Noise Levels for U.S. Certificated and Foreign Aircraft
CESSNA 414 · Type Certificate
Overview
This Advisory Circular (AC) provides updated noise level data for U.S. certificated and foreign aircraft, specifically focusing on compliance with 14 CFR Part 36 and ICAO Annex 16 standards. It includes revisions to previous appendices and presents noise levels for various aircraft types, including turbojet and propeller-driven airplanes. The document serves as a reference for both regulatory compliance and public awareness regarding aircraft noise levels. It is intended for use by aviation professionals, regulatory bodies, and the general public interested in aircraft noise impact.
- This document provides updated noise level data for U.S. certificated and foreign aircraft.
- It includes revisions to Appendices 1 and 8 related to noise levels for turbojet and propeller-driven airplanes.
- Noise levels are measured under 14 CFR Part 36 and ICAO Annex 16 standards.
- Appendices contain detailed tables with noise levels, maximum takeoff weights, and compliance stages.
- The document serves as a reference for regulatory compliance and public awareness regarding aircraft noise.
Document
Source
Originally published by www.faa.gov. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Type Certificate
- Year
- 2012
- Pages
- 364
- File size
- 6.1 MB
- Publisher
- www.faa.gov
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In this document
Purpose
The purpose of this Advisory Circular is to publish necessary updates to existing material regarding aircraft noise levels as a result of new submissions since the last publication. It revises specific appendices related to U.S. certificated turbojet powered airplanes and propeller-driven small airplanes.
Principal Changes
The document outlines the principal changes made to Appendices 1 and 8, which include updated noise level data for various aircraft types. These changes reflect the latest compliance with noise regulations.
Noise Levels
Noise levels for aircraft are measured during type certification under 14 CFR Part 36 and ICAO Annex 16. The document includes detailed tables showing noise levels for different aircraft configurations, including maximum takeoff weights and compliance stages.
Appendices Overview
The document contains multiple appendices that provide detailed noise level data for various categories of aircraft. Appendix 1 focuses on turbojet powered airplanes, while Appendix 8 covers propeller-driven small airplanes. Each appendix includes specific noise level measurements and compliance information.
Distribution
The document provides information on how to request additional copies and how to be added to the mailing list for future revisions of the Advisory Circular.
Full document text
U.S. Department of Transportation Federal Aviation Administration Advisory Circular SUBJECT: Noise Levels for U.S. Certificated and Foreign Aircraft Date: 05/25/2012 Initiated by: AEE-100 AC No: 36-1H Change 1 1. Purpose. a. This Advisory Circular (AC) publishes needed changes to the existing AC material as a result of additions of certificated aircraft noise levels submitted since the AC was published. b. This change revises Appendix 1, U.S Certificated Turbojet Powered Airplanes and Appendix 8, U.S. Certificated Propeller Driven Small Airplanes (14 CFR Part 16, Appendix G), and Appendix 8 Notes. c. The change number and the date of the changed material are shown at the top of each page in Appendix 1, Appendix 8, and Appendix 8 Notes.. 2. Principal Changes. Appendix 1, Appendix 8, and Appendix 8 Notes. 3. Website Availability. To access this AC electronically, go to http://www.faa.gov/regulations_policies/advisory_circulars/ PAGE CONTROL CHART Remove Pages Dated Insert Pages Dated Appendix 1 1 thru 53 Appendix 8 1 and 4 11/15/01 11/15/01 Appendix 1 1 thru 186 Appendix 8 1 thru 7 4/24/2012 4/24/2012 ~~ Advisoryu.s. Department of Transportation CircularFederal Aviation Administration Subject: Date: 11/15/01 Initiated by: AEE-100 AC No: 36-1H Change: NOISE LEVELS FOR U.S. CERTIFICATED AND FOREIGN AIRCRAFT 1. PURPOSE. This circular provides noise level data for aircraft certificated under 14 CFR part 36. Noise level data for foreign aircraft certificated to ICAO Annex 16 standards are also provided in a separate appendix for informational purposes. Other appendices list selected configurations of U.S. certificated aircraft and provide listings of noise levels ranked in descending order. 2. CANCELLATION. Advisory Circular 36-1G, Noise Levels for U.S. Certificated and Foreign Aircraft, dated August 27, 1997, is canceled. 3. BACKGROUND. The agency's regulatory program for aircraft noise requires the quantification of aircraft noise levels. Progress in the control and abatement of aircraft noise continues to be made to achieve further relief and protection to the public. This updated Advisory Circular, containing certificated aircraft noise· levels, will provide both private and public exposure to this progress, as well as offering a common noise level reference for potential future reductions. 4. NOISE LEVELS. Noise levels measured during type certification under 14 CFR part 36 and ICAO Annex 16 are presented in Appendices 1 through 11. Formulas for calculating the appropriate 14 CFR part 36 noise level requirements, as contained in sections C36.5, F36.301, G36.301, H36.305, and 136.305 follow the applicable appendix. Appendix 1 provides noise levels of turbojet powered airplanes, measured during type certification under 14 CFR part 36, Appendix C. This appendix includes tabulations of engine model, maximum takeoff weights, landing weights, flap settings, the "Stage" with which the airplane complies, and the measured noise in Effective Perceived Noise Level (EPNdB). Data are not presented for all of the maximum certificated takeoff weights for each airplane type. Rather, the data presented generally represent the highest and lowest maximum certificated takeoff weight. Airplane noise levels are shown as complying with either Stage 2 or Stage 3. A "Stage 2 airplane" means an airplane that has been shown under 14 CFR part 36 to comply with the Stage 2 noise levels prescribed in section C36.5 of Appendix C (including use of the applicable tradeoff provisions) and that does not comply with the requirements for a Stage 3 airplane. A "Stage 3 airplane" means an airplane that has been shown under 14 CFR part 36 to comply with Stage 3 noise levels prescribed in section C36.5 of Appendix C (including use of the applicable tradeoff provisions). FAA Form 1320-15 (4-82) Supersedes WA Form 1320-2 AC 36-1H 11/15/01 As required by Part 36, certification noise levels for approach are those which are most critical from a noise standpoint, for the airplane configurations used to show compliance with the landing requirements in the airworthiness regulations constituting the type certification basis of the airplane. Takeoff certification noise levels are presented for takeoff with thrust cutback unless there is an asterisk (*) in the "NOTES" column, in which case full takeoff thrust certification noise levels are presented. It should be noted that the sideline noise levels are generally presented for the current 450-meter distance. However, some four-engine airplane configurations were certificated to the earlier 650-meter standard; these configurations are denoted with a double asterisk (**) in the "NOTES" column. Since the original measurement locations and noise test conditions cited in 14 CFR part 36, on November 18, 1969, have been amended through the years, the noise levels contained herein are for the measurement locations and noise test conditions applicable at the time of certification. In each case, the measured data have been corrected to sea level, 77 OF, 70% relative humidity conditions using the procedures outlined in 14 CFR part 36. Specific information providing more detail on either the measurement locations or noise test conditions, if available, are indicated by the notes accompanying each listing. Blank spaces or lack of notes in the report indicate the data were not available. Appendix 2 provides noise levels of foreign turbojet powered airplanes certificated to ICAO Annex 16, Chapters 2 and 3. These noise levels are provided for informational purposes. Airplanes certificated to both 14 CFR part 36 and ICAO Annex 16 are only listed in Appendix l. Appendix 3 provides a listing of U.S. certificated Stage 3 turbojet powered airplanes. These airplanes are also included in Appendix 1. Appendix 4 and 5 represent selected listings of noise levels for turbojet powered airplanes certificated under 14 CFR part 36, Appendix C. Appendices 4 and 5 provide listings of takeoff and approach noise
