L410 Flight Manual

LET L-410 UVP-E · Pilot's Operating Handbook

Free account — keep the POHs & checklists you reference in one place.

Overview

The document is the Flight Manual for the LET L-410 UVP-E aircraft, detailing various operational procedures, limitations, and performance metrics. It serves as a comprehensive guide for pilots and maintenance personnel.

The manual includes sections on normal and emergency procedures.
It provides performance data for the aircraft.
Weight and balance information is included.
The document is approved by relevant aviation authorities.
It contains a list of effective pages for reference.
The manual is structured into multiple sections for easy navigation.

Document

Source

Originally published by x-plane.hu. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

View original at x-plane.hu

Report a problem or request removal

Document details

Type: Pilot's Operating Handbook
Year: 2011
File size: 20 MB
Publisher: x-plane.hu
Language: en

About this document

What is the L410 Flight Manual?

The L410 Flight Manual is a pilot's operating handbook for the LET L-410 UVP-E, dated 2011.

Where does the L410 Flight Manual come from?

This copy of the L410 Flight Manual was originally published by x-plane.hu and is hosted on Sprinkle as a free, searchable reference copy.

What year was the L410 Flight Manual published?

The L410 Flight Manual — the LET L-410 UVP-E pilot's operating handbook on file — is dated 2011.

Documentation completeness

3/7

Most owners only have the POH. Here's the essential set for the LET L-410 UVP-E.

Pilot's Operating Handbook / AFM
Checklist
Maintenance Manual
Parts Catalog (IPC)
Systems & Wiring
Service Bulletins on file
Type Certificate (TCDS)

More LET L-410 UVP-Emanuals & documents

In this document

General

This section provides an overview of the aircraft and its specifications.

Limitations

Details the operational limitations of the aircraft.

Emergency Procedures

Outlines the procedures to follow in case of an emergency.

Performance

Contains performance metrics and capabilities of the aircraft.

Weight & Balance

Provides guidelines for loading and weight distribution.

Systems of Airplane

Describes the various systems and components of the aircraft.

