9.108 -1 GENERAL
DESCRIPTIVE DATA
Maximum Certicated Weights
Landing............................................................................................7255 lb
Tires
Nose ...................................................................22 x 8.00, 6-ply, tube type
Main
................................................. 29 x 11.0, 10-ply, tubeless (with tube)
9.108 -2 LIMITATIONS
GENERAL LIMITATIONS
In order to operate with increased weights, the KODIAK
®
airplane must
be equipped with wing and ap vortex generators through either a factory
conguration or a eld retrot completed in accordance with Quest Field
Service Instruction FSI-007, Vortex Generator Clip Installation. Reference
Quest Service Notice SN-025 for details.
Tire Sizes and Pressures
Aircraft must be equipped with the factory optional large tires on all three
wheels.
Nose
...................................................................22 x 8.00, 6-ply, tube type
Cold, unloaded tire pressure: 35 psi
Main
................................................. 29 x 11.0, 10-ply, tubeless (with tube)
Cold, unloaded tire pressure: 27 psi
Weight Limits
Maximum Landing Weight ............................................................... 7255 lb
CENTER OF GRAVITY (CG) LIMITS
Loading Envelope for Landing
Forward CG Limit at 7,255
.....................................72.60 in. (27.41% mac)
(Linear variation between 6,690 lb and 7,255 lb)
Forward CG Limit at 6,690
.....................................69.25 in. (22.24% mac)
(Linear variation between 5,000 lb and 6,690 lb)
Forward CG Limit at 5,000 lb or less
......................63.90 in. (14.00% mac)
Aft Limit, up to 7,255 lb...........................................80.78 in. (40.00% mac)
Reference Datum
....................................................forward face of rewall
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