Small aircraft suffers loss of engine power while at low altitude with training in progress.

Attributes
ACN	279933
Time
Date	199408
Day	Fri
Local Time Of Day	1801 To 2400
Place
Locale Reference	airport : mi03
State Reference	MI
Altitude	agl bound lower : 400 agl bound upper : 800
Environment
Flight Conditions	VMC
Light	Daylight
Aircraft 1
Controlling Facilities	tower : mia
Operator	general aviation : personal
Make Model Name	Any Unknown or Unlisted Aircraft Manufacturer
Operating Under FAR Part	other : unknown
Flight Phase	descent : approach other other
Flight Plan	None
Person 1
Affiliation	Other
Function	instruction : instructor oversight : pic
Qualification	pilot : instrument pilot : cfi pilot : commercial
Experience	flight time last 90 days : 30 flight time total : 380 flight time type : 120
ASRS Report	279933
Person 2
Affiliation	Other
Function	flight crew : single pilot instruction : trainee
Qualification	pilot : student
Events
Anomaly	aircraft equipment problem : critical
Independent Detector	other flight crewa
Resolutory Action	flight crew : overcame equipment problem flight crew : declared emergency
Consequence	Other
Supplementary
Primary Problem	Aircraft

Narrative:

We were on an instructional flight, practicing basic maneuvers including glides, crabs and wing low crosswind approachs at altitude (approximately 2300 ft AGL to 1000 ft AGL) in an area used as the practice area for the local flight school this area is very sparsely populated. After identifying our emergency landing area (yuba airport, a grass strip) we began practicing rectangular courses, climbs and glides. We then began to practice glides along a straight road in preparation for training in crosswind lndgs. We were gliding down from about 3500 ft MSL (2800 ft AGL) along eht road. Carburetor heat was on. The day was relatively humid. We cleared the engine during the first one third of the glide with normal response. Upon reaching approximately 1000 ft AGL, we added power to climb out for another run. The engine did not respond to throttle advancement. After establishing best glide airspeed, I turned toward yuba, our designated emergency landing strip. We ran the emergency checklist, and by pumping the throttle regained minimal power. I pulled the mixture control to lean, and immediately advanced the control to full rich again, preparing to land, but giving the engine one more chance. After 2 more throttle pumps, the engine caught -- developed full power, and we climbed out without further engine difficulty. My only hypothesis here was that somehow we had fouled the plugs (since the engine was developing minimal power) and that the lean mixture allowed the fouling to burn off prior to engine power developing. We thought that our engine clearing procedure was adequate, but perhaps not.

Original NASA ASRS Text

Title: SMA SUFFERS LOSS OF ENG PWR WHILE AT LOW ALT WITH TRAINING IN PROGRESS.

Narrative: WE WERE ON AN INSTRUCTIONAL FLT, PRACTICING BASIC MANEUVERS INCLUDING GLIDES, CRABS AND WING LOW XWIND APCHS AT ALT (APPROX 2300 FT AGL TO 1000 FT AGL) IN AN AREA USED AS THE PRACTICE AREA FOR THE LCL FLT SCHOOL THIS AREA IS VERY SPARSELY POPULATED. AFTER IDENTIFYING OUR EMERGENCY LNDG AREA (YUBA ARPT, A GRASS STRIP) WE BEGAN PRACTICING RECTANGULAR COURSES, CLBS AND GLIDES. WE THEN BEGAN TO PRACTICE GLIDES ALONG A STRAIGHT ROAD IN PREPARATION FOR TRAINING IN XWIND LNDGS. WE WERE GLIDING DOWN FROM ABOUT 3500 FT MSL (2800 FT AGL) ALONG EHT ROAD. CARB HEAT WAS ON. THE DAY WAS RELATIVELY HUMID. WE CLRED THE ENG DURING THE FIRST ONE THIRD OF THE GLIDE WITH NORMAL RESPONSE. UPON REACHING APPROX 1000 FT AGL, WE ADDED PWR TO CLB OUT FOR ANOTHER RUN. THE ENG DID NOT RESPOND TO THROTTLE ADVANCEMENT. AFTER ESTABLISHING BEST GLIDE AIRSPD, I TURNED TOWARD YUBA, OUR DESIGNATED EMER LNDG STRIP. WE RAN THE EMERGENCY CHKLIST, AND BY PUMPING THE THROTTLE REGAINED MINIMAL PWR. I PULLED THE MIXTURE CTL TO LEAN, AND IMMEDIATELY ADVANCED THE CTL TO FULL RICH AGAIN, PREPARING TO LAND, BUT GIVING THE ENG ONE MORE CHANCE. AFTER 2 MORE THROTTLE PUMPS, THE ENG CAUGHT -- DEVELOPED FULL PWR, AND WE CLBED OUT WITHOUT FURTHER ENG DIFFICULTY. MY ONLY HYPOTHESIS HERE WAS THAT SOMEHOW WE HAD FOULED THE PLUGS (SINCE THE ENG WAS DEVELOPING MINIMAL PWR) AND THAT THE LEAN MIXTURE ALLOWED THE FOULING TO BURN OFF PRIOR TO ENG PWR DEVELOPING. WE THOUGHT THAT OUR ENG CLRING PROC WAS ADEQUATE, BUT PERHAPS NOT.

Data retrieved from NASA's ASRS site as of July 2007 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.