SusiAir PILATUS PORTER PC6, Программа технического обслуживания

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Form ASI-PC6 Alignment & Symmetry Inspection
Reissued: 2
Revision: 1
Date: July 2020 Page 2 of 4
NO. DESCRIPTION TASK NO. MECH. ENG. RII
Deformation and Symmetry Check (Ref. Fig. 1, Table 1 and 2)
1
Put the theodolite in position so that readings can be taken from RP1 b
right and from RP2, 3, 4, 5, 6, 7 and 8, on the left and right wings.
N/A
2
Adjust the theodolite tripod to allow readings to be taken at a level
approximately 100 to 200 mm below lowest point of fuselage.
N/A
3
Level the theodolite:
a) Level the theodolite base, and rotate through 360°, checking every
90° to ensure base is level.
N/A
b) Level theodolite head by turning leveling adjuster to match bubble
halves visible through small leveling eyepiece.
N/A
4 Take reading from measuring tape suspended from the right side RP1b.
N/A
5
Enter reading taken from RP1b right in the appropriate space on the In-
Service Check FORM
N/A
6
Suspend a measuring tape from RP2 under right wing and take reading
from tape. Record the reading on the In Service Check Form.
N/A
7
Repeat the procedure for RP3 through to RP8 right and RP2 through to
RP8 left.
N/A
8
Measure dimensions A, B and C left and right. Record the dimensions
on check form.
N/A
WARNING: IF THE PERMITTED DEVIATIONS ARE NOT IN LIMITS, THE AIRCRAFT MUST NOT BE FLOWN
UNTIL ADVICE FROM PILATUS AIRCRAFT LTD HAS BEEN RECEIVED AND ANY
RECTIFICATION WORK NECESSARY IS COMPLETED.
9
Compare the recorded deviation and permitted deviation. If the readings
are not in limits send copies of the check sheets to Pilatus Aircraft Ltd.
with a report of the incident, and details of damage that was found.
Pilatus will advise repair or inspection procedures that are required to
return the aircraft to service.
N/A
10 Install the underwing fuel tanks (if removed) 28-11-15
N/A
11 Lower the aircraft and remove the jacks 07-10-00 N/A
12 Make sure that the work area is clean and clear of tools and other items. N/A
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 : .......................................