Measured or Estimated Noise Levels from Uncertificated Airplanes

JTI0-7'7Al78 14 0 ". z 100.0 I ID. I 5140 I BOEING B-721-200 112. 5 3 JTID-7 t4 . 0 102.2 100.4 111. 0 15/40 BOEING B-127-200 172 . S I 3 JT1D-7 / 7Al?B 14.0 102.2 100.4 l't I. 0 IS/40 BOEING B-127-UD 1 72. 5 J JTIID-f 14 . S 101 .2 100.4 I 10,. !I I· 1S 140 I 1 BOEINC 8-737-100 110£\NG B-737-100 103. 5 10, . 0 2 JT1D-7l7A/78 2 JT1D-7 / 1Al'18 14.0 14. 0 '3.0 '4.' IO I . 6 10 I . 3 101.3 101.3 I ,;. I/ 40 I 1140 l'J 'f\) (X) "CJ', BOEING 8-737-100 I 110 . 7 I 2 JTIO-flfA 14.5 93 . 7 100., I ti I. 5 t l/4D t I APPtNDU I Al RC RAFT MANUFACTURER AND TYPE "EASUIIED OR ~TIMATED NOISE LEVELS FROM UNCERTIFICATED AIRPLANES TURBOJET POWERED AIRCRAFT ENCINEI TAJCIOFF SIDELINE APPROACH 1--------------------------1---------1----------1----------1CR. WCT. I ND. I THRUST I MIIST HIIST. I HIEST. I FLAPS 1000 LIS.I HODEL 1000 LBS. I EPHDB EPNDB EPND8 ICTOIAPP)I NOTES I\) 'I\) 0) 'CJ"\ BOE INC 8-737-ZOO 100.S I I I JT1D-7l7A/7B 14.0 '2.1 101 .7 I 101.3 1140 I I IOEINC 8-737-100 BOt:ING 8-737-ZOO l OS. S 103. S I JT1D-7l7Al78 2 JTID-tl U 14.0 l4.S '3.Q ,i . 4 IO I . 6 lDO. t I 101.S l 11. s I t I 4 0 1140 I I l BOEINC 8-737-ZOD . BOEING 8-737-IOO BOEING 1-737-200 t Dt. 0 l to . ., 114.S 2 JT1D-7l7Al7I z JTID-,rn I JT10-,ru 14.0 14. S 14. S , •. 7 93 . ., u ., IO l . I l00.6 100.S IOI . S 11 l.' tt I . I I 1140 1140 •.• 1140 t BOEINC 1-73 7-2001 ADV. CATES LEARJET 23 115.S t2. s 2 JTID-UftSA z CJ-610-t l5. s 2., ,. ." 96. I IO 3 . I 103 . 4 111.? 96.7 1140 1 w GENERAL DYNA"ICS CV 180 21 CENERAL DYNAMICS CV 110 ZJH 114.0 193. 0 I I 4 CJ-toS-3 4 CJ-IOS-31 t l . 2 11 . 7 1t S . 0 111. a 10,.0 109 .o I 106.0 I 06. 0 1 I I 1 1 :C, ;l:> 'O 0 'O (I) w ::i0. °'I I-'• (\) X 0 ...... GENERAL CV 990.l DYNAHICS 253. 0 4 CJ-105-23 16.l 110 . 0 t ll. 0 11 Z. 0 t I AIRCRAFT MANUFACTURER AND TYPE I APPEND II I "EASURED OR ESTIMATED NOISE LEVELS FROM UNCERTIFICATED AIRPLANES TURBOJET POVERED AIRCRAFT I ENCINES I TAltEOFF I SIDELINE 1 APPROACH I 1--------------------------1---------1----------1----------1CR. VCT. I NO. THRUST KIEST HIEST. I M/EST. I FLAPS 1000 LB8. I "ODEL 1000 LBS. I EPNDB 'EPNDB EPNDB l<TOIAPPJI I I I NOTES :r, !D "CJ n 'O (1) w ::s 0\ 0. I f-'· [\) X 0 ....... LOCKHEED 1329 JET8TAII 41.0 4 JTtU-9 3.3 106. 6 103. 3 107.S MCDONNELL DC-01-20 DOUGLAS 276. 0 4 JTU-3 l5. I 105.0 107.0 I IZ. 0 I, z. s MCDONNELL DC-01-30 DOUGLAS us.o 4 JT4A-t U.I 10,. 0 107. 0 112. 0 l, 2, S MCDONNELL DC-01-40 DOUGLAS us.o 4 IICO. 11 17.!I I S1. 0 10,.0 ll !I. 0 t, 2, S MCDONNELL DC-01-!IO DOUCLAB HO.O 4 JTID-t t7. 0 106. 0 102.0 114. 0 t. z. !I MCDONNtLL DC-08-SO DOUGLAS 31!1.0 4 JT3D-U ll. 0 101. 0 103.0 114.0 I, I, S MCDONNELL DC-Ol-!IS DOUCLH I 31S.O I 4 JT3D-31 ti .0 tat.a 103.0 I 1 ts. a I, I, !I MCDONNELL DC-Ol-61 DOUCLAI ne.a 4 JTID-31 11. 0 110.0 l03. 0 11!1.0 1, Z, lJ MCDONNELL DC-01-62 MCDONNELL DC-01-U DOUCLAS DOUCLH us.a no.a 4 JT3D-3B 4 JT3D-H ti. 0 11.0 110. a l ts. 0 103.0 101. a lt 4. 0 114. 0 1,2,!I 1.2,S l'0 _, 'N (X) ' °' MCDONNELL DC-08-U DOUGLAS no.a 4 JTJD-7 u.o 111. 0 103.0 ll 4. 0 I •• I , 1 , !I APPINDII I AIRCIIAPT "ANUFACTUIIIII AND TYPI MCDONNELL DOUGLAI oc-oa-u NIA8Ult1D Oil HTl"ATID NOll!IE LEVELS FRO" UNCIRTIFICATED AIRPLANES TUIIIOJIT POWERED AIRCltAFT I INCIN£1 I TAKEOFr SIDILINI APPROACH 1--------------------------1---------1-------~--•----------1GIi. VCT. I NO. I THRUST I NIUT I MIEIT. I KIEST. I FLAPI l 000 LIS. I MODEL 1000 LIi. I EPNOI EPNOI EPNDB IITOIAPP)I I I • I I 1 I I I I I •no.o I JT3D-H II. 0 I 111. a in.a 114. 0 NOTH 1,1,S I\) 'I\) CX> ' °' HCDONHELL oc-01-,3 DOUGLAS US.I •JTID-7 19.0 t ts. 0 1u.o 114.0 1. 2, S NCDONNILt DC-at-lO DOUCI.AS ".1 I JTID-7 14. 0 tt.l lOO. f toS. S t.1,4,S,,,I MCDONNELL DC-09-ZO DOUGLAS ti. 0 I JTID-tl 1S. D "·I tOS. I 103. 7 I I t. z I I, s "CDONNELL DC-Of-30 DOUCLAI IOI. 0 I JTID-7 ". 0 U. I 100.S lOS.7 OISO MCDONNILL DC-Ot-30 DOUGLAS 105. 0 I JTID-7 u.o ,s .• 100.4 t OS. 7 I t,1,4,S,7,I MCDONNELL DC-Ot-30 DOUGLAS IOI. 0 2 JTID•lS ts. s ,s., 102. I 101.7 0/SO t,Z,4,S MCDONNELL DC-Ot-30 DOUGLAS 101.0 I JTID-7 14. D "·I IOD. I ID1. 7 I.,, 1,1 1 4,S,7,I \.J1 NCDONNELL DC-Ot-30 MCDONNELL DC-Of-30 DOUGLAS DOUCUl!I IOI. 0 110. 0 I JTID-f 2 JTID-tS 14. S lS.S ". 4 "·· t O1 . 4 IOZ. I 103.f 103.7 a,u 1,1,4,S,7 I, I, 4, S ):> ):> 'O () 'O (1) w ::s (]\ Q. I f-'• I\.) >< () MCDONNELL DC-0,-30 DOUCLAl!I tl O. D I z JTID-t 14.S ". 2 tot .• 11•. 