FAA's Reported Wire Incidents - Oct and Nov 2008
Author: Lectromec
Published: 01-01-2009
FAA's
Reported Wire Incidents – October & November 2008
Author: Lectromec GSD Team
January 1, 2009
The following are the wire incidents reported in the
FAA’s October and November 2008 Advisory Circular 43-16A –
Alert Number 363 and 364 [Original Document2 Here]
http://www.faa.gov/aircraft/safety/alerts/aviation_maintenance/media/2008/2008_10_Alert.pdf
and here
http://www.faa.gov/aircraft/safety/alerts/aviation_maintenance/media/2008/2008_11_Alert.pdf
Incident #1
DASSAULT
Dassault:
900B; Failed Circuit Breaker; ATA 2400
A
repair station report states, "While troubleshooting AC
electrical outlets for being inoperative, (we)
removed
a floor panel to access the AC inverter and smelled burning plastic.
We found this system had self-resetting circuit breakers installed
that had been (resetting
themselves)—and
were continuing to reset (themselves)—allowing
the Kapton wire insulation and spiral wrap to burn. One of the areas
that burned was only three inches below a carbon flight control rod.
I believe had this happened on a very long flight the outcome could
have been very tragic. (It
is suggested...) replacing
these circuit breakers with (manually
operated) circuit
breakers would prevent the damage (which
this report describes)."
(Original
Part: Kilxon Circuit breaker; P/N M13516/5-1; aircraft total time not
provided.)
Part
Total Time: (unknown).
Incident
#2
FAA
Control Number: GUU2008F00065
Aircraft
Make: Beech
Aircraft
Model: 1900D
Part
Name: Wire
Part
Condition: Out of Position
Difficultly
Date: 9/14/2008
Part
Location: Landing Light
After takeoff
upon turning both landing lights switches off there was a spark
coming out of the switch. Spliced and repositioned wire at LT landing
light switch. Ops check good. (k)
Incident
#2
FAA
Control Number: USA2008F00031
Aircraft
Make: Boeing
Aircraft
Model: 7373G7
Part
Name: Wire
Part
Condition: Broken
Difficultly
Date: 09/15/2008
Part
Location: Emergency Lights
Maint
reported the emergency escape path light on seat row 22, LT side,
inoperative. Maint troubleshot and found a broken wire. Operational
check good. (k)
Incident
#3
FAA
Control Number: USA2008F00032
Aircraft
Make: Boeing
Aircraft
Model: 7374B7
Part
Name: Wire
Part
Condition: Broken
Difficultly
Date: 09/15/2008
Part
Location: Emergency Lights
Maint
reported the seat mounted emergency lights from seat rows 20 to 25
inoperative. Maintenance found a broken wire. Spliced wires together.
Operational check good. (k)
Incident
#4
FAA
Control Number: USA2008F00029
Aircraft
Make: Boeing
Aircraft
Model: 7374B7
Part
Name: Wire
Part
Condition: Broken
Difficultly
Date: 09/13/2008
Part
Location: Emergency Lights
Maintenance
reported the emergency escape path lighting from seat rows 19 to 25,
LT side, inoperative. Maint repaired wiring at seat row 25 IAW
standard practices. Emergency lighting operationally checks
satisfactory. (k)
Incident
#5
FAA
Control Number: EIA2008050
Aircraft
Make: Boeing
Aircraft
Model: 747212B
Part
Name: Wire
Part
Condition: Damaged
Difficultly
Date: 09/17/2008
Part
Location: Emergency Lights
Each
emergency light on upper deck ceiling are out. Emergency light assy
U/D aft replaced IAW mm 33-51-00. Ops checked normal. Repaired wire
at pin NR 3 broken at kite assy IAW standard practices also repaired
pin IAW manual ops checked normal. (k)
Incident
#6
FAA
Control Number: NWAA084196309
Aircraft
Make: Boeing
Aircraft
Model: 747451
Part
Name: Wire
Part
Condition: Loose
Difficultly
Date: 09/8/2008
Part
Location: Emergency Lights
During
over night check, found emergency floor lights from row 51 to 65 ABC
inoperative. Maintenance repaired loose wire at pin connection. Ops
checked good, and aircraft was returned to service.
