DG Flugzeugbau LS8-st User manual

Maintenance Manual LS8-st Contents
Edition: June 2016 Rev. 6 TN 8024 0-1
0 Manual Contents
0.1 Log of Revisions
Rev
no. Pages Reference Rev. date
1 0-1, 0-3, 0-4, 0-5, 0-6, 0-8, 0-11, 1-
27, 3-4, 4-16, 4-19, 4-21,
10-2, 10-8, 11-2, 11-18, 11-20
TN 8017, necessary changes to
the power plant
Nov.
2010
2 0-1, 0-3, 0-7, 1-1, 1-7,
1-11, 1-12, 8-3 TN8019, wheel brake actuated by airbrake handle. Feb. 2011
3 Title page, 0-1, 0-3, 0-4, 0-6 ÷ 0-8,
0-11, 1-3, 1-7 ÷ 1-9, 1-22, 1-29,
1-36, 1-40, 1-48a, 4-1, 4-21, 4-27,
6-4, 10-2a, 11-15, 9E2
ÄM LS8-1, Miscellaneous
improvements Ser.no. 8474
and from ser. No. 8527 on
December
2011
4 0-1, 0-3, 0-7, 1-17, 8-1 TN 8021
Small tailwheel January 2015
5 0-1, 0-4 up to 0-8, 1-28, 1-30, 3-7,
4-12, 4-13, 4-23, 4-24, 4-28, 6-1,
6-2, 9-1, 10-2, 10-2a, 10-9
Mechanical fuel pump
Manual revision
TN 8022
October
2015
6 0-1, 0-3, 0-6 ÷ 0-8, 0-12, 1-10, 4-11,
5-3, 5-4, 5-6, 6-2, 8-1, 8-2, 9-1, 9-2,
10-2
TN 8024
Manual revision, repair manual June 2016

Maintenance Manual LS8-st Contents
Edition: June 2016 Rev. 6 TN 8024 0-3
0.2 List of Effective Pages
Chapter Page Edition Replaced Replaced Replaced
0 Title page April 2005 Dec. 2011
0-1 See log of revisions
0-2 See log of revisions
0-3 See log of revisions
0-4 See log of revisions
0-5 See log of revisions
0-6 See log of revisions
0-7 See log of revisions
0-8 See log of revisions
0-9 April 2005
0-10 April 2005
0-11 April 2005 Nov. 2010 Dec. 2011
0-12 April 2005 June 2016
0-13 April 2005
1 1-1 April 2005 Feb. 2011
1-2 April 2005
1-3 April 2005 Dec. 2011
1-4 April 2005
1-5 April 2005
1-6 April 2005 June 2016
1-7 April 2005 Feb. 2011 Dec. 2011
1-8 April 2005 Dec. 2011
1-9 April 2005 Dec. 2011
1-10 April 2005 June 2016
1-11 April 2005 Feb. 2011
1-12 April 2005 Feb. 2011
1-13 April 2005
1-14 April 2005
1-15 April 2005
1-16 April 2005
1-17 April 2005 Jan. 2015
1-18 April 2005
1-19 April 2005
1-20 April 2005

Maintenance Manual LS8-st Contents
Issued: June 2016 Rev. 6 TN 8024 0-6
0.2 List of Effective Pages (continued)
Chapter Page Edition Replaced
Replaced Replaced
4 4-1 April 2005 Dec. 2011
4-2 April 2005
4-3 April 2005
4-4 April 2005
4-5 April 2005
4-6 April 2005
4-7 April 2005
4-8 April 2005
4-9 April 2005
4-10 April 2005
4-11 April 2005 June 2016
4-12 April 2005 Oct. 2015
4-13 April 2005 Oct. 2015
4-14 April 2005
4-15 April 2005
4-16 April 2005 Nov. 2010
4-17 April 2005
4-18 April 2005
4-19 April 2005 Nov. 2010
4-20 April 2005
4-21 April 2005 Nov. 2010 Dec. 2011
4-22 April 2005
4-23 April 2005 Oct. 2015
4-24 April 2005 Oct. 2015
4-25 April 2005
4-26 April 2005
4-27 April 2005 Dec. 2011
4-28 April 2005 Oct. 2015
4-29 April 2005
4-30 April 2005

