N817AE

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,105 hrs · 34,640 cycles

ROW 1 EMERGENCY FLOOR PROX LIGHT STRIP FAILS TO ILLUMINATE.-C/A-T/S IAW WM 33-50-50. REMOVED AND REPLACED #2 INVERTER IAW AMM 33-50-11. NO FIX. FOUND WIRE BROKEN OFF OF #1 LIGHT STRIP SPLICE SP9020. REMOVED AND REPLACED MALE END OF SPLICE WITH NEW CONTACT PIN IAW SWPM 20-21-00. OPC GOOD IAW AMM 33-50-00-700-801.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,105 hrs · 34,640 cycles

#3 CABIN CEILING EMERGENCY LIGHT FAILS TO ILLUMINATE.-C/A-REMOVED AND REPLACED LAMP IN CABIN AISLE CEILING EMERGENCY LIGHT IAW AMM 33-50-08. NO FIX. T/S IAW WM 33-50-50 AND RAR #4 EPSU IAW AMM 33-50-04. NO FIX. REMOVED AND DISASSEMBLED #3 CEILING LIGHT ASSY AND CLEANED ALL ELECTRICAL CONTACTS IAW SWPM 20-50-00. REASSEMBLED AND REINSTALLED #3 CEILING LIGHT ASSY IAW AMM 33-50-08. OPC GOOD.

Part: ACM — SEIZED (AC BAY) · airframe 36,460 hrs · 34,010 cycles

SMOKE IN THE COCKPIT QRZ AT 16,000FT. VISUAL INDICATION OF SMOKE AND SMELL OF SMOKE. NO SMOKE PRESENT IN THE CABIN AREA. AFTER RUNNING COCKPIT FIRE/SMOKE/FUMES CHECKLIST SMOKE REDUCED AND AFTER LANDING AND REMOVING O2 AND SMOKE GOGGLES NO DISTINCT SMELL PRESENT ON GROUND. C/A-T/S LT SMOKE IN COCKPIT FOUND #1 PACK ACM SEIZED UP REMOVED AND REPLACED #1 PACK ACM IAW AMM 21-51-03-000-801 AND 21-51-03-400-801 AND PREFORMED EO-EM-2100-048 NO DEFECTS NOTED OPS CHECK GOOD.

Part: WIRE — BROKEN (RAM AIR VALVE) · airframe 36,399 hrs · 33,953 cycles

RAM AIR VLV FAIL CAS AFTER TAKEOFF. AIRCRAFT PACK VLV CLSD STAT. AIRCRAFT DOESN'T PRESSURIZE. DECLARED EMRG. NOT AN OVERWEIGHT LANDING. FOUND WIRE W122-0031-24 TO PIN B ON RAM AIR VALVE 1 BROKEN. REPAIRED WIRE IAW SWPM 20-21-00 & POC IAW EMB 140 AMM 21-25-01. OPC GOOD.

Part: CONNECTOR — BROKEN (CABIN) · airframe 36,065 hrs · 33,631 cycles

EMERGENCY FLOOR LIGHT STRIP AT FLOOR BOARD 251 BF WIRE CONNECTOR BROKE. C/A-REPLACED WIRE CONNECTOR AT FLOOR BOARD 251BF IAW SWPM 20-00-03 OPS CHECKS GOOD IAW AMM 33-50-00.

Part: ACM — DAMAGED (AC BAY) · airframe 36,055 hrs · 33,620 cycles

SUPPLEMENTAL FUMES AND SMOKE IN COCKPIT. JUST LEVELED OFF AT FL250 WHEN WE SMELLED SMOKE AND FUMES SMOKE WAS VISIBLE FOR ONLY A FEW MINUTES. C/A-FOUND #1 ACM INOP AND DAMAGED (INTERNAL DMG) DEFERRED #1 PACK IAW MEL 21-30 AUTH 061116D-C. FOUND DTCV TO HEAT EXCHANGER DUCT BLOWN OFF AT DTCV. REATTACHED DUCT IAW ETN-EM-21-056 OPS CHECK OK IAW AMM 21-51-00. MEL RESTORED

Part: ACM — FAILED (LEFT) · airframe 35,926 hrs · 33,486 cycles

DURING CLIMBOUT SMOKE/VAPOR FUMES IN COCKPIT.RETURNED TO DEPARTURE. PROBLEM WENT AWAY WITH PACK 1 OFF. REMOVED AND REPLACED LH AIR CYCLE MACHINE IAW EO EM-2100-048. OP CHECKED GOOD