0 I, 2, 4, S, 7 :x> :x> (J\ "EAIURED OR EITinATED APPENDIX I NOii£ LEVELS FRO" UNCERTIFICATED AIRPLANES 'O 'O (I) ::s 0 w 0\ 0. I TURIOJET POWERED AIRCRAFT I-'• I\) X O AlllCIIAFT ,__________________________ ,_________ ,__________ ,__________ , ENGINES 'I TAKEOFF I SIDELINE I APPROACH NANUFACTUIICR AND TYPI GR. VGT, I NO . I THRUST I NIEST I KfEST. I NIEST. ·1 FLAPI NOTH 1000 LIi.i N0D£t I 1000 LIS. I EPNDI I EPNDI EPNOI IITOIAPPJI ----------- -----'--------'-----'-----'----- -----'----'------' I I MCDONNELL DOUGLII I I I I DC-U-H 114 . 1 JTID-t 14.S 101.0 101.1 I 104.I I 1,1,4,S,7 NCDONN!LL DOUGLAS I DC-0,-tD 114. I JTID-11 IS. I IOI . I 111.D I D4. I 1,1,4,S ROCICVILL I IHIII 40A I U .6 I JTUA-1 1.1 110. S I 00 . I I U.S I NOTES t. THRUST CUTBACK USED 2. NOISE LEVCLS on NOT INCLUDE APPLICATION OF FAR PART 36 AMENDl1ENTS 8 OR 9 S. ZEAO PF.RCENT OVERSPECO ~. SJX PERCENT OUERSPEF.D s . NO Ar.ousTIC ENGINE NAr.ELLE TREATMENT 6. ALSO APPLlr.ABLE TO -1~/-1S/-1~ AIRCRAFT 7. Al.SO APPl .• !CADLE TO -at /-92/ -· 82F AIACRArT 8 . Al.50 APPLlf:ABLE TO -7A ENGINES Stage 2 Noise Certification Limits: Jet and Transport Aircraft Takeoff, Sideline and Approach ...I z0.. w 102 ~+4+~~1---Sideline, Approectt 100H-+~f-+H+H-++++#H-H++t~ttH++mm+,~~,~~ 93 t 'I. IIt 1 ! I I . I I! i 85 L..L..............i.....__._'.,_'._, L.......o..J...u..J..L.I.....L..LJ..l.;.J.u.i...LI..LJ.ilW=lLLJ, ... I ; I 11 ---y • -r r I I . I . I 11 I I ' I I >> "O n fl) w 200 400 600 800 1000 "'C 20 40 60 80 100 ::sQ. °' I ....... N >< n Weight in 1000 lbs >> -o n 00 -0 11) w ::,0.. °' I EQUATIONS FOR THE CALCULATION OF -'•N xn NOISE CERTIFICATION LIMITS ..... AT TAKEOFF, SIDELINE, AND APPROACH STAGE 2* Takeoff Limits Sideline Limits Approach Limits EPNdB EPNdB EPNdB Up to and including 75,000 lbs 93 102 102 Over 75,000 lbs to 600,000 lbs 61.86+16.61 log M 89.54+6.64 log M 89.54+6.64 log M Over 600,000 lbs 108 108 108 M • Maximum Takeoff Mass in 1000 lbs *More stringent noise certification limits exist for aircraft for which application for type certificate was dated on or after November 5, 1976 (Stage 3). "EAIUllED 011 ESTIHATED APPEND II NOISE LEVELS IA FROH FOREICN UNCERTIFICATED AIRPLANES TURBOJET PO\IERED AIRCRAFT 1\) '~ I\) ........ (X) UIICllAFT ENCINES I TAKEOFF SIDELINE I APPllOACH I HANUFACTUREII ,_____.---------------------------------·--------------------------------· a-, AND TYPE Gil. VGT. I ENGINE I NO. I THRUST I H/EST. I HI EST. I M/UT I NOTH lOOO LIS. I HODEL I ENC. I 1000 LBS. I EPNOB EPND8 EPND8 I I I I IAC l -ll Sil!. 100 1,.0 IIPEY HU06 l I 10.4 104 . 7 " . s "·'---' IAC 1 -ll IRS. S00/401 ,,, . ' SPEY HKSII z 1l. 4 '4.l IOJ.4 lOJ.4 _, IAC l-ll lllll. SDO 104, S BPEY HUI l I l I ll.' 10 l . I 101.0 105.7 '---' IAC HSI lS-lA JI. l VIPEll Sil I z I 3 . l 100., 10s . , 1 ,_, ". 3 IAC HSI ZS-IA-SU JI. 2 VJrER SU 2 3.! '3.S 102.S IDS. 4 I IAC HSI lS-lAII-SU II.? VIPER SU 1 3.3 '4.1 lOZ.S IOS . 4 I IAC HSI ZS-3" 21 . 7 VIPER s:n 1 3.3 f4 . 3 102.S 1 OS. S IAC HS12S-3AIIIA 12.7 VIPER SU l 3 , 3 n . 1 I OJ. S l OS. 6 1I ~~ IAC 'Cl 0 'Cl HSUS-400A U.3 VIPER S22 2 3.3 ,s. 7 I 02. S tos., l (() w 1 ___ 1 ::s CJ', 0. I I-'· I\) BAC >< 0 HSI :&S-IIOOA lS. s VIPER 601 1 3.7 f7 . I 103 . 6 I 01. t l :t,, RAC t,1SUPER VClO :us. 0 nco. 0 4 110 .1 1 u. S I 115. l 1 ___ 1 Z1 ' . I\) AlRCIIAFT NANUFACTURlll AND TYPE APPEND II tA K£ASU1l1D OR ISTINATED NOISE LEVELS FRON FOREIGN UNCEllTIFICATED AIRPLANE& TURBOJET POWERED AIRCRAFT ENCINEB TAKEOFF BID£t1NE APPROACH 1---------------------------------------1--------------------------------ICII. WCT. I £NCINE I NO. 1 THRUST I MIEST . 1 M/EST. I N/EST I 1000 LBI. I HODEL I ENC. I 1000 LBS. I EPNDB EPNDB I EPNDI I 1 ___ 1 HOTH ~ ~ 'o 0 'O (I) w ;:I 0\ 0. II-'· I\) >< 0 ~ BAC VClO SRI. 1100 314. 0 RCO. 4J I 4 I zo. 4 t10. Z l 13. Z 114 . I HA\IKER SIDDELEY CONET 4 lU . O RAU Nlt524 4 1 ___ 1 lO. 5 U3.0 to4. 0 l lZ . 0 t HAWKER 81DOEtEY COMET 48 ISi. D RUt HUU 4 1___ 1 10.5 101. 0 104 . 0 II Z. 0 1 HAWKER SIDDELEY COHET 4C 1'1.0 KU• MUUI I 4 I ·---' 10 . 5 103. 0 l04 . 0 tu .a 1 HAWKER SIDDELEY HB125 SERIES IA u., VIPER 511 2 1___ 1 3.0 11.0 ".o I 03. 0 I HAWKER SIODELEY HSI 2S &£RIEi 3 2t. 0 VtPER 122 2 3.4 ., .0 "· o 104.0 HAWKER 81DDELU H812S-400 U . 3 VIPIR SU 2 ,___, 3.4 to .o I ,· ".o 104 . D 1 HAWKER 8IDD1t1Y HltU-600 25 .0 VIPER Ut-U 2 ·---' 3 . 1 ., . 0 ".0 105 . 0 I HAVltEII SIDDELEY TRIDENT I HAWKER 81 DDELEY TRIDENT lE us.o 1,0.0 I RBiU 111161 Mnos-s Nlt511 -5 I 3 I ,___ I 3 ,_1 IO. I 11 . 4 I DO. 0 101.0 I 100.0 106 . 0 IOI. 0 10,. 0 I I\) '-I I\) ' 00 0\ HAVKEII BIDDILIY TRIDENT 21 143.S lllt U MKS U-S 3 1_1 U. 0 1 DI. 0 106.0 10,. 