Zenair CH 601 XL ZODIAC 2002 Technical specifications

SAMPLE
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LU Uý ýN NÍ Í1 18 82 24 4, ,S ST TA AR RÉ ÉM Mċ ċS ST TO O, ,6 68 86 60 02 2, ,C CZ ZE EC CH HR RE EP PU UB BL LI IC C

SAMPLE
i
Document No.:
Z601XLFMEN
Date of Issue:
12/2002
Revision:
T
Te ec ch hn ni ic ca al lC Co om mm mi is ss si io on no of f
L
Li ig gh ht tA Ai ir rc cr ra af ft tA As ss so oc ci ia at ti io on no of ft th he eC
Cz ze ec ch hR Re ep pu ub bl li ic c
represented by:
....................................................................................................................
and as the organization authorized by the Ministry of Transportation and
Communications of the Czech Republic to prove compliance with the
microlight airplane category airworthiness requirements, certifies, that the
airplane design, used materials, flight performance and characteristics comply
with the Czech UL-2 airworthiness requirements and the airplane is
categorized to the following group of microlight airplanes:
U
UL LL La a
A
Ae er ro od dy yn na am mi ic ca al ll ly yC Co on nt tr ro ol ll le ed dM Mi ic cr ro ol li ig gh ht tA Ai ir rp pl la an ne es s
Signature: .............................................
Stamp:
Airplane - Type:
Serial Number:
Registration:
This airplane must be operated in compliance with
information and limitations contained in herein.
This Flight Manual must be available aboard the airplane.

SAMPLE
ii
Document No.:
Z601XLFMEN
Date of Issue:
12/2002
Revision:
0.1 Record of revisions
Any revision of the present manual, except actual weighing data, must be
recorded in the following table.
The new or amended text in the revised pages will be indicated by a black
vertical line in the left hand margin, and the Revision No. and Date will be
shown on the bottom of the page.
Revision No.
Affected
Section
Affected
Pages
Date of
Issue Approved by Date of approval
Date
inserted Signature

SAMPLE
iii
Document No.:
Z601XLFMEN
Date of Issue:
12/2002
Revision:
0.2 List of Effective Pages
Section Page Date of
Issue
Section Page Date of
Issue
2 2-0 12/2002
i 12/2002 2-1 12/2002
ii 12/2002 2-2 12/2002
iii 12/2002 2-3 12/2002
iv 12/2002 2-4 12/2002
v 12/2002 2-5 12/2002
2-6 12/2002
2-7 12/2002
1 1-0 12/2002 2-8 12/2002
1-1 12/2002 2-9 12/2002
1-2 12/2002
1-3 12/2002
1-4 12/2002
1-5 12/2002
3 3-0 12/2002
3-1 12/2002
3-2 12/2002
3-3 12/2002
3-4 12/2002
3-5 12/2002
3-6 12/2002
3-7 12/2002
3-8 12/2002

SAMPLE
iv
Document No.:
Z601XLFMEN
Date of Issue:
12/2002
Revision:
Section Page Date of
Issue
Section Page Date of
Issue
4 4-0 12/2002 6 6-0 12/2002
4-1 12/2002 6-1 12/2002
4-2 12/2002 6-2 12/2002
4-3 12/2002
4-4 12/2002 7 7-0 12/2002
4-5 12/2002 7-1 12/2002
4-6 12/2002 7-2 12/2002
4-7 12/2002 7-3 12/2002
4-8 12/2002 7-4 12/2002
7-5 12/2002
7-6 12/2002
7-7 12/2002
7-8 12/2002
5 5-0 12/2002 7-9 12/2002
5-1 12/2002
5-2 12/2002
5-3 4/2001 8 8-0 12/2002
5-4 12/2002 8-1 12/2002
5-5 12/2002 8-2 12/2002
5-6 12/2002 8-3 12/2002
8-4 12/2002
8-5 12/2002
9 9-0 12/2002
9-1 12/2002
9-2 12/2002

SAMPLE
v
Document No.:
Z601XLFMEN
Date of Issue:
12/2002
Revision:
0.3 Table of Contents
Section
GENERAL.........................................................................1
LIMITATIONS ...................................................................2
EMERGENCY PROCEDURES.........................................3
NORMAL PROCEDURES ................................................4
PERFORMANCE..............................................................5
WEIGHT AND BALANCE ................................................6
AIRCRAFT AND SYSTEMS DESCRIPTION ...................7
AIRCRAFT HANDLING, CARE AND MAINTENANCE ..8
SUPPLEMENTS ...............................................................9

SAMPLE
1-0
Document No.:
Z601XLFMEN
Date of Issue:
12/2002
Revision:
SECTION 1
1. GENERAL
1.1 Introduction
1.2 Certification basis
1.3 Warnings, cautions and notes
1.4 Descriptive data
1.4.1 Aircraft description
1.4.2 Technical data

SAMPLE
1-1
Document No.:
Z601XLFMEN
Date of Issue:
12/2002
Revision:
1.1 Introduction
The airplane Flight Manual has been prepared to provide pilots with
information for the safe and efficient operation of Z ZE EN NA AI IR RC CH H6 60 01 1
X
XL LZ ZO OD DI IA AC C.
It also contains supplemental data supplied by the airplane manufacturer.
1.2 Certification basis
This aircraft type has been approved in compliance with UL-2 regulation,
which is mandatory certification basis for Microlight category airplanes
approved by Light Aircraft Association of the Czech Republic (LAA CR).
Type Certificate No.: .....................
Approved by: Technical Commission of LAA CR
Date of approval: ............................
Certificate of Airworthiness: „P“

SAMPLE
1-2
Document No.:
Z601XLFMEN
Date of Issue:
12/2002
Revision:
1.3 Warnings, cautions and notes
The following definitions apply to warnings, cautions and notes in the flight
manual.
WARNING
Means that the non-observation of the corresponding procedure leads to
an immediate or important degradation of the flight safety.
CAUTION
Means that the non-observation of the corresponding procedure leads to
a minor or possible long term degradation of the flight safety.
NOTE
Draws attention to any special item not directly related to safety, but
which is important or unusual.

SAMPLE
1-3
Document No.:
Z601XLFMEN
Date of Issue:
12/2002
Revision:
1.4 Descriptive data
1.4.1 Aircraft description
Z
ZE EN NA AI IR RC CH H6 60 01 1X XL Lis microlight airplane intended especially for
recreational and cross-country flying, with a limitation to non-aerobatics
operation.
Z
ZE EN NA AI IR RC CH H6 60 01 1X XL Lis a single-engine, all metal, low-wing monoplane of
semimonocoque construction with two side-by-side seats. The airplane is
equipped with a fixed tricycle undercarriage with steerable nose wheel.
The powerplant is composed of ROTAX 912 (80 hp or 100 hp), four
cylinder, four stroke engine and optional propeller by customer’s request.