Part: ACM — FAILED (LEFT) · airframe 35,902 hrs · 33,460 cycles

SMOKE IN THE COCKPIT AT 3000 FT RETURNED BACK TO ORF. IT APPEARS THAT PACK 1 IS INOP.-C/A-DEFERRED PACK 1 AS PER MEL 21-30. REQUIRES COMPLETION OF ETN-EM-72-034 FOR THE SMOKE/ODOR IN COCKPIT. COMPLETED ROLLS ROYCE ENGINE SUPLEMENT ETN-EM-72-034. NO SMOKE OR ODOR FOUND. PACK 1 REMAINS ON MEL. RAN ENGINES WITH CREW. INSTALLED PN FROM KVA PACK EXHAUST DUCT IAW EMB 140 AMM 21-51-02. OPS CHECKS FAILED. SUSPECT POSSIBLE ACM NOT TURNING OR DTCV FAIL. MEL REMAINS OPEN. PER ETN-EM-21-062 REMOVED AND REPLACED LH ACM IAW EO EM-2100-048. OPS CHECK AND LEAK CHECK GOOD.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 34,738 hrs · 32,391 cycles

MAIN DOOR HARD TO OPEN. LUBE MAIN PAX DOOR LOCK MECH IAW AMM 52-18-06, OPS CHK GOOD.

Part: FLASHLIGHT — ABNORMAL (CABIN) · airframe 34,535 hrs · 32,201 cycles

FA FORWARD FLASHLIGHT NOT WORKING. -C/A-REMOVED AND REPLACED FA FLASHLIGHT IAW AMM 33-50-16 OPC GOOD NO DEFECTS NOTED AT THIS TIME.

Part: HANDLE — MALFUNCTIONED (PARKING BRAKE) · airframe 34,273 hrs · 31,970 cycles

PARKING BRAKE HANDLE DOES NOT ROTATE EASILY AND CAN`T CONSISTENTLY SET THE BRAKE PROPERLY. REMOVED AND REPLACED PARKING BRAKE HANDLE IAW AMM 32-44-11. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: TRIM SWITCH — DEFECTIVE (COCKPIT) · airframe 33,983 hrs · 31,687 cycles

CA PITCH TRIM SWITCH WOULD NOT TRIM DOWN IN FLIGHT. REMOVED AND REPLACED CA PITCH TRIM SWITCH IAW AMM 27-40-03. OPC GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,973 hrs · 31,671 cycles

RT OVERWING FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED RT OVERWING FWD EMERGENCY LAMP IAW AMM 33-50-10 OPC GOOD.

Part: SKIN — DENTED (FRAMES 12-12A) · airframe 33,510 hrs · 31,235 cycles

FUSELAGE SKIN DENTED, BETWEEN FRAMES 12 AND 12A, STRINGERS 13R AND 15R. REPAIRED IAW ERS EM-53DF-3023, PART C, AND ERS EM-53MR-3239.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 33,510 hrs · 31,235 cycles

SHEAR TIE AT FRAME 80, STRINGER 7L. FOUND CRACKED APPROX. 3/4". REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (AFT CARGO DOOR) · airframe 33,510 hrs · 31,235 cycles

AFT CARGO DOOR CABLE DRUM SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED AFT CARGO DOOR CABLE DRUM SUPPORT BRACKET IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · airframe 33,510 hrs · 31,235 cycles

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

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 33,510 hrs · 31,235 cycles

RIGHT SHEAR TIE AT FRAME 80, STRINGER 7R FOUND CRACKED, APPROXIMATELY. .5 INCH. INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02.

Part: PITOT SYSTEM — CONTAMINATED · airframe 32,388 hrs · 29,853 cycles

AT FLIGHT LEVEL 360 BOTH PFDS HAD IAS AMBER INDICATION ALONG WITH SPS ADVANCED ON EICAS. ON DESCENT CAPTAINS AIRSPEED ACTED LIKE AN ALTIMETER, THEN ALL WENT NORMAL DESCENDING THROUGH 190. REMOVED WATER FROM PITOT WATER TRAPS IAW AMM 34-13-00. PERFORMED LEAKAGE TEST IAW AMM 34-13-00 IS GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,380 hrs · 29,841 cycles

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

Part: LAMP — DIM (EMERGENCY LIGHT) · airframe 32,380 hrs · 29,841 cycles

MAIN DOOR EMERGENCY LIGHT DIM. R & R DOOR EMERGENCY LAMP IAW AMM 33-50-10.OPS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 32,280 hrs · 29,753 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN-C/A-LUBED ROLLERS AND PERFORMED OPS CK OF MAIN CABIN DOOR REF AMM 52-18-00

Part: B-NUT — LOOSE (NLG STEERING) · airframe 31,288 hrs · 28,774 cycles

HYD SYS 1 FLUID LEAK UPON LANDING TRANSFER TO NRWC 817, DFW-02039, REF NRWC 817, DFW-02039. NOSE WHEEL STEERING B-NUT WAS TIGHTENED. HYD SYS NR 1 SERVICED. HYD SYS NR 1 PRESSURIZED AND BLEAD, NO LEAKS NOTED.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 30,988 hrs · 28,479 cycles

