N846AE

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 32,293 hrs · 28,230 cycles

MAIN CABIN DOOR VERY DIFFICULT TO OPEN. FA WAS UNABLE TO OPEN. FO OPENED DOOR-C/A-LUBRICATED MAIN CABIN DOOR ROLLERS IAW EMB 140 AMM 53-21-02-600-801-A STEP 2J3

Part: DOOR — BINDING (MAIN CABIN) · airframe 32,283 hrs · 28,223 cycles

MAIN CABIN DOOR VERY DIFFICULT FOR FA TO OPEN & CLOSE.-C/A-PERFORMED GVI OF DOOR AND SEALS. PERFORMED OPS CK OF OPEN & CLOSE FUNCTION OF DOOR IAW EMB 145MM 52-10-01. OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,509 hrs · 27,550 cycles

GALLEY OVERHEAD EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED GALLEY OVERHEAD EMERGENCY LIGHT LAMP IAW AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECK GOOD.

Part: BUTTON — DEFECTIVE (RAMP CALL) · airframe 31,381 hrs · 27,404 cycles

CABIN CHIME WOULD NOT STOP DINGING IN FLIGHT. COULD NOT HEAR ATC AND CREW COULD NOT ESTABLISH COMM BETWEEN THE TWO OF US. RETURNED BACK TO BTR AS A RESULT. C/A-FOUND PROBLEM TO BE THE FORWARD RAMP CALL PUSH BUTTON. REPLACED THE FORWARD RAMP CALL PUSH BUTTON IAW AMM 23-51-10, OPC GOOD. PASSENGER ADDRESS & CABIN INTERPHONE SYSTEM IAW AMM 23-31-00-700-801.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 31,264 hrs · 27,295 cycles

SECOND TO LAST EMERGENCY LIGHT FLOOR STRIP INOP. EVALUATED AND FOUND 4 EA DAMAGED WIRE CONNECTORS FOR LAST AND ALSO SECOND TO LAST EMERGENCY LIGHT FLOOR STRIP. RAI'D LAST TWO EMERGENCY LIGHT STRIPS IAW AMM 33-50-12 . REPAIRED 4 EA WIRE CONNECTORS IAW SWPM 20-21-00. MEL ITEM RESTORED. "M" PROCEDURES COMPLIED WITH.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 30,967 hrs · 27,023 cycles

LH FLOOR EDGE EMERGENCY LIGHTING STRIP BETWEEN FRAMES 25 - 27 HAS BROKEN WIRE.-C/A-INSTALLED NEW LH EMERGENCY LIGHTING STRIP IAW AMM 23-50-12. REF: NRWC 846-MQT-02241 FOR OPERATIONAL TEST.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 30,967 hrs · 27,023 cycles

CABIN FLOOR BOARD 231EF IS CRACKED IN HALF-C/A-REMOVED AND REPLACED 231EF IAW AMM TASK 53-01-02.

Part: CRADLE — INOPERATIVE (AFT FLASHLIGHT) · airframe 30,967 hrs · 27,023 cycles

FLASHLIGHT ON RH AFT STOWAGE CLOSET LED CHARGE LIGHT INOP.-C/A-REMOVED AND REPLACED FLASHLIGHT CHARGER ASSY IAW EMB-140 AMM 33-50-16. OPS CHECK GOOD.

Part: TERMINAL — DAMAGED (EMERGENCY LIGHT) · airframe 30,967 hrs · 27,023 cycles

EMERGENCY EXIT LIGHT STRIP WIRES UNDER 251GF HAVE BROKEN TERMINAL ENDS.-C/A-WIRE TERMINAL ENDS FOR THE EMERGENCY EXIT LIGHT STRIP UNDER 251GF WHERE REPAIRED IAW SWPM 20-21-00 AND OPERATIONAL CHECK OF THE LIGHT STRIP CHECK GOOD IAW AMM 33-50-00

Part: LIGHT — INOPERATIVE (ROW 11) · airframe 30,965 hrs · 27,022 cycles

EMERGENCY LIGHT STRIP ROW 11 INOP-C/A-DEFERRED EMERGENCY LIGHT STRIP ROW 11 REF: MEL 33-30 AUTH: 040506-C. BROKEN OFF WIRE TERMINAL ENDS UNDER FLOOR PANEL 251GF WHERE FOUND AND REPAIRED IAW SPWM 20-21-00 AND C/W OPERATIONAL CHECK OF THE EMERGENCY LIGHT STRIP FOR ROW 11 AND 12 AND CHECKED GOOD IAW AMM 33-50-00

