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)

Read the untranslated law here: http://www.gesetze-im-internet.de/luftgerpv1998dv_2/BJNR505800000.html

Second implementing regulation regulation for testing aviation equipment (airworthiness requirements for aircraft) (2. DV LuftGerPV) 2 DV LuftGerPV Ausfertigung date: 03.02.2000 full quotation: "second implementing regulation on the regulation for the testing of aviation equipment (airworthiness requirements for aircraft) of 3 February 2000 (BAnz. (2000 Nr. 58 S. 4897), last by article 1 of the Decree of December 12, 2014 (BAnz. 2014, AT 23.12.2014 V2) has been changed "stand: last V2 amended by art. 1 V v. 12 12 2014 Banz Abbey, AT 23.12.2014 learn more about the stand number in the menu see remarks footnote (+++ text detection from: 24.3.2000 +++) input formula on the basis of § 32 para 4 sentence 1 No. 1 and 3 sentence 3 of the air traffic act as amended by the notice of 27 March 1999 (BGBl. I S.) (550) in conjunction with § 21 of the regulation for the testing of aviation equipment (LuftGerPV) of 3 August 1998 (BGBl. I p. 2010, 2011) prescribed the Luftfahrt-Bundesamt: § 1 airworthiness requirements (building codes) are LuftGerPV to the airworthiness according to § 1 para 2 1 for category a aircraft) aircraft the "joint aviation requirements - large aeroplanes (JAR-25)" in the version of October 1, 2000 ("15") change, and the "joint aviation requirements - all weather operations (JAR-AWO)" in the version of 1 August 1996 ("2") change , b) normal, utility, acrobatic and feeder aircraft the "joint aviation requirements - normal, utility, aerobatic and commuter Catégorie aeroplanes (JAR-23)" of 11 March 1994, c) easy aircraft the "joint aviation requirements - very light aeroplanes (JAR-VLA)" by April 26, 1990, 2 for category a rotorcraft amended by the addition ("orange paper"), VLA/92/1 from 1 January 1992,) normal rotorcraft the "joint aviation requirements - small rotorcraft (JAR-27)" of 6 September 1993 , as last amended by the addition ("orange paper") 27/98/1 of 16 February 1998, b) transport rotorcraft the "joint aviation requirements - large rotorcraft (JAR-29)" dated November 5, 1993, as last amended by the addition ("orange paper") 29/98/1 of 16 February 1998, 3rd for gliders and motor gliders the "airworthiness requirements for gliders and motor gliders (JAR-22), Amendment 6 by 1 August 2001 (NfL II-29/02)" , 4 (dropped out) 5 for airships of category a) normal -, commercial -, and shuttle air ship the "airworthiness requirements for airships of the category normal and shuttle (LFLS)" of 3 August 1999 (NfL II-103/99, NfL II-25/01), b) hot air airships the "airworthiness requirements for hot air airships (LFHLLS)" of 30 October 1997 (BAnz. P. 13 594), c) traffic "Transport Airship Requirements (TAR)" by March 2000 (NfL II-22/01), 6 for manned balloons of category a) hot air balloons the "airworthiness requirements for hot-air balloons (LFHB)" of 23 February 1982 (BAnz. No. 43 of 4 March 1982), b) gas balloons the "airworthiness requirements for manned gas balloon (LFGB)" of 20 September 1993 (BAnz. S. 9286), c) tethered gas balloons the "airworthiness requirements for tethered gas balloons to the passenger transport (LFFB)" by August 12, 1997 (BAnz. P. 10 469), 7 for air sports equipment of category a) aerodynamically-controlled, motor-powered microlights the "airworthiness requirements for aerodynamically controlled microlights" of 30 January 2003 (NfL II-17/03), b) gravity-driven microlights aa) the "airworthiness standards for gravity controlled microlights type: Trike and foot start-UL" bb (NfL II-22/05), 3 February 2005) the "airworthiness standards for gravity controlled microlights type: paramotor and Motorschirmtrike" by February 3, 2005 (NfL II-23/05) , c) hang glider and glider the "airworthiness requirements for gliders and glider" by December 17, 2009 (NfL II-91/09), as amended by the notice of the change of "Airworthiness requirements for gliders and glider" from 24 July 2014 (NfL 2-55-14) and 22 August 2014 (NfL 2-60-14), d) jump parachutes the "airworthiness requirements for crack parachute systems" by 7 February 2000 (NfL II-24/2000, NfL II-20/03), e) rescue device for air equipment the "airworthiness requirements for rescue equipment for microlights" of 30 September 1999 (NfL II-122/99) , f) microlights in the design Drehflügelflugzeuge (autogyro) the "building regulations for ultralight autogyro (piston-single)" changed from September 26, 2001 (NfL II-89/01) by the publication of the amendment of the notice by "building regulations for ultralight autogyro (piston-single)" by February 12, 2009 (NfL II-13/09), as well as by the publication of the amendment of the notice by "building regulations for ultralight autogyro (piston-single)" from 18 October 2012 (NfL II-67/12) , g) aerodynamic controlled air sports equipment with a maximum unladen mass up to 120 kg the announcement by air efficiency requirements for aerodynamically-controlled air sports equipment up to 120 kg unladen mass (not motorized or motorized) by March 22, 2012 (NfL II-23/12), 8 for model aircraft category a) remote-controlled space flight models the "airworthiness requirements for remote controlled model of surfaces aircraft with a maximum take-off weight of more than 25 kg and up to 150 kg" by March 2, 2011 (NfL II-21/11) , b) remote-controlled, unmanned model hot air balloons the "airworthiness requirements for remote, unmanned model hot air balloons with a maximum takeoff weight of more than 25 kg and up to 150 kg" by March 2, 2011 (NfL II-22/11), c) remote-controlled model helicopter the "airworthiness requirements for remote controlled model helicopter with a maximum takeoff weight of more than 25 kg and up to 150 kg" by March 2, 2011 (NfL II-23/11), d) remote-controlled model air ships the "airworthiness requirements for remote controlled model air ships with a maximum permissible take-off weight of more than 25 kg and up to" (150 kg"by March 2, 2011 (NfL II-24/11), 9 for aircraft engines the"joint aviation requirements - engines (JAR-E)"amended on 15 August 1999 ("10 ") change, 10 for propeller the"joint aviation requirements - propeller (JAR-P)"in the version of October 22, 1987 ("change 7"), as last amended by the addition ("orange paper") P/96/1 of 8 August 1996, 11 for other aviation unit a) in article 1, paragraph 1 regulations referred to in no. 11 of air traffic approval regulations , b) the "joint aviation requirements - auxiliary power units (JAR-APU)" in the version of September 26, 1983 ("change 2"), as last amended by the addition ("orange paper"), APU/96/1 of 8 August 1996, c) the "airworthiness requirements for tow couplings" by August 4, 1976 (BAnz. No. 148, August 11, 1976), d) the 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 known made national of technical standards to apply as a airworthiness requirements *). The establishment of case-related additional requirements for "Certification procedures for aircraft and related products, and parts (JAR-21)" remains unaffected.
---*) The joint aviation requirements (JAR) can be obtained from the joint aviation authorities (JAA). The address is: PO box 3000, Saturnusstraat 8-10, 2130KA Hoofddorp, Netherlands.

§ 2 force - section 3 entry into force this regulation enters into force on the day after the announcement.