N833AE

Part: TUBE — INOPERATIVE (ANTI ICE) · airframe 34,970 hrs · 30,713 cycles

INFLIGHT RAN ICE DECTIONS TEST AND GOT A WING ANTI ICE FAIL CAUTION MESSAGE. RAN THE TEST TWICE AND CAUTION MESSAGE CAME ON BOTH TIMES. "TRANSFERRED TO NRWC 833-ORD-03017"-C/A-C/W WORK SCOPE, INSPECTED THE PACK DUCTING FOR LEAKS, TROUBLE SHOT IAW EMB 140 FIM 30-11-00-810-801A AND FIM 30-11-00-810-803A FOUND LEAK AT #1 PACK Y DUCT AND #2 PACK TO HAVE DUCT LOOSE FROM HEAT EXCHANGER TO CONDENSOR /MIXER REPAIRED AS REQUIRED. OPS AND LEAK CHECK GOOD IAW EMB 140 AMM 30-00-00. C/W WORK SCOPE, INSPECTED THE PACK DUCTING FOR LEAKS, TROUBLE SHOT IAW EMB 140 FIM 30-11-00-810-801A AND FIM 30-11-00-810-803A FOUND LEAK AT #1 PACK Y DUCT AND #2 PACK TO HAVE DUCT LOOSE FROM HEAT EXCHANGER TO CONDENSOR /MIXER REPAIRED AS REQUIRED. OPS AND LEAK CHECK GOODIAW EMB 140 AMM 30-00-00. REMOVED AND REPLACED #1 PACK Y DUCT IAW EMB-140 MM 21-60-01 ...OPS CHECK/ LEAK CHECK OF #1 PACK GOOD. PERFORMED OPS AND LEAK CHECK OF WING A/I IAW EMB 140 AMM 30-00-00 OPS AND LEAK CHECK GOOD. REMOVED AND REPLACED PACK 2 DUCT FROM HEAT EXCHANGER TO CONDENSER/MIXER IAW AMM 31-11-09. OPS AND LEAK CHECK GOOD IAW 30-00-00

Part: CONNECTOR — DIRTY (WX RADAR) · airframe 34,341 hrs · 30,113 cycles

RADAR FAILED. REMOVED AND CLEANED THE CONNECTOR PLUG. RESET UNIT. OPS CHECKED GOOD IAW 34-42-00.

Part: ANTENNA — INOPERATIVE (WX RADAR SYS) · airframe 34,341 hrs · 30,114 cycles

RADAR BECAME INOPERATIVE. REMOVED AND REPLACED THE RECIEVER TRANSMITTER ANTENNA ASSY IAW 34-42-01, OPS TESTED GOOD IAW 34-42-00. NO DEFECTS FOUND

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 34,315 hrs · 30,088 cycles

MAIN CABIN DOOR HARD TO OPPERATE. LUBRICATED THE DOOR IAW ETN-EM-52-061. OPS CHECKED GOOD. NO DEFECT NOTED.

Part: SWITCH — FAILED (MLG) · airframe 33,885 hrs · 29,716 cycles

DURING CLIMB, RECEIVED A LG AIR/GND FAIL MESSAGE. COMPLIED WITH QRH, DECLARED AN EMERGENCY AND DIVERTED. TROUBLESHOT IAW FIM 32-63-00-810-806-A SUBTASK 816-003-A. FOUND SIGNS OF CORROSION AND ARCING ON NLG WOW SWITCH CONNECTOR.

Part: DOOR — LACK OF LUBE (PAX) · airframe 33,575 hrs · 29,418 cycles

FA ADVISED THAT THE MAIN CABIN DOOR WAS HARD TO OPEN .CYCLED AND LUBRICATED MAIN CABIN DOOR IAW AMM 52-10-01. NO DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,481 hrs · 29,299 cycles

NUMEROUS FORWARD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY AND CHARGER IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: SKIN — DENTED (RUDDER) · airframe 33,415 hrs · 29,215 cycles

RUDDER LOWER RTH SKIN DENTED BETWEEN RIBS ZV 920 AND ZV 1164. THE RUDDER SKIN WAS REPAIRED IAW SRM 55-40-01, ITEM 2.

