Technify Motors TAE 125-02-114 Guida alla configurazione
Technify Motors GmbH
Platanenstraße 14
D - 09356 St. Egidien
Tel. +49-(0)37204/ 696-0
Fax +49-(0)37204/ 696-2912
www.continentaldiesel.de
support@ccontinentaldiesel.de
Doc.-No.: 50-0310-50022
Approved Airplane Flight Manual Supplement
for the
DA 40 D
Equipped with
TAE 125-02-114 Engine Installation
Issue 2/0
This supplement must be attached to the EASA approved
Airplane Flight Manual when the TAE 125-02-114 engine has
been installed in accordance with EASA STC 10036328.
The information contained in this supplement supersedes or
adds to the EASA approved Airplane Flight Manual only as set
forth herein.
For limitations, procedures, performance and loading
information not contained in this supplement, consult the basic
EASA approved Airplane Flight Manual.
ThisAirplaneFlightManualSupplementisapprovedwithEASA
STC 10036328.
SERIAL No. _______________
REGISTER No. _______________
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AFM Supplement DA 40 D
Page iii
Issue 2
Revision -, Aug. 2015
LOG OF REVISIONS
Revision Chapter Description Approved
Date Endorsed
- All Initial Issue 1 Sept. 01,
2011 EASA STC
10036328
1/1 2 New fuel,
new gearboxoil March 16,
2012
Revision No. 1 to AFM supplement
ref. 50-0310-50021 is approved
under the authority of DOA
ref. EASA.21J.010.
Date: March 16, 2012
Office of Airworthiness
2/0 All Change of Ownership Aug. 15,
2015 EASA STC
10036328,
Rev. 3
2 New gearbox oil
New fuel,
new specs
5 splitted due to new
specs
5a New section
5b new section
6 Equipment list updated
Note: The parts of the text which changed are
marked with a vertical line on the margin of
the page.
AFM Supplement DA 40 D
Page iv
Issue 2
Revision -, Aug. 2015
LIST OF EFFECTIVE CHAPTERS
APPROVAL
The content of approved chapters is approved by EASA. All
other content is approved by TAE under the authority of EASA
DOA No. EASA.21J.010 in accordance with Part 21.
GENERAL REMARK
The content of this AFM supplement is developed on basis of
the EASA-approved AFM, DAI Document No. 6.01.05-E.
Chapter Issue/Revision Date
1 2/0 Aug., 2015
2 2/0 Aug., 2015
3 2/0 Aug., 2015
4A 2/0 Aug., 2015
4B 2/0 Aug., 2015
5a 2/0 Aug., 2015
5b 2/0 Aug., 2015
6 2/0 Aug., 2015
7 2/0 Aug., 2015
8 2/0 Aug., 2015
92/0 Aug., 2015
AFM Supplement DA 40 D
Page v
Issue 2
Revision -, Aug. 2015
TABLE OF CONTENTS
CHAPTER 1..........GENERAL
(a non-approved chapter)
CHAPTER 2..........OPERATING LIMITATIONS
(an approved chapter))
CHAPTER 3..........EMERGENCY PROCEDURES
(a non-approved chapter))
CHAPTER 4a........NORMAL OPERATING PROCEDURES
(a non-approved chapter)
CHAPTER 4b........ABNORMAL OPERATING PROCEDURES
(a non-approved chapter))
CHAPTER 5..........PERFORMANCE
(a non-approved chapter))
CHAPTER 6..........WEIGHT AND BALANCE /
EQUIPMENT LIST
(a non-approved chapter))
CHAPTER 7..........DESCRIPTION OF THE AIRPLANE AND
ITS SYSTEMS
(a non-approved chapter))
CHAPTER 8..........AIRPLANE HANDLING, CARE AND
MAINTENANCE
(a non-approved chapter))
CHAPTER 9..........SUPPLEMENTS
AFM Supplement DA 40 D
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Revision -, Aug. 2015
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AFM Supplement DA 40 D
Page 1-1
Issue 2
Revision -, Aug. 2015
CHAPTER 1
GENERAL
1.1 INTRODUCTION
This supplement must be attached to the EASA approved
Airplane Flight Manual when the TAE 125-02-114 engine has
been installed in accordance with EASA STC 10036328.
