N14943

Part: SKIN — CRACKED (FUSELAGE) · airframe 29,012 hrs · 28,330 cycles

DURING MX INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75, STRINGER 02L. MX PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,012 hrs · 28,330 cycles

DURING MX INSPECTION, FUSELAGE SKIN WAS FOUND TO BE CRACKED ACROSS A RIVET HOLE APPROX 16MM IN LENGTH BETWEEN FRAME 77-78 JUST ABOVE STR 6R. MX INSTALLED A REPAIR DOUBLER ON THE AFFECTED AREA, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,012 hrs · 28,330 cycles

DURING MX INSPECTION, THE FUSELAGE SKIN AT FR 75 ON EITHER SIDE OF STRINGER 2R WAS FOUND TO HAVE TWO CRACKS ONE APPROX .039" AND 1 APPROX .157" LONG. MX PERFORMED A DOUBLER REPAIR ON THE AFFECTED AREA, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 12/02/12.

Part: ENGINE — SMOKE (ZONE 400) · airframe 28,437 hrs · 27,745 cycles

GROUND CREW REPORTED FLAMES FROM NR 1 ENGINE. ENGINE SMOKING 15 MIN AFTER SHUTDOWN. R & R 1 ENGINE IAW AMM 71-00-00. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 27,778 hrs · 27,075 cycles

THE CREW REPORTED A BAGGAGE SMOKE WARNING ON EICAS. THE CREW DISCHARGED THE BAGGAGE FIRE EXTINGUISHERS AND THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND R & R THE FORWARD BAGGAGE SMOKE DETECTOR, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 26,700 hrs · 26,005 cycles

IAH - FLIGHT 4586, THE CREW REPORTED WEIRD SMELL DURING ENGINE START. MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED ENGINE STARTS, OPERATIONALLY CHECKED BLEED SYSTEMS ALL WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 24,969 hrs · 24,209 cycles

FLIGHT 2561 THE CREW REPORTED A BURNING SMOKE SMELL IN THE CABIN WITH THE NUMBER TWO ENGINE, NUMBER 2 BLEED, AND NUMBER TWO PACK RUNNING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NO PARTS WERE IDENTIFIED AS CAUSING THE BURNING SMOKE ODOR.

Part: ACM — SEIZED (AC BAY) · airframe 24,969 hrs · 24,209 cycles

IAH - FLIGHT 2561, THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN ON SHORT FINAL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ACM, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,574 hrs · 23,778 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24-25. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,574 hrs · 23,778 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 33-34. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,574 hrs · 23,778 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAMES 22-23. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01257. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,574 hrs · 23,778 cycles

SHV - DURING C-CHECK THE SHEAR CLIP AT FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 16-17L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW EC5310-01505. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 24,574 hrs · 23,778 cycles

SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 23,944 hrs · 23,136 cycles

MEM - FLIGHT 2249, DURING DESCENT THE CREW REPORTED THAT AUTO PRESSURIZATION FAILED. THE AIRCRAFT LANDED AT MEM WITHOUT INCIDENT WHERE THE CREW PLACED THE AUTO PRESSURIZATION ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE DIGITAL PRESSURIZATION CONTROLLER, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 23,858 hrs · 23,047 cycles

IAH - FLIGHT 2132, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE EXIT SIGN AT SEAT 12C TO BE INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHTS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — FAILED (BLEED AIR SYS) · airframe 23,021 hrs · 23,834 cycles

FLT 2159 MEM-IAH DIVERT TO AEX - BLEED 1 LOW TEMP/ENG OPEN LIGHT NOT ILLUM IN ICING - SHV RECOVERY. MAINTENANCE PERFORMED ANTI-ICE OPERATIONAL CHECKS IAW EMB-145 AMM 30-00-00 (ALL OPS CHECK GOOD). ALSO, MAINTENANCE REMOVED AND REPLACED RELAY KO528 ON RT RELAY SUPPORT. PERFORMED OPERATIONAL CHECK OF ENG 1 BLEED. OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,731 hrs · 22,913 cycles

SEAT 12BC OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB IAW EMB145 AMM 33-50-07, OPS CHECK GOOD.

