N819AE

Part: NIPPLE — OVERHEATED · airframe 37,527 hrs · 33,343 cycles

"TRANSFERRED FROM AML PAGE 4343084 ITEM 1" AFTER APU START AND OPERATING PACK 2 FOR APPROX 3 MINUTES, SMELLED ELETRICAL HEAT/BURNING SMELL WHILE AT THE GATE. F/A REPORTED SMELL BY SEAT 3A FORWARD AND SMELL IN COCKPIT ALSO. NEGATIVE DE-ICE ON ORIGINATION FLIGHT FROM GGG.-C/A-REMOVED AND REPLACED FWD AND AFT HEATED NIPPLES IAW EMB 140 AMM 38-10-04 OPS CK GOOD

Part: ACM — FAILED (RIGHT) · airframe 37,523 hrs · 33,339 cycles

SMELL OF SOMETHING HEATED ODOR AT GATE PRIOR TO PUSH BACK REPEAT WRITE UP FROM PREVIOUS 2 DAYS-C/A-REMOVED AND REPLACED R/H AIR CYCLE MACHINE IAW AMM 21-51-03. OPS CHECK GOOD IAW AMM 21-51-00. REMOVED AND REPLACED GASPER FAN IAW AMM 21-23-03. OPS CHECK GOOD IAW AMM 21-20-00. NO MORE EVIDENCE OF SMELL IN COCKPIT OR IN CABIN AFTER RUNNING BOTH PACKS AND GASPER FOR 45 MINUTES. RECIRCULATION GASPER FAN P/N 4611028900 S/N 02077 AFT

Part: FAN — FAILED (RECIRCULATION) · airframe 37,523 hrs · 33,339 cycles

ELECTRICAL SMELL NOTED IN THE FRONT OF THE CABIN WHEN WE ARRIVED AT THE GATE-C/A-T/S FOUND RT RECIRCULATION FAN BURN. REMOVED AND REPLACED CABIN RECIRCULATION FAN OPS CK GOOD NO ELECTRICAL SMELL NOTED IAW AMM 21-24-01.

Part: PROXIMITY SWITCH — DISCONNECTED (LT MLG) · airframe 36,783 hrs · 32,619 cycles

"LG AIR/GND FAIL" EICAS MESSAGE FROM GEAR RETRACTION UNTIL PARKING. NORMAL BRAKING ON TOUCHDOWN NORMAL SPOILER DEPLOY-C/A-PERFORMED TROUBLESHOOTING PER FIM 32-63-00-810-801A. FOUND LT MLG NR 1 WOW SWITCH TO BE UNPLUGGED. PLUGGED IN NR 1 WOW SWITCH AND RETAPED PER ETN-EM-32-173. OPC GOOD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,482 hrs · 32,354 cycles

LEFT EXTERNAL WING TO FUSELAGE EMERGENCY LIGHT INOPERATIVE. R & R THE FUSE F1 ON BATTERY CHARGER NR 1 IAW CMM 25-60-03. OPS CHECKED GOOD.

Part: CRADLE — DAMAGED (FWD FLASHLIGHT) · airframe 35,376 hrs · 31,124 cycles

FA FORWARD FLASHLIGHT LOOSE IN HOLDER AND NOT CHARGING. REMOVED AND REPLACED THE FLASHLIGHT HOLDER IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: FRAME — CRACKED (FRM 16) · airframe 35,342 hrs · 31,077 cycles

FRAME 23 CRACKED AT STRINGER 16R. REPAIRED THE FRAME IAW EO EM-53MR-1808.

Part: FLOOR SUPPORT — CORRODED (FRAME 44) · airframe 35,342 hrs · 31,077 cycles

LEFT OMEGA BEAM CORRODED AT AND AROUND THE CROSSBEAM AT FRAME 44. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-2929.

Part: STRINGER — GOUGED (FRAME 23) · airframe 35,342 hrs · 31,077 cycles

STRINGER 18R GOUGED AT FRAME 23. REPAIRED THE STRINGER IAW SRM 53-00-03-RE.

Part: FRAME — CORRODED (FRM 13) · airframe 35,342 hrs · 31,077 cycles

FRAME 13 CORRODED AT STRINGER 21L AND 21R. REPAIRED THE FRAME IAW ERS-EM-53MR-2937.

Part: FLANGE — GOUGED (CARGO DOOR) · airframe 35,342 hrs · 31,077 cycles

OUTBOARD LOWER FLANGE OF CARGO DOOR GOUGED. REMOVED AND REPLACED THE FLANGE IAW SRM 51-40-02

Part: FRAME — CHAFED (FRM 18) · airframe 35,342 hrs · 31,077 cycles

FRAME 18 IS CHAFED AT STRINGER 2R. REMOVED AND REPLACED THE FRAME SECTION IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (FRAME 20) · airframe 35,342 hrs · 31,077 cycles

PAX DOOR CUTOUT SUPPORT CRACKED AT FRAME 20, STRINGER 3L. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 49-50) · airframe 35,342 hrs · 31,077 cycles

LEFT OMEGA BEAM IS CORRODED BETWEEN FRAMES 49 AND 50. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-2925

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 35,342 hrs · 31,077 cycles

CO-PILOT WINDSHIELD CUTOUT TOP OTBD CORNER HAS A CRACK ON LATERAL POST FRAME. REMOVED AND REPLACED THE WINDOW FRAME IAW SRM 51-40-02

