Second Implementing Regulation On The Regulation For The Testing Of Aviation Equipment (Airworthiness Requirements For Aircraft)

Original Language Title: Zweite Durchführungsverordnung zur Verordnung zur Prüfung von Luftfahrtgerät (Lufttüchtigkeitsforderungen für Luftfahrtgerät)

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Second Implementing Regulation to the Regulation for the examination of aeronautical equipment (airworthiness requirements for aeronautical equipment) (2. DV LuftGerPV)

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2. DV LuftGerPV

Date of delivery: 03.02.2000

Full quote:

" Second implementing regulation of the Regulation for the examination of aeronautical equipment (airworthiness requirements for aeronautical equipment) of 3. February 2000 (BAnz. 58 p. 4897), as last amended by Article 1 of the Regulation of 12 June 2000. December 2014 (BAnz. 2014, AT 23.12.2014 V2) has been modified "

:Last modified by Art. 1 V v. 12.12.2014 BAnz, AT 23.12.2014 V2

See Notes


(+ + + Text Evidence: 24.3.2000 + + +)

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On the basis of section 32 (4) sentence 1 no. 1 and paragraph 3 sentence 3 of the Aviation Act in the Date of publication of the 27. March 1999 (BGBl. 550) in conjunction with Article 21 of the Aviation Equipment Testing Ordination (LuftGerPV) of 3 June 2008. August 1998 (BGBl. 2010, 2011), the Federal Aviation Office (Bundesamt) orders: Non-official table of contents

§ 1 Airworthiness requirements (building regulations)