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 30,965 hrs · 27,022 cycles

EMERGENCY LIGHT STRIP INOP ON ROW 11 AND 12-C/A-BROKEN OFF WIRE TERMINAL ENDS UNDER FLOOR PANEL 251GF WHERE FOUND AND REPAIRED IAW SPWM 20-21-00 AND C/W OPERATIONAL CHECK OF THE EMERGENCY LIGHT STRIP FOR ROW 11 AND 12 AND CHECKED GOOD IAW AMM 33-50-00

Part: LIGHT — INOPERATIVE (ROW 11) · airframe 30,965 hrs · 27,022 cycles

EMERGENCY LIGHT STRIP ROW 11 INOP. DEFERRED EMERGENCY LIGHT STRIP ROW 11 REF: MEL 33-30 AUTH: 040506-C

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 30,745 hrs · 26,800 cycles

MAIN CABIN DOOR IS HARD TO OPEN. C/A-LUBRICATED MAIN CABIN DOOR ROLLERS AND GUIDES AS PER AMM 52-10-00,OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 30,683 hrs · 26,729 cycles

MAIN CABIN DOOR DIFFICULT TO OPERATE OPEN AND CLOSE-C/A-LUBED FRAME ROLLERS AND RESECURED STOPS,PERFORMED MAIN DOOR OPEN/CLOSE IAW AMM 52-18-00, OPC GOOD

Part: WHEEL — OUT OF LIMITS (NR 4) · airframe 30,120 hrs · 26,214 cycles

UPON PS-1 CHECK FOUND # 4 TIRE WORN OUT OF LIMIT-C/A-REMOVED AND REPLACED # 4 TIRE IAW ENVOY MAIN LANDING GEAR WHEEL ASSY REMOVAL AND INSTALLATION W/C 37-700-11. NO FURTHER DEFECTS NOTED.

Part: ELECTRONIC UNIT — FAILED (LANDING GEAR) · airframe 29,874 hrs · 25,981 cycles

LG FAILED TO RETRACT AFTER TAKEOFF. ENGINE WOULD NOT GO TO CLB OR CRZ MODE.WERE IN ALT T/O-1 FOR @ 15 MIN. GUST LOCK WONT LOCK -C/A-T/S LG FAIL TO RETRACT PER FIM TASK EMB 140 32-63-00-810-804-A CHECK MLG PROXIMITY SWITCHES NO DEFECTS NOTED FOUND LGEU TO BE AT FAULT. REMOVED AND REPLACED LGEU IAW AMM 32-32-01 PERFORMED GEAR SWING IAW AMM 32-30-00 OPC GOOD A/C OK FOR SERVICE. C/W GUST LOCK OPS CHECK IAW AMM 27-71-12. OPS CHECK GOOD. A/C OK FOR SERVICE

Part: ADC — FAILED (LEFT) · airframe 29,713 hrs · 25,837 cycles

RED X ON AIRSPEED- ALT- AND VERTICAL SPEED DURING BEGINING OF APPROACH. BROKE OFF APPROACH AND DIVERTED TO ABI- VFR CONDITIONS. RED X'S OCCURED ON MULTIPLE OCCASIONS DURING FLIGHT CA SIDE ONLY. REMOVED AND REPLACED ADC 1 IAW AMM 34-15-01 LEAK CHECK GOOD OPS CHECK GOOD.

