LBA
AD-No.: |
TN-No.:
|
Subject |
Urgency |
Download |
| |
301-1 |
Additional glass cloth strip in aft
fuselage section, SN 6 up to and incl. SN 35 |
|
 |
|
| |
301-2 |
Repositioning of air-brakes, SN 6 and up |
|
|
|
| |
301-3 |
Improvement
of wing suspension, SN 6 and up |
|
|
|
| |
301-4 |
Improvement
of air-brake actuating linkage SN 7 and up |
|
|
|
| |
301-5 |
Installation of drogue chute (Test with BS 1000) SN 7 only |
|
|
|
| |
301-6 |
Installation of elevator trim on LH side of fuselage SN 7 and up |
|
|
|
| |
301-7 |
Imporvement
of swivel bearings from GL12 to GL14 SN 11 and up |
|
|
|
| |
301-8 |
Reinforcement of fuselage structure All SN’s |
|
|
|
| |
301-9 |
Not
published |
|
|
|
| |
301-10 |
Improvement
of gear actuation locking mechanism, SN 11 and up |
|
|
|
| |
301-11 |
Modification of airbrake pivoting arm, SN 14 and up |
|
|
|
| |
301-12 |
Modification of aileron push-pull rod inside the wing SN 14 and up |
|
|
|
| |
301-13 |
Optional
installation of a tail wheel |
|
|
|
| |
301-14 |
Optional
installation of a drogue chute BS1300 |
|
|
|
| |
301-15 |
Installation of ground straps, all SN |
31.03.66 |
|
|
| |
301-16 |
Improved
bonding procedure of fuselage, SN 19 and up |
|
|
|
| |
301-17 |
Adjustable
horizontal stabilizer, SN 20 and up |
|
|
|
| |
301-18 |
Change of
root rip construction SN 27 and up |
|
|
|
| |
301-19 |
Alteration
of aileron actuationg lever SN 31 and up |
|
|
|
| |
301-20 |
Modification of elevator actuation system SN 20 and up |
|
|
|
| |
301-21 |
Replacement
of fuselage stringers with hollow profiles SN 36 and up |
|
|
|
| |
301-22 |
Modification of ailerons SN 42 and up |
|
|
|
| |
301-23 |
Installation of cable deflectors on c/g tow release, all SN’s |
|
|
 |
| |
301-24 |
Modification of wing Tipps, SN 54 and up |
|
|
|
| |
301-25 |
Installation of locking guide for elevator assembly, SN 2 up to and
incl. 85 |
|
|
|
| |
301-26 |
Improved
elevator actuating bracket, SN 86 and up |
Latest 31.08.1968 |
|
|
| |
301-27 |
Wear of
rudder control cables in the area of S-shaped guides of rudder
pedals |
every 100 h or annually |
|
|
| |
301-28 |
Sealing of
flap control lever for standard class contests |
|
|
|
| |
301-29 |
Color
coding scheme: affixing of different/additional colors. German
registered sailplanes |
|
|
|
| |
301-30 |
Reinforcement of elevator actuating bracket |
Before next flight /
latest 29.02.1976 |
|
|
| |
301-31 |
Elevator
linkage at base of the control stick |
|
|
|
| |
301-32 |
Extension
of service life limit to 6000 hours, |
31.03.1984/ when
reaching 3000 h |
|
|
| 87-83 |
301-33 |
Replacement
of „DIN“ control cables by „LN“ cables |
Every 500 h |
|
|
| |
301-34 |
Elevator
drive bracket: Possibility of replacement by elevator drive bracket
acc. to drawing No. 201-33-4 |
|
|
|
| |
301-35 |
Tow
releases: Optional use of model E85 instead of E72/E75 |
|
|
|
| 96-131 |
301-36 |
Inspection
of glass fiber laminate on spar stub fitting |
annually |
|
|
| 96-137 |
301-37 |
Control
surface weight and static balance |
until 31.3.96 |
|
|
| |
301-38 |
Replacement
of airbrake drive gear inside wing, optional |
|
|
|
| D-2005-118 |
301-39 |
Rudder
gimbal drive – rear actuator arm |
until 31.7.2005 |
|
|
| |
301-40 |
Installation of Mode-S-Transponder and Transponder Antennas |
|
|
|
| |
301-41 |
Spar stub
fitting replacement, standardisation of fittings |
|
|
|
| |
301-42 |
Increase of
maximum mass |
|
|
|
| |
301-43 |
Optional
installation of a 4-inch-wheel with a hydraulic disc brake system |
|
|
 |
