• e US Department MAJOR REPAIR AND ALTERATION Of Transportation

• e US Department MAJOR REPAIR AND ALTERATION Of Transportation Federal (Airframe, Powerplant, Propeller, or Appliance) Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification So- r5DO- 1 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions a d disposition of this form. This report is required bylaw (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for ea such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model 727-100 Serial No. 20115 _ Nationality and Registration Mark USA N908JE 2. Owner Name (As shown on registration certificate) J.E.G.E, Inc. = Nom Only 3. For FAA Use .. ..• • . OCT Tor, data identified here' pties atoverthInes reqiiFements is approved described aircraft, subject ntorrnity ,uthe dram 43, se 43.7. with applicable for the above I by a person 5(-1 --f5V 0— i T Date Sign of Inspector 4. Unit Identificati 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE •VI NICS DIVISION U.S. Certificated Mechanic Radio Class 1,2,3 Limited Airframe Foreign Certificated Mechanic Certificated Repair Station 0 Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date .:,7fr/ C?-7---46'&/-g_. <71,0C)Z Signature of Authorized lndi .d4,31) ,/ eeZ Steve Ouellette (9/W_ 7. Approval for Return to Service Pursuant to the authority given personsRecified Federal Aviation Administration and is below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the APPROVED O REJECTED BY FAA Flt. Standards Inspector Manufacturer inspectfon Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group -b, Date of Approval or Rejection Der-0,57_ ,,ao 6 Certificate or Designation No. SD4R514M Signatur ____ 0: thorized I idu d Ouellette ..______ Steve l FAA Form 337 (12-88) EFTA00277580 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) The purpose of this 337 is for the work performect 1•1908JE under Banyan Air Service; Avionics Division work order #71301 completed on a2s/a6 A. Installed ari AirCell Iridium ST-3100 P/N 400-10680-001 and removed a previously installed AirCell AGT.01 P/N 900001-2. Minor wiring changes were made at the mating connector IAW installation manual P/N 800-10680 Rev. B dated June 2005. B. The above installation was performed in accordance with AC43.13-1B, Chapter 7, sections 1-5, AC43.13-1B Chapterg,'Options,3-17, AC43.13-2A Chapter 1, AC43.13-2A Chapter 2, paragraphs 24 & 25 and the aircraft's maintenance manual. . 111W: C A functional test of the.ab6e/Aniprrient has been performed FAR25.1309 and FAR25 .1431 for proper operation and did not adversely affect any other aircraft systems. An electrical load analysis was conducted and it was confirmed that this installation would not exceed 80% of the generator output. D. A log book entry and equipment list was generated to reflect the above installation. The weight change is negligible. the equipment list was updated to reflect this change. E. Instructions for continued airworthiness is attached.. END ❑ Additional Sheets are Attached EFTA00277581 Instruction for Continued Airworthiness for AirCell ST 3100 Aircraft Subscriber Equipment System Installed on Boeing 727-100 N908JE S/N 20115 Revision O. Dated: 9/17/2006 EFTA00277582 • • e EFTA00277583 • APPLICATION REVISIONS . DESC. NEXT ASSY USED ON REV DESCRIPTION DATE APPROVED ST 3100 ASE SYSTEM BARON 95-B55 A BASELINE RELEASE 2002-10-16 K. FRANTZ B SEE DCN 00179 2002-10-25 K. FRANTZ ._,.... ALL SHEETS CARRY THE SAME REVISION LETTER UNLESS OTHERWISE SPECIFIED DIMENSIONING & TOLERANCING bkW ASME Y14.5M-1994 DIMENSIONS ARE IN INCHES STANDARD TOLERANCES: x = ±..1 )(X= ± .02 )(XX= ± .010 e . AirCell, Inc. no d 1172 Century Drive ..._.7 Suite 280, Building B Louisville, CO 80027 APPROVED DATE INSTRUCTIONS FOR CONTINUED AIRWORTHINESS ST 3100 ASE SYSTEM PREPARED BY K. FRANTZ YEAR-M O-DA 2002-10-16 MECH DESIGN Z. HOH YEAR-MO-DA 2002-10-16 ELEC DESIGN B. SOUKUP YEAR-M O-DA 2002-10-16 TECH SUPPORT B. NIELSON YEAR-MO-DA 2002-10-16 SYSTEMS K. FRANTZ --\ YEAR-MO-DA 2002-10-16 ENGINEERING J. POLSON YEAR-MO-DA 2002-10-16 SIZE A - CAGE CODE 1NO67 DRAWING NUMBER . 820-10680-001 REV B FILE FORMAT: Microsoft Word 2000 SCALE: NONE WEIGHT: NA SH 1 of 8 FILENAME: 820-10680-001-B.doc • S a • • a a S S 699-10077: A-SIZE SPEC TEMPLATE.DOC EFTA00277584 • •• EFTA00277585 p p p p p p p. 9 p p p p p ) ) TABLE OF CONTENTS 1 GENERAL INFORMATION 3 1.1 SCOPE OF THIS DOCUMENT 3 1.2 TECHNICAL SUPPORT CONTACT INFORMATION 3 1.3 • GENERAL. NOTES 3 1.4 ADVISORIES 4 2 SYSTEM DESCRIPTION 4 2.1 TOP LEVEL SYSTEM CONFIGURATION 1 "4 2.2 OPERATION OF THE SYSTEM 6 OPERATIONAL TIME LIMITS AND SCHEDULED MAINTENANCE 7 4 UNSCHEDULED MAINTENANCE 7 4.1 TROUBLESHOOTING PROCEDURE 7 5 AIRWORTHINESS LIMITATIONS 7 FIGURES AND TABLES Table 2.1-1 System Component Definition 5 Figure 2.1-1 Block Diagram of ST 3100 ASE System 6 • AirCell, Inc. SIZE CAGE CODE DRAWING NUMBER REV e 1172 Century Drive A 1NQ67 820-10680-001 B Suite 280, Building B FILE FORMAT: Microsoft Word 2000 SH 2 of 8 Louisville, CO 80027 FILE NAME: 820.10680-001-B.doc 699.10077: A-SIZE SPEC TEMPLATE.DOC EFTA00277586 'I EFTA00277587 GENERAL INFORMATION 1.1 SCOPE OF THIS DOCUMENT This manual defines the instructions for continued airworthiness (ICAW) for an AirCell_ 3000 Series Aircraft