MAIN DOOR HARD TO OPEN. LUBED MAIN PASSENGER DOOR ROLLERS IAW AMM 52-00-04. OPS CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,906 hrs · 28,389 cycles

DURING MBV INSPECTION, A FOUND A CRACK AT A FASTENER HOLE ON FRAME 75 ON STRINGER 2R. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR TO CRACK AT FASTENER HOLE ON FRAME 75 ON STRINGER 2R IAW ERS-EM-53MR-2117. REPAIR MATERIALS DOUBLER 2024T3 .080, FILLER 2024T3 .063, REPAIR ANGLE 2024T3 .050, REPAIR ANGLE FILLER 2024T3 .032.

Part: FRAME — CRACKED (FRAME 23) · airframe 30,890 hrs · 28,372 cycles

DURING MBV INSPECTION, FOUND FRAME 23 PREVIOUS REPAIR, BETWEEN STRINGERS 16R & 15R CRACKED. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. R & R FRAME 23 PREVIOUS REPAIR IAW SRM 53-00-04 REPAIR 3. REPAIR MATERIALS L ANGLE, AL 7475-T761 .040.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,890 hrs · 28,372 cycles

RIGHT AFT FUSELAGE FRAME 75 FASTENER AT STRINGER 2 AREA SKIN CRACKED. PERFORMED CUT OUT AS REQUIRED TO REMOVE DAMAGE FROM FUSELAGE EXTERNAL SKIN AT FRAME 75, STRINGER 2R AREA, FABRICATED & INSTALLED FILLER, DOUBLER, SHIM & DRAG ANGLE REINFORCEMENT IAW ERS-EM-53MR-2117. SEE TASK & WIP ENTRIES FOR DETAILS.

Part: LAMP — ODOR (CABIN LIGHT) · airframe 30,274 hrs · 27,767 cycles

DURING TAXI IN, FLIGHT ATTENDANT REPORTED ELECTRICAL BURNING ODOR IN THE FWD PORTION OF CABIN. REPLACED LAMP IN COURTESY LGIHT. COURTESY LIGHT OPS GOOD IAW AMM 30-26-00-700-801-A.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 29,111 hrs · 26,779 cycles

FIRST OFFICERS EMER FLASHLIGHT CRADLE BROKEN. R & R FIRST OFFICERS EMER FLASHLIGHT SYS IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 28,344 hrs · 26,119 cycles

AFT CABIN FLASHLIGHT CRADLE BROKEN, WILL NOT HOLD FLASHLIGHT. SUPPLIED EQUIVALENT RUGGEDIZED FLASHLIGHT. DEFERRED IAW MEL 25-53. R & R AFT CABIN FLASHLIGHT CRADLE IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 28,243 hrs · 26,035 cycles

FLIGHT ATTENDANT REPORTS FLASHLIGHT, AFT, NOT CHARGING. R & R FLIGHT ATTENDANT AFT FLASHLIGHT IAW AMM 33-51-00, OPERATIONS CHECKED GOOD.

Part: DUCT — CRACKED (AC BAY) · airframe 28,230 hrs · 26,017 cycles

WHILE CLIMBING THRU APPROXIMATELY 22,000, WE HEARD A SINGLE POP SOUND. THE CABIN RATE SHOWED AN IMMEDIATE RATE OF CLIMB OF AROUND 200 FT MIN & THEN WENT TO DASHES. THE CABIN ALTITUDE STARTED TO CLIMB & PEAKED AROUND 11,000 AFTER WE INITIATED AN EMERGENCY DESCENT TO 10,000. AFTER LEVELING AT 10,000, THE PRESSURIZATION SYS WAS ABLE TO MAINTAIN A CABIN ALT OF 5900 FT. PERFORMED VISUAL INSPECTION OF PACK SYS & FOUND LT RAM AIR CHECK VLV DUCT CRACKED. FOUND GND CONNECTION VLV FLAPPER SEAL MISSING. R & R LT RAM AIR CHECK VLV DUCT IAW AMM 21-25-02. REPLACED GND CONNECTION VLV FLAPPER SEAL IAW AMM 21-22-04. PERFORMED FUNCTION TEST OF CABIN LEAKAGE IAW AMM 21-31-00, NO DEFECTS FOUND.

