# N752UP: 1968 Douglas DC-8-71F, registration cancelled 2014-09-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 18, 2014
- Status when cancelled: Valid registration
- 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: 45952
- Year built: 1968
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 16, 1986
- Certificate issued: June 17, 2010
- Last registry action: May 14, 2014
- Mode S code: AA2347
- 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/N752UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=752UP
- Page: https://openairdocs.org/deregistered/N752UP-2014-09-18

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 (362, newest 50)

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

- [SDR IPXA09855477](https://openairdocs.org/sdr/IPXA09855477), Apr 9, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV SS 752-F1-06 STA -77 TO STA -2 L21L TO L24L SKIN SPLICE REPAIR DOES NOT CORRELATE WITH SRM. ACCOMPLISHED REPAIR IAW REO-G12621 REV B AND IPXA
- [SDR IPXA09855476](https://openairdocs.org/sdr/IPXA09855476), Apr 9, 2009: DOUBLER. CRACKED. INSPECTION TYPE:SV SURVEY SEQUENCE 752-F1-59 DOUBLER AT L1 DOOR UPPER AFT CORNER IS CRACKED. ACCOMPLISHED REPAIR IAW DC8 SRM 55-02-00-0 PAGE 1 REV 78.
- [SDR IPXA09855473](https://openairdocs.org/sdr/IPXA09855473), Apr 9, 2009: DOUBLER. DAMAGED. INSPECTION TYPE:SV BS 1600 TO 1657 BETWEEN LONGERON 31R AND 32R AT INTERNAL DOUBLER AREAS HAS NUMEROUS OVERSIZED HOLES. REPAIR PER REO-G127714 REV E EO DC8-5320
- [SDR IPXA09855453](https://openairdocs.org/sdr/IPXA09855453), Apr 8, 2009: STRUCTURE. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQUENCE 752-S4-03 RUDDER LT AT STA ZR 281.250 REPAIR DOES NOT MATCH CURRENT SRM. ACCOMPLISHED REPAIR IAW REO-G12616 REV B AND IPXA EO
- [SDR IPXA09855452](https://openairdocs.org/sdr/IPXA09855452), Apr 8, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQUENCE 752-F1-19 FUSELAGE EXTERIOR SKIN SURFACE STA 1752 - 1774 L33L REPAIR CONFIGURATION DOES NOT CORRELATE TO A SRM REPAIR. ACCOMP
- [SDR IPXA09855451](https://openairdocs.org/sdr/IPXA09855451), Apr 8, 2009: STRUCTURE. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQUENCE 752-F1-72 REPAIR DOUBLER DOES NOT CORRELATE TO SRM REPAIR STA 115.5 TO 126.5. ACCOMPLISHED REPAIR IAW DC8 SRM 53-21-1 FIG 7 S
- [SDR IPXA09855450](https://openairdocs.org/sdr/IPXA09855450), Apr 8, 2009: DOUBLER. DENTED. INSPECTION TYPE:SV SURVEY SEQUENCE 752-S2-06 RT ELEVATOR UPPER SURFACE STA XE 200.2187 8 INTERNAL DOUBLER IS DENTED AND CRACKED. ACCOMPLISHED REPAIR IAW REO-G12
- [SDR IPXA09855449](https://openairdocs.org/sdr/IPXA09855449), Apr 8, 2009: PRESSURE PANEL. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQUENCE 752-F3-08 NOSE SECTION HORIZONTAL PRESSURE WEB DOES NOT CORRELATE TO SRM REPAIR. ACCOMPLISHED REPAIR IAW REO-G12739 REV B AND
- [SDR IPXA09855442](https://openairdocs.org/sdr/IPXA09855442), Apr 8, 2009: LONGERON. MISREPAIRED. INSPECTION TYPE:SV BS 1640 TO 1660 LONGERON 31L HAS NUMEROUS OVERSIZED HOLES. REPAIR ACCOMPLISHED PER REO-G12744 REV B AND EO DC8-5320-33031-A.