Subscriber Equipment (ASE) system. The manual is written to demonstrate compliance with FARs 23.1529 and 25.1529. Specifically, this manual defines the instructions for the Model 3100 Satellite Telephone System (ST 3100). This manual is subdivided into sections to support the general operation, inspection and maintenance of the ST 3100 system. Section 1 defines general information for the maintenance and airworthiness of the ASE system. Section 2 provides general information on the configuration and operation of AirCell ASE systems. Section 3 presents a discussion of the scheduled maintenance and operational time limits for the system. Section 4 and Appendix A provide instructions for system operational checks, troubleshooting, unscheduled maintenance and component replacement. Section 5 provides a brief statement addressing airworthiness limitations for the ST 3100 system. 1.2 TECHNICAL SUPPORT CONTACT INFORMATION Technical support for AirCell products is available from 08:00 to 17:00 United States Mountain Time (Time Zone GMT —7 hours) Monday through Friday. The contact information for AirCell Technical Support is as follows: From a landline: Phone (in the US): 1.888.286.9876 (toll free) Phone (outside the US): 001.303.379.0278 (toll call) From an AirCell phone: From an Air Mode/AMPS phone (in the US): 611 (toll free) From a SAT Mode (Iridium) phone (worldwide): 2471 (toll free) Email: [email protected] Note: The toll free numbers for AirCell phones will only work for AirCell provided phones and services. 1.3 GENERAL NOTES • All pages in this document carry the same revision level. Revision status is indicated by a letter printed on each page of this manual. • The material in this manual is subject to change. Before planning or performing any installation or maintenance operation, check with AirCell Technical Support to verify that this manual is complete and has the latest revision. • AirCell, Inc. welcomes your comments, suggestions, and corrections concerning this manual. Please include in your correspondence the publication number, equipment part number, page or figure number, and a brief description of any problem or consideration you noted. Please send your comments to: AirCell, Inc. Corporate Publication Coordinator 1172 Century Drive Suite 280, Building B Louisville, Colorado 80027 [email protected] elf AirCell, Inc. 1172 Century Drive Suite 280, Building B Louisville, CO 80027 SIZE A CAGE CODE 1NC)67 DRAWING NUMBER 820-10680-001 REV B FILE FORMAT: Microsoft Word 2000 I SH 3 of 8 FILE NAME: 820-10680-001-B.doc 699-10077: A-SIZE SPEC TEMPLATE.DOC EFTA00277588 i EFTA00277589 1.4 ADVISORIES WARNING Statements in this section contain critical safety information. Read these statements carefully before installing this unit. WARNING Observe standard safety precautions and wear safety glasses to prevent personal injury while performing maintenance on this unit in the aircraft. WARNING Shut off power before connecting or disconnecting the ST 3100 system, as voltage transients may damage the unit or the interface wiring. WARNING Components or subassemblies found in this unit may contain materials such as beryllium oxide, acids, lithium, radioactive material, mercury, etc. that can be hazardous to your health. If the component enclosure gal is broken, precautions must be taken against personal contact or inhalation in accordance with OSHA requirements 29CFR 1910.1000 or superseding documents. AirCell strongly discourages the opening or disassembly of sealed components. WARRANTY AND CERTIFICATIONS Any alteration of this product voids the FAA or FCC certification and the AirCell warranty. 2 SYSTEM DESCRIPTION The ST 3100 ASE system provides access to a range of two way communication options from an aircraft, including voice and data applications. With the ST 3100 system these services are available when the aircraft is in the air or on the ground. The AirCell satellite mode communications link is provided using the 1600 MHz Iridium LEO (Low Earth Orbit-485 miles altitude) satellite network, which provides coverage from the ground up over the entire surface of the earth. 2.1 TOP LEVEL SYSTEM CONFIGURATION The ST 3100 system consists of a number of primary system components. The heart of the system is the ST 3100 ASE Transceiver, which includes internal electronics to support operation in the Iridium satellite network. Other system components include the externally mounted antenna, a low loss coaxial cable, and various user interfaces including multiple ASE handsets (up to 9), an RS-232 data port, and an audio panel interface. AirCell'AirCell, Inc. 1172 Century Drive Suite 280, Building B Louisville, CO 80027 SIZE CAGE CODE DRAWING NUMBER REV A 1NO67 820-10680-001 B FILE FORMAT: Microsoft Word 2000 SH 4 of 8 FILE NAME: 820-10680-001-B.doc 699-10077: A-SIZE SPEC TEMPLATE.DOC EFTA00277590 . . I EFTA00277591 The primary components of an ASE system include Line Replaceable Units (LRUs) and AirCell specified assemblies (such as coaxial cables or wiring harnesses) that are manufactured or purchased by the system installer. A list of the LRUs and specified assemblies is provided in Table 2.1-1, and a representative block diagram is provided in Figure 2.1-1 to demonstrate the interconnection of a