Maintenance Manual LS8-st Contents
Edition: June 2016 Rev. 6 TN 8024 0-7
0.2 List of Effective Pages (continued)
Chapter Page Edition Replaced
Replaced Replaced
5 5-1 April 2005
5-2 April 2005
5-3 April 2005 June 2016
5-4 April 2005 June 2016
5-5 April 2005 June 2016
5-6 April 2005
5-7 April 2005
5-8 April 2005
5-9 April 2005
5-10 April 2005
5-11 April 2005
5-12 April 2005
5-13 April 2005
5-14 April 2005
5-15 April 2005
5-16 April 2005
5-17 April 2005
5-18 April 2005
6 6-1 April 2005 Oct. 2015
6-2 April 2005 Oct. 2015 June 2016
6-3 April 2005
6-4 April 2005 Dec. 2011
7 7-1 April 2005
8 8-1 April 2005 Jan. 2015 June 2016
8-2 April 2005 June 2016
8-3 April 2005 Feb. 2011
9 9-1 April 2005 Oct. 2015 June 2016
9-2 April 2005 June 2016
9-3 April 2005

Maintenance Manual LS8-st Contents
Issued: June 2016 Rev. 6 TN 8024 0-8
0.2 List of Effective Pages (continued)
Chapter Page Edition Replaced
Replaced Replaced
10 10-1 April 2005
10-2 April 2005 Nov. 2010 Oct. 2015 June 2016
10-2a Dec. 2011 Oct. 2015
10-3 April 2005
10-4 April 2005
10-5 April 2005
10-6 April 2005
10-7 April 2005
10-8 April 2005 Nov. 2010
10-9 April 2005 Oct. 2015
11 11-1 April 2005
11-2 April 2005 Nov. 2010
11-3 April 2005
11-4 April 2005
11-5 April 2005
11-6 April 2005
11-7 April 2005
11-8 April 2005
11-9 April 2005
11-10 April 2005
11-11 April 2005
11-12 April 2005
11-13 April 2005
11-14 April 2005
11-15 April 2005 Dec. 2011
11-16 April 2005
11-17 April 2005
11-18 April 2005 Nov. 2010
11-19 April 2005
11-20 Nov. 2010
4E01-02 26.05.2005
2E01-01 28.07.2005
9E2 28.11.2008

Maintenance Manual LS8-st Contents
Issued: June 2016 Rev. 6 TN 8024 0-12
0.4 L
IFE L IMITED P ARTS , M AINTENANCE I NSTRUCTIONS
0.4.1 Repairs
Repair or replace damaged parts prior to next flight. Follow the
instructions in the Repair Manual LS8.
Major repairs must be accomplished by an approved repair station or by an
approved mechanic rated for composite aircraft structure work in
accordance with DG repair methods.
Use only genuine spare parts.
For all aircraft under EASA regulations the following applies: According
to part 21, subpart M to accomplish major repairs an approved repair
instruction is required, see also TN DG-G-01 “Approved repair methods
according to EU Commission Regulation 1702/2003 part 21, subpart M”
0.4.2 Airframe structural Life limit
Maximum FRP structural life limit of sailplanes and powered sailplanes is
12000 hours of flight. To reach this limit, special inspections according to
chapter 2.4 of this manual at 3000, 6000, 9000 and beyond that at every
1000 hours of flight must be performed.
0.4.3 Life Limits of Equipment Items
a) Rubber fuel hose (connection between main and feeder tanks) and
drainer sealing (Mogas resistant O-Ring) have a 6 year life limit
and must be exchanged accordingly.
b) Spark plugs have a 25 hours engine time limit and must be
exchanged accordingly.
c) Safety harness webbing life limited to 12 years after manufacture.
Multiple point buckle and brackets on condition (Wear, corrosion
etc.).
d) Further parts:
These parts as for instance wheels, gas struts, control system parts,
pins and bushes are not life limited, but may require exchange based
on condition (Wear, damage, corrosion).

