N858AE

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,964 hrs · 28,739 cycles

RT LATERAL PANEL EMERGENCY LIGHT INOPERABLE. C/A: R & R RT EMERGENCY LIGHT LAMP, IAW EMB 140 AMM 33-50-10. OPERATIONS CHECK GOOD.

Part: CRADLE — BROKEN (C/P FLASHLIGHT) · airframe 31,911 hrs · 28,696 cycles

COCKPIT FLASH LIGHT BRACKET BROKEN. C/A: DEFERED COCKPIT FLASH LIGHT BRACKET. C/W MEL MAINTENANCE PROCEDURES.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 31,850 hrs · 28,630 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN PER THE FLIGHT ATTENDANT. C/A-LUBED MAIN DOOR ROLLERS IN REF TO AMM 53-21-02. OPC GOOD.

Part: LAMP — INOPERATIVE (EMERGENC LIGHTS) · airframe 31,796 hrs · 28,565 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (CHARGER) · airframe 31,757 hrs · 28,517 cycles

LH AND RH EMERGENCY EXIT ROWS EXIT SIGNS INOP-C/A-T/S IAW FIM TASK TASK 33-50-00-810-804-A FOUND NO 3 BATTER CHARGER ASSY CANNON PLUG DISCONNECTED. REINSTALLED IN REFERENCE WITH EMB AMM TASK 33-50-04-400-801-A OPC GOOD

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 31,757 hrs · 28,517 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT IAW EMB AMM 33-50-07-000-801-0A AND 33-50-07-400-801-A.. NO FIX. RAR LH OVERWING EMERGENCY LIGHT ASSY IAW EMB AMM 33-50-07-000-802-A AND 33-50-07-400-802-A. NO FIX. RAR NO 4 INCERTER IAW EMB AMM TASK 33-50-11-000-801-A AND 33-50-11-400-801-A NO FIXRAR BATTERY PACK AND CHARGER IAW EMB AMM 33-50-04-000-801-A AND 33-50-04-400-801-A AND 33-50-04-000-802-A AND 33-50-04-400-802-A. OPS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 31,597 hrs · 28,352 cycles

MAIN DOOR GETS STUCK, REALLY HARD TO OPEN. LUBRICATED MAIN PAX DOOR FRAME ROLLERS IAW AMM 53-21-02, OPENED AND CLOSED MAIN PAX DOOR MULTIPLE TIMES WITH NO ISSUES IAW AMM 52-10-00.

Part: MECHANISM — LACK OF LUBE (MAIN DOOR) · airframe 31,592 hrs · 28,345 cycles

MAIN DOOR ONLY OPENS FROM THE INSIDE. FOUND HANDLE MECHANISM DRY CLEANED AND LUBRICATED AS PER AMM 52-11-00 OPC GOOD.

Part: POWER SUPPLY — INOPERATIVE (EXTERIOR LIGHT) · airframe 31,571 hrs · 28,321 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R THE LT EXTERIOR OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A. NO FIX. R & R THE NR 4 EMERGENCY LIGHTING SYSTEM POWER SUPPLY IAW WORK CARD 33-700-19. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,524 hrs · 28,281 cycles

PROX FLOOR EMERGENCY LIGHTING AT ROW 14A INOP. REMOVED AND REPLACED PROX FLOOR EMERGENCY LIGHTING AT ROW 14 IAW AMM 33-50-12 OPS CHECK GOOD.

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 31,524 hrs · 28,281 cycles

AFT EMERGENCY FLASHLIGHT CHARGING CRADLE BROKEN. REMOVED AND REPLACED THE AFT FLASHLIGHT CHARGING CRADLE, OPS CHECKED GOOD, IAW AMM 33-50-16.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,374 hrs · 28,130 cycles

CENTER AISLE L/H AND R/H OMEGA BEAMS EXISTING REPAIRS AT FR 24 CORRODED.-C/A-CENTER AISLE LH OMEGA BEAM AT FR 24 BLENDED AND REPOSTECTED IAW ETN-GN-51-008 AND ETN -EM -076R1 REMAING THICK .047" ON NOMINAL .050". FOUND WITH IN LIMITS. CENTER AISLE RH OMEGA BEAM AT FR24 REPAIRED IAW SRM 53-00-10 FIG 203.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,374 hrs · 28,130 cycles

