N827AE

Part: BEARING — LACK OF LUBE (PAX DOOR ROLLER) · airframe 37,720 hrs · 33,135 cycles

MAIN DOOR WONT CLOSE-C/A-LUBRICATED MAIN DOOR ROLLER BEARINGS IAW EMB 140 AMM 53-21-02. NO FURTHER DEFECTS NOTED AT THIS TIME. OPC OF DOORGOOD.

Part: BULB — NO TEST (EMERGENCY LIGHT) · airframe 37,100 hrs · 32,490 cycles

DURING PS-1 CHECK FOUND RH FOREWARD EXTERNAL LIGHT INOPERATIVE. R & R THE BULB IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 36,761 hrs · 32,157 cycles

NR 3 EMERGENCY LIGHT FAIL OPC. REMOVED AND REPLACED BATTERY CHARGER IAW EMB 140 AMM 33-50-04, OP CK GOOD

Part: CONNECTOR — DISCONNECTED (FLASHLIGHT) · airframe 36,652 hrs · 32,061 cycles

MEL 2553 - AUTH# 05-564-C AFT FLASHLIGHT NOT CHARGING. C/A-T/S PER WM 33-51-50 FOUND HARNESS CONNECTION ON THE BACK OF FLASHLIGHT ASSY TO NOT BE CONNECTED, RECONNECTED HARNESS OPC GOOD NO DEFECTS NOTED AT THIS TIME MEL RESTORED END.

Part: WIRE HARNESS — DISCONNECTED (FLASHLIGHT) · airframe 36,620 hrs · 32,034 cycles

SUPPLEMENTAL AFT CABIN FLASHLIGHT IS NOT SHOWING A RED CHARGE LIGHT. C/A-DFFERD AFT CABIN FLASHLIGHT M PROCEDURES COMPLIED WITH. REMOVED AND REPLACED AFT CABIN FLASHLIGHT ASSY, OPC BAD IAW AMM 33-50-16. REAPPLIED INOP PLACARD PER MEL 2553 MEL ITEM REMAINS OPEN. T/S PER WM 33-51-50 FOUND HARNESS CONNECTION ON THE BACK OF FLASHLIGHT ASSY TO NOT BE CONNECTED, RECONNECTED HARNESS OPC GOOD NO DEFECTS NOTED AT THIS TIME MEL RESTORED END.

Part: FLASHLIGHT ASSY — BROKEN (FWD CABIN) · airframe 35,615 hrs · 31,072 cycles

FWD FA FLASHLIGHT HOLDER BROKEN-C/A-CREW PLACARDED FWD FA FLASHLIGHT HOLDER MEL 25-53 AUTH# 110865 MOC # 730088. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY AS PER AMM 35-50-16. OPS GOOD. NO FUTER DEFECTS NOTED. MEL RESTORED

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 35,408 hrs · 30,902 cycles

FO PFD BLACKED OUT AND WE SMELL BURNING PLASTIC. DEFERRED FO PFD M PROCEDURES ACCOMPLISHED SWAP FO PFD WITH MFD PER MEL MEL 3401 AUTH 100745DM-B. SWAPPED FO PFD TO ITS ORIGINAL POSITION. REMOVED FO MFD IAW AMM 34-22-01. INSTALLED NEW FO PFD IAW AMM 34-22-01. OPS CHECK GOOD IAW AMM 34-22-00. MEL 34-01 RESTORED. MOC 147032

Part: SELECTOR — MALFUNCTIONED (COCKPIT) · airframe 35,292 hrs · 30,797 cycles

SPEED SELECTOR COURSE SEL ALTITUDE SELECTOR KNOBS INTERMITTENTLY INOP. UNABLE TO DUPLICATE OPS CHECK IAW AMM 22-11-00 REMOVED AND REPLACED FGC FOR PRECAUTIONARY REASONS IAW AMM 22-11-01 OPS CHECK IAW AMM 22-11-00 MEL RESTORED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,114 hrs · 30,587 cycles

MAIN CABIN DOOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED MAIN CABIN DOOR EXTERNAL EMERGENCY LIGHT COVER IAW EMB 140 AMM 25-23-04. LIGHT OPERATIONAL CHECK GOOD.

