N15732

Part: ACTUATOR — FAILED (RT MLG) · airframe 23,354 hrs · 30,747 cycles

RIGHT LANDING GEAR WOULD NOT RETRACT AFTER T/O. BOTH A & B DISAGREEMENT LIGHTS REMAINED ILLUMINATED. REMOVED AND INSTALLED SERVICEABLE MLG ACTUATOR FOR RIGHT MLG PER MM 32-32-10 S/N OFF: 287. INSTALLED SERVICEABLE RELAY AT K0205 POSITION AS REQUIRED. REMOVED AND REPLACED SERVICEABLE WOW PROX SENSOR WIRING HARNESS FOR RIGHT MLG. OPS CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (AUTOPILOT SYS) · airframe 22,902 hrs · 30,222 cycles

F/O AUTOPILOT CAPTURES 400 FT HIGH. INSTALLED SERVICEABLE APP-65 AUTOPILOT CONTROL PANEL. OPS CHECK GOOD. PN: 622-6684-006, SN ON: 2297, SN OFF: 1715.

Part: HMU — MALFUNCTIONED (NR 2 ENGINE) · airframe 22,850 hrs · 30,148 cycles

ON TAXI OUT, RT EEC LIGHT ON RESET AND WOULD NOT RESET. TWO MINUTES LATER, RIGHT GEN CAME OFF LINE. CONSULTED QRH, WOULD NOT RESET. ONE MINUTE LATER, NR 2 ENGINE FAILED, WOULD NOT FEATHER. ACTIVATED ELEC FEATHER. REMOVED AND REPLACED HMU FUEL CONTROL AND FUEL PUMP WITH SERVICEABLE UNIT IAW MM 73-13-00 AND 73-21-00. OPS AND LEAK CHECK GOOD. SN OFF M80569PN OFF 3117095-01 SN OFF 2137

Part: ANNUNCIATOR — MALFUNCTIONED (COCKPIT) · airframe 22,850 hrs · 30,148 cycles

CONTROL FAULT IN FLIGHT AND ON GROUND. ON GROUND: INBOARD'S FLASHING 5 BARS, INDICATOR SHOWING 8 DEGREES WITH FLAPS UP. REMOVED AND REPLACED FLAP ANNUNCIATOR UNIT WITH SERVICEABLE UNIT. OPS CHECK GOOD IAW 27-00-00. SN OFF 0279

Part: RAM AIR DOOR — OPEN (FUSELAGE)

IAH - FLIGHT 3561, THE CREW REPORTED SMOKE IN THE COCKPIT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RAM AIR DOORS TO BE IN THE OPEN POSITION. MAINTENANCE CLOSED THE RAM AIR DOORS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: VALVE — INOPERATIVE (FUSELAGE)

IAH - FLIGHT 2928, THE CREW REPORTED SMOKE IN THE CABIN DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND PACK CONTROL VALVE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH-DURING POSTFLIGHT THE CREW OBSERVED THAT THE LAST SECTION OF EMERGENCY LIGHTS WAS NOT ILLUMINATED. IAH-MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY, PERFORMED AN OPERATIONAL CHECK WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HARNESS — FAULTY (RT MLG)

IAH - FLIGHT 3420, THE CREW REPORTED THAT THE REPORTED THAT THE RIGHT GEAR SYSTEM-B INTRANSIT LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE INDICATION ON MEL 32-60-1B CONTROL NUMBER 007710, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON 03-15-01 WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED B-SYSTEM WIRE HARNESS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,212 hrs · 28,146 cycles

SJK - DURING C-CHECK INSPECTION, ONE CEILING EMERGENCY EXIT LIGHT AND ONE FLOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CEILING EMERGENCY EXIT LIGHT, AND OPERATIONALLY CHECKED THE FLOOR EMERGENCY EXIT LIGHT WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SPAR — CRACKED (LT&RT WING) · airframe 21,212 hrs · 28,146 cycles

SJK - DURING C-CHECK INSPECTION, THE LEFT HAND AND RIGHT HAND SPAR CAPS WERE FOUND TO BE CRACKED AT RIB 17 USING EDDY CURRENT INSPECTION. MAINTENANCE PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH EMB-120 SRM 57-20-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CRACKED (LT WING) · airframe 21,212 hrs · 28,146 cycles

SJK - DURING C-CHECK INSPECTION, TWO WING SKIN SUPPORTS ON RIB 19, AND ONE SKIN SUPPORT ON RIB 20 OF THE LEFT WING WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORTS IN ACCORDANCE WITH EMB-120 SRM 57-20-07, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — LOOSE (COCKPIT)

IAH-CREW REPORTED A BURNING SMELL FROM FIRST OFFICERS SIDE PANEL. A/C LANDED AT IAH WITHOUT INCIDENT. MX INSPECTED A/C AND FLUND A LOOSE LUG ON APU FEEDER PROTECTION RELAY. THE AFFECTED LUG WAS RESECURED AND A/C APPROVED FOR RETURN TO SERVICE.

