N664MS

Part: PIVOT ASSY — OUT OF ADJUST (THRUST REVERSER) · airframe 46,978 hrs · 42,488 cycles

ON TAKEOFF ROLL AROUND 60 KNOTS GOT ENG 2 REV DISAGREE. REJECTED TAKEOFF FACT 10NOV24 04:45 MDT T/S IRT FIM TASK 78-30-00-810-821A. PRFORMED PIVOT DOOR OVERSTOW TEST PROCEDURE IRT AMM 78-31-01. ADJUSTED UPPER AND LOWER PIVOT DOOR ACTUATOR OVERSTOW NUTS IRT AMM 78-31-01. OPS CHECK GOOD, OK FOR SERVICE AT THIS TIME

Part: THRUST REVERSER — WARNING MESSAGE (NR 2) · airframe 46,856 hrs · 42,356 cycles

E2 REV DISAGREE DISPLAYED ON TAKEOFF (DEACTIVATED AND STOWED ENG #2 T/R). MEL 17OCT24 07:05 SBY C29104 78-2 ENG 1 OR 2 REV DISAGREE MESSAGES. FACT 18OCT24 06:33 SBY R&R STOW SWITCHEWS 2L1 AND 2U1 CHECKED RIGGING OF ALL 4 STOW SWITCHES IAW 145AMM 78-34-01 S HOOKS NOT DISCONNECTED REACTIVATED T/R PLUGS INSTALLED BOLTS STOWED OPS CHECK GOOD CLEAR MEL78-2

Part: PROXIMITY SWITCH — FAILED (MLG) · airframe 46,789 hrs · 42,285 cycles

AFTER T/O LG GEAR AIR GND FAIL MSG ON EICAS, CREW WAS NOT RETRACTING GEAR. RETURN TO FIELD AND EMERGENCY DECLARED FACT 06OCT24 13:02 ROA FOUND LG RT WOW PROX SWITCH MESSAGE ON CMC. T/S IAW FIM 32-63-00-810-803-A. R/R'D BOTH R/H MLG PROX SWITCHES

Part: CONTROL LEVER — FAULTED (MLG) · airframe 46,692 hrs · 42,163 cycles

LANDING GEAR WOULD NOT RETRACT IMMEDIATELY AFTER DEPARTURE OF RUNWAY. R&R LANDING GEAR CONROL LEVER IAW AMM 32-32-02-000-801-A OPS CHECK SATISFACTORY

Part: CONTROL UNIT — FAULTED (MLG) · airframe 46,692 hrs · 42,163 cycles

LANDING GEAR WOULD NOT RETRACT IMMEDIATLY AFTER DEPARTURE MOF RUNWAY. RAR LANDING GEAR CONTROL UNIT IAW AMM 32-32-02-000-801-A. OPS CHECK GOOD.

Part: ELECTRONIC UNIT — FAULTED (MLG) · airframe 46,508 hrs · 41,965 cycles

L/G AIR/GRD FAIL EICAS MESSAGE DISPLAYED 3 SECONDS AFTER ROTATION. GEAR WOULD NOT RETRACT. FACT 16AUG24 01:42 PHL T/S IRW FIM 32-63-00-810-801-A. R+R LGEU IAW AMM 32-32-01. PERFORMED MULTIPLE GEAR SWINGS. NO DEFECTS OR MESSAGES NOTED. OPS CHECK GOOD. OK FOR SERVICE

Part: SHEAR TIE — CRACKED (FRM 29 S18-19L) · airframe 46,025 hrs · 41,426 cycles

53-2402 LH SHEAR CLIP CRACKED AT FR29 BTW STR18-19L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (FRM 29) · airframe 46,025 hrs · 41,426 cycles

53-2399 LH COLUMN CRACKED UNDER LH OMEGA BEAM AT FR29. REPAIRED IAW EO1-53-24-0252

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 46,025 hrs · 41,426 cycles

55-2378 RIB EDGE CRACKED ON HOR STAB LH LE AT YH-670. RAR IAW SRM51-40-02

Part: SKIN — CRACKED (FRM 75 S2L) · airframe 46,025 hrs · 41,426 cycles

53-2366 RF1 LH FUSELAGE CRACKED AT STR2L AND FR75 AT RIVET HOLE. REPAIRED IAW EO1-53-24-0276

Part: SKIN — CRACKED (FRM 75 S2R) · airframe 46,025 hrs · 41,426 cycles

53-2367 RF1 FUSALGE SKIN AT STR2R AND FR75 CRACKED AT 1 RIVET. REPAIRED IAW EO1-53-24-0278

Part: TORQUE BOX — CRACKED (RT WING) · airframe 46,025 hrs · 41,426 cycles

57-2275 3 HOLES FOUND WITH NDT INDICATION ON RH WING TQ BOX AT RIB 1. REPAIRED IAW EO1-57-24-0297

Part: TORQUE BOX — CRACKED (LT WING) · airframe 46,025 hrs · 41,426 cycles

57-2274 2 HOLES WITH NDT INDICATIONS ON LH WING TQ BOX AT RIB 1 WITH 1 BUSHING DAMGED. REPAIRED IAW EO1-57-24-0297

Part: SHEAR TIE — CRACKED (FRM 62 S6-8R) · airframe 46,025 hrs · 41,426 cycles

53-2094 SHEAR CLIP CRACKED AT FR62 BTW STR6-8R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (FRM 71 S6-8R) · airframe 46,025 hrs · 41,426 cycles

53-2097 SHEAR CLIP CRACKED AT FR71 BTW STR6-8R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (FRM 66 S7-9L) · airframe 46,025 hrs · 41,426 cycles

53-2096 SHEAR CLIP CRACKED AT FR66 BTW STR7-9L. REPAIRED IAW EO1-53-24-0289

Part: BRACKET — CRACKED (FRM67-68 S4-5R) · airframe 46,025 hrs · 41,426 cycles

53-2102 3 DOOR MECH BRACKET CRACKET AT BTW FR67-68 AND STR 4-5R. RAR BRACKET IAW SRM 51-40-02

Part: SUPPORT — CRACKED (FRMS 61-62 S4-5R) · airframe 46,025 hrs · 41,426 cycles

53-2091 CARGO DOOR SUPPORT ASSY CRACKED BTW FR61-62 AND STR4-5R. RAR SUPPORT ASSY IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (FRM 66 S6-7R) · airframe 46,025 hrs · 41,426 cycles

53-2095 SHEAR CLIP CRACKED AT FR 66 BTW STR6-7R. REPAIRED IAW EO1-53-24-0288

Part: SHEAR TIE — CRACKED (FRM 58 S15-16L) · airframe 46,025 hrs · 41,426 cycles

53-2084 LH SHEAR CLIP CRACKED AT FR58 BTW STR15-16L. RAR CLIP IAW SRM 51-40-02

Part: FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,025 hrs · 41,426 cycles

53-2079 CARGO DOOR LWR CORNER ENTRANCE BEAM FWD FITTING CORRODED. RAR FITING IAW SRM 51-40-02

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 46,025 hrs · 41,426 cycles

53-2075 CARGO DOOR FWD LATERAR L-SHAPE ANGLE CORRODED AT LWR CORNER OF DOOR. REPAIRED IAW EO1-53-24-0256

Part: DOUBLER — CORRODED (FRMS 60-61) · corrosion level 2 · airframe 46,025 hrs · 41,426 cycles

53-2083 LH SIDE OF FRESH WATER DOUBLER CORRODED AT BTW FR60-61. RAR DOUBLER IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED · airframe 46,025 hrs · 41,426 cycles

53-2036 3 CRACKS ON LH OMEGA BEAM #1. REPAIRED IAW EO 1-53-24-0255

Part: ATTACH ANGLE — CRACKED (WNG-BDY FAIRING) · airframe 46,025 hrs · 41,426 cycles

57-2071 LH WING #2 WING TO BODY ATTACH ANGLE CRACKED AFT OF SPAR 2. RAR ANGLE IAW SRM 51-40-02, 57-20-01

Part: SHEAR TIE — CRACKED (FRM 28 S15-16R) · airframe 46,025 hrs · 41,426 cycles

53-2031 SHEAR CLIP CRACKED AT FR28 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: DOUBLER — CORRODED (FRM 20) · corrosion level 2 · airframe 46,025 hrs · 41,426 cycles

53-2040 DOUBLER CORRODED ON RH BEAM AT FR20. RAR DOUBLER IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (FRMS 45-50) · airframe 46,025 hrs · 41,426 cycles