Part: CONTROLLER — UNKNOWN (AUTOPILOT SYS) · airframe 34,656 hrs · 30,184 cycles

FLIGHT GUIDANCE CONTROLLER WAS UNRESPONSIVE IN FLIGHT. PERFROMED A FUNCTIONAL TEST OF AUTOPILOT IAW AMM 22-11-00. FNT PASSED NO FAULT FOUND.

Part: UNKNOWN — UNKNOWN (COCKPIT) · airframe 34,085 hrs · 29,571 cycles

DURING CLIMBOUT, A LOUD CRACKELING SOUND WAS HEARD IN THE FLIGHT DECK. SOUNDED LIKE FROM EXTERIOR, LASTED APPROXIMATELY 5 MINUTES. PERFORMED GVI INSPECTION OF AIRCRAFT ACCESS PANEL, MLG DOORS, HUMP SEALS, WIPERS, BONDING JUMPER, STATIC WICKS FLIGHT DECK PANELS AND NO DEFECTS NOTED IAW SRM 51-10-02. AIRCRAFT OK FOR SERVICE.

Part: LIGHT — OVERHEATED (COCKPIT) · airframe 33,912 hrs · 29,333 cycles

ELECTRICAL BURNING ODOR IN THE COCKPIT. FOUND THE CAPTAIN`S READING LIGHT WITH SIGNS OF OVERHEATING. REMOVED AND REPLACED THE READING LIGHT IAW AMM 33-11-04.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 33,893 hrs · 29,305 cycles

EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. NO DISCREPANCY NOTED

Part: SKIN — CRACKED (FR 75) · airframe 33,893 hrs · 29,305 cycles

RIGHT AFT FUSELAGE SKIN, FR 75 CRACKED ABOVE STRINGER 2. REPAIRED IAW SRM 53-31-01, AND SRM 51-40-02

Part: SKIN — CRACKED (FRAME 75) · airframe 33,893 hrs · 29,305 cycles

LEFT AFT FUSELAGE SKIN, FR 75 CRACKED ABOVE STRINGER 2. REPAIRED IAW SRM 53-31-01, AND SRM 51-40-02.

Part: CONNECTOR — MISSING (EMERGENCY LIGHT) · airframe 33,893 hrs · 29,305 cycles

NR 1 EMERGENCY LIGHT STRIP CONNECTOR MISSING. FOUND ON CLOSE UP. INSTALLED A CONNECTOR AND PIN IAW SWPM 20-21-00.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 33,893 hrs · 29,305 cycles

CARGO DOOR SILL IS CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02, AND 51-20-03.

Part: STRINGER — CRACKED (FRAME 13) · airframe 33,893 hrs · 29,305 cycles

STRINGER 6R IS CRACKED AT FRAME 13. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-02, AND 51-20-03

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 33,893 hrs · 29,305 cycles

SERVICE DOOR CENTER SILL IS CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (FRAMES 22-23) · airframe 33,893 hrs · 29,305 cycles

LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 22 - 23. REPAIRED IAW SRM 53-21-10

Part: SKIN — CHAFED (RUDDER) · airframe 33,893 hrs · 29,305 cycles

RUDDER SKIN CHAFED ABOVE PANEL 326EL. REPAIRED IAW ERS-EM-55MR-618.

Part: SKIN — CHAFED (RUDDER) · airframe 33,893 hrs · 29,305 cycles

RUDDER SKIN CHAFED ABOVE PANEL 326AL. REPAIRED IAW ERS-EM-55MR-618.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 33,893 hrs · 29,305 cycles

FRAME 65 SHEAR TIE CORRODED, STRINGERS 17 - 18L . REPAIRED SHEAR TIE IAW ERS-EM-53DF-414 PT-B.

Part: BEARING CAP — CORRODED (LT MLG) · airframe 33,893 hrs · 29,305 cycles

LT MLG AFT LOWER BEARING CAP CORRODED. REMOVED AND REPLACED THE BEARING CAP IAW AMM 32-10-01, STEPS 2.J.(3-7) AND 3.J.(11-16).

