N71155

Valid Registration

1946 LUSCOMBE 8A

N71155 is a 1946 LUSCOMBE 8A registered to STEP TOO LLC in WILMINGTON, DE. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 1 Airworthiness Directive may apply.

Registration Details

N-Number
N71155
Serial Number
2582
Manufacturer
LUSCOMBE
Model
8A
Year
1946
Registration Status
Valid
Airworthiness Date
1956-07-15
Owner
STEP TOO LLC
Owner City
WILMINGTON
Owner State
DE

The LUSCOMBE 8A is registered with the FAA under N-number N71155. This airframe was manufactured in 1946. Its manufacturer serial number is 2582. The aircraft was issued its airworthiness certificate on 1956-07-15. The current registered owner is STEP TOO LLC, based in WILMINGTON, DE. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

Serious injuries2019-01-05

Casa Grande, AZ, USA

Accident — Luscombe 8 (NTSB GAA19CA127)

Minor injuries1993-06-20

BEACH CITY, OH, USA

Accident — LUSCOMBE 8A (NTSB NYC93LA130)

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

N71155 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

1 found
AD 97-31680Effective: 1997-12-03

Airworthiness Directives; The Don Luscombe Aviation History Foundation Models 8, 8A, 8B, 8C, 8D, 8E, 8F, T-8F Airplanes; Correction

This document clarifies information in airworthiness directive (AD) 96-24-17, which applies to Don Luscombe Aviation History Foundation (Luscombe) Models 8, 8A, 8B, 8C, 8D, 8E, 8F, T-8F airplanes. AD 96-24-17 currently requires installing new inspection holes, modifying the wing tip fairings, and inspecting the wing spars for intergranular corrosion. The actions specified in AD 96-24-17 are intended to prevent wing spar failure from intergranular corrosion, which could result in structural failure of the wings and loss of control of the airplane. The AD was published with an Appendix providing an alternative method of compliance. Since issuance of AD 96- 24-17, the FAA has re-examined the Appendix and has determined that clarification of certain inspections procedures is needed. This action clarifies the procedures specified in the Appendix of AD 96-24-17.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N71155 may be affected by 1 directive. 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.

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Get the complete history for N71155

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

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