Airframe Manufacturer s Perspective Agenda
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1 Agenda August 6, Boeing's Perspective on RVSM 2. Approved Airframes 3. Non Group Airframes 4. Accuracy, Degradation and Maintenance 5. Future Airframe and Airplane System Development 6. Related Issues
2 RVSM Benefits: Boeing's Perspective on RVSM Increased Operating Capacity Increased Controller Flexibility Improved Operating Efficiency Impact to Production, Airplane System Development, and Airplane Maintenance: Minimal impact to production Few modifications are required to in-service airplane Minimal impact to existing airplane maintenance August 6, 2002 CAR/SAM RVSM Implementation Seminar 2
3 Boeing s Perspective on RVSM (con t) No new airplane system installation is required Two or more independent digital air data systems that use crosscoupled static sources Two altitude reporting transponders One altitude alert system Dual or Triple channel autopilot with altitude hold capability Height monitoring results validate airframe design and airplane systems performance. August 6, 2002 CAR/SAM RVSM Implementation Seminar 3
4 Current Production Airplanes Airframe Manufacturer s Perspective Approved Airframes Model Service Bulletin Service Letter Skin Check Pitot Static Probe Life Air Data Computer Operational Change N/A None N/A /-700/ 800/900/BBJ N/A 737-SL C N/A N/A Probes SL B Detailed Measurements Unplated - 3 yrs Plated - No Limit Mach 0.90 in RVSM Airspace Probes SL B Visual Plated - No Limit Mach 0.90 in RVSM Airspace August 6, 2002 CAR/SAM RVSM Implementation Seminar 4
5 Current Production Airplanes Airframe Manufacturer s Perspective Approved Airframes Model Service Bulletin Service Letter Skin Check Pitot Static Probe Life Air Data Computer SL D Visual N/A ADC Upgrade & New SSEC Operational Change N/A 757-SL D N/A N/A / SL C Visual Unplated - 3 yrs Plated - No Limit N/A N/A Plated - No Limit -206 and SSEC required for all Models / SL B Visual N/A August 6, 2002 CAR/SAM RVSM Implementation Seminar 5
6 Current Production Airplanes Airframe Manufacturer s Perspective Approved Airframes Model Service Bulletin Service Letter Skin Check Pitot Static Probe Life Air Data Computer Operational Change MD-81, -82, -83, -87, - 88 MD-90-10, -30, -40 MD N/A Detailed Measurements (Static Plate) MD N/A Detailed Measurements (Static Plate) N/A N/A MD-11 Combi, Freighter, Passenger MD N/A Detailed Measurements N/A August 6, 2002 CAR/SAM RVSM Implementation Seminar 6
7 Approved Airframes Out-of-Production Airplanes Model Service Bulletin Service Letter Skin Check Pitot Static Probe Life Air Data Computer Operational Change / SL Visual N/A New DADC and SSEC SL Visual No limit May require new DADCs /- 400/ SL A Visual No Limit /- 200/-300/SP SL B Detailed Measurements DC-10 DC N/A Detail Measurements (static Plate) Unplated - 4 yrs Plated - No Limit Specific SSEC required Mach 0.90 or weight in RVSM airspace N/A August 6, 2002 CAR/SAM RVSM Implementation Seminar 7
8 Out-of-Production Airplanes Model Airframe Manufacturer s Perspective Non-Group Airframes 707 No Group/Non-Group RVSM Qualification Package Development planned by Boeing. We recommend that operators contact AeroMech Inc for non-group data package development. AeroMech has advised that they have developed a non-group data package for three different operators that has been approved by the necessary regulatory agency No Group/Non-Group RVSM Qualification Package Development planned by Boeing DC-9 DC-8 No group approval is planned and no service bulletins are released. Preliminary equipment analysis indicates that some equipment requires upgrades (ADC, altimeters, altitude alerters, ATC transponders). Aircraft will require detailed measurements of both static plates and flush mounted static ports depending on static plate production cut-in. No group approval is planned. Service Bulletin DC (11/96) is a static port skin waviness inspection bulletin only. Equipment analysis indicates that some equipment required upgrades (ADC, altimeters, altitude alerters, ATC transponders). All static ports are flush mounted. August 6, 2002 CAR/SAM RVSM Implementation Seminar 8
9 Accuracy, Degradation and Maintenance Model Altitude Range Air Data System Accuracy Altimeter Splits (Capt s vs F/O s) 757 / 767 Sea level +/- 15 FT +/- 25 FT 0-10,000 FT +/- 20 FT +/- 60 FT 10,000 TO 30,000 FT +/- 40 FT +/- 135 FT 30,000-50,000 FT +/- 80 FT +/- 160 FT August 6, 2002 CAR/SAM RVSM Implementation Seminar 9
10 Accuracy, Degradation and Maintenance Altimetry system components degradation Scheduled maintenance Cross panel checks (FRM) Event Driven Maintenance Damage/Repairs Assess damage Measure skin waviness Perform repairs (shimming/flush) August 6, 2002 CAR/SAM RVSM Implementation Seminar 10
11 Future Airframe and Airplane System Development All current production airplanes are delivered RVSM qualified. All current airplane systems are adequate for RVSM. Any new airplane systems and new airframe type will be RVSM compliant. August 6, 2002 CAR/SAM RVSM Implementation Seminar 11
12 Future Airframe and Airplane System Development (con t) Boeing has developed an Integrated Standby Flight Display (ISFD) for 737NG/757/767 and model airplanes (and subsequently for 777). The ISFD has the potential to meet RVSM altimetry system accuracy requirements (ISFD is SSEC capable). Currently, Boeing has no plans to apply ISFD for RVSM. Boeing would like to solicit operator feedback/interest on using the ISFD for RVSM operations. August 6, 2002 CAR/SAM RVSM Implementation Seminar 12
13 Related Issues Skin waviness Measuring skin waviness Tool not calibrated properly Tool not situated properly Stencils and markings in the RVSM critical area August 6, 2002 CAR/SAM RVSM Implementation Seminar 13
14 Shimming repair Fabricate shims according to Boeing shim package Identify shim locations Remove fasteners within 10 inches from shim locations Install shims (flat side out) using temporary fasteners Measure skin waviness to verify improvements to waviness Install permanent fasteners Measure skin waviness for final qualification Related Issues (con t) August 6, 2002 CAR/SAM RVSM Implementation Seminar 14
15 Nuisance TCAS alerts Related Issues (con t) Change 7 TCAS service bulletins are available TCAS Advisory Traffic Advisory FL200-FL300 FL300-FL420 Corrective RA FL200-FL300 FL300-FL420 Preventive RA FL200-FL300 FL300-FL420 Altitude Threshold 6.04A 850 Feet 1200 Feet 600 Feet 700 Feet 700 Feet 800 Feet Altitude Threshold Feet 850 Feet 600 Feet 600 Feet 700 Feet 700 Feet August 6, 2002 CAR/SAM RVSM Implementation Seminar 15
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