R/H AND L/H OMEGA BEAMS ANGLES CRACKED BTW FR47-48 (R/H OMEGA BEAM INBD ANGLE, L/H OMEGA BEAM OUTBD ANGLE).-C/A-R/H & L/H OMEGA BEAM ANGLES BETWEEN FR 47-48 (RH OMEGA BEAM INB ANGLE, LH OMEGA BEAM OUTB ANGLE) REPAIRED IAW SRM 53-23-03 & 53-23-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,374 hrs · 28,130 cycles

FR 23 CRACKED AT THE JUNCTION WITH R/H OUTBD FLOOR SILL-C/A-FRAME 23 AT THE JUNCTION WITH RH OUTBOARD FLOOR SILL REPAIRED IAW SRM 53-00-04.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 31,374 hrs · 28,130 cycles

VERTICAL STAB., SKIN BEHIND SPAR 3, R/H LOWER PROFILE CRACKED. -C/A-VERTICAL STABILIZER, RH LOWER PROFILE BTW ZV1430 - ZV1932 REPAIRED IAW ETD 2020-145-010830.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,374 hrs · 28,130 cycles

CENTER AISLE LH AND RH OMEGA BEAMS EXITING REPAIRS AT FR 24 CORRODED-C/A-CENTER AISLE LH OPMEGA BEAM AT FR24 BLENDED AND REPROTECTED IAW ETN GN 51-008 AND ETN EM 076R1 REMAINING THICK .047 ON NOMINAL .050 FOUND WITHIN LIMITS CENTER AISLE RH OMEGA BEAM REPAIR AT FS224 BLENDED AND FOUND OUT OF LIMITS IAW ETN EM 53-076R1 REMOVED TRIM ON RH OMEGA BEAM BTW FS 23-25 FOR ACCESS CENTER AISLE RH OMEGA BEAM PREVIOUS REPAIR AT FR24 REMOVED AND REPLACED IAW SRM 53-00-10 RH OMEGA BEAM TRIM BTW FS23-25 REINSTALLED IAW SPM 31-40-02

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,374 hrs · 28,130 cycles

RH AND LH OMEGA BEAMS ANGLES CRACKED BTW FR47-48 (RH OMEGA BEAM INBD ANGLE LH OMEGA BEAM OUTBD ANGLE)-C/A-LH MAIN PIWER LINE WIRE CLAMPS LOOSEN FOR ACCESS SHEET METALNLH OMEGA BEAM OUTBD ANGLE REMOVED FOR ACCESS REPAIR RH OMEGA BEAM INBD ANGLE REMOVED FOR REPLACEMENT NEW PARTS INTALLED ON RH OMEGA BEAM AS PER SRM 53-23-03 NEW REPAIR PARTS INSTALLED ON LH OMEGA BEAM IAW SRM 53-23-05 LH MAIN POWER LINE WIRE CLAMPS REINSTALLED AS PER AMM 20-10-01

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,374 hrs · 28,130 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RH OVERWING EMERGENCY LIGHT LAMP REPALCED IAW AMM 33-50-01 REFER TO TASK CARD 33-2047 FOR TEST

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 31,374 hrs · 28,130 cycles

ALUMINUM CROSSBEAMS AT FR18 FR20 AND FR24 CORRODED-C/A-ALUMINUM CROSS BEAMS AT FR18, FR20 AND FR24 BLENDED OUT OF LIMITS IAW ETN EM 53-241 AT FRO20 CRISS BEM REMOVED FOR REPLACEMEBT AT FR18 AND 24 CROSSBEAM REMOVED CROSSBEAM FABRICATION COVER ON WC 53 2216 ALUMINUM CROSSBEAM(MADE REPAIR PART CPP) FR 18 20 AND 24 INSTALLED AS PER CTN ETN EM 53-139 ETN EM 53-150 AND SRM 51-40-02