- [SDR IPXA09855441](https://openairdocs.org/sdr/IPXA09855441), Apr 8, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV BS 1614 TO 1657 THE INTERNAL DOUBLER SECTION LOCATED BETWEEN L31L AND 32L HAS NUMEROUS OVERSIZED HOLES. THIS INCLUDES TWO HOLES IN SHEAR TIE 
- [SDR IPXA09855439](https://openairdocs.org/sdr/IPXA09855439), Apr 8, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F1-57 DOUBLER FROM STA 60 T0 STA 67, BETWEEN L7L AND L8L HAS FASTENERS SPACING LESS THAN 4 FASTENER DIAMETER ABOVE L1 DOOR. RE
- [SDR IPXA09855436](https://openairdocs.org/sdr/IPXA09855436), Apr 8, 2009: PRESSURE PANEL. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F3-06 NWW PRESSURE PANEL WEB REPAIR DOES NOT CORRELATE TO A SRM REPAIR ENGINEERING ASSIST REQUIRE FOR DISPOSITION OF THE REPAI
- [SDR IPXA09855434](https://openairdocs.org/sdr/IPXA09855434), Apr 8, 2009: STRUCTURE. DAMAGED. INSPECTION TYPE:SV SURVEY SEQ 752-54-01 RT VERTICAL STAB REPAIR STA ZR 74.000 HAS FASTENER REPAIR. ACCOMPLISHED PER REO-G12648 AND EO DC8-5520-32835.
- [SDR IPXA09855433](https://openairdocs.org/sdr/IPXA09855433), Apr 8, 2009: PRESSURE PANEL. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F3-09 NOSE SECTION HORIZ PRESSURE PANEL REPAIR BS-17. 5 TO-6 LBL 41-LBL 55 DOES NOT CORRELATE TO SRM REPAIR, CONTACT ENGINEERI
- [SDR IPXA09855425](https://openairdocs.org/sdr/IPXA09855425), Apr 8, 2009: PRESSURE PANEL. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F3-11 REPAIR DOUBLER HAS FIELD FASTENERS WITH LESS THAN 4D SPACING. COCKPIT FLOOR PRESSURE DECK STA 37 TO -23.5 RBL 56-62. REP
- [SDR IPXA09855408](https://openairdocs.org/sdr/IPXA09855408), Apr 7, 2009: DOUBLER. BULGED. INSPECTION TYPE:SV SURVEY SEQ 752-S1-07 LT ELEV UPPER SKIN REPAIR DOUBLER HAS A BULGE XE 200.238. REPAIR ACCOMPLISHED PER REO-G12626 REV C AND EO DC8-5520-32977
- [SDR IPXA09855407](https://openairdocs.org/sdr/IPXA09855407), Apr 7, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F1-40 FUSE EXT SURFACE STA 567 TO STA 574 L35R. REPAIR CONFIGURATION DOES NOT CORRELATE TO TO SRM. REPAIR ACCOMPLISHED PER REO
- [SDR IPXA09855406](https://openairdocs.org/sdr/IPXA09855406), Apr 7, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F1-21 STA -128 TO -95.5 L31R TO L25 SKIN SPLICE REPAIR DOES NOT CORRELATE WITH SRM. REPAIR ACCOMPLISHED PER REO-G12621 AND EO 
- [SDR IPXA09855374](https://openairdocs.org/sdr/IPXA09855374), Apr 6, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV EXISTING REPAIR DOUBLER EXT FUSELAGE STA 114 L24L DOES NOT CORRELATE TO A SRM REPAIR. (SURVEY SEQUENCE 752-F1-10). REPAIRED IAW DC8 SRM 53-2-
- [SDR IPXA09855373](https://openairdocs.org/sdr/IPXA09855373), Apr 6, 2009: LONGERON. DAMAGED. INSPECTION TYPE:SV BS 1615 TO 1655 AT LONGERON 32R HAS NUMEROUS OVERSIZED HOLES. REPAIRED IAW DC8 SRM 53-2-2 FIG 10 SHT 4 (TR 53-193) SECTION -7001 VIEW A-A.
