N16729

Part: WIRE — CHAFED (CABIN)

IAH - DURING MAINTENANCE INSPECTION, THE FORWARD SECTION OF AISLE PATH EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPOSITIONED A CHAFED WIRE IN ACCORDANCE WITH EMB120 W/M 20-00-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

LCH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST HALF OF THE AISLE PATH EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT POWER SUPPLY IAW EMB120 MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

IAH - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD SECTION OF AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE IN THE STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (FUSELAGE)

IAH-DURING POST FLIGHT INSPECTION, CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. MX REPAIRED A BROKEN WIRE. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

EFD - DURING MAINTENANCE INSPECTION, THE AFT AISLE PATH EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - DURING MAINTENANCE INSPECTION, THE AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY PACK IAW EMB120 MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING CONTINENTAL EXPRESS C-CHECK, THE LEFT SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 33 TO FRAME 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW EMB120 SRM 53-20-11, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: STRAP — CORRODED (CABIN)

DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 13 TO JUST PAST FRAME 14. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 53-10-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FRAME — CRACKED (RT NACELLE)

DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT NACELLE FRAME ONE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5410-01034, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: PRESSURIZATION — FAILED (CABIN)

AZO - FLT 3019 - THE CREW REPORTED A BURNING SMELL IN CLIMB BEFORE THE PRESSURIZATION FAILED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE AIRCONDITIONER SYSTEM BOTH PACKS OPERATED NORMAL IAW EMB120MM 21-00-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

CLE-SDF - FLT 3285 - THE CREW REPORTED THE LAST FIVE EMERGENCY LIGHT IN THE CABIN AISLE ARE INOPERATIVE. THE AIRCRAFT WAS AT THE GATE, NO FURTHER INCIDENTS REPORTED. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE SYSTEM IAW EMB120MM 33-50-00, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: TRANSDUCER — LEAKING (GREEN HYD SYSTEM)

DTW - DURING FLIGHT THE CREW LOST THE GREEN SYSTEM HYDRAULIC PRESSURE AND QUANTITY INDICATIONS. THE AIRCRAFT DIVERTED TO DTW WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PRESSURE TRANSDUCER IAW EMB-120 MM 29-30-09. OPERATIONAL CHECKS OF THE SYSTEM WAS SATISFACTORY IAW EMB-120 MM 29-00-00. AIRCRAFT WAS FERRY FLIGHTED BACK TO CLEVELAND FOR FURTHER MAINTENANCE. (M)

Part: RETRACT MECH — MALFUNCTIONED (LT MLG)

DTW - THE LEFT MAIN LANDING GEAR WOULD NOT EXTEND, CREW USED THE MANUAL GEAR EXTENSION SYSTEM TO GET THE GEAR DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS FERRY FLIGHTED TO CLEVELAND FOR REPAIRS. MAINTENANCE PERFORMED SEVERAL GEAR SWINGS IAW EMB-120 MM 32-30-00 AND EMERGENCY FREEFALL SYSTEM TEST IAW EMB-120 MM 32-34-00, ALL CHECKS WERE SATISFACTORY, AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: PACK — SMOKING (CABIN)

CLE - THE CREW REPORTED SMOKE IN THE CABIN AND COMING FROM THE RIGHT PACK, THE AIRCRAFT WAS TAXIING TO THE MAINTENANCE HANGAR FOR OTHER MAINTENANCE. MAINTENANCE PERFORMED OPERATIONAL CHECKS ON THE PACK SYSTEM IAW EMB-120 MM 21-00-00, NO DEFECTS WERE NOTED DURING THE CHECKS AND THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: FITTING — CRACKED (RT NACELLE)

DURING C-CHECK INSPECTION, FOUND THE RIGHT MLG INBOARD DOOR ACTUATOR FORWARD SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SUPPORT — CORRODED (BS 44-46)

DURING C-CHECK INSPECTION, FOUND THE LEFT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 44 AND 46 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT. THE AIRCRAFT WAS APPROVED FOR RETURNED TO SERVICE. (M)

