N16731

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

BUTTSTRAP AT YL479.00 FRAME 39-44 IS CORRODED ON THE UNDERSIDE. ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REPLACED IAW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

FRAME 40 BETWEEN CENTER AND RIGHT FLOORBEAMS, INTERCOSTAL IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL PROFILE -T- IAW EMB 120 SRM 51-40-02.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

FRAME 34-38, YR479.00, RIGHT BUTTSTRAP IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP BETWEEN FRAMES 34-38 RT FIT, DRILLED AND INSTALLED IAW EMB 120 SRM 51-40-02.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

FRAME 34-38, CENTER BUTTSTRAP IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND REPLACED BUTTSTRAP IAW EMB 120 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

OMEGA BEAM FROM FRAME 40 TO 38 YL479.00 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW 1C 2004-120/5994.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

FR 13-21, YR 479.00, RIGHT BUTTSTRAP CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED STRAP IAW EMB 120 SRM 51-40-02.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

FUSELAGE FR38 BETWEEN CENTER AND T-PROFLIE IS DAMAGED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED T-PROFILE IAW EMB SRM 51-22-00, 51-40-02.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 25,644 hrs · 32,964 cycles

VERTICAL STAB LOWER RIGHT CLOSING ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CLOSING ANGLE REPAIRED IAW EMB 120 SST-1280/99 REF SB 120-53-0074.

Part: CONTROL ROD — CORRODED (RT ELEVATOR TRIM) · airframe 25,644 hrs · 32,964 cycles

RIGHT ELEVATOR TRIM CONTROL RODS, ROD ENDS AT TAB CONNECTION ARE CORRODED. ITEM FOUND AT C-CHECK INSPECTION. RT ELEVATOR TRIM CONTROL ROD ENDS AT TAB CONNECTION REPLACED IAW AMM 27-32-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

FRAME 30-34 STR 15R, FLOOR SUPPORT CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND REPLACED FLOOR SUPPORT IAW EMB 120 SRM 51-40-02.

Part: ROD — CORRODED (LT ELEVATOR TRIM) · airframe 25,644 hrs · 32,964 cycles

LEFT ELEVATOR TRIM TAB ACTAUTOR ROD ARMS, THE TAB ATTACH, TERMINALS ARE CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED OUTBOARD ROD END ON LEFT ELEVATOR TRIM TAB ACTUATOR ROD ARM. ROD ENDS REPLACED IAW AMM 27-32-02.

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

LEFT FLOORBEAM BUTTSTRAP HAS CHAFING MARKS AT FRAME 16. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTTSTRAP IAW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

FR 34 TO FR 38 SEAT TRACK IS CORRODED BEYOND LIMITS. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SEAT TRACK IAW EMB SRM 51-25-00, 51-40-06, 51-21-02, 51-40-02, AMM 20-10-01.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

CENTER BUTTSTRAP AT FRAME 39-44 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. STRAP REPLACED IAW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00 NW740S.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

INTERCOSTAL IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INTERCOSTAL REPLACED IAW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

OMEGA BEAM CORRODED AT STA X13056.0 YR479.00. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED OMEGA BEAM IAW EMB 120 SRM 51-70-05 FIG 1.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

FRAME 34-38, YL479.00, LEFT BUTTSTRAP IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REPLACED IAW EMB 120 SRM 51-40-02, 51-22-00, 51-25-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

FR 32 TO FR 39 SEAT TRACK IS CORRODED BEYOND LIMITS. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-25-00, 51-40-06, 51-21-02, 51-22-00, 51-40-020 AMM 21-10-01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

FRAME 40, BETWEEN CENTER AND LEFT FLOORBEAMS INTERCOSTAL IS CORRODED ON THE UNDERSIDE. ITEM FOUND AT C-CHECK INSPECTION. T-PROFILE REPLACED IAW EMB 120 SRM 51-40-02 NW740S.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

BUTTSTRAP AT YR 479.00 FRAME 39-114 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REPLACED IAW EMB 120 SRM 51-40-02, 51-22-00, 51-25-00 NW740S.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

SIDEWALL SEAT TRACK CORRODED AT STA X5533.0-10870.0 STR 12L. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-40-02, 51-22-00, 51-25-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

