N23257

Valid Registration

AIR TRACTOR INC AT-301

N23257 is a AIR TRACTOR INC AT-301 registered to PHOENIX EQUIPMENT LC in NICKERSON, KS. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 8 Airworthiness Directives may apply.

Registration Details

N-Number
N23257
Serial Number
301-0371
Manufacturer
AIR TRACTOR INC
Model
AT-301
Year
—
Registration Status
Valid
Airworthiness Date
1981-06-26
Owner
PHOENIX EQUIPMENT LC
Owner City
NICKERSON
Owner State
KS

The AIR TRACTOR INC AT-301 is registered with the FAA under N-number N23257. Its manufacturer serial number is 301-0371. The aircraft was issued its airworthiness certificate on 1981-06-26. The current registered owner is PHOENIX EQUIPMENT LC, based in NICKERSON, KS. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported2013-05-08

Lyons, KS, USA

Accident — AIR TRACTOR INC AT-301 (NTSB CEN13LA265)

No injuries reported1985-07-25

BONITA, LA, USA

Accident — AIR TRACTOR AT301 (NTSB FTW85LA298)

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

N23257 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

8 found
AD E8-9058Effective: 2008-04-28

Airworthiness Directives; Air Tractor, Inc. Models AT-300, AT-301, AT-302, AT-400, and AT-400A Airplanes

The FAA is adopting a new airworthiness directive (AD) to supersede AD 2003-06-01, which applies to all Air Tractor, Inc. (Air Tractor) Models AT-300, AT-301, AT-302, and AT-400A airplanes that have aluminum spar caps; certain Air Tractor Models AT-400 airplanes that have aluminum spar caps; and all Models AT-300 and AT-301 airplanes that have aluminum spar caps and are or have been converted to turbine power. AD 2003-06-01 requires replacing the wing spar lower caps at a specified safe life limit; allows extending the safe life limit on certain airplanes if a wing lower spar cap splice rework is done; allows a limited time of continued operation beyond the safe life limit provided parts are ordered, the replacement is scheduled, and repetitive inspections reveal no cracks; and requires a report of any cracks found during any inspection to the FAA. This AD results from a recent report of cracks found on a Model AT-301 airplane at hours below the modification time specified in AD 2003-06-01. Consequently, this AD retains the wing spar lower cap replacement and reporting requirements from AD 2003-06-01 and adds a repetitive eddy-current inspection. We are issuing this AD to detect and correct cracks in the wing centerline splice joint. If not detected and corrected, these cracks could result in the wing separating from the airplane during flight.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N23257 may be affected by 8 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.

+7 more Airworthiness Directives 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 N23257

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

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