Part: ACM — FAILED (AC BAY) · airframe 27,963 hrs · 25,775 cycles

BLACK SMOKE COMING OUT OF GLARE SHIELD JUST ABOVE EYEBALL VENT. R & R LT ACM. OPERATIONS CHECKED GOOD AT THIS TIME IAW AMM 21-51-03.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,663 hrs · 25,499 cycles

FLIGHT ATTENDANT`S FLASHLIGHT INOPERATIVE CRADLE BROKEN. R & R FLIGHT ATTENDANT`S FLASHLIGHT SYS IAW EMB AMM 33-50-16-000-801-A & 33-50-16-400-801-A, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,614 hrs · 24,511 cycles

FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 33-50-16.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 26,473 hrs · 24,374 cycles

ON ENTERING ACFT, FOUND EMERGENCY LIGHTS WERE LEFT ON. SOME FLOOR LIGHTS WERE INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R THE EMERGENCY LIGHT BATTERY NR 1 IAW AMM 33-50-04. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (SPOILERS) · airframe 26,233 hrs · 24,139 cycles

ON FLIGHT 4250, CREW REPORTED A SPOILER FAIL MESSAGE, IN FLIGHT. SPOILER WAS NOT BEING USED WHEN IT FAILED. INDICATING OPEN WHEN CLOSED. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R RAR CONNECTORS P1166, P1167 ON LT SIDE & P1166 ON RT IAW SWPM 20-50-01. R & R LT SPOILER SWITCHES AND RT OTBD SPOILER PROXIMITY SWITCH IAW AMM 27-63-04. ACFT RETURNED TO SERVICE.

Part: COVER — DAMAGED (CABIN) · airframe 25,949 hrs · 23,914 cycles

DURING MAINTENANCE INSPECTION FOUND SEVEN EMERGENCY PROXIMITY STRIP LIGHT COVER PANEL DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SEVEN EMERGENCY PROXIMITY STRIP LIGHT COVER PANELS AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,894 hrs · 23,866 cycles

DURING MAINTENANCE INSPECTION FOUND THE BATTERY POWER SUPPLY P/N 11-0049 S/N 17155 AND THE BATTERY HOLDER ASSEMBLY P/N 11-0049 EMERGENCY LIGHTS WOULD NOT TURN ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY POWER SUPPLY AND THE BATTERY CHARGER. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,949 hrs · 25,949 cycles

DURING MAINTENANCE INSPECTION FOUND THE LAST TWO FLOOR EMERGENCY LIGHT STRIPS AFT OF THE EMERGENCY EXIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY POWER SUPPLY AND BATTERY PACK IAW EMB 140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — LOOSE (CABIN) · airframe 25,736 hrs · 23,724 cycles

ON FLIGHT 4149 THE FLIGHT ATTENDANT REPORTED THE FORWARD EMERGENCY EXIT SIGN WAS LOOSE AND FALLING OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW SCREW IAW AMM 33-50-15. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POTENTIOMETER — DEFECTIVE (NLG STEERING) · airframe 25,518 hrs · 23,548 cycles

ON FLIGHT 3297 THE CREW REPORTED THAT ON THE TAKEOFF ROLL ABOVE 80 KTS HAD UNCOMMANDED STEERING KICK TO RIGHT WITH STEER INOP EICAS MSG. HIGH SPEED ABORT. AFTER CLEARING RUNWAY AND COMPLETE STOP RE-ENGAGED STEERING TAXI BACK TO GATE, ABORTED AT 110 KTS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FEEDBACK UNIT (POTENTOIMETER) IAW AMM 32-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

1ST EMERGENCY FLOOR LIGHTING STRIP INOP. REPLACED FLOOR STRIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,967 hrs · 23,071 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT AISLE AT SEAT 6 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AISLE EMERGENCY LIGHT AT SEAT 6 IAW EMB AMM TASKS 33-50-08-000-801-A AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,779 hrs · 22,895 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT EMERGENCY LIGHT INOPERABLE AT SEAT 11A. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE INTERIOR OVERWING EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,529 hrs · 22,651 cycles

DURING B INSPECTION, FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY POWER SUPPLY UNIT IAW AE WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GASPER FAN — ODOR (AFT) · airframe 24,371 hrs · 22,500 cycles

FLIGHT 3972, THE CREW REPORTED THAT DURING CLIMB AND CRUISE, STRONG ELECTRICAL/PHOSPHORUS ODOR THROUGH OUT THE AIRCRAFT. THE ODOR DIMINISHED AFTER TURNING THE RECIRCULATION FAN OFF. AIRCRAFT LANDED WITHOUT INCIDENT & REMOVED FROM SERVICE. COMPLIED WITH FAULT ISOLATION MANUAL TASK 21-20-00-810-801-A, AIR CONDITIONING-DISTRIBUTION-SMOKE/ABNORMAL ODOR IN THE CABIN/COCKPIT-UNKNOWN SOURCE FOUND AFT GASPER FAN PRODUCING ODOR. REMOVED AND REPLACED IAW 21-23-03. OPS CHECKED GOOD, NO DEFECT NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 24,228 hrs · 22,363 cycles

