Appendix 7 WP01 VYPOЗ X KHUT VVP04 VVPO5 WУРО6 VYPOS WP09 Figure 6. Bravo Departure Runway Transition Data - Southwest1 DEP mangoo Waypoint Data W098 07 51.90 No FAA checks included.
Database Effective Dates SW DEPARTURE Page 3 of 4 Created : Thu Dec 15 13:22:48 EST 2011 TARGETS 4.8 Beta 12/15/2011 (r23657) A single arrival was designed which is similar to a previously studied design at Fargo, ND. As A7-5
KHUT ~ WP528 ~, WP529 WP522 ' WP527 WP524 WP306 4/7/16 AC 20-138D Change 2 Appendix 7 the aircraft descends and decelerates, it follows a path consisting of a series of RF legs with a turn direction reversal after the first. The second directional turn consists of two back-to-back RF legs with decreasing radii. The arrival is shown in Figure 7 and waypoint information is shown in Table 16.
Figure 7. Arrival A7-6
Runway Trans ition Data - South RNAV STAR OB Waypoint Distance leg FOIFB Latitude l ongitude TC MC Altitude Speed MEA Arc Center l at Arc Cent er Lon Arc Radius fD" M' S.ss'"l to• M' S.ss"l fNMl WPSUWP IF N37 40 27.46 W097 53 15.62 WP522WP 5.40 TF F B N37 45 46.5 1 W097 52 03.10 10.23 4.23 WP313 WP 5.91 RF N37 49 46.57 W097 47 09.39 N37 44 52.99 Wff.J745 5 1.24 5.00 WP306 WP 5.19 RF N37 5305.5 1 W097 42 30. 1g N37 54 37.47 Wff.J7 48 27.02 4 .95 PFAF2 WP 3.86 RF N37 56 42.35 W097 43 28.16 N37 54 14.09 Wff.J7 4656 .16 3.69 WP321 WP 4.70 TF F B N38 00 12.2 1 W097 47 26.74 3 18.04 3 12.04 Waypoint Data OB Waypoint k c ~bU-S~~~ Latitude Lorcl'.~f• ro~~=~.;, ,b~."a~ ~l ,o~t~i~~., ,~!>rlr:se_l Center fDeal PFAF2WP 375642.35N-0974328.16W N37 .9450m WW.7244900 N37 56.706 W97 43.46" N37 56 42.35 W097 43 28.16 WP306WP 375305.5 IN-0974230.19W N 37 .8848637 WW.7083862 N37 53.092 \Y97 42.503 N37 53 05.5 1 W097 42 30.1g WP313WP 374946.57N-09747@.39W N 37 .8296033 WW.7859430 N37 49.776 \\19747.157 N37 49 46.57 W097 47 09.39 WP321WP 3800 12.2 1N-0974726.74W N38 .0033911 WW.7@7609 N3S 002 03 \\197 47.446 N38 00 12.2 1 W097 47 26.74 WP522WP 374546.5 1N-0975203.10W N37 .7629 185 WW.8675290 N37 45.775 \\197 52.052 N37 45 46.5 1 W097 5203.10 WPSU WP 374027A6N-0975315.62W N37 .6742'cl55 WW.8876734 N37 40.458 \\197 53.260 N37 40 27.46 W097 53 15.62 WP527WP y 374452.99N-0974551.24W N 37 .7480540 WW.7642320 N37 44.883 \\197 45.854 N37 44 52.@ W097 45 5 1.24 WP528WP y 375437.47N-0974827 .02W N37 .9 104000 WW.8075046 N37 54.625 \\197 48.450 N37 54 37.47 W097 48 27.02 WP529WP y 3754 14.09N-0974656.16W N 37.9039 145 W fJ7 .7822680 N37 54235 \\197 46.936 N37 54 14.@ W097 46 56.16 No FAA checks included.
No TERPS Surfaces included.
