N12996

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 35,031 hrs · 26,626 cycles

THE CREW REPORTED A MOMENTARY LAVATORY SMOKE MESSAGE DURING FLIGHT. MAINTENANCE INSPECTED AND R & R SMOKE DETECTOR. OPS CHECKS WERE GOOD.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 34,904 hrs · 26,518 cycles

PILOT REPORTED A LAVATORY SMOKE WARNING INDICATION ON EICAS WITH NO INDICATION OF SMOKE OR FIRE. MAINTENANCE INSPECTED LAVATORY FOR SMOKE AND EVIDENCE OF FIRE WITH NOTHING FOUND. MAINTENANCE ALSO PERFORMED OPS CHECK OF LAVATORY SMOKE DETECTOR SYS GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 34,760 hrs · 26,409 cycles

CREW REPORTED A LAVATORY SMOKE MESSAGE ON EICAS AFTER TAKE OFF. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT, LAV WIRING WITH NO DEFECTS NOTED, R & R FOUR FLUORESCENT LIGHT BULBS AS A PRECAUTION AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 3,465 hrs · 26,336 cycles

DURING 1A INSPECTION, A SMALL HOLE WAS FOUND IN THE CARGO DOOR LOWER FWD CORNER. MAINTENANCE PERFORMED AN INTERNAL DOUBLER REPAIR TO THE CARGO DOOR, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRAKE ASSY — SLIPPED (ZONE 700) · airframe 33,909 hrs · 25,731 cycles

PILOT REPORTED THE BRAKES SLIPPING ON LANDING AND VERY NOISE DURING SLOW TAXI. MX R & R 1 BRAKE ASSY OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE

Part: DISPLAY — SHORTED (COCKPIT) · airframe 32,457 hrs · 24,623 cycles

NR 2 PFD CIRCUIT BREAKER TRIPPED WITH BURNING ODOR IN COCKPIT. MAINTENANCE R & R THE NR 2 PFD, OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (ZONE 500) · airframe 31,936 hrs · 24,214 cycles

DURING C-CHECK, LT AILERON OTBD PCA ATTACHMENT FITTING OTBD LUG, OTBD HAT BUSHING MIGRATED. MX R & R THE LT AILERON OTBD PCA ATTACHMENT FITTING IAW EC5750-01177. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,478 hrs · 23,871 cycles

DURING SCHEDULED MX INSPECTION, THE CABIN FLOOR EMERGENCY LIGHTS AT ROW 6 AND 7 WERE INOPERATIVE. MX R & R THE FLOOR STRIP LIGHT WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CANNING (FUSELAGE) · airframe 27,099 hrs · 20,353 cycles

SHV - DURING C-CHECK STRINGER 11 EXTERNAL FUSELAGE PATCH JUST AFT OF PAX DOOR IS OIL CANNING. MAINTENANCE PERFORMED REPAIR AT STRINGER 11L JUST AFT OF PAX DOOR IAW EC5330-02500, NO FURTHER ACTION REQUIRED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,099 hrs · 20,353 cycles

SHV - DURING C-CHECK PAX DOOR FRAME LOWER SECTION HAS CORRODED NUT PLATE HOLES (NEAR DOOR SEAL). MAINTENANCE PERFORMED REPAIR AT PAX DOOR LOWER NUT PLATE AREAS IAW EC5210-01154. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,099 hrs · 20,353 cycles

SHV - DURING C-CHECK CORROSION PRESENT IN AREA WHERE THE SHUNT CONNECTION BAR COMES IN CONTACT WITH STRUCTURE. MAINTENANCE PERFORMED REPAIR AT APU SHUNT FRAME 80 IAW EC5310-01544 REV C, BONDING CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 27,099 hrs · 20,353 cycles

SHV - DURING C-CHECK BAGGAGE DOOR INNER FRAME SKIN GOUGED AT LOWER, FWD AND CENTER AREAS. MAINTENANCE PERFORMED REPAIR ON BAGGAGE DOOR INNER SKIN IAW EC5230-01208. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,099 hrs · 20,353 cycles

SHV - DURING C-CHECK LT OMEGA BEAM SUPPORT FLANGE AT FRAME 21-25 NUT PLATE CORRODED. MAINTENANCE PERFORMED REPAIR AND INSTALLED FABRICATED DOUBLER AT LT OMEGA BEAM FLANGE BETWEEN FRAME 21-22 IAW EC5320-01257 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COMPUTER — FAILED (AHRS) · airframe 26,036 hrs · 19,546 cycles

IAH - FLIGHT 2695, DURING TAKEOFF THE CREW REPORTED THAT THE NUMBER ONE AHRS COMPUTER FAILED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AHRS COMPUTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — FAULTY (COCKPIT) · airframe 24,032 hrs · 18,014 cycles

CLE FLT 2209 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LGEU. OPERATIONAL CHECKS WERE GOOD.

