N619AE

Part: NONE — NONE · airframe 48,288 hrs · 44,253 cycles

OVERWING EMERGENCY EXIT FORWARD CEILING LOCATOR LIGHT INOP-C/A-RAR NO. 6 EMERGENCY LIGHT AC/DC INVERTER IAW EMB 145 AMM 33-50-11. OPC GOOD.

Part: LIGHT — INOPERATIVE · airframe 47,816 hrs · 43,665 cycles

DURING PS-2 CHECK FOUND RH CENTER FAIRING EXTERIOR EMERGENCY LIGHT INOP-C/A-RAR RH CENTER FAIRING EXTERIOR EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD.

Part: LIGHT — BROKEN · airframe 47,793 hrs · 43,637 cycles

EMERGENCY FLOOR LIGHT AT ROW 8/9 WIRE BROKEN OFF-C/A-REPLACED EMERGENCY FLOOR LIGHT STRIP AT ROW 8/9 IAW EMB 145MM 33-50-12.

Part: CLAMP — BROKEN (FLASHLIGHT ASSY) · airframe 47,768 hrs · 43,610 cycles

FA EMERGENCY FLASHLIGHT MOUNT HAS A BROKEN CLAMP-C/A-RAR FWD FA EMERGENCY FLASHLIGHT IAW EMB145 AMM 33-50-16. OPC GOOD.

Part: FLASHLIGHT ASSY — BROKEN (CABIN) · airframe 46,906 hrs · 42,727 cycles

FA EMERGENCY FLASHLIGHT CLIP AND FLASHLIGHT BROKEN. MEL 25-53, AUTH 010001-C, LGPG 4714201, ITEM 1. C/A: REMOVED AND REPLACED F/A EMERGENCY FLASHLIGHT ASSEMBLY, IAW EMB 145 CMM 25-60-14. OPERATIONS CHECKED GOOD. MEL NR 25-53 RESTORED.

Part: LATCH — BROKEN (FLASHLITE CRADLE) · airframe 46,778 hrs · 42,608 cycles

F/A EMERGENCY FLASHLIGHT HOLDER FWD CABIN HAS LATCH BROKE. C/A: R & R FWD EMERGENCY FLASHLIGHT, IAW EMB 145 AMM 33-50-16. OPERATIONS CHECK GOOD.

Part: CONNECTOR — LOOSE (RA ANTENNA) · airframe 46,438 hrs · 42,273 cycles

APROX 15,000 MSL - RECEIVED ARUAL TO LOW TERRAIN WARNING BRIEFLY APPROXIMATELY 4,000 MSL. RECEIVED AURAL TOO LOW TERRAIN AND LANDING GEAR WARNING BRIEFLY. TRANSFERRED TO NRWC 619-ABI-03950 J. WILLIAMS 507866. C/A FOUND LT AND RT RA ANTENNA CONNECTIONS VERY LOOSE AND TIGHTENED CONNECTORS. FOUND EXCESS PAINT ON AFT WING TO FUSELAGE FAIRING BONDING STRAPS SCREW HOLES AND REMOVED EXCESS PAINT. PERFORMED RA OPC. OPC GOOD. SEE NRWC 619-ABI-03950 FOR WORK PERFORMED.

Part: SKIN — DEFORMED (FRAME 23) · airframe 46,437 hrs · 42,272 cycles

SKIN DEFORMATION LOCATED AT FRAME 23 STRINGERS 16R ? 17R.-C/A-SKIN DEFORMATION LOCATED AT FRAME 23 STRINGERS 16R ? 17R. FOUND STRINGER 17R AT FR 23 TO BE BENT. PERFORMED STRINGER REPAIR IAW EMB 145 SRM 53-00-03-RE.

Part: DRAG ANGLE — CRACKED (FRAMES 75-76) · airframe 46,437 hrs · 42,272 cycles

CRACK ON RH FWD VERTICAL TO FUSELAGE DRAG ANGLE NEAR AFT END IN RADIUS.-C/A-REMOVED AND REPLACED RH FWD VERTICAL TO FUSELAGE DRAG ANGLE IAW EMB 145 SRM 51-40-02.

Part: WEB — CHAFED (CARGO DOOR) · airframe 46,437 hrs · 42,272 cycles

CARGO DOOR LOWER FWD WEBBING CHAFED AT FASTENER. REPAIRED CARGO DOOR LOWER FWD WEBBING IAW SRM 52-30-01RE AND ETN-EM-52-043.

Part: RIB — CRACKED (LT WING) · airframe 46,437 hrs · 42,272 cycles

LEFT WING RIB 21 INSIDE PANEL 551CB IS CRACKED. REPAIRED THE LT WING RIB 21 IAW SRM 57-20-07RE ITEM 4.

Part: NUT PLATE — CORRODED (CARGO DOOR) · airframe 46,437 hrs · 42,272 cycles

CARGO DOOR UPPER NUT PLATE HOLES HAVE CORROSION 5 EA. REMOVED AND REPLACED CARGO DOOR UPPER NUT PLATE PROFILE IAW SRM 51-40-02.

Part: NUT PLATE — CORRODED (CARGO DOOR) · airframe 46,437 hrs · 42,272 cycles

CARGO DOOR LOWER NUT PLATE HOLES HAVE CORROSION 7 EA.-C/A-REMOVED AND REPLACED CARGO DOOR LOWER NUT PLATE PROFILE IAW EMB 145 SRM 51-40-02.

Part: YOKE — CRACKED (ENGINE MOUNT) · airframe 46,437 hrs · 42,272 cycles

RH ENGINE FWD LOWER YOKE CRACKED. REMOVED AND REPLACED RH ENGINE FWD LOWER YOKE IAW ERS-EM-54MR-698.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 46,437 hrs · 42,272 cycles

EMERGENCY LIGHT STRIP 8 HAS WIRE INSULATION PULLED OUT OF HOUSING ON BOTH WIRES. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 46,437 hrs · 42,272 cycles

LEFT ELEVATOR TRAIL EDGE UPPER SKIN HAS HOLE. PERFORMED A REPAIR ON THE LT ELEVATOR TRAIL EDGE IAW ERS-EM-55MR-854.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,437 hrs · 42,272 cycles

NR 4 EMERGENCY BATTERY INOP. C/A COMPLETE: R & R NR 4 EMERGENCY BATTERY AND BATTERY POWER SUPPLY, IAW EMB 145 AMM 33-50-04 ETN-EM-20-040 BONDING TEST GOOD. EMERGENCY LIGHTING SYSTEM, OPS CHECK GOOD MILLIOHM METER NR 6488.

Part: LIGHT — CRACKED (CABIN) · airframe 46,437 hrs · 42,272 cycles

LT EMERGENCY LIGHT STRIP PANELS AT POSITIONS 2, 3, 5, AND 8 ARE CRACKED/BROKEN. C/A COMPLETE: REMOVED AND REPLACED LT EMERGENCY LIGHT STRIP COVER PANELS AT POSITIONS 2,3,5, AND 8, IAW EMB-145 AMM 33-50-12. SEE BOW 346487 FOR INSTALL ONTO AIRCRAFT.

