N14933

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,569 hrs · 31,835 cycles

DURING PREFLIGHT INSPECTION, CREW REPORTED THE AFT EMERGENCY EXIT LIGHT AND FLOOR PROXIMITY LIGHTS INOPERATIVE. R & R POWER SUPPLY, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — LEAKING (RT WING FUEL) · airframe 33,091 hrs · 31,356 cycles

THE CREW REPORTED FUEL LEAKING FROM THE RT WING. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE FLAPPER VALVE ON THE RT WING RIB 19, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 32,954 hrs · 31,221 cycles

DURING MX INSP, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 32,787 hrs · 31,054 cycles

DURING 2A INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78 BELOW STR 5R. MC REMOVED THE DAMAGE, AND PERFORMED A FREEZE PLUG REPAIR ISE APPROVED ETD2013-145-027513, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 32,787 hrs · 31,054 cycles

DURING 2A INSPECTION, LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED IN TWO PLACES AT A RIVET ON FRAME 79 BELOW STRINGER 5L. MX REMOVED THE DAMAGE AND PERFORMED A FREEZE PLUG REPAIR IAW IAW APPROVED ETD2013-145-027513, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 32,787 hrs · 31,054 cycles

DURING 2A INSPECTION THE LT SIDE FUSELAGE SKIN WAS FOUND TO BE CRACKED IN 2 PLACES AT A RIVET ON FRAME 77 BELOW STRINGER 8L. MX REMOVED THE DAMAGE AND PERFORMED A FREEZE PLUG REPAIR IAW APPROVED ETD2013-145-027513, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 32,017 hrs · 30,276 cycles

DURING MX INSPECTION, THE NR 5 AISLE PATH LIGHT STRIP WAS FOUND TO HAVE A BROKEN WIRE. MX R & R THE AFFECTED LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 34,093 hrs · 32,361 cycles

DURING MAINTENANCE INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED LIGHT BULB, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,711 hrs · 28,961 cycles

DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH LIGHTING STRIP AT ROW 15A WAS INOPERATIVE. MX R & R THE AFFECTED LIGHT, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,743 hrs · 27,994 cycles

DURING C-CK. CENTER OMEGA BEAM CORRODED FR 18-23. R & R CENTER OMEGA BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — INOPERATIVE (RT MLG) · airframe 29,096 hrs · 27,356 cycles

AMA - FLIGHT 4172, THE CREW REPORTED, RECEIVED A LANDING GEAR LEVER DISAGREE WARNING MESSAGE APPEARED ON CLIMBOUT. THE AIRCRAFT RETURNED TO AMA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR MANEUVERING ACTUATOR, OPERATIONALLY TESTED WITHOUT DEFECT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,924 hrs · 27,176 cycles

IAH - DURING MAINTENANCE INSPECTION THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 28,531 hrs · 26,770 cycles

MAF - FLIGHT 2079, THE CREW REPORTED THAT THE FLIGHT ATTENDANT SMELLED SMOKE IN FLIGHT IN THE FWD CLOSET AREA AND THE AREA OF ROW THREE WITH THE SMELL STILL PREVELANT AFTER SHUTDOWN. THE CREW RAN BOTH ENGINES, AND BOTH PACKS ALL WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — BURNED (CABIN) · airframe 28,355 hrs · 26,598 cycles

DURING GROUND OPERATIONS THE CREW REPORTED A SMOKE SMELL NEAR THE GALLEY. MAINTENANCE FOUND THE CABIN OVERHEAD BALLAST TO BE THE SOURCE OF THE SMOKE AND REPLACED IT. OPERATIONAL CHECKS WERE PERFORMED AND THE DISCREPANCY WAS CLEARED.

