N58733

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 25,376 hrs · 32,813 cycles

WHEN SELECTING FLAPS 25 ON FINAL, RECEIVED A FLAP CONTROL FAULT. REMOVED AND REPLACED FCU. OPERATIONAL CHECK GOOD, REF 27-50-06.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 25,376 hrs · 32,813 cycles

IN CRUISE, RECEIVED A STALL WARNING MAP LIGHT, WITH NO ASSOCIATED LIGHTS ON THE STALL CONTROL PANEL. REMOVED AND REPLACED STALL WARNING COMPUTER. OPERATIONAL CHECK GOOD. REF 27-34-04.

Part: COOLING FAN — FAILED (CABIN COOLING) · airframe 25,376 hrs · 32,813 cycles

AFTER APU START, AND START UP OF PACKS NOTED A SMOKE ODOR. REMOVED AND REPLACED LEFT GROUND COOLING FAN IAW MM REF 21-20-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,376 hrs · 32,813 cycles

EMERGENCY EXIT OVERHEAD LIGHT NOT ILLUMINATED. RELAMPED OVERHEAD EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAPS) · airframe 25,324 hrs · 32,754 cycles

CONTROL FAULT AFTER SELECTING FLAPS 45. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR AND RIGHT NACELLE FLAP ACTUATOR IAW MM 27-50-00. REMOVED AND REPLACED ANNUNCIATOR ASSY IAW 27-50-08; REPLACED FCU IAW MM 27-50-06. OPERATIONAL CHECK GOOD IAW 27-50-00 PN OFF 308200-1007, SN OFF 0353 PN OFF 306900-1005, SN OFF 0108, PN OFF 307500-1001, SN OFF 0215.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 25,277 hrs · 32,696 cycles

EXIT SIGN FROM ROW 6A AT THE FLOOR FELL OFF. REPLACED LEFT OVERWING EMERGENCY EXIT IAW EMB 120 MM 33-00-00. OPERATIONAL CHECK GOOD.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 25,232 hrs · 32,640 cycles

RECEIVED FLAP CONTROL FAULT MESSAGE WHEN SELECTING FLAPS 15. REMOVED AND REPLACED FCU AND LEFT NACELLE ACTUATOR. REFERENCES A/C MM (27-50-08) (27-50-06) OPERATIONAL CHECK GOOD. P/N 347200-1001, S/N OFF 3039, P/N 308200-1007, S/N OFF 016.

Part: SELECTOR — MALFUNCTIONED (FLAPS) · airframe 25,192 hrs · 32,590 cycles

ON FINAL WHEN SELECTING FLAPS 25, CONTROL FAULT WITH ASSOCIATED LIGHTS. INSTALLED SERVICEABLE FLAP HANDLE IAW MM 27-50-00. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 25,134 hrs · 32,523 cycles

RECEIVED A FLAP CONTROL FAULT WHEN SELECTING FLAPS 25. REMOVED AND REPLACED LEFT NACELLE ACTUATOR PER MM 27-50-00. OPERATIONAL CHECK GOOD.

Part: SELECTOR — MALFUNCTIONED (TE FLAPS) · airframe 25,122 hrs · 32,508 cycles

RECEIVED FLAP CONTROL FAULT WHEN SELECTING FLAPS 15. REPLACED FLAP HANDLE. OPERATIONAL CHECK GOOD REFERENCE 27-00-00.

Part: SERVO — MALFUNCTIONED (TRIM SYSTEM) · airframe 25,044 hrs · 32,407 cycles

ELECTRIC TRIM DOES NOT FUNCTION ABOVE 180 KTS.REMOVED AND REPLACED ELECTRIC TRIM MOTOR, REFERENCE 22-10-05. OPERATIONAL CHECK GOOD.

