N15980

Part: WIRE — BROKEN (CABIN) · airframe 46,190 hrs · 35,815 cycles

MX REPORTED THE EMERGENCY FLOOR PROXIMITY STRIP LIGHT BY WING EMERGENCY EXIT INOP. MX REPAIRED EMERGENCY STRIP BROKEN WIRE AND PERFORMED OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 45,641 hrs · 35,343 cycles

PILOT REPORTED A STRONG PETROLEUM ODOR THROUGH VENTILATION SYSTEM OF PACK 1 , NOTICED UPON INITIAL DECENT WHEN POWER PULLED TO IDLE NOTED MULTIPLE TIMES. MX PERFORMED COOLING PACK SYSTEM OPS CHECK (PACK #1) IAW AMM 21-51-00 OPS CHECK GOOD COULD NOT DUPLICATE PROBLEM. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 45,043 hrs · 34,853 cycles

GOUGE AT FRAME 51, STRINGER 19R (193 AREA). REPLACED REPAIR DOUBLER IN ACCORDANCE WITH SRM 53-24-02. AIRCRAFT IS STILL IN MAINTENANCE.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 45,043 hrs · 34,853 cycles

GOUGE AT FRAME 51, STRINGER 19R. REPLACED REPAIR DOUBLER IAW SRM 53-24-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,043 hrs · 34,853 cycles

A/C IS IN C-CHECK WHEN INSPECTION FOUND FRAME 65 CORRODED AT THE CARGO FLOOR SILL. MAINTENANCE REPAIRED CORRODED SHEAR CLIP AT FRAME 65 AT CARGO DOOR SILL IAW SRM 53-31-04 AND FIGURE 212. LIGHT CORROSION.

Part: DOOR — OPEN (NLG) · airframe 44,702 hrs · 34,567 cycles

TYS A/C NOSE LANDING GEAR DOORS OPEN UN-COMMANDED IN FLIGHT. MAINTENANCE CHECKED THE NLG ACTUATOR FOR LEAKAGE, CLEANED AREA, SECURED FITTINGS, CHECKED FOR LOOSE FITTINGS AND CLEANED THE SOLENOID PROX SWITCHES IAW AMM #@-^#-05. ALL CHECKED GOOD, OPS CHECKED GOOD AND WAS RELEASED TO SERVICE.

Part: DUCT — LOOSE (NR 1 A/C PACK) · airframe 42,439 hrs · 32,714 cycles

PILOT REPORTED A BURNING ODOR DURING ICE TEST. MX INSPECTED AND FOUND LOOSE DUCTS ON THE NR 1 PACK. SECURED THE DUCTS AND PERFORMED AN ANTI-ICE TEST, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRUNNION — CRACKED (LT MLG) · airframe 40,778 hrs · 31,408 cycles

DURING C-CK LT MLG AFT TRUNNION CRACKED. REMOVED AND REPLACED LT MLG AFT TRUNNION IAW ETD 2016-145-097296. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAME 59) · corrosion level 2 · airframe 40,778 hrs · 31,408 cycles

DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-24-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (RT ENGINE MOUNT) · airframe 40,778 hrs · 31,408 cycles

DURING C-CHECK, THE RT ENGINE LOWER FORWARD MOUNT YOKE WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE REMOVED AND REPLACED THE YOKE IAW ECTC EA 26-2014-063-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — FAILED (CABIN LIGHT) · airframe 39,810 hrs · 30,616 cycles

A BURNING ODOR WAS REPORTED AT ROW 4. MAINTENANCE INSPECTED THE ACFT AND FOUND A BURNED LIGHT SOCKET AT SEAT 4D. R & R THE HARNESS AT SEAT 4D, OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FRAME 10) · airframe 39,464 hrs · 30,343 cycles

DENT AT FRAME 10 AFT OF NLG. CUTOUT DAMAGE AND INSTALLED FILLER AND DOUBLER IAW ETD2016-145-024575. ACFT RELEASED AND RETURNED TO SERVICE.

