N808AE

Part: REGULATOR VALVE — FAILED (LT WING ANTI ICE) · airframe 37,098 hrs · 34,299 cycles

DURING CLIMB OUT PERFORMED ICE TEST. WE SAW WG A/ICE FAIL, STAB A/ICE FAIL, BLD 1 VLV FAIL, AND BLD 1 VLV CLOSED MESSAGES ON EICAS. "TRANSFERRED TO NRWC 808-DFW-03494"-C/A-REMOVED AND REPLACED ENGINE #1 BLEED VALVE IAW AMM 36-11-05.PERFORMED OPC IAW AMM 36-11-05. OPC GOOD. NO DEFECTS NOTED. SEE NRWC# 808-DFW-03494.

Part: RELAY — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 37,079 hrs · 34,274 cycles

CLIMBING THROUGH FL 190 WHEN BEGAN TO ACCUMLATE ICE AND THE FOLLOWING MSG; ICE COND- A/I INOP, STAB A/ICE FAIL, BLD 1 VLV FAIL, BLD 1 VLV CLSD, WG A/ICE FAIL, AND SPB/ ICE SPEED.-C/A-OHM BLEED 1 PUSH BUTTON SWITCH,SWITCH IS GOOD. REMOVED AND REPLACED RELAY RO 173 IAW WIRE MANUAL 20-13-03. BLEED 1 VALVE OPS CHECK GOOD IAW AMM 36-11-05 AMM

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,978 hrs · 34,180 cycles

COCKPIT EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-05-000-801-A AND 33-50-05-400-801-A. OPC GOOD. END.

Part: STRUT — LOW (NLG) · airframe 36,290 hrs · 33,513 cycles

DURING CLIMB OUT ENG1-2 REV DISAGREE AND LG AIR/GND FAIL MESSAGES PRESENTED. MESSAGES REMAINED ON THE ENTIRE FLIGHT. C/A-UPON A/C ARRIVAL FOUND NOSE LANDING GEAR TO BE BOTTOMED OUT, SERVICED NOSE LANDING GEAR IAW AMM 32-20-01. NO LEAKS NOTED OPC GOOD.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 35,976 hrs · 33,224 cycles

FA REPORTS MAIN CABIN DOOR IS STICKY TO OPEN AND CLOSE. C/A-LUBED AND PERFORMED OPCK OF PAX DOOR IAW AMM 53-21-02 AND 52-00-00. OPCK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,936 hrs · 33,184 cycles

EMERGENCY LIGHT INOP AT ROW 15. C/A-REMOVED AND REPLACED EMERGENCY LIGHT BULB IAW AMM 33-50-08 AND OPS CHECKED GOOD.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 35,843 hrs · 33,079 cycles

FLAP FAIL AT 9 DEGREES. TROUBLESHOT PER FIM TASK 27-51-00-810-801A OPS CHECK FAILED. REMOVED AND REPLACED THE FECU IAW AMM 27-53-02 OPC GOOD. PERFORMED OPERATIONAL CHECK OF FVS AND FLAP ACTUATOR IAW AMM 27-51-00. OPC GOOD. NO DEFECTS NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 35,817 hrs · 33,059 cycles

ON DEPARTURE BURNING SMELL PRESENT IN COCKPIT DESELECTED PACK 1 AND SMELL DISSAPTED. RESELECTED PACK 1 AND BEGAN CLIMB, SMELL INTENSIFIED. PAX REPORTED "BURNING CANDY" SMELL ON TAX IN-C/A-PERFORMED ETN-EM-72-034 NO DEFECTS OR ODORS NOTED. PERFORMED GVI OF COCKPIT AND CABIN LIGHTING NO DEFECTS NOTED (REF ETN-EM-72-034)

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 35,767 hrs · 33,018 cycles

FLAP FAIL DURING FLIGHT. C/A-INTERROGATED CMC FOUND LT FLAP TRANSMISSION FAIL. FOLLOWED FIM TASK 27-51-00-810-816-A PAGE 203 SUBTASK 816-001-A FOUND TO BE TRANSITORY CONDITION OF FLAP CONTROL SYSTEM. NO DEFECTS NOTED GVI OF FLAPS. OPS CHECK GOOD IAW AMM 27-51-00-700-801.

