Federal Aviation Administration, DOT § 91.609

Total Page:16

File Type:pdf, Size:1020Kb

Federal Aviation Administration, DOT § 91.609 Federal Aviation Administration, DOT § 91.609 (4) No person may remove any exit test it or to test any communications that would result in a ratio of max- or electrical equipment installed in the imum number of occupants to approved aircraft; exits greater than 14:1. (4) Ferry a newly acquired aircraft (d) This section does not relieve any from a place where possession of it was person operating under part 121 of this taken to a place where the flight re- chapter from complying with § 121.291. corder or cockpit voice recorder is to be installed; or § 91.609 Flight data recorders and (5) Operate an aircraft: cockpit voice recorders. (i) For not more than 15 days while (a) No holder of an air carrier oper- the flight recorder and/or cockpit voice ating certificate or an operating cer- recorder is inoperative and/or removed tificate may conduct any operation for repair provided that the aircraft under this part with an aircraft listed maintenance records contain an entry in the holder’s operations specifica- that indicates the date of failure, and a tions or current list of aircraft used in placard is located in view of the pilot air transportation unless that aircraft to show that the flight recorder or complies with any applicable flight re- cockpit voice recorder is inoperative. corder and cockpit voice recorder re- (ii) For not more than an additional quirements of the part under which its 15 days, provided that the requirements certificate is issued except that the op- in paragraph (b)(5)(i) are met and that erator may— a certificated pilot, or a certificated (1) Ferry an aircraft with an inoper- person authorized to return an aircraft ative flight recorder or cockpit voice to service under § 43.7 of this chapter, recorder from a place where repair or certifies in the aircraft maintenance replacement cannot be made to a place records that additional time is required where they can be made; to complete repairs or obtain a replace- (2) Continue a flight as originally ment unit. planned, if the flight recorder or cock- (c)(1) No person may operate a U.S. pit voice recorder becomes inoperative civil registered, multiengine, turbine- after the aircraft has taken off; powered airplane or rotorcraft having a (3) Conduct an airworthiness flight passenger seating configuration, ex- test during which the flight recorder or cluding any pilot seats of 10 or more cockpit voice recorder is turned off to that has been manufactured after Octo- test it or to test any communications ber 11, 1991, unless it is equipped with or electrical equipment installed in the one or more approved flight recorders aircraft; or that utilize a digital method of record- (4) Ferry a newly acquired aircraft ing and storing data and a method of from the place where possession of it is readily retrieving that data from the taken to a place where the flight re- storage medium, that are capable of re- corder or cockpit voice recorder is to cording the data specified in appendix be installed. E to this part, for an airplane, or ap- (b) Notwithstanding paragraphs (c) pendix F to this part, for a rotorcraft, and (e) of this section, an operator of this part within the range, accuracy, other than the holder of an air carrier and recording interval specified, and or a commercial operator certificate that are capable of retaining no less may— than 8 hours of aircraft operation. (1) Ferry an aircraft with an inoper- (2) All airplanes subject to paragraph ative flight recorder or cockpit voice (c)(1) of this section that are manufac- recorder from a place where repair or tured before April 7, 2010, by April 7, replacement cannot be made to a place 2012, must meet the requirements of where they can be made; § 23.1459(a)(7) or § 25.1459(a)(8) of this (2) Continue a flight as originally chapter, as applicable. planned if the flight recorder or cock- (3) All airplanes and rotorcraft sub- pit voice recorder becomes inoperative ject to paragraph (c)(1) of this section after the aircraft has taken off; that are manufactured on or after (3) Conduct an airworthiness flight April 7, 2010, must meet the flight data test during which the flight recorder or recorder requirements of § 23.1459, cockpit voice recorder is turned off to § 25.1459, § 27.1459, or § 29.1459 of this 773 VerDate Mar<15>2010 11:09 Mar 07, 2011 Jkt 223044 PO 00000 Frm 00783 Fmt 8010 Sfmt 8010 Y:\SGML\223044.XXX 223044 wwoods2 on DSK1DXX6B1PROD with CFR § 91.609 14 CFR Ch. I (1–1–11 Edition) chapter, as applicable, and