Part: FITTING — CRACKED (LT WING TE FLAP) · airframe 35,892 hrs · 27,505 cycles

DURING C-CHECK LT OTBD FLAP INBD FITTING CRACKED. MAINTENANCE REPAIRED LT OTBD FLAP INBD FITTING IAW TECHNICAL INSTRUCTION TI 145-13-200, REV J. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (LT ENGINE) · airframe 35,892 hrs · 27,505 cycles

DURING C-CHECK LT ENGINE FWD YOKE, FWD LOWER BRACKET IS CRACKED. MAINTENANCE REPAIRED LT ENGINE FWD YOKE FWD FITTING IAW EC5450-01105. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TORQUE BOX — CORRODED (ZONE 600) · corrosion level 2 · airframe 35,892 hrs · 27,505 cycles

DURING C-CHECK, RT TORQUE BOX LOWER INBD BOLT HOLE POSITION NR 1 CORRODED. MAINTENANCE PERFORMED REPAIR TO RT TORQUE BOX LOWER IB BOLT HOLE NR 1 POSITION IAW EC5710-61229. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CRACKED (FRAME 13) · airframe 35,892 hrs · 27,505 cycles

DURING C-CHECK, STRINGER 6R CRACKED AT FRAME 13. MAINTENANCE R & R STRINGER 6R AT FRAME 13 IAW SRM 51-40-02 AND RESTORED ORIGINAL FINISH TO AREA IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TORQUE BOX — GOUGED (ZONE 600) · airframe 35,892 hrs · 27,505 cycles

DURING C-CHECK, RT TORQUE BOX LOWER INBD BOLT HOLE POSITION NR 1 GOUGED ON FWD SIDE AT OPENING. MAINTENANCE PERFORMED AND COMPLETED REPAIR TO RT TORQUE BOX LOWER INBD BOLT HOLE POSITION NR 1 IAW EC5710-01229. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TOILET — CORRODED (LAVATORY) · corrosion level 2 · airframe 35,892 hrs · 27,505 cycles

DURING C-CHECK, LAVATORY TOILET BOWL IS CORRODED. MAINTENANCE R & R DUMP VALVE WASTE, DUMP SUPPORT ASSY IAW AMM 20-10-00 AND EDGE SEALED NUTPLATES, PRIMED AND PAINTED AREAS TO RESTORE IAW CPM 51-21-06 AND IS DETERMINED TO BE MAJOR IAW SOP 5102. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 35,892 hrs · 27,505 cycles

DURING C-CHECK, CARGO DOOR CUTOUT LOWER BEAM FOUND CORRODED BETWEEN FRAMES 65-68. MAINTENANCE REMOVED AND INSTALLED NEW DOOR CUTOUT BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (ZONE 200) · airframe 35,892 hrs · 27,505 cycles

DURING C-CHECK, FRAME 10 FOUND CRACKED. MAINTENANCE R & R THE FRAME IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 79) · airframe 34,965 hrs · 26,792 cycles

DURING 4A, INSPECTION THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED 2.81MM LONG AT A RIVET ON FRAME 79, 1 RIVET BELOW STRINGER 6L. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2014-145-035517, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH ANGLE — CRACKED (VERTICAL TO FUSE) · airframe 34,965 hrs · 26,792 cycles

DURING 4A INSPECTION, THE RT VERTICLE STAB TO FUSELAGE ATTACH ANGLE WAS FOUND TO HAVE A CRACK EXTENDING 22.43MM. MAINTENANCE R & R THE AFFECTED ANGLE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — FAULTY (COCKPIT) · airframe 34,752 hrs · 26,628 cycles

THE CREW REPORTED F/O'S PRIMARY FLIGHT DISPLAY SMOKING AND CIRCUIT BREAKER TRIPPED. DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE F/O'S PRIMARY FLIGHT DISPLAY AND OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,686 hrs · 26,575 cycles

DURING MX INSPECTION, THE FLOOR EMERGENCY LIGHT STRIPS WERE FOUND INOPERATIVE. MX R & R THE NR 2 EMERGENCY LIGHT SYS INVERTER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,471 hrs · 25,612 cycles

LOWER LT EMERGENCY LIGHT IN GALLEY INOPERATIVE. MX R & R NR 2 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04, ACFT RETURNED TO SERVICE.

