N679AE

Part: RELAY — FAULTED (ANTI-ICE SYS) · airframe 47,604 hrs · 44,031 cycles

WING AND STAB ANTI-ICE FAIL MSG IN FLIGHT. REMOVED AND REPLACED RELAYS K0361 AND K0542 IRT SWPM 20-13-03. OPS CHECK GOOD IAW AMM A/I SYS OPS CHECK 30-00-00. AC OK FOR SERVICE.

Part: PRESSURE SWITCH — FAULTED (ZONE 200) · airframe 47,528 hrs · 43,943 cycles

DURING T/O ROLL. MASTER WARNING ILLUMINATED WITH NO T/O BRAKE AURAL MESSAGE. R & R PARK BRAKE PRESSURE SWITCH IAW AMM 32-44-07 OPS CHECK GOOD LEAK CHECK GOOD. A/C OK FOR SERVICE

Part: INVERTER — INOPERATIVE (ZONE 200) · airframe 47,287 hrs · 43,653 cycles

FWD FACING EMERGENCIY EXIT ROW SIGN NOT ILLUMINATING. RAR EMERGENCY LIGHT INVERTER #6

Part: A/C PACK — ODOR · airframe 46,991 hrs · 43,317 cycles

AFTER SUSPECTED LIGHTNING STRIKE MUSTY SMELL FROM PACKS IN FLIGHT DECK. RAN PACK 1 & 2 FOR 10 MINUTES. COULD NOT DUPLICATE MUSTY SMELL COMING FROM PACKS.OK FOR SERVICE AT THIS TIME.

Part: A/C PACK — ODOR · airframe 46,991 hrs · 43,317 cycles

AFTER SUSPECTED LIGHTNING STRIKE MUSTY SMELL FROM PACKS IN FLIGHT DECK. FROM PACKS IN FLIGHT DECK. RAN PACK 1 & 2 FOR 10 MINUTES. COULD NOT DUPLICATE MUSTY SMELL COMING FROM PACKS.OK FOR SERVICE AT THIS TIME.

Part: A/C PACK — ODOR · airframe 46,991 hrs · 43,317 cycles

AFTER SUSPECTED LIGHTNING STRIKE MUSTY SMELL FROM PACKS IN FLIGHT DECK. FROM PACKS IN FLIGHT DECK. RAN PACK 1 & 2 FOR 10 MINUTES. COULD NOT DUPLICATE MUSTY SMELL COMING FROM PACKS.OK FOR SERVICE AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (RUDDER) · airframe 46,942 hrs · 43,256 cycles

ABORTED TAKE OFF DUE TO RUD SYS 1 INOP CAUTION MSG R & R #100 AND AT 00 RUDDER PRESSURE SWITCHES IRT AMM 27-23-04. OPS CHECK OF RUDDER SYSTEMS SATISFACTORY IRT AMM 27-23-00. BOTH SYSTEMS BLED AS NECCESSARY. NO ABNORMAL MSGS SEEN DURING HIGH POWER CHECK. OK FOR SERVICE AT THIS TIME.

Part: ADC — FAILED (NR 1) · airframe 45,666 hrs · 41,866 cycles

ADC 1 FAIL AT ROTATION DURING TAKE OFF. FACT 25DEC24 13:21 CLT R&R'D AIR DATA COMPUTER #1 IAW 34-15-01 AMM EMB 145. LEAK CHECK AND OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSERS) · airframe 45,551 hrs · 41,742 cycles

E2 REV DISAGREE ON TO ROLL, ENG 1 OR 2 REV DISAGREE MESSAGES FACT 07DEC24 21:29 RIC DEINHIBITED #200 TR IRT AMM 78-31-01-980-801-A CYCLED #200 TR MULTIPLE TIMES IRT AMM 78-31-01-940-801/802-A NO DEFECTS NOTED NO CMC MESSAGES ASSOCIATED W/TR'S AC OK FOR SERVICE AT THIS TIME CLEAR MEL

Part: UNKNOWN — OVERHEATED · airframe 45,416 hrs · 41,593 cycles

BURNING RUBBER SMELL IN COCKPIT WHILE ON GROUND. WITH DOOR OPEN, APU RUNNING AND BOTH PACKS RUNNING FACT 09NOV24 11:56 CLT UPON FURTHER INSP FOUND BTC K0081 & SBC K0085 OVER-HEATING. R/R'D BTC K0081 IAW AMM 24-60-01 & R/R'D SBC K0085 IAW AMM 24-60-02. OPS CHECK GOOD. NO BURNING SMELL NOTED. AIRCRAFT OK FOR SERVICE AT THIS TIME.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,154 hrs · 41,303 cycles

53-2418 SHEAR CLIP CORRODED AT FR62 BTW STR19-20R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SKIN — CRACKED (ZONE 300) · airframe 45,154 hrs · 41,303 cycles

55-2341 RH SKIN CRACKED ON BOTTOM OF VERT STAB AFT OF SPAR 3. REPAIRED IAW EO1-55-24-0518

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 45,154 hrs · 41,303 cycles

53-2256 CRACKED ANGLE ON LH FLOOR BEAM OB SIDE AT FR66. RAR ANGLE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,154 hrs · 41,303 cycles

53-2198 SHEAR CLIP CRACKED AT FR71 BTW STR6-10L. RAR SHEAR CLIP IAW EO1-05-24-0496

Part: SHEAR TIE — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,154 hrs · 41,303 cycles

53-2218 CORROSION ON RH GUSSET BTW FR59-61. RAR GUSSET IAW SRM 51-40-02

Part: POST — CRACKED (ZONE 200) · airframe 45,154 hrs · 41,303 cycles

53-2187 RF1, POST BETWEEN CARGO DOOR LWR BEAM AND LH OMEGA BEAM IS CRACKED. RAR LWR BEAM IAW SRM 51-40-02

Part: MECHANISM — CRACKED (CARGO DOOR) · airframe 45,154 hrs · 41,303 cycles

53-2200 BAG DOOR SUPPORT MECHANISM CRACKED AT BTW FR67-68 STR5R. RAR MECHANISM SUPPORT IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,154 hrs · 41,303 cycles

53-2205 FF2, ANGLE CRACKED AT FR10 BTW STR9-10L. RAR ANGLE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,154 hrs · 41,303 cycles

53-2203 SHEAR CLIP CRACKED AT FR67 BTW STR6-7L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,154 hrs · 41,303 cycles

53-2191 SHEAR CLIP CRACKED AT FR67 BTW STR6-7R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,154 hrs · 41,303 cycles

53-2206 SHEAR CLIP CRACKED AT FR61 BTW STR6-7L. RAR SHEAR CLIP IAW EO1-05-24-0496

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,154 hrs · 41,303 cycles

53-2192 SHEAR CLIP CRACKED AT FR68 BTW STR6-10R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,154 hrs · 41,303 cycles

53-2225 RH FLOOR SUPPORT CORRODED AT BTW FR59-61. REPAIRED IAW EO1-53-24-0494

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,154 hrs · 41,303 cycles

53-2196 SHEAR CLIP CRACKED AT FR73 BTW STR8-10L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,154 hrs · 41,303 cycles

53-2209 SHEAR CLIP CRACKED AT FR61 BTW 6-7R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,054 hrs · 41,303 cycles

53-2194 SHEAR CLIP CRACKED AT FR72 BTW STR7-10R. RAR SHEAR CLIP IAW EO1-53-24-0496

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,154 hrs · 41,303 cycles

53-2202 SHEAR CLIP CRACKED AT FR68 BTW STR6-9L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,154 hrs · 41,303 cycles

53-2186 SHEAR CLIP CORRODED AT FR64 BTW STR15-18L. REPAIRED IAW EO1-53-24-0517

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,154 hrs · 41,303 cycles

53-2168 CF3, LH IB OMEGA BEAM ANGLE CRACKED ATR BTW FR47-50. REPAIRED IAW EO 1-53-24-0490

Part: ANGLE — CRACKED (ZONE 100) · airframe 45,154 hrs · 41,303 cycles

53-2166 ANGLE CRACKED AT FR66 STR18L. RAR ANGLE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,154 hrs · 41,303 cycles

53-2151 CF1, RH SHEAR CLIP CRACKED AT FR16 BTW STR16-17R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: PROFILE — CRACKED (ZONE 500) · airframe 45,154 hrs · 41,303 cycles

57-2177 LH WING STUB AREA, UPPER PROFILE CRACKED AT BTW STA 16000 AND 16783.5. RAR PROFILE IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,154 hrs · 41,303 cycles

