N274MA

Valid Registration

2024 PIPER PA-28-181

N274MA is a 2024 PIPER PA-28-181 registered to HOT WINGS AVIATION LLC in FISHERS, IN. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 2 Airworthiness Directives may apply.

Registration Details

N-Number
N274MA
Serial Number
28020174
Manufacturer
PIPER
Model
PA-28-181
Year
2024
Registration Status
Valid
Airworthiness Date
2024-05-21
Owner
HOT WINGS AVIATION LLC
Owner City
FISHERS
Owner State
IN

The PIPER PA-28-181 is registered with the FAA under N-number N274MA. This airframe was manufactured in 2024. Its manufacturer serial number is 28020174. The aircraft was issued its airworthiness certificate on 2024-05-21. The current registered owner is HOT WINGS AVIATION LLC, based in FISHERS, IN. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

Fatal injuries1991-02-22

TULSA, OK, USA

Accident — MITSUBISHI MU-2B-60 (NTSB FTW91FA043)

No injuries reported1982-11-11

ENGLEWOOD, CO, USA

Accident — MITSUBISHI MU-2B-60 (NTSB DEN83LA017)

Severity reflects injuries to people involved, not damage to the aircraft. A “no injuries” accident can still involve significant aircraft damage.

N274MA has been involved in 2 NTSB accidents since 1982. Each record above includes the date, location, severity, and NTSB summary. Buyers should review the full accident narratives and verify repairs in the aircraft's logbooks before purchase.

Applicable Airworthiness Directives

2 found
AD 05-18525Effective: 2005-09-21

Airworthiness Directives; The New Piper Aircraft, Inc., Models PA-28-160, PA-28-161, PA-28-180, and PA-28-181 Airplanes

The FAA adopts a new airworthiness directive (AD) for certain The New Piper Aircraft, Inc. (Piper) Models PA-28-160, PA-28-161, PA- 28-180, and PA-28-181 airplanes that incorporate Petersen Aviation, Inc. Supplemental Type Certificate (STC) SA2660CE installed between April 20, 1998, and April 1, 2005, and incorporate Petersen Aviation, Inc. Service Bulletin SB98-1. This AD requires you to replace the AN894-6-4 bushing screw thread expanders on the gascolator and bushing attached to the inlet of the top fuel pump with NAS1564-6-4J reducers and AN818-6 nuts. This AD results from reports of fuel leaks during the post STC installation tests. We are issuing this AD to prevent fuel fittings used in STC SA2660CE from leaking fuel in the engine compartment, which could result in an engine fire. This condition could lead to loss of control of the airplane.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N274MA may be affected by 2 directives. All applicable ADs must be complied with for the aircraft to remain legally airworthy. Buyers should verify AD compliance in the aircraft's logbooks before purchase.

+1 more Airworthiness Directive found for this aircraft

Full list, with effective dates and links to the official Federal Register documents, is included in the paid report.

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Get the complete history for N274MA

Full accident narratives, all Airworthiness Directives, ownership chain, and a downloadable PDF.

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