Part: BATTERY PACK — NOT REPORTED (EMERGENCY LIGHTS) · airframe 46,437 hrs · 42,272 cycles

A3265 OPS A. REMOVE AND REPLACE EMERGENCY LIGHTING BATTERY ASSY/BATTERY CHARGER EMB WC 33-700-19 CRJ WC 33-002 ETN-EM-25-385 PN 2013-1A SN 10484 POS 3. C/A COMPLETE: REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY ASSY/ BATTERY CHARGER PN 2013-1A SN 104848 POS 3, IAW ENVOY WC 33-700-19. OPS CHECK OF EMERGENCY LIGHTING SYSTEM GOOD.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 46,289 hrs · 42,164 cycles

CABIN ALT REACHED 9600FT @ AT FL190 AFTER DESCENDING TO 10000FT CABIN SLOWLY REPRESSURIZED TO 400 FT (DELTA)P 4.4 NORMAL FOR THAT ALTITUDE-C/A-FOUND PNEUMATIC OUTFLOW VALVE STICKING, REPLACED AND REMOVED P.O.V. IAW AMM 21-31-04. PERFORMED FUNCTIONAL CHECK IAW AMM 21-31-00-05. FNC GOOD AND PERFORMED PRESSURIZATION CHECK IAW AMM 21-31-00-02. PRESSURIZATION CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: SUPPORT — DAMAGED (PAX DOOR) · airframe 46,288 hrs · 42,162 cycles

SUPPLEMENTAL MAIN PAX ENTRY DOOR VERY HARD TO OPEN.-C/A-WHILE T/S HARD TO OPEN AND INSPECTION SUPPORT ASSY BOLTS IAW ETN-EM-52-052 FOUND DAMAGE TO THE BEARING SUPPORT AND LOCKING SHAFT MIGRATING. REF ITEM #3 THIS LOG PAGE FOR DISCREPANCIES. REMOVED AND REPLACED TUBE MOUNT/BEARING ASSY IAW ERS-EM-5200-1082. PULL TO OPEN TEST C/W IAW AMM 52-18-00. RECORED 38LBS. TEST GOOD AT THIS TIME. REMOVED AND REPLACED TUBE MOUNT/BEARING ASSY IAW ERS-EM-5200-1082. PULL TO OPEN TEST C/W IAW AMM 52-18-00. RECORED 38LBS. TEST GOOD AT THIS TIME.

Part: LOCK — LACK OF LUBE (PAX DOOR) · airframe 46,287 hrs · 42,160 cycles

FA REPORTS ENTRY DOOR IS EXTREMELY HARD TO UNLOCK + WILL UNLOCK HALFWAY THEN GOT STUCK. ONCE UNLOCKED IT IS HARD TO PUSH OPEN.-C/A-LUBRICATED PAX DOOR ROLLERS IAW AMM 53-21-03. NO DEFECTS NOTED.

Part: DRIVE UNIT — DAMAGED (TE FLAPS) · airframe 46,005 hrs · 41,868 cycles

FLAP FAIL UPON ACCD ALT ON TAKEOFF-C/A-T/S FLAP FAIL MSG IAW FIM 27-51-00-810-801-A REMOVED AND REPLACED FPDU IAW EMB 145 AMM 27-53-04 NO FIX REMOVED AND REPLACED FECU IAW EMB 145 AMM 27-53-02 OPS CHECK GOOD IAW EMB 145 AMM 27-53-00-700-802-A NO FURTHER DEFECTS NOTED. FLAP ELECTRONIC CONTROL UNIT P/N 363100-1005 S/N 1126A

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 45,985 hrs · 41,847 cycles

GALLEY EMERGENCY LIGHTS NOT PASSING FUNCTIONAL CHECK-C/A-REMOVED AND REOLACED NUMBER 2 EMERGENCY BATTERY POWER SUPPLY ASSY IAW EMB AMM 33-50-04. EMERGENCY LIGHTING BATTERY P/N 2013-1ASMI S/N 67906

Part: WING — DAMAGED (RIGHT) · airframe 45,982 hrs · 41,845 cycles

WX-DMG / A/C LANDED SLID OFF RWY INTO TERRAIN. NO INJ TO CREW/PAX. ALL PAX TRANSPORTED TO TERMINAL BY BUS. EMERGENCY DECLARED.-C/A-PENDING CORRECTIVE ACTIONS. REINSTALLED RH WING SPEED BRAKE ACTUATOR IAW STEPS 3A THRU/INCLUDING 3J(6) OF AMM 27-62-02-400-801A. REPLACED RH WING IAW ERS-EM-5700-1193. REMOVED AND REPLACED STANDBY ALTIMETER IAW AMM 34-11-01. LEAK AND FUNCTIONAL CHECK GOOD. SNDBY (INHG) ALTIMETER P/N C14130AA S/N 224

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,722 hrs · 41,597 cycles

ROW 17 AISLE EMERGENCY LIGHT INOPERATIVE. R & R ROW 17 AISLE EMERGENCY LIGHT LAMP IAW AMM 33-50-08. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 45,200 hrs · 41,172 cycles

BLD 2 LEAK WARNING MSG. C/A-PERFORMED INSPECTION AND LEAK CHECK OF BLEED 2 AIR SYSTEM AS PER AMM 36-11-09. WITH ENGINE RUNNING FOR 25 MINS. NO LEAKS OR FAULTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,558 hrs · 40,575 cycles

MAIN-DOOR EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED MAIN-DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-06-000-801-A AND AMM 33-50-06-400-801-A. OPS CHECK GOOD. NO MORE DEFECTS NOTED AT THIS TIME. END.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,303 hrs · 40,363 cycles

FWD CEILING EMERGENCY LIGHT INOP. R&R EMERGENCY LIGHT IAW AMM 33-50-08. OPC GOOD.

Part: HINGE FITTING — WORN (RT AILERON) · airframe 43,697 hrs · 39,735 cycles

RIGHT AILERON OUTBOARD HINGE FITTING HAS A MIGRATING BUSHING. REMOVED AND REPLACED RT AILERON OB HINGE FITTING/BUSHING ASSY IAW EO EM-27MR-112.

Part: STRUCTURE — UNKNOWN · airframe 43,697 hrs · 39,735 cycles

EM-52MR-236 PTB COCKPIT UNDERFLOOR ACCESS HATCH FRAME REPAIR-C/A-C/W EO# EM-52MR-236 PART B

Part: BRACKET — LOOSE (WOW SWITCH) · airframe 43,499 hrs · 39,561 cycles

LDG AIR/GND FAILED, INSPECTED AND FOUND A LOOSE BRACKET HOLDING THE WOW SWITCH ON THE LT AFT LANDING GEAR, PERFORMED AN OPS CHECK OF ALL 5 WOW SWITCHES INDIVIDUALY. PERFORMED AIR GROUND SYSTEM SIMULATION TEST THREE TIMES, OPS CHECKED GOOD, NO MESSAGE ON EICAS.

Part: WARNING MESSAGE — ILLUMINATED (NR 2 A/C PACK)

NR 2 PACK OVERLOAD. R & R THE SLEEVE, OPS CHECKED GOOD.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 43,213 hrs · 39,494 cycles

FRAME 65 SHEAR TIE CORRODED ON THE LOWER END BY CARGO DOOR SILL. REPAIRED THE SHEAR TIE.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 42,386 hrs · 38,584 cycles

BLEED 2 LEAK ON CLIMB OUT FOUND HIGH STAGE VLV CLAMP LOOSE AND TIGHTENED. FOUND BLEED VALVE NR 2 CLAMP LOOSE AND TIGHTENED. RAN THE LEAK CHECK AT 90%. NO LEAKS NOTED AT THIS TIME.

