N665BC

Part: NONE — NONE (NONE) · airframe 46,857 hrs · 44,246 cycles

SEVERE TURBULANCE EXPERIENCED. INSPECTED AIRCRAFT IAW W/C 05-20-03. NO DFECTS NOTED. OK FOR SERVICE.

Part: RELAY — FAULTED (ZONE 700) · airframe 46,788 hrs · 44,167 cycles

AFTER TAKE OFF AND ATTEMPTING TO RAISE MLG, THE GEAR LEVER WOULD NOT MOVE. RAN QRH AND RETURNED TO FIELD. R & R RELAYS K0024, K0453, AND K0025 IAW AMM 20-13-02. PERFORMED GEAR SWING IAW AMM 32-30-00. SWUNG GEAR , MULTIPLE TIMES NO DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: CONTROL LEVER — STUCK (ZONE 700) · airframe 46,772 hrs · 44,146 cycles

GEAR LEVER WAS STUCK IN DOWN POSITON AFTER TAKEOFF. FACT 15DEC25 11:22 CLT R+R LANDING GEAR CONTROL LEVER IAW AMM 32-32-02. OPS CHECK GOOD. GOOD FOR SERVICE.

Part: WIRE — DAMAGED (CHART LIGHT) · airframe 46,391 hrs · 43,696 cycles

CAPT YOKE CHART HOLDER LIGHT WIRING IS DAMAGED AND C/B H-11 IS POPPED. -C/B H-11 POWERS LIGHT-. COLLARED C/B H-11 MEL 02OCT25 08:41 LYH C27511 33-1 FLT COMPARTMENT INSTRUMENT LIGHTING FACT 04OCT25 02:05 SBY R&R'D CA CHART HOLDER ASSY IAW AMM 25-12-11. RESET C/B H11 OPS CHECK GOOD CLEAR MEL 33-1 CA CHART HOLDER OK FOR SERVICE AT THIS TIME

Part: WIRE — DAMAGED (CHART LIGHT) · airframe 46,391 hrs · 43,696 cycles

CAPT YOKE CHART HOLDER LIGHT WIRING IS DAMAGED AND C/B H-11 IS POPPED. -C/B H-11 POWERS LIGHT- COLLARED C/B H-11 MEL 02OCT25 08:41 LYH C27511 33-1 FLT COMPARTMENT INSTRUMENT LIGHTING

Part: UNKNOWN — ODOR (CABIN) · airframe 45,332 hrs · 42,486 cycles

IN FLIGHT BURNING ELECTRICAL SMELL IN FLIGHT DECK AND CABIN WITH PACKS RUNNING. FUMES DISSAPETED AFTER 5 MINUTES. FACT 23MAR25 04:30 TYS RAN PACKS REF AMM 21-51-00. NO FUMES NOTED. INSPECTED BOTH PACKS NO DAMAGE NOTED. REINSTALLED PACK PANELS. OK FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 45,014 hrs · 42,133 cycles

DURING T/O ROLL ENGINE 1 OIL PRESSURE WENT TO 170 PSI. E-1 HAD BEEN OPERATING AT LEAST 20 MINUTES AT THE TIME. DURATION AND TEMP UNKNOWN. (NOTHING ON CMC) C/W RR FIM 79-37-00-810-805 STEPS 1 THRU 7, 20. OIL PRESSURE & TEMP REMAINED IN REGION A. PEAK OIL PRESSURE 136 PSI @ TEMP 48C AT THRUST SET. OPS CK GOOD. A/C OK FOR SERVICE.

Part: SKIN — DENTED (ZONE 600 FLAP) · airframe 44,510 hrs · 41,557 cycles

RH IB FLAP UPPER SKIN TE DENTED IN 2 PLACES. REPAIRED IAW EO1-57-24-0560

Part: TILLER — FAULTED (NLG STEERING) · airframe 44,246 hrs · 41,263 cycles

DURING TAXI NLG STEERING OVER CONTROLING FACT 29JUN24 18:30 PHL R+R TILLER IAW 32-50-01. PERFORMED ADJUSTMENT TEST ON LOAD POT IAW 32-50-05. FOUND W/I LIMITS PERFORMED TAXI CHECK. OPS CHECK GOOD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,307 hrs · 40,221 cycles

AUTO PILOT WOULD NOT ENGAGE WITH FLIGHTG DIRECTOR GIVING ERRATIC INDICATIONS WITH SELECTION OF RIGHT TURN FLIGHT DIRECTOR WOULD INITATE LEFT TURN. PERFORMED OPS CHECK OF AUTOPILOT SYSTEM IAW AMM 22-11-00. AUTOPILOT SYSTEM OPS CHECK GOOD FOR SERVICE AT THIS TIME.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,257 hrs · 40,156 cycles

BLD 1/2 LOW TEMP WITH WING A/I FAIL AND WING STAB FAIL. REMOVED AND REPLACED THERMOSTAT FAN A/C IAW AMM 36-11-06 PERFORMED OPS CHECK IAW AMM 36-00-00 OPS CHECK GOOD A/C OK FOR SERVICE AT THIS TIME

Part: NONE — NONE · airframe 41,708 hrs · 38,392 cycles

BURNING SMELL NOTED IN FLIGHT DECK AND CABIN UPON LANDING HISTORY: NONE FACT 04MAR23 20:46 FLO TROUBLE SHOT IAW FIM 21-20-00-810-801-A WITH NO DEFECTS NOTED. RAN APU AND PACKS INDEPENDENTANTLY WITH CREW WITH NO DEFECTS NOTED. A/C OK FOR SERVICE

Part: NONE — NONE · airframe 41,708 hrs · 38,392 cycles

DURING TAKE OFF ROLL STRONG SMOKE ODOR NOTED IN FLIGHT DECK AND CABIN. ODOR DISSIPATED WHEN RETURNING TO GATE. HISTORY: SECOND OCCURENCE, NO HISTORY 30 DAYS FACT 04MAR23 02:19 FLO REMOVED BOTH PACK PANELS AND PERFORMED GVI - NO DEFECTS NOTED FOR LH AND RH PACKS. REINSTALLED BOTH PACK PANELS. INSPECTED DUCTS IN REAR AVIONICS BAY WITH NO DEFECTS NOTED. PERFORMED ENG RUN WITH CREW, FOUND

Part: ENGINE — UNKNOWN (NR 2) · airframe 41,094 hrs · 37,712 cycles

DURING CLIMB ENG 2 OUT EICAS MESSAGE WITH NOTABLE POP SOUND. R&R #2 ENGINE IAW W/C 71-00-00

Part: A/C PACK — ODOR (NR 2) · airframe 40,645 hrs · 37,201 cycles

WITH TEMP IN AUTO MODE USING NO.2 PACK ONLY CREW EXPERIENCED A SMOKE SMELL IN THE COCKPIT. CONFIRMED NO.2 PACK WAS ORIGIN OF SMELL. TROUBLESHOOT REFERING TO FIM 21-20-00-810-801A BAD RATTLING NOISE COMING FROM #2 ACM WHILE RUNNING AND SMOKE IN COCKPIT SUSPECT #2 ACM FAILURE END OF TROUBLE SHOOTING SEE LOG PAGE 275375-1 FOR REPAIR ACTION TAKENR&R'D #200 PACK ACM IAW AMM 21-51-03 RAN PACK #2 HOT AND FULL COLD. OPS CHECK GOOD.

