CHAPTER 7 ABNORMAL FLOWS AND CHECKLISTS TABLE OF CONTENTS

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Transcription:

CHAPTER 7 ABNORMAL FLOWS AND CHECKLISTS TABLE OF CONTENTS ELECTRICAL FAULTS...3 Alternator Failure / Low Voltage...3 INSTRUMENTS...7 Low vacuum indication / vacuum failure...7 Erroneous airspeed / altitude / vertical speed indications...8 LANDING GEAR and TIRES...9 Manual landing gear extension...9 Gear up emergency landing...12 Landing with a flat nose tire...14 Landing with a flat main tire...15 OTHER ABNORMAL SITUATIONS...17 Open Door In Flight...17 NF ISSUE 9/12 ABNORMAL Flows and Checklists 1

CAUTION DO NOT RUSH THESE PROCEDURES. In nearly all situations involving abnormal problems, it is important to first realize that the airplane remains completely flyable to the limits of its fuel load. Although any problem addressed in this chapter is to be considered serious, it is NOT grounds for hurrying a procedure and possibly missing a step that, if properly executed, would have resulted in correcting the problem. Conduct the procedures carefully and systematically as a coordinated crew (when applicable) in combination with assistance received from outside sources. This Space is Intentionally Left Blank NF ISSUE 9/12 ABNORMAL Flows and Checklists 2

ELECTRICAL FAULTS CAUTION Whenever electrical failure is experienced in-flight, the electrical system is considered suspect even if normal operation appears to be restored after troubleshooting. The possibility of the failure re-occurring during the remainder of the flight must be kept in mind at all times, and the PIC should plan accordingly. The electrical system must be checked by Maintenance as soon as possible. WARNING Do not reset a circuit breaker if it can be avoided. In all cases, NEVER reset a circuit breaker more than once. CAUTION Landing gear CANNOT be retracted without electrical power. ALTERNATOR FAILURE / LOW VOLTAGE (Ammeter indicates ZERO output) AMMETER FUNCTION... VERIFY BY LOADING THE ALTERNATOR VOLTAGE... (if installed) CHECKED ELECTRICAL LOAD...REDUCE ALTERNATOR CIRCUIT BREAKERS... (as required) CHECK IF ALT CIRCUIT BREAKER POPS AGAIN... DO NOT RESET - IF ALTERNATOR CIRCUIT BREAKERS ARE CLOSED OR REMAIN CLOSED AFTER RESET - ALT SIDE of MASTER SWITCH... (for 3 seconds) OFF ALT SIDE of MASTER SWITCH... ON AMMETER / VOLTAGE(if installed)... CHECKED - IF AMMETER INDICATES ZERO OUTPUT AGAIN ALTERNATOR SIDE OF MASTER SWITCH ONLY... OFF ELECTRICAL LOAD... MINIMIZE to ESSENTIAL ONLY BATTERY VOLTAGE... (if installed) MONITOR TERMINATE FLIGHT... AS SOON AS POSSIBLE IF IN VMC...REMAIN AND LAND VFR IF IN IMC... OBTAIN ATC ASSISTANCE TO NEAREST VMC NF ISSUE 9/12 ABNORMAL Flows and Checklists 3

WARNING If alternator output is not restored and battery is completely discharged, in the cases of total loss of electrical power, the gear will have to be deployed manually using Emergency Gear Extension procedures, and gear position lights will be inoperative even if emergency gear extension is successful. Consult POH / AFM. ALTERNATOR FAILURE / LOW VOLTAGE (Ammeter indicates ZERO output) EXPANDED AMMETER FUNCTION... VERIFY BY LOADING THE ALTERNATOR Before executing the rest of the procedure, establish that the alternator output indicated on the ammeter is zero and not merely low, by activating an electrically powered device, such as a landing light. Then, check the ammeter to see if the alternator is producing electrical output. If the ammeter is still indicating zero when it should indicate a positive load, it would imply the alternator is indeed inoperative. Any indication greater than zero would imply that alternator is producing an electrical load. VOLTAGE... (if installed) CHECKED If a voltage indicator is installed (such as JDM-700), appropriate to the specific aircraft, check the system voltage to confirm that the alternator is not producing proper output and that only battery voltage is indicated. ELECTRICAL LOAD... REDUCE Turn off all non-essential equipment to minimize total electrical load. This will allow the battery to supply the essential electrical equipment for the longest possible time. ALTERNATOR CIRCUIT BREAKERS... (as required) CHECK Check that the alternator circuit breakers are IN. If any are found to be out, and, in PIC judgment, the flight can be safely concluded as soon as possible on battery power, PIC may consider leaving the breaker out. If the decision was made that having the alternator is essential for the flight considering the circumstances, reset the alternator circuit breakers. IF ANY ALT CIRCUIT BREAKER POPS AGAIN... DO NOT RESET Under no circumstances should a circuit breaker be reset more than once. If it pops after one reset attempt, leave it out and continue on battery power. Before battery power runs out, enlist all necessary assistance, including ATC help, and land as soon as practical NF ISSUE 9/12 ABNORMAL Flows and Checklists 4

