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|
Attributes | |
ACN | 1693886 |
Time | |
Date | 201910 |
Local Time Of Day | 1201-1800 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Flight Conditions | VMC |
Aircraft 1 | |
Make Model Name | Zenith Undifferentiated or Other Model |
Operating Under FAR Part | Part 91 |
Flight Phase | Landing |
Route In Use | Visual Approach |
Flight Plan | None |
Person 1 | |
Function | Pilot Not Flying |
Qualification | Flight Crew Commercial Flight Crew Flight Instructor Flight Crew Multiengine Flight Crew Instrument |
Events | |
Anomaly | Deviation - Procedural Published Material / Policy Deviation - Speed All Types Flight Deck / Cabin / Aircraft Event Other / Unknown Ground Event / Encounter Other / Unknown |
Narrative:
I went along as a passenger in my hangar neighbor's zenith 801. It was explained by this owner/ pilot/ builder these model planes have counter intuitive characteristics to typical major certified aircraft; and though it is a STOL aircraft; it requires a good deal of power and acutely higher pitch up for proper landings. Because of this; [pilot] was practicing simulated emergency engine out landings should he ever experience and engine failure. Though riding as a passenger; I am a commercially rated pilot and CFI; so I'm filing this form for the intended purpose of this NASA safety program. Naturally these same reasons; I did not want to be acting as an instructor or crew for this flight.my observations; the first power off landing was a made with no flaps and I thought was just ideal in every way. This second power off landing; was done with some with flaps extended when the field was thought to be made; I estimate 10-degree flaps were deployed. I noted an acute reduction aspect ratio after flaps were lowered. Realizing on short final that a power off glide was going to be short; pilot said: 'perhaps I should go around' and introduced power; plane then quickly achieved what appeared the needed glide path; it looked ideal; and he said; 'I think I will try to make this work'. Unfamiliar with this plane; sight picture would seem very reasonable. Pilot continued his power off glide toward the runway with similar aoa as previous landing. As we approached close to flare altitude; I looked over to notice airspeed indicator at 54 mph and falling rapidly! Alarmed by the rapid deceleration; I yelled 'power!' by that time indicator was passing though 50mph.there was a throttle on my side of the airplane; but since I was not acting as a pilot or instructor and for the unfamiliarity of this aircraft; I thought it safer and only appropriate to only advise the observation of critical airspeed decay; so I didn't consider counter control input or trying to add power myself.the pilot dropped the nose and added power to recover; from my experience in certified aircraft; for a balked landing I would have added power and pulled the nose up; but this zenith 801 is so different I thought best to only alert the pilot the urgency to take action for the decaying airspeed. There was some mild wind gust; and we were in the unfortunate phase of those gust as well. After exhaustive thought; for the unusual flight characteristics of this zenith 801 with flaps deployed; I still cannot say definitively what the correct correction of pitch should have been for this situation of low airspeed and low altitude for this aircraft. [Pilot] is a very conscientious and exemplary pilot; I'm inclined to believe that this experimental model aircraft with flaps deployed; may simply be inherently hazardous for power off landings. Perhaps this could be very useful in advising other similar experimental owners; builders; and pilots of this designs insidious power off characteristics.
Original NASA ASRS Text
Title: Passenger reported a significant loss of airspeed during final approach that would have resulted in a stall if corrective action were not immediately taken.
Narrative: I went along as a passenger in my hangar neighbor's Zenith 801. It was explained by this owner/ pilot/ builder these model planes have counter intuitive characteristics to typical major certified aircraft; and though it is a STOL aircraft; it requires a good deal of power and acutely higher pitch up for proper landings. Because of this; [pilot] was practicing simulated emergency engine out landings should he ever experience and engine failure. Though riding as a passenger; I am a commercially rated pilot and CFI; so I'm filing this form for the intended purpose of this NASA safety program. Naturally these same reasons; I did not want to be acting as an instructor or crew for this flight.My observations; the first power off landing was a made with no flaps and I thought was just ideal in every way. This second power off landing; was done with some with flaps extended when the field was thought to be made; I estimate 10-degree flaps were deployed. I noted an acute reduction aspect ratio after flaps were lowered. Realizing on short final that a power off glide was going to be short; pilot said: 'perhaps I should go around' and introduced power; plane then quickly achieved what appeared the needed glide path; it looked ideal; and he said; 'I think I will try to make this work'. Unfamiliar with this plane; sight picture would seem very reasonable. Pilot continued his power off glide toward the runway with similar AOA as previous landing. As we approached close to flare altitude; I looked over to notice airspeed indicator at 54 mph and falling rapidly! Alarmed by the rapid deceleration; I yelled 'power!' by that time indicator was passing though 50mph.There was a throttle on my side of the airplane; but since I was not acting as a pilot or instructor and for the unfamiliarity of this aircraft; I thought it safer and only appropriate to only advise the observation of critical airspeed decay; so I didn't consider counter control input or trying to add power myself.The pilot dropped the nose and added power to recover; from my experience in certified aircraft; for a balked landing I would have added power and pulled the nose up; but this Zenith 801 is so different I thought best to only alert the pilot the urgency to take action for the decaying airspeed. There was some mild wind gust; and we were in the unfortunate phase of those gust as well. After exhaustive thought; for the unusual flight characteristics of this Zenith 801 with flaps deployed; I still cannot say definitively what the correct correction of pitch should have been for this situation of low airspeed and low altitude for this aircraft. [Pilot] is a very conscientious and exemplary pilot; I'm inclined to believe that this experimental model aircraft with flaps deployed; may simply be inherently hazardous for power off landings. Perhaps this could be very useful in advising other similar experimental owners; builders; and pilots of this designs insidious power off characteristics.
Data retrieved from NASA's ASRS site and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.