Part: O-RING — LEAKING (BLEED AIR SYS) · airframe 23,728 hrs · 17,799 cycles

IAH - FLIGHT 2948, THE CREW REPORTED A BLEED ONE LEAK IN CLIMB OUT THAT CLEARED UPON CLOSING BLEED ONE WITH NO APU. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED BLEED DUCT O-RING AT JOINT 19B IN THE LT CARGO COMPARTMENT, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS NOTED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,588 hrs · 16,971 cycles

SHV - DURING C-CHECK FUSELAGE FLOOR SKIN CORRODED (LEVEL 2 LOCAL) BETWEEN FRAMES 61-62 STRINGERS 21L-21R. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN BETWEEN FRAMES 61-62 STRINGERS 21L-21R IAW EMB-145 SRM 53-31-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,588 hrs · 16,971 cycles

SHV - DURING C-CHECK, FR 10 CRACKED AT STR 10L. REMOVED AND REPLACED FRAME IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,588 hrs · 16,971 cycles

SHV - DURING C-CHECK RT UPPER SEAT TRACK SUPPORT CORRODED (LEVEL 2 LOCAL) AT FRAME 50 IAW EC5320-01512. MAINTENANCE REPAIRED RT UPPER SEAT TRACK SUPPORT AT FRAME 50 IAW EC5320-01512. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 22,588 hrs · 16,971 cycles

SHV - DURING C-CHECK LT UPPER SEAT TRACK SUPPORT CORRODED (LEVEL 3 LOCAL) AT FRAME 50 ATTACHMENT. MAINTENANCE REPAIRED LT UPPER SEAT TRACK SUPPORT AT FRAME 50 IAW EC5320-01512. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,588 hrs · 16,971 cycles

SHV - DURING C-CHECK RT UPPER SEAT TRACK SUPPORT CORRODED (LEVEL 2 LOCAL) AT FRAME 46. MAINTENANCE REPAIRED RT UPPER SEAT TRACK SUPPORT AT FRAME 46 IAW EC5320-01512. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,588 hrs · 16,971 cycles

SHV - DURING C-CHECK RT HALF FRAME AT FRAME 10 IS CRACKED AT DV WINDOW. MAINTENANCE REMOVED AND REPLACED RT HALF FRAME AT FRAME 10 AT DV WINDOW. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 22,588 hrs · 16,971 cycles

SHV - DURING C-CHECK LT UPPER SEAT TRACK SUPPORT CORRODED (LEVEL 3 LOCAL) AT FRAME 46 ATTACHMENT. MAINTENANCE REPAIRED LT UPPER SEAT TRACK SUPPORT AT FRAME 46 IAW EC5320-01512. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 22,442 hrs · 16,850 cycles

RIC MX - DURING ROUTINE MAINTENANCE, MX FOUND EXIT SIGN IN FRONT OF SEAT 3B INOPERATIVE. MX REMOVED AND REPLACED EXIT SIGN AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: POWER SUPPLY — NOT SEATED (CABIN) · airframe 21,820 hrs · 16,395 cycles

RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND RIGHT WING AFTERWARD EMERGENCY LIGHT AND EMERGENCY LIGHT IN FRONT OF SEAT 3B INOPERATIVE. MX RESEATED NR 3 EMERGENCY LIGHT POWER PACK AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,946 hrs · 15,732 cycles

EWR MX - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY EXIT LIGHT ON AFT GALLEY WALL INOPERATIVE. MX REMOVED AND REPLACED NR 2 BATTERY AND PERFORMED OPERATIONAL SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,946 hrs · 15,735 cycles

EWR MX - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY EXIT LIGHT AT OVERWING CEILING INOPERATIVE. MX REMOVED AND REPLACED NR 3 BATTERY AND PERFORMED OPERATIONAL SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: TRIM SWITCH — INTERMITTENT (COCKPIT) · airframe 20,865 hrs · 15,670 cycles

CLE FLIGHT 2080 - THE CREW REPORTED THE PITCH TRIM WAS INOPERATIVE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS PITCH TRIM SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 20,628 hrs · 15,508 cycles

OKC - FLIGHT 2205 - THE CREW REPORTED THAT THE FIRST OFFICERS WINDSHIELD CRACKED ON CLIMBOUT BLOCKING VISIBILITY. THE AIRCRAFT RETURNED TO OKC WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 20,570 hrs · 15,470 cycles

MCI - DURING MAINTENANCE INSPECTION THE RIGHT OVERWING EMERGENCY EXIT MARKER LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,036 hrs · 19,034 cycles

MCI - DURING MAINTENANCE INSPECTION THE FORWARD OVERWING CEILING EXIT LOCATOR SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 6 EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DIRTY (CABIN) · airframe 15,686 hrs · 11,996 cycles

EWR LOG SQUAWK FLT 2347 FORWARD OVERHEAD EMERGENCY EXIT LOCATER SIGN AT ROW 11 OUT. CLEANED CONNECTOR AND RESECURED FORWARD EMERGENCY EXIT LOCATER AT ROW 11 IAW EMB145 AMM 33-50-13. OPS CHECK GOOD. CLOSED

Part: SIGN — FAULTY (EMERGENCY LIGHT) · airframe 12,292 hrs · 9,331 cycles

DURING SERVICE ROUTINE CHECK ON OVERNIGHT, MAINTENANCE FOUND ROW 12 OVERHEAD EMERGENCY EXIT SIGN NOT WORKING. REMOVED AND REPLACED ROW 12 OVERHEAD EMERGENCY EXIT SIGN IAW EMB145 AMM 33-50-15, OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO SMOKE) · airframe 11,501 hrs · 8,692 cycles

MHT FLIGHT 3054, THE CREW REPORTED A BAGGAGE COMPARTMENT SMOKE INDICATION ON THE EICAS THAT WOULD NOT CLEAR. MAINTENANCE INSPECTED AND RESET AIRCRAFT POWER. OPERATIONAL CHECKS WERE GOOD.

