Kodiak 100 Series Quick setup guide

PrefaceGeneralEmergency LimitationsAbnormalProcedures
PerformanceWeight & Bal.
SystemsService
Supplements
QUEST AIRCRAFT COMPANY
1200 Turbine Drive
Sandpoint, ID 83864
Phone: [phone]
Fax: [phone]
www.questaircraft.com
PREFACE-1
Airplane Information Manual
(DOCUMENT NO: AM901.201)
100 SERIES AIRCRAFT
WARNING/NOTICE
At the me of issuance, this informaon manual was an exact
duplicate of the ight informaon contained within the Pilot’s
Operang Handbook and FAA Approved Airplane Flight Manual.
The informaon contained within this manual is to be used for
general purposes only and may NOT substute for the ocial Pilot’s
Operang Handbook. The informaon within this manual was
current as of the date listed below, and is for reference only.
DO NOT USE THIS MANUAL FOR
FLIGHT OPERATIONS
Revision 16
February 2015
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Table of Sections
CONTENTS SECTION
GENERAL ................................................................................................................ 1
LIMITATIONS ........................................................................................................... 2
EMERGENCY PROCEDURES ................................................................................ 3
ABNORMAL PROCEDURES ................................................................................ 3A
NORMAL PROCEDURES........................................................................................ 4
PERFORMANCE...................................................................................................... 5
WEIGHT AND BALANCE ........................................................................................ 6
AIRPLANE & SYSTEMS DESCRIPTIONS.............................................................. 7
HANDLING, SERVICE & MAINTENANCE.............................................................. 8
SUPPLEMENTS....................................................................................................... 9
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SECTION 1
GENERAL
Table of Contents
CONTENTS PAGE
GENERAL .............................................................................................................1-3
INTRODUCTION ...................................................................................................1-3
THREE VIEW DRAWING ......................................................................................1-3
DESCRIPTIVE DATA ............................................................................................1-5
ENGINE..............................................................................................................1-5
PROPELLER......................................................................................................1-5
FUEL ..................................................................................................................1-6
OIL......................................................................................................................1-7
MAXIMUM CERTIFICATED WEIGHTS .............................................................1-7
TYPICAL AIRPLANE WEIGHTS ........................................................................1-7
CABIN, CARGO, AND ENTRY DIMENSIONS ...................................................1-8
BAGGAGE/CARGO COMPARTMENT DIMENSIONS.......................................1-8
SPECIFIC LOADINGS .......................................................................................1-8
SYMBOLS, ABBREVIATIONS, AND TERMINOLOGY ........................................1-9
GENERAL AIRSPEED TERMINOLOGY AND ABBREVIATIONS ......................1-9
METEOROLOGICAL TERMINOLOGY ............................................................1-10
ENGINE POWER TERMINOLOGY..................................................................1-10
AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY......1-12
WEIGHT AND BALANCE TERMINOLOGY......................................................1-12
WARNINGS, CAUTIONS, AND NOTES DEFINED..........................................1-14
MEANING OF “SHALL,” “WILL,” “SHOULD,” AND “MAY” ...............................1-14
MEANING OF “LAND AS SOON AS POSSIBLE” OR “PRACTICABLE” .........1-14
CONVERSION CHARTS.....................................................................................1-14
KILOGRAMS AND POUNDS ...........................................................................1-15
NAUTICAL MILES, STATUTE MILES, AND KILOMETERS.............................1-16
LITERS, IMPERIAL GALLONS, AND U.S. GALLONS.....................................1-17
TEMPERATURE CONVERSION CHART ........................................................1-20
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1-1 GENERAL
This section of the Pilot’s Operating Handbook provides basic data and
information for the pilot which is useful in loading, hangaring, handling, and
accomplishing routine preight inspections of the airplane. This section
also provides denitions and explanations of symbols, abbreviations and
terminology used in this handbook.
1-2 INTRODUCTION
This handbook contains 9 sections and includes the material required to be
furnished to the pilot by the Federal Aviation Regulations, as well as additional
information provided by Quest Aircraft Company, and constitutes the FAA
Approved Airplane Flight Manual. Refer to the Table of Sections in the
“Preface” of this manual for a complete listing of the sections contained in this
handbook.
