N647AE

Part: SHUTOFF VALVE — FAULTED (ZONE 400)

CRUISING LEVEL AT 280 KTS ANTI ICE/STAB A/ICE FAIL DISPLAYED, RESET & FAIL WENT AWAY. THEN WING A/ICE FAIL, RESET & FAIL WENT AWAY. THEN E-1 A/ICE FAIL DID NOT GO AWAY AFTER RESET TILL ON APPROACH. R & R ENGINE PRSOV IRT AMM 36-11-05. LEAK CHECK OK. PERFORMED OPS CHECK OF ANTI ICING SYSTEM IAW AMM 30-00-00. NO DEFCTS NOTED. OPS CHECK OF BLD VLV GOOD IAW AMM 36-00-00

Part: AUTOPILOT SYS — MALFUNCTIONED

DURING CLIMB AT ABOUT 5K AUTO PILOT FAIL WITH CHIME. C/W AUTOPILOT FUNC TEST IAW AMM 22-11-00 OPS CHECK GOOD. A/C OK FOR SRVICE

Part: INVERTER — ABNORMAL (RECIRC FAN) · airframe 54,418 hrs · 51,913 cycles

DURING CLIMB TO 10,000 FEET LOUD WHINING NOISE FROM INSTRUMENT PANEL. P/C C/B F-5 . C/W MNT PROCEDURE. FWD ELEC COMP BAY RECIRC FAN. R&R RECIRC FAN #2 INVERTER IAW AMM 21-26-03. OPS CHECK GOOD IAW AMM 21-26-00. A/C OK FOR SERVICE AT THIS TIME. CLEAR MEL 21-11-3

Part: PROXIMITY SWITCH — FAULTED (ZONE 700) · airframe 53,596 hrs · 50,991 cycles

SPS ADVANCE FAIL MESSAGE IN FLIGHT AT 9000' WENT AWAY AROUND 2000' FACT 09FEB25 14:07 PHL T/S USING FIM 32-61-00-810-806-A. VERIFIED LEGU CONNECTOR ARE FREE OF CORROTION AND INSTALLED PROPERLY. FOUND PROX SWITCH ON R/H MLG DOWNLOCK INOP R&R RH MLG DOWN LOCK #2 PROX SW IAW AMM 32-61-02. OPS CHECK GOOD. OK FOR SERVICE

Part: WARNING UNIT — FAULTED · airframe 53,396 hrs · 50,775 cycles

TAKE OFF CONFIG FLAPS AURAL WARNING CAME ON AFTER FLAP RETRACTION AT 1,000 AGL FACT 05JAN25 08:19 TLH R&R AURAL WARNING UNIT IAW AMM 31-51-01-00 AND 400-801-A. OPS CHECK IAW AMM 31-51-00-700-801-A. OPS CHECK OK. OK FOR SERVICE.

Part: SEAL — OUT OF ADJUST (ZONE 800) · airframe 53,228 hrs · 50,575 cycles

LOUD SQUEAL FROM PAX DOOR FACT 05DEC24 10:08 MDT UPON INSP OF MAIN DOOR SEAL, FOUND SEAL NEEDED ADJ'D. ADJ'D AND RE-SEATED SEAL IN REF TO AMM 52-18-04. OPS CHECK GOOD IN REF TO AMM 21-31-00. A/C OK FOR SERVICE AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSERS) · airframe 52,822 hrs · 50,132 cycles

PRIOR TO TAKE OFF ROLL ON RUNWAY SUSPECT ENG REV DISAGREE MSG ON EICAS. UNSURE OF WHICH ENGINE. NO RELATED CMC MSG. FACT 22SEP24 CLT PERFORMED OPS CHECK IAW EMB 145 AMM 78-30-01. OPS CHECK GOOD. OK FOR SERVICE. NO CMC MSG PRESENT.

Part: UPLOCK — FAULTED (NLG) · airframe 52,635 hrs · 49,910 cycles

IN FLIGHT LOUD THUD UB=NDER FLIGHT DECK HAPPENED FIVE TIMES IN FLIGHT. CMC MSG LG RIGHT UP PROX SW FAIL AND LG UP/DN PROX SW/LGEU FAIL. FACT 17AUG24 02:35 CLT R/R NLG UPLOCK BOX IAW AMM 32-33-07 PERFORMED MULTIPLE GEAR SWINGS. NO ABNORMAL NOISES NOTED. OPS CHECK/LEAK CHECK GOOD. OK FOR SERVICE.

Part: WIRE HARNESS — DAMAGED (NR 2 ENGINE)

#2 ENG HUNG START WITH HEAVY FUEL SMELL (ONLY 0N FADEC 2A). MEL 28MAR24 06:10 RIC B08803 74-1 IGNITION SYSTEM CHANNELS. FOUND DAMAGED/BENT PIN ON PMA A PLUG PIN A. R+R PIN A IAW RR MM 74-11-15. R+R W11 BLUE EXTERNAL HARNESS IAW RR MM 76-11-20. LEAK CK. GOOD. THIS CLEARS MEL 74-1

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,416 hrs · 48,498 cycles

E011061 CORROSION ON LH CENTER AISLE OMEGA BEAM BENEATH THE CROSSBEAM AT FR54. INSTALLED EXTERNAL ANGLE DOUBLER, FILLER AND 2 SHIMS FOR REPAIR OF LH CENTER AISLE OMEGA BEAM AT FR54 CROSSBEAM IAW ETD2023-145-031082 AND PIEDMONT EO1-53-23-0444.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E010216 ACCOMPLISH FCD1-53-23-0180, FUSELAGE WINDOW PILLAR REINFORCMENT. ACCOMPLISHED PIEDMONT AIRLINES FCD1-53-23-0180

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E010800 FRAME 25 CRACKED AT STRINGERS 15R-16R. FABRICATED AND INSTALLED “U” SHAPED DOUBER FOR REPAIR OF FRAME 25 AT STRINGERS 15R-16R IAW EMB145 SRM 53-00-04RE, ITEM 4, FIG 201 AND EO1-53-23-0429

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,416 hrs · 48,498 cycles

E008351 REPAIR DOUBLER CORRODED ON THE LH CENTER AISLE OMEGA BEAM BETWEEN FRAMES 58-59, ACCOMPLISHED REPAIR OF THE CENTER AISLE OMEGA BEAM BETWEEN FRAMES 58-59 IAW EMB ETD2023-145-028762 AND EO1-53-23-0407

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,416 hrs · 48,498 cycles

E008405 CORROSION ON L/H FLOOR BEAM AT FRAME 30. PERFORMED CUTOUT, FABRICATED SHIMS AND DOUBLER AND INSTALLED ON LH OMEGA BEAM AT FR 30 IAW ETD2023-145-028675 AND EO1-53-23-0408