0 I AlltCRAFT "ANUFACTUIIIR AND TYPI HAWKl:11 IIDDILIY TRIDENT H APPEND I I IA NEA9Ull1D 011 EB~l"ATID NOISE LEYELB FllOH FOREIGN UNCEIITIFICATID AIRPLANE& TUIIIOJIT POWERED AIRCRAFT I I ENCINEB I TAKEOrr I SIDELINE I APPROACH I 1---------------------------------------1--------------------------------· CR. WGT. I INCINI I NO . I THRUST I "/EtlT. I HIEBT. I NIIBT I 1100 LIi. i HODEL I ENC. I IDOO LIi . i EPNDI I EPNDI I EPNDI I ,_, I I I I I I I ,_,I , I __, no.a llllU KKSU-S I 4 I ti . ' I ID4. 0 I lOS , O 110.0 NOTH l, I I\) ...... I\} ...... OJ °' UI 1111 COMNODOH IAI tlU VESTVIND 11.S ao., I I CJUG-S C,U lO-t 2 1_1 I I I I 1__ , 3 . D I. I ua., too., 114 .1 IOS. 0 101. I '°' .• MIi "" 110 NANIA IO. I I CJUO-S I ,___, 1.0 100., IOS. 0 IH . O SUD-AVIATION CARAVILLI 1 OIi ..... JTID-1 I I I I ,_, 14.0 n ., 102.0 101 . S 1 SUD-AVIATION CARAVEL LI 111 101. 4 RAU NUl7 I I I ,___, ti. 4 104.0 10,.0 Ill. 0 l IUD-AYUTION CARAVELU VIN I . I Ill. I RAU MUU I 1_1 II.I 114 , 0 It I . 0 ... ., I w SUD-AVIATION CARAVEL LI V 111 vrw-rokKER vrw U4 NOTES ti D. 2 44.0 AVON SUII HOH NKSOI I ,___, I 2 I 1 __._1 12 . • 7.1 114 . D ,0, s 111. D f2. I 107. I " . l I I ,I l ~ ~ 'O 0 'O (1) w ::s0. °'I t-'~ I\.) X o _.. :i:,. t. e. THRUST CUTSAr.K USEn NOISE LEVELS DO NOT ANENOf'ENT~ 8 OR 9 INCLUDE APPLICATION Of' FAR PART 36 I\) '...... I\) APPENDIX I I 'CD MEASURED OR EST I HATED NOI5E LEVELS FROH UNCERTIFICATED AIRPLANES °' tARCE TRANSPORT CATECORY AIRCRAFT AIRCRAFT MANUFACTURER AND TYPE CR. WGT 1000 LBS. ENGINES TAKEOFF SIDELINE -------------------1---------t---------NO. SHP HIEST HIEGT HODEL EPNDB EPNDB APPROACH --..---------1H/EST EPNOB NOTH, AEROSPATIALE NORD 262C 22.9 BASTAN 2 VI I 1065 90 0 91. 0 99 0 FOKKER F-27 HK. 200 43.5 HK53i-? 2 2050 90 ' 102.0 100.3 FOKKER F-2? MK 4001600 '13. 5 HK532-?R 2 2140 89 0 92.5 99.0 1 LOCKHEED L-100-50 170.Q S01-D22A 4 4200 99.8 93 5 '}8. 2 LOCKHEED L-188 1 I 6 0 501-013 4 3750 9~.0 'J 3 . 0 99.0 LOCKHEED L- 400 84.D S01-D22A 2 4591 92 7 '11 . ? ., 7 5 See Appendix 1 for Charts and Equations for calculation of Noise Certification limits )>)> "O n -0 Cl> OJ :, ti'\ C.. I _,, N X ("") N MEASURED OR EST I HATED APPENDIX t ll NOISE LEVELS FROM UNCERTlFICATED AIRPLANES I\) "PROPELLER DRIVEN SHALL AIRPLANES I\) "co()"\ AIRCRAFT MANUFACTURER AND TYPE GR . ENGINES 1---------------------------1WGT. I HO. I HP I MODEL PROPELLER FLYOVER 1---------I "/EST DBA BEECH Z3 2300 0-320-D28 160 HC:.-121L-6F 70.0 BEECH 35 2550 E-185-l 1 ,n B-215-l07 1l. 0 BEECH 35-33 UDO 10-470-J z:&5 BHC-92ZF-1D1 79.0 BECCH 35-A33 3000 I 10-4'10-K 225 F-12 tl . O BEECH 35-B33 3000 10-470-K 225 BHC-UZF-lDl 71 . 0 BEECH 35-C33 3050 10-470-Jt 1 z:as MCC . 2A36C23-CD 10 . 0 BEECH 35-C33A 3300 10-520-8 1 215 MCC . 2AUC23-CP u .o BEECH· 358 BEECH 36 lltCH 56TC 3300 3600 5990 I 10-520-BA 10-520-8 2 TI0-:541-£184 215 I 215 310 HCC. 2A:UC23 MCC.2A36C23-CP HC-F3YR-2 I. .,.o 13. 0 12 . 0 :x,. :x,. 'O 0 'O <b w ~ ()"\ 0. I I-'• I\) >< 0 w "EASURED OR APPENDIX ti I ESTl".\TCD NOISE LEVELS FRON UNCERTIFJCATED AIRPLANES :i> :i> 'O (") 'O PROPELLER DRIVEN S"AtL AIRPLANES (1) w ::l0. °'I 1-'• F\.l ~ 0 AIRCRAFT MANUFACTURER AND TYPE CR. ENCtNES 1---------------------------1 VCT. I NO. I HP 1 I MODEL I I PROPELLER I FLYOVER 1---------HIEBT DH w BEECH :SI 5400 I0-520C 2 us PHC-J3YF_-2F f FC76 6 3-2R 112. 0 BEECH 60 6725 1 2 TI0-54 t-Et A4 320 HC-F3YR-Z 117 . 0 BU:CH 65 7700 ' 2 IGS0-00-AIA6 320 HC-93Z20-ZCt 90.0 BEECH 9:S-A:55 4180 J0-4Jl?OL 2 2.6 0 "CC.ZAF34CSS-D7IFF-O 83. 0 BEECH '5-855 uoo I J 0-470L z 260 IHC-C2YF-ZCHRIFCl465-6 14.0 BEECH 9S-8SS 5100 10-470L 2 260 PHC-3YF-2FIFC-7663-2R 11 . 0 BEECH 9S-D5S 5300 10-52DC 2 215 MCC. 3AF32C7S u .o BEECH 95-ESS 5300 1 JO-SZOC 2 us I PHC-C3YF-Z/FC7663-2R It . o' BEECH A23-H B&ECH A24R :u:so 2750 l 10-360-AZB 10-360-AIB 200 zoo HCC. IBZ3S1BFA776Z "cc. 2D34C9-N 71.0 74.0 f\) 'f\) co ' °' MEASURED OR APPENDIX ll I ESTINA:rED NOISE LEVELS FROM PROPELLER DRIVEN S11ALL UNCERTIFICATED AIRPLANES AIRPLANES I\) 'I\) 'OJ ()\ AIRCRAFT HANUFACTURER AND TYPE CR. ENCINES 1---------------------------1WCT. I NO. I HP I 110DEL PROPELLER FLYOVER :---------KIEST DBA BEECH uo 677S I 2 TIO-S4t-EIA4 323 HC-F3YR-2 16.0 BEECH i\60 67?5 I 2 TIO-S41-E1A4 3110 HC-F3YR-2' 90.0 BEECH 824R 2750 I t 10-360-Al 86 200 HC-H2YR-lBF/F7666-2R 1. ?2. 0 BEECH C tll B 7150 2 R-911S-AN-t 400 HAl'I . ZD-30-237 16. 0 BEECH C23 24SO I 1 0-320-DZB uo BEH8.76EH1SS-0-60 70.0 BEECH C35 HOO I E-225-11 l 185 8-215-10? 74. 