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|
Attributes | |
ACN | 1700499 |
Time | |
Date | 201911 |
Local Time Of Day | 0601-1200 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Make Model Name | Skylane 182/RG Turbo Skylane/RG |
Operating Under FAR Part | Part 91 |
Flight Phase | Takeoff |
Route In Use | Direct |
Flight Plan | VFR |
Component | |
Aircraft Component | RPM/N1/N2/Etc Indication |
Person 1 | |
Function | Single Pilot |
Qualification | Flight Crew Instrument Flight Crew Multiengine Flight Crew Commercial |
Experience | Flight Crew Last 90 Days 20 Flight Crew Total 379 Flight Crew Type 48 |
Events | |
Anomaly | Aircraft Equipment Problem Critical Deviation - Procedural Published Material / Policy Deviation - Procedural Clearance |
Narrative:
During the take-off roll or just after departing the surface of runway xx; the engine began to not develop full power; RPM's were fluctuating between 2000 and 2200. The take-off roll was sluggish; but not excessive. Upon noting the decreased engine performance; decision was made to abort the take-off and land on the remaining surface. We advised ATC. The subsequent descent and landing were un-eventful. Upon exiting the runway; I requested and was granted clearance for a high speed taxi on an adjacent taxi-way that was clear of traffic. I performed this high speed taxi at full power for a few seconds and noted similar indications; RPM's fluctuated between 2100 and 2300. Oil pressure; oil temperature; and cylinder head temperature were normal. Oil was observed at 10 quarts during the pre-flight. Pre-flight and run-up were completed with a few slight abnormalities.the engine start was difficult and priming was required. A normal start in this aircraft doesn't require priming beyond a couple pumps of the throttle. However; the primer plunger was needed to start the engine in this case. The weather was cool in the morning and the aircraft had not flown. During run-up; the carburetor heat check produced RPM's barely 100 lower than without carburetor heat. After run-up; the engine idled at a much higher RPM than usual (1000 vs. 650).
Original NASA ASRS Text
Title: C182 pilot reported that a partial loss of engine power on takeoff resulted in a precautionary landing.
Narrative: During the take-off roll or just after departing the surface of Runway XX; the engine began to not develop full power; RPM's were fluctuating between 2000 and 2200. The take-off roll was sluggish; but not excessive. Upon noting the decreased engine performance; decision was made to abort the take-off and land on the remaining surface. We advised ATC. The subsequent descent and landing were un-eventful. Upon exiting the runway; I requested and was granted clearance for a high speed taxi on an adjacent taxi-way that was clear of traffic. I performed this high speed taxi at full power for a few seconds and noted similar indications; RPM's fluctuated between 2100 and 2300. Oil pressure; oil temperature; and cylinder head temperature were normal. Oil was observed at 10 quarts during the pre-flight. Pre-flight and run-up were completed with a few slight abnormalities.The engine start was difficult and priming was required. A normal start in this aircraft doesn't require priming beyond a couple pumps of the throttle. However; the primer plunger was needed to start the engine in this case. The weather was cool in the morning and the aircraft had not flown. During run-up; the carburetor heat check produced RPM's barely 100 lower than without carburetor heat. After run-up; the engine idled at a much higher RPM than usual (1000 vs. 650).
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.