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|
Attributes | |
ACN | 1314558 |
Time | |
Date | 201511 |
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 | Lancair IV/IVP |
Operating Under FAR Part | Part 91 |
Route In Use | Direct |
Flight Plan | IFR |
Component | |
Aircraft Component | Hydraulic System Pump |
Person 1 | |
Function | Pilot Flying Single Pilot |
Qualification | Flight Crew Instrument Flight Crew Commercial |
Experience | Flight Crew Last 90 Days 40 Flight Crew Total 700 Flight Crew Type 50 |
Events | |
Anomaly | Aircraft Equipment Problem Less Severe Deviation - Procedural Published Material / Policy Deviation - Procedural FAR |
Narrative:
We had a hydraulic pump that was performing erratically and after maintenance inspection the plane was returned to service; but we pulled the circuit breaker on the hydraulic pump and placarded it as inoperable for the flight as a precaution after initially charging the hydraulic pressure in case any was needed. As a further safety precaution we elected not to raise the gear and flew below gear extension speed limits. We flew filed IFR (but entirely in VMC conditions) directly to the location of the builder of the airplane; to have the pump inspected by the people most knowledgeable about the plane; who designed and built the system; as the plane is experimental and there is no stock maintenance guide for an unfamiliar mechanic to follow.
Original NASA ASRS Text
Title: LNP4 pilot reported ferrying the aircraft for maintenance after a hydraulic pump malfunctioned.
Narrative: We had a hydraulic pump that was performing erratically and after maintenance inspection the plane was returned to service; but we pulled the circuit breaker on the hydraulic pump and placarded it as inoperable for the flight as a precaution after initially charging the hydraulic pressure in case any was needed. As a further safety precaution we elected not to raise the gear and flew below gear extension speed limits. We flew filed IFR (but entirely in VMC conditions) directly to the location of the builder of the airplane; to have the pump inspected by the people most knowledgeable about the plane; who designed and built the system; as the plane is experimental and there is no stock maintenance guide for an unfamiliar mechanic to follow.
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.