To test the Airworthiness in accordance with § 1 para. 2 LuftGerPV are
for aircraft of category
Transport aircraft the "Joint Aviation Requirements-Large Aeroplanes (JAR-25)" in the version of the 1. October 2000 ("change 15"), and the "Joint Aviation Requirements-All Weather Operations (JAR-AWO)" in the version of 1. August 1996 ("change 2"),
Normal, useful, acrobatics, and feeder aircraft the " Joint Aviation Requirements-Normal, Utility, Aerobatic and Commuter Categorie Aeroplanes (JAR-23) " of 11. March 1994,
Single aircraft, the "Joint Aviation Requirements-Very Light Aeroplanes (JAR-VLA)" of 26 March 1994. 4 April 1990, as last amended by the supplement ("orange paper") VLA/92/1 of 1. January 1992
for category
Normal rotary wing the "Joint Aviation Requirements-Small Rotorcraft (JAR-27)" of 6. September 1993, as last amended by the supplement ("orange paper") 27/98/1 of 16. February 1998,
The "Joint Aviation Requirements-Large Rotorcraft (JAR-29)" of the 5th edition of the "Transport Shooting Wing" of the 5th edition of the German Transport Committee. November 1993, as last amended by the supplement ("orange paper") 29/98/1 of 16 November 1993. February 1998
for gliders and sailors the " Airworthiness requirements for sailplanes and motor sailers (JAR-22), Amendment 6 of 1. August 2001 (NfL II-29/02) ",
for airships of category
Normal, utility, and feeder airships " Airworthiness requirements for category airships Normal and Zubringer (LFLS) " of 3. August 1999 (NfL II-103/99, NfL II-25/01),
Hot-air airships the "Airworthiness Requirements for Hot Air Airships (LFHLLS)" of 30 August 1999. October 1997 (BAnz. 13 594),
Transport of the Transport Airship Requirements (TAR) of March 2000 (NfL II-22/01)
for manned balloons of category
Hot air balloons the "Airworthiness requirements for hot air balloons (LFHB)" of 23. February 1982 (BAnz. No. 43 of 4. March 1982),
Gas balloons, the "Airworthiness Requirements for manned gas balloons (LFGB)" of 20. September 1993 (BAnz. S. 9286),
captured gas balloons, the "Airworthiness Requirements for Tied Gas Balloons for Personnel Transport (LFFB)" of 12. August 1997 (BAnz. 10 469)
for category
a) air sports equipment
motorized, aerodynamically controlled ultralight aircraft the "airworthiness requirements for aerodynamically controlled ultralight aircraft" of the 30. January 2003 (NfL II-17/03),
heavyweight ultralight aircraft
the "Airworthiness Requirements for Gravity Controlled Ultralight Aircraft Design: Trike and Footstart UL" of the 3. February 2005 (NfL II-22/05),
The "airworthiness requirements for heavy-power ultralight aircraft type: motorshade and motor umbrella trike" of 3 February 2005. February 2005 (NfL II-23/05)
Hangglider and Sliding Sail the "Airworthiness Requirements for Hangglider and Sliding Sail" of 17 February 2005. December 2009 (NfL II-91/09), as amended by the notice on the amendment of 'Airworthiness requirements for hang gliders and floorsail' of 24 December 2009. July 2014 (NfL 2-55-14) and 22. August 2014 (NfL 2-60-14),
Jump umbrellas are the "Airworthiness Requirements for Diving Parachute Systems" of 7. February 2000 (NfL II-24/2000, NfL II-20/03),
Air-sports equipment rescue device for "airworthiness requirements for rescue equipment for ultralight aircraft" of the 30th of June 2000. September 1999 (NfL II-122/99),
Ultralight aircraft in the design of rotary wing aircraft (gyroscope) the "construction regulations for ultra-light power-carrying helicopters (single-engine)" of the 26. September 2001 (NfL II-89/01), amended by the Notice of Amendment of the Notice of "Construction Regulations for Ultralight Helicopters (einmotorig)" of 12 September 2001. February 2009 (NfL II-13/09), as well as by the notice of the amendment of the Notice of Construction Regulations for Ultralight Helicopters (single-engined) of 18 February 2009 (NfL II-13/09). October 2012 (NfL II-67/12),
aerodynamic controlled air sports equipment with a maximum permissible laden mass of up to 120 kg the " Announcement of Airworthiness requirements for aerodynamically controlled air sports equipment up to 120 kg of empty mass (not motorized or motorized) " of 22. March 2012 (NfL II-23/12),
for category
flight models
remote-controlled surface flight models the "airworthiness requirements for remote-controlled surface flight models with a maximum allowable starting mass of more than 25 kg and up to 150 kg" of the 2. March 2011 (NfL II-21/11),
Remote-controlled, unmanned model hot air balloons " Airworthiness requirements for remote-controlled, unmanned model-hot air balloons with a maximum permissible starting mass of more than 25 kg and up to 150 kg " of the 2. March 2011 (NfL II-22/11),
Remote-controlled model helicopters the " Airworthiness requirements for remote-controlled model helicopters with a maximum allowable Starting mass of more than 25 kg and up to 150 kg " of the 2. March 2011 (NfL II-23/11),
Remote-controlled model airships "The" airworthiness requirements for remote-controlled model airships with a maximum starting mass " more than 25 kg and up to 150 kg " of the 2. March 2011 (NfL II-24/11)
for aircraft engines, the "Joint Aviation Requirements Engines (JAR-E)" in the version of 15. August 1999 ("change 10"),
for Propeller the "Joint Aviation Requirements-Propellers (JAR-P)" in the version of the 22. October 1987 ("change 7"), as last amended by the supplement ("orange paper") P/96/1 of 8. August 1996,
for other aeronautical device
the regulations referred to in § 1 para. 1 no. 11 of the Air Traffic Authorisation Order,
the " Joint Aviation Requirements-Auxiliary Power Units (JAR-APU) " in the version of the 26. September 1983 ("change 2"), as last amended by the supplement ("orange paper") APU/96/1 of 8. 8 August 1996,
the "Airworthiness requirements for tow couplings" of 4. August 1976 (BAnz. N ° 148 of 11
the National Technical Institutes of NfL II-39/01, II-60/01, II-73/01, II-77/01, II-87/01, II-25/02, II-78/02, II-101/02, II-19/03 and II-29/03. Standards,
to be used as airworthiness requirements *). This does not affect the setting of individual additional requirements according to "Certification Procedures For Aircraft and Related Products and Parts (JAR-21)".
The Joint Aviation Requirements (JAR) can be obtained through the Joint Aviation Authorities (JAA). The address is: PO Box 3000, Saturnusstraat 8-10, 2130KA Hoofddorp, The Netherlands.
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§ 2 External force

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§ 3 Entry into force

This Regulation will enter into force on the day after the announcement.