0 BEECH D35 2725 E-zn-• l 111 S HC-A2ll20-4At 70.0 w BEECH D'1:IA BEECH En BEECH r:u 4200 2725 3050 2 I0-360-B1B l E-U5-8 I0-47D-K 110 115 in HC-UVK-28 B-zt S-107 11cc. ZA36CU 71.0 7\L 0 SO . 0 :i,,.:i,,. 'O 0 'O (D w :::s (J"\ 0. I I-' · I\) :,.: 0 w MEASURED OR ESTU1ATED APPEND[I ll t NOISE LEVELS FRON UNCERTIFICATEO AlRPLANES PP 'O 0 'O CD W °'PROPELLER DRIVEN SHALL AIRPLANES ::l0. I t-'· I\) >< 0 w AIRCRAFT MANUFACTURER AND TYPE CR. ENCINES 1---------------------------1\,/CT. I NO. I HP I HODEL PROPELLER FLYOVER 1---------I ti/EST DBA BEECH F33A 3400 t0-S20-8 1 :us HCC. U36C23 81. 0 BEECH f3S 27:10 E-US-9 l 115 B-215-107 73.0 BEECH C35 27?5 E-225-9 1 111!1 B-215-107 70.0 BEECH cso 7 t !10 z lCS0-410-AlU 230 HC-93U0-2Cl 19 .0 BEECH V35 3400 10-S20-B 1 :us HCC. 2A36Cll3-CP 10.0 BEECH V3S 3400 1 . TSIO-:SZO-D 215 PHC-A3VF-4 83.0 BEECH V35B 3400 1 10-SZO-IA 215 I HCC . 3A32C76/S82NB-Z 78. 0 BEECH V3S8 I 3400 l T810-S20-P 285 I MCC. U.32C76 83 . 0 BELLANCA 1 ECA BELLANCA ' CCAA 1650 1'!10 1 0-ZOO-A l 0-320-UI 100 150 NCC. 1AlOOACt16941 HCC. U170/7441 69.0 76 . 0 I\) 'I\) (P '0\ MEASURED OR EST I HATED APPENDIX 111 NOISE LEVELS FROM UNCERTI FI CAT ED AIRPLANES I\) 'PROPELLER DRIVEN SHALL AIRPLANES I\) co '()\ AIRCRAFT MANUFACTURER AND TYPE I GR . I ENCINES I 1---------------------------1lolCT. I NO HP HODEL PROPELLER FLYOVER ----------HfEST DBA BELLANCA 7 CCB 1650 1 0-3110-A:tB 150 HCC. 1"17017448 70 . 0 BELLANCA I GCBC I I 2 I :I 0 1 0-360-UA 110 HCC. 1A20DFA/7846 7' . 0 BELLANCA(CHAHPION) ?ECA 16:10 1 D-J3:1-K2C 115 BEN . 74 Dt16 S8-1-:16 611. 8 BELLANCACCHAHPION> 7GCAA 16 :IO t 0-320-A2B/-A2D l :S 0 SEN. 74Dl"l658-l -:16 68. II BELLANCA<CKAHPION> ?GCBC 16SD t 0-320-UBI-UD 150 SEN. 74DH688-1-:U 6B.8 .. BELLANCACCHAHPlON) ?GCBC SEAPLANE 1800 0-320 l 150 HCC. 1A1 ?:SCMA/8040 70 . 3 BELLANCACCHAHPION> 8GCBC 2150 l 0-360-CUf-Cl E 180 HTZ. HC-C2YR-1BFIF?666A n., Vl BELLANCA<CHAHPION> 8CCBC BELLANCACCHAHPION> 8CCBC SEAPLANE BELLANCA<CHAHPION> 8KCAB 2 1:50 2t :SD 1100 0-3&0-C2A/-C2E D-360 l AEl0-320-E 18 190 tBO 150 l HCC. HCC. HTZ. tUOO/HFA 1 UDO IHFA HC-C2YL-4<F)/(F)C?663-4 • 72.11 ?2.1 '10 . 0 ~ :x, u n 'O (l) w ::s ()\ 0. I I-' · I\) X 0 w MEASURED OR ESTIMATED APPEND II Ill NOISE LEVELS FROH UNCERTIFICATED AIRPLANES ):,,):,, "O 0 'O PROPELLER DRIVEN SMALL AIRPLANES (I) w ::, {J'\ 0. I t-'· I\) >< n AIRCRAFT MANUFACTURER AND TYPE CR. ENCINES ·---------------------------1WCT. I NO. I HP I I MODEL I I PROPELLER I FLYOVER 1---------K·/EST DIA w BELLANCA(CHAHPION) IKCAB 1100 1 AEJ0-320-EU 150 SEN. 74DMUI-O ". 2 BELLANCA(CHAHPJON> UCCAB 1100 I AE I 0-360-.HU 180 HTZ. HC-C2YR-4CFIFC?666A-2 '7. 2 BELLANCA(VJKINC> 17-30A 3325 10-520-K ZZ5 HTZ. HC-C2YF-1BF/F84?5-6 • 77 . S BELLANCA<VIKINC> 1?-30A 332S I 10-520-K 1 us HTZ. HC-C3YF-tRF/Fl461-IR 71 . S BELLANCA(VIKJNC> 1?-30A 332S 10-1120-k 1 us MCC. DU32Ct0 I 12NC-4 11 . S BELLANCA<VJKING> t?-30A 3325 I 10-520-K 1 225 I HCC . D3A34C40l/90DFA-12 77.S CESSNA U0D 1'00 0-200-A 1 100 I MCC. U101 '7. 0 CESSNA t?O 2200 C-lU-:1 1 145 MCC . IA1?0/DM76S6 73 . 0 CESSNA l?OA CEl5SNA 1708 2200 2200 1 0-340-AlA 1 C-145-1 170 14S HC-IJIL-lD/1433-1:1 MCC . 1A170/DM76~6 70.0 75 . 0 f\.) 'f\.) (X) '{J'\ HEASUREO OR APPENDIX 11 l EST I HATED NOISE LEVELS FRON PROPELLER DRIVEN SHALL UNCERTIFlCAT£0 AIRPLANES AIRPLANES N -..... I\) -..... co O'\ AIRCRAFT HANUF ACTURER ANO TYPE CR. I ENClNES I 1---------------------------1VCT. I NO. HP I MODEL PROPELLER I FLYOVER t---------KIEST DBA CESSNA t ?2 2.300 0-300-A 145 I HCC.tA171/EN7653 71.0 CESSNA t?S 23SO 6A-3SO-C1 1110 NCC.2A31Clt/114S-6 116. 0 CESSNA t7SA Z3SO I 0-360-AlD 110 HC-C2YK-1 ?2. 0 CESSNA l?S8 2.3SO 1 0-360-AlO 1110 NCC.2D36Cl4l?IKK-4 74.0 CESSNA 17? 3500 1 0-360-AlF6 ua I NCC. 2D34C201 74 .o CESSNA 180 2100 o-410-J 1 225 HC-821F-l-D1 7' . 0 CESSNA 180 2800 0-470-J us IIC-1:ZXF-lC 71.0 CESSNA 112H CESSNA 1192P CEHNA 310 2100 29'50 3100 I 0-470-R 0-470-R 10-410-£ l l 230 I 230 260 NCC. 2U4CS0 NCC . 2A34C203 NCC. DU36C33 76.0 71.0 11.0 :X,,;t> 'O () 'O (l) w ::s O'\ 0. I I-'• I\) >< () w AIRCRAFT MANUFACTURER AND TYPE APPENDIX 111 NEASURED OR ESTINATED NOISE LEVELS FROM UNCERTIFJCATED AIRPLANES PROPELLER DRIVEN SMALL AIRPLANES I ENGINES I 1---------------------------1GR. WCT. I NO. 1 HP I PROPELLER HODEL FLYOVER 1---------1 M/EST D8A ::i, ::i, 'O (") 'O (l) w ::s0. °'I ~ N >< 0 w CESSNA 310C 41130 10-470-D 2 uo HC-UIF-2 14.0 CESSNA 310F 4130 10-470-D 2 260 HC-A21F-2 11. 0 CESSNA 310N llZOO 10-4?0-V 2 260 I HCC.D3AF32CIOll2NC-4 10.0 CESSNA 3lOQ I I I S300 2 10-470-VO 26D HCC.3AF3ZC8?/82NC-4 u .o CESSNA 3t0Q 5300 2 10-470-VO 260 MCC.D3AF32C71ll4JF-3 86. 