Part: UNKNOWN — ABNORMAL (CABIN PRESSURE) · airframe 30,520 hrs · 27,294 cycles

AIRCRAFT WOULD NOT PRESSURIZE ON CLIMBOUT.-C/A-DEFERRED PRESSURIZATION SYSTEM. M PROCEDURES C/W. MEL 21-19 AUTH 090955DM-C. PERFORMED OPC IAW EMB 140 AMM 21-31-00. OPC OF MANUAL AND AUTO PRESSURIZATION GOOD. NO DEFECTS NOTED. MEL RESTORED. M- PROCEDURES REVERSED.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 30,381 hrs · 27,142 cycles

CA MFD WENT BLANK IN FLIGHT FOLLOWED BY SMOKE/ ACRID SMELL. EMERGENCY DESCENT AND DIVERSION TO FSM. C/A-PERFORMED FIM PROCEDURES FOR SMOKE AND SMELL IN COCKPIT IAW FIM 21-20-00. MFD REMOVED AND INSPECTED. FOUND BURNED PIN ON MFD ELECTRICAL CONNECTOR AND MFD PIN 106. ELECTRICAL SMELL COMING FROM MFD AND ELECTRICAL CONNECTOR. REINSTALLED IN SAME PLACE IAW AMM 34-22-01. DEFERRED CA MFD PER MEL 34-2. M PROCEDURES C/W REF: MEL 34-2 AUTH: 090094M-B. REMOVED AND REPLACED PIN 106 OF CONNECTOR J1028 IAW SWPM 20-50-01. REMOVED AND REPLACED MFD 1 IAW AMM 34-22-01. OPS CHECK GOOD IAW AMM 34-22-00. MEL RESTORED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,240 hrs · 26,988 cycles

EMERGENCY LIGHT AT 6A INOPERATIVE. REMOVED AND REPLACED CEILING EMERGENCY LIGHT AT 6A IAW AMM 33-50-08. OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 30,160 hrs · 26,891 cycles

SERVICE DOOR EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-09 OPC GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 29,639 hrs · 26,377 cycles

PTRIM MAIN INOP PTRIM BACKUP INOP. C/A-REMOVED AND REPLACED HSCU IAW AMM 27-40-01. OP CK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 29,638 hrs · 26,376 cycles

PTRIM MAIN AN BACKUP INOP. C/A-C/W FIM TASK 27-43-00-810-820-A NO FAULTS FOUND TRANSITORY CONDITION OF THE HORZ STAB CTL UNIT OK FOR SERVICE OPS CK GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 29,067 hrs · 25,820 cycles

MOST AFT FLOOR EMERGENCY LIGHT STRIP HAS BROKEN WIRES. C/A-REMOVED DAMAGED MOST AFT FLOR EMERGENCY LIGHT STRIP AND INSTALLED NEW LIGHT STRIP IAW AMM 33-50-12-400-801.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,791 hrs · 25,578 cycles

EMERGENCY LIGHT OVER SERVICE DOOR INOP-C/A-FOUND EMERGENCY LIGHT INVERTER #2 BAD. RAR #2 EMERGENCY LIGHT INVERTER OPS CHECK GOOD IAW EMB AMM 33-50-12

Part: FIRE DETECTOR — FAILED (NR 1 ENGINE) · airframe 28,691 hrs · 25,481 cycles

E1 FIRE DET FAIL ON EICAS IN CRUISE/DESCENT/LANDING & TAXI IN NO OTHER ADNORMALLITIES NOTED-C/A-REMOVED AND REPLACED LH ENGINE FIRE LOOP DETECTOR IAW EMB 140 AMM 26-11-01 OPS CHECKS GOOD

Part: FUEL CONTROL — LEAKING (APU) · airframe 28,592 hrs · 25,387 cycles

WITH APU ON & APU BLEED & PACKS OPEN, THERE IS A STRONG EXHAUST/FUEL SMELL IN AIRCRAFT. DEFERRED APU FUEL SHUT OFF VALVE PER MEL 28-5. MTX PROCEDURE C/W. FOUND LEAKING APU FUEL CONTROL. R&R APU FUEL CONTROL IAW ENGINE MANUAL 49-32-01. OPC AND LEAK CHK GOOD.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 27,034 hrs · 23,853 cycles

LT/RT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 4 EMERGENCY POWER SUPPLY UNIT IAW AMM 33-50-04 OPC GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 24340. LIGHT EMERGENCY L/H P/N 30-2510-3.