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levels in EPNdB, respectively, in descending order. Representative models of each airplane are listed, using the maximum takeoff weight available. These listings are presented as a convenience in locating noise level data on specific airplane models. For a more detailed listing on variations of a representative model, see Appendix 1. Appendix 6 contains noise levels of propeller-driven transport category airplanes. Noise levels measured during type certification were obtained under 14 CFR part 36, Appendix C. This appendix includes tabulations of maximum takeoff weights, landing weights, engine type, horsepower, propeller type, propeller diameter, and flap settings. The "Stage" with which the airplane complies is also provided, as well as the Effective Perceived Noise Level (EPNdB). Appendix 7 lists the certificated airplane noise levels for propeller-driven small airplanes certificated under 14 CFR part 36, Appendix F. This appendix includes a tabulation of maximum takeoffweights, landing weights, engine type, horsepower, propeller type, and propeller diameter. The measured A-weighted sound levels (dBA) for flyovers have been corrected to sea level 77 OF, 70% relative humidity conditions where required by 14 CFR part 36, Appendix F. Page 2 . Burleson 11115/01 AC 36-1H Appendix 8 lists the certificated airplane noise levels for propeller-driven small airplanes and commuter category airplanes certificated under 14 CFR part 36, Appendix G. This appendix includes a tabulation of maximum takeoff weights, landing weights, engine type, horsepower, propeller type and propeller diameter, and the noise level in dB(A). Note that the 14 CFR part 36, Appendix G noise certification requirements for propeller-driven small airplanes and commuter category airplanes superseded those of 14 CFR part 36, Appendix F for noise certification tests conducted on or after December 22, 1988. Appendix 9 contains noise levels for propeller-driven small airplanes certificated under ICAO Annex 16, Chapter 6. These noise levels are listed for informational purposes. Appendix 10 lists the certificated noise levels for helicopters certificated under 14 CFR part 36, Appendix H. Helicopter noise levels are classified as either Stage 1 or Stage 2. A II Stage 2" helicopter means a helicopter that has been shown under 14 CFR part 36 to comply with the Stage 2 noise levels prescribed in section H36.305 of Appendix H (including use of applicable tradeoff provisions). Appendix 11 lists the certificated noise levels for helicopters certificated under 14 CFR part 36, Appendix J. Appendix J prescribes alternative (to 14 CFR part 36 Appendix H) noise certification requirements for helicopters in the primary, normal, transport, and restricted categories having maximum certificated takeoff weight of not more than 6,000 pounds. Appendix 12 defines the abbreviations that are used in this Advisory Circular. 5. Distribution. Requests for additional copies of this Advisory Circular should be sent to: u.s. Department of Transportation Subsequent Distribution Office Ardmore East Business Center 3341 Q 75th Avenue Landover, MD 20785 Requests to be placed on the mailing list to receive future revisions of this Advisory Circular should be sent to: u.S. Department of Transportation Distribution Requirements Section SVC-121.21 Washington, DC 20590. 6. REVISIONS. This Advisory Circular will be revised and updated periodically. 'irector, of Environment and Energy Page 3 AC 36-1H 11/15/01 LIST OF APPENDICES Appendix 1 Appendix 2 Appendix 3 Appendix 4 Appendix 5 Appendix 6 Appendix 7 Appendix 8 Appendix 9 Appendix 10 Appendix 11 Appendix 12 Aircraft Noise Data for United States Certificated Turbojet Powered Airplanes Aircraft Noise Data for Foreign Certificated Turbojet Powered Airplanes Stage 3 Turbojet Powered Airplanes Aircraft Noise Certification Levels in Descending EPNdB for US. Certificated Turbojet Powered Airplanes - Takeoff Aircraft Noise Certification Levels in Descending EPNdB for US. Certificated Turbojet Powered Airplanes - Approach Aircraft Noise Data for Propeller Driven Airplanes Certificated in the Transport Category Aircraft Noise Data for US. Certificated Propeller Driven Small Airplanes (14 CFRPart 36, Appendix F) Aircraft Noise Data for US. Certificated Propeller Driven Small Airplanes and Commuter Category Airplanes (14 CFR part 36, Appendix G) ; Aircraft Noise Data for Foreign Certificated Propeller Driven Small Airplanes Aircraft Noise Data for US. Certificated Helicopters (14 CFR part 36, Appendix H) Aircraft Noise Data for US. Certificated Helicopters (14 CFR part 36, Appendix J) Abbreviations Page 4 04/24/2012 MANUFACTURER AEROSPATIALE MODEL SN601 CORVETTE 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 13.90 12.40 JT15D-4 2 2.50 2.68 TO AP FLAPS 15 35 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 80.4 85.4 89.5 3 * AEROSPATIALE SN601 CORVETTE 14.60 13.20 JT15D-4 2 2.50 2.68 15 35 74.0 81.0 90.0 3 AIRBUS A300 B4-605R 330.40 290.00 CF6-80C2A5F 2 61.50 5.00 0 40 87.4 98.8 99.5 3 AIRBUS A300 B4-605R 385.46 319.38 CF6-80C2A5F 2 61.50 5.00 0 40 91.5 98.5 100.0 3 AIRBUS A300B2-1C 291.00 268.00 CF6-50C2-R 2 50.40 4.40 0 25 89.9 97.5 102.9 3 AIRBUS A300B2-1C 313.00 286.60 CF6-50C2-R 2 50.40 4.40 0 25 91.8 97.4 103.1 3 Page 1 04/24/2012 MANUFACTURER AIRBUS MODEL A300B2-203 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 313.10 286.60 CF6-50-C2 2 51.80 4.30 TO AP FLAPS 16 25 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 91.1 97.9 103.1 3 AIRBUS A300B4-103 347.20 295.40 CF6-50-C2 2 51.80 4.30 16 25 93.6 97.7 103.0 3 AIRBUS A300B4-203 313.05 286.60 CF6-50C2 2 51.80 4.30 0 25 90.5 97.3 102.4 3 31 AIRBUS A300B4-203 363.70 299.83 CF6-50-C2 2 51.80 4.30 0 25 94.0 96.9 102.4 3 31 AIRBUS A300B4-622R 330.00 275.00 PW-4158 2 58.00 4.85 0 40 88.0 98.3 101.3 3 AIRBUS A300B4-622R 385.00 304.50 PW-4158 2 58.00 4.85 0 40 93.1 97.9 101.9 3 Page 2 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES AIRBUS A310-221 305.60 267.90 JT9D-7R4D1 2 48.00 4.50 15 40 90.5 94.8 100.6 3 AIRBUS A310-304 275.58 261.25 CF6-80C2A2 2 53.50 5.00 0 40 85.7 96.5 98.5 3 AIRBUS A310-304 352.74 286.60 CF6-80C2A2 2 53.50 5.00 0 40 92.9 96.1 98.8 3 AIRBUS A310-324 330.69 271.16 PW-4152 2 52.00 4.85 15 40 90.6 97.2 100.2 3 AIRBUS A318-111 123.46 123.46 CFM56-5B8/P 2 21.60 6.00 10 40 79.1 91.1 93.8 3 AIRBUS A318-111 149.91 126.77 CFM56-5B8/P 2 21.60 6.00 10 40 84.1 90.4 93.9 3 Page 3 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER AIRBUS MODEL A318-112 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 130.07 123.46 CFM56-5B9/P 2 23.30 5.90 TO AP FLAPS 10 40 TO SL AP NOISE LEVEL (EPNdB) 79.4 92.3 93.8 STAGE 3 NOTES AIRBUS A318-112 149.91 126.77 CFM56-5B9/P 2 23.30 5.90 10 40 83.0 91.9 93.9 3 AIRBUS A319-111 136.69 134.48 CFM56-5B/P w/ Mod No. 2 22.00 5.90 10 40 80.5 91.1 93.2 3 27772 and w/ or w/o Mod No. 38770 (HPC upgrade Kit) or CFM56-5B5/3 (Mod No. 37147) w/ Mod No. 27772 AIRBUS A319-111 136.69 134.48 CFM56-5B5 2 22.00 5.90 10 40 81.0 91.5 92.4 4 AIRBUS A319-111 136.69 134.48 CFM56-5B5/P Mod No. 2 22.00 5.90 10 40 81.2 91.8 93.4 4 25800 w or w/o Mod No. 38770 or CFM56-5B5/3 (Mod No. 37147) AIRBUS A319-111 168.65 137.79 CFM56-5B/P w/ Mod No. 2 22.00 5.90 10 40 87.8 90.0 93.5 4 27772 and w/ or w/o Mod No. 38770 (HPC upgrade Kit) or CFM56-5B5/3 (Mod No. 37147) w/ Mod No. 27772 Page 4 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MANUFACTURER AIRBUS MODEL A319-111 1000# MTOW 168.65 1000# MLW 137.79 ENGINE MODEL CFM56-5B5 NO. 2 THRUST 1000# 22.00 BPR 5.90 TO AP FLAPS 10 40 TO SL AP NOISE LEVEL (EPNdB) 88.2 90.5 92.6 STAGE 4 NOTES AIRBUS A319-111 168.65 137.79 CFM56-5B5/P Mod No. 2 22.00 5.90 10 40 88.7 90.6 93.6 4 25800 w or w/o Mod No. 38770 or CFM56-5B5/3 (Mod No. 37147) AIRBUS A319-112 123.45 121.25 CFM56-5B6/P 2 23.50 6.00 10 40 78.5 93.2 93.7 3 AIRBUS A319-112 136.69 134.48 CFM56-5B6 2 23.50 6.00 10 40 80.4 92.4 92.4 4 AIRBUS A319-112 136.69 134.48 CFM56-5B6/2P w/ Mod No. 2 23.50 6.00 10 40 81.5 93.3 94.2 4 25800 & 25530 AIRBUS A319-112 136.69 134.48 CFM56-5B6/2P w/ Mod No. 2 23.50 6.00 10 40 80.8 92.4 93.9 4 26610 and w/ or w/o Mod No. 27772 Page 5 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MANUFACTURER AIRBUS AIRBUS MODEL A319-112 A319-112 1000# MTOW 136.69 136.69 1000# MLW 134.48 134.48 ENGINE MODEL CFM56-5B6/P Mod No. 27772 and/or CFM56-5B6/3 Mod No. 37147 w/ Mod No. 27772, w or w/o Mod No. 28342 CFM56-5B6/P w or w/o Mod No. 38770 or CFM56- 5B6/3 (Mod No. 37147) NO. 2 2 THRUST 1000# 23.50 23.50 BPR 6.00 6.00 TO AP FLAPS 10 40 10 40 TO SL AP NOISE LEVEL (EPNdB) 80.4 92.2 93.5 81.0 92.9 93.4 STAGE 4 4 NOTES AIRBUS A319-112 168.65 137.79 CFM56-5B6 2 23.50 6.00 10 40 87.0 91.8 92.6 4 AIRBUS A319-112 168.65 137.79 CFM56-5B6/2P w/ Mod No. 25800 & 25530 2 23.50 6.00 10 40 87.8 92.6 94.5 4 AIRBUS A319-112 168.65 137.79 CFM56-5B6/2P w/ Mod No. 26610 and w/ or w/o Mod No. 27772 2 23.50 6.00 10 40 87.0 91.7 94.0 4 AIRBUS A319-112 168.65 137.79 CFM56-5B6/P Mod No. 27772 and/or CFM56-5B6/3 Mod No. 37147 w/ Mod No. 27772, w or w/o Mod No. 28342 2 23.50 6.00 10 40 86.9 91.4 93.7 4 Page 6 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER AIRBUS MODEL A319-112 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 168.65 137.79 CFM56-5B6/P w or w/o Mod No. 38770 or CFM56- 5B6/3 (Mod No. 37147) 2 23.50 6.00 TO AP FLAPS 10 40 TO SL AP NOISE LEVEL (EPNdB) 87.7 92.2 93.6 STAGE 4 NOTES AIRBUS A319-112 166.44 149.91 CFM56-5B6/P 2 23.50 6.00 10 40 86.3 92.0 94.4 3 AIRBUS A319-113 123.46 121.25 CFM56-5A4 2 22.00 6.00 10 40 80.1 93.9 94.0 3 AIRBUS A319-113 136.69 134.48 CFM56-5A4 w/ Mod No. 22495 2 22.00 6.00 10 40 81.6 93.1 94.5 4 AIRBUS A319-113 168.65 137.79 CFM56-5A4 w/ Mod No. 22495 2 22.00 6.00 10 40 89.0 91.9 94.6 4 AIRBUS A319-113 158.73 149.91 CFM56-5A4 2 22.00 6.00 10 40 87.5 93.1 94.8 3 Page 7 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER AIRBUS MODEL A319-114 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 123.45 121.25 CFM56-5A5 2 23.50 6.00 TO AP FLAPS 10 40 TO SL AP NOISE LEVEL (EPNdB) 79.5 94.9 94.0 STAGE 3 NOTES AIRBUS A319-114 136.69 134.48 CFM56-5A5 w/ Mod No. 22495 2 23.50 6.00 10 40 80.9 94.2 94.5 4 AIRBUS A319-114 168.65 137.79 CFM56-5A5 w/ Mod No. 22495 2 23.50 6.00 10 40 87.4 93.5 94.6 4 AIRBUS A319-114 163.14 149.91 CFM56-5A5 2 23.50 6.00 10 40 86.8 94.2 94.8 3 AIRBUS A319-115 136.69 134.48 CFM56-5B7 and/or CFM56- 5B7/P and/or CFM56-5B7/3, w or w/o Mod No. 28342 2 27.00 10 40 78.8 95.0 93.5 4 AIRBUS A319-115 168.65 137.79 CFM56-5B7 and/or CFM56- 5B7/P and/or CFM56-5B7/3, w or w/o Mod No. 28342 2 27.00 10 40 85.1 94.2 93.7 4 Page 8 MANUFACTURER 04/24/2012 AIRBUS MODEL A319-131 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 123.46 121.25 V2522-A5 2 22.00 4.90 TO AP FLAPS 10 40 TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 79.2 92.5 94.0 3 AIRBUS A319-131 136.69 134.48 IAE V2522-A5 w or w/o Mod No. 37868 2 22.00 4.90 10 40 80.2 91.5 94.2 4 AIRBUS A319-131 168.65 137.79 IAE V2522-A5 w or w/o Mod No. 37868 2 22.00 4.90 10 40 86.6 90.5 94.3 4 AIRBUS A319-131 158.73 149.91 V2522-A5 2 22.00 4.90 10 40 85.3 91.4 94.5 3 AIRBUS A319-132 123.45 121.25 V2524-A5 2 23.50 4.90 10 40 78.5 93.0 94.0 3 AIRBUS A319-132 136.69 134.48 IAE V2524-A5 w or w/o Mod No. 28342 2 23.50 4.80 10 40 79.5 92.2 94.3 4 Page 9 MANUFACTURER 04/24/2012 AIRBUS MODEL A319-132 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 168.65 137.79 IAE V2524-A5 w