N905JH

Part: ICU — FAULTED (ZONE 200) · airframe 45,554 hrs · 42,195 cycles

AFTER T/O EXTREME STATIC ON COMM AND INTERPHONES. ON COMM 1, 2 & 3. STATIC CLEARED ON GROUND. R & R #100 INTEGRATED COMMUNICATIONS UNIT ITW AMM 23-00-01. OPS CHECK GOOD. A/C OK FOR SERVICE AT THIS TIME

Part: CABIN PRESSURE — FAULTED (ZONE 100) · airframe 45,528 hrs · 42,164 cycles

CABIN ALTITUDE WAS AT 300 CABIN RATE DIDNT INCREASE IN CLIMB IN AUTO MODE. PERFORMED FUNCTIONAL TEST OF PRESSURE CONTROL SYSTEM IN AUTOMATIC MODE PER AMM 21-31-00. CHECKED GOOD, NO DEFECTS NOTED AT THIS TIME. CLEAR MEL 21-12-3. PRESS CONTROL AUTO AND MANUAL

Part: UNKNOWN — ODOR (CABIN) · airframe 45,360 hrs · 41,953 cycles

IN FLIGHT HAD A BURNING PLASTIC SMELL FOR ABOUT 4 MINUTES THEN DISSAPATED. PERFORMED GVI OF ICU PANEL WIRING AS REQ'D. NO DEFECTS NOTED OR SMELL OF BURNING PLASTIC PRESENT AT THIS TIME. OK FOR SERVICE.

Part: CONDENSER — FAILED (NR 1 A/C PACK) · airframe 45,071 hrs · 41,593 cycles

AFTER T/O SMOKE IN FLT DECK WITH PACK 1 SELECTED, SMOKE CLEARED WHEN PACK 1 DESELECTED AIR CONDITIONING PACKS R & R HEAT EXCHANGER,CONDENSOR MIXER, AND WATER COLLECTOR. OPS CHECK GOOD WITH APU AND ENGINES PACK 1 SELECTED NO SMOKE IN COCKPIT.

Part: A/C PACK — OVERHEATED (NR 1) · airframe 45,070 hrs · 41,591 cycles

SMOKE IN RHE CABIN DURING TAKEOFF. PACK 1 OVERHEAT MSG NOTICED AFTER LANDING. FACT 11AUG25 00:37 CLT RAN PACKS FOUND PACK 1 TO CONSTANTLY OVERHEAT AFTER 30 SECS AND COCKPIT RECIRC SMOKING WHILE TRYING TO RUN PACK 1 SOUNDS VERY WEAK AND ONLY BLOWS SUPER HOT AIR. REF LP 330173 SEQ 3 AND 330174 SEQ 1 FOR PACK 1 AND RECIRC 1 MEL. RAN PACK 2 AND CABIN RECIRC FAN NO SMOKE OR DEFECTS NOTED. FOUND COCKPIT RECIRC FAN TO BE PULLING INSUFFICIENT VOLTAGE AND SMOKING WHEN TRYING TO RUN FAN. R/R'D COCKPIT RECIRC FAN IRT AMM 21-24-01, OPS CHECK GOOD. A/C GOOD FOR SERVICE AT THIS TIME.

Part: ACM — ABNORMAL (ZONE 100) · airframe 45,066 hrs · 41,585 cycles

BLACK SMOKE REPORTED IN CABIN AFTER GRINDING SOUND COMING FROM NR 2 ENG. BURNT RUBBER SMELL IN FLIGHT DECK. OXYGEN MASKS IN FLIGHT DECK DEPLOYED. FOUND ACM TO BE FAULTY. R & R #100 ACM IAW AMM 21-51-03. AC OK FOR SERVICE

Part: DAU — FAILED (ZONE 200)

AT 33000 FEET UNTIL 20000 ELECTRICAL BURNING FUMES CAUSING LIGHT HEADEDNESS IN FLIGHT DECK. INSPECTED AND FOUND NR 200 DAU INOPERATIVE. R & R NR 200 DAU IAW AMM 31-41-01-000-801-A AND 31-41-01-400-801-A. OPS CHECK GOOD. NO SMELLS NOTED AT THIS TIME. OK FOR SERVICE.

Part: TRANSMISSION — ABNORMAL (FLAP SYS) · airframe 44,932 hrs · 41,430 cycles

FLAP LOW SPEED DISPLAYED AFTER TAKE OFF. CW MX PROCEDURE FOR FLAP CHANNEL 2 FACT 20JUL25 06:15 SBY T/S USING FIM 27-51-00-810-801 R&R'D LH FLAP TRANSMISSION BRAKE IAW AMM 27-51-01. OPS CHECK GOOD

Part: ELEC CONNECTOR — LOOSE (PROXIMITY SWITCH) · airframe 44,821 hrs · 41,290 cycles

LOW SPEED REJECTED TAKEOFF AT 20 KNOTS DUE TO OPEN SPOILER INDICATION ON EICAS AND UNCOMMANDED PITCH TRIM MOVEMENT, UP 9 DOWN 4 FACT 23JUN25 23:04 CLT INSPECTED SPOILER SYSTEM AND FOUND LH OB SPOILER PROX SWITCH CONNECTOR PLUG LOOSE AND WOULD NOT STAY TIGHTENED. R&R'D CANNON PLUG & BACKSHELL IRT EMB SWPM 20-50-00. ALSO R&R'D LH OB SPOILER PROXIMITY SENSOR IRT EMB AMM 27-63-04. OPS CHECK GOOD, AC OK FOR SERVICE

Part: SENSOR — FAULTED (TAT) · airframe 44,051 hrs · 40,455 cycles

TAT 1 HT INOP MSG DISPLAYED AFTER TAKEOFF EXTINGUISHED AFTER LANDING. FACT 18FEB25 06:55 PHL T/S USIING FIM TASK 30-33-00-810-801-A FROM STEP 1-8 FAILURE OF TAT SENSOR 1 (PROBE). R/R TAT SENSOR 1 PROBE IAW AMM 34-15-03. OPS CHECK GOOD ALL OK FOR SERVICE.