Part: SELECTOR — MALFUNCTIONED (TE FLAPS) · airframe 25,029 hrs · 32,387 cycles

PILOT REPORTS CONTROL FAULT WHEN SELECTING FLAPS FROM 15 TO 25 DEGREES. REMOVED AND REPLACED FLAP SELECTOR HANDLE. OPERATIONAL CHECK GOOD. P/N 120-6920-615CON, S/N OFF 120182.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 25,003 hrs · 32,352 cycles

ON TAXI OUT WITH FLAP SELECTOR 15 DEGREES, FLAPS WERE STILL AT 0 DEGREES. REMOVED AND REPLACED LEFT & RIGHT NACELLE FLAP ACTUATORS IAW MM 27-50-00. OPERATIONAL CHECK GOOD. LT P/N: 308200-1007, S/N OFF: 0242 RT, P/N: 308200-1007, S/N OFF: 0405.

Part: SERVO — WEAK (ELEVATOR) · airframe 25,003 hrs · 32,352 cycles

ELECTRIC TRIM WEAK ABOVE 180 KNOTS INDICATED AIRSPEED. REMOVED AND REPLACED ELECTRIC TRIM (ELEVATOR) SERVO IAW 27-32-00. OPERATIONAL CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 24,945 hrs · 32,273 cycles

DURING FINAL APPROACH, SELECTED FLAPS 25 AND GOT CONTROL FAULT ON FLAP PANEL WITH FLAP AND ADV SWS ON MAP. STALL WARNING COMPUTERS 1 & 2 WERE REPLACED. OPERATIONAL CHECK GOOD. REFERENCING 27-34-00 & 27-50-00. P/N C-8106-1, S/N OFF 472.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 24,915 hrs · 32,237 cycles

WITH FLAPS SELECTED TO 45 DEGREES, RECEIVED CONTROL FAULT AND SWS ON MAP PANEL. REPAIRED WIRE AS REQUIRED AT LT NACELLE ACTUATOR CONNECTOR. REPLACED LEFT NACELLE FLAP ACTUATOR AND RIGHT NACELLE FLAP ACTUATOR IAW EMB 120 MM 27-50-08 AND MM 27-50-00. OPERATIONAL CHECK GOOD. P/N 308200-1007, S/N OFF 0170.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 24,902 hrs · 32,219 cycles

FLAPS INDICATE CONTROL FAULT ON OB FLAPS. REPLACED LT OB FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD.

Part: FLAP TRACK — CRACKED (WING) · airframe 24,877 hrs · 32,186 cycles

DISCOVERED CRACK ON THE FLAP TRACK (NEXT TO ROLLER) IMMEDIATELY OB OF THE NR 1 ENGINE NACELLE. REPLACED LT OB FLAP IB ROLLER BRACKET WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.

Part: ANNUNCIATOR — FALSE INDICATION (TE FLAPS) · airframe 24,820 hrs · 32,113 cycles

IN-FLIGHT AND ON GROUND MASTER CAUTION (FLAP) WITH DISAGREEMENT, ASYMMETRY AND CONTROL FAULT. REPLACED FLAP ENUNCIATOR UNIT WITH SERVICEABLE UNIT. REF EMB 120 MM 27-50-00. OPERATIONAL CHECK GOOD.

Part: RELAY — FAILED (APU) · airframe 24,725 hrs · 31,984 cycles

ELECTRICAL BURNING ODOR EMINATING FROM F/O'S WALL PANEL AREA, VERY HOT TO THE TOUCH. REMOVED AND REPLACED APU FEEDER PROTECTION RELAY K0152 AND APU START CONTACTOR K0089, APU FEEDER PROTECTION RELAY PHENOLIC SEAT AND ASSOCIATED BUS BARS. OPERATIONAL CHECK GOOD.

Part: COOLING FAN — MALFUNCTIONED (COCKPIT) · airframe 24,649 hrs · 31,882 cycles

SMOKEY ODOR IN COCKPIT FROM LEFT PACK WHILE ON THE GROUND. REPLACED LEFT GROUND COOLING FAN IAW EMB 120 21-20-00. P/N AE1711AA0, S/N ON 136, S/N OFF 112.

