N505LP

Valid Registration

2000 CESSNA 172S

N505LP is a 2000 CESSNA 172S registered to WIFA (WASHINGTON INTERNATIONAL FLIGHT ACADEMY) LLC in GAITHERSBURG, MD. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 12 Airworthiness Directives may apply.

Registration Details

N-Number
N505LP
Serial Number
172S8546
Manufacturer
CESSNA
Model
172S
Year
2000
Registration Status
Valid
Airworthiness Date
2000-08-22
Owner
WIFA (WASHINGTON INTERNATIONAL FLIGHT ACADEMY) LLC
Owner City
GAITHERSBURG
Owner State
MD

The CESSNA 172S is registered with the FAA under N-number N505LP. This airframe was manufactured in 2000. Its manufacturer serial number is 172S8546. The aircraft was issued its airworthiness certificate on 2000-08-22. The current registered owner is WIFA (WASHINGTON INTERNATIONAL FLIGHT ACADEMY) LLC, based in GAITHERSBURG, MD. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported2025-08-21

Gaithersburg, MD, USA

Accident — CESSNA 172 (NTSB ERA25LA311)

No injuries reported2020-12-22

Culpeper, VA, USA

Accident — CESSNA 172S (NTSB ERA21LA092)

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

N505LP 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

12 found
AD E8-1460Effective: 2008-01-31

Airworthiness Directives; Cessna Aircraft Company Models 172R and 172S Airplanes

We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 172R and 172S airplanes. This AD requires you to inspect the fuel return line assembly for chafing; replace the fuel return line assembly if chafing is found; and inspect the clearance between the fuel return line assembly and both the right steering tube assembly and the airplane structure, adjusting as necessary. This AD results from reports of chafed fuel return line assemblies, which were caused by the fuel return line assembly rubbing against the right steering tube assembly during full rudder pedal actuation. We are issuing this AD to detect and correct chafing of the fuel return line assembly, which could result in fuel leaking under the floor and fuel vapors entering the cabin. This condition could lead to fire under the floor or in the cabin area.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N505LP may be affected by 12 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.

+11 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 N505LP

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

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