Part: VALVE — INOPERATIVE (A/C PACK)

LCH - FLT 3083 - THE CREW REPORTED A DUCT LEAK LIGHT ON THE NR 1 PACK WITH SMOKE IN THE CABIN. MAINTENANCE PLACED THE PNEUMATIC SYSTEM ON MEL ATA 36-21-1(C), AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NR 1 PACK VALVE IAW EMB145 MM 21-24-01. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CONTROL CABLE — LACK OF LUBE (COCKPIT)

IAH - FLT 2936 - THE CREW REPORTED THAT THE BRAKES LOCKED UP ON THE TAXIWAY. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE LUBRICATED THE EMERGENCY BRAKE CABLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: HANDLE — INOPERATIVE (COCKPIT)

IAH - FLIGHT 3315 - THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR RELAY BOX IAW EMB120MM 32-31-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY REPEATED ON FLIGHT 3463, WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE. THE AIRCRAFT WAS TEST FLOWN SATISFACTORILY AND THEN RELEASED THE AIRCRAFT FOR RETURN TO SERVICE. (M)

Part: RELAY — INOPERATIVE (COCKPIT)

IAH - FLIGHT 3683 - THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT UNLESS MANUALLY OVERRIDDEN, THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY REPEATED ON FLIGHT 3423 WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR RELAY BOX. THE AIRCRAFT WAS TEST FLOWN SATISFACTORILY AND THEN RELEASED THE AIRCRAFT FOR RETURN TO SERVICE. (M)

Part: HYD SYSTEM — LOW (NACELLE)

CLE - FLT 3392 - THE CREW REPORTED THAT AFTER GEAR RETRACTION, ALL THREE 'B' SYSTEM RED LIGHTS REMAINED ILLUMINATED FOR 45 SECONDS AFTER GEAR WAS APPARENTLY UP. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT WHERE MAINTENANCE FOUND THE GREEN HYDRAULIC SYSTEM TO BE LOW. MAINTENANCE SERVICED THE AFFECTED HYDRAULIC SYSTEM, AND PERFORMED GEAR EXTENSION/RETRACTION IAW EMB120 MM 32-32-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LATCH — FAILED (LT MLG)

FLT 3348 - THE CRWE REPORTED THE LEFT MAIN GEAR DOOR WOULD NOT CLOSE. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD OUTBOARD GEAR DOOR LATCH AND PERFORMED OPERATIONAL CHECKS IAW EMB120 MM 32-12-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: CIRCUIT BREAKER — TRIPPED (AURAL WARNING)

FLT - 3297 - THE CREW REPORTED THEY GOT THE AURAL WARNING 'TAKEOFF TRIM' WITH THE ELEVATORS IN THE GREEN ARC, THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE AURAL WARNING C/B AND PERFORMED OPERATIONAL CHECKS WITH THE ENGINES RUNNING IAW EMB120 MM 71-00-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: SKIN — CHAFED (FUSELAGE)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND RT AIR CONDITIONER COMPARTMENT FUSELAGE SKIN AND FASTENER CHAFED. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM'S 51-14-02, 53-00-01, AND 51-40-02. (X)

Part: STRAP — CORRODED (FUSELAGE)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON RT BUTT STRAP FROM FRAME 27 TO FRAME 44. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,015.8 HOURS. TAC: 24,392. (X)

Part: CROSSBEAM — CORRODED (FUSELAGE)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON RT OUTBOARD FLOOR CROSSBEAM AT FRAME 36. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,015.8 HOURS. TAC: 24,392. (X)

Part: ANGLE — CORRODED (FUSELAGE)

DURING CONTINENTAL EXPRESS C-CHECK, FLOOR STRUCTURE, RT OUTBOARD SUPPORT ANGLE FOUND CORRODED. FRAME 27 TO FRAME 44. REMOVED AND REPLACED SUPPORT ANGLE AFT '2' SECTIONS IAW SRM 51-40-02. CLEANED AND TREATED FORWARD '2' SECTIONS. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,015.8 HOURS. TAC: 24,392. (X)

Part: CONTROL UNIT — FAILED (TE FLAPS)

CLE - FLT 3183 - CREW REPORTED THAT THEY RECEIVED A FLAP CONTROL FAULT ON TAXI OUT, AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL UNIT IAW EMB-120 MM 27-50-06, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: SKIN — DENTED (RUDDER)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND DENT IN AFT RUDDER, LOWER RT SIDE. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR IAW SRM'S 51-10-02, 55-00-01 AND 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,015.8 HOURS. TAC: 24.392. (X)

Part: CONNECTOR — DIRTY (RT MLG)

CLE - FLT 3221 - CREW REPORTED THAT UPON RAISING THE LANDING GEAR THE RIGHT MAIN RED 'A' INDICATION LIGHT STAYED ILLUMINATED. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED CANNON PLUG P0950, OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB120 MM 32-30-00. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: CONTROL UNIT — FAILED (TE FLAPS)

CLE - FLT 3296 - CREW REPORTED THEY RECEIVED MULTIPLE FLAP CONTROL FAULTS IN THE AIR AND ON THE GROUND. MAINTENANCE INSPECTED THE FLAP SYSTEM AND FOUND A FAULTY FLAP CONTROL UNIT. THE CONTROL UNIT WAS REMOVED AND REPLACED IAW EMB-120 MM 27-50-06, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: SIGNAL COND UNIT — FAILED (RT ENGINE)