Part: ACTUATOR — MALFUNCTIONED (ELEVATOR TRIM) · airframe 24,361 hrs · 31,511 cycles

ELEVATOR TRIM ACTUATOR FREEZES UP AT HIGH ALTITUDES. SIGNIFICANT SNAP-BACK WITH BOTH MANUAL AND ELECTRIC TRIM INPUTS, 17,000 FT AND HIGHER. REPLACED LEFT AND RIGHT ELEVATOR TRIM ACTUATORS WITH SERVICEABLE UNITS IAW AMM 27-32-02. OPS CHECK GOOD. P/N: 5299-1.

Part: SELECTOR SWITCH — FAILED (RT A/C PACK) · airframe 24,276 hrs · 31,412 cycles

SMOKE IN CABIN DURING TAXI OUT. REPLACED RCCB FOR RIGHT GROUND COOLING FAN AND REPLACED MODE SELECTOR SWITCH FOR RIGHT PACK IAW MM 21-00-00. OPS CHECK GOOD.

Part: SERVO — MALFUNCTIONED (STICK SHAKER) · airframe 23,489 hrs · 30,436 cycles

LT STICK SHAKER INOPERATIVE. REPLACED SHAKER. OPS CHECK GOOD. SN OFF: 518

Part: ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 23,461 hrs · 30,405 cycles

CONTROL FAULT AT 16,000 & STAYED ON AFTER LANDING. REMOVED AND REPLACED FLAP ANNUNCIATOR AND RIGHT NACELLE FLAP ACTUATOR. OPS CHECK GOOD.

Part: SELECTOR — MALFUNCTIONED (TE FLAP) · airframe 23,416 hrs · 30,356 cycles

DURING DESCENT INTO IAH THERE WERE NUMEROUS CONTROL FAULT ON OVERHEAD WITH FLAP AND ADVANCED SWS ON MAP THAT APPEARED FOR A COUPLE SECONDS THEN CLEARED ITSELF. REMOVED AND REPLACED FLAP CONTROL LEVER PER MM 27-00-00. OPS CHECKS GOOD.

Part: CONTROL UNIT — FAILED (COCKPIT)

FLIGHT 3583 IAH TO VCT -A- INDICATION CB POPPED FOR LANDING GEAR. RESET UNSUCCESSFUL, QRH UNSUCCESSFUL. RECYCLED GEAR, IT WOULD NOT COME UP OR DOWN, B SYSTEM INDICATES DOWN AND LOCKED, THE AIRCRAFT LANDED AT VCT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL MODULE, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — BURNED OUT (FUSELAGE)

IAH - Maintenance found the right overwing emergency exit light to be inoperative. Maintenance removed and replaced the affected lamp, operationally checked the lighting system and approved the aircraft for return to service.

Part: COOLING FAN — FAILED (A/C BAY)

IAH- AFTER TAKEOFF FLIGHT 3917 THE CREW NOTED SMOKE IN THE COCKPIT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO IAH WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE GROUND COOLING FAN, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — FROZEN (FUSELAGE)

IAH - FLIGHT 3518, THE CREW REPORTED THAT AFTER ENGINE START THE CABIN FILLED WITH SMOKE. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NUMBER TWO ACM ON MEL 21-50-2/C CONTROL NUMBER 015282, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON 08/30/01 WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ACM, REMOVED THE MEL, AND APPROVED THE AIRCRAFT FOR RETURN TO SERVICE.

Part: TANK — ODOR (APU)

IAH - AFTER ENGINE SHUTDOWN ON TAXI TO GATE THE CREW REPORTED A FUEL SMELL IN THE CABIN AFTER APU START. MAINTENANCE DRAINED THE APU EPA TANK, OPERATIONALLY CHECKED THE APU WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN)

IAH - FLIGHT 3035, THE CREW REPORTED A STRONG FUEL ODOR FROM THE APU. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE AIR CONDITIONING SYSTEM USING THE APU BLEED AIR WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR — OUT OF ADJ (LT MLG)

IAH - FLIGHT 3244, THE CREW REPORTED THAT THE SYSTEM-A GEAR INDICATION LIGHT ILLUMINATED ON TAKEOFF ROLL. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE ADJUSTED THE LEFT MAIN LANDING GEAR A-SYSTEM PROXIMITY SENSOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TANK — ODOR (APU)

