Cirrus Design TPOH AFM Temporary Change 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 Manuals: PN 13772-006 Original Issue (FAA Approved) PN 13772-006AR Original Issue (FAA Approved on behalf of ANAC-DA of Argentina) PN 13772-006E Original Issue (FAA Approved on behalf of EASA) PN 21400-006 Original Issue (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 Remove and discard the superseded pages.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 adds the Oxygen System CAS Messages/Procedures. Affected Sections: Section 3 - Emergency Procedures - Table of Contents, pages 3-1 and 3-2 - Oxygen System Emergencies, pages 3-28.1 thru 3-28.2 Section 3A - Abnormal Procedures - Table of Contents, pages 3A-1 and 3A-2 - Oxygen System, pages 3A-21 thru 3A-21.3 TPOH 17-04 1 of 2 11 May 2018
TPOH AFM Temporary Change Cirrus Design Intentionally Left Blank 2 of 2 TPOH 17-04 11 May 2018
Cirrus Design Section 3 Emergency Procedures Section 3: Emergency Procedures Table of Contents Introduction... 3 Emergency Procedures Guidance... 4 CAPS Guidance... 4 Preflight Planning... 4 Preflight Inspections/Maintenance... 4 Methodology... 4 Circuit Breakers... 5 Memory Items... 6 Landing Guidance... 6 Airspeeds for Emergency Operations... 7 Engine Failures... 8 Engine Failure On Takeoff (Low Altitude)... 8 Engine Failure In Flight... 9 Airstart... 10 Engine Airstart... 10 Smoke and Fire... 11 Cabin Fire In Flight... 11 Engine Fire In Flight... 12 Wing Fire In Flight... 13 Engine Fire During Start... 13 Smoke and Fume Elimination... 14 Emergency Descent... 15 Emergency Descent... 15 Maximum Glide... 15 Forced Landings... 16 Emergency Landing Without Engine Power... 16 Ditching... 17 Landing Without Elevator Control... 17 Engine System Emergencies... 18 Engine Partial Power Loss... 18 Oil Pressure Out of Range... 20 Oil Temperature High... 20 High Cylinder Head Temperature... 21 Propeller System Emergencies... 22 Engine Speed High... 22 Propeller Governor Failure... 22 TPOH 17-04 3-1
Section 3 Emergency Procedures Cirrus Design Fuel System Emergencies...23 High Fuel Flow...23 Low Fuel Quantity...23 Fuel Imbalance...24 Electrical System Emergencies...25 High Voltage on Main Bus 1...25 High Voltage on Main Bus 2...26 High or Low Voltage on Essential Bus...27 Environmental System Emergencies...28 Carbon Monoxide Level High...28 Oxygen System Emergencies...28.1 Oxygen System Fault - Above 10,000 Ft...28.1 Oxygen Quantity Low...28.2 Integrated Avionics System Emergencies...29 Attitude & Heading Reference System (AHRS) Failure...29 Air Data Computer (ADC) Failure...29 PFD Display Failure...29 Unusual Attitude Emergencies...30 Inadvertent Spin Entry...30 Inadvertent Spiral Dive During IMC Flight...31 Other Emergencies...32 Power Lever Linkage Failure...32 Emergency Engine Shutdown On Ground...32 Left/Right Brake Over-Temperature Annunciation...33 Starter Engaged Annunciation...33 Emergency Ground Egress...34 CAPS Deployment...35 3-2 TPOH 17-04
Cirrus Design Section 3 Emergency Procedures Oxygen System Emergencies Oxygen System Fault - Above 10,000 Ft OXYGEN FAULT Warning OXYGEN FAULT 1. Oxygen Flow Rate... CHECK If no flow: 2. Initiate Emergency Descent to below 10,000 ft: a. Power Lever... IDLE b. Mixture... AS REQUIRED c. Airspeed... VNE (205 KIAS) If flow is normal: 3. Oxygen Flow Rate... MONITOR 4. Initiate Normal Descent as soon as practical. Below 10,000 ft: 5. Oxygen System...OFF 6. Flight... CONTINUE Remain below altitudes requiring supplemental oxygen. Annunciation indicates tank solenoid failed (open or closed) or flow rate is low. If flow is checked and confirmed present, solenoid has failed OPEN; system will continue to provide oxygen until depleted, but unnecessary flight at altitudes requiring oxygen is not recommended. TPOH 17-04 3-28.1
Section 3 Emergency Procedures Oxygen Quantity Low OXYGEN QTY Warning Cirrus Design OXYGEN QTY 1. Oxygen Pressure and Flow Rate... CHECK 2. Initiate Normal Descent (non-emergency) below 10,000 ft. 3. Oxygen Flow Rate... MONITOR Below 10,000 ft: 4. Flight... CONTINUE Remain below altitudes requiring supplemental oxygen. 1. Annunciation indicates tank pressure is below 400 PSI, see Oxygen Duration Table of the Precise Flight Fixed Oxygen System AFMS to determine duration. 3-28.2 TPOH 17-04
