Lancair ES-P Manuel du propriétaire
PILOT'S
OPERATING
HANDBOOK
AND
AIRPLANE FLIGHT MANUAL
®ES-P
Manufacturer: Heizer IJ
Serial No: 001
Model: ESP
Lancair Kit No: 120
This aircraft is FAA Approved in the EXPERIMENTAL
category based on FAR 23. This document must be carried in
the aircraft.
Originally Published by
Lancair International Inc.
2244 Airport Way
Redmond, Oregon 97756
Adapted for Heizer IJ ESP Serial Number 001 by
Isaac Heizer
Woodinville, Washington
98072
WARNING
This is an experimental aircraft having
experimental documentation. No aspect
of this documentation can be assumed
correct. The pilot must accept all risk and
responsibility associated with being
anywhere near this airplane – do not fly in
this aircraft if you do not personally agree
and accept all responsibility!
INTRODUCTION
This Pilot’s Operating Handbook is in the format and contains most
data recommended in the GAMA (General Aviation Manufacturers
Association) Handbook Specification Number 1.
Use of the Terms Warning, Caution and Note
The following conventions will be used for the terms, Warning,
Caution, and Note.
WARNING
The use of a Warning symbol means that
information which follows is of critical
importance and concerns procedures and
techniques which could cause or result in
personal injury or death if not carefully
followed.
CAUTION
The use of a Caution symbol means that
information which follows is of significant
importance and concerns procedures and
techniques which could cause or result in
damage to the airplane and/or its
equipment if not carefully followed.
NOTE
The use of the term “NOTE” means the
information that follows is essential to emphasize.
SECTION 2 GENERAL
TABLE OF CONTENTS
IMPORTANT NOTICE......................................................................2
DESCRIPTIVE DATA........................................................................4
GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS........7
METEOROLOGICAL TERMINOLOGY .......................................8
POWER TERMINOLOGY................................................................9
ENGINE CONTROLS / INSTRUMENTS........................................9
PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY
.............................................................................................................10
WEIGHT AND BALANCE TERMINOLOGY..............................11
This is a state-of-the-art, high performance general aviation aircraft.
Its performance is spectacular and its life almost beyond measure when
given reasonable care. You must become familiar with this handbook
as well as the FARs that are applicable to its operation. The
combination will provide you with safe and sound knowledge for
operation of your personally manufactured Lancair.
IMPORTANT NOTICE
This handbook must be read carefully by the owner or operator(s) of
this aircraft in order to become familiar with its operation and to obtain
all it has to offer in terms of both speed and reliability. Herein are
suggestions and recommendations to help you obtain safe performance
without sacrificing economy. You are encouraged to operate your
machine in accordance with and within the limits identified in this
Pilot's Operating Handbook as well as any placards located in the
airplane.
Again, the operator should be familiar with the Federal Aviation
Regulations as applicable to the operation and maintenance of
experimental airplane and FAR Part 91 General Operating and Flight
Rules. The aircraft must be operated and maintained in accordance
with any FAA Airworthiness Directives that may be issued against it.
It is also prudent and mandatory to operate within any established
limits or Service Bulletins.
The FARs place the responsibility for the maintenance of this airplane
on the owner and the operator who must ensure that all maintenance is
accomplished by the owner or qualified mechanics in conformity with
all airworthiness requirements established for this airplane.
All limits, procedures, safety practices, time limits, servicing, and
maintenance requirements contained in this handbook are considered
mandatory for the continued airworthiness of this airplane, in a
condition equal to that of its original manufacture.
NOTE
Except as noted, all airspeeds quoted in this
handbook are Indicated Airspeeds (IAS) in Knots
and assume zero instrument error.
The owner/operator should frequently refer to all supplements, whether
STCs (Supplemental Type Certificate) or Lancair Supplements direct
from Lancair, for appropriate placards, limitations, normal, emergency
and other operational procedures for proper operation of their Lancair
with any optional equipment installed.
WARNING
When this handbook is used for airplane
operational purposes, it is the pilot's responsibility
to maintain it in current status.
DESCRIPTIVE DATA
ENGINE
This aircraft is fitted with a Continental TSIO-550E (3) six cylinder
fuel injected twin-turbocharged engine.
PROPELLER
This aircraft is equipped with an MT MTV-9-D/198-58a 3 blade
hydraulic constant speed propeller with a McCauley C290D3-R/T43
propeller governor. The propeller is 77.9 inches diameter.
FUELS
100 or 100LL (Minimum grade Aviation Gasoline conforming to
ASTM D0-76 & MLG-5572, latest revision).
SYSTEMS CAPACITIES
Fuel capacity 105 US gallons
Oil Capacity 12 quarts
FILTERS
Oil Filter CH48109-1
WEIGHTS
Empty weight 2480 lbs.
Max gross take-off 3600 lbs.
Max landing weight 3550 lbs.
Max weight in baggage compartment 175 lbs.
CABIN DIMENSIONS
Length 74 inches
Height (max) 47 inches
Width
Front seat 45 inches
Rear seat 42 inches
BAGGAGE
Length 40 inches
Width (Front) 37 inches
Width (Rear) 22.5 inches
Height (Front) 29.5 inches
Height (Rear) 23 inches
SPECIFIC LOADING (max take-off weight)
Wing area 140 ft2
Wing loading 25.7 lb./ft2
Power loading (350 HP) 10.3 lb./h.p.
Basic Airframe Dimensions
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