Maintenance Manual LS8-st Systems
Edition: June 2016 Rev. 6 TN 8024 1-10
1. S YSTEM D ESCRIPTION AND A DJUSTMENT D ATA (continued)
1.4 Elevator Control System (continued)
1.4.2 Deflections and Tolerances
Elevator: up 28° - 30°
down 22° - 26°
For easier checking, measured angles may be converted to mm / in
deflection values, using the actual local radius of the defined measuring
place. See also table below.
Limit values for elevator deflections in Millimetres/Inches
local radius 22°to 26° 28°to 30°
down up
mm in mm in mm in
67 2.638 26 to 30 1.024 to 1.181 32 to 35 1.260 to 1.378
68 2.677 26 to 31 1.024 to 1.220 33 to 35 1.299 to 1.378
69 2.717 26 to 31 1.024 to 1.220 33 to 36 1.299 to 1.417
70 2.756 27 to 31 1.063 to 1.220 34 to 36 1.339 to 1.417
71 2.795 27 to 32 1.063 to 1.260 34 to 37 1.339 to 1.457
72 2.835 27 to 32 1.063 to 1.260 35 to 37 1.378 to 1.457
1.4.3 Stops
Elevator stops at lower control stick end. Adjustment by use of two
10◦mm open end wrenches.
1.4.4 Elevator Rear Edge Play
Play should be measured with control stick fixed to neutral position.
Elevator : maximum 2.5 mm <0.1 in> at inner edge

Maintenance Manual LS8-st Instructions
Edition: June 2016 Rev. 6 TN 8024 4-11
4.5 Installation of Control Surfaces (continued)
Disassembly of Rudder
(1) disconnect rudder cables.
Attention: Don’t loose spacing casings.
Attention: Rudder cables may be drilled. If this is changed
unintentionally, neutral positions of rudder and pedals do no longer
correspond and must be realigned as detailed below.
(2) loosen nut at lower bearing (6mm thread, M6 LN 9348 or DIN 985-8zn,
width over flats 10mm) using a socket wrench, remember sequence and
position of washers.
(3) lift rudder upward from bearings.
Assembly of Rudder
(1) grease bearings according to lubrication schedule, see section 3.3.
(2) If need be, install new V-type internal seal, see section 4.6.
(3) lower rudder into bearings, do not use force !
(4) check radial play of upper bearing: maximum permissible radial play 0.5
mm <0.02 in>. If necessary renew brass bushing. Make sure, that non-
concentric position of bearing keeps relative position to direction of flight.
Bond bushing with for instance Loctite 72 b (672).
(5) connect rudder cables provisionally, do not forget to insert spacing casings
into thimbles.
(6) check rudder pedal alignment: with pedals in neutral position check if
rudder is neutral.
If rudder is deflected to one side, twist opposite cable counter-clockwise
(maximum 5 turns) until properly aligned.
Should more than 5 turns be necessary for alignment, exchange cables.
Caution: Never turn cables clockwise !
(7) place washers on cable connection bolts and tighten nuts M6 LN 9348 or
DIN 985-8zn, width over flats 10 mm, with maximum torque 6.4 Nm
(0.65 mkg, 4.623 ft lbs).
(8) set up washers at lower bearing as found during disassembly (normally:
recessed washer first, then large washer). Tighten nut (6 mm thread, LN
9348 or DIN 985-8zn, width over flats 10 mm) with maximum torque 6.4
Nm, (0.64 mkg, 4.623 ft lbs). After assembly the rudder should have
audible axial play, maximum axial play 1 mm (0.04 in), see section 1.5.
(9) if necessary, restore gap seals (convex plastic strip) on both sides, see
section 4.6.

Maintenance Manual LS8-st Weight and Balance
Edition: June 2016 Rev. 6 TN 8024 5-3
5.2 Calculation of Loading Limits
1. Determine Minimum Cockpit Load for 15 m wingspan and full and empty
tail fin tank version following procedure given in section 5.1 from table
“Empty Weight C.G. Position”, section 5.4 in <kg/mm> or <in/lbs>.
Minimum Cockpit Load for tail fin battery (3BR-199) removed (and
installed in baggage compartment, when required) decreases by 10 kg
<22 lbs>.
Finally resulting 4 different cockpit loads should be entered in the
following places:
a. in weighing report of inspection
b. in Flight Manual section 6.2
c. in cockpit placard under instrument panel cover
d. in cockpit on data placard
1. Minimum Cockpit Load for full tail fin tank with tail fin battery
2. Minimum Cockpit Load for empty tail fin tank with tail fin battery
3. Minimum Cockpit Load for full tail fin tank without tail fin battery
4. Minimum Cockpit Load for empty tail fin tank without tail fin battery