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E008160 FRAME 67 CRACKED AT 3RD FASTENER DOWN FROM LOWER CARGO DOOR SILL. PERFORMED CUTOUT AS REQUIRED TO REMOVE DAMAGED SECTION OF FR 67 INBD OF CARGO DOOR CUTOUT LOWER SILL AND FABRICATED AND INSTALLED REPLACEMENT SECTION AND SPLICE CHANNEL IAW EMB-145 SRM 53-00-04 SECTION 4 AND FIGURE 201 AND EO1-53-23-0410

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 512,416 hrs · 48,498 cycles

E008015 NO REPAIR INFO FOUND FOR EXTERNAL FUSELAGE SKIN REPAIR BUSHING AT FR 77 STR 8R-9R. RE-ACCOMPLISHED BUSHING REPAIR AT FR. 77 STRG. 8R-9R IAW EMB 145 SRM 53-32-01, ITEM 9, FIG. 213 AND PIEDMONT EO1-53-23-0447.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E007941 NO REPAIR INFO FOUND FOR FUSELAGE EXTERNAL SKIN 2 REPAIR BUSHINGS AT FR 77 BETWEEN STR 8L AND 9L. RE-ACCOMPLISHED REPAIRS ON 2 EACH BUSHING HOLES AT FR 77 BTW STR 8L-9L IAW EMB 145 SRM 53-32-01-RE, ITEM 9, FIG. 213 AND PIEDMONT EO1-53-23-0446

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E007129 : NO REPAIR INFO FOUND FOR INT DOUBLER REPAIR FR 74-75 STR 10R-11R. RE-ACCOMPLISHED INTERIOR DOUBLER REPAIR AT FR. 74-75, STRG. 10R-11R IAW ETD2023-145-029756 AND PIEDMONT EO1-53-23-0443.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E007138 NO REPAIR INFO FOUND FOR LH ELEVATOR LE LOWER SKIN DOUBLER REPAIR AT FAILSAFE ROD CUTOUT. RE-ACCOMPLISHED REPAIR OF THE LH ELEVATOR LOWER SKIN AT THE LEADING EDGE FAIL SAFE ROD CUTOUT IAW EMB-145 SRM 55-20-01 AND EO1-55-23-0409

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E007137 NO REPAIR INFO FOUND FOR LH ELEVATOR LE UPPER SKIN DOUBLER REPAIR OUTB OF THE #3 HINGE. RE-ACCOMPLISHED REPAIR OF THE LH ELEVATOR LEADING EDGE UPPER SKIN OTBD OF THE #3 HINGE IAW EMB ETD2023-145-028920 "REV A" AND EO1-55-23-0402

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E007125 : FR 65 SHEAR CLIP REPAIR STGR 17L-18L HAS NO DTI INFORMATION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SHEAR CLIP SECTION FOR REPAIR OF FR65 SHEAR CLIP AT LOWER FWD CORNER OF CARGO DOOR CUTOUT STR17L-18L IAW ETD2023-145-028759 REV “A”. AND EO1-53-23-0426

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E007128 NO REPAIR INFO FOUND FOR TRIPLER DOUBLER REPAIR FR 72-73 STGR 11R-13R

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E007091 NO REPAIR INFO FOUND FOR EXT DOUBLER REPAIR FR 20 STGR 2L-2R. FOUND REPAIR INFO AND RECIEVED ETD2023-145-028736 AND EO1-53-23-0403, ACCEPTING REPAIR AS IS.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,416 hrs · 48,498 cycles

E007000 REAR FUSELAGE 1 WASTE LAV BUCKET HAS CORROSION. FABRICATED, DRILLED, AND INSTALLED DOUBLER FOR REPAIR OF REAR FUSELAGE 1 WASTE LAV BUCKET IAW EMB145 SRM 53-31-02RE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E006520 ANGLE AT STGR 06R JUST FWD OF FR13 IS CRACKED. : REMOVED AND INSTALLED SERVICEABLE ANGLE AT STGR 6R FWD OF FR 13 IAW EMB 145 SRM 51-40-02 AND EO1-53-23-0436

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E006521 FR10 JUST BELOW PILOTS DV WINDOW IS CRACKED. REMOVED AND INSTALLED SERVICEABLE FR10 JUST BELOW PILOTS DV WINDOW AND INSTALLED 4EA SHEAR CLIPS ON FR10 AND 2EA BRACKETS ATTACHED TO FR10 IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E006277 SSI 53-20-11 CORROSION ON CENTER BEAM BETWEEN FRAMES 58-59. REPAIRED THE CENTER BEAM BETWEEN FRAMES 58-59 IAW EMBRAER ETD2023-145-030008 AND EO1-53-23-0435

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E006432 PILOT'S BULKHEAD UPPER OTBD GUIDE PIN HOLE IS GOUGED. INSTALLED SERVICEABLE DOUBLERS FOR REPAIR ON GUIDE PIN HOLE ON PILOT'S BULKFEAD UPPER OUTBD COCKPIT PARTITION IAW EMB 145 SRM 53-21-02 RE, ITEM 4, FIG 204 AND PIEDMONT EO1-53-23-0445

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,416 hrs · 48,498 cycles

E005962 CARGO DOOR LWR THRESHOLD CUT-OUT STRUCTURE CORRODED. : RAR CARGO DOOR LWR THRESHOLD CUT-OUT STRUCTURE IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E005564 BAGGAGE DOOR INTERNAL WEB IS CHAFED IN MULTIPLE AREAS. FABRICATED AND INSTALLED REPLACEMENT DOUBLERS FOR RE-ACCOMPLISMENT OF PREVIOUS REPAIR 1 & 2 IAW EMB-145 SRM 52-30-01 RE ITEM #12, ALSO ALL BLENDED AREAS FOUND TO BE WITHIN LIMITS IAW EMB 145 SRM 52-30-01AD AND EO1-52-23-0428

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E005299 LEFT WING #1 TORQUE BOX FWD AND AFT INBD FASTENER HOLES HAVE VISIBLE DAMAGE, WHICH GIVES CRACK INDICATIONS DURING EDDY CURRENT INSPECTION. REAMED TWO HOLES ON L/H WING #1 TORQUE BOX FWD AND AFT INBD FASTENER HOLES TO .309” AND INSTALLED FASTENERS IAW ETD2023-145-027223 REV A AND EO1-57-23-0369

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E005496 LH ENGINE FWD LWR YOKE FITTING IS CRACKED. REMOVED AND REPLACED LH UPPER/LOWER FWD AND AFT ENGINE YOKE FITTING IAW EMB 145 FCD1-54-21-0015 REV D

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,416 hrs · 48,498 cycles

E004903 THE LH WING SPAR 1 LOWER FLANGE IS CRACKED AT RIB 9. LH WING SPAR 1 LOWER FLANGE IS CRACKED AT RIB 9 FABRICATED SHIMS AND FILLER, INSTALLED LH SPAR 1 REPAIR PARTS IAW ETD# ETD2023-145-027168 AND PIEDMONT EO1-57-23-0448

