N821AE

Part: DUCT — LEAKING (A/C PACK) · airframe 35,238 hrs · 31,293 cycles

PACK 2 VLV OVHT PACK 2 VLV CLOSED BLD 2 VLV CLOSED ON DESCENT (TWICE) AND ONCE DURING TAXI ALSO SOCK SMELL ON TAKEOFF. FOUND AIR LEAK COMING OFF Y-DUCT TO PACK VLV AND REMOVED AND REPLACED BOTH SLEVES PER AMM 21-51-02. OPC GOOD. NO ;LEAKS NOTED. NO MSG

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,019 hrs · 31,089 cycles

R/H WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED R/H WING EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,005 hrs · 31,077 cycles

BOTH LH AND RH EXTERNAL AFT EMERGENCY LIGHTS INOP-C/A-RAR BOTH LH AND RH EXTERNAL AFT EMERGENCY LIGHTS BULBS IAW EMB AMM 33--50-10-000-801-A AND 33-50-10-400-801-A NO FIX FURTHER T/S PER WM 33-50-50 RAR #4 EMERGENCY BATTERY AND CHARGER IAW W/C 33-700-19 OPC GOOD

Part: SERVO — FAILED (RUDDER) · airframe 34,493 hrs · 30,556 cycles

DURING CLIMB OUT, AROUND 2000FT AGL0 WITH AUTO PILOT OFF AND YD ON EXPERIENCED UNCOMMANDED30* ROLL TO THE RIGHT CONTINOUSLY CORRECTED WITH AILERON AND RUDDER TO REGAIN DIRECTIONAL CONTROL RUDDER PEDALS ON BOTH SIDES WERE VERY STIFF ON BOTH SIDES .RAN QRD YAW DAMP BOTH FAIL QRH PROCEDURE AFTER EICAS MSG LANDED BELOW MAX LANDING WEIGHT. R & R A/P RUDDER SERVO ASSY. IAW EMB-140 AMM 22-11-05. A/P SYS. FUNCTIONAL TEST IS GOOD IAW EMB-140 AMM 22-11-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,889 hrs · 29,971 cycles

RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. C/A-RAR RT AFT OVERWING EMERGENCY EXTERNAL LIGHT IAW AMM 33-50-10. OPC GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,683 hrs · 29,782 cycles

OVER WING EXTERNAL EMERGENCY LIGHTS INOP-C/A-REMOVED AND REPLACED #4 BATTERY PACK IAW EMB 140 AMM 33-50-04. OPC GOOD. REMOVED AND REPLACED #4 EMERGENCY LIGHTS BATTERY CHARGER IAW EMB 140 AMM 33-50-04. OPC GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,551 hrs · 29,651 cycles

BOTH AFT OVERWING EMERGENCY LIGHTS INOP. C/A-REPLACED THE NR 4 EMERGENCY BATTERY IAW AMM 33-50-04. BATTERY CHARGER ASSY P/N 11-0049 S/N 24703.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,318 hrs · 29,435 cycles

EXTERNAL EMERGENCY LIGHT TOP LT WING AND TOP RT WING INOP PER COURTESY CHECK. REMOVED AND REPLACED BATT POWER SUPPLY NR 4 AND BATT NR 4 IAW AMM 33-50-04. PERFORMED OPC IAW AMM 33-50-00. OPC GOOD. NO DEFECTS NOTED.

Part: HOLDER — DEFECTIVE (CABIN) · airframe 33,248 hrs · 29,372 cycles

FOUND LT & RT OVERWING EMERGENCY LIGHTS OUT DURING PS-1 CHECK IN THE EXTERIOR. REMOVED AND REPLACED BATTERY POWER SUPPLY HOLDER IAW AMM 33-50-04. OPC GOOD. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (OVER WING) · airframe 32,981 hrs · 29,105 cycles

LT AND RT EMERGENCY LIGHT OVER WING INOP. REMOVED AND REPLACED LT AND RT OVER WING EMERGENCY LIGHTS OPS CHECK GOOD IAW AMM 33-50-10.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 32,878 hrs · 29,006 cycles

LAST EMERGENCY FLOOR LIGHT STRIP IN CABIN HAS A BROKEN CONNECTOR-C/A-INSTALLED NEW CONNECTOR FOR EMERGENCY FLOOR LIGHT STRIP IAW EMB SWPM 20-50-00 OPC OF LIGHT STRIP GOOD

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 32,851 hrs · 28,978 cycles

DURING PS-1 FOUND RH AND LH OVER WING EMERGENCY LIGHT INOP-C/A-RAR #4 BATTERY POWER SUPPLY IAW EMB 140 AMM 33-50-04. OPC CK GOOD ON BOTH SIDE NO DEFECTS NOTED AT THIS TIME