0 CESSNA 320 :5200 I 2 TSIO-llZ0-8 285 3AF32Cll7/82NC-4 73., CESSNA 320A 5200 2 TSI0-470-8 uo HC-AUF-2 12. 0 CESSNA 320C 5200 l TSI0-470-D 260 HCC. D2AF34C54 13.0 CESSNA HOE CESSNA nor 5300 5300 2 TSI0-520-B 2 TlUO-S20-B U5 2115 3AF32Cl7/12NC-4 3lF:UC8?/UNC-4 74. 2 74.5 N '...., I\) co ' °' MEASURED OR ESTlMATED APPENDIX l l I NOISE LEVELS FRON UNC ERT l Fl CAT ED AIRPLANES N ....... PROPELLER DRIVEN SMALL AIRPLANES I\) (X) '(J\ AIRCRAFT MANUFACTURER AND TYPE CR. r ENGINES I 1---------------------------1lo/CT. NO. HP MODEL PROPELLER I FLYOVER 1---------HIEST OBA CESSNA 33?F 4630 10-360-C J 210 I l1CC.D2AF34C II:!. 0 CESSNA 340 ,,n 2 TSI0-520-K Jl5 MCC'.3AF32C87182NC-4 83 . 0 CESSNA 401 6300 2 T8l0-S20-E 300 HCC. 3AF32CII? I, 79.0 CESSNA 414 63:50 2 TSI0-520-J 310 I HCC. 3AF32C'3 112 . 0 CESSNA 421 1450 2 CTB I 0-520-D 375 MCC.3AF34C92 u . o CESSNA 4 2l B ?450 2 CTSI0-520-H 37:1 HCC. 3AF34C92 It. 0 CESSNA Al 115F 3350 J0-520-D 1 285 I l1CC.D2A34C58/90AT-9.5 n . o CESSNA A188B 4000 10-!IJO-D 1 Jl5 HCC . D2A34C5ll?OAT-1 15 . 0 CESSNA F150J CESSNA Fl50L 1600 1600 0-240-A 0-200-A 1 t 130 100 11CC.lA1351BRM7l50 MCC.1Al01IHCH6?41 • ?a.5 ". 0 ~~ 'O 0 'O (D w :::i a, Q. I I-'· I\) >< 0 w APPENDIX 111 ;x:,;x:, MEASURED OR ESTIMATED NOISE LEVELS FROM UNCERTIFICATED AIRPLANES 'O (") ..... 'O 0 (l) w PROPELLER DRIVEN SHALL AIRPLANES ::s a- Q. I μ. f\J >< (") AIRCRAFT MANUFACTURER ANO TYPE GR. I ENGINES I 1---------------------------1 VGT. I NO. Hl" HODEL PROPELLER I FLYOVER 1---------HI EST DIA w CESSNA Fl ?:it 2300 t 0-3ZO-E2D 150 J MCC. 1Cl60fCTH?553 74. 0 CESSNA Fl77RG 21100 l 10-360-At86 200 HCC.S2D34C206f78TA 76.0 CESSNA FRl ?2F 2220 l 0-360-D uo HCC. DZA34C67L ll. 0 CESSNA FR17'2G UZD I 10-360-D 210 HCC . D2A34C67L 77 . 0' CESSNA FRA-UOL UDO 0-240-A 130 MCC.1At3Sf1RM7ISO 73 . 0 CESSNA T1D7 UDO I . I TSl0-510-G 285 KCC.D1A34C78-L 11.0 CESSNA T2101: 3400 1 TSI0-520-C 215 I HCC . D3A31C88/l2NC-Z 71.0 CESSNA T210L 31DO 1 TIIO-S20-H 215 MCC.D3A3ZCl8l.2NC-2 12.0 CESSNA T3 I OP CESSNA T310P 5400 S400 2 TSI0-520-8 2 TBI0-520-8 215 us HCC.3AF32Cl7flZNC-4 HCC. DZAF3 4C?l L 74. 7 n . o f\J ..... 'I\) 'co O'I APPEND It 11 J MEASURED OR £8TtMATED NOtSE LEVELS FROM UNCERTtFtCATED AIRPLANES I\) PROPELLER DRIVEN SHALL AIRPLANE$ '_. I\) ........ 0) O'\ AIRCRAFT ENGINES FLYOVER MANUFACTURER 1---------------------------1 1---------AND TYPE GR. VGT. I NO. HP I PROPELLER M/EBT I N0D£L I DIA C£88NA 2 T3tOQ ssoo TII0-520-8 21S HCC.3AF32Cl7/12NC-4 75.2 CESSNA 2 T3tOR ssoo TSJ0-520-B 21S MCC.3AF32Cl7/82NC-4 77.7 CESSNA l TU-J06-t uoo I Ta10-s20-c 2n ncC.D3A32C90ll2NC 77. 0 GRUHHAN AHERICAN I AA-lA l560 0-235-CZC SOI HCC. U l OS8CM7t 5 3 70.0 GRUHHAN AMERICAN 1 AA-5 :noo I o-no-nc; uo ncc.1c11a&'l'.'J173s, 72.0 MAULE M-4-21 Ot 1300 IO•Uf-A 1'5 HCC.D2A34C67 ". a MAULE l .,. H-4-UOC uoo 6A-3SO-Cl HCC.2U1C2l 7'.0 MOONEY M 20 C Z575 0-360-AtD uo HC-C2YK-1Af1666-J 75.5 ~ :i,. -c,o MOONEY l 'O <D w H 20 t 2575 0-31.D-AlD 110 MCC.2D34C53A/74E-O 75.' :::s O'\ Q. I t-'• I\) X. (") MOONEY 1 M 20 E 2575 10-UO-AU 200 HC-CJYK-lA/1666-2 14.3 w • l'J AIRCRAFT 11"ANUFACT\IRER AND TYPE APPENDIX III MEASURED OR ESTUfATED NOISE LEVELS FROtl UNCERTIFICATED AIRPLANES PROPELLER DRIVEN SKALL AIRPLANES J:NCINES !-------------- ·------------tCR. 'JCT. I NO. I HP I PROPELLER HODEL I FLYOVER 1---------I H/EST OBA ;i:, :t> 'O n 'O <D w :l 0-, Q, I I-' · (\) ~ n w HOONEY M 20 F 2740 1 J0-360-AIA 200 HC-C2YK-1A/7666-2 74.' MOONEY M 22 3680 t TI 0- 54 1 -A 1A 31D HC-C2YK-1B/847S-4 80.0 PIPER PA-18-1SO 1. 1 t?SO 0-320-UB ' 150 1174D11-0-SO 72.0 PIPER PA-ll-150 1?50 t 0-UO-UB lSO H74DH-S6 70.0 PIPER PA-22-135 1950 0-290-D2 in H74DH 74. 0 PIPER PA-2 3-160 3800 2 0-320-Bt A 160 HC-82XC-28 75. 0 PIPER PA-23-ZSO 5200 2 TI0-540-C lA 250 HC-UYR-2RB 77.0 PIPER PA-24-250 2100 0-540-Al 05 250 HC-A2XK-1 76.0 PIPER PA-24-260 2700 1 IO-HD-RIAS 260 HC-E2YR-18 76 . 0 l'J ' PIPER PA-29-140 2lSO 1 0-320-EU 150 1174DH-0-60 73 . 0 l'J co 'a, MEASURED OR APPENDlX I 11 ESTll1ATED NOISE LEV&LS FROM PROPELLER DRIVEN SHALL UNCERTIFICATED AIRPLANES AIRPLANES N ' I\) '(I) ~ AIRCRAFT MANUFACTURER ,I.ND TYPE GR. ENC rNES 1---------------------------1W'GT. I NO. I HP MODEL PROPELLER FLYOVER ---------KIEST OBA PIPER p,1.-28-1S1 2325 0-320-ElD 150 74DH6-0-51 ?5.0 PIPER P,1.-28-180 I r 2400 0-360-A.3" 180 H?6 74. 0 PIPER f,1.-28-180 HOO 1 0-360-A4A 180 1'EH8S5-0-60 ?8.0 PIPER PA-2B-lll0 2500 1 10-360-BlE 110 HC-C2YK-1 ?3.0 PIPER PA-28-200 2600 10-360-C.lC 200 HC-C2YK-1 ??.O PIPER PA.-28-23S HOO 1 0-540-B4BS 235 HC-C2YK-l 11. 