Part: LIGHT — DAMAGED (CABIN) · airframe 33,364 hrs · 29,155 cycles

PROXIMITY LIGHT FOUND DAMAGED. R & R THE LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,292 hrs · 29,061 cycles

DURING PS-2 INSPECTION FOUND LT FAIRING FWD EMERGENCY LIGHT INOP. R&R BATTERY POWER SUPPLY IAW AMM 33-50-04. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. LT LIGHT EMERGENCY P/N 30-2510-3

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 33,202 hrs · 28,954 cycles

AT CRUISE ALT SPS ADVANCE AND FLAP LOW SPEED MSG. REF LOG PAGE 4000496 ITEM 3 FOR ACTION TAKEN. SPS SYSTEM RESET PER AMM 27-36-00. NO MESSAGE NOTED, OPS GOOD

Part: PRESSURE SWITCH — INOPERATIVE (RUDDER) · airframe 32,896 hrs · 28,674 cycles

RUDDER SYSTEM 1 AND 2 EICAS MESSAGE. TROUBLESHOT IAW FIM 27-22-00 AND ENVOY ETN -EM -27 -079. REMOVED AND REPLACED NR 1 & 2 RUDDER PRESSURE SWITCH IAW 27-23-04. OPS CHECK GOOD IAW MM 27-23-00 . LEAK CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,825 hrs · 28,613 cycles

RIGHT EXTERIOR EMERGENCY LIGHT FORWARD OF WING INOPERATIVE. REPLACED THE LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 32,132 hrs · 27,810 cycles

HYD LO QTY ADVISORY NR 1 HYD SYS IS IN AMBER, NO RECOVERY & CONTINUED TO DROP. NO INDICATION OF HYD LEAK ON POST FLIGHT. R & R NR 1 EDP IAW AMM CH 29-10-03. OPERATIONS & LEAK CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,912 hrs · 27,531 cycles

SERVICE DOOR CEILING EMER LIGHT INOPERATIVE. REMOVED & INSTALLED SERVICEABLE SERVICE DOOR CEILING EMER LIGHT LAMP IAW AMM 33-50-09. OPERATIONAL CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,828 hrs · 27,452 cycles

1ST CEILING LIGHT IN CABIN INOPERATIVE. R & R NR 1 BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: FIRE LOOP — CHAFED (APU) · airframe 31,777 hrs · 27,398 cycles

MOMENTARY APU FIRE INDICATION. PERFORMED GVI AROUND APU, NO DEFECTS FOUND. DEFERRED APU, M PROCEDURES COMPLIED WITH IAW 49-1. FOUND APU FIRELOOP CHAFFING AGAINST HOT SPOT ON ENGINE. REMOVED AND REPLACED APU FIRELOOP IAW AMM 26-12-01. OPS CXK GOOD. MEL 49-01 IS RESTORED.

Part: SPOILER SYS — MALFUNCTIONED · airframe 31,758 hrs · 27,366 cycles

ON DECENT WHILE USING SPOILERS TO ASSIST THE DECENT, ONCE THE SPOILERS HANDLE WAS RETURNED TO STOWED POSITION, EICAS MSG SPOILER FAIL WITH SPOILERS INDICATION ON OPEN. FOLLOWED EPC EMERGENCY PROCEDURES. PERFORMED SPOILER & SPEED BRAKE SYS. OPERATIONS GOOD & FAULT SYS OPERATES AS REQUIRED IAW AMM 27-63-01.