Part: SKIN — CORRODED · corrosion level 2 · airframe 30,919 hrs · 23,599 cycles

CORROSION OUT OF LIMITS ON SKIN PANEL BETWEEN FRAMES 13 AND 14, STRINGER 19L TO 21L. R & R SKIN PANEL. REMAP OF RVSM AREA IS WITHIN LIMITS.

Part: SIGN — INOPERATIVE (CABIN) · airframe 28,350 hrs · 21,517 cycles

DURING ROUTINE MAINTENANCE INSPECTION RIC MX DISCOVERED THE EMERGENCY LIGHT SIGN AT ROW 3B INOPERATIVE. RIC MX REMOVED AND REPLACED THE EMERGENCY LIGHT SIGN AT ROW 3B IAW EMB145 AMM 33-50-00 WITH OPERATIONAL CHECK SUCCESSFUL. ACFT WAS RETURNED TO SERVICE.

Part: INVERTER — FAULTY (CABIN) · airframe 28,269 hrs · 21,449 cycles

RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND SEAT 12BC UPPER EMERGENCY EXIT SIGN INOP. MX REMOVED AND REPLACED INVERTER NR 5 AND EXIT SIGN IAW EMB145 AMM 33-50-11 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — FAULTY (NR 2 ENGINE) · airframe 26,944 hrs · 20,362 cycles

IAD FLT 5821 THE CREW REPORTED A LAV SMOKE WARNING MESSAGE ON TAKEOFF. ALSO REPORTED A SMOKE SMELL. NO SMOKE WAS NOTED. THE AIRCRAFT RETURNED TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE CVG ACTUATOR. OPERATIONAL CHECKS WERE GOOD.

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 26,648 hrs · 20,120 cycles

IAH - FLIGHT 2468 THE CREW REPORTED THAT THE BRAKES TOOK FOUR SECONDS LONGER TO GRAB UPON LANDING. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED THE BRAKING WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,488 hrs · 20,004 cycles

IAH - FLIGHT 2429, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED CONNECTOR P8500, THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, AND THE NUMBER ONE BATTERY PACK POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 26,488 hrs · 20,004 cycles

IAH - FLIGHT 2429, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED CONNECTOR P8500, THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, AND THE NUMBER ONE BATTERY PACK POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 26,488 hrs · 20,004 cycles

IAH - FLIGHT 2429, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED CONNECTOR P8500, THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, AND THE NUMBER ONE BATTERY PACK POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,403 hrs · 19,942 cycles

RIC - ROW 6 EMERGENCY LIGHT STRIP OUT. REMOVED AND REPLACED EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 25,985 hrs · 19,602 cycles

SHV - DURING C-CHECK LT SKIN PANEL HAS CRACKS AROUND RIVETS BTW FR 77-79. REPAIRED SKIN IAW EC5330-02259. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 25,985 hrs · 19,602 cycles

SHV - DURING C-CHECK RT SKIN PANEL HAS CRACKS AROUND RIVETS BETWEEN FR 77-79. REPAIRED SKIN IAW EC5330-02259. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 25,486 hrs · 19,209 cycles

FLIGHT 2057 - CHS - FLIGHT CREW REPORTED BAG SMOKE DET LIGHT DID NOT ILLUMINATE DURING TEST. EWR MX REMOVED AND REPLACED BAGG SMOKE DETECTOR AFT POSITION AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: OXYGEN SYSTEM — LEAKING (COCKPIT) · airframe 24,292 hrs · 18,335 cycles

IAH - FLIGHT 2274, DURING CLIMB THE CREW REPORTED THAT THE CREW OXYGEN WAS LEAKING. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE FIRST OFFICERS OXYGEN MASK BOX, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 23,580 hrs · 17,787 cycles

IAH - FLIGHT 2314, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY EXIT SIGN AT 12BC TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SIGN, OPERATIONALLY TESTED WITH NO DEFECTS NOTED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — ACTIVATED (FUEL SYSTEM) · airframe 23,282 hrs · 17,577 cycles

TYS - AIRCRAFT 980, FLIGHT NUMBER 2432 DIVERTED TO TYS BECAUSE OF WEATHER CONDITIONS, THEN DEVELOP A NR 1/2 FUEL QUANTITY INDICATION. CREW AND PASSENGERS SWAP TO A/C 551.

