Epstein Secrets

ached Form 33? 004.8 SDNY_GM_02755243 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA (X)242165 EFTA01327283 • • • SDNY GM 02755244 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00242166 EFTA01327284 NOTICE Weight and balance or operating limi

Nam (As shown on registration certificate) AIR GHISLAINE INC SOUTHEASTERN MILLS INC ASCENT II LLC Addre

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

duCann can/tka nprnaO TYPE CERTIFICATE OTHER C. GM QUANTITY OF CERTIFICATES REQUIRED FOR OFERATIM3 N

Name (As shown on registration certificate) AIR GHISLAINE INC SOUTHEASTERN MILLS INC ASCENT II LLC Addre

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.

t manual equipment list. Log book entry made. Ref: W/O C02456EA, C02457EA, C02572EA. END Additional Sheets are Attached FAA Form 337 (124S) SDNY GM 02756540 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243462 EFTA01328578 SDNYGM02756541 SUBJECT TO PROTECTIVE ORDER P

Name (As shown on regiStrehOn CeitifiCete) AIR GHISLAINE, INC Address (As shown on reputation certifiCefi

ecord. An alteration must be compatible with as previous alterations to assure continued conformity with the applicable airworthiness requirements. B. Description of Work Accomplished tit mole space h required. attach additional sheets. Identity mtn secret nationally and registration mark and date work completed) N40

EFERENCES 1 MIL-HDBK-5F Metallic Materials and Elements for Aerospace Vehicle Structures. 2 FAR 25. Page 2 DA- G1085 Rev NC 05-08-2000 SDNY GM 02754002 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240924 EFTA01326517 SDNY_GM_02754003 SUBJECT TO PROTECTIVE ORDER

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

xetedusg 11,000, or impruorvnent not trending 3 yeas>. or both. This eta maybe tvensfersed in heeeniener with FAR 21.17. es,, e-alto-3O0-01) SDNY GM 02755335 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242257 EFTA01327375 .,. SDNY_GM_02755336 SUBJECT TO PROTECTIVE

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

105 VI. PRODUCTION PUSHY TESTING A. MANUFACTURER . . . . NAME ADDRESS B. PRODUCTION BASIS (Check •Plattable Kern) PRODUCTION CERTIFICATE (GM pultrodon cetera,. number) TYPE CERTIFICATE ONLY APPROVED PRODUCTION INSPECTION SYSTEM C. GIVE QUANTITY OF CERTIFICATES REOUIRED e FOR OPERATING

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

ST EOM ASCE SPEC TEMPLATE DOC SDNY_GM_02 759669 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024659 I EFTA01331054 SDNY GM 02759670 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246592 EFTA01331055 1 GENERAL INFORMATION 1.1 SCOPE OF THIS DO

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 math and date work accomplish