Georg Küper Profil

Profil
Georg Küper
Vita
2. Mai 1957
1977-1978
1978-1982
1982-1985
1984
1991-1992
seit 1982
1990-1992
1993
1994-2002
2003
geb. in Essen
Vorbereitung zum Musikstudium durch Prof. Helmuth Weinrebe, Köln.
Studium an der Musikhochschule Aachen,
Abschluß: Diplom Instrumentalpädagogik.
Hauptfachunterricht bei Prof. Ulla Graf.
Privatstudium bei der rumänischen Pianistin Rosemarie Mastero.
Meisterkursus Klavier bei Jacques Chapuis, Lion.
Privatstudium bei Prof. Werner Seiss, Dortmund.
Tätig als Pianist, Komponist, Pädagoge, Korrepetitor und Chorleiter.
Grafiker, Marketing Assistent, später Marketing Leiter bei MAG, Bochum
Fortbildung bei DAA Recklinghausen
Abschluß: Technischer Redakteur
Technischer Redakteur bei EXTRA Flugzeugbau GmbH, Hünxe
Selbständigkeit in den Bereichen Musik, Fotografie, Marketing, technische
Redaktion
Marketing
Wasserburg Lüttinghof
Haus für Kultur, Innovation
und interdisziplinären Austausch
in inspirierender Atmosphäre
Corporate Design
Pressearbeit
Anzeigen
Mailings
Flyer
Prospekte
Präsentationen
Grafische Entwürfe
Firmenlogos
Messeplanung
Messestandentwurf
r
Traditionelle
Chinesische Medizin
ganzheitliche Diagnostik
Akupunktur
Kräuterheilkunde
Chinesische
Ernährungsberatung
begleitende
Sauerstofftherapie
Am Anfang steht immer
eine gute Idee
Pilot’s Operating Handbook
EA-400
Technische Dokumentation
Section 921
Moritz Instrumentation Package
Pilot’s Operating Handbook
EA-400
920
920.1
Section 920
GARMIN GTX 327
GARMIN GTX 327
Section 1 - General
The GARMIN GTX 327 is a panel-mounted TSO.d transponder
with the addition of timing functions. The transponder is a radio
transmitter and receiver that operates on radar frequencies, receiving ground radar interrogations at 1030 MHz and transmitting a coded response of pulses to ground-based radar on a
frequency of 1090 MHz.
The GTX 327 owner accepts all responsibility for obtaining
the proper license before using the transponder.
Bedienungsanleitungen
Flughandbücher
Wartungshandbücher
Teilekataloge
Service Bulletins
Pressetexte
921-5
Pilot’s Operating Handbook
EA-400
Section 7
Description of the Airplane and its Systems
GARMIN GTX327
Figure 920-1
SWITCHES ON
EXT PWR
BATT
MAIN
The coverage you can expect from the GTX 327 is limited to
“line of sight”. Low altitude or aircraft antenna shielding by
the aircraft itself may result in reduced range. Range can be
improved by climbing to a higher altitude. It may be possible
AVIONIC MASTER
to minimize antenna shielding by locating the antenna where
ALT 1
ALT 2
RADIO 1 RADIO 2
EFIS
dead spots are only noticed during abnormal flight attitudes.
STROBE
The GTX 327 should be turned off before starting or shutting
down aircraft engine.
LDG
RECO
MAP
INSTR
DOME
LIGHTS
SWITCHES 920-3
CABIN
NIGHT
ICE*
DAY
DUMP
AIR CON VENT
Pilot’s Operating Handbook
EA-400
PITOT L PITOT R
PRESS
HEAT
CABIN
HI
LO
Section 2
Limitations
OFF
TEST
TEST
VFR- VFR- IFR- IFRICE
Day Night Day Night
DEICESystem and/or Equipment
PROP
WINDSH BOOTS
HI**
LO**
Horizontal Stabilizer Trim Position
Indicator
DC BUS 1
CIRCUIT
BREAKERS
*) From S. No 28
**) Up to S. No 27
7-10
DC BUS 2
HYDR
RADIO 2
GEAR CTRL
1
1
1
1
1
Maintenance Manual and Illustrated Parts Catalogue
Extra EA-400
Time Limits and Maintenance Checks
1
1
1
1
1
05-23-00
1
1
1
1
1
1
1
1
1
1
Fuel System
MAIN CB
RADIO 1
Boost Pump
Fuel Flow Indicator
SWITCHES OFF
PULL TO
EXTEND
Fuel Pressure Indicator
Left Side Panel
Figure 7-6
Fuel Quantity Indicator
Low Fuel Annunciation
Light
Issued:
15.
