SusiAir PILATUS PORTER PC6, Программа технического обслуживания

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WHEEL AND BRAKES INSPECTION SHEET OF PILATUS
PORTER PC6
Form No. ASI/MD-71 Revision 3, July 2020 Page 1 of 4
Aircraft Registration : Date :
Job No. : Hours :
NO. DESCRIPTION MECH. ENG.
1. Perform Detail Visual Inspection with Flash Light, Mirror, and Magnifying Glass of
the Brake Pedals and System for Cracks, Corrosion, and Security of Installation.
2. Inspect Wheel and Brakes IAW ATA 32-40-00 and BERINGER Time Limits /
Maintenance Checks MC-STC-002.
3.
Inspect hydraulic brake fluid reservoir, check brake fluid level, apply brakes,
examine system for leaks, and service with MIL-PRF-5606 (ROYCO 756)
hydraulic fluid as required.
4.
Inspect tire condition IAW ATA 12-14-32 and Michelin Aircraft Tire Care and
Service Manual (Michelin Service Manual can be used as a guide line for all
approved main tires but will not supersede manufacture inspection
recommendations)
5. Check Brake Disc Thickness Record_____________mm/inch.
Minimum brake disc thickness 0.252 inch / 6.4 mm.
6. Examine brake disc condition for Coning, Groove and Bumps. See figure 2 as
attached.
7.
Inspect Brake Pad for wear. Brake Pad must be changed before grooves are
invisible. See figure 3 as attached. Friction material on Brake Pad minimum
thickness 0.100 inch / 2.5 mm.
8. Check play between disc and key disc drive. Max play
0.024 inch / 0.6 mm . See
figure 3 as attached.
9. Check Main wheels Tire. Examine and check inflation pressure 3,3 bar (
49 psi ).
10. Check Tail wheel. Examine and check for installation and inflation pressure 2,2
bar ( 47 psi ).
11. Check and examine brake master cylinders for leaks and connections.
12. After complete installation, check disc safety wire. Safety wire (
0.041 ) must be in
place to prevent disc from sliding out the slots. See figure 1 as attached.
13.
Record both Main Wheel Tire:
S/N LH_____________ and Hub S/N_____________
S/N RH_____________ and Hub S/N_____________
14. Record Tail Wheel Tire S/N ____________________ Hub S/N_____________
MAINTENANCE RELEASE
I hereby certify that aircraft parts and component mentioned above has been inspected and
maintained in accordance with the Maintenance Program and meets requirements of applicable
Civil Aviation Safety Regulations that is determined to be in an airworthy condition.
Name : .......................................
Signature : .......................................
Authorization Card’s No. : .......................................
Date : .......................................