Part: CLAMP — DEFECTIVE (NR 1 ENGINE) · airframe 23,610 hrs · 22,786 cycles

IAH - FLIGHT 2069 THE CREW REPORTED A BLEED ONE LEAK DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FORWARD CLAMP ON THE NUMBER ONE ENGINE BLEED VALVE. OPERATIONAL AND LEAK CHECKS WERE COMPLETED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — LEAKING (BLEED AIR SYS) · airframe 23,603 hrs · 22,776 cycles

IAH - FLIGHT 2277, THE CREW REPORTED A BLEED ONE LEAK MESSAGE DURING CRUISE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT CARGO WALL "T" DUCT, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THERMOSTAT — INOPERATIVE (NR 1 ENGINE) · airframe 23,593 hrs · 22,765 cycles

IAH - FLIGHT 2413 - THE CREW REPORTED A BLEED 1 LOW TEMP DURING ICING TEST. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE BLEED THERMOSTAT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 23,341 hrs · 22,506 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED AISLE PATH EMERGENCY LIGHTS TO BE INOPERATIVE IN THE REAR OF THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE LAST INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (MLG) · airframe 22,693 hrs · 21,809 cycles

DURING CLIMB THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE. ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE LT MAIN GEAR WOW PROXIMITY SWITCH ON THE SHOCK ABSORBER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (LT MLG) · airframe 22,693 hrs · 21,809 cycles

IAH - FLIGHT 2703 - DURING CLIMB THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR WOW PROXIMITY SWITCH ON THE SHOCK ABSORBER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 16,363 hrs · 12,527 cycles

IAH - DURING A-CK INSPECTION THE LT FORWARD WING BOX EMERGENCY LIGHT, PAX DOOR EMERGENCY LIGHT, AND EMERGENCY LIGHT ABOVE THE FORWARD F/A SEAT WERE FOUND TO BE INOPERATIVE. MX R&R THE NR 1 EMERGENCY LIGHT BATTERY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,463 hrs · 20,524 cycles

IAH - FLIGHT 2372 - THE FLIGHT ATTENDANT REPORTED A BURNING ODOR COMING FROM ROWS 8-10. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFECTS NOTED, AND COULD NOT DUPLICATE THE DISCREPANCY. THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE. (A)

Part: BLEED VALVE — FAULTY (NR 1 ENGINE) · airframe 20,382 hrs · 19,440 cycles

BWI FLIGHT 2247 - THE CREW REPORTED A NR 1 ENGINE BLEED VALVE FAIL MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: GENERATOR — INOPERATIVE (NR 1) · airframe 20,205 hrs · 19,265 cycles

FLT 3142 - EWR - CREW REPORTED APU GENERATOR AND GENERATOR NR 1 OFF BUSS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED APU GCU AND GENERATOR NR 1 AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: GCU — INOPERATIVE (APU) · airframe 20,205 hrs · 19,265 cycles

FLT 3142 - EWR - CREW REPORTED APU GENERATOR AND GENERATOR NR 1 OFF BUSS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED APU GCU AND GENERATOR NR 1 AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: WIRE — CHAFED (EMERGENCY LIGHTS) · airframe 20,105 hrs · 19,169 cycles

FLT 2616 - RIC - CREW REPORTED PAX DETECTED ELECTRIC TYPE OF SMOKE. RIC MX FOUND ELECTRIC EMERGENCY SIGN AT ROW 3BC WITH BARE WIRE EXPOSED. MX REPAIRED WIRE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: RELAY — FAILED (SMOKE DETECTION) · airframe 20,014 hrs · 19,074 cycles

FLIGHT 2929 - EWR - CREW REPORTED BAGG SMOKE LIGHT ON, BUT NO VISUAL SMOKE IN CARGO BAY. EWR MX REMOVED AND REPLACED BAGG SMOKE TEST RELAY AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,813 hrs · 18,856 cycles

SHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION ON FR 20. MX REPAIRED LEFT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-13. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 18,861 hrs · 17,847 cycles

IAH - FLIGHT 2277, THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN ABOVE THE F/A SEAT WORKED INTERMITTENTLY. MAINTENANCE INSPECTED THE AIRCRAFT AND RESECURED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 17,484 hrs · 16,196 cycles