Part: HYDRAULIC LINE — DAMAGED (HYDRAULIC SYS) · airframe 31,741 hrs · 27,354 cycles

RAMP PERSONNEL INDICATE SUSPICIOUS ODOR IN THE CARGO COMPARTMENT. TRANSFERRED TO NRWC 833-DFW-02181. PERFORMED PERMANENT REPAIR TO RUDDER PRESS LINE AT LAVATORY & CARGO BULKHEAD IAW AMM 20-10-03. SEE NRWC 833-DFW-02181 FOR MORE INFO. CONFIRMED DAMAGED RUDDER PRESS HYD LINE. PERFORMED PERM SWAGE REPAIR IAW AMM 20-10-03. OPERATIONS CHECK & LEAK CHECK FOUND OK.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 30,425 hrs · 26,072 cycles

NUMBER 1 & 2 PFD'S ARE DISPLAYING AN AMBER WX IN THE RADAR INFO AREA. BOTH WX RADARS ARE DEPICTING ERRONEOUS & INVALID WEATHER RETURNS. R & R WX RADAR ASSEMBLY IAW AMM 34-42-01. OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 30,262 hrs · 25,935 cycles

CAPTAINS FLASHLIGHT HOLDER BROKEN. R & R CAPTAINS FLASHLIGHT HOLDER ASSEMBLY IAW AMM 33-60-02. OPERATIONS CHECKED GOOD.

Part: TRANSMITTER — FAILED (FUEL QTY) · airframe 29,519 hrs · 25,307 cycles

RIGHT FUEL QTY INDICATION ON EICAS DECREASED TO 0 IN FLIGHT, FOLLOWED BY MFD TOTAL INDICATION LOSS ASSOCIATED MASTER CAUTION FUEL IMBALANCE. ON FINAL APPROACH ALL FUEL QTY INDICATIONS RETURNED TO NORMAL. R & R RT WING NR 5 FUEL TANK UNIT IAW AMM 28-41-02. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE · airframe 29,219 hrs · 25,042 cycles

EMERGENCY FLASHLIGHT CHARGER ASSEMBLY INOPERATIVE. R & R EMER FLASHLIGHT & CRADLE ASSEMBLY IAW AMM 33-50-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,878 hrs · 24,710 cycles

RIGHT UPPER FUSELAGE SKIN HAS 2 AREAS WITH RELEVANT CRACK INDICATIONS JUST AFT OF FRAME 75 & ABOVE STRINGER 2R. REPAIRED RT UPPER FUSELAGE SKIN JUST AFT OF FRAME 75 & ABOVE STRINGER 2R IAW ERS-EM-53MR-564.

Part: WIRE — BROKEN (CABIN) · airframe 28,878 hrs · 24,710 cycles

EMERGENCY LIGHT LENS NR 2 HAS BROKEN WIRES. R & R FLOOR EMER LIGHT STRIP NR 2 IAW AMM 33-50-12. SEE NRTC BOW 158177 FOR OPERATIONAL CHECK OF EMER FLOOR LIGHTS FOUND DURING OPEN UP.

Part: WIRE — BROKEN (CABIN) · airframe 28,878 hrs · 24,710 cycles

EMERGENCY LIGHT STRIP 3 HAS BROKEN WIRES. R & R FLOOR EMER LIGHT STRIP 3 IAW AMM 33-50-12. SEE NRWC BOW 158177 FOR FLOOR EMER LIGHTS OPERATIONAL CHECK. FOUND DURING OPEN UP.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,878 hrs · 24,710 cycles

FRAME 23 CRACKED BETWEEN STRINGER 15R & 16R. REPAIRED FRAME 23 BETWEEN STRINGER 15R & 16R IAW EM-53MR-1808.

Part: RELIEF VALVE — FAILED (PARKING BRAKE) · airframe 28,878 hrs · 24,710 cycles

EMERGENCY PARKING BRAKE SYS THERMAL RELIEF VLV FAILED FUNCTIONAL CHECK. REMOVED & RELOCATED EMER PARKING BRAKE SYS THERMAL RELIEF VLV WITH A SERVICEABLE UNIT IAW AMM 32-44-06. LEAK CHECKED GOOD.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,878 hrs · 24,710 cycles

RIGHT BEAM CRACKED AT INBD & OTBD SUPPORTS AT FRAME 47. R & R INBD OTBD SUPPORTS FOR RT OMEGA BEAM BETWEEN FRAME 46 - 50 IAW SRM 53-23-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,878 hrs · 24,710 cycles

LEFT BEAM CRACKED AT OTBD SUPPORT AT FRAME 47. R & R LT BEAM OTBD SUPPORT IAW SRM 53-23-02.

