DG Flugzeugbau DG-1000T Maintenance Manual Download Page 4

Maintenance Manual DG-1000T 

Issued: February 2008 

 

TN 1000/13 

1.10

c)

With TN1000/13 executed, standard from ser. no. 10-133 on:

:

Adjust the stop bolt in part 10FW74 so that dimension a will be between 14,5 and  
15.5 mm (.57 in. and .61 in.) see diagram 18. 
Adjust the cable via the adjustment screw in part 10FW74 so that the locking pin 
disengages when retracting the landing gear. The distance 1mm according to 
diagram 17 also applies for the disengaged locking pin.  
Don’t tighten the cable too much! 

1.6.1.3 Free play 
Free play between bellcrank 10FW15/1 and shaft 10FW13/1 is not allowed. 

If there is any free play tighten the two securing bolts M 6x35 at the bellcrank and the 
two securing bolts M6x35 inside the landing gear box at the shaft with a 10 mm open-
end wrench. If there is still some free play, the bolts should be removed and the holes 
drilled out and reamed to diameter 8 H7. M 8 x 40 LN 9037 bolts should then be 
installed. The bolts for installation inside the landing gear box must be shortened to 
36mm. 

1.6.2

Main wheel (Version with nose wheel) 

1.6.2.1 Undercarriage control circuit 
see diagram 8 

In the retracted position the undercarriage is locked by an overcentre device. In the 
extended position the lock is by a locking notch at pushrod 5FW38 in the rear cockpit. 
A gas strut reduces the retraction force and keeps the undercarriage in the overcentre 
locking position (retracted and extended). 

1.6.2.2 Adjustment 
a)

Overcentre lock in retracted position:

 Adjustment at the adjustment screw 

between landing gear operating lever 5FW8 and the bellcrank 5FW36.  
The stop is located at the pushrod 5FW38 and stops against the pedestal 5FW41. 
Adjust this stop after adjusting the lock in the extended position see b) by gluing 
slotted shims onto the stop-sleeve of pushrod 5FW38. 

b)

In extended position

 (landing gear struts over centre) a max. free play of ca. 0.5 

mm (0.02 in.) between the lock at pushrod 5FW38 and the locking plate 5FW35 is 
allowed. Adjustment at the rod end in pushrod 5FW37 between 5FW38 and 5FW 
36.

1.6.2.3 Free play 
Free play between lever 5FW8 and the upper strut 5FW12 is not allowed. 

If there is any free play, the two securing bolts M 6 x 40 should be tightened with a 10 
mm open-end wrench. If there is still some free play, the bolts should be removed and 
the holes drilled out and reamed to diameter 8 H7. M 8 x 40 LN 9037 bolts should 
then be installed. 

Maintenance Manual DG-1000T 

 

Issued: March 2008 

ÄM1000/02 

1.14

 

1.8.2

 

Fin tank 

The fin ballast tank is constructed as integral tank.  
a)

 

Adjustment 
The release cable must be adjusted so that the cable just becomes loose when 
the handle is parallel to the fuselage wall. 

b)

 

Inspection 
According to sect. 2.2 a special inspection is to be carried out on the fin 
ballast tank system at each annual inspection.  
The dump time of the full fin tank should be timed and should not exceed 
120 seconds.  
Check the calibration of the outside air temperature gauge (in the DEI-NT). 

Up to ser.no. 10-100 and ser.no. 10-102 to 10-127:

  

Remove the tailwheel and the cover plate in the tailwheel box. Check the 
control cable and the lever of the valve carefully for wear. Check the control 
cable at the operating handle too. If the cable or the lever is worn, further use 
of the fin tank is prohibited. Please contact the manufacturer for a detailed 
repair instruction.  

Ser.no. 10-101, and from ser. no. 10-128 on:

  

Check the control cable at the operating handle and at the dump valve 
(installed in the lower rudder mounting bracket). If the cable is worn, further 
use of the fin tank is prohibited. 
 

 
 

Summary of Contents for DG-1000T

Page 1: ...vice TN1000 13 February 2008 6 0 3 0 4 0 6 0 10 1 19 2 1 diagram 19 enclosure 3 TN1000 15 Throttle handle in rear Cockpit Option March 2008 7 0 3 0 6 0 10 1 14 diagram 6a M 1000 02 Fin ballast tank va...

Page 2: ...ive pages continued diagram issued replaced replaced replaced 1 May 2004 2 Nov 2001 3 June 2005 4 Nov 2001 5 Nov 2001 January 2007 6 Nov 2001 January 2007 March 2008 Not valid for 10 101 and from 10 1...

Page 3: ...the undercarriage in the retracted overcentre locking position With TN1000 13 executed standard from ser no 10 133 on An additional landing gear positive locking device notch and latch at the landing...

Page 4: ...r adjusting the lock in the extended position see b by gluing slotted shims onto the stop sleeve of pushrod 5FW38 b In extended position landing gear struts over centre a max free play of ca 0 5 mm 0...

Page 5: ...dder cables for wear especially around the S tubes on the rudder pedals Worn rudder cables should be replaced see section 4 2 Check the sealing of the rudder see section 1 3 5 B Annual inspection and...

Page 6: ...l DG 1000T Issued February 2008 TN 1000 13 4 8 F Removal of the front fork 10Fw10 1 1 Remove the baggage compartment floor and the rear cover of the baggage compartment 2 Remove the main wheel see A 3...

Page 7: ...e shaft 10Fw15 3 left and 10Fw15 2 right to the fork 10Fw13 1 With TN1000 13 executed standard from ser no 10 133 on remove the locking catch lock for retracted position 9 Shift the shaft 10Fw15 3 tow...

Page 8: ...positive locking device diagram17 issued February 2008 TN1000 13 installation of the notch LG extended to 10FW12 2 Installation of the locking catch View LG retracted locking catch not engaged directi...

Page 9: ...upwards 4 Remove line 2 from the front cylinder To accomplish this press the black securing ring into the terminal nipple Push one50 ml syringe into the line 5 Remove line 2 from the rear cylinder Ins...

Page 10: ...fluid Move the cylinder into position 2 Connect the tube to the front terminal rear cylinder resp the upper terminal front cylinder Insert the other end of the tube into a container with hydraulic flu...

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