(b)
Examine all control cables.
(c)
Examine the stabilizer jack screws.
(d)
Examine all hinge surfaces of the flight controls.
(e)
Examine the tracks and flap mechanisms of the trailing edge flaps.
(f)
Examine the track fairings and linkages of the trailing edge flap.
(g)
Examine the leading edge slats and mechanisms.
S. Examine the Wing and Engine Nacelle Thermal Anti-Ice Systems
S 022-100
(1)
Remove the Thermal Anti-Ice Valve of the wing to be examined (AMM 30-11-02).
S 212-101
(2)
Examine the Thermal Anti-Ice Valves of the wing for volcanic ash contamination (AMM 30-11-02).
S 022-102
(3)
Remove the Thermal Anti-Ice Valves of the engine inlet to be examined (AMM 30-21-03).
S 212-103
(4)
Examine the Thermal Anti-Ice Valves of the engine inlet for signs of volcanic ash contamination (AMM 30-21-03).
T. Examine the Airplane Internally
S 212-104
(1) Examine the airplane internal areas that follow for signs of volcanic ash contamination:
(a)
The main deck cabin.
(b)
The closets
(c)
The passenger seats
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(d)
The powered crew seats
(e)
The flight instruments
(f)
The electrical/electronic control panels
(g)
The lavatories
(h)
The lavatory components
(i)
The galleys
(j)
The galley components
(k)
The floor coverings.
S 212-105
(2)
Examine the refrigeration/chiller units (if installed) for volcanic ash contamination.
S 212-106
(3)
Examine the baggage/cargo systems for volcanic ash contamination.
S 212-107
(4)
Examine the main electrical/electronic bay and compartments for volcanic ash contamination.
U. Put the Airplane Back To Its Initial Condition
S 942-108
(1) Put the airplane back to its initial condition after all necessary volcanic ash conditional inspections are completed.
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TAIL STRIKE/SKID CONDITIONAL INSPECTION
_______________________________________
1. General_______
A. This inspection procedure must be done if an airplane tail strike (tail dragged or touched the runway) occured when the airplane landed or during takeoff.
B. This procedure has the following task(s):
(1) Tail Strike Inspection
TASK 05-51-32-212-011
2. Tail Strike Inspection______________________
A. References
(1)
AMM 27-41-00/501, Horizontal Stabilizer Trim Control System
(2)
AMM 27-48-00/501, Stabilizer Trim Position Indicating System
(3)
AMM 27-48-03/401, Stabilizer Position Module-Remove
(4)
AMM 27-48-03/401, Stabilizer Position Module-Installation
B. Access
(1) Location Zones
163 Area Below Bulk Cargo Compartment, Left
300 Empennage and Body Section 48
311 Area Aft of Bulkhead, Left
312 Area Aft of Bulkhead, Right
C. Tail Strike Inspection Procedure
S 212-015
(1) Inspect the external skin surface of the lower aft fuselage.
(a) Look from station 1620 (approximate aft cargo bay aft bulkhead) to the APU compartment (Fig. 201). 1) Look for signs of
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