typical ST 3100 system. For detailed information on the system components, please refer to ST 3100 ASE System installation manual (AirCell document 800-10680), or contact AirCell Technical Support for assistance. Table 2.1-1 System Component Definition System Component Designatio n Description AirCell PN. Approved Alternate(s) AirCell PN of Alternate System Transceiver LRU ST 3100 ASE Transceiver 400-10680-001 none Transceiver :Mounting Tray LRU 3/8 ATR Width Mounting Tray 800007-1 3000 Series Mounting Rails 151-10689-001 System Wiring Harness Specified Assembly 26 wire System Harness NA ASE Handset LRU Flush Mount ASE Handset 400-10001-10X* Standard ASE Handset Portable Coilcord ASE Handset Custom Retractable ASE Handset 400-10035-00X* 400-10015-00X* 400-10019-00X* Satellite ASE Antenna LRU 1600 MHz Satellite ASE Antenna, Patch Style 015-10306-001 1600 MHz Satellite ASE Antenna, Blade Style 015-10683-001 Satellite Channel Coaxial Cable Specified Assembly. Low Loss Coaxial Cable NA (vendor item)" ** "X" designates the color of the ASE handsets. The system coaxial cable is a required item that is not provided by AirCell. The system installer will need to purchase this item from an approved vendor as defined later in this document. (MICA: AirCell, Inc. 1172 Century Drive Suite 280, Building B Louisville, CO 80027 SIZE CAGE CODE DRAWING NUMBER REV A 1NQ67 820-10680-001 B FILE FORMAT: Microsoft Word 2000 I SH 5 of 8 FILE NAME: 820-10680-001-B.doc AAt4r4fAco" 699-1C077:A-SIZE SPEC TEMPLATE.DOC EFTA00277592 • . . . .. : I EFTA00277593 ASE SATELLITE \/ ANTENNA I 0 p I I I I I I I I I I ) ) .44111.\_ AIRCRAFT FUSELAGE ASE SYSTEM XCVR SAT ANTENNA ID AUX CNCTR NO CONNECTION SYS CNCTR ASE SYS HS CNCTR ASE SYS HS CNCTR 1=1--M120 ASE 5Y5 HS CNCTR D ASE SYS RS232 CNCTR ASE HANDSET CHANNEL ASE HANDSET CHANNEL Mffal ASE HANDSET CHANNEL TO AUDIO PANEL TO RS232 DATA TERMINAL TO AIRCRAFT POWER (2.8 Vdc) AIRCRAFT FUSELAGE Figure 2.1-1 Block Diagram of ST 3100 ASE System Note: Each 'Handset Channel' listed above is capable of supporting up to 3 ASE handsets, making it possible to integrate up to 9 handsets in the ST 3100 system. 2.2 OPERATION OF THE SYSTEM The user interface and operation of the ST 3100 system is designed to be very similar to the operation of a terrestrial cellular or PCS phone. Some key features of the ST 3100 system are as follows: • The system will power up when the avionics master switch for the aircraft is powered on. The AirCell system is always on when the avionics master is powered on. • ' The Satellite mode network provides coverage anywhere on (or above) the surface of the earth with a clear view of the sky in all directions. • To place a call from the system handset, the user must verify that the system is 'in service'. SAT mode calls are typically dialed as international long distance calls (00 + country code + phone number). After dialing, the user must press the " SND " key on the handset, and the phone call will proceed as a typical cellular or PCS call. At the completion of a call, the user may press the " END " key to terminate the call. • The user may receive incoming (ground to air) phone calls depending on the in service condition. The user can answer these calls by pressing the " SND " key on the handset. • Data calls can be made from Air to Ground over the ST system by connecting a Data Terminal Equipment device (such as a PC) to the RS-232 port of the system. The ST system has a built in modem function, so some user setup of the DTE will be required. More detailed operating instructions are provided for this system in the ST 3100 User's manual (AirCell document 810-10680). 6N_j.ri•Celf AirCell, Inc. 1172 Century Drive Suite 280, Building B Louisville, CO 80027 SIZE CAGE CODE DRAWING NUMBER REV A 1NQ67 820-10680-001 B FILE FORMAT: Microsoft Word 2000 SH 6 of 8 FILE NAME: 820-10680-001-B.doc 699-10077: A-SIZE SPEC T EMPLATE.D GC EFTA00277594 I EFTA00277595 3 OPERATIONAL TIME LIMITS AND SCHEDULED MAINTENANCE The ST 3100 system is designed and manufactured to be maintenance free after installation. As a result of this design, there are no operational time limits or periodic maintenance checks or procedures that must be performed for the system. Inspections and/or system verification checks are only required in the event of a system failure (On Condition), as defined in Section 4 of this document. As an option, the system operator may perform a visual inspection of the various system components at the aircraft annual inspection, or other periodic maintenance interval as defined by the aircraft manufacturer. 4 UNSCHEDULED MAINTENANCE The ST 3100 system is designed for "On Condition" maintenance only. In the event of a system failure, the system user/aircraft operator is advised to follow the troubleshooting procedure defined in Appendix A of this manual. After performing the basic procedure, the user will either have returned the system to normal operation, or should contact AirCell technical support for additional guidance. Note that, in the process of performing the troubleshooting procedure, authorized field service personnel are permitted to perform repairs to wiring harnesses, RF cable assemblies, mounting interfaces, or (with prior approval from AirCell Technical Support) to remove and replace any of the primary system Line Replaceable Units (LRUs). AirCell does not, under any circumstances, authorize field repair or subassembly level maintenance on any LRU. Sealed LRUs should always be returned to the AirCell FAA Repair Station for evaluation and repair. 