N810AE

Part: FAN — FAILED (E/E BAY) · airframe 33,683 hrs · 30,733 cycles

ELECTRICAL SMELL IN FLIGHT DECK "TRANSFERRED TO NRWC 810-DFW-02773"-C/A-REMOVED AND REPLACED # 2 FWD ELECK COMPT COOLING FAN IAW AMM 21-26-02. OPCK GOOD. PERFORMED FIM TASK 21-20-00-810-801-A , TO COMPLETION. NO SMELL AT THIS TIME.

Part: O-RING — LEAKING (NR 2 BLEED SYS) · airframe 33,541 hrs · 30,581 cycles

BLD 2 LEAK IMMEDIATLY AFTER TAKE OFF. REMOVED AND REPLACED THE O-RINGS AT JOINT 4 AND JOIMT 20 IAW AMM 36-11-00. PERFORMED A LEAK CHECK AND FOUND SATISFACTORY IAW AMM 36-10-00.

Part: PRECOOLER — FAILED (RIGHT) · airframe 33,541 hrs · 30,582 cycles

BLEED 2 LEAK LEAK AFTER TAKEOFF AT TAKEOFF POWER @ 500' AGL. PERFORMED BLLED AIR SYSTEM LEAK CHECK IAW WORK CARD 36-700-06, AND REPLACED ORING AT RH BLEED JOINTS 6, 16, 20, 22 IAW AMM 36-11-10, REPLACED SEAL FOR RH FAN AIR CONTROL THERMOSTAT IAW AMM 36-11-06. REMOVED AND REPLACED THE RT ANGLE DUCT BETWEEN FRAME 56 AND 60 IAW AMM 36-11-09-400-801-A STEP (5) (I) 1 THRU 6. APPLIED SEALANT ON RT DUCT BETWEEN FRAMES 56 AND 60 IAW AMM 36-11-09-400-801-A STEP (5) (J). AND 20-30-03. REMOVED AND REPLACED THE RT PRECOOLER IAW AMM 36-11-04. PERFORMED OPERATIONAL TEST AND LEAK CHECK ON RT PRECOOLER IAW AMM 36-00-00-700-803-A/ OPS AND LEAK CHECKED GOOD.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 33,540 hrs · 30,580 cycles

BLD 2 LEAK IMMEDIATELY AFTER TAKEOFF. WAS NOT AN OVERWEIGHT LANDING.-C/A- REMOVED AND REPLACED O-RING AT JOINT NUMBER 26 AND 4 IAW AMM 36-11-10. PERFORMED LEAK CHECK AND FOUND SATISFACTORY IAW AMM 36-10-00. PERFORMED OPERATIONAL CHECK ON # 2 BLEED SYS. IAW AMM 36-00-00-700-803-A. OPERATIONAL CHECK GOOD AND NO DEFECTS NOTED.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 33,064 hrs · 30,128 cycles

SUPPLEMENTAL BLEED 2 LEAK WARNING. C/A-FOUND LEAKING CONNECTION AT BLEED LINE #18 JOINT. REMOVED AND REPLACED #2 SYSTEM BLEED LINE O-RINGS AT #18 CONNECTION IAW AMM 36-11-10 OPS CECK GOOD NO LEAKS NOTED.

Part: O-RING — LEAKING (BLEED DUCT) · airframe 33,000 hrs · 30,072 cycles

BLEED 2 LEAK DURING CLIMBOUT. AFTER INSPECTION OF DUCT LINES, FOUND 12 AND 22 TO BE DAMAGED AND LEAKING IAW AMM 36-11-09. R & R THE DUCTS 12 AND 22 O-RINGS IAW AMM 36-11-09. PERFORMED AN OPS CHECK OF BLEED AIR SYSTEM IAW AMM 36-00-00-700-803-A/500. OPS CHECKED GOOD, NO LEAKS NOTED. INSTALLED PANELS ZONE 161, 162 AND 272 BF IAW AMM 36-11-09. NO FURTHER DEFECTS NOTED.