53-2056 CTR FUSE 3 UNDERFLOOR, RH OMEGA BEAM AFT IB ANGLE CRACKED AT FR45-50. RAR BEAM IAW SRM51-40-02

Part: FLOOR SUPPORT — CRACKED (FRM 29) · corrosion level 2 · airframe 46,025 hrs · 41,426 cycles

53-2026 CTR OMEGA BEAM #1 CRACKED AND CORRODED AT FR29. REPAIRED IAW EO1-53-24-0245

Part: SHEAR TIE — CRACKED (FRM 25 S15-16R) · airframe 46,025 hrs · 41,426 cycles

53-2028 SHEAR CLIP CRACKED AT FR25 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SUPPORT — CORRODED (NR 2) · corrosion level 2 · airframe 46,025 hrs · 41,426 cycles

53-2023 LH SILL #2 CORRODED. RAR SILL IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (FRM 24 S15-16R) · airframe 46,025 hrs · 41,426 cycles

53-2027 SHEAR CLIP CRACKED AT FR24 BTW STR15-16R. RAR SHEAR CLIP IAW SRM51-40-02

Part: ATTACH ANGLE — CRACKED (WNG-BDY FAIRING) · airframe 46,025 hrs · 41,426 cycles

57-2071 LH WING #2 WING TO BODY ATTACH ANGLE CRACKED AFT OF SPAR 2. RAR ANGLE IAW SRM51-40-02, 57-20-01

Part: FLOOR SUPPORT — CRACKED (FRMS 35-36) · airframe 46,025 hrs · 41,426 cycles

53-2051 CTR FUSE 3 UNDERFLOOR, RH SILL BTW FR35-36 IS CRACKED. RAR SILL IAW SRM 51-40-02

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 46,025 hrs · 41,426 cycles

53-2032 RH SILL #1 CORRODED. RAR SILL IAW SRM51-40-02

Part: ATTACH ANGLE — CRACKED (WNG-BDY FAIRING) · airframe 46,025 hrs · 41,426 cycles

57-2070 RH WING #2 WING TO BODY FAIRING ATTACH ANGLE CRACKED AFT OF SPAR 2. RAR ANGLE IAW SRM51-40-02

Part: FLOOR SUPPORT — CRACKED (FRMS 35-39) · airframe 46,025 hrs · 41,426 cycles

53-2063 CTR FUSE 3 UNDERFLOOR, CTR OMEGA BEAM IB FLANGE CRACKED AT BTW FR35-39. REPAIREDE BEAM IAW EO1-53-24-0249

Part: FLOOR SUPPORT — CRACKED (NR 2) · corrosion level 2 · airframe 46,025 hrs · 41,426 cycles

53-2025 LH OMEGA BEAM #2 HAS 4 CRACKS AND CORROSION. RAR OMEGA BEAM IAW SRM 51-40-02

Part: DOUBLER — CORRODED (FRM 22) · corrosion level 2 · airframe 46,025 hrs · 41,426 cycles

53-2041 DOUBLER CORRODED ON RH BEAM AT FR22. RAR IAW SRM 51-40-02

Part: GUSSET — CORRODED (FRMS 20-23) · corrosion level 2 · airframe 46,025 hrs · 41,426 cycles

53-2037 CTR GUSSET CORRODED AT BTW FR20-23. RAR GUSSET IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (FRMS 35-39) · corrosion level 2 · airframe 46,025 hrs · 41,426 cycles

53-2061 CTR FUSE 3 UNDERFLOOR, LH OMEGA BEAM IB FLANGE CORRODED AT FR35-39. REPAIRED IAW EO1-53-24-0250

Part: ATTACH ANGLE — CRACKED (WNG-BDY FAIRING) · airframe 46,025 hrs · 41,426 cycles

57-2072 LH WING #3 WING TO BODY FAIRING ATTACH ANGLE CRACKED AFT OF SPAR 2. RAR ANGLE IAW SRM 51-40-02, 57-20-01

Part: SHEAR TIE — CRACKED (FRM 26 S16-17R) · airframe 46,025 hrs · 41,426 cycles

53-2030 SHEAR CLIP CRACKED AT FR26 BTW 16R-17R.. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (FRM 36) · airframe 46,025 hrs · 41,426 cycles

53-2059 CTR FUSE 3 UNDERFLOOR, LH OMEGA BEAM IB FLANGE CRACKED AT FR36. REPAIRED IAW EO1-53-24-0254

Part: SHEAR TIE — CRACKED (FRM 26 S15-16R) · airframe 46,025 hrs · 41,426 cycles

53-2029 SHEAR CLIP CRACKED AT FR26 BTW 15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (FRM 15 S15-16R) · airframe 46,025 hrs · 41,426 cycles

53-2034 SHEAR CLIP CRACKED AT FR15 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: BEAM — CORRODED (FRSM 20-22) · corrosion level 2 · airframe 46,025 hrs · 41,426 cycles

53-2039 SERVICE DOOR CUTOUT LWR BEAM CORRODED BTW FR20-22. RAR BEAM IAW SRM 51-40-02

Part: SKIN — GOUGED (FRM 7-8 S20-21R) · airframe 46,025 hrs · 41,426 cycles

53-2017 MULTIPLE GOUGES FOUND ON FUSELAGE EXTERNAL SKIN AT FR7-8 STR20R-21R. REPAIRD IAW EO1-53-24-0260

Part: SKIN — CRACKED (FRMS 77-78 S6-8R) · airframe 46,025 hrs · 41,426 cycles

53-2021 2 CRACKS BTW STR6R-8R AND FR77-78. REPAIRED IAW EO1-53-24-0247

Part: SKIN — DENTED (FRM 9 S20L) · airframe 46,025 hrs · 41,426 cycles

53-2014 DENT FOUND ON FUSELAGE SKIN ON FR9 AND 6" ABOVE STR20L. REPAIRED IAW EO1-53-24-0264

Part: SKIN — DENTED (FRM 23 S13L) · airframe 46,025 hrs · 41,426 cycles

53-2020 DENT ON FUSELAGE 3" FWD OF FR23 AND 2" ABOVE STR13L. REPAIRED IAW EO1-53-24-0253

Part: UNKNOWN — ODOR (CABIN) · airframe 45,827 hrs · 41,215 cycles

ON LANDING ROLLOUT REACHING TAXIWAY MODERATE SMELL OF HYD FLUID FOR ONE MINUTE IN FLIGHT DECK. CHECKED COCKPIT FOR HYD FLUID SMELL RAN BOTH ENGINES OPERATED BOTH BLEEDS NO DEFECTS NOTED OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,562 hrs · 40,892 cycles

FUEL QTY DASHED OUT ON BOTH MFD AND #1 FUEL QTY ON EICAS(MX CONFIRMED FUEL QTY DASHED ON BOTH MFD'S AND EICAS WAS TANK. TROUBLESHOT USING FIM 28-41-00-810-916A. FOUND TO BE TRANSITORY CONDITION OF THE WING FCU. R&R FCU AS POSITIVE MAINTENANCE ACTION IAW AMM 28-41-01 OPS CHECK GOOD CLEAR MEL 28-9

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,779 hrs · 39,984 cycles

E2 FIRE DET FAIL ON TAKEOFF. CREW REPORTED THE MESSAGE EXTINGUISHED BUT CAME BACK ON WITHIN A MINUTE-- T/S IRT FIM 26-11-00-810-808-A STEP 1-5 + 14 R&R E2 FIRE CONTROL IAW AMM 26-11-03 OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. T/S E2 FIRE DET FAIL MSG IRT FIM 26-11-00-810-804-A + MTL 2023-E-6. R&R E2 CONTROL MODULE MX ACTION COMPLETE SUBJECT TO SATISFACTORY EVALUATION FLIGHT. EVAL FLIGHT UNSAT. AT APPROX V1/ROTATION E2 FIRE DET FAIL EICAS CAME ON WENT OUT DURING LEVEL FLIGHT BUT CAME ON DURING LANDING ROLL WITH REVERSE THRUST. UPON INSPECTION OF ENGINE HARNES FOUND ADELE CLAMP CHAFFED THROUGH AND DAMAGED WIRING ON E2. R&R #2 ENGINE HARNESS IRT PPBM 71-00-00.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,778 hrs · 39,982 cycles

