Accident PZL M-18B Dromader N8199W,
ASN logo
ASN Wikibase Occurrence # 39482
 
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:Tuesday 25 May 1999
Time:17:20 LT
Type:Silhouette image of generic M18 model; specific model in this crash may look slightly different    
PZL M-18B Dromader
Owner/operator:Terry L. Pitts
Registration: N8199W
MSN: 1Z027-25
Year of manufacture:1998
Total airframe hrs:84 hours
Engine model:PZL-Kalisz ASZ-62IR-M18
Fatalities:Fatalities: 1 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Altus, OK -   United States of America
Phase: Take off
Nature:Agricultural
Departure airport:(OK83)
Destination airport:
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The Dromader was departing from an 1,800 foot runway with a 250 foot overrun. The airplane was estimated to be 273 pounds overweight, and the density altitude was 3,244 feet. The pilot had set his flaps at 9 degrees, although other operators of the Dromader recommended 15 to 20 degrees of flaps for heavy gross weight takeoffs. The manufacturer's performance charts indicate that 1,800 feet is needed for a 10 degree flap takeoff under these conditions. A witness said that the airplane's engine was running smoothly, but the ground run appeared unusually long, and he saw it hit a small earthen berm at liftoff. He said the airplane popped up, then down, up again, and then nosed over onto its back. The airplane was found with its left main wheel separated, the crew compartment collapsed, the gate box (dump doors) closed, and approximately 510 gallons of applicant in the hopper. The engine was test run in its fuselage and operated normally with the exception of a 'popping' noise heard on its fourth run. Two exhaust valves were found heat blued, and one of the valves had a rub mark down its stem suggesting that it might have been stuck on some occasion.

Probable Cause: The pilot's disregard of takeoff performance data and his failure to jettison the load. Contributing factors were high density altitude, exceeding the aircraft's maximum allowable gross weight, and the berm.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: DEN99FA086
Status: Investigation completed
Duration: 1 year and 7 months
Download report: Final report

Sources:

NTSB DEN99FA086

Location

Revision history:

Date/timeContributorUpdates
24-Oct-2008 10:30 ASN archive Added
21-Dec-2016 19:23 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
26-Nov-2017 15:16 ASN Update Bot Updated [Operator, Departure airport, Source, Narrative]
08-Apr-2024 05:53 ASN Update Bot Updated [Time, Operator, Other fatalities, Departure airport, Source, Narrative, Category, Accident report]

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