4.1 TROUBLESHOOTING PROCEDURE Appendix A provides a guide to identify simple problems that may be identified and/or resolved with simple field inspection and test processes. It is advised that the procedure in this appendix should be performed before contacting AirCell Technical Support for additional instruction. No specialized tools or equipment are required to perform this procedure. In the event that a step in this procedure is not clear, or the results of a procedure are not conclusive, the test operator should feel free to contact Technical Support for assistance. 5 AIRWORTHINESS LIMITATIONS The AirCell ST 3100 ASE system is a non-critical communications system. In accordance with FAR 23.1529 (with Part 23 Appendix G) and FAR 25.1529 (with Part 25 Appendix H) this system has no Airworthiness Limitations for either Part 23 or Part 25 aircraft. The airworthiness limitations section is FAA approved and specifies maintenance required under Sections 43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has been approved. A7-frCelf AirCell, Inc. 1172 Century Drive Suite 280, Building B Louisville, CO 80027 SIZE CAGE CODE DRAWING NUMBER REV A 1NQ67 820-10680-001 B FILE FORMAT: Microsoft Word 2000 SH 7 of 8 FILE NAME: 820-10680-001-B.doc uctict)ticccfoCI 699-10377: A-SIZE SPEC TEMPLATE.DOC EFTA00277596 'a . . % . . . I EFTA00277597 t.d S • 0 P 9 P p p a a a a Appendix A ST 3100 ASE System Troubleshooting Procedure A tirr AirCell, Inc. kjell 1172 Century Drive Suite 280, Building B Louisville, CO 80027 SIZE A CAGE CODE 1NQ67 DRAWING NUMBER 820-10680-001 B F. FILE FORMAT: Microsoft Word 2000 I SH 8 of 8 FILE NAME: 820-10680-001-B.doc 68410077,S. SPEC TEMPLATE.DOC EFTA00277598 • EFTA00277599 TrCell' Symptom Possible Cause Discussion Verification Step(s) Symptom 1 Power is not available to ASE The handset display should always O Verify that the aircraft power system (master avionics switch) is on. Handset Display is System be illuminated when power is O Verify that the ASE system circuit breaker is closed. not illuminated applied to the ASE transceiver. Because the failure of a handset display is unlikely, a `dead' display O Visually inspect the displays of all installed handsets in the system. If all handsets arc off, proceed to the next bullet in this list. If most handsets are illuminated, but one is not, then proceed to Symptom 2. (One or more suggests that there is a problem with O If all handset displays are dead, the problem is likely in the power system wiring handsets integrated in the input power to the ASE system. before the ASE transceiver. Visually check the system connections and the wiring system, no handset . In the event that the one or more harness leads between the transceiver and the aircraft power system. Repair or displays are handset display(s) are not reconnect any obvious problems. illuminated) illuminated, the user/operator should verify that aircraft power is on and O If needed, ring out the power lines per the system wiring diagram. Repair any broken wires or rework to match the system wiring diagram. . available to the ASE transceiver. O If this procedure does not resolve the problem, contact AirCell Technical Support for additional guidance. Symptom 2 Handset Display is Bad connection or faulty wiring between handset and In a system with multiple handsets, if some handsets are operating and - O Some ASE systems integrate multiple handsets. If more than one handset is installed on the system, check the display on all handsets. If only one of multiple not illuminated transceiver. some arc not, then it is likely that either the handset is bad or the handsets is not illuminated, then the problem is either a bad handset or in the handset connection/ wiring harness between that handset cradle and the transceiver. wiring between the handset and the O Perform a visual inspection to verify that ail connections are made in accordance (ASE System has or transceiver is faulty. with the system wiring diagram. Correct any obvious problems. multiple handsets, and the displays of most handsets are on, but one handset is not Bad handset O If all system connections are correct, then switch the `dead' handset with a known good handset and retest the system. If the handset is still dead in the new location, then the handset is bad. Contact AirCell Technical Support for repair/replacement instructions. illuminated.). . O If the known good handset is now dead, then the problem is in the system wiring/connections between the handset and the transceiver. Ring out the lines per the system wiring diagram. Specifically check for 9V power and ground leads on the HS power line from the transceiver system connector. Repair any broken wires or rework the system wiring harness to match the wiring diagram. • O If this procedure does not resolve the problem, contact AirCell Technical Support for additional guidance. A-1 ST 3100 ASE System Troubleshooting Procedure 820-10680-001, Rev B Ceti- IC tttik MiLttlettAdt EFTA00277600 s .0 EFTA00277601 ‘4110 46P 4019-.4m! VaY INV 10, INF 4mY 441,,w 400.4, WINO mi, wut:.