# N880DP: Mcdonnell Douglas DC-9-83(MD-83), registration cancelled 2023-07-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 1, 2023
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas DC-9-83(MD-83)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83) (registry code 3022083)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 49504
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: September 29, 1999
- Certificate issued: May 5, 2021
- Last registry action: May 12, 2023
- Mode S code: AC1E2E
- Owner when cancelled: [Roundball LLC](https://openairdocs.org/faa-owner/ROUNDBALL%20LLC)
- Location: [Waterford, MI](https://openairdocs.org/faa-place/MI/Waterford)
- Owner type: LLC
- Owner's area on the map: 42.6383° N, 83.4107° W: Placed by OpenAirDocs at the center of ZIP code 48327, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N880DP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=880DP
- Page: https://openairdocs.org/deregistered/N880DP-2023-07-01

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-9-83(MD-83): https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83.md

## Service difficulty reports (10)

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

- [SDR DU4R2013004](https://openairdocs.org/sdr/DU4R2013004), Jul 31, 2013: ANGLE. DAMAGED. DURING SCHEDULED INSPECTION, FOUND ELONGATED HOLE IN LOWER RT WING ANGLE FITTING AT XRS 69 BETWEEN S15-16R.
- [SDR DU4R20130724003](https://openairdocs.org/sdr/DU4R20130724003), Jul 24, 2013: CUSP WEB. CRACKED. DURING SCHEDULED INSPECTION, FOUND AFT CABIN BS 1338, LT CUSP WEB LIGHTNING HOLE CRACKED AT TWO AREAS.
- [SDR DU4R20130722002](https://openairdocs.org/sdr/DU4R20130722002), Jul 22, 2013: FLOOR SUPPORT. CRACKED. DURING SCHEDULED INSPECTION, FOUND UPPER FLANGE OF CABIN FLOOR SUPPORT CRACKED AT BS 796 BL 0.
- [SDR DU4R20130711001](https://openairdocs.org/sdr/DU4R20130711001), Jul 11, 2013: STRUCTURE. LOOSE. DURING SCHEDULED INSPECTION, FOUND RT WING TIP (LOWER SIDE, AFT, INBD) HAS LOOSE/SMOKING RIVETS.
- [SDR DU4R20120702001](https://openairdocs.org/sdr/DU4R20120702001), Jul 2, 2012: FRAME. CRACKED. DURING SCHEDULED INSPECTION, FOUND RT OVERWING FRAMES STA 886.0 FOUND CRACK APPROX .300 IN LENGTH. CRACK TIP OUTSIDE SHADOW OF FASTENER HOLE, CRACK FALLS UNDER 
- [SDR ABXA040261](https://openairdocs.org/sdr/ABXA040261), Jun 28, 2004: SUPPORT. CRACKED. LEFT SLAT DRIVE LOWER INBOARD BOLT ATTACHMENT SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1.
- [SDR ABXA040260](https://openairdocs.org/sdr/ABXA040260), Jun 28, 2004: FRAME. CRACKED. INTERCOSTAL FRAME CRACKED IN RADIUS FORWARD END OF FORWARD PASSENGER DOOR VIEWED FROM SECOND LIGHTENING HOLE FROM TOP. REPAIRED INTERCOSTAL IAW DC-9 SRM 52-05. 
- [SDR ABXA040258](https://openairdocs.org/sdr/ABXA040258), Jun 28, 2004: DOOR FRAME. CRACKED. INTERCOSTAL FRAME, INTERIOR OF FORWARD PASSENGER DOOR CRACKED IN RADIUS AFT END VIEWED FROM SECOND LIGHTENING HOLE FROM TOP. REMOVED FITTING AND STOP FOR REPLAC
- [SDR ABXA040259](https://openairdocs.org/sdr/ABXA040259), Jun 28, 2004: FRAME. CRACKED. INTERCOSTAL FRAME, INTERIOR OF FORWARD PASSENGER DOOR CRACKED IN RADIUS AFT END VIEWED FROM THIRD LIGHTENING HOLE FROM TOP. STOP DRILLED CRACK AND REPAIRED PASS
- [SDR ABXA040257](https://openairdocs.org/sdr/ABXA040257), Jun 26, 2004: ATTACH ANGLE. CRACKED. PYLON LEADING EDGE LOWER ATTACH ANGLE ON FUSELAGE CRACKED. INSTALLED NEW ANGLE IAW DC-9 SRM 51-30-2.

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