Part: DOOR — LACK OF LUBE (PAX) · airframe 29,622 hrs · 25,750 cycles

FA REPORTS MAIN CABIN DOOR RED LEVEL IS VERY HARD TO MOVE OPEN AND CLOSE.-C/A-AT THIS TIME LUBE MAIN CABIN DOOR HANDLE PER STANDAR PRACTICE. OPS CK GOOD PER AMM 52-18-00

Part: CONTROL VALVE — FAILED (BRAKES) · airframe 28,769 hrs · 24,946 cycles

BRAKE DEGRADED MESSAGE PRESENTED ON EICAS IN FLIGHT AND ON THE GROUND AFTER LANDING. LT INBD FAILED PRESSURE TEST AND SHOWS EXCESSIVE PRESSURE, WITHOUT BRAKES APPLIED, NO CMC MESSAGE. REMOVED AND REPLACED THE INBD BRAKE CONTROL VALVE IAW AMM 32-41-06, 20-10-03, LEAK CHECKED GOOD, OPS CHECKED GOOD WITH BRAKE ANALYZER.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 28,456 hrs · 24,556 cycles

NR 5 FLOOR EMERGENCY LIGHT INOPERATIVE. R & R THE CONNECTOR IAW SWPM 20-50-01. OPS CHECKED GOOD.

Part: CONTROL UNIT — FAILED (HORIZONTAL STAB) · airframe 28,453 hrs · 24,552 cycles

PITCH TRIM BACKUP INOPERATIVE, WHEN AUTO PILOT ENGAED. PERFORMED TROUBLESHOOTING IAW FIM. R & R THE HORIZONTAL STABILIZER CONTROL UNIT IAW AMM 27-43-02. OPS CHECKED GOOD.

Part: ATTACH FITTING — GOUGED (LT AILERON) · airframe 28,439 hrs · 24,528 cycles

LEFT AILERON DAMPER ATTACH FITTING HINGE IS GOUGED. REMOVED AND REPLACED THE ATTACH FITTING IAW EO EM-27MR-112.

Part: ATTACH FITTING — GOUGED (RT AILERON) · airframe 28,439 hrs · 24,528 cycles

RIGHT AILERON DAMPER ATTACH FITTING HINGE IS GOUGED. REMOVED AND REPLACED THE AILERON DAMPER ATTACH FITTING IAW EO EM-27MR-112.

Part: SKIN — CRACKED (FRAME 75) · airframe 28,429 hrs · 24,513 cycles

RIGHT AFT FUSELAGE SKIN AT FRAME 75 CRACKED ABOVE STRINGER 2R. REPAIRED THE SKIN IAW SRM 53-31-01, FIG 219, SHEET 2.

Part: DOOR SILL — CORRODED (FRAME 66) · airframe 28,429 hrs · 24,513 cycles

CARGO DOOR LOWER SILL IS CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (FRAME 66) · airframe 28,429 hrs · 24,513 cycles

CARGO DOOR LOWER SILL IS CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02

Part: FRAME — CRACKED (FRM 23) · airframe 28,429 hrs · 24,513 cycles

FRAME 23 CRACKED AT STRINGER 16R. REPAIRED THE FRAME IAW SRM 53-00-04, ITEM 3.

Part: SHEAR TIE — CORRODED (FRAME 68) · airframe 28,429 hrs · 24,513 cycles

FRAME 68 SHEAR TIE IS CORRODED AT CARGO DOOR LOWER SILL AREA. REPAIRED THE SHEAR TIE IAW SRM 53-31-04

Part: SHEAR TIE — CORRODED (FR 65) · airframe 28,429 hrs · 24,513 cycles

FRAME 65 SHEAR TIE CORRODED AT THE CARGO DOOR LOWER SILL. REPAIRED THE SHEAR TIE IAW SRM 53-31-04.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,429 hrs · 24,513 cycles

ROW 11 CEILING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY EXIT SIGN IAW AMM 33-50-13. OPS CHECKED GOOD.

Part: SIDEWALL SUPPORT — CORRODED (FRAMES 49-50) · airframe 28,429 hrs · 24,513 cycles

LEFT OMEGA BEAM SIDEWALL IS CORRODED BETWEEN FRAMES 49-50. REPAIRED THE OMEGA BEAM SIDEWALL IAW ERS-EM-53MR-3067.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 28,429 hrs · 24,513 cycles

EMERGENCY LIGHT LOCATED AT THE AFT OF EMERGENCY EXIT ARE NOT FUNCTIONAL. REMOVED AND REPLACED THE NR 6 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 28,146 hrs · 24,275 cycles

MAIN CABIN DOOR VERY HARD TO OPEN. PERFORMED MAIN DOOR INTERNAL ACTUATING HANDLE TEST IAW AMM 52-10-01. LUBRICATED MAIN DOOR ROLLERS. LOAD FALLS WITHIN ALLOWABLE LIMITS. OPERATIONS CHECKED GOOD.