53-2150 CF1, LH OMEGA BEAM CRACKED AT FR23. REPAIRED IAW EO 1-53-24-0537

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,154 hrs · 41,303 cycles

53-2167 CF3, RH IB OMEGA BEAM ANGLE CRACKED AT BTW FR47-50. REPAIRED IAW EO1-53-24-0489

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,154 hrs · 41,303 cycles

53-2152 CF1, RH SHEAR CLIP CRACKED AT FR15 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,154 hrs · 41,303 cycles

53-2098 SHEAR CLIP CRACKED AT FR24 BTW 15-16L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,154 hrs · 41,303 cycles

53-2067 SHEAR CLIP CRACKED AT FR27 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,154 hrs · 41,303 cycles

53-2094 SHEAR CLIP CRACKED AT FR26 BTW STR15-16L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,154 hrs · 41,303 cycles

53-2070 SHEAR CLIP CRACKED AT FR24 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,154 hrs · 41,303 cycles

53-2068 CF2, SHER CLIP CRACKED AT FR26 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,154 hrs · 41,303 cycles

53-2069 SHEAR CLIP CRACKED AT FR25 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SKIN — CRACKED (ZONE 200) · airframe 45,154 hrs · 41,303 cycles

53-2033 CRACK AT RH RF1 FR75 BTW STR2-3R. REPAIRED IAW EO1-53-24-0516

Part: SUPPORT — CRACKED (ZONE 100) · airframe 45,154 hrs · 41,303 cycles

53-2034 LH WING TO FAIRING SUPPORT CRACKED AT BTW FR48-49. REPAIRED IAW E01-53-24-0496

Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,154 hrs · 41,303 cycles

53-2020 CORROSION ON CARGO DOOR CUTOUT LWR BEAM. RAR BEAM IAW SRM 51-40-02

Part: CUP — CORRODED (ZONE 900) · corrosion level 2 · airframe 45,154 hrs · 41,303 cycles

53-2016 TOILET WASTE CUP CORRODED. RAR CUP IAW SRM 51-40-02

Part: SKIN — GOUGED (ZONE 100) · airframe 45,154 hrs · 41,303 cycles

53-2015 GOUGE ON EXTERNAL SKIN AT FR68 BTW STR15-16L. REPAIRED IAW EO1-53-24-0520

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO) · airframe 44,775 hrs · 40,867 cycles

BAG EXTG PUSH BUTTON ILLUMINATED DURING DESCENT BETWEEN FL 240-150. NO EICAS BAGG SMOKE MSG. NO INDICATION OF FIRE THROUGH PEEPHOLE. INSPECTED BAG BAY AND NO DAMAGE NOTED. PERFORMED FIRE DETECTION OPS CHECK IAW AMM 26-10-00. OPS CHECK GOOD. R&R FIRE PANEL IAW 23-00-01 AND RELAY K0629 IAW AMM 20-13-02 AS MX PRECAUTION. A/C OK FOR SERVICE. PER MOC REMOVE AND REPLACE BOTH BAG BAY SMOKE DETECTORS. R&R BOTH BAG BAY SMOKE DETECTORS IAW EMB 145 MM 26-15-01. OPS CHECK GOOD OK FOR SERVICE

Part: CONTROL PANEL — FAULTED (EXTINGUISHER) · airframe 44,763 hrs · 40,858 cycles

BAG EXTG PUSH BUTTON ILLUMINATED DURING DESCENT BETWEEN FL 240-150. NO EICAS BAGG SMOKE MSG. NO INDICATION OF FIRE THROUGH PEEPHOLE. FACT 17MAY24 00:27 PHL INSPECTED BAG BAY AND NO DAMAGE NOTED. PERFORMED FIRE DETECTION OPS CHECK IAW AMM 26-10-00. OPS CHECK GOOD. R&R FIRE PANEL IAW 23-00-01 AND RELAY K0629 IAW AMM 20-13-02 AS MX PRECAUTION. A/C OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,881 hrs · 39,841 cycles

RUDDER 1 INOP MESSAGE ON EICAS AT 60 KNOTS. FACT 04DEC23 16:40 MDT R+R RUD 1 PRESSURE SWITCH AND RELAYS K0365/K0364 IRT AMM 27-23-04 AND SWPM 20-13-03. OPS CHECK SATISFACTORY AT THIS TIME

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,241 hrs · 39,147 cycles

ON APPROACH WITH FLAPS SELECTED TO 45, LANDING GEAR AURAL WARNING, WITH GEAR INDICATING DOWN AND LOCKED. ENERGENCY DECLARED FACT 10JUN23 08:15 BUF R/R AWU IAW AMM 31-51-01 OPS HECK GOOD PERFORMED AIR/GND SYS OPS CHECK AND LANDING GEAR WARNING SYS OPS CHECK IRW AMM32-63-00 AND 32-62-00 OPS CHECK GOOD OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,882 hrs · 38,740 cycles

AT GATE WITH W/S HEAT SELECTED OFF STEAM/SMOKE SEEN AT OUTSIDE BOTTOM OF W/S WITH A BURNING SMELL IN FLT DECK HISTORY: NONE FACT 23MAR23 13:53 YUL INSP AND FOUND TO BE STEAM AT OUTSIDE OF A/C AND NO UNUSUAL SMELL ON FLIGHT DECK

Part: INVERTER — INOPERATIVE (ROW 3) · airframe 41,951 hrs · 37,730 cycles

ROW 3 VERTICAL EMERGENCY LIGHT PLACARD INOP-C/A-RAR ROW 3 VERTICAL EMERGENCY INVERTER IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. OPC GOOD. END.

Part: LAMP — INOPERATIVE (MAIN DOOR) · airframe 41,951 hrs · 37,730 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: LAMP — INOPERATIVE (LH) · airframe 41,446 hrs · 37,189 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR THE LH OVERWING EMERGENCY LT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECK GOOD. END.

Part: NONE — BROKEN (AFT) · airframe 41,361 hrs · 37,091 cycles

AFT CABIN EMERGENCY FLASH LIGHT BRACKET BROKEN-C/A-RAR AFT CABIN EMERGENCY FLASH LIGHT IAW ASTRONICS CMM 25-60-14

Part: NONE — NONE · airframe 41,065 hrs · 36,749 cycles

LH LATERAL PANEL EMERGENCY LIGHT INOP-C/A-RAR LH LATERAL PANEL EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD.

Part: NONE — NONE · airframe 40,901 hrs · 36,556 cycles

AFT CABIN EMEERGENCY FLASH LIGHT CHARGING CRADLE LIGHT NOT ILLUMINATING-C/A-INSTALLED REGULAR FLASH LIGHT D SIZE BATTERY FOR REAR FA. ITEM DEFERRED. (M) COMPLY WITH

Part: NONE — NONE · airframe 40,829 hrs · 36,469 cycles

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

Part: NONE — NONE · airframe 40,829 hrs · 36,469 cycles

LH OVER WING EMERGENCY LIGHT INOP-C/A-RAR LH OVER WING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. NO DEFECTS NOTED. END.

Part: NONE — NONE · airframe 40,813 hrs · 36,449 cycles

LH EMERGENCY LIGHT INOP-C/A-RAR LH EMERGENCY LIGHT IAW AMM 33-50-10 OPS CHECK GOOD

Part: NONE — NONE · airframe 40,736 hrs · 36,364 cycles

LH AILERON PCA ATTACHMENT FITTING ON AILERON HAS MULTIPLE MIGRATING BUSHINGS.-C/A-INSTALLED NEW LH AILERON PCA FITTING IAW EO-EM-27MR-112.

Part: NONE — NONE · airframe 40,663 hrs · 36,275 cycles

PRESSURIZATION ISSUE. DECLARED EMERGENCY. LANDED NORMALLY. PACK 1 VLV FAIL AFTER TAKEOFF. LOUD NOISE HEARD IN CABIN. RESET PACK 1 AND PACK 2 VLV CLOSED EICAS MESSAGE POSTED. RESET PACK 2, LOST ALL PRESSURIZATION. COMPLETED FLIGHT AT 10,000 FT."TRANSFERRED TO NRWC 679-ABI-05638" R. SHERWOOD 696918-C/A-REMOVED AND REPLACED R/H ACM DUCT FROM THE DTCV TO THE HEAT EXCHANGER, REMOVED AND REPLACED BOOTS AND CLAMPS ON LH AND RH ACM DUCT FROM THE DTCV TO THE HEAT EXCHANGER,PEFORMED AIRCRAFT PRESSURIZATION OPC GOOD SEE NRWC 679-ABI-05638 FOR CORRECTIVE ACTION

Part: NONE — NONE · airframe 40,658 hrs · 36,269 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT PROTECTICVE LENS CRACKED-C/A-RAR SERVICE DOOR EXTERNAL EMERGENCY LIGHT LENS IAW EMB 145 AMM 33-50-09.