Part: SENSOR — FAILED (TE FLAP) · airframe 35,768 hrs · 33,020 cycles

SUPPLEMENTAL EICAS MSG: FLAP FAIL. CREW COMPLIED WITH QRH, DECLARED AN EMERGENCY AND DIVERTED TO BGR DUE TO MORE FAVORABLE WEATHER CONDITIONS. C/A-DURING TROUBLESHOOTING FOUND FLAP LT TRANSMISSION FAIL ON CMC. FOUND FLAP VELOCITY SENSOR TO BE FAULTY. REMOVED AND REPLACED FVS IAW AMM 27-51-12. OPC GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — ODOR · airframe 35,676 hrs · 32,946 cycles

SUPPLEMENTAL APU BLEED SOURCE TO PACKS HAS HINT OIL SMELL-C/A-PERFORMED ENG AND APU RUNS IAW ETN-EM-72-034. FOUND ENG 1 AND ENG 2 TO BE WORKING PROPERLY. APU IS SOURCE OF SMELL. DEFERRED APU AS PER MEL 49--1 (M) PROCEDURES C/W AUTH# 030270DM-C. FOLLOWED FIM TASK 21-20-00-810-803-A, NO EVIDENCE OF OIL LEAKS OF APU, ENG1 OR ENG2. PERFORMED OPC OF PACK SYSTEM IAW AMM 21-51-00, NO SMELL OF OIL. OPC GOOD MEL ITEM RESTORED.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 34,744 hrs · 32,059 cycles

MAIN PAX ENTRANCE DOOR IS HARD TO CLOSE AND TO OPEN AS REPORTED BY FLIGHT ATTENDANT "TRANSFERRED TO NRWC 808-DFW-02698"-C/A-REF TO NRWC 808-DFW-02698 FOR CORRECTIVE ACTION. READJUSTED MAIN PAX DOOR AFT UPPER ROLLER IAW EMB140 AMM TASK 52-18-00-820-805-A. OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 34,423 hrs · 31,725 cycles

FORWARD CABIN FA FLASHLIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE FWD FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: HANDLE — LACK OF LUBE (MAIN DOOR) · airframe 34,131 hrs · 31,466 cycles

FA REPORTS MAIN DOOR HARD TO OPEN. APPLIED LUBRICANT TO DOOR HANDLE AS REQUIRED, OPS CHK GOOD IAW AMM 52-10-01.

Part: SHEAR TIE — CRACKED (FRAME 61) · airframe 33,807 hrs · 31,166 cycles

SHEAR TIE CRACKED, 1/4 INCH BETWEEN STRINGERS 7R AND 6R AT FRAME 61. REMOVED AND REPLACED THE SHEAR TIE IAW AMM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FRAMES 48-49) · airframe 33,807 hrs · 31,166 cycles

LEFT WING LATERAL PANEL UPPER ATTACH ANGLE CRACKED BEWTEEN FUSELAGE FRAMES 48 AND 49. COMPLETED A REPAIR TO THE ATTACH ANGLE BETWEEN FUSELAGE FRAMES 48-49 IAW SRM 53-23-12 TYPE II.

Part: ATTACH ANGLE — CRACKED (FRAME 47) · airframe 33,807 hrs · 31,166 cycles

RIGHT WING LATERAL PANEL LOWER ATTACH ANGLE CRACKED AFT OF FUSELAGE FRAME 47. REMOVED AND REPLACED THE ATTACH ANGLE IAW ETN-EM-53-142.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 33,807 hrs · 31,166 cycles

CARGO DOOR LIFTING AND LOWERING MECHANISM, FWD ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED CARGO DOOR LIFTING LOWERING MECHANISM FWD ATTACH BRACKET IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRAME 61) · airframe 33,807 hrs · 31,166 cycles

SHEAR TIE CRACKED 1/4 INCH BETWEEN STRINGERS 7L AND 6L AT FRAME 61. REMOVED AND REPLACED THE SHEAR TIE IAW AMM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FRAME 41) · airframe 33,807 hrs · 31,166 cycles

RIGHT WING LATERAL PANEL LOWER ATTACH ANGLE CRACKED, FRAME 41. REPAIRED THE ATTACH ANGLE IAW ETN-EM-53-142,

Part: BEAM — CORRODED (FRAMES 65-68) · airframe 33,807 hrs · 31,166 cycles

CARGO DOOR, FUSELAGE CUTOUT HAS A CORRODED LOWER BEAM. COMPLIED WITH REMOVED AND REPAIRED OF CARGO DOON SILL IAW SRM 51-40-02.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,320 hrs · 30,675 cycles

FLOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY AND CHARGER IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 32,673 hrs · 29,866 cycles

AFT EMGERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 32,547 hrs · 29,732 cycles

FORWARD CABIN FLASHLIGHT WILL NOT STAY ON WHEN IN USE. R & R THE FLASHLIGHT IAW AMM 33-51-01 STEPS (2)(A)(B)(C)(E) OF FUNTIONAL CK. OP CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 31,798 hrs · 28,886 cycles

COCKPIT FLASHLIGHT OVER CAPTAIN`S SEAT DOES NOT INDICATE CHARGING. F/O COCKPIT FLASHLIGHT R & R WITH SERVICEABLE UNIT IAW AMM CHAP 20. OPS TEST GOOD, FLASHLIGHT SATISFACTORY CHARGING LIGHT GOOD.