Part: BRACKET — CRACKED (RT WING) · airframe 28,124 hrs · 24,262 cycles

BRACKET SUPPORTING RT WING REFUEL TUBE INSIDE ACCESS PANEL 631AB IS CRACKED AT NUT PLATE FOR CLAMP. REPAIRED BRACKET IAW ETN 51-150, INSTALLED IAW SRM 51-40-09. OK FOR SERVICE.

Part: DOOR — OBSTRUCTED (MAIN PAX) · airframe 28,066 hrs · 24,214 cycles

FLIGHT ATTENDANT REPORTED THAT MAIN DOOR IS VERY HARD TO OPEN & CLOSE. FOUND COURTAIN STRAP GETTING BETWEEN PAX DOOR AND DOOR STOP. REPOSITIONED STRAP AND COMPLIED WITH EM -52-029. OPS CHECKED GOOD IAW AMM 52- 18-00.

Part: NUT PLATE — BROKEN (EMERGENCY LIGHT) · airframe 28,042 hrs · 24,191 cycles

LEFT FWD EMER LIGHT HOUSING HAS BROKEN NUTPLATE. R & R LT FWD EMER LIGHT HOUSING IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 28,042 hrs · 24,191 cycles

LEFT FWD EXTERIOR EMER LIGHT INOPERATIVE. R & R FUSE IN NR 1 EMER LIGHT BATTERY CHARGER IAW CMM 25-60-03. OPERATIONS CHECKED IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 28,005 hrs · 24,157 cycles

FLOOR PROXIMITY STRIP POWERED BY NR 3 EMER BATTERY COMES ON & GOES OFF AFTER FEW SECONDS. R & R NR 3 POWER SUPPLY & BATTERY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. EMER LIGHTING BATTERY PN 2013-1A, SN 103959.

Part: VALVE — FAILED (BLEED AIR SYS) · airframe 27,500 hrs · 23,711 cycles

BLEED 2 OVERTEMP CAME ON FOR 2 OR 3 SECONDS THEN WENT OFF. BLEED 2 TEMP WAS IN RED BELOW 10,000 FT MAX CLIMB THRUST. R & R RT FAN AIR VLV IAW AMM 36-11-03. OPERATIONS CHECK FAIL SEE ITEM NR 2 ON THIS LG PAG FOR CORRECTIVE ACTION.

Part: SWITCH — FAULTY (COCKPIT) · airframe 27,499 hrs · 23,710 cycles

E2 ANTI-ICE FAIL MSG, NR 2 BLEED TEMP IN THE RED, E2 ANTI-ICE VLV OPEN INDICATION, AFTER FEW MINUTES EICAS MSG & OPEN INDICATION EXTINGUISHED. HOWEVER BLEED TEMP STILL REMAINED IN TOP OF GREEN, NEVER IN ICING. R & R WITH SERVICEABLE E2 AIR INLET OVERHEAD PANEL PTB SWITCH IAW AMM 20-13 -04.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 27,248 hrs · 23,473 cycles

FLIGHTDECK FLASHLIGHT ON & OFF SWITCH BROKE OFF. DEFERRED CAPTAIN`S FLASHLIGHT IAW MEL 25-53 AUTH 030374-C. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16, CHECKED GOOD & MEL ITEM RESTORED.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 27,190 hrs · 23,417 cycles

MAIN CABIN DOOR HARD TO OPEN. CLEANED & LUBED MAIN CABIN DOOR ROLLER PINS IAW AMM 53-21-02, OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,263 hrs · 22,617 cycles

FWD CEILING EMERGENCY EXIT SIGN INOPERATIVE. R & R NR 1 INVERTER, OPS CHECKED GOOD IAW AMM 33-50-11.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,263 hrs · 22,617 cycles

FWD EMERGENCY EXIT SIGN BELOW COCKPIT DOOR INOPERATIVE. R & R NR 1 EMERG POWER INVERTER IAW AMM 33-50-11, OPC GOOD.

Part: ROLLER — LACK OF LUBE (MAIN DOOR) · airframe 25,815 hrs · 22,207 cycles

F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN. LUBED MAIN DOOR FRAME ROLLERS IAW 52-21-02.