Part: FLASHLIGHT — FAILED (AFT CABIN) · airframe 33,590 hrs · 29,040 cycles

FA REPORTED AFT FA FLASHLIGHT FLICKERS. REMOVED AND REPLACED AFT FA FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: AMPLIFIER — FAILED (PA SYSTEM) · airframe 33,579 hrs · 29,028 cycles

IN FLIGHT, COULD NOT CHIME OR CALL FLIGHT ATTENDANT. COULD NOT MAKE PA'S. NO LIGHTS ON THE ICU PANE WORKED. HARD WIRED TO F/A HANDSET AT ALL TIMES. REMOVED AND REPLACED PA-AMP IAW AMM 23-31-01 OPS CHECK GOOD

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 32,367 hrs · 27,727 cycles

FLASHLIGHT BEHIND CAPTAINS SEAT IS NOT WORKING. R & R LAMP BULB IN FLASHLIGHT IAW STANDARD PRACTICES OPERATION CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 31,957 hrs · 27,292 cycles

DURING PS 2, FOUND OVERHEAD EMER EXIT LIGHT ROW 11, HANGING DOWN & INOPERATIVE. RE-CONNECTED PLUG IN CEILING & SECURED LIGHT IAW SP. OPERATIONS CHECKED GOOD.

Part: AOA — FAILED (RIGHT) · airframe 31,892 hrs · 27,222 cycles

HIGH SPEED ABORT AT ABOUT 100 KTS SPS 1 - 2 INOPERATIVE. SPS ADVANCE CAUTION MESSAGE. REPLACED RT AOA IAW MM 27-36-01. REPLACED SPC IAW MM 27-36-02. OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 31,587 hrs · 26,907 cycles

SPS 2 INOPERATIVE WARNING & SPS ADV MSG ON EICAS, DURING TAKEOFF ROLL OF APPROX 100 KTS. ABORTED THE TAKEOFF, MSGS DISAPPEARED. TROUBLE SHOT BY FIM 27-36-00. PERFORMED OPERATIONS CHECK IAW AMM 27-36-00. OPERATIONS CHECKED GOOD. DETERMINED TO BE TRANSITORY CONDITION. ACFT OK FOR SERVICE.

Part: LIGHT — UNSECURE (CABIN) · airframe 31,566 hrs · 26,888 cycles

EMERGENCY EXIT LIGHT IN AISLE IS DANGLING. SECURED ELECTRO-LUMINESCENT LAMP IAW MM 33-50-15-710. OPERATIONS CHECKED GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 31,566 hrs · 26,888 cycles

EMERGENCY EXIT LIGHT IN AISLE FOR WING EXIT NOT LIGHTING UP & ALSO DANGLING. SECURED AISLE EMER LIGHT ELECTRO-LUMINESCENT LAMP. OPERATIONS CHECKED GOOD IAW MM 33-50-08.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,197 hrs · 26,551 cycles

CABIN FLOOR EMER LIGHT AT ROW 8 & 9 INOPERATIVE. REPLACED CABIN FLOOR EMER LIGHT ASSEMBLY IAW AMM 33-50-12. OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,995 hrs · 26,373 cycles

DURING PS 1 INSPECTION FOUND LT AFT EXTERIOR EMER LIGHT INOPERATIVE. R & R LT AFT EXTERIOR EMER LAMP IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: CLAMP — FAILED (BLEED DUCT) · airframe 30,429 hrs · 25,921 cycles

NR 2 BLEED LEAK CLIMBING OUT OF FL 20,000. FOUND AIR CONDITIONING DUCT BLOWN OFF. REPLACED CLAMP AT HEAT EXCHANGER IAW AMM 21-51-025. LEAK CHECKED GOOD.

Part: PROXIMITY SWITCH — OUT OF POSITION (NLG) · airframe 30,372 hrs · 25,885 cycles

AFTER LIFTOFF RECEIVED A LG AIR GND FAIL CAUTION. LG WOULD NOT RETRACT. RAM AOM 1 CHECKLIST. RETURNED, LANDING WAS NORMAL. LG AIR GND FAIL CAUTION EXTINGUISHED AFTER LANDING. DESCENT RATE ON LANDING WAS 100 FPM. FOUND NOSE WHEEL PROXIMITY SWITCH OFF NORMAL POSITION IAW AMM 32-63-02. FNC GOOD AFTER REPOSITIONING, FNC GOOD IAW ETN-EM-32-245.