or w/o Mod No. 28342 2 23.50 4.80 TO AP FLAPS 10 40 TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 85.5 91.3 94.4 4 AIRBUS A319-132 166.40 149.91 V2524-A5 2 23.50 4.90 10 40 85.9 91.9 94.5 3 AIRBUS A319-133 136.69 134.48 IAE V2527-A5 w or w/o Mod No. 28342 2 26.50 10 40 78.9 93.0 94.3 4 AIRBUS A319-133 168.65 137.79 IAE V2527-A5 w or w/o Mod No. 28342 2 26.50 10 40 84.6 92.5 94.4 4 AIRBUS A320-211 162.00 142.20 CFM56-5A1 2 25.00 6.00 10 35 87.8 94.3 96.4 3 AIRBUS A320-211 149.90 142.20 CFM56-5A1 2 25.00 6.00 10 35 85.3 94.4 96.4 3 Page 10 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES AIRBUS A320-214 132.16 127.80 CFM56-5B4/P 2 27.00 5.90 10 35 78.8 95.2 95.5 3 AIRBUS A320-214 182.80 150.00 CFM56-5B4/P 2 27.00 5.90 10 35 88.0 93.7 95.8 3 AIRBUS A320-231 149.90 142.20 V2500.A1 2 25.00 6.00 10 40 84.0 93.0 96.6 3 AIRBUS A320-231 162.00 142.20 V2500.A1 2 25.00 6.00 10 40 86.6 92.8 96.6 3 AIRBUS A320-232/233 145.51 142.20 (A320-232 Mod No. 34041) 2 26.50 4.80 10 40 80.2 91.7 94.3 4 IAE V2527-A5 w or w/o Mod No. 37868 and (A320- 233 Mod No. 34041) IAE V2527E-A5 w or w/o Mod No. 37868 AIRBUS A320-232/233 145.51 142.20 (A320-232) IAE V2527-A5 2 26.50 4.80 10 40 80.2 91.7 94.3 4 w or w/o Mod No. 37868 and (A320-233) IAE V2527E-A5 w or w/o Mod No. 37868 Page 11 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW MANUFACTURER MODEL 1000# 1000# ENGINE MODEL AIRBUS A320-232/233 171.96 145.51 (A320-232 Mod No. 34041) IAE V2527-A5 w or w/o Mod No. 37868 and (A320- 233 Mod No. 34041) IAE V2527E-A5 w or w/o Mod No. 37868 AIRBUS A320-232/233 171.96 145.51 (A320-232) IAE V2527-A5 w or w/o Mod No. 37868 and (A320-233) IAE V2527E-A5 w or w/o Mod No. 37868 AIRBUS A321-111 171.96 162.04 CFM56-5B1/2P DAC II C w/ Mod. No. 25800 and 26610, w or w/o Mod No. 27772 NO. 2 THRUST 1000# 26.50 BPR 4.80 TO AP FLAPS 10 40 TO SL AP NOISE LEVEL (EPNdB) 84.9 91.3 94.4 STAGE 4 NOTES 2 26.50 4.80 10 40 84.9 91.3 94.4 4 2 30.00 5.70 10 25 84.8 96.1 96.8 4 AIRBUS A321-111 171.96 162.04 CFM56-5B1/P and/or 5B1/3 2 30.00 5.70 10 25 83.8 94.4 96.1 4 w/ basic NIP (Mod No. 32871, 33987) AIRBUS A321-111 171.96 162.04 CFM56-5B1/P w/ Mod No. 2 30.00 5.70 10 25 84.3 96.1 96.5 4 27772 (w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56-5B1/3 (Mod No. 37147) w/ Mod No. 27772 AIRBUS A321-111 171.96 162.04 CFM56-5B1/P w/ or w/o 2 30.00 5.70 10 25 84.9 96.7 96.6 4 Mod No. 38770 (HPC Upgrade Kit)) or CFM56- 5B1/3 (Mod No. 37147) Page 12 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MANUFACTURER AIRBUS AIRBUS MODEL A321-111 A321-111 1000# MTOW 196.21 196.21 1000# MLW 166.45 166.45 ENGINE MODEL CFM56-5B1/2P DAC II C w/ Mod. No. 25800 and 26610, w or w/o Mod No. 27772 CFM56-5B1/P and/or 5B1/3 w/ basic NIP (Mod No. 32871, 33987) NO. 2 2 THRUST 1000# 30.00 30.00 BPR 5.70 5.70 TO AP FLAPS 10 25 10 25 TO SL AP NOISE LEVEL (EPNdB) 89.1 95.6 96.9 87.8 93.9 96.3 STAGE 4 4 NOTES AIRBUS AIRBUS AIRBUS A321-111 A321-111 A321-112 196.21 196.21 171.96 166.45 166.45 162.04 CFM56-5B1/P w/ Mod No. 27772 (w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56-5B1/3 (Mod No. 37147) w/ Mod No. 27772 CFM56-5B1/P w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56- 5B1/3 (Mod No. 37147) CFM56-5B2 2 2 2 30.00 30.00 31.00 5.70 5.70 5.60 10 10 10 25 25 25 88.8 89.5 84.3 95.6 96.2 95.8 96.6 96.8 95.7 4 3 4 AIRBUS A321-112 171.96 162.04 CFM56-5B2/P w/ Mod No. 27772 (w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56-5B2/3 (Mod No. 37147) w/ Mod No. 27772 2 31.00 5.60 10 25 84.1 96.7 96.5 4 Page 13 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MANUFACTURER AIRBUS AIRBUS MODEL A321-112 A321-112 1000# MTOW 171.96 196.21 1000# MLW 162.04 166.45 ENGINE MODEL CFM56-5B2/P w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56- 5B2/3 (Mod No. 37147) CFM56-5B2 NO. 2 2 THRUST 1000# 31.00 31.00 BPR 5.60 5.60 TO AP FLAPS 10 25 10 25 TO SL AP NOISE LEVEL (EPNdB) 84.7 97.3 96.6 88.6 95.4 95.9 STAGE 3 4 NOTES AIRBUS AIRBUS AIRBUS A321-112 A321-112 A321-211 196.21 196.21 165.34 166.45 166.45 143.29 CFM56-5B2/P w/ Mod No. 27772 (w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56-5B2/3 (Mod No. 37147) w/ Mod No. 27772 CFM56-5B2/P w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56- 5B2/3 (Mod No. 37147) CFM56-5B3/P; Mod. No. 27772 2 2 2 31.00 31.00 32.00 5.60 5.60 5.60 10 10 25 25 25 88.4 89.2 82.9 96.2 96.8 97.9 96.6 96.8 95.6 4 3 3 AIRBUS A321-211 205.02 171.51 CFM56-5B3/P; Mod. No. 27772 2 32.00 5.60 25 89.8 97.5 96.6 3 Page 14 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MANUFACTURER AIRBUS MODEL A321-212 1000# MTOW 171.96 1000# MLW 162.04 ENGINE MODEL CFM56-5B1/2P DAC II C w/ Mod. No. 25800 and 26610, w or w/o Mod No. 27772 NO. 2 THRUST 1000# 30.00 BPR 5.60 TO AP FLAPS 10 25 TO SL AP NOISE LEVEL (EPNdB) 84.8 96.1 96.8 STAGE 4 NOTES AIRBUS A321-212 171.96 162.04 CFM56-5B1/P and/or 5B1/3 w/ basic NIP (Mod No. 32871, 33987) 2 30.00 5.60 10 25 83.8 94.4 96.1 4 AIRBUS AIRBUS A321-212 A321-212 171.96 171.96 162.04 162.04 CFM56-5B1/P w/ Mod No. 27772 (w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56-5B1/3 (Mod No. 37147) w/ Mod No. 27772 CFM56-5B1/P w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56- 5B1/3 (Mod No. 37147) 2 2 30.00 30.00 5.60 5.60 10 10 25 25 84.3 84.9 96.1 96.7 96.5 96.6 4 4 AIRBUS A321-212 206.13 171.52 CFM56-5B1/2P DAC II C w/ Mod. No. 25800 and 26610, w or w/o Mod No. 27772 2 30.00 5.60 10 25 91.1 95.1 97.0 3 AIRBUS A321-212 206.13 171.52 CFM56-5B1/P and/or 5B1/3 w/ basic NIP (Mod No. 32871, 33987) 2 30.00 5.60 10 25 89.5 93.4 96.6 4 Page 15 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MANUFACTURER MODEL 1000# MTOW 1000# MLW ENGINE MODEL NO. THRUST 1000# BPR TO AP FLAPS TO SL AP NOISE LEVEL (EPNdB) STAGE NOTES AIRBUS A321-212 206.13 171.52 CFM56-5B1/P w/ Mod No. 27772 (w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56-5B1/3 (Mod No. 37147) w/ Mod No. 27772 2 30.00 5.60 10 25 90.9 95.1 96.8 3 AIRBUS A321-212 206.13 171.52 CFM56-5B1/P w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56- 5B1/3 (Mod No. 37147) 2 30.00 5.60 10 25 91.6 91.8 97.0 3 AIRBUS A321-213 171.96 162.04 CFM56-5B2/P w/ Mod No. 2 31.00 5.60 10 25 84.1 96.7 96.5 4 27772 (w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56-5B2/3 (Mod No. 37147) w/ Mod No. 27772 AIRBUS A321-213 171.96 162.04 CFM56-5B2/P w/ or w/o 2 31.00 5.60 10 25 84.7 97.3 96.6 3 Mod No. 38770 (HPC Upgrade Kit)) or CFM56- 5B2/3 (Mod No. 37147) AIRBUS A321-213 206.13 171.52 CFM56-5B2/P w/ Mod No. 2 31.00 5.60 10 25 90.3 96.1 96.8 3 27772 (w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56-5B2/3 (Mod No. 37147) w/ Mod No. 27772 AIRBUS A321-213 206.13 171.52 CFM56-5B2/P w/ or w/o 2 31.00 5.60 10 25 91.0 96.7 97.0 3 Mod No. 38770 (HPC Upgrade Kit)) or CFM56- 5B2/3 (Mod No. 37147) Page 16 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES AIRBUS A321-231 165.34 143.29 V2533A5 2 33.00 4.46 25 81.8 95.6 95.1 3 AIRBUS A321-231 205.02 171.51 V2533A5 2 33.00 4.46 25 88.2 95.2 95.8 3 AIRBUS A330-301 396.83 361.56 CF6-80E1A2 2 65.80 5.05 14 32 87.0 97.9 98.5 3 AIRBUS A330-301 507.06 418.88 CF6-80E1A2 2 65.80 5.05 14 32 94.2 97.2 98.7 3 AIRBUS A330-321 396.83 330.69 PW4164 2 64.00 4.85 8 32 88.5 98.0 97.3 3 AIRBUS A330-321 507.06 418.88 PW4164 2 64.00 4.85 8 32 95.6 97.5 98.0 3 Page 17 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES AIRBUS A330-322 396.83 330.69 PW4168 2 68.00 4.85 8 32 87.6 98.6 97.3 3 AIRBUS A330-322 507.06 418.88 PW4168 2 68.00 4.85 8 32 94.3 98.3 98.0 3 AIRBUS A340-212 485.01 363.76 CFM56-5C3 4 32.50 6.60 17 32 88.1 95.8 97.3 3 AIRBUS A340-212 595.25 440.92 CFM56-5C3 4 32.50 6.60 17 32 96.1 95.4 97.2 3 AIRBUS A340-312 485.02 363.76 CFM56-5C3 4 32.50 6.60 17 32 88.0 95.8 97.3 3 AIRBUS A340-312 595.24 440.92 CFM56-5C3 4 32.50 6.60 17 32 96.2 95.3 97.2 3 Page 18 MANUFACTURER 04/24/2012 AIRBUS MODEL A340-541 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 672.41 485.02 RR TRENT 553 4 55.78 7.70 TO AP FLAPS 17 34 TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 88.9 95.7 99.3 3 AIRBUS A340-541 870.83 595.25 RR TRENT 553 4 55.78 7.70 17 34 96.9 94.9 99.5 3 AIRBUS A380-841 1254.43 862.01 RR TRENT 970 4 78.30 8.70 8 23 94.8 95.2 98.0 4 AIRBUS A380-841 1254.40 862.01 RR TRENT 970 w/ Post TC Mod No. 65283 4 78.30 8.70 8 23 95.6 94.2 98.0 4 AIRBUS A380-841 1124.36 868.62 RR TRENT 970 4 78.30 8.70 8 23 91.2 95.2 98.0 4 AIRBUS A380-841 1124.40 868.62 RR TRENT 970 w/ Post TC Mod No. 65283 4 78.30 8.70 8 23 91.9 94.6 98.1 4 Page 19 MANUFACTURER 04/24/2012 AIRBUS MODEL A380-842 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 1254.43 862.01 RR TRENT 972 4 80.21 8.60 TO AP FLAPS 8 23 TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 94.3 95.3 98.0 4 AIRBUS A380-842 1254.40 862.01 RR TRENT 972 w/ Post TC Mod No. 65283 4 80.21 8.60 8 23 95.1 94.6 98.0 4 AIRBUS A380-842 1124.36 868.62 RR TRENT 972 4 80.21 8.60 8 23 90.9 95.6 98.0 4 AIRBUS A380-842 1124.40 868.62 RR TRENT 972 w/ Post TC Mod No. 65283 4 80.21 8.60 8 23 91.5 94.9 98.1 4 AIRBUS UK 1-11 200 80.00 71.00 SPEY 506-14 2 10.40 1.00 3 45 93.3 99.1 97.8 2 12 AIRBUS UK 1-11 400 87.00 77.20 SPEY511-14/14W 2 11.40 0.70 0 45 94.8 103.4 99.7 2 12 Page 20 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES AIRBUS UK 1-11 400 89.50 79.00 SPEY511-14/14W 2 11.40 0.70 0 45 95.7 103.3 99.9 2 12 AIRBUS UK 1-11 400 (QTV STC: ST02167AT) 81.90 78.00 SPEY511-14/14W 2 11.40 0.70 26 90.0 96.2 93.8 3 BAE SYSTEMS (AVRO) 146-RJ 100 95.00 83.00 LF 507-1F 4 7.00 5.10 18 33 83.8 88.3 97.2 3 BAE SYSTEMS (AVRO) 146-RJ 100 101.50 88.50 LF 507-1F 4 7.00 5.10 18 33 86.1 88.1 97.6 3 BAE SYSTEMS (AVRO) 146-RJ 70 84.00 83.50 LF 507-1F 4 6.13 5.10 18 33 81.9 87.2 97.5 3 BAE SYSTEMS (AVRO) 146-RJ 70 95.00 83.50 LF 507-1F 4 7.00 5.10 18 33 83.6 88.6 97.5 3 4 Page 21 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BAE SYSTEMS (AVRO) 146-RJ 70 84.00 83.50 LF 507-1F 4 7.00 5.10 18 33 80.2 89.1 97.5 3 4 BAE SYSTEMS (AVRO) 146-RJ 70 90.00 83.50 LF 507-1F 4 6.13 5.10 18 33 84.1 86.9 97.5 3 BAE SYSTEMS (AVRO) 146-RJ 85 89.50 77.50 LF 507-1F 4 7.00 5.10 18 33 81.9 88.7 96.9 3 BAE SYSTEMS (AVRO) 146-RJ 85 97.00 85.00 LF 507-1F 4 7.00 