CLE - FLT 3079 - CREW REPORTED THE AUTOFEATHER SYSTEM WOULD NOT TEST, THE TORQUE WOULD RISE BUT NO ARM LIGHT OR NP CHANGE WAS NOTED. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE TORQUE SIGNAL CONDITION UNIT IAW EMB-120-MM 77-11-01, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: FUSE — BLOWN (CABIN)

IAH - DURING PRE-FLIGHT CHECKS, THE CREW FOUND THE OVERWING EXTERIOR EMERGENCY LIGHTS TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE FUSES FOR THE AFFECTED EMERGENCY LIGHTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: STATOR — BROKEN (LT MLG)

CLE - FLT 3147 - CREW REPORTED THAT DURING TAXI THE LEFT HAND BRAKE LOCKED UP. MAINTENANCE REMOVED THE AIRCRAFT FROM THE TAXI WAY. THE LEFT LANDING GEAR WAS INSPECTED AND THE NR 2 BRAKE ASSEMBLY WAS FOUND TO HAVE A BROKEN STATOR. MAINTENANCE REMOVED AND REPLACED THE NR 2 BRAKE ASSEMBLE IAW CONT EXPRESS MX DIRECTIVE NR 4. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. PLEASE REFER TO SDR NR C2XA97CL087 FOR THE LEFT HAND BRAKE REPLACEMENT. (M)

Part: RT UNIT — FAULTED (ELEC BAY)

CLE - FLT 3215 - CREW REPORTED, RADAR VERY DEGRADED, IT WOULD ONLY PAINT GROUND RETURNS OUT TO APPROXIMATELY 25 MILES AND WOULD NOT PAINT ANY WEATHER. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACD THE RADAR R/T UNIT, ALL OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB120MM 34-41-00. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, STRINGER 18 ON THE RIGHT FUSELAGE WAS FOUND TO BE CORRODED BETWEEN FRAME 38.5 AND FRAME 40. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR PER EMB SRM 53-00-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE LEFT LOWER SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SKIN — CORRODED (LOWER FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE BELLY SKIN BETWEEN FRAMES 39 AND 41 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BELLY SKIN FROM FRAME 38 TO FRAME 42, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BUTTSTRAP — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE LEFT CENTER AND RIGHT FLOOR BUTTSTRAPS FROM FRAME 34 TO FRAME 38 WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED SECTIONS AND SPLICED IN SERVICEABLE SECTIONS OF BUTTSTRAPS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: T-PROFILE — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 40, RIGHT CENTER, WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT CENTER T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FLOOR BEAM — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE CENTER FLOOR BEAM FROM FRAMES 38 TO 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOOR BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BRACKET — BROKEN (CABIN)

IAH - DURING C-CHECK INSPECTION, THE CARGO DOOR TORSION ROD FORWARD BRACKET WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE BRACKET AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CREASE BEAM — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM FROM FRAME 34 TO FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CREASE BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: T-PROFILE — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: T-PROFILE — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE T-PROFILE ON FRAMES 36 AND 38 LEFT WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-PROFILES AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: T-PROFILE — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE T-PROFILES AT FRAMES 36 RIGHT, 38 RIGHT AND CENTER WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-PROFILES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: STRINGER — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, STRINGER 19 ON THE RIGHT FUSELAGE WAS FOUND TO BE CORRODED BETWEEN FRAME 38.5 AND FRAME 40. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR PER EMB SRM 53-00-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CREASE BEAM — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND CREASE BEAM FROM FRAME 38 TO FRAME 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CREASE BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE LEFT AND RIGHT WEB ATTACH ANGLES ON THE FLOOR SUPPORTS AT FRAME 13 WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ATTACH ANGLES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FIRE BOTTLE — UNDER WEIGHT (LAVATORY)

IAH - DURING C-CHECK INSPECTION, THE TOILET TRASH COMPARTMENT FIRE BOTTLE WAS FOUND TO BE UNDER WEIGHT. MAINTENANCE REMOVED AND REPLACED THE FIRE BOTTLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: STRINGER — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, STRINGER 20 ON THE RIGHT FUSELAGE WAS FOUND TO BE CORRODED FROM FRAME 38.5 TO FRAME 40. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR PER EMB SRM 53-00-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FLOOR BEAM — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE RIGHT FLOOR BEAM FROM FRAME 38 TO 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: T-PROFILE — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 42 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ACTUATOR — FAILED (LT MLG)

JAN - FLT NR 2683 - PILOT REPORTED, THAT THE LEFT GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT, AND WAS THEN FERRIED TO IAH, WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT GEAR RETRACT ACTUATOR. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION FOUND LEFT AFT SEAT TRACK CORRODED. MAINTENANCE INSPECTED TRACK AND FOUND IT OUT OF LIMITS, THE SEAT TRACK WAS REMOVED AND REPLACED IAW EMB 120 MM 53-01-05. TT - 8693.4. TC - 13,197. (X)