Part: LINE — DAMAGED (BLEED SERVO) · airframe 43,761 hrs · 40,141 cycles

DURING CLIMB INTO ICING CON. BLEED 2 OVERTEMP. FACT 26DEC24 07:02 MDT REMOVED PRECOOLER PANELS FOR INSP, FOUND HOLE IN RH BLEED AIR SERVO LINE GOING TO FAN AIR VALVE. RR SERVO LINE SECTION IRT AMM 36-11-11. OPS AND LEAK CHK GOOD. REINSTALLED ALL REMOVED PANELS. OK FOR SERVICE AT THIS TIME.

Part: SENSOR — FAULTED (ZONE 400) · airframe 43,740 hrs · 40,115 cycles

ON CLIMB OUT BLEED 2 OVERTEMP DISPLAYED WHENEVER ENGINE,WING, STAB OPEN LIGHT ON PB. FOLLOWED BY WING A/I FAIL IN ICING CONDITION. REMOVED AND REPLACED INLET AND OUTLET BLEED TEMP SENSORS IAW AMM 36-20-01. PERFORMED AMM 36-00-00. OPS AND LEAK CHECK GOOD. A/C OK FOR SERVICE AT THIS TIME

Part: TRANSMISSION — FAILED (ZONE 500 FLAPS) · airframe 43,448 hrs · 39,812 cycles

FLAP FAIL AT 4 DEG. FLAPS STUCK 4 DEGS. L/H TRANSMISSION FAIL. FACT 27OCT24 06:34 MDT T/S IRT FIM TASK 27-51-00-810-816A. INSPECTED LH FLAP FLEXIBLE SHAFTS IRT AMM 27-51-00. NO DEFECTS NOTED R/R'D L/H FLAP TRANSMISSION BRAKE IRT AMM 27-51-01. OPS CHECK GOOD. RAN FLAPS THROUGH MULTIPLE CYCLES. NO DEFECTS NOTED. OK FOR SERVICE AT THIS TIME.

Part: TRANSMISSION — FAILED (TE FLAPS) · airframe 43,407 hrs · 39,770 cycles

AFTER T/O AND FLAP RETRACTION RESULTED IN FLAP FAIL MESSAGE ON EICAS AT 4 DEGREES WITH HANDLE IN UP POSITION, CMC MESSAGE OF L/H FLAP TRANSMISSION FAIL FACT 16OCT24 14:44 CLT PERFORMED FIM TASK 27-51-00-810-816-A BLOCKS 1 TO 12 FIM TASK INDICATED TRANSITORY CONDITION. PER DIRECTIVE OF MOC, R&R'D L/H FLAP VELOCITY SENSOR IAW AMM 27-51-12 FLAP CONTROL SYSTEM OPS CHECK GOOD. OK FOR SERVICE

Part: INDICATION SYS — FALSE INDICATION (TE FLAP)

FLAPS 9 DEGRESS IAS 270 FOR FIVE MINUTES. PERFORMED INSPECTION OF THE LH WING IB/OB FLAP TRACK IRT AMM 05-50-07 TABLE 603 NO DEFECTS NOTED PERFORMED INSPECTION OF THE FLAP INBD AND OUTBD. FLAP TRACKS ON THE RH FLAPS IRT E145 AMM 05-50-07 TABLE 603 NO DEFECTS NOTED.

Part: LAMP — INOPERATIVE (MAIN CABIN DOOR) · airframe 40,775 hrs · 36,891 cycles

PHOTOLUMINESCNET LIGHT INOP MAIN CABIN DOOR LINER, EMERGENCY LIGHT ASSY, DAMAGED-C/A-RAR MAIN CABIN DOOR LINER, EMERGENCY LIGHT ASSY OPC GOOD IAW AMM 25-23-04

Part: LAMP — INOPERATIVE (MAIN) · airframe 39,831 hrs · 35,824 cycles

MAIN DOOR EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPC GOOD. END.

Part: NONE — NONE · airframe 38,921 hrs · 34,781 cycles

LAVATORY EMERGENCY FLASHLIGHT HOLDER BROKEN-C/A-REMOVED AND REPLACED BROKEN EMERGENCY FLASHLIGHT HOLDER AT LAVATORY IAW EMB 145 AMM 33-50-16 AND ETN-EM-33-059 R1. OPC GOOD.

Part: NONE — NONE · airframe 38,545 hrs · 34,341 cycles

AFT FLASHLIGHT INOP-C/A-RAR AFT FLASHLIGHT IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPC GOOD. END.

Part: NONE — NONE · airframe 38,478 hrs · 34,268 cycles

ON APPROACH ICE COND - A/I INOP MESSAGE DISPLAYED DECLARED EMERGENCY-C/A-TROUBLESHOOTED IAW FIM TASK 30-80-00-810-801-A PERFORMED OPERATIONAL CHECK IAW AMM 30-00-00-700-803-A/500 FOUND TRANSITORY CONDITION OF A/I SYS NO DEFECTS NOTED AT THIS TIME.

Part: NONE — NONE · airframe 38,425 hrs · 34,206 cycles

DURING PS-1 CHECK FOUND LH OVER WING EMERGENCY LIGHT INOP-C/A-RAR L/H OVERWING EMERGENCY LIGHT ASSY. IAW EMB-145MM 33-50-10 - OPS CHECK GOOD

Part: NONE — NONE · airframe 38,231 hrs · 33,996 cycles

DURING PS-1 CHECK FOUND EMERGENCY LIGHT LEFT SIDE EXTERIOR AFT LIGHT INOP .-C/A-R&R EMERGENCY LIGHTI IAW AMM 33-50-10 OP'S GOOD NO OTHERE DEFECT NOTED AT THIS TIME

Part: NONE — NONE · airframe 38,212 hrs · 33,976 cycles

FLT ENCOUNTERED SVR ICING FROZEN PITOT TUBES. AT 36,000 FEET, AIRCRAFT ENCOUNTERED SEVERE ICING. CAPTAIN'S IAS COMPARATOR ILLUMINATED ON CA'S PFD. CA'S AIRSPEED STAGNANT AND INITIALLY READ 9 KTS SLOWER. FO AND STBY AIRSPEED CONSISTANT. CA SIRSPEEED LOWER AS WE DESCENDED.-C/A-ADC SYSTEM OPS GOOD. IAW AMM 34-15-00-200-80. PITOT/STATIC SYSTEM LEAK CHECK GOOD IAW AMM 34-15-00-790-802/803. DURING LEAK CHECK STOPPED EVERY 50 FT TO COMPARE AIRSPEED INDICATIONS. CA AND FO AIRSPEED WERE THE SAME UP TO 300 KNOTS WITH AND WITHOUT ALTITUDE ADDED. PITOT TUBE AND STATIC PORT HEATING OPC GOOD IAW AMM 30-31-00-700-801.