5.10 18 33 84.3 88.4 97.3 3 BAE SYSTEMS (BAe) 146-100A 76.00 72.35 ALF502R-3 4 6.70 5.90 18 33 80.7 87.2 95.1 3 BAE SYSTEMS (BAe) 146-100A 76.00 72.35 ALF502R-3A 4 6.70 5.90 18 33 79.0 88.0 94.9 3 Page 22 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BAE SYSTEMS (BAe) 146-100A 82.25 73.35 ALF502R-3A 4 6.70 5.90 18 33 82.3 87.6 95.2 3 BAE SYSTEMS (BAe) 146-100A 82.25 73.35 ALF502R-5 4 6.97 5.70 18 33 82.3 87.6 95.2 3 BAE SYSTEMS (BAe) 146-100A 84.00 77.50 ALF502R-5 4 6.97 5.70 18 33 81.8 87.7 95.6 3 BAE SYSTEMS (BAe) 146-200A 89.50 77.50 ALF502R-3 4 6.97 5.90 18 33 85.9 86.6 95.6 3 BAE SYSTEMS (BAe) 146-200A 89.50 77.50 ALF502R-3A 4 6.70 5.90 18 33 84.9 87.3 95.6 3 BAE SYSTEMS (BAe) 146-200A 89.50 77.50 ALF502R-5 4 6.97 5.70 18 33 84.9 87.3 95.6 3 Page 23 04/24/2012 MANUFACTURER BAE SYSTEMS (BAe) MODEL 146-200A 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 93.00 81.00 ALF502R-5 4 6.97 5.70 TO AP FLAPS 18 33 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 85.2 87.3 95.8 3 BAE SYSTEMS (BAe) 146-300 95.00 83.00 LF 507-1H/-1F 4 7.00 5.10 18 33 84.0 87.9 97.2 3 BAE SYSTEMS (BAe) 146-300 101.50 88.50 LF 507-1H/-1F 4 7.00 5.10 18 33 86.3 87.6 97.6 3 BAE SYSTEMS (BAe) 146-300A 95.00 83.00 ALF 502R-5 4 6.97 5.70 18 33 86.0 87.0 96.0 3 BAE SYSTEMS (BAe) 146-300A 97.50 84.50 ALF502R-5 4 6.97 5.70 18 33 86.5 86.7 95.6 3 BEECH BEECHJET 400 15.78 14.22 JT15D-5 2 2.90 2.10 10 30 88.6 93.7 91.4 3 * Page 24 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL 727-100RE (RHOR STC SA4363NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 174.50 142.50 JT8D-217C/JT8D-7 3 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 88.4 98.0 95.5 STAGE 3 NOTES BOEING 727-100RE (RHOR STC SA4363NM) 169.50 142.50 JT8D-217C/JT8D-7 3 5 30 87.4 98.0 95.5 3 BOEING 727-100RE (RHOR STC SA4363NM) 169.50 142.50 JT8D-217C/JT8D-9 3 5 30 87.3 98.1 95.5 3 BOEING 727-100RE (RHOR STC SA4363NM) 174.50 142.50 JT8D-217C/JT8D-9 3 5 30 88.3 98.0 95.5 3 BOEING 727-100RE (RHOR STC SA4363NM) 174.50 142.50 JT8D-219/JT8D-7 3 5 30 87.7 98.9 95.5 3 BOEING B-707-100B (BAC II STC: ST00956LA) 200.00 160.00 JT3D-1 4 17.00 1.40 20 30 95.5 99.5 101.1 3 12 Page 25 04/24/2012 MANUFACTURER BOEING MODEL B-707-100B (QNC) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 241.30 190.00 JT3D-1 4 TO AP FLAPS 30 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 103.4 102.8 102.8 2 6,** BOEING B-707-100B (QNC) 258.00 190.00 JT3D-3B 4 18.00 1.40 30 103.8 102.7 102.8 2 6,** BOEING B-707-120B (SHANNON) 258.00 190.00 JT3D-1 4 30 103.5 97.6 105.3 2 21,** BOEING B-707-138B (SHANNON) 258.00 190.00 JT3D-1 4 30 103.2 97.6 105.3 2 21,** BOEING B-707-300B ADV/C ( SHN) 322.30 247.00 JT3D-1-3B(IC) 4 14 25 105.5 99.3 105.7 2 6,21,** BOEING B-707-300B ADV/C (QNC) 335.00 247.50 JT3D-3B 4 18.00 1.40 25 104.4 98.9 107.9 2 6,** Page 26 04/24/2012 MANUFACTURER BOEING MODEL B-707-300B ADV/C (SHN) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 330.00 201.00 JT3D-7 4 19.00 1.40 TO AP FLAPS 25 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 104.7 99.6 108.3 2 6,** BOEING B-707-300B ADV/C (SHN) 321.00 240.00 JT3D-3B 4 18.00 1.40 25 104.5 99.2 108.2 2 6,** BOEING B-707-300B/C (QSI STC: ST00702LA) 215.00 190.00 JT3D-3B 4 18.00 1.40 14 25 96.2 99.6 101.4 3 12 BOEING B-707-300B/C (QSI STC: ST00702LA) 336.00 247.00 JT3D-3B 4 18.00 1.40 14 25 99.5 98.2 102.9 3 12 BOEING B-707-300B/C (QSI STC: ST00702LA) 336.00 247.00 JT3D-7 4 19.00 1.40 14 25 98.5 99.3 102.7 3 12 BOEING B-717-200 104.50 98.00 BR700-715A1-30 2 18.50 4.66 5 40 79.6 89.2 91.3 3 48 Page 27 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-717-200 104.50 98.00 BR700-715A1-30 (MP) 2 18.50 4.66 5 40 80.1 89.2 91.3 3 49 BOEING B-717-200 104.50 98.00 BR700-715C1-30 2 21.00 4.66 5 40 78.1 91.7 91.3 3 48 BOEING B-717-200 104.50 98.00 BR700-715C1-30 (MP) 2 21.00 4.66 5 40 78.7 91.7 91.3 3 49 BOEING B-717-200 121.00 110.00 BR700-715A1-30 2 18.00 4.66 5 40 84.0 89.0 91.6 3 48 BOEING B-717-200 121.00 110.00 BR700-715A1-30 (MP) 2 18.50 4.66 5 40 84.1 89.0 92.1 3 49 BOEING B-717-200 121.00 110.00 BR700-715C1-30 2 21.00 4.66 5 40 82.1 91.5 91.6 3 48 Page 28 MANUFACTURER 04/24/2012 BOEING MODEL B-717-200 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 121.00 110.00 BR700-715C1-30 (MP) 2 21.00 4.66 TO AP FLAPS 5 40 TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 82.2 91.5 92.1 3 49 BOEING B-720B (QNC) 234.00 175.00 JT3D-1 4 30 102.3 102.9 101.6 2 6,** BOEING B-720B (QNC) 234.00 175.00 JT3D-3B 4 18.00 1.40 30 99.3 103.2 101.6 2 6,** BOEING B-720B (SHANNON) 234.00 175.00 JT3D-1 4 30 98.9 98.0 104.7 2 6,** BOEING B-720B (SHANNON) 234.00 175.00 JT3D-3B 4 18.00 1.40 30 97.3 99.5 104.7 2 6,** BOEING B-727-100 152.50 135.00 JT8D-7FCD 3 14.00 1.40 5 40 94.4 100.3 104.1 2 3,16 Page 29 MANUFACTURER 04/24/2012 BOEING MODEL B-727-100 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 169.50 137.50 JT8D-1FCD 3 14.00 1.10 TO AP FLAPS 5 40 TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 98.5 99.1 104.3 2 3 BOEING B-727-100 160.50 137.50 JT8D-1FCD 3 14.00 1.10 5 40 96.6 99.2 104.3 2 3 BOEING B-727-100 169.50 137.50 JT8D-7FCD 3 14.00 1.40 5 40 97.9 100.0 104.3 2 3,16 BOEING B-727-100 160.50 137.50 JT8D-9FCD 3 14.50 1.03 5 40 96.1 100.2 105.8 2 3,17 BOEING B-727-100 169.50 137.50 JT8D-9FCD 3 14.50 1.03 5 40 98.3 100.0 105.8 2 3,17 BOEING B-727-100 (Dee Howard) 169.50 137.50 TAY 651-54 3 15.40 5 40 92.1 92.3 98.4 3 Page 30 04/24/2012 MANUFACTURER BOEING MODEL B-727-100 (Dee Howard) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 169.50 142.50 TAY 651-54 3 15.40 TO AP FLAPS 5 30 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 92.1 92.3 95.3 3 BOEING B727-100 (DUGAN AIR STC) 160.50 142.50 JT8D-7 3 14.00 1.40 4 26 93.5 98.6 97.2 3 BOEING B727-100 (DUGAN AIR STC) 174.50 142.50 JT8D-7 3 14.00 1.40 4 26 95.9 99.0 97.2 3 BOEING B727-100 (FED EX; STC SA3993NM) 160.50 137.50 JT8D-7 w/BOEING INLET+CHIN CSD 3 14.00 1.40 5 30 92.5 96.6 97.8 3 35 BOEING B727-100 (FED EX; STC SA3993NM) 163.50 137.50 JT8D-7 w/BOEING INLET+FAN CSD 3 14.00 1.40 5 30 93.2 97.4 97.8 3 35 BOEING B727-100 (FED EX; STC SA3993NM) 169.50 137.50 JT8D-9 w/BOEING INLET+CHIN CSD 3 14.50 1.03 5 30 93.9 97.5 98.1 3 35 Page 31 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B727-100 (FED EX; STC SA3993NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 169.50 142.50 JT8D-7 w/BOEING INLET+FAN CSD 3 14.00 1.40 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 94.5 97.2 98.0 STAGE 3 NOTES 35 BOEING B727-100 (FED EX; STC SA3993NM) 169.50 142.50 JT8D-7 w/BURBANK INLET+ FAN CSD 3 14.00 1.40 5 30 94.1 97.2 98.2 3 35 BOEING B727-100 (FED EX; STC SA3993NM) 169.50 142.50 JT8D-7 w/BURBANK INLET+CHIN CSD 3 14.00 1.40 5 30 94.1 96.6 98.2 3 35 BOEING B727-100 (FED EX; STC SA3993NM) 174.50 142.50 JT8D-9 w/BOEING INLET+CHIN CSD 3 14.50 1.03 5 30 94.1 97.2 98.9 3 35 BOEING B727-100 (FED EX; STC SA3993NM) 169.50 142.50 JT8D-9 w/BOEING INLET+FAN CSD 3 14.50 1.03 5 30 93.9 98.0 98.4 3 35 BOEING B727-100 (FED EX; STC SA3993NM) 174.50 142.50 JT8D-9 w/BURBANK INLET+CHIN CSD 3 14.50 1.03 5 30 94.9 97.1 98.8 3 35 Page 32 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B727-100 (FED EX; STC SA3993NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 160.50 142.50 JT8D-9 w/BURBANK INLET+CHIN CSD 3 14.50 1.03 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 91.7 97.6 98.8 STAGE 3 NOTES 35 BOEING B727-100 (FED EX; STC SA3993NM) 175.50 154.50 JT8D-7 w/BOEING INLET+CHIN CSD 3 14.00 1.40 5 30 96.6 96.9 99.1 3 35 BOEING B727-100 (FED EX; STC SA3993NM) 175.50 154.50 JT8D-7 w/BURBANK INLET+CHIN CSD 3 14.00 1.40 5 30 96.3 96.0 99.1 3 35 BOEING B727-100 (RAISBECK STC ST00448SE) 172.60 142.50 JT8D-7 3 14.00 1.40 5 25 96.6 98.2 97.2 3 16,43 BOEING B727-100 RE (ROHR STC SA4363NM) 174.50 142.50 JT8D-217C/JT8D-9 3 5 30 89.4 98.0 95.4 3 23 BOEING B727-100 RE (ROHR STC SA4363NM) 160.50 142.50 JT8D-217C/JT8D-9 3 5 30 87.0 98.2 95.4 3 23 Page 33 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B727-100 RE (ROHR STC SA4363NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 169.50 142.50 JT8D-219/JT8D-7B 3 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 88.1 98.8 95.4 STAGE 3 NOTES 23 BOEING B727-100 RE (ROHR STC SA4363NM) 174.50 142.50 JT8D-219/JT8D-7B 3 5 30 89.0 98.8 95.4 3 23 BOEING B727-100 RE (ROHR STC SA4363NM) 169.50 142.50 JT8D-219/JT8D-9 3 5 30 88.0 98.9 95.4 3 23 BOEING B727-100 RE (ROHR STC SA4363NM) 174.50 142.50 JT8D-219/JT8D-9 3 5 30 88.8 98.8 95.4 3 23 BOEING B-727-200 184.20 142.50 JT8D-15QN 3 15.50 1.03 5 40 98.8 102.2 103.2 2 2,18 BOEING B-727-200 190.50 142.50 JT8D-15QN 3 15.50 1.03 5 40 100.0 102.2 103.2 2 2,18 Page 34 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-727-200 190.50 142.50 JT8D-17QN 3 16.00 1.01 5 40 99.6 103.7 103.2 2 2,19 BOEING B-727-200 190.50 142.50 JT8D-17RQN 3 17.40 0.97 5 40 98.9 104.7 103.2 2 2,20 BOEING B-727-200 208.00 142.50 JT8D-17RQN 3 17.40 0.97 5 40 102.4 104.2 103.2 2 2,20 BOEING B-727-200 177.60 142.50 JT8D-7FCD 3 14.00 1.40 5 40 99.8 99.8 106.3 2 3,16 BOEING B-727-200 172.50 142.50 JT8D-7FCD 3 14.00 1.40 15 40 100.0 100.4 106.3 2 3,16 BOEING B-727-200 172.50 142.50 JT8D-7QN 3 14.00 1.40 15 40 100.0 100.4 104.9 2 2,16 Page 35 04/24/2012 MANUFACTURER BOEING MODEL B-727-200 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 172.50 142.50 JT8D-9QN 3 14.50 1.03 TO AP FLAPS 15 40 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 99.0 100.4 103.2 2 2,17 BOEING B-727-200 184.80 142.50 JT8D-9QN 3 14.50 1.03 15 40 101.5 100.2 103.2 2 2,17 BOEING B-727-200 178.00 150.00 JT8D-9FCD 3 14.50 1.03 5 30 100.7 99.8 105.8 2 3,17 BOEING B-727-200 203.10 158.00 JT8D-17QN 3 16.00 1.01 5 40 102.0 103.5 104.5 2 2,19 BOEING B727-200 (DUGAN AIR STC) 209.41 164.00 JT8D-15 3 15.50 1.03 4 26 97.0 99.5 97.0 3 BOEING B727-200 (DUGAN AIR STC) 190.50 164.00 JT8D-15 3 15.50 1.03 4 26 94.9 99.2 97.0 3 Page 36 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B727-200 (DUGAN AIR STC) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 190.50 164.00 JT8D-9 3 14.50 1.03 TO AP FLAPS 4 26 TO SL AP NOISE LEVEL (EPNdB) 95.0 98.3 97.0 STAGE 3 NOTES BOEING B727-200 (FED