Part: LINER — CORRODED (PAX DOOR) · airframe 35,342 hrs · 31,077 cycles

MAIN DOOR LOWER EDGE LINER NUTPLATE HOLES ARE CORRODED. REPAIRED IAW SRM 52-10-02, AND ETN-EM-52-041.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 35,342 hrs · 31,077 cycles

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

Part: CHANNEL — CORRODED (SERVICE DOOR) · airframe 35,342 hrs · 31,077 cycles

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

Part: DOOR SILL — CORRODED (CARGO) · airframe 35,342 hrs · 31,077 cycles

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

Part: ANGLE — CRACKED · airframe 35,342 hrs · 31,077 cycles

CENTER BEAM RT FWD TO AFT GALLEY DIGITAL SPLICE ANGLE CRACKED. REMOVED AND REPLACED THE SPLICE ANGLE IAW SRM 51-40-02.

Part: ANGLE — CRACKED · airframe 35,342 hrs · 31,077 cycles

LEFT BEAM INBD FWD TO AFT GALLEY DIGITAL SPLICE ANGLE CRACKED. REMOVED AND REPLACED THE SPLICE ANGLE IAW SRM 51-40-02.

Part: ANGLE — CRACKED · airframe 35,342 hrs · 31,077 cycles

LEFT BEAM OTBD FWD TO AFT GALLEY DIGITAL SPLICE ANGLE CRACKED. REMOVED AND REPLACED THE SPLICE ANGLE IAW SRM 51-40-02.

Part: ANGLE — CRACKED · airframe 35,342 hrs · 31,077 cycles

CENTER BEAM LT FWD TO AFT GALLEY DIGITAL SPLICE ANGLE CRACKED. REMOVED AND REPLACED THE SPLICE ANGLE IAW SRM 51-40-02.

Part: CROSSBEAM — CORRODED (FRAME 20) · airframe 35,342 hrs · 31,077 cycles

FRAME 20 CENTER AISLE CROSSBEAM CORRODED. R & R THE CROSSBEAM IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 57-59) · airframe 35,342 hrs · 31,077 cycles

CENTER OMEGA BEAM CORRODED AT, AND AROUND THE CROSSBEAM BETWEEN FRAMES 57 - 59. ACCOMPLISHED A PERMENANT REPAIR IAW EO-EM-53MR-1518, PART B.

Part: FLOOR SUPPORT — CORRODED (FRAMES 57-59) · airframe 35,342 hrs · 31,077 cycles

LEFT OMEGA BEAM CORRODED AT AND AROUND THE CROSSBEAM BETWEEN FRAMES 57 - 59. ACCOMPLISHED A PERMANENT REPAIR OF THE OMEGA BEAM IAW ERS-EM-53MR-2955.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,228 hrs · 30,988 cycles

LAST CEILING EMERGENCY LIGHT FOUND INOPERATIVE. R & R THE EMERGENCY LIGHT IAW AMM33-50-08-04, OPS CHECKED GOOD

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 34,946 hrs · 30,778 cycles

FLASHLIGHT CRADLE BROKEN AT FWD GALLEY. REMOVED AND REPLACED THE CRADLE AND FLASHLIGHT ASSY. IAW AMM 33-50-16, OPS CHECKED GOOD

Part: ROLLER — UNKNOWN (PAX DOOR) · airframe 34,601 hrs · 30,488 cycles

MAIN CABIN DOOR IS HARD TO OPEN & CLOSE. SERVICED MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR · airframe 34,201 hrs · 30,115 cycles

ON DEPARTURE, GOT BURNING RUBBER ODOR FOLLOWED BY AN SHORT ELECTRICAL ODOR. DECLARED EMERGENCY. COMPLETED FIM TASK 21-20-00-810-A AND FIM TASK 21-20-00-810-803-A. NO EVIDENCE OF BURNING RUBBER ODOR OR ELECTRICAL ODOR NOTED. NO FIX. CW ETN-EM-72-034 ENG ODOR EVENT TRBLSHOOTING SUPPLEMENT. NO ODORS DETECTED. REMOVED ALL DU'S AND PERFORMED DVI OF DU'S AND INSTALLED ALL DU'S IAW EMB 140 AMM 34-22-01. NO DEFECTS NOTED AT THIS TIME. OPS CHECK GOOD AT THIS TIME. FCF FOUND SATISFACTORY.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 33,816 hrs · 29,703 cycles

EMERGENCY LIGHTS IN ROW 7 - 10 & LOWER EMER LIGHTS ON EMER EXIT DOORS INOPERATIVE. TROUBLE SHOT IAW FIM 33-50-00 FOUND INVERTER 5 TO BE INOPERATIVE. R & R INVERTER 5 IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 32,962 hrs · 28,741 cycles

SPOILER FAIL MSG ON EICAS WITH OPEN INSCRIPTION IN SPOILERS STATUS BOX. OCCURRED AT FL 360 WITH NO OBVIOUS CONTROLLABILITY ISSUES. COMPLIED WITH SPOILER OPERATIONAL CHECK IAW AMM 27-63-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 32,892 hrs · 28,662 cycles

REAR CABIN FLASHLIGHT BROKEN. R & R REAR CABIN EMER FLASHLIGHT IAW AMM 25-60-0.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,806 hrs · 28,575 cycles

EMERGENCY LIGHTS AT ROWS 7 - 11 ARE INOPERATIVE. CHARGED EMER LIGHTS AT ROWS 7 - 11. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,619 hrs · 28,389 cycles

