# N955AA: 1970 Beech 99A, registration cancelled 2012-12-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 4, 2012
- Exported to: Bahamas
- Status when cancelled: Valid registration
- Airframe: [Beech 99A](https://openairdocs.org/model/beech-99a) (registry code 1154003)
- Engine: [Pratt & Whitney PT6A series](https://openairdocs.org/engine/pratt-whitney-pt6a-series) (registry code 52032)
- Data sheets: [TCDS A14CE](https://openairdocs.org/tcds/A14CE) (OpenAirDocs)
- Serial number: U128
- Year built: 1970
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: April 16, 1998
- Certificate issued: February 17, 2012
- Last registry action: February 17, 2012
- Mode S code: AD473B
- Owner when cancelled: [Flamingo Air USA LLC](https://openairdocs.org/faa-owner/FLAMINGO%20AIR%20USA%20LLC)
- Location: [Riviera Beach, FL](https://openairdocs.org/faa-place/FL/Riviera%20Beach)
- Owner type: Corporation
- Owner's area on the map: 26.7811° N, 80.0632° W: Placed by OpenAirDocs at the center of ZIP code 33404, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N955AA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=955AA
- Page: https://openairdocs.org/deregistered/N955AA-2012-12-04

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 Beech 99A: https://openairdocs.org/model/beech-99a.md

## Service difficulty reports (8)

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

- [SDR TIMA20090003](https://openairdocs.org/sdr/TIMA20090003), May 18, 2009: RIB. CRACKED. INBOARD RIB WAS CRACKED AT LEADING EDGE. CRACKS BEGIN IN BOTH UPPER AND LOWER FLANGE RADIUS AND PROGRESSED THROUGH THE FIRST RIVET HOLE IN THE WEB. CRACKS EXTEN
- [SDR 20001109SH039](https://openairdocs.org/sdr/20001109SH039), Oct 24, 2000: SKIN. CRACKED. DURING ROUTINE INSPECTION, A CRACK WAS FOUND ON THE LEFT STABILATOR LOWER SKIN. (X)
- [SDR 20000424SH023](https://openairdocs.org/sdr/20000424SH023), Mar 9, 2000: SCISSORS. CRACKED. DURING DETAILED LANDING GEAR INSPECTION, THE SCISSORS ON THE RT MAIN GEAR WERE FOUND CRACKED. THE CRACKS ARE LOCATED NEAR THE MACHINED RADIUS WHERE THE TWO SCIS
- [SDR 99ZZZX4608](https://openairdocs.org/sdr/99ZZZX4608), Nov 29, 1999: HINGE. CRACKED. CREW DOOR MISALIGNED WHEN PILOT ATTEMPTED TO SECURE. INSPECTION REVEALED FORWARD HINGE CRACKED AT HINGE PIN REGION. HINGE HALF WAS REPLACED WITH SERVICEABLE HIN
- [SDR 99ZZZX4394](https://openairdocs.org/sdr/99ZZZX4394), Oct 28, 1999: BOOT. FAILED. LIP DEICE BOOT TRIPPED CIRCUIT BREAKER IN-FLIGHT. POST-FLIGHT INSPECTION REVEALED DEICER BURNED UP LEAVING EXPOSED WIRES AND CHARING ON COWL. DEICER WAS THEN RE
- [SDR 99ZZZX795](https://openairdocs.org/sdr/99ZZZX795), Jan 29, 1999: FUEL CEL. LEAKING. PILOT REPORTED EVIDENCE OF FUEL ON RT OUTBOARD GEAR DOOR. INSPECTION REVEALED FUEL LEAK SOURCE AT BOX FUEL CELL JUST OUTBOARD OF NACELLE, AFT OF SPAR. REPLACED 
- [SDR 98ZZZX4710](https://openairdocs.org/sdr/98ZZZX4710), Nov 3, 1998: ACTUATOR. FAILED. ON POST-FLIGHT INSPECTION, PILOT REPORTED HYDRAULIC FLUID ON LOWER FUSELAGE AND TAIL. MECHANICS WERE NOTIFIED AND CLOSER INSPECTION REVEALED FLUID LEAKING FROM 
- [SDR 98ZZZX1171](https://openairdocs.org/sdr/98ZZZX1171), Feb 1, 1998: NUT. CORRODED. RUDDER TAB ACTUATOR NUT FOUND CORRODED DURING ROUTINE INSPECTION.

## NTSB investigations (1)

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 SEA05LA010](https://openairdocs.org/ntsb/SEA05LA010), Oct 18, 2004: Beech 99A (N955AA), Billings, MT, substantial damage. Probable cause: the pilot's failure to follow the instrument approach procedure, which resulted in a premature descent below the decision height and subsequent collision with a building.

## 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 20041017026999A](https://openairdocs.org/incident/20041017026999A), Oct 17, 2004: Beech 99A (N955AA), Great Falls, MT, Substantial damage. (-23) The aircraft departed Great Falls, MT (gtf) at 2130 IFR for logan int'l, billings, MT (bil). The pilot was executing an ILS approach to 10L at logan…

## Other aircraft with N955AA

- [Registered now](https://openairdocs.org/aircraft/N955AA): Textron 525B, S/N 525B0697, built 2023
- [Cancelled 1990-03-16](https://openairdocs.org/deregistered/N955AA-1990-03-16): Beech 300, S/N FA-86. Exported to Colombia. Owner: [Amr Aircraft Sales Inc](https://openairdocs.org/faa-owner/AMR%20AIRCRAFT%20SALES%20INC), [Ft Worth, TX](https://openairdocs.org/faa-place/TX/Ft%20Worth)

---
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.