# N772CA: 1988 Mcdonnell Douglas DC-8-62, registration cancelled 2013-08-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 8, 2013
- Status when cancelled: Sale reported, canceled
- Airframe: [Mcdonnell Douglas DC-8-62](https://openairdocs.org/model/mcdonnell-douglas-dc-8-62) (registry code 302197B)
- Engine: [Pratt & Whitney JT3D series](https://openairdocs.org/engine/pratt-whitney-jt3d-series) (registry code 52035)
- Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs)
- Serial number: 46131
- Year built: 1988
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 1, 1988
- Last registry action: April 28, 1998
- Mode S code: AA70A8
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Individual
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N772CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=772CA
- Page: https://openairdocs.org/deregistered/N772CA-2013-08-08

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 Mcdonnell Douglas DC-8-62: https://openairdocs.org/model/mcdonnell-douglas-dc-8-62.md

## Service difficulty reports (78, newest 50)

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

- [SDR 96ZZZX3649](https://openairdocs.org/sdr/96ZZZX3649), Jul 4, 1996: SEAL. DEFECTIVE. ON RIA FLT 1712 (CDG/MIA) - DURING CRUISE AT APPROXIMATELY 1830Z, NR 4 ENGINE WAS SHUT DOWN DUE TO OIL PRESSURE LIGHT ON, ENGINE OIL PRESSURE FLUCTUATING AND DE
- [SDR 95ZZZZ221](https://openairdocs.org/sdr/95ZZZZ221), Mar 28, 1995: AILERON. CORRODED. LEVEL 2 CORROSION, LT WING I/B AILERON O/B TAB HAS BULGING CORROSION AT FASTENERS AT I/B END LOWER SURFACE. REMOVED CORROSION AND TREATED AREA FABRICATED AND IN
- [SDR 95ZZZZ220](https://openairdocs.org/sdr/95ZZZZ220), Mar 28, 1995: SKIN. CORRODED. LEVEL 2 CORROSION, RT WING O/B AILERON LOWER SURFACE SKIN AT I/B END HAS CORROSION BULGING AROUND RIVETS. REMOVED CORROSION, TREATED AREA FABRICATED AND INSTALL
- [SDR 95ZZZW571](https://openairdocs.org/sdr/95ZZZW571), Mar 3, 1995: SUPPORT. CORRODED. LEVEL 2 CORROSION, AFT CABIN FLOOR SUPPORT IS CORRODED BETWEEN BS 1574L AND BS 1540L 7 INCHES LBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53
- [SDR 95ZZZW570](https://openairdocs.org/sdr/95ZZZW570), Mar 3, 1995: LONGERON. CORRODED. LEVEL 2 CORROSION, LONGERON 30 LEFT IS CORRODED BETWEEN BS 1606 AND BS 1585. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W)
- [SDR 95ZZZW569](https://openairdocs.org/sdr/95ZZZW569), Mar 3, 1995: SKIN. CORRODED. LEVEL 2 CORROSION, CORROSION BULGING OUT THROUGH FUSELAGE SKIN SURFACE AT AFT RIGHT SIDE OF FUSELAGE BS 1557R BETWEEN LONGERON 28R AND 26R. REMOVED CORROSION FA
- [SDR 95ZZZW568](https://openairdocs.org/sdr/95ZZZW568), Mar 3, 1995: SUPPORT. CORRODED. LEVEL 2 CORROSION, AFT CABIN FLOOR SUPPORT IS CORRODED BETWEEN BS 1574L AND BS 1540L 12 INCHES LBL. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53
- [SDR 95ZZZW535](https://openairdocs.org/sdr/95ZZZW535), Mar 3, 1995: SKIN. CORRODED. LEVEL 2 CORROSION, LEFT HORIZONTAL STABILIZER LOWER SURFACE SKI AT REAR SPAR CAP HAS BULGING CORROSION AROUND RIVETS FROM INBOARD END TO TIP. REMOVED CORROSION 
- [SDR 95ZZZW534](https://openairdocs.org/sdr/95ZZZW534), Mar 3, 1995: WINDOW FRAME. CORRODED. LEVEL 2 CORROSION, WINDOW NR 23R HAS CORROSION INSIDE FRAME. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER RICH EO 9402289.
