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The CG's shown in the following diagrams are those from the example in Section 6.4.3 'CALCULATION OF LOADING CONDITION', rows 8 and 11.
6.4.4 PERMISSIBLE CENTER OF GRAVITY RANGE
Center of Gravity Position [m]
The flight CG position must be within the following limits:
Most forward flight CG:
2.35 m (92.52 in) aft of Datum Plane at 1250 kg (2756 lb)
2.35 m (92.52 in) aft of Datum Plane at 1468 kg (3236 lb)
2.40 m (94.49 in) aft of Datum Plane at max. take off mass (see Section 2.7) linear variation in between
Most rearward flight CG:
2.42 m (95.28 in) aft of Datum Plane at 1250 kg (2756 lb)
2.49 m (98.03 in) aft of Datum Plane at 1600 kg (3527 lb)
2.49 m (98.03 in) aft of Datum Plane at max. take off mass (see Section 2.7) linear variation in between
6.4.5 PERMISSIBLE MOMENT RANGE
The flight mass moments shown in the diagram are those from the example in Table 6.4.3
(a) 'CALCULATION OF LOADING CONDITION', rows 8 and 11.
Flight Mass [kg]
2900
Flight Mass Moment [kg m]
3000 3100 3200 3300 3400 3500 3600 3700 3800 3900 4000 4100 4200 4300 4400 4500
260,000
280,000
300,000
320,000
340,000
360,000
380,000
Flight Mass [lb]
6.5 EQUIPMENT LIST AND EQUIPMENT INVENTORY
All equipment that is approved for installation in the DA 42 is shown in the Equipment List below.
NOTE
The equipment listed below cannot be installed in any arbitrary combination. The airplane manufacturer must be contacted before removing or installing equipment, with the exception of replacing an unit by an identical unit.
The items of equipment installed in your particular airplane are indicated in the appropriate column. The set of items marked as 'installed' constitutes the Equipment Inventory.
Mass and Balance
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DA 42 AFM
Airplane Serial No.: Registration: Date: Mass Lever Arm
Description Type Part No. Manufacturer S/N inst‘d lbs kg in m
AVIONICS COOLING
Avionics Cooling Fan SAFE 328 305 467-00 Sandia Aerospace
PFD Cooling Fan SAFE 128 305 468-00 Sandia Aerospace
MFD Cooling Fan SAFE 128 305 468-00 Sandia Aerospace
AUTOPILOT SYSTEM KAP 140
Flight Computer KC 140 065-00176-7904 Bendix/King 2.040 0.930 70.080 1.780
Pitch servo KS 270 C 065-00178-2500 Bendix/King 2.290 1.040 175.400 4.455
Pitch servo mount KM 275 065-00030-0000 Bendix/King 1.077 0.489 175.400 4.455
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本文链接地址：钻石40系列飞机维护手册 DA 40 SERIES AIRPLANE MAINTENANCE MANUAL 4(2)
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