ARMY TM 5-6115-612-34 NAVY AG -320B0-MME-000 1-7. TABULATED DATA (cont) Table 1-1.  Repair and Replacement Standards -Continued Component Manufacturer Tolerance Desired Clearance Maximum Allowable Maximum Allowable Minimum Maximum Minimum Maximum Wear Clearance ENGINE (Cont) INLET HOUSING (Dwg #101401) Overall Length 7.435 7.460 Inside diameter 3.1875 3.1880 Diameter -A- 10.903 10.907 Diameter -B- 10.7505 10.7530 Diameter -C- 7.747 7.749 Surface -A- Flatness 0.001 Surface -B- parallel to -A- 0.001 Surface -C- parallel to -A- 0.001 Surface -D- parallel o -A- 0.001 LABYRINTH SEAL (COMPRESSOR) Inside Diameter 0.7870 0.7874 Overall length 0.9290 0.9310 Major OD 1.350 1.370 OD over teeth 1.2482 1.2485 LABYRINTH SEAL (TURBINE) Inside Diameter 0.7870 0.7874 Overall length 0.760 0.770 Major OD 1.8530 1.8535 OD over teeth 1.8530 1.8535 TURBINE WHEEL AND SHAFT Major OD (D) 6.325 6.335 Bearing journal (B) 0.6653 0.6655 Blade clearance to nozzle 0.022 0.026 0.026 Diameter -A- 0.6254 0.6256 Diameter -C- 0.7875 0.7878 Surface -E- Perpendicular to centerline 0.0002 TURBINE NOZZLE OUTER (dwg #101687) surface -A- Flatness 0.002 surface -B- 7.3150 7.3160 surface -E- Perpendicular to -B- Diameter -C- 0.001 Diameter -D- 9.665 9.670 9.790 9.795 TURBINE NOZZLE INNER (DWG #101688) Surface -A- (Top of Vanes) Flatness 0.0005 Surface -B- Diameter 4.309 4.311 Perpendicular to -A- 0.001 1-8  Change 4