Part: CHECK VALVE — INOPERATIVE (BLEED SYS) · airframe 25,665 hrs · 22,068 cycles

THE CREW REPORTED A BLEED TWO LEAK INDICATION AFTER TAKEOFF AT 900 FT AGL. THE CREW PERFORMED EMERGENCY PROCEDURES. BLEED 2 LEAK INDICATION EXTINGUISHED AFTER APPROX. 30 SEC. BURNED OFF FUEL BEFORE LANDING. NO OVERWEIGHT LANDING. THE ACFT WAS REMOVED FROM SERVICE. R & R THE FAN AIR VALVE THERMOSTAT, PN: 8166248, SN: 200105088 AND LEAKING GROUND BLEED AIR CONNECTION VALVE IAW AMM 36-10-02, AND 36-11-06. THE OPS CHECK WAS GOOD IAW AMM 36-00-00. THE ACFT WAS RETURNED TO SERVICE.

Part: ECU — FAILED (TE FLAPS) · airframe 25,396 hrs · 21,811 cycles

DURING CRUISE, RECEIVED AN EICAS FLAP LOW SPEED AND SPS ADVANCED MESSAGES. COMPLIED WITH AOM, VOL 1 PROCEDURES. ON APPROACH EICAS FLAP FAIL MESSAGE RECEIVED. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02. OPS CHECK FOUND WORKING PROPERLY IAW 27-53-00-700-802-A. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (PAX DOOR) · airframe 25,149 hrs · 21,617 cycles

DURING B INSPECTION FOUND THE PASSENGER DOOR EMERGENCY LIGHT ON PIVOT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED LENS, REMOVED LIGHT BULB, ROTATED BULB 180 DEGREES AND RE-INSTALLED BULB AND REINSTALLED LENS. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — MALFUNCTIONED (PAX DOOR) · airframe 25,012 hrs · 21,486 cycles

FLIGHT 3370. MAIN CABIN DOOR WAS DIFFICULT TO OPEN & CLOSE. REMOVED MAIN DOOR HANDLE, RETORQUED PIVOT BUSHING BOLT IAW AMM 20-10-01. RETORQUED BOLTS ON INNER HANDLE BOX ASSEMBLY IAW AMM 20-10-01. COMPLIED WITH PROC ETN EM 52-037 SUPPORT BRACKET NO DEFECTS. STEP CHECKED, ROLLER CHECKED & HANDLE LOAD CHECKED GOOD IAW AMM 52-18-00 PULL TEST 29 OPEN 27 CLOSE TDMI 846520829 RESTORED. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,597 hrs · 21,097 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLASHLIGHT AT THE FLIGHT ATTENDANT SEAT POSITION INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT AT THE FLIGHT ATTENDANT SEAT POSITION IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (ENTRY DOOR) · airframe 24,549 hrs · 21,055 cycles

ON FLIGHT 4158 THE FLIGHT ATTENDANT REPORTED THE FORWARD ENTRY DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATE MAIN DOOR FRAME ROLLERS IAW EMB-140 M/M 53-21-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 24,536 hrs · 21,045 cycles

ON FLIGHT 4187 THE CREW REPORTED THE COCKPIT BULKHEAD FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINS EMERGENCY FLASHLIGHT IAW EMB-140 A 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FASTENER — LOOSE (FLASHLIGHT) · airframe 24,416 hrs · 20,935 cycles

ON FLIGHT 4404 THE CREW REPORTED THE FLIGHT ATTENDANT’S FLASHLIGHT HOLDER WAS LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TIGHTENED LOOSE HARDWARE IAW AMM 33-50-16 ON FLIGHT ATTENDANT’S FLASHLIGHT CRADLE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 24,025 hrs · 20,587 cycles

ON FLIGHT 4121 THE FLIGHT ATTENDANT REPORTED THE CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED LUBRICATION OF DOOR IAW EMB-140 AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD, NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,015 hrs · 20,578 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,735 hrs · 20,358 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT IN CEILING FORWARD INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB IN CABIN FORWARD IAW EMB 140 AMM 23-22-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,735 hrs · 20,357 cycles

