Service Bulletin No: 46-004 Date: Apr 26/13 Rev No. 9 Date: Feb 04/20 Page 1 of 66 Service Bulletin No: 46-004 Ref No: ------------306 Modification No: EC-12-0579, EC-13-0221, EC-13-0257, EC-16-0485 ATA Chapter: 46 SERVICE BULLETIN PILATUS AIRCRAFT LTD, STANS, SWITZERLAND SYSTEMS INTEGRATION AND DISPLAY WIRELESS DATA LOADING SYSTEM (CONNECTED FLIGHT DECK) INSTALLATION 1. Planning Information A. Effectivity PC-12/47E aircraft MSN 1001 - 1719, 1721 - 1944 without the factory option - Connected Flight Deck - installed. B. Concurrent Requirements Aircraft with Service Bulletin 45-012 embodied or with Honeywell Primus APEX Operational Software Build 8.8 or higher installed. AFM Report Number 02277 at Revision 16 or higher. C. Reason (1) Problem Database loading and maintenance data downloading is time consuming. Flight plans created off-aircraft cannot be easily loaded to the Primus APEX avionics suite. (2) Solution Install a wireless data loading system. From a Personal Electronic Device (PED), the system can: • Upload databases to the Primus APEX avionics suite • Upload flight plans to the Primus APEX avionics suite on-ground (with APEX Build 8.8) or on-ground and in-air (APEX Build 10 only) • Download and clear maintenance data from the Primus APEX avionics suite • Broadcast flight information and show a moving map on the PED in the passenger cabin. D. Description This Service Bulletin gives the instructions necessary to install a wireless data loading system. A wireless router (the Aspen Connected Gateway CG100P) is installed behind the baggage compartment right trim panel. Two circuit breakers are added for the CG100P electrical power. Wiring is added to interface the CG100P to the Modular Avionics Unit (MAU) and the maintenance panel. The right auxiliary sidewall panel is replaced and modified with a switch and an LED to allow database uploads with aircraft standby power only. Revision 1 to this Service Bulletin modifies the wiring from the WLAN data loader to the MAU. Revision 2 to this Service Bulletin is for aircraft MSN 1209. Aircraft at Revision 1 are not affected
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Service Bulletin No: 46-004 Date: Apr 26/13Rev No. 9 Date: Feb 04/20 Page 1 of 66
Service Bulletin No: 46-004 Ref No: ------------306
Modification No: EC-12-0579, EC-13-0221, EC-13-0257, EC-16-0485 ATA Chapter: 46
SERVICE BULLETIN
PILATUS AIRCRAFT LTD, STANS, SWITZERLAND
SYSTEMS INTEGRATION AND DISPLAYWIRELESS DATA LOADING SYSTEM (CONNECTED FLIGHT DECK) INSTALLATION
1. Planning Information
A. Effectivity
PC-12/47E aircraft MSN 1001 - 1719, 1721 - 1944 without the factory option - Connected Flight Deck - installed.
B. Concurrent Requirements
Aircraft with Service Bulletin 45-012 embodied or with Honeywell Primus APEX Operational Software Build 8.8 or higher installed.
AFM Report Number 02277 at Revision 16 or higher.
C. Reason
(1) Problem
Database loading and maintenance data downloading is time consuming. Flight plans created off-aircraft cannot be easily loaded to the Primus APEX avionics suite.
(2) Solution
Install a wireless data loading system. From a Personal Electronic Device (PED), the system can:
• Upload databases to the Primus APEX avionics suite
• Upload flight plans to the Primus APEX avionics suite on-ground (with APEX Build 8.8) or on-ground and in-air (APEX Build 10 only)
• Download and clear maintenance data from the Primus APEX avionics suite
• Broadcast flight information and show a moving map on the PED in the passenger cabin.
D. Description
This Service Bulletin gives the instructions necessary to install a wireless data loading system. A wireless router (the Aspen Connected Gateway CG100P) is installed behind the baggage compartment right trim panel. Two circuit breakers are added for the CG100P electrical power. Wiring is added to interface the CG100P to the Modular Avionics Unit (MAU) and the maintenance panel. The right auxiliary sidewall panel is replaced and modified with a switch and an LED to allow database uploads with aircraft standby power only.
Revision 1 to this Service Bulletin modifies the wiring from the WLAN data loader to the MAU.
Revision 2 to this Service Bulletin is for aircraft MSN 1209. Aircraft at Revision 1 are not affected
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Service Bulletin No: 46-004 Date: Apr 26/13Rev No. 9 Date: Feb 04/20 Page 2 of 66
SERVICE BULLETIN
by this revision.
Revision 3 to this Service Bulletin modifies the installation instructions and includes aircraft MSN 1001 and Up. A new CG100P (P/N 975.96.32.439) Revision F is installed. A setup and test procedure is included in the Service Bulletin instructions.
Customers who have embodied this Service Bulletin at Revision 1 and Revision 2 shall update to Revision 3 of this Service Bulletin.