FRAME 34-38, STR 15R, RIGHT FLOOR SUPPORT CORRODED. ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT REPLACED IAW EMB 120 SRM 51-40-02.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

FRAME 30-34, YR479.00, RIGHT BUTTSTRAP CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REMOVED AND REPLACED IAW EMB 120 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

LEFT FLOOR SUPPORT IS CORRODED AT FRAME 16, STR 15. ITEM FOUND AT C-CHECK INSPECTION. REPLACED FLOOR SUPPORT IAW SRM 51-25-00, 51-40-06, AND 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

SIDEWALL SEAT TRACK CORRODED AT STA X4600.0-10870.0 STR 12R. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

SIDEWALL SEAT TRACK CORRODED AT STA X11430.0-12860.0 STR 12R. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB SRM 51-40-02, 51-22-00, 51-25-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

OMEGA BEAM DAMAGED AND CORRODED AT FRAME 38 CENTER BUTTSTRAP. ITEM FOUND AT C-CHECK INSPECTION. OMEGA BEAM REPAIRED IAW EMB 120 SRM 51-40-02 AND 51-70-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

OMEGA BEAM AT YL479.0 FROM FRAME 40 TO 44 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. OMEGA BEAM REPLACED IAW EMB 120 SRM 51-40-02, 51-22-00 AND 51-25-00.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

RIGHT OUTBOARD COCKPIT BUTTSTRAP IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTTSTRAP IAW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,644 hrs · 32,964 cycles

RIGHT INBOARD MOST FORWARD SEAT RAIL IS CORRODED IN SEVERAL LOCATIONS. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SEAT RAIL IAW SRM 51-25-00, 51-40-06, 51-40-02, AND MM 20-10-01.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 25,101 hrs · 32,272 cycles

MULTIPLE FLAP CONTROL FAULTS WITH DISAGREEMENT AND ASYMMETRY LIGHTS ON THE GROUND AND IN THE AIR. REMOVED AND REPLACED INBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 25,026 hrs · 32,176 cycles

ON FINAL APPROACH WITH FLAPS 45 DEGREES, RECEIVED A FLAP CONTROL FAULT AND DISAGREEMENT LIGHTS. REMOVED AND REPLACED BOTH NACELLE FLAP ACTUATORS IAW MM REF 27-50-00. OPERATIONAL CHECK GOOD. P/N: 308200-1007, S/N OFF: 0163.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAP) · airframe 24,902 hrs · 32,020 cycles

AFTER FLAPS SELECTED 15 DEGREES,CONTROL FAULT AND ADVANCED SWS. REMOVED AND REPLACED ANNUNCIATOR WITH SERVICEABLE UNIT IAW 27-50-09. OPERATIONAL CHECK GOOD.

Part: INDICATOR — MALFUNCTIONED (FLAP POSITION) · airframe 24,805 hrs · 31,893 cycles

ON TAKEOFF ROLL AT APPROXIMATELY 90 KNOTS, EXPERIENCED A FLAP CONTROL FAULT LIGHT. PROVIDED CHAFE PROTECTION FOR ANNUNCIATOR CANNON PLUG AND REPLACED INDICATOR. OPERATIONAL CHECKS GOOD. P/N 306999-1007, S/N OFF 249.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 24,691 hrs · 31,744 cycles

FORWARD MOST EMERGENCY FLOOR LIGHTING STRIP INOPERATIVE. REPAIRED BROKEN WIRE AND REPLACED BLOWN FUSE. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAP) · airframe 24,655 hrs · 31,693 cycles

ON TAKEOFF ROLL EXPERIENCED FLAP CONTROL FAULT ON NACELLE FLAPS. REPLACED FLAPS CONTROL ELECTRICAL UNIT. OPERATIONAL CHECK GOOD.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAPS) · airframe 24,468 hrs · 31,436 cycles

EN ROUTE TO IAH RECEIVED FLAP ON MAP WITH ASYMMETRY IN OVERHEAD PANEL. LANDED FLAP 0 DEGREES IN IAH. REPLACED FLAP ANNUNCIATOR UNIT IAW AMM 27-50-00. FLAP SYSTEM OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 23,906 hrs · 30,731 cycles

INFLIGHT AUTOPILOT WOULD NOT HOLD ALTITUDE EITHER SIDE. REPLACED CAPTAINS AUTOPILOT COMPUTER WITH SERVICEABLE UNIT. OPS CHECK GOOD.

Part: STICK SHAKER — INOPERATIVE (NR 2 STALL WARN) · airframe 23,552 hrs · 30,312 cycles

NR 2 STALL STICK SHAKER INOP. REPLACED NR 2 STICK SHAKER. OP CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (STALL WARNING) · airframe 23,427 hrs · 30,148 cycles

NR 1 STALL LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED STALL WARNING PANEL. OPS CHECKS GOOD. REF MFG 120 MM 27-50-00.

Part: SELECTOR — MALFUNCTIONED (TE FLAP) · airframe 23,245 hrs · 29,963 cycles

ON SHORT FINAL FLAP ASYMMETRY LEFT OUTBOARD 25 DEGREES, RIGHT OUTBOARD 15 DEGREES. REMOVED AND REPLACED FLAP CONTROL LEVER AND FLAP CONTROL UNIT. OPS CHECK GOOD ON GROUND. S/N OFF: 120197

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 23,166 hrs · 29,887 cycles

SYSTEM ONE ON STALL WARNING TEST FAILS STICK PUSHER TEST, CAPTAINS. REMOVED AND REPLACED STALL WARNING COMPUTER IAW 27-00-00. OPS CHECKS GOOD.

Part: HOSE — PUNCTURED (OIL COOLER)

BPT- DURING FLIGHT 3636 APPROACH, THE CREW NOTED THAT THE #2 ENGINE OIL PRESSURE INDICATED LOW IN FLIGHT. THE PILOT FEATHERED THE #2 PROP, AND LANDED WITHOUT INCIDENT. BPT- MAINTENANCE REMOVED AND REPLACED THE #2 ENGINE OIL COOLER INLET HOSE, SERVICED THE #2 ENGINE OIL, PERFORMED ENGINE RUN AND LEAK CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — BURNED OUT (FUSELAGE)

IAH - During scheduled maintenance the left forward exterior emergency light was found to be inoperative. Maintenance removed and replaced the affected lamp, performed an operational check, and the aircraft was approved for return to service.

Part: BATTERY — DISCHARGED (CABIN)

IAH- DURING MAINTENANCE TEST IT WAS NOTED THAT THE FLOOR EMERGENCY AISLE PATH LIGHT STRIP IN THE AFT CABIN FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS IN THE BACK OF THE CABIN FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AMD REPLACED THE EMERGENCY LIGHT AFT BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUEL LINE — LOOSE (APU)

IAH - FLIGHT 3301, THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE RESECURED THE FUEL LINE ON THE APU FUEL PUMP.THE APU WAS OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETUNRN TO SERVICE. THE DISCREPANCY REPEATED ON FLIGHT 3525. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT AND MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE APU OIL TO BE LOW. MAINTENANCE SERVICED THE APU OIL AND DETERMINED THAT THE FUMES WERE CAUSED BY THE APU AUTO SHUTDOWN. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE.

Part: B-NUT — LOOSE (APU)

IAH - FLIGHT 3443, THE CREW REPORTED A FUEL SMELL FROM THE APU BLEED. MAINTENANCE INSPECTED THE APU AND TIGHTENED THE B-NUT ATTACHING THE APU FUEL LINE TO THE APU, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CRACKED (RT WING)

IAH - DURING MAINTENANCE INSPECTION STRINGER 10 ON THE RIGHT WING WAS FOUND TO BE CRACKED AT ACCESS PANEL 622DB. MAINTENANCE PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5710-01010, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CRACKED (RT MLG DOOR)

IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR INBOARD AFT GEAR DOOR HAD A BROKEN FORWARD HINGE BRACKET. MAINTENANCE REMOVED AND REPLACED THE AFFECTED HINGE BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CRACKED (LT MLG DOOR)

IAH - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR OUTBOARD AFT GEAR DOOR HAD A BROKEN AFT HINGE BRACKET. MAINTENANCE REMOVED AND REPLACED THE AFFECTED HINGE BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — SHORTED (COCKPIT)

IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED SMOKE TO BE COMING FROM THE CAPTAINS AUDIO CONTROL PANEL ABOVE THE NR 2 UHF BUTTON. MAINTENANCE REMOVED AND REPLACED THE AFFECTED AUDIO CONTROL PANEL IAW EMB120 MM 23-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ENGINE — FOD (NR 1)

EFD-DURING POST FLIGHT INSPECTION, CREW REPORTED THAT THE NUMBER ONE ENGINE HAD FOD DAMAGE. MX REMOVED/REPLACED THE AFFECTED ENGINE, AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — BURNED OUT (CABIN)

SHV-DURING 'A' CHECK INSPECTION, THE LEFT HAND FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LAMP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - DURING SERVICE CHECK INSPECTION, THE AISLE PATH, OVERHEAD, AND RIGHT FORWARD EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACKS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CONNECTOR — DIRTY (RT WING TE FLAPS)

ACT - FLT 3050 - THE CREW REPORTED A FLAP ASYMMETRY. THE AIRCRAFT DIVERTED TO ACT WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED, CLEANED, AND REINSTALLED THE CANNON PLUG ON RIGHT OUTBOARD FLAP ASSY, AND OPERATIONALLY CHECKED THE SYSTEM IN REF TO EMB120 MM 27-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CONNECTOR — DIRTY (RT FLAP)

IAH - FLT 3371 - ON APPROACH, THE CREW REPORTED THAT THE RIGHT OUTBOARD FLAP RETRACTED TO 15 DEGREES UNCOMMANDED. THE CREW LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED, CLEANED, AND REINSTALLED THE CANNON PLUG ON RIGHT OUTBOARD FLAP ASSEMBLY, AND OPERATIONALLY CHECKED THE SYSTEM IN REF TO EMB120 MM 27-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: WASHER — BROKEN (RT MLG)

IAH - FLT 3301, THE CREW REPORTED THAT THE RIGHT MLG WOULD NOT RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTEANCE ADJUSTED THE LANDING GEAR UPLOCK PROXIMITY SENSOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE PROBLEM REPEATED ON FLIGHT 3413 AND THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED A BROKEN LOCK WASHER ON THE RIGHT MLG RETRACT ACTUATOR ROD END IAW EMB 120 MM 32-30-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SKIN — DENTED (FUSELAGE)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND FUSELAGE DENTED AT FRAME 44, STRINGER 11R. INSTALLED EXTERNAL DOUBLER REPAIR IAW SRM 53-00-01. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: CROSSBEAM — CORRODED (FUSELAGE)

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

Part: CROSSBEAM — CORRODED (FUSELAGE)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND CROSSBEAM CORRODED AT FRAME 42 BETWEEN LEFT AND CENTER BEAM. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: CROSSBEAM — CORRODED (FUSELAGE)

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

Part: SKIN — GOUGED (BS 2364)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND GOUGE IN FUSELAGE SKIN AT FS 2364.0 STRINGER 13L. INSTALLED EXTERNAL DOUBLER REPAIR IAW SRM 53-00-01. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: FRAME — CRACKED (RT NACELLE)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND RT NACELLE FRAME NR 1 CRACKED. REMOVED AND REPLACED FRAME NR 1 IAW CONTINENTAL EXPRESS EC5410-01033. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: FRAME — CRACKED (LT NACELLE)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT NACELLE FRAME NR 1 CRACKED. REMOVED AND REPLACED FRAME NR 1 IAW CONTINENTAL EXPRESS EC5410-01033. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: BUTTSTRAP — CORRODED (FUSELAGE)

DURING CONTINENTAL EXPRESS C-CHECK, FOUND RT BUTTSTRAP CORRODED AT FRAME 38. REMOVED AND REPLACED BUTTSTRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: WARNING — ACTIVATED (TE FLAPS)

CLE - FLT 3069 - DURING TAKEOFF ROLL, THE CREW ABORTED TAKEOFF DUE TO A ADVANCE STALL WARNING INDICATION AND A FLAP CONTROL FAULT. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE FLAP SYSTEM IAW EMB-120 MM 27-50-00, WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: ACTUATOR — FAULTY (TE FLAP)

