N132CP

Valid Registration

2006 CIRRUS DESIGN CORP SR20

N132CP is a 2006 CIRRUS DESIGN CORP SR20 registered to BALANCED SPEED LLC in FLOWER MOUND, TX. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 12 Airworthiness Directives may apply.

Registration Details

N-Number
N132CP
Serial Number
1715
Manufacturer
CIRRUS DESIGN CORP
Model
SR20
Year
2006
Registration Status
Valid
Airworthiness Date
2006-08-21
Owner
BALANCED SPEED LLC
Owner City
FLOWER MOUND
Owner State
TX

The CIRRUS DESIGN CORP SR20 is registered with the FAA under N-number N132CP. This airframe was manufactured in 2006. Its manufacturer serial number is 1715. The aircraft was issued its airworthiness certificate on 2006-08-21. The current registered owner is BALANCED SPEED LLC, based in FLOWER MOUND, TX. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

Fatal injuries2002-04-27

Alpine, UT, USA

Accident — Piper PA-34-200T (NTSB FTW02FA130)

No injuries reported1990-04-18

Bridgeport, CT, USA

Accident — PIPER PA-34-200T (NTSB NYC90LA089)

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

N132CP 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 E8-15474Effective: 2008-07-10

Airworthiness Directives; Cirrus Design Corporation Model SR20 and SR22 Airplanes

We are adopting a new airworthiness directive (AD) for certain Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. This AD requires you to replace the cabin door rod ends with new parts including a redesigned non-binding hinge pin that replaces the existing pin at the upper door hinge. This AD results from two known occurrences of in-flight cabin door separation (one total separation and one retained by the door strut). The rod ends, a component of the door hinges, may fail and result in a door separation from the airplane while in flight. We are issuing this AD to prevent in-flight failure of the cabin door, which could result in door separation from the airplane.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N132CP 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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Other CIRRUS DESIGN CORP SR20 aircraft in our database

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Get the complete history for N132CP

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

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