Part: SENSE LINE — LOOSE (WINE ANTI ICE) · airframe 40,504 hrs · 37,046 cycles

WING A/I FAIL ON EICAS IN CLIMBOUT. R AND R RH WING A/I VLV IAW AMM 30-11-01 NO FIX. FOUND LOOSE SENSE LINE.TORQUED IAW AMM 30-11-08.OPS CHECK GOOD OK FOR SERVICE.

Part: NONE — NONE · airframe 40,503 hrs · 37,045 cycles

DURING TAKE OFF HIGH STAGE 1 VALVE FAILURE OCCURRED FOLLOWED QRH AND FLEW BELOW FL 250, NO INDICATION ON EICAS AT THIS MOMENT. FACT 18MAY22 04:47 RIC R/R HIGH STAGE ORESSURE SWITCH IN REF TO AMM 35-11-07-000/400-801A.R/R RELAYS K0059 AND K0541 AND R/R HIGH STAGE VALVE IN REF TO AMM 36-11-02-000/400-801A. OPS CHECK GOOD.OK FOR SERVICE CLEAR MEL.

Part: NONE — NONE · airframe 40,272 hrs · 36,781 cycles

NDIS 665 33-50 0039110 02APR22 SBY CLOSE SERVICE DOOR EMERGENCY EGRESS LIGHT INTERMITTENT. FACT 02APR22 10:50 SBY R&R LIGHT ASSY.

Part: NONE — NONE · airframe 40,115 hrs · 36,606 cycles

PDIS 665 21-01 2641011 04MAR22 ORD CLOSE STRONG RUBBER BURNING SMELL COMING FROM CABIN DURING DESCENT FACT 04MAR22 18:50 ORD RAN PACK 1/2 ON APU FOR 20 MINS. SMELL DISSIPATED NO DEFECTS NOTED OK FOR SERVICE.

Part: NOT REPORTED — NOT REPORTED · airframe 40,063 hrs · 36,556 cycles

RIGHT WING RIB 21 UPPER FLANGE IS CRACKED (MARKED INSIDE PCA AREA) .... PERFORMED CUTOUT OF DAMAGE TO RH WING RIB 21 AND FABRICATED, PREPPED, AND INSTALLED REPAIR DOUBLER, REPAIR FILLER, AND SHIM IAW EMB 145 SRM 57-20-07 ITEM 4 FIGURE 203 AND EO1-57-22-0009.

Part: NOT REPORTED — NOT REPORTED · airframe 40,063 hrs · 36,556 cycles

E898758 - CARGO DOOR INTERIOR WEBBING HAS MULTIPLE GOUGES .... RE-ACCOMPLISHED THREE PREVIOUS REPAIRS TO CARGO DOOR INTERIOR WEBBING IAW EMB145 SRM 52-30-01, ITEM 12, FIGURE 213 AND EO1-52-22-0015, AND ETD2022-145-001584REV A AND EO-1-05-22-0018

Part: NOT REPORTED — NOT REPORTED · airframe 40,063 hrs · 36,556 cycles

E898854 - RH #2 FLOORBOARD SUPPORT CORRODED IN MULTIPLE AREAS .... RH #2 FLOORBOARD SUPPORT CORRODED IN MULTIPLE AREAS

Part: NOT REPORTED — NOT REPORTED · airframe 40,063 hrs · 36,556 cycles

E898855 - CENTER #4 FLOORBEAM GUSSET CORRODED IN ONE SPOT .... RAR CENTER #4 FLOOR BEAM GUSSET IAW EMB-145 SRM 51-40-02.

Part: NOT REPORTED — NOT REPORTED · airframe 40,063 hrs · 36,556 cycles

E898655 - PILOTS BULKHEAD UPPER OTBD ATTACHMENT HOLE IS GOUGED ..... REPAIRED GOUGED AREA (BLENDED) ON PILOTS BULKHEAD UPPER OUTBOARD ATTACHMENT HOLE FOUND TO BE WITHIN LIMITS IAW EMB 145 SRM 53-21-02

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 40,063 hrs · 36,556 cycles

E898840 - LH OUTBD FLOOR SUPPORT CORRODED IN IN NUMEROUS AREAS BTWN FR 24-29 .... REMOVED AND REPLACED LH #2 FLOOR SILL IAW EMB 145 SRM 51-40-02 AND 51-20-03

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 40,063 hrs · 36,556 cycles

E899178 - RH OMEGA BEAM GUSSET AT FR 22 IS CORRODED AT FWD SCREW HOLE.(PREVIOUS BLEND) .... REMOVED UN-SERVICEABLE RH OMEGA BEAM GUSSET AT FR 22, POSITIONED, DRILLED AND INSTALLED NEW SERVICEABLE RH OMEGA BEAM GUSSET AT FR 22 IAW EMB 145 SRM 51-40-02 AND EMB 145 SRM 51-20-03

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 40,063 hrs · 36,556 cycles

E899181 - SERVICE DOOR FWD SILL IS CORRODED AT FWD END .... REMOVED AND REPLACED SERVICE DOOR FWD SILL IAW EMB 145 SRM 51-40-02. SEE WIP AND TASK FOR DETAILS

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 40,063 hrs · 36,556 cycles

E899182 - SSI 53-20-11 RH OMEGA BEAM IS CORRODED AROUND SCREW HOLE AT FR 19 .... INSTALLED SERVICEABLE REPAIR DOUBLER AT NUTPLATE HOLE ON RH OMEGA BEAM AT FR 19 IAW ETD2022-145-001841 AND PIEDMONT EO1-53-22-0014.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 40,063 hrs · 36,556 cycles

E898841 - LH FLOOR BEAM GUSSET CORRODED IN NUMEROUS AREAS BTWN FR 24-29 .... RAR LH # 2 FLOOR BEAM GUSSET IAW EMB 145 SRM 51-40-02.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 40,063 hrs · 36,556 cycles

E898987 - RH #3 FLOORBOARD SUPPORT CORRODED IN MULTIPLE AREAS .... RAR RH #3 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02, 51-40-09

Part: NONE — NONE · corrosion level 2 · airframe 40,063 hrs · 36,556 cycles

E898857 - CENTER #2 FLOORBEAM GUSSET CORRODED IN MULTIPLE AREAS .... REMOVED CORRODED CENTER FLOOR BEAM GUSSET #2 AND INSTALLED SERVICEABLE CENTER FLOOR BEAM GUSSET #2 IAW EMB 145 SRM 51-40-02.

Part: NOT REPORTED — NOT REPORTED · airframe 40,063 hrs · 36,556 cycles

E898856 - CENTER #1 FLOORBEAM GUSSET CORRODED IN MULTIPLE AREAS .... REMOVED CORRODED CENTER FLOOR BEAM GUSSET #1 AND INSTALLED SERVICEABLE CENTER FLOOR BEAM GUSSET #1 IAW EMB 145 SRM 51-40-02.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 40,063 hrs · 36,556 cycles

E898968 - LH #4 CABIN FLOOR SILL CORRODED .... RAR CABIN LH OUTBD FLOOR SILL #4 IAW EMB-145 SRM 51-40-02. SEE WIPS AND TASK FOR FURTHER INFORMATION

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 40,063 hrs · 36,556 cycles

E898842 - LH FLOOR BEAM GUSSET CORRODED IN NUMEROUS AREAS BTWN FR 29-35 .... REMOVED CORRODED LH FLOOR BEAM GUSSET BETWEEN FRAMES 29-35 AND INSTALLED SERVICEABLE LH FLOOR BEAM GUSSET BETWEEN FRAMES 29-35 IAW EMB 145 SRM 51-40-02