Database Effective Dates Database Date NFOC 10/2012011
JEPPES EN NIA
IFP OFFLINE NIA AVNIS 12/1512011 benefits NIA
NACO NIA 4/7/16 AC 20-138D Change 2 Appendix 7 Table 16. Arrival Waypoints A7-2.3. Approaches.
a. Four approaches are provided to assess avionics guidance capability through a series of RF leg approach designs. The first three templates are acceptable for both RNP AR and non- RNP AR demonstrations. The fourth template is applicable to RNP AR only. It is acceptable to label the test procedures RNAV (RNP) when demonstrating RNP AR capability. When demonstrating non-RNP AR capability it is acceptable to label the test procedures as RNAV (GPS).
b. As shown in Figure 8, Approach 1 is a teardrop procedure that incorporates a descending RF right turn to final, rolling out at the final approach fix. Note that there is no straight segment 2 NM prior to the final approach fix which will be stressing for RNAV (GPS) final approach guidance due to the reduced scaling transition from terminal mode to approach mode. This path requires the aircraft to descend, decelerate, and then configure for landing all during the RF leg. The missed approach also contains an RF leg en route to the missed approach hold. Waypoint information is shown in Table 17 and vertical error budget information is shown in Table 18.
A7-7
Appendix 7 PFAF7 DA 1775 WP559 KHUT VWP555 VVP557 WP561 WP563 WP562 WWP565 Figure 8. Approach 1 Leg Table 1 Glide Turn Segment Leg Start End Tum Type End ATC End End Art ObsJ Comp Descent Grad Climb Grad End Spd Radiu: comp RuP Tur Spr Intermediate IF WP555 WP555 FB 10129 10129.22 0.0 300.0 1.0 Intermediate TF WP555 WP557 FB 6235 6235.10 165.0 1.0 LEFT Final WP557 PEAFT FB 3172 6235.10 165.0 0.3 RIGHT Final TF PFAF KHUTERWIJ:AER FB 1580 1580.00 165.0 0.3 Missed DA 1775 WF561 FB 4337.40 265.0 1.0 RIGHT Missed RF WF562 FB 4873.04 265.0 1.0 RIGHT Missed TF WF562 WP565 FB 6881.69 265.0 1.0 Missed HM WF565 WF565 FB ฿890.33 265.0 1.0 RIGHT Leg Table 2 Segment Leg Start End Tum Length Leg Lengt Start Course End RF/Flyby „ RF/Flyby Tum Tailwind Type Type (FT) Magnetic Magnetic Change Radius Bank Angle Center Intermediate IF WP555 WP555 FB 0.00 0.00000 Intermediate TF WF:555 WP557 FB 15.50 94644.27202 264.04 263.84 Final RF WP:557 PEAF? FB 9,62 5842749136 263.86 131.96 228.10 2.4156 19.95 59.35 WP559 Final TF PEAF? KHUT:RW13:AER FB 5,00 30380.57743 131.96 132.00 0.00 nia 30.00 Missed TF DA 1775 WP567 FB 5.22 31746,48819 131.95 132.00 Missed WF:561 WP562 FB 6.30 38255.73029 132.00 226.20 94.20 3.8294 24.89 56.65 WP563 Missed TF WP562 WP565 4,02 24409.52927 226.16 226.12 Missed WP565 WP565 FB 4.02 24409.52927 226.16 A7-8
