N841AE

Part: ACM — FAILED (LEFT) · airframe 30,561 hrs · 29,870 cycles

UPON SHUTDOWN OBSERVED SMOKE AND SMELLED SULFUR FROM F/O SIDE APU WAS RUNNING AND #2 PAC WAS DEFERRED THERE WAS A NOSE ASSOCIATED AFTER APU SHUTDOWN SMELL WAS IN CABIN TOO "TRANSFERRED TO NRWC 841-DFW-02673"-C/A- REMOVED AND REPLACED #1 ACM (LH) IAW ENVOY EO#EM-2100-048 OPS CHECK GOOD NO DEFECTS NOTED. REMOVED AND REPLACED #1 PACK RAM AIR VALVE ACTUATOR IAW AMM 21-25-01. OPS CHECK GOOD. PERFORMED OPERATIONAL TEST OF LH ACM IAW EMB 140 AMM 21-51-00 OPS CHECK GOOD. REMOVED AND REPLACED RH ACM IAW EMB 140 AMM 21-50-03 AND ENVOY EO#EM-2100-048 OPS CHECK GOOD NO DEFECTS NOTED. PERFORMED ETN-EM-72-034 FOR ENG ODOR EVENT TROUBLESHOOTING SUPPLEMENT. NO SMOKE OR SULFUR ODOR NOTICED WHILE PERFORMING ENG ODOR EVENT. LINEAR ACTUATOR P/N SYLC51836-1 S/N 598; AIR CYCLE MACHINE RH P/N 815240-3 S/N 200209068

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,398 hrs · 29,679 cycles

CENTER AISLE MIDDLE EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LIGHT BULB IAW AMM 33-50-08 OPC GOOD. SEE NRWC 841-DFW-02609

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,398 hrs · 29,679 cycles

RIGHT HAND WING TO FUSELAGE FWD EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED RIGHT HAND WING TO FUSELAGE FWD EMERGENCY LIGHT ASSY IAW EMB AMM 33-50-10. OPC FAILED. REMOVED AND REPLACED BATTERY POWER SUPPLY IAW AMM 33-50-04. OPC GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,263 hrs · 29,559 cycles

RT EXTERIOR EMERGENCY LIGHT FWD INOPERATIVE. REMOVED AND REPLACED LAMP IAW AMM 33-50-10 OPS CHECED FAILED IAW ITEM 2 THIS NRWC

Part: POTENTIOMETER — FAILED (NLG STEERING) · airframe 29,214 hrs · 28,534 cycles

STEERING INOP AND CLUNKING NOISE WHEN TURNING FULL DEFLECTION TO THE RIGHT-C/A-PERFORMED FIM TASK 32-50-00 REMOVED AND REPLACED FEEDBACK POTENTIOMETER IAW AMM 32-50-07. OPC CHK GOOD NO MSGS AND NOISE NOTED AT THIS TIME. A/C OK FOR SERVICE.

Part: LANDING GEAR — LACK OF LUBE (NOSE) · airframe 29,214 hrs · 28,534 cycles

WITH TILLER DEPRESSED FULLY AND CLOSE TO FULL RIGHT DEFLECTION STEERING DISENGAGES (STEERING INOP) ALSO FEEL CLUNKING NOISE FROM NOSE GEAR SAME TIME, TILLER REMAINED FULLY DEPRESSED ENTIRE TIME. LUBRICATED NLG IAW AMM 32-34-00. PERFORMED OPS CHECK OF NOSE WHEEL STEERING SYSTEM IAW AMM 32-50-00. OPC GOOD. NO FURTHER DEFECTS OR NOISES NOTICED AT THIS TIME A/C OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,765 hrs · 28,079 cycles

MAIN DOOR OVERHEAD EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED MAIN DOOR OVERHEAD EMERGENCY LIGHT LAMP IAW AMM TASK 33-50-06-000-801-A AND 33-50-06-400-801-A. OPC GOOD, NO DEFECTS NOTED. END.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 27,910 hrs · 27,291 cycles

FA REPORTS MAIN CABIN DOOR IS HARD TO OPEN. CLEANED AND LUBRICATED MAIN DOOR FRAME ROLLER IAW ETN-EM-52-061.