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 40,063 hrs · 36,556 cycles

E898787 - LH #7 CABIN FLOOR SILL CORRODED .... RAR LH #7 CABIN FLOOR SILL IAW EMB-145 SRM 51-40-02

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 40,063 hrs · 36,556 cycles

E898853 - RH #1 FLOORBOARD SUPPORT CORRODED IN MULTIPLE AREAS .... RAR RH #1 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02.SEE WIPS AND TASKS FOR DETAILS.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 40,063 hrs · 36,556 cycles

E898839 - LH OUTBD FLOOR SUPPORT CORRODED IN IN NUMEROUS AREAS BTWN FR 29-35 .... INSTALLED SERVICEABLE LH OUTBD FLOOR SUPPORT BTWN FR 29-35 IAW EMB145 SRM 51-40-09 AND 51-40-02

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 40,063 hrs · 36,556 cycles

E898270 - RH ENGINE UPPER COWLING RIB GUSSET FWD OF ANTI/ICE ACCESS PANEL CORRODED .... REMOVED AND REPLACED RH ENGINE UPPER COWLING RIB GUSSET, FORWARD OF ANTI/ICE ACCESS PANEL ,IAW EMB145 SRM 51-40-02.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 40,063 hrs · 36,556 cycles

E898635 - SSI - CARGO DOOR LOWER CENTER SILL IS CORRODED .... MECHANICALLY MEASURED DEPTH OF CORROSION ON LOWER CARGO DOOR SILL AND FOUND IT TO BE OUT OF LIMITS IAW EMB 145 SRM 53-31-15-AD. RAR SERVICEABLE CARGO DOOR CENTER STILL IAW EMB 145 SRM 51-40--02.

Part: UNKNOWN — ODOR (CABIN) · airframe 39,934 hrs · 36,407 cycles

AFTER ELECTRICAL RESET, APU START AND ALL SYS TESTS PASSED, SHORTLY AFTER GOT INDICATION OF BURNING/ELECTRICAL BURNING SMELL IN FLT DECK WITH EMERGENCY LIGHTS TRIPPING ON AND WILL NOT GO OFF. PERFORMED GVI OF CAPTS AND FO RELAY PANELS NO DEFECTS NOTED, PERFORMED GVI OF CB PANEL NO DEFECTS NOTED, CHECKED FLASHLIGHTS NO DEFECTS NOTED. RAN APU + APU BLEED WITH PACKS ON AND AC FULLY POWERED AND NO DEFECTS NOTED AND COULD NOT DUPLICATE PROBLEM AFTER RUNNING FOR 30 MINUTES.

Part: WIRE — CHAFED (PUMP) · airframe 39,139 hrs · 35,533 cycles

NSPECTED C/P P0259 NO DEFECTS NOTED RAN #2 ENGINE WITH P0259 DISCONNECTED PUMP ALTERNATING STILL EXISTED REGRADLESS OF PUMP SELECTED RECONNECTED P0259 AS REQ'D REMOVED RELAY K0300 RAN #2 ENGINE AGAIN NO PUMP ALTERNATING OR OTHER DEFECTS NOTED WITH ANY PUMP SELECTED WITH #2 ENGINE RUNNING FOUND SHORT TO GROUND AT XK0300 PIN B2 HOWEVER SHORT ONLY OCCURS AT AROUND 90 PERCENT N2 AND ONLY WEHN ACCELERATING ENGINE SLIGHTLY FASTER THAN NORMAL WHICH COINCIDES WITH PUMP ALTERNATING DISCREPANCY CONDITIONS WITH PUMP AL TERNATING DISCREPANCY CONDITIONS SHUT DOWN ENGINE REINSTALLED RELAY K0300 IAW AMM 20-13-02-04 FOUND WIRE W407-0020-20 CHAFED AT 3 O CLOCK POSITION OF #2 ENGINE AFT END JUST BELOW C/P P0819. R&R WIRE AND TERMINATED AT P0819 I/A/W SWPM 20-00-03 TERMINATED WIRE #407-0020-20 AT CONNECTOR P0259 IN REF TO SWPM 20-50-00. R&R'D WIRE #407-0007-20 I/A/W SWPM 20-50-00.ERROR & REINSTALLED C/P P0819, P0259. REINSTALLED C/P 0583. RAN A/C OPS CHECK GOOD OKAY FOR SERVICE @ THIS TIME

Part: PRESSURE SWITCH — FAULTED (NR 2 ENGINE FUEL) · airframe 39,139 hrs · 35,532 cycles

REJECTED TAKE OFF WHILE ON TANK 2C PUMPS ALTERNATED FROM 2C TO 2B. R&R'D #2 ENG LOW FUEL PRESS SW IAW AMM 28-45-01-04. RAN #2 ENG ON EACH PUMP (2A,2B,2C) AT VARIOUS POWER SETTINGS. NO ABNORMAL CLICKING OR PUMP CYCLING NOTED AT THIS TIME. OPS AND LEAK CK GOOD.

Part: ENGINE — SHUTDOWN (NR 2) · airframe 38,577 hrs · 34,958 cycles

ENGINE NR 2 SHUTDOWN IN FLIGHT (NO ABNORMAL INDICATIONS PRIOR TO SHUTDOWN). ENGINE IS BEING R&R'D CURRENTLY IN BDL.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 38,329 hrs · 34,673 cycles

RT AFT OVERWING EMERGENCY LIGHT WILL NOT ILLUMINATE. R&R RT EMERGENCY LIGHT IAW AMM TASK 33-50-10-000/400-801-A. OPERATIONS CHECK GOOD, OK FOR SERVICE.

Part: A/C PACK — FAILED (AC BAY) · airframe 38,183 hrs · 34,513 cycles

BURNING SMELL IN COCKPIT AND CABIN CLEARED WHEN GASPER AND RECIRC FANS WERE SELECT OFF PER QRH. MAINTENANCE: TROUBLESHOOT IN REF TO FIM TASK 21-20-00-810-801-A. FOUND TO BE FAILURE OF NR 1 PACK SEE SEQ 2 FOR PACK NR 1 MEL.

Part: PRESSURE SWITCH — DEFECTIVE (RUDDER) · airframe 38,116 hrs · 34,431 cycles

RUDD SYS 1 AND 2 INOP, EICAS MESSAGE DISPLAYED. CREW PERFORMED PROCEDURE AND RUDD 1 CAME BACK ON LINE. RUDD 2 REMAINED INOPERATIVE. TS RUDDER SYS 1+2 INOP MESSAGE REF FIM 27-22-00 STEPS 1 AND 8. R&R NR 1 + NR 2 RUDDER HYDRAULIC PRESSURE SWITCH REF AMM 27-23-04. OPS CHECK GOOD. OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 37,978 hrs · 34,271 cycles

RUDDER SYS 1-2 INOP MSG DISPLAYED. CREW RAN QRH AND MSG CLEARED. MAINTENANCE: C/W OPERATIONAL CHECK OF RUDDER EICAS MESSAGES IAW EMB 145 AMM 27-23-00, OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 37,966 hrs · 34,257 cycles

PDIS 665 27-51 2184402 18MAR20 CLT CLOSE WHEN SELECTING FLAPS TO 9 DEGREES, THEY REMAINED AT 0 DEGREES. NO ASSOCIATED EICAS MESSAGES. 18544 FACT 18MAR20 18:07 CLT POWERED DOW AND POWERED UP, RAN FLAPS SEVERAL TIMES NO DEFECTS NOTED. OK FOR SERVICE.