AFTER T/O FIRE DET 2 FAIL INDICATED ON EICAS.FACT 09AUG23 21:33 CLT GROUND RAN A/C FOR 5 MIN AND OHM OUT #2 FIRE DETECTOR P 0914 AND FIRE LOOP. NO DEFECTS NOTED. OPS CHECK GOOD OK FOR SERVICE. E2 FIRE DET FAIL WITH ENG 2 ON AND THRUST LEVER ADVANCED. PERFORMED FIM TASK 1-5 PASSED. FAILURE OF ENGINE CONTROL MODULE 2 R&R MODULE IAW AMM 26-11-03. GOUND RAN A/C WITH THRUST LEVERS ADVANCED. OPS CHECK GOOD OK FOR SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (MLG) · airframe 44,044 hrs · 39,164 cycles

ON APPROACH HAD A LANDING GEAR DISAGREE AND DECLARED AN EMERGENCY. FLT LANDED SAFELY AND WAS INSPECTED PRIOR TO TAXI TO THE HANGER. NLG LDG DN PROX SW 1 REQUIRES REPLACEMENT FOR CORROSION AND PREVIOUS PIREP OF LG/LEVER DISAGREE AND NLG UNSAFE IDICATION.-C/A-RAR NLG DOWNLOCK PROXIMITY SWITCH 1 AND HARNESS IAW AMM 32-61-02. FUNCTIONAL CHECK GOOD. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: CRADLE — BROKEN (AFT) · airframe 43,805 hrs · 38,922 cycles

AFT CABIN EMERGENCY FLASHLIGHT CRADLE BROKEN-C/A-RAR AFT CABIN EMERGENCY FLASHLIGHT HOLDER CLAMP IAW EMB 145 CMM 25-60-14.

Part: INVERTER — FAULTED (EMERGENCY LIGHTS) · airframe 43,771 hrs · 38,883 cycles

DURING PS-2 CHECK, FOUND EMERGENCY LIGHTS AT BOTH OVERWING EXIT IDENTIFIERS AND FLOOR PROXIMITY STRIPS BETWEEN SEAT 8A AND 12A INOP.-C/A-RAR #3 BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04 AND RAR #5 EMERGENCY LIGHT AC/DC INVERTER IAW EMB 145 AMM 33-50-11. DID NOT FIX. RAR #5 EMERGENCY FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 43,771 hrs · 38,883 cycles

REF ITEM 1 ABOVE EMERGENCY LIGHT BATTERIES 3 AND 4 DEAD-C/A-RAR #3 AND #4 EMERGENCY LIGHT BATTERIES IAW MM 33-50-04

Part: NONE — NONE · airframe 43,610 hrs · 38,706 cycles

PACK 1 AND 2 CLOSED ON EICAS / EMERGENCY NOT DECLARED A/C SWAP. FLIGHT CONTINUED. -C/A-PACK LEAKS FOUND ON PACK 1 AND PACK 2. RAR PACK 1 DUCT FROM THE DUAL HEAT EXCHANGER IAW EMB145 AMM 21-51-02. SEE ITEM 2 THIS AML PAGE FOR #2 PACK.

Part: LAMP — NONE (LH) · airframe 43,465 hrs · 38,549 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-07

Part: BLEED AIR SYS — LEAKING · airframe 43,270 hrs · 38,334 cycles

BLEED 1 LEAK ON FINAL APPROCH EMERGENCY DECLARED. CLEARED WHEN BLD 1 VALVE CLOSED-C/A-FOUND LEK ON LH GRATE ASSY RAR LH GRATE ASSY PER EMB AMM 21-57-02. LEAK CHECK GOOD AT THIS TIME

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,099 hrs · 38,129 cycles

SUPPLEMENTAL CA FOR AFT CABIN EMERGENCY FLASHLIGHT HOLDER CLIP BROKEN-C/A-DEFERRED PER MEL 25-32 AUTH# 060220M-C. -C/A-ACCOMPLISHED AFT CABIN EMERGENCY FLASHLIGHT HOLDER CLIP BROKEN IAW AMM 33-50-16. MEL 25-32 RESTORED.

Part: NONE — NONE · airframe 43,015 hrs · 38,024 cycles

SMOKE/ODOR / SMOKE IN FLTDECK FROM AC PACK 1 . WITH APU RUNNING THERE WAS A GRINDING NOISE. SMOKE SEEN IN COCKPIT - AIRCRAFT POWER AND APU WERE SHUT DOWN - NO SMOKE OR FIRE - SOUND CEASED WHEN APU SHUT DOWN-C/A-CA PENDING

Part: NONE — NONE · airframe 42,699 hrs · 37,707 cycles

REFFERENCE MEL 33-22 AUTH # 030406D-C LH FORWARD LOWER FAIRING EXT EMER LIGHT INOPT 48627391 ITEM 3-C/A-RAR BATTERY POWER SUPPLY/BATTEERY IAW EMB-145 AMM 33-50-04 OPS CHECK GOOD MEL ITEM RESTORED

Part: NONE — NONE · airframe 42,602 hrs · 37,594 cycles

LH FWD WING EMERGENCY LIGHT INOP-C/A-T/S FWD WING EMERGENCY LIGHT INOP IAW FIM TASK 33-50-00-810-8014A. RAR LH FWD WING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. NO FIX RAR #2 EMERGENCY BATTERY IAW EMB AMM 33-50-04-000-802-A AND 33-50-04-400-802-A AND #2 CHARGER IAW EMB AMM 33-50-04-000-801-A AND 33-50-04-400-801-A OPC GOOD. END.

Part: NONE — NONE · airframe 42,602 hrs · 37,594 cycles

FA EMERGENCYFLASHLIGHT CRADLE BROKEN-C/A-RAR FA EMERGENCY FLASHLIGHT IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPC GOOD. END.

Part: NONE — NONE · airframe 42,570 hrs · 37,556 cycles

WINDSHIELD WIPER CAME ON WHILE IN THE SWITCH OFF POS. WIPER MOTOR OVERHEATED. EMERGENCY DECLARED -C/A-FOUND FO'S WIPER IN MIDDLE OF WINDSHIELD. REPLACED FO'S WIPER MOTOR/ CONVERTER IAW EMB 145 AMM 30-41-02-000-801-A & 32-41-02-400-801-A. OPERATIONAL TESTS GOOD. NO FURTHER DEFECTS NOTED. END.

Part: NONE — NONE · airframe 42,377 hrs · 37,347 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT IAW EMB145 AMM 33-50-10

Part: NONE — NONE · airframe 42,328 hrs · 37,292 cycles

EXTERIOR EMERGENCY LIGHT OVER LEFT WING AFT INOP.-C/A-RAR EXTERIOR EMERGENCY LIGHT OVER LEFT WING AFT. OPC GOOD. IAW AMM 33-50-10

Part: NONE — NONE · airframe 42,278 hrs · 37,239 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT BULB IAW EMB AMM 33-31-01. OPC GOOD.

Part: SKIN — LEAKING (LT WING) · airframe 41,695 hrs · 36,571 cycles

E875499 LH WING LOWER SKIN FUEL LEAK RIB 13-14 AT PREVIOUS REPAIR-C/A-C/W REPAIR IAW ERS-EM-57MR-1333

Part: NUT PLATE — MISSING (EMERGENCY LIGHT) · airframe 41,695 hrs · 36,571 cycles

RIGHT OVERWING EMERGENCY LIGHT HAS A MISSING LENS ATTACH NUTPLATE-C/A-COMPLETE:RAR'D EMERGENCY LIGHT IAW AMM 33-50-10, OPS CHECK GOOD

Part: BRACKET — BROKEN (AFT FLASHLIGHT) · airframe 41,695 hrs · 36,571 cycles

AFT EMERGENCY LED FLASHLIGHT MOUNTING/CHARGING BRACKET IS BROKEN.-C/A-COMPLETE:RAR FLASHLIGHT MOUNTING/CHARGING ASSY IAW EMB-145 AMM CH. 33-50-16.

Part: CRADLE — INOPERATIVE (FWD FLASHLIGHT) · airframe 41,641 hrs · 36,502 cycles

FWD CABIN FA EMERGENCY FLASHLIGHT WONT CHARGE. RESET FA EMERGENCY FLASHLIGHT CHARGER.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 40,678 hrs · 35,523 cycles

NR 4 EMERGENCY LIGHT STRIP WIRES BROKEN. C/A: R & R NR 4 FLOOR PROXIMITY LIGHT STRIP, IAW EMB145 AMM 33-50-12. OPERATIONS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (VIBRA SENSOR) · airframe 40,336 hrs · 35,196 cycles

WHEN N1 IN NR 1 ENGINE INCREASED OVER 75% IN CRUISE, 1 HP ENTERS AMBER RANGE. IN CLIMB ENTERS AMBER FOR A FEW SECONDS, GOES BACK IN GREEN AND BACK TO AMBER. MECH ENGINE PROB, NO EMERGENCY DECLARED. RESCUE FLT 9860 SENT TO PROTECT "TRANSFERRED TO NRWC 664-CMH-04960"-C/A-SEE NRWC NR 664-CMH-04960 FOR CORRECTIVE ACTION TAKEN. R & R LT ENGINE COMPRESSOR VIB SENSOR, IAW RR MM 77-41-10.