Maintenance Manual LS8-st Weight and Balance
Edition: June 2016 Rev. 6 TN 8024 5-4
5.2 Calculation of Loading Limits (continued)
2. Maximum approved Weight of Non-lifting Parts may vary between
305◦kg and 315 kg <672 to 694 lbs>, depending on empty weight and
empty weight C.G. position.
In contrast to methods used up to now, maximum weight of non-lifting
parts can be determined in relation to empty weight and empty weight
C.G. position according to table in section 5.3. See also examples on end
of this section.
Maximum weight of Non-lifting Parts should be entered into weighing
report.
3. Determine Maximum approved Cockpit Load from table “Empty Weight
C.G. Position”, section 5.4 <kg/mm> or <in/lbs>. Maximum Cockpit
Load normally should be 110 kg <243 lbs>, as given in empty weight
C.G. table. It may be lower due to trim conditions, excessive equipment or
repairs.
Calculate Maximum Cockpit Load on weighing report, see also examples
at end of this section.
Resulting Maximum Cockpit Load should be entered in the following
places:
a. in weighing report of inspection
b. in Flight Manual, section 6.2
c. on Data Placard in cockpit
4. Empty Weight (perhaps increased by weight of permanently fitted trim
ballast) should be entered in the following places:
a. in weighing report of inspection
b. in Flight Manual section 6.2 for calculation of maximum
permissible water ballast weight
5. Battery position during weighing should be entered in the following
places:
a. in weighing report and equipment list of inspection
b. in section 6.2 of Flight Manual
6. Enter engine installed or removed in Flight Manual section 6.2.
For permanent installation of trim ballast weights, see Maintenance
Manual section 4.15.
Form for Weighing Report, see Maintenance Manual section 11.

Maintenance Manual LS8-st Weight and Balance
Edition: June 2016 Rev. 6 TN 8024 5-6
5.2 Calculation of Loading Limits (continued)
Example for entry in Flight Manual section 6.2:
Wing span [m] 15 18
Empty Mass
[kg] /
[lbs]
316 325
C.G. position
[mm] /
[in]
649
Fuel tank full
[kg] /
[lbs]
110
Max. Cock- pit Load
Fuel tank partly filled
[kg] /
[lbs]
110
Tail tank
full
[kg] /
[lbs]
130
with tail-
battery Tail tank
empty (+)
[kg] /
[lbs]
90
Tail tank
full (+)
[kg] /
[lbs]
120
Minimum Cockpit Loadg
without tail-
battery Tail tank
empty (+)
[kg] /
[lbs]
80
front
[kg] /
[
lbs
]
---
Perm.
fixed Trim
mass
rear
[kg] /
[
lbs
]
---
Seat [No.]
2
Baggage comp.
[No.] 0
Batteries
installed Vert. tail fin
[No.] 1
Engine ( INstalled / REmoved ) IN
Date / Inspector 18.08.2005
GS
The discrepancy between Maximum Cockpit Load of 110 kg <242 lbs> and
Minimum Cockpit Load of 130 kg <286 lbs> with tail fin tank full and tail
fin battery indicates, that before each take off the installation position of
the tail fin battery must be checked and a functional check for the tail fin
tank valve is required to make sure that no unintended amount of water
remains in the fin tank.
To check the valve place tail tank filling adapter into the tank outlet and
open the cockpit lever. If air cannot be blown into the tank, the valve is not
functioning properly (for instance frozen solid or operating cable
fractured).

Maintenance Manual LS8-st Instruments and. Equipment
Edition: June 2016 Rev. 6 TN 8024 6-2
6.3 Seat Belt Harness (with multiple point buckles)
Manufacturer Type TCDS No.
Schroth 4-01-0.104 (Lap belt and
shoulder strap) 40.073/11
Gadringer Lap belt 5202 40.070/32
Shoulder strap 2700 40.071/05
6.4 Compass
Manufacturer Type TCDS No.
Ludolph FK 16, FK 5, FK 10 10.410/3
Airpath C 2300, C 2400 TS 10.220/47
PZL BS1, KJ-13A FD 19/77
Bohli 46 MFK 1 Not approved, only as
additional system
6.5 VHF transceiver
Manufacturer Type TCDS No.
Dittel FSG-40 S 10.911/45
FSG-50 10.911/71
FSG-60 M 10.911/72
FSG-70,71 M 10.911/81
FSG-90 10.911/98JTSO
FSG 2T LBA.0.10.911/103JTSO
Becker AR 3201-(1) 10.911/76
AR 2008/25 (A) 10.911/48
AR 4201 JTSO-2C37 D, ED-23A
AR 6201 EASA.210.1249
Avionik Dittel ATR 720 A 10.911/74
ATR 720 C 10.911/83
ATR 600 LBA.0.10.911/106JTSO
ATR 500 LBA.0.10.911/113JTSO
ATR 833 EASA.210.0193
Dittel Avionik KRT2 EASA.210.10038036
or other radios approved according to TSO, JTSO or ETSO for use in aircraft.