Part: TRIM SYSTEM — INOPERATIVE (PITCH) · airframe 32,190 hrs · 28,367 cycles

PITCH TRIM BACKUP INOPERATIVE EICAS MESSAGE DURING CRUISE. CMC FAULT CODE 274M0300. PERFORMED FIM 27-43-00-810-802-A, BLOCKS 1 AND 7. RESET THE PITCH TRIM 1 AND 2 CIRCUIT BREAKERS, FAULT CLEARED. OPS CHECKED GOOD, NO DESCREPANCIES NOTED.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 32,118 hrs · 28,275 cycles

SMOKE IN COCKPIT/CABIN, PACKS ON APU BLEED, APU FAIL MSG. R&R APU IAW WC 49-800-05.

Part: APU — OIL CONSUMPTION (APU BAY) · airframe 32,087 hrs · 28,230 cycles

SMOKE IN COCKPIT/CABIN PACKS ON APU BLEED. APU FAIL MSG PRETESTED. C/W ETN-EM-72-034 AND FOUND APU OIL CONSUMPTION OUT OF LIMITS. REMOVED AND REPLACED APU IAW W/C 49-800-05.

Part: CONTROL UNIT — FAILED (SPOILER SYS) · airframe 32,064 hrs · 28,198 cycles

SPOILER FAIL ON APPROACH. PERFORMED OPS CHECK OF SPOILER SYSTEM IAW AMM 27-63-01. OPS CHECK GOOD DUE TO REPEAT ISSUE A/C WILL BE FERRIED PULLED CB F13, F14, AND F21 FOR FERRY FLIGHT PURPOSE. CB'S PUSHED BACK IN FOR T/S PURPOSES. REMOVED AND REPLACED SCU IAW AMM 1332 27-63-02. OPERATIONAL CHECK IAW AMM 1332 TASK 27-63-01-700-801-A OPS CHECK GOOD.

Part: PROXIMITY SENSOR — FAILED (SPOILER) · airframe 32,043 hrs · 28,181 cycles

SPOILER FAIL CAUTION MSG ON APPROACH. INSPECTED SPOILERS NO DEFECTS NOTED COMPLIED WITH OPS CHECK IAW AMM 27-63-01 NO FIX. REMOVED AND REPLACED LT CENTER SPOILER PROX SENSOR, REMOVED, CLEANED LT OUTBD LT INBD RT INBD RT OUTBD PROX SENSORS. OPC GOOD.

Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 32,039 hrs · 28,176 cycles

ON FINAL APPROACH, SPOILER FAIL MESSAGE ON EICAS. SPEED BRAKE LEVER WAS NOT ACTUATED WHEN MESSAGE PRESENTED. REMOVED AND REPLACED THE SPOILER CONTROL UNIT IAW AMM 27-63-0. PERFORMED AN OPS CHECK IAW AMM. OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: DOOR SEAL — TORN (EMERGENCY EXIT) · airframe 31,980 hrs · 28,118 cycles

F/O SIDE OVERWING EXIT MAKING LOUD WHISTLING NOISE REPEAT WRITE UP. FOUND RUBBER TRIM SEAL ON FO SIDE EMERGENCY DOOR TO BE TORN, REPAIRED IAW AMM TASK 52-00-01-300-801A, OPS CHK GOOD IAW AMM 21-31-00 NO LEAKS NOTED A THIS TIME.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 31,932 hrs · 28,075 cycles

AFT CABIN FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 33-51-01, OPS CHECKED GOOD.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 31,880 hrs · 28,016 cycles

NR 2 EMERGENCY EXIT LIGHT HAD ONE CONNECTOR DAMAGED, WIRE PULLED ON AIRCRAFT SIDE. INSTALLED A NEW CONNECTOR IAW SWPM 20-21-00.

Part: STRINGER — CRACKED (FRAME 75) · airframe 31,880 hrs · 28,016 cycles

STRINGER 2L WAS CRACKED AT FRAME 75. REPAIRED THE STRINGER IAW ERS-EM-53MR-3286.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 31,880 hrs · 28,016 cycles

NR 3 EMERGENCY LIGHT STRIP HAD ONE CONNECTOR REMOVED FROM WIRE ON AIRCRAFT SIDE. INSTALLED A NEW CONNECTOR IAW SWPM 20-21-00

Part: FLOOR SUPPORT — CORRODED (FRAME 54) · airframe 31,880 hrs · 28,016 cycles

LEFT OMEGA BEAM WAS CORRODED AT CROSSBEAM, FRAME 54. REPAIRED THE OMEGA BEAM IAW SRM 53-00-10.