Part: FITTING — DAMAGED (LT AILERON) · airframe 27,027 hrs · 23,847 cycles

LEFT AILERON, DAMPER ATTACHMENT FITTING ON THE AILERON FRONT SPAR FOUND DAMAGED. REMOVED AND REPLACED THE AILERON DAMPER FITTING IAW EO EM27MR-112.

Part: SHEAR TIE — CORRODED (FRAME 65) · corrosion level 2 · airframe 27,027 hrs · 23,847 cycles

FWD SHEAR TIE AT FRAME 65 CORRODED. THE SHEAR TIE WAS REPAIRED IAW SRM 53-31-04.

Part: CHARGER — FAILED (CABIN) · airframe 26,992 hrs · 23,823 cycles

EMERGENCY LIGHTING SYS FAILED OPERATIONS CHECK. R & R NR 2 EPSU BATTERY CHARGER ASSEMBLY IAW WC 33-700-19 IAW ITEM 3 LG PG 3731174.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,992 hrs · 23,823 cycles

EMERGENCY LIGHTING SYS FAILED OPERATIONS CHECK. R & R NR 2 EMER LIGHTING BATTERY ASSEMBLY IAW WC 33-700-19 IAW ITEM 4 LG PG 3731174.

Part: CLAMP — LOOSE (NR 1 A/C PACK) · airframe 26,727 hrs · 23,609 cycles

DURING ICE PROTECTION TEST, PNEUMATIC IN THE AIR, THE EICAS CAUTION MESSAGE FOR NR 1 A/C PACK VALVE FAIL. MESSAGE WENT AWAY WHEN TEXT ENDED. ADJUSTED & TORQUED NR 1 PACK UPPER CLAMP IAW EM-21-056. PERFORMED OPS CHECK OF ANTI ICE SYSTEM, FOUND GOOD. PERFORMED OPS CHECK OF NR 1 PACK SYSTEM FOUND GOOD IAW AMM 30-00-00 & AMM 21-51-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,260 hrs · 23,204 cycles

DURING PS 1 CHECK FOUND THE UPPER LT EXTERNAL EMER LIGHT TO BE INOPERATIVE. R & R THE LAMP OF THE UPPER LT EXTERNAL EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: BUTTON — DEFECTIVE (AC PACK) · airframe 26,116 hrs · 23,059 cycles

PACK 2 VLV CLSD ICAS IN FLIGHT. COMPLIED WITH VOL 1 CAME ON AGAIN ADVISORY MSG. R & R PACK 2 PUSH BUTTON IAW AMM 20-13-04. OPERATIONS CHECKED GOOD.

Part: HEAT EXCHANGER — FAILED (NR 2) · airframe 26,117 hrs · 23,061 cycles

PACK 2 VLV CLSD DURING CLIMB BELOW 10,000 FT. WE RESET IT & IT CAME BACK ON AT 220 FL, IT WAS RESET 6 TIMES DURING DESCENT. DEFERRED IAW MEL 21-29. REMOVED AND REPLACED NR 2 DUAL HEAT EXCHANGER IAW EMB 140 AMM 21-51-02 AND OPS CHECKED GOOD. MEL ITEM 21-29 RESTORED AND CLEARED.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 25,921 hrs · 22,898 cycles

DURING FLIGHT 2729 FOUND WX RADAR INOPERABLE IS NOT RELIABLE. DOES NOT PAINT KNOWN WX OUTSIDE APPROXIMATELY 12 MILES. DOES NOT DEPICT SEVERITY OF WX. THE ACFT WAS REMOVED FROM SERVICE. R & R WEATHER RTA ASSEMBLY IAW AMM 34-42-01. OPERATIONS CHECKED GOOD. THE ACFT RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,767 hrs · 22,725 cycles

IST ROW OF EMERGENCY STRIP LIGHTS & EXIT SIGN ON LWR FWD SERVICE DOOR INOPERATIVE. R & R NR 2 INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED OF EMERGENCY LIGHTS GOOD IAW 33-50-00.

