Epstein Secrets

n to use this certificate to alter a product, the holder must give that person written evidence of that permission. . 3) For aircraft equipped with Pratt & Whitney ill SD Engines FAA approved Airplane Flight Manual Supplement, Nextant Aerospace LLC Doc. No. 373.00.0008 Revision IR, dated 10/19/2009, or later F

rd An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. B. Description of Work Accomplished (amore space is required. meal adoVthanai sheets. ?dismay Mthilifera nalionlgeY and regisrmtion mad( and date wadi aombraterl) USA N49

OMPANY I ARC-RAPTMOM DESIGNATION 400A AYR MFR 1996 FAA BODING 2/ 45—. O.O 1 0 S. AECRAFT XCOLLI NO. RK-244 S. ENGINE BUILDERS NAME (AIMS) Pratt & Whitney Canada 7. ENGINE MOCEL DESIGNATION JT1SOS 5 /PS 8. NUMBER OF ENGINES 2 0. PROPELLER 13011.00TS NAME (Mho WA IE.PROPELLERMODEL DESIGNATION WA

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

ation sheets 3 and 4. .6:10.4.4101flotet Wee/r/ea/n./Kmres,".. Al 6SW Hawker 13eechcraft 400A Stverfer4kn gam Ylis t refe.wyn. Replacement of Pratt & Whitney JT15D-5 series engine with Williams International F144.3AP engine (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated sys

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

COMPANY 3. AIRCRAFT MODEL DESIGNATION 400A 4.YR. MFR 1999 FM CODING 7,s cc 1 0 5. AIRCRAFT SERIAL NO. RK-244 6. ENGINE BUILDERS NAME WNW Pratt & Whitney Canada 7. ENGINE MODEL DESIGNATION JT15I3-5 tif --; // L S 8. NUMBER OF ENGINES 2 9. PROPELLER BUILDERS NAME (Mike) N/A 10. PROPELLER MODEL

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