Part: EXHAUST NOZZLE — CRACKED (RT ENGINE)

DURING C-CHECK INSPECTION, FOUND THE RIGHT EXHAUST DUCT CRACKED INBOARD ABOVE ATTACH MOUNT BRACKET. REMOVED AND REPLACED RIGHT EXHAUST PIPE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: PANEL — BROKEN (RT NACELLE)

DURING C-CHECK INSPECTION, FOUND ACCESS PANEL 442BB HAD SEVERAL FASTENER HOLES CRACKED AND BROKEN OUT. LOCATED AND DRILLED PANEL. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FRAME — CORRODED (BS 40)

DURING C-CHECK INSPECTION, FOUND THE RIGHT OUTBOARD CROSS FRAME AT FRAME 40 HEAVILY CORRODED. REMOVED AND REPLACED CROSS FRAME. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SUPPORT — CORRODED (BS 45/46)

DURING C-CHECK INSPECTION, FOUND THE RIGHT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 45-46 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: PANEL — CHAFED (LT NACELLE)

DURING C-CHECK INSPECTION, FOUND THE NACELLE ACCESS PANEL 432BB HAD SMALL CHAFE MARKS TO INNER SURFACE. LOCATED AND DRILLED NEW PANEL. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SUPPORT — CORRODED (BS 40-44)

DURING C-CHECK INSPECTION, FOUND THE RIGHT OUTBOARD FLOOR SUPPORT FROM FRAME 40 TO 44 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: STIFFENER — CHAFED (RT NACELLE)

DURING C-CHECK INSPECTION, FOUND THE RIGHT NACELLE AFT END CENTER FLAP WELL LOWER STRUCTURE CHAFED. REMOVED AND REPLACED STIFFENER. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: STRAP — CORRODED (BS 38-40)

DURING C-CHECK INSPECTION, FOUND THE RIGHT BUTT STRAP CORRODED BETWEEN FRAMES 38 AND 40. REMOVED AND REPLACED BUTT STRAP. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SKIN — CRACKED (RT NACELLE)

DURING C-CHECK INSPECTION, FOUND THE RIGHT MLG AFT INBOARD DOOR FORWARD HINGE ATTACH POINT NACELLE SKIN CRACKED AT RIVET. STOP DRILLED AND FABRICATED DOUBLER REPAIR. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FLANGE — CHAFED (MLG DOOR)

DURING C-CHECK INSPECTION, FOUND THE LEFT OUTBOARD FORWARD LANDING GEAR DOOR NACELLE HINGE ATTACH POINT CHAFED. REMOVED AND REPLACED LEFT OUTBOARD FORWARD LANDING GEAR DOOR NACELLE HINGE ATTACH POINT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BRACKET — CRACKED (TE FLAP)

DURING C-CHECK INSPECTION, FOUND THE RIGHT WING INBOARD FLAP HINGE PANEL OUTBOARD ROLLER BRACKET CRACKED. REMOVED AND REPLACED ROLLER BRACKET. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: STRAP — CORRODED (CABIN)

DURING C-CHECK INSPECTION, FOUND THE RIGHT INBOARD FLOOR FLANGE CORRODED BETWEEN FRAMES 33 AND 35. REMOVED AND REPLACED BUTT STRAPS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: TAIL PIPE — CRACKED (LT ENGINE)

DURING C-CHECK INSPECTION, FOUND CRACK IN AFT OUTBOARD MOUNT FLANGE ON LEFT TAIL PIPE. REMOVED AND REPLACED LEFT TAIL PIPE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FITTING — CRACKED (RT NACELLE)

DURING C-CHECK INSPECTION, FOUND THE RIGHT MLG FORWARD OUTBOARD DOOR ACTUATOR FORWARD FITTING CRACKED. REMOVED AND REPLACED FITTING. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FITTING — BROKEN (MLG DOOR)

