WLAN activationElectro-Magnetic Compatibility demonstrationof aeroplane's requiredsystems immunity to worst case...
Overview
Introduction
WLAN activationElectro-Magnetic Compatibility demonstrationof aeroplane's requiredsystems immunity to worst case WLAN IEEE 802.11 a/b/g/n passengerscarry- on TPED transmissions. Certification Basis The Certification Basis for the original product remains applicable tothis certificate/ approval.The certificated noiseand/ or emissions levels of the original productare unchanged and remain applicable to this certificate/ approval. Limitations - Master Data List, Doc. No. BFSLA001-002, Rev. IR, dated 11.01.2013- AFMS, Doc. No. BFLSA001-201-02, Rev. IR, dated 11.01.2013- ICA, Doc. No. BFLSA001-150- 02, Rev. IR, dated 10.12.2012or later revisions of the above listed documents approved by EASA. Conditions S/N: 348 F-GLSA
Product Description
WLAN activationElectro-Magnetic
Compatibility demonstrationof aeroplane's
requiredsystems immunity to worst case
WLAN IEEE 802.11 a/b/g/n passengerscarry-
on TPED transmissions.
Certification Basis
The Certification Basis for the original product
remains applicable tothis certificate/
approval.The certificated noiseand/ or
emissions levels of the original productare
unchanged and remain applicable to this
certificate/ approval.
Limitations
- Master Data List, Doc. No. BFSLA001-002,
Rev. IR, dated 11.01.2013- AFMS, Doc. No.
BFLSA001-201-02, Rev. IR, dated
11.01.2013- ICA, Doc. No. BFLSA001-150-
02, Rev. IR, dated 10.12.2012or later
revisions of the above listed documents
approved by EASA.
Conditions
S/N: 348 F-GLSA
Please contact modification supplier for further details.
STC Status: Revision Level:
STC Date: 17/01/13
Responsible Office: EASA