# N563PC: 1967 Douglas DC-9-15F, registration cancelled 2017-10-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 16, 2017
- Exported to: Mexico
- Status when cancelled: Valid registration
- Airframe: [Douglas DC-9-15F](https://openairdocs.org/model/douglas-dc-9-15f) (registry code 3022037)
- Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 47055
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: November 22, 1967
- Certificate issued: February 28, 2017
- Last registry action: February 28, 2017
- Mode S code: A73357
- Owner when cancelled: [Frontera Flight Holdings Inc](https://openairdocs.org/faa-owner/FRONTERA%20FLIGHT%20HOLDINGS%20INC)
- Location: [Dover, DE](https://openairdocs.org/faa-place/DE/Dover)
- Owner type: Corporation
- Owner's area on the map: 39.1815° N, 75.4736° W: Placed by OpenAirDocs at the center of ZIP code 19901, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N563PC
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=563PC
- Page: https://openairdocs.org/deregistered/N563PC-2017-10-16

From the FAA registry file of October 28, 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-9-15F: https://openairdocs.org/model/douglas-dc-9-15f.md

## Service difficulty reports (96, newest 50)

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

- [SDR EE4Y100356](https://openairdocs.org/sdr/EE4Y100356), Aug 19, 2010: FLOOR SUPPORT. CORRODED. DURING INSP UPPER FUSELAGE PAX CABIN AT STA Y503 AND STA Y525, +X33 FLOOR CHANNEL WITH CORROSION.
- [SDR EE4Y100355](https://openairdocs.org/sdr/EE4Y100355), Aug 19, 2010: EXHAUST DUCT. CORRODED. DURING INSP ENGINE NR2 EXHAUST DUCT WITH SPOT CORROSION AT L/E SKIN.
- [SDR EE4Y100354](https://openairdocs.org/sdr/EE4Y100354), Aug 19, 2010: SKIN. DENTED. DURING INSP EXTERNAL FUSELAGE SKIN WITH DENT AT BS 436.5 BTWN LONG 19L AND LONG 20L.
- [SDR EE4Y100353](https://openairdocs.org/sdr/EE4Y100353), Aug 19, 2010: SPAR. CRACKED. DURING INSP EMPENNAGE HORIZ STABILIZER BTWN XFS 221 AND XFS 235 RT ELEVATOR FRONT SPAR WITH CRACKS.
- [SDR EE4Y100352](https://openairdocs.org/sdr/EE4Y100352), Aug 19, 2010: CHANNEL. CORRODED. DURING INSP LOWER FUSELAGE UNDER WING TO FILLET FAIRING CHANNEL WITH CORROSION FROM STA Y523 TO STA Y547 BTWN LONG 28L AND LONG 29L.
- [SDR EE4Y100317](https://openairdocs.org/sdr/EE4Y100317), Aug 9, 2010: SPAR CAP. CRACKED. LEFT WING FRONT SPAR STA XCW 58.5 UPPER CAP WITH CRACK.
- [SDR EE4Y100316](https://openairdocs.org/sdr/EE4Y100316), Aug 9, 2010: SUPPORT CHANNEL. CORRODED. UPPER FUSELAGE CARGO CABIN AT STA Y680, +X33, Z0 SUPPORT CHANNEL WITH CORROSION.
- [SDR EE4Y100315](https://openairdocs.org/sdr/EE4Y100315), Aug 9, 2010: CHANNEL. CRACKED. UPPER FUSELAGE PAX CABIN AT Y623 +X50 FLOOR CHANNEL WITH CRACK.
- [SDR EE4Y100314](https://openairdocs.org/sdr/EE4Y100314), Aug 9, 2010: PANEL. DELAMINATED. RIGHT WING T/E UPPER FIXED PANEL P/N 5912735-2 DELAMINATED.
- [SDR EE4Y100313](https://openairdocs.org/sdr/EE4Y100313), Aug 9, 2010: SPOILER. DELAMINATED. LEFT WING OUTBOARDD FLIGHT SPOILER P/N 5910055-513, S/N 13033 DELAMINATED.