Part: CRADLE — INOPERATIVE (FLASHLIGHT) · airframe 39,865 hrs · 34,722 cycles

REAR PASSENGER FLASHLIGHT CRADDLE INOP-C/A-REMOVED AND REPLACED REAR PASSENGER FLISHLIGHT CRADDLE IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-000-801-A. OPC GOOD

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,833 hrs · 34,688 cycles

LH INTERIOR OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH INTERIOR OVERWING EMERGENCY LIGHT IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A OPC GOOD END

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,710 hrs · 34,583 cycles

FORWARD FLOOR PROXIMITY STRIP INOP-C/A-REMOVED AND REPLACED FORWARD FLOOR PROXIMITY STRIP IAW AMM 33-50-12. OPS CHECK GOOD.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 39,601 hrs · 34,492 cycles

MEL 2553 - AUTH# 03-83-C FWD FLIGHT ATTENDANT FLASHLIGHT BRACKET BROKEN-C/A-RAR FWD FLIGHT ATTENDANT FLASHLIGHT IAW 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECK GOOD. NO FURTHER DEFECTS FOUND AT THIS TIME. MEL RESTORED. END.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 39,574 hrs · 34,467 cycles

FOWARD FLIGHT ATTENDANT FLASHLIGHT BRACKET BROKEN.-C/A-DEFERRED FLASHLIGHT HOLDER FOR FWD FA LOCATION PER MEL 25-53 AUTH# 030083-C

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 39,534 hrs · 34,425 cycles

FLIGHT ATTENDANT FORWARD HANDHELD FLASHLIGHT INOP-C/A-REMOVED AND REPLACED FLIGHT ATTENDANT FORWARD HANDHELD FLASHLIGHT IAW 33-50-16

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,328 hrs · 34,259 cycles

DURING PS-1 CHECK, FOUND BOTH OVER THE WING EMERGENCY LIGHT INOP.-C/A-FOUND OVERWING EMERGENCY LIGHTS INOP. RAR LH AND RH EMERGENCY LIGHT LAMPS IAW EMB 145 AMM 33-50-07. DID NOT FIX. RAR EMERGENCY LIGHTS BATTERY AND CHARGER IAW EMB 145 AMM 33-50-07.DID NOT FIX. BATTERY CHARGER ASSY P/N 11-0049 S/N 19108; EMERGENCY BATTERY P/N 2013-1A S/N 104936. DEFERRED PER MEL 33-29. EXTERNAL OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED LH OVERWING EMERGENCY LIGHT IAW AMM 33-50-10 OPS CHECK GOOD MEL ITEM RESTORED. LH EMERGENCY LIGHT P/N 30-2510-3

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 39,168 hrs · 34,129 cycles

DURING PS-1 CHECK FOUND LH AND RH EMERGENCY OVER WING LIGHTS INOP-C/A-FOUND FUSE BLOWN ON #4 EMERGENCY BATTERY CHARGER. REMOVED AND REPLACED FUSE IAW CMM 25-60-03 OPS CHECK GOOD IAW AMM 33-50-00-700-801

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,042 hrs · 34,024 cycles

LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND CHARGER IAW AMM 33-50-04. OPC GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 39,016 hrs · 34,007 cycles

FA FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FA FLASHLIGHT IAW AMM 33-50-16 OPS CHECK GOOD IAW AMM 33-51-01

Part: WINDSHIELD WIPER — MALFUNCTIONED · airframe 38,938 hrs · 33,944 cycles

ON APPROACH TO ORD, UNEXPECTED PRECIPITATION WAS ENCOUNTERD. DUE THE MEL 30-19 WHICH PROHIBITS THE AIRCRAFT FROM OPERATING IN PRECIPITATION, THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT.-C/A-PERFORMED WIPER ARM PRESSURE ADJUSTMENT FO'S SIDE & OPERATIONAL CHECK OF WINDSHIELD WIPER FO SIDE .FOUND OPS CHECK GOOD.MEL ITEM RESTORED .PERFORMED OPERATIONAL CHECK OF FO'S WINDSHIELD WIPER SYS IAW EMB145 AMM 30-41-00.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,901 hrs · 33,902 cycles

BOTH EXTERNAL OVERWING AFT EMERGENCY LIGHTS INOP-C/A-T/S IAW EMB WIREING MANUAL 33-50-50, REMOVED AND REPLACED NUMBER 4 BATTERY AND CHARGER IAW W/C 33-700-19. OPC GOOD, NO FUTHER DEFECTS FOUND. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 103797

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,829 hrs · 33,829 cycles

DURING PS-1 CHECK, FOUND BOTH LH AND RH EXTERIOR OVERWING EMERGENCY LIGHTS INOP-C/A-REMOVED AND REPLACED BATTERY ASSEMBLY AND BATTERY CHARGER ASSEMBLY IAW AMM 33-50-04. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. CHARGEDR ASSY BATTERY P/N BA5-0933-901 S/N C01545

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 38,768 hrs · 33,782 cycles

OVERHEAD COCKPIT EMER LIGHTS INOP-C/A-REMOVED AND REPLACED OVERHEAD COCKPIT EMER LIGHT IAW AMM 33-50-05. OPS CHECK GOOD

Part: SOLENOID VALVE — FAULTY (NLG DOOR) · airframe 37,866 hrs · 33,088 cycles

SUPPLEMENTAL AT FL 360 CLIMBING TO FL 370 LOUD DRAG NOISE FROM FRONT OF AC APEARS NOSE LANDING GEAR DOOR CAME OPEN. C/A-RESET CIRCUIT BREAKER E21 PERFORMED GVI OF LANDING GEAR NO DEFECTS NOTED NO FIX. REMOVED AND REPLACED DOOR SOLENOID VALVE OPTS CHECK GOOD IAW AMM 32-33-01 COMPLIED WITH GEAR SWING IAW AMM 32-30-00.

Part: BEAM — CRACKED (NLG) · airframe 37,842 hrs · 33,061 cycles

AFT CROSSBEAM FOR NLG UPLOCK BOX HAS CRACK APPROX 1" IN LENGTH. -C/A-REMOVED AND REPLACED AFT CROSSBEAM IN NLG IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 37,842 hrs · 33,061 cycles

BAGGAGE DOOR LIFTING AND LOWERING MECHANISM FWD SUPPORT BRACKET IS CRACKED.-C/A-REMOVED AND REPLACED BAGGAGE DOOR LIFTING AND LOWER SUPPORT BRACKET IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 37,842 hrs · 33,061 cycles

BAGGAGE DOOR LIFTING AND LOWERING MECHANISM AFT SUPPORT BRACKET APPEARS TO BE CRACKED. -C/A-REMOVED AND REPLACED BAGGAGE DOOR LIFTING AND LOWERING AFT BRACKET IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (FRAME 10) · airframe 37,842 hrs · 33,061 cycles

FO'S SIDE FRAME 10 RT. SUPPORT BRACKET BELOW DV WINDOW LOWER SILL CRACKED APPROX. 1".-C/A-REMOVED AND REPLACED SUPPORT BRACKET ON FO'S SIDE FRAME 10 RT IAW SRM 51-40-02.

Part: CHANNEL — CRACKED (FRAMES 47-48) · airframe 37,842 hrs · 33,061 cycles

RT. OMEGA BEAM SUPPORT HAS 2 EA. CRACKS APPROX. 1/4"LONG EACH BETWEEN FRAMES 47-48RT.-C/A-REMOVED AND REPLACED RH OMEGA BEAM SUPPORTS 2 EA @ FR 47-48 IAW SRM 51-40-02. CLIP P/N 140-04213-603.

Part: SUPPORT BRACKET — CRACKED (LT A/C PACK) · airframe 37,842 hrs · 33,061 cycles

LH PACK VALVE SUPPORT BRACKET ANGLE IS CRACKED. REMOVED AND REPLACED LH PACK VALVE SUPPORT BRACKET ANGLE IAW SRM 51-40-02.