retain at under part 830. The Administrator does least the last 25 hours of recorded in- not use the cockpit voice recorder formation using a recorder that meets record in any civil penalty or certifi- the standards of TSO–C124a, or later re- cate action. vision. (h) All airplanes required by this sec- (d) Whenever a flight recorder, re- tion to have a cockpit voice recorder quired by this section, is installed, it and a flight data recorder, that are must be operated continuously from manufactured before April 7, 2010, must the instant the airplane begins the by April 7, 2012, have a cockpit voice takeoff roll or the rotorcraft begins lift-off until the airplane has com- recorder that also— pleted the landing roll or the rotorcraft (1) Meets the requirements of has landed at its destination. § 23.1457(d)(6) or § 25.1457(d)(6) of this (e) Unless otherwise authorized by chapter, as applicable; and the Administrator, after October 11, (2) If transport category, meets the 1991, no person may operate a U.S. civil requirements of § 25.1457(a)(3), (a)(4), registered multiengine, turbine-pow- and (a)(5) of this chapter. ered airplane or rotorcraft having a (i) All airplanes or rotorcraft re- passenger seating configuration of six quired by this section to have a cockpit passengers or more and for which two voice recorder and flight data recorder, pilots are required by type certifi- that are manufactured on or after cation or operating rule unless it is April 7, 2010, must have a cockpit voice equipped with an approved cockpit recorder installed that also— voice recorder that: (1) Is installed in accordance with the (1) Is installed in compliance with § 23.1457(a)(1) and (2), (b), (c), (d)(1)(i), requirements of § 23.1457 (except for (2) and (3), (e), (f), and (g); § 25.1457(a)(1) paragraphs (a)(6) and (d)(5)); § 25.1457 and (2), (b), (c), (d)(1)(i), (2) and (3), (e), (except for paragraphs (a)(6) and (d)(5)); (f), and (g); § 27.1457(a)(1) and (2), (b), § 27.1457 (except for paragraphs (a)(6) (c), (d)(1)(i), (2) and (3), (e), (f), and (g); and (d)(5)); or § 29.1457 (except for para- or § 29.1457(a)(1) and (2), (b), (c), (d)(1)(i), graphs (a)(6) and (d)(5)) of this chapter, (2) and (3), (e), (f), and (g) of this chap- as applicable; and ter, as applicable; and (2) Retains at least the last 2 hours of (2) Is operated continuously from the recorded information using a recorder use of the checklist before the flight to that meets the standards of TSO–C123a, completion of the final checklist at the or later revision. end of the flight. (3) For all airplanes or rotorcraft (f) In complying with this section, an manufactured on or after April 6, 2012, approved cockpit voice recorder having also meets the requirements of an erasure feature may be used, so that § 23.1457(a)(6) and (d)(5); § 25.1457(a)(6) at any time during the operation of the and (d)(5); § 27.1457(a)(6) and (d)(5); or recorder, information recorded more than 15 minutes earlier may be erased § 29.1457(a)(6) and (d)(5) of this chapter, or otherwise obliterated. as applicable. (g) In the event of an accident or oc- (j) All airplanes or rotorcraft re- currence requiring immediate notifica- quired by this section to have a cockpit tion to the National Transportation voice recorder and a flight data re- Safety Board under part 830 of its regu- corder, that install datalink commu- lations that results in the termination nication equipment on or after April 6, of the flight, any operator who has in- 2012, must record all datalink messages stalled approved flight recorders and as required by the certification rule ap- approved cockpit voice recorders shall plicable to the aircraft. keep the recorded information for at (k) An aircraft operated under this least 60 days or, if requested by the Ad- part under deviation authority from ministrator or the Board, for a longer part 125 of this chapter must comply period. Information obtained from the with all of the applicable flight data record is used to assist in determining the cause of accidents or occurrences in connection with the investigation 774 VerDate Mar<15>2010 11:09 Mar 07, 2011 Jkt 223044 PO 00000 Frm 00784 Fmt 8010 Sfmt 8010 Y:\SGML\223044.XXX 223044 wwoods2 on DSK1DXX6B1PROD with CFR Federal Aviation Administration, DOT § 91.611 recorder requirements of part 125 appli- (ii) A limitation that takeoffs must cable to the aircraft, notwithstanding be made from dry runways unless, such deviation authority. based on a showing of actual operating [Doc. No. 18334, 54 FR 34318, Aug. 18, 1989, as takeoff techniques on wet runways amended by Amdt. 91–226, 56 FR 51621, Oct.