Part: WIRE — BROKEN (CABIN) · airframe 27,713 hrs · 27,118 cycles

EMERGENCY FLOOR STRIP LIGHTING IN FRONT OF LAV HAS BROKEN WIRE. REMOVED AND REPLACED EMERGENCY FLOOR STRIP LIGHTING IN FRONT OF LAV IAW AMM 33-50-08. OPS CHECK GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 27,365 hrs · 26,825 cycles

RIGHT OVERWING EXTERNAL EMERGENCY LIGHT FAILED TO ILLUMINATE. FOUND THE BULB TO BE SHATTERED. INSTALLED A NEW BULB AND OPS CHECKED GOOD IAW AMM 33-50-10.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,171 hrs · 26,641 cycles

LEFT OVERWING EMERGENCY LIGHT WORKS INTERMITTENTLY. FOUND EMERGENCY LIGHT INVERTER TO BE INOPERATIVE. REMOVED AND REPLACED THE INVERTER IAW AMM 33-50-11. OPS CHECKED IAW AMM 33-50-00, OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 27,171 hrs · 26,641 cycles

FLOOR EMERGENCY LIGHTS HAD A BARE WIRE SHOWING, AND A BROKEN WIRE AT RESISTOR. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-50-00, OPS CHECKED GOOD.

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 27,171 hrs · 26,641 cycles

CRACKED SHEAR TIE AT FRAME 24, BETWEEN STRINGERS 15R AND 16R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, AND 51-20-03, AND SRM 51-40-02.

Part: SPLICE — MISSING (EMERGENCY LIGHT) · airframe 27,171 hrs · 26,641 cycles

FLOOR EMERGENCY LIGHT WIRE, MISSING REMOVEABLE SPLICE AT FRAME 49, REPAIRED THE WIRE IAW SWPM 20-21-00.

Part: WIRE — CUT (EMERGENCY LIGHT) · airframe 27,171 hrs · 26,641 cycles

FOUND EMERGENCY LIGHT WIRES CUT AT FLOOR PANEL 251BF. REPAIRED THE WIRES IAW SWPM 20-21-00.

Part: STRUCTURE — CORRODED (FRAME 68) · corrosion level 2 · airframe 27,171 hrs · 26,641 cycles

CARGO DOOR LATERAL L-SHAPE HAS CORROSION ON FRAME 68 BETWEEN STRINGERS 15 AND 16L BLENDED THE CORROSION IAW SRM 51-10-03 AND 51-10-05 AND DETERMINED TO BE OUT OF LIMITS. REMOVED DAMAGED SEGMENT IAW SRM 53-31-04. PERFORMED HFEC INSPECTION ALONG AREAS OF DAMAGE REMOVAL IAW NDTM 51-00-00-916-801-A00, NO DEFECTS NOTED. LOCATED, DRILLED, AND ALODINED NEW SEGMENT IAW SRM 51-20-03, AND CPM 51-21-04. INSTALLED THE NEW SEGMENT IAW SRM 53-31-04, FIG 212.

Part: TEE FITTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 27,171 hrs · 26,641 cycles

CORROSION ARE CARGO DOOR CUT OUT ON TEE FITTING AT FRAME 65 AND STRINGER 16L. REMOVED AND REPLACED THE TEE FITTING IAW SRM 51-40-02 AND CPM 51-21-04.

Part: FRAME — CRACKED (FRM 23) · airframe 27,171 hrs · 26,641 cycles

CRACK IN FRAME 23. REMOVED THE DAMAGED FRAME BETWEEN STRINGERS 15R TO 17 R IAW SRM 51-40-02.

Part: HINGE FITTING — DAMAGED (RUDDER) · airframe 27,171 hrs · 26,641 cycles

DAMAGED LOWER RUDDER HINGE FITTING. REMOVED AND REPLACED THE HINGE FITTING IAW SRM 51-40-02, AMM 20-10-01, SRM 51-20-03, CPM 51-21-04. CPM 51-21-05, AND 51-21-06

Part: FLOOR SUPPORT — CORRODED (FRAMES 9-12) · corrosion level 2 · airframe 27,171 hrs · 26,641 cycles

CORROSION ON THE FLOOR SUPPORT BETWEEN FRAMES 9 AND 12. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: HINGE FITTING — DAMAGED (VERTICAL STAB) · airframe 27,171 hrs · 26,641 cycles

DAMAGED UPPER RUDDER 1 HINGE FITTING ON VERTICAL STAB. REMOVED AND REPLACED THE DAMAGED HINGE IAW SRM 51-40-02, AMM 20-10-01. SRM 51-20-03, CPM 51-21-04. CPM 51-21-05 AND 51-21-06.