Part: A/C PACK — ODOR (NR 1) · airframe 37,344 hrs · 32,993 cycles

SMOKE IN CABIN/COCKPIT - FUMES IN COCKPIT AFTER TAKEOFF DECLARED EMEREGNCY-C/A-PERFORMED ENG ODOR EVENT TROUBLESHOOT IAW ETN-EM-72-034. FOUND FUMES TO BE FROM PACK 1. SEE ITEM 3 THIS LOG PAGE FOR DEFERAL OF PACK 1

Part: LENS — BROKEN (EXTERIOR LIGHT) · airframe 37,288 hrs · 32,931 cycles

FOUND SIDE HINGED MIAN DOOR EXTERNAL EMERGENCY LIGHT LENS BROKEN-C/A-RAR SIDE HINGED MAIN DOOR EXTERNAL EMERGENCY LIGHT LENS IN REF WITH EMB 145 AMM 33-50-10.

Part: FITTING — CHAFED (LT AILERON) · airframe 37,203 hrs · 32,849 cycles

LEFT AILERON FITTING FOR DAMPER ATTACH IS CHAFED.-C/A-RAR'D LH AILERON FITTING IAW EO# EM-27MR-112.

Part: BUSHING — MIGRATED (RT AILERON PCA) · airframe 37,203 hrs · 32,849 cycles

RIGHT AILERON PCA FITTING HAS MIGRATING BUSHINGS. -C/A-RAR RH AILERON PCA FITTING IAW EO-EM-27MR-112.

Part: DOUBLER — CORRODED (COCKPIT FLOOR) · airframe 37,203 hrs · 32,849 cycles

SSI 53-10-27 DOUBLER UNDER CAPT RT SEAT TRACK IS CORRODED AND GOUGED (LEVEL 1 CORROSION)-C/A-REPAIRED DAMAGE IAW ERS-EM-5300-4282.

Part: FRAME — CHAFED (FUSELAGE) · airframe 37,203 hrs · 32,849 cycles

FRAME 15 HAS A CHAFE AT STR 2R. -C/A-C/W REPAIR AT FRAME 15 AND STR 2R IAW ERS-EM-53MR-4279.

Part: DOOR SILL — CORRODED (FWD SERVICE DOOR) · airframe 37,203 hrs · 32,849 cycles

CPCP SSI ITEM. FWD SERVICE DOOR SILL IS CORRODED FROM FR 18 TO FR 20 AT THE FLOOR LEVEL. (LEVEL 1 CORROSION)-C/A-INSTALLED NEW FWD SERVICE DOOR SILL IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 37,203 hrs · 32,849 cycles

CARGO DOOR SILL AREA IS CORRODED BETWEEN FRAMES 60-64. (LEVEL1 CORROSION)-C/A-REPLACED CARGO SILL IAW SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,203 hrs · 32,849 cycles

LEFT FUSELAGE SKIN HAS A CRACK JUST AFT OF FRAME 75 BETWEEN STRS 1L AND 2L.(CRACK APROX 1/2 " LONG )-C/A-REPAIRED LT FUSELAGE SKIN AT FRAME 75 IAW EMB-145 SRM CH. 53-31-01.

Part: SKIN — CRACKED (FRAME 75) · airframe 37,203 hrs · 32,849 cycles

R/H FUSELAGE SKIN HAS A CRACK JUST AFT OF FRAME 75 BETWEEN STRS 1R AND 2R.(CRACK APROX 1/2 " LONG )-C/A-REPAIRED R/H FUSELAGE SKIN AFT OF FRAME 75 BETWEEN STRS 1R AND 2R IAW SRM 53-31-01.

Part: LIGHT — BROKEN (CABIN) · airframe 37,203 hrs · 32,849 cycles

EXTRUSION FOR #6 AND #8 FLOOR EMERGENCY LIGHT STRIP IS BROKEN.-C/A-COMPLETE:RAR EXTRUSION IAW AMM 33-50-12.

Part: WIRE — EXPOSED (EMERGENCY LIGHT) · airframe 37,203 hrs · 32,849 cycles

#1 FLOOR EMERGENCY LIGHT STRIP WIRES (ON AIRCRAFT SIDE) ARE EXPOSED.-C/A-COMPLETE:REPLACED EXPOSED CONNECTOR IAW SWPM 20-21-00

Part: LIGHT — UNSECURE (CABIN) · airframe 37,203 hrs · 32,849 cycles

ALL BLACK ADHESIVE SPLICES BETWEEN FLOOR EMERGENCY LIGHT STRIPS REQUIRE REPLACEMENT.-C/A-COMPLETE:INSTALLED ALL SPLICES BETWEEN FLOOR EMERGENCY LIGHT STRIPS IAW AMM 33-50-12.

Part: APU — SMOKE · airframe 36,954 hrs · 32,600 cycles

DURING BOARDING A BUNCH OF SMOKE CAME INTO CABIN & FLIGHT DECK. APU FAIL CAUTION SHORTLY AFTER & IT SHUT ITSELF DOWN. APU WAS RUNNING WHEN ARRIVED AT AIRCRAFT. C/A: C/W WORKSCOPE, REF NRWC 905-ORD-05100,905-ORD-05101,AND 905-ORD-05104 REF NRWC 905-ORD-05098 FOR APU RAR, OPERATIONS CHECK LEAK CHECK GOOD. NO SMOKE OR ORDER NOTED IN CABIN OR FLIGHT DECK AT THIS TIME END.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 36,818 hrs · 32,486 cycles

FOUND FWD F/A FLASHLIGHT INOPERABLE DURING PS-2. C/A: R & R FWD F/A FLASHLIGHT, IAW AMM TASK 33-50-16. OPERATIONS CHECK GOOD.

