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5-1 CHAPTER 5. INM/AEDT COMMERCIAL TURBOFAN (JET) FLEET For each commercial aircraft in the INM database a decision must be made as to which method I, II or III will be used for the development of the taxi NPD. Table 5-1 lists which NPD Method is to be applied. In some cases, especially for common engine types, aircraft are grouped together. TABLE 5-1 (part 1 of 2) Chosen Taxi NPD Development Method for INM/AEDT Aircraft Madrid Measured NPD Data Data Method 707 Boeing 707-120/JT3C 4 N 707120 Boeing 707-120B/JT3D-3 4 N 707320 Boeing 707-320B/JT3D-7 4 N 707QN Boeing 707-320B/JT3D-7QN 4 N 717200 Boeing 717-200/BR 715 2 N X X II 737300 Boeing 737-300/CFM56-3B-1 2 N 7373B2 Boeing 737-300/CFM56-3B-2 2 N 737400 Boeing 737-400/CFM56-3C-1 2 N 737500 Boeing 737-500/CFM56-3C-1 2 N 737700 Boeing 737-700/CFM56-7B24 2 N X 737800 Boeing 737-800/CFM56-7B26 2 N X X 737N17 B737-200/JT8D-17 Nordam Hushkit 2 N 737N9 B737/JT8D-9 Nordam Hushkit 2 N 757300 Boeing 757-300/RB211-535E4B 2 N II 757PW Boeing 757-200/PW2037 2 N II 757RR Boeing 757-200/RB211-535E4 2 N II A310-304 Airbus A310-304/CF6-80C2A2 2 N X III A319-131 Airbus A319-131/V2522-A5 2 N X X II A320-232 Airbus A320-232/V2527-A5 2 N A320-211 Airbus A320-211/CFM56-5A1 2 N A321-232 Airbus A321-232/IAE V2530-A5 2 N X III DC93LW DC9-30/JT8D-9 Hushkit 2 N III DC95HW DC9-50/JT8D17 Hushkit 2 N III EMB145 Embraer 145 ER/Allison AE3007 2 N X EMB14L Embraer 145 LR / Allison AE3007A1 2 N F10062 F100/TAY 620-15 2 N F10065 F100/TAY 650-15 2 N MD81 MD-81/JT8D-217 2 N X II MD82 MD-82/JT8D-217A 2 N X II MD83 MD-83/JT8D-219 2 N X X II MD9025 MD-90/V2525-D5 2 N MD9028 MD-90/V2528-D5 2 N X X III III II I III II X I III X X X ACFT_ID ACFT_DESCR ENG BODY ANOPP Data X
5-2 TABLE 5-1 (part 2 of 2) Chosen Taxi NPD Development Method for INM/AEDT Aircraft Madrid Measured NPD Data Data Method 767CF6 Boeing 767-200/CF6-80A 2 W III 767JT9 Boeing 767-200/JT9D-7R4D 2 W III 767300 Boeing 767-300/PW4060 2 W X I 767400 Boeing 767-400ER/CF6-80C2B(F) 2 W III 777200 Boeing 777-200ER/GE90-90B 2 W X X I 777300 Boeing 777-300/TRENT892 2 W III Boeing 777/PW 2 W X X I A300-622R Airbus A300-622R/PW4158 2 W III A300B4-203 Airbus A300B4-200/CF6-50C2 2 W A330-301 Airbus A330-301/CF6-80 E1A2 2 W A330-343 Airbus A330-343/RR TRENT 772B 2 W III 74710Q Boeing 747-100/JT9D-7QN 4 W 747200 Boeing 747-200/JT9D-7 4 W 74720A Boeing 747-200/JT9D-7A 4 W 74720B Boeing 747-200/JT9D-7Q 4 W 747400 Boeing 747-400/PW4056 4 W X X X I 747SP Boeing 747SP/JT9D-7 4 W III A340-211 Airbus A340-211/CFM56-5C2 4 W X III 727EM1 FEDX 727-100/JT8D-7 3 N 727EM2 FEDX 727-200/JT8D-15 3 N 727QF UPS 727100 22C 25C 3 N III BAE146 BAE146-200/ALF502R-5 4 N BAE300 BAE146-300/ALF502R-5 4 N DC870 DC8-70/CFM56-2C-5 4 N III DC1010 DC10-10/CF6-6D 3 W DC1030 DC10-30/CF6-50C2 3 W DC1040 DC10-40/JT9D-20 3 W III L1011 L1011/RB211-22B 3 W L10115 L1011-500/RB211-224B 3 W MD11GE MD-11/CF6-80C2D1F 3 W III MD11PW MD-11/PW 4460 3 W III III III III III III III XX ACFT_ID ACFT_DESCR ENG BODY ANOPP Data
