# N807DH: Douglas DC-8-73F, registration cancelled 2022-10-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 4, 2022
- Exported to: Peru
- Status when cancelled: Valid registration
- Airframe: [Douglas DC-8-73F](https://openairdocs.org/model/douglas-dc-8-73f) (registry code 302199F)
- Engine: [NONE](https://openairdocs.org/engine/none) (registry code 00000)
- Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs)
- Serial number: 45990
- Type of aircraft: Fixed wing multi engine
- Engine type: None
- Airworthiness: Standard, transport
- Airworthiness date: July 17, 1968
- Certificate issued: August 31, 2022
- Last registry action: August 31, 2022
- Mode S code: AAFC31
- Owner when cancelled: [Skybus Cargo Jet Inc](https://openairdocs.org/faa-owner/SKYBUS%20CARGO%20JET%20INC)
- Location: [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas)
- Owner type: Corporation
- Owner's area on the map: 36.0845° N, 115.1461° W: Placed by OpenAirDocs at the center of ZIP code 89119, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N807DH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=807DH
- Page: https://openairdocs.org/deregistered/N807DH-2022-10-04

From the FAA registry file of November 3, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Douglas DC-8-73F: https://openairdocs.org/model/douglas-dc-8-73f.md

## Service difficulty reports (580, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DHLA201100539](https://openairdocs.org/sdr/DHLA201100539), Nov 15, 2011: ACTUATOR. LEAKING. AFTER DEPARTURE, ACFT LOST HYDRAULIC LEVEL TO JUST ABOVE THE EMERGENCY LEVEL. ALL PROCEDURES COMPLIED AND ACFT RETURNED TO DEPARTURE. ACFT GROUNDED ON ARRIVAL. 
- [SDR DHLA201100531](https://openairdocs.org/sdr/DHLA201100531), Jun 23, 2011: FITTING. CORRODED. RT OUTER WING FWD BOTTOM PANEL.- FITTING HAS EXFOLIATION CORROSION S-62 (NR 4 ALT TANK) STA XW 408.000 PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, DWG 3640143. 
- [SDR DHLA201100530](https://openairdocs.org/sdr/DHLA201100530), Jun 23, 2011: FITTING. CORRODED. RT OUTER WING FWD BOTTOM PANEL.- FITTING HAS EXFOLIATION CORROSIOIN S-63, STA XW 408.000 (NR4 ALT TANK) PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, DWG 3640143.
- [SDR DHLA201100532](https://openairdocs.org/sdr/DHLA201100532), Jun 7, 2011: STRINGER. CRACKED. RT INNER WING AFT TOP PANEL.- STRINGER NR4 CRACKED STA XRS 87.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 07-21-11, EVA D857-00408 REV IR DATED 07-06
- [SDR DHLA201100527](https://openairdocs.org/sdr/DHLA201100527), Jun 7, 2011: LONGERON. CORRODED. FWD ACCY COMPT- L33R SHOWS EXFOLIATION CORROSION AT STA 14.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 10 SHEET 1,3, TR 53-153 SHEET 4, TR 53-193. REMOVED F
- [SDR DHLA201100521](https://openairdocs.org/sdr/DHLA201100521), Jun 7, 2011: LONGERON. CORRODED. FWD ACCY COMPT- L33R SHOWS EXFOLIATION CORROSION AT STA 14.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 10 SHEET 1,3, TR 53-153, SHEET 4, TR 53-193. REMOVED 
