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Page Title: Table 4-11. Indicator Tolerances (Direct)
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Table 4-9.  Static Friction Error (Counter Drum Pointer) (Vibrator Inoperative)
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TM-1-1500-204-23-4 General Aircraft Maintenance (Electrical and Instrument Maintenance Procedures) Volume 4 Manual
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Figure   4-14.   Synchronous   Rotor   Tachometer Wiring   Diagram

TM    1-1500-204-23-4 Table   4-11.   Indicator   Tolerances   (Direct) Range Types Function Tolerance NOTE If  aircraft  has  just  completed  a  flight  of  one  hour  or  longer  at  altitudes  of  10,000  feet  or  over,  allow  two hours  for  stabilization  before  testing  altimeters. 0 to 25 and MS28061  and Fuel (±0.5)  psi 0 to 35 psi MS28064 C-32  and  C-33 0 to 50 psi O-1  and  O-2 Multi-Purpose (± 1.0) psi 0 to 200 psi B-23 Oil (25.5)  psi 0 to 2000 psi All Hydraulic (±50)  psi 0 to 4000 psi E-6  and  ME-1 Hydraulic (±75)  psi 0 to 5000 psi All Hydraulic (±100)  psi All Altimeters Altitude (±0-05) inch Hg All Barometric barometric   scale Pressure Range 0  to  50  psi Table   4-12.   Indicator   Tolerances   (Remote) Types Function MS28010-1   Indicator, Multi-Purpose MS28005-1    Transmitter Tolerance (k2.0)  psi 0 to 100 psi MS28010-2   Indicator, MS28005-2, MH-2   Transmitter Oil (k3.5)  psi 0 to 200 psi MS28010-3   Indicator, MS28005-3    Transmitter Oil (25.5)  psi 0  to  300  psi 0 to 600 psi MD-1  Indicator, MH-1   Transmitter C-34,   MS28010-7 indicator   E-7 MS280057 Transmitter Oil (k9.0)  psi Fuel (k2.0)  psi 0 to 4000 psi MS28010-5    Indicator MS28005-8 Hydraulic (±100)  psi Change  4 4-21

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