Part: DOOR FRAME — CORRODED (FRAMES 65-68) · airframe 37,842 hrs · 33,061 cycles

CARGO DOOR SILL IS CORRODED NEAR FRAME 67. DRILLED, COUNTERSUNK AND INSTALLED A NEW CARGO SILL IAW SRM 51-40-02.

Part: LIGHT — DAMAGED (CABIN) · airframe 37,842 hrs · 33,061 cycles

EMERGENCY LIGHT STRIP #2,#3,#5,#6,#7,AND #8 DAMAGED. C/A-COMPLETE:INSTALLED NEW EMERGENCY LIGHT STRIP ASSY ON #2,#3,#5,#6,#7,AND #8 ONTO FLOOR SIDEWALL ASSY IAW AMM 33-50-12.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 37,166 hrs · 32,481 cycles

PRESSURIZATION AUTO FAIL AT FL190 AND CAB ALT WARNING CAB ALT 10000 AND RAN PRESS AUTO FAIL QRH COULDNT PRESSURE DOWN IN MAN MODE. DESCENDED TO FL 010 AND SELECTED PRESS DUMP BUTTON. C/A-DEFERRED CABIN PRESSURIZATION AUTO/MANUAL MODES M PROCEDURES C/W MEL 21-19 AUTH 030252DM-C. C/W PRESSURIZATION CONTROL SYS. TEST BOTH AUTO AND MANUAL MODE IAW MM 21-31-00. OPS CHECK GOOD. NO DEFECTS NOTED. MEL ITEM RESTORED.

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 37,048 hrs · 32,395 cycles

E1 A/ICE FAIL ON EICAS-ENG AIR INLET STAYS OPEN. E1 A/ICE DEFERRED AS PER MEL 30-11 AUT 020727DM-C. M PROCEDURE C/W. C/W FIM TASK 30-21-00-810-801-A FOR ENG 1 A/ICE VLV FAIL ON CMC 2X. RAR ENG1 A/ICE VALVE IAW EMB AMM 30-21-01 AND ENG1 PRESSURE TRANSDUCER IAW EMB AMM 30-21-06. OPCS GOOD IAW ETN-EM-30-041, EMB AMM 30-00-00-700-802-A. OPC OF ENGINE A/I SYSTEM GOOD IAW EMB AMM 30-21-00. NO DEFECTS NOTED AT THIS TIME.

Part: PRESSURE SWITCH — FAILED (RIGHT) · airframe 36,962 hrs · 32,327 cycles

UNABLE TO PRESSURIZE ABOVE 10,000FT CAB ALT WENT TO 11,000FT-C/A-DEFERED AUTO AND MANUAL PRESSURIZATION M PROCEDURES C/W REF MEL 21-19 AUTH 020255DM-C. DURING T/S OF MEL 21-19 FOUND PBA PANEL SEAL TO BE TORN. COULD NOT PERFORM OPS CHECK DUE TO PACK 2 MEL. MEL ITEM REMAINS OPEN. M PROCEDURES C/W T/S PACK#2 OVLD IAW FIM 21-51-00-810-802-A FOUND BAD PACK OVER PRESSURE SWITCH, PACK SETDOWN SWITCH AND DUAL HEAT EXCHANGER. REMOVED AND REPLACED PACK SETDOWN SWITCH IAW AMM 21-51-07. PACK#2 MEL REMAIN OPEN DUE TO FURTHER T/S. T/S PERFORMED ON MEL 21-30 AUTH 020230D-C PACK 2 INOP. T/S ORIGINAL DISCREPANCY DUE TO PACK 2 OVLD MESSAGE MSG IAW EMB145 FIM TASK 21-51-00-810-802-A. DURING T/S FOUND BAD RH DUAL HEAT EXCHANGER. REMOVED AND REPLACED RH DUAL HEAT EXCHANGER IAW AMM EMB-145 21-51-02. OPS CHECK GOOD IAW EMB-145 AMM 21-51-00-700-802. DURING REMOVAL OF HEAT EXCHANGER FOUND DUCT DAMAGE. REMOVED AND REPLACED DUCT (IPC EMB-145 21-51-00 FIG 25 ITEM 192) IAW EMB-145 AMM PT 21-51-03.LEAK CHECK GOOD. REMOVED AND REPLACED PANEL SEAL ON GROUND CONNECT VALVE IAW EMB145 IAW AMM 21-22-04. PERFORMED OPS CHECK OF BOTH AUTO AND MANUAL PRESSURIZATION CONTROL SYSTEMS IAW EMB145 AMM 21-31-00. OPS CHECKS GOOD. M PROCEDURES C\W. MEL ITEM RESTORED. RH HEAT EXCHANGER.

Part: BRAKE — OVERHEATED (MLG) · airframe 36,608 hrs · 32,002 cycles

HIGHSPEED ABORT DUE TO BRAKE OVERHEAT ABORT AT 129KTS-C/A-PERFORMED MAIN BRAKE SYSTEM FUNCTIONAOL CK AND PHYSICAL CK OF MAIN TIRES AND BRAKES IAW EMB145 AMM 32-41-00. NO DEFECTSNOTED. DEFERED PER MEL 32-2. ALL MTX ACTIONS C/W

Part: INVERTER — INOPERATIVE (CABIN) · airframe 36,022 hrs · 31,477 cycles

DURING PS-1 CHECK, FOUND NR 2 AND NR 3 FLOOR EMERGENCY LIGHT STRIPS INOP. R&R NR 3 EMERGENCY LIGHT DC/AC INVERTER IAW AMM 33-50-11.

Part: SMOKE DETECTOR — NO TEST (AFT CARGO) · airframe 35,892 hrs · 31,349 cycles

CARGO EXTINGUISHER LIGHT DOES NOT TEST DURING FIRE TEST. REMOVED AND REPLACED THE FWD CARGO SMOKE DETECTOR IAW AMM 26-15-01, OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 35,641 hrs · 31,161 cycles

RT FWD BULKHEAD EMERGENCY LIGHT INOP AT ROW 3. R&R NR 3 EMER LIGHT DC/AC INVERTER IN REF TO AMM 33-50-11, AND OPS CHKED EMER LIGHTS OK IN REF TO AMM 33-50-00.

Part: PROXIMITY SENSOR — FAILED (LT MLG) · airframe 35,594 hrs · 31,114 cycles

LG AIR/GND FAIL CAUTION MESSAGE ON EICAS DURING CLIMB THROUGH 8,000FT. REMOVED AND REPLACED LT NR 1 & 2 WOW PROXIMITY SWITCHES OPTS CHECK GOOD IAW AMM 32-63-01 REFERENCE NRWC 664-MIA 03499 FOR WORK PERFORMED. PROXIMITY SENSOR P/N 80-057-01 S/N 45315 LHG2.

Part: ELECTRONIC UNIT — FAILED (LANDING GEAR) · airframe 35,590 hrs · 31,111 cycles

LG AIR/GND FAIL AFTER DEPARTURE IN CLIMB APPROX 4000' MSL GEAR SHOWED UP + LOCKED INDICATED NEGATIVE STICK SHAKER ON APPROACH/ ENROUTE. TROUBLESHOOTING PER FIM 32-63-00-810-804-A REVEALED POSSIBLE BAD LGEU REFERENCE TURNOVER ITEM 2 THIS NRWC. REMOVED AND REPLACED LANDING GEAR ELECTRONIC UNIT IAW AMM 32-32-01. OPS CHECK GOOD PER FUNTIONAL CHECK OF AIR/GROUND (WOW) SYSTEM SIMULATION AMM TASK 32-63-00-700-801-A. NO FURTHUR DEFECTS NOTED AT THIS TIME.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,410 hrs · 30,965 cycles

EMERGENCY LIGHT IN ROW 3 (B+C SIDE) DID NOT WORK. REMOVED AND REPLACED THE INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 35,141 hrs · 30,662 cycles

BOTH EXIT EMERGENCY LIGHTS AND TWO PROXIMITY LIGHT STRIPS ARE INOPERATIVE. UPON FURTHER INSPECTION FOUND THE CONNECTOR PLUG TO NR 3 EMERGENCY POWER SUPPLY TO BE DISCONNECTED. RECONNECTED IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: PRESSURE SWITCH — FAILED (RIGHT) · airframe 34,617 hrs · 30,163 cycles

DURING TAKEOFF ROLL, A NR 2 BLEED FAIL ACTIVATED ON EICAS. AN ABORT WAS INITIATED AT 80KTS. REMOVED AND REPLACED PRESURE SWITCH IAW AMM 36-11-07 AND E2 REGULATOR VALVE IAW AMM 36-11-05 OPS CHECKED GOOD.