Full document text

L LET, a,.. L 410 UVP-E20 CZECH REPUBUC FLIGHT MANUAL SECTION 0 LIST OF EFFECTIVE PAGES --- SECTION BOOK 1 & 2 Title page Section 0 BOOK 1 General - I PAGE - 0- 1 0-2 0-3 0-4 0-5 0-6 0-7 0-8 0-9 0-10 1-i 1-ii 1-1 1-2 1-3 1-4 1-5 1-6 1-7 1-8 1-9 1-10 1-11 1-12 1-13 1-14 1-15 1-16 1-17 1-18 1-19 1-20 1-21 1-22 1-23 1-24 DATE May 30/011 May 301011 May 301011 May 1/96 May 301011 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 May 1/98 May 301011 Mar 1/96 Mar 1/98 Mar 1/96 Mar 1/98 Apr 1/98 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Apr 1198 Mar 1/96 Mar 1/96 Apr 1/98 Apr 1/98 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 SECTION Limitations - II CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAA Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved Emergency Procedures - 111 CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI A~oroved PAGE - 2 - i 2-ii 2-1 2-2 2-3 2-4 2-5 2-6 2-7 2-8 2-9 2-10 2-1 1 2-12 2-13 2-14 2-15 2-16 2-17 2- 18 2-19 2-20 2-21 2-22 2-23 2-24 2-25 2-26 2-27 2-28 2-29 2-30 3-i 3-ii 3-1 3-2 3-3 3-4 3-5 DATE Apr 1/98 Apr 1/98 May 1/98 May 1196 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1196 May 301011 Mar 1196 Apr 1198 Mar 1196 Mar 1196 Mar 1196 Mar 1/96 Apr 1/98 Apr 1198 Mar 1/96 Mar 1196 Mar 1/96 May 1/98 Apr 1/98 Apr 1198 Apr 1198 May 1/98 Apr 1/98 Apr 1/98 Mar 1/96 Mar 1/96 Mar 1/96 May 1/98 Mar 1/96 Mar 1/96 Mar 1/96 Apr 1/98 Apr 1198 Apr 1/98 Apr 1198 Mar 1/96 May 30101 ( 5 ) 0 - 1 SECTION 0 FLIGHT MANUAL LET, *.a. CZECH REPUBUC SECTION Emergency Procedures - 111 CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved Abnormal Procedures - lllA ICAA Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved ICAA Approved [CAA Approved ICAA Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved LIST OF EFFECTIVE PAGES PAGE DATE Mar 1/96 Mar 1196 Mar 1196 Apr 1198 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Mar 1/96 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 w a y 30101 Apr 1/98 Apr 1/98 Apr 1/98 Mar 1/96 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Mar 1/96 p a y 30101 p a y 30101 p a y 30/01 Apr 1/98 Apr 1198 Apr 1/98 Apr 1/98 Mar 1196 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 SECTION CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved Normal Procedures - IV CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved PAGE 0 - 2 (5) May 30101 DATE Apr 1/98 Mar 1/96 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Mar 1/96 Apr 1/98 " Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 w', Apr 1/98 Apr 1/98 Apr 1198 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 , Apr 1/98 . Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Mar 1/96 Apr 1/98 Apr 1/98 Apr 1/98 ' Apr 1/98 Apr 1/98 Apr 1/98 L ' -/ 8'' '-' -/ .' !/ - / L' / .-' ' \ / \.' - ' " * .' * .' ' / LET, a.r. CZECH REPUBLIC FLIGHT MANUAL SECTION 0 LIST OF EFFECTIVE PAGES SECTION Normal Procedures - IV CAI Approved CAI Approved CAI Approved CAI Approved CAA Approved 1 CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved Performance - V CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved - PAGE - 4-33 4-34 4-35 4-36 4-37 4-38 4-39 4-40 4-41 4-42 4-43 4-44 4-45 4-46 4-47 4-48 5-i 5-ii 5-1 5-2 5-3 5-4 5-5 5-6 5-7 5-8 5-9 5-10 5-1 1 5-12 5- 13 5-14 5-15 5-1 6 5-17 SECTION DATE Apr 1/98 - / Mar 1/96 Apr 1/98 ~ Apr 1/98 May 30101 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1198 May 1/98 Apr 1/98 Apr 1/98 Apr 1/98 Apr 1/98 \-' Mar 1/96 1' Mar 1/96 - ' Apr 1/98 Mar 1196 1. Mar 1/96 " May 1/96 May 1/96 Mar 1/96 \. Mar 1/96 .' Mar 1/96 Mar 1/96 Mar 1/96 Apr 1/98 Mar 1/98 May 1/96 Mar 1/96 Mar 1/96 May 1/96 Mar 1/96 ' CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved ' .: 'h / \ / ' . / \./ - / \ / .' i \ ' 7 PAGE - 5-18 5-19 5-20 5-21 5-22 5-23 5-24 5-25 5 -26 5-27 5-28 5-29 5-30 5-31 5-32 5-33 5-34 5-35 5-36 5-37 5-38 5-39 5-40 5-41 5-42 5-43 5-44 5-45 5-46 5-47 5 -48 5-49 5-50 5-51 5-52 5-53 5-54 5-55 5-56 5-57 5-58 May 30101 (5) 0 - 3 DATE Mar 1/96 Mar 1196 .' Mar 1196 " May 1/96 -" Mar 1/96 -.' Mar 1/96 Mar 1/96 ' May 1/96 . Mar 1/96 Mar 1/96 Mar 1/96 May 1/96 Mar 1/96 Mar 1196 May 1/96 , Mar 1/96 Mar 1/96 , Mar 1/96 Mar 1196 Mar 1/96 Mar 1196 May 1/96 May 1/96 . Mar 1/98 Mar 1/96 May 1/96 May 1/96 May 1/96 May 1/96 .