- [SDR EE4Y100312](https://openairdocs.org/sdr/EE4Y100312), Aug 9, 2010: PANEL. DELAMINATED. RIGHT WING T/E UPPER FIXED PANEL P/N 5912737-2 DELAMINATED.
- [SDR EE4Y100311](https://openairdocs.org/sdr/EE4Y100311), Aug 9, 2010: FLOORBEAM. CORRODED. UPPER FUSELAGE PAX CABIN STA Y786, +X50, -Z4 FLOORBEAM WEB WITH CORROSION.
- [SDR EE4Y100310](https://openairdocs.org/sdr/EE4Y100310), Aug 9, 2010: FITTING. CRACKED. UPPER FUSELAGE PAX CABIN AT STA Y503 +X22, -Z2 FITTING CRACKED.
- [SDR EE4Y100308](https://openairdocs.org/sdr/EE4Y100308), Aug 9, 2010: SKIN. CRACKED. AFT UNPRESSURE FUSELAGE STA Y964 ON LEVEL LONG 19L SKIN WITH CRACK.
- [SDR EE4Y100307](https://openairdocs.org/sdr/EE4Y100307), Aug 9, 2010: FRAME. CRACKED. TAIL COMPARTMENT AT STA Y964.019 CANT FRAME WITH CRACK AT STAIRWAY ACTUATOR SUPPORT FITTING AREA.
- [SDR EE4Y100306](https://openairdocs.org/sdr/EE4Y100306), Aug 9, 2010: SKIN. DENTED. UPPER FUSELAGE EXTERIOR FUSELAGE SKIN WITH DENT AT STA Y933 BETWEEN LONG 6L AND LONG 7L.
- [SDR EE4Y100305](https://openairdocs.org/sdr/EE4Y100305), Aug 9, 2010: FRAME. CRACKED. TAIL COMPARTMENT AT STA Y925.937 CANT, LONG 16L FRAME WITH CRACK.
- [SDR EE4Y100304](https://openairdocs.org/sdr/EE4Y100304), Aug 9, 2010: SKIN. CRACKED. AFT UNPRESSURE FUSELAGE STA Y988 CANT AT +X28 AND Z23 SKIN WITH CRACK.
- [SDR EE4Y100303](https://openairdocs.org/sdr/EE4Y100303), Aug 9, 2010: SKIN. DENTED. EXTERNAL FUSELAGE SKIN WITH DENT AT BS 436.5 BETWEEN LONG 19L AND LONG 20L.
- [SDR EE4Y100302](https://openairdocs.org/sdr/EE4Y100302), Aug 9, 2010: SKIN. BULGED. LOWER FUSELAGE SKIN WITH BULGED AT STA Y490.540 BETWEEN LONG 29L AND LONG 29R.
- [SDR EE4Y100301](https://openairdocs.org/sdr/EE4Y100301), Aug 9, 2010: FLOORBEAM. CORRODED. UPPER FUSELAGE PAX CABIN STA Y786 +X50, -Z4 FLOORBEAM WEB WITH CORROSION.
- [SDR EE4Y100300A](https://openairdocs.org/sdr/EE4Y100300A), Aug 9, 2010: CHANNEL. CORRODED. UPPER FUSELAGE CARGO CABIN AT STA Y680, +X33, Z0 SUPPORT CHANNEL WITH CORROSION.
- [SDR EE4Y100299](https://openairdocs.org/sdr/EE4Y100299), Aug 9, 2010: LONGERON. CRACKED. UPPER FUSELAGE CARGO CABIN STA Y786 LONG 12 LT CRACKED.
- [SDR EE4Y100298](https://openairdocs.org/sdr/EE4Y100298), Aug 9, 2010: LONGERON. CRACKED. UPPER FUSELAGE CARGO CABIN STA Y786 LONGERON 12 RT CRACKED.
- [SDR EE4Y100297](https://openairdocs.org/sdr/EE4Y100297), Aug 9, 2010: FRAME. DAMAGED. UPPER FUSELAGE CARGO CABIN STA Y718 BETWEEN LONG 17 LT AND LONG 18 LT FRAME WITH DOUBLE HOLE.