- [SDR IPXA09855372](https://openairdocs.org/sdr/IPXA09855372), Apr 6, 2009: LONGERON. DAMAGED. INSPECTION TYPE:SV BS 1615 TO 1655 LONGERON 33R HAS NUMEROUS OVERSIZED HOLES. REPAIRED IAW DC8 SRM 53-2-2 FIG 10 SHT 4 (TR 53-193) SECTION -7005 VIE W B-B.
- [SDR IPXA09855371](https://openairdocs.org/sdr/IPXA09855371), Apr 6, 2009: LONGERON. DAMAGED. INSPECTION TYPE:SV BS 1610 TO 1655 LONGERON 32L HAS NUMEROUS OVERSIZED HOLES. REPAIRED IAW DC8 SRM 53-2-2 FIG 10 SHT 4 (TR 53-193) SECTION -7001 VIEW A-A.
- [SDR IPXA09855370](https://openairdocs.org/sdr/IPXA09855370), Apr 6, 2009: LONGERON. DAMAGED. INSPECTION TYPE:SV BS 1614 TO 1655 LONGERON 33L HAS NUMEROUS OVERSIZED HOLES. REPAIRED IAW DC8 SRM 53-2-2 FIG 10 SHT 4 (TR 53-193) SECTION -7005 VIEW B-B.
- [SDR IPXA09855369](https://openairdocs.org/sdr/IPXA09855369), Apr 6, 2009: SKIN PANEL. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F1-11 REPAIR AT STA 167 TO STA 176 L28L TO L30L LOCATED WITHIN RVSM CRITICAL AREA. REF AMM 34-12-02-2 FIG 203 SHT 01. REPAIR A
- [SDR IPXA09855367](https://openairdocs.org/sdr/IPXA09855367), Apr 6, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F1-60 L1 DOOR FWD LOWER CORNER OUTER SKIN REPAIR DOES NOT CORRELATE WITH SRM. REPAIRED PER DC8 SRM 52-2-0 FIG 4 SHT 3.
- [SDR IPXA09855366](https://openairdocs.org/sdr/IPXA09855366), Apr 6, 2009: STRUCTURE. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F1-52 STA 1595 TO 1606 L25R TO L27R HAS FASTENERS WITH LESS THAN 4D SPACING. REPAIR INSTALLED DC8 SRM 53-2-1 FIG 7 SHT 5 T/R 5
- [SDR IPXA09855365](https://openairdocs.org/sdr/IPXA09855365), Apr 6, 2009: PRESSURE PANEL. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F3-7 DOUBLER REPAIR AT NOSE PRESSURE DECK BS 17.5 TO -10.5 BL 0 TO RBL 19.5 DOES NOT CORRELATE TO SRM. REPAIR ACCOMPLISHED PER
- [SDR IPXA09855364](https://openairdocs.org/sdr/IPXA09855364), Apr 6, 2009: STRUCTURE. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F1-07 REPAIR DOUBLER DOES NOT CORRELATE TO A SRM REPAIR, FUSE STA 37 TO 57 L28L TO L30L. REPAIR INSTALLED PER DC8 SRM 53-2-0 F
- [SDR IPXA09855362](https://openairdocs.org/sdr/IPXA09855362), Apr 6, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F1-65, MAIN CARGO DOOR EXTERNAL SKIN REPAIR BS 264 - 270 .5 L20L TO L21L, DOES NOT CORRELATE TO A SRM DUE TO DOUBLER MATERIAL 
- [SDR IPXA09855354](https://openairdocs.org/sdr/IPXA09855354), Apr 6, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F1-03 STA 139 TO STA 97 L31L TO RBL 25 SKIN SPLICE REPAIR DOES NOT CORRELATE WITH SRM. REPAIR ACCOMPLISHED PER REO-G12621 AND 