IAH - FLIGHT 2415, THE CREW REPORTED THAT THE LT FUSELAGE EXTERIOR LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,970 hrs · 14,476 cycles

IAH - FLIGHT 2418, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE LOWER AFT LEFT EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,566 hrs · 13,996 cycles

SHV-DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM FLOOR SUPPORT FLANGE HAS CORROSION BETWEEN FRAMES 20-24. MAINTENANCE REMOVED & REPLACED LT OMEGA BEAM FROM FRAMES 20-23 I/A/W EC 5320-01229. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,566 hrs · 13,996 cycles

SHV-DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM HAS CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FROM FRAMES 11-23 I/A/W EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE — WORN (RUDDER) · airframe 15,566 hrs · 13,996 cycles

SHV-DURING C-CHECK MAINTENANCE FOUND HAT BUSHING HOUSING AT ATTACHMENT FITTING FOR UPPER HYDRAULIC ACTUATOR ON RUDDER I IS WORN. MAINTENANCE REPAIRED HAT BUSHING HOUSING FOR UPPER HYDRAULIC ACTUATOR ON RUDDER I I/A/W EC 5540-01043 REV A. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — LIGHTNING STRIKE (FUSELAGE) · airframe 15,566 hrs · 13,996 cycles

SHV-DURING C-CHECK MAINTENANCE FOUND LIGHTNING STRIKE AT FRAME 23 STR 17R. MAINTENANCE REPAIRED LIGHTNING STRIKE AT FRAME 23 STR 17R I/A/W EC 5330-01480, REPAIR FIGURE #1. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 15,566 hrs · 13,996 cycles

SHV-DURING C-CHECK MAINTENANCE FOUND R/H FUSELAGE SKIN HAS A DENT BETWEEN FRAMES 19 AND FRAME 20 AT STR 17R. MAINTENANCE REPAIRED DENT AT R/H FUSELAGE SKIN AT FRAME 19 -20, STR 18R (INSTEAD OF 17R) I/A/W EC 5330-01480, REPAIR FIGURES 4 AND 7. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — LIGHTNING STRIKE (FUSELAGE) · airframe 15,566 hrs · 13,996 cycles

SHV-DURING C-CHECK MAINTENANCE FOUND LIGHTNING STRIKES AT LOWER RT WING, NEAR PNL 631 AB. MAINTENANCE REPAIRED LIGHTNING STRIKES AT LOWER RT WING, NEAR PNL 631 AB I/A/W EC 5330-01480, REPAIR FIGURES NR 5 7 & 6. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — LIGHTNING STRIKE (FUSELAGE) · airframe 15,566 hrs · 13,996 cycles

SHV-DURING C-CHECK MAINTENANCE FOUND LIGHTENING STRIKES AT FRAME 13, STRS 19R - 20R. MAINTENANCE REPAIRED LIGHTENING STRIKES AT FRAME 13, STRS 19R-20R IAW EC 5330-01480, REPAIR FIGURE 3. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,566 hrs · 13,996 cycles

SHV-DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRAMES 38-46. MAINTENANCE REPAIRED LT OMEGA BEAM BETWEEN FRAMES 38 & 46 I/A/W EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — LIGHTNING STRIKE (FUSELAGE) · airframe 15,566 hrs · 13,996 cycles

SHV-DURING C-CHECK MAINTENANCE FOUND LIGHTENING STRIKE AT FRAMES 21-22, STR 18R. MAINTENANCE REPAIRED LIGHTENING STRIKES AT FRAMES 21-22, STR 18R I/A/W EC 5330-01480, REPAIR FIGURE NR 2. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE — CRACKED (RUDDER) · airframe 15,566 hrs · 13,996 cycles

SHV-DURING C-CHECK MAINTENANCE FOUND RUDDER II UPPER MIDDLE ATTACHMENT BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED RUDDER II UPPER MIDDLE ATTACHMENT BRACKET (HINGE FITTING) I/A/W EC 5540-01028. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,566 hrs · 13,996 cycles

