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37000 Feet | Browse and search NASA's Aviation Safety Reporting System |
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| Attributes | |
| ACN | 115800 |
| Time | |
| Date | 198907 |
| Day | Mon |
| Local Time Of Day | 1801 To 2400 |
| Place | |
| Locale Reference | airport : psp |
| State Reference | CA |
| Altitude | agl bound lower : 0 agl bound upper : 0 |
| Environment | |
| Flight Conditions | VMC |
| Light | Daylight |
| Aircraft 1 | |
| Operator | common carrier : air carrier |
| Make Model Name | Small Transport, Low Wing, 2 Turboprop Eng |
| Flight Phase | climbout : takeoff ground other : taxi |
| Flight Plan | IFR |
| Person 1 | |
| Affiliation | company : air carrier |
| Function | flight crew : captain oversight : pic |
| Qualification | pilot : instrument pilot : atp pilot : cfi pilot : commercial |
| Experience | flight time last 90 days : 227 flight time total : 7401 flight time type : 4940 |
| ASRS Report | 115800 |
| Events | |
| Anomaly | aircraft equipment problem : critical non adherence : far |
| Independent Detector | other flight crewa |
| Resolutory Action | none taken : anomaly accepted |
| Consequence | Other |
| Supplementary | |
| Primary Problem | Flight Crew Human Performance |
| Air Traffic Incident | Pilot Deviation |
Narrative:
During takeoff the engines were brought to high idle abruptly. The rapid increase in fuel flow and high ambient temperatures (110 degree F+) resulted in momentary egt indications of approximately 30 degree C over maximum for that RPM. I didn't recognize the overtemp condition because the change to high idle normally is not temperature critical and the egt observed is very common during engine start. In short I failed to correlate the egt limitation with the RPM. The biggest problem is that the aircraft continued in service for 2 days until I realized my mistake and reported it to the company. My recommendation, aside from vigilance, is for the aircraft and engine manufacturers to revise their operating manuals with a warning about this potential for overtemp.
Original NASA ASRS Text
Title: COMMUTER SMT OVER MAXIMUM EGT WAS NOT REPORTED FOR 2 DAYS. SITUATION OCCURRED WHEN ENGINES WERE BROUGHT TO HIGH IDLE AT THE START OF TKOF. HIGH AMBIENT GND TEMPERATURE WAS A FACTOR.
Narrative: DURING TKOF THE ENGINES WERE BROUGHT TO HIGH IDLE ABRUPTLY. THE RAPID INCREASE IN FUEL FLOW AND HIGH AMBIENT TEMPS (110 DEG F+) RESULTED IN MOMENTARY EGT INDICATIONS OF APPROX 30 DEG C OVER MAX FOR THAT RPM. I DIDN'T RECOGNIZE THE OVERTEMP CONDITION BECAUSE THE CHANGE TO HIGH IDLE NORMALLY IS NOT TEMP CRITICAL AND THE EGT OBSERVED IS VERY COMMON DURING ENGINE START. IN SHORT I FAILED TO CORRELATE THE EGT LIMITATION WITH THE RPM. THE BIGGEST PROBLEM IS THAT THE ACFT CONTINUED IN SERVICE FOR 2 DAYS UNTIL I REALIZED MY MISTAKE AND REPORTED IT TO THE COMPANY. MY RECOMMENDATION, ASIDE FROM VIGILANCE, IS FOR THE ACFT AND ENGINE MANUFACTURERS TO REVISE THEIR OPERATING MANUALS WITH A WARNING ABOUT THIS POTENTIAL FOR OVERTEMP.
Data retrieved from NASA's ASRS site as of August 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.