ON FLIGHT 3937 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE FLIGHT CREW PLACARD PER MEL 2553 AUTH 070274-C MOC 488441. CHARGED FLASHLIGHT. THE OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — UNSERVICEABLE (CABIN) · airframe 24,210 hrs · 22,343 cycles

DURING B INSPECTION FOUND THE FORWARD CABIN EF-2C RECHARGEABLE FLASHLIGHT BOTTOM CAP O-RING SEAL DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN EF-2C RECHARGEABLE FLASHLIGHT. THE FUNCTIONAL CHECK WAS GOOD. NO OTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — UNSERVICEABLE (CABIN) · airframe 24,131 hrs · 22,272 cycles

ON FLIGHT 4150 THE CREW REPORTED THE EMERGENCY EXIT SIGN OVER EXIT ROW/ AFT PART IS COMING UNGLUED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING EXIT SIGN (AFT CEILING PANEL) IAW EMB 140 AMM 33-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: COUPLING — DEFECTIVE (TEMP CONTROL) · airframe 23,363 hrs · 21,536 cycles

ON FLIGHT 4295 PRESSURIZATION FAILED CLIMBING THROUGH 12000FT DESC TO 10000FT ATTEMPTED TO RESET PER RED ADM 1 AC WOULD NOT PRESSURIZE. THE AIRCRAFT WAS REMOVED FROM SERVICE. ON LG PAGE 3165073 REMOVED AND REPLACED COUPLING FOR DUALN TEMPERATURE CONTROL IAW EMB AMM 21-60-01 LEAK CHECK GOOD MEL RESTORED PERFORMED OPERATIONAL CHECK OF PRESSURIZATION IAW AMM 21-31-00 OPERTAIONAL WAS CHECK GOOD. THE AIRCRAFT RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,784 hrs · 21,071 cycles

DURING MAINTENANCE VISIT FOUND THE RIGHT OVERWING REAR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,410 hrs · 20,782 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 3 FLOOR STRIP EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY AND CHARGER IAW EMB AMM TASKS 33-50-04-000-801-A AND 33-50-04-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,993 hrs · 20,404 cycles

ON FLIGHT 4167 THE CREW REPORTED THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW EMB AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHT/EXIT SIGN OVER EMERGENCY EXIT ROW (ROW 11) NOT ILLUMINATING. TROUBLESHOT AND FOUND FAULTY BATTERY PACK, EMERGENCY NR 3. REMOVED AND REPLACED EMER BATTERY NR 3 IAW EMB 140 AMM 33-50-04. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: SOCKET — WORN (CABIN) · airframe 20,973 hrs · 19,584 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND RIGHT WING AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT DUE TO A WORN SOCKET IAW EMBRAER 140 AMM 33-50-10. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — DAMAGED (AILERON) · airframe 20,973 hrs · 19,584 cycles

DURING MAINTENANCE BASE VISIT FOUND LEFT AILERON OUTBOARD ACTUATOR ATTACHMENT BOLT INBOARD HAT BUSHING MIGRATING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED PCA FITTING AND DAMPNER FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CHAFED (AILERON) · airframe 20,973 hrs · 19,584 cycles

DURING MAINTENANCE BASE INSPECTION FOUND RIGHT AILERON DAMPER FITTING CHAFED FROM DAMPER ROD END. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AILERON DAMPER FITTING AND PCA FITTINGS IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CHAFED (AILERON) · airframe 20,973 hrs · 19,584 cycles

DURING MAINTENANCE BASE INSPECTION FOUND LEFT AILERON DAMPER FITTING CHAFED FROM DAMPER ROD END. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DAMPER FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 20,973 hrs · 19,584 cycles

DURING MAINTENANCE BASE VISIT FOUND UPPER CENTER WINDSHIELD CUTOUT CRACKED AT 2 EACH HANDLE ATTACH NUT PLATES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED COCKPIT OVERHEAD RIB AT 2 EACH HANDLE ATTACH NUT PLATES IAW ETN EM-53-145. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — FAILED · airframe 19,371 hrs · 18,212 cycles

ON FLIGHT 3949 DURING CRUISE THE CREW CALLED LOCAL MAINTENANCE WHILE PASSING THROUGH THUNDERSTORMS REPORTING, CREW SMELLED A STRONG ELECTRICAL/SULPHUR ODOR. THE CAUSE OF THE ODOR WAS SUSPECTED TO BE A LIGHTNING STRIKE. THE ODOR LASTED FOR A FEW MINUTES. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED LIGHTNING STRIKE WORK CARD 05-200-00 WITH NO DEFECTS NOTED AND REMOVED AND REPLACED BURNED RECIRCULATION FAN IAW AMM 21-24-01. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PITOT LINE — CRACKED (PITOT/STATIC SYS) · airframe 19,031 hrs · 17,907 cycles