THE LAST FLOOR PROXIMITY STRIP LIGHT IN THE AFT CABIN IS INOPERATIVE. R & R THE LAST FLOOR PROXIMITY LIGHT STRIP IN THE AFT CABIN IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: LIGHT — OUT OF ADJUST (CABIN) · airframe 32,591 hrs · 28,363 cycles

EMERGENCY CTR FLOOR LIGHTING INOPERATIVE. PERFORMED ADJUSTMENT OF EMER LIGHTING SYS IAW AMM 33-50-00. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 32,476 hrs · 28,256 cycles

FORWARD EMER FLOOR STRIP & SERVICE DOOR MARKER LIGHTS INOPERATIVE. R & R EMER LIGHT INVERTER NR 3 IAW AMM 33-50-11. OPERATIONAL CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 32,339 hrs · 28,126 cycles

FIRST FLOOR EMER LIGHT STRIP IN PAX CABIN & SERVICE DOOR LOWER EXIT MARKER DID NOT ILLUMINATE. R & R NR 2 DC & AC INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,114 hrs · 27,915 cycles

DURING PS 1 CHECK, FOUND NR 3 & 4 FLOOR PROXIMITY LIGHT STRIPS INOPERATIVE. R & R NR 3 EMER LIGHTING BATTERY & CHARGER IAW WC 33-700-19. OPERATIONS CHECKED IAW WC 33-700-17. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED. EMER LIGHTING BATTERY PN 2013-1A, SN 104934.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 31,948 hrs · 27,786 cycles

EMERGENCY LIGHTS FOR FLIGHT COMPARTMENT CEILING, LT FWD FAIRING & AISLE CEILING PANEL NR 1 INOPERATIVE. R & R NR 1 EMER LIGHTS BATTERY POWER SUPPLY & BATTERY PACK IAW MM 33-50-04. OPERATIONS CHECKED GOOD. EMER LIGHTING BATTERY PN 2013-1A, SN 104910.

Part: WIRE — BROKEN (CABIN) · airframe 31,840 hrs · 27,694 cycles

EMERGENCY LIGHT STRIP NR 8 HAS A BROKEN WIRE ON THE ACFT SIDE. INSTALLED NEW CONNECTOR AT EMER LIGHT STRIP NR 8 IAW SWPM 20-00-03,20-21-00 & WM 91-10-02.

Part: WIRE — BROKEN (CABIN) · airframe 31,840 hrs · 27,694 cycles

EMERGENCY LIGHT STRIP NR 7 HAS BROKEN WIRES. R & R EMER LIGHT STRIP NR 7 IAW AMM 33-50-12. SEE BOW 181199 FOR OPERATIONS CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 31,840 hrs · 27,694 cycles

EMERGENCY LIGHT STRIP NR 2 HAS BROKEN WIRES. R & R EMER LIGHT STRIP NR 2 IAW AMM 33-50-12. SEE BOW 181199 FOR OPERATIONS CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 31,840 hrs · 27,694 cycles

EMERGENCY LIGHT WIRE AT FRAME 25 BROKEN. FOUND BROKEN WIRES AT FRAME 27 & NOT FRAME 25. REPAIRED WIRES W192-8900-22 & W192-8901-22 FOR EMERGENCY LIGHT WIRES IAW SWPM 91-10-03, 20-21-00,20-00-03 & 20-00-05. CRIMPER SN 6277, GMT 232 SN 2890B. FOR OPERATIONS CHECK SEE BOW 181199.

Part: CONNECTOR — BROKEN (CABIN) · airframe 31,840 hrs · 27,694 cycles

LEFT NR 5 EMER LIGHT STRIP BROKEN AT CONNECTOR, LIGHT STRIP SIDE. R & R LT EMER LIGHT STRIP NR 5 IAW AMM 33-50-12. SEE BOW 181199 FOR OPERATIONS CHECK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,840 hrs · 27,694 cycles

NUMBER 1 FLOOR PROXIMITY EMER LIGHT STRIP INOPERATIVE. R & R NR 1 EMER FLOOR PROXIMITY LIGHT IAW AMM 33-50-12. SEE BOW 181199 FOR OPERATIONAL CHECK OF EMER LIGHTS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,814 hrs · 27,672 cycles

LAVATORY LT OMEGA BEAM IS CORRODED. REPAIRED IAW ERS-EM-53MR-1133.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,814 hrs · 27,672 cycles

FRAME 75 SKIN CRACKED ABOVE STRINGER 2L. REPAIRED IAW ERS-EM-53MR-1132.

Part: SKIN — CORRODED (FUSELAGE) · airframe 31,814 hrs · 27,672 cycles

INTERNAL FUSELAGE SKIN CORRODED BETWEEN FRAMES 37 & 38 & STRINGER 21L & 21R. RESTORED PROTECTIVE FINISH ON INTERNAL SKIN IAW CPM 51-21-06, ETN'S EM-51-075, EM-51--091R5, EM-51-011R4 & GN-51-120R1. DAMAGE ACCEPTED AS IS IAW ERS-EM-53MR-1121.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,814 hrs · 27,672 cycles

LEFT EXTERNAL SKIN CRACKED AROUND FRAME 77 - 79, STRINGER 3L - 7L. PERFORMED CIRCULAR CUT OUTS TO REMOVE DAMAGE & INSTALLED FLANGED BUSHINGS TO REPAIR CRACKS IAW ERS-EM-53MR-1112 PT A.