Part: FLOOR SUPPORT — CORRODED (FRAMES 43-44) · airframe 31,880 hrs · 28,016 cycles

LEFT OMEGA BEAM CORRODED FRAMES 43 - 44. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-3278.

Part: DOOR SILL — CORRODED · airframe 31,880 hrs · 28,016 cycles

CORROSION FOUND ON THE CARGO DOOR SILL. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 54) · airframe 31,880 hrs · 28,016 cycles

CENTER OMEGA BEAM CORRODED AT CROSSBEAM FRAME 54. REPAIRED THE OMEGA BEAM IAW SRM 53-00-10.

Part: FLOOR SUPPORT — CORRODED (FRAME 38) · airframe 31,880 hrs · 28,016 cycles

CENTER OMEGA BEAM CORRODED AT CROSSBEAM FRAME 38. REPAIRED THE OMEGA BEAM IAW SRM 53-00-10.

Part: FLOOR SUPPORT — CORRODED (FRAME 38) · airframe 31,880 hrs · 28,016 cycles

LEFT OMEGA BEAM WAS CORRODED FRAME 38, REPAIRED THE OMEGA BEAM IAW SRM 53-00-10

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 31,880 hrs · 28,016 cycles

FRAME 65 SHEAR TIE CORRODED BETWEEN STRINGERS 15L - 17L. INSTALLED A NEW SHEAR TIE IAW SRM 53-31-04, ITEM 4, FIG 212.

Part: FRAME — CORRODED (FRM 65) · airframe 31,880 hrs · 28,016 cycles

FRAME 65 CORRODED AT LOWER CARGO DOOR STRIKER PLATE. BLENDED THE CORROSION IAW SRM 51-10-03. REPAIRED IAW SRM 53-31-04-AD, TABLE 104.

Part: YOKE — CRACKED (LT ENGINE) · airframe 31,880 hrs · 28,016 cycles

LEFT ENGINE FWD LOWER YOKE WAS CRACKED. REPLACED THE LT ENGINE FWD LOWER YOKE IAW EO EM-54MR-386.

Part: FLOOR SUPPORT — CORRODED (FRAME 57) · airframe 31,880 hrs · 28,016 cycles

OMEGA BEAM CORRODED AT CROSSBEAM FRAME 57. REPAIRED THE OMEGA BEAM IAW EO EM-53MR-1518, PART A.

Part: FLOOR SUPPORT — CORRODED (FRAME 57) · airframe 31,880 hrs · 28,016 cycles

CENTER OMEGA BEAM CORRODED AT CROSSBEAM FRAME 57. REPAIRED THE OMEGA BEAM IAW EO EM-53MR-1518, PART B.

Part: STRINGER — CRACKED (FRAME 75) · airframe 31,880 hrs · 28,016 cycles

STRINGER 2L WAS CRACKED AT FRAME 75. REPAIRED THE STRINGER IAW ERS-EM-53MR-3286.

Part: FLOOR SUPPORT — CORRODED (FRAME 45) · airframe 31,880 hrs · 28,016 cycles

LT OMEGA BEAM CORRODED AT CROSSBEAM FRAME 45. REPAIRED THE OMEGA BEAM BETWEEN FRAMES 43 & 44 IAW ERS-EM-53MR-3278.

Part: LIGHT — CRACKED (CABIN) · airframe 31,880 hrs · 28,016 cycles

NR 1, 2, 4, AND 6 LT EMERGENCY LIGHT STRIP WERE CRACKED. R & R THE EMERGENCY LIGHTS IAW AMM 33-50-12.

Part: FLOOR SUPPORT — CORRODED (FRAME 57) · airframe 31,880 hrs · 28,016 cycles

CENTER OMEGA BEAM CORRODED AT CROSSBEAM FRAME 57. REPAIRED THE OMEGA BEAM IAW EO EM-53MR-1518, PART B.

Part: FLOOR SUPPORT — CORRODED (FRAME 57) · airframe 31,880 hrs · 28,016 cycles

LT OMEGA BEAM CORRODED AT CROSSBEAM FRAME 57. REPAIRED THE OMEGA BEAM IAW EO EM-53MR-1518, PART A.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 31,790 hrs · 27,921 cycles

FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. SECURED FLASHLIGHT IAW SMP. OPERATIONS CHECKED GOOD.