Part: STATOR — DAMAGED (NR 4 BRAKE) · airframe 33,498 hrs · 29,026 cycles

NR 4 WHEEL BRAKE ASSY DAMAGED 1ST STATOR DUE TO PISTON OVERTRAVEL. REMOVED AND REPLACED THE BRAKE ASSY IAW 32-600-14

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 32,962 hrs · 28,577 cycles

EMERGENCY LIGHT AT 251DF HAS BROKEN WIRES. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,945 hrs · 28,559 cycles

AFT FLOOR PROXIMITY LIGHTING DOES NOT ILLUMINATE. REMOVED AND REPLACED THE BATTERY HOLDER AND BATTERY CHARGER ASSEMBLY IAW AMM 33-50-04, OPS CHECKED GOOD.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 32,945 hrs · 28,559 cycles

LEFT NR 1 EMERGENCY LIGHT WIRES PULLED OFF. REMOVED AND REPLACED THE LIGHT STRIP IAW AMM 33-50-12.

Part: DOOR — CORRODED (EMERGENCY EXIT) · airframe 32,945 hrs · 28,559 cycles

LEFT EMERGENCY EXIT DOOR HAS CORROSION ON BOTTOM EDGE AROUND RUBBER STOP. REPAIRED IAW ERS-EM-52MR-712

Part: SKIN — CRACKED (FRAME 79) · airframe 32,945 hrs · 28,559 cycles

CRACKS IN SKIN AT FRAME 79 BETWEEN STRINGERS 5 - 6L. REPAIRED THE SKIN IAW ERS-EM-53MR-2591

Part: YOKE — CRACKED (ENGINE MOUNT) · airframe 32,945 hrs · 28,559 cycles

LT ENGINE FORWARD LOWER YOKE CRACKED BEHIND ENGINE MOUNT. REMOVED AND REPLACED THE YOKE IAW EO EM-54MR-386.

Part: CROSSBEAM — CORRODED (FRAME 20) · airframe 32,945 hrs · 28,559 cycles

CORROSION ON CROSSBEAM AT FRAME 20. REMOVED AND REPLACED THE CROSSBEAM IAW SRM 53-21-10 AND ETN-EM-53-139.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,945 hrs · 28,559 cycles

RT FORWARD FUSELAGE EMERGENCY LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 32,834 hrs · 28,461 cycles

MAIN DOOR EMERGENCY LIGHT FAIRING DAMAGED. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT FAIRING OPC GOOD IAW EMB AMM 25-23-04

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,035 hrs · 27,699 cycles

LEFT OVERWING EXIT LIGHT INOPERATIVE. REPLACED THE LAMP, OPS OK IAW AMM 33-50-10

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,948 hrs · 27,621 cycles

CEILING EMERGENCY EXIT LIGHT AT SEAT ROWS 16 AND 17 INOPERATIVE. R & R CEILING EMERGENCY EXIT LIGHT LAMP AT SEAT ROWS 16 AND 17 IAW AMM 33-50-08. OPS CHECK GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 31,151 hrs · 26,890 cycles

PASSENGER CABIN AFT EMER FLASHLIGHT CRADLE IS BROKEN. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONAL CHECKED GOOD.

Part: CARBON SEAL — NOT REPORTED (ENGINE) · airframe 31,140 hrs · 26,878 cycles

A SLIGHT HINT OF OIL SMELL WHEN ICE PROTECTION SYS WAS ACTIVATED. TRANSFERRED TO NRWC 664-ORD-02423. THIS DISCREPANCY TRANSFERED. EM 1 NEXT LOG PAGE FOR AN INTENDED SFP. IAW NRWC 664-ORD-02423 FOR ADDITIONAL MX IFO. R & R NR 0 CARBON SEAL ASSEMBLY IAW R & R. MM72-25-25-000-801 & 72-25-25-400-801. OPPERATION IS CHECKED & LEAK CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 30,708 hrs · 26,495 cycles

FIRST OFFICERS EMER FLASHLIGHT HOLDER BROKEN. R & R FIRST OFFICERS EMER FLASHLIGHT HOLDER IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 30,138 hrs · 26,030 cycles

HYDRAULIC 1 LOW QTY PRESENTED ON EICAS IN FLIGHT. SHOWS QTY POINTER AMBER & AT AMBER THRESHOLD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 29,979 hrs · 25,873 cycles

CAPTAINS EMER FLASHLIGHT CRADLE BROKEN. R & R CAPTAINS EMER FLASHLIGHT ASSEMBLY IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,993 hrs · 25,044 cycles

LEFT OVERWING EMER LIGHT INOPERATIVE. R & R LT OVERWING EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 28,800 hrs · 24,894 cycles

AFT CABIN FLASHLIGHT WILL NOT STAY ON. R & R AFT CABIN FLASHLIGHT IAW TASK 33-50-16-000-801-A & TASK 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 28,103 hrs · 24,292 cycles

MAIN DOOR LIGHT FAILED FUNCTIONAL CHECK. R & R BATTERY HOLDER, BATTERY CHARGER & LIGHT ASSEMBLY IAW AMM 33-50-04 & 33-50-10. OPERATIONALLY CHECKED GOOD.

Part: CONNECTOR — BROKEN (CABIN) · airframe 28,103 hrs · 24,292 cycles

FOUND NR 8 FLOOR PROXIMITY LIGHT WIRES BROKEN CONNECTORS. REPAIRED NR 8 FLOOR PROXIMITY LIGHT WIRES IAW SWPM 20-00-03 PAGE 65.

Part: CONNECTOR — BROKEN (CABIN) · airframe 28,103 hrs · 24,292 cycles

FOUND NR 3 FLOOR PROXIMITY LIGHT WIRES BROKEN CONNECTORS. REPAIRED NR 3 FLOOR PROXIMITY LIGHT WIRES IAW SWPM 20-00-03 PAGE 65.

Part: SKIN — DENTED (FUSELAGE) · airframe 28,103 hrs · 24,292 cycles

FRAME 23 - 24 STRINGER 17R - 18R HAS MULTIPLE DENTS. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-967.

Part: FITTING — DAMAGED (LT AILERON) · airframe 28,102 hrs · 24,290 cycles

LEFT AILERON DAMPER FITTING DAMAGED. REMOVED & INSTALL DAMPER FITTING IAW EO EM-27MR-112 TDMI REPAIR.

Part: STRUCTURE — CRACKED (RT WING) · airframe 28,102 hrs · 24,290 cycles

RIGHT WING CTR BELLY ATTACHMENT FLANGE IS CRACKED. R & R RT WING CTR BELLY ATTACHMENT FLANGE IAW ERS-EM-5700-342.

Part: ESCAPE ROPE — FRAYED (COCKPIT) · airframe 28,102 hrs · 24,290 cycles

PILOTS ESCAPE ROPE FRAYED AT THE END. R & R PILOTS ESCAPE ROPE IAW AMM 25-60-07 & ETN-EM-25-392.

Part: PRESSURE SWITCH — FAILED (BRAKE SYSTEM) · airframe 28,102 hrs · 24,290 cycles

MAIN BRAKE HYD SUPPLY PRESS SWITCH FAILS MAIN BRAKE FUNCTIONAL TEST & REMAINS RED WHERE IT SHOULD BE GREEN. R & R RT MAIN BRAKE HYD SUPPLY PRESS SWITCH IAW AMM 32-41-04, EASI TORQUE WRENCH 7538.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,043 hrs · 24,240 cycles

DURING PS 2 INSPECTION FOUND EMER LIGHT SYS REAR NR 8, LAST SECTION FLOOR PROX STRIP INOPERATIVE. R & R EMER LIGHT STRIP FLOOR SECTION NR 8 IAW AMM 33-50-12. OPERATIONS CHECKED GOOD. MEL 33-30 RESTORED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,986 hrs · 24,192 cycles

LEFT & RIGHT OVERWING EMER LIGHTS INOPERATIVE. R & R NR 4 EMER LIGHT BATTERY & CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. EMER LIGHTING BATTERY PN 2013-1A & SN 68433.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,188 hrs · 23,544 cycles

EMERGENCY LIGHTS FLOOR STRIP FROM ROWS 12 TO 18 INOPERATIVE. R & R NR 6 INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 27,163 hrs · 23,523 cycles

EMERGENCY FLOOR STRIPS 12A - 18A ARE INOPERATIVE. R & R THE NR 4 EMER CHARGER & BATTERY HOLDER ASSEMBLY IAW WC 33-700-19. OPERATIONS CHECKED IAW WC 33-700-17, OPERATIONS CHECKED GOOD, NO FAULTS FOUND END.