English is the authoritative text of Quest Aircraft Company, L.L.C., and Quest
Aircraft Design, L.L.C., technical publications. If a technical publication is
translated, then the English version will control.
1-3 THREE VIEW DRAWING
See Figure 1-1 for a general arrangement drawing of the KODIAK 100.
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Figure 1-1 – Three View Drawing
Main Landing Gear
Track Width: 137 in
Maximum Height: 14.7 ft
19 in
Wheel Base Length:
130 in
33.8 ft
45.0 ft
Wing Area: 240 sq.ft.
Minimum Turning Radius: 152 in
(Main Landing Gear to
Nose Landing Gear)
Max. Propeller Diameter: 96 in
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1-4 DESCRIPTIVE DATA
ENGINE
Number of Engines: 1
Engine Manufacturer: Pratt & Whitney Canada
Engine Model Number: PT6A-34
Engine Type: The PT6A series engine is a free power, two-shaft turbine
engine. The engine uses a three-stage axial and one-stage centrifugal
compressor section, an annular reverse-ow combustion chamber, single
stage compressor turbine, single stage power turbine. The exhaust gas
is directed through an annular exhaust plenum to the atmosphere via twin
opposed exhaust ports provided in the exhaust duct.
Horsepower Rating:
Type of Engine Power
Shaft
Horsepower
(SHP)
Takeoff 750
Maximum Continuous Emergency 750
Maximum Normal Operating 700
Maximum Climb 700
Maximum Cruise 700
Table 1-1 – Horsepower Rating
PROPELLER
Number of Propellers: 1
Propeller Manufacturer: Hartzell Propeller Inc.
Propeller Model Number: HC-E4N-3P (HC-E4N-3PY) / D9511FSB
Number of Propeller Blades: 4
Propeller Diameter: 95 - 96 inches
Propeller Type: Constant speed, full feathering, reversible, hydraulically
actuated aluminum-bladed propeller, with a feathered blade angle of 86°, a
low pitch blade angle of 17.5°, and a maximum reverse pitch of -10° (at the
30-inch radius).
NOTE: Horsepower ratings are for 2200 RPM (propeller).
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FUEL
The following fuels and fuel additives are FAA approved for use on the
KODIAK 100, subject to the limitations and requirements given in “Section 2”
of this manual.
Approved Fuel Grade Issuing Authority
(Specication) Freezing Point °C (°F) Color
JET A ASTM D 1655 -40 (-40) Straw
JET A-1 ASTM D 1655 or
DEF STAN 91-91 -47 (-53) Straw
JP-1 MIL-T-5616 -46 (-51) Straw
JP-5 MIL-DTL-5624 -50 (-58) Straw
JP-8 MIL-DTL-83133 -60 (-76) Straw
No. 3 Jet Fuel GB6537 (China) -47 (-53) Straw
Table 1-2 – Approved Fuels
Icing Inhibitor Additive Name Concentration Required (% by Volume)
Diethylene Glycol Monomethyl
Ether (DIEGME) conforming to
MIL-DTL-85470 or MIL-I-85470
0.10% to 0.15%
Table 1-2A – Approved Anti-Icing Additive
If additional biocidal protection is desired, the following additive is permitted:
Biocidal Additive Maximum Concentration Allowed (% by Volume)
Biobor JF 0.02% (270 ppm)
Table 1-2B – Approved Biocidal Additive
Fuel Capacity (in U.S. Gallons):
Both Tanks ........................................................320 U.S. Gallons (2177 lb)
Each Tank .........................................................160 U.S. Gallons (1089 lb)
Capacity to Inboard Filler Ports (Both Tanks)....193 U.S. Gallons (1313 lb)
Usable Fuel (Both Tanks ON) ...........................315 U.S. Gallons (2143 lb)
Unusable Fuel (Both Tanks ON) ...............................5 U.S. Gallons (34 lb)
Undrainable Fuel (Both Tanks ON) ........................0.15 U.S. Gallons (1 lb)
CAUTION: JP-5 and JP-8 fuels contain anti-icing additives. Do not use
additional additives with these fuels.
WARNING: All fuels used must contain anti-icing fuel additive
conforming to MIL-DTL-85470 or MIL-I-85470, unless the exceptions given
in “Section 2” of this manual are followed.
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