Part: FUEL FILTER — CLOGGED (NR 2 ENGINE) · airframe 31,502 hrs · 28,573 cycles

E2 FUEL IMP BYP ON EICAS WHILE CLIMBING OUT. R & R E2 FPMU FUEL FILTER IAW MM 73-21-10. OPS AND LEAK CHECK OK.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,520 hrs · 28,589 cycles

FRAME 23 IS CRACKED BETWEEN STR 15R AND STR 16R. REPAIRED SECTION OF FRAME 23 BETWEEN STR 15R AND STR 16R IAW SRM 53-00-04 AND 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,520 hrs · 28,589 cycles

RIGHT AFT FUSELAGE FRAME 75 SKIN CRACK ABOVE STR 2 MARKED. REPAIRED RT AFT FUSELAGE SKIN CRACKED AT FRAME 75 AND ABOVE STR 2R IAW ERS-EM-53MR-2120.

Part: WIRE — BROKEN (CABIN) · airframe 31,495 hrs · 28,567 cycles

LT EMERGENCY LIGHT STRIP NR 1 IS BROKEN. REPAIRED BROKEN WIRE ON LT EMERGENCY LIGHT STRIP NR 1 IAW SWPM 20-21-00. BOW218817 FOR OPC.

Part: LIGHT — BROKEN (CABIN) · airframe 31,495 hrs · 28,567 cycles

LT EMERGENCY LIGHT STRIP NR 2 AND NR 7 ARE BROKEN. R&R LT EMERGENCY LIGHT STRIP NR 2 AND NR7 IAW AMM 33-50-12. BOW218817 FOR OPC.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 31,337 hrs · 28,397 cycles

SFP CLOSING ACTION FOR, RT AFT FUSELAGE 2 SCRATCHS, UPPER ONE 5 3/4 IN LENGTH & LOWER 4" LENGTH, UPPER SCRATCH HAS 1/8 DENT IN LENGTH & .224 IN DENT, MAX WIDTH 1 1/8 LOCATED BETWEEN STRINGERS 14R - 16R & FRAMES 62 & 63. MAJOR REPAIR. REPAIRED DAMAGE TO RT AFT FUSELAGE, BETWEEN FRAME 62 & 63 & STRINGERS 13R - 14R IAW SRM 53-30-01.

Part: DOOR — BINDS (CABIN) · airframe 31,040 hrs · 28,096 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN, SEEMS TO GET CAUGHT ON SOMETHING AFTER HANDLE MOVED TO THE OPEN POSITION. PERFORMED INSPECTION IAW AMM 56-20-01. DELAMINATION AREA < 25%. TDMI REMAINS OPEN. FUNCTIONAL CHECK WAS DONE WITH THE DYNAMOMETER, CHECK WAS FOUND TO BE WITHIN LIMIT LOAD IAW AMM 52-18-00, TDMI CLOSED.

Part: PRECOOLER — FAILED (BLEED AIR SYS) · airframe 30,989 hrs · 28,042 cycles

BLEED 1 LO TEMP, TRANSFERRED TO NRWC 808-ABI-01810. REMOVED AND REPLACED LT PRE-COOLER IAW EMB 140 AMM 36-11-04. SEE NRWC 808-ABI-01811 FOR OPERATIONAL TEST OF THE BLEED AIR SYSTEM. REGULATOR VALVE P/N 3215886-2 P/N 1367C. BLEED TEMPERATURE P/N 0132ADT S/N E0375. FAN AIR VALVE P/N 8166101 S/N 2004050159

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 30,186 hrs · 27,354 cycles

COCKPIT EMER LIGHT INOPERATIVE. R & R COCKPIT EMER LIGHT LAMP IAW AMM 33-50-05. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 29,864 hrs · 27,132 cycles