Part: FLOOR SUPPORT — CORRODED (FRAME 44) · corrosion level 2 · airframe 27,171 hrs · 26,641 cycles

CORRODED LT OMEGA BEAM FRAME 44. REMOVED CORROSION IAW SRM 51-10-03 AND 53-23-10. FOUND TO BE OUT OF LIMITS. REMOVED IAW SRM 53-00-10, FIG 202. PERFORMED HFEC INSP OF CUT OUT AREA IAW NDTM 51-00-00-916-801-A00, NO DEFECTS NOTED. FABRICATED A REPAIR. LOCATED, DRILLED, ALODINED, AND PRIMED THE REPAIR IAW SRM 53-10-10, CPM 51-21-04, AND 51-21-05 . INSTALLED THE REPAIR IAW SRM 51-40-02, AND 53-00-10.

Part: ANGLE — CRACKED (FRAMES 47-48) · airframe 27,171 hrs · 26,641 cycles

CRACK IN THE RT OMEGA BEAM, INBD SUPPORT BETWEEN FRAMES 47 AND 48. FABRICATED A REPAIR IAW SRM 53-23-02. .INSTALLED IAW SRM 53-23-02, 51-40-02, CPM 51-21-05, 51-21-06,AND 51-61-00.

Part: TEE FITTING — CORRODED (FRAME 68) · corrosion level 2 · airframe 27,171 hrs · 26,641 cycles

CORROSION ON THE CARGO DOOR CUT OUT TEE FITTING, LOCATED AT FRAME 68, STRINGER 16L. REMOVED AND REPLACED THE TEE FITTING IAW SRM 51-10-03, 51-40-20, CPM 51-21-04, SRM 51-40-02, AND CPM 51-21-06.

Part: FLOOR SUPPORT — CORRODED (FRAMES 52-59) · corrosion level 2 · airframe 27,171 hrs · 26,641 cycles

CORROSION ON THE LT OMEGA BEAM, CROSS MEMBER AT FRAME 59. REMOVED AND REPLACED THE OMEGA BEAM FROM FRAMES 52 TO 59 IAW SRM 51-40-02 AND CPM51-21-04.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · corrosion level 2 · airframe 27,171 hrs · 26,641 cycles

CORROSION ON THE CENTER OMEGA BEAM AT FRAME 20. BLENDED THE CORROSION AND DETERMINED TO BE OUT OF LIMITS IAW SRM 53-21-10. REMOVED CENTER OMEGA BEAM. LOCATED , DRILLED AND ALODINED NEW OMEGA BEAM IAW SRM 51-20-03, AND CPM 51-21-04, INSTALLED IAW SRM 51-40-02, AND CPM 51-21-06.

Part: BEAM — CORRODED (FRAMES 66-67) · corrosion level 2 · airframe 27,171 hrs · 26,641 cycles

CARGO DOOR LOWER BEAM HAS CORROSION. BLENDED IAW SRM 51-10-03, AND 51-10-05. FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED, ALODINED, AND INSTALLED A NEW BEAM IAW SRM 51-20-03, 51-20-04, AND CPM 51-21-04.

Part: GUIDE — CORRODED (FRAME 65) · corrosion level 2 · airframe 27,171 hrs · 26,641 cycles

CARGO DOOR LATERAL L SHAPE HAS CORROSION ON FRAME 65 BETWEEN STRINGERS 15L AND 16L. FOUND OUT OF LIMITS IAW SRM 51-10-03, AND 51-10-05. REMOVED LATERAL L SHAPE IAW SRM 53-31-04, PERFORMED HFEC INSPECTION ALONG AREAS OF DAMAGE REMOVAL IAW NDTM 51-00-00-916-801-A00. NO DEFECTS NOTED. LOCATED AND DRILLED A NEW SEGMENT OF LATERAL L SHAPE AND ALODINED IAW SRM 51-20-03, AND CPM 51-21-04. INSTALLED AND RESTORED SURFACE PROTECTION IAW SRM 53-31-04, CPM 51-21-04, 51-21-05, AND 51-21-06.