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,193 hrs · 48,247 cycles

BURNING SMELL IN COCKPIT. FOUND AUTOFLIGHT GUIDANCE CONTROLLER TO BE THE CAUSE. RNRD FLIGHT FUIDANCE CONTROLLER IAW AMM 22-11-01-04. OPS CHECK GOOD

Part: NONE — NONE · airframe 48,645 hrs · 45,409 cycles

PDIS 647 27-41 2748311 12JAN22 CLT CLOSE ON CLIMB OUT PTRIM MAIN FAIL DISPLAYED ON EICAS. A/P DISCONNECTED AND WOULD NOT REENGAGE. BACK UP PITCH TRIM OPERATES NORMAL. 32880 00 AD FACT 12JAN22 23:54 CLT REMOVED AND REPLACED HSCU IAW REFERENCE TO AMM 27-40-01, OPS CHECK GOOD. AUTOPILOT OPS NORMAL, NO EICAS FAIL MESSAGES AT THIS TIME. OK FOR SERVICE

Part: NONE — NONE · airframe 48,551 hrs · 45,292 cycles

PDIS 647 30-31 2748091 22DEC21 PHL CLOSE TAT 2 HEAT INOP ON TAKE OFF. MSG REMAINED UNTIL LANDING. FACT 22DEC21 23:58 PHL REMOVED AND REPLACED (#2) TOTAL AIR TEMPERATURE PROBE IAW EMB AMM 34-15-03. OPS CHECK GOOD. OK FOR SERVICE

Part: NOT REPORTED — NOT REPORTED · airframe 48,359 hrs · 45,063 cycles

PDIS 647 34-15 2723171 11NOV21 ALB CLOSE CAPT PFD ALTITUDE DISPLAY RED X. FACT 11NOV21 06:46 ALB RESET CB C-5 AND C-3 SEVERAL TIMES. OPS CHECK GOOD. OKAY FOR SERVICE AT THIS TIME.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 47,883 hrs · 44,529 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED ROW 12 CEILING LIGHT COVER PANEL AND ROW 12CEILING PANEL. R&R LIGHT ASSY IAW AMM 33-50-15-04 AND INSTALLED THE CEILING PANEL AND CEILING LIGHT COVER PANEL USING RETAINED HARDWARE.

Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 43,456 hrs · 31,265 cycles

AFT EMERGENCY LIGHTS ILLUMINATE WHEN NO POWER APPLIED TO AIRCRAFT. REMOVED & REPLACED #400 EMERGENCY BATTERY CHARGER ASSY IN REF TO AMM 33-50-04-000/400-801-A. PERFORMED EMERGENCY LIGHT SYSTEM OPS CHECK IAW W/C 33-70-17. OPS CHECK GOOD. SEE HA-300 SEQ #6 FOR FURTHER TROUBLESHOOTING ON PACKAGE DATED 5-4-21.

Part: FAN — FAILED (EXHAUST) · airframe 47,350 hrs · 43,939 cycles

DURING CLIMB THROUGH 20,000 FT ELECTRICAL FUMES NOTED IN COCKPIT. SMELL EVENTUALLY DISSIPATED. UPON ARRIVAL TO AC NO SMELL NOTED. EXAMINED RH LH PANELS AND FWD AVI BAY. FOUND #2 EXHAUST FAN INOP. R+R FAN IN REF TO AMM 21 26 02. FOUND NO POWER AT INVERTER. R+R RELAY K0040 AND DAMAGED THERMAL SWITCH S0285 IN REF TO AMM 21 26 04. OPS CHECK GOOD. OK FOR SERVICE

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 46,934 hrs · 43,503 cycles

SSI 53-20-10 SERVICE DOOR CENTEER SILL CORRODED AROUND NUT PLATE HOLES....PERFORMED HFEC INSPECTION AND UT THICKNESS IAW EASI NDTM NO RELEVANT INDICATION NOTED,-.068"-.072" MATERIAL REMAINING....PERFORMED HFEC INSPECTION AND UT THICKNESS IAW EASI NDTM NO RELEVANT INDICATION NOTED,-.068"-.072" MATERIAL REMAINING

Part: SKIN — DAMAGED (FRAMES 19-20) · airframe 46,934 hrs · 43,503 cycles

EXTERNAL FUSELAGE SKIN HAS CREASE BTW FRAMES 19-20, STRINGER 13-14L....REPAIRED EXTERNAL FUSELAGE SKIN HAS CREASE BETWEEN FRAMES 19-20, STRINGER 13-14L IAW PIEDMONT EO1-53-21-0018.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 46,934 hrs · 43,503 cycles

CARGO DOOR INTERNAL LOWER WEB HAS GOUGES, HOLES IN SKIN.....REPAIRED CARGO DOOR INTERNAL LOWER WEB GOUGES, AND HOLES IN SKIN IAW PIEDMONT EO1-52-21-0019.

Part: RIB — CRACKED (LT WING) · airframe 46,934 hrs · 43,503 cycles

LH WING RIB 21 CRACKED. PERFORMED REPAIR ON L/H WING RIB 21 IAW EMB 145 SRM 57-20-07 ITEM 4, FIGURE 203 AND EO1-57-21-0009.

Part: SKIN — CRACKED (FRAMES 59-60) · airframe 46,934 hrs · 43,503 cycles

EXTERIOR FUSELAGE SKIN IS CRACKED BETWEEN FR 59-60 STR 4L-5L. INSTALLED REPAIR DOUBLER AND FILLER FOR SKIN CRACK REPAIR BETWEEN FR59 AND 60 AND STGR 4L-5L IAW EO1-53-21-0008

Part: SKIN — DENTED (CARGO DOOR) · airframe 46,934 hrs · 43,503 cycles

CARGO DOOR EXTERNAL SKIN HAS 22 DENTS.....CARGO DOOR EXTERNAL SKIN DENTS #1-7, AND #9-22 ARE ACCEPTED AS PERMANENT ALLOWABLE DAMAGE IAW EO1-52-21-0007. (CUTOUT AND DOUBLER REPAIR)

Part: YOKE — CRACKED (ENGINE MOUNT) · airframe 46,934 hrs · 43,503 cycles

RH ENGINE LOWER FWD YOKE APPEARS TO BE CRACKED.....PERFORMED HFEC INSPECTION IAW EASI NDTM RELEVANT INDICATION NOTED ET EASI 8958....REMOVED AND REPLACED THE RH ENGINE LOWER FORWARD YOKE IAW PIEDMONT EO1-54-20-0448.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 46,934 hrs · 43,503 cycles

FLOOR PROXIMITY LIGHT STRIP CONNECTOR AT PANEL 251HF IS BROKEN....REPLACED BROKEN FLOOR PROXIMITY LIGHT STRIP CONNECTOR AT PANEL 251HF IAW EMB 145 SWPM 20-21-00.