Part: FRAME — GOUGED (FUSELAGE) · airframe 31,814 hrs · 27,672 cycles

FRAME 61 GOUGED IN 3 PLACES BETWEEN STRINGER 3R & 5R. BLENDED GOUGE IN 3 PLACES AS REQUIRED FROM UPPER CARBON BEAM SUPPORT AT FRAME 61 BETWEEN STRINGERS 3R & 5R IAW SRM 51-10-03. ACCEPTED AS IS IAW ERS-EM-53MR-1115.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,814 hrs · 27,672 cycles

EXTERNAL FUSELAGE LOWER SKIN DENTED BETWEEN FRAME 66 - 67 & STRINGER 19L - 20L. RESTORED PROTECTIVE FINISH TO EXTERNAL FUSELAGE SKIN IAW CPM 51-21-06 & ETN GN-51-011R4, EM-51-075, EM-091R5 & GN-51-120R1. DAMAGE ACCEPTED AS IS IAW ERS-EM-53MR-1116.

Part: SKIN — SCRATCHED (EMERGENCY EXIT) · airframe 31,814 hrs · 27,672 cycles

LEFT EMER EXIT HAS MINOR SCRATCH AFT EDGE ADJACENT TO THE WINDOW. APPLIED REPAIR TO LT EMER EXIT SKIN AFT EDGE ADJACENT TO WINDOW IAW ERS-EM-52MR-296.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 31,814 hrs · 27,672 cycles

CARGO DOOR SILL BEAM CORRODED. APPLIED REPAIR TO CARGO DOOR SILL IAW ERS-EM-53MR-1111.

Part: FRAME — CHAFED (FUSELAGE) · airframe 31,814 hrs · 27,672 cycles

LAVATORY LT WALL FRAME 59 IS CHAFED AT STRINGER 5L. APPLIED REPAIR TO FRAME 59 AT STRINGER 5L IAW ERS-EM-53MR-1110.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,814 hrs · 27,672 cycles

LEFT EXTERNAL FUSELAGE SKIN CRACKED AT RIVET FRAME 79. REPAIRED SKIN CRACK ON LT EXTERNAL SKIN AT RIVET IAW ERS-EM-53MR-1112 PART A.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 31,814 hrs · 27,672 cycles

EMERGENCY FLOOR PROX LIGHTS NR 4 & 5, RT & LT EMER EXIT SIGNS INOPERATIVE. RESEATED ELEC CONNECTOR ON EMER LIGHTS POWER SUPPLY NR 3 IAW AMM 33-50-04 & SWPM 20-50-00. OPERATIONAL CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 31,814 hrs · 27,672 cycles

EMERGENCY LIGHT STRIP NR 2 HAS BROKEN WIRES. R & R EMER LIGHT STRIP NR 2 IAW AMM 33-50-12. SEE BOW 181199 FOR OPERATIONS CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 31,814 hrs · 27,672 cycles

EMERGENCY LIGHT STRIP NR 7 HAS BROKEN WIRES. R & R EMER LIGHT STRIP NR 7 IAW AMM 33-50-12. SEE BOW 181199 FOR OPERATIONS CHECK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,814 hrs · 27,672 cycles

NUMBER 1 FLOOR PROXIMITY EMER LIGHT STRIP INOPERATIVE. R & R NR 1 EMER FLOOR PROXIMITY LIGHT IAW AMM 33-50-12. SEE BOW 181199 FOR OPERATIONAL CHECK OF EMER LIGHTS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,814 hrs · 27,672 cycles

LEFT EXTERNAL FUSELAGE SKIN CRACKED AT RIVET, FRAME 78. REPAIRED SKIN CRACK ON LT EXTERNAL SKIN AT RIVET IAW ERS-EM-53MR-1112 PART A.

Part: WIRE — BROKEN (CABIN) · airframe 31,814 hrs · 27,672 cycles

EMERGENCY LIGHT STRIP NR 8 HAS A BROKEN WIRE ON THE ACFT SIDE. INSTALLED NEW CONNECTOR AT EMER LIGHT STRIP NR 8 IAW SWPM 20-00-03, SWPM 20-21-00 & WM 91-10-02. CRIMPER EASI 6277, POSITIONER SER 7151. FOR OPERATIONS CHECK SEE BOW 181199.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,814 hrs · 27,672 cycles

LAVATORY CTR OMEGA BEAM IS CORRODED. REPAIRED LAVATORY CTR OMEGA BEAM IAW ERS-EM-53MR-1133. SEE TURNOVER FOR DETAILS.

Part: LIGHT — BROKEN (CABIN) · airframe 31,814 hrs · 27,672 cycles

LEFT NR 5 EMER LIGHT STRIP BROKEN AT CONNECTOR, LIGHT STRIP SIDE. R & R LT EMER LIGHT STRIP NR 5 IAW AMM 33-50-12. SEE BOW 181199 FOR OPERATIONS CHECK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,814 hrs · 27,672 cycles

LEFT EXTERNAL FUSELAGE SKIN CRACKED AT RIVETS TWO EACH, FRAME 77. REPAIRED SKIN CRACK ON LT EXTERNAL SKIN IAW ERS-EM-53MR-1112 PART A.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 31,777 hrs · 27,641 cycles

FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. R & R FWD FLASHLIGHT IAW AMM 33-16-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,612 hrs · 27,525 cycles