Part: HANDLE — OUT OF POSITION (CABIN DOOR) · airframe 26,841 hrs · 23,211 cycles

FLIGHT ATTENDANT REPORTS THAT MAIN CABIN DOOR HANDLE IS SITTING ON A LEDGE MAKING IT DIFFICULT TO OPERATE. RE-INDEXED HANDLE IAW AMM 32-11-01. OPERATIONS CHECKED GOOD NO DEFECT NOTED.

Part: WIRE — DAMAGED (CABIN) · airframe 26,800 hrs · 23,182 cycles

EMER LIGHTS ARMED MSG INTERMITTENTLY. FOLLOWED FIM TASK 33-50-00 FOUND WIRE SHIELDING ON WIRES OF ATT CONTROL PANEL EXPOSED. REPAIRED WIRES IAW 20-21-00 WM 33-50-50- OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 26,208 hrs · 22,705 cycles

CAPTAIN'S FLASHLIGHT HOLDER BROKEN. R & R CAPTAIN'S FLASHLIGHT HOLDER IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 25,936 hrs · 22,483 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LAMP ON RT OVERWING EMERGENCY LIGHT IAW AMM 33-50-10-420-003-A00, OPERATIONS CHECKED OK.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,549 hrs · 22,181 cycles

ON FLIGHT 3278 THE CREW REPORTED THE FLIGHT ATTENDANT’S FLASHLIGHT WAS NOT WORKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. R & R CAPTAIN`S FLASHLIGHT ASSEMBLY IAW EMB 140 AMM 33-50-16 & OPERATIONAL CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,551 hrs · 21,346 cycles

THE CREW REPORTED THE AFT F/A FLASHLIGHT WAS INOPERATIVE. ACFT OK FOR SERVICE. R & R THE AFT FLASHLIGHT ASSY. OPS CHECKED GOOD IAW 33-50-16. ACFT RETURNED TO SERVICE.

Part: SILL — CORRODED (CARGO DOOR) · airframe 24,231 hrs · 21,089 cycles

DURING HEAVY CHECK, FOUND THE CARGO DOOR SILL HAS CORROSION. THE ACFT WAS REMOVED FROM SERVICE. R & R THE CARGO DOOR SILL IAW SRM 51-40-02. THE OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: SUPPORT BRACKET — CRACKED (PAX DOOR) · airframe 24,189 hrs · 21,051 cycles

PAX DOOR INNER HANDLE HSG SUPPORT BRACKET IS CRACKED. REPAIRED DAMAGED SUPPORT BOX IAW EM-52MR-250.

Part: WIRE HARNESS — INOPERATIVE (FUEL SYS) · airframe 24,095 hrs · 20,980 cycles

AFTER LEAVING DEPARTURE AIRPORT FUEL TANK TEMPERATURE WAS ABOUT 27C. HALF WAY THROUGH THE FLIGHT THE TEMPERATURE HAD DROPPED TO 7C. DECLARED AN EMERGENCY AND DIVERTED. ACFT LANDED WITHOUT INCIDENT. COMPLIED WITH CONTINUITY/ RESISTANCE, INTERNAL SHORTS AND SHORTS TO GROUND ON EXTERNAL ENGINE- INDICATING HARNESS FROM P11 TO J1018 ON DAU 2 IAW FIM 73-31-00-810-802 NO FAULTS FOUND INSPECTED HARNESS ASSY FOR CHAFFING ALSO NO FAULTS FOUND. REMOVED AND REPLACED THE EXTERNAL ENGINE CONTROL (A) HARNESS ON NR 2 ENGINE. OPS CHECKED GOOD IAW RR MM TASKS 76-11-20-000-802 AND 76-11-20-400-802. MEL ITEM RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 23,711 hrs · 20,654 cycles

DURING B INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT BASE IAW EMB 145 AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 23,629 hrs · 20,583 cycles

ON FLIGHT 3440 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RELAMPED FLASHLIGHT AS PER EMB MM 25-60-00. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DAU — INOPERATIVE (NR 2) · airframe 23,498 hrs · 20,477 cycles

FLIGHT 3334, CREW RECEIVED AN EICAS E1 FUEL LOW TEMP MESSAGE. CONTINUED TO MONITOR TEMPERATURE. REQUESTED DESCENT AND TEMPERATURE CONTINUED TO DECREASE. DECLARED AN EMERGENCY, COMPLIED WITH AOM VOL 1 PROCEDURES AND ELECTED TO DIVERT. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 DAU IAW AMM 31-41-00 AND OPS CHECKED GOOD IAW TASK 31-41-00-700-801-A. PERFORMED INSULATION TEST ON PINS A & B, A & C, AND B & C ON RT ENG FUEL TEMP SENSOR C/P P11 TO DAU NR 2 RACK. REF AMM 20-20-03 NO DEFECTS NOTED. RECONNECTED RIGHT ENGINE FUEL TEMP SENSOR C/P REF AMM 20-50-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,169 hrs · 20,192 cycles

DURING B INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,437 hrs · 19,616 cycles

DURING B INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT IAW EMB AMM TASK: 33-50-07-000-801-A, AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,437 hrs · 19,616 cycles

DURING B INSPECTION FOUND THE GALLEY CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY CEILING EMERGENCY LIGHT IAW EMB AMM TASK: 33-26-05-000-801-A, AND 33-26-05-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 22,437 hrs · 19,616 cycles

DURING B INSPECTION FOUND THE FLIGHT ATTENDANT’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT’S FLASHLIGHT BATTERY IAW EMB AMM TASK: 33-50-16-000-801-A, AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — CRACKED (CABIN) · airframe 21,593 hrs · 18,940 cycles

DURING B INSPECTIONS FOUND THE AFT CABIN FLASHLIGHT ASSEMBLY CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT ASSEMBLY IAW EMB-145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 21,536 hrs · 18,900 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT EMERGENCY FLOOR PROXIMITY LIGHT HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT EMERGENCY FLOOR PROXIMITY LIGHT IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 21,469 hrs · 18,848 cycles

DURING B INSPECTION, FOUND THE RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT OVERWING EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-07. THE OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,396 hrs · 18,786 cycles

DURING B INSPECTION, FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT LAMP. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-07. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 21,043 hrs · 18,515 cycles

DURING MAINTENANCE INSPECTION FOUND EMERGENCY FLOOR PATH PROXIMITY STRIP ELECTRICAL CONNECTOR BROKEN. REMOVED AND REPLACED THE EMERGECNY LIGHT STRIP IAW 33-50-12 OPC GOOD MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 20,857 hrs · 18,368 cycles

DURING B-INSPECTION FOUND THE CHARGING STATUS LIGHT ON EMERGENCY FLASHLIGHT ABOVE FLIGHT ATTENDANT SEAT IS INTERMITTENT. WHEN FLASHLIGHT IS MOVED SLIGHTLY STATUS LIGHT EXTINGUISHES. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND FAULT TO BE WITH CRADLE ASSEMBLY. REMOVED AND REPLACED AND CHECKED CRADLE ASSEMBLY IAW EMB145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,824 hrs · 18,340 cycles

DURING B-INSPECTION FOUND THE RIGHT AFT EXTERIOR EMERGENCY LAMP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT EXTERNAL EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,765 hrs · 18,294 cycles

DURING B-INSPECTION FOUND THE EXTERNAL EMERGENCY LIGHT LAMP OF RIGHT SIDE CENTER FAIRINGS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EXTERNAL EMERGENCY LAMP IAW AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 20,523 hrs · 18,102 cycles

ON FLIGHT 2998 THE CREW REPORTED THE AMBER EMERGENCY EXIT STRIP ON FLOOR IS MISPLACED, IT IS NOT IN THE EMERGENCY EXIT ROW. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED EMERGENCY STRIP TO ROW 6 IN THE RIGHT POSITION IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (CABIN) · airframe 20,403 hrs · 18,012 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE FLASHLIGHT BASE BROKEN ABOVE FLIGHT ATTENDANT’S SEAT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FLASHLIGHT BASE AT FLIGHT ATTENDANT’S SEAT IAW 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 20,329 hrs · 17,955 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FIRST OFFICER’S FLASHLIGHT IS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT AND CHARGER ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RECEPTACLE — CORRODED (LAVATORY) · airframe 19,519 hrs · 17,315 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LAVATORY BUCKET HAS 2 SMALL SPOTS OF CORROSION RIGHT AROUND THE VAVLE BODY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED CORROSION ON LAVATORY BUCKET IAW EO EM-53MR-1867. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 19,426 hrs · 17,237 cycles