Part: FUSE — BLOWN (CABIN) · airframe 31,623 hrs · 27,767 cycles

LEFT & RIGHT EXTERIOR OVERWING EMER LIGHTS ARE INOPERATIVE. R & R FUSE IN NR 4 EMER LIGHT POWER SUPPLY IAW RADIANT CMM 25-10-03. OPERATIONS TESTED OK IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,259 hrs · 27,458 cycles

RIGHT & LEFT OVERWING EMER LIGHT INOPERATIVE. TROUBLE SHOT IAW FIM 33-50-00-810-804-A. FOUND NR 4 EMER BATTERY CHARGER AT FAULT. R & R NR 4 BATTERY & CHARGER IAW WC CARD 33-700-19. PERFORMED EMER LIGHTING SYS OPERATIONS CHECK IAW WC 33-700-17. OPERATIONS CHECKED GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 7258.

Part: HOLDER — CRACKED (FLASHLIGHT) · airframe 31,231 hrs · 27,435 cycles

FORWARD ATTENDANTS FLASHLIGHT BASE CRACKED. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 30,925 hrs · 27,218 cycles

LEFT & RIGHT EXTERIOR AFT EMER LIGHT IS INOPERATIVE. R & R NR 4 EMER LIGHT BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONAL CHECKED GOOD. EMER LIGHTING BATTERY PN 2013-1A SN 65477.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,925 hrs · 27,218 cycles

LEFT EXTERIOR FWD EMER LIGHT IS INOPERATIVE. R & R LT EXTERIOR FWD EMER LIGHT LAMP IAW AMM 33-50-10. OPERATIONAL CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,751 hrs · 27,087 cycles

LEFT & RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R THE BULBS IAW AMM 33-50-10. OPS CHECKED FAILED. R & R BATTERY POWER ASSEMBLY IAW AMM 33-21-70. OPS CHECKED GOOD.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 30,646 hrs · 26,994 cycles

FLIGHT ATTENDANT FLASHLIGHT WORKS INTERMITTENTLY. R & R FWD FLIGHT ATTENDANT FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 30,630 hrs · 26,980 cycles

PARKING BRAKE LIGHT INDICATION OUT. RELAMPED COCKPIT PARKING BRAKE LIGHT IAW 20-13-04.

Part: ISIS — MALFUNCTIONED (COCKPIT) · airframe 30,385 hrs · 26,760 cycles

ON TAKEOFF ROLL ISIS FAILED & LOW SPEED ABORT PERFORMED. FOLLOWED AOM 1 PROCEDURE & ITEM CLEARED. ACCOMPLISHED ADJUSTMENT TEST OF INTEGRATED STANDBY INSTRUMENT SYSTEMS IAW AMM 34-01-01. SYS FOUND TO BE WORKING IN PROPER CONDITION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,088 hrs · 26,508 cycles

AISLE EMER LIGHT AT PAX 4 SEAT INOPERATIVE. R & R AISLE EMER LIGHT BULB IAW AMM 33-50-08. OPERATIONS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 29,818 hrs · 26,300 cycles

BROKEN WIRE ON FLOOR PROXIMITY STRIP EMER LIGHTS ROW 14. R & R FLOOR PROXIMITY STRIP EMER LIGHTS ROW 14 IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 29,393 hrs · 25,961 cycles

DURING LANDING, ABNORMAL BRAKING EFFECTIVENESS. BRAKES NOT STOPPING ACFT NORMALLY, LT BRAKES WARMER THAN RT BRAKES. BRAKES MAKING NOISE DURING TAXI IN. DOWNLOADED CMC NO CURRENT RELEVANT MESSAGES NOTED. CLEARED CMC IAW AMM 45-45-00. BLED NORMAL BRAKE SYS IAW AMM 32-40-00 BRAKE SYS FNC GOOD IAW AMM 32-41-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,880 hrs · 25,517 cycles

GALLEY OVERHEAD EMERGENCY LAMP INOPERATIVE. R & R GALLEY OVERHEAD EMERGENCY LIGHT LAMP IAW AMM 33-50-09-000-801-A & 33-50-09-400-801-A, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,869 hrs · 25,503 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R SERVICE DOOR EMERGENCY LIGHT BULB IAW AMM 33-50-09-000-801-A & 33-50-09-400-801-A, OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 28,551 hrs · 25,168 cycles

RIGHT WING AFT EMERGENCY LIGHT INOPERATIVE. R & R NR 4 EMERGENCY BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONS TESTED GOOD. NO FURTHER DEFECT NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,343 hrs · 24,989 cycles

DURING MAINTENANCE INSPECTION FOUND CEILING AFT EMERGENCY LIGHT INOPERATIVE BY SEAT 11A. THE ACFT WAS REMOVED FROM SERVICE. R 7 R REAR EMERGENCY BATT NR 3 IAW ERJ AMM 33-50-04, CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,061 hrs · 23,840 cycles

DURING B-INSPECTION, FOUND THE FORWARD EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LIGHT AND NR 1 EMERGENCY LIGHT BATTERY CHARGER IAW MM 33-50-04. CHARGER BATTERY, PN: BA5-0933-901, SN: C01494. THE OPS CHECK WAS GOOD IAW MM 33-50-00. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,037 hrs · 23,822 cycles