IAH - FLIGHT 3420, THE CREW REPORTED THAT THE APU BLEED CAUSED A FUEL SMELL IN THE CABIN. MAINTENANCE DRAINED THE APU EPA TANK, OPERTAIONALLY CHECKED THE APU AND PACKS SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PLUG — LEAKING (APU)

IAH - FLIGHT 2479, THE CREW REPORTED A STRONG FUEL SMELL AFTER DEPARTURE FROM CLL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE APU EPA TANK DRAIN PLUG, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT)

IAH - FLIGHT 2933, THE CREW REPORTED A FUEL ODOR IN THE COCKPIT. MAINTENANCE DRAINED THE APU EPA TANK AND OPERATIONALLY CHECKED THE AIR CONDITIONING SYSTEM WITH NO FUEL SMELL NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

IAH - FLIGHT 3353, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SEVERAL INOPERATIVE EMERGENCY EXIT LIGHT BULBS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (LT WING)

IAH - FLIGHT 3035, THE CREW REPORTED A LEFT ENGINE DUCT LEAK LIGHT ILLUMINATED IN FLIGHT, THE LEFT ENGINE SHUT DOWN AS A PRECAUTION, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RESECURED A LOOSE WIRE ON A DUCT TEMP SENSOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY REPEATED ON FLIGHT 3442, THE ENGINE WAS PRECAUTIONARILY SHUTDOWN, THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A BROKEN WIRE ON THE LEFT WING INBOARD DUCT LEAK SENSOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: A/C PACK — MALFUNCTIONED (AC BAY)

IAH - FLT 3418 - THE CREW REPORTED A BURNING SMELL IN THE COCKPIT WHEN SELECTING HEAT FROM THE NR 1 AIRCONDITIONING PACK DURING FLIGHT. MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE NR 1 AIRCONDITIONING PACK IAW EMB-120MM 21-40-00 AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: A/C PACK — MALFUNCTIONED (AC BAY)

LRD - FLT 3564 - THE CREW REPORTED SMOKE IN THE CABIN AND PERFORMED AN AIR RETURN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINDED THE SOURCE OF THE SMOKE TO BE COMING FROM THE NR 2 AIRCONDITIONING PACK AFTER PERFORMING OPERATIONAL CHECKS OF THE BLEED AIR SYSTEM. MAINTENANCE PLACED THE NR 2 AIRCONDITIONING PACK ON MEL REFERENCE 21-50-2, CATEGORY ''C'' CONTROL NR 003481. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS)

IAH - FLT 2921 - THE CREW REPORTED A FLAP DISAGREEMENT ON FLAP RETRACTION DURING TAKEOFF. THE CREW PERFORMED AN AIR RETURN AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE FLAPS AND VERIFIED NORMAL OPERATION IAW EMB-120 MM 27-50-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SKIN — GOUGED (FUSELAGE)

IAH-DURING MX INSPECTION, RT AFT FUSELAGE SKIN WS FOUND TO BE DAMAGED. MX REPAIRED THE DAMAGED SECTION OF SKIN IN ACCORDANCE WITH EMBRAER SST 2908/00 AND CONTINENTAL EXPRESS ENGINEERING AUTHORIZATION EC5330-01142, A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: REGULATOR — LEAKING (NR 1 BLEED)

IAH - FLT 3524 - THE CREW REPORTED THAT THE NR 1 BLEED DUCT LEAK LIGHT ILLUMINATED. THE CREW PERFORMED A PRECAUTIONARY NR 1 ENGINE SHUTDOWN, AND RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 1 PRESSURE REGULATOR TO BE LEAKING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED REGULATOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: PANEL — MISSING (NACELLE)

CLL - FLT 3463 - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT HYDRAULIC SERVICE DOOR WAS MISSING. MAINTENANCE REPLACED THE RIGHT HYDRAULIC SERVICE DOOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SIGN — LOOSE (CABIN)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN AT ROW 10 WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE AFFECTED PART, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST TOW RED AND WHITE AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE IN THE LIGHT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - DURING A-CHECK INSPECTION, THE PASSENGER ENTRANCE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW EMB 120 MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATAIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE, TWO, AND THREE EMERGENCY LIGHT BATTERY PACKS IAW EMB120 MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