E2 ATTCS FAIL MASTER WARNING ON TAKEOFF ROLL AT ABOUT 80 KIAS. PERFORMED HIGH SPEED ABORT. PERFORMED TROUBLESHOOTING IAW RRMM 73-25-00-810-858. FOUND WORKING NORMAL ON FADEC A & B, NO FAIL NOTICED AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,572 hrs · 26,855 cycles

AISLE EMERGENCY LIGHT INOPERATIVE AT ROW 11. R & R AISLE EMERGENCY LIGHT LAMP AT ROW 11 IAW AMM 33-50-08-000-801-A & 33-50-08-400-801-A, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — ABNORMAL (COCKPIT) · airframe 28,640 hrs · 25,973 cycles

CAPTAIN`S FLASHLIGHT DIM. R & R CAPTAIN`S FLASHLIGHT IAW EMB AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: ROLLER — DIRTY (PAX DOOR) · airframe 28,538 hrs · 25,873 cycles

MAIN PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE. THE LATCH WOULD ONLY PARTIALLY MOVE. THE OUTSIDE LATCH MOVED ENOUGH TO PUSH THE DOOR OPEN AFTER GATE AGENT RAISED LATCH. CLEANED AND LUBED MAIN PAX DOOR FRAME ROLLERS IAW AMM 53-21-02. FOUND GOOD AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,470 hrs · 25,813 cycles

EMERGENCY LIGHT AT PAX DOOR ENTRANCE INOPERATIVE. R & R PAX DOOR ENTERANCE LIGHT BULB IAW AMM 33-50-06. OPS CHECKED GOOD.

Part: DISPLAY — FAILED (COCKPIT) · airframe 28,449 hrs · 25,790 cycles

LOST CAPTAIN`S PFD DURING LANDING. SMOKE, AND BURNING ODOR. REPLACED CAPTAIN'S PFD IAW AMM 34-22-01. OPS CHECKED GOOD.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 27,851 hrs · 25,238 cycles

F/A FLASHLIGHT BASE CRACKED. R & R F/A FLASHLIGHT CRADLE IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 27,591 hrs · 25,037 cycles

THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. THE ACFT WAS REMOVED FROM SERVICE. LUBED MAIN CABIN DOOR AND THE OPS CHECK WAS GOOD IAW AMM 52-11-00. THE ACFT WAS RETURNED TO SERVICE.

Part: DOOR — BINDING (MAIN CABIN) · airframe 27,498 hrs · 24,957 cycles

THE F/A REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. ACFT REMOVED FROM SERVICE. LUBRICATED AFT ROLLER IAW AMM 52-11-00. THE OPS CHECKED GOOD IAW AMM 52-10-01. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,074 hrs · 24,562 cycles

DURING B INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-30-01-000-801-A AND 33-30-01-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — CRACKED (CABIN) · airframe 27,032 hrs · 24,526 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT NR 1 AND NR 6 FLOOR PROXIMITY LIGHT ASSEMBLY & SIDEWALL ASSEMBLY CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE LEFT NR 1 AND NR 6 FLOOR PROXIMITY LIGHT ASSEMBLY & SIDEWALL ASSEMBLY AMM 33-50-12 IPC 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FASTENER — MISSING (EMERGENCY LIGHT) · airframe 27,032 hrs · 24,526 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT & LEFT EMERGENCY (PROXIMITY) LIGHT STRIP AND SIDEWALL ASSEMBLY HARDWARE CORRODED, STRIPPED AND MISSING. (REF AMM 33-50-12 IPC 33-50-12) THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE EMERGENCY (PROXIMITY) LIGHT STRIP AND SIDEWALL ASSEMBLY HARDWARE CORRODED, STRIPPED AND MISSING. (REF AMM 33-50-12 IPC 33-50-12). THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 27,032 hrs · 24,526 cycles

DURING B INSPECTION FOUND THE CENTER LAV FLOOR GUSSET CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CENTER LAV FLOOR GUSSET IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 27,032 hrs · 24,526 cycles

DURING B INSPECTION FOUND THE LEFT NR 8 FLOOR PROXIMITY ASSEMBLY WIRE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED BOTH CONNECTORS ON NR 8 FLOOR LIGHT STRIP IAW SWPM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 27,032 hrs · 24,526 cycles

DURING B INSPECTION FOUND THE RIGHT LAV FLOOR GUSSET CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT LAV FLOOR GUSSET IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 27,032 hrs · 24,526 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 4 FLOOR PROXIMITY LIGHT STRIP HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 FLOOR PROXIMITY LIGHT STRIP IAW EMB AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — CORRODED (E/E BAY) · airframe 26,962 hrs · 24,459 cycles

