Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Page 2-49
Pilot’s Operating Manual
Revision A2: Nov, 2004
Sub-section 2
GROUND SERVICING
Hawker 800XP Pro Line 21
Section VI - GROUND OPERATIONS
WHEEL REMOVAL
Special tools are required for wheel removal and installation, therefore, reference must be made to the
Airplane Maintenance Manual.
TREAD WEAR CHECK
1. Unless otherwise stated by the appropriate Airworthiness Authority, reject a tire when it is fully worn
as defined by the following.
2. Use the center groove as a wear indicator.
If the tread pattern, shown in Figure 19, does not have a center groove, use the grooves adjacent
to the center rib. A tire is fully worn when the tread is worn to the base of the wear indicating
groove(s).
NOTE: A tire worn beyond the above defined limit cannot normally be retreaded.
TIRE INSPECTION
1. Examine the tire tread as previously defined in Tread Wear Check and reject a tire which is fully
worn.
2. Visually examine the tire for evidence of overheating. Signs of overheating are, blistering, chafing,
melting, or the start of bead failure shown by irregularities in the molding lines near the tire bead.
Reject a tire which has been subjected to excessive heat.
3. Examine the nose wheel tires for cracking along the chine/side-wall junctions. Cracking up to 0.016
in. in depth is permitted. Reject a chined tire with the following:
(a) A crack deeper than 0.016 in. and more than 1.0 inch in length.
(b) A crack deeper than 0.093 in. at any point.
4. Examine the general condition of the tires by using the illustrations and notes provided in Figures
19, 20, 20A and 21 for guidance.