Show full text

Mar 1/96 Mar 1/96 - May 1/96 May 1/96 . May 1/96 May 1196 May 1/96 Apr 1/98 May 1/96 May 1/96 May 1/96 Mar 1/96 -1 \i ,/ / .-. .. -, L'' :.' .' * '.( -/ 7 ' j SECTION o FLIGHT MANUAL LEZ as. CZECH REPUBLIC SECTION Performance - V CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved LIST OF EFFECTIVE PAGES PAGE - 5-59 5-60 5-61 5-62 5-63 5-64 5-65 5-66 5-67 5-68 5-69 5-70 5-71 5-72 5-73 5-74 5-75 5-76 5-77 5-78 5-79 5-80 5-81 5-82 5-83 5-84 5-85 5-86 5-87 5-88 5-89 5-90 5-91 5-92 5-93 5-94 5-95 5-96 5-97 5-98 SECTION DATE Mar 1/96 May 1/96 Mar 1/96 - Mar 1/96 -' May 1/96 Mar 1/96 -,. Mar 1/96 Mar 1/96 May 1/96 ' Mar 1/96 ,- Mar 1/96 Mar 1/96 May 1/96 Mar 1/96 May 1 196 ' May 1/96 L / Mar 1/96 ' May 1/96 . Mar 1/96 Mar 1/96 - Mar 1/96 ,' Mar 1/96 , May 1/96 " May 1/96 Mar 1/96 Mar 1/96 May 1/96 " ' May 1/96 May 1/96 . Mar 1/96 May 1/96 \; Mar 1/96 .,' May1196 May1196 May 1/96 May 1/96 ', Mar 1/96 Mar 1/96 i * Mar 1/96 ( 1 May 1/96 . CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved CAI Approved BOOK 2 Weight & Balance - VI '/ -/ -/ -' ,-I J '/ -: , ' *-/ i u / .' '" ' I ; \ / I! ' PAGE DATE May 1/96 Mar 1/96 May 1/96 Mar 1/96 May 1/96 Mar 1/96 May 1 196 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 May 1/96 May 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 May 1/96 Mar 1/96 May 1/96 Mar 1/96 Mar 1/96 Mar 1196 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1 196 (5) May 30101 LET, as. CZECH REPUBLIC FLIGHT MANUAL SECTION 0 LIST OF EFFECTIVE PAGES 'AGE DATE Mar 1/96 Mar 1196 Mar 1/96 Mar Mar May May May Mar Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1196 Mar 1/96 Mar 1/96 Apr 1/98 Mar 1/96 Mar 1/96 Apr 1198 Mar 1/96 Mar A P ~ Mar Mar Mar Mar Mar Mar Mar Mar Mar 1/96 Mar 1196 Mar 1/96 SECTION PAGE - 7-23 7-24 7-25 7-26 7-27 7-28 7-29 7-30 7-31 7-32 7-33 7-34 7-35 7-36 7-37 7-38 7-39 7-40 7-41 7-42 7-43 7-44 7-45 7-46 7-47 7-48 7-49 7-50 7-51 7-52 7-53 7-54 7-55 7-56 7-57 7-58 7-59 7-60 7-61 7-62 7-63 7-64 7-65 DATE Mar 1/96 Mar 1I96 Mar 1/98 Mar 1I96 Mar 1196 Mar 1/96 Apr 1/98 Apr 1/98 Apr 1I98 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1196 Apr 1I98 Mar 1/96 Mar 1196 Mar 1196 Mar 1/96 Mar 1196 Mar 1I96 Mar 1/96 Apr 1198 Apr 1/98 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1196 Mar 1/96 Mar 1/96 Apr 1/98 Mar 1/98 Mar 1/96 Mar 1/96 Mar 1196 Apr 1/98 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 May 30/01 (5) 0 - 5 SECTION 0 FLIGHT MANUAL LET, 0.r. CZECH REPUBUC SECTION Systems of airplane - VII LIST OF EFFECTIVE PAGES PAGE - 7-66 7-67 7-68 7-69 7-70 7-71 7-72 7-73 7-74 7-75 7-76 7-77 7-78 7-79 7-80 7-81 7-82 7-83 7-84 7-85 7-86 7-87 7-88 7-89 7-90 7-91 7-92 7-93 7-94 7-95 7-96 7-97 7-98 7-99 7-100 7-1 01 7-102 7-103 7-104 7-105 7-106 DATE Mar 1/96 Mar 1/96 may 30/01 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1196 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1196 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1196 Mar 1/96 Mar 1/96 Mar 1196 Mar 1196 Mar 1/96 Mar 1/96 SECTION - - Handling, Servicing & Maintenance - Vlll PAGE DATE Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1196 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1196 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1/96 Mar 1196 .- LET, a.r CZECH REPUBLIC FLIGHT MANUAL SECTION 0 SECTION Supplements .- IX No. l a No. 1c No. I d No. I f No. l g No. li No. 1k No. 1m No. I n No. Ip No. I r No. 1s No. 4 No. 19a No. 20 i No. 34 LIST OF EFFECTIVE PAGES PAGE DATE Mar 1/96 Mar 1/96 Mar 1196 Mar 1196 Mar 1/96 Mar 1/96 Mar 28/97 Mar 28/97 Mar 28/97 Mar 28/97 Mar 28/97 Mar 28/97 Mar 28/97 Mar 28/97 Mar 28/97 Mar.28197 Mar 28/97 Mar 12/98 Apr. 10197 Mar. 25/99 Jun. 1/98 Mar. 20199 SECTION PAGE DATE Mar 1/96 0 - 7 SECTION o FLIGHT MANUAL LET. r r CZ€CW REWLlLlC LIST OF EFFECTIVE PAGES PAGE DATE SECTION PAGE - DATE Mar 1/96 LET, a.r. CZECH REPUBLIC FLIGHT MANUAL SECTION 0 TABLE OF CONTENTS BOOK I SECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LIST OF EFFECTIVE PAGES 0 GENERAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .I LIMITATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .II . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EMERGENCY PROCEDURES 111 ABNORMAL PROCEDURES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .lllA NORMAL PROCEDURES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .IV PERFORMANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .V BOOK 2 SECTION LIST OF EFFECTIVE PAGES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0 WEIGHT & BALANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .VI SYSTEMS OF AIRPLANE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .VII . . . . . . . . . . . . . . . . . HANDLING, SERVICING & MAINTENANCE Vlll SUPPLEMENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .IX Mar 1/96 0-9 SECTION O FLIGHT MANUAL LET, as. CZECH REPUBLIC Intentionally left blank - - - - - - - - - - 0-10 Mar 1/96 SECTION I LET. as. CZECH REPUBLIC FLIGHT MANUAL GENERAL GENERAL TABLE OF CONTENTS ITEM PAGE Mar 1/96 1 - i Log of revisions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1 .1 General description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 .5 Fuselage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 .5 Wing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 - 5 Tail unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Controls 1 5 Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 .6 Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 .6 Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 .6 General arrangement drawing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 .7 Minimum radius of turn on the ground . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 .8 Other dimensional data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 9 . Wing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 .9 Horizontal tail . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 .10 Verticaltail . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 - 1 0 Fuselage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Basic empty weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Definitions and symbols . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Conversion tables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 - 1 1 1 .11 1 12 . , 1 18 . . . . . . . . . . . . . . . . . . . . . . SECTION I GENERAL FLIGHT MANUAL LET, a.8. CZECH REPUBLIC Intentionally left blank Mar 1/96 SECTION I LET. ..a. CZECH REPUBUC FLIGHT MANUAL GENERAL LOG OF-REVISIONS . . The list of current pages is indicated in the Log of.Revisions. When a revision to this Manual is issued, the holder will be provided new revised pages. The holder of this Manual is responsible for ensuring that this Manual is current. The revised pages will be marked with the number and the date of issue of the revision. A marginal notation will be used to indicate those parts of the contents of a page that have been revised. Revision Number Revised pages -- - 0-1 to 3, 5 1-1, 7, 13, 16, 17 2-i, ii, 1, 7, 9, 14, 15, 20 to 25 3-1 t o 4 , 9 t o 1 4 , 1 6 t o 2 0 3A-i, ~ i , 1, 2, 4 to 7, 10 tci 15, 3A-17 to 21, 23 to 26 4-1, ii, 1 to 3, 5 to 25, 27 to 33, 4-35 to 48 5-1, 11, 54 7-5, 8, 11, 29 to 31, 36, 44, 45, 7-52, 57,68 Title pages 0-1, 3 1-1 2-1, 19, 23, 29 4-44 I Description of Revision CAA approved kcording to Approved in Czech vlandatorv language version Mandatory 3ulletin No. -41 0 UVP-U077a I kcording to Mandatory 3ulletin No. -410 UVP-U08la :valid for Model - 41 0 UVP-E20 according to LBA Sermany Type Sertificate) (cont.) Date blay 1/96 4pr 1198 May 1/98 1 May 1198 (3) 1 - 1 SECTION I L 410 UVP-E20 FLIGHT MANUAL GENERAL LET, a,=. CZECH REPUBLIC (cont.) I CAA approved Date I May 30101 1 - 2 ( 5 ) May 30101 SECTION I LET, m.s. CZECH REPUBLIC FLIGHT MANUAL GENERAL Revision Number -- - Revised