CABIN AISLE EMER LIGHT ABOVE ROW 11 INOPERATIVE. RELAMPED CABIN AISLE EMER LIGHT BULB ABOVE ROW 11 IAW AMM 33-50-08. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,612 hrs · 27,525 cycles

RIGHT FWD LOWER FAIRING EMER LIGHT INOPERATIVE. RELAMPED RT FWD LOWER FAIRING EMER LIGHT BULB IAW AMM 33-50-10. OPERATIONAL CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,783 hrs · 26,856 cycles

COCKPIT & LT FWD EXTERIOR EMER LIGHT INOPERATIVE. REPLACED NR 1 EMER LIGHTS BATTERY POWER SUPPLY, BATTERY & CHARGER, IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 SN 14865.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,630 hrs · 26,727 cycles

WHEN REMOVING POWER EMER LIGHTS THAT ARE POWERED BY BATTERY & CHARGER NR 1 WILL NOT SHUT OFF. R & R NR 1 BATTERY & CHARGER IAW WC 33-700-19. OPERATIONS CHECKED GOOD. EMER LIGHT BATTERY PN 2013-1A & SN 103875.

Part: FAN — FAILED (CABIN) · airframe 29,972 hrs · 26,146 cycles

ELECTRICAL SMELL IN FWD CABIN. R & R NR 2 RECIRCULATION FAN IAW AMM 21-24-01. NO SMELLS NOTED AT THIS TIME.

Part: DOOR SEAL — DIRTY (CABIN DOOR) · airframe 29,299 hrs · 25,548 cycles

MAIN CABIN DOOR WILL NOT CLOSE PROPERLY. TOP SEAL REMAINS OPEN EXCESSIVELY, DOOR HANDLE SEEMS TO BIND DURING CLOSING. CLEANED MAIN DOOR SEAL & LUBRICATED ROLLER IAW EMB-140-MM-52-10-01, OPERATIONS CHECKED GOOD, NO FAULTS NOTED.

Part: SEAL — DAMAGED (NR 1 ENGINE) · airframe 29,202 hrs · 25,431 cycles

DURING MAINTENANCE INSPECTION ON FLIGHT 3503 FOUND OPS REPORTS E1 SMOKING AFTER SHUTDOWN. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVE AND REPLACE REAR SHAFT PLUG SEAL IAW WORK CARD 72-200-03 AND R&R THE AGB BREATHER SEAL IAW RR MM 72-63-10. OPS CK GOOD.

Part: SHROUD — DEFECTIVE (TE FLAP) · airframe 29,163 hrs · 25,393 cycles

ON FLIGHT 3398 CREW REPORTED AFTER TAKEOFF RETRACTING FLAP FROM 18 TO 9, RECEIVED A FLAP FAIL MESSAGE WITH FLAP STUCK AT 11. THE CREW DECLARED EMERGENCY & THE ACFT WAS REMOVED FROM SERVICE. AFTER REPLACEMENT OF LT INBD FLAP EXTERNAL SHROUD DRIVER ON NRWC 819-MIA-01414 ITEM NR 3, OPERATIONS CHECK FLAPS & FOUND WORKING PROPERLY IAW EMB 140 TASK 27-51-00. THE ACFT RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,999 hrs · 25,199 cycles

2ND ISLE EMERGENCY CEILING LIGHT INOPERATIVE. R & R 2ND ISLE EMERGENCY CEILING RT LAMP IAW EMB AMM 33-5--08-000-801-A & 33-50-08-400-801-A. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 28,977 hrs · 25,182 cycles

F/O'S FLASHLIGHT NOT WORKING. REMOVED AND REPLACED FLASHLIGHT IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,916 hrs · 25,130 cycles

LEFT EMERGENCY EXTERIOR LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (MAIN CABIN DOOR) · airframe 28,826 hrs · 25,046 cycles

F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPERATE. LUBRICATED PAX DOOR FRAME ROLLERS AND DOOR TOP FLAP AND CHECKED GOOD IAW AMM 53-21-02 AND 52-10-00.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 28,691 hrs · 24,932 cycles

PAX DOOR EMERGENCY LIGHT INOP. REPAIRED DAMAGED WIRE IN DOOR PANEL IAW WM 20-21-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,361 hrs · 24,680 cycles

NR 1 EMERGENCY LIGHT INOPERATIVE. R & R LIGHT IAW AMM 33-50-12, OPS CHECKED GOOD.

Part: ROD END — OUT OF ADJUST (MAIN DOOR) · airframe 28,276 hrs · 24,621 cycles

MAIN ENTRY DOOR IS DIFFICULT TO OPERATE. ADJUSTED MAIN DOOR INTERCONNECT ROD V UPPER RODEND IAW AMM 52-18-00. MAIN DOOR OPERATES NORMALLY AT THIS TIME.

Part: UNKNOWN — UNKNOWN (PAX DOOR) · airframe 28,141 hrs · 24,521 cycles

MAIN DOOR HARD TO OPEN. R & R 2 BOLTS IAW ETN-EM52-052 DID NOT FIX SEE ITEM NR 2 THIS LOG PG.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 28,141 hrs · 24,521 cycles

MAIN CABIN DOOR HARD TO OPEN. SHIMMED FORWARD LOWR ARM FITTING ON MAIN CABIN DOOR IAW AMM 52-18. OPS CHECKED OK.

