N13913

Part: FIREWALL — CRACKED (NR 1 NACELLE) · airframe 42,231 hrs · 32,592 cycles

TYS A/C WAS FOUND WITH THE #1 PYLON FIREWALL SKIN CRACKED, CRACKS CONFIRMED BY NDT AND MAINTENANCE REPAIRED THE CRACK SKIN IAW ECTC ETD 2019-145-16243. ALL WORK ACCOMPLISHED AND WAS RELEASED TO SERVICE.

Part: STRINGER — CORRODED (FRAMES 21-23) · airframe 42,231 hrs · 32,592 cycles

TYS A/C WAS FOUND WITH CORROSION AT STRINGER 17 RIGHT AND BETWEEN FRAMES 21 THRU FRAME 23. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED PERTINENT REPAIRS IAW ETD 2019-145-164017. ALL WORK ACCOMPLISHED AND WAS RELEASED TO SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (SMOKE DETECTION) · airframe 42,240 hrs · 32,598 cycles

THE CREW REPORTED LAV SMOKE IN FLIGHT. NO SMOKE ODOR WAS DETECTED BY F/A. MAINTENANCE INSPECTED AND REPLACED THE FORWARD SMOKE DETECTOR PANEL.

Part: GROUND STUD — DIRTY (EMERGENCY LIGHT) · airframe 41,804 hrs · 32,247 cycles

FLIGHT 4368 THE EMERGENCY LIGHT ON THE PAX DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND CLEANED THE GROUND CONNECTION ON THE LIGHT. OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,269 hrs · 31,811 cycles

DURING MX INSPECTION THE REAR EMERGENCY LIGHT WERE INOP. MX REMOVED AND REPLACED #4 BATTERY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERIVCE

Part: MOUNT — CRACKED (ENGINE) · airframe 37,273 hrs · 28,620 cycles

DURING A C-CHECK. RT FWD LOWER ENGINE MOUNT CRACKED. REMOVED AND REPLACED THE ENGINE MOUNT IAW EC5450-01099. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRUNNION — CRACKED (RT MLG) · airframe 37,273 hrs · 28,620 cycles

DURING C-CHECK, THE RIGHT AFT MLG TRUNNION WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE REMOVED AND REPLACED THE TRUNNION IAW EC5750-01770. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (STROBE) · airframe 36,217 hrs · 27,769 cycles

CREW REPORTED STROBE CIRCUIT BREAKER POPPED IN FLIGHT. ELECTRICAL BURNING ODOR ASSOCIATED, POSSIBLE LIGHTING STRIKE. MX PERFORMED LIGHTING INSPECTION OF ACFT WITH NO VISUAL DAMAGE NOTED. R & R TAIL STROBE POWER SUPPLY, OPS CHECK GOOD. AC WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — MELTED (COFFEEMAKER) · airframe 35,689 hrs · 27,345 cycles

THE CREW REPORTED SMOKE IN THE CABIN GALLEY AREA. ACFT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND NR 1 COFFEEMAKER WIRING HARNESS TO BE MELTED AND DAMAGED SURROUNDING TERMINAL END. COFFEEMAKERS WERE PLACED ON MEL AND THE ACFT WAS RETURNED TO SERVICE.

Part: COFFEEMAKER — FAILED (GALLEY) · airframe 35,689 hrs · 27,345 cycles

SUP: THE CREW REPORTED SMOKE IN THE CABIN GALLEY AREA. MAINTENANCE REPLACED THE NR 1 COFFEE BREWER. OPS CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,915 hrs · 26,728 cycles

DURING ROUTINE MAINTENANCE, THE EXTERIOR RT WING AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE RT EMERGENCY LIGHT ASSY. OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,691 hrs · 24,971 cycles

THE CREW REPORTED THE EMERGENCY LIGHTS IN FRONT OF PLANE TO ROW 7 WOULD NOT STAY ON. SIGNS OVER GALLEY DOOR AND AFT OF GALLEY WOULD NOT STAY ON WHEN TESTED. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER ASSY. OPS CHECKED GOOD.

Part: ATTACH FITTING — WORN (RT AILERON) · airframe 32,453 hrs · 24,789 cycles

RT AILERON PCA ATTACH FITTING ON AILERON SIDE HAS MIGRATED HAT BUSHING ON OTBD LUG OF INBD PCA CONNECTING ROD ATTACH POINT. R & R PCA FITTING IAW EC5760-01044.