pages Description of Revision (cont.) CAI approved Date Mar 1/96 1 - 3 SECTION I GENERAL FLIGHT MANUAL LET, a.r. CZECH REPUBLIC Description of Revision 1 - 4 Mar 1/96 CAI approved Date LET, a.r. CZECH REPUBLIC FLIGHT MANUAL SECTION I GENERAL GENERAL DESCRIPTION The L 410 UVP-E20 airplane is intended for the transport of passengers, mail and cargo and is able to take-off and land on paved as well as unpaved runways. The L 410 UVP-E20 is all metal semimonocoque high design wing. FUSELAGE The fuselage is an all-metal structure consisting of 27 fuselage frames and bulkheads, longitudinal stiffeners, floor and ceiling longitudinal ribs, floors, outer skins and landing gear nacelles. The front part of the fuselage begins with a nose cone, made of glassfibre-reinforced plastic, and ends at frame No 8. In this part of the fuselage are located: the front baggage compartment, the nose landing gear bay, electric and radio equipment bays, and the cockpit is arranged between bulkhead No 4 and frame No 7. The fuselage center section, between frames No 8 and No 18, accommodates the passenger cabin. Four wing attachments are located at frame No 12 and No 14. The rear section of the fuselage extends from frame No 18 to frame No 27 and terminates in a tail cone made of glassfibre-reinforced plastic. The baggage compartment is situated between frames No 19 and No 21. Behind the frame No 21 is located lavatory (version for 19 passengers). The tail attachment fittings are located at the reinforced frames No 25 and No 26. WING The wing is an all-metal structure and consists of two spars, cross ribs and skin with stringers. The wing is attached to the fuselage by means of four attachment lugs, located on the wing rib No 3. The four engine attachment fittings are located on ribs No 8 and No 10. Three wing tip tank attachment fittings are located on ribs No 31. Rubber fuel tanks are installed between the front and rear spars. The double-slotted wing flaps are split into an inner (ribs No 4 to No 10) and outer section (ribs No 10 to No 20). The ailerons are between ribs No 20 and No 31 .Ground spoilers are between ribs No 11 and No 20. Automatic bank control tabs are located between ribs No 27 and No 31. The ailerons are fabric-covered. The LH aileron is fitted with a trim tab. TAIL UNIT The tail unit consists of a horizontal tail, composed of a horizontal stabilizer and an elevator and a vertical tail with a fixed fin as vertical stabilizer and a rudder. CONTROLS The airplane is provided with dual controls. The ailerons and the elevator are actuated by control columns through the system of tie rods. The rudder is controlled by two interconnected pedal units through a system of tie rods and cables. The main landing gear brake valves are also controlled by the pedals. (cont.) Mar 1/96 1 - 5 SECTION I GENERAL L 410 UVP-EZO FLIGHT MANUAL LET. a.8. CZECH REPUBLIC The elevator trim tabs are controlled mechanically by means of a cable circuit. The rudder trim tab and the left aileron trim tab are controlled electrically. The ground spoilers, wing flaps and automatic bank control tabs are controlled electrohydraulically. Nose wheel steering is performed by an electrohydraulic unit which is actuated either manually (by a lever located on the control column) or by pedals. LANDING GEAR The landing gear is of three-wheel design. It consists of the nose and main landing gear, a number of hydraulic, mechanical and electric systems with whose assistance the retracting and extending of landing gear, nose landing gear wheel steering and wheel braking is performed. The system is equipped with the emergency circuit for main landing gear extending and wheel braking for the case of the main hydraulic circuit failure. ENGINE The airplane is equipped with two WALTER M 601 E engines with the V 510 propellers. The engine is designed as a turboprop, two-shaft with engine reverse flow and with free turbine. Shaft power: - maximum take-off - maximum continuous Speeds: - gas generator 750 SHP (560kW) 657 SHP (490kW) 36,660RPM (=lo0%) - free turbine 31,023RPM - the way of starting electric starter PROPELLER Basic technical parameters of V 51 0 propeller: - propeller diameter - number of blades - direction of rotation - propeller speed control range clockwise (viewed from the rear in the direction of flight) 1,700- 2,080RPM 1 - 6 Mar 1/96 SECTION I LET, a.r CZECH RWUBUC FLIGHT MANUAL GENERAL GENERAL ARRANGEMENT DRAWING 47.23 n (14.42 m) 7.9 R 2 0 . 