DURING C-CHECK INSPECTION, FOUND THE RIGHT MLG AFT INBOARD DOOR AFT HINGE FITTING BROKEN. REMOVED AND REPLACED HINGE FITTING. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: HAT SECTION — DAMAGED (LT NACELLE)

DURING C-CHECK INSPECTION, AFTER LEFT WING NACELLE FLAP REMOVAL, FOUND LOWER HAT SECTION DAMAGED (HOLE) IN FLAP WELL. REMOVED AND REPLACED LOWER DAMAGED HAT SECTION. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FRAME — CRACKED (LT NACELLE)

IAH - DURING C-CHECK INSPECTION, THE LEFT NACELLE COWLING SUPPORT FRAME WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE FRAME IAW CONTINENTAL EXPRESS EC 5420-01011, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SPRING — BROKEN (RIGHT PACK)

IAH - FLT 3959 - THE PILOT REPORTED THAT DURING CLIMB, CABIN FILLED WITH SMOKE AND A SMOKE WARNING INDICATION WAS ILLUMINATED. THE CREW TURNED THE AIR CONDITIONING PACK SWITCHES TO LOW AND THE SMOKE INDICATION LIGHT EXTINGUISHED. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT RAM AIR VALVE BROKEN AND DISPATCHED THE AIRCRAFT UNDER MEL NR 21-51-1C. THE DISCREPANCY WAS CLEARED BY REMOVING AND REPLACING THE RIGHT RAM AIR VALVE SPRING, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X)

Part: DUCT ASSEMBLY — BROKEN VALVE (RT RAM AIR)

IAH - FLT 3793 - PILOT REPORTED DURING CLIMB, THERE WAS SMOKE IN CABIN. THE AIRCRAFT RETURNED AND LANDED TO IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT RAM AIR VALVE BROKEN AND THE AIRCRAFT WAS DISPATCHED UNDER MEL 21-51-1C. TO CLEAR THE DISCREPANCY, MAINTENANCE REMOVED AND REPLACED THE RIGHT RAM AIR DUCT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: SWITCH — OUT OF ADJUST (NLG STEERING)

CLE - FLT 3070 - CREW REPORTED, THAT THE NOSE WHEEL STEERING DISCONNECTS WHEN MAKING FULL LEFT TURNS USING THE TILLER. MAINTENANCE INSPECTED AIRCRAFT AND ADJUSTED THE NOSE WHEEL STEERING TILLER MICROSWITCH IAW EMB-120 MM 32-50-00. OPS CHECKS WERE GOOD, AIRCRAFT RETURNED TO SERVICE. (M)

Part: STEERING HANDLE — WORN (NLG STEERING)

CLE - FLT 3216 - CREW REPORTED, THAT THE NOSE WHEEL STEERING DISCONNECTS WHEN MAKING FULL LEFT TURNS WITH THE TILLER AND RUDDER PEDALS. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE STEERING HANDLE IAW EMB-120 MM 32-50-01, OPERATIONAL CHECKS WERE GOOD IAW EMB-120 MM 32-50-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: WHEEL — FAILED (RT MLG)

IAH - FLT 3950 - DURING POST-FLIGHT INSPECTION, PILOT REPORTED THE NR 4 MAIN TIRE WAS BLOWN. MAINTENANCE FOUND THE WHEEL RIM HAD FAILED, REMOVED AND REPLACED THE WHEEL ASSEMBLY, AND APPROVED THE AIRCRAFT FOR RETURN TO SERVICE. AIRCRAFT TOTAL TIME, 13,896.1 HOURS. TOTAL CYCLES, 17,612. (X)

Part: SUPPORT — CRACKED (LT WING)

IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB 22, LOWER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SUPPORT — CRACKED (LT WING)

IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 21, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENACNE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 21, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SUPPORT — CRACKED (LT WING)

IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 21, UPPER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SUPPORT — CRACKED (LT WING)

IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 22, UPPER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, UPPER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