ON FLIGHT 3273 IN CRUISE THE CREW REPORTED AFTER FLYING THROUGH WEATHER THE CAPTAIN AND FIRST OFFICER’S AIR DATA BECAME ERRATIC ALONG WITH THE STALL PROTECTION SYSTEM ADVANCE ON EICAS. THE CAPTAIN REPORTED AT FL360 RECEIVED AN AMBER SPS ADVANCED MESSAGE ON EICAS, 60 SECONDS LATER AP FAIL MESSAGE APPEARED FOLLOWED IN RAPID SUCCESSION IAS AND ALTITUDE ANOMALIES. THE CAPTAIN’S AIRSPEED SHOWED 240 KNOTS AT FL360, ALTIMETER WAS DECREASING TO 25,800. THE FIRST OFFICER’S AIRSPEED FELL TO 48 KNOTS, BUT ALTIMETER SHOWED 36,300. THE CREW ALSO NOTED THAT AIR TRAFFIC CONTROL CONTACTED THE AIRCRAFT STATING THE MODE C WAS INDICATING 300 HIGH COMPARED TO ASSIGNED ALTITUDE. STANDBY INSTRUMENTS WERE USED DURING THE DESCENT. THE CREW ELECTED TO DIVERT TO CRP. THE AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. ALL INSTRUMENTS WERE NORMAL UPON LANDING AT CRP. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND WATER IN CAPTAINS SIDE PITOT-STATIC LINES. DRAINED WATER VIA QUICK-DISCONNECT FITTING. CAPTAINS AIRSPEED AND ALTITUDE INDICATIONS WERE GOOD IAW AMM 34-13-15-00. FOUND CRACK IN THE NR 2 ADC PITOT HOSE. REMOVED AND REPLACED THE PITOT HOSE IAW STANDARD PRACTICES. DRAINED WATER FROM NR 2 SYSTEM VIA QUICK-DISCONNECT. NR 2 PITOT-STATIC SYSTEM LEAK CHECKS GOOD IAW 34-13-00. NR 2 ADC AIRSPEED AND ALTITUDE INDICATIONS GOOD IAW AMM 34-15-00. AUTOPILOT OPERATIONAL CHECK WAS GOOD IAW EMB 140 AMM 22-11-00. THIS AIRCRAFT IS ELIGIBLE FOR FLIGHT IN RVSM AIRSPACE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,940 hrs · 17,827 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50--10-000-801-A AND33-50-10-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — FAILED (NR 2 ENGINE) · airframe 18,539 hrs · 17,492 cycles

ON FLIGHT 3566 DURING CRUISE THE CREW REPORTED ENGINE 2 OIL QUANTITY DROPPED FROM 12 QUARTS TO 3 QUARTS FOLLOWED BY DROP OF OIL PRESSURE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO LRD LANDING WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 ENGINE AIR TURBINE STARTER MECHANICAL CARBON SEAL IAW RR MM CHAP 72-63-10. THE OPERATIONAL AND LEAK CHECK WERE GOOD. NO DEFECTS NOTED AT THIS TIME. REMOVED AND REPLACED ATS IAW EMB140 AMM 80-10-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,622 hrs · 16,687 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LEFT OUTBOARD SILL CORRODED IN THE LAVATORY AREA. THE AIRCRAFT HAS BEEN REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OUTBOARD SILL IN LAVATORY IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,622 hrs · 16,687 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LEFT WEB UNDER CARBON FIBER BEAM TO BE CORRODED AT FRAME 61. THE AIRCRAFT HAS BEEN REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT WEB UNDER CARBON FIBER BEAM AT FRAME 61 IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (AFT BULKHEAD) · airframe 17,622 hrs · 16,687 cycles

DURING MAINTENANCE INSPECTION, FOUND A CRACK ON THE RIGHT AFT BULKHEAD AROUND THE RIGHT MAIN LANDING GEAR. CRACK LENGTHS WERE 6/8 OF AN INCH AND 1 INCH. AIRCRAFT REMOVED FROM SERVICE. REPAIRED CRACKS ON RIGHT BULKHEAD AFT SECTION IAW EMB SRM 53-23-12. AIRCRAFT RETURNED TO SERVICE.

Part: OXYGEN MASK — UNWANTED DEPLOY (COCKPIT) · airframe 16,781 hrs · 15,693 cycles

ON FLIGHT 4774, CREW REPORTED O2 MASKS DEPLOYED UNCOMMENTED ON GROUND. SOME MAY HAVE ACTIVATED IN THE REAR. AIRCRAFT REMOVED FROM SERVICE. INSPECTED EACH O2 MASK AND OXYGEN GENERATOR AND STOWED IAW EMB AMM 35-20-04. ALL GENERATORS IN SERVICEABLE CONDITION. AIRCRAFT RETURNED TO SERVICE.