4 in (2.41 m 5 1 0 rnm) n gf 7.55 ft (2.3 rn) 63.90 ft (19.48 rn) 65.55 ft (19.98 m) Fig. 1 - 1 Apr 1/98 (2) 1 - 7 SECTION I GENERAL FLIGHT MANUAL LET ..r. CZECH REPUBUC MINIMUM RADIUS OF TURN ON THE GROUND Fig. 1 - 2 I 1 1 - 8 Mar 1/96 LET, as. CZECH REPUBLIC FLIGHT MANUAL SECTION I GENERAL OTHER DIMENSIONAL DATA WlNG . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Area (wing tips not included) .375.23 sq.ft (34.86 m2) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Mean aerodynamic chord '1.. 6.29 ft (1,918 mm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Aspect ratio 10.45 Quarter-chord sweepback . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . O0 Angle of incidence at root . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .+2O Dihedral . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1O45' Aerodynamic twist . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . O0 Geometric twist . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .-2.8O The incidence point of the mean aerodynamic chord is 7.19 ft (2,191 mm) behind the reference plane laid perpendicularly through leveling points No 2 on the fuselage. The distance between the reference plane and the fuselage nose is 8.95 ft (2,730 mm). AILERONS Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 x 12.54 ft (2 x 3,822 mm) Area.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 2 x 15.6 sq.ft (2 x 1.45 m2) Deflection: up . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .27O + 1 down . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .14O + I 0 Area of left hand aileron trim tab . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..2.15 sq.ft (0.20 m2) Deflection of trim tab: up . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20° ? 2O down . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20° 5 2O WlNG FLAPS Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 2 x 15.84 ft (2 x 4,830 mm) Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 2 x 31.86 sq.ft (2 x 2.96 m2) Deflection of outer wing flap: take-off . . . . . . . . . . . . . . . . . . . . . . . . . 18O + 1 landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .42O 1tr 1 GROUND SPOILERS Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 2 x 8.84 ft (2 x 2,695 mm) Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 2 x 4.73 sq.ft (2 x 0.44 m2) Deflection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..72030r t 29 (cont.) Mar 1/96 SECTION I GENERAL FLIGHT MANUAL LET. a.s . C~!ECHREPUBLIC AUTOMATIC BANK CONTROL TABS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Length 2 x 4.46 ft (2 x 1.360 mm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Area 2 x 2.64 sq.ft (2 x 0.245 m2) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Deflection 55O +2O HORIZONTAL TAlL Span . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .22.1 ft(6.736mm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Area (total) 102.9 sq.ft (9.56 m2) Quarter-chord sweepback . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .5O . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Dihedral 7O . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Aspect ratio 4.79 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Mean aerodynamic chord 4.82 ft (1.469 mm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Angle of incidence +2O ELEVATOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Area 2 x 1 7 s q . f t ( 2 x 1 . 