- [SDR 95ZZZW533](https://openairdocs.org/sdr/95ZZZW533), Mar 3, 1995: SKIN. CORRODED. LEVEL 2 CORROSION, RT HORIZONTAL STAB UPPER SURFACE SKIN AT REAR SPAR CAP HAS BULGING CORROSION AROUND RIVETS FROM INBOARD END TO TIP. REMOVED CORROSION FABRICA
- [SDR 95ZZZW532](https://openairdocs.org/sdr/95ZZZW532), Mar 3, 1995: SKIN. CORRODED. LEVEL 2 CORROSION, FUSELAGE RT SIDE EXTERIOR SKIN FRAMES 670 TO FS 685 HAS SKIN CRACK AND BULGING AROUND FASTENER HEADS LGRN 21R. REMOVED CORROSION FABRICATED A
- [SDR 95ZZZW531](https://openairdocs.org/sdr/95ZZZW531), Mar 3, 1995: SKIN. CORRODED. LEVEL 2 CORROSION, RT HORIZONTAL STABILIZER LOWER SURFACE SKIN AT REAR SPAR CAP HAS BULGING CORROSION AROUND RIVETS FROM INBOARD END TO TIP. REMOVED CORROSION F
- [SDR 95ZZZW530](https://openairdocs.org/sdr/95ZZZW530), Mar 3, 1995: SPAR CAP. CORRODED. LEVEL 2 CORROSION RT WING LEADING EDGE UPPER AT FRONT SPAR CAP ATTACH FLANGE HAS CORROSION AROUND SCREW HEADS OUTBOARD OF NR 4 PYLON FROM APPROXIMATELY XFS 503 
- [SDR 95ZZZW548](https://openairdocs.org/sdr/95ZZZW548), Mar 2, 1995: SKIN. CORRODED. LEVEL 2 CORROSION, AFT CABIN FUSELAGE SKIN IS CORRODED BETWEEN BS 1586L AND 1574, LONGERON 26L AND LONGERON 24L. REMOVED CORROSION, FABRICATED AND INSTALLED REP
- [SDR 95ZZZW567](https://openairdocs.org/sdr/95ZZZW567), Mar 1, 1995: LONGERON. CORRODED. LEVEL 2 CORROSION, AFT FUSELAGE LONGERON 24R BETWEEN FS 1500 AND 1480 HAS SURFACE CORROSION AND BULGES. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER S
- [SDR 95ZZZW566](https://openairdocs.org/sdr/95ZZZW566), Mar 1, 1995: SKIN. CORRODED. LEVEL 2 CORROSION, FUSELAGE LOWER LOBE SKIN IS CORRODED AT CENTER PRESSURE BULKHEAD VERTICAL SUPPORT 4 INCHES LBL BETWEEN BS 1606 AND 1585. REMOVED CORROSION FA
- [SDR 95ZZZW565](https://openairdocs.org/sdr/95ZZZW565), Mar 1, 1995: WINDOW FRAME. CORRODED. LEVEL 2 CORROSION, AFT FUSELAGE MAIN CABIN WINDOW FRAME FOR WINDOW 19R HAS CORROSION ON INSIDE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR IAW RICH DRAW
- [SDR 95ZZZW547](https://openairdocs.org/sdr/95ZZZW547), Mar 1, 1995: SKIN. CORRODED. LEVEL 2 CORROSION, AFT MAIN CABIN LOWER FUSELAGE SKIN IS CORRODED FROM BS 1530 TO BS 1606 LONGERON 35L TO 35R. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR
- [SDR 95ZZZW546](https://openairdocs.org/sdr/95ZZZW546), Mar 1, 1995: SLOT DOOR. CORRODED. LEVEL 2 CORROSION, LEFT WING NR 1 SLOT DOOR HAS DOUBLER REPAIR THAT IS SURROUNDED BY CORROSION. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER DOUGLAS FI
- [SDR 95ZZZW545](https://openairdocs.org/sdr/95ZZZW545), Mar 1, 1995: FLANGE. CORRODED. LEVEL 2 CORROSION, LEFT AUXILLARY TANK UPPER ATTACH FLANGE HAS INTERGRANULAR CORROSION. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1.