Appendix 7 Waypoint Data DB Waypoint Latitude (Deg) Longitude (Deg, Decimal Min) Latituck (Deg, Decimal Min _ongitud ngitı PEAFT WF N 38.1361836 W97.9417593 N38 8.171 W97 56.506 N38 08 10.26 W097 56 30.33 WP555 WF N 38.0691650 W 97.6507673 N38 4.150 W97.39.046 N38 04 08.99 W097 39 02.76 WP557 WF N 38.0688301 ₩ 97.9795143 N3B 4.133 W97 58.771 N38 04 07.97 W097 58 46.25 WP559 WF N 38.1091856 W 97.9796419 N3B 6.551 ₩97 58.779 N38 06 33.07 W097 58 46.71 WP561 WF N 38.0170377 W97.8059367 N3E 1.022 W97 48.356 N38 01 01.34 W097 48 21.37 WP562 WF N 37.9237951 ₩ 97.8164481 N37 55.428 W97 48.987 N37 55 25.66 W097 48 59.21 WF563 WF N 37.9742701 W 97.8659231 N37 58.456 W97 51.955 N37 58 27.37 W097 51 57.32 WP565 WF N 37.8826581 ₩ 97.8832395 N37 52.959 W97 52.994 N37 52 57.57 W097 52 59.66 PFAF
LAT LON LTP/FTF N38 04 27.15 W097 52 15.90 Runway True Bearing 138.00 FAF Altitude 6235.10 LTP/FTP Elevation 1525.00 TCH 55.00 Glidepath Angle 3.00 GPI 1049.46 88808.07 Feet FAF Distance From LTP/FTP
14.62 NM
LAT LON PFAF N38 04 07.97 W097 58 46.25 RNP Value 0.30 Max Glidepath Angle 3.50 LTP MSL Elevation 1525.00 PFAF Elevation 6235.10 Distance (ft) LTP to PFAF 88808.07 LTP Elevation 1525.0 MSL PFAF Altitude 6235.10 ACT 0.00 Glidepath Angle 3.00 TCH 55.00 Min Glidepath Angle 3.10 Delta ISA (dISA) 0.00 NA Below 11.95 (C) 53.51 F Semispan 131.00 NA Above 46.85 (C) 116.32 (F] Dist (ft) LTP to OCS ORIGIN 3324.7฿ ocs Slope (run: rise) 19.15:1 VEB ROC (a PFAF 72.14 Error Components (Enter Bank Angle, WPR, FTE. and ATIS values below) ta: 250 ft @ PFAF ISAD (dh x dISA|/288 + dISA - 0.5 x .00198 x [dh+h]) 0.00 0.00 BG 40.48 Semispan x sin (Bank Angle) 40.49 40.48 ANPE 1.225 x mp x tan(a) 117.03 117.03 VAE D x (tan(a) - tan(a - 01)) D=250/tan(a) D.83 15.73 WPR 60.00 [WPR x tan(a) 3.14 3.14 FTE 75.00 75.00 ASE -8.8 x 10^-8 x (h + D x tan(a))^2 + 6.5 × 10^-3 x (h + D x tan(a)] + 50 61.26 87.11 ATIS 20.00 20.00 20.00 Table 18. Approach 1 Vertical Error Budget C. Approach 2, as shown in Figure 9, is also a descending right turn to final but has a series of four RF legs with differing radii. Similar to Approach 1 in Figure 8, this path will require the aircraft to descend and decelerate during the RF leg. Waypoint information is shown in Table 19 and vertical error budget information is included in Table 20.
A7-9
Appendix 7 WP371 WP360 OZEdM PFAF5 Z9EdM —WP366 KHUT WP369 WP365 WP373 Figure 9. Approach 2 Leg Table 1 Glide Min Tum Turn Segment Type Leg Start End Jum Type Pati End ATC End End An Obs.J Radius Comp Descent Grad Climb Grad End Spd Radius Comp RHP Alt Alt Spd Intermediate IF WP371 WF 371 FB 12677 12676.98 300.0 1.0 Intermediate TE WP371 WF 369 FB 10009 10009.28 300.0 1.0 RIGHT Intermediate WP369 WF 365 FB 6044 10009.28 300.0 1.0 RIGHT Intermediate RF WPJ65 WF363 FB 6499 8043.55 250.0 1.0 RIGHT Intermediate RE WP363 WF361 FB 5486 6499.25 250.0 1.0 _ RIGHT Intermediate RE WP367 WF360 FBL 3672 54฿6.00 250.0 1.0 RIGHT Intermediate TF WPJ60 PEAFS FB 3172 3172.36 165.0 1.0 RIGHT Final TF PFAF5 KHUT:RW13:AER FB 1580 1580.00 165.0 0.3 Missed TE DA 1775 WF 373 FB 5312.04 265.0 1.0 Missed HM WP37] WF.373 FB 3725.00 