Part: STRUCTURE — CORRODED (FRAME 38) · corrosion level 2 · airframe 27,171 hrs · 26,641 cycles

CORROSION ON THE LT OMEGA BEAM AT CROSS MEMBER, FRAME 38. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-23-10, AND 51-10-03. CUT OUT DAMAGE IAW SRM 53-00-10, PERFORMED HFEC INSP OF CUT OUT AREA IAW NDTM 51-00-00-916-801-A00, NO DEFECTS NOTED. FABRICATED A REPAIR, LOCATED, DRILLED, ALODINE, AND PRIMED THE REPAIR IAW SRM 53-00-10, 51-20-03, CPM 51-21-04, AND 51-21-05. INSTALLED THE REPAIR IAW SRM 53-00-10, 51-40-02, AND CPM 51-21-06.

Part: SHEAR TIE — CRACKED (FRAME 65) · airframe 27,171 hrs · 26,641 cycles

CRACKED SHEAR TIE AT FRAME 65 BETWEEN STRINGERS 7L AND 9L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 53-31-04, AND 51-30-01.

Part: SHEAR TIE — CRACKED (FRAME 73) · airframe 27,171 hrs · 26,641 cycles

CRACKED SHEAR TIE AT FRAME 73 ABOVE STRINGER 9R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, 51-20-03, AND CPM 51-21-04.

Part: FRAME — CRACKED (FRM 23) · airframe 27,171 hrs · 26,641 cycles

CRACKED FRAME 23, STRINGERS 15R-17R. REMOVED DAMAGED PORTION OF THE FRAME IAW SRM 51-40-02, LOCATED, DRILLED, AND ALODINED A REPAIR IAW SRM 51-20-03, AND CPM 51-21-04. INSTALLED THE REPAIR IAW SRM 51-40-02, AND 53-00-04.

Part: STRINGER — CRACKED (FRAME 20) · airframe 27,171 hrs · 26,641 cycles

CRACKED STRINGER 3L AT FRAME 20. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-02, SRM 51-20-03, 51-40-02, AND CPM 51-21-04.

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 27,171 hrs · 26,641 cycles

CRACKED SHEAR TIE AT FRAME 24, BETWEEN STRINGERS 16R AND 17R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, AND DRAWING 145-26855-003.

Part: SHEAR TIE — CRACKED (FRAME 65) · airframe 27,171 hrs · 26,641 cycles

CRACKED SHEAR TIE AT FRAME 65, BETWEEN STRINGERS 18L AND 19L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, 51-20-03, CPM 51-21-04. AND CPM 51-21-06.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 27,128 hrs · 26,602 cycles

BLD 2 LEAK AT 6000' WHILE CLIMBING OUT. IAW NRWC 841DFW01674 & 841DFW01671 FOR ACTION TAKEN & PERFORMED AIR BLEED SYS OPERATIONAL TEST IAW MM 36-00-0. OPERATIONS CHECKED GOOD. R & R NR 2 BLEED SYS JOINTS 4, 14 & 22 O RINGS IAW AMM 36-11-10. R & R RT BLEED DUCT LINE JOINT O RINGS IAW AMM 36-11-10 & ETN-EM 36-063. SEE NRWC 841-DFW-01672FFOR LEAK CHECK.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 27,030 hrs · 26,531 cycles

AT FL360, WE RECEIVED IAS MSG, NR 2 AIRSPEED INDICATION WAS LESS THAN NR 1 & ISIS. DURING DESCENT NR 2 ASI DECREASED AT A RATE EQUAL TO OUR ALTITUDE DECREASE. AT FL310, NR 2 ASI RETURNED TO NORMAL SUDDENLY. DURING AIRSPEED DISCREPANCY WE HAD SPS ADVANCED CAUTION MSG. COMPLIED WITH PITOT STATIC LEAK CHECK IAW WC 34-700-02, LEAK CHECK GOOD. COMPLIED WITH DVI OF PITOT PROBES IAW WC 34-200-02 NO DEFECTS NOTED. INSPECTED PITOT DRAIN LINES IAW AMM 34-13-00 NO DEFECTS NOTED. ISIS FNC GOOD IAW WC 34-700-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,827 hrs · 26,352 cycles