CENTER OMEGA BEAM IS CORRODED BETWEEN FRAMES 57-59. REPAIRED CENTER OMEGA BEAM IAW AE EOEM-53MR-1518.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,735 hrs · 20,357 cycles

LEFT OMEGA BEAM IS CORRODED BETWEEN FRAMES 57-59. REPAIRED OMEGA BEAM IAW AE EO EM-53MR-1518.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 23,743 hrs · 20,368 cycles

DURING B INSPECTION FOUND THE RIGHT BEAM GUSSET CORRODED BETWEEN FRAMES 59-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT BEAM GUSSET BETWEEN FRAMES 59-61 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 23,743 hrs · 20,368 cycles

DURING B INSPECTION FOUND THE CENTER BEAM GUSSET CORRODED BETWEEN FRAMES 59-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CENTER BEAM GUSSET BETWEEN FRAMES 59-61. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 23,743 hrs · 20,367 cycles

DURING B INSPECTION FOUND THE LEFT BEAM GUSSET CORRODED BETWEEN FRAMES 60-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT BEAM GUSSET BETWEEN FRAMES 60-61 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (FLASHLIGHT) · airframe 23,275 hrs · 19,953 cycles

DURING MAINTENANCE INSPECTION, FOUND THE BATTERY CONNECTOR BROKEN ON THE FLIGHT ATTENDANT’S EMERGENCY FLASHLIGHT BATTERY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT THE FLIGHT ATTENDANT’S EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (FLASHLIGHT) · airframe 23,275 hrs · 19,953 cycles

DURING MAINTENANCE INSPECTION, FOUND BATTERY CONNECTOR BROKEN ON THE FIRST OFFICER’S EMERGENCY FLASHLIGHT BATTERY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — FAILED (WOW) · airframe 23,194 hrs · 19,899 cycles

FLIGHT 2766, CREW REPORTED THAT AT ROTATION THEY RECEIVED A LANDING GEAR AIR/GND/FAIL MESSAGE ON EICAS. DID NOT ATTEMPT TO RETRACT GEAR AS THEY CONTINUED THE CLIMB-OUT. FOLLOWED THE AOM VOL 1 PROCEDURES. LANDING GEAR INDICATORS REMAINED GREEN DURING ENTIRE FLIGHT. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICEABLE NOSE LANDING GEAR WEIGHT ON WHEELS SWITCH IAW AMM 32-63-01 & AMM 32-63-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 23,025 hrs · 19,738 cycles

DURING B INSPECTION FOUND THE READING LIGHT ASSEMBLY ABOVE SEAT 11A IS EMITTING A BURNING ODOR AS SMOKE IS VISIBLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LIGHT BULB REMOVED. ENTIRE LIGHT ASSY NEEDS REPLACEMENT. PARTS NOT AVAILABLE. DEFERRED AS NEF 25-21C. ENTERED ON MIC SHEET. REMOVED AND REPLACED THE PSU READING LIGHT 11A IAW EMB AMM TASK 33-25-02-000-801/33-25-02-400-801. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETUTNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (SPOILER) · airframe 23,005 hrs · 19,719 cycles

ON FLIGHT 4228 THE CREW REPORTED THAT WHILE IN FLIGHT WHEN THE SPEED BRAKE LEVER WAS SELECT TO OPEN THE CREW RECEIVED A SPOILER FAIL MESSAGE ON THE EICAS AND THE SPLRS INDICATION INDICATED CLOSED ON THE EICAS. THE CREW DECLARED AN EMERGENCY AND RETURNED TO ORD. THE AIRCRAFT WAS REMOVED FROM SERVICE. WHILE TROUBLESHOOTING FOUND SPBK LEVER SW/RELAY FAIL FLAGGED ON CMC. REMOVED AND REPLACED SPOILER CONTROL UNIT IAW EMB-AMM 27-63-02. THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 AMM 27-63-01. NO OTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 22,235 hrs · 18,889 cycles

FLIGHT 3058, THE CREW REPORTED THE CAPTAIN`S FLASHLIGHT NOT WORKING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAIN`S FLASHLIGHT ASSY IAW AMM 33-50-16 AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INDICATION SYS — DEFECTIVE (FUEL SYSTEM) · airframe 19,606 hrs · 16,006 cycles

