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dreieck.jpg (772 Byte) Technical Notes Glasflügel
  General
Libelle H-301
Glasflügel BS-1
Standard-Libelle 201/201B
Kestrel 401
Glasflügel 604
Club-Libelle 205
Hornet/Hornet C
Mosquito/Mosquito B
Glasflügel 304
does not include 304b + cz
Technical Notes Libelle H-301 + 301B
 
Type Certificate Data Sheet: EASA.A.241

Summary of Technial Notes

pdf.gif (247 Byte)

FAA Memorandum AD2007-05-19

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   pdf.gif (247 Byte)  
  301-3 Improvement of wing suspension, SN 6 and up   pdf.gif (247 Byte)  
  301-4 Improvement of air-brake actuating linkage SN 7 and up   pdf.gif (247 Byte)  
  301-5 Installation of drogue chute (Test with BS 1000) SN 7 only   pdf.gif (247 Byte)  
  301-6 Installation of elevator trim on LH side of fuselage SN 7 and up   pdf.gif (247 Byte)  
  301-7 Imporvement of swivel bearings from GL12 to GL14 SN 11 and up   pdf.gif (247 Byte)  
  301-8 Reinforcement of fuselage structure All SN’s   pdf.gif (247 Byte)  
  301-9 Not published      
  301-10 Improvement of gear actuation locking mechanism, SN 11 and up   pdf.gif (247 Byte)  
  301-11 Modification of airbrake pivoting arm, SN 14 and up   pdf.gif (247 Byte)  
  301-12 Modification of aileron push-pull rod inside the wing SN 14 and up   pdf.gif (247 Byte)  
  301-13 Optional installation of a tail wheel   pdf.gif (247 Byte)  
  301-14 Optional installation of a drogue chute BS1300   pdf.gif (247 Byte)  
  301-15 Installation of ground straps, all SN 31.03.66 pdf.gif (247 Byte)  
  301-16 Improved bonding procedure of fuselage, SN 19 and up   pdf.gif (247 Byte)  
  301-17 Adjustable horizontal stabilizer, SN 20 and up   pdf.gif (247 Byte)  
  301-18 Change of root rip construction SN 27 and up   pdf.gif (247 Byte)  
  301-19 Alteration of aileron actuationg lever SN 31 and up   pdf.gif (247 Byte)  
  301-20 Modification of elevator actuation system SN 20 and up   pdf.gif (247 Byte)  
  301-21 Replacement of fuselage stringers with hollow profiles SN 36 and up   pdf.gif (247 Byte)  
  301-22 Modification of ailerons SN 42 and up   pdf.gif (247 Byte)  
  301-23 Installation of cable deflectors on c/g tow release, all SN’s   pdf.gif (247 Byte) englisch.gif (516 Byte)
  301-24 Modification of wing Tipps, SN 54 and up   pdf.gif (247 Byte)  
  301-25 Installation of locking guide for elevator assembly, SN 2 up to and incl. 85   pdf.gif (247 Byte) englisch.gif (516 Byte)
  301-26 Improved elevator actuating bracket, SN 86 and up Latest 31.08.1968 pdf.gif (247 Byte)  
  301-27 Wear of rudder control cables in the area of S-shaped guides of rudder pedals every 100 h or annually pdf.gif (247 Byte) englisch.gif (516 Byte)
  301-28 Sealing of flap control lever for standard class contests     englisch.gif (516 Byte)
  301-29 Color coding scheme: affixing of different/additional colors. German registered sailplanes   pdf.gif (247 Byte)  
  301-30 Reinforcement of elevator actuating bracket Before next flight / latest 29.02.1976 pdf.gif (247 Byte) englisch.gif (516 Byte)
  301-31 Elevator linkage at base of the control stick   pdf.gif (247 Byte) englisch.gif (516 Byte)
  301-32 Extension of service life limit to 6000 hours, 31.03.1984/ when reaching 3000 h pdf.gif (247 Byte) englisch.gif (516 Byte)
87-83 301-33 Replacement of „DIN“ control cables by „LN“ cables Every 500 h pdf.gif (247 Byte) englisch.gif (516 Byte)
  301-34 Elevator drive bracket: Possibility of replacement by elevator drive bracket acc. to drawing No. 201-33-4   pdf.gif (247 Byte) englisch.gif (516 Byte)
  301-35 Tow releases: Optional use of model E85 instead of E72/E75   pdf.gif (247 Byte) englisch.gif (516 Byte)
96-131 301-36 Inspection of glass fiber laminate on spar stub fitting annually pdf.gif (247 Byte) englisch.gif (516 Byte)
96-137 301-37 Control surface weight and static balance until 31.3.96 pdf.gif (247 Byte) englisch.gif (516 Byte)
  301-38 Replacement of airbrake drive gear inside wing, optional   pdf.gif (247 Byte) englisch.gif (516 Byte)
D-2005-118 301-39 Rudder gimbal drive – rear actuator arm until 31.7.2005 pdf.gif (247 Byte) englisch.gif (516 Byte)
  301-40 Installation of Mode-S-Transponder and Transponder Antennas   pdf.gif (247 Byte) englisch.gif (516 Byte)
  301-41 Spar stub fitting replacement, standardisation of fittings   pdf.gif (247 Byte) englisch.gif (516 Byte)
  301-42 Increase of maximum mass   pdf.gif (247 Byte) englisch.gif (516 Byte)
  301-43 Optional installation of a 4-inch-wheel with a hydraulic disc brake system     pdf.gif (247 Byte)
 

Glasfaser-Flugzeug-Service GmbH
Hansjörg Streifeneder
Hofener Weg
D-72582 Grabenstetten
FON +49 (0)7382 / 1032   
FAX +49 (0)7382 / 1629

Approval according to
EASA  PART 21   DE.21G.0080
EASA PART 145  DE.145.0100

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