Part: GPS — MALFUNCTIONED · airframe 32,944 hrs · 30,027 cycles

UNRELIABLE NAV INFORMATION IN FLIGHT BETWEEN FO X CA MFD FMS AND GPS. RESET AND PERFORMED OPC CHECK OF FMS/GPS IAW AMM 34-62-00. OPC CHECK GOOD. NO FAULTS NOTED AT THIS TIME. FOUND TO BE TRANSITORY CONDITION. A/C OK FOR SERVICE.

Part: FMS — MALFUNCTIONED · airframe 32,944 hrs · 30,027 cycles

UNRELIABLE NAV INFORMATION IN FLIGHT BETWEEN FO X CA MFD FMS AND GPS-C/A-RESET AND PERFORMED OPC CHECK OF FMS/GPS IAW AMM 34-62-00. OPC CHECK GOOD. NO FAULTS NOTED AT THIS TIME. FOUND TO BE TRANSITORY CONDITION. A/C OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (ROWS 7-8) · airframe 32,926 hrs · 30,009 cycles

EMERGENCY LIGHT STRIP INOPERATIVE AT ROWS 7-8. REMOVED AND REPLACED PROXIMITY LIGHT STRIP ON ROW 7-8 IAW AMM 33-50-122. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: FAN — FAILED (RECIRCIRCULATION) · airframe 32,926 hrs · 30,009 cycles

ELECTRICAL ODOR AND VISABLE HAZE IN CABIN REPORTED BY FA AND PAX. DIMINISHED ONCE RECIRC AND PACKS OFF.-C/A-PERFORMED OPERATIONAL CHECK OF THE AIR CONDITIONING DISTRIBUTION SYSTEM IAW AMM 21-20-00. FOUND ODOR TO BE COMING FROM RH CABIN RECIRC FAN. REMOVED AND REPLACED RH CABIN RECIRC FAN IAW AMM 21-24-01. PERFORMED OPERATIONAL CHECK OF THE AIR CONDITIONING DISTRIBUTION SYSTEM IAW AMM 21-20-00. OP CHECK GOOD. NO ODOR NOTED AT THIS TIME. C/W ETN-EM-72-034

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 32,754 hrs · 29,849 cycles

AFT CABIN CREW FLASHLIGHT INOP. C/A-REMOVED AND REPLACED AFT CABIN CREW FLASHLIGHT IAW AMM 33-50-16 STEPS 2.I.(1) AND 3.H.(4). OPC GOOD.

Part: AMPLIFIER — DAMAGED (PA SYSTEM) · airframe 32,453 hrs · 29,529 cycles

CABIN AND CABIN EMERG BUTTON LIT UP IN CRUISE FLIGHT WAS NOT ABLE TO MAKE PA'S NO CHIMES/SOUNDS WITH NO SMOKING AND SEAT BELT SIGN SWITCH BEING TOGGLED. C/A-REMOVED AND CLEANED CONNECTORS ON BOTH FWRD AND AFT F/A HANDSET IAW AMM 23-31-03. OPS CHECK FAILED. FOUND PIN 17, 18, 34, 35 AND 36 BROKEN WIRE AT THE CONNECTOR AFT F/A CRADLE REPAIRED WIRE IAW SPWM 20-51-00. REMOVED AND REPLACED PA AMP IAW AMM 23-31-01 OPS CHECKS GOOD

Part: PROXIMITY SENSOR — FAILED (SPOILER) · airframe 32,290 hrs · 29,379 cycles

DECLARED EMERGENCY AFTER SPOILER FAIL MESSAGE IN FLIGHT AT FL360 WENT AWAY AND BACK 5 TIMES UNTIL EMERGENCY XLIST COMPLETE AND CBS PULLED. OPEN INSCRIPTION ON EICAS AS WELL WITH EICAS MESSAGE NO ADVERSE EFFECT ON AIRCRAFT SPEED OR HANDLING NOTED. FOUND CORRODED CONNECTOR ON RT INBD SPOILER PROXIMITY SWITCH/SENSOR, REMOVED AND REPLACED CONNECTOR AND PROXIMITY SENSOR IAW SWPM 20-50-00 AND AMM 27-63-04 OPS CHECK GOOD. PART NUMBERS INTERCHANGEABLE PER IPC 27-63-01. INSTALLED HEAT SHRINK AND CORROSION PREVENTIVE COMPOUND ON THE RT INBD AND LT INDB SPOILER PROXIMITY SENSORS IAW AMM 27-63-04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,761 hrs · 28,846 cycles

RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED RT AFT OVERWING EMERGENCY EXIT LIGHT BULB IAW AMM 33-50-07. OPS CHECK GOOD.