ON FLIGHT 3045 THE CREW REPORTED THE NR 1 FUEL QUANTITY INDICATION ON EICAS AS UNREADABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT HAND NR 4 TANK UNIT IAW EMB140 AMM 28-41-2. THE OPERATIONAL CHECK WAS GOOD IAW EMB140 AMM 28-41-00, AND THE LEAK CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRIM SYSTEM — MALFUNCTIONED (HORIZ STAB) · airframe 19,154 hrs · 15,552 cycles

ON FLIGHT 4508 THE CAPTAIN ACTIVATED THE PITCH TRIM ON SHORT FINAL AND RECEIVED MASTER A WARNING MICAS "PTRIM MAIN INOP". BOTH CAPTAIN’S AND FIRST OFFICER’S TRIM INOPERATIVE BUT BACKUP SYSTEM WORKED PROPERLY. THE CAPTAIN DECLARED AND EMERGENCY. THE AIRCRAFT LANDED SAFELY AT THE DESTINATION. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET SYSTEM. THE OPERATIONAL CHECK WAS GOOD PER AMM 27-40-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — LACK OF LUBE (CABIN DOOR) · airframe 18,505 hrs · 15,032 cycles

ON FLIGHT 4307 THE CREW REPORTED THAT THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE FIRST OFFICER HAD TO ASSIST THE FLIGHT ATTENDANT TO OPEN AND CLOSE THE DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-ADJUSTED THE MAIN DOOR STOPS IAW EMB 140 AMM 52-18-00. LUBRICATED MAIN DOOR SEAL AND MAIN DOOR ROLLERS IAW AMM 20-30-02 AND ADJUSTED PASSENGER DOOR IAW AMM 52-18-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL AND TENSION CHECK WAS GOOD AND WITHIN TENSION LIMITS. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 18,144 hrs · 14,744 cycles

ON FLIGHT 4340 DURING TAXI THE CREW REPORTED NOTICING ELECTRICAL FUME ODORS IN GALLEY ROW AREA. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BALLASTS (BOTH) IN GALLEY IAW EMB-140 CMM 25-28-24. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 18,137 hrs · 14,735 cycles

FOR FLIGHT 4053 UPON ENTERING THE AIRCRAFT THE FLIGHT CREW REPORTED, SMELLED A STRONG ELECTRICAL ODOR AROUND ROW 3. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT SIDEWALL 3BC BALLAST IAW EMB 140 AMM 33-21-04. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRIM SYSTEM — MALFUNCTIONED (HORIZ STAB)

ON FLIGHT 4394 THE CREW DETERMINED THE MAIN PITCH TRIM WAS INOPERABLE. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. CHECKED HORIZONTAL STABILIZER AND PITCH TRIM SYSTEM PER FIM IAW EMB 140 AMM 27-40-00. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 17,878 hrs · 14,522 cycles

FLIGHT 3445 THE CREW REPORTED THE CABIN MAIN DOOR SENSOR KEPT GIVING A MAIN DOOR OPEN WARNING ON THE GROUND. THE FLIGHT ATTENDANT HAD TO OPEN AND CLOSE THE DOOR TO RESET IT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-ADJUSTED SWITCH ON THE MAIN CABIN DOOR IAW EMB 52-73-01. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 17,871 hrs · 14,514 cycles

ON FLIGHT 2865 THE CREW REPORTED THAT THE MAIN CABIN DOOR REQUIRES EXCESSIVE FORCE TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED THE MAIN CABIN DOOR LOCKING MECHANISM, THE OPERATIONAL CHECK WAS GOOD IAW AMM 52-18-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROFILE — BENT (FUSELAGE) · airframe 16,750 hrs · 13,563 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE FORWARD FUSELAGE 1 BULKHEAD PROFILE AT STRINGER 4L DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FUSELAGE 1 BULKHEAD PROFILE AT STRINGER 4L IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 16,750 hrs · 13,563 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE SKIN SPLICE PLATE AT FRAME 6 AND STRINGER 11L MISS DRILLED DURING TEMPORARY REPAIR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SKIN SPLICE PART NUMBER 120-27430-003 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROFILE — BENT (FUSELAGE) · airframe 16,750 hrs · 13,563 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE FORWARD FUSELAGE 1 BULKHEAD PROFILE AT STRINGER 9L BENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FUSELAGE 1 BULKHEAD PROFILE AT STRINGER 9L IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 16,750 hrs · 13,563 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE SKIN SPLICE PLATE PART NUMBER 123-10953-001 DAMAGED FROM A BIRD STRIKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SKIN SPLICE PLATE PART NUMBER 123-10953-001 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 16,750 hrs · 13,563 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND STRUCTURAL DAMAGE FROM A BIRD STRIKE BELOW THE CAPTAIN’S WINDSHIELD AND FORWARD TO RADOME. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH AMERICAN EAGLE AIRLINES EO EM-53MR-1414, WORK ORDER 36849. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — BURNED (LAVATORY)

