N26549

Part: CONTROL UNIT — MALFUNCTIONED (RUDDER) · airframe 38,667 hrs · 21,806 cycles

THE CREW REPORTED A RUDDER OVERBOOST MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RUDDER POWER CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,208 hrs · 26,648 cycles

EMERGENCY LIGHTS IN GALLEY INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY AND OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAME 60-61) · corrosion level 2 · airframe 33,302 hrs · 25,934 cycles

DURING C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 60-61. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-24-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: VALVE — STUCK (CABIN PRESSURE) · airframe 29,329 hrs · 22,723 cycles

ACFT WAS BEING VECTORED WHEN THE PRESSURIZATION BECAME ERRATIC, COULDN'T GET IT UNDER CONTROL MANUALLY AND FINALLY PRESSURIZATION DEPRESSURIZED AT 5000 FEET. ACFT LANDED AND MAINTENANCE, R THE ELECTROMAGNETIC OUTFLOW VALVE IAW AMM 21-31-03; IPC 21-30-00, FIGURE 30, ITEM 160. R & R THE PNEUMATIC OUTFLOW VALVE IAW AMM 21-31-04;IPC 21-31-00, FIG 30 ITEM 1. ALSO. REPLACED THE DIGITAL CONTROLLER IAW AMM 21-31-01, FIG 04 ITEM 10.OPS CHECK GOOD AND WAS RELEASED. PN OF DIGITAL CONTROLLER 2099L02110, SN 01668. PNEUMMATIC OUTFLOW VALVE, PN 2097K011100 AND SN 01522.

Part: FAN — FAILED (EXHAUST) · airframe 28,886 hrs · 22,455 cycles

PILOT REPORTED AFTER TAKE OFF AND GEAR RETRACTION, A STRANGE ODOR PERCEIVED IN THE FLIGHT DECK. MX PERFORMED AN OPS CHECK OF APU BLEED SYS AND PERFORMED A GVI OF FWD AVIONICS BAY FOR ODOR AND ABNORMALITIES. NO DEFECTS NOTED. AN ASSOCIATED ELECTRONIC BAY EXAUST NR 2 CIRCUIT BREAKER WAS FOUND TRIPPED. AFTER RESET FOUND EXHAUST FAN INOPERATIVE. MAINTENANCE R & R NR 2 EXHAUST FAN WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 28,879 hrs · 22,448 cycles

DURING ROUTINE MAINTENANCE, THE LT FORWARD EXTERNAL EMERGENCY AISLE LIGHT, AND COCKPIT FLOODLIGHT WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE FUSE ON THE NR 1 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECKED GOOD.

Part: FLANGE — CRACKED (RUDDER) · airframe 28,528 hrs · 22,175 cycles

DURING C-CHECK, THE RUDDER II UPPER ATTACHMENT POINT NUTPLATE FLANGE WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FLANGE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,665 hrs · 19,921 cycles

DURING MX INSPECTION THE FORWARD LT EXTERNAL EMERGENCY LIGHT AND FWD CABIN CEILING LIGHT WERE FOUND TO BE INOPERATIVE. MX R & R THE NR 1 EMERGENCY LIGHT BATTERY POWER SUPPLY, OP TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: DETECTION SYS — MALFUNCTIONED (EICAS) · airframe 22,401 hrs · 17,326 cycles

DURING CLIMB THE EICAS DISPLAY INDICATED A SYS NR 1 BLEED AIR LEAK. THE ACFT RETURNED AND LANDED AT WITHOUT INCIDENT WHERE MX PERFORMED TROUBLESHOOTING, PERFORMING SYS OPS CHECKS, HOWEVER THE CONDITION COULD NOT BE DUPLICATED, NOR DID THE WARNING INDICATION ILLUMINATE AGAIN. THE DISCREPANCY WAS CLEARED AND THE ACFT RETURNED TO SERVICE.

Part: CONTROL UNIT — FAULTY (HORIZ STAB) · airframe 21,946 hrs · 16,950 cycles

AFTER TAKEOFF, DURING CLIMB THE CREW REPORTED MAIN PITCH INOP WARNING ON EICAS. CREW PERFORMED AIR RETURN BACK TO IAD. IAD MX REMOVED AND REPLACED HORIZONTAL STABLIZER CONTROL UNIT IAW EMB145 AMM 27-40-01 AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE LOOP — CHAFED (NR 1 ENGINE) · airframe 21,337 hrs · 16,455 cycles

ORF FLT 5867 THE CREW REPORTED A ENGINE FIRE DETECT FAIL MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FIRE LOOP. OPERATIONAL CHECKS WERE GOOD.

