Epstein Secrets

B El 12/29/2013 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified Administrator of the Federal Aviation Administration and is Ell in item 5 was Inspected In the manner presalbecl by the APPROVED K REJECTED FAA Flt Inspector Standards Manufacturer Maintenance

or substantiation of compliance to necessary requirements for the entire repair. 8. PURPOSE OF DATA: Engineering data in support of major repair to Hawker Beechcraft 400A, SIN RK-244. 9. APPLICABLE REQUIREMENTS (List specific sections) CFR Title 14 Part 25.301[25-23), 25.303[25-23), 25.305(a)(b)(c)(25-23], 25.307(a)[

205. Rib — H Stab Cant STA 78.346. e. PURPOSE OF DATA: Engineering data to support repair procedure for Horizontal Stabilizer P/N 45A21002-0121 on Hawker Beechcraft 400A, S/N RK-244. 9. APPLICABLE REQUIREMENTS (List specific sections) CFR Title 14 Part 25.301[25-23], 25.303[25-23), 25.305(a)(b)(c)(25-23), 25.307(a)(

Date of Authorized Ircligdu r ,..„1 7. Approval foe Return Pursuant to the loth:fey given person; Spedtled Wog. the unit idettled Admiritarate Of the Federal Aviation Administration and is O:C in fern 5 was inspected In the manner presets by the APPROVED 0 REJECTED BY FAA Fit Standards IMpeCler tilanklecturer Maintenanc

stantiation of compliance to necessary requirements for the entire alteration. S. PURPOSE OF DATA Engineering data in support of major alteration to Hawker Beechcraft 400A, SIN RK-244. 9. APPLICABLE REQUIREMENTS (List Weak WS4) CFR Title 14 Part 25.301[25-23], 25.303(25-23], 25.305(a)(b)(c)(25.23J, 25.307(a)(25-23], 2

n nice Pursuant to the avirtority awl persons waited below. the un Identeled in nem 5 was impeded in the manner prescribed by the Adrithistrakx of the Federal Aviation Administration and is @APPROVED O REJECTED FM Fit Standards inspector Mani/Kam Maintenance Organization Person Approved by Canadian Departrnent or Transpor

requirements for the entire repair. e. PURPOSE OF DATA. Engineering data to support repair procedure for Horizontal Stabilizer PIN 45A21002-0121 on Hawker Beechcraft 400A, S/N RK-244. 9. APPLICABLE REQUIREMENTS (list swank sectOns) CFR Title 14 Part 25.301[25-23), 25.303)25-23], 25.305(a)(bftc))25-23], 25.307(a)[25-2

Pursuant to the authority given persons speared ['Sow, the unit identified in item 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is El APPROVED K REJECTED BY FAA Fit Standards Inspector Manufacturer Maintenance Organization [Person Approved by Canadian Department of

as "Applicable Requirements." approval of all the to necessary requirements e. PURPOSE OF DATA: Engineering data in support of major alteration to Hawker Beechcraft 400A, SIN RK-244. 9. APPLICABLE REQUIREMENTS (List SpeCiat sections) CFR Title 14 Part 25.301[25-23], 25.303[25-23], 25.305(a)(b)(c)[25-23), 25.307(a)[2