Part: WARNING LIGHT — FALSE ACTIVATION (HYD SYSTEM) · airframe 28,135 hrs · 24,517 cycles

RECEIVED A HYD LOW QTY FOLLOWED BY ENG 1 HYD PUMP FAIL. FOLLOWED AMO VOL 1 PROCDURES AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. INSPECTED LT ENGINE NO HYD LEAKS NOTED. GROUND RAN ENGINE NORMAL HYD PRESSURE. PERFORM HYD SERVICE IAW ETN EM-29-023. NO EXTERNAL LEAKS. ACFT RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 28,093 hrs · 24,482 cycles

MAIN CABIN DOOR VERY HARD TO OPEN. CLEANED AND LUBED PAX DOOR IAW AMM 52-11-00, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,077 hrs · 24,470 cycles

DURING B INSPECTION, FOUND THE LEFT EXTERIOR EMERGENCY LIGHT OVER THE WING INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R THE LT EXTERIOR EMERGENCY LIGHT OVER THE WING IAW AMM 33-50-10. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (MAIN DOOR) · airframe 27,990 hrs · 24,385 cycles

THE CREW REPORTED THE FWD ENTRY DOOR HANGING UP ON FWD TOP ROLLER WHEN ATTEMPTING TO OPEN DOOR. ACFT REMOVED FROM SERVICE. LUBED MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02. THE OPS CHECK WAS GOOD. THE AFT WAS RETURNED TO SERVICE.

Part: HANDLE — OUT OF POSITION (CABIN DOOR) · airframe 27,794 hrs · 24,208 cycles

THE CREW REPORTED THE MAIN DOOR WAS DIFFICULT TO OPEN. THE ACFT WAS REMOVED FROM SERVICE. AT THIS TIME REPOSITIONED MAIN CABIN DOOR INTERNAL HANDLE IAW AMM 52-11-01. COMPLIED WITH OPENING AND CLOSING IAW AMM 52-00-00. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: DOOR — DIRTY (CABIN) · airframe 27,778 hrs · 24,198 cycles

THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN & CLOSE. THE ACFT WAS REMOVED FROM SERVICE. CLEANED & LUBRICATED MAIN DOOR IAW AMM 52-18-00. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — UNSERVICEABLE (COCKPIT) · airframe 27,740 hrs · 24,171 cycles

THE CREW REPORTED THE RED LIGHT ON THE CAPTAIN’S FLASHLIGHT WAS BROKEN. THE ACFT WAS REMOVED FROM SERVICE. R & R THE CAPATIN’S FLASHLIGHT. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 27,675 hrs · 24,111 cycles

THE CREW REPORTED THE MAIN CABIN ENTRY DOOR WAS DIFFFICULT TO OPEN. THE ACFT WAS REMOVED FROM SERVICE. LUBICATED MAIN DOOR ACTUATING AND LOCKING MECHANISM ROLLERS IN REF TO AMM 52-18-00. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 27,668 hrs · 24,104 cycles

THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO PUSH OPEN AFTER UNLATCHING. THE ACFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN DOOR IAW AMM 52-18-00. THE ACFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 27,357 hrs · 23,852 cycles

ON FLIGHT 3900 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED THE MAIN DOOR FRAME ROLLER IAW EMB 140 M/M 53-21-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 27,310 hrs · 23,820 cycles

ON FLIGHT 3279 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED MAIN CABIN DOOR. THE OPERATIONAL CHECK WAS OK. THE AIRCRAFT WAS RETURNED TO SERVICE IAW EMB-140 MM 52-10-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,190 hrs · 23,710 cycles

ON FLIGHT 3245 THE CREW REPORTED THE EMERGENCY LIGHT DID NOT ILLUMINATE WHEN TURNED ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1, 2, 3 & 4 EMERGENCY LIGHTS BATTERY PACK IAW EMB 140 AMM 33-50-04. SERIAL NUMBERS: #1 104904, #2 104956, #3 112034, & #4 109951. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,067 hrs · 23,610 cycles

DURING MAINTENANCE INSPECTION FOUND FRAME 23 CRACKED BETWEEN STRINGER 15R-16R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FUSELAGE SKIN IAW EO EM 53MR-1779. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — GOUGED (RT AILERON) · airframe 27,067 hrs · 23,610 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT AILERON PCA FITTING DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED PCA FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 27,103 hrs · 23,648 cycles

DURING MAINTENANCE INSPECTION FOUND EMERGENCY LIGHT STRIP WIRES BROKEN AT FLOOR PANEL 231GF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED EMERGENCY LIGHT STRIP WIRES AT FLOOR PANEL 231GF IAW EMB140 WMM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,103 hrs · 23,648 cycles

DURING MAINTENANCE INSPECTION FOUND THE PASSENGER DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHTING BATTERY ASSEMBLY BATTERY CHARGER IAW EMB 140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,067 hrs · 23,610 cycles

SKIN AT FRAME 23, STR 15R IS CRACKED. REPAIRED IAW EO EM-53MR-1779.