- [SDR DHLA201100524](https://openairdocs.org/sdr/DHLA201100524), Jun 6, 2011: FRAME. DEFORMED. MAIN CARGO BAY FRAME DEFORMED BS 1580.000 L19TO 21R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 2 SHEET 6, SRM 53-4-1 FIG. 51 SHEET 21. REMOVED DEFORMED FRAME S
- [SDR DHLA201100523](https://openairdocs.org/sdr/DHLA201100523), Jun 6, 2011: FITTING. CORRODED. FWD ACCY COMPT FITTING CORRODED BY EXFOLIATION STA 8.000 L33R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1 REMOVED CORROSION IAW SRM 51-1-8 PG 17-18 FOUND WITHIN
- [SDR DHLA201100529](https://openairdocs.org/sdr/DHLA201100529), Jun 3, 2011: TEE FITTING. CRACKED. R2 SERVICE DOOR INNER FITTING CRACKED 1". REMOVED CRACKED TEE FITTING IAW SRM 51-1-20D, SRM 51-1-21. CLEANED, TREATED & PRIMED AREA IAW SRM 51-1-8B. INSTALLED N
- [SDR DHLA201100520](https://openairdocs.org/sdr/DHLA201100520), Jun 2, 2011: SKIN. CORRODED. EXT FUS LWR SKIN CORRODED STA 1460.000 - 1480.000, L34L TO 35L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0, PG 1, SRM 53-4-1, FIG. 17A SHEET 2. REMOVED LEVEL II CORR
- [SDR DHLA201100522](https://openairdocs.org/sdr/DHLA201100522), Jun 1, 2011: SKIN. CRACKED. RT WING UPPER SKIN 2" CRACK STA XRS 74.869 (BETWEEN CTR SPAR AND S-8). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-28-11, EVA D857-00406 REV IR, ASTAR D
- [SDR DHLA201100519](https://openairdocs.org/sdr/DHLA201100519), Jun 1, 2011: FRAME. DEFORMED. MAIN CARGO COMPT FRAME DEFORMED STA 1580.000 L21 TO 19L PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2, SHEET 6, SRM 53-4-1 FIG 51 SHEET 21. REMOVED DEFORMED FRAME
- [SDR DHLA201100528](https://openairdocs.org/sdr/DHLA201100528), May 31, 2011: ANGLE. CRACKED. NR 2 ENG TO PYLON ANGLE CRACK 10" STA YN 183.000 AT 12 O'CLOCK POS, LT SIDE. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATE 07-02-11, EVA D854-00407, REV IR D
- [SDR DHLA201100526](https://openairdocs.org/sdr/DHLA201100526), May 31, 2011: FITTING. CORRODED. RT MLG WHEEL WELL FITTING CORRODED AT STA 857.125, RBL 47 (EXFOLIATION). REMOVED LEVEL II CORROSION IAW SRM 51-1-8 PG 17-20. FOUND OUT OF LIMITS IAW SRM 53-2-0 
- [SDR DHLA201100518](https://openairdocs.org/sdr/DHLA201100518), May 31, 2011: SKIN. CORRODED. RT AILERON SKIN LOWER PLATING CORRODED STA XA 737.000 - XA 775.000. PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 4. REMOVED LEVEL 2 CORROSION IAW SRM 51-1-8 PG 17-
- [SDR DHLA201000138](https://openairdocs.org/sdr/DHLA201000138), Nov 24, 2010: ENGINE. POWER LOSS. ENG NR1 ROLLED BACK ON CLIMBOUT. PERFORMED ENG SHUTDOWN & RE-LIGHT. NO FUTHER PROBLEMS. ACFT WAS GROUNDED UPON ARRIVAL. C/W TROUBLESHOOTING IAW MM AND MM 71-00.
- [SDR DHLA201000119](https://openairdocs.org/sdr/DHLA201000119), Oct 16, 2010: LAMP. INOPERATIVE. EMERGENCY LIGHT DISARMED LIGHT NOT ILLUMINATED ON DIMM SETTING. ACFT WAS GROUNDED. RELAMPED DISARMED LIGHT IAW MM 33-13-0. OPS GOOD PN 313.