- [SDR IPXA09855353](https://openairdocs.org/sdr/IPXA09855353), Apr 6, 2009: STRUCTURE. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-S1-02 LT HORIZ STAB DOUBLER AT XFS 115.00 MINIMUM REPAIR FASTENER DIAMETER, AS MARKED. REPAIR ACCOMPLISHED PER REO-G12621 AND 
- [SDR IPXA09855352](https://openairdocs.org/sdr/IPXA09855352), Apr 6, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-W3-8 LT WING CENTER L/E LWR SURFACE REPAIR STA XFS 426 DOUBLER IS NOT ALUMINUM MATERIAL REF APPX H ITEM A-31. REPAIR ACCOMPLIS
- [SDR IPXA09855351](https://openairdocs.org/sdr/IPXA09855351), Apr 6, 2009: DOUBLER. GOUGED. INSPECTION TYPE:SV SURVEY SEQ 752-W4-20 RT OUTBOARD FLAP STA 213.248 TOP SIDE DOUBLER GOUGED. REPAIR ACCOMPLISHED PER REO-G12587 AND EO DC8-5720-32215.
- [SDR IPXA09855331](https://openairdocs.org/sdr/IPXA09855331), Apr 4, 2009: STRUCTURE. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-52-10 DOES NOT CORRELATE TO ANY SRM REPAIR. ACCOMPLISHED REPAIR PER DC8 SRM 55-2-1 FIG 4.
- [SDR IPXA09855330](https://openairdocs.org/sdr/IPXA09855330), Apr 4, 2009: SKIN. DAMAGED. INSPECTION TYPE:SV LT ELEVATOR OUTBOARD TRAILING EDGE UPPER SURFACE AND ATTACH CHANNEL HAS SEVERAL DOUBLE DRILL FASTENER HOLES. REMOVED AND REPLACED ATTACHED AN
- [SDR IPXA09855329](https://openairdocs.org/sdr/IPXA09855329), Apr 4, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F1-71, FUSE EXT SURFACE STA 1695-1703 L16R-L17R, REPAIR CONFIGURATION DOES NOT CORRELATE TO A SRM REPAIR. REPAIR ACCOMPLISHED 
- [SDR IPXA09855328](https://openairdocs.org/sdr/IPXA09855328), Apr 4, 2009: SKIN PANEL. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-W4-17 REPAIR AT RT WING UPPER SURFACE STA XRS 467AAT FRONT SPAR DOES NOT CORRELATE TO AN SRM REPAIR. REPAIR ACCOMPLISHED PER T
- [SDR IPXA09855326](https://openairdocs.org/sdr/IPXA09855326), Apr 4, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F1-70 EXT FUSELAGE, STA 11-18 L16L, REPAIR CONFIGURATION DOES NOT CORRELATE TO A SRM. REPAIR ACCOMPLISHED PER TIMCO REO-G12624
- [SDR IPXA09855321](https://openairdocs.org/sdr/IPXA09855321), Apr 3, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F1-05, FWD FUSE STA 35-7 L23L TO L28L, REPAIR CONFIGURATION DOES NOT CORRELATE TO A SRM. REPAIR ACCOMPLISHED PER TIMCO RE0-G12
- [SDR IPXA09855320](https://openairdocs.org/sdr/IPXA09855320), Apr 3, 2009: LONGERON. DAMAGED. INSPECTION TYPE:SV LONGERON 33L APPROX STA 1652 TO 1660, FWD END OF SHORT LONGERON, HAS OVERSIZE HOLES. REPAIR SECTION INSTALLED PER DC8 SRM 51-1-20D REV 78.