Part: CHARGER — FAILED (CABIN) · airframe 31,513 hrs · 28,567 cycles

CABIN FLOOR EMER LIGHT 1,2 & 3 INOP. R&R NR 2 BATT PACK AND CHARGER IAW AMM 33-50-04. OP CK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 84695.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,489 hrs · 28,544 cycles

LT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT IAW AMM 33-50-07. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,408 hrs · 28,451 cycles

SECOND EMERGENCY PROXIMITY STRIP FROM MAIN ENTRANCE TO SEAT 3A INOPERATIVE. REMOVED AND REPLACED EMERGERCY LIGHT IAW AMM 33-57-12. OPS CHECKED GOOD.

Part: ANTENNA — FAILED (VHF COMM) · airframe 31,299 hrs · 28,350 cycles

LIGHTNING STRIKE AT 16,000 FEET IN CRUISE CLEAN CONFIGURATION ARCED ACROSS NOSE OF AIRPLANE LOST COMMS 1+2 OR THE REGAINED COMM 1. COMM 2 IS RECEIVE ONLY OR WONT TRANSMIT. ALSO ONLY ONE CRACKLES WHEN PTT IS PRESSED. NR 1 VHF COMM OPC GOOD IAW AMM 23-12-00. R&R NR 2 VHF ANTENNA IAW AM 23-12-04 FNC GOOD. APPLIED AERODYNAMIC SEALANT TO VHF NR 2 ANTENNA IAW SRM 51-20-01.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 31,205 hrs · 28,275 cycles

FUEL QUANTITY INDICATION ON BOTH ENGINES AND TOTAL FUEL INDICATED INCREASED AND DECREASED UP TO 900 POUNDS. THE FUEL IMBALANCE MESSAGE APPEARED AND DISAPPEARED MULTIPLE TIMES DURING FLIGHT. PERFORMED FUEL BALANCE (WING TRANSFER) IAW AMM 28-10-00. NO FURTHER IMBALANCE NOTED. OPS CHECK FUEL IND IAW AMM 28-14-00. OPS CHECK GOOD ALSO RAN ENGINES IAW GHC NO DEFECTS NOTED.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 31,037 hrs · 28,102 cycles

ABORTED TAKEOFF BELOW V1, DUE TO A CARGO DOOR OPEN EICAS MESSAGE. ADJUSTED THE CARGO DOOR WARNING SWITCHES IAW AMM 52-76-01. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 30,443 hrs · 27,498 cycles

FLOOR EMERGENCY LIGHT STRIP ASSEMBLY AT 261BF HAS A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 30,443 hrs · 27,498 cycles

DOOR EXTERNAL SKIN HAS 1 DENT APPROX. 2 INCHES, FRONT FWD EDGE AND 6 INCHES FROM UPPER EDGE. SKIN IS BENT AND KNIFE EDGED APPROXIMATELY 8 INCHES FROM UPPER EDGE. REPAIRED THE DOOR SKIN IAW ERS-EM-52MR-857.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 30,443 hrs · 27,498 cycles

SERVICE DOOR SILL IS CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (FRAMES 65-68) · airframe 30,443 hrs · 27,498 cycles

CARGO DOOR SILL IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE CARGO DOOR SILL IAW SRM 51-40-02.

Part: FRAME — CRACKED (FRM 10) · airframe 30,443 hrs · 27,498 cycles

RIGHT FRAME 10 CRACKED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.

Part: FRAME — CRACKED (FRM 10) · airframe 30,443 hrs · 27,498 cycles

LEFT FRAME 10 CRACKED. REMOVED AND REPLACED THE FRAMEIAW SRM 51-40-02.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 30,443 hrs · 27,498 cycles

LEFT NR 3 EMERGENCY LIGHT STRIP HAS A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 30,443 hrs · 27,498 cycles

LEFT NR 7 EMERGENCY LIGHT HAS A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: WEB — CHAFED (EMERGENCY EXIT) · airframe 30,443 hrs · 27,498 cycles

LEFT OVERWING EMERGENCY EXIT INTERNAL WEB CHAFED ABOVE WINDOW CUTOUT. REPAIRED IAW ERS-EM-52MR-854

Part: FRAME — CRACKED (FRM 23) · airframe 30,443 hrs · 27,498 cycles

FRAME 23 IS CRACKED BETWEEN STRINGERS 16R - 15R. REPAIRED THE FRAME IAW EM-53MR-1808.

