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|
Attributes | |
ACN | 965574 |
Time | |
Date | 201108 |
Local Time Of Day | 0001-0600 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Light | Night |
Aircraft 1 | |
Make Model Name | Q400 |
Operating Under FAR Part | Part 121 |
Flight Phase | Initial Approach |
Flight Plan | IFR |
Component | |
Aircraft Component | Indicating and Warning - Hydraulics |
Person 1 | |
Function | Captain |
Qualification | Flight Crew Air Transport Pilot (ATP) |
Events | |
Anomaly | Aircraft Equipment Problem Critical Deviation - Procedural Published Material / Policy Deviation - Procedural MEL |
Narrative:
On approach to ZZZ; Q400 aircraft power transfer unit (ptu) light did not come 'on' with selection of flaps five or when ptu switch was selected 'on'. Upon landing and shutdown; ptu advisory bulb tested good. Maintenance control was consulted; and as per their request and the 'ptu light inoperative' MEL provisions; engine # 1 was started to attempt to verify ptu operation. Following engine shutdown; I realized there was a probable typographical error in the step # 10 of the maintenance action portion of the MEL; leading to an unsuccessful test outcome (referring to system # 3 hydraulic pressure vs.the appropriate system # 2 hydraulic pressure). Maintenance control was consulted on this issue; whereupon they sent out contract maintenance to redo the MEL maintenance action; which resulted in a satisfactory ptu system test. Upon consultation with and regulation interpretation from the duty officer; the ptu MEL was accepted by the pilots and maintenance control. The unsuccessful ptu operation's test conducted in accordance with (in accordance with) ptu light inop MEL; was resultant from a typographical error in step # 10 of the pilot or maintenance procedure. The step tells the performer to verify system # 3 hydraulic pressure vs. The correct system # 2 pressure.
Original NASA ASRS Text
Title: While on initial approach; a Q400 Captain noticed the Power Transfer Unit (PTU) light did not come 'On' with selection of Flaps Five; or when the PTU switch was selected 'On'. A typographical error in Step # 10 of the Maintenance Action portion of the MEL led to an unsuccessful test outcome; when attempting to satisfy the MEL Maintenance Action requirement.
Narrative: On approach to ZZZ; Q400 aircraft Power Transfer Unit (PTU) light did not come 'On' with selection of Flaps Five or when PTU switch was selected 'On'. Upon landing and shutdown; PTU advisory bulb tested good. Maintenance Control was consulted; and as per their request and the 'PTU Light INOP' MEL provisions; engine # 1 was started to attempt to verify PTU operation. Following engine shutdown; I realized there was a probable typographical error in the Step # 10 of the Maintenance Action portion of the MEL; leading to an unsuccessful test outcome (referring to System # 3 Hydraulic pressure vs.the appropriate System # 2 Hydraulic pressure). Maintenance Control was consulted on this issue; whereupon they sent out Contract Maintenance to redo the MEL Maintenance Action; which resulted in a satisfactory PTU System Test. Upon consultation with and regulation interpretation from the Duty Officer; the PTU MEL was accepted by the pilots and Maintenance Control. The unsuccessful PTU Operation's Test conducted In Accordance With (IAW) PTU Light Inop MEL; was resultant from a typographical error in Step # 10 of the Pilot or Maintenance procedure. The Step tells the performer to verify System # 3 Hydraulic pressure vs. the correct System # 2 pressure.
Data retrieved from NASA's ASRS site as of April 2012 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.