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EFTA01326217 | EFTA01326685 FM AIRCRAFT CAMTRA NO. ISIKY DATE: 12 -9- 74 • NOTICE Weight and balance or operating thretabon changes shall be entered in the appropriate airerae reconi An alteration must be cons pa olge with all previous alterations to ass= continued cantos:miry with the applicable airworthiness 11881801:Mall3. 8. Dvscriptlec of Work Accomplished of more spice is remand. each adduiciutl them. thmtity with that mdonally and mist mark and dee work completed.) in order to provide cordhurty during future inspections, maintenance, and alterations a true copy of this FAA Form 337 is required to be kept on board the aircraft as long as the alteration remain in effect AUGUST:26. 1994. Gulhtream Aerospace Corporation (GAC) Model G-IV. Said Number 1085, N880A, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-savice data ••• 1786.6 hours. & 736 landings. Refs to the following FAA Approved Dalt GAC Aircraft Service Change (MC} 232, SUBJECT: ICE AND RAIN PROTECTION (ATA 30) WING TEMPERAWRE LOW MESSAGE — PROVISIONS, dated December 17, 1993. The purpose of this alteration is to activate the "WING TEMP LOW" message (Amber) on the Engine Instruments Crew Alerting System (EICAS) and mask alert if the wing has not reached 100 &tors Fahrenheit after two minutes from being selected ON. Performed all of ASC 232's modification instructions effective fOr A/C 1085 except for the following minor dm.iations: • Coacplt Overhead Panel: Existing wires1H151D20, IFINA20, 2H151C20, and 2E126A20 were replaced with new NSW. 22759116-17 to ft GA0335)4L22DS contacts provided with new wing anti-ice:wit. Avioniat Shelf Assemblies: Al added wire connections to the Fault Warning Computer(s) and Data Acquisition Diggs) 'Mt made directly to the rack <on:tenons) Stead or through the shelf disconnects. Main Junction and Relay Panel: Wets IH152F22 and I.H152X22 was remove from T113M positions If and G respectively and spliced together. Win 2H152.1G2 and 2H152F22 way rand from T720 position G and K respectively and spliced Wither. Wire H9076B22 was spike to wire 1H1S2Y22 near Data Acquisition US MI, 95A4PIB pia, 17. Wire H9071322 was spliced to wire 211i 32T22 near Dan Acquisition Und 12, 95A5FIB pin 17. Wen /49078A22 and H9078AA22 were spliced bribe( with wire I HI87D22 nor connector NAINC pin 89. Wires k19079A22 and 119079AA22 were spliced togetha with wire 2H1I37Dn near connector Nmptc pin 91. . AU of the deviations that wire made to the apprerred design %Senecessary to provide for compatibility with existing approved configurations: It has been determined that the deviation made did no after the intent or operation of the • • -approved eiraeft savice change, -•• All parts were provided in kit fotro and obtained from Gulf:strain Arrospece Produh Ruppert, Savannah, GA Sucossfully performed ASC 732's operational lest. Recorded compliance with this FAA loon 337 in the aircraft's rneintenan ce records and reigned the aircraft to fl ight . . _ The effort of thirchange at the aircraft's basic weight and balance was negligible and no changes sect rna..te to the aircraft's hthic weight and balance mon. 01/2691Strt PY lli.as =war romiud fonaprrmul br. aOdsI Omani,' WOAD 6 Oa NO ADDMONAL stores AtEMTACIIED •E`te 0 Additional Sheets Are Atractu:d • • ST-, - .• • ....atejalate-, ••• J . • ' 4 -1;4 • • . .klietialHAPP4 • 1 • 7:7-.7 SDNY GM_02754170 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241092 EFTA01326685
February 17, 2026 at 8:55 PM