Part: SENSOR — LOOSE (BLEED DUCT) · airframe 42,386 hrs · 38,583 cycles

NR 2 BLEED LEAK IN FLT, WHILE CLIMBING THROUGH 13,000 FEET. QRH PERFORMED, NO CHANGE. SECURED A LOOSE TEMP SENSOR ON THE DUCT FORWARD OF THE NR 2 PRE COOLER. OPS CHECKED GOOD.

Part: O-RING — LEAKING (NR 2 BLEED SYS) · airframe 42,385 hrs · 38,582 cycles

NR 2 BLEED LEAK WARNING IN FLIGHT. FOUND A BROKEN O-RING AT DUCT JOINT 14. R & R O-RING. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 42,353 hrs · 38,553 cycles

EICAS WARNING BAGG SMOKE DURING PUSH. BAGGAGE FIRE EXT BUTTON PRESSED. REMOVED AND REPLACED FWD CARGO BAY SMOKE DETECTOR. OPS CHECK GOOD.

Part: SKIN — GOUGED (FRAME 75) · airframe 42,348 hrs · 38,549 cycles

SKIN REPAIR DOUBLER AT FRAME 75, STRINGER 2R GOUGED. REPAIRED THE SKIN DOUBLER.

Part: FRAME — CRACKED (FRM 66) · airframe 42,348 hrs · 38,549 cycles

FRAME 66 CRACKED AT STRINGER 16R. REPAIRED THE FRAME.

Part: FRAME — CRACKED (FRM 73) · airframe 42,348 hrs · 38,549 cycles

FRAME 73 CRACKED JUST BELOW THE RT AFT FLOOR SILL. R & R THE FRAME LOWER SECTION.

Part: SHEAR TIE — CORRODED · airframe 42,348 hrs · 38,549 cycles

FRAME 65 SHEAR TIE CORRODED IN THE CARGO DOOR CUTOUT, LOWER CORNER. REPAIRED THE SHEAR TIE.

Part: SKIN — GOUGED (FRAME 75) · airframe 42,348 hrs · 38,549 cycles

RIGHT SIDE OF FUSELAGE SKIN GOUGED AFT OF FRAME 75, BELOW STRINGER 6R. REPAIRED THE SKIN.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 42,348 hrs · 38,549 cycles

CARGO DOOR SKIN HAS A POSSIBLE CRACK AT AFT UPPER CORNER OF CARGO DOOR HANDLE CUTOUT (MARKED). REPAIRED CARGO DOOR SKIN.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,348 hrs · 38,549 cycles

PERFORM PERMANENT REPAIR TO DENT ON RT FWD FUSELAGE BETWEEN FR3 AND 4, STRINGERS 9R & 11R. PERFORMED PERMANENT REPAIR TO DENT ON RT FWD FUSELAGE BETWEEN FR3 AND 4, STRINGERS 9R & 11R.

Part: BULB — INOPERATIVE (FLOOD LIGHT) · airframe 41,647 hrs · 37,907 cycles

RIGHT AFT WING TO BODY FAIRING EXTERIOR FLOOD LIGHT INOPERATIVE. R & R THE FAIRING EXTERIOR FLOOD LIGHT BULB, OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 41,371 hrs · 37,649 cycles

FWD CABIN FLASHLIGHT INOPERATIVE. R & R FWD CABIN FLASHLIGHT. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSER) · airframe 41,661 hrs · 37,698 cycles

THRUST REVERSER FAILURE ON THE NR 2 ENGINE DURING FLIGHT. PERFORMED OPS CHECK OF RT THRUST REVERSER DURING TAXI IAW AMM 78-31-01. OPS CHECKED GOOD

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,994 hrs · 35,654 cycles

PAX DOOR SWING ARM EMERGENCY LIGHT INOPERATIVE LENS CRACKED. REPLACED THE BULB AND REPLACED LENS ON PAX DOOR SWING ARM EMEGENCY. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,455 hrs · 35,209 cycles

ENTRANCE EMERGENCY CEILING FLOOD LIGHT NR 13 INOPERATIVE. R & R BULB IN ENTRANCE EMERGENCY FLOOD LIGHT NR 13. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,067 hrs · 34,893 cycles

EMERGENCY LIGHT 17A, 20 AND 19 WILL NOT ILLUMINATE. MAINTENANCE REPLACED BULBS, OPS CHECKED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 38,063 hrs · 34,889 cycles

LEFT NUMBER 1 EMERGENCY LIGHT STRIP WIRE IS BROKEN OFF. R & R NR 1 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: FRAME — CHAFED (FUSELAGE) · airframe 38,063 hrs · 34,889 cycles

FRAME 70 CHAFED, FROM SCREW, INSIDE CARGO BETWEEN STRINGER 12R & 13R. REPAIRED FRAME 70 BETWEEN STRINGERS 12R & 13R IAW ERS-EM-53MR-1512.

Part: CONNECTOR — BROKEN (CABIN) · airframe 38,063 hrs · 34,889 cycles

LEFT EMER LIGHT STRIP NR 1 HAS A BROKEN CONNECTOR. R & R CONNECTOR ON LT EMER LIGHT STRIP NR 1 IAW SWPM 20-21-00. SEE BOW 196324 FOR OPERATIONS CHECK. FOUND ON OPEN UP.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 38,063 hrs · 34,889 cycles

THE CTR & RT CTR LAVATORY FLOOR GUSSETS ARE CORRODED AT THE NUTPLATE HOLES. ACCOMPLISHED REPAIR TO THE CTR & RT CTR LAVATORY FLOOR GUSSETS IAW SRM 51-40-02. REPAIRED LAVATORY RT FLOORBEAM IAW ERS-EM-53MR-1501.

Part: PROFILE — CRACKED (FRAMES 23-24) · airframe 38,063 hrs · 34,889 cycles

LEFT NR 1 OMEGA BEAM AFT END CRACKED AT LOWER FLOOR SUPPORT BETWEEN FRAME 23 - 24. REPAIRED LEFT NR 1 OMEGA BEAM AFT END CRACKED AT LOWER FLOOR SUPPORT BETWEEN FRAME 23 - 24 IAW ERS-EM-53MR-1513.

Part: SKIN — CRACKED (FRAME 75) · airframe 38,063 hrs · 34,889 cycles

LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. REPAIRED LEFT UPPER FUSELAGE SKIN CRACK AFT OF FRAME 75 IAW ERS-EM-53MR-1517.

Part: SKIN — CRACKED (FRAME 75) · airframe 38,063 hrs · 34,889 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED AT FIRST FASTENER BELOW STRINGER 2R ON FRAME 75 CRACK. REPAIRED FRAME 75 IAW ERS-EM-53MR-1518.

