2.3 Honeywell Engines, Systems & Support TEST FLIGHT FACILITY Honeywell has maintained a small fleet of test aircraft at its Phoenix facility for many years. For aircraft equipped with engine inlet ice protection, revise the applicable Emergency Procedures or Abnormal Procedures Section of the applicable Flight Manual to include the following paragraph relating to a non-responsive power lever.
We provide a complete range of services designed to get you back in the air as quickly, safely and affordably as possible. 7 Information for reworking second stage turbine stator assemblies is available in Honeywell SB TPE331-72-2085RWK.Do not install any second stage turbine stator assembly P/N 894528-1, -2, -3, -5, -6, -10, and -11. after the effective date of this AD. 3 - Effective 14 May 1982 3. A product of evolution, the TPE 331-10T engine has earned a reputation of significant performance and reliability. 2016-18-17 - Effective 4 November 2016
RATINGS), the TPE331 met the requirements of many different business or commuter type airplanes with seating capacities of up to thirty-one seats. Turn to the pros at Turbine Standard for a mid-life Hot Section or Gear Box Inspection. 4 provides instructions for re-identification of stator assemblies from P/N 868379-1 to 868379-3. Our vast experience with the TPE331 enables us to provide you with an expert analysis of your engine's condition. DCA/AIR/25 - First Stage Turbine Disks - Effective 1 September 2009 With more than 13,000 engines delivered and more than 122 million hours of flight time, the TPE331 is one of the most reliable turboprop engines in the world. Honeywell International Inc. ASB No.
Turbine Standard knows the TPE331 inside u0003and out.
Airlines Pile On The Power To Beat The Challenges Of Their Harsh EnvironmentAviation is the most efficient way to travel in Southeast Alaska and there are two companies that specialize in flying around this challenging region. To prevent an engine fire caused by a fuel manifold assembly leak, accomplish the following:- Replace per Garrett Alert SB TPE331-A73-0198 Revision 1, Stratoflex Manifolds P/N 3102469-2 with dates of manufacture listed in Table 1 of the SB. And for every service we offer, we'll provide you with an accurate estimate, fast turn time and a warranty on our work. TPE331-72-A2150 dated 13 June 2008 pertains to the subject of this AD. DCA/AIR/8 - Third Stage Stators - Inspection. National Flight specializes in TPE 331 services including the tpe331-1, tpe331-2 Tpe331 strain gage torque system | TPE331 Strain Gage Torque System . 7.8 (TYP) 23.75 (TYP) 42.82 The engines power output ranges from 575 to 1650 shaft horsepower (shp). To prevent third stage turbine wheel separation due to fatigue cracking and shifting of the third stage turbine stator, which could result in an uncontained engine failure and damage to the aircraft, accomplish the following:- For engines with third stage turbine stators with S/Ns listed in Table 1 of National Flight Services ASB NF-TPE331-A72-10961, no action is required. All model TPE331-25AA and TPE331-1-151A not incorporating Airesearch SB's 659, 632 or TPE331-62-0064 All model TPE331-1, -2, -2UA, -3U, -3UW, -5, -5A, -6, -6A and TSE331-3U engines with third stage stator assembly P/N 868379-1, -3 or -5. We stock one of the world's largest inventories of accessories and LRU's (line replaceable units) for every model of Honeywell TPE331-1 through -14 series engine. DCA/AIR/7A - Oil Scavenge Pump Assembly - Inspection. DCA/AIR/20 - Second Stage Turbine Stator - Replacement 10 - Effective 28 November 2002 2018-22-01 - Second Stage Turbine Rotor Assembly - Effective 10 December 2018 $3,393.00. Social Honeywell TPE331-1, -2, -2UA, -3U, -3UW, -5, -5B, -6, -6A, -8, -10, -10AV, -10N, -10P, -10R, -10T, -10U, -10UA, -10UF, -10UR turboprop and TSE331-3U turboshaft engines fitted with hydraulic torque sensor gear assemblies P/N 3101726-1, -2 or -3.
3 - Effective 15 May 1974 Convert to TPE331-10 Engines, With Propulsion Internationals Low Entry Cost Options Cut Your Operating Cost Today. the TPE331-1 to 10s have the hydraulic torque sensing systems, RATINGS), the TPE331 met the requirements of many different business or commuter type airplanes with seating capacities of up to thirty-one seats. Perform repetitive FPIs of first stage turbine disks P/N 3101520-1 and P/N 3107079-1, per accomplishment instructions 2.B. Remove impellers with more than 8,900 cycles since weld repair, within 3,600 CIS, or at the next engine overhaul, or at the next major CAM compressor section inspection, whichever occurs first. honeywell, garrett, tpe 331, tas300-01-dt-230, tas300-01u-dt-230, tpe-331 tpe 331u tpe-331u.
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