DURING MX INSP, FOUND THE TOP OVERWING EMERGENCY LIGHTS INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 4 EMERGENCY BATTERY AND CHARGER IAW W/C 33-700-19. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 27,005 hrs · 23,796 cycles

DURING MX INSP, FOUND THE LAST EMERGENCY FLOOR STRIP HAS A BROKEN WIRE AFTER REMOVED FLOOR PANEL 261BF. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LAST EMERGENCY FLOOR STRIP IAW MM 33-50-12. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — BURNED (RUDDER) · airframe 26,905 hrs · 23,716 cycles

DURING MAINTENANCE INSPECTION FOUND THE RUDDER II LOWER LEFT & RIGHT SIDES HAVE BURN MARK. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR IAW AEA EO-EM-55MR-420. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — MISSING (EMERGENCY LIGHT) · airframe 26,920 hrs · 23,733 cycles

DURING B INSPECTION, FOUND THE EMERGENCY LIGHT CONNECTOR MISSING. ACFT WAS REMOVED FROM SERVICE. REPLACED THE EMERGECNY LIGHT CONNECTOR IAW WM 91-10-02 AND SWPM 20-00-03. THE OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,666 hrs · 23,493 cycles

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

Part: INVERTER — INOPERATIVE (CABIN) · airframe 26,666 hrs · 23,493 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLOOR EMERGENCY AISLE LIGHTS AT 4 AND 5 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 5 INVERTER IAW AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR SEAL — TORN (CABIN DOOR) · airframe 26,455 hrs · 23,289 cycles

ON FLIGHT 2914 THE CREW REPORTED THE MAIN CABIN ENTRY DOOR UPPER RIGHT CORNER DOOR SEAL WAS TORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN CABIN DOOR SEAL IAW EMB 140 AMM 52-10-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,054 hrs · 22,985 cycles

DURING B INSPECTION FOUND THE NR 4 FLOOR LIGHT SRTIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 FLOOR LIGHT STRIP IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,682 hrs · 22,655 cycles

DURING B INSPECTION FOUND THE FRONT 3 EMERGENCY LIGHT STRIPS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY AND THE NR 2 EMERGENCY POWER SUPPLY IAW WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 25,449 hrs · 22,467 cycles

ON FLIGHT 2931 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED DOOR FRAME ROLLERS IAW EMB 53-21-02. THE OPERATIONAL CHECK WAS GOOD IAW 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: COUPLING — SEPARATED (RAM AIR VALVE) · airframe 25,268 hrs · 22,317 cycles

FLIGHT 2711, CREW REPORTED ON DESCENT FROM FLIGHT LEVEL 210 TO 13000, NOTICED AMBER DASHES ON EICAS CABIN RATE OF CLIMB AND CABIN ALTITUDE STARTED CLIMBING. PROCEEDED WITH CABIN PRESSURE FAIL AOM VOL1. CREW COULD NOT CONTROL CABIN ALTITUDE IN MANUAL. CABIN ALTITUDE CONTINUED TO CLIMB, CONTINUED USING CHECKLIST AND SELECTED AUTO AND "DUMP" ON CONTROLLER. CABIN ALTITUDE CLIMB TO MEET AIRCR. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND PACK 2 CONNECTION COUPLING SEPARATED AT RAM AIR CHECK VALVE. REMOVED AND REPLACED THE SERVICEABLE COUPLING IAW AMM 21-25-02. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PITOT SYSTEM — CONTAMINATED · airframe 25,266 hrs · 22,314 cycles

FLIGHT 2726, CREW REPORTED DURING DESCENT OUT OF FL370, RECEIVED "IAS" COMPARE FLAGS ON BOTH FIRST OFFICERS AND CAPTAINS PFD. CAPTAIN`S IAS WAS UNRELIABLE, SHORTLY AFTER RECEIVED AN AMBER "ALT" COMPARE FLAGS AS WELL. SELECTED NR 2 ADC ON CAPTAIN`S REVERSIONARY PANEL, EXITED IMC/ICING CONDITIONS AND DIVERTED. AFTER LANDING IN WARMER TEMP DESELECTED ADC REVERSION ALL FLGHT INSTRUMENTS APPEARED NORMAL. COMPLETED AOM VOL 1 CHECKLIST AND DECLARED AN EMERGENCY AND ELECTED TO DIVERT. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED WATER FROM CAPTAIN`S PITOT SYSTEM PER MM 34-30-00 AND PERFORMED OPS CHECK PER MM 34-15-00. OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 24,538 hrs · 24,538 cycles