- IF ALTERNATOR CIRCUIT BREAKERS ARE CLOSED OR REMAIN CLOSED AFTER RESET If the alternator breakers are found to be closed, or remain closed after the single reset attempt, perform the following actions. ALT SIDE of MASTER SWITCH... (for 3 seconds) OFF Turn only the ALT side of the master switch to OFF and wait at least 3 seconds. ALT SIDE of MASTER SWITCH... ON After the 3 second wait, turn the ALT side of the electrical master switch to ON, thereby completing recycling alternator. AMMETER / VOLTAGE (if installed)... CHECKED Check the ammeter for proper alternator output indications. A zero indication would imply that the alternator is still not functioning. As described earlier in this procedure, load the alternator to check that the gauge indeed reads zero and is not merely low. Check the voltage indicator (if installed, appropriate to the specific aircraft) for the correct voltage, to determine if the alternator/charging system are functioning properly. - IF AMMETER INDICATES ZERO OUTPUT AGAIN Perform the following action if the ammeter again indicates zero output, and it has been confirmed that the alternator is still inoperative, or has again become inoperative. ALTERNATOR SIDE OF MASTER SWITCH ONLY... OFF Turn the alternator OFF, by moving the ALT side only of the master switch to the OFF position. The other side (battery) portion of the switch should remain on, to provide electrical power to the aircraft, supplied by the battery only. CAUTION Compass errors may occur when the alternator side of the battery master switch is in the OFF position. ELECTRICAL LOAD... MINIMIZE to ESSENTIAL ONLY Turn OFF all non-essential electrical equipment to prolong battery life. Do not turn off the battery side of the master switch. BATTERY VOLTAGE (if installed)... MONITOR Monitor battery voltage on the appropriate indicator (if installed in the aircraft) through the remainder of the flight to help determine when the battery is beginning to be depleted. TERMINATE FLIGHT... AS SOON AS POSSIBLE Head to the nearest suitable airport and terminate the flight as soon as practical. Before battery power runs out, enlist all necessary assistance, including ATC help, for the successful conclusion of the flight. Have the electrical system checked out by Maintenance. NF ISSUE 9/12 ABNORMAL Flows and Checklists 5

IF IN VMC... REMAIN AND LAND VFR If in VMC, maintain VFR and divert to the nearest suitable airport to land under VFR. IF IN IMC... OBTAIN ATC ASSISTANCE TO NEAREST VMC Enlist ATC help in determining the nearest VMC/VFR conditions, and then divert to exit the IMC as soon as possible. This Space is Intentionally Left Blank NF ISSUE 9/12 ABNORMAL Flows and Checklists 6