Part: MANIFOLD — FAULTY (NLG STEERING) · airframe 25,728 hrs · 22,685 cycles

DURING TAKEOFF ROLL AT APPROXIMATELY V1, 119 KTS, THE STEERING JERKED HARD TO THE RIGHT. ACFT ROTATED AT 124 KNOTS WITH NO EICAS ANNUNCIATIONS. A NORMAL LANDING WAS DONE WITH NO FURTHER STEERING PROBLEMS. STEERING WAS DISENGAGED ON LANDING ROLLOUT & TAXI WAS NOT ATTEMPTED, TRANSFERRED TO NRWC 858-ORD-01394. REPLACED STEERING MANIFOLD IAW NRWC 858-ORD-01395 & RUDDER PEDAL POTENTIOMETER IAW NRWC 858-ORD-01390 & BLEED AIR OUT OF NOSE STEERING ACTUATOR IAW CMM 32-21-11. STEERING OPERATIONS CHECKED GOOD IAW AMM 32-50-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,618 hrs · 22,568 cycles

LT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LT FWD FAIRING PANEL LIGHT IAW MM 33-50-10, OPERATIONS CHECKED GOOD.

Part: PIN — POPPED (WINDOW) · airframe 25,527 hrs · 22,494 cycles

ON ROTATION CAPTAIN`S DV WINDOW PIN POPPED UP. WINDOW APPEARED CLOSED & CABIN MAINTAINED 500 FT PRESSURIZATION. OPENED & CLOSED DV WINDOW FOR CAPTAIN`S SIDE IAW AMM 56-11-00, OPERATIONS CHECKED GOOD.

Part: BLEED AIR SYS — OVERHEATED (NR 1) · airframe 25,434 hrs · 22,397 cycles

BLEED 1 OVERHEAT DURING CLIMB OUT.

Part: ENGINE — FAILED (RIGHT) · airframe 24,743 hrs · 21,828 cycles

RT ENGINE VIBRATION BY SOUND AND FEEL ON APPROACH AND SHUTDOWN. OIL DOWN TWO QUARTS ON TWO HOUR FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED RT ENGINE IAW W/C71-000-00. THE OPS CHECKED GOOD. NO LEAKS NOTED. ACFT RETURNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (BRAKE SYSTEM) · airframe 24,309 hrs · 21,429 cycles

THE CREW REPORTED THAT ON FINAL APPROACH THEY RECEIVED AN EICAS BREAK INBD INOPERATIVE MESSAGE WHEN THE LANDING GEAR WAS SLECTED DOWN. THE CREW COMPLIED WITH AOM VOL 1 PROCEDURES AND AN EMERGENCY WAS DECLARED. THE ACFT LANDED WITH FLAPS AT 45 WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R THE BRAKE CONTROL UNIT IAW AMM 32-41-02. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (AFT CABIN) · airframe 24,273 hrs · 21,400 cycles

AFT CABIN FLASH LIGHT INOPERATIVE. R & R FLASHLIGHT ASSY IAW AMM 33-50-16, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,101 hrs · 21,254 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-50-10 AND OPS CHECKED GOOD IAW 33-50-00.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 23,751 hrs · 20,958 cycles

DURING MX INSPECTION, FOUND THE NR 2 EMERGENCY BATTERY WON'T HOLD A CHARGE. ACFT REMOVED FROM SERVICE. R & R NR 2 EMERGENCY BATTERY AND CHARGER IAW 33-50-04. THE OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: DAU — FAULTY (BRAKE SYSTEM) · airframe 23,647 hrs · 20,866 cycles

