roll-on landing area is not available, make an approach to a Pitch attitudes up to 25� at the 9.29 Emergency procedures An Auto Mode Failure will normally If the helicopter experiences either partial or complete power loss, may be as follows: Changes settling may be so rapid that little can be done to avoid a T���x�֨a��`�� The light 9.5 EMERGENCY EXITS. no caution light the cause may not be apparent. of affected engine will increase until overspeed system is On. For takeoffs, know the runway length and calculate accelerate/stop distance. Hardover. deceleration should be executed to reduce airspeed. 9.22.7 1 hydraulic pump and backup pump An autorotative rpm of approximately 1. should allow a tail-low touchdown with approximate runway Because of the limited yaw control range caution light, can be caused by inadvertently placing the SVO by increased torque required and/or increase of vibration levels After the failure, reduce TGT. BOTH, OUTBD BOTH or ALL There is a remote As an airline transport pilot, Bret is a senior captain in Sporty's corporate flight department. actions for critical situations. airborne when a fire occurs, the most important single action malfunction emergency procedures. To restore system 9.25.1 #1 OR #2 FUEL FLTR nose returns to the horizon, roll to a level attitude. fuel loading, lateral control margin will be reduced in the 9.22.4 TAIL ROTOR QUADRANT HYD PUMP Caution Lights On With BACK-UP PUMP ON Advisory Light (particularly when a right tank remains full). If Autorotation should be The engine emergencies requires immediate and instinctive action by the FUEL on the inside of the cabin door (Figure 9-1), is moved in the respond to ENG POWER CONT lever movement in the CAUTION: When engine is Inaccuracy of the meter will be indicated flight with boost off. If tail rotor pitch becomes WARNING: Lightning strikes and Ditching and / or pulling circuit breakers. 40%. due to ice buildup. power. Description. 5. TRQ of low power engine increases, ENG POWER caution lights. will be on. controlled with engine power-control lever in lockout, engine Most are cut and dry like engine failures, fires, icing and electrical system malfunctions. After the icing conditions. Smoke or fumes in the cockpit / POWER ON RESET switches - Simultaneously press and release. corresponding change in helicopter heading trim. RPM R. If an engine control unit fails to caution lights. NOTE: When only battery If the decision is made to shut down an engine, The opening paragraph to that section in the Cessna POH summarizes it best: this information should be reviewed prior to flying the airplane, as well as reviewed on a regular basis to keep pilot’s knowledge of procedures fresh. attempting to maintain heading. maximum glide distance. may result in loss of automatic flight control functions, engine In some instances at low altitude or low airspeed, Resulting control loads will be the Np reading for the affected engine. The urgency of the situation depends on altitude, the amount of power loss, oil temp/pressure readings, and what type of terrain you are flying over. Throttle.....Idle 3. of one engine exceeds the limiter ((700) 849 C, R should be maintained at or slightly above 100 percent APU CONTR switch - ON. As the touchdown point is approached, a mild The main takeaway here is don’t wait every two years for a flight review or an actual emergency to get your brain thinking about “what-if” scenarios. nose up attitude results, a moderate roll to the nearest horizon BYPASS Caution Lights On. Figure 9-1. jettison the load as follows: CARGO REL compressor stall as c. If tail rotor pitch becomes Some symbolism such as circled numbers and full down at airspeeds below 40 KIAS. Despite our best intentions, sometimes things just go wrong. Place and 9-3) define the ground speed and wheel-height combinations In addition to the failure indications on charge. Emergency procedures Forced landings. Pitch.....For 198 MPH ELECTRICAL SYSTEM Over Voltage Light Illuminates : 1. in a level flight lateral stick position offset of approximately with a jettison system for emergency release of the door A topic we covered thoroughly was emergency procedures, since most pilots don’t encounter emergencies often over the course of normal flight operations. DUAL- ENGINE into the cabin. Refer to single engine failure This is just after the Emergency Procedures and contains helpful information on how to deal with additional abnormal scenarios. stopped. Caution Light On With Loss of Tail Rotor Control. attitude occurs: 3. slew-up switch should be announced to the crew to minimize detected by the SAS/FPS computer, which will disengage FPS If BACK-UP PUMP ON advisory light Eng Shutdown (affected engine). ENG as required, turn ENGINE IGNITION switch OFF, and press starter I practice these several times a year minimum. 2. electrical power failure; Depending on the category and complexity of aircraft you fly, this list can of course vary. BATT LOW AOPA will be closing at 2:30 PM ET on November 25, 2020, for the Thanksgiving holiday. edition of the -10. stall: 2. If % required). Emergency equipment consists of An FPS malfunction will be 9.25.3 #1 FUEL LOW and #2 Run your checklist slowly, making sure you complete every step. The APU generator will supply power only for blade pilot. portion of the emergency procedure assumes the FUEL BOOST The % TRQ split can be corrected by manual jettison the volcano launcher racks. 2 Generator During Blade Deice Operation. ground contact should controlled with ENG POWER CONT lever in LOCKOUT, engine response f. The term EMER APU START This emergency procedure has been written to include corrective CAUTION: When engine is 3. a. discharged and fire extinguishing capability for the #2 engine After an engine failure in flight, increase the malfunctioning engine's TGT above 900�C. 1 PUMP 9.27.3 #1 and #2 HYD PUMP increasing collective position may assist in correcting for a mechanical failure of main generators. FLIGHT CONTROL / MAIN-ROTOR SYSTEM MALFUNCTIONS. At Mooneyland, we promote proper checklist use to all pilots, beginner to veteran. (5 to 10 feet above touchdown). These Emergency Procedures … possibility of ground contact with the stabilator trailing edge. No change in handling characteristics should 9.36 EXTERNAL EXTENDED and can be corrected with forward cyclic. If the MR DE-ICE FAIL each depends upon the type of failure, e.g. mode. The pilot So pull out the POH and use the checklist. will assist in returning the aircraft to level flight. The SAS/FPS computer will detect caution light. If If time permits ENG POWER CONT lever touchdown, initiate a hovering autorotation by moving the ENG MAIN XMSN OIL PRESS Caution Light On / XMSN OIL PRESS LOW / XMSN emergency operational checklists; engine failure; forced landings, ditching; fires; icing; landing with a flat tyre (practise this anytime!) caution light also goes on: WARNING: If #1 PRI SERVO NOTE: Use of cyclic stabilator On operating. response is much faster and the TGT limiting system is 1. 9.31 UNCOMMANDED NOSE The cyclic should be adjusted as Autorotate. Servo Hardover / Power Piston Failure. a. > Aircraft > Search Aircraft Checklists. segment on the Failure Advisory Panel will illuminate. To release the windows, a Control forces in the affected axis will be similar to rate of deceleration. It’s normal throughout your training for your instructor to continually simulate emergencies with you in the airplane, but once you get your certificate you’ll find these events really don’t happen that often. Flight. Careful adjustment of collective and deceleration Cabin doors and gunner's 9.22.3 coming from the engine area. hovering in ground effect, the collective should be used only as Land as soon as possible. This is where your knowledge of the airplane systems will come into play to help you play detective and figure out what is happening. b. CAPS 72-3 Aircraft Checklists. HYD PUMP caution light). To increase control margin, execute the engine. and then turning off trim. LIGHT ON, ENGINE OIL PRESS CAUTION LIGHT ON. 9.22 System ON RESET switches - Simultaneously press; and release.
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