Part: WIRE HARNESS — FAILED (RT MLG) · airframe 23,090 hrs · 17,444 cycles

GRR - FLIGHT 2775 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RT MAIN GEAR WOW PROXIMITY SWITCH HARNESS. OPERATIONAL CHECKS WERE GOOD.

Part: ELECTRONIC UNIT — MALFUNCTIONED (LANDING GEAR) · airframe 23,037 hrs · 17,406 cycles

IAH - FLIGHT 2206, THE CREW REPORTED A LANDING GEAR AIR / GROUND FAIL MESSAGE ON CLIMB. THE AIRCRAFT RETURNED TO AMA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND THE AIRCRAFT WAS SUBSEQUENTLY FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE LGEU, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HOSE — LEAKING (VALVE) · airframe 22,979 hrs · 17,358 cycles

DURING CLIMB THE CREW REPORTED A PACK 1 FAIL WHILE THE NR 2 PACK WAS ON MEL. ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE 4 HOSES ON THE TORQUE MOTOR DUAL VALVE, OPS AND LEAK CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SENSOR — DEFECTIVE (ZONE 700) · airframe 22,922 hrs · 17,317 cycles

LANDING GEAR AIR/GROUND MESSAGE AFTER TAKEOFF. REMOVED AND REPLACED RT MLG SHOCK ABSORBER WOW SWITCH IAW AMM 32-63-01. ACFT WAS APPROVED FOR RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 22,874 hrs · 17,279 cycles

IAH - FLIGHT 2028 - THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE ON EICAS, AND THE LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE LGEU, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (NLG) · airframe 22,825 hrs · 17,241 cycles

HSV - FLIGHT 2855 - THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO HSV WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS INSPECTED AND APPROVED FOR A FERRY FLIGHT TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR WOW PROXIMITY SENSOR, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — INTERMITTENT (COCKPIT) · airframe 22,730 hrs · 17,159 cycles

DAY FLIGHT 2082 - CREW REPORTED LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS AFTER TAKEOFF. MAINTENANCE PERFORMED PROXIMITY SWITCH SENSOR HEALTH CHECK AND AIR/GROUND SYSTEM OPERATIONAL CHECK. MAINTENANCE REPLACED RELAY KO353 AIR/GROUND POSITION RELAY. ALL OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — DEFECTIVE (LANDING GEAR) · airframe 22,628 hrs · 17,079 cycles

FLIGHT 2212 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR/GRND FAIL ON EICAS AFTER TAKEOFF. EWR MX REMOVED AND REPLACED LGEU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROL LEVER — DEFECTIVE (COCKPIT) · airframe 22,530 hrs · 16,998 cycles

FLIGHT 2724 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAILURE INDICATION ON EICAS AFTER TAKEOFF AND THE LANDING GEAR LEVER LOCKED IN THE DOWN POSITION. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED LANDING GEAR CONTROL LEVER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: TURBINE WHEEL — CRACKED (NR 2 ENGINE) · airframe 22,442 hrs · 16,942 cycles

DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.

Part: SIGN — INOPERATIVE (CABIN) · airframe 22,408 hrs · 16,920 cycles

EMERGENCY SIGN AFT OF LT EMERGENCY DOOR IN CABIN INOP. REMOVED AND REPLACED EMERGENCY EXIT SIGN IAW EMB 145 AMM 33-50-13. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: RELAY — INOPERATIVE (LANDING GEAR) · airframe 22,305 hrs · 16,840 cycles

SHV - AIRCRAFT N15980 WAS GIVEN A FERRY FLIGHT RELEASE PERMIT FROM DFW TO SHV BECAUSE OF AN AIR GROUND SENSOR FAIL ON T/O OUT OF OKC AND WAS UNABLE TO RETRACT THE LANDING GEAR, THEN IT WENT AWAY AND GEAR RETRACTED (CAME UP). MAINTENANCE IN SHV REMOVED AND REPLACED RELAY K0024 IAW EMB145 FIM 32-32-00-810-801-A. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: VALVE — UNKNOWN (CABIN PRESSURE) · airframe 22,305 hrs · 16,840 cycles