Part: FLOOR SUPPORT — CORRODED (FRAME 44) · airframe 30,443 hrs · 27,498 cycles

LEFT CENTER OMEGA BEAM CORRODED UNDER THE CARBON CROSS MEMBER AT FRAME 44. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-3147.

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · airframe 30,443 hrs · 27,498 cycles

PASSENGER DOOR LOWER FRAME CORRODED AT 2 NUTPLATE HOLES. REPAIRED DOOR FRAME IAW ERS-EM-52MR-858.

Part: FLASHLIGHT — DIM (COCKPIT) · airframe 29,950 hrs · 27,059 cycles

CAPTAIN`S SIDE FLASHLIGHT VERY DIM. R & R FLASHLIGHT IAW ETN-EM-33-034, OPS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 29,618 hrs · 26,796 cycles

FLIGHT ATTENDANT REPORTS STRONG ODOR OF BURNING SMELL WHEN SHE TURNED LIGHTS ON AFTER LANDING. SMELL IS IN FWD PART OF CABIN. TRANSFERRED TO NRWC 810-ORD-01663. FOUND FWD SOCKET ON CEILING LIGHT HARNESS ABOVE SEAT 1A TO BE BURNT. R & R ELEC HARNESS IAW AMM 33-21-06. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED AT THIS TIME IAW NRWC 810-ORD-01663.

Part: WIRE — FAILED (COFFEEMAKER) · airframe 29,466 hrs · 26,662 cycles

FLIGHT ATTENDANT REPORTED THAT AFTER LANDING GEAR EXTENSION, A MEDIUM STRENGTH ODOR OF BURNING RUBBER LASTING 1 TO 3 MINUTES IN THE FWD GALLEY AREA & FWD ENTRY AREA. FOUND & REPAIRED DAMAGED WIRING AT LT HOT JUG RECEPTACLE. IAW NRWC 810-DFW-1600 TESTED & FOUND HOT JUG RECEPTACLES FUNCTIONING NORMALLY IAW WM 25-31-50. NO FURTHER ODORS DETECTED.

Part: CHARGER — FAILED (CABIN) · airframe 29,254 hrs · 26,431 cycles

PASSENGER DOOR & OVERHEAD ENTRY EMERGENCY LIGHT BULBS INOPERATIVE, 0 VOLTS. R & R NR 1 EMERGENCY BATTERY CHARGER & OPERATIONS CHECKED GOOD IAW AMM 33-50-04.

Part: DISPLAY — FAILED (COCKPIT) · airframe 29,034 hrs · 26,251 cycles

AT INITIAL POWER UP CAPTAIN'S MFD DID NOT COME ON ASSOCIATED WITH A STRONG ODOR. MFD 1 CB FOUND POPPED. R & R NR 1 MFD IAW AMM 31-41-02, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 27,674 hrs · 25,035 cycles

DURING B INSPECTION, FOUND THE FWD CABIN EMERGENCY FLASHLIGHT INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE FORWARD CABIN EMERGENCY FLASHLIGHT IAW WC 33-700-20. THE ACFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,674 hrs · 25,035 cycles

DURING B INSPECTION, FOUND FORWARD LEFT EMERGENCY LIGHTING AND SERVICE DOOR LOWER EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R NR 2 EMERGENCY LIGHT BALLAST INVERTER IAW AMM 33-50-11. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 27,214 hrs · 24,622 cycles

DURING B INSPECTION FOUND THE AFT LEFT EMERGENCY LIGHT STRIP HAD A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHTING STRIP IAW EMB AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 26,736 hrs · 24,214 cycles

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

Part: CONNECTOR — UNSERVICEABLE (BRAKE SYS) · airframe 26,680 hrs · 24,168 cycles

ON FLIGHT 3866 THE CREW REPORTED THAT DURING CRUISE FLIGHT LEVEL 360 A BRAKE LIGHT CAME ON AND REMAINED ON TO THE GATE. THE CREW DECLARED AN EMERGENCY. THE FLIGHT AND LANDING WERE NORMAL. NO MALFUNCTION NOTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ELECTRICAL CONNECTOR P0799 IAW EMB 140 STANDARD WIRING PRACTICES MANUAL 20-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — FUMES (COCKPIT) · airframe 26,580 hrs · 24,079 cycles

DURING MAINTENANCE INSPECTION WHEN APU WAS STARTED FUEL FUMES WERE NOTICED IN THE COCKPIT WITH THE ENGINE RUNNING. THE AIRCRAFT WAS REMOVED FROM SERVICE. RAN BOTH ENGINES IAW ERJ GHC AND OPS CHECKED THE APU IAW AMM 49-02-00. OPS CHECK GOOD. NO FUEL SMELL NOTED. COULD NOT DUPLICATE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — DAMAGED (RT AILERON) · airframe 26,227 hrs · 23,729 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT AILERON DAMPER FITTING OUTBOARD LUG SCORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DAMPER FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,227 hrs · 23,729 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT VERTICAL STABILIZER TO FUSELAGE ANGLE AT FRAME 76 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-1281, PART B. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — DENTED (FUSELAGE) · airframe 26,236 hrs · 23,738 cycles

DURING HEAVY CHECK INSPECTION FOUND THE RIGHT OMEGA BEAM BETWEEN FRAME 71 AND 72 HAS A LARGE DENT ON UPPER SURFACE. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIR TO RIGHT OMEGA BEAM BETWEEN FRAME 71-72. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — DENTED (FUSELAGE) · airframe 26,227 hrs · 23,729 cycles

DURING MAINTENANCE INSPECTION, FOUND RIGHT OMEGA BEAM BETWEEN FRAME 71 AND 72 HAS A LARGE DENT ON UPPER SURFACE. AIRCRAFT REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-2045. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CRACKED (E&E DOOR) · airframe 26,235 hrs · 23,737 cycles

DURING HEAVY CHECK INSPECTION FOUND REAR ELECTRONICS COMPARTMENT DOOR 272DR HAS 2 EACH CRACKS UNDER THE ATTACHMENT HOOK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED AFT AVIONICS DOOR IAW EO EM-52MR-334. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,227 hrs · 23,729 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT FUSELAGE SKIN HAS A CRACK 3/8" LONG AT FRAME 75 AND STRINGER 2R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED RIGHT FUSELAGE SKIN IAW EO EM-53MR-2039. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,271 hrs · 23,778 cycles

DURING MAINTENANCE INSPECTION FOUND THE CENTER FLOOR LEFT FLOOR STRIP NR 1, 5 & 7 REQUIRES REPLACEMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1, 5 & 7 FLOOR STRIP IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 26,271 hrs · 23,778 cycles

DURING MAINTENANCE INSPECTION FOUND THE MOST FORWARD EMERGENCY LIGHT STRIP HAS WIRES BROKEN OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MOST FORWARD EMERGENCY LIGHT STRIP IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRIP — MISSING (CABIN) · airframe 26,271 hrs · 23,778 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FLOOR PROXIMITY LIGHTS MISSING FILLER STRIPS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLOOR PROXIMITY LIGHT FILLER STRIPS IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SHUTTLE VALVE — FAULTY (BRAKE SYS) · airframe 26,009 hrs · 23,518 cycles

ON FLIGHT 4057 THE CREW REPORTED THEY RECEIVED A "HYD 1 LOW QTY" AND MFD HYDRAULIC PAGE CONFIRMS HYD SYS 1 QTY IN AMBER LOW RANGE. REPEAT WRITE UP. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BRAKE SHUTTLE VALVE IAW EMB AMM 32-49-03. ALSO REPLACED NR 4 SHUTTLE VALVE OUTER BRAKE HOSE IAW EMB AMM 32-49-03. NO LEAKS FOUND AT THIS TIME. OTHER PARTS REMOVED AND REPLACED: PART HOSE BRAKE, PART NUMBER AE713800-1. PART TYWRAP, PART NUMBER PLT4S-M76. PART PACKING, PART NUMBER 68-404. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 24,865 hrs · 24,865 cycles