Recommended publications
  • Guide to Methods & Tools for Airline Flight Safety Analysis, Issue 2
    PAGE LEFT BLANK Guide to METHODS & TOOLS FOR AIRLINE FLIGHT SAFETY ANALYSIS Prepared by: GAIN Working Group B, Analytical Methods and Tools Second Edition – June 2003 THIS PAGE LEFT BLANK GAIN Guide to Methods & Tools for Airline Flight Safety Analysis Table of Contents Page Foreword...................................................................................................................................v Acknowledgements .................................................................................................................vi 1.0 Introduction.......................................................................................................................1 1.1 Purpose of Guide .........................................................................................................1 1.2 GAIN Overview ..........................................................................................................1 1.3 Working Group B: Analytical Methods and Tools .....................................................1 1.4 Scope ...........................................................................................................................2 1.5 Definitions ...................................................................................................................2 1.6 Review of Methods and Tools.....................................................................................2 1.7 Organization of this Guide ..........................................................................................3 1.8 Changes
    [Show full text]
  • FLYHT 2019 July Investor Presentation
    July 2019 FLYHT Aerospace Solutions Ltd. TSX.V: FLY OTCQX: FLYLF 1 TSX.V: FLY OTCQX: FLYLF Disclaimer www.flyht.com Forward Looking Statements This discussion includes certain statements that may be deemed “forward-looking statements” that are subject to risks and uncertainty. All statements, other than statements of historical facts included in this discussion, including, without limitation, those regarding the Company’s financial position, business strategy, projected costs, future plans, projected revenues, objectives of management for future operations, the Company’s ability to meet any repayment obligations, the use of non-GAAP financial measures, trends in the airline industry, the global financial outlook, expanding markets, research and development of next generation products and any government assistance in financing such developments, foreign exchange rate outlooks, new revenue streams and sales projections, cost increases as related to marketing, research and development (including AFIRS 228), administration expenses, and litigation matters, may be or include forward-looking statements. Although the Company believes the expectations expressed in such forward-looking statements are based on a number of reasonable assumptions regarding the Canadian, U.S., and global economic environments, local and foreign government policies/regulations and actions and assumptions made based upon discussions to date with the Company’s customers and advisers, such statements are not guarantees of future performance and actual results or developments may differ materially from those in the forward- looking statements. Factors that could cause actual results to differ materially from those in the forward-looking statements include production rates, timing for product deliveries and installations, Canadian, U.S., and foreign government activities, volatility of the aviation market for the Company’s products and services, factors that result in significant and prolonged disruption of air travel worldwide, U.S.
    [Show full text]
  • The Deadline for Airlines to Comply with the GADSS Mandate Is 1St of January 2021
    23 I AIRLINE & AIRCRAFT OPERATIONS The deadline for airlines to comply with the GADSS mandate is 1st of January 2021. The mandate requires aircraft operators to automate aircraft tracking capabilities. The hardware options available for operators are reviewed here. The avionic options to comply with GADSS he impetus for the International aircraft designs submitted after the updated to include new documents and Civil Aviation Organization’s introduction of the GADSS mandate must amendments pertaining to how data is (ICAO’s) Global Aeronautical be capable of timely FDR data recovery stored in distributed server networks, TDistress and Safety Systems in addition to having the standard flight such as a data-cloud and accessed and (GADSS) standards came from two high- recorders. used in an accident investigation. profile aircraft accidents. These were the The mandatory GADSS requirements Current Annex 13 legislation is based loss of Air France (AF) 447 in 2009 and will be effective from 1 January 2021. around flight data information, including the disappearance of Malaysian Airways its location during the post-flight location MH370 in 2014. and recovery (PFLR) phase. Despite flying in surveyed airspace at ICAO GADSS is defined as a performance- the time it went missing, AF447 was only A special multidisciplinary meeting on based approach, meaning the system is found about two years later. global flight tracking (MMGFT) was graded on functionality rather than In 2014 MH370 was lost in the convened in May 2014 to propose mandating a specific solution. Indian Ocean, which is very deep in recommendations for future actions. One parts. Usual methods of accurately of the main decisions taken was the need locating the wreckage have so far been for operators to pursue aircraft flight- Background unsuccessful.