SHV - AIRCRAFT N15980 WAS GIVEN A FERRY FLIGHT RELEASE PERMIT FROM DFW TO SHV BECAUSE PACK VALVE 1 CLOSED, COULD NOT RESET. CABIN ALT RAISED PASSED 8,000FT UP TO 14,000FT AT 14:00. EMERGENCY DESCENT WAS PERFORMED. ALSO, O2 MASKS DEPLOYED COMING OUT OF OKC. MAINTENANCE IN SHV PERFORMED OPERATIONAL CHECK OF PACK 1 VALVE IAW EMB145 AMM 21-31-00. OPERATIONAL CHECK GOOD. PRESSURIZATION CHECK PASSED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FALSE INDICATION (NLG) · airframe 22,188 hrs · 16,758 cycles

IAH/TYS- LANDING GEAR AIR/GROUND FAIL AFTER TAKEOFF. TYS MX REMOVED AND REPLACED THE NOSE PROXIMITY SWITCH WEIGHT ON WHEELS SYSTEM IAW EMB 145AMM 32-63-02. A/C WAS RETURNED TO SERVICE.

Part: SWITCH — FAULTY (PARKING BRAKE) · airframe 21,812 hrs · 16,474 cycles

CAE FLIGHT NR3114 THE CREW REPORTED A NO TAKEOFF CONFIG WARNING ON THE EICAS ON TAKE OFF ROLL. THE CREW ABORTED TAKEOFF AND TAXIED TO THE GATE. MX INSPECTED AND REPLACED THE PARKING BRAKE SWITCH AND RELAY K0212. OPS CHECKS WERE GOOD. RELAY P/N M83536/6-022M.

Part: CONNECTOR — FAULTY (BRAKE SYSTEM) · airframe 21,772 hrs · 16,442 cycles

CLE FLT 2538 - THE CREW REPORTED A "NO TAKEOFF CONFIG" MESSAGE ON TAKEOFF. ABORTED TAKEOFF AND TAXIED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BRAKE PRESSURE SWITCH CONNECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: VALVE — FAULTY (BLEED SYSTEM) · airframe 21,700 hrs · 16,385 cycles

CLE FLIGHT NR 2344 THE CREW REPORTED A BLEED 2 OVERTEMP WARNING WITH THE ANTI-ICE SYSTEM TURNED ON. MSG CLEARED WITH ANTI-ICE OFF. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,457 hrs · 16,202 cycles

RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT FLOOR STRIP INOPERATIVE. MX REMOVED AND REPLACED STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,691 hrs · 15,672 cycles

MCI - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHTING BETWEEN SEATS 15A & 17A WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: INVERTER — DEFECTIVE (EMERGENCY LIGHT)

RIC - DURING ROUTINE MAINTENANCE, RIC MAINTENANCE FOUND FLOOR BOARD EMERGENCY LIGHTS INOPERATIVE FROM ROW 12A TO 19A. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLOOR BOARD LIGHT INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,581 hrs · 14,917 cycles

EMERGENCY LIGHT AT SEAT 12BC INOP. REMOVED AND REPLACED LAMP IAW EMB 145 AMM 33-50-06. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (NLG) · airframe 19,983 hrs · 14,787 cycles

FLT 2652 - BNA - CREW REPORTED "LG AIR/GND FAIL" CAUTION MESSAGE CAME ON AFTER AIRBORNE AT 100' ARL AND MESSAGE WENT OFF UPON TOUCHDOWN (AIR RETURN). BNA MX FOUND "LG NOSE WOW SW FAIL" MESSAGE ON CMC. MX REMOVED AND REPLACED NLG WOW PROX SW AND PERFORMED TEST FLIGHT SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. AFTER T/O, CREW REPORTED "LG AIR/GND FAIL" CAUTION MESSAGE CAME ON AFTER AIRBORNE AT 100' ARL AND MESSAGE WENT OFF UPON TOUCHDOWN (AIR RETURN)AGAIN. BNA MX ADJUSTED NLG WOW PROXIMITY SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (AIR GROUND SYS) · airframe 19,233 hrs · 14,676 cycles