- [SDR DHLA201000092](https://openairdocs.org/sdr/DHLA201000092), Sep 26, 2010: SKIN. CORRODED. FUSELAGE SKIN BULGING WITH SEVERAL CORROSION INDUCED CRACKS AT FS 26.0, RBL5.0, BETWEEN LONGERONS 36 AND 35R. RESOLUTION: ACCOMPLISHED FUSELAGE SKIN DOUBLER AND
- [SDR DHLA201000015](https://openairdocs.org/sdr/DHLA201000015), Feb 8, 2010: TIRE. FAILED. ON LANDING, SIGNIFICANT ACFT VIBRATION NOTED. AFTER CLEARING RUNWAY GROUND CONFIRMED 2 LT TIRES WERE BLOWN. NOTE ANTI-SKID ON DMI NR 35939 AT THE TIME OF INCIDE
- [SDR DHLA201000003](https://openairdocs.org/sdr/DHLA201000003), Jan 14, 2010: LAMP. INOPERATIVE. DURING EMERGENCY LIGHTING CHECK, ONLY 2 OF THE 3 REQUIRED LTS ILLUMINATED ON INSTRUMENT PANEL GLARESHIELD. RELAMPED IAW MM 33-50. OPS CK OK IAW MM 33-5. FOUND D
- [SDR DHLA2010807501](https://openairdocs.org/sdr/DHLA2010807501), Dec 14, 2009: KEELBEAM. CRACKED. MLG W/W KEEL BEAM TEE ANGLE CRACKED 1/4" AT STA 940.000. REMOVED AND REPLACED TEE ANGLE AT STA 940.000 IAW JC EC-01874-001 AND DWG NR 4645516 AND IAW SRM 51-1-2
- [SDR DHLA2010807502](https://openairdocs.org/sdr/DHLA2010807502), Dec 10, 2009: DOUBLER. CRACKED. FUSE NOSE SECTION ACCESS DOOR NR 2 INLET INTERNAL DOUBLER CRACKED 1 3/4". PERFORMED MAJOR REPAIR IAW 8110-3 DTD 12-04-09 EVA D853-00286 REV IR DTD 11-20-09 REMO
- [SDR DHLA2010807504](https://openairdocs.org/sdr/DHLA2010807504), Dec 2, 2009: BEAM. CORRODED. FWD CARGO COMPT, BEAM CORRODED STA 180.000 LBL 5. PERFORMED MAJOR REPAIR IAW SRM 51-2-1 SHEET 9,12 TR NR 51-130, DTD 01-26-04.
- [SDR DHLA2010807508](https://openairdocs.org/sdr/DHLA2010807508), Nov 26, 2009: SKIN. CRACKED. LT INBD FLAP LWR SKIN CRACKED STA XCW 64.000. PERFORMED MAJOR REPAIR IAW SRM 57-7-1-FIG1 PG2.
- [SDR DHLA2010807503](https://openairdocs.org/sdr/DHLA2010807503), Nov 26, 2009: SKIN. CRACKED. LEFT WING UPPER SKIN CRACKED STA XRS 74.000 S-9. PERFORMED MAJOR REPAIR ON LT WING UPPER SKIN AT STA XRS 74.000 S-9 IAW SRM 57-2-1, FIG 17.
- [SDR DHLA2010807505](https://openairdocs.org/sdr/DHLA2010807505), Nov 25, 2009: SKIN. SCRATCHED. REMOVE PAINT AND INSPECT FUSELAGE SKIN FOR DEEP SCRATCHES AT STA 1360 L-24L. PERFORMED MAJOR REPAIR IAW SRM 53-2-1-FIG 7 SHEET 2,23,24 AND TR NR 53-203 DTD 01/2
- [SDR DHLA200900051](https://openairdocs.org/sdr/DHLA200900051), Oct 23, 2009: BATTERY PACK. DISCHARGED. ON PRE-DEPARTURE CHECK FOUND EMERGENCY LIGHT INOP. R & R BATTERY PACK IAW MM 33-51-1 CHECKED OPERATION OK. AIRCRAFT WAS GROUNDED
- [SDR DHLA200900050](https://openairdocs.org/sdr/DHLA200900050), Sep 12, 2009: LIGHT. BURNED. DURING ENGINE START, ODOR OF SMOKE IN COCKPIT, S/O OBSERVED SMOKE COMING FROM PANEL NEAR DOOR HANDLE, PANEL WAS HOT AND PAINT WAS BURNED. FOUND READ, ENTRY , IN
- [SDR DHLA200900045](https://openairdocs.org/sdr/DHLA200900045), Aug 13, 2009: PUMP. FAILED. CLIMBING THROUGH FL 210 IN LEFT TURN NR 4 ENGINE FLAMED OUT. RAN CHECK LIST ABNORMAL PROCEDURES RESTARTED ENG, ALL PARAMETERS OK. CLEANED CBP LINE IAW CFM MM 73