Part: WIRE — BURNED (PITOT HEAT) · airframe 43,471 hrs · 31,361 cycles

FOUND BURNED/CHAFED WIRE AT NR 3 PITOT/STATIC HEATING CONNECTION ON PITOT/STATIC PORT. AFTER REPAIR, PERFORM FCD1-30-16-0172. REMOVED AND REPLACED CONNECTOR P0089, WIRE W102-1271-16N FROM P0089 TO GS0575 AND WIRE W102-0270-16 FROM P0089 BASE XK0058 PIN C3. DONE IAW SWPM 20-50-00 AND 20-50-01. GS0575 STILL REQUIRES ATTACHMENT TO GROUNDING BASE. OPERATIONS CHECK GOOD AND FCD1-30-16-0172 STILL REQUIRED. COMPLETED FCD1-30-16-0172 REV C NO DEFECTS NOTED. HEATING OPERATIONS CHECK GOOD, IAW AMM 30-31-00-700-801-A. LEAK CHECK GOOD, IAW AMM 34-13-00-790-804-A.

Part: CONTROL UNIT — SMOKE (COCKPIT) · airframe 46,104 hrs · 42,518 cycles

DURING CLIMB OUT CREW NOTICED SMELL, THEN DURING CRUISE SMELL REMAINED WITH SMOKE COMING FROM GLARE SHIELD AREA.....FIX: R&RD FLIGHT GC IAW EMB 145 AMM 22-11-01,OPS CHECK GOOD AT THIS TIME,OK FOR SERVICE. NOTE: CREW DONNED 02 MASKS EMERGENCY DESCENT. CONTINUED FLT TO BOSTON

Part: DRAIN LINE — FAILED (NR 2 PITOT) · airframe 45,940 hrs · 42,345 cycles

CAPT,S AND F/O SPEED INDICATORS OFF BY 15 KNOTS AND FLASHING YELLOW IAS SPEED. REJECTED T/O.....FIX: R&RD PITOT 2 DRAIN LINE AS REQ,D. REF LP 226938-3. PERFORMED LEAK TEST IAW EMB AMM 34-13-00. LEAK CHECK GOOD. OK FOR SERVICE

Part: ENGINE — ODOR (NR 2) · airframe 45,597 hrs · 41,948 cycles

LAVATORY SMOKE EICAS MESSAGE DISPLAYED AFTER TAKE OFF, F/A REPORTED SMOKE IN AFT CABIN. THE NR 2 ENGINE WAS REMOVED AND REPLACED AT A MAINTENANCE VISIT.

Part: UNKNOWN — ODOR (CABIN) · airframe 45,597 hrs · 41,946 cycles

LAVATORY SMOKE MESSAGE ON EICAS AT 400 FT. SMELLED SMOKE IN CABIN AND LAVATORYSHE ALARM WENT OFF. R & R THE LAVATORY SMOKE DETECTOR AND TESTED PER AMM 16-14-02. OPS CHECK GOOD. OK FOR RETURN TO SERVICE IAW FIM 26-14-00-810-802-A. TROUBLESHOOTING SMELLED SURFACE IN CABIN, RAN BOTH ENGINE AND APU IN MANY PACK / BLEED CONFIGURATION EVALUATION FLIGHT SATISFACTORY

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 45,596 hrs · 41,945 cycles

LAVATORY SMOKE ALARM WENT OFF AFTER TAKEOFF. STRANGE CAME FROM GALLEY. R & R THE LAVATORY SMOKE SENSOR IAW AMM 26-14-01 AND OPS CHECK IAW AMM 26-14-00, OPS CHECK OK FOR SERVICE. RAN BOTH ENGINES WITH AND WITHOUT BLEED 1 AND 2, PACKS 1 AND 2 AT HIGH POWER FOR 2 MINUTES NO EICAS MESSAGE OBSERVED.

Part: BLADE — DAMAGED (NR 2 ENGINE FAN) · airframe 45,254 hrs · 41,546 cycles

NR 2 ENGINE FAN BYPASS VANES DAMAGED. REPLACED ALL 15 FAN BLADES IAW ENG MANUAL 72-25-10-400-801.

Part: FAIRING — DAMAGED (WING TIP) · airframe 45,254 hrs · 41,546 cycles

RIGHT WING TIP FAIRING DAMAGED. R & R WING TIP FAIRING IAW AMM 57-30-00-400-801-A.

Part: FLOW SENSOR — DEFECTIVE (NR 1 ENGINE) · airframe 44,838 hrs · 41,066 cycles

647 73-30 2007141 19MAY19 CHS CLOSE NR 1 ENG FUEL FLOW WENT TO ZERO ON EICAS AND RMU DURING T/O ROLL. HISTORY: NONE MEL 19MAY19 10:55 CHS C13909 73-6 FUEL FLOW INDICATORS FACT 21MAY19 04:59 PHL R&R RUEL FLOW SENSOR IAW MM 73-35-10. OPS CHECK GOOD OK FOR SERVICE AT THIS TIME. CLEAR MEL 73-6.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,666 hrs · 40,870 cycles

NDIS 647 33-20 0007870 20APR19 RIC CLOSE EXIT ROW EMERGENCY LIGHT ON RH SIDE WON'T ILLUMINATE FACT 20APR19 09:51 RIC REMOVED & REPLACED RH OVERWING EMERGENCY LIGHT IN RE F TO AMM 33-50-13-000/400-801-A OK FOR SERVICE P/N ON OVERWING EXIT SIGN 1013836 P/N OFF OVERWING EXIT SIGN 1013836

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,424 hrs · 40,581 cycles

NDIS 647 33-51 0006820 06MAR19 ROA CLOSE LT, FWD EMERGENCY LIGHT IS INOP FACT 06MAR19 10:47 ROA R&R THE LAMP/BULB ON THE LT, FWD EMERG LIGHT OPS CHECK GOOD OKAY FOR SERVICE AT THIS TIME PART INSTALLED/REMOVED LAMP/BULB - 8330012 SN N/A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,367 hrs · 40,515 cycles

NDIS 647 33-40 0006660 01MAR19 SBY CLOSE RT OVERWING EMERGENCY LIGHT INOP. 35718 00 SPE FACT 01MAR19 11:48 SBY R & R EMERGENCY LIGHT IAW TASKS 33-50-14-000-801-A AND 33-50-14-400-801-A.

Part: INVERTER — MALFUNCTIONED (ELECTRICAL SYS) · airframe 43,758 hrs · 39,784 cycles

115 VOLT AC BUS OFF ON T/O ROLL, REJECTED T/O. R&R STATIC INVERTER IAW AMM 24-20-01-04. OPS CHECKS GOOD AT THIS TIME.

Part: ACCESS DOOR — LACK OF LUBE · airframe 43,268 hrs · 39,211 cycles

ACCESS DOOR OPEN EICAS MSG. DOOR SCREEN SHOWS FWD ACCESS HATCH. HATCH IS CLOSED (C/W MX PROCEDURE). LUBRICATED FWD NOSE ACCESS DOOR AND ACCOMPLISHED OPS CK IAW AMM 52-71-00-710-002A.

