From: Sent: To: Subject: Attachments: Lvjet < Friday, April 11, 2014 8:36 PM [email protected] Fwd: Pree-inductiontest of ESN 726121 - WO 800724 IMG_4020JPG; IMG_4022JPG; IMG_4025JPG; IMG_4036JPG; IMG_4044JPG; 20140407073609311.pdf From: MANNYFJTP < To: JETCARE ; aircraftem < >; Ivjet < Sent: Tue, Apr 8, 2014 7:07 am Subject: Re: Pree-inductiontest of ESN 726121 - WO 800724 Good morning Larry: ESN 726122 ><=r> Cc: fjturbinepower Attached are the pre-induction test results for ESN 726122, test was g=od, it has 1°C margin to EHM. This engine will go into disassembly tomorro=. ESN 726121 Engine in disassembly, finding heavy corrosion, delaminating and =oss of acoustical liners inside the fan duct (pictures attached). Regards, Manny Cas=ariedo Vice President F. J. Turbine Power, Inc. CFM 56 & JT8D FAA Repair Station F7JR192Y Phone: E-mail: <mailto chttp://www.fiturbinepower.net> > Web Page= www.fjturbinepo=er.net In a message dated 4/2/2014 6:39:00 P.M. Eastern Daylight Time, <mailto > writes: Hi Manny Make sure to cc Larry Morrison on these emials,. It's very important t= include him,. Thx Larry Visoski JEGE Inc N908JE EFTA_R1_02132617 EFTA02712819

Sent from my iPad On Apr 2, 2014, at 4:46 PM, wrote: Mike: Engine tested today, attached test cell report. It was rejected for being -2°C on EHM margin and slow acceleratio= and auto reserve power (related to FCU). Recommend to OH FCU. ESN 726122 will go to test cell tomorrow and test later tomorrow or Friday. Regards, Manny Cas=afiedo Vice President F. J. Turbine Power, Inc. CFM 56 & JT80 FAA Repair Station F7JR192Y Phone: E-mail: <mailto <http://www.fjturbinepower.neth C0140402144442653.pdf> > Web Page: www.fjturbi=epower.net 2 EFTA_R1_02132618 EFTA02712820