ROW 13 - 15 FLOOR EMERGENCY LIGHT STRIP INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: SWITCH — FAULTY (BLEED AIR SYS) · airframe 26,404 hrs · 25,983 cycles

SHORTLY AFTER TAKEOFF, CLIMBED THROUGH ICING LAYER & ANTI-ICE SYS CAME ON. BLEED 2 LOW TEMP ON EICAS WITH POINTER BELOW GREEN ARC. AFTER 10K, PERFORMED ANTI-ICE PNEUMATIC TEST FOR 1 MINUTE & AGAIN GOT MSG. ON APPROACH BACK TO ORD, FOLLOWED AOM PROCEDURE & TURNED OFF BLEED & PACK 2, OPENED X BLEED. POINTER ON NR 2 ECS PAGE RETURNED TO GREEN ARC. ON GLIDE SLOPE & POWER REDUCTION, RECEIVED ANTI-ICE INOPERATIVE WARNING, BLEED 1/2 LOW TEMP, WING ANTI-ICE FAIL, STAB ANTI-ICE FAIL. R & R NR 2 BLEED PB SWITCH IAW AMM 20-13-04 & OPERATIONS CHECK IAW AMM 36-00-00. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,378 hrs · 25,953 cycles

PART OF THE EMERGENCY LIGHTING CAME ON AFTER FLT CREW LT FROM PREVIOUS FLT WHEN THE EMERGENCY LT SWITCH WAS SELECTED TO THE ON POSITION. THE FIRST SET OF LIGHTS DIMMED IMMEDIATELY THE REMAINING LIGHTS FUNCTIONED NORMALLY. SYS CHARGED ON ACFT IAW CMM 25-60-03, OPERATIONAL CHECK CO, CHECKED SERVICEABLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,297 hrs · 25,875 cycles

ROW 12 BC OVERHEAD INTERIOR EMERGENCY LIGHT INOPERATIVE. R & R ROW 12 BC OVERHEAD EMERGENCY LIGHT BULB IAW AMM 33-50-07-000-801-A & 33-50-07-400-801-A. OPERATIONS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 26,082 hrs · 25,675 cycles

DURING PS 1 CHECK FOUND MAIN DOOR ENTRANCE EMERGENCY FLASHLIGHT HOLDER CRADLE BRACKET BROKEN. R & R MAIN DOOR ENTRANCE EMERGENCY FLASHLIGHT ASSEMBLY IAW MM 33-50-16, OPERATIONS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,234 hrs · 24,983 cycles

GALLEY OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECKED GOOD.

Part: ENGINE — BIRD INGESTION (LEFT & RIGHT) · airframe 24,395 hrs · 24,272 cycles

THE PILOT REPORTED HE WAS UNAWARE OF A BIRDSTIKE THAT MUST HAVE OCCURRED. HE SAID THAT HE USED THE CAPTAIN’S FLASHLIGHT AND MISSED IT ON THE POST INSPECTION. WHILE TROUBLESHOOTING, SMOKE IN THE COCKPIT FOUND NR 2 ENGINE SMELLING LIKE A BIRD HAD GONE THROUGH IT. SUSPECT SMELL IS RESIDUAL FROM BIRD STRIKE ON 05/31/13. PERFORMED INSPECTION OF NR 2 ENGINE INLET AND FAN BLADES IAW R & R/ MM TASK72-00-00-200-801. FOUND NO EVIDENCE OF BIRD INGESTION. PREFORMED BORESCOPE OF NR 2 ENGINE COMPRESSOR IAW R & R/ MM TASK 72-30-00-200-801 AND ETN EM-72-026. FOUND NO EVIDENCE OF BIRD INGESTION. ALSO, FOUND NO EVIDENCE OF COKING ON CVG'S OR OIL LEAKAGE. PERFORMED ETN-EM-72-034. SMALL ODOR NOTED. UPON FURTHER INSP FOUND SMELL OF BIRD COMING FROM FRONT OF LT AND RT ENGINES. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,364 hrs · 24,240 cycles