Part: NONE — NONE · airframe 40,528 hrs · 36,116 cycles

REF LOG PAGE 4489946 MEL 33-23 AUTH# 09-375-C . ROW 16 FLOOR PROX LIGHTING INOP-C/A-FOUND FLOOR PROXIMITY EMERGENCY LIGHT #7 TO HAVE SPLICE SP9114 BROKEN. INSTALLED NEW SPLICE IAW SWPM 20-21-00. OPS CHECK GOOD. TRANSFERRED TO AML 4489950 ITEM #1.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,318 hrs · 35,866 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EXTERNAL EMERGENCY LIGHT IAW EMB145 AMM 33-50-09. OPS CHECK GOOD.

Part: FIRE WARNING — ACTIVATED (CARGO BAY) · airframe 39,358 hrs · 34,849 cycles

BAGGAGE SMOKE WARNING MESSAGE ON APPROACH FIRE BOTTLE DISCHARGE EMERGENCY DECLARED-RE-ENTER MEL 26-09 AUTH #020234D-C-C/A-RAR BAGGAGE COMPARTMENT FIRE BOTTLES IAW AMM 26-23-01 OP CHECK GOOD IAW AMM 26-15-00. MEL RESTORED.

Part: CRADLE — BROKEN (FWD FLASHLIGHT) · airframe 39,322 hrs · 34,814 cycles

FA EMERGENCY FLASHLIGHTS AND HOLDER HOLDER BROKEN PLACARDED BY:<CREW ID:<635971 LOGPAGE: 4721919 ITEM: 1 . RESTORATION OF MEL ITEMSMEL 2553 - AUTH# 02-71-C FWD -C/A-REMOVED AND REPLACED FWD FLIGHT ATTENDANT FLASH LIGHT HOLDER IAW EMB 145 AMM 33-50-16 MEL ITEM RESTORED.

Part: CRADLE — BROKEN (FWD FLASHLIGHT) · airframe 39,315 hrs · 34,808 cycles

FWD FA EMERGENCY FLASHLIGHT HOLDER BROKEN-C/A-FLIGHT CREW PLACARDED FWD FA EMERGENCY FLASHLIGHT HOLDER. M PROCEDURES C/W. MEL 25-53 AUTH 020071-C

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 38,847 hrs · 34,341 cycles

SEAT 3 B/C EMERGENCY EXIT SIGN INOPERABLE. C/A: T/S SEAT 3 B/C EMERGENCY EXIT SIGN, IAW FIM TASK 33-50-00-810-804-A FOUND BACKPLATE ON CANNON PLUG TO BE LOOSE. OPERATIONS CHECK GOOD, NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,535 hrs · 34,021 cycles

RIGHT CABIN EMERGENCY DOOR TOP EMERGENCY LIGHT OUT. R & R THE RIGHT CABIN EMERGENCY DOOR TOP EMERGENCY LIGHT IAW AMM 33-50-14 NO OTHER DEFECTS NOTED AT THIS TIME

Part: PRESSURE SWITCH — MALFUNCTIONED (BRAKE SYSTEM) · airframe 38,480 hrs · 33,961 cycles

REJECTED TAKEOFF EICAS WARNING "T/O CONFIG BRAKE" BRAKE WAS OFF. R&R PRESSURE SWITCH IAW AMM 32-44-07. OPC & LEAK CHECK GOOD AT THIS TIME & AMM 31-51-00.

Part: HOSE — DISCONNECTED (AC BAY) · airframe 38,287 hrs · 33,777 cycles

DURING CLIMB THE AIRCRAFT FAILED TO PRESSURIZE. PACK 2 CLSD AND BLEED 2 CLSD AFTER TAKE-OFF -- CYCLED, THEM PACK2 & BLEED 2 WERE OPEN -- THEN ABOUT 5 SECONDS LATER PACK 1-2 CLOSED POSTED -- RAN QRH CHECKLIST: GOT PACK 1 BACK EVENTUALLY, BUT NOT PACK 2-C/A-FOUND HOSE DISCONECTED AT #2 PACK AT AT DUAL TEMP CONTROLL VALVE(LARGE HOSE FWD POSITION). REMOVED AND REPLACED HOSE . GROUND RAN OPS CHECK OF BOTH PACKS GOOD IAW ETN -EM-21-056 AND AMM P.T. 21--60-01

Part: SWITCH — FAILED (AC BAY) · airframe 38,129 hrs · 33,608 cycles

SUPPLEMENTAL PACK 2 OVHT AND PACK 2 OVLD CAUTIONS ON EICAS WHILE ON FINAL APPROACH WITH ENGINE 1 AND 2 BLEED ON AND APU 0FF EMERGENCY DECLARED. FLT CONT-C/A-ITEM DEFFERED. PERFORMED LEAK CHK OF #2 ECS AREA INCLUDING PRESSURE LINES, NO LEAKS NOTED. FOUND PACK #2 SETDOWN SWITCH OPEN, REMOVED AND REPLACED SETDOWN SWITCH IAW AMM CH 21-51-07, NO FURTHUR DISCREPANCIES NOTED OPS CHK OK IAW AMM 21-51-00

Part: COUPLING — LEAKING (AC BAY) · airframe 38,115 hrs · 33,593 cycles

ACCT BLEED 2 LEAK. EMERGENCY DECLARED-C/A-REMOVED & REPLACED FLEXIBLE COUPLINGS ON RH DUEL TEMPERATURE CONTROL VALVE & PERFORMED OPS TEST IAW AMM 21-51-00, OPS TEST GOOD. NO LEAKS NOTED AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LGIHT) · airframe 37,790 hrs · 33,311 cycles

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

Part: CONTROL MODULE — FAILED (CABIN LIGHTS) · airframe 37,788 hrs · 33,309 cycles

BURNING WIRE SMELL FROM OVERHEAD FLUORESCENT LIGHTING OVER SEAT 1A-C/A-REMOVED AND REPLACED LIGHTING CONTROL MODULE IAW AMM 33-21-01.OPS CHK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,673 hrs · 33,229 cycles

LH EXTERNAL CENTER FAIRING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH EXTERNAL CENTER FAIRING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 37,015 hrs · 32,624 cycles

DURING PS-1 CHECK FOUND LH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH OVERWING EMERGENCY LIGHT BULB IAW AMM 33-50-07.OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,928 hrs · 32,533 cycles

OVERWING EXTERNAL EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: CIRCUIT BREAKER — SHORTED · airframe 36,814 hrs · 32,413 cycles

CIRCUIT BREAKER BEHIND CAPTAIN SEAT B2 (HEAT PITOT 1) WHEN PULLED ELECTRIC BURN SMELL.-C/A-FOUND K0054 RELAY PITOT CURRENT SENSOR TO HAVE A ELECTRIC BURN SMELL. REMOVED AND REPLACED PITOT CURRENT SENSOR K0054 IAW EMB 145 AMM 30-31-01. PERFORMED OPERATIONAL CHECK OF PITOT / STATIC PORT HEATING IAW EMB 145 AMM 30-31-00. OPS CHECK GOOD. NO BURN / ELECTRIC SMELL PRESENT.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 PITOT) · airframe 36,802 hrs · 32,398 cycles

PITOT 2 INOPERATIVE EICAS MESSAGE. PERFORMED AN OPERATIONAL CHECK OF PITOT NR 2 IAW AMM 30-31-00. NO EICAS OR CMC MESSAGES FOUND. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 36,801 hrs · 32,396 cycles

L/H OVERWING EXT EMERGENCY LIGHT INOP.-C/A-REMOVED AND REPLACED THE LH OVERWING EXIT LIGHT IAW EMB 145 AMM 33-50-10. OPC GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 36,697 hrs · 32,295 cycles

CARGO DOOR CUT OUT SILL IS CORRODED. C/A- REMOVED AND REPLACED CARGO DOOR CUTOUT SILL IAW 51-40-02.

Part: SUPPORT — CRACKED (FUSELAGE FAIRING) · airframe 36,697 hrs · 32,295 cycles

LT WING TO FUSELAGE FAIRING UPPER SUPPORT CRACKED AT APPROX. FR 49. C/A-REPLACED SUPPORT IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (NLG WW) · airframe 36,697 hrs · 32,295 cycles

NLG UPLOCK BOX LT SIDE SUPPORT IS CRACKED. C/A-REMOVED AND REPLACED NLG UPLOCK BOX SIDE SUPPORT IAW SRM-51-40-02.