Part: BULB — INOPERATIVE (EXTERIOR LIGHT) · airframe 36,753 hrs · 32,433 cycles

LT EXTERIOR EMERGENCY EXIT LIGHT OVER WING INOPERABLE. C/A: R & R LT EXTERIOR EMERGENCY EXIT LIGHT BULB, IAW EMB145 AMM TASK 33-50-10-400-801.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,520 hrs · 32,189 cycles

OVERWING EMERGENCY RT SIDE INOPERATIVE. R & R THE OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,520 hrs · 32,189 cycles

GALLEY SERVICE DOOR LOWER EMERGENCY MARKER AND FIRST EMERGENCY FLOOR STRIP DID NOT ILLUMINATE. R & R EMERGENCY LIGHT DC/AC INVERTER NR 2 IAW AMM 33-50-11 WITH WM 33-50-50. OPC GOOD IAW AMM 33-50-00-700-801-A. NO OTHER DEFECTS NOTED.

Part: PROXIMITY SENSOR — FAULTY (NLG) · airframe 36,436 hrs · 32,118 cycles

LG AIR/GND FAIL CAUTION MESSAGE DURING TAKEOFF LANDING GEAR LEVER LOCKED INTO DOWN POSITION AND GEAR WOULD NOT RETRACT. ALL INDICATIONS INDICATED DOWN AND LOCKED. RESTORED LATERAL PLAY IN NLG TRUNNION REPLACED NLG WOW PROX SENSOR AND HARNESS. REF NRWC 942-ORD-04796 THUR 942-ORD-04804 FOR WORK PREFORMED. REF LOG PAGE 4667438 ITEM NR 1 FOR FCF.

Part: PROXIMITY SWITCH — OUT OF ADJUST (NLG) · airframe 36,435 hrs · 32,117 cycles

LAND GEAR EICAS MSG, FLT DECLARED EMERGENCY. LG AIR/GND FAIL REPEAT WRITE-UP, TRANSFERRED TO NRWC 905-ORD-04793. SERVICED NOSE STRUT. PERFORMED OPS OF NOSE PROX SWITCH. PERFORMED PROX SWITCH CLEARANCE GAP ADJUSTMENT. PERFORMED RETRACTION AND EXTENSION OF LANDING GEAR. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,375 hrs · 32,056 cycles

L/H OVERWING EXTERIOR EMERGENCY LIGHT INOP.-C/A-REMOVED AND REPLACED L/H OVERWING EXTERIOR EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,825 hrs · 31,578 cycles

FOUND L/H WING EMERGENCY LIGHT INOP-C/A-RELAMPED L/H WING EMERGENCY LIGHT IAW EMB145 AMM 33-50-10. OPS CHECK GOOD

Part: MANIFOLD — FAILED (NR 1 HYD SYSTEM) · airframe 35,824 hrs · 31,577 cycles

HYD SYS 1 FAILED, HYD 1 LOW QTY, E1 HYD PUMP FAIL. EMERGENCY DECLARED. REMOVED AND REPLACED THE NR 1 HYD MANAFOLD IAW AMM 29-10-07, TEPS K-1 TO 8, OPS TESTED GOOD, NO LEAKS NOTED.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 35,405 hrs · 31,226 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED RH OVERWING EMERGENCY LIGHT ASSEMBLY IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,177 hrs · 31,009 cycles

PAX EMERGENCY GROUND ILLUMINATION LIGHT INOPERATIVE. INSPECTED AND CORRECTLY REASSEMBLED PAX EMERGENCY GROUND ILLUMINATION LIGHT ASSY IAW EMB 145 AMM 33-50-10, OPC GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,116 hrs · 30,958 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-06-000-801-A, AND 33-50-06-400-801-A. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,995 hrs · 30,860 cycles

ROW 17 AISLE EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED ROW 17 AISLE EMERGENCY LIGHT LAMP. OPS CHECK GOOD. NO FURTHER DEFECTS FOUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,882 hrs · 30,758 cycles

MAIN DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD, NO DEFECTS NOTED AT THIS TIME. END.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,040 hrs · 29,928 cycles

PAX DOOR EMERGENCY LIGHT INOP. PAX DOOR EMERGENCY LIGHT LAMP REMOVED AND REPLACED IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,708 hrs · 29,570 cycles

RT EXTERIOR OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RT EXTERIOR OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD.

Part: LIGHT — BROKEN (RT OVERWING) · airframe 33,477 hrs · 29,299 cycles

TDMI 905T3354 PERFORME PERMANENT REPAIR OF RH OVERWING EMERGENCY LIGHT N/P BROKEN-C/A-RAR RH OVERWING EMEGENCY LIGHT ASSEMBLY IAW ERS-EM-33DF-024 AND EMB145 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: LIGHT — BROKEN (RT OVERWING) · airframe 33,472 hrs · 29,291 cycles

TDMI 905T3354 C/W REINSP OF RH OVERWING EMERGENCY LIGHT N/P BROKEN PER ERS-EM-33DF-024 PTB-C/A-PERFORMED GVI OF SPEED TAPE ON RH OVERWING EMERGENCY LIGHT IAW ERS-EM-33DF-024 NO DEFECTS NOTED TDMI REMAINS OPEN

Part: LIGHT — INOPERATIVE (ROW 12) · airframe 33,460 hrs · 29,275 cycles

ROW 12 CEILING EMERGENCY LT INOP-C/A-RAR ROW 12 CEILING EMERGENCY LT IAW 33-50-08-000-801-A AND 33-50-08-400-801-A OPS CHECK GOOD END

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 32,906 hrs · 28,694 cycles

AFT CABIN FLASHLIGHT CRADLE CRACKED-C/A-REMOVED AND REPLACED AFT CABIN FLASHLIGHT CRADLE BASE IAW GENERAL MAINTENANCE KNOWLEDGE OPS CHECK GOOD AT THIS TIME END

Part: RIB — DAMAGED (RT TE FLAP) · airframe 32,559 hrs · 28,363 cycles

RIGHT OTBD FLAP, OTBD ROLLER BUSHING BORE WAS SCORED. REMOVED AND REPLACED THE RT RIB 19 IAW ERS-EM-57MR-1001 R1.

Part: PAN — CRACKED (FUSELAGE) · airframe 32,559 hrs · 28,363 cycles

FWD AVIONICS BAY FLOOR PAN IS CRACKED AT FRAME 5 CROSSBEAM. (CROSSBEAM JUST AFT OF THE NLG UPLOCK BOX.) REPAIRED FWD AVIONICS BAY FLOOR PAN AT FRAME 5 CROSSBEAM IAW SRM 53-11-10 AND ERS-EM-5300-3340.

