{"id":231,"date":"2022-10-07T14:41:10","date_gmt":"2022-10-07T09:11:10","guid":{"rendered":"https:\/\/hal-india.co.in\/backend\/?page_id=231"},"modified":"2024-11-20T09:47:56","modified_gmt":"2024-11-20T04:17:56","slug":"itso-products","status":"publish","type":"page","link":"https:\/\/hal-india.co.in\/backend\/hi\/itso-products\/","title":{"rendered":"\u0906\u0908\u091f\u0940\u090f\u0938\u0913 \u0909\u0924\u094d\u092a\u093e\u0926"},"content":{"rendered":"
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The Air data computer (ADC 3600A CVL1) measures Pressure Altitude, Calibrated Airspeed, True Airspeed, Mach number, Vertical Speed and Temperature in the atmosphere with high accuracy and stability based on Pneumatic inputs (Pitot and Static ports) and electrical input (OAT probe). OAT probe is an Aerodynamic structure intended to measure total air temperature. ADC 3600A CVL1 can be installed on civil Aircraft and Helicopters.<\/p>\n

TECHNICAL SPECIFICATIONS<\/strong><\/p>\n

\n\n\n\n\n\n\n\n\n\n\n\n\n\n
PARAMETER<\/th>\nSPECIFICATION<\/th>\n<\/tr>\n
Indicated static pressure<\/td>\n35 mbar to 1100mbar<\/td>\n<\/tr>\n
Indicated differential pressure<\/td>\n0 mbar to 510 mbar<\/td>\n<\/tr>\n
Total Air Temperature<\/td>\n-55\u2070C to 75\u2070C<\/td>\n<\/tr>\n
Pressure Altitude<\/td>\n0 to 35000 ft<\/td>\n<\/tr>\n
Vertical Speed<\/td>\n\u00b120000 ft\/min<\/td>\n<\/tr>\n
Calibrated Airspeed<\/td>\n30 to 600 Knots<\/td>\n<\/tr>\n
Mach Number<\/td>\n0.1 to 0.9 M<\/td>\n<\/tr>\n
Maximum Allowable Airspeed<\/td>\n30 to 600 Knots<\/td>\n<\/tr>\n
True Air Speed<\/td>\n50 to 650knots<\/td>\n<\/tr>\n
Static Air Temperature<\/td>\n-90\u2070C to 75\u2070C<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/figure>\n
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OAT Probe<\/h4>\n<\/div>\n
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ADC 3600A CVL1<\/h4>\n

Salient Features:<\/h4>\n

Signal Inputs<\/strong><\/p>\n