N802AE

Part: VALVE — DEFECTIVE (GROUND AIR) · airframe 32,070 hrs · 27,195 cycles

AUTO & MANUAL PRESSURIZATION INOPERATIVE. MAX DELTA P ACHIEVED DURING FLIGHT .4 PSI ALL AOM 1 PROCEDURES ACCOMPLISHED. R & R GND CONNECTION VLV IAW AMM 21-22-04. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 31,763 hrs · 26,979 cycles

BRAKE ON LIGHT WILL NOT ILLUMINATE. REPLACED PARK BRAKE LIGHT IAW AMM 20-13-04 & RESET EMER BRAKE CB. OPERATIONS CHECKED GOOD IAW AMM 32-44-11. BULBS USED FROM ACFT KIT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,178 hrs · 26,473 cycles

RIGHT WING TO FUSELAGE FAIRING FWD EMER LIGHT INOPERATIVE. R & R RT WING TO FUSELAGE FAIRING FWD EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LAMP — OUT OF POSITION (EMERGENCY LIGHT) · airframe 30,816 hrs · 26,091 cycles

LEFT SIDE EMERGENCY LIGHTS AFT LIGHT IS OUT. REPOSITIONED LAMP IAW AMM 33-50-10, LIGHT ILLUMINATES, OPS CHECKED GOOD.

Part: AUDIO PANEL — FAILED (COCKPIT) · airframe 30,752 hrs · 26,041 cycles

DURING DESCENT INTO ABI FIRST OFFICER`S ACP APPEARED TO SHORT OUT WITH STATIC NOISE IN FIRST OFFICER`S SPEAKER & HEADSET. ALSO STRONG SMELL OF BURNING ELEC CIRCUITS. R & R FIRST OFFICER'S DAP IAW AMM 23-51-01, 23-51-00. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 30,535 hrs · 25,830 cycles

FLASHLIGHT ABOVE FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. R & R FLASHLIGHT ASSEMBLY IAW AMM 25-60-11, OPERATIONS CHECKED GOOD.

Part: SEALANT — LOOSE (EMERGENCY LIGHT) · airframe 30,344 hrs · 25,650 cycles

CA SIDE OVERWING EMERGENCY LIGHT SEALANT COMING OFF. RE-SEALED EMERGENCY LIGHT SLEEVE IAW 140 MM 51-00-00 SRM.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 29,726 hrs · 25,081 cycles

F/A REAR FLASHLIGHT HOLDER BROKEN. REPLACED AND OPS CHECK AFT F/A FLASH LIGHT BRACKET IAW AMM 33-50-16. OPS CHECK GOOD.

Part: WHEEL — ABNORMAL (NLG) · airframe 29,106 hrs · 24,558 cycles

THE CREW ABORTED TAKEOFF DUE TO EXCESSIVE NOSE WHEEL SHIMMY ON TAKEOFF ROLL OVER 80 KTS. ACFT REMOVED FROM SERVICE. COMPLIED WITH HIGH SPEED TAXI. NO EXCESSIVE NOSE WHEEL SHIMMEY. ACFT IS OK FOR SERVICE.

Part: DOOR — BINDING (MAIN PAX) · airframe 29,013 hrs · 24,488 cycles

DURING MX INSPECTION, FOUND MAIN PASSENGER DOOR HARD TO OPEN. ACFT REMOVED FROM SERVICE. ADJUSTED AFT UPPER STOP AND LUBED DOOR IAW 52-18-00. OPS CHECKED AND OPENING PRESSURE ON DOOR HANDLE WAS WITHIN ALLOWABLE LIMITS. ACFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,800 hrs · 24,308 cycles

DURING B INSPECTION FOUND THE NR 4 AND NR 5 FLOOR EMERGENGY LIGHT STRIPS INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 3 EMERGENCY BATTERY AND CHARGER ASSY IAW W/C 33-700-19. THE OPS CHECK WAS GOOD IAW AE WC 33-700-17. THE ACFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 28,489 hrs · 24,049 cycles

ON FLIGHT 4263 THE CREW REPORTED THE CABIN MAIN DOOR WAS HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBRICATED DOOR ROLLER IAW EMB 140 AMM STANDARD PRATICES. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 28,256 hrs · 23,836 cycles