IAH - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT POWER SUPPLY IAW EMB 120 MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: WASHER — BROKEN (NLG)

VCT - DURING TRAINING FLIGHT 200, THE CREW REPORTED THAT THE NOSE GEAR DISAGREEMENT LIGHTS WOULD NOT EXTINGUISH UPON GEAR RETRACTION. THE AIRCRAFT LANDED AT VCT WITHOUT INCIDENT WHERE A FERRY FLIGHT WAS ARRANGED TO IAH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT AND MAINTENANCE REMOVED AND REPLACED A BROKEN LOCK WASHER ON THE NOSE LANDING GEAR RETRACT ACTUATOR ROD END. THE LANDING GEAR OPERATIONLLY CHECKED GOOD IAW EMB120 MM 32-32-11, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FUSE — FAILED (CABIN)

IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE EXTERIOR EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FUSE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CROSSBEAM — CORRODED (FRAME 36)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND LOWER FUSELAGE CROSSBEAM CORRODED AT FRAME 36. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE (M)

Part: CROSSBEAM — SCORED (FRAME 40)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND LOWER FUSELAGE CROSSBEAM SCORED AT FRAME 40. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: CROSSBEAM — CORRODED (FRAME 16)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND LOWER FUSELAGE CROSSBEAM CORRODED AT FRAME 16. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: SKIN — CHAFED (FUSELAGE)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND LOWER FUSELAGE SKIN WORN INTO BY SCREWS FROM PANELS 191 AND 192. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: BUTTSTRAP — CORRODED (FRAME 34-39)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND LOWER FUSELAGE, LT BUTTSTRAP CORRODED BETWEEN FRAMES 34/39. REMOVED AND REPLACED BUTTSTRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: FRAME — CRACKED (NR 1 NACELLE)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT ENGINE NACELLE NR 1 FRAME CRACKED. REMOVED AND REPLACED NR 1 FRAME IAW SB 120-54-0036 AND EC5410-01034. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: BUTT STRAP — CORRODED (FRAME 13-16)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND LOWER FUSELAGE CENTER BUTT STRAP CORRODED BETWEEN FRAMES 13 AND 16. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: CROSSBEAM — CORRODED (FRAME 33)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND LOWER FUSELAGE CROSSBEAM CORRODED AT FRAME 33. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: BUTTSTRAP — CORRODED (FRAME 14-21)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND LOWER FUSELAGE, LT BUTTSTRAP CORRODED BETWEEN FRAMES 14 AND 21. REMOVED CORRODED SECTION OF BUTTSTRAP AND SPLICED IN NEW SECTION IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: WIRE — BROKEN (LANDING GEAR)

CLE - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF AND THE UP/DOWN CONTROL C/B POPPED. AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED A WIRE AT THE LANDING GEAR CONTROL HANDLE IAW EMB120 WM 20-21-00. OPERATIONAL CHECKS OF THE RETRACTION AND EXTENSION SYSTEM WERE SATISFACTORY IAW EMB-120 MM 32-30-00. AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

IAH - DURING 'A' CHECK INSPECTION, THE RIGHT FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB IAW EMB120-ER MM 33-51-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

IAH - DURING 'A' CHECK INSPECTION, THE LEFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB IAW EMB120 ER MM 33-51-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

IAH - DURING 'A' CHECK INSPECTION, THE AFT AISLE PATH EMERGENCY RED LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB IAW EMB120-ER MM 33-51-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CONTROL MODULE — FAILED (NLG STEERING)

CLE - FLT 3216 - CREW REPORTED THAT THEY LOST ALL STEERING DURING LANDING ROLL OUT AND NEVER GAINED IT BACK. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE STEERING CONTROL MODULE IAW EMB120 MM 32-50-03. OPERATIONAL CHECKS WERE SATISFACTORY. RELAY K0123 WAS ALSO REPLACED FOR PRECAUTIONARY MEASURES. AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: MANIFOLD — FAILED (NLG STEERING)

