Garmin Part 23 AML STC FAA Approved Airplane Flight Manual Supplement
Contents
1. e eite RAE m M 4 1 2 RVSM GROUP AIRWORTHINESS APPROVAL 4 1 3 DESCRIPTION erem toe bete estes 4 1 4 DEFINITIONS e eise heed Mise es 6 SECTION 2 14 5 7 2 1 STATIC PORTS uem et 7 2 2 ADC 1 2 SWITCH oeste IM edere te seb Ate 7 2 3 REQUIRED EQUIPMENT ss cccccccecsessaececececsessaececececsensaaeeeceesceensneaeees 7 SECTION 3 EMERGENCY 8 3 1 EMERGENCY PROCEDURES eene hehe hehehe enne eere nennen 8 3 2 ABNORMAL PROCEDURES sssseseseeeseseseseseseceveceseceseseseseseseseseeeeeeees 12 SECTION 4 NORMAL 5 13 4 1 PREFLIGHT INSPECTION 13 4 2 13 4 3 CRUISE 13 SECTION 5 eere eee eese eaae 14 SECTION 6 WEIGHT AND BALANCE ee ee ee 14 SECTION 7 DESCRIPTIQON oves en sane e enar ea peo teen a eb eE aa eee PR Re eaa 15 7 1 PITOT STATIC SYSTEM ir titor om ee ti Hiseis2. 2 FAA APPROVED Page 14 of 15 Section 7 DESCRIPTION 7 Pitot Static System The pitot static instruments that are part of this RVSM configuration are connected to the sources specified in the following table Instrument Pitot Source Static Source ADC 1 GDC 74B Pitot 1 Static 1 Emergency ADC 2 AM 250 Pitot 2 Static 2 Pilot s Standby Altimeter N A Static 2 Pilot s Standby Airspeed Pitot 2 Static 2 Source is selected by the emergency static valve Sources for other instruments are unchanged by this modification 7 2 Transponder Altitude Sources Transponder 1 receives altitude data from the G600 PFD and will report the pressure altitude from the source that is displayed on the PFD In normal operations Transponder 1 will report the pressure altitude from ADC 1 If ADC 2 is selected for display on the PFD then Transponder 1 will report the pressure altitude from ADC 2 Transponder 2 if installed receives altitude data from the AM 250 ADC 2 Transponder 2 will always report the pressure altitude from ADC 2 Section 8 HANDLING SERVICING AND MAINTENANCE Instructions for Continued Airworthiness are contained in Garmin document number 190 00601 00 Revision K or later AFMS TBM 700 850 G600 RVSM 190 00601 34 Rev 2 Page 15 of 15
3. 15 7 2 TRANSPONDER ALTITUDE SOURCES eee 15 SECTION 8 HANDLING SERVICING AND MAINTENANCE 15 AFMS TBM 700 850 G600 RVSM 190 00601 34 Rev 2 FAA APPROVED Page 3 of 15 Section 1 GENERAL 1 1 Applicability This supplement applies to TBM 700 850 aircraft which have been modified for Reduced Vertical Separation Minimum RVSM in accordance with Supplemental Type Certificate STC SA02153LA D It applies to TBM 700 850 aircraft which have been modified in accordance with Appendix P of the G600 AML STC Installation Manual for RVSM flight operations For general limitations procedures and performance information on the G600 system refer to the G600 AFMS Garmin part number 190 00601 01 NOTE The basic G600 AFMS includes limitations and procedures for the altitude preselector 12 RVSM Group Airworthiness Approval Aircraft equipped with this modification have been evaluated in accordance with 14 CFR Part 91 Appendix G Operations in Reduced Vertical Separation Minimum RVSM Airspace and FAA Advisory Circular 91 85 Authorization of Aircraft and Operators for Flight in Reduced Vertical Separation Minimum Airspace and are qualified for RVSM operations as a group aircraft This finding does not constitute approval to conduct RVSM operations Additional approval to conduct RVSM operations may be required by the local aviation authority 13 Description The RVSM configuration consists of the followin
4. Garmin International Inc 1200 E 151 Street Olathe Kansas 66062 U S A FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT for the GARMIN G600 SYSTEM WITH REDUCED VERTICAL SEPARATION MINIMUM RVSM CAPABILITY as installed in TBM 700 A B C1 C2 and N 850 Registration Number Serial Number This document serves as an Airplane Flight Manual Supplement when the aircraft is modified in accordance with Supplemental Type Certificate SA02153LA D for RVSM group airworthiness approval with the Garmin 600 system This document must be carried in the airplane at all times The information contained herein supplements or supersedes the information in the approved Airplane Flight Manual Pilot s Operating Handbook only in those areas listed herein For limitations procedures and performance information not contained in this document consult the basic Airplane Flight Manual Pilot s Operating Handbook or other applicable supplements FAA APPROVED BY ET Michael Warren ODA STC Unit Administrator GARMIN International Inc ODA 240087 CE DATE 2 DZ 2043 AFMS TBM 700 850 G600 RVSM 190 00601 34 Rev 2 FAA APPROVED Page of 15 LOG OF REVISIONS Rev Section Description FAA Approval See Page 1 AFMS TBM 700 850 G600 RVSM 190 00601 34 Rev 2 FAA APPROVED Page 2 of 15 TABLE OF CONTENTS SECTION Te GENERAL 5e eene ee reae o e eere oe TUE pone Cea eu pega uae 4 1 1