Part: BATTERY — OVERHEATED (NR 2) · airframe 26,860 hrs · 25,062 cycles

IAH - FLIGHT 2735 THE CREW REPORTED A NUMBER TWO BATTERY OVERTEMP INDICATION ON DESCENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO MAIN BATTERY. OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — OVERHEATED (CABIN) · airframe 26,002 hrs · 24,175 cycles

IAH - FLIGHT 3027, THE CREW REPORTED AN ELECTRICAL BURNING SMELL AROUND ROW 2A. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LIGHT BALLAST AT SEAT 2A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GROUND WIRE — DEFECTIVE (SPOILER) · airframe 25,552 hrs · 23,706 cycles

IAH - FLIGHT 2963, THE CREW REPORTED A SPOILER FAIL AND SPOILER OPEN INDICATION IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, CLEANED ALL PROXIMITY SWITCH CONNECTOR, REPAIRED A DEFECTIVE GROUND WIRE ON THE LT INBOARD SPOILER PROXIMITY SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: REVEAL — LOOSE (CABIN) · airframe 25,381 hrs · 23,529 cycles

CRP - FLIGHT 2820, THE CREW REPORTED THAT THE WINDOW REVEAL AT ROW 18A WAS FOUND TO BE LOOSE. THE AIRCRAFT DIVERTED TO CRP WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE SECURED THE WINDOW REVEAL, AND PLACED IT ON NEF CB-15 CTL#181048 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT SUBSEQUENTLY LANDED AT IAH WHERE MAINTENANCE SECURED THE WINDOW REVEAL IN ACCORDANCE WITH EMB-145 AMM 25-23-09, REMOVED THE NEF, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STARTER GEN — MALFUNCTIONED (APU) · airframe 25,279 hrs · 23,422 cycles

IAH - FLIGHT 3020, THE CREW REPORTED A BURNING SMELL AFTER ENGINE 1 START. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THE SMELL TO BE CAUSED BY THE APU. THE APU WAS PLACED ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT SUBSEQUENTLY RETURNED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE APU STARTER GENERATOR, OPERATIONALLY TESTED WITH NO DEFECTS, THE MEL WAS CLEARED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 24,860 hrs · 22,994 cycles

TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE SERVICE DOOR SILL CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB 135/145 SRM 51-40-02. ALODINED, PRIMED AND PAINTED IAW CPM 51-21-07. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 24,860 hrs · 22,994 cycles

TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND CORROSION AT FRAME 22 AT THE SERVICE DOOR CUTOUT. MAINTENANCE CUT OUT THE DAMAGE SECTION AND REPLACED. COLD WORK THE TWO HOLES FOR THE DOOR STOPS IAW EA 5310-01054. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FIREWALL — CRACKED (APU BAY) · airframe 24,860 hrs · 22,944 cycles

TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND A CRACK IN THE APU FIREWALL. MAINTENANCE REMOVED AND REPLACED THE FIREWALL IAW EMB 145 SRM 51-40-02 AND IC 2009-145/06143. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,859 hrs · 22,994 cycles

GALLEY CENTER AISLE LT RAMP ANGLE CRACKED. REMOVED AND REPLACED RAMP ANGLE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,859 hrs · 22,994 cycles

SHEAR CLIP CRACKED AT FRM 77 STR 1R. REMOVED AND REPLACED CRACKED SHEAR CLIP.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 24,859 hrs · 22,994 cycles

BRACKET CRACKED AT FRM 81 TO STR 8R. REMOVED AND REPLACED SHEAR CLIP.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,859 hrs · 22,994 cycles

GALLEY AREA CENTER OMEGA BEAM TOP CAP HAS SMALL AREAS OF CORROSION. CENTER TOP CAP WAS REMOVED AND REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,859 hrs · 22,994 cycles

SHEAR CLIP CRACKED AT FRM 81 TO STR 8L. REMOVED AND REPLACED SHEAR CLIP.

Part: BEARING CAP — CORRODED (RT MLG) · airframe 24,860 hrs · 22,994 cycles

TYS - A/C CURRENTLY IN C-CHECK AND INSPECTION FOUND CORROSION ON THE RIGHT FORWARD MAIN LANDING GEAR BEARING CAP WITH DEEP PITTING. MAINTENANCE REMOVED AND REPLACED THE BEARING CAP IAW EMB 145 AMM 32-20-01-400-801-A, SSI REFERENCE 57-26-94. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. THE CORROSION WAS BEYOND MFG'S LIMITS.

Part: SILL — CORRODED (FUSELAGE) · airframe 24,860 hrs · 22,944 cycles

TYS - A/C IN C-CHECK WHEN INSPECTION FOUND THE LEFT FLOOR SILL CORRODED FROM FRAME 23 TO FRAME 29 (SSI 53-20-11). MAINTENANCE REMOVED AND REPLACED THE FLOOR SILLS WHICH WERE OUTSIDE THE MFG'S LIMITS. ALL WORK WAS DONE IAW EMB 145 SRM 51-20-03 AND 51-40-02. A/C WILL BE RELEASED AT THE END OF THE CHECK.