Maintenance Manual LS8-st Placards
Edition: June 2016 Rev. 6 TN 8024 8-1
8. Markings and Placards
LS8-st Checklist
This powered sailplane must be operated in
compliance with operating limitations stated in
the form of markings, placards and Flight
Manual. Under instrument panel cover
1. Main pins secured ?
2. Horizontal tail secured ?
3. Winglets secured ?
4. Test controls ?
5. Tail fin valve operating checked ?
6. When water ballast, then always
in wings and tail tank !
7. Check loading conditions
8. Check tail dolly removed
9. Fasten seat belt harness
10. Connect parachute static line
11. Lock air brakes
12. Check trim position
13. Check release system
14. Lock canopy
15. Propulsion system ready for use ?
16. Sufficient amount of fuel ?
17. Propulsion system retracted?
At underside of instrument panel
Tyre pressure
3.5 bar on right
(51 psi) landing gear door
Tyre pressure above tail wheel,
2.5 - 3.5 bar when fitted
(36 to 51 psi)
At right cockpit wall
at Baggage Compartment
Maximum Baggage weight 5 kg (11 lbs) Ball of bearing at forward horizontal tail
(For soft items only) must be fixed attachment on vertical tail fin
DG-Flugzeugbau GmbH
TYPE LS8-t . CLOSED ◄Fuel Cock ►OPEN
TCDS- No. 902 . Right Cockpit side at fuel cock
Serial Number 8xxx .
Reg. Signs D-xxxx . OPEN ◄Deco ►CLOSED
Type placard at main bulkhead Left Cockpit side at Deco-lever
Refueling pump at instrument panel
Tyre Pressure above tailwheel
6,2 bar/90 psi small tailwheel according to TN 8021, if installed
MINIMUM COCKPIT LOAD: kg / lbs
with tail battery, tail tank full min. ________
with tail battery, tail tank empty min. ________
without tail battery, tail tank full min. ________
without tail battery, tail tank empty min. ________
DG Flugzeugbau GmbH
Type: LS8-t Serial No.:_______
Data Placard
Airspeed Limits: km/h Kt MPH.
Winch launch/Auto tow 140 76 87
Aero tow 195 105 121
In rough air 195 105 121
Never exceed (VNE) 280 151 174
Extend/retract engine 110 59 68
Engine extended 160 99 86
m ft kg lbs
Max. Take-off Mass *) 15 42 525 1157
with 4“-wheel: 18 59 525 1157
with 5“-wheel: 18 59 575 1267
*) including water ballast
Aerobatic manoeuvres not approved
Take-off under own power not approved
Weight Limitations
Maximum Cockpit Load max. ______kg/lbs
Minimum Cockpit Load
with tail battery, tail tank full min. ______kg/lbs
with tail battery, tail tank empty min. ______kg/lbs
without tail battery, tail tank full min. ______kg/lbs
without tail battery, tail tank empty min.______kg/lbs
Lighter pilots must compensate lack of weight as
suggested in Flight Manual

Maintenance Manual LS8-st Placards
Edition: June 2016 Rev. 6 TN 8024 8-2
8. Markings and Placards (continued)
▲Soaring at instrument panel FUEL: Two stroke Mixture 1:40 of
Vario ASI Static/pitot switches Unleaded Four Star/Premium min. 95 ROZ
▼powered (Option) or AVGAS 100 LL
with 2-stroke oil Castrol Super TT/TTS
at left side of main bulkhead near
refuelling pump
16 Right- and left When using a battery in the
15 at main fuel tank front vertical tail fin. Minimum
14 Cockpit Load must be
13 redetermined by weighing
12 Use vertical tail fin battery only
11 with main fuse at battery
10 at vertical tail fin battery cover
9
8
Canopy Emergency Release: open left side normally,
pull right side with approx.15 kg/33 lbs force to stop
at right canopy frame
Altitude related
Never Exceed Speed km/h
Altitude related Never
Exceed Speed km/h Kt. mph
Up to 2000 m MSL 280 Up to 6500 ft MSL 280 151 174
Up to 3000 m MSL 266 Up to 9800 ft MSL 266 144 165
Up to 4000 m MSL 253 Up to 13100 ft MSL 253 136 157
Up to 6000 m MSL 227 Up to 19700 ft MSL 227 122 141
Up to 8000 m MSL 202 Up to 26200 ft MSL 202 109 126
Up to 10000 m MSL 179 Up to 32800 ft MSL 179 97 111
Up to 12000 m MSL 156 Up to 39400 ft MSL 156 84 97
On panel near airspeed indicator, On panel near airspeed indicator
for countries operating with metric
units only.
DEI-NT Placarding
0-5500
17 5500-6000
0,3 L 6000 RPM
Above DEI-NT Display
on
Fuel pump
off on
Kraftstoffpumpe
Main
Haupt-
schalter
auto
Below DEI-NT Switches