THE CREW REPORTED THAT ON APPROACH TO LAND WHEN THEY PUT THE GEAR DOWN THEY RECEIVED AN OTBD BRAKE INOP MESSAGE ON EICAS. THE CREW WENT AROUND TO RUN THE CHECKLIST. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED A CONTINUITY AND INSULATION TEST OF WIRING FROM BCU J2 CONNECTOR PIN 79 TO DAU 1 J1019 CONNECTOR PIN A3. TESTED GOOD. R & R AFDAU IAW AMM NR 31-31-07. OPS CK GOOD. NO FAULTS NOTED. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 23,259 hrs · 20,551 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT INTERMITTENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR EMERGENCY LIGHT LAMP REF EMB 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LANDING GEAR — CONTAMINATED (LEFT) · airframe 22,528 hrs · 19,910 cycles

FOR FLIGHT 3405 THE CREW/MAINTENANCE REPORTED SMOKE COMING FROM THE LEFT MAIN LANDING GEAR. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED GEARS AND FOUND NO INDICATION OF LEAKAGE OR OVER HEATING. MANITENANCE NOTED GLYCOL DRIPPING FROM THE GEAR WELL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,510 hrs · 19,896 cycles

DURING B INSPECTION FOUND THE ENTRY AREA CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK IAW EMB-140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,510 hrs · 19,896 cycles

DURING B INSPECTION FOUND THE CABIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK IAW EMB-140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 22,413 hrs · 19,830 cycles

ON FLIGHT 3294 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS NOT ILLUMINATING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,371 hrs · 19,794 cycles

DURING MAINTENANCE INSPECTION FOUND FRAME 23 BETWEEN STRINGER 15R AND 16R CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED PERMANENT REPAIR IAW EO EM-53MR-1808. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,371 hrs · 19,794 cycles

DURING MAINTENANCE INSPECTION FOUND LAV RIGHT OMEGA BEAM CORRODED AROUND FORWARD NUT PLATE HOLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED PERMANENT REPAIR IAW EO EM-53MR-2048. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 22,372 hrs · 19,795 cycles

DURING MAINTENANCE INSPECTION FOUND EMERGENCY LIGHT STRIP NR 8 HAS DAMAGED WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 8 EMERGENCY LIGHT STRIP IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (LAVATORY) · airframe 22,372 hrs · 19,794 cycles

LAV RT OMEGA BEAM CORRODED AROUND FWD NUTPLATE HOLE. ACCOMPLISHED AEA EO EM-53MR-2048, PART A RT LAVATORY FLOORBEAM CORROSION REPAIR.

Part: LIGHT — DAMAGED (CABIN) · airframe 22,372 hrs · 19,795 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT STRIP NR 1 & 5 DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 & 5 EMERGENCY LIGHT STRIP IAW EMB 140 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 22,372 hrs · 19,795 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 2 EMERGENCY LIGHT STRIP HAS BROKEN WIRE ON STRIP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT STRIP IAW EMB 140 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,372 hrs · 19,795 cycles

DURING MAINTENANCE INSPECTION FOUND NR 4 EMERGENCY LIGHT BATTERY FAILED OPERATIONAL CHECK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY AND CHARGER IAW AEA W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: VALVE — INOPERATIVE (NLG) · airframe 21,291 hrs · 18,554 cycles

FLIGHT 3065, RECEIVED A LANDING GEAR AIR FAIL MESSAGE ON EICAS ON TAKEOFF ABOUT 1000 FT AGL. RECEIVED A THRUST REVERSER DISAGREE MESSAGE AT 1500 FT AGL, GEAR DOWN, FLAPS 45, AIRSPEED 140 KTS, MESSAGES WENT AWAY ON SHORT FINAL. DECLARED AN EMERGENCY. AIRCRAFT BEHAVED NORMALLY ON LANDING, ROLLOUT AND TAXI. AIRCRAFT REMOVED FROM SERVICE. FOUND NOSE LANDING GEAR CHARGING VALVE LEAKING. PERFORMED EXTENSION AND RETRACTION GEAR SWING OPS CHECK. REMOVED AND REPLACED NOSE LANDING GEAR CHARGING VALVE IAW CMM 32-21-10. SERVICED NOSE LANDING GEAR IAW MM 32-20-01. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — FAILED (NR 1) · airframe 21,157 hrs · 18,400 cycles