Revision 4 to this Service Bulletin updates the login procedure. Customers who have embodied this Service Bulletin at Revision 3 need not do further work.
Revision 5 to this Service Bulletin modifies the installation instructions and introduces new pins and sockets for cross-over connectors P188-4A and J188-4A. This revision also updates the grounding point for wire U28A22N. Customers who have embodied this Service Bulletin at an earlier revision need not take further action.
Revision 6 to this Service Bulletin updates the procedure to incorporate software Build 8.8 and corrects a part number error. It is highly recommended that customers who have embodied this Service Bulletin at an earlier revision upgrade to Build 8.8.
Revision 7 to this Service Bulletin introduces a new CG100P unit (P/N 975.96.32.456) with software Build Revision G. The old CG100P units (P/N 975.96.32.439) are updated to the new unit with a software loader tool. This software build is field-loadable and introduces new functionality, e.g. deletion of Aircraft Condition Monitoring System (ACMS) maintenance data from the Primus APEX avionics suite. Customers who have incorporated this Service Bulletin at an earlier revision can incorporate Service Bulletin 46-006 to upgrade the CG100P unit to the latest software version.
Revision 8 to this Service Bulletin updates the procedure to support the CG100P unit with either Software Build Revision G or Software Build Revision H. Revision 8 also adds an export control statement.
Revision 9 to this Service Bulletin updates the effectivity. Customers who have embodied this Service Bulletin at an earlier revision need not take further action.
This Service Bulletin gives an instruction to remove AFM TR 37.
Customers with a configured CG100P unit who have incorporated this Service Bulletin at an earlier revision must incorporate Service Bulletin 46-007 (at the latest revision). This will upgrade the CG100P unit to software Build Revision H.
E. Compliance
Optional.
F. Approval
The technical content of this Service Bulletin is approved under the authority of DOA No. EASA. 21J.357.
PILATUS advises Operators/Owners to check with their designated Airworthiness Authority for any changes, local regulations or sanctions that may affect the embodiment of this Service Bulletin.
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G. Copyright and Legal Statement
© Pilatus Aircraft Ltd. This document contains proprietary information that is protected by copyright. All rights are reserved. No part of this document may be copied, reproduced or translated to other languages without the prior written consent of Pilatus Aircraft Ltd.
In connection with the use of this document, Pilatus does not provide any express or implied warranties and expressly disclaims any warranty of merchantability or fitness for a particular purpose. This document contains trade secrets, confidential and/or proprietary information of Pilatus and technical data subject to export control laws and regulations, including the U.S. Export Administration Regulations (EAR). Disclosure or distribution of this document contrary to the EAR, and other laws and regulations, is strictly forbidden. The above restrictions may apply to data on all pages of this document.
H. Manpower
Note: Man-hours are calculated as work done at annual inspection.
I. Weight and Balance
Weight change: +0,789 kg (+1.7 lb)
Moment change: +6,373 kg m (+553.15 lb in.).
J. Electrical Load Data
Nominal current (28 VDC): 0.25 Amps
Maximal current (28 VDC): 1.1 Amps.
K. Software
Honeywell Primus APEX Operational Software Build 8.8 or higher is required.
CG100P Software Build Revision H (version 2.2).
Task Man-hours
Preparation 10
Modification 28
Test 2
Close up 10
TOTAL MAN-HOURS 50
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L. References
Aircraft Maintenance Manual (AMM)
Tool and Equipment Manual (TEM):
M. Publications Affected
AFM, AMM, IPC, TEM, SRM, WDM.
N. Interchangeability of Parts
Not applicable.
12-B-06-20-00-00A-040A-A 12-B-20-31-00-00A-070A-A 12-B-20-50-10-00A-920A-A
12-B-24-00-00-00A-901A-A 12-B-24-52-51-00A-920A-A 12-B-25-10-01-00A-920A-A
12-B-25-21-01-00A-920A-A 12-B-25-21-04-00A-920A-A 12-B-25-21-07-00A-920A-A
12-B-25-22-01-00A-920A-A 12-B-25-22-04-00A-920A-A 12-B-25-23-01-00A-920A-A
12-B-31-41-00-00A-903A-A 12-B-31-41-00-00A-920A-A 12-B-31-42-00-00A-920A-A
12-B-45-45-00-00A-331A-A 12-B-45-45-00-00A-550A-A
12-B-45-45-00-00A-066A-A 12-B-46-21-00-00A-066A-A
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2. Material Information
A. Material - Price and Availability
Operators that require additional information and/or Service Bulletin Material should contact their authorized Pilatus Service Center, or Pilatus Customer Support on www.pilatus-aircraft.com contact us
Part Numbers given in this Service Bulletin are correct at the time of approval. Pilatus AircraftLtd. reserves the right to change the part numbers as necessary. Part numbers of items deliveredwith the kit are correct when the kit is dispatched. This could lead to differences between thosepart numbers quoted in this Service Bulletin and the kit if parts are superseded. Operators arerequested to check the IPD for delivered parts which differ from those listed in the ServiceBulletin Materials Kit List.
B. Warranty
Not applicable.
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