ON FLIGHT 3987 FOUND MAIN CABIN DOOR HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVE FROM SERVICE. LUBRICATED MAIN CABIN DOOR GUIDE ROLLERS AND PERFORMED MAIN DOOR INTERNAL ACTUATING HANDLE TEST IAW EMB AMM 52-18-00. OPS CHECK GOOD FOUND TO BE WITHIN LIMITS. THE AIRCRAFT RETURN TO SERVICE.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 27,911 hrs · 23,533 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT FORWARD FUSELAGE TO VERTICAL DRAG ANGLE HAS 2 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-53MR-1281 PART B. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,911 hrs · 23,533 cycles

DURING MAINTENANCE INSPECTION FOUND LEFT REAR FUSELAGE I SKIN ABOVE FRAME 75 CRACKED BEYOND THE LIMITS OF THE SRM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-53MR-2064. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,915 hrs · 23,537 cycles

DURING MAINTENANCE INSPECTION FOUND THE LAST 3 CENTER AISLE EMERGENCY LIGHT STRIPS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 8 DC/AC INVERTER IAW EMB 140 AMM 33-50-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED · airframe 27,915 hrs · 23,537 cycles

FRAME 23, CRACKED BETWEEN STR 15R AND 16R. REPAIRED FRAME 23 BETWEEN STR 15R AND 16R IAW AEA EO EM-53MR-1808.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 27,915 hrs · 23,537 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — CUT (FUSELAGE) · airframe 27,915 hrs · 23,537 cycles

DURING B INSPECTION FOUND THE PASSENGER DOOR FRAME SEAL CUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN PASSENGER DOOR FRAME SEAL IAW EMB 140 AMM 53-21-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (CARGO DOOR) · airframe 27,915 hrs · 23,537 cycles

CARGO DOOR SHEAR TIE AT FRAME 65 CORRODED. REPAIRED SHEAR TIE IAW AEA EO-EM53-MR-1129.

Part: CONNECTOR — BROKEN (CABIN) · airframe 27,915 hrs · 23,537 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT STRIP 3 CONNECTOR BETWEEN FRAME 34 AND FRAME 35 BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE EMERGENCY LIGHT STRIP 3 CONNECTOR BETWEEN FRAME 34 AND FRAME 35 IAW EMB 140 SWPM 20-00-03, 20-21-00 AND 20-50-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,689 hrs · 23,083 cycles

DURING MAINTENANCE INSPECTION, FOUND THE EXTERIOR RIGHT AFT EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EXTERIOR RIGHT AFT EMERGENCY LIGHT IAW 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: GASPER FAN — MALFUNCTIONED (CABIN) · airframe 26,636 hrs · 22,379 cycles

ON FLIGHT 2897 THE FLIGHT ATTENDANT REPORTED A LIGHT ODOR OF SMOKE IN MID CABIN FOR A SHORT TIME. THE ODOR WAS ALSO PRESENT IN THE COCKPIT. THE ODOR WAS NOT ELECTIRCAL AND LASTED 30 SECONDS. THE ODOR REPEATED ON FINAL INTO DFW. THE FLIGHT ATTENDANT DESCRIBED THE ODOR LIKE A CIGARETTE OR DUST BURNING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED GASPER FAN AS PER EMB 140 AMM 21-23-03 DUE TO ABNORMAL NOISE. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PANEL — DAMAGED (MAIN DOOR) · airframe 26,377 hrs · 22,190 cycles

DURING B INSPECTION, FOUND THE MAIN DOOR EMERGENCY LIGHT COVER PANEL HAS DIME SIZE HOLE NEXT TO LIGHT ASSEMBLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT COVER PANEL PER EMB 140 AMM 25-23-04. EMERGENCY LIGHTS OPERATIONAL CHECK WAS GOOD PER EMB 140 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UPLOCK — INOPERATIVE (RT MLG) · airframe 25,971 hrs · 21,900 cycles

ON FLIGHT 3366 THE CREW REPORTED THAT AFTER TAKEOFF WHEN GEAR WAS SELECT DUP, GOT A LANDING/DISAGREE MESSAGE RIGHT GEAR SHOWED UNSAFE. COMPLIED WITH AOM PROCEDURES AND DECLARED EMERGENCY AND RETURNED TO CAE NO OTHER PROBLEMS NOTED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED RIGHT MAIN LANDING GEAR UPLOCK BOX IAW MM 32-33-10. THE OPERATIONAL CHECK WAS GOOD IAW MM 32-30-00 NO LEAKS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR SEAL — TORN (CABIN) · airframe 25,905 hrs · 21,852 cycles