Part: AMPLIFIER — FAILED (PA) · airframe 10,276 hrs · 7,752 cycles

ORF - FLT 2017, DURING PREFLIGHT CHECK THE CREW FOUND CABIN AND CABIN EMERGENCY LIGHTS IN OVERHEAD PANEL ILLUMINATED AND CABIN INTERPHONE AND PA INOP. MAINTENANCE REMOVED AND REPLACED PA AMP. OPERATIONAL CHECKS PERFORMED SUCCESSFULLY. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 2266, THE CREW REPORTED THAT THE SECOND TO AFT EMERGENCY LIGHT STRIP WAS INOP WHEN TESTED. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE LIGHT STRIP. ALL OPERATIONAL CHECKS WERE GOOD.

Part: TRIM SYSTEM — MALFUNCTIONED (ROLL TRIM)

IAH FLIGHT 2390 CREW REPORTED, ROLL TRIM RUN-AWAY AFTER TAKEOFF FROM IAH. CREW FOLLOWED QRH AND RESET CIRCUIT BREAKER FOR AILERON TRIM. SYSTEM OPS CHECKED GOOD. CREW CONTINUED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM WITH NO DEFECTS FOUND.

Part: ANGLE — CHAFED (NR 2 COWLING) · airframe 8,080 hrs · 6,045 cycles

SHV-DURING C CHECK THE NR 2 ENGINE LOWER COWLING AFT OB EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,080 hrs · 6,045 cycles

SHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 20 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 8,080 hrs · 6,045 cycles

SHV- DURING C-CHECK THE FWD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 8,080 hrs · 6,045 cycles

SHV- DURING C-CHECK THE NUMBER 2 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIB — GOUGED (NACELLE) · airframe 8,080 hrs · 6,045 cycles

DURING C CHECK THE AFT EDGE MEMBER WAS FOUND TO BE GOUGED AT THE SIX O'CLOCK POSITION. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 8,080 hrs · 6,045 cycles

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

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 8,080 hrs · 6,045 cycles

SHV-DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (CABIN) · corrosion level 2 · airframe 8,080 hrs · 6,045 cycles

SHV-DURING C-CHECK THE RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,080 hrs · 6,045 cycles

SHV- DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A FILLER AND SHIM REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,080 hrs · 6,045 cycles

SHV- DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,080 hrs · 6,045 cycles

SHV- DURING C-CHECK THE CABIN FLOOR STRUCTURE AFT DIGITAL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT DIGITAL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — GOUGED (FUSELAGE) · airframe 8,080 hrs · 6,045 cycles

SHV- DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19 R WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR · airframe 6,402 hrs · 4,682 cycles

EWR AFTER T/O WITH THE GEAR UP INDICATION ON EICAS THERE WAS LOUD WIND NOISE AND VIBRATION COMING FROM NOSE GEAR AREA. ALL DOORS CLOSED ON MFD. WENT AWAY AFTER 10 MINS. DURING CLIMB. HYD PUMPS AND PRESSURE WERE NORMAL AT ALL TIMES. REMOVED AND REPLACED NLG DOOR SEQUENCE PROXIMITY SENSOR IAW EMB145AMM 32-63-03. SWUNG NLG. OPS CHECK GOOD IAW EMBAMM 32-30-00.

Part: CONTROL HANDLE — FAILED (COCKPIT)

CLE FLIGHT 4059 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM CLEVELAND. RECEIVED A LG/LEVER DISAGREE MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (LANDING GEAR)

YUL - FLIGHT 3675, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE CREW CYCLED THE LANDING GEAR IN ACCORDANCE WITH THE QRH, AND THE GEAR RETRACTED SUCCESSFULLY AFTER SIX ATTEMPTS. THE AIRCRAFT CONTINUED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONICS UNIT. OPERATIONALLY CHECKED THE GEAR WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO FLIGHT.

Part: SKIN — BIRD STRIKE (FUSELAGE)

IAH - FLT 4255 - DURING APPROACH, THE CREW REPORTED A BIRD STRIKE TO THE RIGHT SIDE NOSE AREA. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SKIN, EFFECTED FRAMES 1A, 2 AND 3, AND STRINGER 15 RIGHT FROM FRAME 1A TO FRAME 4. MAINTENANCE PERFORMED IAW EMBRAER REF SST-3546/00 AND EMB-145 SRM 51-40-02. THE AIRCAFT WAS APPROVED FOR RETURN TO SERVICE. (M)