DURING MAINTENANCE INSPECTION FOUND NUMEROUS EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY AND CHARGER IAW EMB 140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 24,798 hrs · 22,465 cycles

ON FLIGHT 2847 THE CREW REPORTED THE LANDING GEAR DISAGREE APPROX 2800FT WITH GEAR DOWN SHOWING 3 GREEN MASTER WARNING. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH FIM TASK 32-32-00-810-803-A OPERATIONAL CHECK LANDING GEAR EXTENSION/RETRACTION SEVERAL TIMES. LEVEL DISAGREEMENT MESSAGE DID NOT APPEAR ON EICAS, POSSIBLE TRANSITORY CONDITION. AT THIS TIME OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,648 hrs · 22,362 cycles

DURING B-INSPECTION FOUND THE COCKPIT STEP EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER NR 1 IAW EMB AMM 33-50-11 IAW WC 33-700-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — LOOSE (COCKPIT)

DURING MAINTENANCE INSPECTION FOUND THE COCKPIT FLASHLIGHT ABOVE THE CAPTAINS HOLDER IS LOOSE, NOT CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINS FLASHLIGHT AND HOLDER ASSEMBLY IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — INOPERATIVE (WINDOW HEAT) · airframe 23,110 hrs · 21 cycles

ON FLIGHT 2997 THE CREW REPORTED THE NR 1 WINDSHIELD HEAT 1 FAILED IN CRUISE. THE CREW ELECTED TO RETURN TO MLM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED CAPTAINS WINDSHIELD TEMPERTURE CONTROLLER PER AMM 30-42-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,977 hrs · 21,089 cycles

EMERGENCY FLOOR LIGHT STRIP AT LT OVERWING EMERGENCY DOOR IS INOP. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT AT EMERGENCY EXIT IAW EMB-140 AMM 33-50-12, OPS CHECK GOOD.

Part: WIRE HARNESS — CHAFED (COCKPIT) · airframe 22,367 hrs · 220,626 cycles

ON FLIGHT 4243 THE CREW REPORTED SMOKE IN THE COCKPIT AND THE SMELL OF BURNING WIRE. THE SMOKE SEEMED TO ORIGINATE FROM THE GLARESHIELD AND BY BOTH SETS OF RUDDER PEDALS. THE ODOR WAS A SULFUR SMELL THEN WIRE BURNING. THE CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TO DTW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. CHAFING OF WIRE HARNESS W102-7473-24 LIMITED TO INSULATION ONLY, NO DAMAGE TO SHIELDING OR WIRING. PERFORMED WIRE INSULATION REPAIR IAW EMB140 AE SWPM 20-21-00 AND WM 23-80-51. ALSO AMM 23-81-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,833 hrs · 20,209 cycles

FOR FLIGHT 4060 DURING PREFLIGHT INSPECTION FOUND THAT THE RIGHT OVERWING EMERGENCY LIGHT FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (SUBMITTED WITH N-NUMBER 810A, AS A PIPER PA22, SG)

Part: SKIN — DAMAGED (RUDDER) · airframe 21,468 hrs · 19,863 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND RUDDER NR 2 HAS A SMALL HOLE THROUGH THE RIGHT AND LEFT SKIN 10 MILLIMETERS ABOVE THE THIRD RIB FROM THE TOP. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED REPAIR DOUBLER ON THE LEFT AND RIGHT SIDES OF RUDDER NR 2 IAW EO EM-55MR-342. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,468 hrs · 19,863 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE CENTER HAT BEAM TO BE CORRODED AT FRAME 20. REMOVED AND REPLACED THE CENTER HAT BEAM IAW EMBRAER STRUCTURAL REPAIR MANUAL 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 21,468 hrs · 19,863 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND FRAME 23 TO BE CRACKED BETWEEN STRINGER 15 RIGHT AND 14 RIGHT. REPAIRED FRAME 23 IAW EO EM-53-MR-1736. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FADEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 20,727 hrs · 19,252 cycles