5. cedures specified in the basic AFM POH or applicable supplements 4 1 Preflight Inspection 1 Visually inspect the static ports and the RVSM critical region for damage or surface irregularities 4 2 Before Takeoff 1 Select ADC 2 amber using ADC 1 2 switch a Verify that PFD altitude matches AM 250 altitude b Verify that PFD airspeed and vertical speed tapes are indicating correctly approximately zero NOTE If the GAD 43e is providing attitude to the autopilot a yellow CHECK ATTITUDE banner will be displayed on the PFD while ADC 2 is selected 2 Select ADC 1 green using ADC 1 2 switch 3 Check both primary altimeters and standby altimeter a With all altimeters using same altimeter setting the difference between the highest and lowest altimeter must not exceed 80 feet 4 3 Cruise 1 Set PFD altitude alerter to assigned altitude 2 Engage automatic altitude hold mode a Refer to autopilot AFM and basic G600 AFMS for autopilot and altitude preselect procedures 3 Cross check altimeters a Verify altimeter settings e g 29 92 inHg b Note differences between primary and standby altimeters in accordance with RVSM procedures NOTE Difference between primary altimeters must be less than 200 feet AFMS TBM 700 850 G600 RVSM 190 00601 34 Rev 2 FAA APPROVED Page 13 of 15 Section 5 PERFORMANCE No change Section 6 WEIGHT AND BALANCE No change AFMS TBM 700 850 G600 RVSM 190 00601 34 Rev
6. e g 29 92 inHg 2 Attempt to identify the incorrect primary altimeter If the PFD altimeter ADC 1 is determined to be incorrect e Perform procedure 3 1 1 ADC 1 Failure If the AM 250 altimeter ADC 2 is determined to be incorrect e Perform procedure 3 1 2 ADC 2 Failure If unable to determine which primary altimeter is incorrect e Perform procedure 3 1 3 ADC 1 and ADC 2 Failure AFMS TBM 700 850 G600 RVSM 190 00601 34 Rev 2 FAA APPROVED Page 10 of 15 3 1 5 PFD Failure RVSM considerations WARNING This procedure is to be performed in addition to the PFD 1 Failure procedure in the basic G600 AFMS This procedure only addresses RVSM considerations for PFD failure In addition to the loss of flight instruments PFD failure will result in the loss of altitude alerting and Transponder 1 altitude reporting 1 Monitor AM 250 altimeter to maintain assigned altitude using autopilot or manual control 2 Select Transponder 2 if installed NOTE If Transponder 2 is not installed or inoperative per MEL continue to operate Transponder 1 without altitude reporting stop altitude squawk 3 Execute RVSM contingency procedures for the following e Loss of one primary altimetry system e Loss of altitude alerting e Loss of altitude reporting if Transponder 2 is not installed or inoperative AFMS TBM 700 850 G600 RVSM 190 00601 34 Rev 2 FAA APPROVED Page 11 of 15 3 2 Abnormal Procedures 3 2 Los
7. g equipment GDU 620 Primary Flight Display PFD GDC 74B Air Data Computer ADC 1 GAD 43e adapter 250 altimeter air data computer ADC 2 ADC 1 2 selector switch KFC 275 325 autopilot system Transponder 1 Transponder 2 optional A block diagram of the configuration is shown in Figure 1 1 AFMS TBM 700 850 G600 RVSM 190 00601 34 Rev 2 FAA APPROVED Page 4 of 15 SNOILVH3T3JOOV 1VNOlLdO c TV 244 OGM 39VON3 M STVNDIS 1 LIY 9 SA dude Liv I nbg Bunsixa3 b 018 0099290 Occ dOM bos 209 UO Liv J 7 22 55 ody z ody 1011 029 NAD AW1dSIO LOTId J paesu Is L Figure 1 1 RVSM equipment block dicrum 190 00601 34 Rev 2 AFMS TBM 700 850 G600 RVSM FAA APPROVED Page 5 of 15 14 Definitions The following acronyms are used within this document ADC Air Data Computer GPS Global Positioning System IFR Instrument Flight Rules KOEL Kinds of Operation Equipment List OAT Outside Air Temperature PFD Primary Flight Display RVSM Reduced Vertical Separation Minimum TAS True Air Speed AFMS TBM 700 850 G600 RVSM FAA APPROVED 190 00601 34 Rev 2 Page 6 of 15 Section 2 LIMITATIONS 2 1 Stat
8. ic Ports RVSM operations are not permitted if the static ports are damaged or if there is damage or surface irregularities within the RVSM critical area NOTE The RVSM critical area encompasses approximately 18 inches forward and 8 inches above below aft of the static ports If damage or surface irregularities are suspected to be within this area consult maintenance personnel 22 ADC 1 2 Switch During normal operations the ADC 1 2 switch must be selected to the ADC 1 green source Selection of the ADC 2 amber source is only permitted during system testing and emergency procedures 2 3 Required Equipment The following equipment must be operational before initiating RVSM flight operations e Garmin G600 equipment installed in the pilot s instrument panel e AM 250 altimeter installed in the copilot s instrument panel e Autopilot system including altitude hold function e 1 2 switch e 1 transponder with altitude reporting function AFMS TBM 700 850 G600 RVSM 190 00601 34 Rev 2 FAA APPROVED Page 7 of 15 Section 3 EMERGENCY PROCEDURES 3 1 Emergency Procedures NOTE The ADC failure procedures in this AFMS supersede the ADC failure procedure in the basic G600 AFMS 3 1 1 ADC 1 Failure ADC 1 failure is indicated by a red X and yellow text over the airspeed altimeter vertical speed TAS and OAT displays on the PFD Wind calculations will also be unavailable If valid GPS data is available the PFD will aut
