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Public Record · As of May 5, 2026

N75AS

Pilatus B4-PC11AF · 1977 View Type →

Status

Registration Valid

Type

Glider

Engine

NONE NONE

Last Cert Issue

—

01 /  Registration

Filed with the Federal Aviation Administration

Every cell below is a literal field from the FAA Aircraft Registry. Click any value to open the FAA registry record for N75AS.

Tail Number

N75AS

Serial Number

274

Make

PILATUS

Model

B4-PC11AF

Year of Manufacture

1977

Mfr / Model Code

7090103

Type Aircraft

Glider

Type Engine

None

Engines

—

Seats

1

Engine Manufacturer

NONE

Engine Model

NONE

Horsepower

—

Weight Class

CLASS 1

Certification

Standard · code 1

Registrant

COFFIELD ALAN · Individual

Address

22050 VILLAGE WAY DR · CANYON LAKE, CA 92587-7543

FAA Region

4 · County 065

Status

Registration Valid

Airworthiness Date

—

Cert Issue Date

—

Expiration Date

—

Last FAA Action

—

Mode S Hex (ICAO24)

AA17C1

Mode S (Octal)

52413701

Live position via ICAO24 AA17C1

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02 /  NTSB Records

Events on file with the National Transportation Safety Board

03 /  Airworthiness Directives

Applicable to PILATUS B4-PC11AF

Federal Aviation Administration airworthiness directives matched to make and model. Each entry links to the Federal Register publication.

  • Apr 21, 2005

    Airworthiness Directives; Pilatus Aircraft Limited Models B4-PC11, B4-PC11A, and B4-PC11AF Sailplanes

    The FAA adopts a new airworthiness directive (AD) for all Pilatus Aircraft Limited (Pilatus) Models B4-PC11, B4-PC11A, and B4- PC11AF sailplanes. This AD requires you to repetitively inspect the control-column support for cracks and, if any cracks are found, replace the control-column support with a new support. This AD results from mandatory continuing air…

    Federal Register →

  • Feb 11, 2005

    Airworthiness Directives; Pilatus Aircraft Limited Models B4- PC11, B4-PC11A, and B4-PC11AF Sailplanes

    The FAA proposes to adopt a new airworthiness directive (AD) for all Pilatus Aircraft Limited (Pilatus) Models B4-PC11, B4-PC11A, and B4-PC11AF sailplanes. This proposed AD would require you to repetitively inspect the control-column support for cracks and, if any cracks are found, replace the control-column support with a new support. This proposed AD resu…

    Federal Register →

04 /  Service Difficulty Reports

FAA SDR filings

The FAA does not currently expose a public API for Service Difficulty Reports. We do not back-fill or paraphrase. Search the FAA SDR portal directly →

05 /  Sources & Methodology

Every fact on this page links to its primary US-government source

We render only what the agency publishes. Found a factual error? Report it → We acknowledge within 5 business days and resolve within 14.