    [Show full text]
  • Instrument and Equipment
    PCAR PART 7 Republic of the Philippines CIVIL AVIATION REGULATIONS (CAR) PART 7 INSTRUMENT AND EQUIPMENT July 2021 Edition i U N C O N T R O L L E D C O P Y W H E N D O W N L O A D E D PCAR PART 7 INTENTIONALLY LEFT BLANK PAGE July 2021 Edition ii U N C O N T R O L L E D C O P Y W H E N D O W N L O A D E D PCAR PART 7 July 2021 Edition iii U N C O N T R O L L E D C O P Y W H E N D O W N L O A D E D PCAR PART 7 July 2021 Edition iv U N C O N T R O L L E D C O P Y W H E N D O W N L O A D E D PCAR PART 7 July 2021 Edition v U N C O N T R O L L E D C O P Y W H E N D O W N L O A D E D PCAR PART 7 RECORD OF AMENDMENTS Amendment No. Date Subject Incorporated By Original Issue 23 June 2008 Ruben F. Ciron First Amendment 21 March 2011 1. 7.2.9 Navigation Equipment Ramon S. Gutierrez Second Amendment 01 August 2013 Inserted vertical bars on the LT GEN William K previous amendments Hotchkiss III AFP (Ret) Third Amendment 31 October 2013 1.
    [Show full text]
  • Aircraft Accident Report: American Airlines, Inc., Mcdonnell Douglas
    Explosive decompression, American Airlines, Inc., McDonnell Douglas DC-10-10, N103AA, Near Windsor, Ontario, Canada, June 12, 1972 Micro-summary: On climb, this McDonnell Douglas DC-10-10 experienced an opening of a cargo door, explosive decompression, and a main cabin floor collapse, disrupting the flight control system. Event Date: 1972-06-12 at 1925 EST Investigative Body: National Transportation Safety Board (NTSB), USA Investigative Body's Web Site: http://www.ntsb.gov/ Cautions: 1. Accident reports can be and sometimes are revised. Be sure to consult the investigative agency for the latest version before basing anything significant on content (e.g., thesis, research, etc). 2. Readers are advised that each report is a glimpse of events at specific points in time. While broad themes permeate the causal events leading up to crashes, and we can learn from those, the specific regulatory and technological environments can and do change. Your company's flight operations manual is the final authority as to the safe operation of your aircraft! 3. Reports may or may not represent reality. Many many non-scientific factors go into an investigation, including the magnitude of the event, the experience of the investigator, the political climate, relationship with the regulatory authority, technological and recovery capabilities, etc. It is recommended that the reader review all reports analytically. Even a "bad" report can be a very useful launching point for learning. 4. Contact us before reproducing or redistributing a report from this anthology. Individual countries have very differing views on copyright! We can advise you on the steps to follow.
    [Show full text]
  • 6 10 13 35 28 16 37 20 24 4 Message from The
    THE ICAO JOURNAL Contents Volume 70, Number 3, 2015 ETHEditorial ICAO JOURNAL Message from the ICAO Council President ICAOVolume Communications 69, Number Unit 1, 2014 4 Tel: +1 (514) 954-8221 Editorialwww.icao.int Landmark World Aviation Forum to Address Sustainable Development ICAO [email protected] Unit twitter.com/icaoTel: +1 (514) 954-8221 6 Challenges www.icao.int The ICAO World Aviation Forum (IWAF) in Montréal will bring together States Editor: [email protected] Rick Adams and the donor/development community to help optimize air transport AeroPerspectivestwitter.com/icao Tel: (33) 434 10 77 05 partnerships and opportunities. Photography [email protected] Photography Website: of AeroPerspectives.com official ICAO events and signings provided by: Aviation Training: Responding to State and Industry Needs Vanda D’Alonzo Photography 10 The annual ICAO Council Off-site Strategy Meeting (COSM 2015) sharply Bang E-mail:Marketing [email protected] StéphanieWebsite: Kennan www.vandaphoto.com focused a short list of new training priorities. Tel: +1 (514) 849-2264 B ang E-mail:Marketing [email protected] Stéphanie Website: Kennan www.bang-marketing.com A Framework for Aviation Capacity Building Tel: +1 (514) 849-2264 13 The key concepts and principles which guide ICAO’s aviation security AdvertisingE-mail: [email protected] assistance and capacity-building through No Country Left Behind. FCM Website:Communications www.bang-marketing.com Inc. Yves Allard Advertising Tel: +1 (450) 677-3535 “Fostering the Conversation” FCM Fax:Communications +1 (450) 677-4445 Inc. Yves E-mail:Allard [email protected] 16 An interview with Stephen Creamer, Director, ICAO Air Navigation Bureau (ANB).