Part: ANTI-ICE VALVE — FAILED (NR 2 ENGINE) · airframe 30,296 hrs · 25,820 cycles

E2 A/ICE FAIL MESSAGE-C/A-REMOVED AND REPLACED ENG ANTI-ICE VALVE IAW AMM 30-21-01. OPS CHECK FAIL.REMOVED AND REPLACED ENG #2 ANTI-ICE PRESSURE TRANSDUCER IAW AMM 30-21-06. OPS CHECK TEST GOOD. P/N APS51500 S/N 71115267

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 30,262 hrs · 25,788 cycles

SEATS 3B,C FWD BULKHEAD EMER LIGHT SIGN WILL NOT ILLUMINATE. TROUBLE SHOT & FOUND CONNECTOR P8048 DISCONNECTED. RECONNECTED CONNECTOR P8048 IAW SMP. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 30,132 hrs · 25,679 cycles

DURING CLIMB & ENTERING ICING CONDITIONS CREW RECEIVED BLEED1 VLV FAIL MSG & ANTI-ICE INOPERATIVE MSG. CREW COMPLIED WITH AOM VOL 1 PROCEDURES & RETURNED WITHOUT INCIDENT.

Part: CONTROL PANEL — FAILED (BLEED AIR SYS) · airframe 30,088 hrs · 25,640 cycles

AFTER TAKEOFF TURNED OFF BLEED 1 VLV CLOSED DISPLAYED ON EICAS. FOLLOWED CHECKLIST & COULD NOT GET VLV TO RESET. REQUESTED RETURN. R & R NR 1 ENG BLEED VLV AMM 36-11-05 AIR BLEED SYS OPERATIONAL TEST FAILED DID NOT FIX. R & R CONTROL PANELS OF THE AIR CONTROL PNEUMATIC IAW AMM 20-13-10. PERFORMED OPERATIONAL TEST 36-00-00 GOOD. PN3215886-2 SN 864C.

Part: MECHANISM — DIRTY (CABIN DOOR) · airframe 29,705 hrs · 25,277 cycles

MAIN CABIN DOOR HANDLE DIFFICULT TO OPERATE. CLEANED, INSPECTED & LUBRICATED MAIN DOOR MECHANISM IAW AMM 52-18-00. OPERATIONAL CHECKED GOOD.

Part: ROLLER — DIRTY (PAX DOOR) · airframe 29,247 hrs · 24,737 cycles

FLIGHT ATTENDANT SAYS THE MAIN CABIN ENTRY DOOR IS HARD TO OPEN & CLOSE. CLEANED & LUBED MAIN PAX DOOR ROLLERS IAW AMM 52-10-00. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (GALLEY) · airframe 29,191 hrs · 24,668 cycles

ABOUT 5 MIN AFTER TAKEOFF, WE SMELLED A MELTING PLASTIC SMELL. IT WAS MOST PREVALENT FROM THE GALLEY FWD, IT PERSISTED THE REST OF THE FLIGHT. COMPLIED WITH ETN EM- 72-034, ENG ODOR EVENT. NO ODORS. UPON FURTHER INVESTIGATION, FOUND HOT JUG PLUG SCORCHED & BURNED.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 29,151 hrs · 24,632 cycles

RIGHT BEAM SUPPORT OTBD SIDE CRACKED IN WING BOX AREA. R & R RT BEAM SUPPORT OTBD SIDE IN WING BOX AREA IAW EMB SRM 53-23-02.

Part: LIGHT — DAMAGED (CABIN) · airframe 29,151 hrs · 24,632 cycles

EMERGENCY LIGHT EXTRUSIONS NR 1, 4, 5 & 8 ARE DAMAGED. R & R EMERGENCY LIGHT STRIP EXTRUSIONS NR 1, 5 & 8 IAW EMB 140 AMM 33-50-12. NR 4 EXTRUSION WAS FOUND SERVICEABLE.

Part: CONNECTOR — BROKEN (CABIN) · airframe 29,151 hrs · 24,632 cycles

EMERGENCY LIGHT STRIP NR 1 HAS BROKEN CONNECTOR ON ACFT SIDE. INSTALLED NEW CONNECTOR EMERGENCY LIGHT STRIP NR 1 IAW EMB 140, WM 91-10-02 & SWPM 20-00-03. FOR OPERATIONS CHECK SEE BOW 153182.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,151 hrs · 24,632 cycles

SERVICE DOOR EMERGENCY WHITE LIGHT INOPERATIVE ON SERVICE DOOR HINGE. R & R SERVICE DOOR EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-10.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 29,151 hrs · 24,632 cycles

FLASHLIGHT CRADLE LOCATED IN COCKPIT IS CRACKED. R & R FLASHLIGHT ASSEMBLY IN COCKPIT BEHIND PILOTS SEAT IAW EMB 140 AMM 33-50-16.