INSTRUMENTS and VACUUM FAULTS LOW VACUUM INDICATION / VACUUM FAILURE AUXILARY VACUUM SYSTEM (if installed)... ON ENGINE RPM... (as required) INCREASE ALTITUDE... (if possible) DESCEND VACUUM GAUGE... (4.9 5.1 hg) MONITOR IF IN VMC...REMAIN AND LAND VFR IF IN IMC... OBTAIN ATC ASSISTANCE TO NEAREST VMC LOW VACUUM INDICATION / VACUUM FAILURE, EXPANDED AUXILARY VACUUM SYSTEM (if installed)... ON If vacuum indications are low or complete vacuum failure is experienced, engage the auxiliary vacuum system, if installed in the aircraft. This may allow the flight to continue normally and land as soon as possible. ENGINE RPM...(as required) INCREASE Increase engine RPM, if practical, in order to increase the speed at which the vacuum pump turns, thus producing the most available vacuum pressure. ALTITUDE... (if possible) DESCEND If situation permits, descend to a lower altitude, which may allow the vacuum pump to produce acceptable vacuum pressure. VACUUM GAUGE... (4.9-5.1 Hg) MONITOR Check the vacuum gauge for an indication of 4.9 to 5.1 inches Hg (Mercury). If this vacuum value cannot be maintained, the vacuum powered instruments are considered unreliable. Monitor secondary instruments and terminate the flight as soon as practical. IF IN VMC... REMAIN AND LAND VFR If in VMC, maintain VFR and divert to the nearest suitable airport to land under VFR. IF IN IMC... OBTAIN ATC ASSISTANCE TO NEAREST VMC Enlist ATC help in determining the nearest VMC/VFR conditions, and then divert to exit the IMC as soon as possible. NF ISSUE 9/12 ABNORMAL Flows and Checklists 7

ERRONEOUS AIRSPEED / ALT / VSI INDICATIONS ALTERNATE STATIC SOURCE...ON PITOT HEAT (if in visible moisture)...on IF IN VMC... REMAIN AND LAND VFR IF IN IMC... OBTAIN ATC ASSISTANCE TO NEAREST VMC ERRONEOUS AIRSPEED / ALT / VSI INDICATIONS, EXPANDED ALTERNATE STATIC SOURCE...ON When erroneous pitot / static system indications are detected, activate the alternate static source by pulling the alternate static source valve lever out. Monitor the instruments to determine if the problem has been corrected. PITOT HEAT... (as required) ON If pitot mast blockage is suspected, especially in visible moisture, turn the pitot heat ON. Even if there is no visible moisture, previously trapped moisture in the pitot mast may have frozen, so consider using pitot heat as situation requires. IF IN VMC... REMAIN AND LAND VFR If in VMC, maintain VFR and divert to the nearest suitable airport to land under VFR. IF IN IMC... OBTAIN ATC ASSISTANCE TO NEAREST VMC Enlist ATC help in determining the nearest VMC/VFR conditions, and then divert to exit the IMC as soon as possible. This Space is Intentionally Left Blank NF ISSUE 9/12 ABNORMAL Flows and Checklists 8

LANDING GEAR and TIRES CAUTION DO NOT RUSH THESE PROCEDURES. In nearly all situations involving problems with the landing gear, it is important to first realize that the airplane remains completely flyable to the limits of its fuel load. Although any problem with the landing gear is to be considered serious, it is NOT grounds for hurrying a procedure and possibly missing a step that, if properly executed, would have resulted in correcting a previous mechanical problem and extending the landing gear. Conduct the procedure carefully and systematically as a coordinated crew (when applicable) in combination with assistance received from outside sources. WARNING If all electrical power has been lost and battery depleted, the gear will have to be deployed manually using Emergency Gear Extension procedures, and the gear position light will be inoperative, even if emergency gear extension is successful. Consult POH / AFM. MANUAL LANDING GEAR EXTENSION (normal extension failed, one or more green lights fail to illuminate) IF SIMULATING... PULL LANDING GEAR PUMP CIRCUIT BREAKER MASTER SWITCH... ON CIRCUIT BREAKERS... (as required) CHECK / RESET NAVIGATION and PANEL LIGHTS... (in daytime) OFF LANDING GEAR SELECTOR SWITCH... DOWN LANDING GEAR LIGHTS... (swap bulbs if necessary) TESTED - IF THE BULBS ARE NOT THE PROBLEM - AIRSPEED... BELOW 100 MPH LANDING GEAR SELECTOR SWITCH... VERIFY DOWN EMERGENCY GEAR EXTENSION LEVER... HOLD DOWN LANDING GEAR LIGHTS... CHECK 3 GREEN, NO RED - IF GEAR IS STILL NOT DOWN AND LOCKED - YAW THE PLANE ABRUPTLY with RUDDER... EXECUTE SLOW DOWN to MCA (if previous step failed)... EXECUTE LANDING GEAR LEVER (at MCA)... CYCLE UP, then DOWN NF ISSUE 9/12 ABNORMAL Flows and Checklists 9