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

Part: SEAT TRACK — CORRODED (CABIN)

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

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN NR 2, NR 3 SKIN SUPPORTS CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

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

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN NR 2, SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

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

Part: T-PROFILE — CORRODED (AFT CABIN)

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

Part: SUPPORT — CRACKED (LT WING)

IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN NR 4, SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (RT NACELLE)

IAH - DURING C-CHECK INSPECTION, FOUND RT NACELLE FRAME NR 2 ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: SPRING — BROKEN (LT CONTL COLUMN)

IAH - DURING C-CHECK INSPECTION, FOUND SPRING ON CAPTAINS CONTROL COLUMN BROKEN. MAINTENANCE REMOVED AND REPLACED THE SPRING, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN NR 1, SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: SUPPORT — CRACKED (RT WING)

IAH - DURING C-CHECK INSPECTION, FOUND RT WING LOWER SKIN NR 3 SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (RT VERT STAB)

IAH - DURING C-CHECK INSPECTION, FOUND RIGHT DRAG ANGLE CRACKED NEAR FORWARD END. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (LT VERT STAB)

IAH - DURING C-CHECK INSPECTION, FOUND LEFT DRAG ANGLE CRACKED NEAR FORWARD END. MAINTENANCE REMOVED AND REPLACED THE DRAG ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (RT NACELLE)

IAH - DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE NACELLE FRAME, NR 2 UPPER ANGLE, CRACKED AT FASTENER LOCATIONS. MAINTENANCE REMOVED AND REPLACED THE ANGLE. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: SELECTOR HANDLE — FAILED (TE FLAPS)

FLT NR 3263 - CLE-CVG - AFTER TAKEOFF, FLAPS SELECTOR TO 0. OUTBOARD FLAPS STAYED AT 15. DISAGREEMENT LIGHT CAME ON. RETURNED TO CLE. MAINTENACNE REMOVED AND REPLACED FLAP SELECTOR HANDLE IAW EMB 120 MM 27-50-01. AIRCRAFT WAS TEST FLOWN. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ANNUNCIATOR PNL — FAILED (COCKPIT)

FLT NR 3263 - CLE-CVG - AFTER TAKEOFF FLAPS SELECTOR TO OUTBOARD FLAPS STAYED AT 15. DISAGREEMENT LIGHT CAME ON. RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED ANNUNCIATOR UNIT IAW EMB MM 27-50-05. AIRCRAFT WAS TEST FLOWN. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: TRANSPONDER — INOP (AVIONICS BAY)

FLT NR 3183 - CLE-SYR - MODE C- INOP BOTH NR 1 AND NR 2 TRANSPONDERS. MAINTENANCE REMOVED AND REPLACED NR 1 TRANSPONDER RECEIVER/TRANSMITTER. OPS CHECKED NR 1 AND NR 2 GOOD. RETURNED TO SERVICE. (W)

Part: FIRE EXTINGUISH — CRACKED (COCKPIT)

CLE/SYR - FLT 3180 - DURING FLIGHT, COCKPIT FIRE EXTINGUISHER DISCHARGED. AIRCRAFT DIVERTED TO ROC, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FIRE BOTTLE. AIRCRAFT RETURNED TO SERVICE. (X)

Part: ROLLER'S — BINDING (LT TE FLAP)

CLE-DTW - FLT 3141 - AIR RETURN, O/B FLAP DISAGREEMENT. MAINTENANCE REMOVED AND REPLACED LT O/B FLAP ACTUATOR IAW EMB MM 27-50-09. OPS CHECK GOOD. ACFT SENT ON TEST FLIGHT, TEST FLIGHT FAILED. MAINTENANCE REMOVED AND REPLACED LT O/B FLAP ROLLER'S IAW EMB MM 27-50-12. OPS CHECK GOOD. ACFT SENT ON TEST FLIGHT, TEST FLIGHT WAS SATISFACTORY. ACFT RETURNED TO SERVICE 02/07/95. (W)