Part: O-RING — WORN (BLEED AIR SYS) · airframe 20,287 hrs · 15,568 cycles

FLIGHT 4936 - JAX - FLIGHT CREW REPORTED NR 1 BLEED LEAK ON CLIMB. CREW PERFORMED AIR RETURN AND LANDED SAFELY. MX REMOVED AND REPLACED SEVERAL O-RINGS FWD OF LAV NR 1 BLEED SIDE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 19,451 hrs · 14,917 cycles

TYS - IN BNA THE CREW EXPERIENCED A FUNNY SMELL AND VIBES AT 5000 FEET ON DESCENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE AND WILL BE RELEASED AT THE END OF THE CHANGE AND OPS CHECKS.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 19,314 hrs · 14,830 cycles

IAH - FLIGHT 2493, DURING CLIMB THE CREW REPORTED THAT THE BAGGAGE EXTINGUISHER LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT SMOKE DETECTORS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 19,314 hrs · 14,830 cycles

IAH - FLIGHT 2493, DURING CLIMB THE CREW REPORTED THAT THE BAGGAGE EXTINGUISHER LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT SMOKE DETECTORS, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,251 hrs · 14,783 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 19,251 hrs · 14,783 cycles

SHV - DURING C-CHECK LT FRAME 10 WAS FOUND TO BE CRACKED AT STRINGER 10L DIRECTLY BELOW THE PILOT DV WINDOW. MAINTENANCE REMOVED AND REPLACED THE FRAME SEGMENT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 19,251 hrs · 14,783 cycles

SHV - DURING C-CHECK THE RT FRAME 10 SEGMENT AT STRINGER 10R WAS FOUND TO BE CRACKED DIRECTLY BELOW THE F/O DV WINDOW. MAINTENANCE REMOVED AND REPLACED THE FRAME SEGMENT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 16,902 hrs · 13,014 cycles

IAH - FLIGHT 2550, THE CREW REPORTED THAT THE CAPTAINS WINDSHIELD SHATTERED ON CLIMBOUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FASTENER — LOOSE (ENGINE MOUNT) · airframe 16,481 hrs · 12,685 cycles

NR 2 ENGINE FWD MOUNT YOKE O/B PLATE HAS SEVERAL LOOSE FASTENERS. REMOVED AND REPLACED 13 LOOSE JO-BOLTS IAW EMB 145 SRM 51-40-02. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 15,440 hrs · 11,930 cycles

FLIGHT CREW REPORTED EMERGENCY LIGHT STRIP ROW 8 TO 12 INOPERATIVE. MX REMOVED AND REPLACED AC INVERTER AND PERFORMED OPS TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 15,305 hrs · 11,836 cycles

IAH - DURING A-CK INSPECTION THE EMERGENCY LIGHT STRIPS BETWEEN ROWS 8 & 9 WERE FOUND TO BE INOPERATIVE. MX INSPECTED THE LIGHTING SYSTEM, OPS TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE

Part: STRINGER — TORN (S19L)

A/C WAS GROUND DAMAGED IN JAX AND FERRY FLOWN TO TYS FOR REPAIR. STR 19L AT FRM 66 WAS FOUND TORN. THE DAMAGED SECTION OF STR 19L FRM 67 TO FRM 61 WAS REMOVED AND A NEW SECTION WAS CUT AND DRILLED. FWD SECTION OF STR 19L AND STR SPLICE AT FRM`S 66-67 WERE INSTALLED. ALL IAW EMB 145 SRM 51-40-02 AND 53-00-03.

Part: STRINGER — TORN (S21L)

A/C WAS GROUND DAMAGED IN JAX AND FERRY FLOWN TO TYS FOR REPAIR. STR 21L AT FRM 66 WAS FOUND TORN. THE DAMAGED SECTION OF STR 21L AT FRM 64-68 WAS REMOVED AND A NEW SECTION WAS CUT AND DRILLED. THE NEW SECTION OF STR 21L AND STR SPLICE AT FRAMES 61-62 WERE INSTALLED. ALL IAW EMB 145 SRM 51-40-02 AND 53-00-03.

Part: HANDLE — OUT OF ADJUST (PAX DOOR)

FLT 0053 RNO FLIGHT CREW REPORTED AFTER LANDING IN RNO PAX DOOR DIFFICULT TO OPEN FROM INSIDE. REPO ACFT 188 ONT RNO TO COVER FLIGHT 53 AND ROUTE MECHANICS AND PARTS TO REPAIR 549. MX PERSONNEL ADJUSTED PAX DOOR INTERNAL HANDLE. OPS CHECK SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT FLOOR STRIP WILL NOT ILLUMINATE BETWEEN ROWS 8A AND 10A. REMOVED AND REPLACED EMERGENCY LIGHT FLOOR STRIP IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD. (S)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,392 hrs · 11,016 cycles

SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB ON SERVICE DOOR IAW EMB 145AMM 33-50-10, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 13,987 hrs · 10,654 cycles

SHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION AT FR 20. MX REPAIRED LEFT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: DOOR FRAME — CORRODED (PAX DOOR) · airframe 13,897 hrs · 10,654 cycles

SHV - DURING C-CHECK MAIN DOOR LOWER FRAME HAVE CORROSION AROUND NUT PLATE HOLES. MX REPAIRED MAIN DOOR LOWER FRAME IAW EMB 145 EC 5210-01154. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: ATTACH BRACKET — DAMAGED (LT AILERON) · airframe 13,897 hrs · 10,654 cycles

