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Autopilot: Triple Collins 701 Communication Radios: Dual Collins VHF-7008w18.33 spacing CVR: Fairchld A100 DME: Dual Collins DME-700 EFIS: Collins EFIP-701E FDR: Sundstrand Flight Director: Tnple Collins EFIP-701E Flight Phone: MagnaStar w/Aerocom interface FMS: Dual Honeywell PEG-009 G
e New: Eng 1 (L) 7,461 his / Eng 2 (R): 7,534 hrs Cycles Since New: Eng 1 (L): 2,661 In / Eng 2 (R) 2,702 hrs AUXILIARY POWER UNIT (APU) Model: AlliedSignal GTCP 331-200ER Serial 0: P1592 Total Time Since New: 7,199 hrs artr:iwt""41.7 EFTA00791721 BOEING 757-200 SN 424923 Opus Aeronautics 10, Av
Program) Engine Overhaul By:</=> <=> Hot Inspection By:=/u> =/span> Damage History Notes: Certifications:</rpan> RVSM <=> Inspection: RVSM. Collins TDR=90D Mode S enhanced 02/19/10. 96-Month inspection c/w 10/30/09 at 4601TT. =44-Month inspection c/w 02/19/10 at 4650TT. Inspection: ASC 189 Win
<=r>EXTERIOR DETAILS Rating: Done By: M M/YYYY: Colors: White w/red & black accent stripes</=> a> AVIONICS ADF: Dual Collins ADF-462 AFIS: AlliedSignal AFIS <=td> Avionics Package:</=> Collins Pro Line = Communication Radios: Dual Collins VHF-422=w/8.33 MHz spacing CVR: </=d>CVR</=pan> 9 EFT
ogram) En=ine Overhaul By: Ho= Inspection By: Oa=age History Notes: Ce=tifications: 5 EFTA_R1_02032311 EFTA02691047 RVSM In=pection: RVSM. Collins =DR-90D Mode S enhanced 02/19/10. 96-Month inspection c/w 10/30/09 at =60111. 144-Month inspection c/w 02/19/10 at =65011. In=pection: ASC 189 Win
: 11150 4,800 7,000 2,628 3 EFTA_R1_02032309 EFTA02691045 En=ine 3 (Left) : En=ine 4 (Right) : =o:p> AU=ILIARY POWER UNIT (APU) Mo=el: AlliedSignal =E220 Se=ial tt: AP= Maintenance Plan: 4 EFTA_R1_02032310 EFTA02691046 Unknown&=bsp; To=al Time (Hours) Since New: 2,628 Si=ce Overhaul (SO
k and date work completed.) Modified the existing Third Comm & Nat Systems by removing the Gables G6860-09 Conun/Nav Control Head, and installing a Collins CTL-23 Digital Control Head, P/N 622-9851-001. The third Comm / NAV system's interface was retained as previously installed with the exception of th
ning to GPWS. Maintenance Requirements - Instruction for Continued Airworthiness, GAC Document No. 5C41 349A01, Rev. 1, dated 6/22/97 with attached AlliedSignal.Line Maintenance Manual, Doc. No. 060- 4199-014 is required for this approval. Eating wiring diagrams affected by the above referenced systems are r
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