA201100044](https://openairdocs.org/sdr/DHLA201100044), Mar 29, 2011: FRAME. WORN. NR 2 ENG HALF THRUST REVERSER STRUCTURAL FWD FRAME SHOWS EXISTING WEAR DAMAGE STA YN 202.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-22-11, EVA D87
- [SDR DHLA201100509](https://openairdocs.org/sdr/DHLA201100509), Mar 28, 2011: SKIN. DELAMINATED. LT WING T/E LOWER PANEL EXT SKIN DELAMINATED STA XF 339.000- 409.000. R & R LT WING T/E LOWER PANEL IAW SRM 51-3-0, 51-3-1.
- [SDR DHLA201100505](https://openairdocs.org/sdr/DHLA201100505), Mar 28, 2011: DOOR FRAME. MISREPAIRED. REPAIR LOCATED ON C4 DOOR FRAME STA 1440.000, L 30R TO L 32R DOES NOT CONFORM , REMOVED REPAIR IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED FILLER, DOUBLER, & TRIP
- [SDR DHLA201100511](https://openairdocs.org/sdr/DHLA201100511), Mar 26, 2011: SKIN. MISREPAIRED. SKIN MISREPAIRED. PERFORMED MAJOR REPAIR IAW FORM 8110-3, DATED 05-04-11, EVA D853-00403, REV IR DATED 04-11-11. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51
- [SDR DHLA201100002](https://openairdocs.org/sdr/DHLA201100002), Feb 13, 2011: SKIN. CRACKED. FUSELAGE SKIN CRACKED BETWEEN 2 FASTENERS AT FS 24.5, BETWEEN LONGERONS 31R AND 32R. ACCOMPLISHED FUSELAGE SKIN DOUBLER AND FILLER REPAIR IAW EVA D853-00398, RE
- [SDR DHLA201000105](https://openairdocs.org/sdr/DHLA201000105), Oct 10, 2010: PAN. CRACKED. INNER PAN AT AIR START DOOR ACCESS IS DAMAGED FS. -156.000. R & R DAMAGED INNER PAN AT AIR START ACCESS DOOR IAW SRM 51-1-21 AND DWG ED-4985 DTD 09/05/09 AND IA
- [SDR DHLA201000065](https://openairdocs.org/sdr/DHLA201000065), Jul 26, 2010: SKIN. CORRODED. FUSELAGE SKIN CORRODED AT FS 1281.0 AND 1260, LONGERON 36, BL 0. CUT OUT CORRODED AREAS OF SKIN THAT EXCEEDED DAMAGE LIMITATIONS. FABRICATED 2EA REPAIR FILLERS 
- [SDR DHLA201000016](https://openairdocs.org/sdr/DHLA201000016), May 2, 2010: SKIN. DAMAGED. ACCOMPLISHED PERMANENT MAJOR REPAIR AT WING STA XFS 392.5, IAW EVA 857-00329 REV 1 AND DWG NR D85700329-001-D REV "A" APPROVED BY 8110-3 SIGNED DERT-510080-CE D
- [SDR DHLA201000007](https://openairdocs.org/sdr/DHLA201000007), Feb 27, 2010: DOOR. GOUGED. RT OTBD WING SLOT DOOR HAS A DEEP GOUGE IN OUTER PLATING LOWER SURFACE APPROX AT WS XS 493.0. ACCOMPLISHED EXTERNAL DOUBLER REPAIR TO PN 5769946-502 SLOT DOOR I
- [SDR DHLA200900053](https://openairdocs.org/sdr/DHLA200900053), Nov 3, 2009: A/C PACK. ODOR. CHEMICAL OIL ODOR COMMING FROM LT PACK. RAN LT PACK, SUSPECT WAS FROZE UP PACK. OPS CK GOOD NO DEFECT NOTED IAW MM 36-10-0.
- [SDR 2009F00101](https://openairdocs.org/sdr/2009F00101), Oct 2, 2009: SKIN. MISREPAIRED. REMOVE EXTERNAL REPAIR DOUBLER AT FUSELAGE STATION 1750 LONGERON 34L AND REPLACE WITH REPAIR IAW APPROVED DATA. INDICATE TYPE OF REPAIR AND REINSPECTION INTERVA
- [SDR 2009FA0000946](https://openairdocs.org/sdr/2009FA0000946), Oct 2, 2009: SKIN. DAMAGED. REMOVE EXTERNAL REPAIR AT LT MAIN LANDING GEAR DOOR CUT OUT (CRACKS IN INBD FWD CORNER) AND REPLACE WITH REPAIR IAW APPROVED DATA. INDICATE TYPE OF REPAIR AND R
- [SDR DHLA20098051](https://openairdocs.org/sdr/DHLA20098051), Sep 27, 2009: DOOR FRAME. CRACKED. FWD SVC DOOR FWD UPPER JAMB CORNER CRACKED 1/4 INCH. C/A INSTALLED DOUBLER REPAIR IAW DWG SR08530021, SRM 53-4-1 FIG 9 ITEM D, AND AD-2000-20-08 S/BDC8-53-075.
- [SDR DHLA20098054](https://openairdocs.org/sdr/DHLA20098054), Sep 21, 2009: DOOR FRAME. CRACKED. MAIN CARGO DOOR LWR. JAMB CRACKED 1/2 INCH STA. 200.000 L-21L TO 22L. REF N/R 229834: CUT OUT DAMAGED SECTION AND INSTALLED REPAIR IAW DWG ED-4987 AND SRM 51-1-
- [SDR DHLA20098053](https://openairdocs.org/sdr/DHLA20098053), Sep 21, 2009: DOUBLER. DAMAGED. APPEARS THAT AIRSTART NOZZLE IS HITTING HARD ON INTERNAL DOUBLER FLANGE AT STA 156.000. REMOVED EXISTING REPAIR AND REWORK. REMOVED AND REPLACED DOUBLER IAW NR 