0 Pl PER PA-30 3'00 2 J0-320-CtA 160 MC-E2YL-28 14. 0 w PIPER PA-31 PIPER PA-31 ,soo 6S00 2 TI 0-5 'I 0-A lA 2 Tt0-540-AU 310 310 HC-E2YR-2D HC-E3YR-U 16.0 81.0 :r:, :i:,. 'O 0 'o (l) w ~ °' 0. I 1-'·N >< 0 w APPENDIX 111 MEASURED OR £STll1ATCD NOISE LEVELS FROH UNCERTIFICATED AIRPLANES ;i.,. :i,, 'O (") __, 'O (t) w ~ PROPELLER DRIVEN Sl1ALL AIRPLANES :::s 0. °'I 1-' •f\J >< (") AIRCRAFT ENGINES FLYOVER w MANUFACTURER 1---------------------------1 1---------AND TYPE CR. VCT. I NO. I HP I PROPELLER 1 HIEST MODEL OBA PIPER z PA-31P 7100 TICO-S4 I-E1A 42' HC-C3YN-ZL 85.0 PIPER 2 PA-31P-350 7200 TJO/LTI0-540-V2AD 3:10 HC-I3YR-2UF/FC7154/ZLUF/YJCl7l:14K 10., PIPER l PA-32-:uo 3400 O-S40-E4D:I 260 HC-CZYK-18 11. 0 PIPER PA-32-300 3400 10-540-KlAS 300 HC-C2YK-18 13.0 PIPER I PA-34-200 4200 I 10-360-ClE& 200 I HC-CZYK-2 7' .0 PIPER 2 PA-34-20DT 4570 Tll0-3'0-E ILTS us I IHC-C2YF-2IFJCl45f-lR 77.0 ROCKWELL INT. l 112 U50 10-U0-C1D6 200 HC-E2YR-1BFIF7&6&-A 72.0 ROCKWELL INT. 2 no 67:SO GS0-410-AIA6 320 HC-131Z0-2C/9333 81. 0 ROCK\IELL INT. I 2 UOFL . I I\) noo ICS0-S40-81A 3'0 HC-t3i30-ZB19349-6 . S 1, .'o ....... ..... I\) ....... TAYLORCRAFT l (X) F-1' 1500 0-200-A 100 MCC . lAIOSISCMUSO • "·" (}\ APPEND IX 111 MEASURED OR ESTlHATED NOlSE LEVELS FROM UNCERTlFlCATtD AIRPLANES PROPELLER DRIVEN SMALL AIRPLANES AIRCRAFT I ENCi NEB I I FLYOVER HANUFACTURER 1---------------------------1 1---------AND TYPE CR. VCT. I NO HP PROPELLER H/EST I HODEL DU TAYLORCRAFT F-21 1500 0-235-LZC 112 SEN. ?2CK-O-!IO U.8 TAYLORCRAFT F-2 U l!IOO 0235-LZC 112 SEN. ?2CK-0-50 '8.8 2 I. AEROSTAR Ut !1700 10-540-PlA!I 290 HC-C3YR/C8Ull-8R 84.0 TED SHlTH ;ta, ;ta, 'O 0 'O (D w ::s 0\ ..... 0.. I u, I-'· rv >< 0 w •••• ):,, ):,, -o n -0 Cl) w:::, 0) C.. I -'• N >< n wNoise Certification Limits for Propeller-Driven Aircraft Under 12,500 lbs 100. •••• <?! ;,;~: !jll ~f !pi !!li J!!ff !j'l I I ' I !It11 !lri ~· lj l '.tJ f1 J /1 r ! it ll ll 't~jμ1: l11;l,l1 ftiH(i :!i \jlj 111! !t J? Iii!::: : :: ;: 1::: :: :: :; 1; : ; i :. .I !i:: ; :· I 1 , · 11 1 ., I 1: ? r I: TI J ]i:. L !: l! d I i:I 1 ;ri (:;: :::: · ;:: ::·~ :::: :::: :!::: ::!! 1H;i h 1 ') ;; :!i 1 '1"11i ; 1 l l I : 'f 1 f lj!i :•!! 11111 :1 !Iii' l lt !!i: !:!I ;;! : ;: : 1 I.... ·- .. ,i; , ... ,. ••,• ,1-!I • ;, ,l.l II 1• tl i f M-M-1+++<1+< u·tt•tt· tt-tt-tti H-fHHH~IJIHl~l+I I ' 't 11· :H-f I Ii i ~ t rttf. ~·· ·~ ·· · :!~i :? l? 111; rm 11!1 :, i ,ii t 11 i ll I ii : 11: 1l i111! ii i l 1 !i i1! 1:. 1 1:1\ ; iiF \1\:<( 90 :::: 1·!:: lj;: :::; J\J; :fi! r~,:; !1T1 ,· r': Iti I I ; '11 I I ~ I, 11·1T rm ·, .. 1 1· :,·1· 11:11·.·mj :,,::_ · :.T.:,1.1'::.::. ..11n · 1·11,1: 1'1 ,· ..::~: .::: ;. :: :::: ti;: :r.: I !1 ,,. . i! 11 Ll ' f! ·1IH+I--H-HCU I ti ~ :11 II ' ,I ,. ' l' u .. ., .... .... .. I m t .. · f:-n1 • :tt· 11 i1 HI rt I 1ml t , i r; • • • • ,.i- ff·· ... r.r,-:-:;;1~: "C :(\ ~7:: :~~! :~'.:r:t!: j! ;:: .in Iil1. 1 "!1 ! : ~ i Ii Ii !iii::!!, !!!:!.:!,:! :; !! :,i! !:!: ::: : :!: [: ·: 1 .. .. . ... r.. . ... ,". . '.~ ,~. . , .. I 1' q II jl I . 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'I'!' ·,,11 I I l nlr:i I I I l ~1 •::: 11· i:T! 111111m :;;J 11;! ; 1!! :::: :: l: r: r: ::::::: :::: ;::: ::::.!:1~ a·:; .. ~ i;;l~J11 l·lf :t: ;ii ;.1 . . . • · .. ~ : , 1 .: , . 1 • ::ir !J r ! , ~i 1:.~ ;:. ? i. ,: ;:.~ :~.! : ::: : :~ : ::~: : : : : !:: 1 ::; ~~: :!~: :::: :~: il · U: lH ii[j / !i ~ljl !Jii .!I:~··.. I iii !i ii ! IJI Jffi ! I J j! 11 j ·) nil qq LJiJ!H ?! ?l i? id! Ii!! ) ( ii~i i: j( iiii mi ii:it (~i I!H iw i tr ~ll r~ ffll i 1r~ t TI l rjl trp I l 1! I I ii ,11m~ttti n!l rrrn I; ·ni ?! i;i; TIE/70 · · ·· · - ·· ........ ,ft .. ,;l, · ·1 ·i·· ... . . ,, J'' 111111 , , I 'I' 1• , !I 1, .. ;, 1,1 'l ' '(U.U.I ,,, , ;,1,.,. ,1,. :r 1. .. · 111 ; :: :· ::: · :: :· ·: :: 1'1:: ·: :~:·:· :. :: ...... "!;ll I i :1:!i' J l t lj ~ 1 H 111 ti. 'I ·u u!J U,:~P1, \Ii :Ji.ii !:. :!:: ::: : ;: ;: '.::\ 68 ... ..... .... ............... . ,. , .;•fj 1mH ~ hi '1 I . . . IT l I I l !11 tn1 : ·. ~.· :·rr. ' 1111 :·,., , : ·,,· ;!!l :::: :;;: ::: : ::: : :::: ::: · ::: : :::: ;::: ::i: :1!: ::•; ;,·· I 1 ii 11. I I I l i I I · .. · · - · · • · · · · · · · -· •· .. •, , • · · .. I, · I 1 , I , 11 " , I , ,, I I I: : : I (, ' l;; , j i!I ! : : ; ! 1; ! ! I II I: 1;:;: : I : : ; : : : 1 1 ~JD. 1? 1< <: :~11 1~; :(J1Jw D11,~+:! .1 !t 11 r i. r~ t11 , 1 1 r1 .i1,1 μ,i, !j ~ WJI jilI !! 1 !·,;·~~ !? \J2.rt1i w.; 1\ 1 'r 1:;,· ........... . ..... . ·-·• ....... ' .. ,, f;. ·1·· I t I I ' I t ' I I "! ' •• .. .. . ... . • . .. 