Part: SKIN — CRACKED (FRAME 77) · airframe 38,063 hrs · 34,889 cycles

EXTERNAL FUSELAGE SKIN CRACK AT FRAME 77, STRINGER 4R. REPAIRED EXTERNAL FUSELAGE SKIN AT FRAME 77, STRINGER 4R IAW ERS-EM-53MR-1515.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,063 hrs · 34,889 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED, JUST AFT OF FRAME 75 & ABOVE STRINGER 2R, CRACK IS APPROXIMATELY 1/2" LONG. EASI 8071 USED, FREQ.=400 KHZ, V-GAIN=77.0, H-GAIN=64.0 LPF=100, 100-500 KHZ PROBE. RIGHT UPPER FUSELAGE SKIN CRACK JUST AFT OF FRAME 75 & ABOVE STRINGER 2R HAS BEEN ADDRESSED WITH ETD2015-145-014350. SEE ASSOCIATED NRTC E460799 FOR REPAIR INFORMATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,063 hrs · 34,889 cycles

LEFT UPPER FUSELAGE SKIN CRACKED AT FIRST FASTENER BELOW STRINGER 2L ON FRAME 75, CRACK IS APPROXIMATELY 1/4" LONG. EASI 8071 USED, FREQ.=400 KHZ, V-GAIN=77.0, H-GAIN=64.0 LPF=100, 100-500 KHZ PROBE. SEE NTRC E460796 FOR WORK ACCOMPLISHED. REPAIR COVERED IN ETD2015-145-014350.

Part: LIGHT — INOPERATIVE (PARKING BRAKE) · airframe 36,495 hrs · 33,423 cycles

PARKING BRAKE LIGHT INOPERATIVE. R & R PARKING BRAKE LIGHT BULBS. OPERATIONS CHECKED GOOD IAW SMP.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 36,460 hrs · 33,382 cycles

FLIGHT ATTENDANT`S EMER FLASHLIGHT HAS A BROKEN ON & OFF BUTTON. R & R IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: PRESSURE SWITCH — FAILED (ANTI-ICE SYS) · airframe 36,356 hrs · 33,297 cycles

E2 ANTI-ICE FAIL MSG ON CLIMB AT APPROX 500 FEET AGL. DEFERRED IAW MEL 30-11. M PROCEDURE COMPLIED WITH. R & R NR 2 ENG ANTI-ICE LOW PRESS SWITCH IAW AMM 30-21-02. PERFORMED OPERATIONS CHECK OF ENG THERMAL ANTI-ICING SYS IAW AMM 30-21-00. NO DEFECTS FOUND. MEL 30-11 RESTORED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,510 hrs · 31,820 cycles

DURING MX INSPECTION ON FLIGHT 2842 FOUND LT & RT OVERWING EMERGENCY LIGHTS INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 4 EMERGENCY BATTERY & CHARGER, CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,510 hrs · 31,820 cycles

LEFT & RT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 EMERGENCY BATTERY & CHARGER IAW AMM 33-700-19. OPERATIONS CHECK BAD.

Part: SKIN — GROOVED (RUDDER) · airframe 34,348 hrs · 31,692 cycles

RUDDER 1 LE GROOVED. REPAIRED RUDDER 1 GROOVED AREA ON LE IAW ERS-EM-55MR-009.

Part: VALVE — FAILED (BLEED AIR SYS) · airframe 34,415 hrs · 31,745 cycles

BLEED 2 OVER TEMPERATURE ON EICAS CLIMBING THROUGH 17000' WHILE IN ICING CONDITIONS. FOLLOWED PROCEDURE IN AOM VOL 1 & THE MESSAGE WENT OUT. LINE DISCONNECTED BETWEEN BLEED VLV & THERMOSTAT. RECONNECTED LINE, R & R FAN AIR VLV & PERFORMED OC & LEAK CHECKED GOOD IAW AMM 36-11-03 & AMM 36-00-00.

Part: SEAL — DAMAGED (BLEED AIR SYS) · airframe 34,414 hrs · 31,744 cycles

FLIGHT 3417 BLEED 2 LEAK WARNING MSG WING ANTI-ICE FAIL IN FLIGHT. DECLARED EMERGENCY LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED FUSELAGE BLEED LEAK CHECK IAW AMM 36-00-00. FOUND LEAK AT JOINT 24 AS LABELED IN AMM 36-11-00 & REPLACED SEALS IAW AMM 36-11-00. LEAK CHECKED GOOD AT 250 PSI IAW AMM, NO OTHER LEAKS NOTED.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 34,384 hrs · 31,719 cycles

UPON PWR BACK FOR DESCENT, BLD 2 LEAK INDICATION ON EICAS. EXECUTED EPC & AOM 1 PROCEDURES. DECLARED EMERGENCY & LANDED LFT. TORQUED RT ENG BLEED VLV CLAMP, LEAK CHECKED GOOD IAW AMM CH 36-11-05.

Part: DAU — FAULTY (NR 2) · airframe 34,383 hrs · 31,718 cycles

IN CRUISE FLIGHT EICAS ILLUMINATED, A DAU 2 WRN MISCOMP, 214M1302 THEN FOLLOWED BY BLD 2 LEAK WARNING. EXECUTED AOM PROCEDURES & LANDED SAFELY. R & R NR 2 DAU, OPERATIONS CHECKED GOOD IAW AMM CH 31-41-01. PERFORMED LEAK CHECK OF THE NR 2 BLEED SYS WITH NO DEFECTS NOTED IAW AMM CH 36-11-09.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,348 hrs · 31,692 cycles

NUMBER 4 LT FLOOR PROXIMITY STRIP LIGHT BROKEN. REPLACED NR 4 LT FLOOR PROXIMITY STRIP LIGHT IAW EMB 145 AMM 33-50-12.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,348 hrs · 31,692 cycles

FR 13 IS CORRODED BETWEEN STRINGER 21L & 21R. REPAIRED FR 13 IAW AE ERS-EM-53MR-053.

Part: FRAME — GOUGED (FUSELAGE) · airframe 34,348 hrs · 31,692 cycles

MACHINED FRAME AT FR 70 AT APPROXIMATELY STRINGER 13R GOUGED ON FACE. REPAIRED FRAME 70 IAW AE ERS-EM-53MR-052.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,348 hrs · 31,692 cycles

RIGHT LAVATORY FLOOR BEAM BETWEEN FR 59 - 61 CORRODED AROUND NUTPLATE HOLES. REPAIRED LAVATORY FLOOR BEAM IAW ERS-EM-53MR -051.