Part: FITTING — WORN (LT AILERON) · airframe 32,559 hrs · 28,363 cycles

LT AILERON DAMPER FITTING HAS WORN BORES / NICKS AND GOUGES. REMOVED AND REPLACED LT AILERON DAMPER FITTING IAW EO EM-27MR-112.

Part: BUSHING — MIGRATED (LT AILERON) · airframe 32,559 hrs · 28,363 cycles

LT AILERON, PCU FITTING, OUTBOARD HAT BUSHING IS MIGRATED. REMOVED AND REPLACED AILERON PCU FITTING IAW EO EM-27MR-112.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 32,559 hrs · 28,363 cycles

CARGO DOOR FUSELAGE FWD ANGLE SUPPORT HAS AREAS OF CORROSION BOTTOM AREA. REPAIRED CARGO DOOR FUSELAGE FWD ANGLE SUPPORT IAW SRM 53-31-04-RE.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 32,559 hrs · 28,363 cycles

CARGO DOOR SILL HAS AREAS OF CORROSION. REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02.

Part: LIGHT — DAMAGED (CABIN) · airframe 32,559 hrs · 28,363 cycles

CABIN FLOOR LT #4 EMERGENCY LIGHT STRIP DAMAGED AT AFT END. C/A-COMPLETE:INSTALLED EXISTING LIGHT STRIP IN NEW EXTRUSION IAW 33-50-12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 32,559 hrs · 28,363 cycles

CENTER OMEGA BEAM HAS SPOTS OF CORROSION AT FRAMES 27 AND 28. (MARKED IN RED)-C/A-COMPLETE:REPAIRED CENTER OMEGA BEAM AT FRAMES 27 AND 28 IAW SRM 53-22-10.

Part: CHANNEL — DAMAGED (FUSELAGE) · airframe 32,559 hrs · 28,363 cycles

CENTER HAT BEAM HAS AN ELONGATED NUT PLATE HOLE AFT OF FRAME 59. REPAIRED CENTER HAT BEAM IAW SRM 53-24-10.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 32,559 hrs · 28,363 cycles

CENTER CROSS BEAM BETWEEN FRAMES 24/25 IS CORRODED. C/A-COMPLETE:REPAIRED CENTER CROSS BEAM BETWEEN FRAMES 24/25 IAW ETN-EM-53-241.

Part: LIGHT — DAMAGED (CABIN) · airframe 32,559 hrs · 28,363 cycles

CABIN FLOOR LT #6 EMERGENCY LIGHT STRIP DAMAGED AT FWD AND AFT END. C/A-COMPLETE:INSTALLED EXISTING LIGHT STRIP IN NEW EXTRUSION IAW 33-50-12

Part: FITTING — GOUGED (LT AILERON) · airframe 32,559 hrs · 28,363 cycles

LT AILERON DAMPER FITTING HAS WORN BORES/NICKS AND GOUGES. REMOVED AND REPLACED DAMPER FITTING IAW EO EM-27MR-112.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 32,559 hrs · 28,363 cycles

CENTER CROSS BEAM AT FRAME 20 IS CORRODED. C/A-COMPLETE:REPAIRED CENTER CROSS BEAM AT FRAME 20 IAW ETN-EM-53-241.

Part: WIRE — DAMAGED (CABIN) · airframe 32,559 hrs · 28,363 cycles

LT #8 PROXIMITY FLOOR LIGHT STRIP HAS DAMAGED WIRES. C/A-COMPLETE:REPLACED LT #8 PROXIMITY FLOOR LIGHT STRIP IAW 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 32,559 hrs · 28,363 cycles

LT #2 EMERGENCY FLOOR LIGHT STRIP HAS BROKEN WIRE (BROKE FLUSH WITH LIGHT UNREPAIRABLE). C/A-COMPLETE:REPLACED LIGHT STRIP AND EXTRUSION IAW 33-50-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 32,559 hrs · 28,363 cycles

CABIN FLOOR LT #7 EMERGENCY LIGHT STRIP DAMAGED AT FWD END. C/A-COMPLETE:INSTALLED EXISTING LIGHT STRIP IN NEW EXTRUSION IAW 33-50-12.

Part: WIRE — DAMAGED (CABIN) · airframe 32,559 hrs · 28,363 cycles

RT #4 PROXIMITY FLOOR LIGHT STRIP HAS DAMAGED WIRES. C/A-COMPLETE:REPLACED LT #4 PROXIMITY FLOOR LIGHT STRIP IAW 33-50-12.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,120 hrs · 27,898 cycles

LEFT AFT EMERGENCY EXTERIOR LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-10. OPS CHECKED GOOD IAW 33-50-00.

Part: CONNECTOR — DIRTY (MLG) · airframe 31,386 hrs · 27,232 cycles

LG AIR/GRD FAIL EICAS CLIMBING OUT OF FL180. DID NOT CLEAR. FOLLOWED FIM 32-63-00, CLEANED CONNECTORS AND REPLACED AD TAPE ON ALL MLG WOW SWITCH IAW SWPM 20-50-00. PERFORMED A FUNCTIONAL CHECK IAW AMM 32-63-05 AND OPS TESTED IAW W/C 32-700-16. OPS CHECKED GOOD, NO FURTHER DEFECT NOTED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,128 hrs · 26,040 cycles

DURING PS-2 INSPECTION FOUND LT EXTERIOR AFT OVERWING LIGHT INOPERATIVE. REMOVED AND REPLACED NR3 BATTERY AND CHARGER IAW AMM 33-50-04. REMOVED AND REPLACED LT EXTERIOR AFT OVERWING LIGHT BULB IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 29,631 hrs · 25,563 cycles

EMERGENCY LIGHT AT ROWS 17 AND 18 INOPERATIVE. INSTALLED PIN ON WIRE SPLICE SP9213 FOR THE EMERGENCY LIGHT IAW SWPM 20-51-01. OPS CHECKED GOOD.

Part: FLASHLIGHT — MISSING (FWD CABIN) · airframe 29,474 hrs · 25,419 cycles

FOUND FWD FA FLASHLIGHT MISSING. NSTALLED FWD FA FLASHLIGHT IAW AMM 33-50-16.