‘soilmOlpf wov011OtiOWWW14104rOVINVOtiOVIOU Symptom Possible Cause • Discussion Verification St,9(s) Symptom 3 Handset Display is illuminated and display indicates no signal for Satellite (SAT) mode. Possible Cause 3A' System antenna does not have Line of Sight (LOS) view to satellite. The ST 3100 transceiver operates in Satellite (SAT) mode. When in coverage the ST system should detect and register for SAT mode service. If the system does not register, then it is likely that either the antenna does not have a LOS to a satellite (3A), or there is a problem with the RF channel in the aircraft (3B). In this condition, it is unlikely that there is a problem with the system transceiver. Verification Test 3A O Verify that the system SAT antenna has a clear LOS to the sky in all directions. A clear LOS is defined to exist when there are no obstructions (such as buildings, trees, vehicles etc) that are higher than 30 degrees above aircraft horizon in any direction. This should never be a problem in flight. • O Use the handset to enter the SAT lock mode (FCN,.3, 3) keys on the handset. The handset will display the word "IRIDIUM" when the SAT mode is locked. O Once the LOS has been established the system should register on the SAT network within 60 seconds. The system is registered when the "NO SVC" indicator is not visible on the handset display. 0 If the "NO SVC" indicator extinguishes, then the SAT mode is engaged, and the problem is resolved. The user may choose to make a test call and verify the • operation the system. 0 If the "NO SVC" indicator stays illuminated, then the system cannot register, and it is likely that there is an installation or equipment problem. Either contact AirCell Technical Support for additional guidance, or proceed to Verification Test 3B. No Satellite mode signal Possible Cause 3B There is a problem with the Satellite RF channel. • • Verification Test 3B O While the aircraft is on the ground, perform a visual inspection of the ASE system satellite antenna. Verify that the antenna is installed to the aircraft fuselage in accordance with the system antenna installation drawings. Verify the mechanical integrity of the antenna, and that the antenna is reasonably free of dirt, oil, ice and other undesired coatings. O Visually inspect the RF satellite channel, including the coaxial connections to the antenna and the system transceiver. Inspect the coaxial connectors to verify that they are connected in accordance with the system wiring diagram, and that they are not damaged. Look for breaks, kinks or other damage to the coaxial cable. 0 The user is authorized to correct installation errors (such as cabling errors), or to repair minor damage (such as broken coaxial connections, damaged coaxial cables, etc). The user is not authorized to open or modify sealed LRUs. O If these steps do not resolve the problem, contact AirCell Technical Support for additional guidance. Other conditions For all other conditions, contact AirCell Technical Support for guidance. • A-2 ST 3100 ASE System Troubleshooting Procedure 820-10680-001, Rev B EFTA00277602 • • • EFTA00277603 --tt US Department MAJOR REPAIR AND ALTERATION 0f Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FA Use Only Office IdentificatioA (5 O-rspo- iqINSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing _ Model 727-100 Serial No. 20115 Nationality and Registration Mark USA N908JE 2. Owner Name (As shown on registration certificate) J.E.G.E, Inc. Address (as shown on registration certificate) 103 Foulk Road STE 202 Wilmington, DE. 19803-3742 3. For FAA Use Only -,i-c:;;;;:.,:•• _ •*4-4 .:, 4. Unit identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE AVIONICS DIVISION 1635 NW 51st Place Ft. Lauderdale, FL 33309 U.S. Certificated Mechanic Radio Cl SD4R514M Class Limited Airframe Foreign Certificated Mechanic El Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) *dentified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date October 10, 2006 Signature of Authorized Indivi Steve Ouellette c.- ---- 7. Approval for Return to Service Pursuant to the authority given persons s• • cified below, Federal Aviation Administration and is e. APPROVED the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the O REJECTED BY FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection October 10, 2006 Certificate or Designation No. SD4R514M Signature of orized Ind* - I Steve Ouellette FAA Form 337 (12-88) EFTA00277604 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) The purpose of this 337 is for the work performed on N908JE under BanYan Air Service; Avionics Division work order #71301 completed on October 4, 2006. A. Installed an AirCell Iridium Antenna P/N S67-1575-109 in accordance with DER Services drawing number 2006-173-1 approved per FAA form 8130-3 signed by Robert Belgau DERT designation number DERT-510024-CE. The above installation was performed in accordance with AC43.13-1B, Chapter 7, sections 1-5, AC43.13-1B Chapter 11, sections 3-17, AC43.13-2A Chapter 1, AC43.13-2A Chapter 3, paragraphs 43 & 44 and the aircraft's maintenance manual. A log book entry and equipment list was generated to reflect the above installation. The weight change is negligible. the equipment list was updated to reflect this change. Instructions for Continued Airworthiness is "on condition only." END Additional Sheets are Attached EFTA00277605 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE October 07, 2006 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL 727-31 TYPE (A irPlane. Radio, Helicopter, etc) Airplane NAME OF APPLICANT Banyan Air Services LIST OF DATA IDENTIFICATION TITLE DER Services Drawing: 2006-173-1 _ Rev. I/R -i.'