FOR FLIGHT 3421 THE GATE AGENT REPORTED THE CABIN DOOR SEAL (FRAME SIDE) HAS A TEAR ON UPPER SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR ON MAIN DOOR FRAME RUBBER SEAL (UPPER TRAILING EDGE) IAW AMM 53-21-01. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 24,995 hrs · 21,119 cycles

TRIED TO START THE APU WITH THE GPU. THE APU DID NOT START & THEN A BURNING SMELL WAS PRESENT IN THE COCKPIT. RESET GPU. STARTED APU IAW EMB GHC. NO DEFECTS NOTED.

Part: LIGHT — NOT SEATED (CABIN) · airframe 24,855 hrs · 21,021 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT AND RIGHT EMERGENCY LIGHT ABOVE WING INOPERABLE. FOUND THE LIGHT IN FRONT OF THE LEFT WING EMERGENCY LIGHT INOPERABLE. FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESEATED THE LEFT AND RIGHT EMERGECNY LIGHT ABOVE WING IAW EMB 140 AMM. RE-SEATED THE LIGHT BULB IN FRONT OF LEFT WING EMERGENCY LIGHT IAW EMB 140 AMM 33-50-07. RE-SEATED THE BULB AT MAIN DOOR EMERGENCY LIGHT IAW EMB 140 AMM 33-50-06. ALL PARTS WERE LOOSE AND NEEDED ADJUSTMENT ONLY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,361 hrs · 20,592 cycles

FOR FLIGHT 4167 DURING INSPECTION FOUND THE FRONT EMERGENCY FLOOR PROXIMITY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FRONT EMERGENCY FLOOR PROXIMITY LIGHT IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,254 hrs · 19,741 cycles

FOR FLIGHT 2712 DURING PREFLIGHT INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT IAW EMB 140 AMM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 22,982 hrs · 145,471 cycles

WHILE ON THE RAMP THE AIRCRAFT WAS STRUCK BY A DEICE TRUCK NEAR THE SERVICE DOOR. SKIN HAS SEVERAL DENTS ON FRAME 22 BETWEEN STRINGERS 20 AND 18. THE SHEAR CLIP FROM 18 TO 19 CRACKED. SHEAR CLIP FROM 19 TO 20 WAS DENTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FUSELAGE IAW EO EM-53MR-1776.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,946 hrs · 19,473 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND CENTER SERVICE DOOR SILL TO HAVE CORROSION AROUND THE NUT PLATES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW CENTER SERVICE DOOR SILL IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,946 hrs · 19,473 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT OMEGA BEAM BETWEEN FRAMES 59-60 TO HAVE CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIR TO THE LEFT OMEGA BEAM BETWEEN FRAMES 59-60 IAW EO EM-53MR-1518 PART A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,946 hrs · 19,473 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT OMEGA BEAM CORRODED (FORWARD AND AFTWARD OF FRAME 20 ON A PREVIOUS REPAIR). THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED DOUBLER ON THE LEFT OMEGA BEAM AT FRAME 20 IAW EMBRAER SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,946 hrs · 19,473 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND RIGHT FRAME 23 CRACKED AT THE FLOOR LEVEL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED CRACKED FRAME IAW EO EM-53MR-1759. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,946 hrs · 19,473 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT OMEGA BEAM AT FRAME 27 TO HAVE CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT OMEGA BEAM AT FRAME 27 IAW EMBRAER SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,946 hrs · 19,473 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT OMEGA BEAM FORWARD OF FRAME 25 AT THE CARBON CROSSMEMBER TO HAVE CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED REPAIR DOUBLER IAW EMBRAER SRM 53-00-10 AND 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (VHF COMM) · airframe 22,609 hrs · 19,196 cycles