SHV-DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM LOWER FLANGE IS CORRODED BETWEEN FRAMES 53-59. MAINTEANACE REPAIRED LOWER FLANGE AT FRAME 54 I/A/W EMB 145 SRM 53-00-10 & EC 5320-01140. INSTALLED NEW NUTPLATES I/A/W EC 5320-01137. PREPPED, PRIMED & PAINTED ALL BLEND OUTS ON LT OMEGA BEAM LOWER FLANGE BETWEEN FRAMES 53-59 I/A/W EMB 145 CPM 51-21-06. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — LIGHTNING STRIKE (FUSELAGE) · airframe 15,566 hrs · 13,996 cycles

SHV- DURING C-CHECK MAINTENANCE FOUND LIGHTENING STRIKES FROM FRAMES 19-20, STR 18R (MID) & 18R(AFT). MAINTENANCE REPAIRED LIGHTENING STRIKES AT FRAMES 19-20, STR 18R MID & 18R AFT I/A/W EC 5330-01480, REPAIR FIGURES 4 & 7. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,566 hrs · 13,996 cycles

SHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION BTW FR 28-33.MAINTENANCE BLENDED LT OMEGA BEAM FRMS 28-33. FR 33 IS OUT OF LIMITS ALL OTHER FRMS WITHIN LIMITS IAW EMB 145 SRM 53-22-10.REPAIRED LT OMEGA BEAM AT FR 33 IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,566 hrs · 13,996 cycles

SHV-DURING C-CHECK LT OMEGA BEAM HAS VARIOUS AREAS OF CORROSION BTW FR 45-52.MAINTENANCE BLENDED LT OMEGA BEAM BTW FR 45-52. FR 49 IS OUT OF LIMIT ALL OTHER FRMS WITHIN LIMIT IAW EMB SRM 53-23-10. REPAIR OMEGA BEAM AT FR 49 IAW EMB 145 SRM 53-00-10 FIGURE 202, SHEET 2.INSTALLED NUTPLATES IAW EC 5320-01137. THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,566 hrs · 13,996 cycles

SHV-DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BTW FRM 35-39. MAINTENANCE BLENDED LT OMEGA BEAM BTW FRMS 35-39. FR 38 IS OUT OF LIMIT ALL OTHER FRMS ARE WITH IN LIMITS IAW EMB 145 SRM 53-23-10. REPAIRED L/H OMEGA BEAM AT FRM 38 IAW EMB 145 SRM 53-00-10 SECTION 3 FIGURE 202 SHEET 1. INSTALLED NUTPLATE IAW EC 5320-01137. THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,566 hrs · 13,996 cycles

SHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BTW FRMS 38-46. MAINTENANCE BLENDED LT OMEGA BEAM BTW FRMS 38-46. FR 44 IS OUT OF LIMIT ALL OTHER FRMS WITHIN LIMIT IAW EMB 145 SRM 53-23-10.REPAIRED LT OMEGA BEAM AT FR 44 IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE

Part: FIREWALL — CRACKED (AFT APU) · airframe 15,566 hrs · 13,996 cycles

SHV-DURING C-CHECK APU FIREWALL HAS MULTIPLE CRACKS (4) AROUND RIVETS. MAINTENANCE STOP DRILL CRACKS PER SRM 51-10-02 AND INSTALL DOUBLER SIZE TO ENCOMPASS CRACKS USING PRINCIPLES DESCRIBE IN SRM 53-32-12 ITEM 6 AND USING EC 5330-01473.THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 15,485 hrs · 13,893 cycles

FO'S FLASHLIGHT BROKEN. REPLACED BROKEN FLASHLIGHT OPS CHECK GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,566 hrs · 13,996 cycles

SHV-DURING C- CHECK LT OMEGA BEAM LOWER FLANGE IS CORROED BTWN FR 53-59. MAINTENANCE BLENDED LT OMEGA BEAM BTWN FR 53-59. FR 54 OUT OF LIMIT ALL OTHER FRMS WITHIN LIMIT IAW EMB 145 SRM 53-24-10. PERFORMED OMEGA BEAM REPAIR ON LT OMEGA BEAM LWR FLANGE AT FR 54 IAW EMB 145 SRM 53-00-10 AND EC 5320-01140.INSTALLED NEW NUTPLATES IAW EC 5320-01137.THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 15,276 hrs · 13,656 cycles