Part: BEARING CAP — CORRODED (RT MLG) · corrosion level 2 · airframe 24,860 hrs · 22,994 cycles

RIGHT AFT MAIN LANDING GEAR BEARING CAP HAS DEEP PITTING CORROSION. REMOVED AND REPLACED CAP.

Part: CASE — CORRODED (NR 2 ENGINE) · corrosion level 2 · airframe 24,860 hrs · 22,994 cycles

NR 2 ENG FAN CASE FWD FLANGE HAS CORROSION IN BOLT HOLES. REMOVED CORROSION FROM 12 HOLES BY REAMING IAW EC 7220-01066.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 24,860 hrs · 22,994 cycles

GALLEY CENTER AISLE RT RAMP ANGLE CORRODED BEYOND LIMITS AT CARBON CROSS BEAM. REMOVED AND REPLACED RAMP ANGLE.

Part: FITTING — WORN (SPOILER ACTUATOR) · airframe 24,860 hrs · 22,940 cycles

RT SPEED BRAKE ACTUATOR BRACKET LOWER ATTACHMENT HAT BUSHING BORE OUT OF LIMITS. REMOVED AND REPLACED FITTING.

Part: BUSHING — WORN (SPOILER) · airframe 24,860 hrs · 22,944 cycles

TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE RIGHT GROUND SPOILER, CENTER HINGE BRACKET HAT BUSHING RACE OUT OF MFG'S LIMITS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW EMB 145 SRM 51-40-02. A/C WILL BE RELEASED AT THE END OF THE CHECK. SSI REFERENCE 57-28-70.

Part: SPAR CAP — CORRODED (LT WING) · airframe 24,860 hrs · 22,944 cycles

TYS - SURFACE CORROSION WAS FOUND ON THE LEFT WING SPAR ONE I/B CAP. MAINTENANCE REMOVED THE LITE CORROSION IAW EMB 135/145 SRM 57-20-01. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: HINGE — CORRODED (HORIZONTAL STAB) · airframe 24,860 hrs · 22,940 cycles

LEFT AND RIGHT HORZ STAB HINGE PINS PITTED AND HAVE CORROSION. REPLACED HINGE PINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,785 hrs · 21,840 cycles

IAH - FLIGHT 2819 - DURING POST FLIGHT INSPECTION THE CREW REPORTED THE 3RD AISLE PATH EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED AISLE PATH LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (GALLEY) · airframe 23,720 hrs · 21,766 cycles

IAH - FLIGHT 3059 THE CREW REPORTED A BURNING SMELL IN THE GALLEY DURING TAXI. THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED ENGINE RUNS, AND OPERATIONALLY CHECKED THE COFFEEMAKERS, ALL WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — UNKNOWN (MLG) · airframe 23,571 hrs · 21,611 cycles

IAH FLIGHT 3123 THE CREW REPORTED A LOUD THUMPING NOISE 3 OR 4 TIMES AFTER GEAR RETRACTION. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, OPS CHECKED THE LANDING GEAR EXTENSION AND RETRACTION MULTIPLE TIMES WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UPLOCK — DEFECTIVE (LT MLG) · airframe 22,205 hrs · 20,299 cycles

FLIGHT 2400 - EWR - CREW REPORTED NOSE LANDING GEAR MADE CONTINUOUS BANGING SOUND AFTER RETRACTION. CREW DIVERTED FLIGHT TO EWR AND LANDED AIRCRAFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED LEFT MAIN GEAR UPLOCK BOX AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROL UNIT — FAULTY (MLG) · airframe 20,095 hrs · 18,101 cycles

CLE FLIGHT 2727 THE CREW REPORTED LOUD NOISE AND VIBRATION FROM FRONT OF AIRPLANE. THE GEAR WAS RECYCLED AND THE NOISE WENT AWAY. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS STAYING OPEN. THE LGEU WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,138 hrs · 17,071 cycles

RIC - MX DURING ACFT ROUTINE INSPECTION, MX FOUND NR 7 FLOOR PROXIMITY EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED PROXIMITY LIGHT ASSY. OPERATIONAL TEST PERFORMED SUCCESFULLY. ACFT APPROVED TO RETURN TO SERVICE.