CLE - FLIGHT 3176 - CREW REPORTED THAT THEY RECEIVED A FLAP CONTROL FAULT IN FLIGHT. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP ACTUATOR IAW EMB-120 MM 27-50-07, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY IAW EMB-120 MM 27-50-00. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: FLAP TRACK — WORN (LT WING)

GSO - FLT 3352 - CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A FLAP ASYMMETRY WARNING ON THE OUTBOARD AND NACELLES. AIRCRAFT RETURNED TO FIELD. THE AIRCRAFT WAS MAINTENANCE FERRIED TO CLE, AFTER INSPECTION THE LEFT OUTBOARD LOWER CHANNEL INBOARD ROLLER WAS FOUND TO BE FALLING OFF THE TRACK. THE LEFT LOWER CHANNEL ASSEMBLY WAS REMOVED AND REPLACED IAW EMB-120MM 57-52-02. OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: CONNECTOR — CONTAMINATED (LT TE FLAPS)

ORF - FLT 3347 - CREW REPORTED THAT DURING CLIMB-OUT THEY RECEIVED A FLAP DISAGREEMENT AND THE OUTBOARD FLAPS WOULD NOT RETRACT, AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED THE LEFT OUTBOARD FLAP ACTUATOR CANNON PLUG, OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB 120 MM 27-50-00. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: SWITCH — LEAKING (LT ENGINE)

CLE - FLT 4399 - CREW REPORTED THAT AFTER TAKEOFF THE LEFT ENGINE DUCT LEAK LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. THE LEFT ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED SEVERAL COMPONENTS INCLUDING THE ALARM LIGHT CONTROLLER, HP BLEED VALVE, AND SHUTOFF VALVE. THE AIRCRAFT FAILED TEST FLIGHT, THE DE-ICE PRESS SWITCH WAS REMOVED AND REPLACED IAW EMB-120 MM 36-10-00, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: TUBE — TORN (LT ENGINE)

MKE - FLT 3293 - THE CREW REPORTED THAT DURING CRUISE, RECEIVED A DUCT LEAK LIGHT ON THE LEFT ENGINE. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO CLE AND THE LEFT ENGINE BLEED AIR TUBE ASSEMBLY WAS REMOVED AND REPLACED IAW EMB-120 MM 36-10-01. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: CHANNEL — CRACKED (LT TE FLAP)

BUF - FLT 4377 - CREW REPORTED THAT AFTER TAKEOFF FOR A FERRY FLIGHT TO CLE THEY RECEIVED A FLAP DISAGREEMENT THAT WOULD NOT CORRECT ITSELF, AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS INSPECTED AND FERRIED TO CLE, WHERE THE LEFT OUTBOARD FLAP LOWER CHANNEL WAS REMOVED AND REPLACED ALONG WITH THE INBOARD BEARING AND BRACKET IAW EMB-120 MM 27-50-04. OPERATIONAL CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: SENSORS — FAILED (LT WING)

BUF - FLT 3261 - CREW REPORTED THAT DURING CLIMB THE LEFT ENGINE DUCT LEAK LIGHT ILLUMINATED, THE LIGHT WOULD NOT EXTINGUISH AFTER CHECK LIST COMPLETION AND THE ELFT ENGINE WAS SHUT DOWN. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO CLE AND THE LEFT ENGINE DUCT LEAK SENSORS WERE REMOVED AND REPLACED IAW EMB-120 MM 36-20-01, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: VALVE — FAILED (LT ENGINE)

ORF - FLT 3347 - CREW REPORTED THE LEFT ENGINE DUCT LEAK LIGHT ILLUMINATED IN FLIGHT AND REMAINED ILLUMINATED AFTER THE CHECKLIST WAS ACCOMPLISHED. THE LEFT ENGINE WAS SECURED AND THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO CLE, AND THE LEFT ENGINE BLEED PRESSURE REGULATOR/SHUTOFF VALVE WAS REMOVED AND REPLACED IAW EMB-120 MM 21-50-01. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: LINE — SPLIT (LT ENGINE)