    [Show full text]
  • Federal Aviation Administration, DOT Pt. 135, App. F
    Federal Aviation Administration, DOT Pt. 135, App. F APPENDIX F TO PART 135—AIRPLANE FLIGHT RECORDER SPECIFICATION The recorded values must meet the designated range, resolution and accuracy requirements during static and dynamic condi- tions. Dynamic condition means the parameter is experiencing change at the maximum rate attainable, including the maximum rate of reversal. All data recorded must be correlated in time to within one second. Accuracy (sensor Seconds per Parameters Range input) sampling interval Resolution Remarks 1. Time or Rel- 24 Hrs, 0 to ±0.125% Per 4 ........................ 1 sec ................. UTC time preferred when ative Time 4095. Hour. available. Counter incre- Counts 1. ments each 4 seconds of system operation. 2. Pressure Alti- ¥1000 ft to max ±100 to ±700 ft 1 ........................ 5′ to 35″ ............. Data should be obtained tude. certificated alti- (see table, from the air data computer tude of aircraft. TSO C124a or when practicable. +5000 ft. TSO C51a). 3. Indicated air- 50 KIAS or min- ±5% and ±3% .... 1 ........................ 1 kt .................... Data should be obtained speed or Cali- imum value to from the air data computer brated airspeed. Max Vsoü and when practicable. Vso to 1.2 V.D. 4. Heading (Pri- 0¥360° and Dis- ±2° ..................... 1 ........................ 0.5° .................... When true or magnetic head- mary flight crew crete ‘‘true’’ or ing can be selected as the reference). ‘‘mag’’. primary heading reference, a discrete indicating selec- tion must be recorded. 5. Normal Accel- ¥3g to +6g ....... ±1% of max 0.125 ................. 0.004g eration range exclud- (Vertical) 9. ing datum error of ±5%. 6. Pitch Attitude .
    [Show full text]
  • Mcdonnell Douglas DC 10-30, PP-VMD
    McDonnell Douglas DC 10-30, PP-VMD AAIB Bulletin No: 7/97 Ref: EW/C97/2/1Category: 1.1 Aircraft Type and Registration: McDonnell Douglas DC 10-30, PP-VMD No & Type of Engines: 3 CF6 turbofan engines Year of Manufacture: 1975 Date & Time (UTC): 8 February 1997 at 2227 hrs Location: London Heathrow Airport Type of Flight: Scheduled Passenger Persons on Board: Crew - 18 - Passengers - 127 Injuries: Crew - None - Passengers - None Nature of Damage: No 7 and 8 wheels and tyres badly damaged Commander's Licence: Airline Transport Pilot's Licence Commander's Age: 50 years (approximately) Commander's Flying Experience: 14,000 hours (of which 4,500 were on type) Last 90 days - 60 hours Last 28 days - 20 hours Information Source: AAIB Field Investigation History of Flight The aircraft involved in this accident arrived at London HeathrowAirport from Rio de Janeiro earlier the same day at 1233 hrs. On arrival it was parked at Gate H30 and later towed to its departureGate H5 at 1945 hrs. At 2207 hrs the flight was cleared for enginestart and push-back and it commenced taxiing to Runway 27R nineminutes later. The taxi route to the runway took the aircraftdirectly onto the outer taxiway and then onto Runway 23 whichit backtracked. The total time spent taxiing was approximatelynine minutes. The flight destination was São Paulo, Brazil and, due tothe length of the flight, two flight deck crews were on board. The crew had arrived two days previously and, for the departure,consisted of a Captain in the left hand seat, who was undertakinga conversion from a different aircraft type, and a training Captainin the right hand seat who was the designated aircraft commander.
    [Show full text]
  • Testimony of Ms. Dana Schulze Acting Director, Office of Aviation Safety
    Testimony of Ms. Dana Schulze Acting Director, Office of Aviation Safety National Transportation Safety Board Before the Subcommittee on Aviation Committee on Transportation and Infrastructure United States House of Representatives — On — Status of Aviation Safety — Washington, DC • July 17, 2019 An Independent Federal Agency Good morning, Chairman Larsen, Ranking Member Graves, and Members of the Subcommittee. Thank you for inviting the National Transportation Safety Board (NTSB) to testify before you today. I am the Acting Director of the Office of Aviation Safety within the NTSB. The NTSB is an independent federal agency charged by Congress with investigating every civil aviation accident in the United States and significant accidents in other modes of transportation – highway, rail, marine, and pipeline. We determine the probable cause of the accidents we investigate, and we issue safety recommendations aimed at preventing future accidents. In addition, we conduct special transportation safety studies and special investigations and coordinate the resources of the federal government and other organizations to assist victims and their family members who have been impacted by major transportation disasters. The NTSB is not a regulatory agency – we do not promulgate operating standards nor do we certificate organizations and individuals. The goal of our work is to foster safety improvements, through formal and informal safety recommendations, for the traveling public. We investigate all civil domestic air carrier, commuter, and air taxi accidents; general aviation accidents; and certain public-use aircraft accidents, amounting to approximately 1,400 investigations of accidents and incidents annually. We also participate in investigations of airline accidents and incidents in foreign countries that involve US carriers, US-manufactured or - designed equipment, or US-registered aircraft.