- [SDR 95ZZZW544](https://openairdocs.org/sdr/95ZZZW544), Mar 1, 1995: SUPPORT. CORRODED. LEVEL 2 CORROSION, AFT CABIN TRIANGLE FLOOR WEB SUPPORT IS CORRODED AT BS 1574 CENTER, CENTER LINE 12 INCHES LBL 12 INCHES RBL. REMOVED AND REPLACED TRIANGLE FL
- [SDR 95ZZZW543](https://openairdocs.org/sdr/95ZZZW543), Mar 1, 1995: FRAME. CORRODED. LEVEL 2 CORROSION, AFT CABIN CIRCUMFERENTIAL FRAME IS CORRODED AT BS 1574L FROM LONGERON 24 TO 26L. REMOVED CORROSION AND REPLACED FRAME SECTION PER SRM 53-1-0.
- [SDR 95ZZZW542](https://openairdocs.org/sdr/95ZZZW542), Mar 1, 1995: FLOOR BEAM. CORRODED. LEVEL 2 CORROSION, AFT CABIN FLOOR BEAM CAP AT BS 1540 IS CORRODED FROM 45 INCHES LBL TO 45 INCHES. REMOVED AND REPLACED FLOOR BEAM CAP PER SRM 53-1-0.
- [SDR 95ZZZW539](https://openairdocs.org/sdr/95ZZZW539), Feb 24, 1995: FLOOR BEAM. CORRODED. LEVEL 2 CORROSION, ENTIRE FLOOR BEAM CAP AT BS 1586 IS CORRODED FROM LEFT TO RIGHT SIDE OF CABIN. CLEANED CORROSION, FABRICATED, AND INSTALLED NEW FLOOR BEAM PE
- [SDR 95ZZZW538](https://openairdocs.org/sdr/95ZZZW538), Feb 24, 1995: FITTING. CORRODED. LEVEL 2 CORROSION, LONGERON 32 RIGHT END BATHTUB FITTING IS CORRODED AT PRESSURE BULKHEAD BS 1606R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 5
- [SDR 95ZZZW537](https://openairdocs.org/sdr/95ZZZW537), Feb 24, 1995: FITTING. CORRODED. LEVEL 2 CORROSION, AFT CARGO COMPARTMENT BATHTUB FITTING IS CORRODED AT BS 1530R, LONGERON 30R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-
- [SDR 95ZZZW536](https://openairdocs.org/sdr/95ZZZW536), Feb 24, 1995: SKIN. CORRODED. LEVEL 2 CORROSION, FUSELAGE SKIN CORRODED BETWEEN BS 1530 AND BS 1540 BETWEEN LONGERON 36 AND LONGERON 34 LEFT. REMOVED CORROSION, FABRICATED AND INSTALLED REPA
- [SDR 95ZZZZ153](https://openairdocs.org/sdr/95ZZZZ153), Feb 22, 1995: SUPPORT. CORRODED. LEVEL 2 CORROSION/AFT CABIN FLOOR PANEL SUPPORT IS CORRODED BETWEEN BS 1606 AND BS 1585, 9 INCHES LBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SR
- [SDR 95ZZZZ152](https://openairdocs.org/sdr/95ZZZZ152), Feb 22, 1995: LONGERON. CORRODED. LEVEL 2 CORROSION/LONGERON 26 LEFT END FITTING IS CORRODED AT BS 1530 LEFT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.