Part: COVER — CRACKED (PAX DOOR) · airframe 29,035 hrs · 24,522 cycles

PAX DOOR EMERGENCY LIGHT TRIM COVER CRACKED NEF 52-10B AUTH 030558M N. R & R PAX DOOR EMERGENCY LIGHT TRIM COVER IAW AMM 25-23-04 NEF 52-10B AUTH 030558M N RESTORED.

Part: WARNING LIGHT — UNKNOWN (UNKNOWN) · airframe 28,116 hrs · 23,746 cycles

AT 37000 FT, A TAS COMPARRISON FLAGS ANTI-ICE TURNED ON MANUALLY AND ICE ON WINDSHIELDS IN OVERSPEEDS, OVERHEAD SPS ADVANCE, PLT CAME DOWN 3 DIFFERENT READINGS ON THE CAPT PFD FO, PFD ISIS INSTRUMENT ERRORS AIRSPEED DIFFERENCE BETWEEN F/O, 130 KIAS AND CAPT, 250 KIAS, ISIS 230 KIAS INSTRUMENTS SLOWLY CAME BACK AT 20,000 OUT OF IMC CONDITIONS AND THEY APPEARED TO BE WORKING OK. PERFORMED OPS CHECK OF ICE DET SYSTEM IAW 30-80-00. OPS CHECKED GOOD. PERFORMED OPS CHECK OF A/I SYSTEM IAW 30-00-00 SYS CHECK NORMAL ACFT STATIC PITOT SYSTEM SERVICING IAW 34-13-00. ACFT OK FOR SERVICE, ALL CHECK PERFORMED WAS OK FOR RETURN TO SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 27,733 hrs · 23,379 cycles

MAIN CABIN DOOR GROUND ILLUMINATION EMERGENCY LIGHT INOPERATIVE. TIGHTENED CONNECTIONS ON MAIN CABIN DOOR GROUND ILLUMINATION EMERGENCY LIGHT IAW AMM 33-50-06. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,323 hrs · 22,999 cycles

DURING B INSPECTION, FOUND THE LT OVER WING EMERGENCY LIGHT LAMP INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R THE LT OVER WING EMERGENCY LIGHT LAMP IAW AMM 33-50-07. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,323 hrs · 22,999 cycles

DURING B INSPECTION, FOUND THE AFT AISLE EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R THE AFT AISLE EMERGENCY LIGHT LAMP IAW AMM 33-50-08. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 27,191 hrs · 22,871 cycles

DURING MX INSP FOUND THE F/O’S EMERGENCY FLASHLIGHT BASE BROKEN. THE ACFT WAS REMOVED FROM SERVICE. R & R THE CO-PILOTS EMERGENCY FLASHLIGHT CRADLE IAW AMM 33-50-16. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 27,129 hrs · 22,810 cycles

THE CREW REPORTED THE CAPTAIN’S EMERGENCY FLASHLIGHT HOLDER RETAINING CLIP WAS BROKEN. THE ACFT WAS REMOVED FROM SERVICE. R & R THE CAPTAIN’S EMERGENCY FLASHLIGHT HOLDER IAW AMM 335016. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (LANDING GEAR) · airframe 26,623 hrs · 22,370 cycles

ON FLIGHT 2776 THE CREW REPORTED THEY RECEIVED A LANDING GEAR/GROUND FAIL MESSAGE ON UPON RETRACTING GEAR. THE MESSAGE STAYED ON THE ENTIRE FLIGHT. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND RIGHT MAIN LANDING GEAR AFT WEIGHT ON WHEELS SWITCH BRACKET LOOSE. RE-SECUERD BRACKET IAW ELEB CMM 32-10-01 & PERFORMED OPERATIONAL CHECK IAW ETN-EM-32-245. REMOVED AND REPLACED THE LANDING GEAR ELECTRONINC UNIT IAW EMB 140 AMM 32-32-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 25,941 hrs · 21,845 cycles

DURING MAINTENANCE INSPECTION FOUND THE COCKPIT FLASHLIGHT MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW FLASHLIGHT BEHIND PILOT SEAT AMM 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — LOOSE (CABIN DOOR) · airframe 25,480 hrs · 21,440 cycles

