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TECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002466 I8 EFTA01331081 0 ._ us Depactran MAJOR REPAIR AND ALTERATION or Trainecetarthe Faders (Airframe, Powerplant, Propeller, or Appliance) Awoke, MminIstnalon Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification So

ED FLIGHT MANUAL SUPPLEMENT DOC NUMBER B727-16236100, REV A. SHEETS 1 THRU 9. DATED 5/8/02 HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL END K Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 SDNY_GM_02759738 - SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246660 EFTA01331123 Apr -1

FICATION - Under authority vested by direcdon of the Adminittnuor and in accords= with condidons and limitations of appohmornt under part IS3 of the Faders! Aviation Regulations. dam tined above and on Matched sheds cumbered N/A have been examined in accordance with established procedures and found to

NUED AIRWORTHINESS DUE TO THIS MODIFICATION. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION. END K Additional Sheets Are Attached * V.S. G.P.O 1990-781.753 I SDNY_Gtol_02759780 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246702 EFTA01331165 a D

h4 agent) ot the aircraft described Mame: that at encratIoregistereiS with the Federal Aviation Administration in accordance wills Sechon 501 of the Faders, Aviation Ad of 18613. end applicable Fodivid Aviilion Regastions: and Mat Me aircraft has been enspecled and is airworthy for the Ilighi ' describ

LE CHANGE IN THE WEIGHT AND BALANCE. THIS MODIFICATION DOES NOT CHANGE THE MANUFACTURER'S CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS. END K Additional Sheets Are Attached U.S. G.P.O 1990-761-753 EFTA00278236 • . • r DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE