N825AE

Part: CONTROL VALVE — FAILED (NR 2 A/C PACK) · airframe 34,826 hrs · 29,816 cycles

AFTER TAKEOFF, THE NR 2 PACK VALVE CLOSED ON EICAS. RESET IAW QRH. CREW SMELLED SLIGHT BURNING SMELL. NO ODOR NOTED IAW ETN-EM-72-034. REMOVED AND REINSTALLED THE RT DUAL TEMPERATURE CONTROL VALVE, INSTALLED A NEW SLEEVE ON CONTROL VALVE IAW AMM 21-60-01, PERFORM AN OPERATIONAL TEST IAW AMM 21-51-00, OPS CHECKED GOOD, NO ABNORMAL ODOR NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO DOOR) · airframe 34,687 hrs · 29,684 cycles

AFTER TAKE OFF "BAGGAGE DOOR" LIGHT ILLUMINATED RETURNED TO DFW "BAGGAGE DOOR LIGHT" TURNED OFF AFTER LANDING-C/A-DEFFERED BAGGAGE DOOR INDICATION PER MEL 52-5. CLEANED BAGGAGE DOOR WARNING MICROSWITCHES AND PERFORMED OPS TEST IAW EMB 140 AMM 52-76-01. OPS TEST GOOD AT THIS TIME. MEL RESTORED.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 34,679 hrs · 29,679 cycles

DURING PS-1 CHECK INSPECTION FOUND EMERGENCY FLOOR PROXIMITY STRIP LIGHT INOP-C/A-REPAIRED ELECTRICAL CONNECTOR AT AFT EMERGENCY FLOOR LIGHT STRIP PER SWPM 20-50-00 OPS CHECK GOOD

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,631 hrs · 29,633 cycles

PACK 1 OVERHEAT IN CRUISE BURNING SMELL RIGHT BEFORE CATION MESSAGE-C/A-FOUND PACK 1 SWITCH IN MANUAL MODE AND IN FULL HOT POSITION. PERFORMED PACK DUCT INSP. IAW AMM 21-51-14. PERFORMED GVI ACM INLET IAW AMM 21-51-00 NO DEFECTS NOTED PERFORMED OPS CHECK IAW AMM 21-51-00 OPS CHECK GOOD. C/W CMC DOWNLOAD IAW AMM 45-45-00 NO PACK RELATED MESSAGES NOTED. PERFORMED FIM 21-51-00-810-803 PACK 1 OVHT MESSAGE ON EICAS TRANSITORY CONDITION PERFORMED FIM 21-20-00-810-801-A. SMOKE/ABNORMAL SMELL IN COCKPIT/CABIN- NO SMELL DETECTED PERFORMED ETN-EM-72-034- ENG ODOR EVENT NO ODORS DETECTED

Part: COUPLING — LEAKING (BLEED SYS) · airframe 34,138 hrs · 29,110 cycles

BLEED 2 LEAK IMMEDIATELY AFTER TAKEOFF ASSOCIATED EICAS MESSAGE AND RED LEAK ON BLEED 2 BUTTON-C/A-INSPECTED AND FOUND ENGINE START GROUND CONNECTION COUPLING TO BE LEAKING SEVERLY. RAR GROUND CONNECTION COUPLING PER AMM 36-10-02. LEAK CHECK GOOD. NO BLEED 2 LEAK MESSAGE NOTED

Part: PITOT TUBE — CONTAMINATED · airframe 32,893 hrs · 27,902 cycles

EMERGENCY DIVERT DUE TO UNRELIABLE AIRSPEED ON ALL 3 AIRSPEED INDICATORS AT FL 300. THE ISSUE DID NOT CLEAR UP UNTIL DESCENDING THROUGH FL 190 APPROXIMATLY. DECLARED EMERGENCY FLIGHT CANCELED.-C/A-INSPECTED PITOT DRAIN PROT AND EMPTIED MOISTURE IAW E145 AMM 34-13-00-690-801. PERFORMED ADC OPS CHECK IAW E145 AMM 34-15-00-05. OPS CHECK GOOD. ACFT OK FOR SERVICE

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 32,602 hrs · 27,610 cycles

FA FLASHLIGHT BROKEN. REMOVED AND REPLACED FA FWD FLASHLIGHT IAW AMM 33-50-16 AND PERFORMED OPS CHECK IAW AMM 33-51-01. OPS CHK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,063 hrs · 27,103 cycles

FLOOR EMERGENCY LIGHT STRIPS NEAR THE LAVATORY WAS INOPERATIVE. REMOVED AND REPLACED FLOOR THE EMERGENCY LIGHTS IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,063 hrs · 27,103 cycles

FLOOR EMERGENCY LIGHT STRIPS BY THE SERVICE DOOR WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT BY SERVICE DOOR IAW AMM 33-50-12. OPS CHECKED GOOD. NO FURTHER DEFECT NOTED.

Part: RELAY — FAILED · airframe 31,886 hrs · 26,946 cycles

SMELL OF BURNING ELECTRICAL STRONGEST ON CA SIDE DURING CRUSE. REMOVED AND REPLACED RELAY K0550 IAW AMM 20-13-02. OP CHECKING GOOD IAW AMM 27-25-00 SUBTASK 710-002-A UP TO STEP J(11). PERFORMED FIM TASKS 21-20-00-810-801 (UP TO PG 3, BLOCK 33), 34-22-00-810-835 (ALL). CHECKED BEHIND ALL CONTROL PANELS, CLOCKS, KICK PANELS. RAN ENGINES AND PACKS. NO SMOKE, FUMES, BURNING SMELLS OR DEFECTS NOTED. OPC GOOD IAW AMM 33-51-01, 34-22-00, 21-20-00.

Part: BATTERY — FAILED (FLASHLIGHT) · airframe 31,874 hrs · 26,930 cycles

WEAK SMELL OF "WARM/OVERHEATED" ELECTRONICS MOSTLY AT CRUISE FL220 AND AQT CA SIDE. REMOVED AND REPLACED BOTH COCKPIT EMER FLASHLIGHT BATTERIES IAW CMM 25-60-11. (OLD BATTERIES HAD A VERY WEAK ELECTRICAL SMELL TO THEM NO FUTHER DEFECT NOTED)

Part: SMOKE DETECTOR — NO TEST (CARGO BAY) · airframe 31,720 hrs · 26,749 cycles

CARGO SMOKE DETECTOR DID NOT TEST PROPERLY. LIGHT WILL NOT ILLUMINATE DURING THE TEST BUT AFTER TEST IT WILL. REMOVED AND REPLACED THE SMOKE DETECTOR IAW AMM 26-14-01. OPS CHECKED GOOD IAW AMM 26-15-00.

Part: FITTING — DAMAGED (LT AILERON) · airframe 31,692 hrs · 26,714 cycles

LEFT AILERON PCA FITTING WAS NICKED AND GOUGED. REMOVED DAMAGE, AND FOUND TO BE OUT OF LIMITS IAW SRM 57-60-02. REMOVED AND REPLACED THE PCA FITTING IAW SRM 51-40-02, AMM 20-10-07, SRM 51-20-03,CPM 51-21-04, CPM 51-21-05, 51-21-06, AND ETN EM-51-091.

Part: FITTING — DAMAGED (RT AILERON) · airframe 31,692 hrs · 26,714 cycles

RIGHT AILERON PCA FITTING WAS NICKED AND GOUGED. REMOVED DAMAGE, AND DETERMINED TO BE OUT OF LIMITS IAW SRM 57-60-02. REMOVED THE PCA FITTING IAW SRM 51-40-02. LOCATED DRILLED AND ALODINED NEW FITTING IAW SRM 51-20-03, AND CPM 51-21-04. INSTALLED THE NEW FITTING AND RESTORED SURFACE PROTECTION IAW SRM 51-40-02, CPM 51-21-04, 51-21-05, 51-21-06, AND ETN EM-51-091.

Part: SHEAR TIE — CRACKED (FRAME 66) · airframe 31,692 hrs · 26,714 cycles

CRACK IN SHEAR CLIP AT FRAME 66 BETWEEN STRINGERS 6L AND 7L-C/A-INSTALLED EWIS PROTECTION IAW EMB SWPM 20-21-00. REMOVED LH PRECOOLER FLEXIBLE DUCT TO FOM IAW EMB 140 AMM 36-11-04. REMOVED SHEAR CLIP IAW EMB 140 SRM 51-40-02. LOCATED DRILLED AND ALODINED NEW CLIP IAW EMB 140 SRM 51-20-03 AND CPM 51-21-04. INSTALLED NEW CLIP IAW EMB SRM 53-31-04 FIG 203. APPLIED TOP COAT TO RIVET HEADS IAW EMB 140 CPM 51-21-06 AND APPLIED CIC TO SHEAR CLIP IAW CPM 51-61-00. REINSTALLED PREVIOUSLY REMOVED FLEIBLE PRECOOLER DUCT AND PERFORMED BLEED SYSTEM OPS CHECK IAW EMB 140 AMM 36-11-03 AND AMM 36-00-00. NO DEFECTS NOTED. REMOVED EWIS PROTECTION IAW EMB SWPM 20-21-00

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,692 hrs · 26,714 cycles

LEFT EMERGENCY LIGHT, NR 6 LIGHT ASSY HAD A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12, OPS CHECKED GOOD

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,692 hrs · 26,714 cycles

NUMBER 1 AISLE EMERGENCY LIGHT AND COCKPIT ENTRANCE LIGHT DID NOT OPERATE. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND BATTERY CHARGER IAW AMM 33-50-04, AND OPS CHECKED GOOD IAW AMM 33-50-00-700-801.

Part: SIGN — INOPERATIVE (LT OVERWING) · airframe 31,692 hrs · 26,714 cycles

LEFT OVERWING EXIT UPPER EMERGENCY EXIT SIGN WAS INOPERATIVE. REMOVED AND REPLACED THE SIGN IAW AMM 33-50-14. OPS CHECKED GOOD IAW 33-50-00.

Part: BEAM — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 31,692 hrs · 26,714 cycles

COROSSION IN CARGO DOOR CUTOUT LOWER THRESHOLD BEAM BETWEEN FRAMES 65 AND 68. REMOVED THE THRESHOLD BEAM IAW SRM 51-40-02, SRM 51-20-03, AND CPM 51-21-04.

Part: FLOOR SUPPORT — CORRODED (FRAMES 23-32) · corrosion level 2 · airframe 31,692 hrs · 26,714 cycles

CORROSION FOUND ON THE LT OMEGA BEAM, FRAMES 23 TO 32. BLENDED CORROSION ON THE OMEGA BEAM IAW SRM 53-22-10 AND 51-10-03, FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED, AND ALODINED A NEW OMEGA BEAM IAW SRM 51-20-03 AND CPM 51-21-04. INSTALLED THE NEW OMEGA BEAM IAW SRM 51-40-02, AND 51-40-08.

Part: SUPPORT — CRACKED (FRAMES 45-50) · airframe 31,692 hrs · 26,714 cycles

CRACKED LT OMEGA BEAM OTBD SUPPORT BETWEEN FRAMES 47 AND 48. CUT THE LT OMEGA OTBD SUPPORT IAW SRM 53-23-02. PERFORMED HFEC INSPECTION ALONG THE CUT LINE IAW NDTM 51-00-00-916-803 A, NO DEFECTS NOTED. LOCATED, DRILLED, AND ALODINED A REPAIR IAW SRM 51-20-03, 53-23-02, AND CPM 51-21-04. INSTALLED THE REPAIR IAW SRM 53-23-02, AND SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FRAME 65) · corrosion level 2 · airframe 31,692 hrs · 26,714 cycles

CORROSION IN THE LATERAL L SHAPE AT FRAME 65, AT THE LOWER DOOR STOP. REMOVED THE DAMAGED SEGMENT OF LATERAL L SHEAR TIE AT FRAME 65 BETWEEN STRINGERS 15L AND 16L IAW SRM 53-31-04, FIG 212. PERFORMED HFEC ALONG CUT OUT , NO DEFECTS NOTED IAW NDTM 51-00-00-916-801-A00. LOCATED DRILLED AND ALODINED IAW SRM 53-31-04, 51-20-03, AND CPM 51-21-04. INSTALLED SEGMENT IAW SRM 53-31-04, AND 51-40-02 .

Part: SHEAR TIE — CRACKED (FRAME 68) · airframe 31,692 hrs · 26,714 cycles

CRACKED SHEAR TIE, FRAME 68, BETWEEN STRINGERS 6L AND 7L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, AND SRM 53-31-04, FIG 205.

Part: SHEAR TIE — CRACKED (FRAME 65) · airframe 31,692 hrs · 26,714 cycles

CRACKED SHEAR AT FRAME 65, BETWEEN STRINGER 7L AND 9L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, 53-31-04, FIGURE 202, CPM 51-21-04, CPM 51-21-06, AND CPM 51-61-00.

Part: STRINGER — CRACKED (FRAMES 20) · airframe 31,692 hrs · 26,714 cycles

STRINGER 3L CRACKED AT FRAME 20, REMOVED THE STRINGER IAW SRM 51-40-02. LOCATED, DRILLED, ALODINED AND INSTALLED THE NEW STRINGER IAW SRM 51-20-03, CPM 51-21-04, CPM 51-21-05, 51-21-06, ETN EM-51-091, AND AMM 20-10-01.

Part: SHEAR TIE — CRACKED (FRAME 67) · airframe 31,692 hrs · 26,714 cycles

CRACK IN THE SHEAR TIE AT FRAME 67, BETWEEN STRINGER 6L AND 7L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, 53-31-04, FIGURE 204, CPM 51-21-04, SRM 53-31-04 CPM 51-21-06, AND CPM 51-61-00.

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 31,692 hrs · 26,714 cycles

CRACKED SHEAR TIE AT FRAME 24, BETWEEN STRINGERS 15R AND 16R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-04, CPM 51-21-06 AND ETN EM-51-091.

Part: SHEAR TIE — CRACKED (FRAME 61) · airframe 31,692 hrs · 26,714 cycles

CRACKED SHEAR TIE AT FRAME 61, BETWEEN STRINGER 6L AND 7L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-04, CPM 51-21-06 AND ETN EM -51-091.

Part: SHEAR TIE — CRACKED (FRAME 46) · airframe 31,692 hrs · 26,714 cycles

CRACKED SHEAR TIE AT FRAME 46, STRINGER 16L. REMOVED THE SHEAR TIE IAW SRM 51-40-02. LOCATED, DRILLED, ALODINED, AND INSTALLED A NEW SHEAR TIE IAW SRM 51-20-03, CPM 51-21-04, SRM 51-40-02, CPM 51-21-06, AND ETN EM-51-091.

Part: FLASHLIGHT — DAMAGED (CABIN) · airframe 31,588 hrs · 26,608 cycles

FORWARD CABIN EMER FLASHLIGHT HAS DAMAGED CONNECTOR. R & R FWD CABIN EMER FLASHLIGHT IAW WC 33-700-20. OPERATIONAL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,193 hrs · 26,231 cycles

4TH FROM FWD EMER PROXIMITY LIGHTED STRIP IS INOPERATIVE. R & R 4TH FWD EMER PROXIMITY LIGHTED STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 30,073 hrs · 25,375 cycles

STAND BY ATT CAGED BETWEEN 80 & 90 KTS ON TAKEOFF ROLL. PERFORMED FIM TASK 34-01-00-816-001-A. ATT FUNCTION SET TO TRUE VALUE IN STABILIZED CONDITION. CONSIDERED TO BE TRANSITORY CONDITION IAW FIM 34-01-00.

Part: SWITCH — BROKEN (FLASHLIGHT) · airframe 29,984 hrs · 25,300 cycles

FLIGHT ATTENDANT FLASHLIGHT BUTTON ON & OFF BROKEN OFF. LOOSE FAS SEAT. REPAIRED WITH SERVICED FLASHLIGHT SWITCH. OPERATIONS CHECKED GOOD SMP.

Part: BRAKE ASSY — LEAKING (NR 3) · airframe 29,848 hrs · 25,133 cycles

EMER BRAKE LOW PRESS ON EICAS. PARKING BRAKE NOT HOLDING PRESS. FOUND NR 3 BRAKE LEAKING & NR 4 BRAKE SHUTTLE VLV SEE NRWC 825-MIA-01756 FOR COMPLIANCE OF WORK PERFORMED. R & R NR 3 MLG BRAKE ASSEMBLY IAW 32-600-14 & 32-700-11. R & R NR 4 BRAKE SHUTTLE VLV IAW ETN ETN-EM-32-236. OPERATIONS CHECKED GOOD. SHUTTLE VLV PN 211-118 SN 3313. HOSE BRAKE PN AE713800-1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,517 hrs · 23,920 cycles