Part: FLASHLIGHT — FAILED (COCKPIT) · airframe 29,474 hrs · 25,419 cycles

FUMES IN CABIN AND COCKPIT AT ALTITUDE STRONG ODOR OF ELEECTICAL EMERGENCY LANDING. REMOVED AND REPLACED THE FLASHLIGHT ASSY IAW 33-50-16 CHECKED GOOD.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 28,600 hrs · 24,619 cycles

BLD 2, LEAK AFTER TAKEOFF. R & R BLEED LINE O-RINGS AT 18 AND 23 IAW AMM 36-11-10, 36-11-09. CHECK GOOD, NO LEAKS NOTED.

Part: NUT PLATE — CORRODED (CARGO DOOR) · airframe 28,464 hrs · 24,495 cycles

CARGO DOOR AFT FRAME ANGLE NUTPLATE CORRODED. REPAIRED CARGO DOOR AFT FRAME ANGLE NUTPLATE CORRODED IAW ENVOY ERS-EM-52MR-576

Part: DOOR SILL — CORRODED (FRAME 66) · airframe 28,464 hrs · 24,495 cycles

CARGO DOOR SILL CORRODED AROUND FASTENER ART FR 66. PERFORMED PERMANENT REPAIR ON CARGO DOOR SILL IAW SRM 53-31-15 ITEM #

Part: CONTACTOR — MALFUNCTIONED · airframe 28,339 hrs · 24,372 cycles

ABOUT 5 SECONDS AFTER SELECTING ENG 1 TO STOP WHILE PULLING INTO GATE SAW & HEARD ELEC ARCHING THOUGH SCREEN PANEL DIRECTLY BEHIND FIRST OFFICERS SEAT. ELEC BURNING SMELL FOLLOWED, NO ABNORMAL MSGS OR INDICATIONS ON EICAS OR ELEC PAGE ON MFD. R & R CONTACTOR K0190 IAW AMM 21-24-03. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,062 hrs · 22,251 cycles

CAPTAINS FLASHLIGHT INOPERATIVE. R & R CAPTAINS FLASHLIGHT AS REQUIRED. OPERATIONS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,952 hrs · 22,158 cycles

LEFT WING AFT EMERGENCY LIGHT INOPERATIVE. R & R LAMP. OPS GOOD IAW AMM 33-50-10.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 25,653 hrs · 21,896 cycles

FLIGHT OFFICERS EMER FLASHLIGHT INOPERATIVE. R & R FLIGHT OFFICERS EMER FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 25,170 hrs · 21,455 cycles

CAPTAIN`S FLASHLIGHT HOLDER BROKEN. R & R CAPTAIN`S FLASHLIGHT HOLDER IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,720 hrs · 20,988 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. DEFERRED AFT FLIGHT ATTENDANT FLASHLIGHT IAW MEL 25-53. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD. MEL ITEM RESTORED. FLASHLIGHT OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,671 hrs · 20,933 cycles

COCKPIT STEP & FIRST OVERHEAD CEILING LONG EMER LIGHTS INOPERATIVE. R & R IAW AMM 33-50-11. PERFORMED OPERATIONS CHECK IAW AMM 33-50-00. OPERATIONS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 24,651 hrs · 20,909 cycles

FLIGHT ATTENDANT REPORTS THAT AFT CABIN FLASHLIGHT CRADLE IS BROKEN & WILL NOT CHARGE UNLESS HELD IN PLACE. R & R IAW AMM-33-51-01. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,573 hrs · 20,850 cycles

RIGHT AISLE OVERWING EMER LIGHT INOPERATIVE. R & R RT AISLE OVERWING EMER LIGHT BULB IAW AMM 33-50-07.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 24,399 hrs · 20,729 cycles

AFTER TAKEOFF, MAIN ALT HAD YELLOW DASHES ON EICAS. DEFERRED IAW MEL 21-18. PERFORMED OPERATIONS CHECK OF PRESSURIZATION CONTROL SYS IN BOTH MANUAL & AUTO MODES IAW AMM 21-31-00. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED. MEL RESTORED.

Part: ANTI-ICE VALVE — FAILED (NR 2 ENGINE) · airframe 24,370 hrs · 20,705 cycles

DURING FLIGHT GOT E-2 ANTI-ICE FAIL ON EICAS. DEFERRED E-2 ANTI-ICE M PROCEDURE. COMPLIED WITH MEL 30-11. R & R ENG 2 ANTI-ICE VLV. OPERATIONS CHECKED GOOD IAW AMM 30-21-01. MEL ITEM RESTORED.

Part: ICU — FAILED (NR 2) · airframe 24,152 hrs · 20,541 cycles

ADC 1 & 2 FAIL WITH AP FAIL & AIRSPEED & ALT PRESELECT FAIL VERT SLOPE OFF. R & R REPLACED 2 ICU IAW AMM 23-00-01. OPERATIONS CHECKED GOOD & PERFORMED FNC OF ADC 1 & 2 IAW AMM 34-15-00. OPERATIONS CHECKED GOOD.

Part: INDICATION SYS — MALFUNCTIONED (FUEL QTY) · airframe 23,926 hrs · 20,382 cycles

NUMBER 1 FUEL QTY INDICATIONS ON EICAS & MFD WENT OUT SHOWING DASHES DURING FLIGHT, INDICATIONS CAME BACK SEVERAL TIMES DURING FLIGHT SHOWING DIFFERENT LEVELS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,910 hrs · 20,363 cycles

ALL EMER LIGHTS INOPERATIVE. R & R NR 1, 2, 3 & 4 EMER LIGHT BATTERIES IAW MM 33-50-04. OPERATIONS CHECKED GOOD. PN 2013-1A, SN 112892 NR 2, SN 114996 NR 3 & SN 104852 NR4.

Part: WIRE — BROKEN (CABIN) · airframe 23,692 hrs · 20,193 cycles

FWD GALLEY EMERGENCY LIGHT STRIP WIRES BROKE. R & R FWD GALLEY EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12.