265.0 1.0 RIGHT Leg Table 2 Segment Type Start End Tum Type Len (NI) Leath Len (FT Course Magnetic Magnetic Start Course End Course Change REFlyby Radius RE/Flyby Tum Angle Tailwind Center Intermediate IF WP.371 WP371 FB 0,00 0.00000 Intermediate TF WP 371 WF369 FB 10.67 64836:91202 223.80 223.70 Intermediate WP369 WP365 FB 7.86 47776.01926 223.70 283.59 59.89 7.5100 19.36 66.82 WP370 Intermediate RF WP 365 WF363 FB 6.18 37533,45966 283.59 353.36 69.76 5.0700 19.68 62.93 WP366 Intermediate RF WP363 WF361 FB 4.05 24626.59378 353.36 42.16 48.81 4.7600 19.79 59.87 WP364 Intermediate RF WP 361 WP360 FB 7,25 44079.45700 42.16 132.22 90.05 4,6200 19.55 57.86 WP362 Intermediate TF WP 360 PFAFS FB 2.00 12152,23097 132.22 132.23 0.02 nia 30,00 Final TF PFAF5 KHUT: RW1J:AER FB 5.00 30380.57743 132.23 132.28 1.16 nia 30.00 Missed TF DA 1775 WP373 FB 7.17 43590,52964 131.07 131.14 Missed WP 373 WP373 FB 4.00 24304.46194 131.07 A7-10
Appendix 7 Waypoint Data DB Waypoint Latitude (Deg) Longitude (Deg. Decimal Min) Deg, Decimal Min Longitud D°M S.SS S.ss" PFAF5 WF N 38.1364523 W 97.9413803 N38 8.187 ₩97 56.483 N38 08 11.23 W097 56 28.97 WP360 WP N 3B.1613379 W 97.9695326 N38 9.680 W97 58.172 N38 09 40,82 W097 58 10.32 WP361 WF N 38.1673998 W 93.1073560 N38 10.044 W98 6.441 N38 10 02.64 W098 06 26.48 WF362 WF N 38.1099519 W 98.0422797 N3B 6.597 W98 2.537 N38 06 35.83 W098 02 32.21 WP363 WP N 38.1073598 W 98.1408183 N38 6.442 W98 8.449 N38 06 26.50 W098 08 26.95 WF364 WF N 38.1082105 W 98.0403093 N38 6.493 W98 2.419 N38 06 29.56 W09B 02 25.11 WF365 WF N 38.0285723 ₩ 98.0696613 N3B 1.714 ₩98 4.180 N38 01 42.86 W098 04 10.78 WP366 WF N 38.1082629 ₩ 98.0337635 N3B 6.496 W98 2.026 N38 06 29.75 W098 02 01.55 WF369 WF N 38.0510922 W 97.9138308 N38 3.066 ₩97 54,830 N38 03 03.93 W097 54 49.79 WP370 WF N 38.1466107 W 98.0164594 N38 8.797 W98 0.988 N38 08 47.80 W098 00 59.25 WF371 WP N 38.1661249 W 97.7418454 N38 9.967 W97 44.511 N38 09 58.05 W097 44 30.64 WP373 WP N 37.9941400 W 97.7766721 N37 59.648 W97 46.600 N37 59 38.90 W097 46 36.02 PFAF
LAT LON LTP/FTP N38 04 27.15 W097 52 15.90 Runway True Bearing 138.00 FAF Altitude 3172.36 LTP/FTP Elevation 1525.00 TCH 55.00 Glidepath Angle 3.00 GPI 1049.46 30380.58 Feet FAF Distance From LTP/FTP
5.00 NM
LAT LON PFAF N38 08 11.23 W097 56 28.97 Table 19. Approach 2 Waypoints RNP Value 0.30 Max Glidepath Angle 3.50 LTP MSL Elevation 1525.00 PFAF Elevation 3172.36 Distance (ft) LTP to PFAF 30380.58 LTP Elevation 1525.0 MSL PFAF Altitude 3172.36 ACT 0.00 Glidepath Angle 3.00 TCH 55.00 Min Glidepath Angle 3.10 Delta ISA (dISA) 0.00 NA Below 11.95 (C) 53.51 (F Semispan 131.00 NA Above 45.68 (C) 114.23 (F) Dist (ft) LTF to OCS ORIGIN 3324.90 OCS Slope (run:rise) 19.15:1 VEB ROC (a) PFAF 216.86 Error Components (Enter Bank Angle, WPR, FTE. and ATIS values below) (a) 250 ft @ PFAF ISAD (dh x diSA/288 + dISA - 0.5 x .00198 x [dh+h]) 0.00 0.00 BG 25.00 semispan x sin (Bank Angle) 25.00 25.00 ANPE 1.225 x rp x tan(a) 117.03 117.03 YAE D x (tan(a) - tan(a - 01)) D=250/tan(a) 0.83 5.50 WPR WPR x tan(a) 3.14 3.14 FTE 75.00 75.00 75.00 ASE •8.8 x 10^-8 x (h + D x tan(a))^2 + 6.5 x 10^-3 x (h + D x tan(a)] + 50 61.26 69.73 ATIS 20.00 20.00 20.00 Table 20. Approach 2 Vertical Error Budget