MANUAL LANDING GEAR EXTENSION, EXPANDED (normal extension failed, one or more green lights fail to illuminate) CAUTION In any situation where a flight crew detects a problem with the landing gear, the flight crew shall terminate the training event and troubleshoot the problem. The crew shall contact the appropriate resources (BSU Dispatch if available by direct or relay communication, then ATC/Tower facility) prior to attempting a landing. This will ensure that the flight crew receives maximum available assistance prior to landing the aircraft. IF SIMULATING...PULL LANDING GEAR PUMP CIRCUIT BREAKER If performing this procedure and simulating gear failure for training purposes, prior to execution, pull the LANDING GEAR PUMP circuit breaker out. This will prevent the landing gear pump from activating during the procedure. MASTER SWITCH...ON Verify that the master switch is ON. CIRCUIT BREAKERS... (as required) CHECK / RESET Check the appropriate landing gear circuit breakers. If tripped, reset, but no more than once. PANEL and NAVIGATION LIGHTS... (in daytime) OFF Check that PANEL and NAVIGATION LIGHTS are OFF. The landing gear indicator lights are dimmed when panel and navigation lights are on, and thus may appear to be inoperative. LANDING GEAR SELECTOR SWITCH... DOWN Ensure that the landing gear selector switch is DOWN to perform the following landing gear indicator light checks. LANDING GEAR LIGHTS... (swap bulbs if necessary) TESTED Check that all three (3) green landing gear lights are ON and that the red Gear Up Warning light is OFF. If any gear down green bulb fails to illuminate while another green bulb is lit, it is possible that the bulb is burned out while the gear is actually down. Troubleshoot by pulling out and switching the square green landing gear lights to test bulb/socket operation. Execute this step deliberately and carefully to avoid dropping and losing either landing gear bulb. - IF THE BULBS ARE NOT THE PROBLEM If the bulb checks fail to establish the bulb as the problem, proceed with the manual gear deployment in the next steps. AIRSPEED... BELOW 100 MPH Slow down below the maximum manual gear deployment airspeed of 100 MPH. LANDING GEAR SELECTOR SWITCH... VERIFY DOWN Ensure that the landing gear selector switch is DOWN. NF ISSUE 9/12 ABNORMAL Flows and Checklists 10

EMERGENCY GEAR EXTENSION LEVER... HOLD DOWN Push the emergency gear extension lever DOWN and HOLD IT DOWN until manual gear deployment is complete, and only then release the lever. LANDING GEAR LIGHTS... CHECK 3 GREEN, NO RED Check that all three (3) green landing gear lights are now ON and the red warning light is out. If any gear down green bulb still fails to illuminate while another green bulb is now lit, it is possible that the manual gear extension was successful but the bulb is burned out. Troubleshoot as before by pulling out and switching the square green landing gear lights to test bulb/socket operation. - IF ANY GEAR IS STILL NOT DOWN AND LOCKED - If all of the above steps fail to extend the landing gear, try the following steps. Consult POH / AFM for additional information. YAW THE PLANE ABRUPTLY with RUDDER... EXECUTE Yaw the plane abruptly with the rudder in an attempt to dislodge the gear. SLOW DOWN to MCA (if previous step failed)... EXECUTE If previous step failed to deploy the gear, slow down to minimum controllable airspeed in preparation for the next step. LANDING GEAR LEVER (at MCA)... CYCLE UP, then DOWN While maintaining minimum controllable airspeed, recycle the landing gear switch. If all attempts to deploy the landing gear fail, prepare for Gear Up Emergency Landing. This Space is Intentionally Left Blank NF ISSUE 9/12 ABNORMAL Flows and Checklists 11