EX; STC SA4833NM) 172.50 148.00 JT8D-9 w/BURBANK INLET+CHIN CSD 3 14.50 1.03 5 30 94.6 97.2 100.1 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 172.50 150.00 JT8D-7 w/BOEING INLET+CHIN CSD 3 14.00 1.40 5 30 95.9 96.3 99.0 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 172.50 150.00 JT8D-7 w/BOEING INLET+FAN CSD 3 14.00 1.40 5 30 95.9 97.0 99.0 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 172.50 150.00 JT8D-7 w/BURBANK INLET+ FAN CSD 3 14.00 1.40 5 30 95.6 96.5 98.9 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 172.50 150.00 JT8D-7 w/BURBANK INLET+CHIN CSD 3 14.00 1.40 5 30 95.6 95.8 98.9 3 35 Page 37 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B727-200 (FED EX; STC SA4833NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 169.50 150.00 JT8D-9 w/BURBANK INLET+ FAN CSD 3 14.50 1.03 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 94.1 97.8 100.2 STAGE 3 NOTES 35 BOEING B727-200 (FED EX; STC SA4833NM) 177.60 154.50 JT8D-7 w/BOEING INLET+CHIN CSD 3 14.00 1.40 5 30 95.2 97.3 99.0 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 177.60 154.50 JT8D-7 w/BOEING INLET+FAN CSD 3 14.00 1.40 5 30 95.2 97.9 99.0 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 178.42 154.50 JT8D-7 w/BURBANK INLET+CHIN CSD 3 14.00 1.40 5 30 97.0 96.0 99.1 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 177.60 154.50 JT8D-9 w/BOEING INLET+CHIN CSD 3 14.50 1.03 5 30 94.7 97.7 99.7 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 171.44 154.50 JT8D-9 w/BOEING INLET+CHIN CSD 3 14.50 1.03 5 30 94.9 97.6 99.9 3 35 Page 38 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B727-200 (FED EX; STC SA4833NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 165.60 154.50 JT8D-9 w/BOEING INLET+FAN CSD 3 14.50 1.03 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 93.7 98.4 99.9 STAGE 3 NOTES 35 BOEING B727-200 (FED EX; STC SA4833NM) 177.60 154.50 JT8D-9 w/BOEING INLET+FAN CSD 3 14.50 1.03 5 30 94.7 98.2 99.7 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 177.60 154.50 JT8D-9 w/BURBANK INLET+ FAN CSD 3 14.50 1.03 5 30 94.1 98.0 100.3 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 177.60 154.50 JT8D-9 w/BURBANK INLET+CHIN CSD 3 14.50 1.03 5 30 94.1 97.5 100.3 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 178.00 161.00 JT8D-7 w/BURBANK INLET+ FAN CSD 3 14.00 1.40 5 30 96.9 96.6 99.4 3 35 BOEING B727-200 (FED EX; STC SA5839NM) 155.00 150.00 JT8D-9 w/BOEING INLET+CHIN CSD 3 14.50 1.03 5 30 89.2 97.9 97.4 3 27 Page 39 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B727-200 (FED EX; STC SA5839NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 155.00 150.00 JT8D-9 w/BOEING INLET+FAN CSD 3 14.50 1.03 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 89.2 98.4 97.4 STAGE 3 NOTES 27 BOEING B727-200 (FED EX; STC SA5839NM) 155.00 150.00 JT8D-9 w/BURBANK INLET+ FAN CSD 3 14.50 1.03 5 30 88.5 98.1 98.0 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 155.00 150.00 JT8D-9 w/BURBANK INLET+CHIN CSD 3 14.50 1.03 5 30 88.5 97.6 98.0 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 160.00 154.50 JT8D-15 w/BOEING INLET+CHIN CSD 3 15.50 1.03 5 30 92.2 98.0 97.6 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 160.00 154.50 JT8D-15 w/BOEING INLET+FAN CSD 3 15.50 1.03 5 30 92.2 98.2 97.6 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 178.90 154.50 JT8D-15 w/BURBANK INLET+ FAN CSD 3 15.50 1.03 5 30 94.3 97.3 98.2 3 27 Page 40 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B727-200 (FED EX; STC SA5839NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 184.20 154.50 JT8D-17 w/BOEING INLET+CHIN OR FAN CSD 3 16.00 1.01 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 95.3 98.8 97.6 STAGE 3 NOTES 27 BOEING B727-200 (FED EX; STC SA5839NM) 184.20 154.50 JT8D-17 w/BURBANK INLET+CHIN OR FAN CSD 3 16.00 1.01 5 30 94.8 98.6 98.2 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 197.00 154.50 JT8D-17R w/BOEING INLET+CHIN OR FAN CSD 3 17.40 0.97 5 30 96.0 99.4 97.6 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 190.50 154.50 JT8D-17R w/BOEING INLET+CHIN OR FAN CSD 3 17.40 0.97 5 30 96.4 99.2 97.6 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 184.50 154.50 JT8D-17R w/BURBANK INLET+CHIN OR FAN CSD 3 17.40 0.97 5 30 94.8 99.1 98.2 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 204.50 159.00 JT8D-17 w/BURBANK INLET+CHIN OR FAN CSD 3 16.00 1.01 5 30 97.7 98.6 98.4 3 27 Page 41 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B727-200 (FED EX; STC SA5839NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 191.20 160.00 JT8D-9 w/BURBANK INLET+ FAN CSD 3 14.50 1.03 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 97.4 96.3 98.5 STAGE 3 NOTES 27 BOEING B727-200 (FED EX; STC SA5839NM) 191.20 160.00 JT8D-9 w/BURBANK INLET+CHIN CSD 3 14.50 1.03 5 30 97.4 95.7 98.5 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 197.50 161.00 JT8D-17R w/BURBANK INLET+CHIN OR FAN CSD 3 17.40 0.97 5 30 96.9 98.8 98.4 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 199.05 166.00 JT8D-15 w/BOEING INLET+CHIN CSD 3 15.50 1.03 5 30 97.6 98.0 98.1 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 199.05 166.00 JT8D-15 w/BOEING INLET+FAN CSD 3 15.50 1.03 5 30 97.6 98.2 98.1 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 201.00 166.00 JT8D-15 w/BURBANK INLET+ FAN CSD 3 15.50 1.03 5 30 97.7 97.6 98.6 3 27 Page 42 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B727-200 (FED EX; STC SA5839NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 203.10 166.00 JT8D-17 w/BOEING INLET+CHIN OR FAN CSD 3 16.00 1.01 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 96.8 99.1 98.0 STAGE 3 NOTES 27 BOEING B727-200 (FED EX; STC SA5839NM) 196.00 166.00 JT8D-9 w/BOEING INLET+CHIN CSD 3 14.50 1.03 5 30 97.5 96.1 98.0 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 196.00 166.00 JT8D-9 w/BOEING INLET+FAN CSD 3 14.50 1.03 5 30 97.5 96.6 98.0 3 27 BOEING B727-200 (RAISBECK STC ST00399SE) 166.40 153.30 JT8D-9 3 14.50 1.03 5 25 96.5 97.9 97.6 3 17,34,43 BOEING B727-200 (RAISBECK STC ST00555SE) 179.70 166.00 JT8D-9 3 14.50 1.03 5 30 97.0 97.6 97.2 3 34,44 BOEING B727-200 (RAISBECK STC ST00685SE) 193.00 161.00 JT8D-15 3 15.50 1.03 5 30 97.4 96.5 99.9 3 45 Page 43 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B-727-200 RE (ROHR STC SA4363NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 190.50 152.50 JT8D-219/JT8D-9 3 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 90.9 99.2 98.8 STAGE 3 NOTES 23,60 BOEING B-727-200 RE (ROHR STC SA4363NM) 184.00 156.00 JT8D-217C/JT8D-15 3 5 30 89.8 99.2 98.9 3 23,61 BOEING B-727-200 RE (ROHR STC SA4363NM) 184.00 156.00 JT8D-217C/JT8D-9 3 5 30 90.2 98.4 98.9 3 23,60 BOEING B-727-200 RE (ROHR STC SA4363NM) 190.50 159.00 JT8D-217C/JT8D-17 3 5 30 91.2 99.3 99.0 3 23,62 BOEING B-727-200 RE (ROHR STC SA4363NM) 197.00 159.00 JT8D-219/JT8D-15 3 5 30 92.8 99.5 99.0 3 7,23,64 BOEING B-727-200 RE (ROHR STC SA4363NM) 209.50 162.00 JT8D-217C/JT8D-17 3 5 30 95.2 99.2 99.0 3 23,62 Page 44 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B-727-200 RE (ROHR STC SA4363NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 198.50 162.00 JT8D-217C/JT8D-9 3 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 93.7 98.2 99.0 STAGE 3 NOTES 23,60 BOEING B-727-200 RE (ROHR STC SA4363NM) 198.70 162.00 JT8D-219/JT8D-15 3 5 30 92.7 99.4 99.0 3 7,23,64 BOEING B-727-200 RE (ROHR STC SA4363NM) 198.70 162.00 JT8D-219/JT8D-17 3 5 30 92.8 99.5 98.9 3 23 BOEING B-727-200 RE (ROHR STC SA4363NM) 198.70 162.00 JT8D-219/JT8D-9 3 5 30 93.0 99.1 99.0 3 23,60 BOEING B-727-200 RE (ROHR STC SA4363NM) 198.70 162.00 JT8D-219/JT8D-9 3 5 30 92.7 99.5 99.0 3 7,23,63 BOEING B-727-200 RE (ROHR STC SA4363NM) 209.42 164.00 JT8D-217C/JT8D-15 3 5 30 95.3 98.8 99.1 3 23,61 Page 45 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B-727-200 RE (ROHR STC SA4363NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 203.10 164.00 JT8D-217C/JT8D-17A 3 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 93.4 99.6 99.3 STAGE 3 NOTES 23 BOEING B-737-200 (AVAERO;STC ST223CH) 128.10 88.00 JT8D-17 2 16.00 1.01 1 40 91.4 97.5 96.7 3 27 BOEING B-737-200 (AVAERO;STC ST223CH) 117.00 90.00 JT8D-15 2 15.50 1.03 1 40 89.7 96.7 98.1 3 35,42 BOEING B-737-200 (AVAERO;STC ST223CH) 128.10 93.00 JT8D-15 2 15.50 1.03 1 40 92.1 96.5 97.1 3 27,42 BOEING B-737-200 (AVAERO;STC ST223CH) 100.80 95.00 JT8D-15 2 15.50 1.03 1 40 83.7 96.8 97.2 3 27,42 BOEING B-737-200 (AVAERO;STC ST223CH) 100.80 95.00 JT8D-9 2 14.50 1.03 1 40 85.2 95.5 97.2 3 27,41 Page 46 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B-737-200 (AVAERO;STC ST223CH) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 100.50 98.00 JT8D-15 2 15.50 1.03 TO AP FLAPS 1 40 TO SL AP NOISE LEVEL (EPNdB) 84.9 96.9 98.6 STAGE 3 NOTES 35,42 BOEING B-737-200 (AVAERO;STC ST223CH) 100.50 98.00 JT8D-9 2 14.50 1.03 1 40 86.3 95.7 98.6 3 35,41 BOEING B-737-200 (AVAERO;STC ST223CH) 121.50 107.00 JT8D-15 2 15.50 1.03 1 30 91.3 96.9 96.3 3 35,42 BOEING B-737-200 (AVAERO;STC ST223CH) 128.10 107.00 JT8D-15 2 15.50 1.03 1 30 92.1 96.5 94.8 3 27,42 BOEING B-737-200 (AVAERO;STC ST223CH) 115.00 107.00 JT8D-17 2 16.00 1.01 1 40 87.6 97.5 98.0 3 27 BOEING B-737-200 (AVAERO;STC ST223CH) 128.10 107.00 JT8D-17 2 16.00 1.01 1 30 91.4 97.5 94.8 3 27 Page 47 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B-737-200 (AVAERO;STC ST223CH) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 118.50 107.00 JT8D-9 2 14.50 1.03 TO AP FLAPS 1 30 TO SL AP NOISE LEVEL (EPNdB) 91.5 94.9 96.3 STAGE 3 NOTES 35,41 BOEING B-737-200 (AVAERO;STC ST223CH) 121.50 107.00 JT8D-9 2 14.50 1.03 1 40 91.5 94.8 98.0 3 27,41 BOEING B-737-200 (NORDAM;STC ST00131SE) 103.50 98.00 JT8D-15 w/LGW HUSHKIT 2 15.50 1.03 1 30 86.4 97.1 95.9 3 37 BOEING B-737-200 (NORDAM;STC ST00131SE) 103.50 98.00 JT8D-15 w/LGW-L HUSHKIT 2 15.50 1.03 1 30 85.7 97.1 95.7 3 37 BOEING B-737-200 (NORDAM;STC ST00131SE) 119.50 103.00 JT8D-15 w/LGW HUSHKIT 2 15.50 1.03 1 30 91.1 97.0 95.8 3 37 BOEING B-737-200 (NORDAM;STC ST00131SE) 119.50 103.00 JT8D-15 w/LGW-L HUSHKIT 2 15.50 1.03 1 30 90.2 96.8 95.8 3 37 Page 