9. omatically display GPS altitude relative to mean sea level above the altitude tape If the GAD 43e is providing attitude to the autopilot a yellow CHECK ATTITUDE banner will be displayed on the PFD and the autopilot will disconnect 1 Monitor AM 250 altimeter to maintain assigned altitude Refer to standby airspeed indicator for airspeed reference 2 Select ADC 2 for display on PFD using ADC 1 2 switch When ADC 2 data is displayed on PFD the PFD may be used for altitude airspeed and vertical speed references The PFD altitude alerter function will be restored TAS OAT and wind calculations will remain unavailable If the GAD 43e is providing attitude to the autopilot the CHECK ATTITUDE banner will remain displayed on the PFD and the autopilot will be inoperative 3 Execute RVSM contingency procedures for the following e 055 of one primary altimetry system e Loss of all automatic altitude hold systems if CHECK ATTITUDE is displayed on PFD AFMS TBM 700 850 G600 RVSM 190 00601 34 Rev 2 FAA APPROVED Page 8 of 15 3 1 2 ADC 2 Failure ADC 2 failure is indicated as blank or FAIL text in place of the normal altitude readout on the AM 250 LCD display Automatic altitude control mode will be inoperative 1 Disengage the autopilot and maintain assigned altitude manually by reference to the PFD altimeter 2 If Transponder 2 is installed and selected select Transponder 1 NOTE If Tran
10. s of Altitude Reporting If loss of transponder altitude reporting is suspected or reported 1 Select other transponder for operation if installed and operative If other transponder is not installed or inoperative per MEL 2 Continue to operate installed operative transponder without altitude reporting stop altitude squawk 3 Execute appropriate RVSM contingency procedure for loss of altitude reporting 3 2 2 Loss of Automatic Altitude Hold If the autopilot or altitude hold mode fails for any reason e g loss of attitude servo failure or trim failure 1 Disengage autopilot and maintain assigned altitude manually using available primary or standby altimeters 2 Execute appropriate RVSM contingency procedure for loss of all automatic altitude hold systems 3 2 3 Loss of Altitude Alerting NOTE This procedure applies to loss of altitude alerting due to an inability to select the desired altitude or loss of altitude alert tones Refer to PFD or ADC failure procedures for other failure scenarios 1 Engage autopilot altitude hold mode at assigned altitude 2 Monitor primary altimeters while maintaining assigned altitude 3 Execute appropriate RVSM contingency procedure for loss of altitude alerting AFMS TBM 700 850 G600 RVSM 190 00601 34 Rev 2 FAA APPROVED Page 12 of 15 Section 4 NORMAL PROCEDURES The normal procedures in this section are for RVSM flight operations and are in addition to all other normal pro
11. sponder 1 is inoperative per MEL continue to operate Transponder 2 if installed without altitude reporting stop altitude squawk 3 Execute RVSM contingency procedures for the following e Loss of one primary altimetry system e Loss of all automatic altitude hold systems e Loss of altitude reporting if Transponder 1 is inoperative 3 1 3 ADC 1 and ADC 2 Failure ADC 1 and ADC 2 failures are indicated as described in procedures 3 1 1 and 3 1 2 1 Disengage the autopilot and maintain assigned altitude manually by reference to the standby altimeter 2 Execute RVSM contingency procedures for the following e Loss of all primary altimetry systems e Loss of all automatic altitude hold systems e Loss of altitude alerting e Loss of altitude reporting AFMS TBM 700 850 G600 RVSM 190 00601 34 Rev 2 FAA APPROVED Page 9 of 15 3 1 4 Difference in Primary Altimeters If the primary altimeters PFD and AM 250 differ by 200 feet or more attempt to identify the incorrect primary altimeter WARNING The standby altimeter uses the same static source as the AM 250 ADC 2 The standby altimeter does not have static source error correction applied and will therefore differ slightly from the primary altimeters during normal operation Do not use the standby altimeter as the only means of determining the incorrect altimeter 1 Verify all altimeters both primary altimeters and standby are set to the correct altimeter setting
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