5 8 m 2 ) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Deflection: up 30° + 1 down . . . . . . . . . . . . . . . . . . ..... . . . . . . . . . . . . . . . . .14O r 1 Trim tab area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2 x 2.05 sq.ft (2 x 0.1 9 m2) Trim tab deflection: up . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1O0 2 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . down 16°+10 VERTICAL TAlL Height . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .10.86 ft ($31 0 mm) Area (total) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .78.57 sq.ft (7.30 m2) Quarter-chord sweepback . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .35O . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Aspect ratio 1.5 Mean aerodynamic chord . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7.49 ft (2.285 mm) (cont.) Mar 1/96 SECTION I GENERAL FLIGHT MANUAL LET, as. CZECH REPUBLIC DEFINITIONS AND SYMBOLS MEANS THAT THE NON - OBSERVATION OF THE CORRESPOND- ING PROCEDURE LEADSTOAN IMMEDIATEOR IMPORTANTDEG- RADATION OF THE FLIGHT SAFETY. A ABC AC ADF AGL ALT Altitude AP ATC ASDA MEANS THAT THE NON - OBSERVATION OF THE CORRESPONDING PROCEDURE LEADS TO A MINOR OR LESS LONG TERM DEGRADATION OF THE FLIGHT SAFETY. NOTE Draws the attention on any special item not directly related to safety but which is important or unusual. ampere automatic bank control system Alternating current automatic direction finding above ground level altitude The altitude specified in this manual is pressure altitude which is the expression of atmospheric pressure in terms of altitude above mean sea level according to inter-relations of these factors in the International Standard Atmosphere. This altitude may be determined by setting the sub-scale of an accurate pressure type altimeter at 1.013 hPa (29.92 in. Hg). autopilot air traffic control accelerate - stop distance available (cont.) 1 - 1 2 Mar 1/96 SECTION I LET, a.s. CZECH REPUBLIC FLIGHT MANUAL GENERAL O C CAI CAS CDI CG; cg cm COM or COMM CVR CWD DA DC DH DME EAS ELT OF FAA FAR FD FDR ft Wmin or fpm F.S. 9 GPS degrees Celsius Civil Aviation lnspectorate of the Czech Republic calibrated air speed course deviation indicator centre of gravity centimeterlcentimeters (lcm = 0.394 inch) communication cockpit voice recorder central warning display decision altitude direct current decision height distance measuring equipment equivalent airspeed emergency locator transmitter degrees Fahrenheit Federal Aviation Administration Federal Aviation Regulation - flight director flight data recorder footlfeet (1ft = 0.3048 m) feet per minute (100 Wmin = 0.508 mls) fuselage station - the distance from the fuselage davm (leveling point No 2.) acceleration due to gravity ( l g = 9.81m/s2) global positioning system Gradient of climb The gradient of climb is the ratio, in the same units, and expressed as a percentage, of: Change of Altitude Horizontal Distance Travelled The gradients of climb shown in the graphs are true gradients, i. e. they are derived from true (not pressure) rates of climb. (cont.) Apr 1/98 (2) 1 - 1 3 SECTION I GENERAL FLIGHT MANUAL LET,..a. czEcn REPUBUC Gross performance Hard runway Height HF HP hPa hr Hz IAS ICAO IELU IFR ILS IMC in ISA ITT kg kHz KlAS km kmlhr IAS kp kt kW I Ib Gross performance is such that the performance of any airplane of the type, measured at any time, is at least as likely to exceed the gross performance as not. A runway with a concrete or tarmac surface. The vertical distance between the lowest part of the airplane and the ground (AGL). high frequency horse power (1HP = 735.499 W) hektopascal hourlhours Hertz indicated airspeed International Civil Aviation Organization integrated electronic limiter unit instruments flight rules instrument landing system instrument meteorological conditions inchlinches (1 inch = 0.0254 m) International