EWR - CO2338, DURING SERVICE AND ROUTINE CHECK MAINTENANCE FOUND THE LEFT EMERGENCY EXIT SIGN WINDOW EXIT DOES NOT ILLUMINATE. REMOVED AND REPLACED LEFT EMERGENCY EXIT SIGN WINDOW EXIT IAW EMB AMM NR 33-50-13, OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,964 hrs · 13,326 cycles

CLE FLIGHT 2322 THE CREW REPORTED THE MID CABIN EMERGENCY LIGHTS NOT ILLUMINATING DURING PREFLIGHT TEST. MAINTENANCE REPLACED THE CENTER CABIN EMERGENCY LIGHTING INVERTER AND OPERATIONAL CHECKS GOOD.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 14,283 hrs · 12,595 cycles

CLE THE CREW REPORTED THE AISLE PATH EMERGENCY LIGHTS AT ROW 8 THRU 12 WERE INOPERATIVE. MAINTENANCE INSPECTED AND CLEANED THE AISLE PATH EMERGENCY LIGHT CONNECTORS. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 14,017 hrs · 12,288 cycles

DURING REFLIGHT INSPECTION THE CREW REPORTED THE SECOND AISLE PATH LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTION ON THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED GOOD IAW EMB-145 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — LOOSE (GALLEY)

IAH - FLIGHT 2551, DURING PREFLIGHT INSPECTION THE LOWER FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE LOOSE. MAINTENANCE RESECURED THE AFFECTED EMERGENCY LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

IAH- FLIGHT 2673, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE GALLEY EMERGENCY LIGHT, AND FLOOR PROXIMITY LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE GALLEY EMERGENCY LIGHT BULB, RESET THE EMERGENCY LIGHT SYSTEM, AND OPERATIONALLY CHECKED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — FAILED (NR 1) · airframe 13,507 hrs · 11,620 cycles

CREW REPORTED, NR 1 ENGINE FAILED INFLIGHT. N1 STABILIZED AT ABOUT 14 PERCENT AND 100 DEGREES. FAILURE OCCURRED DURING CLIMBOUT IN SHALLOW LEFT BANK WITH CLIMB THRUST SET. PERFORMED AIR RETURN TO NEWARK. LANDED UNEVENTFULLY. MAINTENANCE FOUND UNACCEPTABLE DEBRIS ON INDICATING CHIP DETECTOR, ALSO NOTED RAPID N2 RISE DURING ATTEMPTED START (APPROXIMATELY 50 PERCENT N2 WITHIN 3 SECONDS). SUSPECTED DAMAGE TO ACCESSORY DRIVE UNIT. REMOVED AND REPLACED NR 1 ENGINE IAW EXPRESS JET EMB145 TASKCARD 627001. OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTS ON THE FLOOR WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR THE FLOOR EMERGENCY LIGHTS, OPERATIONALLY TESTED THE SYTEM, AND CLEARED THE DISCREPANCY.

Part: WIRE — LOOSE (EMERGENCY LIGHT)

DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT ON THE THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REPAIRED WIRE SPLICE SP3676, OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,668 hrs · 10,656 cycles

CREW REPORTED TWO STRIPS OF EMERGENCY FLOOR LIGHTING INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM, NO FAULTS NOTED, OPS CHECKED GOOD IAW EMB145 AMM NR 33-50-00.

Part: ACTUATOR — DEFECTIVE (SPEED BRAKE) · airframe 1,174 hrs · 9,731 cycles

TYS DURING A DESCENT INTO THE EWR AREA PILOT ENGLEBERT, FLIGHT 2560 HAD TWO UNCOMMANDED ROLLS TO THE RIGHT. A/C LANDED SUCCESSFULLY AND WAS FERRIED TO TYS. MAINT REMOVED AND REPLACED LT & RT PCA SOLENOIDS & LT & RT SPEED BRAKE ACTUATORS IAW AMM 27-12-01 AND 27-13-01. OPS AND LEAK CHECKS GOOD. A/C WAS REL. FOR TEST FLIGHT AND WAS TEST FLOWN SUCCESSFULLY WITHOUT ANY DEFECTS OR PROBLEMS AND WAS REL TO SERVICE.

