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TM 9-2990-206-34&P
INSPECTION-Continued.
INSPECT COMPRESSOR WHEEL AND NUT
TOOLS:
0.3125 to 0.5000 inch telescope gage
O.(X) to 1.00 inch micometer
1. Inspect compressor wheel nut (A) for thread damage
or deformation.
CAUTION
Cracked compressor wheel blades will break
during operation and-cause failure..
2. Inspect compressor wheel (B) for cracked, broken, bent,
eroded, or missing blades.  Inspect rear surface of
compressor wheel for evidence of wear or scoring.
3. Measure and record compressor wheel bore diameter
(C) using telescope gage and micromter.
4. Replace dammed comressor wheel nut. Replace com-
pressor wheel if damaged, or if bore diameter ex-
ceeds 0.3739 inch (9.497 mm).
INSPECT BACKPLATE
TOOLS:
0.5000 to 0.7500 Inch telescope gage
0.00 to 1.00 inch micrometer
1. Inspect backplate (D) for cracks. Inspect mounting flange
and machined mating surface for distortion or warpage.
2. Flush oil hole with solvent. Solvent must enter
through hole (E) and flow freely through three holes (F).
3. Inspect thrust bearing (G) for evidence of overheating,
scoring, or looseness.  The three thrust bearing pads
(H) must be smooth and flat. All three pads (H) must be
parallel to surface (J) within 0.0010 Inch (0.025 mm).
Surface (J) flatness must not exceed 0.0005 inch total
indicator reading (TIR) (0.0127 mm TIR).
4. Inspect bore (K) for scratches or scoring. Measure bore
diameter (K) using telescope gage and micrometer. Re-
place backplate If bore diameter exceeds 0.6885 inch
(17.49 mm).
5. Measure depth from surface (J) to thrust bearing pad (L).
Replace backplate if depth exceeds 0.3980 inch 10.11 mm).
6. Replace backplate if cracked, distorted, or does not meet
TA097818
wear limit requirements.
3-12

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