Part: SOLENOID VALVE — STICKING (NLG) · airframe 18,649 hrs · 16,525 cycles

CLE FLIGHT 2236 THE CREW REPORTED THE NOSE GEAR DOORS STAYED OPEN AFTER GEAR RETRACTION. EVENTUALLY SLAMMED SHUT. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR DOOR SOLENOID VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: DUCT — FAILED (NR 2 A/C PACK) · airframe 16,871 hrs · 14,480 cycles

BNA/EWR---CO2882, DURING PREFLIGHT INSPECTION CREW REPORTED, SMOKE FROM VENTS, ELECTRICAL IN NATURE FROM PACK NR 2. NASHVILLE MAINTENANCE INSPECTED AIRCRAFT AND RELEASED IAW MEL NR 21-51-00/1 CATEGORY-C CONTROL NUMBER 059962. AIRCRACT ARRIVED IN EWR AND NEWARK MAINTENANCE PERFORMED OPERATIONAL CHECK OF PACK NR 2. FOUND BLOWN DUCT ON PACK NR 2 REPLACED DUCT ON NR 2 PACK IAW EMB AMM 21-51-03. RAN FOR 30 MINUTES. NO FAULTS [OR SMOKE] NOTED IAW EMB145 AMM 21-51-00. OPS CHECKED GOOD. REMOVED AIRCRAFT FROM MEL.

Part: APU — ODOR (APU BAY) · airframe 16,857 hrs · 14,468 cycles

DURING ROUTINE MAINTENANCE, OIL ODOR IN CABIN WAS NOTED WHEN APU BLEED WAS SELECTED. MX RELEASED ACFT IAW MEL 49-00-00. MX REPLACED APU. OPS CHECKS WERE GOOD.

Part: SMOKE DETECTOR — INTERMITTENT (LAVATORY) · airframe 16,842 hrs · 14,450 cycles

CREW REPORTED INTERMITTENT LAVATORY SMOKE WARNING ON GROUND AND INFLIGHT. MX INSP AND REPLACED LAVATORY SMOKE DETECTOR. OPS CHECKS GOOD.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 16,255 hrs · 13,834 cycles

RIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND SERVICE DOOR OVERHEAD EMERGENCY LIGHT (ONE BULB) NOT WORKING. MAINTENANCE REPOSITION BULB AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — FAULTY (FUSELAGE) · airframe 16,068 hrs · 13,621 cycles

EWR---CO2383, CREW REPORTED RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT HOUSING IAW EMB145 AMM NR 33-50-10, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 15,734 hrs · 13,265 cycles

DURING C CHECK, THE FASTENER HOLES AT FRAME 61, STRINGER 11R WHERE FOUND DAMAGED. INSTALLED A REPAIR DOUBLER IAW 51-40-02 AND CMP 51-21-04/05. AIRCRAFT RETURNED TO SERVICE

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,734 hrs · 13,265 cycles

DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 20 TO 22. REMOVED THE CORRODED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5320-01131 AND SRM 53-21-10. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

CLE FLIGHT NR 2278 THE CREW REPORTED THE EMERGENCY EXIT SIGN BEHIND THE F/A SEAT WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

THE CREW REPORTED THE FORWARD EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. MAINTENANCE REPLACED THE EXIT MARKING SIGN. OPERATIONAL CHECKS WERE GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 12,325 hrs · 9,751 cycles

BWI---CO2476, CREW REPORTED FIRST OFFICERS WINDSHIELD SHATTERED IN FLIGHT AIRCRAFT DIVERTED TO BWI. AIRCRAFT LANDED UNEVENTFULLY. EWR MAINTENANCE WORKING WINDSHIELD CHANGE AT THIS TIME.