- [SDR 95ZZZZ151](https://openairdocs.org/sdr/95ZZZZ151), Feb 22, 1995: SUPPORT. CORRODED. LEVEL 2 CORROSION/AFT CABIN FLOOR SUPPORT IS CORRODED BETWEEN BS 1480L AND BS 1520L, 15 INCHES LBL. CLEANED CORROSION AND FABRICATED AND INSTALLED REPAIR PER SR
- [SDR 95ZZZZ150](https://openairdocs.org/sdr/95ZZZZ150), Feb 22, 1995: FITTING. CORRODED. LEVEL 2 CORROSION/LONGERON 30 RIGHT END FITTING IS CORRODED AT BS 1530 RIGHT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.
- [SDR 95ZZZZ149](https://openairdocs.org/sdr/95ZZZZ149), Feb 22, 1995: SUPPORT. CORRODED. LEVEL 2 CORROSION/AFT CABIN FLOOR PANEL SUPPORT IS CORRODED BETWEEN BS 1606 AND BS 1585, 22 INCHES RBL. REMOVED CORROSION AND FABRICATED AND INSTALLED REPAIR PE
- [SDR 95ZZZZ148](https://openairdocs.org/sdr/95ZZZZ148), Feb 22, 1995: SUPPORT. CORRODED. LEVEL 2 CORROSION/AFT CABIN SQUARE FLOOR SUPPORT FRAME IS CORRODED BETWEEN BS 1586 AND BS 1574. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-
- [SDR 95ZZZZ147](https://openairdocs.org/sdr/95ZZZZ147), Feb 22, 1995: WINDOW. CORRODED. LEVEL 2 CORROSION/MAIN CABIN WINDOW NR 18R HAS CORROSION ON INSIDE SURFACE OF FRAME. FABRICATED AND INSTALLED REPAIR PER RICH REPAIR SKETCH 5164-6.
- [SDR 95ZZZZ146](https://openairdocs.org/sdr/95ZZZZ146), Feb 22, 1995: WEB. CORRODED. LEVEL 2 CORROSION/AFT CARGO COMPARTMENT CIRCUMFERRENTIAL WEB CORRODED AT BS 1540 FROM 34L TO 34R. REMOVED CORROSION AND REPLACED SPLICE PLATE PER SRM 51-1-0.
- [SDR 95ZZZZ145](https://openairdocs.org/sdr/95ZZZZ145), Feb 22, 1995: FLOOR SUPPORT. CORRODED. LEVEL 2 CORROSION/AFT CARGO COMPARTMENT OVERHEAD FLOOR SUPPORT CORRODED BETWEEN BS 1460 AND BS 1500, 12 INCHES LBL. CLEANED CORROSION AND FABRICATED AND INSTALL
- [SDR 95ZZZZ144](https://openairdocs.org/sdr/95ZZZZ144), Feb 22, 1995: ANGLE. CORRODED. LEVEL 2 CORROSION/AFT CABIN FLOOR SUPPORT ANGLE AT BS 1520 IS CORRODED FROM 12 INCHES RBL TO 45 INCHES LBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR P
- [SDR 95ZZZW242](https://openairdocs.org/sdr/95ZZZW242), Feb 22, 1995: FRAME. CORRODED. LEVEL 2 CORROSION, CIRCUMFERRENTIAL FRAME IS CORRODED AT BS 1574 BETWEEN LONGERON 24 RT AND 26 RT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53
- [SDR 95ZZZW241](https://openairdocs.org/sdr/95ZZZW241), Feb 22, 1995: FITTING. CORRODED. LEVEL 2 CORROSION, LONGERON 30 LT END BATHTUB FITTING IS CORRODED AT BS 1606L. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.
