Epstein Secrets

P rsuant to the authority g yen persons specified below. the unit identified in item 5 was 'nspeded in the manner prescribed by the A minetrator of the Federal Aviation Administration and S InApproved JDRejected BY FAA Fit. Standards Inspector Manufacturer Maintenance Organization PiaraOnS ArCeOveci by Cartbdian Deparallel

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 • •

ce Pursuant to the authority g yen persons specified below, the u ' retied in rem 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration end is XIApproved I—Rejected BY FAA Fri Standards Inspector Manufacturer Maintenance Organization Pawns Approved by Canadian Depannuthr or T

and FAA Form 8110-3. 2. Records of all work accomplished is on file at this repair station under service order 185006. 3. Aircraft was weighed and Weight and Balance updated accordingly. 4. All repairs are permanent unless otherwise stated. -end-- C I Additional Sheets Are Attached * us GOWN*41DIT PIUN114O

Approval for Return To seniadlit4e ce Pursuant Administrator BY to the authority given persons specified below, the unit identified in item of the Federal Aviation Administration and is El APPROVED 4 was inspected in the manner prescribed by the REJECTED • FAA Flt. Standards Inspector Manufactora Inspection Authorizati

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.

ursuant to the authority given persons specified below, the unit identified in item 5 was inspected in the manner prescribed by the Adnwiistrator of the Federal Aviation Administration and is n APPROVED O REJECTED FM FN. Standards Inspector Manufacturer Maintenance Organization Persons Approved by Canadian Department of Tran

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

. A • proval for Return to Service Pursuant to the authority paten persons specified below. the Lilt Wenn, In item 6 va tinspected Administrator of the Federal Aviation Administration and la I Approved In the mama prescribed by the Rigel:led BY --"' FAA Fit. Standards Inspector — Manufacturer — — Maintenance OrgaNzatlon

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.

ursuant to the authority given persons specified below, th Oriitlid fie in item 4 was inspected in the manner prescribed by the •. Administrator of the Federal Aviation Administration and is. Q APPROVED 0 REJECTED ; ', ..- ! 1 0%,......"• O. BY FAA Flt Standards inspector Manufacturer Inspection Authorization Other (Spec

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 IAW the prescribed loading information from the manufacturer. E