Part: TRUNNION — CRACKED (LT WING) · airframe 43,127 hrs · 39,056 cycles

LEFT WING MLG AFT UPPER TRUNION WAS CRACKED AT THE OUTBOARD LOWER RADIUS. COMPLIED WITH ERS-EM-57MR-965.

Part: RIB — CRACKED (WINDOW AREA) · airframe 43,127 hrs · 39,056 cycles

RIB ABOVE CAPTAINS WINDSHIELD HAS A 1/4 INCH CRACK AROUND THE NUTPLATE HOLE. REPAIRED THE RIB IAW SRM-53-12-16.

Part: SUPPORT ANGLE — CRACKED (FRAME 48) · airframe 43,127 hrs · 39,056 cycles

LEFT WING TO FUSELAGE UPPER SUPPORT ANGLE WAS FOUND CRACKED, 1 1/2 INCH LONG AT FRAME 48. REPAIRED IAW SRM 53-23-12.

Part: SUPPORT ANGLE — CRACKED (FRAME 49) · airframe 43,127 hrs · 39,056 cycles

RIGHT WING TO FUSELAGE UPPER SUPPORT ANGLE IS CRACKED 2 1/2 ICHES LONG AT FRAME 49. REPAIRED IAW SRM 53-23-12.

Part: SUPPORT ANGLE — CRACKED (FRAME 42) · airframe 43,127 hrs · 39,056 cycles

RIGHT WING TO FUSELAGE UPPER SUPPORT ANGLE FOUND CRACKED, 1 INCH LONG AT FRAME 42. REAPIRED IAW SRM 53-23-12.

Part: SUPPORT BRACKET — CRACKED (LT WING ROOT) · airframe 43,127 hrs · 39,056 cycles

LEFT OVERWING ROOT FAIRING L BRACKET SUPPORT ON UPPER WING SURFACE IS CRACKED. REPAIRED IAW ETN-EM-53-142.

Part: SUPPORT BRACKET — CRACKED (LT WING ROOT) · airframe 43,127 hrs · 39,056 cycles

LEFT OVERWING ROOT FAIRING SUPPORT BRACKET ON THE UPPER SURFACE WAS FOUND CRACKED, JUST INBD OF THE GROUND SPOILER. REPAIRED THE SUPPORT BRACKET IAW ETN-EM-53-142

Part: BULKHEAD — CRACKED · airframe 43,127 hrs · 39,056 cycles

LT MLG WHEEL WELL AT THE AFT BULKHEAD WALL HAS TWO CRACKS. INSTALLED THE BULKHEAD IAW SRM 51-40-02.

Part: LIGHT — DETACHED (CABIN FLOOR) · airframe 43,127 hrs · 39,056 cycles

CABIN FLOOR EMERGENCY LIGHT DEBONDED FROM STRIP. INSTALLED THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 43,127 hrs · 39,056 cycles

ILLUMINATED EXIT SIGN HAD A DAMAGED WIRE. REPLACED THE EXIT SIGN.

Part: LIGHT — DAMAGED (CABIN FLOOR) · airframe 43,127 hrs · 39,056 cycles

CABIN FLOOR EMERGENCY LIGHT STRIP NR 1 WAS DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 43,127 hrs · 39,056 cycles

CABIN FLOOR EMERGENCY LIGHT STRIP NR 6 WAS DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 43,127 hrs · 39,056 cycles

NR 8 FLOOR EMERGENCY LIGHT STRIP WIRING WAS DAMAGED AT THE BASE OF THE STRIP. REMOVED AND REPLACED THE LIGHT STRIP IAW AMM 33-50-12.

Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 42,964 hrs · 38,904 cycles

FOUND EMERGENCY LIGHT TO BE INOPERATIVE IN GALLEY. REMOVED AND REPLACED THE BATTERY AND CHARGER IAW IAW AMM 33-50-04. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,916 hrs · 38,847 cycles

RIGHT EXTERIOR WING EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE OVERWING EMERGENCY LIGHT BULB IAW AMM 33-50-07, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,730 hrs · 38,654 cycles

NR 4 AISLE EMERGENCY LIGHT INOP PER PS-2 CHECK. REMOVED AND REPLACED LAMP ON NR 4 AISLE EMERGENCY LIGHT IAW AMM 33-50-08. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,561 hrs · 38,487 cycles

ROW 17 EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-08-000-801-A, AND 33-50-08-400-801-A. OPS CHECKED GOOD.

Part: CABLE — MALFUNCTIONED (PAX DOOR) · airframe 42,194 hrs · 38,121 cycles

MAIN DOOR WILL NOT OPEN FROM OUTSIDE. REMOVED AND REPLACED INTERNAL HANDLE CABLE IAW AMM 52-18-09, OPS CHECKED GOOD.

Part: WIRE SPLICE — DAMAGED (EMERGENCY LIGHTS) · airframe 42,137 hrs · 38,075 cycles

NR 7 FLOOR EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT IAW WM 33-50-50. FOUND THE SPLICES SP9113 AND SP9114 BAD. R & R THE WIRE SPLICES IAW SWPM 20-50-01, NO FURTHER DEFECTS NOTED.

Part: FLASHLIGHT ASSY — BROKEN (AFT CABIN) · airframe 41,986 hrs · 37,948 cycles

AFT FA FLASHLIGHT BROKEN AND NOT WORKING. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: CAM — OUT OF ADJUST (PAX DOOR) · airframe 41,771 hrs · 37,730 cycles

MAIN ENTRY DOOR HARD TO OPEN AND CLOSE. ADJUSTED THE FWD CAM OF THE SIDE HINGED ON MAIN DOOR IAW AMM 52-18-00, AND ETN EM-52-029. INTERNAL ACTUATING HANDLE TESTED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,734 hrs · 37,678 cycles

DURING PS-1, FOUND THE LAST ASILE EMERGENCY LIGHT INOPERATIVE. REPLACED THE BULB IAW AMM 33-50-08, OPS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 41,649 hrs · 37,583 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. LUBRICATED THE DOOR ROLLERS. PERFORMED A TEST OF MAIN DOOR IAW AMM 52-10-01. OPS CHECKED GOOD.