DURING B INSP, FOUND THE LT SIDE CENTER FUSELAGE FAIRING EXTERNAL EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LT SIDE CENTER FUSELAGE FAIRING EXTERNAL EMERGENCY LIGHT LAMP IN REF WITH AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 23,802 hrs · 23,732 cycles

DURING B INSPECTION FOUND THE CEILING EMERGENCY LIGHT AT ROW 1 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RECONNECTED CONNECTOR ON FORWARD PASSENGER CABIN CEILING EMERGENCY LIGHT IAW EMB 140 AMM 25-22-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 23,665 hrs · 23,618 cycles

ON FLIGHT 2721 THE CREW REPORTED THE FORWARD CABIN FLASHLIGHT CHARGES INTERMITTENTLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN FLASHLIGHT AND CHARGER ASSEMBLY IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — UNSERVICEABLE (CABIN) · airframe 23,122 hrs · 23,210 cycles

DURING MAINTENANCE CHECK FOUND THE NR 3 EMERGENCY POWER SUPPLY BATTERY NEEDED TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY POWER SUPPLY BATTERY IAW WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,854 hrs · 23,001 cycles

DURING B INSPECTION FOUND THE AISLE EMERGENCY LIGHT AT ROW 3 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT AT ROW 3 IAW EMB AMM TASK: 33-50-08-000-801-A, AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 23,063 hrs · 23,164 cycles

DURING B INSPECTION FOUND THE RIGHT OUTBOARD OMEGA BEAM SUPPORT CRACKED BETWEEN FRAMES 47 AND 48. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OUTBOARD OMEGA BEAM SUPPORT. LOCATED DRILLED AND INSTALLED NEW OMEGA BEAM SUPPORT REF EMB 145 SRM 53-23-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,062 hrs · 23,163 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHTING AISLE LAST ON E INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAST AISLE EMERGENCY LIGHT STRIP REF EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 22,863 hrs · 23,009 cycles

DURING B INSPECTION FOUND CORROSION ON FORE AND AFT ON CENTER FLOOR BEAM FOR LAV FLOOR BETWEEN FR 59 AND FR61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CENTER OMEGA BEAM DIGITAL GUSSET REF SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,140 hrs · 22,329 cycles

DURING B INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,048 hrs · 22,246 cycles

DURING B INSPECTION, FOUND THE RIGHT WING AFT EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT WING AFT EMERGENCY LIGHT BULB IAW AMM 33-50-07. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 21,764 hrs · 22,002 cycles

DURING B-INSPECTION FOUND THE FORWARD CABIN EMERGENCY FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT AND CRADLE ASSEMBLY IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PBE — UNSERVICEABLE (CABIN) · airframe 21,463 hrs · 21,719 cycles

DURING MAINTENANCE INSPECTION FOUND THE GALLEY PROTECTIVE BREATHING EQUIPMENT TO BE PUNCTURED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PROTECTIVE BREATHING EQUIPMENT IAW EO EM- 2500-200R1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,279 hrs · 21,561 cycles

DURING B-INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT BULB INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,162 hrs · 21,449 cycles

ON FLIGHT 4545 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT BULB IAW CMM 25-60-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (COCKPIT) · airframe 20,812 hrs · 21,141 cycles

ON FLIGHT 4457 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED CAPTAIN’S FLASHLIGHT HOLDER IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UPLOCK — DEFECTIVE (NLG) · airframe 19,738 hrs · 20,186 cycles

SEVERAL LOUD THUMPING SOUNDS HEARD COMING FROM NOSE GEAR DURING CLIMB. NO NOISE HEARD DURING DESCENT. REMOVED AND REPLACED NLG UPLOCK BOX REF TASK NR 32-33-07-400-801-A. STEP 3 (J) AND OPS & FNC- GOOD PER EMB 140 AMM 32-33-07.