Cirrus Design Section 3A Abnormal Procedures Section 3A: Abnormal Procedures Table of Contents Introduction... 3 Abnormal Procedures Guidance... 4 Circuit Breakers... 4 Landing Guidance... 4 Flight Environment... 6 Inadvertent Icing Encounter... 6 Inadvertent IMC Encounter... 6 Door Open In Flight... 6 Abnormal Landings... 7 Landing With Failed Brakes... 7 Landing With Flat Tire... 7 Engine System... 8 Low Idle Oil Pressure... 8 Starter Engaged Annunciation... 9 Fuel System... 10 Low Fuel Quantity... 10 Left Fuel Tank Quantity... 10 Right Fuel Tank Quantity... 11 Fuel Imbalance... 11 Electrical System... 13 Low Voltage on Main Bus 1... 13 Low Voltage on Main Bus 2... 13 Battery 1 Current Sensor... 13 Low Alternator 1 Output... 14 Low Alternator 2 Output... 15 Integrated Avionics System... 16 Avionics Switch Off... 16 PFD Cooling Fan Failure... 16 MFD Cooling Fan Failure... 16 Flight Displays Too Dim... 17 Pitot Static System... 18 Pitot Static Malfunction... 18 Pitot Heat Current Sensor Annunciation... 19 Pitot Heat Required Annunciation... 19 Flight Control System... 20 Electric Trim/Autopilot Failure... 20 TPOH 17-04 3A-1
Section 3A Abnormal Procedures Cirrus Design Flap System Exceedance...20 Landing Gear System...21 Brake Failure During Taxi...21 Left/Right Brake Over-Temperature...21 Oxygen System...21.1 Oxygen Quantity Low...21.1 Other Conditions...22 Aborted Takeoff...22 Parking Brake Engaged Annunciation...23 Communications Failure...23 3A-2 TPOH 17-04
Cirrus Design Landing Gear System Brake Failure During Taxi Section 3A Abnormal Procedures 1. Engine Power... AS REQUIRED To stop airplane - REDUCE If necessary for steering - INCREASE 2. Directional Control...MAINTAIN WITH RUDDER 3. Brake Pedal(s)...PUMP If directional control can not be maintained: 4. Ignition Switch...OFF Ground steering is accomplished by differential braking. However, increasing power may allow some rudder control due to increased groundspeed and airflow over the rudder. Left/Right Brake Over-Temperature BRAKE TEMP Caution BRAKE TEMP 1. Stop aircraft and allow the brakes to cool. Brake temperature is between 270 F and 293 F for more than 5 seconds. Refer to Section 10, Taxiing, Steering, and Braking Practices for additional information. TPOH 17-04 3A-21
Section 3A Abnormal Procedures Oxygen System Oxygen Quantity Low OXYGEN QTY Caution Cirrus Design OXYGEN QTY 1. Oxygen Pressure and Flow Rate... CHECK 2. Oxygen Duration... CALCULATE a. See Precise Flight Fixed Oxygen System AFMS; calculate duration based on remaining pressure, number of occupants and type of device (mask or cannula). 3. Perform Normal Descent as necessary, dependent on duration calculation. 1. Annunciation indicates tank pressure is between 800 and 400 PSI at pressure altitudes at and above 10,000 ft, see Precise Flight Fixed Oxygen System AFMS to determine remaining duration. OXYGEN RQD Caution OXYGEN RQD 1. Oxygen Masks or Cannulas...DON 2. Oxygen System... ON 3. Oxygen Flow Rate...ADJUST AS NECESSARY FOR CRUISE ALTITUDE Annunciation indicates that aircraft is above 10000 ft and system is not ON. 3A-21.1 TPOH 17-04
Cirrus Design OXYGEN QTY Advisory Section 3A Abnormal Procedures OXYGEN QTY On-Ground 1. Oxygen Supply... REPLENISH IF USE OF OXYGEN IS ANTICIPATED In-Flight 1. If use of oxygen is anticipated, verify adequate oxygen supply for flight duration. Refer to Duration chart in Precise Flight Fixed Oxygen System AFMS. Annunciation indicates oxygen tank pressure is below 800 PSI at pressure altitudes below 10,000 ft. OXYGEN SYSTEM LEFT ON Advisory OXYGEN LEFT ON 1. Oxygen System...OFF Annunciation indicates that oxygen system has been left ON after onground engine shutdown. If system is left ON and aircraft power is turned OFF, the solenoid valve will remain open and may result in unexpected leakage and pressure loss. TPOH 17-04 3A-21.2
Section 3A Abnormal Procedures Cirrus Design Intentionally Left Blank 3A-21.3 TPOH 17-04