SR22 Airplane Flight Manual (AFM) Temporary Change
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1 Cirrus Design TPOH Airplane Flight Manual (AFM) Temporary Change Information in this Temporary Change adds to, supersedes, or deletes information in the basic Pilot s Operating Handbook. Affected Publications: Filing Instructions: Purpose: Basic Airplane Flight Manual: PN Rev A10 (FAA Approved) PN AR Rev A10 (FAA Approved on behalf of ANAC-DA of Argentina) PN E Rev A10 (FAA Approved on behalf of EASA) PN Rev 6 (FAA Approved on behalf of ANAC of Brazil) Insert the following revised pages and retain until further notice. Remove and discard the superseded pages. Insert this TPOH cover page adjacent to the last page of the List of Effective Pages and retain until further notice. This POH Temporary Change revises the Fuel Annunciation description. Affected Sections: Section 7 - Airplane and Systems Description - Pages 7-57 through 7-60 TPOH of 2 11 May 2018
2 TPOH Cirrus Design Intentionally Left Blank 2 of 2 TPOH May 2018
3 Cirrus Design Fuel Quantity Indicator TPOH A dual reading 2¼ fuel quantity indicator is installed on the console immediately forward of the fuel selector valve. The LEFT pointer indicates left tank fuel quantity and sweeps a scale marked from 0 to 41 U.S. gallons in 5-gallon increments. The RIGHT pointer sweeps an identical scale for the right tank. Each scale is marked with a yellow arc from 0 to 14 U.S. gallons. The indicators are calibrated to read '0' when no usable fuel remains. The FUEL annunciator also provides an output signal to illuminate the FUEL caution light when the fuel quantity is low. The fuel quantity indications are derived from float-type fuel-level sensors installed in each main tank and each collector tank. The indicator is internally lighted. Serials 0002 through 1601, 1603 through 1643 and 1645 through 1662: 28 VDC for fuel quantity system operation is supplied through the 5-amp ENGINE INST circuit breaker on Main Bus 1. Serials 1602, 1644, 1663 and subsequent: 28 VDC for fuel quantity system operation is supplied through the 5-amp FUEL QTY / HOBBS circuit breaker on Main Bus 1. Note When the fuel tanks are 1/4 full or less, prolonged uncoordinated flight such as slips or skids can uncover the fuel tank outlets. Therefore, if operating with one fuel tank dry or if operating on LEFT or RIGHT tank when 1/4 full or less, do not allow the airplane to remain in uncoordinated flight for periods in excess of 30 seconds. TPOH
4 TPOH Cirrus Design 4 Serials 0002 thru 1601, 1603 thru 1643, 1645 thru LEGEND 1. Fuel Pump Switch 2. Fuel Quantity Gage 3. Fuel Selector Valve 4. Fuel Flow _FM07_2226 Figure 7-11 Fuel System Controls and Indicating (Sheet 1 of 2) 7-58 TPOH 18-03
5 Cirrus Design TPOH OIL LOW VOLTS FUEL 9 PITOT HEAT ALT 1 ALT 2 Annunciator Panel Primary Flight Display LEGEND Multifunction Display 4. Fuel Flow 5. Fuel Used (EMax only) 6. Fuel Remaining (EMax only) 7. Time Remaining (EMax only) 8. Fuel Economy (EMax only) 9. Fuel Caution Light Serials 1602, 1644, 1663 & subs. _FM07_2228 Figure 7-11 Fuel System Controls and Indicating (Sheet 2 of 2) TPOH
6 TPOH Fuel Flow Indication Cirrus Design Serials 0002 through 1601, 1603 through 1643 and 1645 through 1662: Fuel flow indication is integral to the combination Fuel Flow/ Manifold Pressure Gage. Refer to preceding discussion on Fuel Flow and Manifold Pressure Gage for complete description of fuel flow indication. Serials 1602, 1644, 1663 and subsequent: Fuel flow is shown as text in the fuel data block located in the lower right section of the MFD and is also continuously displayed in the engine data block located in the lower right corner of the PFD. The MFD and PFD receives a fuel-flow rate signal via the DAU from a fuel-flow transducer on the right side of the engine in the fuel line between the engine driven fuel pump and throttle body metering valve. In the event fuel flow exceeds 30.0 gallons per hour, the MFD will display Check Fuel Flow in a red advisory box in the lower right corner of the MFD. 28 VDC for the digital instrument operation is supplied through the 2- amp ANNUN / ENGINE INST circuit breaker on the Essential Bus. Fuel Caution Light The amber FUEL caution light in the annunciator panel comes on to indicate a low fuel condition. If the FUEL caution light comes on in flight, refer to the Fuel Quantity gages to determine fuel quantity. The light is powered by 28 VDC through the 2-amp ANNUN / ENGINE INST circuit breaker on the Essential Bus TPOH 18-03
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