Part: STRIP — MISSING (CABIN) · airframe 27,103 hrs · 23,648 cycles

DURING MAINTENANCE INSPECTION FOUND NUMEROUS EMERGENCY LIGHT FILLER STRIPS MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED EMERGENCY LIGHT FILLER STRIPS IAW EMB140 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 27,103 hrs · 23,648 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT EMERGENCY LIGHT STRIP 1 HAS BROKEN WIRE AT FUSELAGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT EMERGENCY LIGHT STRIP NR 1 WIRE IAW EMB140 WMM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 23,610 hrs · 23,610 cycles

DURING MAINTENANCE INSPECTION THE BATTERY POWER SUPPLY ONLY PARTIAL EMERGENCY LIGHTS CAME ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY POWER SUPPLY. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — UNSERVICEABLE (CABIN) · airframe 27,103 hrs

DURING MAINTENANCE INSPECTION FOUND EMERGENCY LIGHTING BATTERY ASSEMBLY/ BATTERY CHARGER NEEDS TO BE REPLACED. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY ASSEMBLY BATTERY CHARGER 3 S/N 70401 IAW WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — BROKEN (COCKPIT) · airframe 26,638 hrs · 23,199 cycles

ON FLIGHT 4013 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT BRACKET WAS BROKEN. ENTERED INTO MEL 25-53 AUTH 111408-C. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD - IAW EMB AMM 33-50-16 - THIS ACTION RESTORES MEL 25-53 AUTH 111408-C. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,581 hrs · 23,155 cycles

DURING B INSPECTION FOUND THE OVERHEAD EMERGENCY DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OVERHEAD EMERGENCY LIGHT BULB AT THE EMERGENCY DOOR IAW EMB 140 AMM 33-50-08. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: O-RING — FAILED (BLEED DUCT) · airframe 25,807 hrs · 22,501 cycles

FLIGHT 2720, CREW REPORTED THAT SHORTLY AFTER TAKEOFF THEY RECEIVED A BLEED LEAK 1 MESSAGE. RAN EPC BLEED LEAK CHECK LIST. DECLARED AN EMERGENCY AND LEVELED OFF AT 5100 FT AND CONTINUED CHECKLIST IN AOM1. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED AMM TASK FOR LEFT FUSELAGE AIR BLEED DUCT LEAK TEST 36-00-00 UP TO AND INCLUDING STEP 19. FOUND JOINTS LEAKING. REMOVED AND REPLACED O-RINGS IAW AMM 36-11-10. REMOVED AND REPLACED CHECK VALVE IAW AMM 36-12-02, NO LEAKS NOTED AT THIS TIME AT THE CHECK VALVE. AIRCRAFT RETURNED TO SERVICE.

Part: O-RING — CRACKED (FLASHLIGHT) · airframe 25,723 hrs · 22,436 cycles

DURING INSPECTION, FOUND TOP CAP O-RING AND BOTTOM O-RING ON FORWARD CABIN EF-2C RECHARGEABLE FLASHLIGHT CRACKED AND NICKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,876 hrs · 21,804 cycles

DURING B-INSPECTION, FOUND EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,837 hrs · 21,777 cycles

DURING B-INSPECTION FOUND THE CEILING ENTRY WAY EMERGENCY AND COURTESY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LAMPS AS PER EMB 140 AMM 33-26-04 PER EMB 140 AMM 33-26-00 AND 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,662 hrs · 21,646 cycles

DURING B-INSPECTION FOUND THE AFT CABIN EMERGENCY FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT IAW AMM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,409 hrs · 21,423 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT REAR OVERWING EXTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY PACK NR 4 CHARGER IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD ON CHARGER AND EXTERIOR LIGHTING. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — SMOKE (NR 1)

AFTER LANDING SHUTDOWN NR 1 ENGINE NORMAL INDICATIONS AS WE PULLED INTO THE GATE RAMPERS REPORTED NR 1 ENGINE WAS SMOKING, EVEN AFTER 15 MINS SMOKE WAS STILL COMING OUT OF THE FRONT AND BACK. REMOVED AND REPLACED E1 OPC GOOD, NO LEAKS NOTED.

Part: PANEL — UNKNOWN (FUSELAGE) · airframe 22,726 hrs · 19,978 cycles

ON FLIGHT 3285 DURING CRUISE THE FIRST OFFICER OBSERVED SMOKE, THEN THE CAPTAIN AND FIRST OFFICER NOTICED A BURNING ODOR. THE CAPTAIN AND FIRST OFFICER PUT ON THEIR O2 MASK AND DECLARED AN EMERGENCY. THE CAPTAIN ELECTED TO DIVERT TO SAT AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED PANEL 242BF IAW EMB AMM 53-01-02, PERFORMED GVI OF AC DUCTS IAW EMB AMM 21-22-05. REMOVED AND REPLACED PANEL 242CF IAW EMB AMM 53-01-02, PERFORMED GVI OF AC DUCTS IAW EMB AMM 21-22-05. REMOVED AND REPLACED PANEL 241DF IAW EMB AMM 53-01-02, PERFORMED GVI OF AC DUCTS IAW EMB AMM 21-22-05. REMOVED AND REPLACED PANEL 251DF IAW EMB AMM 53-01-02, PERFORMED GVI OF AC DUCTS IAW EMB AMM 21-22-05. REMOVED AND REPLACED PANEL 251JF IAW EMB AMM 53-01-02, PERFORMED GVI OF AC DUCTS IAW EMB AMM 21-22-05. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,315 hrs · 19,655 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW EMB 140 AMM 33050-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,201 hrs · 19,565 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND FRAME 23 CRACKED JUST BELOW FLOOR LEVEL BETWEEN STRINGERS 15 RIGHT AND 16 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME IAW EO EM-53MR-1779. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 22,201 hrs · 19,565 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND RIGHT WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE, SECOND ONE AFT CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW ATTACH ANGLE IAW EMBRAER SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 22,201 hrs · 19,565 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND BAGGAGE DOOR TORSION BAR FORWARD SUPPORT ATTACH BRACKET AT FRAME 61 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BAGGAGE DOOR TORSION BAR SUPPORT ATTACH BRACKET AT FRAME 61 IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,201 hrs · 19,565 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE LEFT SIDE VERTICAL STABILIZER TO FUSELAGE FORWARD ANGLE CRACKED ON AFT END. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ANGLE IAW EO EM-53MR-1281 PART A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,937 hrs · 18,541 cycles