Part: ADC — FAILED (NR 1) · airframe 19,614 hrs · 20,078 cycles

ON FLIGHT 4250 THE CREW REPORTED THAT DURING CRUISE THEY HAD A LOSS OF AIR SPEED. THE INSTRUMENTS SHOWED ZERO AND ALTIMETER 2000 FEET IN FLIGHT. THE CAPTAIN DECLARED AN EMERGENCY. PRIOR TO LANDING THE INDICATIONS RETURNED TO NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 AIR DATA COMPUTER IAW AMM 34-15-01. THE OPERATIONAL CHECK WAS GOOD. THIS AIRCRAFT IS RVSM ELIGIBLE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 19,187 hrs · 19,692 cycles

ON FLIGHT 3038 THE FLIGHT ATTENDANT COMPLAINED OF A BURNING RUBBER/SMOKE ODOR IN THE CABIN. IT WAS ALSO NOTICED IN THE COCKPIT AND BY A PASSENGER. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED INSPECTION OF BOTH LEFT AND RIGHT ENGINES NR 4 CARBON SEAL NO LEAKS FOUND IAW RR MM 72-30-00-200-801. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 19,128 hrs · 19,619 cycles

ON FLIGHT 3080 DURING CLIMBOUT THE CREW REPORTED A STRONG OIL SMOKE FROM PAC IN THE COCKPIT. THE CREW ELECTED TO RETURN TO LAX. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH ETN EM-72-034R4 AND NO ODOR OR SMOKE WAS DETECTED. NO PARTS REMOVED OR REPLACED. A FUNCTIONAL CHECK FLIGHT WAS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — INOPERATIVE (CABIN) · airframe 17,495 hrs · 18,154 cycles

ON FLIGHT 3039 DURING CRUISE THE CREW REPORTED A VERY STRONG ODOR LIKE AN ELECTRICAL BURNING ODOR THAT COULD BE SMELLED THROUGHOUT THE CABIN AND COCKPIT. NO SMOKE OR FLAMES WERE VISIBLE. NO EICAS MESSAGES WERE PRESENTED. THE ODOR LASTED UNTIL AFTER LANDING. THE CAPTAIN ELECTED TO DIVERT TO BFL AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. UPON ENTERING AIRCRAFT, NOTICED NO ODOR. POWERED UP BATTERIES, NO ODORS NOTED. STARTED APU & PACKS 1 AND 2. NO ODORS NOTED. POWERED ALL AVIONICS, NO ODORS NOTED. POWERED WINDSHIELD HEAT 1 AND 2 AND ALL ANTI-ICE, NO ODORS NOTED. POWERED RECIRCULATION FANS, FOUND CABIN RECIRCULATION FAN INOPERATIVE. PERFORMED ELECTRONIC COMPARTMENT VENTILATION SYSTEM OPERATIONAL CHECK IAW EMB140 AMM 21-26-00. THE OPERATIONAL CHECK WAS GOOD. REMOVED AND REPLACED THE CABIN RECIRCULATION FAN IAW EMB 140 AMM 21-24-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 17,287 hrs · 17,881 cycles

DURING MAINTENANCE BASE VISIT FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERATIVE DURING INSPECTION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED BROKEN WIRE W716-0008-20 IAW WM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 12,899 hrs · 12,323 cycles

ON FLIGHT 317, CREW REPORTED WITH APU BLEED OPEN AIR ON PACK 1 AND 2 ODOR OF OIL IN COCKPIT. AIRCRAFT REMOVED FROM SERVICE. DEFERRED PER MEL 36-6 AUTH NR 041010DM-C, PERFORMED AIR BLEED THROUGH APU IAW EMB 140 AMM 36-00-00. COULD NOT DUPLICATE SMELL MEL RESTORED, AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,347 hrs · 10,631 cycles

EMERGENCY FLOOR STRIP LIGHTS AT ROW 3 THROUGH ROW 6 INOPERATIVE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,707 hrs · 8,824 cycles

CARGO DOOR CENTER FRAME SILL FOUND CORRODED. CLEANED, TREATED, REMOVED AND REPLACED SILL IAW EMB SRM 51-21-01, 51-2103, 51-40-04 AND 51-40-06. AIRCRAFT RETURN TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

DISC - EMERGENCY LIGHT AT OVERHEAD SERVICE DOOR INOPERATIVE. FOUND WIRE SPLICE BROKEN. REPAIRED WIRING. OPERATIONAL CHECKED GOOD. AC RETURNED TO SERVICE. (K)