FOR FLIGHT 2855 SOC REPORTED THE CREW LOST COMMUNICATION RADIOS 1 & 2, WOULD NOT TRANSMIT. THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. AFTER TROUBLESHOOTING CANNOT DUPLICATE PROBLEM. BOTH ICUS WELL SEATED. BOTH VHF ANTENNA’S HAVE NO VISIBLE DEFECTS. THE OPERATIONAL CHECK OF COMMUNICATION 1 & 2 RADIOS WAS GOOD IAW AMM 23-12-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,198 hrs · 18,033 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT 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 33-50-07-000-801A AND 33-00-07-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (RT MLG) · airframe 20,412 hrs · 17,367 cycles

ON FLIGHT 4602 AFTER TAKEOFF THE CREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. COULD NOT SELECT GEAR UP. THE CREW ELECTED TO RETURN TO BOS. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT WEIGHT ON WHEELS SWITCH IAW EMB 140 AMM 32-61-02. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (LT MLG) · airframe 20,407 hrs · 17,362 cycles

ON FLIGHT 4694 AFTER TAKEOFF THE CREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. THE LANDING GEAR WAS NOT RETRACTED. THE CREW ELECTED TO RETURN TO JFK. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN LANDING FORWARD WEIGHT ON WHEELS PROXIMITY SWITCH IAW EMB 140 AMM 32-63-00. OPERATIONAL CHECK WAS GOOD. ALSO REMOVED BLOCKAGE FROM RIGHT MAIN LANDING AFT PROXIMITY WEIGHT ON WHEELS SWITCH TARGET. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (LT MLG) · airframe 20,407 hrs · 17,362 cycles

ON FLIGHT 4455 AFTER TAKEOFF THE CREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE AND A WEIGHT ON WHEEL INOPERABLE MESSAGE ON EICAS. THE CREW ELECTED TO RETURN TO JFK. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT ARM PROXIMITY SWITCH IAW EMB AMM 32-63-01. REMOVED AND REPLACED DOWNLOCK PROXIMITY SWITCH HARNESS AS PER AMM 20-50-00. RETRACTION AND EXTENSION CHECK FOUND TO BE WORKING. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 19,449 hrs · 16,525 cycles

ON FLIGHT 4913, DURING CLIMB OUT THE OUTER PANE OF THE FIRST OFFICERS COCKPIT WINDSHIELD SHATTERED. THE CREW ELECTED TO RETURN TO LGA. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERS COCKPIT WINDSHIELD IAW AMM 5610-01 MANUAL. COMPLIED UP TO STEP J OF AMM 56-10-01 MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 19,449 hrs · 16,255 cycles

ON FLIGHT 4913 DURING CLIMBOUT THE OUTER PANE OF THE FIRST OFFICERS COCKPIT WINDSHIELD SHATTERED. THE CREW ELECTED TO RETURN TO LGA. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERS COCKPIT WINDSHIELD IAW AMM 5610-01. COMPLIED UP TO STEP J OF AMM 56-10-01. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,346 hrs · 15,610 cycles

DURING HMBV THE LEFT OMEGA BEAM AT FRAME 27 WAS FOUND CORRODED. CUT OUT THE DAMAGED AREA. PREPARED A 1.6" X 12.25" FILLER FROM P/N EPNEM53EP54703 AND A 15.5" X 3.6" DOUBLER FROM P/N EPNEM53EP54701. CLEANED, TREATED AND INSTALLED REPAIR PIECES IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,346 hrs · 15,610 cycles

DURING HMBV THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED SERVICE DOOR SILL IN TWO AREAS. ALODINE AND PRIMED BLENDED AREA. FILLED BLENDED AREA USING EPOXY RESIN HYSOL 9894. FABRICATED, ALODINED, PRIMED AND INSTALLED TWO DOUBLERS ONE 1.1" X 3.2" AND ONE 1.1" X 3.1" FROM AL2024T3 .063 IAW EMB SRM 53-21-02. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CRACKED (ZONE 100) · airframe 13,511 hrs · 11,830 cycles

CRACK DEVELOPED DURING DAMAGE CONTOUR. CUT OUT DAMAGE AREA. FABRICATED DOUBLER AND FILLER. INSTALLED IAW EMB IC 2007-145/03554A, PARAGRAPH 1.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,511 hrs · 11,830 cycles

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

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,511 hrs · 11,830 cycles

GALLEY CENTER HAT BEAM CORRODED. REMOVED AND REPLACED HAT BEAM IAW EMB SRM 51-40-02 AND 51-40-04. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — SHUTDOWN (NR 1) · airframe 13,317 hrs · 11,678 cycles