48 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B-737-200 ADV (NORDAM; STC SA5730NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 110.20 98.00 JT8D-9 2 14.50 1.03 TO AP FLAPS 1 40 TO SL AP NOISE LEVEL (EPNdB) 87.3 94.7 98.2 STAGE 3 NOTES 27,41 BOEING B-737-200 ADV (NORDAM; STC SA5730NM) 105.60 103.00 JT8D-15 2 15.50 1.03 1 40 84.6 96.3 98.4 3 27,42 BOEING B-737-200 ADV (NORDAM; STC SA5730NM) 115.50 103.00 JT8D-17 2 16.00 1.01 1 40 86.8 97.0 98.4 3 27 BOEING B-737-200 ADV (NORDAM; STC SA5730NM) 126.70 107.00 JT8D-15 2 15.50 1.03 1 40 91.0 96.0 98.6 3 27,42 BOEING B-737-200 ADV (NORDAM; STC SA5730NM) 126.50 107.00 JT8D-17 2 16.00 1.01 1 40 90.0 96.9 98.6 3 27 BOEING B-737-200 ADV (NORDAM; STC SA5730NM) 124.50 107.00 JT8D-9 2 14.50 1.03 1 40 91.9 94.4 98.6 3 27,41 Page 49 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B-737-200 ADV (NORDAM; STC ST00131SE) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 100.50 95.00 JT8D-9 w/LGW HUSHKIT 2 14.50 1.03 TO AP FLAPS 1 30 TO SL AP NOISE LEVEL (EPNdB) 86.1 96.7 96.2 STAGE 3 NOTES 36 BOEING B-737-200 ADV (NORDAM; STC ST00131SE) 103.50 98.00 JT8D-15 w/LGW HUSHKIT 2 15.50 1.03 1 30 86.4 97.1 96.0 3 37 BOEING B-737-200 ADV (NORDAM; STC ST00131SE) 103.50 98.00 JT8D-15 w/LGW-L HUSHKIT 2 15.50 1.03 1 30 85.7 97.1 95.8 3 37 BOEING B-737-200 ADV (NORDAM; STC ST00131SE) 115.50 98.00 JT8D-17/-17A w/LGW HUSHKIT 2 16.00 1.01 1 30 89.7 97.5 96.0 3 BOEING B-737-200 ADV (NORDAM; STC ST00131SE) 109.00 98.00 JT8D-7 w/LGW-N HUSHKIT 2 14.00 1.40 1 30 89.2 96.3 96.2 3 40 BOEING B-737-200 ADV (NORDAM; STC ST00131SE) 100.50 98.00 JT8D-9 w/LGW-N HUSHKIT 2 14.50 1.03 1 30 86.1 96.9 96.2 3 36 Page 50 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B-737-200 ADV (NORDAM; STC ST00131SE) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 100.50 99.00 JT8D-9 w/LGW-L HUSHKIT 2 14.50 1.03 TO AP FLAPS 1 30 TO SL AP NOISE LEVEL (EPNdB) 86.9 96.5 95.8 STAGE 3 NOTES 36 BOEING B-737-200 ADV (NORDAM; STC ST00131SE) 121.60 107.00 JT8D-15 w/LGW HUSHKIT 2 15.50 1.03 1 30 91.7 96.7 95.9 3 37 BOEING B-737-200 ADV (NORDAM; STC ST00131SE) 125.90 107.00 JT8D-15 w/LGW-L HUSHKIT 2 15.50 1.03 1 30 91.8 97.0 95.9 3 37 BOEING B-737-200 ADV (NORDAM; STC ST00131SE) 120.50 107.00 JT8D-17/-17A w/LGW HUSHKIT 2 16.00 1.01 1 30 90.8 97.6 95.9 3 BOEING B-737-200 ADV (NORDAM; STC ST00131SE) 117.00 107.00 JT8D-7 w/LGW-N HUSHKIT 2 14.00 1.40 1 30 91.6 95.9 96.2 3 40 BOEING B-737-200 ADV (NORDAM; STC ST00131SE) 118.70 107.00 JT8D-9 w/LGW HUSHKIT 2 14.50 1.03 1 30 91.6 96.1 95.9 3 36 Page 51 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B-737-200 ADV (NORDAM; STC ST00131SE) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 122.90 107.00 JT8D-9 w/LGW-L HUSHKIT 2 14.50 1.03 TO AP FLAPS 1 30 TO SL AP NOISE LEVEL (EPNdB) 91.8 96.0 95.9 STAGE 3 NOTES 36 BOEING B-737-200 ADV (NORDAM; STC ST00131SE) 118.50 107.00 JT8D-9 w/LGW-N HUSHKIT 2 14.50 1.03 1 30 91.6 96.5 96.2 3 36 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 119.50 88.00 JT8D-15 2 15.50 1.03 1 40 90.3 96.8 97.7 3 35,42 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 100.80 95.00 JT8D-15 2 15.50 1.03 1 40 83.7 96.9 96.9 3 27,42 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 119.50 95.00 JT8D-9 2 14.50 1.03 1 40 91.7 95.0 98.1 3 35,41 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 100.80 95.00 JT8D-9 2 14.50 1.03 1 40 85.3 95.7 96.9 3 27,41 Page 52 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B-737-200 ADV(AVAERO;STC ST223CH) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 100.50 98.00 JT8D-15 2 15.50 1.03 TO AP FLAPS 1 40 TO SL AP NOISE LEVEL (EPNdB) 85.0 97.0 98.3 STAGE 3 NOTES 35,42 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 128.10 98.00 JT8D-15 2 15.50 1.03 1 40 92.1 96.5 97.1 3 27,42 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 100.50 98.00 JT8D-9 2 14.50 1.03 1 40 86.4 95.8 98.3 3 35,41 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 124.50 107.00 JT8D-15 2 15.50 1.03 1 30 91.8 96.7 96.3 3 35,42 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 128.10 107.00 JT8D-15 2 15.50 1.03 1 30 92.1 96.5 94.8 3 27,42 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 115.00 107.00 JT8D-17 2 16.00 1.01 1 40 87.5 97.5 97.7 3 27 Page 53 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B-737-200 ADV(AVAERO;STC ST223CH) 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 128.10 107.00 JT8D-17 2 16.00 1.01 TO AP FLAPS 1 30 TO SL AP NOISE LEVEL (EPNdB) 91.2 97.7 94.8 STAGE 3 NOTES 27 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 125.00 107.00 JT8D-17 2 16.00 1.01 1 40 90.2 97.5 97.7 3 27 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 121.50 107.00 JT8D-9 2 14.50 1.03 1 40 91.5 95.0 97.7 3 27,41 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 119.50 107.00 JT8D-9 2 14.50 1.03 1 30 91.7 95.0 96.3 3 35,41 BOEING B-737-200 ADV. 128.10 79.10 JT8D-17QN 2 16.00 1.01 1 40 97.0 104.1 102.8 2 2,19 BOEING B-737-200 ADV. 128.10 88.00 JT8D-15QN 2 15.50 1.03 1 40 97.7 102.4 103.8 2 2,18 Page 54 04/24/2012 MANUFACTURER BOEING MODEL B-737-200 ADV. 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 115.50 95.30 JT8D-17QN 2 16.00 1.01 TO AP FLAPS 1 40 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 93.6 104.4 104.5 2 2,19 BOEING B-737-200 ADV. 115.50 101.00 JT8D-15QN 2 15.50 1.03 1 40 94.4 103.1 105.0 2 2,18 BOEING B-737-200 ADV. 115.50 103.00 JT8D-9QN 2 14.50 1.03 1 40 95.3 100.6 105.1 2 2,17 BOEING B-737-200 ADV. 122.50 105.00 JT8D-9QN 2 14.50 1.03 1 40 96.9 99.9 105.3 2 2,17 BOEING B-737-200 NON-ADV. 100.50 95.00 JT8D-7QN 2 14.00 1.40 1 40 92.1 101.7 102.1 2 2,16 BOEING B-737-200 NON-ADV. 109.00 95.00 JT8D-9QN 2 14.50 1.03 1 40 93.2 100.7 104.8 2 2,17 Page 55 04/24/2012 MANUFACTURER BOEING MODEL B-737-200 NON-ADV. 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 109.00 98.00 JT8D-7QN 2 14.00 1.40 TO AP FLAPS 1 40 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 94.7 101.3 102.1 2 2,16 BOEING B-737-200 NON-ADV. 117.00 101.70 JT8D-9QN 2 14.50 1.03 1 40 95.5 100.3 105.3 2 2,17 BOEING B-737-300 124.50 110.00 CFM56-3 w/HWFAP 2 20.00 5.00 1 40 82.4 89.7 98.5 3 BOEING B-737-300 124.50 110.00 CFM56-3 w/HWFAP 2 20.00 5.00 1 40 82.4 89.7 97.4 3 38 BOEING B-737-300 124.50 110.00 CFM56-3 w/HWFAP 2 22.00 5.00 1 40 81.6 91.2 98.5 3 BOEING B-737-300 124.50 110.00 CFM56-3 w/HWFAP 2 22.00 5.00 1 40 81.6 91.2 97.4 3 38 Page 56 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-300 124.50 110.00 CFM56-3-B1 2 20.00 5.00 1 40 84.4 90.4 99.6 3 BOEING B-737-300 124.50 110.00 CFM56-3B-2 2 22.00 4.90 1 40 82.8 92.2 99.6 3 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 2 20.00 5.00 1 40 85.2 89.2 98.6 3 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 2 22.00 5.00 1 40 83.9 90.9 97.6 3 38 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 2 20.00 5.00 1 40 85.2 89.2 97.6 3 38 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 2 22.00 5.00 1 40 83.9 90.9 98.6 3 Page 57 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B-737-300 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 139.50 121.00 CFM56-3-B1 2 20.00 5.00 TO AP FLAPS 1 40 TO SL AP NOISE LEVEL (EPNdB) 87.5 89.9 100.1 STAGE 3 NOTES BOEING B-737-300 139.50 121.00 CFM56-3B-2 2 22.00 4.90 1 40 85.7 91.9 100.1 3 BOEING B737-300 124.50 110.00 CFM56-3B2,-3C1 HWFAP @ -3B2 THRUST RATING 2 0.00 0.00 0 40 81.6 91.6 97.2 4 38,52 BOEING B737-300 139.50 121.00 CFM56-3B1,-3B2,-3C1 HWFAP @ -3B1 THRUST RATING 2 0.00 0.00 0 40 86.0 89.5 97.6 4 38,52 BOEING B737-300 138.50 121.00 CFM56-3B1,-3B2,-3C1 HWFAP @ -3B1 THRUST RATING 2 0.00 0.00 0 40 85.7 89.6 97.6 4 38,52 BOEING B737-300 139.50 121.00 CFM56-3B2,-3C1 HWFAP @ -3B2 THRUST RATING 2 0.00 0.00 0 40 84.4 91.1 97.6 4 38,52 Page 58 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 22.00 5.00 5 40 82.8 91.2 98.6 3 BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 83.8 89.8 97.7 3 38 BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 83.8 89.8 98.6 3 BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 22.00 5.00 5 40 82.8 91.2 97.7 3 38 BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 23.50 5.00 5 40 82.4 92.1 97.7 3 38 BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 23.50 5.00 5 40 82.4 92.1 98.6 3 Page 59 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-400 138.50 121.00 CFM56-3-B1 2 20.00 5.00 5 40 87.2 90.0 100.2 3 BOEING B-737-400 142.50 121.00 CFM56-3-B1 2 20.00 5.00 5 40 88.9 89.6 100.2 3 BOEING B-737-400 138.50 121.00 CFM56-3B-2 2 22.00 4.90 5 40 85.7 92.1 100.2 3 BOEING B-737-400 138.50 121.00 CFM56-3C-1 2 23.50 5.00 5 40 85.0 93.2 100.2 3 BOEING B-737-400 142.50 124.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 86.9 88.9 97.7 3 38 BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 2 22.00 5.00 5 40 86.3 90.7 97.7 3 38 Page 60 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 2 22.00 5.00 5 40 86.3 90.7 98.6 3 BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 2 23.50 5.00 5 40 85.9 91.8 97.7 3 38 BOEING B-737-400 142.50 124.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 86.9 88.9 98.6 3 BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 2 23.50 5.00 5 40 85.9 91.8 98.6 3 BOEING B-737-400 150.00 124.00 CFM56-3B-2 2 22.00 4.90 5 40 87.7 91.7 100.2 3 BOEING B-737-400 150.00 124.00 CFM56-3C-1 2 23.50 4.90 5 40 87.1 93.1 100.2 3 Page 61 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B737-400 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 125.50 121.00 CFM56-3B2,-3C1 HWFAP @ -3B2 THRUST RATING 2 0.00 0.00 TO AP FLAPS 0 40 TO SL AP NOISE LEVEL (EPNdB) 83.1 91.8 97.8 STAGE 4 NOTES 38 BOEING B737-400 125.50 121.00 CFM56-3C1 HWFAP @ - 3C1 THRUST RATING 2 0.00 0.00 0 40 82.5 93.1 97.8 4 38 BOEING B737-400 150.00 124.00 CFM56-3B2,-3C1 HWFAP @ -3B2 THRUST RATING 2 0.00 0.00 0 40 88.0 90.7 97.9 4 38 BOEING B737-400 150.00 124.00 CFM56-3C1 HWFAP @ - 3C1 THRUST RATING 2 0.00 0.00 0 40 87.1 92.4 97.9 4 38 BOEING B-737-500 108.00 105.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 80.4 90.2 97.2 3 38 BOEING B-737-500 108.00 105.00 CFM56-3 w/HWFAP 2 18.50 5.00 5 40 81.0 89.3 98.4 3 Page 62 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-500 108.00 105.00 CFM56-3 w/HWFAP 2 18.50 5.00 5 40 81.0 89.3 97.2 3 38 BOEING B-737-500 108.00 105.