Part: ENGINE — FIRE (NR 1) · airframe 37,880 hrs · 34,168 cycles

ON #1 ENG SHUTDOWN. RAMP REPORTED FIRE FROM ENGINE EXHAUST. CREW FOLLOWED QRH, FIRE EXTINGUISHED DURING QRH PROCEDURES. PULLED T-HANDLE BUT DID NOT BLOW BOTTLE. EXTENSIVE SMOKE CONTINUED AFTER FIRE DISSIPATED....FIX: R&RD #1 ENG IAW W/C 71-00-00. PERFORMED ENG RUN-UP IAW W/C 72-70-00. NO DEFECTS NOTED. OK FOR SERVICE.

Part: ENGINE — FIRE (NR 1) · airframe 37,885 hrs · 34,174 cycles

PDIS 665 05-50 2184241 02MAR20 PHL ASSGN ENGINE #1 TAILPIPE FIRE REPORTED ON ENGINE SHUTDOWN. RAN QRH, FIRE EXTINGUISHED ENGINE IS BEING R&R'D IN PHL

Part: VALVE — FAILED (FAN AIR) · airframe 37,523 hrs · 33,753 cycles

NR 2 ENGINE BLLED OVERTEMP EICAS MSG WITH MASTER WARNING AND FULL RED INDICATION ON THE EICASW BLEED 2 TEMP INDICATOR . REMOVED AND REPLACED FAN AIR VALVE IAW AMM 36-11-03-000-801-A, AND 36-11-03-400-801-A. LEAK AND OPS CHECKED GOOD. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 37,000 hrs · 33,151 cycles

NDIS 665 33-40 0020660 27SEP19 SBY CLOSE OVER WING EMERGENCY LIGHT INOP ON RH SIDE 35717 00 BRA FACT 27SEP19 13:31 SBY R AND R OVER WING EMERGENCY LIGHT IAW AMM TASK 33-50 -10-04 SUBTASK 020-004A AND SUBTASK 420-005-A OPS CH ECK GOOD OK FOR SERVICE

Part: PRESSURE SWITCH — MALFUNCTIONED · airframe 36,342 hrs · 32,408 cycles

PDIS 665 30-21 1872011 18APR19 BTV CLOSE E2 A/I INOP MSG DISP ON T/O ROLL. C/W MAINTENANCE PR OCEDURE. FACT 18APR19 07:56 PHL R&R PRESSURE-ELECTRONIC SWITCH IAW EMB 145 AMM 30-21 -06. OPS CHECK GOOD. OK FOR SERVICE AT THIS TIME. CL EAR MEL 30-8-1

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 36,108 hrs · 32,157 cycles

PDIS 665 21-50 2015091 07MAR19 ROC CLOSE PFD FAILURE FOLLOWED BY ELECTRICAL SMELL IN COCKPIT AND CABIN FACT 07MAR19 21:33 RIC SWAPPED #1 DU WITH #4 DU PER AMM 34-22-01. OPS GOOD, OK FOR SERVICE. (SEE L/P 201510-1 FOR #4 DU MEL.)

Part: UNKNOWN — ODOR (COCKPIT) · airframe 35,374 hrs · 31,309 cycles

PDIS 665 05-52 1743622 02OCT18 PHL CLOSE POSSIBLE LIGHTNING STRIKE IN CRUISE FLIGHT. CREW RETURNED TO PHL AIRPORT. STRONG ELECTRICAL SMELL IN COCKPIT. 22107 00 JJC HISTORY: NO ISTORY: .FACT 02OCT18 23:42 PHL INSP A/C IAW W/C 05-20-00 FOUND ON EVIDENCE OF LIGHTNING STRIKE AND FOUND NO FOUL ODORS OR ELECTRIC SMELLS COMING OUT OR FROM A/C OK FOR SERVCE AT THIS TIME

Part: MUFFLER — OBSTRUCTED (RECIRCULATION) · airframe 35,133 hrs · 31,014 cycles

CREW REPORTED A STRONG ODOR WITH THE NR 2 PACK SELECTED. FOUND AN OBSTRUCTION IN THE RECIRCULATION SYS. CLEANED THE MUFFLER IAW 21-24-02-100-801-A. NO ABNORMAL ODORS NOTED.

Part: RETAINING CLIP — BROKEN (SPOILER SYS) · airframe 34,975 hrs · 30,845 cycles

SPOILERS OPEN AND CLOSE INTERMITTENTLY DURING TAXI UNDER 25 KTS. SPOILER FAIL MESSAGE DISPLAYED. CONFIRMED DISCREPENCY. INSPECTED WHEEL SPEED DRIVES REF 32-49-02/600. FOUND BROKEN CLIP. REPLACED NR 4 HUBCAP AND REPLACED RELAYS K0059 AND K0363 AS PRECAUTIONARY MEASURE. TAXIED AIRCRAFT. NO DISCREPENCIES NOTED AT THIS TIME. REF FIM TASK 27-63-00-810-805A.

Part: O-RING — LEAKING (LPT SHAFT PLUG) · airframe 34,744 hrs · 30,579 cycles

WHITE SMOKE COMING FROM THE NR 1 ENGINE EXHAUST . REPLACED THE LPT SHAFT PLUG O-RING.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 34,123 hrs · 29,893 cycles

LAVATORY SMOKE EICAS MESSAGE . NO SIGNS OF SMOKE OR FIRE. R & R THE LAVATORY SMOKE DETECTOR IAW AMM 26-14-01. OPS CHECKED GOOD. AIRCRAFT GOOD FOR SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 34,118 hrs · 29,887 cycles

LAVATORY SMOKE WARNING MESSAGE ILLUMINATED ON EICAS WITH FIRE ALARM IN CABIN. PERFORMED AN OPS CHECK OF THE LAVATORY SMOKE DETECTION SYSTEM IAW AMM 26-14-00. NO SIGNS OF SMOKE OR FIRE. OPS CHECKED GOOD. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (E/E BAY DOOR) · airframe 34,083 hrs · 29,853 cycles

REJECTED TAKEOFF DUE TO A FORWARD ELECTRONIC COMPARTMENT ACCESS HATCH OPEN INDICATION. RETURN TO GATE. DEACTIVATED IAW 52-71-01-000-801-A.

Part: WARNING LIGHT — FALSE ACTIVATION (DE ICE SYS) · airframe 33,460 hrs · 29,214 cycles

BOTH BLEEDS WENT OVERTEMP DURING ICE TEST. DOWNLOADED CMC TO MFD WITH NO RELATED CMC MESSAGES PRESENT AND NO RECENT HISTORY OF DISCREPANCY. PERFORMED AN ICE PROTECTION TEST SEVERAL TIMES WITH NO DEFECTS NOTED. OPS CHECKED GOOD. ALL SYSTEMS OPERATE NORMALLY AT THIS TIME. OKAY FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED · airframe 32,923 hrs · 28,641 cycles

EICAS MESSAGE FOR E1 NO DISPATCH, CMC MESSAGE GVG SYS DIFF. OPEN

Part: ADAPTER — FAILED (ELECTRICAL) · airframe 32,569 hrs · 32,258 cycles

ABORTED TAKEOFF AT 60 KTS. DUE TO EICAS WARNING OF E1, N1.ENGINE ON FADEC A. CREW NOTICED A RUSH OF AIR PRIOR TO EICAS MESSAGE, THEN AIR STOPPED AFTER MESSAGE ON HIGH PRESSURE VIB METER. #I ENGINE NOTICEABLY HIGHER AFTER ABORT. INSPECTED CONNECTOR J4 ON FADEC POSITION 2A S/N BX161213. OPEN FADEC 2A CIRCUIT BREAKER, REMOVED J4 CONNECTOR AND REMOVED THE DIODE ADAPTER. REINSTALL CONNECTOR J4 IAW 70-00-00-910-804 AND TEST ENGINE IAW 72-00-00-700.