Part: FADEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 27,940 hrs · 23,841 cycles

ON FLIGHT 3350 CREW REPORTED E2 SHORT DISPATCH ADVISORY CAME ON WHILE ENG NR 1 SHUT DOWN. THE ACFT WAS REMOVED FROM SERVICE. RESET E 2 FADEC SYS, OPERATIONS CHECKED NORMAL MM 73-21-00. THE ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,772 hrs · 23,696 cycles

CEILING EMERGENCY LAMP AT ROW 11 INOPERATIVE. REMOVE AND REPLACED AISLE EMERGENCY LIGHT AT ROW 11 IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPS CHECK GOOD.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 27,735 hrs · 23,647 cycles

ENTRANCE EMERGENCY FLASHLIGHT MISSING. INSTALLED FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16.

Part: CRADLE — BROKEN (AFT CABIN) · airframe 27,637 hrs · 23,522 cycles

AFT CABIN FLASHLIGHT MOUNT IS BROKEN. REPLACED AFT CABIN FLASHLIGHT IAW AMM 33-50-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 24,384 hrs · 20,708 cycles

DURING MAINTENANCE INSPECTION, FOUND FRAME 23 HAS 3/4 INCH CRACK AT LOWER ATTACHMENT RIVET BETWEEN STRINGERS 15R AND 16R. AIRCRAFT REMOVED FROM SERVICE. COMPLETED REPAIR IAW EO EM-53MR-1808. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 24,377 hrs · 20,702 cycles

DURING B INSPECTION, FOUND THE EMERGENCY LIGHT WIRING BROKEN . AIRCRAFT REMOVED FROM SERVICE. REPLACED CONNECTOR AT SPLICE SP9115 IAW SWPM 20-21-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 24,375 hrs · 20,698 cycles

RT CABIN FRAME 23 HAS .7500" CRACK AT LOWER ATTACHMENT RIVET BETWEEN STRINGER 15R AND 16R. REPAIRED IAW EO EM-53MR-1808, PART A.

Part: UNKNOWN — ODOR (CABIN) · airframe 19,676 hrs · 16,216 cycles

ON FLIGHT 4220 THE CREW REPORTED A DISTINCT BURNING SMELL ON APPROACH THAT SEEMED TO EMANATE FROM THE PACKS AND WHEN THROTTLE LEVER WAS AT HIGHER THRUST SETTINGS. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ETN EM 72-034 R4 WITH CREW AND FOUND NO EVIDENCE OF SMELL NOTED AT THIS TIME. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SCAVENGE PUMP — INOPERATIVE (NR 2 ENGINE) · airframe 19,589 hrs · 16,148 cycles

ON FLIGHT 4238 DURING CRUISE THE CREW REPORTED THE ENGINE OIL QUANTITY FOR THE NR 2 ENGINE WENT TO 4 QUARTS. THE CAPTAIN ELECTED TO MAKE A PRECAUTIONARY LANDING AND DIVERTED TO IND. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OIL SCAVENGE PUMP IAW MM 79-21-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 19,516 hrs · 16,088 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE SKIN CRACKED AT FRAME 75 BETWEEN STRINGERS 1L AND 2L. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED CRACKED SKIN AT FRAME 75 IAW ENGINEERING ORDER EM-53-MR-1596. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE INDICATION (NLG DOOR) · airframe 15,866 hrs · 12,937 cycles