    [Show full text]
  • FY 2014 R&D Annual Review
    FY 2014 R&D Annual Review August 2015 Report of the Federal Aviation Administration to the United States Congress pursuant to Section 44501(c) of Title 49 of the United States Code FY 2014 R&D Annual Review August 2015 The R&D Annual Review is a companion document to the National Aviation Research Plan (NARP), a report of the Federal Aviation Administration to the United States Congress pursuant to Section 44501(c)(3) of Title 49 of the United States Code. The R&D Annual Review is available on the Internet at http://www.faa.gov/go/narp. FY 2014 R&D Annual Review Table of Contents Table of Contents Introduction ..............................................................................................................1 R&D Principle 1 – Improve Aviation Safety ......................................................... 2 R&D Principle 2 – Improve Efficiency ................................................................79 R&D Principle 3 – Reduce Environmental Impacts ..........................................93 Acronym List ........................................................................................................106 i FY 2014 R&D Annual Review List of Figures List of Figures Figure 1: Simulation Validation of GSE Impact Loading on 5-Frame .......................................... 2 Figure 2: Shear Tie Crushing Model Validation............................................................................ 3 Figure 3: Skin Cracking Model Validation ...................................................................................
    [Show full text]
  • Flight Data Recorder Handbook for Aviation Accident Investigations
    National Transportation Safety Board Vehicle Recorder Division Flight Data Recorder Handbook for Aviation Accident Investigations Office of Research and Engineering Office of Aviation Safety Washington, DC 20594 A Reference for Safety Board Staff ii FOREWORD This handbook provides general information to assist the investigator-in-charge, group chairmen, and other Safety Board staff who may encounter a flight data recorder during the course of an aviation accident investigation. It is intended to provide guidance on the procedures, laws and standard practice surrounding the flight data recorder and its recorded information during the course of an investigation. The Vehicle Recorder Division will be responsible for keeping this handbook updated. The handbook's printing date will be indicated in the upper left corner of each page. While the intent of the handbook is to provide guidance for handling a flight data recorder and its recorded information, the handbook may not cover all situations, and any questions or concerns may be directed to the Chief of the Vehicle Recorder Division for immediate assistance. This handbook is an NTSB staff product and is intended to provide information and guidance to NTSB employees who are involved in the flight data recorder portion of an aviation accident investigation. This handbook has not been adopted by the NTSB Board Members, is not regulatory in nature, is not a binding statement of policy, and is not all- inclusive. The recommended procedures are not intended to become obligations of the NTSB or to create any rights in any of the parties to an NTSB investigation. Deviation from the guidance offered in this handbook will at times be necessary to meet the specific needs of an investigation.
    [Show full text]
  • CS-25 / Amendment 23
    CS-25 AMENDMENT 23 — CHANGE INFORMATION EASA publishes amendments to certification specifications as consolidated documents. These documents are used for establishing the certification basis for applications made after the date of entry into force of the amendment. Consequently, except for a note ‘[Amdt No: 25/23]’ under the amended paragraph, the consolidated text of CS-25 does not allow readers to see the detailed changes introduced by the new amendment. To allow readers to also see these detailed changes, this document has been created. The same format as for publication of Notices of Proposed Amendments (NPAs) has been used to show the changes: (a) deleted text is struck through; (b) new or amended text is highlighted in blue; (c) an ellipsis ‘[…]’ indicates that the remaining text is unchanged. Page 1 of 17 BOOK 1 SUBPART D — DESIGN AND CONSTRUCTION CS 25.791 Passenger information signs and placards (See AMC 25.791) […] (d) Lavatories must have ‘No Smoking’ or ‘No Smoking in Lavatory’ placards conspicuously positioned located on or adjacent to each ashtray side of the entry door. The placards must have red letters at least 13 mm (0·5 inches) high on a white background of at least 25 mm (1·0 inches) high. (A No Smoking symbol may be included on the placard.) […] CS 25.831 Ventilation (a) Each passenger and crew compartment must be ventilated and each crew compartment must have enough fresh air (but not less than 0.28 m3/min. (10 cubic ft per minute) per crewmember) to enable crewmembers to perform their duties without undue discomfort or fatigue.
    [Show full text]