# N706UP: 1969 Douglas DC-8-71F, registration cancelled 2010-03-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 30, 2010 - Status when cancelled: Triennial form not returned - Airframe: [Douglas DC-8-71F](https://openairdocs.org/model/douglas-dc-8-71f) (registry code 302199D) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs) - Serial number: 46056 - Year built: 1969 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 18, 1989 - Certificate issued: October 28, 1988 - Last registry action: September 15, 2009 - Mode S code: A96CA8 - Owner when cancelled: [Aersale Inc](https://openairdocs.org/faa-owner/AERSALE%20INC) - Location: [Coral Gables, FL](https://openairdocs.org/faa-place/FL/Coral%20Gables) - Owner type: Corporation - Owner's area on the map: 25.7533° N, 80.2704° W: Placed by OpenAirDocs at the center of ZIP code 33134, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N706UP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=706UP - Page: https://openairdocs.org/deregistered/N706UP-2010-03-30 From the FAA registry file of October 29, 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-8-71F: https://openairdocs.org/model/douglas-dc-8-71f.md ## Service difficulty reports (179, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UPS06848022](https://openairdocs.org/sdr/UPS06848022), Sep 21, 2006: SLIDE. INOPERATIVE. MAIN CABIN EXIT SLIDE/SLIDE INOP, LOW PRESSURE. REMOVED AND REPLACED SLIDE ASSY PER 25-60-01-2. CLEARED, PLACARD REMOVED AND BOTH COURIER SEATS REACTIVATED. - [SDR UPS06846679](https://openairdocs.org/sdr/UPS06846679), Mar 29, 2006: DOOR FRAME. CRACKED. INSPECTION TYPE:C3 VISUAL AND HFEC INSP DETECTED A CRACK APPROX .125" ON THE L-2 DOOR UPPER FWD DOOR JAMB CORNER EXTENDING FROM FASTENER. CUT OUT DAMAGE AT L-2 - [SDR UPS06846711](https://openairdocs.org/sdr/UPS06846711), Mar 24, 2006: FAIRING. CORRODED. INSPECTION TYPE:C3 LT STA 98 CANOE CORRODED UNDER BOTH FLAP TRACKS. REMOVED LT STA 98 FLAP CANOE IAW DC8-MM 27-51-12. REMOVED CORROSION BY MACHINING IAW SB 27-1 - [SDR UPS06846718](https://openairdocs.org/sdr/UPS06846718), Mar 23, 2006: STRINGER CLIP. CRACKED. INSPECTION TYPE:C2 CRACKED STRINGER CLIP ON OTBD SKATE ANGLE C/S-STRINGER 62 NR 4 MAIN TANK. REMOVED CRACKED CLIP AT OTBD SKATE ANGLE C/S STRINGER 62 NR 4 MAIN - [SDR UPS06846598](https://openairdocs.org/sdr/UPS06846598), Mar 23, 2006: LONGERON. CRACKED. FOUND LONGERON SPLICE L36 STA 1260-1280 IS CRACKED. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 1260-1280 L36 IAW SRM 51-1-20D, AND 51-1-8. - [SDR UPS06846719](https://openairdocs.org/sdr/UPS06846719), Mar 21, 2006: FITTING. CRACKED. INSPECTION TYPE:C3 STA 98 FLAP ACTUATOR REAR SPAR FITTING O/B LUG FOR SUPPORT LINK ARM IS BROKEN. FABRICATED AND INSTALLED NEW FITTING FROM 7050-T7451 PER AMS 4 - [SDR UPS06846709](https://openairdocs.org/sdr/UPS06846709), Mar 21, 2006: FAIRING. CORRODED. INSPECTION TYPE:C3 FLAP STA 