# N133HP: 1989 Lockheed C-130A, registration cancelled 2018-03-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 9, 2018
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Lockheed C-130A](https://openairdocs.org/model/lockheed-c-130a) (registry code 5262502)
- Engine: [Allison T-56-A-7 series](https://openairdocs.org/engine/allison-t-56-a-7-series) (registry code 03009)
- Serial number: 57-0482
- Year built: 1989
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Restricted, agriculture and pest control, forest, carriage of cargo
- Airworthiness date: May 10, 1993
- Certificate issued: March 7, 2007
- Last registry action: June 20, 2013
- Mode S code: A08713
- Owner when cancelled: [International Air Response Inc](https://openairdocs.org/faa-owner/INTERNATIONAL%20AIR%20RESPONSE%20INC)
- Location: [Mesa, AZ](https://openairdocs.org/faa-place/AZ/Mesa)
- Owner type: Corporation
- Owner's area on the map: 33.3207° N, 111.6313° W: Placed by OpenAirDocs at the center of ZIP code 85212, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N133HP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=133HP
- Page: https://openairdocs.org/deregistered/N133HP-2018-03-09

From the FAA registry file of November 12, 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 Lockheed C-130A: https://openairdocs.org/model/lockheed-c-130a.md

## Service difficulty reports (2)

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

- [SDR 16138C](https://openairdocs.org/sdr/16138C), Sep 18, 2002: SKIN. CRACKED. LOWER CENTER WING SKIN CRACKED AT FASTINER HOLES.
- [SDR 2002FA0000995](https://openairdocs.org/sdr/2002FA0000995), Jun 27, 2002: SPAR. CRACKED. FRONT WING SPAR WEB WAS CRACKED IN THE SAME LOCATION ON BOTH WINGS JUST ABOVE THE LOWER SPAR CHORD AT THE LANDING GEAR BEAM

---
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, except the copies of manufacturers’ service documents, which belong to their rights holders.