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 80.4 90.2 98.4 3 BOEING B-737-500 115.50 105.00 CFM56-3-B1 2 20.00 5.00 5 40 82.7 90.8 99.4 3 BOEING B-737-500 115.50 105.00 CFM56-3-B1(R) 2 18.50 5.00 5 40 83.6 89.9 99.4 3 BOEING B-737-500 132.80 114.00 CFM56-3 w/HWFAP 2 18.50 5.00 5 40 85.4 88.2 97.6 3 38 BOEING B-737-500 139.00 114.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 85.4 89.2 97.6 3 38 Page 63 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-500 139.00 114.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 85.4 89.2 98.7 3 BOEING B-737-500 132.80 114.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 85.4 88.2 98.7 3 BOEING B-737-500 139.00 114.00 CFM56-3-B1 2 20.00 5.00 5 40 87.3 90.0 100.0 3 BOEING B-737-500 132.80 114.00 CFM56-3-B1(R) 2 18.50 5.00 5 40 87.7 88.9 100.0 3 BOEING B737-500 108.00 105.00 CFM56-3B1,-3B2,-3C1 2 0.00 0.00 0 40 80.6 89.6 96.9 4 38,52 HWFAP @ 18,500 SLST BOEING B737-500 108.00 105.00 CFM56-3B1,-3B2,-3C1 2 0.00 0.00 0 40 80.6 97.1 90.6 4 38 HWFAP @ -3B1 THRUST RATING Page 64 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 MANUFACTURER BOEING MODEL B737-500 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 132.80 114.00 CFM56-3B1,-3B2,-3C1 HWFAP @ 18,500 SLST 2 0.00 0.00 TO AP FLAPS 0 40 TO SL AP NOISE LEVEL (EPNdB) 86.0 88.6 97.3 STAGE 4 NOTES 38,52 BOEING B737-500 139.00 114.00 CFM56-3B1,-3B2,-3C1 HWFAP @ -3B1 THRUST RATING 2 0.00 0.00 0 40 87.3 89.2 97.5 4 38 BOEING B-737-600 143.50 120.50 CFM56-7B/2 DAC (B18 derate) 2 19.50 5.60 1 40 85.2 88.7 95.8 3 50 BOEING B-737-600 124.00 120.50 CFM56-7B/2 DAC (B18 derate) 2 19.50 5.60 1 40 82.0 89.7 95.8 3 50 BOEING B-737-600 124.00 120.50 CFM56-7B18 2 19.50 5.60 1 40 82.6 90.3 95.5 3 BOEING B-737-600 143.50 120.50 CFM56-7B18 2 19.50 5.60 1 40 85.7 89.3 95.5 3 Page 65 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-600 143.50 120.50 CFM56-7B20 2 20.60 5.60 1 40 85.4 90.7 95.5 3 BOEING B-737-600 124.00 120.50 CFM56-7B20 2 20.60 5.60 1 40 81.9 91.3 95.5 3 BOEING B-737-600 124.00 120.50 CFM56-7B20/2 DAC 2 20.60 5.60 1 40 81.3 90.7 95.8 3 50 BOEING B-737-600 143.50 120.50 CFM56-7B20/2 DAC 2 20.60 5.60 1 40 84.9 90.0 95.8 3 50 BOEING B-737-600 143.50 120.50 CFM56-7B22 2 22.70 5.40 1 40 84.4 92.3 95.5 3 BOEING B-737-600 124.00 120.50 CFM56-7B22 2 22.70 5.40 1 40 80.9 92.9 95.5 3 Page 66 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-600 143.50 120.50 CFM56-7B22/2 DAC 2 22.70 5.40 1 40 83.7 91.6 95.8 3 50 BOEING B-737-600 124.00 120.50 CFM56-7B22/2 DAC 2 22.70 5.40 1 40 80.2 92.2 95.8 3 50 BOEING B-737-700 133.00 128.00 CFM56-7B20 2 20.60 5.60 1 40 83.8 90.9 95.8 3 BOEING B-737-700 133.00 128.00 CFM56-7B20/2 DAC 2 20.60 5.60 1 40 83.0 90.3 96.1 3 50 BOEING B-737-700 133.00 128.00 CFM56-7B22 2 22.70 5.40 1 40 82.6 92.5 95.8 3 BOEING B-737-700 133.00 128.00 CFM56-7B22/2 DAC 2 22.70 5.40 1 40 81.8 91.8 96.1 3 50 Page 67 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-700 133.00 128.00 CFM56-7B24 2 24.20 5.30 1 40 82.1 93.6 95.8 3 BOEING B-737-700 133.00 128.00 CFM56-7B24/2 DAC 2 24.20 5.30 1 40 81.1 93.0 96.1 3 50 BOEING B-737-700 133.00 128.00 CFM56-7B26 2 26.30 5.10 1 40 81.4 95.4 95.8 3 BOEING B-737-700 133.00 128.00 CFM56-7B26/2 DAC 2 26.30 5.10 1 40 80.3 94.7 96.1 3 50 BOEING B-737-700 154.50 129.20 CFM56-7B20 2 20.60 5.60 1 40 87.1 89.8 95.9 3 BOEING B-737-700 154.50 129.20 CFM56-7B20/2 DAC 2 20.60 5.60 1 40 86.4 89.2 96.2 3 50 Page 68 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-700 154.50 129.20 CFM56-7B22 2 22.70 5.40 1 40 86.3 91.9 95.9 3 BOEING B-737-700 154.50 129.20 CFM56-7B22/2 DAC 2 22.70 5.40 1 40 85.6 91.2 96.2 3 50 BOEING B-737-700 154.50 129.20 CFM56-7B24 2 24.20 5.30 1 40 85.9 93.0 95.9 3 BOEING B-737-700 154.50 129.20 CFM56-7B24/2 DAC 2 24.20 5.30 1 40 84.7 92.3 96.2 3 50 BOEING B-737-700 154.50 129.20 CFM56-7B26 2 26.30 5.10 1 40 84.6 94.7 95.9 3 BOEING B-737-700 154.50 129.20 CFM56-7B26/2 DAC 2 26.30 5.10 1 40 83.8 94.0 96.2 3 50 Page 69 MANUFACTURER 04/24/2012 BOEING MODEL B-737-700 IGW/-700C 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 159.00 134.00 CFM56-7B24 2 24.20 5.30 TO AP FLAPS 1 40 TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 86.6 92.9 96.1 3 51 BOEING B-737-700 IGW/-700C 171.00 134.00 CFM56-7B24 2 24.20 5.30 1 40 88.6 92.5 96.1 3 51 BOEING B-737-700 IGW/-700C/BBJ 159.00 134.00 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 85.2 94.6 96.1 3 51 BOEING B-737-700 IGW/-700C/BBJ 171.00 134.00 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 87.1 94.3 96.1 3 51 BOEING B-737-700 IGW/BBJ 159.00 134.00 CFM56-7B27/B3 2 27.30 5.10 1 40 84.8 95.5 96.1 3 51 BOEING B-737-700 IGW/BBJ 171.00 134.00 CFM56-7B27/B3 2 27.30 5.10 1 40 86.6 95.2 96.1 3 51 Page 70 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-800 155.50 144.00 CFM56-7B24 2 24.20 5.30 1 40 85.5 92.5 96.4 3 BOEING B-737-800 155.50 144.00 CFM56-7B24/2 DAC 2 24.20 5.30 1 40 84.7 91.8 96.7 3 50 BOEING B-737-800 155.50 144.00 CFM56-7B26/2 DAC 2 26.30 5.10 1 40 83.7 93.5 96.7 3 50 BOEING B-737-800 155.50 144.00 CFM56-7B27/2 DAC 2 27.30 5.10 1 40 83.2 94.4 96.7 3 50 BOEING B-737-800 155.50 144.00 CFM56-7B27/2B1 DAC 2 27.30 5.10 1 40 83.1 94.7 96.7 3 50 BOEING B-737-800 174.20 146.30 CFM56-7B24 2 24.20 5.30 1 40 88.6 92.1 96.5 3 Page 71 04/24/2012 MANUFACTURER BOEING MODEL B-737-800 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 174.20 146.30 CFM56-7B24/2 DAC 2 24.20 5.30 TO AP FLAPS 1 40 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 87.8 91.4 96.8 3 50 BOEING B-737-800 174.20 146.30 CFM56-7B26/2 DAC 2 26.30 5.10 1 40 86.7 93.1 96.8 3 50 BOEING B-737-800 174.20 146.30 CFM56-7B27/2 DAC 2 27.30 5.10 1 40 86.1 93.9 96.8 3 50 BOEING B-737-800 174.20 146.30 CFM56-7B27/2B1 DAC 2 27.30 5.10 1 40 85.9 94.3 96.8 3 50 BOEING B-737-800/BBJ 2 155.50 144.00 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 84.4 94.2 96.4 3 BOEING B-737-800/BBJ 2 155.50 144.00 CFM56-7B27/B1; -7B27/B2 2 27.30 5.10 1 40 84.0 95.5 96.4 3 Page 72 04/24/2012 MANUFACTURER BOEING MODEL B-737-800/BBJ 2 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 155.50 144.00 CFM56-7B27; -7B27/B3 2 27.30 5.10 TO AP FLAPS 1 40 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 84.1 95.2 96.4 3 BOEING B-737-800/BBJ 2 174.20 146.30 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 87.4 93.8 96.5 3 BOEING B-737-800/BBJ 2 174.20 146.30 CFM56-7B27/B1; -7B27/B2 2 27.30 5.10 1 40 86.8 95.0 96.5 3 BOEING B-737-800/BBJ 2 174.20 146.30 CFM56-7B27; -7B27/B3 2 27.30 5.10 1 40 87.0 94.7 96.5 3 BOEING B-737-800W 155.50 144.00 CFM56-7B24 2 24.20 5.30 1 40 84.5 92.5 96.3 3 52 BOEING B-737-800W 155.50 144.00 CFM56-7B24/2 DAC 2 24.20 5.30 1 40 83.8 91.8 96.5 3 50,52 Page 73 04/24/2012 MANUFACTURER BOEING MODEL B-737-800W 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 155.50 144.00 CFM56-7B26/2 DAC 2 26.30 5.10 TO AP FLAPS 1 40 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 82.7 93.5 96.5 3 50,52 BOEING B-737-800W 155.50 144.00 CFM56-7B27/2 DAC 2 27.30 5.10 1 40 82.3 94.4 96.5 3 50,52 BOEING B-737-800W 155.50 144.00 CFM56-7B27/2B1 DAC 2 27.30 5.10 1 40 82.2 94.7 96.5 3 50,52 BOEING B-737-800W 174.20 146.30 CFM56-7B24 2 24.20 5.30 1 40 87.5 92.1 96.3 3 52 BOEING B-737-800W 174.20 146.30 CFM56-7B24/2 DAC 2 24.20 5.30 1 40 86.9 91.4 96.6 3 50,52 BOEING B-737-800W 174.20 146.30 CFM56-7B26/2 DAC 2 26.30 5.10 1 40 85.6 93.1 96.6 3 50,52 Page 74 04/24/2012 MANUFACTURER BOEING MODEL B-737-800W 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 174.20 146.30 CFM56-7B27/2 DAC 2 27.30 5.10 TO AP FLAPS 1 40 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 85.1 93.9 96.6 3 50,52 BOEING B-737-800W 174.20 146.30 CFM56-7B27/2B1 DAC 2 27.30 5.10 1 40 85.0 94.3 96.6 3 50,52 BOEING B-737-800W/BBJ 2 155.50 144.00 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 83.5 94.2 96.3 3 52 BOEING B-737-800W/BBJ 2 155.50 144.00 CFM56-7B27/B1; -7B27/B2 2 27.30 5.10 1 40 83.0 95.5 96.3 3 52 BOEING B-737-800W/BBJ 2 155.50 144.00 CFM56-7B27; -7B27/B3 2 27.30 5.10 1 40 83.2 95.1 96.3 3 52 BOEING B-737-800W/BBJ 2 174.20 146.30 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 86.4 93.8 96.3 3 52 Page 75 04/24/2012 MANUFACTURER BOEING MODEL B-737-800W/BBJ 2 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 174.20 146.30 CFM56-7B27/B1; -7B27/B2 2 27.30 5.10 TO AP FLAPS 1 40 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 85.8 95.0 96.3 3 52 BOEING B-737-800W/BBJ 2 174.20 146.30 CFM56-7B27; -7B27/B3 2 27.30 5.10 1 40 86.0 94.7 96.3 3 52 BOEING B-737-900 164.00 146.30 CFM56-7B24 2 24.20 5.30 1 40 86.6 92.0 96.4 3 BOEING B-737-900 164.00 146.30 CFM56-7B26 2 26.30 5.10 1 40 85.5 93.7 96.4 3 BOEING B-737-900 164.00 146.30 CFM56-7B27 2 27.30 5.10 1 40 85.1 94.5 96.4 3 BOEING B-737-900 164.00 146.30 CFM56-7B27/B1 2 27.30 5.10 1 40 85.0 95.0 96.4 3 Page 76 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-900 174.20 147.30 CFM56-7B24 2 24.20 5.30 1 40 88.4 91.8 96.4 3 BOEING B-737-900 174.20 147.30 CFM56-7B26 2 26.30 5.10 1 40 87.2 93.5 96.4 3 BOEING B-737-900 174.20 147.30 CFM56-7B27 2 27.30 5.10 1 40 86.7 94.2 96.4 3 BOEING B-737-900 174.20 147.30 CFM56-7B27/B1 2 27.30 5.10 1 40 86.6 94.7 96.4 3 BOEING B-747-100 710.00 400.00 JT9D-3A 4 43.60 5.10 10 30 105.4 102.1 104.6 3 29 BOEING B-747-100 750.00 400.00 JT9D-7F 4 48.00 5.10 10 30 104.5 103.5 104.5 3 29 Page 77 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-100 734.00 425.00 JT9D-7 4 46.30 5.10 10 30 105.1 102.7 104.6 3 29 BOEING B-747-100 734.00 460.00 JT9D-7A 4 47.00 5.10 10 30 104.3 102.6 105.3 3 29 BOEING B-747-100 750.00 520.00 JT9D-7F 4 48.00 5.10 10 25 104.5 103.5 104.5 3 29 BOEING B-747-100 710.00 540.00 JT9D-3A 4 43.60 5.10 10 25 105.4 102.1 104.6 3 29 BOEING B-747-100 734.00 540.00 JT9D-7 4 46.30 5.10 10 25 105.1 102.7 104.1 3 29 BOEING B-747-100 710.00 564.00 JT9D-3A 4 43.60 5.10 10 30 108.4 99.7 107.2 2 * ** Page 78 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-100 734.00 564.00 JT9D-3A 4 43.60 5.10 10 30 109.4 99.6 107.2 2 * ** BOEING B-747-100 710.00 