ON FLIGHT 4176 THE CREW REPORTED THEY COULD NOT OPEN MAIN CABIN DOOR FROM INSIDE OF CABIN DOOR. THE DOOR WOULD ONLY OPEN USING LEVER FROM OUTSIDE OF THE AIRCRAFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED INTERNAL ACTUATING HANDLE ON PASSENGER DOOR IAW EMB 140 AMMM 52-18-05. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: COUPLING — BLOWN (AC BAY) · airframe 25,365 hrs · 21,329 cycles

ON FLIGHT 4060 THE CREW REPORTED THAT THE PACK 2 VALVE CLOSED ON EICAS. THE CREW RESET PER AOM, PACK 2 VALVE RESET THEN CLOSED AGAIN (PACK 2 VALVE CLOSED). THIS WAS FOLLOWED BY A BURNING ODOR IN THE COCKPIT, WHICH CLEARED AFTER 3 MINUTES. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND COUPLING AT DUAL TEMPERATURE CONTROL VALVE BLOWN OUT THAT GOES TO THE HEAT EXCHANGER. REMOVED AND REPLACED THE COUPLING IAW AMM 21-60-01. THE OPERATIONAL CHECK WAS GOOD. NO ODOR NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INDICATOR — ERRATIC (FUEL) · airframe 24,937 hrs · 20,914 cycles

FLIGHT 4537, CREW REPORTED THAT AFTER TAKEOFF BOTH FUEL INDICATORS SHOWED DASHES. BOTH CAME BACK AFTER 2-3 SECONDS WITH ERRATIC INDICATIONS FOLLOWED BY FUEL IMBALANCE CAUTION MESSAGE ON EICAS. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REBALANCE FUEL WITH FUEL TRUCK AND OPS CHECK FUEL SYSTEM IAW AMM 28-41-00 AND 28-20-04. NO DEFECTS NOTED. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 24,849 hrs · 20,828 cycles

DURING MAINTENANCE INSPECTION, FOUND THE MAIN ENTRY DOOR WILL NOT OPEN OR CLOSE. AIRCRAFT REMOVED FROM SERVICE. ADJUSTED MAIN DOOR ROLLERS SUPPORT AND CHECK OK IAW MM 52-18-00. ADJUSTED LEFT UPPER ROLLER. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — LOOSE (CABIN) · airframe 24,816 hrs · 20,795 cycles

ON FLIGHT 3913 THE CREW REPORTED THE FLIGHT ATTENDANT FLASHLIGHT BRACKET WAS LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT HOLDER ASSEMBLY IAW AMM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,424 hrs · 20,475 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY OVERWING LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING PANEL OVERWING EMERGENCY EXIT LIGHT ASSEMBLY IAW EMB 140 AMM 33-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 24,454 hrs · 24,454 cycles

DURING MAINTENANCE INSPECTION FOUND THE CABIN FLOOR NR 1 EMERGENCY LIGHT STRIP HAS TWO BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED WIRE FOR FLOOR STRIP NR 1 IAW EMB 140 WM 20-21-00. THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (PAX DOOR) · airframe 2,729 hrs · 20,493 cycles

DURING MAINTENANCE INSPECTION FOUND THE PASSENGER DOOR SWING ARM EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND TREATED GRN TO PASSENGER DOOR SWING ARM EMERGENCY LIGHT IAW EMB140 AMM 20-13-21. THE SYSTEM CHECK WAS GOOD IAW EMB140 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 24,423 hrs · 20,474 cycles

FRAME 23 CRACKED AT RT OTBD FLOOR SUPPORT. REPAIRED IAW EO EM-53MR-1808.

Part: LIGHT — WRONG PART (CABIN) · airframe 24,454 hrs · 24,454 cycles

DURING MAINTENANCE INSPECTION FOUND THE CABIN EMERGENCY LIGHT STRIP NR 1 TO BE WRONG PART NUMBER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT STRIP NR 1 IAW EMB140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,264 hrs · 20,351 cycles

DURING MAINTENANCE INSPECTION FOUND NR 1 EMERGENCY BATTERY CHARGER ASSEMBLY INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY CHARGER ASSY IAW 33-700-19. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,016 hrs · 20,157 cycles

DURING B-INSPECTION FOUND THE SERVICE DOOR OVERHEAD EMERGENCY EXIT SIGN LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT INVERTER IAW EMB 140 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,989 hrs · 20,138 cycles