Part: BEAM — CORRODED (FUSELAGE) · airframe 23,692 hrs · 20,192 cycles

GALLEY RT HAT BEAM HAS CORROSION AT NUTPLATE HOLE AT FRAME 23. REPAIRED IAW ERS-EM-53MR-407.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 23,692 hrs · 20,192 cycles

PAX DOOR EMERGENCY LIGHT INOPERATIVE ON DOOR HINGE. REMOVED & INSTALLED NR 1 EMERGENCY BATTERY POWER SUPPLY IAW WORK CADR 33-700-17 & 33-700-19, OPERATIONAL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 23,433 hrs · 19,974 cycles

LT & RT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R RT & LT OVERWING EMERGENCY BULBS IAW AMM 33-50-07, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 22,887 hrs · 19,556 cycles

DURING MAINTENANCE INSPECTION ON AC905 FOUND LT LATERAL PANEL EMERGENCY OVERWING LIGHT INOPERABLE. R & R THE LT LATERAL PANEL EMERGENCY OVERWING LIGHT ASSEMBLY IAW 145 AMM 33-50-10, CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,751 hrs · 19,447 cycles

EMERGENCY LIGHT STRIP AT ROW 11 & 12 IS INOPERATIVE. R & R FLOOR PROXIMITY LIGHT AT ROW 11 & 12 IAW EMB-145 AMM 33-50-12, OPERATIONS CHECKED GOOD.

Part: ELECTRONIC UNIT — FAILED (MLG) · airframe 22,548 hrs · 19,274 cycles

GEAR WOULD NOT RETRACT AFTER TAKEOFF. DURING RETURN TO DEPARTURE, RECEIVED "TAKEOFF, FLAPS, GEAR, TRIM" AURAL WARNING. EXECUTED A NORMAL LANDING AND IMMEDIATELY AFTER TOUCHDOWN RECEIVED LG AIR/GROUND FAIL AND IC 1-2 WOW INOP EICAS MESSAGES. AFTER PARKING TRIED TO CONNECT GPU BUT PLANE WASN'T SEEING IT ON ELECTRIC PAGE - SHUTDOWN NR 1 ENGINE AND LOST CAPT PFD + FO MFD. ON SHUTTING DOWN NR 2 ENGINE THE F/O PFD. R & R LANDING GEAR ELECTRONIC UNIT IAW AMM 32-32-01. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 22,482 hrs · 19,224 cycles

FWD CEILING EMERGENCY LIGHT INOPERATIVE. FOUND CONNECTORS DIRTY, CLEANED CONNECTORS AS REQUIRED. OPS GOOD AT THIS TIME, NO OTHER DEFECTS NOTED.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 22,482 hrs · 19,224 cycles

COCKPIT STEP EMERGENCY LIGHT INOP. FOUND CONNECTORS DIRTY. CLEANED CONNECTORS AS REQUIRED. OPS GOOD AT THIS TIME, NO OTHER DEFECTS NOTED.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,294 hrs · 19,070 cycles

LEFT OVERWING UPPER EMERGENCY LIGHT INOPERATIVE. R & R NR 4 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11, OPS CHECKED GOOD IAW WC 33-700-17.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,958 hrs · 18,803 cycles

EMERGENCY EXIT SIGN BEHIND GALLEY AT PAX SEAT 3 INOPERTIVE. R & R NR 3 INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,880 hrs · 18,745 cycles

FLOOR EMERGENCY LIGHT FROM SEAT 8 TO 10 INOPERATIVE. R & R NR 3 EPSU BATTERY AND CHARGER OPS CHECKED GOOD IAW AE WC 33-700-19.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 21,689 hrs · 18,578 cycles

THE F/A REPORTED THE PASSENGER DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED MAIN DOOR AND ROLLERS IN REF TO AMM 52-18-00 AND 52-21-02. THE OPS CHECK OF THE OPEN AND CLOSED DOOR IS GOOD AT THIS TIME. THE ACFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 21,662 hrs · 18,553 cycles

DURING MX INSPECTION, FOUND LIGHTED EMERGENCY "EXIT" SIGN ON THE AFT SIDE OF THE AFTER GALLEY WALL IN FRONT OF ROW 3 BC, DID NOT ILLUMINATE. ACFT REMOVED FROM SERVICE. FOUND BACK SHELL LOOSE ON CONNECTER P8003, TIGHTENED CONNECTER IAW SWPM 20-50-00. OPS CHECKED GOOD IAW AMM 33-50-00. ACFT RETURNED TO SERVICE.

Part: SWITCH — BROKEN (FLASHLIGHT) · airframe 21,624 hrs · 18,530 cycles

DURING MX INSPECTION FOUND CAPTAIN’S FLASHLIGHT SWITCH BROKEN. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 20,859 hrs · 17,925 cycles

ON FLIGHT 2888 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT REAR BRACKET WAS BROKEN. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT ASSEMBLY IAW EMB-145 AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: A/C PACK — DIRTY (AC BAY) · airframe 19,571 hrs · 16,917 cycles

FLIGHT 3916, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN IMMEDIATELY AFTER PUSHBACK FROM GATE. AIRCRAFT REMOVED FROM SERVICE. FOUND NR 2 PACK BLOWING DUST & DIRT. NO EVIDENCE OF SMOKE OR OIL ODOR. REMOVED AND REPLACED THE NR 1 PACK VALVE IAW AMM 21-51-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BEARING — LACK OF LUBE (CABIN DOOR) · airframe 19,363 hrs · 16,756 cycles

ON FLIGHT 2897 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBE MAIN DOOR ROLLER BEARING, DOOR OPEN /CLOSE CHECK WAS GOOD IAW EMB 145 52-18-00 AMM. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: YOKE — CRACKED (ENGINE MOUNT) · airframe 19,332 hrs · 16,730 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT ENGINE LOWER FORWARD YOKE CRACKED FORWARD OF ENGINE MOUNT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT ENGINE LOWER FORWARD YOKE FORWARD OF ENGINE MOUNT IAW EO EM-54MR-386. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,339 hrs · 16,735 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR AFT SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR AFT SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 19,339 hrs · 16,735 cycles

DURING B INSPECTION FOUND THE DIAMOND GUSSET AT FRAME 20 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DIAMOND GUSSET AT FRAME 20 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: YOKE — CRACKED (LT ENGINE) · airframe 19,333 hrs · 16,730 cycles

LEFT ENGINE LOWER FWD YOKE CRACKED FWD OF ENGINE MOUNT. R & R LT ENGINE LOWER FWD YOKE FITTING IAW AEA EO EM-54MR-386.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,339 hrs · 16,735 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR FORWARD SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR FORWARD SILL IAW EMB145 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 19,339 hrs · 16,735 cycles