Part: SEAL — DETACHED (PAX DOOR) · airframe 41,241 hrs · 37,197 cycles

MAIN DOOR GETS STUCK WHEN OPENING AND IS DIFFICULT TO OPEN. INSPECTED AND FOUND RUBBER TRIM SEAL AT TOP REAR CORNER DETACHED. REPAIRED IAW AMM 52-00-04. OPS CHECKED NORMAL. ACFT OK FOR SERVICE

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 41,213 hrs · 37,172 cycles

MAIN CABIN DOOR HARD TO OPEN. ADJUSTED BOTH UPPER PAX DOOR ROLLERS IAW AMM 52-10-01. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,213 hrs · 37,172 cycles

MAIN CABIN DOOR EMERGENCY LIGHT COVER BROKEN AND LIGHT INOPERATIVE. MAIN CABIN DOOR EMERGENCY LIGHT COVER AND LIGHT BULB REPLACED IAW AMM 20-21-00

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 41,212 hrs · 37,171 cycles

MAIN CABIN DOOR HARD TO OPEN. JAMBS WHEN TRYING TO OPEN. PERFORMED AN ADJUSTMENT OF MAIN DOOR IAW AMM 52-10-01. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: HINGE — LACK OF LUBE (PAX DOOR) · airframe 41,168 hrs · 37,124 cycles

FA REPORTED MAIN CABIN DOOR DIFFICULT TO OPEN. LUBRICATED MAIN CABIN DOOR HINGE POINTS IAW AMM 52-11-00. OPS CHECKED OK

Part: HANDLE — LOOSE (PAX DOOR) · airframe 40,930 hrs · 36,958 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN. DURING DETAILED VISUAL INSPECTION, FOUND THE BOLTS FOR THE INTERNAL HANDLE BOX LOOSE. TIGHENED BOLTS AND PERFORMED SIDE HINGED MAIN DOOR ADJUSTMENT TEST. OPS CHECKED GOOD. OK FOR SERVICE. ALL WORK DONE IAW AMM 52-18-00.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 40,856 hrs · 36,897 cycles

FA COULD NOT GET MAIN CABIN DOOR OPEN ON A NUMBER OF ATTEMPTS, FA BELIEVES ITS ONE OF THE BOTTOM LATCHES. LUBED MAIN DOOR ROLLERS AND PERFORMED OPS CHECK IAW AMM 53-21-01. OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: DOOR — LACK OF LUBE (MAIN CABIN) · airframe 40,551 hrs · 36,614 cycles

MAIN CABIN DOOR IS HARD TO OPEN. LUBRICATED AND PERFORMED OPERATIONAL CHECK MAIN CABIN DOOR AND FOUND OK IAW AMM 52-10-01

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,149 hrs · 36,279 cycles

RT EXTERIOR OVER THE WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-10 SUBTASK 020-004-A.OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (INSPECTION LIGHT) · airframe 39,993 hrs · 36,140 cycles

RIGHT WING INSPECTION LIGHT INOPERATIVE. REPLACED THE BULB IAW AMM 33-50-10-04, OPS CHECKED GOOD.

Part: STOP FITTING — LOOSE (PAX DOOR) · airframe 39,307 hrs · 35,535 cycles

MAIN CABIN DOOR VERY DIFFICULT TO OPEN. TIGHTENED MANY LOOSE STOPS ON MAIN PAX DOOR IAW MM 52-10-01 AND LUBED FRAME ROLLERS IAW MM 53-21-02

Part: LIGHT — WEAK (CABIN) · airframe 39,309 hrs · 35,540 cycles

FWD RT EMERGENCY LIGHT DIM. REMOVED AND REPLACED FWD RT EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED NORMAL.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 39,267 hrs · 35,495 cycles

DURING PS-1 INSPECTION, FOUND LAST THREE EMERGENCY FLOOR LIGHT STRIPS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND BATTERY CHARGER ASSEMBLY IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: BLEED VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 39,267 hrs · 35,495 cycles

BLEED 1 VALVE CLOSED ADVISORY ON CLIMB OUT.PERFORMED AOM1 PROCEDURE. REMOVED AND REPLACED BLEED 1 PBA IAW AMM 20-13-04. BLEED OPERATIONAL CHECKED GOOD IAW AMM 36-11-05.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 39,258 hrs · 35,484 cycles

FA STATED THAT THE MAIN CABIN DOOR WAS STICKING. DIFFULCT TO OPEN. LUBRICATED ROLLERS IAW TASK 53-21-02-400. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 38,990 hrs · 35,229 cycles

MAIN CABIN DOOR HANGS UP WHILE OPENING. VERY DIFFICULT TO OPEN. READJUSTED MAIN PAX DOOR IAW AMM 52-18-00. OPS CHECK GOOD.

Part: ROLLER — DEFECTIVE (DOOR FRAME) · airframe 38,886 hrs · 35,127 cycles

FLIGHT ATTENDANT REPORT MAIN DOOR IS EXTREMELY DIFFICULT TO OPEN. PERFORMED MAIN DOOR FRAME ROLLER SERVICING IAW MM 53-21-02. OPERATIONS CHECKED GOOD.

Part: CONTROLLER — FAILED (WINDOW HEAT) · airframe 38,874 hrs · 35,113 cycles

STRANGE ODOR ALMOST LIKE A BURNING PLASTIC ODOR CAME & THEN WENT AWAY. TROUBLE SHOT SMELL IAW FIM 21-20-00-810-801-A FOUND NR 1 WINDSHIELD TEMP CONTROLLER TO BE BAD. REF ITEM 1 OF THIS LOG PAGE FOR R & R. R & R WINDSHIELD TEMPERATURE CONTROLLER FOR THE NR 1 WINDSHIELD HEAT UNIT IAW AMM 30-42-01. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — MISSING (CABIN) · airframe 38,854 hrs · 35,092 cycles

NUMBER 3 EMER LIGHT STRIP CONNECTOR ON ACFT SIDE MISSING. FOUND DURING CLOSE UP. INSTALLED SERVICEABLE SPLICE SP9036 ON NR 3 EMER LIGHT STRIP CONNECTOR ON ACFT SIDE IAW SWPM 20-21-00.

Part: CHANNEL — DAMAGED (FUSELAGE) · airframe 38,854 hrs · 35,092 cycles

INBOARD RIVET HOLE DAMAGED AT FRAME 54 ON RT ELEVATOR CABLE FAIRLEAD. ACCOMPLISHED REPAIR TO THE INBD RIVET HOLE IAW ERS-EM-53MR-2093.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,854 hrs · 35,092 cycles

LEFT UPPER FUSELAGE SKIN CRACKED 2 PLACES. CRACK 1 IS JUST FWD OF FRAME 75 & JUST ABOVE STRINGER 2L, CRACK IS APPROX 1.25" LONG. CRACK 2 IS AT THE FIRST FASTENER BELOW STRINGER 2L ON FRAME 75, CRACK IS 1/4" LONG. PERFORMED REPAIR AT LT UPPER FUSELAGE SKIN CRACK FWD OF FRAME 75 ABOVE STRINGER 2L & ON FRAME 75 BELOW STRINGER 2L IAW ERS-EM-53MR-2099.