AFT ELECTRONIC COMPARTMENT DOOR HAS CORROSION UNDER THE FOWARD LOWER DOOR GUIDE. REPAIRED AFT ELECTRONIC COMPARTMENT DOOR IAW EO EM-52MR-352.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,962 hrs · 24,459 cycles

FUSELAGE SKIN CRACKED, APPROX .7500" LONG AT FR 75, STR 2L. REPAIRED DAMAGED AREA IAW EO EM-53MR-2113.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,848 hrs · 23,481 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT ABOVE 11A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT ABOVE 11A 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: FLASHLIGHT — ODOR (CABIN) · airframe 24,784 hrs · 22,480 cycles

ON FLIGHT 4071 THE CREW REPORTED AN ELECTRICAL ODOR IN THE CABIN. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND FORWARD FLIGHT ATTENDANT HANDSET THE SOURCE OF THE ODOR. REMOVED AND REPLACED THE FORWARD HANDSET CRADLE IAW EMB140 AMM 23-31-03 AND REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 23,860 hrs · 21,627 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 6 FLOOR PROXIMITY EMERGENCY LIGHT STRIP WIRE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED WIRE IAW SPWM 20-21-00. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,782 hrs · 21,551 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT FORWARD SID CENTER FAIRING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACTUATOR — INOPERATIVE (HORIZ STAB) · airframe 23,667 hrs · 21,445 cycles

ON FLIGHT 3955 THE CREW REPORTED THE PITCH TRIM MAIN INOPERABLE. REPORTED THE BACKUP TRIM WORKED IF AUTO PILOT LEFT ON. GOT AP MIS TRIM ALL LANDING PARAMETERS NORMAL. THE CREW DECLARED AN EMERGENCY AND RETURNED TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR IAW 140 AMM 27-40-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,984 hrs · 20,895 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT EXTERIOR EMERGENCY LIGHT IAW EMB 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ADC — MALFUNCTIONED (NR 1)

ABORTED TAKEOFF (AROUND 60KTS) DUE TO CA'S AIRSPEED INDICATOR STAGED IE NO AIRSPEED INDICATION. REMOVED AND REPLACED NR 1 ADC IAW AMM 34-15-01 OPS TEST GOOD. LEAK CHECK GOOD IAW AMM 34-13-00, NO LEAKS NOTED.

Part: SIGN — INOPERATIVE (CABIN) · airframe 22,583 hrs · 20,583 cycles

FOR FLIGHT 2969 DURING PREFLIGHT INSPECTION FOUND THE FORWARD CEILING EMERGENCY EXIT MARKER WOULD NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EXIT SIGN IAW EMB 140 AMM 30-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,037 hrs · 20,093 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME 23 BETWEEN STRINGERS 15 RIGHT AND 16 RIGHT CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED BY SPLICING IN A NEW SECTION OF FRAME IAW AE EO EM-53MR-1775. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 20,096 hrs · 18,397 cycles

ON FLIGHT 3211 DURING THE CLIMB THE FLIGHT ATTENDANT REPORTED A BURNING SMELL AND SMOKE IN THE GALLEY AREA. THE CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FORWARD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY AND CAPTAIN FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (BRAKE SYSTEM) · corrosion level 2 · airframe 18,521 hrs · 16,996 cycles

ON FLIGHT 4732 THE CREW NOTICED THE BRAKES GRABBING. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE BRAKE CONTROL UNIT IAW EMB-140 AMM 32-41-02, AND PERFORMED MAIN BRAKE FUNCTIONAL CHECK IAW AMM 32-41-00. ALL OPERATIONAL TESTS GOOD, NO FURTHER DEFECT NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,691 hrs · 16,317 cycles

DURING IMBV INSPECTION, FOUND LT OMEGA BEAM NEAR FRAME 33 IS CORRODED. REPAIRED OMEGA BEAM IAW SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,691 hrs · 16,317 cycles

DURING IMBV INSPECTION, FOUND LT OMEGA BEAM IS CORRODED BY FRAME 27. REPAIRED OMEGA BEAM IAW SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,691 hrs · 16,317 cycles

DURING MBV INSPECTION, FOUND LEFT OMEGA BEAM CORRODED AT FRAME 20 WHERE CROSSBEAM ATTACHES. REPAIRED OMEGA BEAM IAW SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,691 hrs · 16,317 cycles