ON FLIGHT 3131 THE CREW REPORTED THE NUMBER 1 ENGINE FAILED ON CLIMBOUT WITH A LOUD BANG. THE CREW RECEIVED E1 ENGINE EXCEEDANCE ON EICAS. THE CREW DECLARED AN EMERGENCY AND THE ENGINE WAS SHUT DOWN IN FLIGHT. THE CREW DID NOT ATTEMPT E1 ENGINE RESTART, AS THE EICAS DID NOT DISPLAY ANY USEABLE E1 ENGINE INDICATIONS. E2 ENGINE INDICATIONS DISPLAYED NORMALLY. THE CREW FOLLOWED ALL CHECKLIST. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE IAW W/C 71-000-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TIRE — PUNCTURED (MLG) · airframe 20,865 hrs · 18,040 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 3 MAIN TIRE HAS PUNCTURE OUT OF LIMITS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 MAIN TIRE IAW W/C 32-700-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 20,775 hrs · 17,934 cycles

ON FLIGHT 3053 THE FLIGHT ATTENDANT REPORTED SHE COULD SMELL GASOLINE LIKE FUMES FROM ROW 11 AND AFT OF ROW 11. THIS WAS CONFIRMED BY SEVERAL OTHER PASSENGERS. THIS HAPPENED ON APPROACH. APU WAS OFF. NO FUMES WERE PRESENT ON THE FLIGHT DECK. THE CREW REPORTED THEY COULD NOT SMELL ANYTHING ON POSTFLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED GENERAL VISUAL INSPECTION OF AFT CABIN AND AFT FUSELAGE SECTION AND FUEL DRAIN AREA. NO FUEL EVIDENCE IS FOUND. PERFORMED EMB 140 ETN # EM-72-034-R4, ENGINE ODOR EVENT TROUBLESHOOTING SUPPLEMENT AND NO GASOLINE OR FUME WAS DETECTED AT THIS TIME. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 20,628 hrs · 17,778 cycles

ON FLIGHT 3126 THE CREW FOUND FIRST OFFICER FLASHLIGHT INOPERABLE. DEFERRED F/O FLASHLIGHT PER MEL: 25-53. AUTH#021054-C MAINTENANCE ACTION C/W MEL OPEN. CORRECTIVE ACTION IS PENDING.

Part: SENSOR — INOPERATIVE (BRAKE SYSTEM) · airframe 17,885 hrs · 14,826 cycles

ON FLIGHT 2842 THE CREW REPORTED THAT AFTER TAKEOFF RECEIVED AN EICAS MESSAGE ABOUT THE BRAKE OVERHEAT INDICATION BEING AT THE TOP OF SCALE. THE CREW LOWERED THE LANDING GEAR IN ACCORDANCE WITH THE AIRCRAFT OPERATIONS MANUAL VOL 1. THE TEMPERATURE DECREASED SOME BUT REMAINED IN YELLOW. THE CAPTAIN ELECTED TO RETURN TO DFW, LANDING WITH NO USE OF THE BRAKE. THE TEMPERATURE INCREASED AGAIN TO TOP OF SCALE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BRAKE TEMPERATURE SENSOR NR 3 IAW AMM 32-47-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: COVER — BROKEN (COCKPIT) · airframe 17,463 hrs · 14,319 cycles

ON FLIGHT 3157 DURING TAXI THE CREW REPOPTED THE ESCAPE DOOR ROPE ON THE CAPTAINS SIDE HAS A BROKEN HINGE TAB. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ESCAPE ROPE DOOR ON CAPTAINS SIDE IAW EMB 140 AMM 25-60-07. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,989 hrs · 13,736 cycles