EMERGENCY CEILING LIGHT AT LT EMERGENCY EXIT INOPERATIVE. R & R LAMP IAW AMM 33-50-09. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: HYDRAULIC SYSTEM — WARNING MESSAGE · airframe 27,385 hrs · 22,965 cycles

DURING DESCENT AFTER GEAR RETRACTION, HYD SYS 1 QTY LOWERED TO THE BOTTOM OF THE GREEN RANGE, BUT WAS STILL IN THE GREEN RANGE. RECEIVED AN EICAS HYD 1 QTY LOW MESSAGE. THE QTY WAS AT THE TOP OF THE YELLOW RANGE AND STABLE. DECLARED AN EMEGENCY. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. PERFORMED VISUAL INSPECTION OF NR 1 AND NR 2 HYD SYS FOUND NO LEAKS PROCEEDED TO PERFORM HYD SERVICE OF NR 1 SYS IAW AMM 12-13-01. ACFT RETURNED TO SERVICE.

Part: ROLLER — DAMAGED (PAX DOOR) · airframe 27,048 hrs · 22,692 cycles

DURING B-INSPECTION, FOUND THE MAIN CABIN DOOR UPPER AFT FRAME ROLLER OUT OF ROUND AND DIFFICULT TO ROTATE. THE DOOR WAS DIFFICULT TO OPERATE. ACFT REMOVED FROM SERVICE. R & R ROLLER IAW AMM 53-21-02 AND OPS GOOD. ACFT RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 26,714 hrs · 22,402 cycles

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

Part: LIGHT — DAMAGED (CABIN) · airframe 26,714 hrs · 22,402 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT EMERGENCY LIGHT EXTRUSIONS (1, 2, 3, 4, 6) DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EMERGENCY LIGHT EXTRUSIONS (1, 2, 3, 4, 6) IAW EMB 140 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 26,714 hrs · 22,402 cycles

DURING B INSPECTION FOUND THE LAVATORY CENTER BEAM GUSSET CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CORRODED LAVATORY CENTER BEAM GUSSET, DRILLED AND INSTALLED NEW LAV GUSSET IAW EMB SRM 51-40-02 51-20-03. LEVEL OF CORRSION NOT SPECIFIED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TERMINAL — MISSING (CABIN) · airframe 26,714 hrs · 22,402 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT STRIP NR 5 WIRE TERMINALS MISSING ACFT SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP NR 5 WIRE TERMINALS ON ACFT SIDE IAW EMB-140 SWPM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 26,611 hrs · 22,330 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLASHLIGHT ABOVE FLIGHT ATTENDANT’S SEAT WORKING INTERMITTANT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT IAW EMB-140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD IAW 33-51-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,396 hrs · 22,118 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT WING FUSELAGE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FUSELAGE EMERGENCY LIGHT IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 26,105 hrs · 21,855 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT IN THE COCKPIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50-05-000-801-A AND 33-50-05-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 25,894 hrs · 21,655 cycles

ON FLIGHT 4463 THE CREW REPORTED THE COCKPIT FLASHLIGHT WAS INOPERATIVE AND SWAPPED WITH AFT CABIN FLASHLIGHT. THE FLIGHT CREW PLACARD PER MEL 25-53 AUTH # 120852-C MOC #498684. REPLACED AFT CABIN FLASHLIGHT ASSEMBLY IAW EMB MM 33-50-16. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,833 hrs · 21,598 cycles

ON FLIGHT 4243 THE CREW REPORTED THE AFT FLASHLIGHT WAS INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT IAW EMB-140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — DAMAGED (COCKPIT) · airframe 24,655 hrs · 20,598 cycles

DURING MAINTENANCE INSPECTION FOUND THE COCKPIT FLASHLIGHT CRADLE RETAINING TAB BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT FLASHLIGHT CRADLE IAW/EMB140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DISPLAY — FAILED (FIRST OFFICER'S) · airframe 24,550 hrs · 20,493 cycles

FLIGHT 4450 - FIRST OFFICER’S PRIMARY FLIGHT DISPLAY UNIT FAILED, TOTAL DARK AT 65 KTS, RETURNED TO GATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S PRIMARY FLIGHT DISPLAY UNIT IAW AMM 34-22-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,209 hrs · 20,157 cycles

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

Part: LAMP — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 24,099 hrs · 20,042 cycles