Standard Atmosphere - the air is a dry perfect gas - the temperature at sea level is 15 OC (59 OF) - the pressure at sea level is 10122 hPa (29.92 in. Hg) interturbine temperature kilogramlkilograms (1 kg 2.20462 Ib) kilohertz inaicated airspeed in knots kilometerlkilometers (1 km = 0.5399 Nm) indicated airspeed in kilometers per hour kilopondlkiloponds (1 kp = 9.81 N) knotlknots (1 kt =1NM per hour) kilowatt (1 kW = 1.34 HP) liter (1 liter = 0.26417 U.S. gallon) poundlpounds (1 Ib = 0.453 kg) (cont.) 1 - 1 4 Mar 1/96 L 410 UVP-EZO SECTION I LET, &s. CZECH REPUBUC FLIGHT MANUAL GENERAL LDA LH m MAC max M DA MDH MHz mm min MKR MM MSG N nG P NAV Net performance NM OAT OM PA PCL PROP psi QFE QNH landing distance available left hand side meterlmeters (1 m = 3.280 ft) mean aerodynamic chord maximum minimum descent altitude minimum descent height megahertz millimeterlmillimeters minimum/minute marker middle marker message Newton gas generator speed propeller speed navigation The majority of data given in this Flight Manual is net performance which is the gross performance diminished by certain margins to allow for various contingencies which cannot be directly accounted for during expected operation (e. g. need to manoeuvre, unavoidable variations in piloting technique, temporary below average performance, etc.). It is unlikely that the net performance will not be achieved in operation, provided the airplane is flown in accordance with the recommended techniques. C nautical miles (1 NM = 1.852 km) outside air temperature outer marker public address propeller control lever propeller pounds per square inch atmospheric pressure at aerodrome elevation altimeter setting to obtain elevation when on the ground (cont.) Mar 1/96 1 - 1 5 SECTION I GENERAL FLIGHT MANUAL LET, ..a. CZECH REPUBUC QTY RB RH RMI RPM SIA, S2B sec SHP SSR STBY or SBY TAS TBO TC L TEMP TODA TORA TQ v VFR VHF VMC VA VB VFE VFO VLE Y o VMCA VMCG VMCL quantity radio beacon right hand side radio magnetic indicator revolution per minute emergency bus bars seconds shaft horse power transponder (see also XPDR) standby true airspeed time between overhaul throttle control lever temperature take-off - distance available take-off run available torque speed or volt whichever applies visual flight rules very high frequency visual meteorological conditions design maneuvering speed design speed for maximum gust intensity maximum flaps extended speed maximum flaps operating speed maximum landing gear extended speed maximum landing gear operating speed minimum control speed for take-off minimum control speed for take-off run minimum control speed for landing (cont.) 1 - 1 6 (2) Apr 1/98 LET, a,*. CZECH REPUBUC SECTION I FLIGHT MANUAL GENERAL "MO vso VSPOIL VSI vx VY v1 - - - v2 VR WPT XPDR YD maximum operating limit speed stalling speed in the landing configuration maximum permissible spoiler extension speed stalling speed, with idle power, in a configuration other than landing best angle of climb speed best rate of climb speed take-off decision speed - - - - - - - take-off safety speed rotation speed waypoint transponder yaw damper SECTION I FLIGHT MANUAL L€r. ....CZECH REPUBUC CONVERSION TABLES 1. CONVERSION OF MM TO INCH 1 - 1 8 Mar 1/96 SECTION I LET, a.m. CZECH REPUBLIC FLIGHT MANUAL GENERAL 2. CONVERSION OF INCH TO M M Mar 1/96 1 - 1 9 SECTION I L 410 UVP-E20 FLIGHT MANUAL LET. a.3. GENERAL CZECH REPUBLIC 3. CONVERSION OF M TO FOOT 1 - 20 Mar 1/96 LET a.m. L 410 UVP-E20 SECTION I CZECH REPUBLIC FLIGHT MANUAL GENERAL 4. CONVERSION OF FOOT TO M Mar 1/96 SECTION I L 410 UVP-E20FLIGHT MANUAL LET, a.,. GENERAL CZECH REPUBLIC 5. CONVERSION OF KG TO POUND 1 - 2 2 Mar 1/96 SECTION I LET, a... CZECH REPUBLIC FLIGHT MANUAL GENERAL 6. CONVERSION OF POUND TO KG Mar 1/96 1 - 2 3 SECTION I GENERAL FLIGHT MANUAL LET. as. CZECH REPUBLIC Intentionally left blank 1 - 2 4 Mar 1/96

All LET L-410 UVP-E pilot's operating handbook