ON FLIGHT 4498 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 24,427 hrs · 21,611 cycles

DURING B-INSPECTION FOUND SEAT 11C EMERGENCY EXIT SIGN LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RECONNECTED EMERGENCY EXIT SIGN CONNECTORS AT SEAT 11C IN REFERENCE WITH AMM TASKS 33-50-14-000-801-A AND 33-50-14-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BUTTON — STUCK (ICU PANEL) · airframe 24,129 hrs · 21,318 cycles

ON FLIGHT 4150 THE CREW REPORTED THE CABIN EMERGENCY BUTTON ON OVERHEAD ICU PANEL WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BUTTON PARTIALLY STUCK ON AFT FLIGHT ATTENDANT PHONE, RE-SET AS PER STANDARD PRACTICES. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 23,820 hrs · 21,074 cycles

ON FLIGHT 2996 THE FLIGHT ATTANDANT REPORTED THE MAIN CABIN DOOR WAS HARD TO CLOSE AND OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED MAIN DOOR FRAME ROLLER LUBRICATION IAW EMB 140 AMM 53-21-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,396 hrs · 20,784 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT EXIT AISLE OVERHEAD EMERGENCY (WHITE) LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EXIT AISLE OVERHEAD EMERGENCY LIGHT IAW EMB 140 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LINER — ODOR (CABIN) · airframe 23,031 hrs · 20,517 cycles

ON FLIGHT 2777 THE CREW REPORTED THAT AFTER TAKEOFF THE FLIGHT ATTENDANT REPORTED A STRONG ODOR COMING FROM THE AREA AROUND THE MAIN CABIN DOOR. NO SMOKE WAS NOTED. THE CREW ELECTED TO RETURN TO DFW AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ODOR TO COME FROM MAIN DOOR LINER. CLEANED MAIN DOOR LINER AND SURROUNDING INTERIOR LINING IAW AMM 25-00-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,852 hrs · 20,374 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT FORWARD FUSELAGE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FORWARD FUSELAGE EMERGENCY LIGHT LAMP IAW AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,263 hrs · 19,903 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT FRAME 23 CRACKED AT STRINGER 15. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 IAW EO EM-53MR-1808. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,086 hrs · 18,914 cycles

FOR FLIGHT 2712 MAINTENANCE REPORTED THE SERVICE DOOR EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR CEILING PANEL EMERGENCY LIGHT IAW EMB 140 AML 33-26-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — LACK OF LUBE (PAX DOOR) · airframe 19,106 hrs · 17,357 cycles

ON FLIGHT 3903 THE CREW REPORTED THE PASSENGER PAX DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED DIRTY FRAME AND PASSENGER DOOR SEAL AND LUBRICATED IAW EMB 140 AMM 52-18-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUIDE — LACK OF LUBE (PAX DOOR) · airframe 19,004 hrs · 17,261 cycles

FOR FLIGHT 3988 THE CREW REPORTED THAT THE PASSENGER DOOR IS CATCHING AND NOT OPENING FREELY WHEN OPENED. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED THE MAIN DOOR FRAME ROUTERS IAW EMB 140 AMM P/T 53-21-02. THE DOOR OPERATIONAL CHECK WAS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 18,967 hrs · 17,221 cycles

ON FLIGHT 4048 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS VERY HARD TO OPEN. NOTICED UPPER STOPS DRAGGING ON UPPER FUSELAGE STOPS WHEN OPENING & CLOSING DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ROLLERS BINDING. LUBED ROLLERS & SEALS IAW EMB-140 53-21-02 AMM AND 52-18-00 AMM, THE OPERATIONAL CHECK WAS GOOD. NO PARTS REMOVED OR REPLACED. NO FURTHER DEFECTS NOTED AT THIS CURRENT TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRIM PANEL — LOOSE (CABIN DOOR) · airframe 18,945 hrs · 17,203 cycles

FOR FLIGHT 4244 PRIOR TO FLIGHT THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND DOOR TRIM LOOSE AND INTERFERING WITH DOOR OPERATION. RE-SECURED TRIM AND THE OPERATIONAL CHECK WAS GOOD IAW EMB MM 52-18-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACTUATOR — INOPERATIVE (NLG DOOR) · airframe 18,214 hrs · 16,509 cycles