d. Approach 3 is shown in Figure 10. This procedure uses an RF leg early in the procedure followed by a briet straight segment, then two back-to-back RF legs with a turn direction reversal. The second RF leg terminates at the final approach fix. As on the other approaches, the aircraft will be required to descend, decelerate and configure for landing during the series of RF legs. The missed approach also includes an RF leg to the missed approach A7-11
Appendix 7 hold. Waypoint information is shown in Table 21 and vertical error budget information is included in Table 22.
WP571 ...
_KHUT *P742 PFAF4 WP572 WP531 WP741 WP325 WP532 WP533 WP534 WP536 WP535 WP537 Figure 10. Approach 3 Leg Table 1 Glide Kadies DeScent Turn Segment Type Leg Start End Type Path ATC End End Aft Comp Climb Grad End Spd Radius Comp RHP Alt Spo Intermediate IF WP537 WP537 FB 10584 10583.57 0.0 300.0 1.0 Intermediate TF WP537 WP535 FB 8641 B641.47 250.0 1.0 _RIGHT Intermediate RF WP535 WP534 _ FB 7193 B641.47 250.0 1.0 _RIGHT Intermediate TF WP534 WP532 FB 6193 6192.56 250.0 1.0 RIGHT Intermediate RE WP532 WF 325 FB 4937 6192.56 250.0 1.0 RIGHT Intermediate RF WP325 PFAF4 FB 3162 4936.79 250.0 1.0 LEFT Final TF PFAF4 KHUT:RW3T:AER FB 1570 1570.00 165.0 0.3 Missed TF DA 1765 WP571 FB 2615.00 265.0 0.5 LEFT Missed RF WP571 WP572 FB ฿536.36 265.0 1.0 LEFT Missed TF WP572 WF741 FB 10854.65 265.0 1.0 LEFT Missed HM WP741 WF741 FB 13172.95 265.0 1.0 RIGHT Leg Table 2 Segment Type Start End Type Leg eneg Leg Magnetic Magnetic Course Start Course End Change Course RF/Flyby Radus RE/Flyb BanI Tailwind RF Leg Center _Arc Angle Intermediate WP537 WP537 FB 0.00 0.00000 Intermediate TF WP537 WP535 FD 7.77 47201.70006 278.82 278.72 Intermediate RF WP535 WP534 FB 5.80 35214,94480 278.72 342.26 63.54 5.2220 19.55 64.11 WP536 Intermediate TF WP534 WP532 FB 4.00 24304.46194 342.26 342.25 Intermediate RE WP532 WP.325 FB 5.02 30520.94148 342.25 42,26 60.00 4.7980 19.44 59.26 WP530 Intermediate WF 325 PFAF4 FB 7.10 43126.52487 42.26 312.31 ฿9.95 4.5209 19.67 56.77 WP531 Final TF PFAF4 KHUT:RWJ1:AER FB 5.00 30380.57743 312.31 312.27 0.00 nia 30.00 Missed TF DA 1765 WP571 FB 1.80 10937.00787 312.31 312.29 Missed RF WP571 WP572 FB 13.64 82894.71614 312.29 133.02 179.27 4.3623 24.99 63.90 WP742 Missed TF WP572 WP741 FD 4,64 28172.46233 133.02 133.06 Missed WP741 WP741 FB 4.64 28172.46233 133.02 A7-12
