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

ore space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Removed existing MK-VI GPWS system in conjunction with installation of new TAWS (EGPWS) system reference FM form 337 dated 12-22-04. Aircraft weight and balance and equipment

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

N ACCORDANCE WITH FAR 25.1431 FOR OPERATING SATISFACTORILY AND DID NOT ADVERSELY AFFECT OTHER COMPONENTS INSTALLED IN THE AIRCRAFT. THE SUNDSTRAND MK-VI GPWS APPROVED FLIGHT MANUAL SUPPLEMENT, REV. B DATED 03-30-93 HAS BEEN INSERTED IN THE SUPPLEMENT SECTION OF THE AIRCRAFT FLIGHT MANUAL AND THE GPWS PIL

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

ore space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Removed existing MK-VI GPWS system in conjunction with installation of new TAWS (EGPWS) system reference FM form 337 dated 12-22-O4. Aircraft weight and balance and equipment

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

N ACCORDANCE WITH FAR 25.1431 FOR OPERATING SATISFACTORILY AND DID NOT ADVERSELY AFFECT OTHER COMPONENTS INSTALLED IN THE AIRCRAFT. THE SUNDSTRAND MK-VI GPWS APPROVED FLIGHT MANUAL SUPPLEMENT, REV. B DATED 03-30-93 HAS BEEN INSERTED IN THE SUPPLEMENT SECTION OF THE AIRCRAFT FLIGHT MANUAL AND THE GPWS PIL