Part: WIRE — SHORTED (WARNING SYS)

CLE FLT 2224 THE CREW REPORTED THAT THE LANDING GEAR AURAL WARNING SOUNDED ON TAKEOFF WITH THE GEAR SELECTED AND INDICATING UP. AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED SHORTED WIRE BEHIND AURAL WARNING RACK W001-0892-24. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CORRODED (LAVATORY) · airframe 11,339 hrs · 9,353 cycles

DURING A SCHEDULED INSPECTION THE LAVATORY L/H FLOOR SIDEWALL FRAME AT STRINGER 15 LT WAS FOUND TO BE CORRODED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE SIDEWALL FRAME IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 11,339 hrs · 9,353 cycles

DURING A SCHEDULED INSPECTION THE OMEGA BEAM GUSSET WAS FOUND TO HAVE SEVERAL AREA OF CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE OMEGA BEAM GUSSET AT FRAME 20 IAW EMB145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 11,339 hrs · 9,353 cycles

DURING A SCHEDULED 3C INSPECTION, A GOUGE WAS DISCOVERED IN THE FLOORBEAM LOCATED JUST AFT OF THE LAV. BULKHEAD, RT SIDE. THE RT FLOORBEAM TOP CAP WAS REMOVED AND REPLACED IAW THE EMB 135/145 SRM 51-70-02. ACFT. WAS RELEASED FOR SERVICE FOLLOWING THE COMPLETION OF THE SCHEDULED INSPECTION.

Part: GUSSET — GOUGED · airframe 1,139 hrs · 9,353 cycles

DURING A SCHEDULED 3C INSPECTION, A GOUGE WAS FOUND ON THE TOP CAP LOCATED IN THE GALLEY AREA AFT OF THE FWD. DIGITAL. THE AFT GUSSET WAS REMOVED AND REPLACED IAW THE EMB 135/145 SRM 51-70-02. THE ACFT. WAS RELEASED FOR SERVICE FOLLOING THE COMPLETION OF THE SCHEDULED INSPECTION.

Part: GUSSET — CORRODED (PAX DOOR) · airframe 11,339 hrs · 9,353 cycles

TYS DURING A SCHEDULED 3-C INSPECTION, CORROSION WAS FOUND ON THE TOP CAP INSIDE THE PAX DOOR. MAINT R & R THE GUSSET IAW EMB 135/145 SRM 51-40-02.ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: GUSSET — GOUGED · airframe 11,339 hrs · 9,353 cycles

DURING A SCHEDULED 3C INSPECTION, A GOUGE WAS DISCOVERED ON THE TOP CAP LOCATED IN THE GALLEY AREA, JUST AFT OF THE FWD. DIGITAL. THE AFT GUSSET WAS REMOVED AND REPLACED IAW THE EMB 135/145 SRM 5170-02. ACFT. WAS RELEASED FOR SERVICE AFTER THE COMPLETION OF THE 3C CHECK.

Part: WINDSHIELD — ARCED (FUSELAGE)

MHT FLIGHT#3595 THE CREW REPORTED THE FIRST OFFICER'S WINDSHIELD HEATING ELEMENT WAS ARCHING.MAINTENANCE INSPECTED AND REPLACED THE FIRST OFFICER'S WINDSHIELD.OPERATIONAL CHECKS WERE GOOD.

Part: FIREWALL — CRACKED (AFT FUSELAGE)

DURING A ROUTINE INSPECTION THE APU FIREWALL WAS FOUND CRACKED AT THE UPPER RIGHT ATTACH POINT.MAINTENANCE REPAIRED THE APU FIREWALL I/A/W GST 3249/02.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,115 hrs · 8,147 cycles

EWR- DURING PREFLIGHT INSPECTION CREW REPORTED EMERGENCY LIGHTS FROM ROW 12 TO ROW 15 ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IN ROW 12 TO ROW 15 FLOOR AREA IAW EMB145 MM 33-0-08.

Part: WIRE — BROKEN (CABIN)

CREW REPORTED AISLE FLOOR PATH LIGHTING INOPERATIVE. MAINTENANCE REPAIR A BROKEN WIRE ON REAR SECTION OF EMERGENCY AISLE PATH LIGHTING AND OPS CHECKED SYSTEM GOOD.