Appendix 7 Waypoint Data DB Waypoint Latitude (Deg] Longitude (Deg, Decimal Min) (Deg, Decimal Man) PFAF4 WF N 37.9975785 W 97.7847137 N37 59.855 W97 47.083 N37 59 51.28 W097 47 04.97 WP325 WF N 37.8911180 ₩ 97.7924249 N37 53.467 W97 47.545 N37 53 28.02 W097 47 32.73 WP531 WF N 37.9473859 W 97.8556480 N37 56.843 W97 51.351 N37 56 50.59 W097 51 21.05 WP532 WP N 37.8151083 W 97.8240457 N37 48.906 ₩97 49.443 N37 48 54.39 W097 49 26.56 WP533 WP N 37.8313647 W 97.7252214 N37 49.882 W97 43.513 N37 49 52.91 W097 43 30.80 WP534 WP N 37.7497614 W 97.8069336 N37 44.986 W97 48.416 N37 44 59.14 W097 48 24.96 WP535 WF N 37.6831652 W 97.7273613 N37 40.990 W97 43.642 N37 40 59.39 W097 43 38.50 WP536 WP N 37.7674351 ₩ 97.6994648 N37 46.046 W97 41.968 N37 46 02.77 W097 41 58.07 WP537 WP N 37.6501154 ₩ 97.5696646 N37 39.007 W97 34.181 N37 39 00.42 W097 34 10.86 WP57:1 WP N 38.0746550 W 97.8715595 N3B 4.479 W97 52.294 N38 04 28.76 W097 52 17.61 WP572 WP N 37.9784995 W 98.0097230 N37 58.710 W98 0.583 N37 58 42.60 W098 00 35.00 WP741 WF N 37.9200757 W 97.9456813 N37 55.205 ₩97 56.741 N37 55 12.27 W097 56 44.45 WP742 WP N 38.0262098 W97.9402549 N3B 1.573 W97 56.415 N38 01 34.36 W097 56 24.92 PEAF
LAT LON LTP/FTP N38 03 35.48 W097 51 17.61 Runway True Bearing 318.00 FAF Altitude 3162.36 LTP/FTP Elevation 1515.00 TCH 55.00 Glidepath Angle 3.00 GPI 1049.46 30380.58 Feet FAF Distance From LTP/FTP 5.00 NM
LAT LON PFAF N37 59 51.28 W097 47 04.97 Table 21. Approach 3 Waypoints RNP Value 0.30 Max Glidepath Angle 3.50 LTP MSL Elevation 1515.00 PFAF Elevation 3162.36 Distance (ft) LTP to PFAF 30380.58 LTP Elevation 1515.0 MSL PFAF Altitude 3162.36 ACT 0.00 Glidepath Angle 3.00 TCH 55.00 Min Glidepath Angle 3.10 Delta ISA (dISA) 0.00 NA Below 11.97 (C) 53.55 (F) Semispan 131.00 NA Above 45.70 (C) 114.27 (F) Dist (ft) LTP to OCS ORIGIN 3324.27 OCS Slope (run:rise) 19.15:1 VEB ROC (0) PFAF 216.83 Error Components (Enter Bank Angle, WPR, FTE. and ATIS values below) (a). 250 ft 1@ PFAF ISAD (dh x dISA)/288 + dISA - 0.5 x .00198 x [dh+ h]) 0.00 0.00 BG 25.00 semispan x sin (Bank Angle) 25.00 25.00 ANPE 1.225 x mp x tan(a) 117.03 117.03 YAE D x (tan(a) - tan(a - 01)) D=250/tan(a) 0.83 5.50 WPR 60.00 WPR x tan(a) 3.14 3.14 FTE 75.00 75.00 ASE •8.8 x 10^-8 x (h + D x tan(a)) ^2 + 6.5 × 10^-3 x (h + D x tan(a)) + 50 61.20 69.68 ATIS 20.00 20.00 20.00 Table 22. Approach 3 Vertical Error Budget
e. Approach 4 is shown in Figure 11. This procedure is intended for RNP AR operations only. The procedure is unique and incorporates an RF leg beginning at the missed approach point. This configuration will require the aircraft to begin the missed approach and track the RF leg while climbing and accelerating. The initial RF leg is followed consecutively A7-13
,,.----4 .. __ -· r ... _ ,,• WP761 • ••
• • • • • • • • • • : WP762~ . _,h"' :
~ WP773 WP771 : KHUT • • • WP767 '¥ • • • • • • • • • '\ '\ IZAGI
• • • • ~ ' ETISE WP770 4/7/16 AC 20-138D Change 2 Appendix 7 by two additional RF legs each with increasing radii. Waypoint information is shown in Table
23.