NUMBER ONE ENGINE SHUTDOWN UNCOMMANDED ON GROUND, DOWN LOADED FADEC AND CMC DISCREPANCIES LABELS AND FOUND NO FAULT MESSAGES. INSPECTED INLET AND EXHAUST WITH NO DISCREPANCIES NOTED, GROUND RUN NUMBER ONE ENGINE IAW ROLLS ROYCE MM, CHAPTER 72-00-00 WITH NO DISCREPANCIES. RETURNED AIRCRAFT TO SERVICE.

Part: ENGINE — LEAKING (NR 2) · airframe 13,300 hrs · 11,665 cycles

OIL ODOR COMING FROM NUMBER 2 ENGINE BLEED SYSTEM, RETURNED TO RDU. REMOVED AND REPLACED NUMBER 2 ENGINE IAW AMERICAN EAGLE WORK CARD 72-000-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: DUCT — BLOWN (CABIN) · airframe 13,287 hrs · 11,652 cycles

LAVATORY SMOKE AURAL WARNING ON TAKEOFF, SMOKE NOTED IN CABIN. RETURNED TO LGA. REMOVED AND REPLACED DUCT IAW EMB AMM 21-22-06. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 12,629 hrs · 11,168 cycles

FALP FAIL MESSAGE WHEN FLAPS SELECTED TO 9 DEGREE POSITION, FLAPS REMAINED AT ZERO. REMOVED AND REPLACED NUMBER 1, 2, 3 AND 4 FLAP SCREW ACTUATORS

Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 12,627 hrs · 11,167 cycles

FLAP FAIL MESSAGE, EMERGENCY DECLARED. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT, NUMBER 1 AND 2 FLAP TRANSMISSION BRAKES. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: STRINGER — CHAFED (FUSLAGE)

DURING INSPECTION FOUND EXTERNAL STRINGER 19 RT HAS CHAFE DAMAGE BETWEEN FRAMES 52 AND 53. REPAIRED DAMAGE IAW SRM REINFORCEMENT REPAIR. AIRCARAFT WAS RETURNED TO SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING INSPECTION, FOUND LT OMEGA BEAM CORRODED BETWEEN FRAMES 22 AND 25. REPAIRED LT OMEGA BEAM BETWEEN FRAMES 22 AND 25 IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: STRINGER — CHAFED (CABIN)

DURING INSPECTION, FOUND EXTERNAL STRINGER 19 LT HAS CHAFE DAMAGE BETWEEN FRAMES 52 AND 53. REPAIRED DAMAGE IAW SRM REINFORCEMENT REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING INSPECTION, FOUND RT OMEGA BEAM CORRODED BETWEEN FRAMES 22 AND 25. COMPLETED REPAIR TO OMEGA BEAM IAW SRM DOUBLER REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING INSPECTION FOUND LT OMEGA BEAM CORRODED AT FRAME 20. REPAIRED LT OMEGA BEAM AT FRAME 20 IAW SRM, DOUBLER REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: CONTROL UNIT — INOPERATIVE (PITCH TRIM)

PITCH TRIM 1-2 INOPERATIVE ON EICAS AT 520 FT SHORTLY AFTER DISCONNECTING AUTO PILOT. REPLACED HSCU. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406976)

Part: SKIN — DENTED (FUSELAGE)

ABI - DURING AN MBV INSPECTION A DENT WAS FOUND BETWEEN FRAME 75 AND 75A AND STRINGERS 10L, 11L. PERFORMED AN EDDY CURRENT INSPECTION OF THE DENT. NO DEFECTS NOTED. REMOVED DAMAGED AREA BY CREATING A 2 INCH BY 3 INCH CUTOUT. PERFORMED ADDITIONAL NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A DOUBLER, TRIPLER AND FILLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/1358, IC2003-145/1393 AND STANDARD EMB SRM, SRM 145/1142 REV 21 PRACTICES. (M)

Part: LIGHT — INOPERATIVE (CABIN)

BGR - FLT 4620 - MAINTENANCE FOUND THE LEFT FORWARD FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A LIGHT STRIP IN THE FORWARD CABIN IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)