2.1.
1
Look for fuel leaks or seepage from seams and rivet heads in the wing integral tank areas.
2.1.
2
Examine the complete wing, engine compartment, fuselage and horizontal stabilizer for distortion and loose or
missing rivets.
2.2
Landing Gear
2.2.
1
Examine the tires and wheels for damage.
2.2.
2
Examine the landing gear legs for leaks and damage.
2.2.
3
Examine the landing gear attachment points for damage.
2.2.
4
Examine the shock absorber top and bottom attachment points for damage.
2.2.
5
Examine the landing gear compartments for damage.
2.2.
6
Examine the nose and main landing gear drag links for damage.
2.2.
7
Examine the main landing gear folding struts for damage.
3
Detailed Examination
3.1
Preparation
Raise the aircraft on jacks, refer to AMM 12-B-07-10-00-00A-901A-A.
3.2
Structure
3.2.
1
Remove access panels near the damaged area and examine internal structure as far as possible.
3.2.
2
Lower the flaps. Examine the flaps and flap coves. Raise the flaps. Make sure flap movement is smooth.
3.2.
3
Move the ailerons up and down and make sure movement is smooth and there are no unusual noises.
3.3
Landing Gear
3.3.
1
Make sure that the wheels are free to rotate.
3.3.
2
Move the rudder pedals left and right and make sure that the nose wheel steering movement is satisfactory.
3.3.
3
Do the adjustment/test of the landing gear, refer to AMM 12-B-32-30-00-00A-903B-A.
3.4
Engine
Do the engine heavy/hard landing inspection (Ref. P&WC EMM 72-00-00).
3.5
Navigation
3.5.
1
Do a check swing of the ADAHRS, refer to AMM 12-B-34-25-00-00A-903A-A.
3.5.
2
Do a check swing of the ESIS (if installed), refer to AMM 12-B-34-26-40-00A-903B-A.
PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 27 MSN 545, 1001-1719, 1721-1942
12-B-AM-00-00-00-I
UNCLASSIFIED
Effectivity: All
12-B-05-50-01-00A-282B-A
UNCLASSIFIED
19.11.2019 Page 3