FOR FLIGHT 2712 MAINTENANCE FOUND THE EMERGENCY LIGHT STRIPS FROM ROW 3 TO ROW 8 TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY BATTERY AND CHARGER. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 16,676 hrs · 13,456 cycles

ON FLIGHT 3978 DURING CRUISE THE CAPTAIN REPORTED, NR 1 ENGINE STARTED LOSING OIL AFTER DEPARTURE. ELECTED TO DIVERT TO GRR DUE TO OIL LEVEL WENT FROM 9 QUARTS TO 3 QUARTS. IT WAS AN OVERWEIGHT LANDING BUT WAS WELL UNDER THE 360 FEET PER MINUTE SINK RATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE CORRECTIVE ACTION INFORMATION IS PENDING.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 15,897 hrs · 12,752 cycles

ON FLIGHT 4431 THE CREW REPORTED THAT WHILE LEVEL AT 31,000 FEET STARTED TO GET SMALL PRESSURIZATION BUMPS. BEGAN A PRECAUTIONARY DESCENT DURING WHICH CABIN RATE SWINGS BECAME MORE EXTREME. FOLLOWING AIRCRAFT OPERATING MANUAL PROCEDURES, SELECTED MANUAL MODE ON THE PRESSURIZATION CONTROL BUT THIS APPEARED TO HAVE NO EFFECT. THE CREW DESCENDED TO 10,000 FEET AND DUMPED CABIN PRESSURIZATION PER THE AIRCRAFT OPERATING MANUAL. THE AIRCRAFT LANDED WITH NO INCIDENT AT DESTINATION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED PNEUMATIC OUTFLOW VALVE IAW EMB-140 AMM 21-31-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (PAX DOOR)

PS-1 CHECK, PAX DOOR EMERGENCY LIGHT INOPERATIVE. RAR LIGHT ASSY. (K)

Part: INVERTER — INOPERATIVE (CABIN) · airframe 13,024 hrs · 10,216 cycles

FLIGHT 3852 - CREW REPORTED CABIN EMERGENCY LIGHTING FLOOR STRIP AT SEATS 1 AND 2 INOPERATIVE AT THE MOST FORWARD STRIP. CREW RESET AIRCRAFT POWER NO CHANGE. AIRCRAFT REMOVED FROM SERVICE. REMOVED & REPLACED NR 2 BATTERY POWER SUPPLY IAW EMB AMM 33-50-04, NO FIX. REMOVED & REPLACED NR 2 EMERGENCY LIGHT INVERTER IAW EMB AMM 33-50-11, EMERGENCY LIGHTS OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,542 hrs · 7,622 cycles

FLOOR SUPPORT CENTER HAT BEAM AT FRAME 20 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,542 hrs · 7,622 cycles

LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 24 AND 25. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,542 hrs · 7,622 cycles

PASSENGER DOOR THRESHOLD ATTACH ANGLE CORRODED. REMOVED AND REPLACED ATTACH ANGLE IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,542 hrs · 7,622 cycles

PASSENGER DOOR THRESHOLD ATTACH ANGLE CORRODED. REMOVED AND REPLACED ATTACH ANGLE IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,542 hrs · 7,622 cycles

LEFT OMEGA BEAM CORRODED AT FRAME 20. REPAIRED BEAM IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,542 hrs · 7,622 cycles

SERVICE DOOR CENTER SILL CORRODED. REMOVED AND REPLACED IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — DAMAGED (SERVICE DOOR)

THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED THE SILL TO REMOVED THE DAMAGE. APPLIED ALODINE, EPOXY PRIMER AND POLYURETHANE PAINT TO BLENDED AREA. FILLED THE BLENDED AREA WITH HYSOL 9394 RESIN AND CURED. FABRICATED TWO DOUBLERS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 30, CHAPTER 53-21-02 PARA 2. (M)

Part: FLOOR SUPPORT — CORRODED (FS 25)

THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE CENTER OMEGA BEAM TO REMOVED THE DAMAGE. FABRICATED A FILLER, EXTERNAL, ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 30, CHAPTER 53-00-10 FIG 203. (M)