- [SDR IPXA09855270](https://openairdocs.org/sdr/IPXA09855270), Apr 1, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV LT WING UPPER EXT SURFACE SKIN XRS 139 BETWEEN FWD SPAR AND STR 515 REPAIR DOUBLER DOES NOT CORRELATE TO SRM REPAIR SURVEY SEQ 752-W3-16. REP
- [SDR IPXA09855269](https://openairdocs.org/sdr/IPXA09855269), Apr 1, 2009: STRUCTURE. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-W4-04, DOUBLER ATTACH FASTENER SPACING LESS THAN 4 FASTENERS DIAMETER AND ED LESS THAN 1.5 DIAMETER OF FASTENERS BETWEEN XFS 3
- [SDR IPXA09855395](https://openairdocs.org/sdr/IPXA09855395), Mar 31, 2009: STRUCTURE. MISREPAIRED. INSPECTION TYPE:SVC PREVIOUS FLUSH REPAIR AT STA -16.5 TO -8.75 L31R HAS 4EA ATTACHED FASTENER ED LESS THAN 1.5D AT FWD AND AFT EDGES. REMOVED EXISTING REPAIR D
- [SDR IPXA09855394](https://openairdocs.org/sdr/IPXA09855394), Mar 31, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SVC EXISTING FLUSH REPAIR AT STA -95.5 TO STA 3.5 L21R TO L24R DOES NOT CO CONFORM TO SRM REQUIREMENTS. REMOVED EXISTING SKIN SPLICE. FABRICATED
- [SDR IPXA09855182](https://openairdocs.org/sdr/IPXA09855182), Mar 27, 2009: SKIN. CRACKED. INSPECTION TYPE:SV SURVEY SEQ 752-W4-05 REPAIR RT WING LEADING LOWER SURFACE AT STA XFS 310 HAS FASTENER SPACING LESS THAN 4D & TRACK EXTENDS THROUGH PREVIOUS S
- [SDR IPXA09855181](https://openairdocs.org/sdr/IPXA09855181), Mar 27, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV SEQ SURVEY 752-W3-11 REPAIR ON LT WING O/B LEADING EDGE LOWER EXTERIOR SURFACE, XFS 618 FAILS APPX H. REPAIRED PER TIMCO REO-G12589 AND UPS E
- [SDR IPXA09855180](https://openairdocs.org/sdr/IPXA09855180), Mar 27, 2009: STRUCTURE. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-F1-74, FUSELAGE REPAIR AT STA 1727 TO 1740, L28L TO L30. DOES NOT CORRELATE TO A SRM REPAIR. REPAIRED PER TIMCO REO-G12623 AND
- [SDR IPXA09855179](https://openairdocs.org/sdr/IPXA09855179), Mar 27, 2009: STRUCTURE. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQUENCE 752-F1-75, FUSELAGE REPAIR AT STA 1727 TO 1740.5, L28R TO L30R. DOES NOT CORRELATE TO AN SRM REPAIR. REPAIRED PER REO-G12623 
- [SDR IPXA09855174](https://openairdocs.org/sdr/IPXA09855174), Mar 26, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV SURVEY SEQ 752-W4-18 RT WING L/E UPPER REPAIR AT STA XFS 556. DOUBLER SKIN THICKNESS LESS THAN SRM CALLOUT. REPAIRED PER 57-02-01-0 FIG 38 SH
- [SDR IPXA09855172](https://openairdocs.org/sdr/IPXA09855172), Mar 26, 2009: SKIN. MISREPAIRED. INSPECTION TYPE:SV SS 752-W2-03 RT WING LOWER SURFACE DOUBLER AT XW 238.000 DOES NOT MEET THE CRITERIA OF ANY SRM REPAIR. REPAIRED PER DWG 5895686-3.

All 362: https://openairdocs.org/deregistered/N752UP-2014-09-18/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 19870306015429I](https://openairdocs.org/incident/19870306015429I), Mar 6, 1987: Doug DC871F (N752UP), Louisville, KY. Deflection of rudder on liftoff. Returned with yaw damper off. Replaced rudder power control unit, shut off valve.

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