Incident
#7
FAA
Control Number: 2008FA0000671
Aircraft
Make: Cessna
Aircraft
Model: 208B
Part
Name: Wire Harness
Part
Condition: Chafed
Difficultly
Date: 09/24/2008
Part
Location: Flap System
Tie
wrap was missing from the clamp at FS 201.50, which allowed the
wiring bundle containing the wires for the flap sys primary motor to
sag and chafe through wire NR CC75 to the flap system and partially
through LA61 to the cargo area lights on the bulkhead. This caused
the flaps to only receive power to the primary motor in one
direction. Since wire LA61 wasn't chaffed completely through the
cargo area lights were still working.
Incident
#8
FAA
Control Number: COMA0860391
Aircraft
Make: CNDAIR
Aircraft
Model: CL6002B19
Part
Name: Wire Harness
Part
Condition: Failed
Difficultly
Date: 09/15/2008
Part
Location: NLG
Received
gear disagree MSG on T/O. NLG did not retract. Performed GRH for gear
disagree. Emergency declared, A/C returned back and landed safely.
Removed and replaced NLG WOW NR 2 wire harness.
Incident
#9
FAA
Control Number: COMA0860390
Aircraft
Make: CNDAIR
Aircraft
Model: CL6002B19
Part
Name: Wire Harness
Part
Condition: Failed
Difficultly
Date: 09/12/2008
Part
Location: RT MLG
On
climbout, received anti-skid caution MSG. Emergency declared, A/C
returned back and landed safely. Removed and replaced RT MLG OB
anti-skid wire harness.
Incident
#10
FAA
Control Number: MWE2008F00038
Aircraft
Make: DOUG
Aircraft
Model: DC981
Part
Name: Wire
Part
Condition: Broken
Difficultly
Date: 08/27/2008
Part
Location: Emergency Light
Emergency
floor level lights out row 5-8. Found broken wire and repaired.
Incident
#11
FAA
Control Number: AALA200802267
Aircraft
Make: DOUG
Aircraft
Model: DC983
Part
Name: Wire Harness
Part
Condition: Loose
Difficultly
Date: 09/03/2008
Part
Location: Cabin
Emergency
light at seat 15D inoperative. Secured wire harness for emergency
light at seat 15D. System ground checked normal operation.
Incident
#12
FAA
Control Number: WGE2008F00002
Aircraft
Make: Eclipse
Aircraft
Model: Eclipse A500
Part
Name: Wire
Part
Condition: Damaged
Difficultly
Date: 09/02/2008
Part
Location: Overheat Sensor
Repaired
fire overheat sensor high wire engine R0612-22 IAW EA 500 wiring
repair manual section 3.27 for ops check C/W fire detection wire
adjustment/ test IAW EA500, AMM 26-10-00-071-801. Ops check good.
Reference log page 0875, DIS NR 2.
Incident
#13
FAA
Control Number: C2X2008F00043
Aircraft
Make: EMB
Aircraft
Model: EMB145EP
Part
Name: Wire Harness
Part
Condition: Burned
Difficultly
Date: 09/07/2008
Part
Location: Emergency Lights
During
preflight inspection the crew reported a smoke odor coming from seats
3 & 4a. The A/C was released on MEL 33-20-00 Cat C control NR
153947. The ac landed, where maintenance removed and replaced the
light socket harness assy at row 4A, operationally checked with no
defects, removed the MEL, and the A/C was approved for return to
service.