Note: At the AC publication date, approach 4 was only intended for future RNP AR operations. This does not impact previous recognition of RF leg capability.
Figure 11. Approach 4 A7-14
Path From IZAGI Leg Table 1/2 Leg Tum Min End Max End L~ ~ajll, start End Cour.;e Tum Segment Type start End Type RNP FlxAJt FlxAJt Cour.;e Cour.;e Change Dir INMII IFTI True True INTERM EDIATE IF IZAGI INFDCI IZAGI INFD CI FB 1.0 3400.00 0.0000 0.00000 INTERMEDIA TE TF IZAGI INFDCI ETISE INFD CI FB 1.0 7.0859 43054.72936 42.3 130 42.3748 0.0008 RIGHT FINAL TF ETISE fNFl1Cl WU DNU fNF DCI FB 0.3 3.4141 20744.4 1667 42.3756 42.4055 0.0032 FINAL TF WUDNU INFD CI K HUT:RW04:AER FB 0.3 1.7000 10329.45409 42.4022 42.4172 MISSED APPROACH RF KHUT:RW04AER WP762 FB 1.0 4.5803 27830.28432 42.4 186 350.3648 52.0539 LEFT MISSED_APPROACH RF WP762 WP761 FB 1.0 8.3775 50902.8 1282 350.364 278.4359 71.9289 LEFT 8 MISSED_APPROAC H RF WP761 WP767 FB 1.0 15.6858 95308.95821 278.435 143.8 122 134.6236 LEFT 9 MISSED_APPROACH TF WP767 WP770 FB 1.0 12.0000 729 13.38583 143.812 143.9038 0 Path From IZAGI Leg Table 2/2 Leg Tum EndFlx RF Leg Flyby Tum Talt.r.rlnd :cir,'\, Reduced Segment start End Speed Bank Angle ~ Type Type Res1J1dlon Radius O\len1de OVerrlde ROC
INTERMEDIATE IF IZAGI INFD CI IZAGI INFDCI FB INTERMEDIATE TF IZAGI INFD Cl ETISE INFnrl FB FINAL TF ETISE (NFDC] WUDNU (NFDC] FB FINAL TF WUDNU rNFDCl KHUT:RW04AER FB MISSED APPROACH RF KHUT:RW04:AER WP762 FB 5.0400 WP771 MISS ED APPROACH RF WP762 WP76 1 FB 6.6800 WP772 MISSED APPROACH RF WP761 WP767 FB 6.6800 WP773 MISSED APPROACH TF WP767 WP770 FB Waypoint Data DB waypoint Latitude L=e Lalltude 1n.n~"=Mlnl Lalltwe (~~~~, (f)pn\ 1n.n, Decimal Mini (D" M'S .ss'1 NFDC ETISE N37.99630 W97.93545 N37 59.77783 W97 56.127 17 N37 59 46.67000 W097 56 7.63000 NFDC IZAGI N37.9089 1 W98.00603 N37 54.53467 W982.16167 N37 54 32.08000 W098 02 9.70000 WP761 WP N 38.22 164 W97 .95474 N38 13.29863 W97 57.284 19 N38 13 17.9179 1 W097 57 17.05128 WP762WP N 38. 13013 W97.83636 N38 7.80785 W97 50.18133 N38 07 48.47124 W097 50 10.87986 WP767WP N 38.04564 W98.08928 N38 2.73849 W9B 5.35700 N38 02 44.30923 W098 05 21.41989 WP770WP N 37.88395 W97.94012 N37 53.03696 W97 56.40730 N37 53 2 .21756 W097 56 24.43804 WP771WP N 38. 11601 W97 .94129 N38 6.96055 W97 56.47760 N38 06 57.633 11 W097 56 28.65604 WP772WP N 38. 11139 W97.97543 N38 6.68363 W97 58.52586 N38 06 41.01778 W097 58 31.55178 WP773WP N 38. 11139 W97.97543 N38 6.68362 W97 58.52587 N38 06 41.01708 W097 58 31 .55191 NFDC WUDNU N 38.03837 W97 .88691 N38 2.30217 W97 53.2 1450 N38 02 18.13000 W097 53 12.87000 PFAF
LAT LON LTP/FTP N38 03 33.52 W097 51 45.78 Runwav True Bearina 42.43 FAF Altitude 3200.00 L TP/FTP Elevation 1516.30 TCH 55.00 Glldepath Anale 3.00 GPI 1049.46 FAF Distance From L TP/FTP 31073.87 Feet 5.11 NM