CLE - FLT 3294 - CREW REPORTED THAT THE NOSE WHEEL STEERING FAILED COMPLETELY DURING LANDING WHEN THE NOSE WHEEL TOUCHED DOWN. THE CREW ALSO REPORTED LITTLE TO NO ABILITY TO CONTROL DIRECTION ON THE GROUND. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE STEERING MANIFOLD IAW EMB-120 MM 32-50-04, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: WIRE HARNESS — CHAFED (RT NACELLE)

IAH - DURING FLIGHT 3950 FROM VCT TO IAH, THE NUMBER 2 ENGINE EXPERIENCED A TORQUE SURGE FOLLOWED BY A LOSS OF POWER. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REPAIRED THE NR 2 ENGINE EEC WIRE HARNESS, AND THE AIRCRAFT WAS APPROVED FOR RETURNED TO SERVICE. (M)

Part: FLAP CONTL UNIT — FAULTED (E/E COMPT)

SBN - FLT 3190 - CREW REPORTED THAT AFTER TAKEOFF, AND BEFORE ANY FLAP CHANGE THEY RECEIVED A FLAP ASYMMETRY AND CONTROL FAULT. AIRCRAFT RETURN TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT AND RESET THE FLAP SYSTEM BY REMOVING AND RE-INSTALLING THE FLAP CONTROL UNIT IAW EMB 120 MM 27-50-06. OPERATIONAL CHECKS WERE GOOD, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: ANNUNCIATOR — FAILED (E/E BAY)

CLE - FLT 4244 - THE CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A FLAP CONTROL FAULT WHICH WOULD NOT RESET. THE AIRCRAFT RETURNED TO BASE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE FLAP ANNUNCIATOR ASSEMBLY. OPERATIONAL CHECKS WERE GOOD IAW EMB120 MM 27-50-00. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - INSPECTION CHECK 1C, 2C, 4C - DURING A ROUTINE INSPECTION, THE FORWARD CABIN RIGHT SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DAMAGED TRACK AND THE AIRCRAFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M)

Part: BUTT STRAP — CORRODED (CABIN)

IAH - DURING A ROUTINE INSPECTION, THE AFT CABIN RIGHT FLOOR BEAM BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES NR 33-39. MAINTENANCE REMOVED AND REPLACED THE DAMAGED BUTT STRAP AND THE AIRCRAFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M)

Part: CROSSBEAM — CORRODED (CABIN)

IAH - DURING A ROUTINE INSPECTION, FRAME NR 36 FLOOR CROSSBEAM WAS FOUND TO BE CORRODED ON RIGHT SIDE OF CABIN. MAINTENANCE REMOVED AND REPLACED THE DAMAGED CROSSBEAM AND THE AIRCRAFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - INSPECTION CHECK 1C, 2C, 4C - DURING A ROUTINE INSPECTION, THE FORWARD CABIN FLOOR LEVEL LEFT SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACD THE DAMAGED TRACK AND THE AIRCRAFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M)

Part: BUTT STRAP — CORRODED (CABIN)

IAH - INSPECTION CHECK 1C, 2C, 4C - DURING A ROUTINE INSPECTION, THE AFT CABIN CENTER FLOOR BEAM BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES NR 33-39. MAINTENANCE REMOVED AND REPLACED THE DAMAGED PORTION OF THE BUTT STRAP AND THE AIRCRAFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M)

Part: CROSSBEAM — CORRODED (CABIN)

IAH - DURING A ROUTINE INSPECTION, FRAME NR 38 FLORO CROSSBEAM WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DAMAGED CROSSBEAM AND THE AIRCRAFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M)

Part: CROSSBEAM — CORRODED (CABIN)

