KitLog pro

Powered By Kitlog Pro v2.0

ONEX #54 Web Site
' style=
Date:  8-29-2014
Number of Hours:  0.00
Manual Reference:  B04
Brief Description:  Flight #27-28, Max gross weight test, 1:58

Flight #27 was to evaluate t/o, climb and stall performance at the maximum gross takeoff weight of 950#. It was a relatively cool day for this test with a t/o density altitude of 500'.

Added a 50# bag of sand under the seat cushion and a 20# bag of plaster mix in the baggage area to bring my gross weight to 950#. Average climb to 4000' was ~440fpm. Power on/off stalls and departure stalls were normal with no abrupt departures. Stalls were "mushy" and easily recovered by lowering the nose and adding power where required.

Flt #27 AWOS at PYM 070/08, V10, Few @2700, 21c/12c, 30.21, DA500' TAC time :25. Fuel used 1.6g.

Flight #28 was gathering cruise data at 2500'-3500', 2800rpm, approaches at CQX and 5B6.

Flt #28 AWOS at PYM 050/06, V10, Clr, 21c/11c, 30.22, DA500. TAC time 1:33, fuel used 4.5g. Avg TAS ~100mph.
' style=

Max gross weight stalls

Max gross weight stalls

' style=

AVARE Flt 27 & 28

AVARE Flt 27 & 28

' style=

AV8OR Flt 28 cruise track

AV8OR Flt 28 cruise track

' style=










Copyright © 2001-2024 Matronics. All Rights Reserved.