GEAR UP EMERGENCY LANDING (manual gear extension failed) SEATBELTS and SHOULDER HARNESSES... TIGHTEN FLAPS... AS REQUIRED RUNWAY... ASSURED - BEFORE TOUCHDOWN FUEL SELECTOR... OFF MASTER SWITCH... OFF MAGNETO SWITCH... OFF MIXTURE... IDLE CUT-OFF TOUCHDOWN... MINIMUM AIRSPEED EVACUATION... COMPLETE GEAR UP EMERGENCY LANDING, EXPANDED (manual gear extension failed) NOTE If In case of a planned gear-up landing, this checklist assumes that all possible options for extending the landing gear have been exhausted, and that company dispatch and ATC assistance has been obtained and is standing by, as appropriate. The flight crew should coordinate their interaction to ensure the procedure is conducted in a systematic and thorough manner. In a solo pilot operation, the pilot should verbalize and verify each step in the procedure as it is conducted. CAUTION Because of the unavailability of power after the execution of this procedure, it should be conducted only after the flight crew has committed to the landing. SEATBELTS and SHOULDER HARNESSES... TIGHTEN Ensure that all occupants have their seat belts and shoulder harnesses securely fastened, and TIGHTEN EACH INDIVIDUAL BELT, as the deceleration forces during gear up landing will be greater than during a normal landing. FLAPS... AS REQUIRED Set flaps as desired for the approach and landing. RUNWAY... ASSURED Establish on an approach with runway assured, and perform the following only when no possibility of a go-around exists. NF ISSUE 9/12 ABNORMAL Flows and Checklists 12

- BEFORE TOUCHDOWN - Once the runway has been assured, and before touchdown, perform the following steps. FUEL SELECTOR... OFF Turn the fuel selector to OFF (depress the safety latch first) to cut the fuel supply from the tanks to the rest of the fuel system and thus minimize the risk of fire on touchdown. MASTER SWITCH... OFF Turn the master switch OFF to minimize the risk of spark from energized electrical system. MAGNETO SWITCH... OFF Turn the magneto switch OFF to minimize the risk of spark from the ignition system. MIXTURE... IDLE CUT-OFF Move the mixture control to full aft, IDLE CUT-OFF position to cut the fuel to the engine. TOUCHDOWN... MINIMUM AIRSPEED Touchdown softly at minimum airspeed. EVACUATION... COMPLETE Promptly evacuate the aircraft and obtain external assistance. This Space is Intentionally Left Blank NF ISSUE 9/12 ABNORMAL Flows and Checklists 13

LANDING WITH A FLAT NOSE TIRE RADIO... TRANSMIT INTENTIONS BEFORE LANDING CHECKLIST... EXECUTE TOUCHDOWN... ON MAIN WHEELS ONLY NOSEWHEEL... HOLD OFF THE GROUND AFTER NOSEWHEEL TOUCHDOWN... YOKE FULL AFT TAXIING... MINIMIZE LANDING WITH A FLAT NOSE TIRE, EXPANDED NOTE If a flat tire or tire separation occurs during takeoff and an aborted takeoff is not feasible, land as soon as practical. RADIO... TRANSMIT INTENTIONS Transmit aircraft condition and intentions on ATC, Tower, CTAF or UNICOM frequency, as appropriate. BEFORE LANDING CHECKLIST... COMPLETE Execute the Before Landing Checklist in preparation for the approach. Plan to conduct a normal approach, as appropriate for the conditions. TOUCHDOWN... ON MAIN WHEELS ONLY Do not allow the nosewheel come in contact with the ground during touchdown. NOSEWHEEL... HOLD OFF THE GROUND Hold the nosewheel off the ground as long as possible while slowing down. AFTER NOSEWHEEL TOUCHDOWN... YOKE FULL AFT After the nosewheel touches down, maintain FULL AFT yoke deflection to take as much weight as possible off the nosewheel. TAXIING... MINIMIZE Taxi as little as possible after landing. Clear the runway, as necessary, communicate with ATC and obtain external assistance. Do not taxi on a flat tire unless moving the aircraft is necessary for safety. NF ISSUE 9/12 ABNORMAL Flows and Checklists 14