IAH - DURING A ROUTINE INSPECTION, FRAME NR 36 FLOOR CROSSBEAM WAS FOUND TO BE CORRODED ON LEFT SIDE OF CABIN. MAINTENANCE REMOVED AND REPLACED THE DAMAGED CROSSBEAM AND THE AIRCRFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - INSPECTION CHECK 1C, 2C, 4C - DURING A ROUTINE INSPECTION, THE AFT CABIN RIGHT FLOOR LEVEL SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DAMAGED TRACK AND THE AIRCRFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - INSPECTION CHECK 1X, 2C, 4C, - DURING A ROUTINE INSPECTION, THE FORWARD CABIN LEFT SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DAMAGED TRACK AND THE AIRCRAFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - INSPECTION CHECK 1C, 2C, 4C - DURING A ROUTINE INSPECTION, THE FORWARD CABIN FLOOR LEVEL RIGHT SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SEAT TRACK AND THE AIRCRAFT WAS LATER RETURNED TO SERVICE. (M)

Part: O-RINGS — CUT (RT ENGINE)

BUF - FLT 3000 - CREW REPORTED THAT DURING CRUISE, THE RIGHT HAND ENGINE LOST OIL PRESSURE, AIRCRAFT DIVERTED TO BUF. MAINTENANCE INSPECTED O-RINGS IAW EMB-120 MM 73-12-00. OPERATIONAL AND LEAK CHECKS WERE GOOD IAW EMB-120 MM 71-00-00. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BEARING — RUSTED (RT ELEVATOR)

IAH - DURING C-CHECK INSPECTION, FOUND RT ELEVATOR INBOARD PIVOT POINT BEARING RUSTED. MAINTENANCE REMOVED AND REPLACED THE BEARING, AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACFT TT - 9,056.6. ACFT TOTAL CYCLES - 13,433. (X)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, FOUND RT WING RIB, NR 15 LOWER, NR 4 SKIN SUPPORT, CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACFT TT - 9,056.6. ACFT TOTAL CYCLES - 13,433. (X)

Part: SUPPORT — CRACKED (LT WING)

IAH - DURING C-CHECK INSPECTION, FOUND LT WING LOWER SKIN SUPPORT NR 4 AFT, CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE BRACKET, AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACFT TT 9056.6. CYCLES - 13433. (X)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, FOUND RT WING RIB, NR 16 LOWER, NR 4 SKIN SUPPORT, CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACFT TT - 9,056.6. ACFT TOTAL CYCLES - 13,433. (X)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, FOUND RT WING RIB NR 15 LOWER NR 3 SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACFT TT - 9056.6. CYCLES - 13433. (X)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, FOUND RT WING RIB NR 15 LOWER NR 2 SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (X)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, FOUND RT WING RIB, NR 16 LOWER, NR 3 SKIN SUPPORT, CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACFT TT, 9,056.6. ACFT TOTAL CYCLES - 13,433. (X)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING INSPECTION CHECK 6C, FOUND RT WING RIB NR 15 LOWER SURFACE SKIN SUPPORT CRACKED. CRACKED BRACKET IS NR 4 FROM FRONT OF RIB. REPLACED SKIN SUPPORT. WORK ACCOMPLISHED IAW AIRCRAFT MANUFACTURER SRM. ACFT TT - 9,056.6. ACFT TOTAL CYCLES - 13,433. (X)

Part: LAMP — BURNED OUT (RT FWD EEL)

DURNG SCHEDULED MAINTENANCE CHECK, FOUND INTERNAL EMERGENCY LIGHT INOP AT SEAT 6C. MAINTENANCE REMOVED AND REPLACED LAMP IAW 33-51-01. OPERATIONAL CHECK GOOD IAW 33-50-00. AIRCRAFT RETURNED TO SERVICE. (W)

Part: DISPLAY UNIT — INTERMITTENT (LT COCKPIT)

CLE/CLE - FLT 3136 - ABORTED TAKEOFF DUE TO THE CAPTAIN'S EADI AND EHSI INTERMITTENTLY FAILED ON TAKEOFF ROLL. CLE MAINTENANCE REMOVED AND REPLACED THE NR 1 DPU IAW EMB-120 MM 34-23-03. OPERATIONAL CHECKS WERE GOOD IAW EMB-120, MM 34-21-00. AIRCRAFT RETURNED TO SERVICE. (X)