Epstein Secrets

ished Of more space Is required attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) Removed Collins Part Number 822.9210-008 TDR-94D Mode S Diversity Transponders Serial Numbers 2221 and 3672 and Installed factory modified per Service Bulletin 504

cord. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Work Accomplished (If more space is required, attach addiffonal sheets. Identity with aircraft net-Iona* and repiygapn Tat* and date work completed.) US

5.1353 (aXe) Based on 14 CFR §§ 21 115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Collins Profile 21 FMS-6100 with LPV Approach enabled and UASC TAWS was determined to be TCDS Al 6SW and the following later regulations: AmdclOriginall

cord. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft actionably and registration mark end date work completed)

AVOliCS Callenlien Center 400 Collins Road NE Mad Station 164100 Cedes Rapids. IA 52498 Tel. 319295.2185 Fax 319 295O337 Rockwell Collins May 14, 2003 W0030737.DOC Flight Options 26180 Curtiss-Wright Parkway Cleveland, 011 44143 Tel: (216) 797-3500 Attention: Subject: Mr. Jody

ecord An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Work Accomplished Wince space is repine; attach addifional shags. Aka* with aircraft nationality and registration nark and date work completed) MAKE: RA

• 1. The following equipment was removed from the aircraft: PART NUMBER QTY MAKEJMODEUDE.SCRIPTION STATION INSTALLATION DATA 622-7203-101 3 Collins VHF-422b Comm 2. The following equipment was Installed In the aircraft. PART NUMBER QTY MAIEJMODEUDESCFtIPTIoN C37c, C38c TSO 450.0 • STATIO

cord. An alteration must be compatible with all previous alterations to assure continued confonnisy with the applicable airworthiness requirements. S. Description of Work Accomplished (If more spaces required, attach additional sheets. Identify with aircraft nationality and registration mask and date work completed.)

B. supplied to the operator. Where the CTL-92E Controller is referenced in the ICA, refer to the existing aircraft maintenance documentation for the Collins RTU-4200 Radio Tuning Unit. • No change to the electrical load for this rotorcraft. • Refer to the updated Aircraft Computed Weight and Balance,

record An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements S. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work accomplish