- [SDR EE4Y100296](https://openairdocs.org/sdr/EE4Y100296), Aug 9, 2010: FRAME. CRACKED. UPPER FUSELAGE CARGO CABIN STA Y680 BETWEEN LONG 13R AND LONG 14R.
- [SDR EE4Y100295](https://openairdocs.org/sdr/EE4Y100295), Aug 9, 2010: SKIN. CORRODED. LOWER FUSELAGE SKIN CORRODED FROM STA Y643 TO STA Y718 BETWEEN LONG 18L AND LONG 29L.
- [SDR EE4Y100294](https://openairdocs.org/sdr/EE4Y100294), Aug 9, 2010: LONGERON. CRACKED. LOWER FUSELAGE STA Y465 LONG 21 LT CRACKED.
- [SDR EE4Y100293](https://openairdocs.org/sdr/EE4Y100293), Aug 9, 2010: FRAME. DAMAGED. MAIN CARGO CABIN AT STA Y465 LONGERON 15 RT FRAME WITH DOUBLE HOLE.
- [SDR EE4Y100292](https://openairdocs.org/sdr/EE4Y100292), Aug 9, 2010: FRAME. DAMAGED. MAIN CARGO CABIN AT STA Y446 BETWEEN LONG 9 RT AND LONG 11 RT FRAME WITH DOUBLE HOLES.
- [SDR EE4Y100291](https://openairdocs.org/sdr/EE4Y100291), Aug 9, 2010: FRAME. DAMAGED. MAIN CARGO CABIN AT STA Y427 LONGERON 15 RT FRAME WITH DOUBLE HOLE.
- [SDR EE4Y100290](https://openairdocs.org/sdr/EE4Y100290), Aug 9, 2010: FRAME. DAMAGED. MAIN CARGO CABIN AT STA Y408, LONGERON 15 RT FRAME WITH DOUBLE HOLE.
- [SDR EE4Y100289](https://openairdocs.org/sdr/EE4Y100289), Aug 9, 2010: FRAME. DAMAGED. MAIN CARGO CABIN AT STA Y389, LONGERON 15 RT WITH DOUBLE HOLE.
- [SDR EE4Y100288](https://openairdocs.org/sdr/EE4Y100288), Aug 9, 2010: FRAME. DAMAGED. MAIN CARGO CABIN AT STA Y370, LONGERON 15 RT FRAME WITH DOUBLE HOLE.
- [SDR EE4Y100287](https://openairdocs.org/sdr/EE4Y100287), Aug 9, 2010: FRAME. DAMAGED. MAIN CARGO CABIN AT STA Y370, LONGERON 15 RT FRAME WITH DOUBLE HOLE.
- [SDR EE4Y100286](https://openairdocs.org/sdr/EE4Y100286), Aug 9, 2010: FRAME. DAMAGED. MAIN CARGO CABIN AT STA Y332 BETWEEN LONG 10 RT AND LONG 11 RT FRAME WITH DOUBLE HOLES.
- [SDR EE4Y100285](https://openairdocs.org/sdr/EE4Y100285), Aug 9, 2010: FRAME. DAMAGED. MAIN CARGO CABIN AT STA Y313 BETWEEN LONG 10R AND LONG 11R FRAME WITH DOUBLE HOLES.
- [SDR EE4Y100284](https://openairdocs.org/sdr/EE4Y100284), Aug 9, 2010: FRAME. DAMAGED. MAIN CARGO CABIN AT STA Y294, LONGERON 15 RT FRAME AND STRAP WITH DOUBLE HOLES.
- [SDR EE4Y100283](https://openairdocs.org/sdr/EE4Y100283), Aug 9, 2010: FRAME. WORN. MAIN CARGO CABIN AT STA Y275 BETWEEN LONG 14R AND LONG 15R AND LONG 17R AND LONG 18R FRAME WORN.
- [SDR EE4Y100282](https://openairdocs.org/sdr/EE4Y100282), Aug 9, 2010: FRAME. DAMAGED. MAIN CARGO CABIN AT STA Y275 LONG 15 LT FRAME WITH ELONGATED HOLE.