98FH, CORROSION FOUND ON CANOE UNDER FLAP TRACKS. REMOVED STA 98 RH FLAP CANOE IAW DC8-MM 27-51-12. REMOVED CORROSION FROM FLAP CANO - [SDR UPS06846680](https://openairdocs.org/sdr/UPS06846680), Mar 21, 2006: SPLICE. CORRODED. A-PIT TORQUE BOX STA 280-270 LONGERON 34L-35L FITTING HAS CORROSION. REMOVED BATH TUB FITTING AT STA 280, AND REMOVED LONGERON SPLICE FITTING AT STA 270-280 L35 - [SDR UPS06846597](https://openairdocs.org/sdr/UPS06846597), Mar 20, 2006: LONGERON. CRACKED. INSPECTION TYPE:C3 LONGERON 15R IS CRACKED WHERE VERTICAL STAB ATTACHES STA 1740. REMOVED CRACKED LONGERON SECTION AT STA 1730-1750 15R IAW SRM 51-01-21-0 AND S - [SDR UPS06846518](https://openairdocs.org/sdr/UPS06846518), Mar 18, 2006: RIB. CRACKED. INSPECTION TYPE:C3 LT CENTER LE XRS 323 RIB IS CRACKED AT AFT UPPER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-02-0, 57-3-1 AND 51-01- - [SDR UPS06846059](https://openairdocs.org/sdr/UPS06846059), Jan 27, 2006: WINDSHIELD. CRACKED. OUTER PANE WINDSHIELD ON F/O'S SIDE CRACKED. REMOVED AND REPLACED RT WINDSHIELD PER MM 56-10-02-2, OPS AND LK CKS OK. - [SDR UPS05845646](https://openairdocs.org/sdr/UPS05845646), Oct 26, 2005: ENGINE. FLAMED OUT. NR 4 ENGINE FLAMED OUT IN CRUISE FLIGHT. T/S PER MM 71-00-00-1 FIG 139 SHT 1&2. REPLACED FUEL FILTER ELEMENT, RAN ENG WITH FEED & BOOST PUMP OFF, FUEL PRESS WIT - [SDR UPS04843616](https://openairdocs.org/sdr/UPS04843616), Dec 20, 2004: A/C PACK. ODOR. ON TOP OF DESCENT STRONG DIESEL FUEL JET FUEL ODOR WAS PRESENT AND SMELLED. ODOR WAS VERY STRONG. PRESSURIZED A/C, RAN BOTH PACKS FOR 30 MIN. NO ODOR NOTED. INS - [SDR UPS04843555](https://openairdocs.org/sdr/UPS04843555), Nov 29, 2004: BATTERY PACK. DISCHARGED. EMER LIGHTS STAY ON FOR LESS THAN A SECOND. REMOVED AND REPLACED EMER LIGHTS BATT PACK. OPS CK GOOD. - [SDR UPS04843333](https://openairdocs.org/sdr/UPS04843333), Oct 9, 2004: LAMP. INOPERATIVE. INSPECTION TYPE:N/A 3 EA LIGHTS FOR EMERGENCY LIGHTING AT ENTRY DOOR INOP. RELAMPED LIGHTS. OPS CHECKS GOOD. - [SDR UPS04842661](https://openairdocs.org/sdr/UPS04842661), Jul 7, 2004: LINK. BROKEN. NR 4 BRAKE COMPENSATING LINK BROKE AND BRAKE SPUN. REMOVED AND REPLACED COMPENSATING LINK IAW MM 32-42-04-4, 32-33-00-2 ATTACHED LINK TO MLG 29046. SECURED LINK - [SDR UPS04842061](https://openairdocs.org/sdr/UPS04842061), Mar 6, 2004: FITTING. CRACKED. INSPECTION TYPE:C2 STATION 270 BETWEEN LONG 35L-36 BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 53-2-0 FIG 2D. - [SDR UPS04842063](https://openairdocs.org/sdr/UPS04842063), Mar 5, 2004: LONGERON. CRACKED. INSPECTION TYPE:C2 STATION 257 LONGERON 34R I/B SIDE IS CRACKED. CUT OUT DAMAGED LONGERON SECTION BETWEEN STATION 230-290, FABRICATED AND INSTALLED LONGERON SEC - [SDR UPS04842062](https://openairdocs.org/sdr/UPS04842062), Mar 5, 2004: LONGERON. CRACKED. INSPECTION TYPE:C2 STATION 257 LONG 36 RIGHT IS CRACKED. REMOVED LONGERON SECTION BETWEEN STATION 