CLE - FLT 33259 - THE CREW REPORTED THAT DURING CLIMB-OUT, THE LEFT HAND ENGINE LOST OIL PRESSURE. THE CREW SUCCESSFULLY COMPLETED A PRECAUTIONARY ENGINE SHUT DOWN, AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE INSPECTED THE ENGINE THEN REMOVED AND REPLACED A SPLIT LINE ON THE LEFT HAND ENGINE OIL COOLER IAW EMB-120 MM 79-21-01. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. ACFT TT: 15,849.9 HOURS. TOTAL CYCLES: 21,630. (X)

Part: SEAT TRACK — CORRODED (CABIN)

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

Part: SEAT TRACK — CORRODED (CABIN)

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

Part: SEAT TRACK — CORRODED (CABIN)

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

Part: SEAT TRACK — CORRODED (CABIN)

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

Part: BUTTSTRAP — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE RIGHT BUTTSTRAP FROM FRAME 33 TO 44 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BUTTSTRAP — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE CENTER BUTTSTRAP FROM FRAME 35 TO 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

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

Part: FLOOR BEAM — CRACKED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT AT FRAME 16 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACD THE AFFECTED FLOOR 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 AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: T-PROFILE — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE T-PROFILE FROM FRAME 36 TO 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FLOOR BEAM — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT FROM FRAME 39 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: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, THE RT WING RIB 15, NR 4 FROM FWD SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (Z)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, THE RT WING RIB 16, NR 2 UPPER FROM AFT SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, THE RT WING RIB 16, NR 2 LOWER FROM FWD SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, THE RT WING, RIB 16 AFT LOWER SKIN SUPPORT BRACKET WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z)

Part: BRACKET — CRACKED (RT WING)

DURING C-CHECK INSPECTION, THE RT WING DEFUEL VALVE DISCHARGE BRACKET WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, THE RT WING RIB 16, NR 3 FROM FWD SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, THE RT WING RIB NR 15, NR 1 FWD SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, THE RT WING, RIB 15, NR 2 FROM FWD SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, THE RT WING 15, NR 3 FWD SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z)

Part: SUPPORT — CRACKED (LT WING)

IAH - DURING LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF RIVET, THE SKIN SUPPORT NR 34 ON RIB NR 16 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 34 IAW EMB 120 SRM 51-40-02. AIRCRAFT RELEASED FOR SERVICE. (W)

Part: SUPPORT — CRACKED (LT WING)

IAH - DURING A LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF THE RIVET, THE SKIN SUPPORT NR 35 ON RIB NR 16 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 35 IAW EMB 120 SRM 51-40-02. AIRCRAFT RELEASED FOR SERVICE. (W)

Part: SUPPORT — CRACKED (LT WING)

IAH - DURING A LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF THE RIVET, THE SKIN SUPPORT NR 24 ON RIB NR 15 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 24 IAW EMB 120 SRM 51-40-02. AIRCRAFT RELEASED FOR SERVICE. (W)

Part: SUPPORT — CRACKED (LT WING)

IAH - DURING A LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF RIVET, THE SKIN SUPPORT NR 22 ON RIB NR 15 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 22 IAW EMB 120 SRM 51-40-02. AIRCRAFT RELEASED FOR SERVICE. (W)

Part: SUPPORT — CRACKED (LT WING)

IAH - DURING A LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF THE RIVET, THE SKIN SUPPORT NR 23 ON RIB NR 15 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 23 IAW EMB 120 SRM 51-40-02. AIRCRAFT RELEASED FOR SERVICE. (W)

Part: SUPPORT — CRACKED (LT WING)

IAH - DURING A LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF RIVET, THE SKIN SUPPORT NR 25 ON RIB NR 15 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 25 IAW EMB 120 SRM 51-40-02. AIRCRAFT RELEASED FOR SERVICE. (W)

Part: ACTUATOR — OUT OF ADJUST (RT MLG DOOR)

PNS - DLT 2801 - AFTER TAKEOFF, THE RIGHT MLG WOULD NOT RETRACT, AND THE GREEN LIGHTS REMAINED ILLUMINATED. MAINTENANCE INSPECTED THE GEAR AND RESECURED AND ADJUSTED THE RIGHT INBOARD LANDING GEAR DOOR ACTUATOR ROD END IN REFERENCE TO EMB 120 MM 32-12-00. OPERATIONAL CHECKS GOOD, ACFT RELEASED FOR SERVICE. (Z)