564.00 JT9D-7 4 46.30 5.10 10 30 108.0 100.2 107.4 2 * ** BOEING B-747-100 750.00 585.00 JT9D-7A 4 47.00 5.10 10 30 107.8 98.8 106.9 2 * ** BOEING B-747-100 750.00 585.00 JT9D-7F 4 48.00 5.10 10 30 107.7 99.0 107.4 2 * ** BOEING B-747-100 750.00 585.00 JT9D-7FW 4 50.00 5.10 10 30 107.6 99.4 107.4 2 * ** BOEING B-747-100 750.00 585.00 JT9D-7WET 4 47.90 5.10 10 30 107.4 99.3 106.9 2 * ** Page 79 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-100 750.00 585.00 RB211-524C2 4 51.60 4.50 10 30 104.5 96.9 106.5 2 * ** BOEING B-747-100 734.00 630.00 JT9D-7A 4 47.00 5.10 10 25 104.3 102.6 105.5 3 29 BOEING B-747-200 770.00 475.00 JT9D-7J 4 50.00 5.10 10 30 103.6 103.0 105.9 3 30 BOEING B-747-200 710.00 520.00 JT9D-3A 4 43.60 5.10 10 30 104.4 100.8 106.9 3 30 BOEING B-747-200 750.00 520.00 JT9D-7F 4 48.00 5.10 10 30 103.5 102.0 106.9 3 30 BOEING B-747-200 734.00 540.00 JT9D-7 4 46.30 5.10 10 30 104.2 101.3 106.7 3 30 Page 80 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-200 767.00 564.00 JT9D-3A 4 43.60 5.10 10 30 110.0 98.2 106.5 2 * ** BOEING B-747-200 770.00 564.00 JT9D-7 4 46.30 5.10 10 30 108.9 98.8 106.7 2 * ** BOEING B-747-200 734.00 564.00 JT9D-7A 4 47.00 5.10 10 30 103.5 101.2 106.9 3 30 BOEING B-747-200 775.00 564.00 JT9D-7F 4 48.00 5.10 10 30 108.6 98.9 107.2 2 * ** BOEING B-747-200 785.00 564.00 JT9D-7R4G2 4 54.75 4.80 10 30 100.1 98.6 105.4 2 ** BOEING B-747-200 775.00 585.00 CF6-50E 4 52.50 4.10 10 30 100.7 101.1 105.9 3 Page 81 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-200 773.00 585.00 JT9D-3AWET 4 45.80 5.10 10 30 109.1 98.7 106.7 2 * ** BOEING B-747-200 833.00 585.00 RB211-524C2 4 51.60 4.50 10 30 106.5 99.7 107.0 3 * BOEING B-747-200 833.00 600.00 JT9D-7Q 4 53.00 4.90 10 30 103.2 103.5 106.6 3 BOEING B-747-200 820.00 630.00 CF6-50E 4 52.50 4.10 10 30 102.5 100.9 107.0 3 BOEING B-747-200 833.00 630.00 CF6-50E2 4 52.50 4.10 10 30 102.6 101.7 106.5 3 BOEING B-747-200 820.00 630.00 CF6-50E2 4 52.50 4.10 10 30 102.1 101.7 106.5 3 Page 82 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-200 710.00 630.00 JT9D-3A 4 43.60 5.10 10 25 104.4 100.8 105.7 3 30 BOEING B-747-200 734.00 630.00 JT9D-7 4 46.30 5.10 10 25 104.2 101.3 105.2 3 30 BOEING B-747-200 820.00 630.00 JT9D-70A 4 53.00 4.90 10 30 101.1 98.5 106.0 3 BOEING B-747-200 785.00 630.00 JT9D-7A 4 47.00 5.10 10 30 109.3 98.7 107.3 2 * ** BOEING B-747-200 734.00 630.00 JT9D-7A 4 47.00 5.10 10 25 103.5 101.2 105.0 3 30 BOEING B-747-200 750.00 630.00 JT9D-7F 4 48.00 5.10 10 25 103.5 102.0 106.0 3 30 Page 83 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-200 800.00 630.00 JT9D-7F 4 48.00 5.10 10 30 109.7 98.8 107.8 2 * ** BOEING B-747-200 805.00 630.00 JT9D-7FW 4 50.00 5.10 10 30 109.4 99.2 107.8 2 * ** BOEING B-747-200 812.00 630.00 JT9D-7FW/-7J 4 50.00 5.10 10 30 109.7 99.2 107.4 2 * ** BOEING B-747-200 770.00 630.00 JT9D-7J 4 50.00 5.10 10 25 103.6 103.0 106.0 3 30 BOEING B-747-200 800.00 630.00 JT9D-7J 4 50.00 5.10 10 30 109.3 99.2 107.8 2 * ** BOEING B-747-200 833.00 630.00 JT9D-7Q 4 53.00 4.90 10 25 103.2 103.5 104.4 3 Page 84 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-200 833.00 630.00 JT9D-7R4G2 4 54.75 4.80 10 30 102.4 97.9 106.6 2 ** BOEING B-747-200 785.00 630.00 JT9D-7WET 4 47.90 5.10 10 30 108.7 99.1 107.3 2 * ** BOEING B-747-200 800.00 630.00 RB211-524B/B2 4 50.10 4.30 10 30 105.5 96.0 107.3 2 * ** BOEING B-747-200 820.00 630.00 RB211-524B/B2 4 50.10 4.30 10 30 105.5 95.6 107.3 2 ** BOEING B-747-200 833.00 630.00 RB211-524D4 4 53.10 4.20 10 30 103.9 99.7 104.9 3 BOEING B-747-300 600.00 564.00 CF6-80C2B1 4 56.70 5.00 10 30 89.8 99.1 102.5 3 Page 85 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-300 775.00 564.00 RB211-524D4 4 53.10 4.20 10 30 101.5 97.1 104.3 2 ** BOEING B-747-300 800.00 585.00 JT9D-70A 4 53.00 4.90 10 30 99.2 95.8 105.4 2 ** BOEING B-747-300 775.00 585.00 RB211-524B2 4 50.10 4.30 10 30 103.3 96.1 106.5 2 ** BOEING B-747-300 800.00 630.00 CF6-50E2 4 52.50 4.10 10 30 101.6 101.8 106.5 3 BOEING B-747-300 820.00 630.00 JT9D-70A 4 53.00 4.90 10 30 100.2 95.5 105.3 2 ** BOEING B-747-300 833.00 630.00 JT9D-7R4G2 4 54.75 4.80 10 30 102.4 101.3 106.6 3 Page 86 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-300 785.00 630.00 JT9D-7R4G2 4 54.75 4.80 10 30 100.1 101.5 106.6 3 BOEING B-747-300 820.00 630.00 RB211-524B2 4 50.10 4.30 10 30 105.5 95.6 107.3 2 ** BOEING B-747-300 833.00 630.00 RB211-524D4 4 53.10 4.20 10 30 103.9 96.5 104.9 2 ** BOEING B-747-300 833.00 666.00 CF6-80C2B1 4 56.70 5.00 10 30 99.0 98.2 105.2 3 BOEING B-747-400 600.00 564.00 CF6-80C2B1F 4 57.90 5.00 10 30 89.6 99.1 101.7 3 BOEING B-747-400 830.00 564.00 CF6-80C2B5F 4 60.80 5.00 10 30 96.0 100.4 101.7 3 Page 87 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-400 600.00 564.00 PW4056 4 56.75 4.80 10 30 89.5 100.7 103.1 3 BOEING B-747-400 600.00 564.00 RB211-524G 4 58.00 4.30 10 30 89.1 98.9 102.4 3 BOEING B-747-400 600.00 564.00 RB211-524H 4 60.60 4.10 10 30 88.7 99.7 102.4 3 BOEING B-747-400 870.00 652.00 CF6-80C2B1F 4 60.20 5.20 25 99.7 98.3 101.4 3 BOEING B-747-400 875.00 652.00 CF6-80C2B1F 4 57.90 5.00 10 30 99.8 98.2 103.8 3 BOEING B-747-400 875.00 652.00 CF6-80C2B1F W/N1 MOD 4 57.30 5.00 10 30 99.9 97.9 103.8 3 Page 88 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-400 875.00 652.00 CF6-80C2B5F 4 60.80 5.00 10 30 97.5 100.3 103.8 3 BOEING B-747-400 870.00 652.00 PW 4056 4 56.75 4.80 10 30 101.5 99.7 104.7 3 BOEING B-747-400 875.00 652.00 PW4056 4 56.75 4.80 10 30 101.6 99.7 104.7 3 BOEING B-747-400 875.00 652.00 PW4056 PH3 (FB2B) 4 56.80 4.80 10 30 99.7 98.6 103.6 3 BOEING B-747-400 875.00 652.00 PW4056 PH3 (FB2C) 4 56.80 4.80 10 30 98.6 98.4 103.0 3 BOEING B-747-400 875.00 652.00 PW4056 PH3 (FB2C) NR 4 56.80 4.80 10 30 97.4 98.1 102.1 3 Page 89 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-400 875.00 652.00 PW4056 PKG B/PHASE I 4 56.80 4.80 10 30 99.3 98.5 103.4 3 BOEING B-747-400 875.00 652.00 RB211-524G 4 58.00 4.30 10 30 99.2 98.0 103.8 3 BOEING B-747-400 870.00 652.00 RB211-524H 4 60.60 4.10 10 30 97.8 98.8 103.8 3 BOEING B-747-400 875.00 652.00 RB211-524H2 4 58.00 4.10 10 30 98.0 98.8 103.8 3 BOEING B747-8 700.00 600.00 Genx-2B(EIS) 4 0.00 0.00 0 30 85.3 94.8 99.6 4 BOEING B747-8 987.00 688.00 Genx-2B(EIS) 4 0.00 0.00 0 30 94.5 94.0 100.4 4 Page 90 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B747-8F 700.00 600.00 Genx-2B(EIS) 4 0.00 0.00 0 30 85.3 94.8 99.6 4 BOEING B747-8F 975.00 761.00 Genx-2B(EIS) 4 0.00 0.00 0 30 94.0 94.0 100.9 4 BOEING B-747-SP 702.00 410.00 RB211-524D4 4 53.10 4.20 10 30 99.2 99.8 107.0 3 BOEING B-747-SP 660.00 450.00 JT9D-7A 4 47.00 5.10 10 30 99.6 101.3 102.5 3 BOEING B-747-SP 702.00 450.00 JT9D-7J 4 50.00 5.10 10 30 100.1 103.3 103.2 3 BOEING B-747-SP 696.00 450.00 RB211-524B2 4 50.10 4.30 10 30 99.5 99.8 103.2 3 Page 91 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-SP 701.00 465.00 JT9D-7A 4 47.00 5.10 10 30 102.0 101.1 102.9 3 BOEING B-747-SP 660.00 475.00 JT9D-7F 4 48.00 5.10 10 30 98.7 102.3 103.8 3 BOEING B-747-SP 702.00 475.00 JT9D-7J 4 50.00 5.10 10 30 100.1 103.3 103.8 3 BOEING B-747-SP 696.00 475.00 JT9D-7J 4 50.00 5.10 10 30 99.8 103.5 103.8 3 BOEING B-747-SR 571.00 564.00 CF6-45A2 4 46.50 4.10 10 30 98.4 93.2 105.4 3 BOEING B-747-SR 570.00 564.00 JT9D-7A 4 47.00 5.10 10 30 100.2 101.8 106.9 2 * Page 92 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-SR 610.00 564.00 JT9D-7A 4 47.00 5.10 10 30 101.8 101.6 106.9 3 * BOEING B-757-200 187.00 198.00 PW 2037 2 37.00 5 30 81.5 94.3 97.7 3 BOEING B-757-200 220.00 198.00 PW 2037 2 38.20 5.80 5 30 86.2 94.0 97.7 3 BOEING B-757-200 187.00 198.00 PW 2037QFC 2 37.00 5 30 80.1 93.7 97.0 3 59 BOEING B-757-200 220.00 198.00 PW 2040 2 41.70 5.70 5 30 84.6 94.5 97.7 3 BOEING B-757-200 190.00 198.00 PW 2040QFC 2 40.00 5 30 79.4 95.1 97.0 3 59 Page 93 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-757-200 220.00 198.00 RB211-535C 2 37.40 4.50 5 30 85.5 94.0 100.3 3 BOEING B-757-200 220.00 198.00 RB211-535-E4 2 40.10 4.10 5 30 82.2 93.3 95.0 3 BOEING B-757-200 220.00 198.00 RB211-535-E4 2 40.10 4.10 5 30 82.9 93.4 95.0 3 58 BOEING B-757-200 220.00 198.00 RB211-535E4-B 2 43.10 4.10 5 30 82.1 94.2 95.0 3 58 BOEING B-757-200 220.00 198.00 RB211-535E4-B 2 43.10 4.10 5 30 81.3 94.4 95.0 3 BOEING B-757-200 255.50 210.00 PW 2037 2 38.20 5.80 5 30 91.4 93.7 98.1 3 Page 94 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-757-200 255.50 210.00 PW 2037QFC 2 37.00 5 30 89.7 92.7 97.3 3 59 BOEING B-757-200 255.50 210.00 PW 2040 2 41.70 5.70 5 30 89.7 94.2 98.1 3 BOEING B-757-200 255.50 210.00 PW 2040QFC 2 40.00 5 30 88.1 94.0 97.3 3 59 BOEING B-757-200 240.00 210.00 RB211-535C 2 37.40 4.50 5 25 88.1 93.8 99.6 3 BOEING B-757-200 255.50 210.00 RB211-535-E4 2 40.10 4.10 5 30 86.8 93.0 95.2 3 BOEING B-757-200 255.50 210.00 RB211-535-E4 2 40.10 4.10 5 30 87.3 93.0 95.2 3 58 Page 95 04/24/2012 MANUFACTURER BOEING MODEL B-757-200 1000# 1000# ENGINE MODEL THRUST 1000# BPR NO. AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW 255.50 210.00 RB211-535E4-B 2 43.10 4.10 TO AP FLAPS 5 30 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 85.7 94.1 95.2 3 BOEING B-757-200 255.50 210.00 RB211-535E4-B 2 43.10 4.10 5 30 86.2 93.8 95.2 3 58 BOEING B757-200 (STC ST02200LA) 220.00 198.42 RB211-535E4 2 0.00 0.00 5 30 83.9 96.0 98.1 4 BOEING B757-200 (STC ST02200LA) 255.50 210.00 RB211-535E4 2 0.00 0.00 5 30 89.3 95.5 98.4 4 BOEING B-757-300 236.00 210.00 RB211-535-E4 2 40.10 4.10 5 30 84.8 93.9 95.2 3 58 BOEING B-757-300 235.87 210.00 RB211-535E4-B 2 43.10 4.10 5 30 84.0 95.2 95.2 3 58 Page 96 04/24/2012 AC 36-1H APPENDIX 1, CHANGE 1 AIRCRAFT NOISE DATA FOR UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-757-300 235.87 210.00 RB211-535E4-C 2 43.00 5 30 84.0 95.2 95.2 3 58 BOEING B-757-300 275.00 224.00 RB211-535-E4 2 40.10 4.10 5 30 89.8 93.5 95.4 3 58 BOEING B-757-300 275.00 224.00 RB211-535E4-B 2 43.10 4.10 5 30 88.4 94.8 95.4 3 58 BOEING B-757-300 275.00 224.00 RB211-535E4-C 2 43.00 5 30 88.
What's in the CESSNA 414 TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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