Part: SKIN — GROOVED (RUDDER) · airframe 34,348 hrs · 31,692 cycles

RUDDER 1 LE GROOVED. REPAIRED RUDDER 1 GROOVED AREA ON LE IAW ERS-EM-55MR-009.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,348 hrs · 31,692 cycles

FUSELAGE INNER SKIN CORRODED BETWEEN FR 13 & FR 14, BETWEEN STRINGER 19R & STRINGER 21L. REPAIRED IAW AE ERS-EM-53MR-057.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,348 hrs · 31,692 cycles

EMERGENCY FLOOR LIGHTS NR 4 & NR 5 & RT & LT EXIT IDENTIFIERS ARE INOPERATIVE. R & R NR 3 BATTERY POWER SUPPLY & BATTERY IAW EMB-145 AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: TIRE — FAILED (NLG) · airframe 34,261 hrs · 31,625 cycles

DURING TAKEOFF ROLL, NOTICED A STRONG VIBRATION IN COCKPIT. RETRACTED GEAR WITH NO ABNORMALITIES NOTED. SUSPECTED A POSSIBLE BLOWN TIRE. ATC REPORTED RUBBER FOUND ON THE RUNWAY. COMPLIED WITH AOM, VOL 1 PROCEDURES, CONTACTED SOC AND CONTINUED FLIGHT. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R LT NOSE WHEEL ASSY IAW W/C 32-700-17, OK FOR SERVICE. R & R RT NOSE TIRE IAW WC 32-700-17, OK FOR SERVICE. R & R THE NLG STEERING HARNESS IAW WM 20-21-00, PERFORMED NOSE STEERING SYS CHECK IAW AMM 32-50-00. OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: ENGINE — LEAKING (RIGHT) · airframe 33,689 hrs · 31,175 cycles

AFTER TAKEOFF THEY GOT A LAVATORY SMOKE WARNING. NO SMOKE SEEN, NOTICED AN ELECTRICAL ODOR. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND OIL POOLING BEHIND THE IVG'S AT THE 6 O`CLOCK POSITION IAW ETN-EM-79-014 ON THE RT ENGINE. R & R THE RT ENGINE IAW AE W/C 71-000-00. THE OPS CHECK WAS GOOD, NO LEAKS NOTED, NO SMOKE NOTED/DETECTED. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 33,168 hrs · 30,727 cycles

THE CREW REPORTED THE CABIN AND CABIN EMERGENCY LIGHTS WOULD NOT EXTINGUISH. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED FULL ELECTRICAL RESET IAW AMM 24-31-00. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,056 hrs · 30,630 cycles

THE F/A REPORTED THE FLASHLIGHT ABOVE THE JUMPSEAT DOES NOT APPEARS TO BE CHARGING AS THE RED LIGHT DID NOT ILLUMINATE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE BRACKET FOR FLASHLIGHT ABOVE THE JUMPSEAT IAW AMM 25-60-01. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: DOOR — OBSTRUCTED (CABIN) · airframe 32,993 hrs · 30,584 cycles

ON FLIGHT 4290 THE FLIGHT ATTENDANT REPORTED SHE HAD A DIFFICULT TIME OPENING THE MAIN CABIN DOOR. THE HANDLE OPERATED SMOOTHLY, YET DOOR WAS HUNG UP AND MAIN CABIN DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND SEVERAL SECURITY SEALS ON DOOR FRAME SEAL. REMOVED SECURITY SEALS. DOOR OPERATIONAL CHECK WAS GOOD IAW EMB-145 M/M TASK 52-18-00-820-001-A00. DOOR TEST AT 39 LBS. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ALTIMETER — FAILED (COCKPIT) · airframe 32,771 hrs · 30,411 cycles

FOR FLIGHT 4100 THE CREW REPORTED THAT DURING TAKEOFF ROLL ABOVE 80 KTS ELECTRICAL SMOKE SMELL WAS SENSED, TAKEOFF WAS ABORTED, THE FLIGHT ATTENDENT REPORTED THAT SHE ALSO SMELLED THE ELECTRICAL SMOKE ODORS. ALL THE PASSENGERS (INCLUDING TWO PILOTS SITTING IN THE MID AIRCRAFT) DID NOT SMELL THE ODOR. ONE PASSENGER SITTING NEAR THE FLIGHT ATTENDANT THOUGHT SHE SMELLED THE ODOR. WHEN CFR INITIALLY BOARDED THE AIRCRAFT THEY REPORTED A STRONG ELECTRICAL SMOKE TYPE ODOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED AIRCRAFT AND UNABLE TO REPRODUCE OR LOCATE ANY ELECTRICAL ODOR. AFTER RETURNING TO GATE CB # 33 "STBY ALT" WAS OUT. REMOVED AND REPLACED THE STANDBY ALTIMETER IAW EMB 145 AMM 34-12-01. LEAK TEST GOOD IAW 34-13-00-790-804-A. OPC GOOD IAW 34-12-00-700-801-A, AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — OBSTRUCTED (CABIN) · airframe 32,587 hrs · 30,258 cycles

ON FLIGHT 4010 THE CREW REPORTED THE MAIN CABIN DOOR WAS STUCK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED DEBRIS FROM DOOR. OPERATED DOOR & NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — UNSERVICEABLE (CABIN) · airframe 32,179 hrs · 29,946 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY POWER SUPPLY UNIT BATTERY NEEDED REPLACEMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BATTERY ASSEMBLY IAW WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — OBSTRUCTED (PAX DOOR) · airframe 3,455 hrs · 29,904 cycles

ON FLIGHT 3455 THE FLIGHT ATTENDANT REPORTED THE MAIN PASSENGER DOOR WAS HARD TO OPEN & CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED BROKEN SECURITY SEALS FROM PASSENGER DOOR SEAL REF EMB 145-AMM 52-18-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,947 hrs · 29,765 cycles

DURING B INSPECTION FOUND THE AFT EXIT RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP PER EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. LAMP PART NUMBER 1317. NO FIX. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY, ALSO REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK PER WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,418 hrs · 29,377 cycles

DURING B INSPECTION FOUND THE AISLE (CEILING) EMERGENCY LIGHT AT EMERGENCY EXIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AISLE EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-08. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 31,303 hrs · 29,271 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY STRIP LIGHTS INOPERABLE FROM ROW 12 TO THE LAVATORY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 INVERTER IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 30,784 hrs · 28,854 cycles

FLIGHT 3220, FLIGHT ATTENDANT REPORTED MAIN CABIN DOOR WAS HARD TO OPEN AND CLOSE. AIRCRAFT REMOVED FROM SERVICE. LUBRICATED AIRFRAME ROLLERS ON MAIN CABIN DOOR IAW AMM 53-21-02. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 30,739 hrs · 28,819 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED RIGHT WING EMERGENCY LAMP IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,100 hrs · 28,312 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FLOOR STRIP LIGHTS NR 1, 2, 3 INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE INVERTER 2 AND 3 IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — FAILED (FLASHLIGHT) · airframe 30,081 hrs · 28,294 cycles

FLIGHT 3229, CREW REPORTED THE FLIGHT ATTENDANT'S FLASHLIGHT WON'T STAY CHARGED, APPEARED CONNECTED BUT LOOSE. VIBRATIONS MAY CAUSE CHARGING TO START AND STOP. AIRCRAFT REMOVED FROM SERVICE. FOUND DAMAGED WIRE FOR FLASHLIGHT HOLDER. REPAIRED DAMAGED WIRE PER SPWM 20-10-00. REMOVED AND REPLACED FLASHLIGHT HOLDER REF AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — MISSING (CABIN) · airframe 30,051 hrs · 28,270 cycles

FLIGHT 2977, CREW REPORTED FORWARD EMERGENCY FLASHLIGHT MISSING. AIRCRAFT REMOVED FROM SERVICE. INSTALLED FORWARD EMERGENCY FLASHLIGHT. OPS CHECKED GOOD IAW 25-60-00. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,866 hrs · 28,141 cycles