Part: DUCT — DAMAGED (NR 2 ENGINE)

FLIGHT 3789, THE CREW NOTED A FIRE INDICATION NR 2 ENGINE AFTER TAKEOFF. THE CREW SHUTDOWN NR 2 ENGINE, DECLARED EMERGENCY, AND, RETURNED TO HSV, AND, LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ANTI ICE BLEED DUCT, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE,

Part: PRESSURE SWITCH — FAILED (RUDDER)

THE CREW NOTED THAT THE RUDDER SYSTEMS NR 1 AND NR 2, INOPERATIVE. ON DEPARTURE, THE CREW DECLARED EMERGENCY. PERFORMED AN EMERGENCY DESCENT. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 RUDDER SYSTEM PRESSURE SWITCH. PERFORMED AN OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRESSURE SWITCH — INOPERATIVE (TAIL)

IAH- FLIGHT 3558, THE CREW NOTED THAT THE RUDDER SYSTEMS #1 & #2 INOPERATIVE, ON DEPARTURE FOR (TYS), THE CREW DECLAIRED EMERGENCY, AND, PERFORMED AN EMERGENCY DESCENT. THE AIRCRAFT RETURNED TO (IAH), AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE #1 RUDDER SYSTEM PRESSURE SWITCH, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CIRCUIT CARD — MALFUNCTIONED (AUTOPILOT SYS)

THE CREW NOTED THAT THE AUTOPILOT/YAW DAMPER FAILED. MAINTENANCE REMOVED AND REPLACED THE NR 1 IC-600. PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CRACKED (CABIN) · airframe 11,963 hrs · 9,373 cycles

DURING C CHECK LT OMEGA BEAM WAS FOUND TO HAVE A CRACK ON RIVET AT FRAME 22. MAINTENANCE REPAIRED CRACK ON RIVET IAW CONTINENTAL EXPRESS EC 5320-01081. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,963 hrs · 9,373 cycles

DURING C CHECK, LT FLOORBEAM RAMP ANGLE INBOARD AT FRAME 20 HAS CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,963 hrs · 9,373 cycles

SHV-DURING C CHECK LEFT HAND SILL WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 23 AND 24. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,963 hrs · 9,373 cycles

SHV-DURING C CHECK CROSS BEAM BETWEEN FRAMES 23 AND 24 FROM CENTER OMEGA BEAM T O RIGHT HAND OMEGA BEAM WAS FOUND TO HAVE CORROSION. MAITENANCE REMOVED DAMAGE AND REPLACED AFFECTED CROSS BEAM IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 11,963 hrs · 9,373 cycles

SHV-DURING C CHECK THE SUPPORT RAMP ON CENTER OMEGA BEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACE SUPPORT RAMP IAW EMB SRM51-20-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,963 hrs · 9,373 cycles

SHV- DURING C CHECK NUTPLATES WITH CORROSION WERE FOUND JUST FOWARD OF SERVICE DOOR THRESHOLD. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SILL IAW EMB SRM 51-20-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,963 hrs · 9,373 cycles

SHV- DURING C CHECK CENTER FLOOR BEAM STRAP AT DOUBLER WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 15 AND16. MAINTENANCE REMOVED DAMAGE AND PEFPORMED A DOUBLER REPAIR IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: THRESHOLD — CORRODED (CABIN) · corrosion level 2 · airframe 11,963 hrs · 9,373 cycles

DURING C CHECK AFT SUPPORT UNDER MAIN DOOR THRESHOLD WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SUPPORT IAW 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,963 hrs · 9,373 cycles

DURING C CHECK, THE CENTER FLOORBEAM AT FRAME 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 11,963 hrs · 9,373 cycles

SHV DURING C CHECK THE CENTER OMEGA BEAM STRAP BETWEEN FRAMES 18 AND 23 WAS FOUND HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED THE AFFECTED OMEGA BEAM STRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — FAULTY

EWR---CO4085, CREW REPORTED, "BOTH EMERGENCY LIGHTS OVER WING INOPERATIVE....MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT UNITS FOR BOTH EMERGENCY LIGHTS OVER THE WINGS IAW EMB145 AMM #33-50-04. OPS.CHECKED GOOD.