DURING B INSPECTION FOUND THE GALLEY CEILING PANEL 233BLC EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RECONNECTED GALLEY CEILING PANEL 233BLC EMERGENCY LIGHT CONNECTOR IAW EMB 145 AMM 25-22-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (HORIZONTAL STAB) · airframe 19,228 hrs · 16,643 cycles

FLT 4038, CREW REPORTED PITCH TRIM BACKUP INOPERATIVE MASTER WARNING AND EICAS MESSAGE PRESENTED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED HSCU IAW AMM 27-40-01. OPS CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 18,828 hrs · 16,327 cycles

ON FLIGHT 3909 THE CREW REPORTED THE SWITCH ON THE CAPTAIN’S FLASHLIGHT WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,206 hrs · 15,858 cycles

DURING B-INSPECTION, FOUND THE FIRST FLOOR EMERGENCY LIGHT STRIP AND SERVICE DOOR LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY INVERTER. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (COCKPIT) · airframe 18,085 hrs · 15,758 cycles

DURING B-INSPECTION FOUND THE FLASHLIGHT HOLDER BEHIND CAPTAIN’S SEAT BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT HOLDER IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A NO FURTHER DEFECTS NOTED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — MALFUNCTIONED (CABIN DOOR) · airframe 17,596 hrs · 15,400 cycles

ON FLIGHT 3249 THE CREW REPORTED THE CABIN ENTRY DOOR HANDLE OPERATION IS DIFFICULT AND PRODUCES A SNAPING SPRING EFFECT WHEN LOCKING -REPEAT WRITE UP PAGE 3160411. THE AIRCRAFT WAS REMOVED FROM SERVICE. MAIN ENTRY DOOR ROLLERS SERVICED IAW AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — BINDS (CABIN) · airframe 16,864 hrs · 14,827 cycles

ON FLIGHT 3959 THE FLIGHT ATTENDANT REPORTED THE MAIN ENTRY DOOR WAS DIFFICULT TO OPERATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CONDUCTED AN OPERATIONAL CHECK OF THE MAIN PAX DOOR IAW EMB-145 AMM 52-18-00. THE PASSENGER DOOR CHECKED AS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,525 hrs · 13,066 cycles

DURING MAINTENACE BASE VISIT FOUND THE SERVICE DOOR SILL HAS CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE SERVICE DOOR SILL IAW EMBRAER SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 14,462 hrs · 13,012 cycles

FOR FLIGHT 4224 MAINTENANCE FOUND THE EMERGENCY LIGHT STRIP AT ROW 8 AND 9 TO HAVE BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP AT ROW 8 AND 9. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PIN — MISSING (FIRE BOTTLE) · airframe 14,087 hrs · 12,704 cycles

FOR FLIGHT 4090 DURING INSPECTION FOUND THE HALON FIRE EXTINGUISHER IN AFT CABIN MISSING A SAFETY PIN AND WIRE (YELLOW BUTTON STILL PRESENT). THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED SAFETY PIN AFTER LOCATING IT IAW ETN GN-26-001R1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 13,307 hrs · 12,052 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FLOOR EMERGENCY LIGHTS FROM ROW 12 AFT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 INVERTER. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,577 hrs · 11,425 cycles

DURING PS2 INSPECTION FOUND THE REAR CABIN EMERGENCY FLOOR PROXIMITY FLOOR LIGHT STRIP TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM FLOOR STRIPS IAW EMS AMM 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 10,296 hrs · 9,340 cycles

AIRCRAFT ARRIVED FOR REPAIR OF ACCIDENTAL DAMAGE THAT OCCURRED TO RT AFT FUSELAGE BETWEEN FR 61 AND 62 AND BETWEEN STR 13R AND 14R. PERFORMED A CUT OUT OF THE FUSELAGE SKIN TO REMOVE THE DAMAGE. FAB A FILLER, DOUBLER FOR REPAIR. DRILLED, CLEANED, TREATED AND INSTALLED REPAIR PARTS. REPAIR DONE IAW EMBRAER 145 SRM (SRM EMB-145/1142 REV 40) CHAPTER 53-31-01. AIRCRAFT RETURNED TO SERVICE.

Part: CARBON SEAL — FAULTY (NR 1 ENGINE) · airframe 7,969 hrs · 7,055 cycles

ON FLIGHT 4200, CREW REPORTED A ABORTED TAKEOFF AT 100 KNOTS AFTER F/O NOTICED EVIDENCE OF SMOKE IN THE COCKPIT. THE F/A ALSO REPORTED VISIBLE SMOKE AROUND GALLEY AREA AND AFTER SHUTDOWN THE PACKS THE SMOKE WENT AWAY. THE SMOKE DID NOT HAVE A ODOR OF ELECTRICAL OR OIL ODOR LIKE. THE SMOKE ODOR LIKE BURNING PAPER AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER ONE ENGINE. REMOVED AND REPLACED THE NR 4 CARBON SEAL PER SERVICE BULLETIN 72-348. THE OPERATIONAL CHECKS WERE GOOD.

Part: SWITCH — PINCHED (AUTOPILOT) · airframe 6,647 hrs · 5,787 cycles

PTRIM MAIN INOP MESSAGE FOLLOWED BY PTRIM BACKUP INOP MESSAGE. FOUND PILOTS AUTO PILOT/TRIM/PUSHER DISCONNECT SWITCH PINCHED. REPOSITIONED WIRES. SYSTEM OPERATIONAL CHECK GOOD IAW EMB 27-11-00-700-803A AND AMM 27-40-00. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,664 hrs · 4,131 cycles

SERVICE DOOR CENTER SILL FOUND CORRODED. FABRICATED REPAIR DOUBLER, INSTALLED AND RESTORED PROTECTIVE FINISH IAW EMB SRM 53-21-02. RETURNED AIRCRAFT TO SERVICE.

Part: SKIN — DAMAGED (RT WING)

AIRCRAFT LIGHTNING STRIKE. ACCOMPLISHED LIGHTNING STRIKE INSPECTION IAW AMERICAN EAGLE WORK CARD 05-200-00. REPAIRED RIGHT TRAILING EDGE OF WING TIP IAW 51-21-07 WORK CARD 05-200-00. REPAIRED RIGHT TRAILING EDGE OF WING TIP IAW 51-21-07. RETURNED AIRCRAFT TO SERVICE. (M)