...- *-::-i:Dtd. 27-Sep-06 END END • Iridium Antenna END END END Effectivity: S/N: 20115, T/N: N908JE Installation STA 515 - BTWN S-2R & END END END END END_ _ _ _ _ _ ___ 98-11-03 RI. Certification to FAR 25.571, may be required. Per Advisory Circular 25.1529-1 Repairs on Transport Category Airplanes, of the structure must be performed before of the above listed data are approved design data and is not installation approval. info) aircraft model and serial number listed Approved structural analysis on file Services, Inc. office in Birmingham Serial No. 20115 S-3R . END_ END Note: This aircraft is effected fatigue evaluation Continued Airworthiness and fatigue Notes: by AD of structure of Structural evaluation . only for more valid for the based on FAA FL. or DER 727.-31 Damage - tolerance and Instructions for; the damage tolerance 4/11/2003. . herein. This approval below at DER Services office AL. 1) The structural aspects is only for the engineering (Ref. 8110.45 8/30/02 2) This approval is 3) This approval is in Ft. Lauderdale, Model No. PURPOSE Approve data for low profile antenna installation (structural aspects only, Static Analysis) OF DATA APPLICABLE REQUIREMENTS (LIST SPECIFIC SECTIONS) CAR 4b.200, 4b.201, 4b.202, 4b.260, 4b301, 4b302, 4b303, 4b.306 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with condition and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data I (We) Therefore pi Approve these data SIGNATURES) OF DESIGNATED ENGINEERING REPRESENTIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) Robert J. Belgau DERT-510024-CE Structures — , FAA FORM 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION DER SERVICES PROJECT NO. F2006-173 EFTA00277606 - a EFTA00277607 8 7 6 5 4 3 2 1 D C -o B A GENERAL NOTES: 1. FABRICATE PART(s) AS SHOWN. 2. BEFORE INSTALLATION OF DOUBLER, ROLL TO MATCH AIRCRAFT MOLD LINE RADIUS. 3. BREAK ALL SHARP EDGES .0201.030 R. 4. TREAT ALL REWORKED AREAS USING ALODINE 1201S (PER MIL-C-5541, CLASS 1A) AND TVVO (2) COATS OF EPDXY POLYAMIDE PRIMER (PER MIL-P-233377, TYPE I). 5. FINISH ALUMINUM PARTS USING ALODINE 1201S AND TWO (2) COATS OF EPDXY PRIMER. 6. MAINTAIN MINIMUM 2D + 1/16" EDGE DISTANCE FOR ALL FASTENERS ON DETAILS; MINIMUM 2D EDGE DISTANCE ON ASSEMBLY. 7, ALL FASTENERS ARE TO BE INSTALLED IN TRANSITION -FIT HOLES. HOLE TOLERANCE PER NAS618. 8. ALL FASTENER LENGTHS ARE TO BE VERIFIED FOR TOLERANCE PRIOR TO INSTALLATION. 9. INSTALL ALL PARTS AND THREADED FASTENERS WET USING PR1436G TYPE III SEALANT ON ALL FAYING SURFACES. 10. RESTORE ORIGINAL FINISH PER B727 M.M. 51-21. 11. PROTECT REWORKED AREA AGAINST CORROSION PER B727 SRM, CHAPTER 51-10-2. 12. REFERENCE 8727 S.R.M, CHAPTER 51-30 FOR FASTENER REMOVAL AND INSTALLATION PROCEDURES. S - 3R STA 510 13. REINSTALL ALL ADJACENT STRUCTURE REMOVED TO FACILITATE ANTENNA INSTALLATION. 14. BEAD SEAL ANTENNA WITH PRC 1422 SEALENT. 15. REVISE AIRCRAFT RECORDS TO REFLECT INSTALLATION. STA 515.00 S - 2R EXISTING BONDED STRAPS (REF) DESCRIPTION DATE APPROVED I/R INITIAL RELEASE 09-27-2006 EXISTING FUSELAGE SKIN (REF) NAS 1097AD4 - 2 FASTENER CODES ITEM DESCRIPTION ❑ LU❑ itj NASI097AD4 (TY'P 50 PLS) x 64510428AD 3 (TYP 8 PLS) x STA 520 50 COUNTERSUNK RIVET OPL 8 RIVET - NUTPLATE MS20426AD3- 2 QPL 4 4 SCREW MS24694C55 OPL 3 4 NUTPLATE NAS 1 473A3 QPL 2 1 1 1 DOUBLER - INTERNAL L1 CPS-IRIDIUM ANTENNA 567- 1575-109 0.050" 2024-T3 00 -A -250/5 QPL QPL ITEM QTY NAME PART NUMBER MATERIAL MIL-SPEC VENDOR Ports List CRAVING CREATED FCN, BANYAN AIR SERVICE CRAVING SIZE, B DATE APPROVED 09-27-2006 lJ DER SERVICES 2100 kV 6.311 STREET, Suitt C-I09, FT. LAITIRDAI.E rl. =9. (9509TI.3B32, FAX(954)971-3059 nes date Is provided as • CONFIDENTIAL AND PRIVILEGED 00C(JMENTOebecin BANYAN AIR SERVICE & DER 5•M ass. My oN use of raproductco *afoul the expnrssed tten coneare of DER Sareloatbaxpassly latedcius. My M4064 of 0is docurnerd incluctify INN not Potted IS) rasldabon In pen riOsoul send.n consent ci DER Son nee Is expressly Portirkeen. This aporovei Es Pew] upon AN. mod sr-esti@ ID DER Servicsrs torn BANYAN AIR SERVICE al So. Offs of nsporl corrphillon. My iddlaccial data Mich Osamu reale:is. may mull b afnenftn; 0r COnctoslco(s) expressed haneln UNLESS OTHERWISE SPECIFIED DIMENSIONS ARE IN INCHES UNSPECIFIED TOLERANCE FRACTIONS ANGLES DECIMALS DRAVN BTU W.D.OLIVERI CHECKED BY' R.J.BELGAU STRESS BY' W.D.OLIVERI ±1/32 .15 MACH. .2 FORMED .X ± .1 .XX t .03 .XXX_ t .010 APPROVED BY. R.J.BELGAU 8 7 5 4 3 TITLE IRIDIUM ANTENNA INSTALLATION STA 515 - BTWN S-2R & S-3R A/C Typr BOEING T'G 2006-173-1 N.A.REV I/R Nod No ' 727-31 TAIL No. r N908JE PROJ 2006-173 -SCALE. SERIAL No 20115 STRL INSTL SHEET 1 OF 3 2 1 D C 4- B A EFTA00277608 J EFTA00277609 8 7 6 5 4 3 2 STA 510 EXISTING FUSELAGE SKIN (REF) VIEW LOOKING UP SOME STRUCTURE REMOVED FOR CLARITY 01.00 CONNECTOR CUTOUT IN SKIN STA 520 IRIDIUM ANTENNA INSTALLATION @ STA 515.00 - BTWN S-2R & S-3R EXISTING BONDED STRAPS (REF) EXISTING BONDED STRAPS (REF) TN. deer b prose.. as • COW IDENTIX. AND PFUYILED0ED DOCUMENT between BANYAN AIR SERVICE DER SerrIces. My Other use or (spend ucton ecnotrt De esOreesslawrInen mos. of DER SessIcse N.sweaty MPMM. My ndsyse of Pis Ovarrent bOumrq (bvl rot ernlletl b) qv...Jon b pert with. written consent of DER Se.. M -Drew lortedden. T. *pus.* Is based v.n dab ft.., sessiebb lo DER Sen.. Rom BANYAN AIR SERVICE al be SIR ot report corrode., My ...Ye/ dale. eh. becomes rear.. may row. In •^r•ran5 eye con:Susie*/ bIreesedb... 4 4 EXISTING BONDED STRAPS (REF) EXISTING FUSELAGE SKIN (REF) SECTION A-A D C 4- DER SERVICES ,'),`." 2006-173-1 2700 N.W. 62/10 STREET, 6us C-109, FT. LAUDERDALE. R 33XS. (554) 571.3832. FAX (M.) .7 14.0 B SIZE DRAWN BY, W.D.OLIVERI REV UR SERIAL No. . 20115 SCALE 3= 4 SWET 2 OF 3 8 I 7 I 6 5 4 3 2 B A EFTA00277610 3 • EFTA00277611 8 7 6 5 4 3 2 1 -0 B 01.62 FASTENER PATTERN (TYP 6 PLS) 00.20 ANTENNA MOUNT HOLE (TYP 4 PLS) 01.00 CONNECTOR CUTOUT ITEM 2 / DOUBLER FABRICATION USE NUTPLATE AS PATTERN FOR RIVET HOLES. (TYP 8 PLS) R 0.25 4.50 0 0 0 0 0 (TYP 4 PLS) 4.13 0 0 0 3.66 O O O 3.19 3.19 O o 2.72 -0 0 0 ( 0 o o o 2.24 Ck O o 1.78 0 1.38 o O ED O o 0 O 1.29 O 0.84 O O O O O O 0 0.38 O 0.00 o CO tO CI O W.to Cl CD CO 1O cn O CO LO C') O cr) t•- e ill CO N CO CD 0, cO CV CO O o o o cNi N (vi ri 4 4 4 4- B A A This data le ortroldid ae • CONFIDENTIAL AND PRA/ILEDDED DOCUMENT betetern BANYAN AiR SERVICE DERE...Mon. Any caw, ow or reproduction without the eapreesed rattan oznunt of DER BeMc.e4 expreeffy forbidden. Any mg.*. of AN 6:.O...nt I:Coelho (but not United quotation in pert without written coreenl of DER Serelpe b eefe...fY forbidden. Thts *pommel Is bawl upon date mad. sysliftes to DER Sonia. eon BANYAN AIR SERVILE el Ow erne of 1900 etelpfli3on. Any edditionei date. which becomes eveiletie, rney refue tr. emending tne oonclusicn(s) freereased herein. DER SERVICES NQG 2006-173-1 2700 N.W. 132.3 STREET. &Ate C-I09, FT. LAUDERDALE. FL. 11309. (p 6e) 971-3832. FAX (964)971-3059 SIZE ERAVN BY. REV W.D.OLIVERI l/R SERIAL No. .2O 1 1 5 SCALE 0.5 = 1 SET 3 C.F 3 8 7 6 5 fi 4 3 2 EFTA00277612 EFTA00277613 • , C US Department MAJOR REPAIR AND ALTERATION Of Transportation Federal (Airframe, Powerplant, Propeller, or Appliance) Aviation Administration Form Approved OMB No. 2120-0020 For FA Use Only Office Identification SO- (3 DO -17 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model 727-100 Serial No. 20155 Nationality and Registration Mark USA N908JE 2. Owner Name (As shown on registration certificate) J.E.G.E. Inc. Address (as shown on registration certificate) 103 Foulk Road, Ste 202 Wilmington, DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE AVIONICS DIVISION 1635 NW 51st Place Ft. Lauderdale, FL 33309 U.S. Certificated Mechanic Radio C SD4R514M Class Limited Airframe Foreign Certificated Mechanic 0 Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 8 November 2004 Signature of Authoriz_e_ii.i licyl . 7.2; /d -‘,/ e Steve Ouellette 7. Approval for Return to Service Pursuant to the authority Federal Aviation Administration given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the and is II APPROVED II REJECTED BY FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 19 November 2004 Certificate or Designation No. SD4R514M Signature of _---) _ Authorized Individual Steve Ouellette C FAA Form 337 (12-88) EFTA00277614 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) The purpose of this 337 is for the FAA approval of the new flight manual supplement on N908JE under Banyan Air Servive, Avionics Division work order #68062. A. Removed existing TDR-94 transponders P/N 622-9210-003 and routed to the manufacture for upgrade to P/N 6252-9210-007 to provide flight ID. System ground and flight checked good. B. The weight & balance is not affected and equipment list was updated. C. Instructions for continued airworthiness are "on condition only". END ❑ Additional Sheets are Attached G' fin Og(10.b ffL, EFTA00277615 ' . 0 ••--- . -I US Department MAJOR REPAIR AND ALTERATION Of Transportation Federal (Airframe, Powerplant, Propeller, or Appliance) Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification 5a — r 51)6-17 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions a disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model 727-100 Serial No. 20115 Nationality and Registration Mark USA N908JE 2. Owner Name (As shown on registration certificate) J.E.G.E, Inc. - Address (as shown on registration certificate) 103 Foulk Road STE 202 Wilmington, DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE AVIONICS DIVISION 1635 NW 51st Place Ft. Lauderdale, FL 33309 U.S. Certificated Mechanic M Radio C SD4R514 lass 1,2,3 Limited Airframe Foreign Certificated Mechanic a Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. . Date 7 . 