ON FLIGHT 9800 THE CREW REPORTED THE EMERGENCY LIGHT ON THE LEFT EMERGENCY ROW INOPERABLE IN THE CEILING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT EMERGENCY EXIT LIGHT IAW EMB 145 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (RT WING) · airframe 29,874 hrs · 28,146 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT RIB 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED RIB 5 AND IAW EO-EM-57MR-595. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (LT WING) · airframe 29,874 hrs · 28,146 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT RIB 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE LEFT RIB 5 AND IAW EO-EM-57MR-595. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CRACKED (LT PYLON) · airframe 29,865 hrs · 28,140 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT ENGINE FORWARD PYLON YOKE LOWER FITTING CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED LEFT ENGINE FORWARD PYLON YOKE LOWER FITTING IAW EO EM-54MR-386. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,767 hrs · 28,057 cycles

ON FLIGHT 2920 THE CREW REPORTED THE FORWARD CABIN FLASHLIGHT CHARGE LIGHT BLINKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN FLASHLIGHT ASSEMBLY IAW EMB 145 CMM 25-60-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 29,074 hrs · 27,550 cycles

ON FLIGHT 3913 THE FLIGHT ATTENDANT NOTICED A "BURNING SMELL" BY MAIN CABIN DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND LIGHT SOCKET ON PASSENGER SIDEWALL LIGHT ASSEMBLY DS8411 BURNED. REPLACED WIRE HARNESS FROM BALLAST RT8500-231 TO LIGHT ASSYMBLY DS8410 AND DS8411 IAW STANDARD MAINTENANCE PRACTICES. PERFORMED OPERATIONAL TEST OF THE PASSENGER CABIN LIGHTS IAW EMB-145 AMM 33-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 25,670 hrs · 24,953 cycles

FOR FLIGHT 4007 MAINTENANCE FOUND THE AFT CABIN FLASHLIGHT HOLDER (CRADLE) TO BE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT HOLDER (CRADLE) IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 25,012 hrs · 24,424 cycles

ON FLIGHT 2720 THE CREW REPORTED THE MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED MAIN CABIN DOOR ROLLER IAW AMM 53-21-02 THE OPERATIONAL CHECK WAS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CHAFED (FUSELAGE) · airframe 24,876 hrs · 24,314 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT FUSELAGE SKIN CHAFED BETWEEN FRAMES 67-68 INSIDE PYLON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED CHAFE TO SKIN IN ACCORDANCE WITH ENGINEERING ORDER EM-53MR-1492. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CHAFED (FUSELAGE) · airframe 24,876 hrs · 24,314 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT FUSELAGE SKIN TO BE CHAFED BETWEEN FRAMES 67-68 INSIDE PYLON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED CHAFE TO SKIN IN ACCORDANCE WITH ENGINEERING ORDER EM-53MR-1492. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,876 hrs · 24,314 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 24-25. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED WITH A DOUBLER REPAIR IAW SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ATTACH ANGLE — CRACKED (STAB TO FUSELAGE) · airframe 24,876 hrs · 24,314 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT SIDE VERTICAL STABILIZER TO FUSELAGE FORWARD ATTACHED ANGLE TO BE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED ATTACH ANGLE AND REPLACED WITH A NEW ANGLE IAW ENGINEERING ORDER EM-53MR-1281. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 21,815 hrs · 21,619 cycles

ON FLIGHT 3570 CREW REPORTED ON PREFLIGHT FORWARD ZONE EMERGENCY LIGHTS NOT ON OVER FLIGHT ATTENDANT SEAT EXIT SIGN BELOW COCKPIT FLOOR, AND EXIT SIGN-CEILING GALLEY EXIT SIGN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 BATTERY PACK IAW EMB 145 AMM 33-50-04-000-801-A, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE SWITCH — LEAKING (HYDRAULIC SYSTEM) · airframe 20,412 hrs · 20,453 cycles

ON FLIGHT 4371, CREW REPORTED LOSS OF HYDRAULIC FLUID THEN HYD SYSTEM 2 FAILED. CREW DECLARED EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RT PRESSURE SWITCH LEAKING. REMOVED AND REPLACED PRESSURE SWITCH IAW EMB145 32-41-04. ALSO REMOVED AND REPLACED NR 2 ENGINE DRIVEN PUMP IAW EMB-145 29-10-03. OPERATIONAL CHECK GOOD AT THIS TIME. AIRCRAFT RETURN TO SERVICE.

Part: LEVER — INOPERATIVE (COCKPIT) · airframe 20,156 hrs · 20,199 cycles

ON FLIGHT 4501 CREW REPORTED WHILE ON CLIMB-OUT LANDING/LEVER DISAGREE ON EICAS. GEAR WILL NOT RETRACT. CYCLED GEAR LEVER AND CONFIRMED 3 GREEN DOWN LIGHT. RETURN TO ORD. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LANDING GEAR SELECTOR LEVER IAW EMB AMM TASK 32-32-02-000-800A AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,212 hrs · 19,977 cycles

DURING MBV INSPECTION, FOUND SERVICE DOOR CENTER SILL CORRODED. REPLACED SERVICE DOOR SILL IAW EMB SRM 51-40-02. A/C RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 20,212 hrs · 19,977 cycles

DURING MBV INSPECTION, FOUND LT OMEGA BEAM CORRODED AT FR 20 AT CARBON CROSS MEMBER AREA. INSTALLED NEW REPAIR DOUBLERS FROM PREVIOUS REPAIR IAW SRM 53-00-12. A/C WAS RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,212 hrs · 19,977 cycles

DURING HEAVY CHECK, FLOORBEAM BETWEEN FRAME 24 AND FRAME 29, AT FRAME 25, WAS FOUND TO HAVE CORROSION. FLOORBEAM WAS REPAIRED IAW SRM 53-22-10. AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — DAMAGED (NLG WOW) · airframe 19,830 hrs · 19,870 cycles

ON FLIGHT 4370, CREW REPORTED LANDING GEAR DID NOT RETRACT AFTER TAKEOFF WITH ASSOCIATED AIR GROUND CAUTION MESSAGE ON EICAS. AIRCRAFT REMOVED FROM SERVICE. PERFORMED GVI AND CONTINUITY TEST OF THE NLG WOW PROX SWITCH HARNESS FROM PIN C TO HARNESS SHIELDING AND VOLTAGE READINGS. CONTINUITY AND VOLTAGE READINGS NORMAL. NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK OF AIR/GROUND SYSTEM IAW AE MTX WC NR 32-700-16. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: GROUND STUD — SHORTED (SPOILERS) · airframe 19,542 hrs · 19,630 cycles

ON TAKEOFF ROLL AT 10 KTS IN THRUST SET POSITION GOT NO TAKEOFF CONFIGURING EICAS SPOILER SHOWED OPEN. GOT NO SPOILER AURAL WARNING. ABORTED TAKEOFF AND SPOILER CLOSED AT IDLE THRUST. FOUND GROUND BLOCKS GS0163 DC AND GS 0186 DC TO HAVE HIGH OHMS TO GROUND. CLEANED AND REINSTALLED PER WM 20-10-01. SPOILERS OPS CHECK GOOD PER EMB 145 AMM 27-63-01. BOTH STATIC AND DURING GROUND TAXI CHECK. AIRCRAFT RETURNED TO SERVICE.