Part: WINDSHIELD — ODOR (COCKPIT) · airframe 32,535 hrs · 28,222 cycles

WINDSHIELD NR 1 HEAT FAIL CAUTION MESSAGE APPEARED. CREW PULLED C/B G13. BURNING ODOR NOTED FROM WINDOW. PERFORMED OPS CHECK IAW TASK NUMBER 30-42-00-700-801-A. COULD NOT DUPLICATE THE PROBLEM, OPS CHECKED GOOD. OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (NLG ACCESS PANEL) · airframe 32,506 hrs · 28,192 cycles

NOSE GEAR ACCESS PANEL INDICATION INFLIGHT.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 32,493 hrs · 28,180 cycles

SERVICE DOOR FWD LWR STOP BACK UP STRUCTURE BRACKET HAS CRACK. REMOVED AND REPLACED SERVICE DOOR FWD LWR BEAM IAW SRM 51-40-02.

Part: CONNECTOR — BROKEN (CABIN) · airframe 32,492 hrs · 28,179 cycles

NR 1 LT FLOOR PROXIMITY LIGHT CONNECTOR BROKEN. REMOVED AND REPLACED NR 1 LT FLOOR PROXIMITY LIGHT IAW AMM 33-50-12.

Part: WEB — GOUGED (CARGO DOOR) · airframe 32,492 hrs · 28,179 cycles

CARGO DOOR INNER WEB IS GOUGED AT LOWER END BELOW TORSION BAR. REPAIRED CARGO DOOR LOWER INNER WEB IAW SRM 52-30-01 AND ETN-EM-52-043.

Part: WEB — GOUGED (CARGO DOOR) · airframe 32,492 hrs · 28,179 cycles

CARGO DOOR INNER WEB FWD LOWER PREVIOUS REPAIR IS GOUGED. REMOVED AND REPLACED CARGO DOOR INNER WEB FWD LOWER PREVIOUS REPAIR IAW SRM 52-30-01 AND ETN-EM-52-043.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,492 hrs · 28,179 cycles

BURN IN SKIN AT FRAME 29 BETWEEN STRINGERS 18R-19R. REPAIRED FUSELAGE SKIN BURN AT FRAME 29 BETWEEN STRINGERS 18R-19R IAW ERS-EM-53MR-2557.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 32,492 hrs · 28,179 cycles

LT EMERGENCY EXIT LOWER FRAME CORRODED AROUND SCREW HOLE. REPAIRED LT EMERGENCY EXIT LOWER FRAME CORROSION AROUND SCREW HOLE IAW ERS-EM-52MR-700.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,492 hrs · 28,179 cycles

LT AFT FUSELAGE FR 75 SKIN CRACK ABOVE STR 2L. PERFORMED PERMANENT REPAIR OF LT AFT FUSELAGE FR 75 SKIN CRACK ABOVE STR. 2L IAW SRM 53-31-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,492 hrs · 28,179 cycles

BURN IN SKIN BETWEEN FRAMES 23-24 AT STRINGER 19R. REPAIRED BURN IN SKIN BETWEEN FRAMES 23-24 AT STRINGER 19R IAW ERS-EM-53MR-2556.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,492 hrs · 28,179 cycles

BURN IN SKIN BETWEEN FRAMES 23-24 AT STRINGER 19R. REPAIRED BURN IN SKIN BETWEEN FRAMES 23-24 AT STRINGER 19R IAW ERS-EM-53MR-2556.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,492 hrs · 28,179 cycles

RT AFT FUSELAGE FR 75 SKIN CRACK ABOVE STR 2R. PERFORMED REPAIR OF RT AFT FUSELAGE FR 75 SKIN CRACK ABOVE STR. 2R IAW SRM 53-31-01.

Part: WIRE — BROKEN (CABIN) · airframe 32,492 hrs · 28,179 cycles

LT CABIN FLOOR EMERGENCY PROXIMITY LIGHT STRIP NR 3 WIRES BROKEN. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,492 hrs · 28,179 cycles

RT AFT FUSELAGE FR 75 SKIN CRACK ABOVE STR 2R MARKED. REPAIRED RT AFT FUSELAGE FR 75 SKIN CRACK ABOVE STR 2R IAW SRM 53-31-01 ITEM 11. SEE TASKS AND WIPS FOR DETAILS.

Part: SKIN — CRACKED (FRAME 75) · airframe 32,492 hrs · 28,179 cycles

LEFT AFT FUSELAGE FRAME 75 SKIN CRACKED BELOW STRINGER 2L. REPAIRED IAW SRM 53-31-01.

Part: ANGLE — CRACKED (WING) · airframe 32,492 hrs · 28,179 cycles

ANGLE ABOVE 156EZ CUTOUT IS CRACKED ON FWD SIDE AT OTBD END. REMOVED CRACKED ANGLE ABOVE 156EZ CUTOUT ON FWD SIDE AT OTBD END AND INSTALLED SERVICEABLE ANGLE IAW SRM 51-40-02 AND SRM 51-20-01.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 32,492 hrs · 28,179 cycles

LT OVERWING EXIT LOWER FRAME IS CORRODED AROUND SCREW HOLE. PERFORMED CUT OUT OF DAMAGE, INSTALLED DOUBLER AND FILLER ON LT OVERWING EXIT LOWER FRAME IAW ERS-EM-52MR-700.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 31,848 hrs · 27,558 cycles

RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-07. OPS CHECK FAILED.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 31,848 hrs · 27,558 cycles

LEFT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-07. OPS CHECK FAILED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,761 hrs · 27,469 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. REPLACE AFT CABIN AISLE EMERGENCY LIGHT AND OPC, GOOD, REFER TO AMM 33-50-08.

Part: PUMP — FAILED (LT ENGINE) · airframe 31,634 hrs · 27,346 cycles

HYD 1 LOW QTY, ENG 1 HYD PUMP FAIL, THEN RECOVERED, ALSO LEAKING HYD FLUID, ENGINE 1. R & R ENGINE 1 HYD ENGINE DRIVEN PUMP IAW AMM 29-10-03. ITEM NR 2 ON THIS LOG PG FOR LEAK TEST. PERFORMED EDPM NR 1 ENGINE LEAK TEST IAW AMM 29-10-03 SECTION J, ITEM 7. OPS CHECK GOOD, NO LEAKS NOTED.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 31,418 hrs · 27,145 cycles

FA REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE REPET WRITE UP PG 3900301. LUBRICATED MAIN DOOR FRAME ROLLERS IAW MM 53-21-02, OPS CHECKED OK IAW MM 52-10-01

Part: SEAL — LACK OF LUBE (PAX DOOR) · airframe 31,399 hrs · 27,125 cycles

MAIN CABIN DOOR IS HARD TO OPERATE. LUBED DOOR SEALS AND OPS CHECKED IAW 51-10-01 OPS CHECKED GOOD.