DURING B-INSPECTION, FOUND THE LEFT WING EMERGENCY LIGHT [LOWER] INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-07. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,091 hrs · 20,035 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY EXIT SIGN INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY EXIT DOOR SIGN IAW MM 33-50-14. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,072 hrs · 20,014 cycles

DURING B-INSPECTION, FOUND THE RIGHT EMERGENCY EXIT WINDOW OVER WING EXIT SIGN INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EXIT SIGN. OPS CHECKED GOOD IAW AMM 33-50-13. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,809 hrs · 19,796 cycles

DURING B-INSPECTION FOUND THE LEFT FORWARD OVERWING EMERGENCY LIGHT INOP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FORWARD OVERWING EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50-10. OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 23,371 hrs · 19,392 cycles

FOR FLIGHT 4392 THE CREW REPORTED THE FLASHLIGHT BEHIND CAPTAIN’S SEAT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN'S FLASHLIGHT ASSEMBLY IAW EMB-140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 233,227 hrs · 19,352 cycles

DURING MAINTENANCE BASE VISIT FOUND THE NR 4 EMERGENCY LIGHTED FLOOR STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHTED FLOOR STRIP IAW EMB AMM 33-50-12-000-801-A AND 33-50-12-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 23,108 hrs · 19,249 cycles

FOR FLIGHT 3927 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. C/W OPERATIONAL TEST OF THE FIRST OFFICER’S FLASHLIGHT IAW EMB-145 AMM 33-51-01. THE OPERATIONAL TEST WAS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 2,240 hrs · 18,637 cycles

ON FLIGHT 4157 THE CREW NOTICED THE A "BAGGAGE SMOKE" EICAS MESSAGE AND "BAGAGGE FIRE EXTG" LIGHT WOULD NOT ILLUMINATE WHEN FIRE TEST SWITCH, ON OVERHEAD PANEL, IS PRESSED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BAGGAGE SMOKE DETECTOR IAW EMB 140 AMM 26-15-01. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — BENT (FUSELAGE) · airframe 22,348 hrs · 18,586 cycles

DURING MAINTENANCE BASE VISIT WHILE DOING BIRD STRIKE REPAIR FOUND THE SHAPE Z AT FRAME 9 BENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED Z-SHAPE IAW EMBRAER STRUCTUAL REPAIR MAUNUAL 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — BENT (FUSELAGE) · airframe 22,348 hrs · 18,586 cycles

DURING MAINTENANCE BASE VISIT WHILE DOING BIRD STRIKE REPAIR FOUND THE SHAPE Z AT FRAME 9 UPPER RIGHT SIDE AT STRINGER 2 RIGHT BENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED Z MEMBER IAW EMBRAER STRUCTUAL REPAIR MANUAL 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,348 hrs · 18,586 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUIND THE RIGHT HAND FRAME 23 CRACKED AT THE FLOOR LEVEL. THE AIRCRAFT WAS REMOVED FROM SERVICE. C/A: COMPLIED WITH FRAME 23 REPAIR IAW EO EM-53MR-1808. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 20,274 hrs · 16,782 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY FLOOR STRIP LIGHT AT ROW 16 TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. DID AN OPERATION CHECK OF THE EMERGENCY LIGHT SYSTEM IAW EMB AMM 33-50-00, ALL LIGHTS INCLUDING ROW 16 (FLOOR). THE OPERATIONAL CHECK WAS GOOD, NO DEFECTS NOTED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHECK VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 19,726 hrs · 16,295 cycles

ON FLIGHT 4513 DURING CRUISE THE CREW RECEIVED A BLEED 1 LEAK WARNING ON EICAS. THE CREW FOLLOWED THE AIRCRAFT OPERATING MANUAL AND DESCENDED TO FL23/LT STAYED ON AND DESCENDED 10 FL10 AND STILL STAYED ON. THE CAPTAIN SHUT DOWN THE NR 1 ENGINE AND DIVERTED TO ELM (ELMIRA) IN HORSEADS, NY. NO OTHER ISSUES NOTED. THE CREW DID DECLARE EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED AUXILIARY POWER UNIT BLEED AIR CHECK VALVE AND GASKETS IAW AMM 36-12-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 8,565 hrs · 16,150 cycles

