Serious incident Piper PA-32R-300 N1358H,
ASN logo
ASN Wikibase Occurrence # 314415
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Wednesday 14 March 2012
Time:14:45 LT
Type:Silhouette image of generic P32R model; specific model in this crash may look slightly different    
Piper PA-32R-300
Owner/operator:private
Registration: N1358H
MSN: 32R7780155
Year of manufacture:1977
Total airframe hrs:3944 hours
Engine model:Lycoming IO-540 SER
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: None
Category:Serious incident
Location:Warrenton, Virginia -   United States of America
Phase: Landing
Nature:Training
Departure airport:Manassas Regional-Harry P. Davis Field, VA (MNZ/KHEF)
Destination airport:Warrenton Fauquier Airport, VA (KHWY)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
During the landing flare, the pilot heard a "boom," the airplane's nose dropped, and the airplane contacted the runway. Examination of the airplane revealed that the lower stabilator control cable turnbuckle had fractured as a result of stress corrosion cracking. An annual inspection was completed on the airplane the day before the accident. According to the airframe logbook entry, the inspection was performed in accordance with the PA32R-300 inspection checklist, which required, in part, inspection of the stabilator cable terminals and turnbuckles. The NTSB issued recommendations in 2001 to the FAA regarding the failure of control cable turnbuckles and recommending issuance of an airworthiness directive to require inspections of affected aircraft. On August 2, 2012, the FAA issued a notice of proposed rulemaking indicating the intention to adopt a new airworthiness directive (AD) that would require inspections of the stabilator control system and replacement of parts as necessary. The AD would be applicable for PA-28, PA-32, PA-34, and PA-44 airplanes.

Probable Cause: Maintenance personnel's failure to identify stress corrosion cracking in the stabilator control cable during the most recent inspection, and the subsequent failure of the cable on the flight after the inspection.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: ERA12IA237
Status: Investigation completed
Duration: 9 months
Download report: Final report

Sources:

NTSB ERA12IA237

Location

Revision history:

Date/timeContributorUpdates
02-Jun-2023 17:13 ASN Update Bot Added

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org