ON FLIGHT 4354 CREW REPORTED ON ARRIVAL THAT THE FLIGHT ATTENDANT SMELLED SMOKE COMING FROM LAV AREA NEAR THE ELT. CREW CONFIRMED SMELL BUT NO VISIBLE SMOKE. ACFT REMOVED FROM SERVICE. C/A FOUND FLUORESCENT BULB ABOVE TOILET WITH BURNT SOCKET. REMOVED BULB. DEFER LAVATORY PER MEL 38-03 AUTH 090830DM-C. C/A R&R LIGHT HARNESS ASSEMBLY. OPS CHECK GOOD. IAW EMB AMM. MEL ITEM RESTORED. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 11,476 hrs · 9,178 cycles

EMERGENCY LIGHTS NO TEST. REMOVED AND REPLACED ALL FOUR BATTEY PACKS IAW EMB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: ENGINE — LEAKING (NR 2) · airframe 10,652 hrs · 8,633 cycles

RECEIVED LAVATORY SMOKE INDICATION ON CLIMB-OUT, NO VISUAL INDICATION OF SMOKE, FAINT SMELL NOTED. REMOVED AND REPLACED NUMBER TWO ENGINE IAW AMERICAN EAGLE WORKCARD 72-000-00. OPERATIONAL AND LEAK CHECK GOOD WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

CREW REPORTED CARGO SMOKE WARNING AT 31,000 FEET, DECLARED EMERGENCY, DISCHARGED FIRE BOTTLES, DIVERTED TO ALB. RAI BAGGAGE COMPARTMENT HIGH RATE AND LOW RATE FIRE BOTTLES, IAW EMB AMM 26-23-01, RAI FORWARD BAGGAGE SMOKE DETECTOR IAW EMB 140 AMM 26-15-01. RAI AFT BAGGAGE SMOKE DETECTOR IAW EMB 140AMM 26-15-01. RAI FIRE DETECT CONTROL MODULE IAW EMB AMM 26-00-01. ALL COMPONENTS OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: WARNING SYSTEM — ACTIVATED (CARGO BAY)

JAX - FLT 4497 - BAGGAGE SMOKE INDICATION IN FLIGHT. CREW DISCHARGED FIRE BOTTLES. REMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT FIRE EXTINGUISHER BOTTLES. PART NR FOR FIRE BOTTLE, IAW EMB140, AMM 26-23-01. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT)

FOUND EMERGENCY EXIT LIGHT STRIP AT EXIT ROW INOP. RESECURED CONNECTOR ON THE STRIP, OPS CHECKED GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 4,639 hrs · 4,148 cycles

DURING AN MBV INSPECTION THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW SRM. (SW21200502476) (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 4,639 hrs · 4,148 cycles

DURING AN INSPECTION OF AIRCRAFT THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED AN EXTERNAL ANGLE, FILLER PLATE AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200502476) (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 4,639 hrs · 4,148 cycles

DURING AN INSPECTION, THE LT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA TO REMOVE CORROSION. FABRICATED A FILLER, DOUBLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200502476) (K)

Part: FLASHLIGHT — ODOR (CABIN)

STRONG ELECTRICAL ODOR IN FORWARD CABIN. ODOR ISOLATED TO FLIGHT ATTENDANTS FORWARD FLASHLIGHT. REPLACED FLIGHT ATTENDANTS FORWARD FLASHLIGHT IAW EMB 145 MM 25-60-00, OPS CHECK GOOD. (M)