Part: CROSSMEMBER — CORRODED (FUSELAGE) · airframe 38,854 hrs · 35,092 cycles

THE FLOOR CROSS MEMBER AT FRAME 20 IS CORRODED. REMOVED DAMAGED CROSS MEMBER AT FRAME 20 & DRILLED, COUNTERSANK, FAY SEALED & INSTALLED SERVICEABLE CROSS MEMBER IAW SRM 51-40-02, 51-20-03, 51-20-01, 51-40-06, ETNS EM-53-139-R4 & EM-53-150-R2. SEE WIPS & TASKS FOR FURTHER INFORMATION.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 38,854 hrs · 35,092 cycles

SERVICE DOOR CUT OUT FRAME 22 CORRODED AROUND LOWER NUTPLATE HOLE. INSTALLED INTERNAL & EXTERNAL REPAIR DOUBLERS & FILLER IAW SRM 53-00-04 ITEM 16 FIG 208.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,844 hrs · 35,081 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED, CRACK IS AT THE FIRST FASTENER BELOW STRINGER 2R ON FRAME 75, CRACK IS 1/4" LONG. PERFORMED REPAIR AT RT UPPER FUSELAGE SKIN CRACK AT FIRST FASTENER, BELOW STRINGER 2R ON FRAME 75, ERS-EM-53MR-2099. SEE TASKS & WIPS FOR DETAILS.

Part: DRAIN LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 38,795 hrs · 35,029 cycles

FIRST OFFICER AIRSPEED INDICATOR UNRELIABLE, FL 370 CAPTAINS SIDE SHOWS 240, FIRST OFFICERS & STAND BY AGREE DURING DECENT. ALL AIRSPEED INDICATIONS NORMALIZED & WERE READING IN SYNC & NORMAL. FOUND WATER & MOISTURE IN PITOT DRAIN LINE IAW AMM 34-13-00. ADC OPERATIONS TESTED IAW AMM 34-15-00. SYS CHECKED GOOD, NO MSGS NOTED. ACFT OK FOR SERVICE.

Part: UNKNOWN — ODOR · airframe 38,155 hrs · 34,463 cycles

WHILE STARTING AT THE GATE, APU FIRE WARNING ON EICAS MSG WITH A BURNING SMELL. DEFERRED APU M PROCEDURES COMPLIED WITH IAW 49-1. PERFORMED INSPECTION OF APU FIRE WARNING IAW TASK 05-50-11-200-801-A. PERFORMED SEVERAL START CYCLES OF APU IAW 49-10-00-910-802-A & LET RUN FOR SEVERAL MINUTES EACH TIME. NO FAULTS OR DEFECTS NOTED AT THIS TIME, MEL RESTORED. END ITEM LOG PAGE 2897500 APU FIRE WARNING ON EICAS APU BOTTLE DISCHARGED. PERFORMED GVI INSIDE APU COWLING IAW AMM 49-11-01, NO DEFECTS NOTED. DEFERRED APU FIRE EXTINGUISHING SYS IAW 26-6. R & R APU FIRE EXT BOTTLE IAW AMM TASK 26-22-01-000-801-A & 26-22-01-400-801-A. MEL RESTORED.

Part: BRAKE ASSY — FAILED (NR 2) · airframe 38,155 hrs · 34,464 cycles

NUMBER 2 BRAKE FAILED CARBON INSPECTION. R & R NR 2 BRAKE IAW WC 32-600-14.

Part: SENSOR — FAULTY (TE FLAP) · airframe 37,957 hrs · 34,258 cycles

FLAP FAIL ON APPROACH, FLAPS AT ZERO DEGREES. TRANSFERRED TO NRWC 647-ORD-02283. R & R FLAP VELOCITY SENSOR IAW AMM 27-51-12. REFER TO NRWC 647-ORD-02283. R & R FLAP TRANSMISSION BRAKE IAW AMM 27-51-01. ACCOMPLISHED OPERATIONS CHECK IAW AMM 27-51-00. OPERATIONS CHECKED GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 37,933 hrs · 34,233 cycles

FLAP FAIL ON APPROACH, FAILED AT 0. RESET FLAP SYS & PERFORMED OPERATIONS TEST IAW AMM 27-51-00, WITH NO DEFECTS.

Part: ACTUATOR — FAILED (TE FLAP) · airframe 37,934 hrs · 34,234 cycles

FLAPS FAIL ON APPROACH, FAILED AT 0. RESET FLAP SYS & OPERATIONS CHECK IAW AMM 27-51-00. OPERATIONS CHECKED GOOD, NO MSGS NOTED. WHILE TROUBLESHOOTING FLAP RT TRANSMISSION FAIL CMC MSG. FOUND RT NR 3 FLAP ACTUATOR, RT OTBD FLAP LT SIDE, LEAKING & RESERVOIR EMPTY. R & R RT NR 3 FLAP ACTUATOR IAW AMM 27-51-10. OPERATIONS CHECKED GOOD & SERVICED LT FSA 1, 2, 3 & NR 4 & RT FSA 1, 2 & 4 IA AMM 27-51-00-600-803A. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 37,928 hrs · 34,231 cycles

EMERGENCY LIGHTS LISTED ARE INOPERATIVE. EXTERNAL LT FWD WING FUSELAGE, MAIN DOOR ARM LIGHT & MAIN DOOR EXIT SIGN. R & R NR 1 EMER LIGHT BATTERY & BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. EMER LIGHTING BATTERY PN 2013-1ASMI & SN 67025

Part: CONTROLLER — FAILED (TE FLAPS) · airframe 37,911 hrs · 34,213 cycles

FLAP FAIL ON EICAS MSG DURING APPROACH. TROUBLESHOOTING IAW FIM TASK 27-51-00-810-817. CMC INDICATED RT TRANSMISSION FAIL. RESET FLAP SYS & PERFORMED OPERATIONAL CHECK. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED OR MSGS NOTED. ON PUSHBACK AFTER NR 1 ENG START RECEIVED, FLAP FAIL, MSG REPEAT ON LAST FLIGHT. R & R FECU IAW AMM 27-53-02. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,887 hrs · 34,191 cycles

LEFT FWD EXTERIOR EMER LIGHT INOPERATIVE. R & R THE FWD EXTERIOR EMER LIGHT ASSEMBLY IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,840 hrs · 34,139 cycles

LEFT FWD EXTERIOR EMER LIGHT INOPERATIVE. TRANSFERRED TO AML PAGE 3909957 ITEM 1. DEFERRED IAW MEL 33-29. R & R EXTERNAL LT FWD LIGHT ASSEMBLY IAW MM 33-50-10. OPERATIONS TESTED GOOD IAW MM 38-50-00. MEL RESTORED & PLACARD REMOVED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 37,838 hrs · 34,137 cycles