Part: WIRE — BROKEN (CABIN)

IAH- WHILE PERFORMING PREFLIGHT INSPECTION THE CREW NOTED THAT A SECTION OF EMERGENCY LIGHTING DID NOT ILLUMINATE. IAH- MAINTENANCEREPAIRED A BROKEN WIRE ON THE EMEMGENCY LIGHT STRIP, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: APU — LEAKING (APU BAY)

AMA- THE CREW NOTED THAT AN ELECTRICAL SMELL WAS PRESENT IN THE CABIN/COCKPIT WHILE THE APU IS RUNNING, WITH THE APU BLEED SELECTED OFF. MAINTENANCE REMOVED AND REPLACED THE APU, PERFORMED A OPERATIONAL CHECK AND A LEAK CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL HANDLE — FAULTY (COCKPIT) · airframe 9,501 hrs · 7,056 cycles

EWR---CO4292, CREW REPORTED LANDING GEAR DID NOT RETRACT ON TAKEOFF. INDICATIONS SHOWED GEAR DOWN. CYCLED HANDLE, LANDING GEAR CAME UP AND INDICATED UP. NOSE GEAR DOORS STAYED OPEN. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 MM 32-32-02. OPERATIONALLY CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN)

CLE FLIGHT 3690 THE CREW REPORTED THE 2ND STRIP OF AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR OF THE 2ND STRIP OF EMERGENCY LIGHTS. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACM — FAILED (A/C BAY)

CLE FLIGHT 3992 THE CREW REPORTED A HEAVY BURNING ODOR IN THE COCKPIT AND CABIN FOLLOWED BY SMOKE DURING TAKEOFF AND AFTER LANDING. RECEIVED A PACK NR 1 OVERHEAT MESSAGE. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE — BROKEN (CABIN)

CLE FLIGHT NR 3623 THE CREW REPORTED AISLE PATH EMERGENCY LIGHTS BY SEATS 8 AND 9 INOPREATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND OPERATIOMAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FIRE BOTTLE — INOPERATIVE (NR 2 ENGINE)

CLE FLIGHT 4089 THE CREW REPORTED EXTINGUISHER BOTTLE-B INOP MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE FIRE BOTTLE. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: A/C PACK — FAILED (NR 1)

DAL - FLIGHT 4061, THE CREW REPORTED THAT ON INITIAL CLIMBOUT, THE COCKPIT AND CABIN FILLED WITH SMOKE ACCOMPANIED BY AN ELECTRICAL BURNING SMELL. THE AIRCRAFT RETURNED TO DAL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE NUMBER ONE PACK HAD FAILED. MAINTENANCE PLACED THE AFFECTED PACK ON MEL 21-51-00 CAT-C CONTROL NUMBER 004973, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON 01/16/01, WHERE MAINTENANCE REMOVED AND REPLACED THE NR 1 PACK AIR CYCLE MACHINE, REMOVED MEL 21-51-00 CONTROL 004973, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRAP — CORRODED (CABIN)

DURING C-CHECK INSPECTION, RIGHT SIDE FLOORBEAM BUTT-STRAP BETWEEN FRAMES 59 TO 61 WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED CORRODED SECTION OF FLOORBEAM IAW EMB145 SRM 51-40-02. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CRACKED (FUSELAGE)

DURING C-CHECK INSPECTION, REAR SECTION II, STRINGER #16 RIGHT AT APU FIREWALL. THE SUPPORT ANGLE WAS FOUND TO BE CRACKED. MX REMOVED/REPLACED THE CRACKED ANGLE WITH A FABRICATED PART IAW EMB145 SRM 51-40-02 AND 51-30-01. A/C WAS APPROVED FOR RETURN FOR SERVICE.

Part: STRAP — CORRODED (CABIN)

DURING C-CHECK INSPECTION, THE CENTER FLOOR BEAM BUTT-STRAP BETWEEN FRAMES 60 TO 61 WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED CORRODED SECTION OF THE FLOOR BEAM IAW EMB145 SRM 51-40-02. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CHAFED (CARGO BAY)

DURING C CHECK INSPECTION, FRAME 65 RIGHT SIDE FLANGE WAS FOUND TO BE CHAFED BY A CARGO LINER FASTENER. MX REPAIRED THE FRAME AND REPOSITIONED THE CARGO LINER FASTENER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5310-01146

Part: FLOORBEAM — CORRODED (FUSELAGE)

IAH-DURING C-CHECK INSPECTION, THE CENTER FLOOR BEAM WAS FOUND TO BE CORRODED FROM FRAME 60-61. MX REMOVED/REPLACED AFFECTED FLOOR BEAM IN ACCORDANCE WITH EMB145 SRM 51-40-02 AND A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE)