SUPPLEMENTAL INFORMATION - ON FLIGHT 4339 DURING DESCENT THE CREW REPORTED THAT WHEN EXTENDING THE GEAR RECEIVED A LANDING GEAR DISAGREE MESSAGE ON EICAS. THE LANDING GEAR POSITION INDICATION WAS GREEN. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED EXTENSION / RETRACTION OF LANDING GEAR MULTIPLE TIMES IAW EMB AMM 32-30-00. REMOVED AND REPLACED THE LEFT NOSE LANDING GEAR DOOR ACTUATOR IAW EMB 140 AMM 32-33-01. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 17,751 hrs · 16,055 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT OMEGA BEAM AT FRAMES 46-52 L-ANGLE SUPPORT CRACKED. AIRCRAFT HAS BEEN REMOVED FROM SERVICE.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 17,751 hrs · 16,055 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT OMEGA BEAM AT FRAMES 46-52 L-ANGLE SUPPORT CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW RIGHT OMEGA L-ANGLE SUPPORT BETWEEN FRAMES 46-52 IAW EMB 145 SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 17,751 hrs · 16,055 cycles

DURING MAINTENANCE INSPECTION REPORTED DENT WITH CREASE IN RIGHT FUSELAGE 1 BETWEEN FRAMES 67-68 AND ST 17R AND 18R. AIRCRAFT REMOVED FROM SERVICE. REPAIRED DENT WITH CREASE IAW EMB 53MR-1368. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,751 hrs · 16,055 cycles

DURING MAIN BASE VISIT INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AROUND THE CARBON CROSSBEAM FORWARD OF FRAME 27. AIRCRAFT REMOVED FROM SERVICE. REPAIRED THE LEFT OMEGA BEAM AROUND CARBON CROSSBEAM AT FORWARD OF FRAME 27 IAW EMB 145 SRM, 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,751 hrs · 16,055 cycles

DURING MAIN BASE VISIT INSPECTION FOUND THE CENTER OMEGA BEAM CORRODED AROUND THE CARBON CROSSBEAM FORWARD OF FRAME 27. AIRCRAFT REMOVED FROM SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,751 hrs · 16,055 cycles

DURING MAIN BASE VISIT INSPECTION FOUND THE CENTER OMEGA BEAM CORRODED AROUND THE CARBON CROSSBEAM FORWARD OF FRAME 27. AIRCRAFT REMOVED FROM SERVICE. REPAIRED THE CENTER OMEGA BEAM FORWARD OF FRAME 27 AND REINSTALLED CARBON CROSSBEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,751 hrs · 16,055 cycles

DURING MAIN BASE VISIT INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AROUND THE CARBON CROSSBEAM FORWARD OF FRAME 27. AIRCRAFT REMOVED FROM SERVICE.

Part: BRAKE ASSY — DISINTEGRATED (NR 3)

ON FLIGHT 3127, CREW REPORTED ON TAXI OUT THE BRAKE DEGRADE/BRAKE LO PRESS AND HYD SYS 2 AT BOTTOM OF YELLOW BAND AND EVIDENCE OF HYDRAULIC LEAK AT RT MAIN LANDING AREA. AIRCRAFT REMOVED FROM SERVICE C/A: INSPECTED AND FOUND NR 3 BRAKE HAD DISINTEGRATED REMOVED AND REPLACED NR 3 BRAKE ASSY. AC RETURNED TO SERVICE. (K)

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 13,727 hrs · 11,771 cycles

AIRCRAFT WAS RETURNING TO FIELD WITH A TRIM PROBLEM CREW REPORTED ON THE GROUND THAT THE MAIN PITCH TRIM WAS INOP FOLLOWED THE AOM RETURNED TO LAX. REMOVE AND REPLACE HSCU IAW EMB 140 AMM 27-40-01, OPS CHK GOOD. AIRCRAFT RETURN TO SERVICE.

Part: PROXIMITY SENSOR — FAILED (ZONE 200) · airframe 13,344 hrs · 11,347 cycles

ABNORMALLY LOUD SQUEAL FROM FRONT OF AIRCRAFT, POST INSPECTION FOUND NOSE LANDING GEAR DOOR SEQUENCE PROXIMITY SHOWED IN CLOSE POSITION. REMOVED AND REPLACED NOSE LANDING GEAR DOOR SEQUENCE PROXIMITY SENSOR IAW EMB 32-63-03. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SUPPORT BRACKET — CRACKED (ZONE 800) · airframe 13,157 hrs · 11,141 cycles

MAIN DOOR HANDLE BRACKET CRACKED. REPAIRED DOOR BRACKET IAW EMB IC2007-145/05000 DATED JULY 24, 2007.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,157 hrs · 11,141 cycles

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

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,157 hrs · 11,141 cycles

LEFT OMEGA BEAM CORRODED AT FRAME 20. REPAIRED CORRODED AREA IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO COMPT)