Part: LIGHT — DAMAGED (CABIN) · airframe 36,697 hrs · 32,295 cycles

FOUND 7 EMERGENCY FLOOR LIGHTS DAMAGED.-C/A-COMPLETE:REPLACED 7 EMERGENCY FLOOR LIGHTS AND INSERTED THEM ONTO THE FLOOR PROFILE READY TO INSTALL SEE BOW 324814 FOR INSTALLATION OF CARPET FLOOR PROFILES AND E727950 FOR OPS CHECK.

Part: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,697 hrs · 32,295 cycles

EMERGENCY LIGHTS ARE INNOP WHEN USING FLIGHT ATTENDANT PANEL "NORM/ON" PUSH BUTTON.-C/A-COMPLETE:REMOVED AND REPLACED FLIGHT ATTENDANT PANEL IAW AMM 25-27-09. OPS CHECK GOOD, EMERGENCY LIGHTS ILLUMINATE.

Part: LIGHT — DAMAGED (CABIN) · airframe 36,697 hrs · 32,295 cycles

4 EACH EMERGENCY LIGHT STRIPS FLOOR ANGLES ARE CRACKED.-C/A-COMPLETE:REPLACED 4 EACH EMERGENCY LIGHT STRIP FLOOR ANGLES AND INSERTED EMERGENCY LIGHT STRIPS IN ANGLE PROFILES READY TO INSTALL ON AIRCRAFT SEE BOW324814 FOR INSTALLATION OF EMERGENCY LIGHT STRIPS ON AIRCRAFT.

Part: LIGHT — CRACKED (CABIN) · airframe 36,697 hrs · 32,295 cycles

#1 FLOOR EMERGENCY LIGHT PROXIMITY STRIP IS CRACKED-C/A-COMPLETE:REPLACED #1 EMERGENCY FLOOR STRIP AND INSERTED EMERGENCY LIGHT ONTO STRIP READY TO INSTALL SEE BOW324814 FOR INSTALLATION AND OPERATIONAL TEST OF FLOOR STRIPS.

Part: LIGHT — OUT OF ADJUST (CABIN) · airframe 36,324 hrs · 31,957 cycles

EMERGENCY EXIT LIGHT ON RT SIDE FIRST ROW NOT WORKING. C/A-EMERGENCY EXIT LIGHT ON RT SIDE FIRST ROW ADJUSTED IAW AMM 33-50-00. OPC GOOD.

Part: PRINTER — FAILED (COCKPIT) · airframe 36,256 hrs · 31,899 cycles

STRONG BURNING SMELL COMING FROM ACARS PRINTER.-C/A-REMOVED AND REPLACED ACARS PRINTER IAW AMM 23-22-02. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (ROW 12 BC) · airframe 36,204 hrs · 31,843 cycles

12 B/C OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT LAMP AT SEAT 12 B/C IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A OPC GOOD END.

Part: UNKNOWN — MALFUNCTIONED (ANTI-ICE SYS) · airframe 35,589 hrs · 31,293 cycles

ICE COND- A/I INOP IN FLIGHT. C/A-PERFORMED ANTI-ICING SYSTEM OPERATIONAL TEST IAW AMM 30-00-00. OPERATIONAL TEST IS GOOD. PERFORMED ANTI-ICING VALVES OPERATIONAL TEST IAW AMM 30-00-00. OPERATIONAL TEST OF VALVES WAS GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: SLEEVE — LEAKING (CONTROL VALVE) · airframe 35,376 hrs · 31,118 cycles

DIVERSION FLIGHT# 3667 FOR "UNABLE TO PRESSURIZATION"-C/A-FOUND SMALL SLEEVE AFT OF DUAL TEMP CONTROL VALVE TO BE LEAKING. REMOVED AND REPLACED DUAL TEMP CONTROL SLEEVE AND CLAMPS, PACK OPC GOOD, OPC OF MANUAL PRESSURIZATION GOOD PER EMB AMM 21-51-00-700-801-A AND 21-31-00-700-801-A

Part: DRAIN — CONTAMINATED (STATIC SYSTEM) · airframe 35,211 hrs · 30,945 cycles

LOST AIRSPEED AND ALT IN CRUISE-C/A-FOUND WATER IN BOTH #1 AN #2 STATIC DRAINS. DRAINED 1 AN 2 IAW AMM EMB 145 AMM 34-13-00-680-801-A COMPLIED WITH OPERATIONAL CTEST IAW EMB145 AMM 34-15-00-700-802-A OPS CHECK GOOD

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 35,118 hrs · 30,859 cycles

AFT EMERGENCY FLASHLIGHT CHARGING INDICATOR LIGHT INOP. REMOVED AND REPLACED AFT EMERGENCY FLASHLIGHT IAW AMM 33-50-16. OPS CHECK GOOD.

Part: FUSE — DAMAGED (DC DISTR BOX) · airframe 34,778 hrs · 30,540 cycles

DURING THE TAKE OFF ROLL (MID TO LATE) ELECTRICAL FUMES WERE INCREASING. HIGH SPEED ABORT BETWEEN 100-120 KTS. SUSPECTED FAULTY FUSE OR CONTACTOR IN RT DC DISTR BOX. REMOVED AND REPLACED FUSE FOR HYD PUMP NR 2 IAW AMM 24-65-01. NO DEFECTS NOTED AT THIS TIME. OPC GOOD. PERFORMED A HIGH POWER ENGINE RUN. SIMULATED TAKEOFF SPEED WITH FLIGHT CREW NO ABNORMALITIES NOTED AT THIS TIME COULD NOT DUPLICATE ANY FAULTS. OPC GOOD.

Part: PRESSURE SWITCH — FAILED (ANTI ICE SYSTEM) · airframe 33,793 hrs · 29,625 cycles

WING ANTI-ICE FAILED AND ICE COND A1 INOPERATIVE MESSAGE ON EICAS IN FLT, IN ICE CONDITIONS. REMOVED AND REPLACED THE WING NR 1 ANTI-ICE PRESSURE SWITCH IAW AMM 30-11-02, FOUND A LOOSE SENSE LINE, INSTALLED THE LINE, NR 2 WING OPS CHECKED IAW AMM 30-00-00, CHECKED GOOD. AIRCRAFT OK FOR SERVICE

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 33,320 hrs · 29,235 cycles

FLOOR EMERGENCY LIGHT IN FRONT OF SEAT 4A INOPERATIVE. CONNECTED THE ELECTRICAL CONNETOR. OPS CHECKED GOOD IAW 33-60-00

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 33,320 hrs · 29,235 cycles

FLOOR EMERGENCY LIGHT, IN FRONT OF SEAT 6A INOPERATIVE. CONNECTED THE ELECTRICAL CONNECTOR. LIGHT OPS CHECKED GOOD. IAW AMM 33-60-00.

Part: WARNING LIGHT — ACTIVATED (E/E BAY DOOR) · airframe 33,202 hrs · 29,128 cycles

ABORTED TAKE OFF DUE TO A FORWARD AVIONICS DOOR OPEN INDICATION DURING INITIAL TAKE OFF ROLL.

Part: PROFILE — CORRODED (RT OVERWING EXIT) · airframe 31,921 hrs · 27,885 cycles

RIGHT OVERWING EXIT BOTTOM EDGE IS CORRODED AROUND SPRING. R & R THE RT OVERWING EXIT BOTTOM EDGE IAW SRM 51-40-02

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,921 hrs · 27,885 cycles

NR 1 LT EMERGENCY LIGHT HAS A BROKEN WIRE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: FRAME — CRACKED (FRM 73) · airframe 31,921 hrs · 27,885 cycles

FRAME 73 CRACKED BELOW THE RT OTBD FLOOR SUPPORT. REMOVED AND REPLACED THE FRAME SECTION IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (CARGO DOOR) · airframe 31,921 hrs · 27,885 cycles

CARGO DOOR LOWER SILL CORRODED ON FORWARD END. REMOVED AND REPLACED THE CARGO DOOR SILL IAW SRM 51-40-02.