Part: POTENTIOMETER — INOPERATIVE (NLG STEERING) · airframe 13,533 hrs · 13,144 cycles

ON FLIGHT 4614, CREW REPORTED THAT THEY HAD AN UNCOMMANDED SWERVING BACK AND FORTH OF THE STEERING SYSTEM, ALMOST RAN OFF RUNWAY. CREW WAS ABLE TO STOP ON TAXI WAY USING RUDDER AND DIFFERENTIAL BRAKING. AIRCRAFT TOWED TO THE GATE WITH A TUG. AIRCRAFT REMOVED FROM SERVICE. UPON FURTHER TROUBLESHOOTING FOUND FEEDBACK POTENTIOMETER INOPERATIVE. REMOVED AND REPLACED FEEDBACK POTENTIOMETER IAW EMB AMM 32-50-07. OPERATIONAL CHECK GOOD. ALSO, ADJUSTED LOAD POTENTIOMETER IAW EMB AMM 32-50-05. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,828 hrs · 12,576 cycles

DURING A MBV INSPECTION, THE CARGO DOOR FWD LOWER SHEAR CLIP AT FRAME 65 WAS FOUND CORRODED. REPAIRED SHEAR CLIP IAW EMB IC2007-145/06674 DATED 1 OCT 07. AIRCRAFT RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,828 hrs · 12,576 cycles

DURING A MBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND LIMITS. REPAIRED SILL IAW EMB SRM CHAPTER 51-40-02. AIRCRAFT RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 145,554 hrs · 12,576 cycles

DURING A MBV INSPECTION, FUSELAGE FRAME BETWEEN STRINGERS 15 AND 16 RIGHT WAS FOUND TO HAVE A CRACKED FLANGE. REPAIRED THE FLANGE IAW EMB IC 2007-145/06705 DATED 27 SEPT 07. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,829 hrs · 12,576 cycles

DURING A MBV INSPECTION A PREVIOUSLY REPAIR ANGLE ON THE LT OMEGA BEAM WAS FOUND CORRODED BETWEEN 24 AND 25. REPAIRED OMEGA BEAM IAW EMB 145 SRM CHAPTER 53-00-10 AND 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,829 hrs · 12,576 cycles

DURING A MBV INSPECTION A PREVIOUS REPAIR BETWEEN FRAMES 24 AND 25 ON THE CENTER OMEGA BEAM WAS FOUND CORRODED. REMOVED EXISITING REPAIR AND REPLACE WITH NEW IAW EMB SRM 53-00-10, 51-40-02, AND 53-22-10. RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,829 hrs · 12,576 cycles

DURING A MBV INSPECTION, THE CENTER BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED OLD DOUBLER AND REPLACED WITH A NEW DOUBLER IAW EMB 145 SRM 53-21-10 STEPS 1-6. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,828 hrs · 12,576 cycles

DURING A MBV INSPECTION, THE CENTER BEAM AT FRAME 20 WAS FOUND TO BE CORRODED ON THE LT SIDE. REMOVED OLD DOUBLER AND REPLACED WITH A NEW DOUBLER IAW EMB 145 SRM 53-21-10 STEPS 1-6. AIRCRAFT RETURNED TO SERVICE

Part: RADAR — INOPERATIVE (WX SYSTEM) · airframe 12,813 hrs · 12,563 cycles

RADAR INOP IN FLIGHT DUE TO WEATHER EN ROUTE DISPATCH AND CREW ELECTED TO RETURN TO DFW. REMOVED AND REPLACED WEATHER RT UNIT, OPS CHK GOOD IAW EMB AMM 34-42-00. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,442 hrs · 12,163 cycles

RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 28 AND 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE SWITCH — FAILED (HYD PUMP)

LAX - FLT 3198 - ABORTED TAKEOFF E1 HYD PUMP FAIL AND HYD NR 1 SYSTEM FAIL. (M)

Part: HOUSING — CORRODED (NLG)

DURING MBV INSPECTION, FOUND NOSE LANDING GEAR LEFT MAIN STRUT BEARING HOUSING SHOWS SIGNS OF PITTING. REWORKED BEARING HOUSING TO WITHIN LIMITS IAW SRM 53-11-08 PAGE 101. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FR 20)

SAW - DURING CPCP INSPECTION, FOUND LEFT OMEGA BEAM CORRODED AT FRAME 20. INSTALLED DOUBLER IAW SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: HOUSING — CORRODED (NLG)

SAW - DURING MBV INSPECTION, FOUND NOSE LANDING GEAR LEFT STRUT DRAG BRACE BEARING HOUSING SHOWS SIGNS OF PITTING. REWORKED BEARING HOUSING TO WITHIN LIMITS IAW SRM 53-11-08 PAGE 101. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (SERVICE DOOR)