SHV - DURING C-CHECK LEFT WING AILERON HAS EXCESSIVE PLAY AT PCA RODS AND MIGRATED HAT BUSHING AT ATTACHMENT LUG. MX REMOVED AND REPLACED LEFT AILERON PCA BRACKET IAW EMB 145 SRM 51-40-02 & EC5750-01177. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 13,897 hrs · 13,528 cycles

SHV - DURING C-CHECK RIGHT HORIZONTAL STAB L/E HAS PITTING CORROSION. MX REPAIRED RIGHT HORIZONTAL L/E IAW EC5530-01116 REV D. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: STATIC PORT — INOPERATIVE (FUSELAGE) · airframe 11,549 hrs · 8,986 cycles

CLE FLIGHT 2061 THE CREW REPORTED A PITOT NR 2 INOPERATIVE MESSAGE ON THE ECIAS WITH A BURNING SMELL IN THE COCKPIT. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 STATIC PORT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: HEATER — ODOR (WINDSHIELD) · airframe 10,176 hrs · 7,907 cycles

IAH - FLIGHT 2392, THE CREW REPORTED AN ACRID ODOR IN THE COCKPIT DURING APPROACH INTO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE PACKS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. FLIGHT 2214 IN IAH, THE CREW REPORTED ODOR OF SMOKE APPROXIMATELY ONE MINUTE AFTER WINDSHIELD HEAT WAS SELECTED. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE WINDSHIELD HEAT ON MEL 30-42-02 CAT C CONT NUMBER 103235, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,002 hrs · 7,002 cycles

SHV-DURING C CHECK THE BAGGAGE DOOR LOWER CUTOUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — FAILED (NR 1) · airframe 7,639 hrs · 5,917 cycles

CLE FLIGHT 2668 THE CREW REPORTED A LOUD BANG FOLLOWED BY NR 1 ENGINE SHUTDOWN. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD.

Part: FUEL NOZZLE — FAULTY (ZONE 400)

CREW REPORTED THAT THERE WERE FUMES IN THE CABIN AND COCKPIT DURING ANTI-ICE OPERATION. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FUEL NOZZLES. THE ENGINES WERE RUN AND THE ANTI-ICE SYSTEM OPERATED WITH NO FURTHER SMELL NOTED. THE DISCREPANCY WAS THEN CLEARED.

Part: RIB — GOUGED (LT NACELLE) · airframe 4,567 hrs · 3,523 cycles

SHV - DURING C-CHECK THE LEFT UPPER COWLING OUTBOARD REINFORCEMENT ANGLE WAS FOUND TO BE GOUGED BETWEEN STATION XN 2355 AND XN 3168. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 4,567 hrs · 3,523 cycles

SHV - DURING C-CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER END OF THE RIGHT VERTICAL STIFFENER. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, SECTION 6, FIGURE 205. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 4,567 hrs · 3,523 cycles

SHV - DURING C-CHECK, THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER/SHIM REPAIR IAW EMB 145 SRM 53-21-10, FIG 201, SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 4,567 hrs · 3,523 cycles

SHV - DURING C-CHECK, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED AT FRAME 21. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (CABIN) · airframe 4,567 hrs · 3,523 cycles

SHV - DURING C-CHECK, THE L-BRACKET AFT OF THE CENTER BUTTSTRAP AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 4,567 hrs · 3,523 cycles

SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RIGHT HAND UPPER SUPPORT ARM MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 4,567 hrs · 3,523 cycles

SHV- DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO BE CHAFED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INTAKE — GOUGED (NR 1 ENGINE) · airframe 4,567 hrs · 3,523 cycles

SHV- DURING C-CHECK THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INTAKE — GOUGED (NR 2 ENGINE) · airframe 4,567 hrs · 3,523 cycles

SHV- DURING C-CHECK THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 4,567 hrs · 3,523 cycles

SHV- DURING C-CHECK THE RIGHT HAND FORWARD OMEGA BEAM DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 4,567 hrs · 3,523 cycles

SHV-DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT HAND UPPER APU SUPPORT ARM MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 4,567 hrs · 3,523 cycles

SHV- DURING C-CHECK THE CROSSBEAM AT FRAME 23 BETWEEN THE CENTER OMEGA BEAM AND THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — FAILED (T/E FLAP)

IAH- DURING FLIGHT 3642, AT CRUISE ALTITUDE THE CREW NOTED A FLAP FAIL MESSAGE AND RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT, PERFORMED A OPERATIONAL CHECK OF THE FLAP SYSTEM AND NO DEFECTS NOTED. PERFORMED A TEST FLIGHT, WHICH WAS SATISFACTORY. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MOTOR — FAILED (T/E FLAP)

IAH- THE CREW NOTED THAT THE FLAPS FAIL IN FLIGHT. NO POSITION INDICATION OF FLAPS ON EICAS. THE CREW RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP DRIVE MOTOR UNIT, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.