The information contained in this supplement supersedes or
adds to the EASA approved Airplane Flight Manual only as set
forth herein.
For limitations, procedures, performance and loading
information not contained in this supplement, consult the basic
EASA approved Airplane Flight Manual.
1.2 CERTIFICATION BASIS
The certification basis for the TAE 125-02-114 engine
installation is CS-23, dated November 14, 2003.
1.5 DEFINITIONS AND ABBREVIATIONS
(i) Miscellaneous
EASA: European Aviation Safety Agency
1.8 SOURCE DOCUMENTATION
UPDATE AND REVISION OF THE MANUAL
WARNING: A safe operation is only assured with an up
to date AFM supplement. Information about
actual AFM, supplement issues and
revisions are published in the Service
Bulletin TM TAE 000-0004.
Note: The Doc.-No of this AFM supplement is
published on the cover sheet of this
supplement.
AFM Supplement DA 40 D
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Revision -, Aug. 2015
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AFM Supplement DA 40 D
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Revision -, Aug. 2015
CHAPTER 2
OPERATING LIMITATIONS
2.4 POWERPLANT LIMITATIONS
a) Engine manufacturer: .......................Technify Motors GmbH
b) Engine designation:.....................................TAE 125-02-114
c) RPM limitations (shown as propeller PRM)
Maximum: .................................................................2300 RPM
Maximum overspeed:..........................2500 RPM (max 20 sec)
d) Engine Power
Max. take-off power: ................ 114 kW (155 HP) at 2300 RPM
Max. continuous power:........... 114 kW (155 HP) at 2300 RPM
Max. recommended cruise power:......................................85%
e) Oil Pressure
Min. oil pressure:.............................................................1.2 bar
Min. oil pressure (at Take-off power): .............................2.3 bar
Min. oil pressure (in flight):..............................................2.3 bar
Max. oil pressure:............................................................6.0 bar
Max. oil pressure (cold start < 20 sec.):..........................6.5 bar
g) Oil Temperature
Min. oil temperature (engine starting temp.): ....................-32°C
Min. oil temperature (min. operating limit temp.):...............50°C
Max. oil temperature:.......................................................140°C
h) Coolant Temperature
Min. coolant temp. (engine starting temp.):.......................-32°C
Min. coolant temp. (min. operating limit temp.):.................60°C
Max. coolant temperature:...............................................105°C
AFM Supplement DA 40 D
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Revision -, Aug. 2015
j) Manufacturer:......................MT Propeller Entwicklung GmbH
k) Model: ....................................................... MTV-6-A/187-129
........................................................................ MTV-6-A/190-69
l) Propellerdiameter:........................1.87 m (MTV-6-A/187-129)
..........................................................1.90 m (MTV-6-A/190-69)
m) Propeller pitch angle (0.75R):............................13.5° to 28°
n) Oil Specification:............AERO SHELL OIL DIESEL ULTRA
....................................................SHELL HELIX ULTRA 5W-30
....................................................SHELL HELIX ULTRA 5W-40
..........................................AERO SHELL OIL DIESEL 10W-40
o) Coolant: ...........Water/Radiator Protection at a ratio of 50:50
Radiator Protection:............. BASF Glysantin Protect Plus/G48
........................................................Mobil Antifreeze Extra/G48
.......................................................ESSO Antifreeze Extra/G48
.............................. Comma Xstream Green - Concentrate/G48
..................................................................Zerex Glysantin G48
p) Gearbox Oil:..........................Shell Spirax S6 GXME75W-80
.........................................................Shell Spirax S4 G 75W-90
......................................Shell Getriebeöl EP 75W-90 API GL-4
............................................................ Shell Spirax EP 75W-90
CAUTION: The use of water which does not meet the
specifications according to the applicable
OM-02-02 may cause engine damage.
CAUTION: If the coolant level is too low the reason
must be determined and the problem must
be corrected by authorized personnel.
Indice
Altri manuali Technify Motors Motore