DURING IMBV INSPECTION, FOUND CENTER OMEGA BEAM CORRODED NEAR FRAME 25. REPAIRED OMEGA BEAM IAW SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,691 hrs · 16,317 cycles

DURING IMBV INSPECTION, FOUND CARGO DOOR CUTOUT SILL CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,468 hrs · 13,736 cycles

CREW REPORTED PART OF THE EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED NR 1, NR 2, NR 3, NR 4 BATTERY POWER SUPPLIES IAW EMB 140 AMM 33-50-04. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 14,361 hrs · 13,659 cycles

AFTER DEPARTURE OBSERVED SMELL OF BURNING RUBBER IN THE COCKPIT AND F/A VERIFIED SMELL IN GALLEY PASSENGER COMPARTMENT. CREW RETURNED TO THE BLOCK. REMOVED AND REPLACED RIGHT ENG IAW EMB WCNR 71-000-00 AND OPS CHECK WAS DONE PER WORK CARD NR 72-700-00. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 14,359 hrs · 13,656 cycles

IN ICE CONDITION GOT STRONG BURNING RUBBER SMELL IN COCKPIT AND CABIN. REMOVED AND REPLACED NR 1 ENGINE IAW WC NR 71-000-00. NO BURNING SMELL NOTED DURING OPS CHECK. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — BURNED (WINDSHIELD HEAT) · airframe 14,336 hrs · 13,644 cycles

ELECTRICAL ODOR IN COCKPIT AND FLT ATTENDANT REPORTED SMOKE/HAZE AT ROWS 10 AND 11. UPON INSPECTION FOUND BURNT CONNECTOR AT THE F/O WINDSHIELD POWER CONNECTOR. REPLACED BURNT CONNECTOR IAW EMB 140 WM 20-00-0. REATTACHED CONNECTOR TO FO WINDSHIELD IAW EMB 30-43-04. AIRCRAFT RETURNED TO SERVICE.

Part: BRACKET — CRACKED (ZONE 800) · airframe 12,717 hrs · 12,492 cycles

MAIN ENTRANCE DOOR LOCKING HANDLE BRACKET CRACKED. STOP DRILLED, FABRICATED AND INSTALLED DOUBLER IAW EMB IC2007/145-0259A. RETURNED AIRCRAFT TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT)

LEFT WING LOWER EMERGENCY LIGHT INOPERATIVE. REPLACED NR 1 BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 FOUND CORRODED. BLENDED DAMAGED AREA TO REMOVE CORROSION. APPLIED ALODINE AND EPOXY PRIMER TO EXPOSED SURFACE. FABRICATED DOUBLER FOR REPAIR. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/2057 PARA 5 DATED APRIL 25, 2005. (M)

Part: SILL — CORRODED (FUSELAGE)

SERVICE DOOR CENTER SILL FOUND CORRODED. BLENDED CORROSION OUT. FABRICATED 2 DOUBLERS. REPAIR DONE IAW EMB IC2005-145/2057, DATED APRIL 25, 2005. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

CENTER OMEGA BEAM AT FRAME 27 WAS FOUND TO HAVE ELONGATED HOLE IN AN EXISTING REPAIR. REMOVED EXISTING REPAIR AND FABRICATED NEW REPAIR DOUBLER. REPAIR DONE IAW EMB IC2005-145/2057 DATED APRIL 22, 2005. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CENTER HAT BEAM AT FRAME 20 FOUND TO BE CORRODED. REMOVED CORRODED CENTER HAT BEAM AND INSTALLED SERVICEABLE BEAM. REPAIR DONE IAW EMB SRM 145/1142 REV 28, CHAPTER 51-40-02. (M)

Part: CONTROL UNIT — INOPERATIVE (HORIZONTAL STAB)

ON FINAL APPROACH CREW RECEIVED PITCH TRIM 1-2 INOPERATIVE ON EICAS. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB)

BOS - FLT 4546 - MOMENTARY PITCH 1 AND 2 TRIM INOPERATIVE OCCURRING ON FINAL. FLAP AT 22 DEGREE, GEAR UP. LASTED APPROX 5 SECONDS. REPLACED HSCU. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN MBV INSPECTION, THE LT FLOORBEAM AT FRAME 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT THE DAMAGE SECTION OF THE LEFT OMEGA BEAM, CLEANED, AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 21, CHAPTER 53-21-10 FIG 202, SHEET 2 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN MBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGE OF LEFT FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AND EXTERNAL ANGLE, FILLER, PLATE AND SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 21, CHAPTER 53-21-10 FIG 201. (M)