SAW - DURING CPCP INSPECTION, FOUND SERVICE DOOR AFT SILL HAS CORROSION. INSTALLED NEW AFT SILL PLATE IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FR 24-25)

SAW - FOUND DURING CPCP INSPECTION, LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 24-25. REPLACED DAMAGED AREA IAW SRM 53-00-01 FIG 202 AND IC2005-145/4572. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FR 18-19)

SAW - DURING CPCP INSPECTION, FOUND RIGHT HAT BEAM IS CORRODED BETWEEN FRAMES 18-19. REPLACED HAT BEAM IAW EMB IC2005-145/4638. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CAP — CORRODED (BEARING)

DURING MBV INSPECTION, FOUND NOSE LANDING GEAR RIGHT DRAG BRACE BEARING CAP HAS SIGNS OF PITTING. REMOVED NEGLIGIBLE PITTING FROM BEARING CAP FOUND TO BE IN LIMITS IAW SRM 53-11-08 PAGE 101. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP INSPECTION, FOUND RIGHT UPPER 3RD FROM FRONT SEAT TRACK CORRODED AROUND SCREW HOLES. REPLACED SEAT TRACK IAW EMB AMM 53-01-06-400-801A. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP INSPECTION, FOUND LEFT FORWARD SEAT TRACK CORRODED AROUND SCREW HOLES. REPLACED SEAT TRACK IAW EMB AMM 53-01-06-400-801-A. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP INSPECTION, FOUND LEFT UPPER 4TH SEAT TRACK FROM FRONT IS CORRODED AROUND SCREW HOLES. REPLACED SEAT TRACK IAW EMB AMM 53-01-06-400-801A. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CAP — CORRODED (RT MLG)

SAW - DURING MBV INSPECTION, FOUND RIGHT MLG AFT BEARING CAP CORRODED. REMOVED AND REPLACED RIGHT MLG AFT BEARING CAP IAW EMB 140 WORK CARD 57-200-84. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (FR 22)

DURING CPCP INSPECTION, FOUND LEFT CREASE BEAM CORRODED AT FRAME 22. INSTALLED NEW CREASE BEAM IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP INSPECTION, FOUND LEFT UPPER 5TH FROM FRONT SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: INTERCOSTAL — CORRODED (FR 20)

SAW - DURING CPCP INSPECTION, FOUND RIGHT INTERCOSTAL FOR AISLE RAMP AT FRAME 20 IS CORRODED. INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: DOUBLER — CORRODED (FR 22)

SAW - DURING CPCP INSPECTION, FOUND DOUBLER PLATE WHERE RIGHT HAT BEAM AND FLOORBEAM AT FRAME 22 MEET IS CORRODED. REPLACED DOUBLER IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP INSPECTION, FOUND RIGHT UPPER 4TH FROM FRONT SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW EMB AMM 53-01-06-400-801-A. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CAP — CORRODED (RT MLG)

SAW - DURING MBV INSPECTION, FOUND RIGHT MAIN LANDING GEAR FORWARD BEARING CAP CORRODED. REPLACED BEARING CAP IAW EMB 140 WORK CARD 57-200-84. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

CREW DISCOVERED ON PREFLIGHT THAT EMERGENCY STRIP LITES IN FLOOR FROM ROW 11 AFT WILL NOT ILLUMINATE. REPLACED NR 4 BATTERY POWER SUPPLY IAW MM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K)

Part: CONTROL MODULE — INOPERATIVE (TEMP CONTROL)

AMA - FLT 3545 - CREW REPORTED SMOKE AND AN ELECTRICAL ODOR FROM THE FIRST OFFICERS SIDE INSTRUMENT PANEL. SHUTOFF ALL POWER AND SMOKE AND ODOR STARTED TO DISSIPATE. MAINTENANCE REPLACED TEMPERATURE CONTROL MODULE IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CHARGER — INOPERATIVE (CABIN)

CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT ROWS 7 THROUGH 11 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY CHARGER IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200503041) (K)

Part: CHARGER — INOPERATIVE (CABIN) · airframe 6,607 hrs · 6,216 cycles

EMERGENCY FLOOR LIGHTS AT ROWS 7 THROUGH 11 INOPERATIVE. REPLACED NR 3 EMERGENCY BATTERY CHARGER. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200503043) (K)

Part: CONTROL PANEL — MALFUNCTIONED (FIRE WARNING)

ORD - FLT 4269 - DURING FIRE TEST NO LIGHT IN THE BAGGAGE EXTINGUISHER BOTTLE INOPERATIVE ON EICAS. REPLACED FIRE PANEL AND BAGGAGE EXTINGUISHER BOTTLE, 337000271 S/N 41573D1. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, FOUND STRINGER 19L WAS FOUND CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-21-02 FIG 201. (M)