Incident
#14
FAA
Control Number: RAIA00809029
Aircraft
Make: EMB
Aircraft
Model: EMB145EP
Part
Name: Wire
Part
Condition: Broken
Difficultly
Date: 09/27/2008
Part
Location: NLG WOW
Landing
gear air/ground fail message on the EICAS. Maint found a broken wire
at the NLG WOW switch. Wires were repaired and ops check proved good
fix.
Incident
#15
FAA
Control Number: FDK2008F00011
Aircraft
Make: EMB
Aircraft
Model: EMB145LR
Part
Name: Wire
Part
Condition: Broken
Difficultly
Date: 09/09/2008
Part
Location: Emergency Lights
Both
lower exit signs and 2 floor strips inoperative. Maintenance repaired
broken wire at lower assy.
Incident
#16
FAA
Control Number: C2XA08CL102
Aircraft
Make: EMB
Aircraft
Model: EMB145LR
Part
Name: Wire Harness
Part
Condition: Defective
Difficultly
Date: 08/31/2008
Part
Location: NLG
CLE
flight NR2320 the crew reported an air/ground fail message in flight.
The gear would not retract. The A/C returned to CLE and landed
without incident. Maintenance inspected and replaced the nose gear
wow harness and proximity switch. Ops checks were good.
Incident
#17
FAA
Control Number: JJW2008F00000
Aircraft
Make: ROBSIN
Aircraft
Model: R44RavenII
Part
Name: Wire
Part
Condition: Chafed
Difficultly
Date: 03/25/2008
Part
Location: Cabin Air
Found
wiring to freeze switch had chafed through the capillary tube temp
sensor releasing all its refrigerant, causing switch to open and not
allow compressor to run. Switch not field replaceable, had to sent to
factory for repairs. Installed spiral wrap anti-chafe to wiring on
repaired part to prevent reoccurrence. Notified mfg product support
of problem and was told a service bulletin would be issued.
Incident
#18
FAA
Control Number: 2008FA0000685
Aircraft
Make: LEAR
Aircraft
Model: 45LEAR
Part
Name: Wire
Part
Condition: Chafed
Difficultly
Date: 09/26/2008
Part
Location: Fire Detection
APU
fire detection circuit breaker popped on RT cockpit circuit breaker
panel during power up of aircraft. Troubleshot system found wiring
chafed at fuselage station 614.210 aft equipment bay upper avionics
shelf support angle PN 4525708307. The angle does not have any
protection to prevent chafing of wiring from the factory and it
appears that clearance is not great enough to keep the wiring from
chafing. Have notified mfg tech support.
Incident
#19
FAA
Control Number: M7KA0628084134
Aircraft
Make: UROCOP
Aircraft
Model: EC130B4
Part
Name: Wire Harness
Part
Condition: Damaged
Difficultly
Date: 09/01/2008
Part
Location: Potentiometer
Failure
code at shutdown indicated fault with the collective potentiometer. A
new potentiometer was installed and no further defect reported. It
was recently discovered that the routing of air conditioning system
wiring in contact with the unshielded electrical harness for the
potentiometer was causing spurious signals in the control data which
were interpreted as a pontentiometer failure. Dozens of these
pontentiometers were replaced. Rerouting the air conditioning wiring
has almost entirely eliminated the need to replace these
potentiometers.
Incident
#20
FAA
Control Number: MWE2008F00032
Aircraft
Make: Douglas
Aircraft
Model: DC981
Part
Name: Wire
Part
Condition: Broken
Difficultly
Date: 08/19/2008
Part
Location: Emergency Light
Emergency
floor level lights inoperative from row 9 to 20. Repaired broken wire
in center section of light track.
Incident
#21
FAA
Control Number: 2008FA0000561
Aircraft
Make: Piper
Aircraft
Model: PA44180
Part
Name: Wire
Part
Condition: Broken
Difficultly
Date: 05/13/2008
Part
Location: Alternator
Internal
failure due to broken wires internally, heavy sparking inside engine
compartment.