Part: SKIN — DENTED (FRAMES 20-21) · airframe 32,454 hrs · 24,789 cycles

DURING A C-CHECK, FOUND MULTIPLE DENTS IN ACFT SKIN BETWEEN FRAMES 20 AND 21,STRINGERS 11 AND 12L. MAINTENANCE REPAIRED THE SKIN PANEL IAW EC 5320-01967 REF 602, 1043497 FOR PRESSURE CHECK AT THE END OF ALL CHECKS.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 32,316 hrs · 24,676 cycles

DURING ROUTINE MAINTENANCE, THE NR 2 EMERGENCY LIGHT BATTERY DID NOT TEST. MAINTENANCE REPLACED THE BATTERY. OPS CHECKED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,316 hrs · 24,676 cycles

DURING ROUTINE MAINTENANCE, THE AFT GALLEY EXIT MARKING SIGN DID NOT ILLUMINATE. MAINTEANCE REPLACED THE POWER SUPPLY. OPS CHECKED.

Part: BLEED VALVE — STUCK (NR 1 ENGINE) · airframe 31,370 hrs · 23,965 cycles

ENROUTE, RECEIVED AN EICAS MESSAGE FOR ANTI-ICE INOPERATIVE. WING AND STAB ANTI-ICE FAIL. ACFT DIVERTED TO MAINTENANCE R & R THE NR 1 ENGINE BLEED VALVE IAW AMM 36-11-05, IPC REF IPC 36-11-05, FIGURE 01A, OPS CHECK GOOD AND WAS RELEASED BACK TO SERVICE.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 27,619 hrs · 21,039 cycles

DURING C-CHECK THE VERTICAL STABILIZER FITTING AT FRAME 75 WAS ORIGINALLY REMOVED FOR EVIDENCE OF FRETTING AND THEN FOUND TO BE CRACKED AROUND AN UPPER BOLT HOLE. MX R & R THE FITTING IAW EC5310-01317. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED · corrosion level 2 · airframe 27,619 hrs · 21,039 cycles

DURING C-CHECK THE CARGO DOOR FRAME LOWER CUT-OUT BEAM WAS FOUND TO BE CORRODED. MX R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — OVERHEATED (NR 1) · airframe 25,325 hrs · 19,258 cycles

A/C PACK 1 OVERHEAT MESSAGE ON EICAS WITH SMOKE. OPERATED PACK SYS 1 AND 2, NO SMOKE IN CABIN BUT PACK 1 OVERHEAT MESSAGE REAPPEARED ON EICAS. R & R NR 1 AIR CYCLE MACHINE IAW AMM 21-51-03, PERFORMED OPS CHECKS AND CLEARED THE MEL. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: B-NUT — LOOSE (CABIN PRESSURE) · airframe 23,790 hrs · 18,083 cycles

IAH - FLT 2129 THE CREW REPORTED AMBER DASHES ON THE CABIN ALTITUDE RIGHT AFTER TAKE OFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, TIGHTENED A "B"-NUT ON THE SENSE LINE GOING TO THE ELECTRO PNEUMATIC OUTFLOW VALVE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (RT MLG) · airframe 23,436 hrs · 17,814 cycles

FLIGHT 2526 - EWR - FLIGHT CREW REPORTED THAT AFTER DE-ICING, ANOTHER ACFT SPOTTED SMOKE COMING FROM RIGHT MLG. EWR MX INSPECTED RIGHT MLG AND NO DEFECTS WERE FOUND. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,658 hrs · 17,230 cycles

SHV - DURING C-CHECK DOUBLER AT FRAME 20 IS CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM FRAME 18-23 IAW EMB-145 EC5320-01229. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — WORN (SPOILER) · airframe 22,658 hrs · 17,230 cycles

SHV - DURING C-CHECK RT GROUND SPOILER I/B ATTACHMENT BRACKET HAS A MIGRATED HAT BUSHING. MAINTENANCE REMOVED AND INSTALLED NEW BRACKET ON RT GROUND SPOILER I/B ATTACHMENT POINT IAW EMB-145 AMM 57-51-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 22,658 hrs · 17,230 cycles

SHV - DURING C-CHECK STRINGER 19R CHAFED BETWEEN FRAME 52-53. MAINTENANCE PERFORMED REPAIR ON STRINGER 19R BETWEEN FRAME 52-53 IAW EMB-145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (NR 2) · airframe 22,102 hrs · 16,817 cycles

IAH - DURING CRUISE FLIGHT THE CREW REPORTED A BATTERY TWO OVERTEMP. THE AIRCRAFT LANDED AT OIAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 MAIN BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DIRTY (NR 2 OIL SYSTEM) · airframe 18,819 hrs · 14,365 cycles

