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|
Attributes | |
ACN | 482285 |
Time | |
Date | 200008 |
Day | Wed |
Local Time Of Day | 1201 To 1800 |
Place | |
Locale Reference | airport : ggg.airport |
State Reference | TX |
Altitude | msl single value : 2500 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Operator | general aviation : instructional |
Make Model Name | Skyhawk 172/Cutlass 172 |
Operating Under FAR Part | Part 91 |
Navigation In Use | other |
Flight Phase | cruise : level |
Flight Plan | None |
Person 1 | |
Affiliation | other |
Function | instruction : instructor |
Qualification | pilot : cfi pilot : commercial pilot : instrument |
Experience | flight time last 90 days : 160 flight time total : 600 flight time type : 300 |
ASRS Report | 482285 |
Person 2 | |
Affiliation | other |
Function | instruction : trainee |
Qualification | pilot : student |
Events | |
Anomaly | aircraft equipment problem : critical other anomaly other |
Independent Detector | other controllera other flight crewa |
Resolutory Action | controller : issued advisory controller : provided flight assist flight crew : declared emergency flight crew : diverted to another airport |
Consequence | other other |
Supplementary | |
Problem Areas | Flight Crew Human Performance Maintenance Human Performance Aircraft |
Primary Problem | Aircraft |
Narrative:
Training flight in a C172 at 2100 ft cruise climb to 2500 ft when loss of RPM occurred. Violent shaking under the cowling and engine roughness was observed. We were able to sustain altitude at vy and 1800 RPM. Oil temperature and oil pressure remained constant -- no rise in temperature or loss of pressure. My first thought was fouled magnetos or a bad cylinder. We declared an emergency, as RPM's decreased and vibrations increased -- failure was imminent. Longview approach confirmed thompson airport was in our vicinity and we made a landing approximately 10 mins after initial loss of power occurred. It was determined by a mechanic that the rods on the #3 cylinder had snapped -- probably due to the exhaust valve not opening.
Original NASA ASRS Text
Title: A C172 IN CRUISE AT 2500 FT DECLARED AN EMER AND DIVERTED DUE TO LOSS OF PWR CAUSED BY A FAILED CONNECTING ROD.
Narrative: TRAINING FLT IN A C172 AT 2100 FT CRUISE CLB TO 2500 FT WHEN LOSS OF RPM OCCURRED. VIOLENT SHAKING UNDER THE COWLING AND ENG ROUGHNESS WAS OBSERVED. WE WERE ABLE TO SUSTAIN ALT AT VY AND 1800 RPM. OIL TEMP AND OIL PRESSURE REMAINED CONSTANT -- NO RISE IN TEMP OR LOSS OF PRESSURE. MY FIRST THOUGHT WAS FOULED MAGNETOS OR A BAD CYLINDER. WE DECLARED AN EMER, AS RPM'S DECREASED AND VIBRATIONS INCREASED -- FAILURE WAS IMMINENT. LONGVIEW APCH CONFIRMED THOMPSON ARPT WAS IN OUR VICINITY AND WE MADE A LNDG APPROX 10 MINS AFTER INITIAL LOSS OF PWR OCCURRED. IT WAS DETERMINED BY A MECH THAT THE RODS ON THE #3 CYLINDER HAD SNAPPED -- PROBABLY DUE TO THE EXHAUST VALVE NOT OPENING.
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.