Falcon: Passenger O2 Masks Life Limit
The Chapter 5 service life limitation for Passenger O2 masks has been removed. Keep reading to learn the new inspection schedule.
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The Chapter 5 service life limitation for Passenger O2 masks has been removed. Keep reading to learn the new inspection schedule.
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August 5, 2014, is the deadline for AD 2013-13-09 on Learjet 60 aircraft. It requires up to four different Service Bulletins be installed, depending on serial number. Keep reading for a brief explanation of each.
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Many Cessna operators have already complied with Cessna’s mandatory Service Bulletin SB560XL-27-34. Don’t forget the second step to this SB that is optional, but just as important.
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Out of production Hawker aircraft parts cause major delays and frustrations. Duncan Aviation wants to share with you their success.
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The Gulfstream IV Structural Repair Manual is very specific on rivet substitution i.e.: It is not permissible to substitute a mechanical fastener in place of a solid fastener. Check all references to assure correct fastener installation.
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In response to customers’ growing maintenance needs in large cabin Embraer and Gulfstream aircraft, Duncan Aviation has added a new tech to support these airframes at its Lincoln, Nebraska, headquarters.
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The original equipment landing lights on Hawker aircraft have been a frequent source of frustration for operators. LoPresti BoomBeam lights use mercury and Xenon gas which yield whiter, truer colors and better performance.
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Honeywell has made CAMP program a requirement for all Honeywell MSP and FMP engines. However, it is not a requirement for non-MSP operators.
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Don’t allow your DME-42 / DME-442 to fail due to out-of-date capacitors.
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Sulfation of the plates and damaged terminal studs are common warranty claims on Securaplane Batteries. Both can be prevented or lessened by following simple operational and maintenance procedures.
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There are two steps to Airworthiness Directive 2010-07-02. You are not in compliance unless you have completed both.
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Due to a small number of turbine blade separations related to stress ruptures, Honeywell issued SB TFE731-72-3494 to significantly increase the reliability of the turbine blades and reduce the risk of sudden inflight failures and the maintenance costs associated with them.
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Task card 57-00-00-210-801 has just been revised to clarify and provide less restrictive instructions for inspecting the outboard slats for overheat.
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Rolls Royce issued a recent News Flash about the potential for nuisance T2.5 Faults occurring following engine starts on AE 3007C Series engines on Citation X aircraft.
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Recent revisions to the Learjet Replacement Schedule have installed an ultimate life on the MLG Strut Torque Links. Keep reading for the stipulations required for each model of aircraft.
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