- [SDR EE4Y100281](https://openairdocs.org/sdr/EE4Y100281), Aug 9, 2010: FRAME. DAMAGED. MAIN CARGO CABIN AT STA Y237 LONGERON 11 RT FRAME WITH DOUBLE HOLES.
- [SDR EE4Y100280](https://openairdocs.org/sdr/EE4Y100280), Aug 9, 2010: FRAME. DAMAGED. MAIN CARGO AT STA Y206 BETWEEN LONG 16R AND LONG 17 RT FRAME RADIUS WITH HOLE.
- [SDR EE4Y100279](https://openairdocs.org/sdr/EE4Y100279), Aug 9, 2010: MEMBRANE. CORRODED. MAIN CARGO CABIN FROM STA Y200 TO STA Y218, -X48, Z0 FLOOR MEMBRANE WITH CORROSION.
- [SDR EE4Y100278](https://openairdocs.org/sdr/EE4Y100278), Aug 9, 2010: LONGERON. CRACKED. CARGO CABIN AT STA Y160, LONG 4L WITH CRACK.
- [SDR EE4Y100277](https://openairdocs.org/sdr/EE4Y100277), Aug 9, 2010: LONGERON. CRACKED. UPPER FUSELAGE PAX CABIN AT STA 160 LONGERON 3L RADIUS WITH CRACK.
- [SDR ABXR070251](https://openairdocs.org/sdr/ABXR070251), Jul 16, 2007: GUSSET. CRACKED. PASSENGER AFT ENTRANCE DOOR AFT PRESSURE BULKHEAD CUTOUT LOWER LEFT CORNER LEAKED AND SHOWED EVIDENCE OF A CRACK IN THE DOUBLERS. REPAIRED LOWER AFT PRESSURE BU
- [SDR GAIA00422B](https://openairdocs.org/sdr/GAIA00422B), Aug 8, 2000: DOUBLER. CRACKED. DURING INSPECTION PER SB 56-11 A CRACK WAS FOUND IN UPPER AFT CORNER OF THE LEFT COCKPIT SLIDING WINDOW FRAME INTERNAL DOUBLER. THE AIRCRAFT WAS FERRIED FROM FW
- [SDR GAIA00492](https://openairdocs.org/sdr/GAIA00492), Jul 31, 2000: DOUBLER. CRACKED. DURING INSPECTION PER SB 56-11 A CRACK WAS FOUND IN UPPER AFT CORNER OF THE LEFT COCKPIT SLIDING WINDOW FRAME INTERNAL DOUBLER. THE AIRCRAFT WAS FERRIED FROM FW
- [SDR GAIA99162](https://openairdocs.org/sdr/GAIA99162), Nov 5, 1999: INTERCOSTAL. CORRODED. DURING C-CHECK INSPECTION, FOUND CORROSION ON THE INTERCOSTAL FROM STA 710 TO STA 718 BETWEEN L29L TO L30. THE INTERCOSTAL WAS REPLACED IAW DC-9 SRM. THE AIRCRA
- [SDR GAIA99152](https://openairdocs.org/sdr/GAIA99152), Oct 7, 1999: CONNECTOR. DIRTY. FLT 563 - EWR-DFW - AFTER LANDING AT DFW ON ROLL OUT THE LEFT BRAKE WOULD NOT APPLY. THE BRAKE OPERATED NORMALLY WITH THE ANTI-SKID OFF. THE AIRCRAFT TAXIED TO 

All 96: https://openairdocs.org/deregistered/N563PC-2017-10-16/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 19951227044769I](https://openairdocs.org/incident/19951227044769I), Dec 27, 1995: Doug DC915F (N563PC), Rochester, NY. Narrative: on December 27, 1995, at 1355 EST, a Douglas DC-9-15F operated as kitty hawk aircargo flight 290 was on approach to the Rochester, NY airport. When…
- [Incident 19870508019899I](https://openairdocs.org/incident/19870508019899I), May 8, 1987: Doug DC915F (N563PC), Indianapolis, IN. Thrust reverser unlock light came on en route. Engine shutdown. Found control cables were out of adjustment.

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