ON FLIGHT 4099 THE CREW REPORT THAT DURING CRUISE AT FLIGHT LEVEL 290 THE AIRCRAFT YAWED RIGHT, NOTED THAT ENGINE 2 N1 TARGET AND N1 INDICATION DECREASING TO LESS THAN 70% WITHOUT TL MOVEMENT N1 DECREASE TO APPROXIMATELY 87.5% WITH SLIGHT VARIATION FOR APPROXIMATELY 5 MINUTES. THE AIRCRAFT YAWED RIGHT A SECOND TIME N1 TARGET AND N1 ON ENGINE 2 DROPPED TO THE LOW 60% RANGE AND RECOVERED TO APPROXIMATELY 87.5%. NO POWER VARIATION NOTED ON DESCENT OR LANDING. ON ROLL OUT AFTER LANDING NO MESSAGES APPEARED ON EICAS FOR ENGINES 1 AND 2. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FULL AUTHORITY DIGITAL ENGNE CONTROL 2B (FADEC). THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

FOUND RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAME 24 TO FRAME 28. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

RIGHT OMEGAS BEAM INBOARD SIDE FOUND CORRODED BETWEEN FRAME 31 AND FRAME 33. REMOVED AND REPLACED OMEGA BEAM IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

FOUND LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAME 19 TO FRAME 24. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

LEFT GUSSET CORRODED BETWEEN FRAME 59 AND FRAME 61. REMOVED AND REPLACED GUSSET IAW EMB SRM 51-40-02 AND EMB IC2007-145/02567. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

LEFT OMEGA BEAM CORRODED AT FRAME 20 CROSSMEMBER, REPLACED PREVIOUS DOUBLERS IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

FOWARD DIGITAL CORRODED BELOW FLIGHT DECK THRESHOLD. REMOVED DAMAGED AREA AND SPLICED IN NEW FORWARD THRESHOLD IAW EMB SRM, RETURNED AIRCRAFT TO SERVICE.

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

FOUND RIGHT GUSSET CORRODED BETWEEN FRAME 59 AND FRAME 61. REMOVED AND REPLACED GUSSET IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

FLOOR SUPPORT CORRODED AT FRAME 25 AROUND FASTENERS. REMOVED AND REPLACED FLOOR SUPPORT IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

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

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

RIGHT OMEGA BEAM INBOARD SIDE CORRODED BETWEEN FRAME 24 AND FRAME 25. REMOVED AND REPLACED OMEGA BEAM IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAME 36 TO FRAME 46. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

LEFT OMEGA FOUND CORRODED AT FRAME 24 AND FRAME 25. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10, FIGURE 202. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAME 19 TO FRAME 23. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: SUPPORT BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

RIGHT HAT BEAM DOUBLER CORRODED AT FRAME 20. REMOVED DAMAGED AREA AND INSTALLED NEW DOUBLER IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

RIGHT OUTBOARD SEAT TRACK CORRODED AT FRAME 36 TO 46. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHINCAL NOTICE 53-110-R2. AIRCRAFT RETURNED TO SERVICE

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

FOUND GUSSET AT FRAME 20 CORRODED. REMOVED AND REPLACED GUSSET IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

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

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

RIGHT HAT BEAM DOUBLER CORRODED AT FRAME 22. REMOVED AND REPLACED DOUBLER AT FRAME 22. REMOVED AND REPLACED DOUBLER IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,175 hrs · 11,446 cycles

LEFT OUTBOARD SEAT TRACK CORRODED AT FRAME 46 TO 52. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL ORDER 53-110-R2. RETURNED AIRCRAFT TO SERVICE

Part: THRUST REVERSER — FAILED

SDF - FLT 3980 - NR 2 ENGINE THRUST REVERSER FAILED MESSAGE INFLIGHT. ENGINE WENT TO FLIGHT IDLE. UPON LANDING, AIRCRAFT HAD NO BRAKING ACTION FROM EITHER THE CAPTAINS OR FIRST OFFICER PEDALS OR PARKING BRAKE. AIRCRAFT DEPARTED RUNWAY. (M)

Part: INVERTER — FAILED (CABIN)

RIGHT OVERWING EXIT SIGN ON SIDEWALL WILL NOT ILLUMINATE. REPLACED EMERGENCY LIGHT INVERTER NR 5 IAW AMM 33-50-11. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CARTRIDGE — OUT OF ADJUST (GUST LOCK)

