Accident Piper PA-28R-201 Arrow III N3783M,
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ASN Wikibase Occurrence # 189128
 
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Date:Saturday 6 August 2016
Time:11:45
Type:Silhouette image of generic P28R model; specific model in this crash may look slightly different    
Piper PA-28R-201 Arrow III
Owner/operator:Northhampton Aeronautics
Registration: N3783M
MSN: 28R-7837137
Year of manufacture:1978
Total airframe hrs:10855 hours
Engine model:Lycoming IO-360-C1C6
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Northampton Airport (7B2), Northampton, MA -   United States of America
Phase: Initial climb
Nature:Training
Departure airport:Northampton, MA (7B2)
Destination airport:Northampton, MA (7B2)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The flight instructor indicated that, during a simulated soft-field takeoff on an instructional flight, the airplane's climb performance noticeably deteriorated. As the airplane reached about 150 ft above ground level, the engine started to lose power. The flight instructor chose to make an emergency off-airport landing, during which the right wing and firewall were substantially damaged. A postaccident examination of the airplane revealed that the alternate air valve plate was lodged in the air intake and blocked the fuel servo. Further examination revealed that the hinge pin that held the alternate air valve plate was worn completely through, which caused the plate assembly to separate from its mounting location and lodge in the fuel servo. This obstruction likely restricted the intake air to the engine and thus led to the loss of engine power on takeoff. Examination of the alternate air valve plate revealed that it had been altered from its original design, although there were no maintenance records documenting the alteration. The investigation could not determine whether this alteration contributed to the failure of the alternate air valve plate's mounting mechanism.


Probable Cause: The failure of the alternate air valve plate hinge pin, which caused the alternate air valve plate to lodge in the fuel servo assembly, which resulted in a restriction of air to the fuel servo assembly, a loss of engine power, and an off-airport emergency landing.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: ERA16LA280
Status: Investigation completed
Duration: 3 years and 8 months
Download report: Final report

Sources:

NTSB
FAA register: http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=N3783M

Location

Revision history:

Date/timeContributorUpdates
06-Aug-2016 20:19 Geno Added
07-Aug-2016 08:12 bovine Updated [Source]
07-Aug-2016 08:12 Anon. Updated [Damage]
09-Nov-2016 21:06 Anon. Updated [Total occupants, Phase]
22-Apr-2020 17:01 ASN Update Bot Updated [Time, Operator, Departure airport, Destination airport, Source, Damage, Narrative, Accident report, ]

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