- [SDR 95ZZZW240](https://openairdocs.org/sdr/95ZZZW240), Feb 22, 1995: FRAME. CORRODED. LEVEL 2 CORROSION, AFT CABIN LOWER CIRCUMFERRENTIAL FRAME 'J' FLANGES ARE CORRODED, UPPER AND LOWER AT BS 1586 FROM LONGERON 24L TO 24R. REMOVED CORROSION, FABR
- [SDR 95ZZZW239](https://openairdocs.org/sdr/95ZZZW239), Feb 22, 1995: FLOORBEAM. CORRODED. LEVEL 2 CORROSION, AFT CABIN FLOORBEAM CAP AT BS 1574 IS CORRODED FROM 36 INCHES LBL TO 36 INCHES RBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SR
- [SDR 95ZZZW238](https://openairdocs.org/sdr/95ZZZW238), Feb 22, 1995: LONGERON. CORRODED. LEVEL 2 CORROSION, LONGERON 36 IS CORRODED AT BS 1550. REMOVED CORROSION, FABRICATED AND INSTALLED REPAI ER SRM 53-2-2.
- [SDR 95ZZZW237](https://openairdocs.org/sdr/95ZZZW237), Feb 22, 1995: LONGERON. CORRODED. LEVEL 2 CORROSION, LONGERON 36 IS CORRODED 6 INCHES FWD AND AFT OF BS 1574. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2.
- [SDR 95ZZZW236](https://openairdocs.org/sdr/95ZZZW236), Feb 22, 1995: LONGERON. CORRODED. LEVEL 2 CORROSION, LONGERON 36 IS CORRODED BETWEEN BS 1606 AND BS 1585. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2.
- [SDR 95ZZZW235](https://openairdocs.org/sdr/95ZZZW235), Feb 22, 1995: LONGERON. CORRODED. LEVEL 2 CORROSION, LONGERON 32 RT IS CORRODED BETWEEN BS 1606 AND 1585. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2.
- [SDR 95ZZZW234](https://openairdocs.org/sdr/95ZZZW234), Feb 22, 1995: FLOORBEAM. CORRODED. LEVEL 2 CORROSION, AFT CABIN FLOORBEAM CAP IS CORRODED AT BS 1440 FROM 45 INCHES LBL TO 45 INCHES RBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SR
- [SDR 95ZZZW233](https://openairdocs.org/sdr/95ZZZW233), Feb 22, 1995: FITTING. CORRODED. LEVEL 2 CORROSION, LONGERON 30 RT END BATHTUB FITTING IS CORRODED AT PRESSURE BULKHEAD BS 1606R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1
- [SDR 95ZZZW253](https://openairdocs.org/sdr/95ZZZW253), Feb 10, 1995: SEAT TRACK. CORRODED. LEVEL 2 CORROSION, SEAT TRACK CORRODED FROM BS 150 RT TO BS 1540 RT, 39 INCHES RBL. REMOVED DAMAGED TRACK, FABRICATED REPAIR, CLEANED AREA, TREATED, PRIMED AND 
- [SDR 95ZZZW252](https://openairdocs.org/sdr/95ZZZW252), Feb 10, 1995: SEAT TRACK. CORRODED. LEVEL 2 CORROSION, SEAT TRACK CORRODED FROM BS 1500 RT TO BS 1540 RT 25 INCHES RBL. REMOVED DAMAGED TRACK, FABRICATED REPAIR, CLEANED AREA TREATED, PRIMED AND I
- [SDR 95ZZZW251](https://openairdocs.org/sdr/95ZZZW251), Feb 10, 1995: SKIN. CORRODED. LEVEL 2 CORROSION, FUSELAGE RT EXTERIOR SKIN AT WINDOW NR 14R HAS CORROSION AROUND FASTENERS. REMOVED WINDOW, REMOVED CORROSION, FABRICATED REPAIR, TREATED, PRI

All 78: https://openairdocs.org/deregistered/N772CA-2013-08-08/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 19960613029389I](https://openairdocs.org/incident/19960613029389I), Jun 13, 1996: Doug DC862 (N772CA), Philadelphia, PA, Minor damage. Narrative: during a maintenance nighttime taxi operation the aircraft's left wing tip and closure rib was damaged after striking the right wing tip of a world…

## Other aircraft with N772CA

- [Registered now](https://openairdocs.org/aircraft/N772CA): Piper PA-28-181, S/N 2881740, built 2024

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