- [SDR DHLA200900043](https://openairdocs.org/sdr/DHLA200900043), Aug 5, 2009: FIRE WARNING. FALSE ACTIVATION. ENG NR 1 FIRE INDICATION. SHUT ENG DOWN WITH NORMAL LANDING. INSPECTED NR 1 ENGINE, NO EVIDENCE OF FIRE INDICATED, ALSO INSPECTED FIRE DETECTION SYSTEM AND ENGI
- [SDR DHLA200900017](https://openairdocs.org/sdr/DHLA200900017), Mar 19, 2009: LINE. CRACKED. NR 4 OIL QUANTITY WENT TO 0 AND OIL 8 PSI ADHERED TO EMERGENCY PROCEDURE. FOUND OIL LINE TO ENG OIL PRESSURE XMITER CRACKED. REMOVED AND REPLACED LINE. OPS AND 
- [SDR DHLA200800005A](https://openairdocs.org/sdr/DHLA200800005A), Jan 25, 2009: WIRE HARNESS. FAILED. NR 4 ENGINE FIRE WARNING ILLUMINATED COMPLETED CHECKLIST. IFSD ENGINE NR 4, FOUND "A" LOOP CORE LT SIDE PYLON HARNESS PIN BROKEN. REPLACED CONNECTOR PER S/W/P 2
- [SDR DHLA200800004A](https://openairdocs.org/sdr/DHLA200800004A), Jan 23, 2009: ELEMENT. FAILED. WHILE IN A LOOP ENGINE FIRE LIGHT ON NR 4 ENGINE ILLUMINATED MOMENTARILY THEN WENT OUT SWITCHED TO B LOOP LIGHT STAYED OUT FOR THE DURATION OF THE FLT. REPLACED
- [SDR DHLA200800112](https://openairdocs.org/sdr/DHLA200800112), Oct 9, 2008: FIRE WARNING. MALFUNCTIONED. PRIOR TO DESCENT NR 3 FIRE WARNING HANDLE ILLUMINATED AND MASTER FIRE WARNING BELL SOUNDED INTERMITTENTLY THEN EXTINGUISHED FIRE LOOP TESTED OK. RESOLUTION DESC
- [SDR DHLA200800071](https://openairdocs.org/sdr/DHLA200800071), Jun 17, 2008: FIRE LOOP. SHORTED. ENG FIRE WARNING NR 3 COMPLIED WITH PHASE 1 EMERG CHECKLIST ABNORMAL PROCEDURES AGENT DISCHARGED. INSPECTED ENG, NO FIRE IS LOCATED FAULT AND DETERMINED "A" LOO
- [SDR DHLA200800069](https://openairdocs.org/sdr/DHLA200800069), Jun 17, 2008: FIRE LOOP. MALFUNCTIONED. FLT 916 - NR 3 ENGINE FIRE INDICATION IN CRUISE SHUT DOWN PER EMER CHECK LIST AND BLEW BOTH BOTTLES. INDICATION PERSISTED OFF AND ON. LT BOTTLE SHOWED BLOWN AT 
- [SDR DHLA200800070](https://openairdocs.org/sdr/DHLA200800070), Jun 17, 2008: FIRE LOOP. MALFUNCTIONED. FLT 916 - NR 3 ENGINE FIRE INDICATION IN CRUISE SHUTDOWN PER EMER CHECK LIST AND BLEW BOTH BOTTLES. INDICATION PERSISTED OFF AND ON. LT BOTTLE SHOWED BLOWN AT S
- [SDR DHLA200800064](https://openairdocs.org/sdr/DHLA200800064), Jun 17, 2008: CONNECTOR. MALFUNCTIONED. FLT 916 - NR 3 ENGINE FIRE INDICATION IN CRUISE SHUT DOWN PER EMER CHECK LIST AND BLEW BOTH BOTTLES. INDICATION PERSISTED OFF AND ON. LT BOTTLE SHOWED BLOWN AT 
- [SDR DHLA200800057](https://openairdocs.org/sdr/DHLA200800057), Jun 9, 2008: FIRE LOOP. FALSE INDICATION. NR 3 ENG FIRE WARNING. COMPLETED CHECK LIST LIGHT REMAINED ON. PERFORMED NR 3 ENG RUN PER JRH 11.1 ALL SYSTEMS OPERATE NORMALLY. NO LEAKS NOTED SYS B-LOOP CHECK
- [SDR DHL2008807525](https://openairdocs.org/sdr/DHL2008807525), May 19, 2008: FITTING. CRACKED. FWD CARGO COMPT FITTING CRACKED STA 300.000 L-26L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED,