DURING PS-2 INSPECTION FOUND THE LEFT AND RIGHT EXTERIOR AFT EMERGENCY LIGHT NOT ILLUMINATING. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND FOUND THE LEFT OVERWING LIGHT HAS A SHORT BLOWING FUSION POWER SUPPLY. REMOVED AND REPLACED THE LEFT OVER WING LIGHT IAW AMM 33-700-19. REMOVED AND REPLACED THE NR 4 POWER SUPPLY AND BATTERY. THE OPERATIONAL CHECK WAS GOOD IAW WC 33-700-7. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,622 hrs · 18,325 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LAST CABIN FLOOR PROXIMITY LIGHT STRIP TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY LIGHT STRIP. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT) · airframe 20,611 hrs · 18,319 cycles

ON FLIGHT 2942 DURING CRUISE THE CAPTAIN REPORTED A STRONG ELECTRICAL BURNING ODOR FOLLOWED BY FAINT SMOKE IN THE COCKPIT AFTER STARTING TO DESCEND. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 WINDSHIELD TEMPERATURE CONTROLLER IAW EMB 140 AMM 30-42-01. THE OPERATIONAL CHECK WAS GOOD AS PER EMB AMM 30-42-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 20,285 hrs · 17,997 cycles

ON FLIGHT 3309 DURING TAKEOFF THE CREW REPORTED, RECEIVED AN UNCOMMANDED YAW DAMPER ENGAGEMENT AND A YAW DAMPER FAIL MESSAGE ON EICAS. THE TAKEOFF WAS ABORTED. AFTER THE AIRCRAFT CLEARED THE RUNWAY THE YAW DAMPER DISENGAGED AND "YAW DAMPER FAIL" MESSAGE ON EICAS RE-APPEARED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE INTEGRATED COMPUTER-600 NR 1 AMM 31-42-01 THE OPERATIONAL TEST WERE GOOD IAW AMM 22-11-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — SMOKE (NR 1) · airframe 14,717 hrs · 12,185 cycles

ON TAKEOFF ROLL, APU OFF, ENG BLDS ON, PACKS ON (NORMAL CONFIG) SMOKE IN CKPT. NO SMOKE OBSERVED IN CABIN. ABORTED T/O WITH NORMAL BRAKING. REMOVED AND REPLACED NR 1 ENGINE IAW MTX WORK CARD 71-000-00, OPS CHECK GOOD AND LEAK CHECK GOOD. NO DEFECTS NOTED. RAN ENGINE IAW WC 72-700-00. NO SMOKE DETECTED IN CABIN AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — SMOKE (RIGHT) · airframe 14,715 hrs · 12,183 cycles

CREW NOTED ON CLIMB-OUT SMOKE IN CABIN. CREW GOT THE LAV SMOKE DETECTOR, FOLLOWED MANUAL AND DECLARED EMERGENCY AND RETURNED TO SDF FOR MTX. LANDED SAFELY WITH NO OTHER PROBLEMS. REMOVED AND REPLACED RT ENGINE. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,303 hrs · 11,255 cycles

CENTER OMEGA BEAM CORRODED AT FRAME 25. REMOVED CORROSION, CLEANED, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10 AND 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 13,303 hrs · 11,255 cycles

MAIN ENTRANCE DOOR INNER HANDLE BRACKET CRACKED. STOPPED DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW EMB IC 2007-145/30894, PARAGRAPH ONE AND IC2007-145/6600A. RETURNED AIRCRAFT TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,303 hrs · 11,255 cycles

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

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,303 hrs · 11,255 cycles

SERVICE DOOR SILL FOUND CORRODED. BLENDED CORROSION AREA, FILLED WITH HYSOL EA934NA RESIN, APPLIED ALODINE, PRIMER AND TOP COAT TO BLENDED AREA AND INSTALLED DOULBER IAW EMB SRM 53-21-02. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 7,169 hrs · 6,495 cycles

EMERGENCY EXIT SIGN ABOVE SEAT, 3B INOPERATIVE. RECONNECTED THE CONNECTOR PLUG AT ROW 3B EMERGENCY EXIT SIGN. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200503030) (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED BELOW SRM LIMITS. BLENDED THE DAMAGE AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR DOUBLER, FILLER, SHIMS AND REPAIR PLATE. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2681. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, STRINGER 19L WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 22, CHAPTERS 53-24-02. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN MBN INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED ARE AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE, SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-24-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. PERFORMED A CUTOUT OF THE CORRODED SECTION OF THE OMEGA BEAM. FABRICATED A REPAIR DOUBLER, FILLER TWO SHIMS AND A REPAIR PLATE. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 22, CHAPTERS 53-21-10, FIGURE 201. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED BELOW SRM LIMITS. CUT OUT SECTION OF DAMAGED OMEGA BEAM. FABRICATED A REPAIR ANGLE, FILLER, SHIMS, REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-22-10 FIGURE 201. (M)