Part: DOOR — NONE · airframe 31,392 hrs · 27,117 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOS. TESTED MAIN CABIN DOOR IAW AMM 52-10-01-05. OPS CHECK GOOD

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 31,384 hrs · 27,109 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. LUBRICATED MAIN PASSENGER DOOR ROLLERS IAW EMB AMM 52-18-00. DOOR OPENS AND CLOSES PROPERLY

Part: DUCT — CRACKED (BLEED AIR SYS) · airframe 31,378 hrs · 27,101 cycles

ENROUTE, CREW EXPERIENCED AN ODOR OF SMOKE AND HAZE IN THE COCKPIT. COMPLIED WITH AOM VOL 1 PROCEDURES, DECLARED AN EMERGENCY AND DIVERTED. CRF CLEARED THE AIRCRAFT. DURING TROUBLESHOOTING FOR SMOKE & FUMES, FOUND NR 1 BLEED DUCT CRACKED AT ELBOW NEAR ROW 17 - 18 WHERE DUCT TRANSITIONS TO BELLY OF AIRCRAFT. R & R THE DUCT ASSY IAW AMM 36-11-09. DURING TROUBLESHOOTING OF SMOKE/FUMES IN COCKPIT NOTED THAT THE NR 1 ACM APPEARS SEIZED, IT IS NOT DWG AIR IN AND THERE IS LITTLE AIR FLOW COMING OUT THE EXHAUST. R & R NR1 PACK ACM IAW 21-51-03, AMM. OPS CHECK, LEAK CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,379 hrs · 27,102 cycles

EMERGENCY LIGHT ROWS 10,11, & 12 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 31,121 hrs · 26,885 cycles

FLIGHT ATTENDANT FLASHLIGHT CRADLE CRACKED. R & R FLIGHT ATTENDANT FLASHLIGHT CRADLE IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: PITOT SYSTEM — CONTAMINATED (NR 1) · airframe 28,905 hrs · 24,759 cycles

LOST CAPTAIN'S AIRSPEED INDICATOR, SWITCHED TO ADC FROM FIRST OFFICER'S SIDE. SPS ADVANCED SHOWED ON EICAS. INSPECTED & FOUND WATER IN NR 1 PITOT SYS. DRAINED WATER & PERFORMED LEAK CHECK IAW AMM 34-13-00. OPERATIONS CHECK OF ADC IAW AMM 34-15-00, OPERATIONS CHECK & LEAK CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 28,206 hrs · 24,049 cycles

FIRST OFFICER`S FLASHLIGHT CRADLE BROKEN. R & R FIRST OFFICER`S FLASHLIGHT CRADLE IAW AMM 33-50-16-000-801 & 33-50-16-400-801. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,180 hrs · 24,029 cycles

COCKPIT FLASHLIGHT CLIP HOLDER BROKEN. ISSUING MEL 25-53, CAT C. R & R FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: LIGHT — WRONG PART (CABIN) · airframe 28,076 hrs · 23,939 cycles

EMERGENCY LIGHTING AISLE FLOOR STRIP IS THE WRONG COLOR AT ROW 18. REPLACED IAW AMM CPT 32-50-12. OPERATIONS CHECKED OK.

Part: FRAME — CHAFED (FUSELAGE) · airframe 27,946 hrs · 23,818 cycles

FRAME 15 IS CHAFED AT STRINGER 2R. COMPLIED WITH REPAIR TO FRAME 15 AT STRINGER 2R IAW ERS-EM-53MR-944.

Part: BUSHING — CORRODED (RUDDER) · airframe 27,946 hrs · 23,818 cycles

RUDDER 2 UPPER HINGE FITTING HAS CORRODED HAT BUSHINGS, FOUND BORE DAMAGED. INSTALLED NEW RUDDER 2 UPPER HINGE FITTING ASSEMBLY IAW SRM 55-40-02 & ETN EM-55-070. REPLACED BOTH SLEEVE BUSHINGS & BOLT WITH NEW IAW IPC 27-21-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,946 hrs · 23,818 cycles

LEFT REAR FUSELAGE SKIN NR 2 HAS CRACKS BY THE RIVET AT FRAME 78 BETWEEN STRINGERS 3L - 4L. REPAIRED DAMAGE AT FRAME 78, STRINGER 3L - 4L IAW ERS-EM-5300-960.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,946 hrs · 23,818 cycles

RIGHT REAR FUSELAGE SKIN NR 2 HAS CRACK BY THE RIVET AT FRAME 79 JUST BELOW STRINGER 6R. COMPLETED DOUBLER REPAIR TO SKIN AT FRAME 79 RT IAW ERS-EM-5300-959.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 27,946 hrs · 23,818 cycles

FRAME 80 RT STRINGER 8R SUPPORT CLIP IS CRACKED. INSTALLED A NEW SUPPORT CLIP IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 27,946 hrs · 23,818 cycles

CARGO DOOR ASSIST CABLE ROD SUPPORT BRACKET IS CRACKED ON THE FRONT END AT FRAME 61 RT. R & R CARGO DOOR ASSIST CABLE ROD SUPPORT BRACKET AT FRAME 61 RT IAW SRM 51-40-02.

Part: PROFILE — CRACKED (E&E DOOR) · airframe 27,946 hrs · 23,818 cycles

REAR ELECTRONICS COMPARTMENT DOOR UPPER PROFILE CRACKED UNDER DOOR SUPPORT BRACKET. REPAIRED REAR ELECTRONICS COMPARTMENT DOOR UPPER PROFILE UNDER DOOR SUPPORT BRACKET IAW ERS-EM-5200-262.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 27,946 hrs · 23,818 cycles

FRAME 80 LT STRINGER 8L SUPPORT CLIP IS CRACKED. R & R SHEAR CLIP IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,946 hrs · 23,818 cycles

RIGHT OVERWING FUSELAGE PANEL UPPER ATTACH ANGLE AFT END HAS SHEARED RIVETS & IS CRACKED. REPAIRED RT OVERWING FUSELAGE PANEL UPPER ATTACH ANGLE IAW SRM 53-23-12 ITEM 3 TYPE 1 REPAIR.

Part: WIRE HARNESS — CHAFED (NR 2 ENGINE) · airframe 27,894 hrs · 23,759 cycles

IN FLIGHT AFTER EXITING ICING CONDITION E2 ANTI-ICE FAIL WITH VLV IN OPEN POS, SHOULD HAVE CLOSED. RESET IAW AOM VOL 1 PROC TESTED ANTI-ICE IN ALL E2 ANTI-ICE FAIL MSG. VLV WOULD NOT OPEN. LATER IN FLT E2 ANTI-ICE VLV OPENED UNCOMMANDED WITH ELECTOR IN AUTO, NOT IN ICING COND, STAYED ON 10 MIN THEN CLOSED. DEFERRED IAW MEL 30-11 M PROCEDURES COMPLIED WITH. FOUND E2 EXTERNAL INDICATING HARNESS CHAFED. R & R E2 EXTERNAL INDICATING HARNESS IAW AMM 71-51-01. OPERATIONS CHECKED GOOD IAW RR MM 72-00-00-710-001. OPERATIONS CHECK E2 ANTI-ICE VLV GOOD IAW AMM 30-00-00-700-802. OPERATIONS CHECK E2 ANTI-ICE TRANSDUCER GOOD IAW AMM 30-21-00. PRESS TRANSDUCER PN APS51500 & SN 8176-3-177.