- [SDR DHL2008807526](https://openairdocs.org/sdr/DHL2008807526), May 14, 2008: STIFFENER. CRACKED. KEEL BEAM TEE STIFFENER (EXTRUSION) HAS TWO CRACKS OF 0.250 INCH STA 896.000. REMOVED CRACKED TEE STIFFENER IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA I
- [SDR DHL2008807530](https://openairdocs.org/sdr/DHL2008807530), May 13, 2008: SKIN. CRACKED. FUSELAGE NOSE SECTION, MODIFICATION DOUBLER AT AFT UPPER CORNER OF RT PRIMARY HEAT EXCHANGER, STA -12.000 L-24R (0.500" SKIN CRACKED) MAJOR REPAIR. PERFORMED MA
- [SDR DHL2008807528](https://openairdocs.org/sdr/DHL2008807528), May 11, 2008: SKIN. CRACKED. LT ELEV UPPER SKIN CRACKED 2 INCHES AND SEVERAL FASTENERS LOOSE (STA XE 79.531) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-4-1 FIG 1 SHEET 1-2. REMOVED DAM
- [SDR DHL2008807523](https://openairdocs.org/sdr/DHL2008807523), May 9, 2008: SKIN. CANNING. RT RUDDER SKIN OIL CANNING (STA ZR 136.000 - 125.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG
- [SDR DHL2008807513](https://openairdocs.org/sdr/DHL2008807513), May 9, 2008: STIFFENER. CRACKED. RUDDER INTERNAL STRUCTURE STIFFENER CRACKED 1.500 INCH STA ZR 162.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-
- [SDR DHL2008807512](https://openairdocs.org/sdr/DHL2008807512), May 9, 2008: STIFFENER. CRACKED. RUDDER INTERNAL STRUCTURE STIFFENER CRACKED 1.500 INCH STA ZR 105.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-
- [SDR DHL2008807521](https://openairdocs.org/sdr/DHL2008807521), May 9, 2008: FITTING. CRACKED. MAIN CARGO COMPT FRAME FITTING CRACKED 3 INCHES STA 857.125 L-19R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51
- [SDR DHL2008807511](https://openairdocs.org/sdr/DHL2008807511), May 9, 2008: PANEL. DELAMINATED. WING TO FUS LWR PANEL NR 732 INTERNAL SKIN DELAMINATED (STA 980.000 - 1050.000). REMOVED WING TO FUS LWR PANEL NR 732 IAW SRM 51-3-0. CLEANED, TREATED AND PRIME
- [SDR DHL2008807527](https://openairdocs.org/sdr/DHL2008807527), May 8, 2008: NONE. NONE. REMOVED AND REPLACED EXISTING REPAIR AT FUSELAGE STA 320 LT SIDE L-28L WITH PERMANENT TYPE REPAIR PER SRM. INDICATE TYPE OF REPAIR, RE-INSPECTION INTERVAL AND N
- [SDR DHL2008807536](https://openairdocs.org/sdr/DHL2008807536), May 8, 2008: SKIN. CORRODED. FUSELAGE EXTERNAL SKIN CORRODED (STA 665.000 - 680.000, L-35L - L-36) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1-4. REMOVED CORROSION IAW

All 580: https://openairdocs.org/deregistered/N807DH-2022-10-04/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20100208004889I](https://openairdocs.org/incident/20100208004889I), Feb 8, 2010: Douglas DC-8-73F (N807DH), Memphis, TN, Minor damage. During landing at Memphis the left rear main inboard and outboard tires blew. The tire debris struck the left inboard flap causing a 12" by 10" up to 0.250"…

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