Part: NOZZLE — DIRTY (ENGINE)

WHEN THRUST LEVERS PUSHED FWD, SMOKE FILLED COCKPIT AND WHEN THRUST LEVERS PULLED BACK SMOKE STARTED TO DISSIPATE. AIRCRAFT RETURNED TO SERVICE. CLEANED EXHAUST NOZZLE NR 1. OPERATIONAL CHECK GOOD IAW EMB 145 AMM 36-10-00 AIRCRAFT RETURNED TO SERVICE

Part: ENGINE — SMOKE (NR 1) · airframe 19,542 hrs · 19,630 cycles

RETURN TO GATE DUE TO SMOKE IN COCKPIT. REMOVED AND REPLACED NR 1 ENG IAW W/C 71-000-00. OPS CHECKS, LEAK CHECK GOOD. AIRCRAFT RETURN TO SERVICE.

Part: SPOILER SYS — UNWANTED DEPLOY · airframe 19,527 hrs · 19,617 cycles

CREW ABORTED T/O AT 30 KNTS FOR UNCOMMENTED SPOILER DEPLOYMENT.

Part: GROUND STUD — LOOSE · airframe 19,527 hrs · 19,617 cycles

CREW ABORTED T/O AT 30 KNTS FOR UNCOMMANDED SPOILER DEPLOYMENT. TROUBLESHOT PER EMB 145FIM27-63-00. FOUND LOOSE GROUND STUD. TIGHTENED. GROUND STUD IAW EMB AMM 20-10-01. OPS CK GOOD OF SPOILER SYSTEM IAW AMM27-62-00. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — FAILED (ZONE 100) · airframe 18,710 hrs · 18,919 cycles

VIBRATION IN FLIGHT CONTROLS FELT THROUGH ELEVATOR AND FUSELAGE. REMOVED AND REPLACED LEFT RAM VALVE IAW EMB AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — LEAKING (LEFT) · airframe 18,632 hrs · 18,844 cycles

LAVATORY SMOKE ALARM GOING OFF INFLIGHT, NO SMOKE NOTED. REMOVED AND REPLACED NUMBER 1 ENGINE IAW AMERICAN EAGLE WORKCARD 72-000-00. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: BALLAST — DEFECTIVE (CABIN LIGHTS) · airframe 18,168 hrs · 18,400 cycles

FLIGHT ATTENDANT REPORTED A ELECTRICAL ODOR IN FRONT OF CABIN. REMOVED AND REPLACED GALLEY CEILING LIGHT BALLAST IAW EMB MM. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: BALLAST — BLOWN (CABIN LIGHT) · airframe 18,169 hrs · 18,400 cycles

FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL IN FRONT OF CABIN. REMOVED AND REPLACED GALLEY AREA CEILING LIGHT BALLAST IAW EMB AMM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DUCT — LEAKING (ZONE 400) · airframe 17,889 hrs · 18,126 cycles

RECEIVED LAVATORY SMOKE INDICATION WITH BLEEDS ON, PACKS CLOSED AND APU OFF, SMOKE WAS NOTICED FROM PSU GASPERS. CIRCUIT BREAKERS PULLED PER AIRCRAFT OPERATING MANUAL AND SMOKE AND SMELL DISAPPEARED. RETURNED TO JFK. REMOVED AND REPLACED RIGHT HAND ENGINE DUCT ASSEMBLY IAW EMB AMM 36-11-00. OPERATIONAL CHECK GOOD WITH NO SMOKE NOTED - PERFORMED FUNCTIONAL CHECK FLIGHT. RETURNED AIRCRAFT TO SERVICE

Part: FLOOR SUPPORT — CORRODED (FUSLEAGE) · airframe 20,212 hrs · 19,977 cycles

DURING MBV INSPECTION, FOUND UPPER FLOOR SUPPORT FRAME 24 RT SIDE CORRODED. INSTALLED NEW UPPER FLOOR SUPPORT BTW FR 23 AND 24 IAW SRM 51-40-02. A/C WAS RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 17,552 hrs · 17,806 cycles

EMERGENCY LIGHTS NOT ARMED AND ELECTRICAL ABNORMAL MESSAGE, AIRCRAFT RETURNED TO MQT. REMOVED AND REPLACED NUMBER 2 BATTERY SWITCH IAW EMB AMM 24-31-00. OPERATIONAL CHECK GOOD - PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED - RETURNED AIRCRAFT TO SERVICE.

Part: BUSHING — WORN (RUDDER)

CLIMBING THROUGH 27,000 FT AT .56 MACH VIBRATION IN YOKE WITH OR WITH OUT AUTOPILOT ENGAGED. THROUGH 16,000 FEET AT 250KTS THE VIBRATION SUBSIDED DURING DESCENT. THE VIBRATION SEEMED TO BE ONLY FORWARD TO AFT ON YOKE. CREW TRIED DIFFERENT PITCH SETTINGS WITH NO CHANGE. COMPLIED WITH WORK CARD 12-200-0, VIBRATION INSPECTION PROCEDURE AND FOUND RUDDER 1 LOWER ATTACH FITTING WORN AND RUDDER 2 UPPER BUSHING WORN. RAI FITTING WITH SERVICEABLE FITTINGS IAW EMB 145 AMM 55-31-01. OPS CHECK GOOD. FCF FOUND SATISFACTORY. TRIAD RELEASED AND AIRCRAFT RETURNED TO SERVICE. (M)

Part: BUSHING — WORN (RUDDER)

DURING CLIMB, VIBRATION FELT IN YOKE. REPLACED RUDDER BUSHINGS. TRIAD APPROVED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PRESSURE SENSOR — RUPTURED (NR 1 BRAKE)

IN FLIGHT NR 1 HYDRAULIC QUANTITY LOW LIGHT CAME ON. QUANTITY CONTINUED TO DROP AND PRESSURE STARTED TO FLUXUATE 2900 TO 2500. ELECTED TO DIVERT, DECLARED EMERGENCY AND LANDED. NO OTHER PROBLEMS NOTED. FOUND NR 1 BRAKE PRESSURE SENSOR RUPTURED AND REPLACED. AIRCRAFT RETURNED TO SERVICE. (K)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2

DURING HMBV INSPECTION, FOUND SKIN CORRODED AROUND TOILET DISCHARGE VALVE. INSTALLED REPAIR DOUBLER AROUND TOILET DISCHARGE VALVE IAW SRM. AC RETURNED TO SERVICE. (K)

Part: SILL — CORRODED (GALLEY) · corrosion level 2

DURING HMBV INSPECTION FOUND FORWARD SERVICE DOOR SILL HAS CORROSION AROUND SCREW HOLES. REPLACED FORWARD SILL IAW SRM. AC RETURNED TO SERVICE. (K)

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2

DURING HMBV INSPECTION FOUND CENTER OMEGA BEAM STRAP IN LAVATORY AREA HAS CORROSION. INSTALLED EXTERNAL DOUBLER IAW SRM. AC RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

DURING IMBV INSPECTION FOUND LT OB NR 4 SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW AMM. AC RETURNED TO SERVICE. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING HMBV INSPECTION FOUND TOP OF CENTER FLOORBEAM AT FRAME 19A CORRODED. REPAIRED FLOORBEAM WITH DOUBLER IAW SRM. AC RETURNED TO SERVICE. (K)