250-290, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL, FABRICATED - [SDR UPS04842035](https://openairdocs.org/sdr/UPS04842035), Mar 3, 2004: FLOOR SUPPORT. CORRODED. INSPECTION TYPE: C2, FLOOR SUPPORT IS CORRODED BEYOND LIMITS BETWEEN STATION 1702 -1723 AT LBL 19. REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG 5755032 AND - [SDR UPS04842034](https://openairdocs.org/sdr/UPS04842034), Mar 3, 2004: SKIN. CRACKED. INSPECTION TYPE: C2, REMOVE EXTERNAL DOUBLER AT STATION 1722 LONGERON 17R-18R IAW EO DC8-5330-17288-A APPROX C AND REPAIR IAW SRM 53-2-1 FIG 7. REMOVED EXISTING - [SDR UPS04842031](https://openairdocs.org/sdr/UPS04842031), Mar 3, 2004: SUPPORT FITTING. CRACKED. INSPECTION TYPE: C2, STATION 780 FLOORBEAM SUPPORT FITTING IS CRACKED AT XC46R. REMOVED AND REPLACED FITTING IAW DWG 3641126 AND SRM 51-1-20D, 51-3-0. - [SDR UPS04842029](https://openairdocs.org/sdr/UPS04842029), Mar 3, 2004: LONGERON. CRACKED. INSPECTION TYPE:C2 STATION 1753 LONG 13R IS CRACKED. REMOVED DAMAGED LONGERON SECTION, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION, INSTALLED STRAPS A - [SDR UPS04842014](https://openairdocs.org/sdr/UPS04842014), Mar 3, 2004: DOUBLER. CORRODED. INSPECTION TYPE: C2, AFT SIDE STATION 1540 LONGERON 31L FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW SRM 53-4-1 - [SDR UPS04842013](https://openairdocs.org/sdr/UPS04842013), Mar 3, 2004: LONGERON. CRACKED. INSPECTION TYPE: C2, STA 1733 LONG 14L IS CRACKED. REMOVED, FABRICATED AND INSTALLED LONGERON SECTION, STRAPS AND INSTALLED SPLICE FITTING IAW SRM 53-2-2 FIG 10 - [SDR UPS04842010](https://openairdocs.org/sdr/UPS04842010), Mar 3, 2004: SHEAR TIE. CRACKED. INSPECTION TYPE:C2 STATION 1600 SHEAR TIE IS CRACKED BETWEEN LONGERONS 28L-29L. REMOVED DAMAGE, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL. FABRICATED AND INSTALL - [SDR UPS04842033](https://openairdocs.org/sdr/UPS04842033), Mar 2, 2004: FRAME. CORRODED. INSPECTION TYPE: C2, STATION 1300 FRAME IS CORRODED BEYOND LIMITS ON LOWER FLANGE AT LONG 36. CUT OUT DAMAGED FRAME SECTION, FABRICATED, INSTALLED 2 SPLICES, AN - [SDR UPS04842030](https://openairdocs.org/sdr/UPS04842030), Mar 2, 2004: SKIN. CRACKED. INSPECTION TYPE: C2, FUSELAGE SKIN IS CRACKED AT STATION 1730 LONG 8L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, FILLE - [SDR UPS04842017](https://openairdocs.org/sdr/UPS04842017), Mar 2, 2004: SKIN. CRACKED. INSPECTION TYPE: C2, RUDDER EXTERIOR SKIN IS CRACKED AT RT UPPER SIDE. REMOVED AND REPLACED RUDDER IAW MM 27-21-01. - [SDR UPS04842011](https://openairdocs.org/sdr/UPS04842011), Mar 2, 2004: SKIN. CORRODED. INSPECTION TYPE: C2, RIGHT HORIZONTAL STAB L/E SKIN HAS INTERGRANULAR CORROSION AT XFS 178.750. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW - [SDR UPS04842009](https://openairdocs.org/sdr/UPS04842009), Mar 2, 2004: FITTING. CRACKED. INSPECTION TYPE: C2, LONGERON 31L SPLICE FITTING IS CRACKED BETWEEN STA 1260-1280. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 51-1-20D, 53-1-0. - [SDR UPS04842067](https://openairdocs.org/sdr/UPS04842067), Feb 28, 2004: SKIN. CORRODED. INSPECTION TYPE:C2 LOWER FUSELAGE SKIN IS BULGED AT STA 275 LONG 34R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, TRIPLER, INTERNAL DOUBLER FILLER AND SKI - [SDR UPS04841751](https://openairdocs.org/sdr/UPS04841751), Jan 16, 2004: RELIEF VALVE. STUCK. DURING CRUISE NOTICED HYDRAULICS DECREASING. FOLLOWED POM PROCEDURE AND DEPRESSURIZED AND ISOLATED THE SYSTEM. FOUND BOGIE UNLOCK CYLINDER RELIEF VALVE ON LEFT - [SDR UPS03841456](https://openairdocs.org/sdr/UPS03841456), Oct 17, 2003: SKIN. CORRODED. FOUND EXTENSIVE CORROSION AT STATION 1746 SEVERAL RIVETS PULLED THROUGH SKIN. SKIN IS CRACKED AT L36 AND STA 1746. REMOVED FASTENERS IN CORRODED AREA FOUND L36 - [SDR UPS03841223](https://openairdocs.org/sdr/UPS03841223), Sep 15, 2003: FITTING. CRACKED. LT INBOARD FLAP HINGE CRACKED (MARKED) LT WING STA 98. DEFERRED PER FERRY PERMIT 9020. REMOVED STA 98 BASED FTG & ATTACHING STRUCTURE. LOCATED & DRILLED NEW 575 - [SDR UPS03840376](https://openairdocs.org/sdr/UPS03840376), Mar 27, 2003: SMOKE DETECTOR. INOPERATIVE. NR 3 SMOKE DETECTOR DOES NOT TEST. RELAMPED, OPS CHECK GOOD. - [SDR UPS02837958](https://openairdocs.org/sdr/UPS02837958), Mar 30, 2002: ODOR. DETECTED. INSPECTION TYPE:N/A ODOR IN COCKPIT FROM A/C UNIT. RAN BOTH PACKS WITH GROUND CART AND OFF ENGINE BLEEDS, COULD NOT DUPLICATE ODOR. OK FOR CONTINUED SERVICE. - [SDR UPS02837935](https://openairdocs.org/sdr/UPS02837935), Mar 11, 2002: FITTING. CORRODED. INSPECTION TYPE:C1 STA 70 FWD SIDE LONG 31R UPPER FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4614397, AND SRM 51-1-20D, 51-1-21. - [SDR UPS02837932](https://openairdocs.org/sdr/UPS02837932), Mar 8, 2002: DOUBLER. CORRODED. INSPECTION TYPE:C1 STA 25 TO 60 INTERNAL DOUBLER IS CORRODED BEYOND LIMITS BETWEEN LONG 26R TO 31R. REMOVED AND REPLACED DOUBLER IAW DWG 5649028, AND SRM 51-1-2 - [SDR UPS02837908](https://openairdocs.org/sdr/UPS02837908), Mar 8, 2002: LONGERON. CORRODED. INSPECTION TYPE:C1 STA 1650 LONG 35L LONGERON AND END FITTINGS ARE CORRODED BEYOND LIMITS. REMOVED END FITTINGS, AND LONG 35L BETWEEN STA 1650-1680, FABRICATED - [SDR UPS02837897](https://openairdocs.org/sdr/UPS02837897), Mar 8, 2002: FITTING. CRACKED. INSPECTION TYPE:C1 STA 1220 BATHTUB FITTING IS CRACKED BETWEEN LONG 34R-35R. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D, 51-1-20D. - [SDR UPS02837896](https://openairdocs.org/sdr/UPS02837896), Mar 8, 2002: FITTING. CRACKED. INSPECTION TYPE:C1 STA 1200 BATHTUB FITTING IS CRACKED BETWEEN LONG 33R-34R. REMOVED AND REPLACED FITTING IAW DWG 3755841 AND SRM 51-1-20D, 53-2-0 FIG 2D. - [SDR UPS02837911](https://openairdocs.org/sdr/UPS02837911), Mar 7, 2002: FITTING. CRACKED. INSPECTION TYPE:C1 STA 960 T-FITTING BETWEEN MAIN LANDING GEAR DOORS IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5616306, AND SRM 51-1-20D. - [SDR UPS02837914](https://openairdocs.org/sdr/UPS02837914), Mar 6, 2002: SKIN. CRACKED. INSPECTION TYPE:C1 LT MID GALLEY DOOR LOWER FWD CORNER CUTOUT SKIN IS CRACKED AT STA 1306 BETWEEN LONG 20L AND 21L. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS - [SDR UPS02837904](https://openairdocs.org/sdr/UPS02837904), Mar 6, 2002: SKIN. CRACKED. INSPECTION TYPE:C1 L2 DOOR JAMB LOWER FWD CORNER SKIN IS CRACKED BETWEEN LONG 20L AND 21L STA 1620. CUT OUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABR - [SDR UPS02837900](https://openairdocs.org/sdr/UPS02837900), Mar 6, 2002: SKIN. CRACKED. INSPECTION TYPE:C1 L-1 LOWER AFT CORNER DOUBLER AND TRIPLER DOES NOT CONFORM TO SRM 53 -2-0 FIG 15 AND SRO8530021, AND SKIN IS CRACKED AT STA 60 BETWEEN LONG 20 - [SDR UPS02837899](https://openairdocs.org/sdr/UPS02837899), Mar 6, 2002: SKIN. CRACKED. INSPECTION TYPE:C1 REPAIR AT STA 1440, UPPER AFT CORNER D-PIT DOOR IS A CATEGORY D PER EO DC8-5330-12800, AND SKIN IS CRACKED AT LONG 22R APPROX. REMOVED EXISTI - [SDR UPS02837895](https://openairdocs.org/sdr/UPS02837895), Mar 6, 2002: FITTING. CORRODED. INSPECTION TYPE:C1 MAIN CARGO DOOR JAMB NR 7 LATCH SPOOL FITTING HAS LOWER JAMB FITTINGS FWD AND AFT OF LATCH SPOOL FITTING HAVE INTERGRANULAR CORROSION AT STA - [SDR UPS02837878](https://openairdocs.org/sdr/UPS02837878), Mar 6, 2002: DOOR FRAME. CRACKED. INSPECTION TYPE:C1 L1 DOOR UPPER FWD PAN IS CRACKED IN CORNER, STA 25 LONG 10L. CUT OUT CRACK, NDT VERIFIED NO CRACK. FABRICATED AND INSTALLED DOUBLER IAW SRM 5 - [SDR UPS02837873](https://openairdocs.org/sdr/UPS02837873), Mar 6, 2002: SKIN. CRACKED. INSPECTION TYPE:C1 REPAIR AT STA 280 FWD LOWER CORNER OF A PIT DOOR CUTOUT IS A CATEGORY D PER EO DC8-5330-12800 AND SKIN IS CRACKED BETWEEN LONG 31R AND 32R. F All 179: https://openairdocs.org/deregistered/N706UP-2010-03-30/reports.md ## FAA accident and incident reports (2) 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 19950123002859I](https://openairdocs.org/incident/19950123002859I), Jan 23, 1995: Doug DC871F (N706UP), Philadelphia, PA. Narrative: flight crew reported enroute and inbound of a possible chemical spill. Their exposure time to unrecognizable fumes was approximately 30 minutes… - [Incident 19911227061899I](https://openairdocs.org/incident/19911227061899I), Dec 27, 1991: Doug DC871F (N706UP), Syracuse, NY. NR1 engine flamed out in flight. Completed flight. Unable to restart engine on ground. ## Other aircraft with N706UP - [Cancelled 2018-02-20](https://openairdocs.org/deregistered/N706UP-2018-02-20): Mcdonnell Douglas MD-90-30, S/N 53504. Registration expired, pending cancellation. Owner: [Aersale Inc](https://openairdocs.org/faa-owner/AERSALE%20INC), [Coral Gables, FL](https://openairdocs.org/faa-place/FL/Coral%20Gables) --- 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.