Part: FRAME — CORRODED (FRM 65) · airframe 31,921 hrs · 27,885 cycles

FRAME 65 IS CORRODED AT DOOR GUIDE PLATE. REPAIRED THE FRAME IAW SRM 53-31-04.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 31,921 hrs · 27,885 cycles

FRAME 65 SHEAR TIE IS CORRODED. REPAIRED THE SHEAR TIE IAW SRM 53-31-04 AND ETN-EM-53-272.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 31,921 hrs · 27,885 cycles

EMERGENCY LIGHT WIRE CONNECTORS AT FLOOR PANEL 251BF ARE BROKEN. REMOVED AND REPLACED THE WIRE CONNECTOR IAW SWPM 20-00-03.

Part: CHARGER — NOT REPORTED (EMERGENCY LIGHTS) · airframe 31,921 hrs · 27,885 cycles

NR 3 EMERGENCY LIGHTING BATTERY AND BATTERY CHARGER . REMOVED AND REPLACED BATTERY HOLDER AND BATTERY CHARGER ASSEMBLY IAW WC 33-700-19

Part: YOKE — CRACKED (RT PYLON) · airframe 31,921 hrs · 27,885 cycles

RIGHT FWD PYLON LOWER YOKE CRACKED. REMOVED AND INSTALLED A SERVICEABLE YOKE IAW EO EM-54MR-386

Part: NUT PLATE — BROKEN (EMERGENCY LIGHT) · airframe 31,921 hrs · 27,885 cycles

RIGHT FWD OF WING EXTERNAL EMERGENCY LIGHT HAS BROKEN NUT PLATE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-10, SYS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,921 hrs · 27,885 cycles

EMERGENCY LIGHT IN GALLEY CEILING PANEL 234ARC INOPERATIVE. REMOVED AND REPLACED THE AC/DC INVERTER IAW AMM 33-50-11, EMEGENCY LIGHT CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,921 hrs · 27,885 cycles

EMERGENCY LIGHT NOT WORKING IN CABIN OVERHEAD AT RT PSU EXIT ROW. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-07, SYS CHECKED GOOD.

Part: BRAKE — FAILED (MLG) · airframe 28,623 hrs · 24,771 cycles

ON POST FLIGHT, SMOKE OUT RT LG BRAKE TEMPS BOTH ON GREEN RANGE, INBD & OTBD. TROUBLE SHOT & FOUND NR 3 BRAKE TO HAVE COME APART. CATASTROPHIC FAILURE, BRAKE PISTONS PUSHED THROUGH BACKING PLATE & INTO ROTOR. NO DAMAGE TO SURROUNDING AREA NOTED. REPLACED NR 3 BRAKE IAW WC 32-600-14 & NR 3 MLG WHEEL & TIRE ASSEMBLY IAW WC 32-700-11. NO FURTHER DEFECTS NOTED.

Part: CONTROL UNIT — FAILED (BRAKE SYSTEM) · airframe 28,623 hrs · 24,770 cycles

AFTER LANDING, THE INBD BRAKES WERE IN THE AMBER WITH THE NR 3 RT INBD BRAKE, CAUSING A BREAK OVERHEAT ON THE EICAS. THE NR 1 & 4, BOTH OTBD BRAKES WERE SHOWING IN THE GREEN RANGE, AS THOUGH THEY HAD DONE NO BRAKING. R & R BRAKE CONTROL UNIT IAW AMM 32-41-02 & NR 3 WHEEL SPEED TRANSDUCER IAW AMM 32-41-03. OPERATIONS CHECKED GOOD IAW FIM TASK 32-41-00-810-803-A. WHEEL SPEED TRANSDUCER PN 140197 & SN 4967.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE, NOSE SKIN WAVY FROM FRAME 2 - 6 ON CTR BUTT STRAP. PERFORMED REPAIR OF NOSE SKIN WAVINESS IAW ERS-EM-53MR-1660.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT, REPLACE RT ELEVATOR INBD LE. R & R RT ELEVATOR INBD LE IAW SRM 51-40-02, 51-20-01, 55-20-01, ETN-EM-55-073 & ETN-EM-55-076.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT. REPLACE LT CTR FUSELAGE 1 SKIN. R & R LT CTR FUSELAGE 1 SKIN IAW SRM 53-22-01 SI, 51-40-02, 51-20-01, 51-20-03, 51-40-06, ETN-EM-53-26 & ETN-EM-51-118.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR MID SKIN TIP. R & R RT ELEVATOR MID SKIN TIP IAW SRM 51-40-06, 51-20-01, 51-40-02 & ETN-EM-55-076. SEE NRTC BOW 198154 FOR WEIGHT & BALANCE.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE, REPLACE RT ELEVATOR UPPER CTR SKIN. R & R RT ELEVATOR UPPER CTR SKIN IAW SRM 55-20-01, 51-20-01/03, 51-40-02 06, ETN-EM-55-073 & ETN-EM-55-076.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT, REPLACE LT ELEVATOR UPPER CTR SKIN. R & R LT ELEVATOR UPPER CTR SKIN IAW SRM 55-21-01, 51-40-02, ETN-EM-55-073 & ETN-EM-55-076.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT, REPLACE LT STAB UPPER SKIN. R & R LT STAB TOP SKIN IAW SRM 51-40-02, 51-20-03, 51-40-06, 51-40-03, 51-20-01, 55-10-01SI, ETN EM-55-073 & EM 55-074.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT, REPLACE LT ELEVATOR INBD LE. REMOVED & INSTALLED, APPLIED EDGE SEALANT TO LT ELEVATOR INBD LE IAW SRM 55-20-01, 51-20-01, 51-40-02, ETN-EM-55-073 & ETN-EM-55-076.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT, REPLACE LT ELEVATOR OUTER LE. R & R LT ELEVATOR OUTER LE 145-30807-004 IAW SRM 51-20-01, 51-40-02, 55-20-01, ERS-EM-5500-331, ETN-EM-55-073 & ETN-EM-55-076.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT, REPLACE CTR FUSELAGE IV TOP SKIN. R & R CTR FUSELAGE IV TOP SKIN IAW SRM 53-24-01SI, SRM 51-20-03, 51-40-03, 51-20-01, 51-40-02, 51-40-06, ETN-EM-51-118 & ETN EM-53-265.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT, REPLACE LT ELEVATOR, OTBD UPPER SKIN TIP. R & R LT ELEVATOR, OTBD UPPER SKIN TIP IAW SRM 55-20-01, 51-40-02, ETN-EM-55-073 & ETN-EM-55-076.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT, REPLACE RT ELEVATOR OTBD UPPER SKIN TIP. R & R RT ELEVATOR OTBD UPPER SKIN TIP IAW SRM 55-20-01, 51-20-01, 51-40-02, 51-40-06, ETN-EM-55-073 & ETN-EM-55-076.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT, REPLACE RT ELEVATOR OUTER LE. R & R RT ELEVATOR OUTER LE IAW SRM 51-20-01, 51-40-02, 55-20-01, ERS-EM-5500-331, ETN-EM-55-073 & ETN-EM-55-076.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT, REPLACE CTR FUSELAGE II SKIN PANEL. R & R CTR FUSELAGE II SKIN IAW SRM 51-40-02 & ETN-EM-53-263.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE II SKIN WIPER. R & R FWD FUSELAGE II SKIN IAW SRM 53-12-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02, CPM 51-21-04, ETN-EM-51--118 & ETN-EM-53-206.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT, REPLACE LT ELEVATOR MID SKIN TIP. R & R LT ELEVATOR MID SKIN TIP IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06, 55-20-01, ETN EM-55-073R2 & ETN-EM-55-076.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE I RT SKIN PANEL. R & R FWD FUSELAGE I RT SKIN IAW SRM 51-40-02 & ETN-EM-53-206.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE I LT SKIN PANEL. R & R FWD FUSELAGE I LT SKIN IAW SRM 51-40-02 & ETN-EM-53-206.

Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 28,401 hrs · 24,548 cycles

HAIL DAMAGE EVENT, REPLACE RT STAB SKIN. R & R RT STAB TOP SKIN IAW SRM 51-40-02, 51-20-03, 51-40-06, 51-40-03, 51-20-01, 55-10-01SI, ETN EM-55-073 & EM-55-074.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 28,074 hrs · 24,260 cycles

AFT EMER FLASHLIGHT HOLDER BROKEN. R & R AFT EMER FLASHLIGHT HOLDER ASSEMBLY. OPERATIONS CHECKED GOOD IAW AMM 33-50-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,009 hrs · 24,208 cycles

LEFT OVERWING EMER LIGHT INOPERATIVE. R & R LT OVERWING EMER LIGHT BULB IAW AMM 33-50-07. PERFORMED EMER LIGHT OPERATIONS CHECK IAW AMM 33-50-00. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,997 hrs · 24,194 cycles

MAIN DOOR EMER LAMP INOPERATIVE. R & R MAIN DOOR EMER LAMP IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SPLICE — UNKNOWN (CABIN) · airframe 27,967 hrs · 24,170 cycles

RIGHT FWD EXTERNAL OVERWING EMER EXIT LIGHT INOPERATIVE. TRANSFERRED TO AML PAGE 3822947 ITEM 1, DEFERRED IAW MEL 33-29. REQUIRES FURTHER TROUBLESHOOTING. R & R SPLICE NR SP8924 AT OVERHEAD PANEL CEILING 9A IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD THIS CLEARS MEL 33 - 29.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,804 hrs · 24,015 cycles

EMERGENCY EXIT SIGN NEAR MAIN DOOR INOPERATIVE. EMER LIGHT DC & AC INVERTER NR 1 IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,712 hrs · 23,943 cycles

EMERGENCY LIGHT IN MAIN DOOR IS INOPERATIVE. R & R WITH SERVICEABLE MAIN DOOR EMER LT BULB FROM SPARE BULB KIT IAW AMM 33-50-10. OPERATIONS CHECKED OK.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 27,412 hrs · 23,663 cycles

CAPTAINS FLASHLIGHT HOUSING BROKEN. AFT CABIN FLASHLIGHT HOUSING BROKEN, ON LAVATORY WALL. R & R BOTH CAPTAINS FLASHLIGHT BRACKET & AFT CABIN ON LAVATORY WALL FLASHLIGHT BRACKET & FLASHLIGHT IAW 145 EEL 08 12. OPERATIONS CHECKED GOOD.

Part: SKIN — DAMAGED (LT WING) · airframe 27,335 hrs · 23,588 cycles

EDDY CURRENT INSPECTION RIBS, TORQUE BOX NDIM 57-28-00-250-807 & NDIM 57-28-00-250-806-A00. A1519 A1522 COMPLIED WITH. LOCK FASTENER HOLE DAMAGES REPAIRED IAW ERS-EM-57MR-395.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 27,335 hrs · 23,588 cycles

LEFT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE JUST AFT OF SPAR 2 HAS A 3 INCH CRACK. R & R ANGLE IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 27,335 hrs · 23,588 cycles

RIGHT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE JUST AFT OF SPAR 2 HAS A 1/4 INCH CRACK. R & R ANGLE IAW SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,335 hrs · 23,588 cycles

LEFT SIDE OF VERTICAL STAB AT FRAME 75 BETWEEN STRINGERS 02L & 03L HAS A CRACK IN THE SKIN, OUT OF A RIVET MARKED IN RED. COMPLIED WITH ERS-EM-53MR-1118.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 27,335 hrs · 23,588 cycles

SUPPORT FOR CTR FLIGHT COMPARTMENT GRAB HANDLE IS CRACKED AROUND LT NUTPLATE HOLE. REPAIRED SUPPORT FOR CTR FLIGHT COMPARTMENT GRAB HANDLE AT LT NUTPLATE HOLE IAW SRM 53-12-16.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,335 hrs · 23,588 cycles

SHEAR CLIP ON FRAME 65 BETWEEN STRINGER 17L & 18L IS CRACKED. REMOVED CRACKED SHEAR CLIP. FABRICATED NEW SHEAR CLIP IAW SRM 51-30-01 & 53-31-04. INSTALLED SHEAR CLIP IAW SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,335 hrs · 23,588 cycles

FRAME 66 IS CRACKED AT RIVET HOLE BETWEEN STRINGER 16L & 17L. REPAIRED DAMAGED SECTION OF FRAME 66 IAW SRM 53-00-04 REPAIR FIGURE 201. SPLICE PN 145-64268-00.

Part: SUPPORT ANGLE — DAMAGED (FUSELAGE) · airframe 27,335 hrs · 23,588 cycles

CARGO RAMP FLOOR SUPPORT ANGLE AT FRAMES 66 - 67 ARE BENT & CRACKED. INSTALLED NEW SUPPORT ANGLE AT FRAME 66 - 67 IAW SRM 51-40-02. UNDRILLED ANGLE PN 145-25681-611.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,335 hrs · 23,588 cycles

FRAME 67 IS CRACKED AT RIVET HOLE BETWEEN STRINGER 16L & 17L. REPAIRED IAW ERS-EM-53MR-1120. FRAME PN 145-25764-007.

Part: FITTING — WORN (RT AILERON) · airframe 27,335 hrs · 23,588 cycles

RIGHT AILERON DAMPER HAS A MIGRATING BUSHING AT THE AILERON INBD SIDE. REPLACED RT AILERON DAMPER FITTING IAW EO EM 27MR-112.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,335 hrs · 23,588 cycles

SEVEN DENTS IN FUSELAGE SKIN BETWEEN FRAME 19 & 21, STRINGERS 16R & 17R. COMPLIED WITH ERS-EM-53MR-1102 FOR PERMANENT REPAIR.

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 27,335 hrs · 23,588 cycles

APU FIREWALL HAS A 3/8 INCH CRACK BY LOWER RT MOUNT POINT. REPAIRED APU FIRE WALL IAW EO EM-53AD-1883 R 4 PART C.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 27,335 hrs · 23,588 cycles

CARGO DOOR SILL IS CORRODED. R & R OF CARGO DOOR SILL IAW SRM 51-40-02.

Part: CONNECTOR — BROKEN (CABIN) · airframe 27,335 hrs · 23,588 cycles

AFT FLOOR EMER LIGHT HAS A BROKEN OFF CONNECTOR. REPLACED CONNECTOR IAW SWPM 20-50-01.

Part: WIRE — BROKEN (CABIN) · airframe 27,335 hrs · 23,588 cycles

NUMBER 1 LT CABIN EMER LIGHT HAS A BROKEN WIRE ON THE FUSELAGE SIDE. REPLACED CONNECTOR AT NR 1 LT EMER LIGHT IAW SWPM 20-50-00.

Part: CONNECTOR — BROKEN (CABIN) · airframe 27,335 hrs · 23,588 cycles

EMERGENCY LIGHT STRIP SPLICE CONNECTOR BROKEN AT FS 38. REPLACED CONNECTOR AT SPLICE SP9103 IAW SWPM 20-50-00.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 27,322 hrs · 23,576 cycles

BLEED 2 OVERTEMP AFTER EXITING ICING. COMPLIED WITH FIM 36-11-00-810-804-A BLOCK 1. PERFORMED VISUAL INSPECTION OF PRE COOLER AREA & FOUND LOOSE CLAMP AT ENG SIDE TUBE ASSEMBLY. REPOSITIONED & TIGHTENED IAW AMM 36-11-04 & REMOVED & INSTALLED FAN AIR VLV FILTER IAW AMM 36-11-03. OPERATIONS CHECKED GOOD, NO FAULTS.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 27,246 hrs · 23,508 cycles

AFT CABIN FLASHLIGHT INDICATES NORMAL CHARGING BUT DOES NOT HOLD A CHARGE. R & R AFT CABIN FLASHLIGHT IAW AMM 33-50-16.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 26,748 hrs · 23,016 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. LUBRICATED MAIN CABIN DOOR FRAME ROLLERS IAW AMM 52-18-00. TESTED SATISFACTORY.

Part: SPRING — FAILED (BRAKE PEDAL) · airframe 26,748 hrs · 23,016 cycles

AFTER PUSH OUT WITH NR 1 ENG RUNNING & UPON SETTING THE PARKING BRAKE, THE CAPTAIN`S SIDE LT BRAKE PEDAL MADE A POPPING NOISE, LOST ALL BRAKE PRESS. THE FIRST OFFICER`S LT BRAKE PEDAL CONTINUED TO WORK. INSTALLED SPRING ON CAPTAIN'S LT PEDAL. OPERATIONS CHECKED GOOD IAW AMM 27-21-03.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 26,128 hrs · 22,438 cycles

AT 25,000 CABIN ALTITUDE WENT TO 11,200. FOLLOWING FIM TASK 21-31-00-810-809 PERFORMED PRESSURIZATION CONTROL SYS FUNCTIONAL TEST IN THE AUTOMATIC MODE & FOUND SYSTEM OK IAW AMM 21-31-00-700-802-A.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 25,922 hrs · 22,232 cycles

CLIMBING THROUGH 17000 FT, CABIN PRESSURE ALTITUDE STARTED RISING, STARTED A DESCENT, CABIN WENT UP TO 10200 FT, LEVELED OFF AT 10000 FT. DECLARED AN EMERGENCY, RECEIVED RAM AIR VALVE FAIL MESSAGE A FEW TIMES, ALSO DU5 OVERHEAT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,492 hrs · 21,083 cycles

NUMBER 3 FLOOR PROXIMITY STRIP LIGHT INOPERATIVE. R & R NR 3 FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-50-12.