CREW NOTED IN CRUISE, THE GUST LOCK LIGHT CAME ON AND LANDED AT THE NEAREST AIRPORT WITH NO PROBLEMS. ADJUSTED GUST LOCK SPRING CARTIRIDGE MECHANISM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DISC-EMERGENCY LIGHTS AFT OF EMERGENCY EXIT ROW COME ON AFTER BATTERIES TURNED OFF WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECK GOOD, NO FURTHER DEFECTS. (SW21200406974)

Part: CONTROL UNIT — FAILED (HOIZONTAL STAB)

DFW - FLT 3544 - PITCH TRIM SYSTEM 1-2 INOPERATIVE ON EICAS. COMPLIED WITH ETN EB27-022 AND PERFORMED TROUBLESHOOTING IAW EMB FAULT ISOLATION MANUAL. REMOVED AND INSTALLED HSCU. OPERATIONAL CHECK GOOD IAW 27-40-01. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

CREW REPORTED GALLEY EMERGENCY LIGHTS AND RIGHT BULKHEAD EMERGENCY LIGHT WERE INOPERATIVE. FOUND CONNECTOR BY SERVICE DOOR OVERHEAD CEILING PANEL DISCONNECTED AT P8530. RECONNECTED CONNECTOR, OPS CHECK GOOD. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN MBV, THE CENTER FLOORBEAM LOWER FLANGE WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAME 26 AND 27. BLENDED THE DAMAGED AREA TO REMOVE ALL CORROSION. PERFORMED AN EDDY CURRENT INSPECTION OF THE BLENDED AREA WITH NO DEFECTS NOTED. FABRICATED A REINFORCEMENT DOUBLER. REPAIR DONE IAW EMB STATEMENT IC2003-145/1766, EMB SRM, SRM EMB 145/1142 REV 21, 53-21-10 PARA 9 FIG 208 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV, THE CENTER FLOORBEAM LOEWR FLANGE WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAME 24 AND 25. BLENDED THE DAMGED AREA TO REMOVE ALL CORROSION. PERFORMED AN EDDY CURRENT INSPECTION OF THE BLENDED AREA WITH NO DEFECTS NOTED. FABRICATED A REINFORCEMENT DOUBLER. REPAIR DONE IAW EMB STATEMENT IC2003-145/1766, EMB SRM 145/1142 REV 21, 53-21-10 PARA 9, FIG 208 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUTOUT DAMAGE SECTION OF LEFT FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AND 18 INCH BY 2 INCH EXTERNAL ANGLE, 10 INCH BY 2 INCH FILLER, 8 INCH BY 1 INCH PLATE AND 6 INCH BY 1 INCH SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142, REV 21, CHAPTER 53-21-10 FIG 201 SHEET 1. (M)

Part: SWITCH — INOPERATIVE (THRUST REVERSER)

WHEN BOTH ENGINES WERE ADVANCED FOR TAKEOFF, THE NR 2 ENGINE REACHED N1 OF 70 PERCENT AND THEN DROPPED TO IDLE SPEED, THEN JUMBED BACKUP TO 70 PERCENT N1. THE CREW NOTICED A YAW MOTION ON THE AIRCRAFT. THE TAKEOFF WAS ABORTED. MAINTENANCE REMOVED AND REPLACED THE ENGINE TWO THRUST REVERSER LOWER DEPLOY SWITCH IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: RHEOSTAT — INOPERATIVE (CABIN)

SYR - FLT 4291 - SYR - DURING DESCENT, CREW REPORTED THE OVERHEAD LIGHTS FLICKERING ON AND OFF WITH A ELECTRICAL ODOR. MAINTENANCE REPLACED THE OVERHEAD LIGHT RHEOSTAT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCAFT WAS RETURNED TO SERVICE. (M)

Part: CONTACTOR — BURNED (NLG)

ORD - FLT 4251 - CREW REPORTED AN ELECTRICAL BURNING SMELL IN COCKPIT WITH NO VISIBLE SMOKE NOTED. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO ORD WITHOUT FURTHER INCIDENT REPORTED. MAINTENANCE FOUND A BURNED NOSE LANDING LIGHT CONTACTOR. WHICH WAS REPLACED IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)