ON FLIGHT 4740 CREW REPORTED AFTER DEPARTURE NOSE LANDING GEAR DOOR NOT CLOSING. THE LANDING GEAR INDICATION WAS NORMAL WITH 3 GREEN AND NO WARNING MESSAGES. CREW PERFORMED A FLY BY AT JFK WHICH RETURNED UNREMARKABLE. CREW DECLARED AN EMERGENCY AND LANDED SAFELY AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED GEAR SWING IAW EMB AMM NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: CARBON SEAL — WORN (NR 1 ENGINE) · airframe 14,096 hrs · 11,585 cycles

ON FLIGHT 3900 - CREW REPORTED NUMBER 1 ENGINE OIL QUANTITY WENT FROM 11 TO 4 QTS IN LESS THAN 15 MINUTES. PERFORMED PRECAUTIONARY SHUTDOWN. OVERWEIGHT LANDING PERFORMED 43700 LBS TOUCHDOWN OF LESS THAN 100 FPM. AIRCRAFT LANDED UNEVENTFULLY. AIRCRAFT REMOVED FROM SERVICE. REMOVED NR 1 ANGLE GEARBOX BREATHER MAGNETIC CARBON SEAL IAW ROLLS ROYCE FIM TASK 72-00-00-810-815, REF ETN EM 79-007 R1. RESERVICED OIL WITH 14 PTS IAW AMM 79-11-01. NO DEFECTS NOTED. PASSED FCF AND COMPLETED TRIAD EVENT AIRCRAFT RETURNED TO SERVICE.

Part: ECU — MALFUNCTIONED (LANDING GEAR) · airframe 15,905 hrs · 12,969 cycles

ON FLIGHT 4533 CREW REPORTED NLG DOORS DID NOT RETRACT/CLOSE UPON GEAR RETRACTION. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED LANDING GEAR ELECTRONIC CONTROL UNIT IAW AMM 32-32-01. OPS CHECK GOOD, ACFT PASSED FCF. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,952 hrs · 10,758 cycles

LEFT EXTERNAL OVERWING EMERGENCY LIGHT INOP. ISSUED MEL 33-29 AUTH 100824D-C.

Part: PROXIMITY SENSOR — SHORTED (MLG) · airframe 10,754 hrs · 9,153 cycles

LANDING GEAR HANDLE WOULD NOT ALLOW LANDING GEAR TO RETRACT. RECEIVED LG AIR/GND FAIL MESSAGE AND RETURNED TO DFW. REMOVED AND REPLACED PROXIMITY SWITCH IAW EMB AMM 32-63-02 AFTER FINDING PIN A SHORTED. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND LEFT OUTBOARD SEAT TRACK NR 1 IS CORRODED. RAI`D SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED

DURING IMBV INSPECTION, FOUND RIGHT OUTBOARD SEAT TRACK NR 5 IS CORRODED. RAI`D SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: GUSSET — CORRODED (FLOOR SUPPORT)

DURING MBV INSPECTION, FOUND GUSSETT AT FRAME 24 ON TOP OF LEFT INBOARD OMEGA BEAM CORRODED. REPAIRED GUSSET IAW IC 2006-145/5449 BY CUTTING OUT DAMAGE AND SPLICING IN A NEW PIECE. AIRCRAFT WS RETURNED TO SERVICE (M)

Part: CAP — CORRODED (MLG BEARING)

DURING MBV INSPECTION, FOUND RIGHT MAIN LANDING GEAR AFT BEARING CAP CORRODED. INSTALLED NEW BEARING CAP IAW WORK CARD 57-700-84. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CAP — CORRODED (LT MLG BEARING)

DURING MBV INSPECTION, FOUND LEFT MAIN LANDING GEAR FORWARD BEARING CAP CORRODED. INSTALLED NEW BEARING CAP IAW WORK CARD 57-700-84. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING MBV INSPECTION, FOUND LEFT OMEGA BEAM HAS CORROSION AT CARBON CROSSBEAM BETWEEN FRAMES 24-25. REPAIRED OMEGA BEAM BY CUTTING OUT DAMAGE AND INSTALLING A DOUBLER OVER DAMAGED AREA IAW SRM 51-40-02 AND 53-00-10 FIGURE 202. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND LEFT INBOARD SEAT TRACK NR 1 IS CORRODED. RAI`D SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING IMBV INSPECTION, FOUND RIGHT OUTBOARD SEAT TRACK NR 1 IS CORRODED. RAI`D SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED

DURING IMBV INSPECTION, FOUND LEFT OUTBOARD SEAT TRACK NR 4 IS CORRODED. RAI`D SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING MBV INSPECTION, FOUND RIGHT UPPER FLOOR SUPPORT BETWEEN FRAMES 22 AND 22A TO BE CORRODED. RAI`D FLOORBEAM IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND RIGHT INBOARD SEAT TRACK NR 1 IS CORRODED. RAI`D SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING IMBV INSPECTION, FOUND LEFT OUTBOARD SEAT TRACK NR 2 IS CORRODED. R&I SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (CORRODED)

DURING MVB INSPECTION, FOUND LEFT OMEGA BEAM ANGLE ATTACHMENT AT FRAME 19 TO 19A CORRODED. REPLACED ANGLE IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED

DURING IMBV INSPECTION, FOUND RIGHT INBOARD SEAT TRACK NR 2 IS CORRODED. RAI`D SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND RIGHT OUTBOARD SEAT TRACK NR 4 IS CORRODED. RAI`D SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED

DURING IMBV INSPECTION, FOUND LEFT INBOARD SEAT TRACK NR 3 IS CORRODED. RAI`D SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND LEFT INBOARD SEAT TRACK NR 2 IS CORRODED. RAI`D SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CAP — CORRODED (RT MLG BEARING)

DURING MBV INSPECTION, FOUND RIGHT MAIN LANDING GEAR FORWARD BEARING CAP CORRODED. INSTALLED NEW BEARING CAP IAW WORK CARD 57-700-84. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CAP — CORRODED (MLG BEARING)

DURING MBV INSPECTION, FOUND LEFT MAIN LANDING GEAR AFT BEARING CAP CORRODED. INSTALLED NEW BEARING CAP IAW WORK CARD 57-700-84. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND RIGHT OUTBOARD SEAT TRACK NR 2 IS CORRODED. R&I SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — OVERTEMP (NOSE)

NR 1 BATTERY OVERTEMP. C/A REPLACED NR 1 BATTERY. FOLLOWED ETN EM-05-009. AIRCRAFT RETURNED TO SERVICE. (K)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

SGF - FLT 3788 - ENTRY, GALLEY DOOR, ROW 1 THROUGH ROW 8 AND LEFT EMERGENCY LIGHTS DO NOT ILLUMINATE. REPLACED EMERGENCY BATTERY PACKS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 3472 - BTR - CREW REPORTS EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED 2 FLOOR LIGHT STRIPS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

ORD - FLT 1484 - CREW REPORTED THE EMERGENCY LIGHT AT ROW 3 BC TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT INVERTER IAW EMB EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ORD - MAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT STRIP AT ROW 16 TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP AT ROW 16 IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 5,079 hrs · 4,757 cycles

CREW REPORTED THE THIRD EMERGENCY LIGHT TO BE INOPERATIVE DURING PREFLIGHT. MAINTENANCE REMOVED AND REPLACED THE NR 3 BATTERY CHARGER IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (GALLEY)

DURING A MBV INSPECTION THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA OF THE LT OMEGA BEAM. FABRICATED A DOUBLER, FILLER, PLATE AND 2 SHIMS FOR REPAIR. REPAIR DONE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (GALLEY)

DURING A MBV INSPECTION THE RT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA. FABRICATED A DOUBLER FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501186)

Part: CONTROL UNIT — INOPERATIVE (HORIZONTAL STAB)

DURING DESCENT CREW REPORTED PITCH .5 INOP MESSAGE. MESSAGE WENT OUT AFTER 10 SECONDS. MAINTENANCE REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT IAW MFG MM. OPERATIONAL CHECK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. ETN EB WAS COMPLIED WITH. (SW21200407369)