Part: O-RING — FAILED (BLEED SYS) · airframe 23,797 hrs · 20,535 cycles

THE CREW REPORTED THAT WHILE CRUSING AT FL 370, THEY RECEIVED AN EICAS BLEED 1 LEAK MESSAGE. THEY NOTICED AN INTERMITTENT BLEED 1 LEAK ON THE BLEED VALVE. THE CREW COMPLIED WITH AOM, VOL 1 PROCEDURES AND THE MESSAGE RETURNED. THE CREW DECLARED AN EMERGENCY AND DIVERTED. THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R THE O-RINGS AT FITTING NR 1 IAW AMM 36-11-10. RAN BLEED AIR THROUGH APU IAW TASK 36-00-00-860-802-A. INSPECTED JOINT. NO FURTHER DEFECTS NOTED. OPC GOOD. R & R THE FAN AIR VALVE FILTER ON ENG 1 IAW AMM 36-11-03. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 23,796 hrs · 20,533 cycles

EMERGENCY LIGHT INOPERATIVE. R & R IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: O-RING — LEAKING (BLEED DUCT) · airframe 23,641 hrs · 20,408 cycles

A BLEED LEAK EICAS MESSAGE ON NR 1 ENGINE. RAN CHECK LIST, DECLARED AN EMERGENCY AND DIVERTED. BLEED LEAK INDICATION WENT AWAY AFTER THE COMPLETION OF THE OF THE CHECKLIST. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. INSPECTED ALL JOPINTS ON NR 1 BLEED DUCT (1- 29) R & R O-RINGS ON JOINTS 1, 3, 9 &17 IAW AMM 36-11-10, NO LEAKS NOTED AT THIS TIME. THE ACFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (LAVATORY) · airframe 23,515 hrs · 20,308 cycles

DURING B INSPECTION, FOUND THE LAVATORY LT GUSSET BEAM CORRODED. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LAVATORY LT GUSSET BEAM IAW SRM 51-40-02. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — CRACKED (CABIN) · airframe 23,515 hrs · 20,308 cycles

DURING MX INSPECTION, FOUND LT FLOOR PROXIMITY LIGHT AND EXTRUSION CRACKED. ACFT REMOVED FROM SERVICE. R & R LIGHT AND EXTRUSION IAW AMM 33-50-12. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR)

LEFT FWD EXTERNAL EMERGENCY LIGHT INOP. REPLACED BULB.

Part: HOLDER — BROKEN (COCKPIT) · airframe 21,813 hrs · 18,949 cycles

ON FLIGHT 3335 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT HOLDER IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TERMINAL — LOOSE (FLASHLIGHT) · airframe 21,529 hrs · 18,721 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT FLIGHT ATTENDANT FLASHLIGHT INOPERABLE. DURING TROUBLESHOOTING, FOUND NO POWER AT FEMALE END OF HARNESS FOR FLASHLIGHT. SECURED TERMINAL IN SPLICE SP3558. THE OPERATIONAL CHECK WAS GOOD IAW EMB145 AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 21,475 hrs · 18,683 cycles

ON FLIGHT 4322 THE CREW REPORTED THE CABIN EMERGENCY AFT FLASHLIGHT DID NOT INDICATE CHARGING WHEN STOWED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (FLASHLIGHT) · airframe 21,330 hrs · 18,567 cycles

ON FLIGHT 3974 THE CREW REPORTED THE FLIGHT ATTENDANT FLASHLIGHT IN AFT CABIN HAD A RED LIGHT AND WAS NOT WORKING. RECONNECTED CONNECTOR TO FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. FOUND CONNECTOR DISCONNECTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 21,294 hrs · 18,535 cycles

ON FLIGHT 4269 THE CREW REPORTED THE AFT FLIGHT ATTENDANT FLASHLIGHT WILL NOT CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (FLASHLIGHT) · airframe 21,284 hrs · 18,527 cycles

ON FLIGHT 4202 THE CREW REPORTED THE REAR FLASHLIGHT HOLDER RED CHARGE LIGHT WAS INTERMITTENT WHEN IN THE CRADLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. DEFERRED AFT FLASHLIGHT PER 25-53. PERFORMED OPERATIONAL CHECK OF EMERGENCY FLASHLIGHTS. NO DEFECTS FOUND. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-51-01 MEL ITEM RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — FAILED (FLASHLIGHT) · airframe 21,163 hrs · 18,427 cycles

ON FLIGHT 4248, THE CREW REPORTED THE AFT CABIN FLASHLIGHT WAS NOT CHARGING. REMOVED AND REPLACED THE FLASHLIGHT WIRING HARNESS AND FLASHLIGHT ASSEMBLY IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — MALFUNCTIONED (AFT CABIN) · airframe 21,093 hrs · 18,369 cycles

FLIGHT 2830, FOUND REAR CABIN FLASHLIGHT CHARGING LIGHT NOT ILLUMINATED. THE AIRCRAFT WAS REMOVED FROM SERVICE.

Part: FLASHLIGHT — DISCHARGED (AFT CABIN) · airframe 20,929 hrs · 18,243 cycles

FLIGHT 2852, CREW REPORTED THE AFT CABIN FLASHLIGHT WAS NOT CHARGING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT. OPS CHECKED GOOD IAW AMM 25-60-00. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,789 hrs · 18,143 cycles

DURING B INSPECTION FOUND THE LEFT UPPER WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT UPPER WING EMERGENCY LIGHT IAW AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 20,723 hrs · 18,096 cycles

ON FLIGHT 2796 THE FLIGHT ATTENDANT REPORTED THE AFT FLASHLIGHT CHARGER IS ONLY WORKING INTERMITTANT WITH THE RED LIGHT OFF AND ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 20,301 hrs · 20,301 cycles

ON FLIGHT 3214 IN CRUISE FLIGHT THE CREW REPORTED THEY GOT E1 BLEED LEAK EICAS MESSAGE FOLLOWED AOM E1 BLEED SHUT OFF MESSAGE CLEARED AND EMERGENCY DECLARED AND LANDED IN MAF. THE AIRCRAFT LANDED WITHOUT INCIDENT. NO OTHER PROBLEMS NOTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED O-RINGS AT JOINTS 1, 9, 21 & 23 ON NR 1 BLEED DUCT AS PER EMB MM 36-11-10. LEAK CHECK FOUND TO BE GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CIRCUIT BREAKER — MALFUNCTIONED (FLASHLIGHT) · airframe 20,109 hrs · 17,597 cycles

FLIGHT 2876, THE CREW REPORTED THE AFT FLIGHT ATTENDANT FLASHLIGHT DOES NOT INDICATE CHARGING. THE RED LIGHT DID NOT ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. RESET CIRCUIT BREAKER OF FLASHLIGHT. NO PARTS REMOVED OR REPLACED. OPS CHECKED GOOD IAW AMM 33-50-16. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 20,095 hrs · 17,584 cycles

DURING MAINTENANCE INSPECTION, FOUND AFT FLIGHT ATTENDANT FLASHLIGHT NOT CHARGING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED AFT FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY PER AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 19,962 hrs · 17,455 cycles

ON FLIGHT 3300 THE FLIGHT ATTENDANT REPORTED THE LAV SMOKE DETECTOR APPEARED TO BE INOPERABLE. (NO GREEN LIGHT). THE ITEM DEF PER MEL 26-2 AUTH 030850DM-C. REMOVED AND REPLACED LAV SMOKE DETECTOR SENSOR IAW EMB 145 AMM 26-14-01. RESTORED MEL. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 19,934 hrs · 17,433 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLOOR PROXIMITY EMERGENCY LIGHT AT ROW 9 WORKING INTERMITTENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ROW 9 FLOOR PROXIMITY LIGHT IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 19,458 hrs · 17,065 cycles

DURING MAINTENANCE INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT SWITCH BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FIRST OFFICERS FLASHLIGHT ASSY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 19,001 hrs · 16,729 cycles

DURING MAINTENANCE VISIT FOUND THE AFT EMERGENCY FLASHLIGHT WAS INOPERABLE. THE FLASHLIGHT WAS PLACED ON A MEL. REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IAW AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING MAINTENANCE INSPECTION FOUND THE OVERWING EXIT CEILING FORWARD LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICEABLE LIGHT ON OVERWING CEILING PANEL IAW EMB 145 AMM 33-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — CRACKED (DOOR) · airframe 18,862 hrs · 16,625 cycles

