Grob G 103 TWIN II User Manual

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FLIGHT HANDBOOK GROB G 103
5a
If the fuselage reinforcement according to OSB 315-66 had not been Dertormed the
following is applicable:
The glider GROB G 103A "WIN
I1 ACRO is derived from the GROB G 103 "WIN II". Due
to structural reinforcements the 'TWIN
II ACRO is approved in the category "Acrobatic".
According to MSB 315-65 only "simple aerobatics" (Loop. Turn, Lazy Eight, Chandelle, Spin)
is approved (refer to 11.2 and IV.9)
The
Flight Handbook for Aerobatics
-
GROB G 103A "WIN II ACRO"
Edition February 1984
f LBA approved
is unvaiid according to MSB 315-65 and must be removed from the Flight Handbook.
If the fuselage reinforcement according to
OSB 315-66 had been performed the
following is applicable:
The aiider GROB G 103 A 'TWIN
II ACR0 is derived from the GROB G 103 "TWIN 11". Due 1
to stnctural re.nforcements the "WIN II ACRO' is approved and certtfied for acrobatics in
conlunction with [he following valld operating instructions:
FI ght handbook for acrooatics,
GROB G 103 A
" Wih II ACRO.
edition February 1964,
LBA approved.
These operating instructions must be added to the flight manual and contain special
instructions valid for acrobatic operations. Main modifications to the "normal" Right manual
are contained in the following sections:
- Airworthiness group (11. 1)
"? - Permitted operating conditions (11. 2)
- Minimum equipment (11. 3)
- Maximum speeds (11. 4)
- Flight envelope (1 1.5)
- Load scheme (11.6)
The following items were modified in the maintenance handbook with respect to the acrobatic
version:
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- Weights and moments of control surfaces (VI)
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References to the flight handbook for acrobatics are shown on the affected pages of the
"standard" flight manual.
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Rev. 4, 16.10.2003
FAA Issue

Grob G 103 TWIN II Specifications

General

Brand	Grob
Model	G 103 TWIN II
Category	Aircrafts
Language	English