- [SDR DHLA20098052](https://openairdocs.org/sdr/DHLA20098052), Sep 17, 2009: LONGERON. DAMAGED. FUSELAGE STA 1749 LONGERON HAS RT EXISTING REPAIR IN POOR CONDITION. REM AND REP WITH PERMANENT TYPE REPAIR IAW APPROVED DATA. INDICATS REINSPECTION INTERVAL IF
- [SDR 2009F00103](https://openairdocs.org/sdr/2009F00103), Sep 2, 2009: DOOR FRAME. DAMAGED. FUSELAGE STATION 1660 LONGERON 15 RT. REMOVE AND REPLACE THIS REPAIR AT R-2 AFT DOOR JAMB WITH REPAIR IAW APPROVED DATA. INDICATE REINSPECTION INTERVAL IF REQUI
- [SDR 2009F00102](https://openairdocs.org/sdr/2009F00102), Sep 2, 2009: TAB. DELAMINATED. RT ELEVATOR GEARED TAB IS DELAMINATED.
- [SDR DHLA2009805303](https://openairdocs.org/sdr/DHLA2009805303), Jul 11, 2009: SKIN. CRACKED. 1 1/8 INCH CRACK ON FUSELAGE TAIL SECTION RT SIDE AT STA.1746.00,SR17R-S18R.
- [SDR DHLA2009805302](https://openairdocs.org/sdr/DHLA2009805302), Mar 2, 2009: LINK. CRACKED. RIGHT WING AT STATION XW97 FLAP DRIVE LINK ASSY HAVE CRACK AT ACTUATOR HOOK UP END.
- [SDR DHL200800093](https://openairdocs.org/sdr/DHL200800093), Aug 13, 2008: CONNECTOR. MALFUNCTIONED. FIRE WARNING LIGHT ON AND FIRE BELL RINGING NR 3 ENG. SWITCHED TO B LOOP LIGHT AND BELL WENT OUT. DEFERRED NR 3 ENG A LOOP PER EML 26-2-3 CAT C PLACARD ISN`T DM
- [SDR DHL2008805532](https://openairdocs.org/sdr/DHL2008805532), Mar 25, 2008: FITTING. CRACKED. CENTER WING REAR SPAR UPPER CAP FITTING CRACKED STA 857.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALL
- [SDR DHL2008805533](https://openairdocs.org/sdr/DHL2008805533), Mar 25, 2008: STIFFENER. CORRODED. RT MLG W/W STIFFENER CORRODED AT STA 857.000. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18 AND FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED ANGLE IAW
- [SDR DHL2008805506](https://openairdocs.org/sdr/DHL2008805506), Mar 24, 2008: SKIN. DAMAGED. LT WING INBD L/E LWR SURFACE HAS ELONGATED HOLES AT STA XILD 42. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-24-08, EVA D853-00046, DWG AF12-57-101 REV 
- [SDR DHL2008805537](https://openairdocs.org/sdr/DHL2008805537), Mar 24, 2008: CARGO TRACK. WORN. UPPER CARGO COMPT NR 7 TRACK LUG WORN (STA 290.000 - 340.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-3 PG 49-50. REMOVED TRACK DAMAGED SEGMENT IAW SR
- [SDR DHL2008805536](https://openairdocs.org/sdr/DHL2008805536), Mar 24, 2008: CARGO TRACK. WORN. UPPER CARGO COMPT NR 3 TRACK LUG WORN (STA 590.000 - 620.000) MAJOR REPAIR. CUT OUT TRACK SEGMENT AND FABRICATED (3EA) SPLICES (AL7075T6 0.100", 0.125" AND 0.16
- [SDR DHL2008805534](https://openairdocs.org/sdr/DHL2008805534), Mar 23, 2008: RIB. WORN. LT MLG W/W DOOR UPLATCH RAIL RIB WORN AT STA 890.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00840-001D, DWG DOUGLAS NR 5653490. REMOVED WORN RIB IAW S
- [SDR DHL2008805502](https://openairdocs.org/sdr/DHL2008805502), Mar 18, 2008: ANGLE. CORRODED. CORROSION AT RT VERT STAB TO FUSELAGE JOINT LWR ANGLE, STA 1800.000 L-2R - L-3R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-5 FIG 16A SHEET 1, 2. REMOVE
- [SDR DHL2008805511](https://openairdocs.org/sdr/DHL2008805511), Mar 18, 2008: FLAP. DAMAGED. RT OUTBD FLAP L/E PLATING HOLES ELONGATED (STA XF 325.000 - 243.000). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-12-08, ASTAR EVA D857-00049 REV IR DAT

All 760: https://openairdocs.org/aircraft/N805DH/unmatched-reports.md

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Maher James P DYKE DELTA aircraft: https://openairdocs.org/model/maher-james-p-dyke-delta/aircraft.md
- The Amateur-built UNKNOWN ENG engine: https://openairdocs.org/engine/amateur-built-unknown-eng.md

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