IAH - FLIGHT 2606 - DURING CRUISE AT 18000FT THE CREW REPORTED THAT THE NUMBER TWO ENGINE OIL PRESSURE WENT INTO THE AMBER RANGE AND WHEN POWER WAS PULLED BACK TO DETENT THE PRESSURE WENT BACK INTO THE GREEN RANGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, CLEANED DEBRIS FROM THE NR 2 OIL PRESSURE SWITCH CONNECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLANGE — CORRODED (NR 1 ENGINE)

ACFT WAS IN FOR A 3C INSPECTION AND THE NR 1 ENGINE FORWARD BOLT FLANGE WAS FOUND CORRODED. 2 BOLT HOLES AT NR 29 AND NR 45 WERE FOUND IF REPAIRED WOULD RESULT IN BEING BEYOND THE MM LIMITS AND REPAIR OF THE HOLES WOULD RESULT IN A THINWALL CONDITION. ALL OTHER CORROSION WAS WITHIN LIMITS. THE BOLT HOLES WERE REPAIRED BY PERFORMING A KEYHOLE REPAIR AND INSTALLING REINFORCEMENT PLATES PER SERVICE BULLETIN AE3007A-72-247. ALL WORK WAS ACCOMPLISHED IN REFERENCE TO THE SB AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: UNKNOWN — ODOR

FLIGHT CREW REPORTED BURNING ODOR IN CABIN DURING TAXI OUT. MX PERFORMED OPS CHECK OF AIR CONDITIONING, ELECTRICAL AND BLEED SYSTEMS AND COULD NOT DUPLICATE THE ODOR. ACFT WAS APPROVED TO RETURN TO SERVICE. (K)

Part: SENSOR — BURNED (COCKPIT) · airframe 16,791 hrs · 12,937 cycles

FLIGHT NR 2706 THE CREW REPORTED A ELECTRICAL ODOR IN THE COCKPIT. MAINT INSPECTED AND REPLACED THE NR 1 PITOT CURRENT SENSOR AND SOCKET. OPERATIONAL CHECKS WERE GOOD.

Part: RELAY — BURNED (COCKPIT) · airframe 16,765 hrs · 12,918 cycles

MKE FLIGHT 3009 - THE CREW REPORTED SMOKE IN THE CABIN AND FLIGHT DECK AT FLIGHT LEVEL 36,000.PRIOR TO SMOKE THERE WAS A (TAT 2 HEAT INOP) MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 TAT CURRENT SENSOR RELAY KO494 AND SOCKET XK0494. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,714 hrs · 11,461 cycles

THE RIGHT EMERGENCY LIGHT OVER THE WING IS INOP. REMOVED AND REPLACED THE BULB IAW EMB 145 MM 33-30-07 OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 13,610 hrs · 10,615 cycles

BTV ROUTINE CHECK FLT NR 2043 FOUND SERVICE DOOR EMERGENCY LIGHT(EXTERIOR) INOP. RECONNECTED SERVICE DOOR EMERGENCY LIGHT CONNECTER IAW EMB145 AMM STANDARD PRACTICES. OPS CHECK GOOD. CLOSED

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 11,745 hrs · 9,122 cycles

IAH - FLIGHT 2203, DURING TAKEOFF THE CRE REPORTED A LANDING GEAR DISAGREE WITH AN ENGINE ONE & TWO REV DISAGREE. THE CREW RETRACTED THE GEAR USING THE OVERRIDE BUTTON AND CONTINUED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR PROXIMITY SENSOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LANDING GEAR — MALFUNCTIONED · airframe 1,149 hrs · 8,657 cycles

MCI - FLIGHT 3006, THE CREW REPORTED THAT UPON ROTATION, LANDING GEAR AIR GROUND FAIL MESSAGE APPEARED ON EICAS, AND THE GEAR WOULD NOT RETRACT. THE AIRCRAFT DIVERTED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FUNCTIONAL CHECKS, AND OPERATIONAL CHECKS OF THE LANDING GEAR RETRACTION/EXTENSION SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (MAIN DOOR) · airframe 10,767 hrs · 8,359 cycles

MKE FLIGHT NR 3009, THE CREW REPORTED A STRONG ELECTRICAL ODOR COMING FROM BREAKER BOX BEHIND CAPTAINS SEAT WHILE TAXING INTO GATE. THE TAXI LIGHT CAME ON, FLICKERED, THEN WENT OUT WITHOUT SWITCH BEING TURNED ON. MAINTENANCE INSPECTED AND RELEASED AIRCRAFT IAW MEL 33-42-00.