IAH-DURING C-CHECK INSPECTION, RH FLOOR BEAM WAS FOUND TO BE CORRODED FROM FRAME 59-61. MX REMOVED/REPLACED THE AFFECTED FLOOR BEAM IN ACCORDANCE WITH EMB145 SRM 51-40-02, AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: STRAP — CORRODED (CABIN)

YYZ-DURING MOD-LINE INSPECTION, THE FORWARD CENTER BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND INSTALLED A REPAIR DOUBLER IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5310-01107, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — MALFUNCTIONED (FUSELAGE)

BTV - FLT 4201 - CREW REPORTED SMOKE IN THE COCKPIT AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO TYS WHERE ROLLS ROYCE SERVICE BULLETIN NR AE3007A-A-72-156 WAS COMPLIED WITH ON THE LEFT ENGINE. THE ENGINE FAILED OPERATIONAL CHECKS DUE TO HIGH OIL PRESSURE AND WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. THE OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: SEAL — LEAKING (FAN)

BTV-TYS - FLT 4201 - CREW REPORTED SMOKE IN COCKPIT AFTER TAKEOFF. AIR RETURNED TO BTV. TROUBLESHOT AND DETERMINED THAT OIL WAS LEAKY FAN SEAL. AIRCRAFT MAINTENANCE FERRIED TO TYS MAINTENANCE COMPLIED WITH ROLLS ROYCE SERVICE BULLETIN AND REPLACED TELFON LIP SEAL WITH NEW ONE. LEAKS AND OPS CHECK GOOD AIRCRAFT RETURNED TO SERVICE. (M)

Part: DUCT — WEAK (LT PACK)

CLE - FLT 3942 - SMOKE FROM CENTER CONSOLE ALONG WITH SMOKE IN THE CABIN AND COCKPIT. AIRCRAFT RELEASED IAW MEL 36-11-05 CONTROL NR 184831. MAINTENANCE REMOVED AND REPLACED THE LT PACK DTV DUCT AND REPLACED THE BROKEN CLAMP IAW EMB-145 MM 36-11-9. OPS AND LEAK CHECKS WERE GOOD. REF: EMB-145 IPC 21-51-00 FIG 25 ITEMS 130, 180, 230, FOR PARTS CHANGED. AIRCRAFT IS RELEASED. REF: OPERATOR CNTRL NR C2XA99CL073 DATED 8-10-99. REF: OPERATOR CNTRL NR C2XA99CL074.

Part: DUCT — LOOSE (LT PACK)

MSP/CLE - FLT 4012 - THE CREW REPORTED SMOKE FROM THE CENTER CONSOLE ALONG WITH SMOKE IN THE CABIN AND COCKPIT. THE AIRCRAFT DIVERTED TO GRB AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A DUCT HAD BLOWN OFF THE LEFT PACK SYSTEM, THEY RELEASED THE AIRCRAFT IAW MEL 36-11-05, CONTROL NUMBER 184831 DAT 'C'. THE AIRCRAFT WAS RELEASED TO SERVICE. (X)

Part: CLAMP — BROKEN (LT PACK)

CLE - FLT 3942 - SMOKE FROM CENTER CONSOLE ALONG WITH SMOKE IN THE CABIN AND COCKPIT. AIRCRAFT RELEASED IAW MEL 36-11-05 CONTROL NR 184831. MAINTENANCE REMOVED AND REPLACED THE LT PACK DTV DUCT AND REPLACED THE BROKEN CLAMP IAW EMB-145 MM 36-11-9. OPS AND LEAK CHECKS WERE GOOD. REF: EMB-145 IPC 21-51-00 FIG 25 ITEMS 130, 180, 230, FOR PARTS CHANGED. AIRCRAFT IS RELEASED. REF: OPERATOR CNTRL NR C2XA99CL073 DATED 8-10-99. REF: OPERATOR CNTRL NR 99ZZZX3197. (X)

Part: ENGINE — LEAKING (LEFT)