DURING B-INSPECTION FOUND THE INTERIOR EMERGENCY LIGHT OVER SERVICE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. AFTER FURTHER INSPECTION FOUND EMERGENCY LIGHT OPERATIVE IAW EMB 140 AMM 33-50-00. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (NLG) · airframe 23,392 hrs · 19,729 cycles

ON FLIGHT 3293 THE CREW REPORTED THAT AFTER TAKEOFF, AFTER RETRACTING GEAR THE WIND NOISE IN COCKPIT WAS EXCEPTIONALLY LOUD. UPON ACCELERATION, THE NOISE GOT EXTREMELY LOUD, NOT NORMAL. ALL 3 GEAR INDICATIONED UP. ALL INDICATIONS ON HYD PAGE OF MFD WERE NORMAL. NOISE SOUNDED LIKE IT WAS COMING FROM UNDER THE NOSE AREA. THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND NOSE LANDING GEAR DOORS NOT CLOSED AFTER RETRACTION. REMOVED AND REPLACED NOSE LANDING GEAR DOORS PROXIMITY SWITCH IAW EMB 140 AMM 32-61-01. THE OPERATIONAL CHECK WAS GOOD, THE GEAR SWING TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — MISSING (FIRE BOTTLE) · airframe 23,250 hrs · 19,622 cycles

ON FLIGHT 2803 THE CREW REPORTED THE SAFTY SEAL MISSING ON THE COCKPIT FIRE EXTINGUISHER. THE AIRCRAFT WAS REMOVED FROM SERVICE. VISUALLY INSPECTED COCKPIT FIRE EXTINGUISHER PER EMB AMM 26-24-00 AND RE-INSTALLED SEAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RELIEF VALVE — FAULTY (OIL SYSTEM) · airframe 21,277 hrs · 18,003 cycles

ON FLIGHT 2909 THE CREW REPORTED THE NR 2 ENGINE OIL QUANTITY WENT FROM 9 QUARTS TO A LOW OF 3 QUARTS. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. UPON SHUT DOWN THE AIRCRAFT SHOWED 5 QUARTS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT ENGINE OIL TANK PRESSURE RELIEF VALVE IAW RRMM 79-27-40. NO FURTHER LEAKS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BOLT — BROKEN (MAIN DOOR) · airframe 20,981 hrs · 17,726 cycles

ON FLIGHT 3240 THE FLIGHT ATTENDANT COULD NOT OPEN THE MAIN DOOR WITH INSIDE DOOR HANDLE. DOOR COULD BE OPENED FROM THE OUTSIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND MAIN DOOR INTERNAL BOLT BROKEN. REMOVED AND REPLACED BOLT IAW EMB 140 52-18-00-841 STEP I PREPARATION STEP 2. THE OPERATIONAL CHECK OF THE DOOR HANDLE WAS GOOD IAW EMB 140 52-18-00 AMM. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (COCKPIT) · airframe 20,119 hrs · 17,078 cycles

ON FLIGHT 3307 DURING THE CLIMB THE CREW REPORTED, RECEIVED A SPOILER FAIL INDICATION MESSAGE ON EICAS. THE CAPTAIN DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SPOILER CONTROL UNIT. THE OPERATIONAL TEST WAS GOOD IAW AMM CH 27-63-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — INOPERATIVE (COCKPIT) · airframe 19,784 hrs · 16,807 cycles

ON FLIGHT 3947 DURING THE CLIMBOUT THE CREW REPORTED EVERY ERRATIC CABIN RATE FLUCTUATIONS. THE CREW WAS UNABLE TO CONTROL THE CABIN ALTIMETER IN AUTO AND MANUAL. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ELECTRO PNEUMATIC OUTFLOW VALVE IAW EMB 140 AMM 21-21-03. REMOVED AND REPLACED THE DIGITAL CONTROLLER IAW EMB 140 AMM 21-31-01. THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 AMM 21-31-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 19,670 hrs · 16,709 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHTS FORWARD LIGHT STRIP, RIGHT WING FORWARD LIGHT, SERVICE DOOR LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY AND CHARGER LAW WC 33-700-19. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — WORN (AILERON) · airframe 19,556 hrs · 16,606 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT AILERON POWER CONTROL UNIT ATTACHMENT FITTING ON AILERON HAS WORN AND HAD MIGRATING HAT BUSHINGS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED POWER CONTROL UNIT FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,275 hrs · 15,762 cycles