1 1 1 1 11 60 :;:,.: :::: :::~ :: :: ~·~- : i.:; :..::: :~::1Pt•lll~; lll I 1 11 'I i Ii ! 1 • ,1:~ . • ! 1: 1 :::i :L: ih: !;:: :: : :!: ; :: ~: ::: : :::; :; :: :: :: :: : : ~::: :::· lit!1 :;i~ 'l:; : ·:: :: ' !1i 1' I If ,' I' Ii ii 11· i 11! ,l 'lj, n.rn. 1"1'11·=.·1:. :.~.:.!l!·1·1.1:1•,.r1:, •. '•• !·, .: :,_: ;::: :::: :: :: 1 i1 :::~ :::: :::: :~:; ::~;: tW :~:: ::;; :Tif: !I il If j H f1i l i' 111 il1i iii ti l ti~ ~ri \Hr ft+l ~;:: ;;:; ;;; '.;:~ ;;;; \'. ::+~ fr1r1· tt+t+-tt-HI-H< :::: n:: .::1 :; :.,~!,: : :-::: i: 1 i:,; 11 i 11, ,! ,, . 1;i, 1 • ii1 . ·I'· ·· ·;· .,1 . .. . 1 .. . 1 ... . ....... . ... :, :.:_i :.:. .:=. •••• .... . , H••• •• · 1 ltH, t· ,-..~; .,~ f'l1 fl •f• r1 If t p 11•41 I 1[~. 1 1 , , · t• •• •• . ,., •l j , ,, ~ ·,• -~· • ., , 1 :] 0166 495 990 1320 3300 3630 I\) ....... 1. Airplane Type Certificate Applied For on or After October 10, 1973 2. Airplane Type Certificate Applied For on or After January 1, 1975, or I\) application for a standard or restricted category airworthiness certificate ~ after January 1, 1980 EQUATIONS FOR THE CALCULATION OF NOISE CERTIFICATION LIMITS FOR PROPELLER-DRIVEN AIRCRAFT UNDER 12,500 LBS Application for Type Certification on or After October 10, Up to and including 1,320 lbs Over 1,320 lbs up to and including to 3,630 lbs Over 3,630 lbs up to and including 12,500 lbs Application for Type Certification on or After January 1, 1973: LIMIT 68.dB(A) 68 + 1 dB for each 165 lb increment of T.O. weight above-1320 lbs. 82 dB(A) 1975 or application for a standard or restricted category airworthiness certificate after January 1, 1980. Up to and including 1320 lbs. Over 1320 lbs. up to and including 3300 lbs. Over 3300 lbs. up to and includ 1.ng 12500 lbs. 68 dB{A) 68 + ldB(A) for each );:I, ):a -o n165 lb. -0 It) w increment of ::, 0\ a. I T.o. weight ...,.N )( (") above w 1320 lbs. 80 dB(A) APPENDIX 11.1 MEASURED OR ESTIMATED NOISE LEVELS FROM UNCERTIFICATED AIRPLANES CIVIL SUPERSONIC AIRCRAFT ENGINES TAKEOFF SIDELINE APPROACH :HRF'LANE MODEL NO. THRUST GR. WGT. M/EST, M/EST, M/EST. 1000 LBS. 1000 LBS. EPNDI! EPNDB EPNDB TU-144 4 360,0 110,0 114. 0 110,0 :i> :i> 'O (") 'O (I) w ::s °' 0. I I-' • I\) ~ 0 -1:: APPENDIX 'I NO:SE DATA ~HEET FOR noTARY WING AIRCRAFT f-'.AtltJ r !I. ,:-1_1 RE R CC'MMl1:I ~JAl':E MTO\J KG NUMllCJ: CNC ENG:NE MAt:E HP PER vv· VH : KMH: VNE!ROTORS MAIN/TAtL: NOISE LEVELS - EFNL : ·----------------·---------------------!KMH : orAM. :NUM :FLYOVER: T/0 : APP REFERENCE N ' P.l!D MIJDF.!. LBS AIID MOOT;;L CNC '<T: KT : t!Pltl 1 Hl I BL : Rl't! : f < I I I I I I I t - -- --- --- ---- --- -- 500FT ,._pp : 6 OEG O'.) Q'I AEROSF,-.TlAlE t 0 9 6 : ~92' IO.? I 87 . 2 8 9 . 2 91 2 :VGIB VIP 25 SC1U i RHEL 41~0:LYCOMTNG I. 8 6: t\3 :i-; a :LYCOMING I.TS 1 0 1 ------ -- - . ' . --- --- -- - --- --A[ROSrATl/1.lE IO 9 9 5: 3 ! 5 '5 0: 1 8. 9: 6 zo1: 92 o lA-2 s•,rprFREL')N 2424<':TURBOMECA 4. 0 0: 5 990: SA 3 Z, :TURHO 3C '' -- - '. --- --- ---- --- ---'HlOS\'AT!ALE 1147'5: 3 15701 8. 6 0 1 6 207: 92.0 98.4 98.6 IWG/B WIP 25 SlfF/fRE!.ClN z:;3oz:TURBOMECA 6 0: 5 9901 SA 2 2 11' :TVRMO :J E 6 -- - . . ' . ' ' --- --- ---- -- --- AEROEFAT!ALE 5540: 2 1435: I 5. 0: 4 93.6 IA-2 PUMA 12251 ITURBOMECA 3. 0 <l: S s" 3 3 o :TURMC ~C A EROS PAT I ,._LE 7012: 2 1,575 : ?O: 2601 2601 1 5 . l : 4 26?: 91.4 95.4 95. 6 IFA1'-EE-7'-03 PtrM,. SA 330J 15 S 32: TURBOME CA : 7tJRMO 4,: 140: I 6 1 : 3. 0 4 I S '' :' AEROSPATIALE !8001 590: 65: 264: 264: 10.'51 3 2671 80.1 9 2 . 5 89 . '5 :FAA-EE-79-03 G ,zEL t.E 3968 :Tl'RBOMECA 142: 164: 0 . 70:13 SA 341~ :A5TAZOU JA AERIJSl'ATIALE 18961 590: 1 0. '5 I 3 e 8 . 2 89.8 95 5 IWG/B W/P 25 GAZELLE 4180:TURBOMECA 0.10: 13 31' 34 2 !ASTAZOU 1A -- .- --- --- ---- --- ---AEROSPATl1>.LE 2994: 1oso: 11 5 : 4 92.4 1WGfB WfP 25 DAUPH!N 66011TURB0M'ECA 0 9 0: 1 g SA :uoc lASTAZOU 18A -- ' - --- --- ---- -- --- AEROSPATl1>.LE! 339,1: 2 6501 11. 5: 4 89.4 9 4 . 0 : WG f B W f P 2 5 DAUPHIN;: 7481 ITl/RBOMECA 0.90113 SA 36> IASTAZOU ARRIEL -- .- --- --- ---- -- ---- AEROSPATlALE DA'JPH:N-2 8<18131 18716:TURE'OMECA 2 7101 751 150: 202: 11.9: 4 0 90113 365: 4706: 98.3 96 . 5 :FAA-EE-841-2 C2) :i:,. 1J 'O ~ (') SA 363H AGUST,._ :ARR!EL tC 25991 5730:ALLlSON 2 '. -- -420: . . . ' --- --- ---- -- ---- ----o: 1 0 . ? : 4 3851 9 l . 7 1H: I 8 2: 2 . 0 J l 2 92.9 96 . 0 IFAA-AEE-80-16 ( 1) CD W ::-s0. °'I 1--'•N >< () A109 1250-C20B \JI : : -- - - - -- : - -- BELL l 8 l 'l : 420: sz: 2111: 241 : 1 l . 3 l 2 85 . 8 85.9 90.3 IFAA-EE-19-03 LONCRPHGER 40001ALLlS0N 1 JO : 150: . 