Part: RELAY — FAULTY (COCKPIT) · airframe 10,769 hrs · 8,360 cycles

MKE---CO3009, STRONG ELECTRICAL ODOR COMING FROM THE BREAKER BOX BEHIND THE CAPTAINS SEAT ODOR NOTED WHILE TAXIING INTO THE GATE. IN ADDITION, THE NOSE TAXI LIGHT CAME ON AND FLICKERED OFF WITHOUT BEING TURNED ON FROM THE COCKPIT. AIRCRAFT PLACED ON MEL AND RETURNED TO SERVICE. UPON ARRIVAL IN IAH, MAINTENANCE REMOVED AND REPLACED RELAY KO235AND VERIFIED NORMAL OPERATION IAW EMB145 MM NR 20-10-05, MEL REMOVED AND AIRCRAFT RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 8,926 hrs · 6,898 cycles

SHV-DURING SERVICE/ROUTINE CHECK, THE AFT CABIN OVERHEAD EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LAMP IAW EMB 145 AMM33-50-08. THE ENSUING OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 8,406 hrs · 6,506 cycles

DURING SERVICE AND ROUTINE CHECK IN BTV MAINTENANCE FOUND THE EMERGENCY LIGHT INOPERATIVE AT SEAT 12A PSU. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY BULB AT SEAT 12A PSU IAW EMB145 AMM 33-50-07. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 8,269 hrs · 6,405 cycles

DURING C-CHECK THE CENTER OMEGA BEAM AT FRAME 20 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: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 7,646 hrs · 5,909 cycles

DURING 1A INSPECTION MAINTENANCE FOUND THE RT OVERWING EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT BULB IAW AMM NR 33-50-10. OPS CHECK GOOD.

Part: SENSOR — BURNED (COCKPIT)

CLEVELAND FLIGHT NUMBER 3247, ON DESCENT STRONG ELECTRICAL BURNING SMELL IN COCKPIT AND CABIN. FLIGHT ATTENDANT NOTED A SLIGHT HAZE IN CABIN. MAINTENANCE REPLACED PITOT/STATIC CURRENT SENSOR K0057 ON THE RIGHT DC POWER PANEL. ALL OPERATIONAL CHECKS WERE GOOD.

Part: PANEL — CONTAMINATED (EMERGENCY LIGHT)

IAH - FLIGHT 2186, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS CAME ON WHEN CALLING THE FLIGHT ATTENDANT. MAINTENANCE CLEANED THE FLIGHT ATTENDANT CALL PANEL OF MOISTURE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (COCKPIT)

DURING FLIGHT THE CREW NOTED THAT THE AIR/GROUND FAIL MESSAGE ILLUMINATED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW EMB 145 AMM 32-32-01. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 3,995 hrs · 2,950 cycles

SHV- DURING C CHECK REAR FUSELAGE SKIN WAS FOUND TO HAVE A GOUGE JUST BELOW CENTER OF CARGO DOOR BUMPER PLATE. MAINTENANCE REPAIRED GOUGE IN AFFECTED AREA IAW CONTINENTAL EXPRESS EC 5330-01219. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BEAM — CORRODED (CABIN) · corrosion level 2 · airframe 3,995 hrs · 2,950 cycles

DURING C-CHECK LT OMEGA BEAM AT FRAME 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 3,995 hrs · 2,950 cycles

SHV- DURING C CHECK APU FIREWALL CRACKED AT TOP RIVET OF RIGHT HAND VERTICAL REINFORCEMENT. MAINTENANCE REMOVED DAMAGE AND REPAIRED CRACK IAW CONTINENTAL EXPRESS EC 5330-01202. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 3,995 hrs · 2,950 cycles

SHV- DURING C CHECK EXTERNAL GOUGE WAS FOUND ON STRINGER T REINFORCEMENT AT FRAME 52 STRINGER 19R. MAINTENANCE REMOVED DAMAGE AND PERFORMED DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 3,995 hrs · 2,950 cycles

SHV DURING C CHECK GOUGE WAS FOUND ON STRINGER 19L ON T REINFORCEMENT AT FRAME 52. MAINTENANCE REMOVED AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONNECTOR — FAULTY

BTV---DURING 1A INSPECTION, MAINTENANCE FOUND SERVICE DOOR EMERGENCY LIGHT TO BE INOPERATIVE.....FOUND ELECTRICAL PIN ON CONNECTOR J7198 TO BE PUSHED BACK. REPLACED (LOCKED) PIN INTO CONNECTOR IAW EMB145 MM 20-50-00. SERVICE DOOR EMERGENCY LIGHT OPS.CHECKED GOOD.

Part: ACTUATOR — LEAKING (LEFT WING)

CLE FLIGHT#3213 THE CREW REPORTED THE #2 HYDRAULIC SYSTEM FAILED.LOST HYDRAULIC QUANTITY.THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE #1 SPEED BRAKE ACTUATOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.