DURING MAINTENANCE INSPECTION FOUND THE CARGO DOOR SILL CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR SILL PLATE AT FRAME 65 TO FRAME 68, IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 4,767 hrs · 12,313 cycles

DURING A MBV INSPECTION, THE RT OMEGA BEAM AT FRAME 23 WAS FOUND CORRODED. BLENDED THE CORRODED AREA TO REMOVE THE DAMAGE. APPLIED ALODINE AND EPOXY PRIMER TO THE REWORKED AREA. FAB A 4.0 BY 2.0 REPAIR DOULBER FROM AL - 2024-T3 INSTALLED REPAIR. WORK DONE WITH EMBRAER 145 SRM (SRM EMB-145/1142 REV.38) CHAPTER 53-21-10 FIGURE 206. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 14,767 hrs · 12,313 cycles

DURING A MBV INSPECTION, A PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. PREPARED A DOUBLER AND FILLER. CLEANED AND TREATED REPAIR PARTS. REPAIR DONE IAW EMBRAER 145 SRM (SRM 145/1142 REV 39) CHAPTERS 53-00-10, FIGURE 206. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — MALFUNCTIONED (ANTI-ICE SYS) · airframe 13,774 hrs · 11,566 cycles

NR 2 ENGINE ANTI ICE SYSTEM FAILED IN ROUTE TO LEX. A/C DIVERTED TO ICT DUE TO IN ROUTE WEATHER. CONTRACT MX ISSUED MEL 30-11 TO THE AIRCRAFT. REMOVED AND REPLACED NR 2 ENG ANTI-ICE VALVE IAW EMB AMM 30-21-01 OPS CHECK GOOD IAW EMB AMM P/T 30-00-00-700-802-A MEL ITEM RESTORED AIRCRAFT RETURNED TO SERVICE

Part: UNKNOWN — SMOKE (CABIN) · airframe 13,577 hrs · 11,396 cycles

SMOKE IN CABIN AFTER TAKEOFF, SMOKE DISSIPATED.

Part: TOILET — ODOR (LAVATORY) · airframe 13,677 hrs · 11,396 cycles

ON CLIMB-OUT, FLIGHT ATTENDANT REPORTED FAINT ODOR OF BURNING RUBBER IN CABIN. ODOR WENT AWAY AFTER 5 MINUTES. FOUND ODOR COMING FROM LAV. FOUND LAV LEAKING. REMOVED AND REPLACED LAV TOILET UNIT IAW EMB140 AMM 38-32-01. NO LEAKS OR ODOR NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (ZONE 700) · airframe 12,658 hrs · 10,728 cycles

CLUNK SOUND HEARD JUST BEFORE TOUCHDOWN FOLLOWED BY LOUD BANGING NOISE DURING TAXI. INSPECTED GROUND CONNECTOR P0040 FOUND UNSERVICEABLE. REMOVED AND REPLACED CONNECTOR IAW EMB SPWM 20-50-00 AND EMB 32-63-05. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: TERMINAL — UNSECURE (EMERGENCY LIGHT) · airframe 11,177 hrs · 9,698 cycles

EMERGENCY EXIT LIGHT AT ROW 11 INOPERATIVE. RESECURED LIGHT THERMINALS, IAW AMM 33-50-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: PRESSURE SWITCH — INOPERATIVE (NR 2 RUDDER)

DURING CLIBM CREW REPORTED RUDDER SYSTEM 1/2 INOPERATIVE MESSAGE ON EICAS FOLLOWED BY A YAW DAMPNER FAIL. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 2 RUDDER PRESSURE SWITCH IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ODOR — DETECTED (CABIN)

DURING CRUISE FLIGHT, THE CREW REPORTED A BURNING INSULATION ODOR. AIRCRAFT WAS DIVERTED TO LIT. (M)

Part: ODOR — DETECTED (CAIBN)

CREW REPORTED A BURNING INSULATION ODOR IN FLIGHT. AIRCRAFT WAS DIVERTED TO LIT AND LANDED WITH NO OTHER INCIDENT REPORTED. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. BLEED SYSTEM WAS INSPECTED AND AN OPERATIONAL CHECK WAS COMPLIED WITH. NO ODOR WAS NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. (M)