ON FLIGHT 4395 THE CREW REPORTED THE LEFT ENGINE HAD EXCESSIVE SMOKE AFTER SHUTDOWN AFTER 10 MINUTES STILL HAD SMOKE EMITTING FROM EXHAUST. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED E1 IAW AE MTX WC 71-000-00. THE OPERATIONAL CHECKS AND LEAK CHECKS WERE GOOD. NO DEFECTS NOTED AT THIS PRESENT TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PITOT LINE — INOPERATIVE (NR 1) · airframe 18,980 hrs · 16,871 cycles

ON FLIGHT 4022 DURING CRUISE THE CAPTAINS AIRSPEED AND ALTIMETER WENT TO ZERO AND THE ATTITUDE INDICATOR WAS NOT SHOWING THE CORRECT ATTITUDE. THE CREW DECLARED AN EMERGENCY. ALL INDICATIONS ON THE CAPTAINS SIDE RETURNED. THE AIRCRAFT LANDED WITHOUT INCIDENT AT THE DESTINATION. THE AIRCRAFT WAS REMOVED FROM SERVICE. DRAINED PITOT LINE NR 1 AND CLEARED WITH NITROGEN IAW EMB-145 AMM 34-13-00. REMOVED AND REPLACED THE NR 1 PITOT HOSE. THE LEAKAGE CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,008 hrs · 14,616 cycles

DURING MAINTENANCE BASE PS2 VISIT FOUND THE RIGHT OVERWING EMERGENCY LIGHT TO BE OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (LT WING) · airframe 14,586 hrs · 13,536 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT WING LOWER SKIN TO BE DENTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE LEFT WING LOWER SKIN IAW EO EM-57MR-421. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BUSHING — DAMAGED (LT WING) · airframe 14,586 hrs · 13,536 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT LOWER SPAR CAP INBOARD HOLE BUSHING DAMAGED IN TORQUE BOX 1. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE LEFT LOWER SPAR CAP INBOARD HOLE BUSHING IN TORQUE BOX 1 IAW EO EM-57MR-452. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 14,586 hrs · 13,536 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE CARGO DOOR OPEN/CLOSE PULLEY CABLE BRACKET CRACKED AT THE UPPER FORWARD FITTING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICEABLE CARGO DOOR OPEN/CLOSE PULLEY BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 14,586 hrs · 13,536 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE CARGO DOOR TORSION RODS FORWARD BRACKET CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR TORSION RODS FORWARD BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 14,586 hrs · 13,536 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE SERVICE DOOR CENTER SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE SERVICE DOOR CENTER SILL NUT PLATE WAS REPAIRED IAW EMB SRM 53-21-02, 51-40-02 AND CPM 51-21-06. THE CORROSION LEVEL WAS RECORDED AS A LEVEL ONE CORROSION ISSUE, HOWEVER THE REPAIR WAS CONSIDERED TO BE A MAJOR REPAIR. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ELECTRICAL SYS — FIRE · airframe 13,390 hrs · 12,623 cycles

ON FLIGHT 3464 AT GATE, CREW REPORTED FIRE AT FORWARD ENTRY RIGHT ABOVE FLIGHT ATTENDANT FLASHLIGHT AT TOP OF DOOR FRAME. CREW SHUT DOWN ALL POWER TO ACFT AND FLAME EXTINGUISHED. NO CIRCUIT BREAKER POPPED OR OTHER PROBLEMS NOTED. AIRCRAFT REMOVED FROM SERVICE. JET BRIDGE GPU WAS SHORTED AND WHEN PULL UP TO ACFT, ACFT ACTED AS THE GROUND REMOVE GPU AND JET BRIDGE ACFT INSPECTED AND ALL SYSTEM CHECK NORMAL. AIRCRAFT FERRIED TO DFW FOR REPAIR OF INSIDE PANELS AND TRIM. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 11,849 hrs · 11,280 cycles

FLIGHT 4292 - ON CLIMBOUT CREW OBSERVED SMOKE IN THE CABIN AND COCKPIT. CREW ELECTED TO RETURN TO CMH. AIRCRAFT LANDED AND TAXIED SAFELY TO THE GATE WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER ONE ENGINE IAW WORK CARD 71-000-00. GROUND OPERATIONAL AND LEAK CHECKS GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: FAN — FAILED (CABIN)

CREW REPORTS THAT ON APPROACH, THE CABIN WAS FILLING UP WITH A HAZY SMOKE. UPON GATE ARRIVAL THE CABIN WAS QUITE HAZY. APU ON UNTIL AFTER LANDING AND THERE WAS NO CHANGE IN THE CABIN. ACFT REMOVED FROM SERVICE. C/A REMOVED AND REPLACED BOTH RECIRC FANS AND EXHAUST, OPERATION CHECKED GOOD. ACFT RETURNED TO SERVICE. (K)

Part: FAN — SMOKE

ON FLIGHT 4433, CREW REPORTS THAT ON APPROACH,, THE CABIN WAS FILLING UP WITH A HAZY SMOKE. UPON GATE ARRIVAL THE CABIN WAS QUITE HAZY. APU ON UNTIL AFTER LANDING AND THERE WAS NO CHANGE IN THE CABIN. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH RECIRC FANS AND EXHAUST, OPERATION CHECKED GOOD. ACFT RETURNED TO SERVICE. (K)

Part: FUEL CONTROL — FAULTY (APU) · airframe 10,361 hrs · 9,771 cycles

ON FLIGHT 4101, CREW REPORTED STRONG FUEL SMELL WHEN APU POWERING PACKS AND OIL SMELL WHEN ENGINES POWERING PACKS. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED APU FUEL CONTROL IAW EMB 145 AMM 49-32-01-000-801-A 49-32-01-400-801-A LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ACM — ODOR · airframe 10,361 hrs · 9,771 cycles

ON FLIGHT 4101, CREW REPORTED A STRONG FUEL ODOR WHEN APU IS POWERING PACKS AND OIL ODOR WHEN ENGINES POWERING PACKS.

Part: CAP — CORRODED (NOSE GEAR) · airframe 9,613 hrs · 9,089 cycles

DURING MBV, THE NOSE LANDING GEAR WAS INSPECTED (CPC CARD NUMBER 53-200-06) AND FOUND CORROSION ON THE LANDING GEAR CAP. REMOVED AND REPLACED WITH NEW IAW EMB AMM AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE SWITCH — FAILED (RUDDER) · airframe 9,718 hrs · 9,167 cycles

EMERGENCY DECLARED, RUDDER 1/2 INOP IN FLIGHT LANDED SAFELY. REMOVED AND REPLACED NR 1 RUDDER PRESSURE SWITCH IAW EMB 145 AMM 27-23-04. OPS CHECK AND LEAK CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 9,613 hrs · 9,089 cycles

DURING MBV INSPECTION, THE BAGGAGE DOOR LOWER SILL WAS FOUND TO BE CORRODED. REPLACED BAGGAGE DOOR LOWER SILL PER EMB SRM 145/1142 REV 38 CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 8,607 hrs · 8,138 cycles

EMERGENCY LIGHT SYSTEM MALFUNCTION. REMOVED AND REPLACED FOUR POWER PACKS IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

FOUND EMERGENCY LIGHTS OUT AT FLOOR STRIPS FROM 7A FORWARD. ALSO, EMERGENCY EXIT SIGN OUT AND EMERGENCY EXIT IDENT OUT AT THE SERVICE. RAI BATTERY POWER SUPPLY NR 2, OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUTOUT. PREPARED A DOUBLER, FILLER, 2 SHIMS AND PLATE. REPAIR DONE IAW EMB. (K)

Part: SILL — CORRODED (SERVICE DOOR)

THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED THE CORRODED AREA. CLEANED AND TREATED THE BLENDED AREA AND FILLED WITH EPOXY RESIN EA934A. FABRICATED 2 REPAIR DOUBLERS. REPAIR DONE IAW EMB SRM. (K)

Part: ENGINE — DAMAGED (NR 2) · airframe 2,496 hrs · 2,477 cycles

DURING CLIMB AND CRUISE, NR 2 ENGINE HIGH ITT. FOUND CUSTOMER SERVICE MANIFOLD HAD COME OFF ENGINE. REPLACE NR 2 ENGINE ASSY. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE.