# N1140W: Bell 47J-2A, registration cancelled 1977-07-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 6, 1977
- Status when cancelled: Valid registration
- Airframe: [Bell 47J-2A](https://openairdocs.org/model/bell-47j-2a) (registry code 1181106)
- Data sheets: [TCDS 2H1](https://openairdocs.org/tcds/2H1) (OpenAirDocs)
- Serial number: 3118
- Type of aircraft: Rotorcraft
- Certificate issued: June 15, 1967
- Mode S code: A03D7C
- Owner when cancelled: [Copter Inc](https://openairdocs.org/faa-owner/COPTER%20INC)
- Owner type: Corporation
- The mark today: https://openairdocs.org/aircraft/N1140W
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1140W
- Page: https://openairdocs.org/deregistered/N1140W-1977-07-06

From the FAA registry file of November 5, 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 Bell 47J-2A: https://openairdocs.org/model/bell-47j-2a.md

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB NYC75AN108](https://openairdocs.org/ntsb/NYC75AN108), May 20, 1975: Bell 47J-2A (N1140W), Philadelphia, PA, substantial damage
- [NTSB NYC68D0427](https://openairdocs.org/ntsb/NYC68D0427), Apr 3, 1968: Bell 47J-2A (N1140W), Concord Twp, PA, substantial damage

## 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.

- [Accident 19750520020229A](https://openairdocs.org/incident/19750520020229A), May 20, 1975: Bell 47J2A (N1140W), Philadelphia, PA, Substantial damage. Valve rocker shaft retaining plate not installed nr 6 cyl. Rocker arm shaft displaced.

---
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.