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|
Attributes | |
ACN | 455923 |
Time | |
Date | 199911 |
Day | Sun |
Local Time Of Day | 1201 To 1800 |
Place | |
State Reference | NC |
Altitude | msl single value : 2500 |
Environment | |
Flight Conditions | VMC |
Light | Night |
Aircraft 1 | |
Operator | general aviation : personal |
Make Model Name | Chancellor 414A & C414 |
Operating Under FAR Part | Part 91 |
Flight Phase | climbout : initial |
Route In Use | departure other |
Flight Plan | None |
Person 1 | |
Affiliation | other |
Function | flight crew : single pilot |
Qualification | pilot : commercial pilot : multi engine pilot : private pilot : instrument |
Experience | flight time last 90 days : 60 flight time total : 3050 flight time type : 50 |
ASRS Report | 455923 |
Person 2 | |
Affiliation | other |
Function | controller : local |
Qualification | controller : non radar |
Events | |
Anomaly | aircraft equipment problem : critical other anomaly other |
Independent Detector | aircraft equipment other aircraft equipment : engine power loss other flight crewa |
Resolutory Action | flight crew : landed in emergency condition other |
Consequence | other |
Supplementary | |
Problem Areas | Aircraft |
Primary Problem | Aircraft |
Narrative:
Departed after normal run-up. On climb out, left manifold pressure dropped to 26 inches. Adjusting throttle did nothing. A visual out the window confirmed suspicion of exhaust failure. Secured left engine, returned to departure airport. Single engine landing completed, secured aircraft. Observed heat damage to engine cowling. The next day the mechanic looked and found that the wye connector on the right bank of cylinders had failed. This caused heat damage to hoses downstream.
Original NASA ASRS Text
Title: PLT OF A CESSNA 414 RETURNED TO LAND AFTER SHUTTING DOWN THE L ENG DUE TO AN ENG PWR LOSS ASSOCIATED WITH AN ENG EXHAUST FAILURE.
Narrative: DEPARTED AFTER NORMAL RUN-UP. ON CLBOUT, L MANIFOLD PRESSURE DROPPED TO 26 INCHES. ADJUSTING THROTTLE DID NOTHING. A VISUAL OUT THE WINDOW CONFIRMED SUSPICION OF EXHAUST FAILURE. SECURED L ENG, RETURNED TO DEP ARPT. SINGLE ENG LNDG COMPLETED, SECURED ACFT. OBSERVED HEAT DAMAGE TO ENG COWLING. THE NEXT DAY THE MECH LOOKED AND FOUND THAT THE WYE CONNECTOR ON THE R BANK OF CYLINDERS HAD FAILED. THIS CAUSED HEAT DAMAGE TO HOSES DOWNSTREAM.
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.