DURING MAINTENANCE BASE VISIT FOUND THE 272DR CRACKED UNDER HINGE RING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-52MR-293. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,862 hrs · 16,625 cycles

DURING MAINTENANCE BASE VISIT FOUND THE SHEAR CLIP AT FRAME 65 AND CARGO DOOR CUTOUTS TO HAVE CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-1129. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — FAILED (NR 1) · airframe 18,157 hrs · 16,075 cycles

ON FLIGHT 2826 AT 24000 FEET THE CREW REPORTED THEY SAW AND SMELLED SMOKE IN THE COCKPIT COMING FROM THE CEILING VENT. THE CREW FOLLOWED AOM PROCEDURES AND AFTER CLOSING BLEED 1 THE SMOKE DISSIPATED QUICKLY. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO ATL. THE AIRCRAFT MADE AN OVERWEIGHT LANDING. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 AIR CYCLE MACHINE. THE OPERATIONAL CHECK WAS GOOD WORK DONE IAW EMB 145 AMM 21-51-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (RT MLG) · airframe 16,785 hrs · 15,075 cycles

ON FLIGHT 4217 ON APPROACH THE CREW REPORTED THE MAIN GEAR WAS DOWN & LOCKED. AT 1000 FEET THE RIGHT MAIN SHOWED INTRANSIT, THEN UNLOCKED. AFTER GO AROUND CYCLED GEAR TWICE AND PERFORMED ABNORMAL LANDING GEAR EXTENSION AND TOUCH DOWN LANDING WAS LOCKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD DOWNLOCK PROXIMITY SWITCH IAW M/M 32-61-02. THE OPERATIONAL CHECK SEVERAL TIMES WAS GOOD IAW M/M 32-32-00. NO DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — FAILED (COCKPIT) · airframe 15,232 hrs · 13,872 cycles

ON FLIGHT 4253 DURING TAXI THE CREW REPORTED THE EMERGENCY LIGHT WAS NOT ARMED WITH COCKPIT IN ARM POSITION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT ARM SWITCH IAW AMM 20-43-03. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL MODULE — FAILED (CABIN) · airframe 15,232 hrs · 13,872 cycles

ON FLIGHT 4216 DURING TAXI THE CREW REPORTED, RECEIVED AN EICAS DISPLAY CAUTION MESSAGE EMERGENCY LIGHT NOT ARMED EVEN THOUGH OVERHEAD SWITCH WAS IN THE ARMED POSITION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROL MODULE ASSEMBLY IAW 145 AMM 33-21-01. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145-AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 14,801 hrs · 13,550 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT ASSEMBLY, AND OPERATION CHECK IAW EMB145 AMM 33-50-09. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 14,681 hrs · 13,455 cycles

ON FLIGHT 4026 AFTER TAKEOFF AROUND FLIGHT LEVEL 120 THE CREW REPORTED HEARING A POP IN THE CABIN FOLLOWED BY A STRONG ODOR IN THE COCKPIT. THE FLIGHT ATTENDANT REPORTED A ZIP SOUND AROUND ROW 10. THE CREW DECLARED AN EMERGENCY AND RETURNED TO GREEN BAY AND LANDED WITHOUT INCIDENT. THE ODOR DISAPPEARED. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED INSPECTION OF AIR CONDITIONING DUCTING INSIDE AND OUTSIDE OF AIRCRAFT. NO DEFECTS NOTED. PERFORMED POWER RUNS IAW AMM 71-00-01 AND PRESSURIZED AIRCRAFT IAW AMM 21-31-00. NO SMOKE SMELL OR POPPING NOISE NOTED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — CRACKED (CARGO BAY) · airframe 13,874 hrs · 12,752 cycles

DURING MAINTENANCE BASE VISIT FOUND THAT THE CARGO DOOR LIFTING AND LOWERING MECHANISM AFT BRACKET WAS CRACKED AT THE HI-LOK INBOARD SIDE OF THE BRACKET. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICEABLE AFT BRACKET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 9,357 hrs · 8,769 cycles

DURING AN IMBV INSP, THE CENTER HAT BEAM WAS FOUND TO BE CORRODED ON THE LEFT SIDE. REPAIR, REMOVED CENTER BEAM GUSSET, MADE A CUTOUT TO REMOVE THE CORROSION. FABRICATED A DOUBLER USING AL2024T3, TH-.040. CLEANED AND TREATED REPAIR PART. REPAIR DONE IAW AEA ETA-EM-53MR-030 AND EMBRAER SRM (SRM145/1142 REV. 39) CHAPTER 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,357 hrs · 8,769 cycles

DURING A IMBV INSP, THE LT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. REPAIR, PERFORMED A CUTOUT OF BEAM, PREPARED A DOUBLER, FILLER AND TWO SHIMS. CLEANED AND TREATED REPAIR PARTS AND INSTALLED. REPAIR DONE IAW EMBRAER 145 SRM (SRM EMB 145/1142 REV. 39) CHAPTER 53-00-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,357 hrs · 8,769 cycles

DURING MBV INSP, THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REPAIR, PERFORMED A CUT OUT ON LEFT OMEGA BEAM. PREPARED EXTERNAL ANGLE, FILLER AND TWO SHIMS. PARTS CLEANED AND TREATED AND INSTALLED IN AIRCRAFT. REPAIR DONE IAW EMBRAER 145 SRM (SRM EMB-145/1142 REV 39) CHAPTER 53-00-10 FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,357 hrs · 8,769 cycles

DURING MBV INSP, THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REPAIR, PERFORMED A CUT OUT ON LEFT OMEGA BEAM. PREPARED EXTERNAL ANGLE, FILLER AND TWO SHIMS. PARTS CLEANED AND TREATED AND INSTALLED IN AIRCRAFT. REPAIR DONE IAW EMBRAER 145 SRM (SRM EMB-145/1142 REV 39) CHAPTER 53-00-10 FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,357 hrs · 8,769 cycles

DURING A IMBV INSP,THE CENTER OMEGA BEAM BETWEEN FRAME 24 AND 25 WAS FOUND CORRODED. REPAIR, PERFORMED A CUT OUT OF THE OMEGA BEAM. FAB AN EXTERNAL ANGLE, FILLER AND SHIMS. CLEANED AND TREATED PARTS AND INSTALLED IN AIRCRAFT. WORK DONE IAW EMBRAER 145 SRM (SRM EMB-145/1142) CHAPTER 53-00-10 FIGURE 203.

Part: WARNING MESSAGE — ILLUMINATED

CAPT REPORTED, GOT WING A/I FAIL MESSAGE. FOLLOWED AOM PROCEDURES AND COULD NOT GET MESSAGE TO CLEAR. DUE TO WEATHER ELECTED TO DIVERT TO CMH.

Part: PLATE — LOOSE (SERVICE DOOR) · airframe 8,538 hrs · 7,998 cycles

CREW NOTED 2 MINUTES INTO FLIGHT, HEARD A FLAPPING NOISE COMING FROM THE SERVICE DOOR AREA. THE CAPT DECLARED AN EMERGENCY AND WENT TO ORD FOR MTX. LANDED WITHOUT INCIDENT. NO OVERWEIGHT LANDING. REMOVED AND RE-INSTALLED SVC DOOR PROTECTIVE PLATE IAW EMB 145 AMM 53-21-13. THIS PLATE WAS LOOSE AND CAUSED FLAPPING SOUND. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — FAILED (RT OVERWING) · airframe 6,737 hrs · 6,397 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW EMB 33-50-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (ENGINE OIL SYS)

DFW - FLT 3601 - A OIL SMELL IN COCKPIT AND CABIN AFTER NR 2 ENGINES START WITH OIL PRESSURE ONLY READ 19 PSI. RAI RIGHT ENGINE OIL PRESSURE SWITCH, IAW ROLLS ROYCE MM 79-33-10, OPS CHECK NORMAL. PERFORMED ROLLS ROYCE FIM TASK 72-00-00-810-814. PERFORMED BLOCKS 12, 13, 14 OF FIM ABOVE IDLE RUN, NO OIL SMELL NOTED. OPS CHECK GOOD IAW EMB 145, AMM 72-00-00. AIRCRAFT RETURNED TO SERVICE. (M)

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

SERVICE DOOR SILL AFT GALLEY BOLT HOLE CORRODED OUT OF LIMITS. REPLACED SILL IAW SRM. AIRCRAFT RETURNED TO SERVICE. (K)