AIRCRAFT
DA 42 NG AMM
Fuselage
Doc # 7.02.15
Rev. 4
53-10-00
Page 9
15 Mar 2018
J. Vertical Stabilizer Front Lower Rib
The vertical stabilizer front lower rib is a rigid GFRP molding. It bonds to the fuselage shell at the
bottom of the vertical stabilizer. It also bonds to the vertical stabilizer front web. It has a hole for the
flexible control cable for the elevator trim tab.
K. Vertical Stabilizer Rear Lower Rib
The vertical stabilizer rear lower rib is a rigid GFRP molding. It bonds to the fuselage shell at the
bottom of the vertical stabilizer. It also bonds to the vertical stabilizer front and rear webs. It has a
large slot for the elevator control pushrod.
L. Vertical Stabilizer Front Web
The vertical stabilizer front web is a rigid GFRP molding. It bonds to the fuselage shell. It also
bonds to the vertical stabilizer lower ribs and to the top of the rear web.
The top of the front web is a rigid channel section. GFRP inserts give strength to the area where
the horizontal stabilizer mounts attach.
M. Vertical Stabilizer Rear Web
The vertical stabilizer rear web is a rigid GFRP molding. It bonds to the fuselage shell and it bonds
to the vertical stabilizer front web. The top of the rear web has the top mounting for the rudder. It
also has a reinforcing rib bonded to the rear face.
The vertical stabilizer rear web closes the rear of the vertical stabilizer.
N. Trim Weight
The trim weight can be varied in 3.0 kg (6.6 lb) steps up to 15 kg (33 lb) by installing the required
number of lead plates. For each number of lead plates, the attachment bolts with adequate length
must be used. The lead plates are fixed by seven bolts to the attachment plate. The trim weight
assembly replaces the access hole cover in the lower vertical tail and is fixed by eleven screws.
O. Trim Weight (if MÄM 42-600 is installed, Serial numbers 42.N100 and subsequent)
The trim weight can be varied in 1.0 kg (2.2 lb) steps from 2 kg (4.4 lb) up to 12 kg (26.4 lb) by
installing the required number of steel plates (minimum 2 to max. 12 plates). For each number of
steel plates, attachment bolts with adequate length must be used.
Summary of Contents for DA 42 NG
Page 933: ...AIRCRAFT DA 42 NG AMM Fuel Doc 7 02 15 Rev 4 28 TITLE Page 1 15 Mar 2018 CHAPTER 28 FUEL ...
Page 1459: ...AIRCRAFT DA 42 NG AMM Lights Doc 7 02 15 Rev 4 33 TITLE Page 1 15 Mar 2018 CHAPTER 33 LIGHTS ...
Page 1711: ...AIRCRAFT DA 42 NG AMM Doors Doc 7 02 15 Rev 4 52 TITLE Page 1 15 Mar 2018 CHAPTER 52 DOORS ...
Page 1853: ...AIRCRAFT DA 42 NG AMM Wings Doc 7 02 15 Rev 4 57 TITLE Page 1 15 Mar 2018 CHAPTER 57 WINGS ...
Page 2071: ...AIRCRAFT DA 42 NG AMM Engine Doc 7 02 15 Rev 4 72 TITLE Page 1 15 Mar 2018 CHAPTER 72 ENGINE ...
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