Part: ANTI-ICE VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 27,892 hrs · 23,758 cycles

ON TAKEOFF ROLL HAD EICAS CAUTION MSGS E2 ANTI-ICE FAIL, PACK 2 OVERHEAT THEN AS ABORT WAS CALLED, EICAS WARNING OF SPS 1-2 INOPERATIVE. BEFORE ABORT WAS COMPLETE WE HAD COME PAST 80KTS THRESHOLD. ALL MSGS CLEARED AS ACFT CLEARED RUNWAY. TRANSFERRED TO NRWC 665-ORD-01842. R & R ENG 2 ANTI-ICE PRESS TRANSDUCER IAW AMM 30-21-06. OPERATIONS CHECK FAILED. R & R ENG 2 ANTI-ICE VLV IAW AMM 30-21-01. OPERATIONS CHECK GOOD IAW AML PAGE 3705021 ITEM 3 FOR PACK 2 OVERHEAT CORRECTIVE ACTION. IAW AML PAGE 3705021 ITEM 4 FOR SPS 1 - 2 INOPERATIVE. PACK TWO OPERATES AS NORMAL IAW MM 24-51-00. NO OVERHEAT MSG NOTED. STALL PROT SYS OPERATES AS NORMAL IAW MM 27-36-00. PRESS TRANSDUCER PN APS51500, SN 6810771 LT ENG FAILURE & DAMAGE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,683 hrs · 23,529 cycles

LEFT EXTERNAL OVERWING EMER LAMP INOPERATIVE. R & R IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: BRAKE ASSY — DAMAGED (NR 1) · airframe 27,228 hrs · 23,087 cycles

NUMBER 1 MLG SMOKING AT GATE. REPLACED NR 1 MLG BRAKE ASSEMBLY IAW WC 32-600-14.

Part: PACKING — LEAKING (MLG) · airframe 27,226 hrs · 23,085 cycles

SMOKE & HYD FLUID ON ON LT MAIN GEAR. R & R BLEEDER VLV PACKING IAW CMM 32-49-03. OPERATIONS CHECKED GOOD IAW AMM 32-49-07. LEAK CHECKED GOOD.

Part: ADC — MALFUNCTIONED (COCKPIT) · airframe 26,905 hrs · 22,773 cycles

AT FL 360 CAPTAIN`S AIRSPEED INDICATED 244, FIRST OFFICER`S 248 & STANDBY 248. BRIEFLY SPS ADV ON EICAS. AT FL 350 CAPTAIN`S AIRSPEED 231 FIRST OFFICER`S 248 & STANDBY 244. SOMEWHERE BETWEEN FL 350 & 310 CAPTAIN`S AIRSPEED & ALTITUDE DROPPED ABNORMALLY LOW. CAPTAIN`S PFD ALSO SHOWED AMBER IAS THROUGHOUT THIS TIME. INSPECTED PITOT DRAIN TUBES FOR WATER NONE FOUND. R & R NR 1 ADC IAW 124 34-15-1. PERFORMED OPERATIONAL TEST IAW 34-15-00-700-802 & PERFORMED NR 1 PITOT LEAK CHECK IAW 34-13-00-790-802. ACFT IS COMPLIANT FOR CONTINUE CAT II OPERATION.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,871 hrs · 22,736 cycles

CAPTAIN`S FLASHLIGHT RED LIGHT WILL NOT ILLUMINATE. R & R CAPTAIN`S FLASHLIGHT IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,460 hrs · 22,419 cycles

EMERGENCY LIGHTS COME ON TWO ROWS 8 - 11 WHEN POWER TURNED OFF. R & R NR 3 BACK UP EMERGENCY BATTERY & CHARGER ASSEMBLY IAW AMM 33--50-04. OPERATIONS CHECKED GOOD IAW WC 33-700-17 IAW EMB WC 32-700-19.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,352 hrs · 22,341 cycles

PAX MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R PAX MAIN DOOR EMERGENCY LIGHT IAW AMM 33-50-09. OPS CHECKED GOOD.

Part: PRESSURE SWITCH — CORRODED (BRAKE SYSTEM) · airframe 26,273 hrs · 22,271 cycles

TAKEOFF CONFIG CHECK GETS YOU AURAL WARNING, BRAKES, EVEN THOUGH THE PARKING BRAKES ARE OFF WITH THE BRAKES ON LIGHT EXTINGUISHED. FOUND CONNECTOR CONNECTION TO PRESS SWITCH TO BE CORRODED, BRAKE. R & R PRESS SWITCH IAW AMM 32-44-07. CLEANED PLUG END IAW WM 20-50-00. OPERATIONS CHECK PERFORMED IAW AMM 31-51-00-700-801, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,861 hrs · 21,930 cycles

MAIN CABIN DOOR EMERGENCY LAMP INOPERATIVE. R & R LAMP IN MAIN CABIN DOOR EXTERNAL EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,680 hrs · 21,774 cycles

MAIN DOOR HINGE EMERGENCY LAMP INOPERATIVE. R & R MAIN ENTRY DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A, OPERATIONS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,422 hrs · 21,569 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RT EXTERIOR OVERWING EMERGENCY LAMP IAW AMM TASK 33-50-10-000-801/33-50-10-400-801, OPS GOOD.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 23,856 hrs · 20,303 cycles

DURING MAINTENANCE INSPECTION FOUND FRAME 65 CORRODED AROUND CARGO DOOR FORWARD LOWER STRIKER PLATE NUT PLATE HOLES. THE AIRCRAFT WAS REMOVED FROM SERVICE. BLENDED OUT CORROSION AND INSTALLED REINFORCEMENT DOUBLER IAW AE EO EM-53MR-2123. THE LEVEL OF CORROSION WAS NOT SPECIFIED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 23,921 hrs · 20,355 cycles

DURING B INSPECTION FOUND THE NR 2, 3, 5, 7 EMERGENCY LIGHT STRIPS HAVE BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2, 3, 5, 7 EMERGENCY LIGHT STRIPS IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 23,921 hrs · 20,355 cycles

DURING B INSPECTION FOUND THE NR 4 EMERGENCY LIGHT STRIP HAD A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 23,857 hrs · 20,303 cycles

FRAME 65 SHEAR TIE CORRODED AT FWD LOWER CORNER OF CARGO DOOR CUTOUT. REPAIRED SHEAR TIE IAW AE EO EM-53MR-1129.

Part: LIGHT — BROKEN (CABIN) · airframe 23,921 hrs · 20,355 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT EMERGENCY LIGHT STRIP PROFILE NR 1 AND 2 BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 & 2 RIGHT EMERGENCY FLOOR SIDEWALL ASSEMBLY IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 23,841 hrs · 20,294 cycles

ON FLIGHT 3339 THE CREW REPORTED THE COCKPIT FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RELAMPED EMERGENCY COCKPIT FLASHLIGHT IAW EMB-145 MM 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 23,210 hrs · 19,821 cycles

DURING B INSPECTION FOUND THE CABIN FORWARD OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 DC/ AC INVERTER IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 22,911 hrs · 19,577 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT ELEVATOR UPPER AND LOWER SKINS CREASE/PUNCTURED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED ELEVATOR IAW AEA EO EM-55MR-377. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 22,370 hrs · 19,142 cycles

DURING B INSPECTION FOUND THE FORWARD AISLE CEILING EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD AISLE CEILING EMERGENCY EXIT SIGN IAW EMB 145 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 21,056 hrs · 18,074 cycles

ON FLIGHT 2761 THE FLIGHT ATTENDANT FORWARD FLASHLIGHT HOLDER WAS FOUND TO BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT BRACKET IAW EMB-145 AMM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 20,891 hrs · 17,948 cycles

DURING B-INSPECTION FOUND THE RIGHT SEAT 3B FORWARD EXIT SIGN EMERGENCY INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 INVERTER FOR EXIT SIGN AT SEAT 3B IAW EMB- AMM 33-50-11 IAW EMB AMM 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 20,625 hrs · 17,728 cycles

DURING B-INSPECTION, FOUND THE WALL EXIT LIGHT OUT AT SEAT 3BC. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYSTEM. OPS CHECKED GOOD IAW W/C 33-700-17. AIRCRAFT RETURNED TO SERVICE.

