Service difficulty report · Transceiver

Difficulty date
March 16, 2010
Submitted
March 24, 2010
Operation
General aviation
Part
Transceiver
Part number
9810871
Part serial
FD3213
Condition
Malfunctioned
Location
Glideslope
Stage of operation
IN
How discovered
C
Nature of condition
L
Precautionary procedure
K

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

ON 01/30/2010 POST INSTALLATION, EMI TESTING WAS CONDUCTED IAW APPENDIX B OF TDFM-136 INSTALLATION AND OPERATING INSTRUCTIONS TIL DOC NR 99RE255, REV D ISSUE 7, DATED APRIL 2004. AS A RESULT OF THOSE TESTS IT WAS DETERMINED THAT AN INTERFERENCE PROBLEM EXISTS AS PERTAINING TO THE OPERATION OF THE ACFT GLIDESLOPE SYS WHILE BEING RAMP CHECKED. THIS INTERFERENCE OCCURS IN THE FORM OF THE GLIDESLOPE FLAGGING A LOSS OF SIGNAL AND/OR GLIDESLOPE NEEDLE DEFLECTIONS. 3 DIFFERENT ACFT AND 7 DIFFERENT TDFM-136 TRANSCEIVERS WERE RAMP TESTED AND IT WAS DETERMINED THAT THE PROBLEM IS PREVALENT IN ALL TDFM-136 TRANSCEIVERS TESTED. MFG REP INDICATED THE MFG CONDUCTS HARMONIC ATTENUATION LEVEL TESTING AT THE TEST FREQUENCIES OF 138, 156, AND 174 MHZ. THE FREQUENCIES DO NOT GENERATE A 2ND HARMONIC WITHING THE GLIDESLOPE FREQUENCY RANGE AND THE TRANSMIT FREQUENCIES OF 164.575 THROUGH 167.500 WHICH WOULD GENERATE AND 2ND HARMONIC WITHIN THE GLIDESLOPE FREQUENCY RANGE ARE NOT BEING CHECKED AS PART OF FINAL CERTIFICATION TESTING. ORU TESTING SHOWS SIGNIFICANT 2ND HARMONICS WITHIN THE 164.575 THROUGH 167.500 MHZ RANGE WHICH ARE OF SUFFICIENT ENOUGH LEVEL AS TO INTERFERE WITH RECEPTION OF THE GLIDESLOPE SIGNAL DURING RAMP TESTING. MFG ISSUED TIL NR TIBFM 03-06 DATED 03/09/10 REQUIRING PLACARDING OF ACFT WHILE THEY ENGINEER A REPAIR FOR REDUCING EXCESSIVE 2ND HARMONIC LEVELS FROM THEIR TRANSCEIVER.