Part: SILL — CORRODED (CABIN) · corrosion level 2

DURING HMBV INSPECTION FOUND SERVICE DOOR AFT SILL PLATE CORRODED. REPLACED SILL PLATE IAW SRM. RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

DURING IMBV INSPECTION FOUND RT OB NR2 SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW AMM. AC RETURNED TO SERVICE. (K)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

THREE FORWARD EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WHEN TURNED ON. REMOVED AND REPLACED FORWARD EMERGENCY BATTERY CHARGER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STARTER GEN — MALFUNCTIONED (APU) · airframe 12,430 hrs · 13,060 cycles

CREW REPORTED ELECTRICAL SMELL IN COCKPIT AFTER ATTEMPTED APU START WHICH FAILED. INSPECTED APU AND FOUND STARTER GENERATOR TO BE MAKING LOUD NOISES AND SPARKING ON START UP. MAINTENANCE REMOVED AND REPLACED THE STARTER/GENERATOR IAW MM. GROUND RUN WAS COMPLIED WITH AND NO SMELL NOTED. (SW21200501803) (K)

Part: BUSHING — WORN (HORIZONTAL STAB)

DURING SCHEDULED MAINTENANCE, FOUND HORIZONTAL STAB HAS PLAY AT RIGHT AFT HINGE MOUNT PIN. REPAIRED HORIZONTAL STAB REAR MOUNT BUSHING IAW EMB 145 SRM 55-10-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PRESSURE SWITCH — INOPERATIVE (RUDDER)

DURING CRUISE FILGHT CRWE REPORTED THE RUDDER 1/2 TO BE INOPERATIVE. AIRCRAFT WAS DIVERTED TO STL AND LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE NR 2 RUDDER PRESSURE SWITCH IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: STRINGER — CRACKED (FUSELAGE)

ABI - FOUND PIT ON STRINGER 4R BETWEEN FRAMES 27 AND 28 TO HAVE A .1875 INCH CRACK ON OUTER EDGE. REMOVED DAMAGE BY CUTOUT. FABRICATED A DOUBLER AND FILLER. REPAIR DONE IAW EMB145 SRM 145/1142, CHAPTER 53, REV 18 53-22-01, GST 2136/02, AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING INSPECTION FOUND STRINGER 19R CHAFED. BLENDED CHAFE, PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A DOUBLER ANGLE, AND TWO SHIMS. REPAIR DONE IAW EMB-145 SRM 145/1142, CHAPTER 53, REV 18, 53-24-02 AND STANDARD SRM PRACTICES. (M)

Part: SKIN — DENTED (PAX DOOR)

ABI - MAIN DOOR HAS ONE DENT AT APPROX 4 INCHES FORWARD OF AFT LOWER CORNER ON EDGE OF SKIN, 9 INCH BY .033 INCH. (M)

Part: SUPPORT — CRACKED (TAIL)

ABI - FOUND PULLEY SUPPORT ANGLE IS CRACKED ON LEFT END BETWEEN VERTICAL SPARS 3 AND AUX SPAR 52 PERCENT AND BELOW ZV 3145.0 MM. (M)

Part: SKIN — DENTED (APU COWLING)

ABI - FOUND TWO PROTRUSION ON LEFT SIDE OF APU COWL. (M)

Part: SKIN — DENTED (PAX DOOR)

ABI - FOUND PASSENGER DOOR HAS DENT 10 INCHES FROM TOP AND 2.5 INCHES FROM LEADING EDGE 2 INCHES BY 3 INCHES BY .021 INCH. (M)

Part: SKIN — DENTED (FUSELAGE)

ABI - TWO PROTRUSIONS BETWEEN FRAME 9 AND 10 AND STRINGERS 18L AND 20L, .3 BY .3 BY .001, AND ONE DENT .7 BY .5 BY .002. PERFORMED EDDY CURRENT INSPECTION AND FOUND NO DEFECTS. DENT FOUND TO BE WITH IN EMB145 SRM 53-12-01. (M)

Part: SKIN — DENTED (FUSELAGE)

ABI - DENT BETWEEN FRAMES 20 AND 21 AND STRINGERS 3L AND 4L, 1.6 BY 3 BY .052. PERFORMED EDDY CURRENT INSPECTION, NO DEFECTS. DENT FOUND TO BE WITHIN EMB 145 SRM 53-21-10. (M)

Part: SKIN — DENTED (FUSELAGE)

ABI - THREE DENTS BETWEEN FRAMES 19 AND 20, STRINGERS 11L AND 12L. (M)

Part: SKIN — SCRATCHED (FUSELAGE)

ABI - FOUND SCRATCH BETWEEN FRAMES 29 AND 30, STRINGERS 21L AND 21R. BLENDED AREA, PERFORMED EDDY CURRENT AND THICKNESS, NO DEFECTS. SCRATCH FOUND TO BE WITHIN EMB 145 SRM 53-22-10 TABLE 101 LIMITS. (M)

Part: SKIN — DAMAGED (FUSELAGE)

ABI - FOUND DENTS/SCRAPE BETWEEN FRAMES 19 AND 20 AND STRINGERS 15L AND 16L. BLENDED AREA PERFORMED EDDY CURRENT AND THICKNESS, NO DEFECTS. DENT FOUND TO BE WITHIN EMB 145 SRM 53-21-10 TABLES 101 AND 102 LIMITS. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING IMBV INSPECTION MAINTENANCE, FOUND THE CARGO DOOR LOWER SILL CORRODED. REMOVED CORRODED SILL BEAM. INSTALLED NEW BEAM IAW EMB145 SRM 145/1142, CHAPTER 51, REV 18 51-20-01, 02, 03, 04, AND 06 CPM 51-21-04 AND 05 AND STANDARD SRM PRACTICES. (M)

Part: ENGINE — SHUTDOWN (NR 1)

TYS - FLT 3718 - NR 1 ENGINE AUTO SHUTDOWN CLIMBING 11,000 FEET. ENGINE SURGED THEN SHUTDOWN WITH SMELL IN CABIN OF BURNING OIL. RAI, NR 1 ENGINE. (M)

Part: LIGHT — FAILED (CABIN)

XNA - FLT 3687 - CREW REPORTED AISLE FLOOR LIGHTING STRIP BETWEEN ROWS 14 AND 16 INOPERATIVE. REMOVED AND REPLACED FLOOR LIGHTING STRIP BETWEEN ROWS 14 AND 16 IAW AMM. OPS CHECK GOOD. (M)

Part: A/C PACK — CONTAMINATED (A/C BAY)

ORD - FLT 4256 - FOUND CREW REPORTED SMOKE IN CABIN AFTER TAKEOFF WHEN TURNING ON BLEED SYSTEM. FOUND PACKS TO BE SATURATED WITH GLYCOL. CLEANED LINES IAW AMM. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

ORD - FLT 4110 - EMERGENCY FLOOR LIGHTS INOPERATIVE AT SECTION 2 AND 3. REMOVED AND REPLACED EMERGENCY POWER SUPPLY. OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - FLT 4211 - FIRST TWO CABIN EMERGENCY FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED ONE EMERGENCY BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (X)