OMA - FLIGHT 2145, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON TAKEOFF. THE AIRCRAFT RETURNED TO OMA WHERE IT LANDED WITHOUT INCIDENT. THE CREW SUCCESSFULLY RESET THE AIR GROUND SYSTEM PER MAINTENANCE CONTROL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (NLG) · airframe 19,163 hrs · 14,633 cycles

IAH - FLIGHT 2173, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL ON TAKEOFF. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SENSOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (LANDING GEAR) · airframe 19,129 hrs · 14,612 cycles

IAH FLIGHT 2881, DURING CLIMB, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE AND THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE LEFT MAIN GEAR PROX SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — DAMAGED (NOSE GEAR) · airframe 18,811 hrs · 14,384 cycles

MDW FLIGHT 2432 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO MDW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR WOW PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 11,611 hrs · 8,732 cycles

DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED AND REPLACED BEAM IAW 51-40-02.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 11,611 hrs · 8,732 cycles

DURING C-CHECK STRINGER 19R WAS FOUND GOUGED BETWEEN FRAME 52 AND 53. REMOVED DAMAGED AREA AND INSTALLED DOUBLER IAW 53-24-02.

Part: BEARING CAP — CORRODED (NLG) · airframe 11,611 hrs · 8,732 cycles

DURING C-CHECK NOSE GEAR RIGHT BEARING CAP WAS FOUND PITTED. REPLACED BEARING CAP IAW 32-20-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 7,661 hrs · 5,576 cycles

DURING A SCHEDULED 2-C INSPECTION, MULTIBLE SEAT TRACKS HAD CORROSION. MAINTENANCE REMOVED AND REPLACED SEAT TRACKS IN THE CABIN IAW EMB 145MM-53-01-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 7,661 hrs · 5,576 cycles

DURING A SCHEDULED 2-C INSPECTION MAINTENANCE FOUND CHAFING ON STRINGERS 19L-19R AT FRAME 53. MAINTENANCE REMOVED DAMAGED AREA AND REPAIRED BOTH AREAS IAW EMB 135/145 SRM 53-24-02. ALODINED AND PRIMED IAW EMB 135/145 CPM51-21-04;05. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 7,661 hrs · 5,576 cycles

DURING A SCHEDULED 2-C INSPECTION THE RAMP ANGLE AT THE FWD CENTER OMEGA BEAM WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,661 hrs · 5,576 cycles

DURING A SCHEDULED 2-C INSPECTION THE CARGO DOOR SILL WAS FOUND CORROCDED. MAINTENANCE REMOVED DOOR, REMOVED THE COVER SILL, LOCATED, DRILL NEW DOOR SILL, INSTALLED DOOR PROTECTIVE STRIPS AND INSTALLED DOOR. PRESSURE CHECK WAS GOOD IAW 135/145 SRM 53-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: BEAM — CORRODED (FUSELAGE) · airframe 7,661 hrs · 5,576 cycles

DURING A SCHEDULED 2-C INSPECTION THE LT OMEGA BEAM AND RAMP ANGLE WERE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA; FAB FILLER, SHIM, EXTERNAL LT RAMP ANGLE IAW EMB 135/145 SRM 53-21-10. ALODINED AND PRIMED IAW EMB 135/145 CPM51-21-04;05. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: BEAM — CORRODED (FUSELAGE) · airframe 7,661 hrs · 5,576 cycles

DURING A SCHEDULED 2-C INSPECTION THE FWD-CENTER OMEGA BEAM TOP CAP WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: BRACE — CORRODED (NLG) · airframe 7,661 hrs · 5,576 cycles

DURING A SCHEDULED 2-C INSPECTION MAINT FOUND CORROSION ON THE LT AND RT NLG BRACE CAPS. MAINTENANCE REMOVED AND REPLACED BOTH CAPS IAW EMB 135/145 AMM 32-20-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: BEAM — CORRODED (FUSELAGE) · airframe 7,661 hrs · 5,576 cycles

