04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
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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 />
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