Part: CONTROL HANDLE — FAILED (COCKPIT)

CLE FLIGHT 3284 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT ON THE FIRST ATTEMPT AFTER TAKEOFF. THE CREW RECYCLED THE GEAR HANDLE AND THE GEAR DID RETRACT ON THE SECOND ATTEMPT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE — DAMAGED (CABIN)

CLE FLIGHT 3021 THE CREW REPORTED THE EMERGENCY LIGHTS WERE OUT AT ROWS 3-7. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY AISLE PATH LIGHT STRIP AT ROW 7. ALSO REPAIRED WIRING AT ROW 7 FOR THE LIGHT STRIP. MAINTENANCE ALSO REPLACED THE EMERGENCY LIGHT BATTERY CHARGER. P/N 11-0049, S/N:11534

Part: WINDSHIELD — CRACKED (COCKPIT)

IAH - FLIGHT 3712, THE CREW REPORTED THAT THE FIRST OFFICERS WINDSHIELD SHATTERED ON APPROACH. THE CREW DECLARED AN EMERGENCY, PERFORMED AN EMERGENCY DESCENT, AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED WINDSHIELD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN)

IAH - FLIGHT 3936, THE CREW REPORTED A STRONG EXHAUST ODOR IN THE CABIN AND COCKPIT AFTER STARTING THE APU IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MX PLACED THE APU ON MEL. AIRCRAFT RETURNED TO IAH ON FLIGHT 4129 WHERE MAINTENANCE PERFORMED OPERATIONAL CHECKS ON THE APU AND PAX SYSTEMS WITH NO DEFECTS NOTED. AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. DISCREPANCY REPEATED ON 04/12/01. MAINTENANCE AGAIN PERFORMED OPERATIONAL CHECKS ON THE AFFECTED SYSTEMS WITH NO DEFECTS NOTED. AIRCRAFT WAS AGAIN APPROVED FOR RETURN TO SERVICE.

Part: LINE — DEFECTIVE (BLEED VALVE) · airframe 7,558 hrs · 5,901 cycles

ENGINE NR 2 WILL NOT HOLD ITT AT CLIMB THRUST. MAXIMUM CONTINUOUS EXCEEDED 930 DEGREES MAXIMUM. MAINTENANCE REMOVED AND REPLACED LOWER BLEED CONTROL VALVE LINE IAW ROLLSROYCE MM 75-31-25, OPS CHECKED GOOD. ITT DID NOT EXCEED LIMITS, NO FURTHER ACTION REQUIRED IAW ROLLS ROYCE MM 77-00-00. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 7,382 hrs · 5,749 cycles

IAH - DURING C-CHECK INSPECTION, THE EMERGENCY EXIT LIGHT ABOVE SEAT 12CB WAS FOUND TO BE INOPERATIVE. MAINTENANCE REINSPECTED THE AIRCRAFT AND FOUND THE AFFECTED LIGHT ASSY TO BE FUNCTIONING PROPERLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 7,382 hrs · 5,749 cycles

IAH - DURING C-CHECK INSPECTION, THE SILL PLATE FROM FRAME 18 TO FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL PLATE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,382 hrs · 5,749 cycles

IAH - DURING C-CHECK INSPECTION, THE LEFT HAND AND CENTER FLOOR SUPPORTS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER FLOOR SUPPORT, AND PERFORMED A DOUBLER REPAIR ON THE LEFT HAND SUPPORT IN ACCORDANCE WITH EMB145 SRM 53-21-10, AND 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BLADE — NICKED (NR 2 ENGINE) · airframe 7,382 hrs · 5,749 cycles

IAH - DURING C-CHECK INSPECTION, THE NUMBER TWO ENGINE WAS FOUND TO HAVE A NICKED FAN BLADE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CAP — CORRODED (LT MLG) · corrosion level 2 · airframe 7,382 hrs · 5,749 cycles

IAH - DURING C-CHECK INSPECTION, THE LEFT MAIN LANDING GEAR LOWER FORWARD BEARING CAP WAS FOUND TO HAVE PITTING CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARING CAP IN ACCORDANCE WITH EMB-145 M/M 57-26-00-220-803-A00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BLADE — CRACKED (NR2 ENGINE) · airframe 7,382 hrs · 5,749 cycles