5 8: 2 206L :2SO-C20B NOISE DATA SHEET Art'ENOIX V FOR ROTARY WING AIRCRAFT !l> !l> 'O (') 'O I\) 11AH1J F f.,':TlJR ER l'TO\J NUMBER I:NG HP VY'. VH I VNE:ROTons MAIN/TAIL: NOI3E LEVELS - EPNL : '----------------·---------------------' (1) w :::s 0\ 0. I 1--'·l'v CC·MMC•N N~ME t:G ENGINE MAKE PER KMH: KMH:OJAM :NUM. l IFLYOVERI TIO : APP REFERENCE >< 0 A.Ht: MOD~:!. t.9S AND MODEL ENG KT: KT : MPH l (M) I Dt.. I RPM I 5DOrT APF 16 DEC U1 ------- f I I I I I I I o • I I - - -- --- -- - --BELL 47f2! 2 6451 ss: 194: 1851 14 61 2 94.6 91 . ? 95.? :FAA-EE-79-03 ~, - 1 :0500!PRATT • 'WHJTUEY : 1041 1151 2.S?! 2 'PT61'-3 I I t I I I o I I • I I -- - - - -- --- -- ____ : __ _!ltLT. 113 9 2: ! 280! 90. '3 99.6 lFAA-RD-77-94 29SO!AVCO-LYCOM~NC • 4".'C ITV0-435-GtA . . . . . ' -- - - -·-- -- - ---BEtt. :JS 6 0: 2 57S! ,',SI 12 1: Z 3 4 8 1 8?.9 98.2 lFAA-EE-94-1 CZ) ?849:LYC'C'MJNC : 1411 !62; 1.98: 2 : 1881: BELL 222 ltTSl01-6~0C-3 -·-- I . o. o. -- - -- -- -- - --EO'E!NG 204111 2 3? 5 DI I 8. 3: 97.D 9?.0 10Z.01MANUFACTURER 45006: LYCOMING 1 8. 3: 1 VERTOL 23~ lT5S-L-l1C H\.'GHES 8 l 6: 190 l 8. 1 8: 3 82.0 1?99!LYCOM1NG : 1 . 3 0: Z 3 O'JC IHI0-360-0lA -- I __.__ I I , __. t ___.__ I, ___HUGHES LO 9 4: zsz: 8 03: 4 9 1 . I rA-2 241Z!ALLIS0N I 1 . 3 0: 2 369A IT63-A-SA I I I I I I I > tI I I -- - - - -- --- ---HlViHES 1 IS? : 4001 so: 2441 8. 03: 4 85.8 8 S . I B?.? : rAA-EE-?9-03 2 5 5 1 : ALL I SCIN : 1311 I 1 . 3 0; 2 :; 0 oc: l2!)0-Cl8A -- - ~ __ , 1 I I __ , ___ , __ , ___HV·';H£5 839! 4201 8 . 0 5 I S 88? IA-2 ·1 8 ~ 9 ! ALL I SON 1 . 3 0: Z 5000 !250-C20B I r I I -- - - - I I I I -- -- --MESSER~Cl-:MlTT! 2300! 2 420: 101 241: 210: 9 92: 4 88.4 e 9. 1 91.7 lFAA-EE-79-03 5071 !ALLISON 130: 167! 1 901 2 so-io ~ :2so-c1e -- -- ' ' - - .. - -- .' --- -- 111 L 3Slll! 2 450: 3 89.8 ?6. S 1WG/B ,.,, P zs · 7 7 5 7 : ( SC'TOV Z 3 11 I l !GT0-350P -- '. '. - - - -- -- --- Mtl 42500! 2 S SO O I 35 0: S 103.7 107.81WG/B 'WfP ZS 93?J0!S0L : 6. 3 0 l 4 Mt 11\ : D - Z 5 V ,.rv - 2 BM 1l43 6 I 2 1700: 2 1 . 3: S ?7.6 100 Ol'WC/B 'W/P 25 2 5 2 : 6 I ( SOTOV 2 : 3. \I 1 : 3 Ml 8 :TB-2-ll?A ___ , __ , __.__.___.__ , __ _ I I I I I I -- -- --- --- --- -- --- -------- --- -- -- -- --- --- --- --- -- -- -- --- --- --- .I\I'I'CND( )( V NOISE DATA fHEET fOR R0TAnY VING AIRCRAFT VY'. VH l VNElROTORS MAIN/TAIL: NOl3E LEVEL5 - EPNL I MAMIJFACTURER MTOV NU:1BER EllG HP :----------------:---------------------· COMr"l,W ~;AME KG FNG:JH: HAKE PER KMHl KMHlDIAM. :NUM: :rtYOVERl TfO : APP REFERENCE MHI MODEL LBS 1\110 MODEL ENG. KT! KT : Ml'Hl (H) l llL : RPM I :'.iOOI'T 1\Pl' 16 DEG f I I I . . . . S!KORS!<Y 10000: 2 1400: 74: Zi.?l l 8. 9 l 5 I' 2. 6 95.9 94.0 lFAA-EE-79-03 H -1 22049:CENERAL ELECTRIC 1u: l J l 5 l 5 S-61 lTSO-r.t- \ 0 ___ 1 __ : __ 1 __ : ___ : __ 1 ___ S l KOR,,~;y 19459: 2 48001 2 2. 0: 6 97.0 99.D lWG/8 W/P 25 42,01:PRATT WHITNEY : 4. 8 8: 4 S-64 :JFTD12-SA f , I I f I I ' 0 0 I • S!KORSK'! 16??51 2 3780l ?6l 196: 2 2 0: (, 97 1 95 7 99.9 :FAA-EE-79-03 H-53 36~88:GENERAL ELECTRIC : 1? 0 : l 4 881 4 s ... 6 5 IT64 ___ : __ : __ : __ : ___ : __ : ___ SIKORSl"Y 4545: 2 6501 11 9: 4 2931 89.1 91 . 3 95.1 IFAA-EE-81-16 (1) 10021 lALLtSON 14&: 1781 2 44: 4 s -r7 t,,· :2SO-CJO : I : I StKORS1<.Y 91851 2 1 4 l 4 : I 6 . 4 I 4 285! 96.9 89.6 96.7 IAEE-80-16 BL.I\CKHAWK 202501GENERAL ELECTRIC 1&s: 224: 3.Js: 4 : . UH-601\ IT?OO-GE-700 WESTLAND 56001 2 11201 621 1201 5.241 4 3261 93.6 92.8 98.0 :MANUFACTURER \il-30 12347:ROLLS ROYCE : 120: 1381 2.44: 4 I 6 4 7 t "130.:100 lR.R GEM4l-1MK510! (I) Dita calculated fr- thla report. (2) Data oot corrected to •tendard reference reference flight peth (a• •••ured data). A-2 Advtaory Circular 36-2 Dated 2/6/78 WG/1 V/P 2S ICAO WorltingGroup 12/14/78 day uor correct..! to :r,, :i> 'O n 'O (1) w ~ 0, a, I I-'• I\) X n w U1 -0 .)> .)> /CAO Noi• Certification Umits for -o n (1) w Helicopters at Takeoff, Approach and Flyover ::::s 0) 107 106 106 1-++t-+++ttt+tttttttifflf z 96 1-1--1--1-4-+++~~~= a. w 87 88 8& 100 1000 1737 10,000 100,000 178,370 Weight 0.. I -'• N xn (Jl 107 106 105 1,000,000 C* lJl (;") . "0 . EQUATIONS FOR THE CALCULATION OF ICAO HELICOPTER NOISE STANDARDS AT TAKEOFF, APPROACH, AND FLYOVER Takeoff Limits EPNdB Approach Limits EPNdB Flyover Limits EPNdB Up to and including 1,737 lbs 86 87 85 Over 1,737 lbs to 176,370 lbs 83.61+9.97 log M 84,61+9.97 log M 82.61+9,97 log M Over 176,370 lbs 106 107 105 M = Maximum Takeoff Mass in 1000 lbs ~~ 'O 0 'O CD W ~ CJ' 0.. I t-'· N >< 0 \Jl U1