DURING MAINTENANCE BASE PHASE 2A INSPECTION FOUND THE FORWARD EMERGENCY FLASHLIGHT TO BE INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT ASSEMBLY LAW AMM 33-51-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 4388-5125) · corrosion level 2 · airframe 18,201 hrs · 14,908 cycles

DURING MAINTENANCE INSPECTION, FOUND THE GALLEY FORWARD DIGITAL CORRODED OVER THE LEFT OMEGA BEAM. THE AIRCRAFT WAS REMOVED FROM SERVICE. CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR SECTION AND DOUBLER IAW EM-53MR-1383. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRESSURE SWITCH — DEFECTIVE (OIL SYSTEM) · airframe 13,515 hrs · 11,189 cycles

ENGINE 2 OIL PRESS FLUX EN ROUTE TO GDL ELECTED TO RETURN TO DFW DISC. REMOVED AND REPLACED LOW OIL PRESSURE SWITCH IAW RR MM 79-33-10. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — FAILED · airframe 13,282 hrs · 11,040 cycles

RAM AIR FAIL MSG ON EICAS AFTER TAKEOFF COMPLIED WITH AOM VOL 1 RETURNED TO ABI. ADJ RT RAM AIR LINER ACTUATOR IAW EMB-140 AMM 21-25-03. SYS CKS GOOD AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — FAILED (ZONE 600) · airframe 12,520 hrs · 10,477 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT EMERGENCY EXTERNAL WING LIGHT IAW EMB 53-04-10 AND PERFORMED OPERATIONAL CHECK IAW EMB AMM 33-50-00 WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (NLG)

AFTER SELECTING GEAR UP A LOUD RUMBLING NOISE HEARD FROM AROUND NOSE GEAR AREA. SOUNDED LIKE A GEAR DOOR DID NOT CLOSE, AIRSPEED LESS THAN 200 KNOTS. REMOVED AND REPLACED NOSE LANDING GEAR PROXIMITY SWITCH. OPERATIONAL CHECKED GOOD. AIRCRAF RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 27. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: STRINGER — CHAFED (FR 52)

STRINGER 19R WAS FOUND TO BE CHAFED AT FRAME 52. BLENDED AND TREATED THE CHAFED AREA WITH EA934. FABRICATED A REPAIR ANGLE AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: STRINGER — CHAFED (FUSELAGE)

STRINGER 19L WAS FOUND TO BE CHAFED AT FRAME 52. BLENDED THE CHAFED AREA AND APPLIED EA 934. FRABRICATED A REPAIR ANGLE AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FR 27 LT)

THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 27. REMOVED THE CORROSION BY MAKING A CUT OUT. PREPARED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: SILL — CORRODED (FUSELAGE)

THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED EXISTING AND INSTALLED SERVICEABLE SILL IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. CUT OUT SECTION OF BEAM TO REMOVE CORROSION. PREPARED A DOUBLER, FILLER, SHIMS AND A PLATE. REPAIR DONE IAW SRM. (K)

Part: SILL — CORRODED (FUSELAGE)

THE BAGGAGE DOOR SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND INSTALLED SERVICEABLE SILL IAW SRM. (K)

Part: WINDSHIELD — MALFUNCTIONED (COCKPIT)

ON APPROACH, ENTERED ICING AND THEN NOTED SMOKE COMING UP BETWEEN THE TWO FORWARD WINDSHIELDS WHEN THE AI SYSTEM CAME ON. CREW DECLARED AN EMERGENCY AND AIRCRAFT WAS LANDED SAFELY WITH NO INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD AND CABLE TERMINAL END IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION, THE LEFT FLOORBEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGE SECTION OF LEFT FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB-145/1142, REV 24, CHAPTERS 53-21-10, FIGURE 202. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN MBV INSPECTION, THE CENTER FLOORBEAM BETWEEN FRAME 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGED SECTION OF THE CENTER FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB145/1142, REV 24, CHAPTER 53-22-10, FIG 201 SHEET 2. (M)

Part: SWITCH — OUT OF ADJUST (COCKPIT)

BHM - FLT 3765 - CREW REPORTED A GUSTLOCK LIGHT INDICATION DURING FLIGHT. CREW DECLARED AN EMERGENCY AND DIVERTED TO BHM. AIRCRAFT WAS LANDED WITH NO FURTHER PROBLEMS. MAINTENANCE ADJUSTED MICROSWITCH S0658 IN PEDESTAL IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)