CARGO SMOKE LIGHT ILLUMINATED IN FLIGHT, FOLLOWED AOM AND DISCHARGED FIRE BOTTLES AND DECLARED EMERGENCY AND DIVERTED. REPLACED CARGO FIRE BOTTLES AND BOTH CARGO SMOKE DETECTORS. PERFORMED COMPLETE OPERATIONAL CHECK OF SYSTEM WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (K)

Part: FITTING — DAMAGED (RT WING AILERON)

ABI - THE RIGHT AILERON PCA FITTING INBOARD BUSHING HOLE WAS FOUND DAMAGED. REMOVED AND THE EXISTING PCA FITTING. INSTALLED NEW PCA FITTING IAW EMB 145 SRM, SRM EMB-145/1142 REV 30, CHAPTERS 51-40-02 AND EMB REPAIR STATEMENT IC2005-145/4844 DATED SEPT 2, 2002 PARA 1. (M)

Part: SILL — CORRODED (SERVICE DOOR)

ABI - THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE SERVICE DOOR SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM, SRM EMB145/1142 REV 30, CHAPTERS 51-40-02 AND 51-20-01. (M)

Part: LIGHT — ODOR (PAX DOOR)

CREW REPORTED A BURNING ODOR IN AIRCRAFT. MAINTENANCE FOUND THE ODOR COMING FROM THE PASSENGER DOOR ENTRY LIGHT. LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — INOPERATIVE (SPOILERS)

LAX - FLT 3159 - DURING CRUISE FLIGHT CREW REPORTED AN UNCOMMANDED DEPLOYMENT OF SPOILERS AT HIGH SPEED RESULTING IN A 15 DEGREE BANK TO THE RIGHT. MAINTENANCE REMOVED AND REPLACED THE SPOILER CONTROL UNIT IAW EMB MM. AIRCRAFT WAS RELEASED FOR AND PASSED A FUNCTIONAL CHECK FLIGHT. AIRCRAFT WAS THEN RETURNED TO SERVICE (M)

Part: ODOR — DETECTED (CABIN)

DURING APU START, THE APU FAILED TO START. WHEN BATTERY SWITCHES WERE RETURNED TO AUTO CREW REPORTED A STRONG BURNING ELECTRICAL ODOR. MEL WAS ISSUED AT THIS TIME. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AN OPERATIONAL CHECK OF THE APU SYSTEM WAS COMPLIED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

CREW REPORTED THE EMERGENCY LIGHTING BREAKER POPS OUT. DURING TROUBLESHOOTING MAINTENANCE FOUND THE NR 1 EMERGENCY BATTERY WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT)

LAX - FLT 3160 - EMERGENCY LIGHTS CB POPPED WILL NOT RESET AND EXIT LIGHT FOR MAIN ENTRANCE DOOR WILL NOT GO OUT. RAI NR 1 EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW EMB 140 AMM 33-50-04. OPS CHECK GOOD. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 22, CHAPTERS 53-24-02 AND EMB IC2003-145/3093A. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, THE CENTER FLOORBEAM BETWEEN FRAMES 24 AND 25 AS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGE SECTION OF THE CETNER FLOORBEAM, CLEANED, AND TREATED THE REPAIR AREA. FABRICATED A EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB, EMB 145/1142 REV 22, CHAPTER 52-3-22-10 FIG 201, SHEET 2 CPM 51-21-04, 51-21-05, 51-21-06 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING A MBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMTIS. CUT OUT DAMAGE SECTION OF BEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142, REV 22, CHAPTER 53-21-10 FIG 201 AND CPM 51-61-00. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING A MBV INSPECTION, FOUND STRINGER 19L WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142, REV 22, CHAPTER 53-24-02 AND EMB IC2003-145/3093A. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

RIC - FLT 4128 - DURING CLIMB AT ABOUT 10,000 FEET, CREW NOTED FIRST OFFICER WINDSHIELD ARCING SHORTLY AFTER HEAT WAS SELECTED OFF THE WINDSHIELD STARTED TO SHATTER. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITH NO FURTHER PROBLEMS REPORTED. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: TIRE — BLOWN (RT MLG)

PHX - FLT 3420 - DURING TAKEOFF ROLL, CREW FELT A SHUDDERING FROM RIGHT SIDE OF AIRCRAFT DUE TO A TIRE BLOW OUT. CREW TAXIED AIRCRAFT OFF THE RUNWAY AND DEPLANED THE PASSENGERS WITH NO FURTHER INCIDENTS REPORTED. AFTER POST FLIGHT INSPECTION MAINTENANCE NOTED DAMAGE TO RIGHT MLG DOOR, BOTH NR 3 AND 4 TIRES WERE OFF THEIR RIMS, RUBBER MARKS ON RIGHT SIDE OF FUSELAGE, AND POSSIBLE INGESTION INTO NR 2 ENGINE. (M)