October
1999
Issued:
15. July 2002
2
2
2
2
2
1
1
1
1
1
The maintenance checks described in this section include all the scheduled
checks, which must be performed. Maintenance checks must be accomplished
in accordance with CFR 14 P 43 App. D.
Pilot’s Operating Handbook
EA-400
2.6
Scheduled Maintenance Charts
Section 2
Limitations
Use the following schedule and the lubrication charts.
Powerplant Instrument Markings
Prior to inspection, the aircraft and engine should be thoroughly cleaned, all
inspection panels, access doors or fairings should be removed.
Landing Gear
Landing Gear Position Indication (3x
green)
Landing Gear Warning Horn
Landing Gear Warning Light
1
Section 1
General
1.12
1
1
1
Landing Gear Hydraulic Pump
1.12a
Hydraulic Pump Operating Annunciation
Light
CAS
KCAS
1
Landing Light
GS
Landing Light Operation Indication Light
Navigation Light System
IAS
Issued: 15. October
July 20021999
KIAS
TAS
VO
1
1
1
1
1
1
1
1
1
1
1
Instrument
1
1
1
1
1
1
1
1
1
Calibrated Airspeed means the indicated speed of an air
craft, corrected for position and instrument error. Calibrat ed airspeed is equal to true airspeed in standard
atmosphere at sea level.
1
1
1
1
Calibrated Airspeed expressed in “knots”.
1
1
1
Ground Speed is the speed of an airplane relative to the
1
1
1
ground.
1
1
1
1
Indicated Airspeed is the speed of an aircraft as shown in
the airspeed indicator when corrected for instrument error.
IAS values published in this handbook assume zero instru
2-11
ment error.
Indicated Airspeed expressed in “knots”.
True Airspeed is the airspeed of an airplane relative to undisturbed air which is the CAS corrected for altitude, tem perature and compressibility.
Operating maneuvering Speed is the maximum speed at
which application of full available aerodynamic control
will not overstress the airplane.
VFE
Maximum Flap extended speed is the highest speed per missible with wing flaps in a prescribed extended position.
VLE
Maximum Landing Gear Extended Speed is the maximum
speed at which an aircraft can be safely flown with the lan ding gear extended.
VLO
Min.
Limit
Pilot ’s Operating Handbook
EA-400
Symbols, Abbreviations and Terminology
General Airspeed Terminology and Symbols
1
Lights
Anti-Collision Light System
1
Red
Line
Yellow Arc Green Arc Yellow Arc
05-23-01
Caution
Range
Manifold Pressure
in. Hg.
bar
0-37.5
0-1.27
Exhaust Gas Temp.
°C
°F
93-191
200-375
Oil Temperature
°C
°F
38
100
Oil Pressure
bar
PSI
0.7
10
77-93
170-200
0.7-2.1
10-30
66
150
Fuel Pressure
bar
PSI
2.1-4.1
30-60
82-93
180-200
0-0.21
0-3
0.21-0.41
3-6
Turbine Inlet Temp.
°C
°F
4.5
Inspector
Serial No.:
Mechanic
Description
39.5
1.34
Rotating propeller can cause death or injuries!
954 Ground magneto primary circuit before working on engine.
1750
X
X
X
X
X
X
191
375
Perform an inspection operational run-up. Refer to the latest
TCM Operation and Maintenance Instructions (Form OMI-15),
Section 2. Record and verify the engine operating parameters.
Start engine (in accordance with the Pilot's Operating Handbook).
X93-110
X
X110 Check the parking brake and toe brakes.
