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Zlin Aircraft Z 242 L User Manual

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AIRPLANE FLIGHT MANUAL
Z 242 L
Document No. 003.012.1
Serial No.: ................................................
Registration Mark: ................................................
Manufacturer: ZLIN AIRCRAFT a.s.
OTROKOVICE 765 02
CZECH REPUBLIC
Category: ACROBATIC (A)
UTILITY (U)
NORMAL (N)
Certification Basis: FAR Part 23 as amended trough Amendment 23 - 41 inclusive
FAR Part 36 as amended trough Amendment Amdt. 36 - 20 inclusive
ICAO, Annex 16.
THIS DOCUMENT MUST BE CARRIED IN THE AIRPLANE AT ALL OPERATION TIMES!
THIS AIRPLANE FLIGHT MANUAL IS EASA APPROVED UNDER APPROVAL NO.: 10042932.
DATE OF APPROVAL: 7.1.2013
The English version has been translated with care and is accurate to the best of editor’s
knowledge. However in all official matters the original Czech version is the authoritative
document.
THIS AIRPLANE FLIGHT MANUAL SUPERSEDES ALL “AIRPLANE FLIGHT MANUALS OF THE
Z 242 L AIRCRAFT” ISSUED IN ENGLISH VERSION, WHICH ARE NOT MARKED ON THE TITTLE
PAGE WITH DOCUMENT NUMBER 003.012.1
Copyright © 2011
ZLIN AIRCRAFT a.s.
765 02 OTROKOVICE
Czech Republic
ISSUE OF REVISION No. 3 IS APPROVED UNDER DOA No. EASA.21J.110 APPROVAL
DATE OF APPROVAL: 9.3.2017
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Zlin Aircraft Z 242 L Specifications

General IconGeneral
Crew1
Capacity1 passenger
EngineLycoming AEIO-360-A1B6
TypeTrainer aircraft
ManufacturerZlin Aircraft
Length6.94 m
Height2.85 m
Max takeoff weight970 kg
PowerplantLycoming AEIO-360-A1B6
Rate of climb5 m/s

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