Maintenance Manual LS8-st Placards
Issued: June 2016 Rev. 6 TN 8024 9-1
9. Parts List
In this list, the most important parts of propulsion system, electrical system as
well as components of control surface sealing and water ballast system are
provided.
For drawing numbers of control system parts refer to diagrams section 1. For
drawing numbers of propulsion system brackets refer to diagrams section 10.
9.1 Engine parts
a) necessary for the 25 hours inspection
40050360 Spark plug S36 (Bosch W5AC Electrode gap 0,5 mm <0,02
in>) with pressed on screw cap, marked by red dot on
insulator.
60507571 Fuel filter
b) Spare parts
45002085 Spark plug cap Denso, 5kOhm
60510601 Ignition coil for SOLO 2350
45002081 Exhaust gasket, 1.5mm thick (2 units required)
45002071 Decompression valve (2 units installed)
45002088 Lift cylinder for LS8-t, HG7000-12-225-30, modified
45002038 Gas strut 600N for extension-retraction mechanism
45002039 Gas strut 100N for propeller stopper
45002074 Propeller stopper rubber stop
Shock mounts for engine installation
45002079 Upper engine shock mounts (2 units installed)
45002080 Lower engine shock mounts (2 units installed)
Fuel system
60507608 Fuel quick connector KL-006-2-SL007
(Coupling for re-fuelling line)
60507550 Drainer CAV 110 (1/8“ NPT)
Caution: Exchange O-ring (Avgas type) as delivered with drain valve against
part No. 60504402 !
60504402 O-Ring for Drainer CAV 110 (Mogas type)
30092049 Fuel hose PUR 3x1,5x6mm hydrolyse and microbe-resistant
30092050 Fuel hose PUR 5x1,5x8mm hydrolyse and microbe-resistant
60000103 Fuel hose PUR 6x1,5x9 hydrolyse and microbe-resistant
60000102 Fuel hose PUR 8x2x12 hydrolyse and microbe-resistant
30092051 Metal mesh inner dia. 8 mm (for fuel lines)
60507525 Fuel hose with textile farbic 9,5x15
60507561 Electric fuel pump Facet 40106 (engine fed and re-fuelling)
60500164 Mechanical fuel pump Bing 8080 (no more available)
60500257 Mechanical fuel pump Mikuni DF44-18 from ser. no. 8529
on and as spare part (for installation follow TN 8022)
45000162 Fuel cock 4M1-034

Maintenance Manual LS8-st Parts List
Edition: June 2016 Rev. 6 TN 8024 9-2
Propeller attachment
45002052 Rubber stop for propeller
9.2 Parts for electrical system
45002070 Battery for power supply 12V/min.7Ah (2 installed)
45002049 DEI-NT for LS8-t
45002050 Control box-NT for LS8-t
60510463 limit switch 164-564 with plug contacts for positions
retracted and extended
60510815 limit switch 164-025 with roller and screw contacts for
intermediate positions
45002075 Proximity switch for RPM measurement, complete with three
pin plug
60510484 manual extend-retract switch
60510478 master switch
60510360 fuel pump switch
60510375 refuelling pump switch
60510385 Protective circuit breaker ETA 2A (automatic cut out)
60510386 Protective circuit breaker ETA 3A (automatic cut out)
60510387 Protective circuit breaker ETA 4A (automatic cut out)
45002072 Flat plug type fuse 15 A (blue) for batteries (main fuse)
60510797 Plug BSK12 (for 12V socket BSB12)

Maintenance Manual LS8-st Diagrams
Issued: June 2016 Rev. 6 TN 8024 10-2
Diagram 2: Fuel system up to serial no. L8528
In Datei br-236