X200-230
X
X230 Check the fuel flow, fuel pressure and fuel quantity indication.
X 4.1-7X
X 7 Check the fuel pump and fuel selector valve.
X60-100
X
X100 Check the oil pressure and oil temperature.
X
X
X
X
X
X
Check the cabin heater operation.
X
>0.41
>6 X
X
Check the cabin pressurizing operation.
X
X
X
Check the aircon operation.
X
X
X1750 Check the de-ice system operation.
X
X
X
X
X
X
93-110
X200-230
X
4.5-5.2
Issued: 15.
October 1999
8. December
2000
Maximum Landing GearOperating Speed is the maximum
speed at which the landing gear can be safely extended
or retracted.
Issued: 15. October 1999
37.5-39.5
1.27-1.34
WARNING
Page 14
1-8
Caution or Max.
TakeoffHoursLimitDate:
Flight
650-954
1200-1750
Cylinder Head
Temp.
°C
°F
Vacuum Diff. Press.
in. Hg
Operational Checks
600-2,500 2,500-2,600 2,600
Tachometer, RPM
Coolant
Temperature
°C
°F
Normal
Operating
Red
Line
1000
Issued:
1999
Issued:15.
13.October
July 2001
100
The GTX 327 Transponder is powered on by pressing the STBY,
ALT or ON keys, or by the respective AVIONIC MASTER
NAV
asspecified
Caution
50
Figure 921-3
Notes
Issued: 15.
1999
13. October
September
2001
110
Check the alternator 1 + 2 output.
X230 Check the manifold pressure indicator.
954
Check the windshield heater operation.
5.2
Check magneto RPM drop at 1700 RPM (allowed drop is 150
RPM and no greater difference between L + R than 50 RPM).
2-7
Check
X
X
X
X
X
X
Check response of the engine by power setting changes.
X
X
X
Check the propeller response at 1700 RPM when changing pitch.
05
idle speed (between 600 and 750 RPM).
Page Date: 5. July 2002
Portrait
Architektur
Technik
Makro bis 1:1
Mikro bis 1:10
künstlerisch
Fotografie
Musik
Pianist
Pädagoge
Komponist
Chorleiter
Weiteres
SAMPLE SEQUENCE CONSTRUCTION
1.6.1
9.1.1.6
9.9.1.4
10
15
15
40
Fig 2
1.14.3
9.1.4.6
9.4.1.5
15
10
18
43
Fig 3
1.35.3
9.11.1.4
9.1.5.1
9.1.2.2
9.10.7.4
9.10.5.3
9.1.5.1
25
5
2
6
17
13
2
70
Fig 4
5.1.3
9.1.1.8
9.9.5.4
18
18
11
47
Fig 5
8.2.2
9.4.1.4
9.8.5.2
9.4.5.2
17
15
7
5
44
Fig 6
8.57.1
9.4.2.8
9.1.5.6
12
22
10
44
Fig 7
7.9.1
9.1.2.4
9.2.4.4
15
10
9
34
Fig 8
6.2.1
9.2.1.4
9.10.5.4
9.4.5.3
15
13
13
8
49
Fig 9
1.7.1
9.1.1.1
9.10.1.4
9
6
17
32
Fig 10
2.15.4
25
25
Fig 11
8.16.1
9.1.2.2
9.10.9.6
14
6
19
39
Fig 12
1.1.1
9.4.3.2
9.8.3.2
2
5
7
14
2
1/4
3
Fig 1
4
1
1/4
3/4
1/4
4/8
4
4
8
2/4
4
4
6
BREAK
5
2
2
7
11
8
10
3/4
9
1/4
12
2/4
4
4
8
4/8
Total K = 481
Figure 26
15
2nd Edition, 1999
Luftfahrerschein für Segelflugzeuge (PPLC)
Kunstflugberechtigung
Führerschein Kl. 1 + 3
Technisches Englisch
Softwarekenntnisse:
Microsoft Office, Autocad,
Corel Draw, Corel Photo Paint,
Corel Ventura, Pagemaker
www.georgkueper.de