Part: HOLDER — CRACKED (COCKPIT) · airframe 20,586 hrs · 17,703 cycles

ON FLIGHT 3286 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT HOLDER WAS CRACKED, IT DID NOT SECURE THE FLASHLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT BASE BRACKET HOLDER IAW EMB 145 AMM CHAP 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 20,344 hrs · 17,538 cycles

ON FLIGHT 3441 THE CREW REPORTED THE FLASHLIGHT OVER THE CAPTAINS SEAT SWITCH IS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN'S FLASHLIGHT IAW EMB 145 AMM 33-50-16 P/T. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,086 hrs · 16,658 cycles

DURIING MAINTENANCE BASE VISIT FOUND THE EXTERIOR FUSELAGE AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IAW EMB 145 AMM 33-50-07. THE OPERATIONAL GOOD WAS GOOD.

Part: BRAKE — CONTAMINATED (MLG) · airframe 17,677 hrs · 15,645 cycles

ON FLIGHT 3325 UPON LANDING THE TOWER REPORTED SMOKE COMING FROM THE LEFT MAIN WHEEL. AN EMERGENCY WAS DECLARED ON THE GROUND. THE AIRCRAFT ROLLED SAFELY TO A STOP. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED DE-ICING FLUID FROM BOTH BRAKES. PERFORMED LEAK CHECK AND VISUAL INSPECTION PER EMB AMM 32-49-03. NO DEFECTED NOTED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: THERMOSTAT — INOPERATIVE (BLEED AIR SYS) · airframe 17,129 hrs · 15,259 cycles

ON FLIGHT 4080 THE CREW REPORTED THAT DURING THE CLIMB AT APPROXIMATELY FLIGHT LEVEL 160, RECEIVED A BLEED 2 OVER TEMPERATURE MESSAGE IN ICING CONDITIONS. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO RETURN TO ORD. THE AIRCRAFT LANDED AND RETURNED TO THE GATE WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 FAN AIR CONTROL THERMOSTAT IAW EMB AMM 36-11-06. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — INOPERATIVE (COCKPIT) · airframe 16,376 hrs · 14,665 cycles

ON FLIGHT 4149 CREW REPORTED BURNING SMELL IN COCKPIT ON CLIMB. RETURNED TO ORD. NO SMOKE WAS DETECTED. THE AIRCRACFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINS WINDSHIELD TEMPERATURE CONTROLLER IAW EMB 145 AMM 30-42-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRANSDUCER — FAILED (LEFT BRAKE) · airframe 15,560 hrs · 14,064 cycles

FLT 2788 AFTER LANDING, DURING THE TAXI IN THE CREW REPORTED THE LEFT SIDE INBOARD-OUTBOARD BRAKE TEMP CLIMBED INTO THE HIGH AMBER RANGE WITH RIGHT SIDE BRAKES SIDE COOL (BELOW MIDDLE GREEN TEMP ANGLE). WITH THE AIRCRAFT STOPPED ON THE TAXI WAY AN AIRPORT VEHICLE REPORTED VIA RADIO SEEING FIRE / SMOKE AND REDNESS AT LEFT MAIN GEAR WHEEL AREA. WHILE STOPPED THE CREW REPORTED THE LEFT SIDE TEMPERATURE RETURNED TO HIGH GREEN. DURING TAXI IN NO BRAKING AND 1 TEMPERATURE BECAME LOW AMBER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OUTBOARD LEFT BRAKE TRANSDUCER IAW AMM 32-41-01. INSPECTED NR 1 AND NR 2 BRAKE. THE OPERATIONAL CHECK WAS GOOD IAW AMM 32-41-00. FOUND NO DAMAGE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: NUT PLATE — BROKEN (FUSELAGE) · airframe 15,418 hrs · 13,954 cycles

FOR FLIGHT 3588 THE CREW REPORTED THAT THE MAIN CABIN DOOR WAS HARD TO CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED PERMANENT REPAIR IAW EO-EM-5300-1510. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (MLG) · airframe 14,590 hrs · 13,285 cycles

ON FLIGHT 3854 DURING TAKEOFF THE CREW REPORTED THAT THE TAKEOFF AND GEAR RETRACTION DID NOT HAVE IN TRANSIT INDICATION. ALSO DURING EXTENSION NO IN TRANSIT AND NO 1 THRUST SETTING. THE CREW MANUALLY DEPLOYED THE LANDING GEAR. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE LANDING GEAR ELECTRONIC CONTROL UNIT IAW EMB AMM 32-32-01. THE OPERATIONAL CHECK WAS GOOD. PERFORMED OPERATIONAL CHECK OF WEIGHT ON WHEELS INPUT SIGNAL TO FULL AUTHORITY DIGITAL ENGINE CONTROL IAW EMB AMM 76-AMM 76-12-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TORQUE BOX — DAMAGED (RT WING) · airframe 14,323 hrs · 13,042 cycles

DURING INSPECTION 2 ELONGATED HOLES WERE FOUND IN THE RIGHT INBOARD TORQUE BOX. THE AIRCRAFT HAS BEEN REMOVED FROM SERVICE. PERFORMED AN EDDY CURRENT INSPECTION OF THE RIB, TORQUE BOX 57-28-00-250-806 AND 57-28-00-250-807 A1519. INSTALLED TWO FASTENERS ON THE RIGHT INBOARD SIDE PER EO EM 57-MR-445. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STARTER — SEIZED (APU) · airframe 7,585 hrs · 6,969 cycles

ACID SMELL IN CABIN AND FLIGHT DECK FOLLOWED BY INTERMITTENT APU GENERATOR OFF BUSS MESSAGE ON EICAS. COULD NOT DUPLICATE SMELL IN CABIN OR FLIGHT DECK. PERFORMED ELECTRICAL SYSTEM INSPECTION ON WINDSHIELD CONTROLLER TERMINALS WITH NO DEFECTS. FOUND APU STARTER GENERATOR SEIZED. REMOVED AND REPLACED APU STARTER GENERATOR IAW AMERICAN EAGLE WORK CARD 24-800-01. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: ENGINE — FAILED (NR 2)

CREW REPORTED DURING CRUISE FLIGHT E2 SHUT DOWN WITH NO OTHER IND, ATTEMPTED 1 RESTART PER THE AOM WITH NO SUCCESS, DECIDED TO DIVERT TO YYZ. RAI NR 2 ENGINE. OPS CHECKS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FS 20)

THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUT OUT. PREPARED A DOUBLER, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 31, CHAPTER 53-00-10. (M)

Part: SKIN — DAMAGED (FUSELAGE)

ABI - DURING A DROP IN REPAIR, AIRCRAFT ARRIVED FOR REPAIR OF ACCIDENTAL DAMAGE ON THE RT AFT FUSELAGE BETWEEN FRAMES 71 AND 73 AND BETWEEN STRINGERS 15R AND 17R. PERFORMED A CUTOUT OF THE SKIN TO REMOVE THE DAMAGE. FABRICATED A FILLER, DOUBLER, FAIL/SAFE STRAP AND SHEAR CLIP. REPAIR DONE IAW EMB REPAIR SATEMENT IC2005-145/1186 DATED MARCH 5, 2005 AND IC2005-145/1208 DATED MARCH 7, 2005. (M)