IAH - DURING C-CHECK INSPECTION, THE NUMBER TWO ENGINE WAS FOUND TO HAVE A CRACKED FAN BLADE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE IN ACCORDANCE WITH ROLLS ROYCE AE3007A-M/M 72-21-15-300-801, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CAP — CORRODED (LT MLG) · corrosion level 2 · airframe 7,382 hrs · 5,749 cycles

IAH - DURING C-CHECK INSPECTION, THE LEFT MAIN LANDING GEAR AFT LOWER BEARING CAP WAS FOUND TO HAVE PITTING CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARING CAP IN ACCORDANCE WITH EMB-145 M/M 57-26-00-220-803-A00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (MLG PROX SENSOR)

DAL - FLT 4162 - THE CREW REPORTED THE RIGHT MLG WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO DAL, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RESECURED THE DOWNLOCK CANNON PLUG AND OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WA APPROVED FOR RETURN TO SERVICE. (M)

Part: CONNECTOR — LOOSE (RT MLG)

DAL - FLT 4162 - THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO DAL WITHOUT INCIDENT WHERE MAINTENANCE RESECURED THE CANNON PLUG ON THE RIGHT MLG SQUAT SWITCH, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

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

IAH - FLIGHT 3775, THE CREW REPORTED AN AIR / GROUND FAIL MESSAGE AFTER TAKEOFF. THE GEAR WAS CYCLED TWO TIMES WITH NO HELP. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE RIGHT HAND AIR / GROUND PROXIMITY SENSOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — CORRDOED (BAGG COMP)

EWR - FLT 4130 - CREW REPORTED BAGGAGE SMOEK EICAS MESSAGE IN FLIGHT. AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE CLEANED CORROSION AT CANNON PLUG OF NR 2 SMOKE DETECTOR AND RETURNED THE AIRCRAFT TO SERVICE. (M)

Part: LIGHT ASSEMBLY — INOPERATIVE (FUSELAGE)

IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT EXTERNAL EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB-145 MM 33-50-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (VERT STAB)

IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL 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 EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (VERT STAB)

IAH - DURING C-CHECK INSPECTION, THE RIGHT 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 EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BULB — FAILED (RT EMER EXIT)

IAH - DURING C-CHECK INSPECTION, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING C-CHECK INSPECTION, THE NR 7 EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED AISLE PATH LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ACTUATOR — MALFUNCTIONED (LT ENG TR UNIT)

CRP - UPON LANDING AT CRP, THE CREW REPORTED ANR 1 ENGINE THRUST REVERSER DISAGREE MESSAGE ON THE EICAS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 1 ENGINE UPPER THRUST REVERSER ACTUATOR ADJUSTABLE ROD END TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE AFFECTED THRUST REVERSER ACTUATOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (LT EXTERIOR)

EWR - FLT 4296 - CREW REPORTED LEFT WING FAIRING FUSELAGE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT. OPS CHECKED GOOD. (M)

Part: RETRACT MECH — MALFUNCTIONED (LANDING GEAR)

CLE - FLT 4053 - CREW REPORTED THAT THEY RECEIVED A LANDING GEAR DISAGREEMENT AFTER LIFT OFF, AND AFTER SEVERAL ATTEMPTS THE MAIN LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LANDING GEAR SYSTEM AND NO DEFECT WERE NOTED. THE OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB-145 MM 32-10-00, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: AIR DIST — ODOR (CABIN)

CLE - FLT 4056 - CREW REPORTED THAT DURING CLIMB THEY RECEIVED SMOKE IN THE COCKPIT AND CABIN. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE APU AS WELL AS THE APU COMPARTMENT FULL OF GLYCOL. THE AREAS WERE CLEANED OF GLYCOL IAW STANDARD MAINTENANCE PRACTICES, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: SWITCH — LEAKING (HYDRAULIC SYSTEM)

GSO - FLT 4071 - REPORTED 'NR 1 HYD LO QTY', 'NR 1 ENG HYD PUMP FAIL IN-FLIGHT', AND 'EMERG GEAR EXTENSION PROCEDURE C/W'. FOUND LT HYDRAULIC PRESSURE SUPPLY SWITCH LEAKING. REMOVED AND REPLACED SWITCH, REFILLED SYSTEM. OPS CHECKED PUMPS GOOD, LEAK CHECKED GOOD. ACFT TT: 1,371.8 HOURS. ACFT CYCLES: 1,117. (X)