M+D JS-MD 1C 2017, Руководство по эксплуатации воздушного судна

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JS-MD 1C Aircraft Flight Manual
MD01-AFM-00-001
Issue: 02
Rev. 00 Rev. Date: 14.09.2017 Page 2–7
Table 2.5.0-2 gives the forward and rear centre of gravity limits (no
payload) for different empty masses that will allow a cockpit range of 70
kg to 115 kg.
Empty mass
Empty Centre of Gravity range
Forward limit to allow a
maximum cockpit load of
115kg (253 lbs)
Rear limit to allow a
minimum cockpit load of
70kg (154 lbs)
kg lbs 18 m 21 m 18 m & 21 m
320 705
558 mm
22.0 in.
593 mm
23.4 in.
597 mm
23.5 in.
330 727
553 mm
21.8 in.
587 mm
23.1 in.
593 mm
23.4 in.
340
749
548 mm
21.6 in.
582 mm
22.9 in.
590 mm
23.2 in.
350 771
543 mm
21.4 in.
577 mm
22.7 in.
586 mm
23.1 in.
360 793
538 mm
21.2 in.
572 mm
22.5 in.
583 mm
23.0 in.
370 815
534 mm
21.0 in.
568 mm
22.4 in.
580 mm
22.8 in.
380 838
529 mm
20.8 in.
563 mm
22.2 in.
577 mm
22.7 in.
Table 2.5.0-2
If the calculated empty centre of gravity falls outside of this envelope,
the minimum and maximum cockpit loads must be determined using
the formula given in the MD01-AMM-00-001 JS-MD 1C Aircraft
Maintenance Manual Section 9.