1/6/1•1/9e -:-/ a 4:2C7 (71Signature of Authori 4i.s.Jualit ‘C Steve Ouellette 7. Approval for Return to Service Pursuant to the authority given personsirficied below, the Federal Aviation Administration and is APPROVED unit identified in item 4 was inspected in the manner prescribed by the Administrator of the • REJECTED BY FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection / / r Ahi/6Arc e__c72O) C Certificate or Designation No. SD4R5 14M Signature o d Indivi Steve Ouellette FAA Form 337 (12-88) EFTA00277616 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) The purpose of this 337 is for the work performed on N908JE under Banyan Air Service, Avionics Division work order #68062. A. Installed a Universal Avionics Systems Corp. Terrain Avoidance and Warning System in accordance with SIP Technical Services, Inc. data list 7280-DL-001-501, Rev. H dated December 2002 or later. (STC# ST09951SC) B. The above installation was performed in accordance with AC43.13-1B, Chapter 7, sections 1-5, AC43.13-1B Chapter 11, sections 3-17, AC43.13-2A Chapter 1, AC43.13-2A Chapter 2, paragraphs 24, 25, and 28, AC25-23 and the aircraft's maintenance manual. C. A functional test of the above equipment has been performed FAR25.1309 and FAR25 1431 for proper operation and did not adversely affect any other aircraft systems. An electrical load analysis was conducted and it was confirmed that this installation would not exceed 80% of the generator output. D. A log book entry and equipment list was generated to reflect the above installation. A weight & balance was calculated. An FAA approved flight manual supplement provided with the above STC, Document No. 7280-FM-001, dated December 13, 2002 or later E. Instructions for continued airworthiness provided by SIP Technical Services Report No. 7280-ICA-001 Rev. F dated June 6, 2002. END *Ay ❑ Additional Sheets are Attached EFTA00277617 pniteb tutes jArrirriCn Prpartrrttnt of Zrartsportation - grbrral czAfliatinn cAbmirtistration ,upialentenial `Tuve Certificate t.471teinh.fe ST09951SC e°rlteak 1,:s,tezeti/o .SIP Technical Services, Inc. 10107 McAllister Freeway San Antonio, TX 78216 cu.-44,1 dead; ejange art de; *//ze tleJe 7y r1.4 a‘e.it,72/<cikelled/f bre dindal4vzs rz./sticevu‘4.-ivz.s . dercAr ens .yieceAdife .,,eevinee4s de izievz-c-vakeaeJis "e9ece.:vnuva.4.t ei4:7tr."/ 4b c/a; Civil Air Refez44iva.s. 6isr:;th2aigivekcl n'iv0cale A3WE ,d&zZe.- Boeing .A6esehi.• 727-100 Series .gesc. ,04"evz c>4.F1//ze Wiazife. - Installation of a Universal Avionics Systems Corporation Terrain Awareness and Warning System in accordance with SIP Technical Services, Data List 7280-DL-001-501, Revision H, dated December 5, 2002, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement Document Number 7280-FM-001, dated December 13, 2002, or later FAA approved revision is required. eindg7cyzeita..s.• Compatibility of this design change with previously approved modifications must be determined by the installer. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. ce,-10cate and14 6:- .111/2/2O/66.iip ektet tcs/ficiza 9ga Jarre feei .1‘.4.3/2eze , reecch geeicv , a te..rmZaaleiva eizhr c3 cae.e<av:se e...ilae°4‘ede;/ dt; .../ge/z71.44e:stkzkv , €/° ev-a,'._/gotallevt.AeGitzikeafinciliark. :gale e3:rev/i&alei -vz, .• August 02, 2001 Lale 9/4,sa.z/ue ..December 13, 2002 :2ale rez,...uaed; gale ez,,vezaeAl.• (Sign ture) ces Co er, Spe ial Ce cation Office South4vest Region (Title) Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA Form 8110-2(10-68) Page 1 of 2 This certificate may be transferred in accordance with FAR 2I.47. EFTA00277618 . . EFTA00277619 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BOEING 727-100 WITH UNIVERSAL AVIONICS SYSTEMS CORPORATION DUAL MULTISENSOR UNS-ID+ FLIGHT MANAGEMENT SYSTEMS REG #. N908.TE SERIAL #. 20115 M This supplement must be attached to the FAA Approved Airplane Flight Manual when the Universal Avionics System Corporation UNS-1D+ Flight Mana•ement System (FMS) is .in§talled in accordance with field approved 337 dated 1Voll (2200 )4' . The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this supplement; consult the basic Airplane Flight Manual. FAA APPROVED Gary Justice Principal Avionics Inspector Federal Aviation Administration Flight Standards District Office #17 Ft. Lauderdale, FL 33315 Date: NOV 8 2004 Rev. 0 '.'Pl‘ge 1 of 9 EFTA00277620 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 Table of Contents Flight Manual Supplement UNS-1D+ FMS N908JE BOEING 20115 SECTION PAGE GENERAL 3 LIMITATIONS 3 EMERGENCY PROCEDURES 3 NORMAL PROCEDURES 3 PERFORMANCE 6 Revision 0 All Date: NOV 8 2004 RECORD OF REVISIONS Pages Description Initial Release Rev. 0 Approved . NOV 8 71104 Pige 2 of 9 EFTA00277621 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 SECTION 1- GENERAL 1. INSTALLATION DESCRIPTION. Flight Manual Supplement UNS-1D+ FMS N908JE BOEING 20115 The Universal Avionics Systems Corporation dual FMS's use inputs from their integral GPS Receivers, Navigation Receivers and DME Transceivers to provide a blended position for navigation. Each FMS contains an internal TSO C129a GPS sensor (GNSS 2400), which is cross-wired to the other FMS such that both systems have GPS 1 and GPS 2 data as inputs. The FMS's receive air data parameters from an Air Data Computer. A Data Transfer Unit (DTU100) is used to load periodic navigation data base updates via zip disks. The systems provide navigation an