Epstein Secrets

manual. Inspection intervals shall remain as indicated in the aircraft maintenance manual or operators approved inspection program as appropriate. Weight and Balance unaffected. Reference Constant Aviation work order CCM-3160 END MAGUS:nal Sews NO needled FM Form 337 (10/06) Page 2 SDNY_GM_02754906 • •

record An alteration must be compatible with all previous alterations to assure continued conformity with the appltable airworthiness requirements S. Description of Work Accomplished (If nave space is required attach adationat sheets Identify with aircraft nationally and regatta:ran mark and So work completed) /419

aintenance instructions to ensure continued airworthiness any time the above equipment Is removed and/or repaired and reinstalled. 9. The aircraft Weight and Balance is unchanged and Equipment List has been amended. 10. The aircraft must be loaded JAW the prescribed loading' Information from the manufacturer.

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.)

Latches is an on-condition component with no airworthiness life limited parts This alteration does not require a Rotorcraft Flight Manual revision Weight and Balance is not affected by this alteration Airworthiness Inspections will be accomplished IAW the existing Sikorsky Airworthiness Limitations and Inspectio

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

board the aircraft as a guide to equipment operation. 3.) This install is for VFR use, altitude above the terrain is advisory information only. 4.) Weight and Balance computed. and equipment list updated. 5.) An electrical load analysis determined that the electrical load of the aircraft does not exceed 80% of the

ecord. An alteration must be compatible with all prewous alterations to assure continued conformity with The applicable airworthiness requirements. S. Description of Work Accomplished (lt more space is required. attach additional sheets Mewl), with aircraft nationality and registration mark and date work completed) N

manual. Inspection intervals shall remain as indicated in the aircraft maintenance manual or operators approved inspection program as appropriate. Weight and Balance unaffected. Reference Constant Aviation work order CCM-3160 END =Additional Sheets Arc Attached FAA Form 337 (10/06) Pagc 2 EFTA00011670 U.

ecord. M alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Work Accomplished (Il more space is moulted. attach additional sheets. Identify mitt steal? nationally end registratIon m** end date work completed) UNI