DURING A SCHEDULED 2-C INSPECTION THE CENTER OMEGA BEAM WAS CORRODED. MAINTENANCE CUT OUT THE DAMAGED AREA AND FAB NEW FILLER REPAIR. INSTALLED NEW PIECE IAW EMB 135/145 SRM 53-21-10; 51-40-02. ALODINED, PRIMED IAW EMB 135/145 CPM 51-21-04;05. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: BEAM — CORRODED · airframe 7,661 hrs · 5,576 cycles

TYS DURING A SCHEDULED 2-C INSPECTION THE FORWARD FLOOR SUPPORT BEAM FOR PANEL 242AF WAS FOUND CORRODED. MAINT. CLEANED AREA,FAB.,ALLODINED AND PRIMED A DOUBLER AND INSTALL IAW EMB 135/145 SRM-51-10-02 AND CMP-51-21-04/05/06.ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: BRACKET — DAMAGED · airframe 7,661 hrs · 5,576 cycles

TYS, During a scheduled inspection both left hand outbd aileron PCA attachmrnt points have migrating bushings. Maintenance removed and replaced the aileron attchment bracket I/A/W-EMB-SRM-51-21-04/05/06 and EC5750-0117. Aircraft will be released to service upon complection of inspection.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 7,661 hrs · 5,576 cycles

DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD FLOOR SUPPORT DIGITAL PLATE AFT OF THE COCKPIT DOOR. MAINTENANCE REMOVED AND REPLACED THE DIGITAL PLATE IAW-EMB-145-SRM-57-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,661 hrs · 5,576 cycles

DURING A SCHEDULED INSPECTION THE FORWORD TOP CAP BELOW THE LT SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REPLACED THE RIVETS AND CLEANED CORROSION OFF OF THE TOP CAP IAW-EMB-145-SRM-57-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.

Part: SILL — CORRODED · airframe 7,661 hrs · 5,576 cycles

TYS, During a scheduled inspection the service door aft sill was found corroded. Maintenance removed and replaced the sill I/A/W-EMB-SRM-51-40-02. Aircraft will be released to service upon complection of inspection.

Part: HOUSING — GOUGED · airframe 7,661 hrs · 5,576 cycles

TYS, During a scheduled inspection the right vertical stab spherical bearing housing support has internal gouges at 1 and 8 oclock position. Maintenance reamed the hole and installed a bushing I/A/W-EMB-EC5510-01049. Aircraft will be released to service upon complection of inspection.

Part: BELLCRANK — CRACKED (EMPENAGE) · airframe 5,942 hrs · 4,218 cycles

TYS, During a scheduled EA2730-01044 inspection of the elevator control system, the right hand rear mechanism quadrant bellcrank was found cracked. Maintenance removed and replaced the bellcrank. I/A/W-EMB-145-MM-27-31-01. Operational checked good, aircraft released to service.

Part: ODOR — DETECTED (COCKPIT)

CLE FLIGHT 3030 THE CREW REPORTED A FUEL SMELL IN THE COCKPIT WHEN THE APU WAS STARTED IN FLIGHT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE FOUND.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CHECK VALVE — COKED (APU)

CLE FLIGHT# 3199 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT WHEN STARTING THE APU ON THE GROUND OR IN THE AIR.MAINTENANCE PLACED THE APU ON MEL.MAINTENANCE PERFORMED CLEANING OF THE APU COMBUSTOR DRAIN CHECK VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ODOR — DETECTED (COCKPIT)

CLE FLIGHT 3198 THE CREW REPORTED A STRONG FUEL SMELL IN COCKPIT WHEN STARTING APU BOTH ON GROUND AND IN FLIGHT. MAINTENANCE PERFORMED APU OPERATIONAL CHECKS AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BOLT — LOOSE (CABIN DOOR)

CLE FLIGHT#3242 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN AND CLOSE.MAINTENANCE INSPECTED AND RESECURED BOLT ON THE INNER HANDLE OF MAIN CABIN DOOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DAY - DURING MAINTENANCE INSPECTION, THE AISLE PATH EMERGENCY LIGHTS AT ROWS 12-15 WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE AFFECTED SECTION OF LIGHT STRIP ON MEL 33-50-00-2 CAT C, CONTROL NUMBER 014639, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 08/11/01 THE AIRCRAFT RETURNED TO EWR WHERE MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP AT ROWS 12 THRU 15. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