BTV - FLT 4201 - CRWE REPORTED, 'LAV SMOKE INDICATION FOLLOWED BY BAG SMOKE IN INDICATION AFTER TAKEOFF, BOTH INDICATIONS EXTINGUISHED ON GROUND AFTER AREA RETURN. CAUSED OVERWEIGHT LANDING'. PRESENTLY MAINTENANCE IS TROUBLESHOOTING CAUSE OF INDICATIONS. PERFORMED OVERWEIGHT LANDING INSPECTION AND NO DEFECTS WERE NOTED. FOUND NR 1 ENGINE FAN SEAL LEAKING MAINTENANCE REMOVED AND REPLACED THE ENGINE OPS CHECKED AND LEAKED CHECKED ENGINE OK. RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — FOD (BAGGAGE COMP)

BTV - MAINTENANCE TROUBLESHOT AND REPAIRED BAGGAGE SMOKE WARNING ON LANDING REPORT FROM CREW. FOUND SCREW STUCK IN BAGGAGE FORWARD SMOKE DETECTOR. REMOVED SCREW, OPS CHECKED SYSTEM GOOD AND RETURNED TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

IAH - DURING C-CHECK INSPECTION, FOUR OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULBS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BEAM — CORRODED (FRAME 20)

IAH - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20 EXTENDING UNDER THE BUTT STRAP. MAINTENANCE REMOVED THE CORROSION AND INSTALLED REINFORCEMENTS IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01106, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (VERT STAB)

IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD FUSELAGE TO VERTICLE STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5530-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (VERT STAB)

IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD FUSELAGE TO VERTICLE STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5530-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: AIR DIST — ODOR (COCKPIT)

CLE - FLT 4059 - CREW REPORTED THAT AFTER SETTING TAKEOFF POWER THEY RECEIVED A SMOKE SMELL IN THE COCKPIT. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND RELEASED IT IAW MEL 21-51-00 CONTROL NR 173359. ON 3/24/99 MAINTENANCE PERFORMED A SYSTEM OPERATIONAL CHECK OF THE LEFT PACK, NO DEFECT WERE NOTED IAW EMB145 MM 21-51-00. AIRCRAFT REMOVED FROM MEL. (M)

Part: SKIN — CRACKED (FUSELAGE)

SMALL CRACK IN SECTION OF FUSELAGE BEHIND PASSENGER DOOR. REPAIRED DAMAGED SECTION OF FUSELAGE IAW SRM. PRESSURE CHECKED GOOD. (M)

Part: AIR DISTRIBUTION — SMOKE (COCKPIT)

FLT 4251 - CREW REPORTED SMOKE IN COCKPIT IMMEDIATELY AFTER ADVANCING THRUST LEVER FOR TAKEOFF. TAKEOFF WAS REJECTED. MAINTENANCE INSPECTED NR 1 AND NR 2 ENGINES, APU COMPARTMENT, AVIONIC BAYS FORWARD AND AFT, HYD COMPARTMENTS, LAV AND BAGGAGE COMPARTMENTS FOR PRESENTS OF SMOKE OR EXCESSIVE HEAT. PERFORMED ENGINE GROUND RUNS FOR 20 MINS AT VARIOUS THRUST SETTINGS AND VARIOUS PACK SETTINGS. NO SMOKE OR OTHER DEFECTS NOTED, REF EMB145 MM 71-00-01 FOR RUNS. (M)

Part: ENGINE — FAILED (RT ENG OIL PRESS)

CLE - FLT 4006 - CREW REPORTED WHEN THE POWER LEVERS WERE PLACED IN THE TAKEOFF OR CONTINUAL THRUST DETENT, THE LEFT HAND AND RIGHT HAND ENGINES' OIL PRESSURE REMAINED HIGH. AFTER EXTENSIVE TROUBLESHOOTING, MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X)

Part: ENGINE — FAILED (LEFT)

CLE - FLT 4006 - CREW REPORTED WHEN POWER LEVERS PLACED IN THE TAKEOFF OR CONTINUAL THRUST DETECT, THE LEFT HAND AND RIGHT HAND ENGINES' OIL PRESSURE REMAINED HIGH. AFTER EXTENSIVE TROUBLESHOOTING, MAINTENANCE REMOVED AND REPLACED THE LEFT HAND ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS SATISFACTORY. THE RIGHT HAND ENGINE REMOVAL AND REPLACEMENT IS PENDING. (X)