LANDING WITH A FLAT MAIN TIRE RADIO... TRANSMIT INTENTIONS BEFORE LANDING CHECKLIST... EXECUTE FLAPS... FULL RUNWAY SELECTION... CROSSWIND OPPOSITE FLAT TIRE TOUCHDOWN POINT... RWY SIDE OPPOSITE FLAT TIRE TOUCHDOWN... INFLATED TIRE FIRST NOSEWHEEL... LOWER IMMEDIATELY AILERON... HOLD OFF FLAT TIRE AS LONG AS POSSIBLE TAXIING...MINIMIZE LANDING WITH A FLAT MAIN TIRE, EXPANDED NOTE If a flat tire or tire separation occurs during takeoff and an aborted takeoff is not feasible, land as soon as practical. RADIO... TRANSMIT INTENTIONS Transmit aircraft condition and intentions to ATC, Tower, CTAF or UNICOM frequency, as appropriate. BEFORE LANDING CHECKLIST... COMPLETE Execute the Before Landing Checklist in preparation for the approach. Plan to conduct a normal approach, as appropriate for the conditions. FLAPS... FULL Set flaps to FULL, to allow the airplane to touch down at the lowest possible speed. RUNWAY SELECTION... CROSSWIND OPPOSITE DEFECTIVE TIRE If possible, select a runway so that the crosswind comes from the side opposite the defective tire. It will allow the airplane to touch down on the inflated tire first. It will also assist in the directional control after touchdown, as the airplane will tend to weathervane into the wind and the force of wind will oppose the friction force of the defective tire. If no such runway is available, select the runway with the most headwind. Avoid runways with crosswind on the same side as the defective tire, as it will possibly cause a touchdown on the defective tire first, and have a detrimental effect on directional control after touchdown. TOUCHDOWN POINT... RUNWAY SIDE OPPOSITE DEFECTIVE TIRE Touch down on the runway side opposite the defective tire. That way, if the aircraft starts yawing toward the defective tire due to the friction drag it produces, there will be the greatest runway width safety margin while the pilot establishes aircraft directional control. NF ISSUE 9/12 ABNORMAL Flows and Checklists 15

TOUCHDOWN... INFLATED TIRE FIRST Touch down on the inflated tire first. If crosswind exists from the side opposite the defective tire, the aircraft will naturally tend to touch down on the inflated tire. As the defective tire touches down following the inflated tire, anticipate immediate yawing motion toward the defective tire. AILERON... HOLD OFF FLAT TIRE AS LONG AS POSSIBLE If possible, use the aileron to first hold off, then lighten the load on the defective tire by applying the aileron control in the direction of the side opposite the defective tire. The aileron on the defective tire wing would then deflect down, generating more lift, and the weight on the defective tire would be reduced. TAXIING... MINIMIZE Taxi as little as possible after landing. Clear the runway, as necessary, communicate with ATC and obtain external assistance. Do not taxi on a flat tire unless moving the aircraft is necessary for safety. This Space is Intentionally Left Blank NF ISSUE 9/12 ABNORMAL Flows and Checklists 16

OTHER ABNORMAL SITUATIONS OPEN DOOR IN FLIGHT NOTE In the unlikely event of open door in flight, the airplane normal flight characteristics will not be affected, and the airplane can land normally with the door open. Therefore, it may be inadvisable for a single pilot to attempt to close the door, and proceeding to land may be the best course of action. Maintaining aircraft control shall be the utmost priority. With two pilots occupying front seats, the following procedure may be attempted, with one pilot safely maintain control of the aircraft, while the other is executing the procedure and shutting the door. OPEN DOOR IN FLIGHT AIRSPEED... BELOW 100 MPH CABIN AIR VENTS... CLOSED STORM WINDOW... OPEN IF TOP LATCH OPEN... CLOSE IT IF LOWER LATCH OPEN... OPEN TOP LATCH, PUSH DOOR OUT, CLOSE RAPIDLY TOP LATCH... CLOSE IT OPEN DOOR IN FLIGHT, EXPANDED AIRSPEED... BELOW 100 MPH Slow down below 100 MPH in order to reduce airflow over the cabin door. CABIN AIR VENTS... CLOSED Close all cabin air vents in order to reduce air pressure inside the cabin, which would be working against the door during attempts to shut it. STORM WINDOW... OPEN Open the storm window on the left side, which will have the effect of slightly lowering the cabin pressure, and assisting in shutting the door. IF TOP LATCH OPEN... CLOSE IT If only the top latch is open, latch it shut. IF LOWER LATCH OPEN.. OPEN TOP LATCH, PUSH DOOR OUT, CLOSE RAPIDLY If the lower latch is open, then open the top latch, push the door out and then close it rapidly. If done properly, this action will engage the lower latch. TOP LATCH... CLOSE IT With the lower latch engaged, top latch may also be latched closed, thereby completely securing the door. NF ISSUE 9/12 ABNORMAL Flows and Checklists 17