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

SLP - FLIGHT 4054, THE CREW REPORTED THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO SLP WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE RIGHT MAIN LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR — OUT OF RIG (ENTRY DOOR)

IAH - FLIGHT 3300, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE MAIN CABIN DOOR INDICATED CLOSED AND LOCKED WHILE OPEN. MAINTENANCE RIGGED THE CABIN DOOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 3,445 hrs · 2,431 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT HAND OMEGA BEAM RAMP ANGLE WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-145 SRM-51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: STIFFENER — CHAFED (LT COWLING) · airframe 3,445 hrs · 2,431 cycles

TYS DURING A SCHEDULED INSPECTION THE LEFT ENGINE UPPER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REPAIRED THE COWLING IAW EMB GST-0999/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,445 hrs · 2,431 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REPAIRED OMEGA BEAM IAW EMB GST-1030/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 3,445 hrs · 2,431 cycles

TYS DURING A SCHEDULED INSPECTION THE RIGHT OMEGA BEAM TOP CAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 19 AND 22. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB-145 SRM-51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 3,445 hrs · 2,431 cycles

TYS DURING A SCHEDULED INSPECTION THE CARGO DOOR SKIN WAS FOUND CHAFED AT THE EDGES OF EXTERNAL HANDLE CUTOUT. MAINTENANCE REPAIRED THE DAMAGED AREA IAW EMB GST-0998/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SKIN — DAMAGED (APU COWLING) · airframe 3,445 hrs · 2,431 cycles

TYS DURING A SCHEDULED INSPECTION THE APU COWLING L-PROFILE WAS FOUND TO BE DAMAGED. MAINTENANCE REPAIRED THE APU COWLING IAW EMB GST-0971/01, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF INSPECTION.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 3,445 hrs · 2,431 cycles

TYS DURING A SCHEDULED INSPECTION THE AFT LEFT HAND RAMP ANGLE ON THE LEFT OMEGA BEAM WAS FOUND TO CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-145 SRM-51-30-01, 51-40-02 AND EMB-145 CPM-51-21-03. THE REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SKIN — NICKED (TAIL CONE) · airframe 3,445 hrs · 2,431 cycles

TYS DURING A SCHEDULED INSPECTION THE TAIL CONE WAS FOUND TO BE NICKED BEYOND MANUFACTURES LIMITS. MAINTENANCE REPAIRED THE TAIL CONE IAW EMB GST-0994/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION

Part: FRAME — CHAFED (FUSELAGE) · airframe 3,445 hrs · 2,431 cycles

TYS DURING A SCHEDULED INSPECTION, FRAME 63 BETWEEN STRINGERS 7 AND 8 WAS FOUND TO BE CHAFED. MAINTENANCE REPAIRED DAMAGED AREA IAW EMB GST-0967/01, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: ROLLER — LACK OF LUBE (FWD DOOR)

EWR FLIGHT 4258 THE CREW REPORTED THE FORWARD DOOR IS VERY DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND LUBED THE DOOR ROLLERS. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DUCT — CRACKED (BLEED AIR)

CLE - FLT 3641 - THE CREW REPORTED ON CLIMB-OUT, RECEIVED A NR 2 BLEED LEAK INDICATION. THE REPORTED A STRONG BURNING SMELL UNTIL THE BLEED WAS SHUT OFF. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 BLEED AIR DUCT ASSEMBLY IAW EMB MM 21-60-01. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: LINE — FAILED (LEFT ENGINE)

EWR - FLT 4253 - THE CREW REPORTED THAT THEY LOST NR 1 HYDRAULIC SYSTEM PRESSURE. THE AIRCRAFT DIVERTED INTO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 HYDRAULIC PUMP PRESSURE LINE IAW EMB145 MM 29-10-00. MAINTENANCE ALSO BLEED THE HYDRAULIC SYSTEM IAW 29-10-06. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)