LAT LON PFAF N37 5946.67 W097 56 07.63 4/7/16 AC 20-138D Change 2 Appendix 7 Table 23. Approach 4 Waypoints A7-3. Test Guide.
a. Paragraph A7-3 provides guidance that may be used to conduct development and/or airworthiness RF leg testing for new equipment hardware/software, or updates to existing equipment hardware/software. The guidance is designed to be used in collaboration with the templates described in paragraph A7-2 to create “FOR TEST ONLY” terminal area instrument procedures (departures, arrivals and approaches). The intent of this regimen is to provide a set A7-15
Appendix 7 of rigorous instrument procedures that the applicant can use to demonstrate meeting the RF leg airworthiness approval criteria.
b. The test instrument procedures are designed and located at an airport with an elevation of approximately 1500 ft MSL. The waypoint and navigation leg data is provided so that the procedures can be “translated” to another location suitable to the applicant. However, the new airport elevation should be within the range of 1000 - 2000 ft MSL to ensure that the designed turn radii and bank angles do not change significantly (see paragraph A7-1.e). The applicant will be required to obtain a navigation database for their respective navigation system that contains the test procedures.
c. The information in the following paragraphs describes test conditions such as generic aircraft performance parameters, desired atmospheric conditions, and considerations to assist the applicant with creating a detailed test plan. Applicants are encouraged to use these recommended guidelines. However, amendments may be made as required to accommodate unique equipment designs, test environment, testing methods or other considerations.
A7-3.1. Initial Set-Up.
a. Configure the aircraft for individual trials using two gross weight conditions:
(1) Nominal heavy weight resulting in lower accelerations to climb speed and higher speeds on approach.
(2) Nominal light weight resulting in higher accelerations to climb speed and lower speeds on approach.
b. Verify that a navigation database with the FAA “FOR TEST ONLY” terminal procedures is loaded in the FMS.
c. Verify desired data parameters will be recorded (if data recording capability is available).
Note: In addition to the desired data parameters, the lateral path definition (desired path) and lateral path “cross-track error” (distance from path centerline) should be included in the recorded data parameters to monitor/review path maintenance performance.
d. Configure the simulation (if practical) for trials using two atmospheric conditions:
(1) Standard day, standard lapse rate.
(2) 35o C outside air temperature, with standard lapse rate.
e. If practical, simulated wind direction should be set to a tailwind for each turn entry.
The wind velocity for the respective altitude should approximate those values shown below.
A7-16