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<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />

10<strong>01</strong>6451 PANASONIC AVIONICS CORPORATION <strong>EASA</strong>.IM.A.S.02797 - BOEING 757-200 SERIES Installation of a Matsuhita Avionics Audio Prior to installation of this modification the<br />

18.07.2008<br />

System on a Boeing 757-200 Aircraft. installer must determine that the<br />

interrelationship between this modification and<br />

any other previously installed modification will<br />

introduce no adverse effect upon the<br />

airworthiness of the product. The install<br />

10<strong>01</strong>6826 PARAVION TECHNOLOGY INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>196 FAA STC SR00338DE BELL 407 Installation of Anti-Torque Extention Adjustment None<br />

System<br />

30.06.2006<br />

10<strong>01</strong>6875 PARAVION TECHNOLOGY INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>252 FAA STC SR00375DE BELL 206A/B/L/L-1/L-3/L-4 Laser Mapping Installation This STC is approved only for the product<br />

15.09.2006<br />

BELL 206L-4<br />

configuration as defined in the approved design<br />

data referred to in the paragraph "Description".<br />

Compatibility with other aircraft/engine<br />

configurations shall be determined by the<br />

installer.<br />

10<strong>01</strong>6949 PARAVION TECHNOLOGY INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>344 FAA STC SR0<strong>04</strong>89SE BELL 407 Installation of Cabin Air Conditioner System. 21.08.2007<br />

10<strong>01</strong>6950 PARAVION TECHNOLOGY INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>345 FAA STC SR00280DE BELL 407 Installation of Bleed Air Cabin Heater System. 21.08.2007<br />

10<strong>01</strong>6952 PARAVION TECHNOLOGY INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>348 FAA STC SR00025DE BELL 206A/B/L/L-1/L-3/L-4, 407 Installation of an Equipment Tray. This approval is for a shelf only. The shelf is<br />

rated for a 15 pound load and must be<br />

placarded as shown in drawing 206ET-1000,<br />

Revision B dated 9 February 1993 or later<br />

approved revision.On 206A and B models, this<br />

approval is for serial numbers 154 and su<br />

10<strong>01</strong>6953 PARAVION TECHNOLOGY INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>349 FAA STC SR00335DE BELL 407 Snow Pads Installation. 21.08.2007<br />

10<strong>01</strong>6954 PARAVION TECHNOLOGY INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>350 FAA STC SR00344DE BELL 407 Installation of External Mirror. (This STC has<br />

been classified as “BASIC” by the FAA in<br />

accordance with FAA Order 8110.52 and has<br />

been approved using the PTVP Procedures.)<br />

06.09.2007<br />

10<strong>01</strong>6955 PARAVION TECHNOLOGY INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>351 FAA STC SR00<strong>01</strong>1DE BELL 206B/L/L-1/L-3/L-4, 407 Provision for Mount of a Video Monitor Placed<br />

on Left or Right Instrument Panel Console.<br />

10<strong>01</strong>6956 PARAVION TECHNOLOGY INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>352 FAA STC SR0<strong>04</strong>86DE BELL 407 Installation of mounting hardware and approval<br />

for the aircraft to be operated by a single pilot<br />

from the left crew seat.<br />

This approval is for the Mount Assembly only.<br />

The monitor installed must meet the<br />

requirements shown in drawings approved<br />

under theMaster Drawing List No. DL-<br />

206/407MM-110 revision N/C dated 27 July<br />

1999 or later approved revision.On Bell 206B<br />

models, this<br />

For left seat operation of equipment originally<br />

intended to be operated by the pilot from the<br />

right crew seat, provisions must be made to<br />

ensure that such equipment can be equally<br />

operable from the left crew seat with similar<br />

controls.<br />

10<strong>01</strong>6957 PARAVION TECHNOLOGY INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>353 FAA STC SR0<strong>04</strong>11DE BELL 407 Installation of Mounting Hardware to Support<br />

Blade Folding Kit.<br />

10.09.2007<br />

10<strong>01</strong>6964 PARAVION TECHNOLOGY INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>365 FAA STC SR00574DE BELL 407 Installation of 407FL-100 FADEC/Check<br />

instrument auxiliary annunciation system. (This<br />

STC has been classified as “BASIC” by the<br />

FAAin accordance with FAA Order 8110.52<br />

and has been approved using the PTVP<br />

Procedures.)<br />

06.09.2007<br />

10<strong>01</strong>6965 PARAVION TECHNOLOGY INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>366 REV. 1 FAA STC SR00349DE BELL 407 Installation of a Searchlight. This STC has been<br />

classified as “BASIC” by the FAA and has been<br />

approved under the PTVP.<br />

19.03.2008<br />

10<strong>01</strong>6966 PARAVION TECHNOLOGY INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>367 FAA STC SR00348DE BELL 407 Infrared Imaging System Installation. This STC None.<br />

has been classified as “BASIC” by the FAA and<br />

has been approved under the PTVP.<br />

22.05.2008<br />

10<strong>01</strong>6998 PARAVION TECHNOLOGY INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>408 FAA STC SH2726NM 269A, 269B, 269C Cabin Heater Installation. Prior to installation of this modification the<br />

installer must determine that the<br />

interrelationship between this modification and<br />

any other previously installed modification will<br />

introduce no adverse effect upon the<br />

airworthiness of the product. The install<br />

10<strong>01</strong>7038 PARAVION TECHNOLOGY INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong><strong>462</strong> FAA STC SR0<strong>04</strong><strong>01</strong>DE BELL 206L/L1/L3/L4 AND 407 Snow deflector Installation. 18.07.2008<br />

10<strong>01</strong>7<strong>04</strong>1 PARAVION TECHNOLOGY INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>465 FAA STC SR00334DE BELL 407 Pneumatic Door Opener (PDO). This STC has<br />

been classified as “BASIC” by the FAA and has<br />

been approved under the PTVP.<br />

09.06.2008<br />

<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 353/<strong>462</strong><br />

21.08.2007<br />

21.08.2007<br />

21.08.2007<br />

24.09.2008

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