DURING CLIMB, IN ICING CONDITIONS, EICAS DISPLAYED WING ANTI-ICE FAIL & WING PB OPEN INSCRIPTION DID NOT ILLUMINATE. IAW AOM 1 PROCEDURE SELECTED OVERRIDE TO ALL VLV SEEMED TO OPEN BUT BROKE OUT ON TOP & EXITED ICING CONDITIONS. KNOWING WE WOULD HAVE TO DESCENT THROUGH ICING CONDITIONS WE RAN ICE PROTECTION PNEUMATIC TEST IAW AOM 1 TO ASSURE SYS WAS FUNCTIONING DURING TEST, ALSO GOT WING ANTI-ICE FAIL M. PERFORMED OPERATIONAL TEST OF ANTI-ICE SYS IAW AMM 30-00-00. NO DEFECTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 37,838 hrs · 34,137 cycles

DURING CONFIGURATION FOR LANDING FLAP FAIL MSG DISPLAYED UPON SELECTION OF FLAPS 9. FLAPS FAILED AT 0. RAN AOM 1 PROCEDURE LANDED FLAPS UP, TOUCHDOWN NORMAL. VREF 158 KTS USED MAX REVERSE. TROUBLE SHOT IAW FIM 27-51-00-810-817. CHECKED SCREWS, NO DEFECTS NOTED TRANSITORY CONDITION OF THE FLAP RESET SWITCH.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,678 hrs · 34,010 cycles

AFT CABIN EMER LIGHTING INOPERATIVE. R & R NR 4 EMER LIGHT BATTERY PACK IAW AMM 33-50-04. TESTED SATISFACTORY.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 37,213 hrs · 33,577 cycles

ON CLIMB OUT CABIN PRESSURIZATION WOULD NOT STABILIZE IN AUTO MODE. DEFERRED PRESSURIZATION CONTROL AUTO MODE SYS IAW MEL 21-16. AFTER PUSHBACK ACFT UNCONTROLLABLE CABIN ALT READ OUT WENT TO DASHES, DIFFICULTY IN MANUAL MODE. REPLACED DIGITAL CONTROLLER IAW AMM 21-31-01. OPERATIONS CHECKED GOOD, MANUAL PRESS OPERATIONS CHECKED GOOD IAW AMM 21-31-00.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 37,193 hrs · 33,556 cycles

FLIGHT ATTENDANT FLASHLIGHT CRADLE BROKEN. R & R IAW AMM 33-50-16. OPERATIONS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,083 hrs · 33,444 cycles

AFT EMER FLOOR LIGHTING INOPERATIVE WHEN TESTED. R & R NR 4 BATTERY PACK IAW AMM 35-50-04. OPERATIONS CHECKED SATISFACTORY IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,044 hrs · 33,417 cycles

FLOOR PROXIMITY LIGHT INOPERATIVE ROW 5A & 6A. R & R FLOOR PROXIMITY LIGHT ROW 5A & 6A IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 36,835 hrs · 33,232 cycles

WHILE ENROUTE AT FL360, LOST PRESSURIZATION. CABIN ALTITUDE JUMPED TO 12500. SWITCHED TO MANUAL PRESSURIZATION & CABIN ALTITUDE STABILIZED. ABLE TO USE MANUAL MODE & DIVERTED. R & R DIGITAL CONTROLLER IAW AMM 21-31-01. OPS CHECKED GOOD IAW 21-16.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 36,428 hrs · 32,875 cycles

REFERENCE TO MEL 25-53 AFT FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. R & R AFT FLIGHT ATTENDANT FLASHLIGHT HOLDER ASSEMBLY & CHECKED OK IAW 25-60-00. RESTORE MEL 25-53.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 36,358 hrs · 32,817 cycles

LEFT EXIT MARKING SIGN INOPERATIVE. REMOVED AND INSTALLED NEW INVERTER AT POSITION NR 4. OPERATIONS CHECKED GOOD IAW AMM 33-50-11.

Part: HINGE — OUT OF ADJUST (CABIN DOOR) · airframe 35,202 hrs · 31,795 cycles

FLIGHT ATTENDANT REPORTS CABIN DOOR HARD TO OPEN. IT MUST BE LIFTED TO GET IT TO SWING OPEN. COMPLIED WITH ETN EM-52-013R1 MAIN SIDE DOOR HINGE ADJUSTMENT.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 35,188 hrs · 31,776 cycles

MAIN DOOR HARD TO OPEN CATCHES ON ON FRAME. INSPECTED & LUBED MAIN CABIN DOOR IAW AMM 52-10-01. OPERATIONS CHECKED GOOD OK FOR SERVICE.

Part: ROLLER — LACK OF LUBE (DOOR FRAME) · airframe 35,181 hrs · 31,767 cycles

FLIGHT ATTENDANT REPORTS MAIN DOOR HARD TO OPEN, UNLOCK. SERVICED FRAME ROLLERS IAW AMM 53-21-02. COMPLIED WITH HANDLE TEST IAW AMM 52-18-00-820-801-A. FOUND GOOD AT THIS TIME.

Part: ROLLER — OUT OF ADJUST (CABIN DOOR) · airframe 35,176 hrs · 31,760 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN. ADJUSTED THE MAIN DOOR ROLLERS IAW AMM 52-10-01-820-806-A. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED.

Part: ROLLER — LACK OF LUBE (FUSELAGE) · airframe 35,050 hrs · 31,645 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR HARD TO OPEN. LUBE MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02. OPERATIONS CHECKED GOOD.

Part: COUPLER — FAILED (BLEED AIR SYS) · airframe 34,852 hrs · 31,493 cycles

ON TAKEOFF PASSING THROUGH 8000 FT GOT BLEED 2 LEAK. COMPLIED WITH EPC EMER PROCEDURES. BLEED 2 LEAK SECURED & RETURNED. PERFORMED LEAK CHECK OF NR 2 BLEED SYS IAW AMM 36-11-09. REPLACED GND CONNECTION COUPLING IAW AMM 36-10-02. OPERATIONS CHECKED GOOD IAW AMM 36-00-00.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 34,784 hrs · 31,433 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR HAS TO BE LIFTED IN ORDER TO OPEN, NOT OPENING NORMALLY. PERFORMED LUBE TO MAIN DOOR FRAME ROLLERS IAW AMM 53-21-03. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 34,634 hrs · 31,310 cycles

ICING CONDITIONS, OR POSSIBLE ICING CONDITIONS WERE ENCOUNTERED & ANTI-ICING DID NOT ACTIVATE. MANUALLY ACTIVATED ANTI-ICE & A STRONG UNUSUAL ODOR WAS OBSERVED. ODOR QUICKLY DISSIPATED WHEN ANTI-ICING WAS TURNED OFF. IT MAY HAVE SIMPLY BEEN ICE CRYSTALS ON THE WINDSHIELD INSTEAD OF ICE, SO IT MAY BE APPROPRIATED THAT THE ICE DETECTOR DID NOT ACTIVATE THE SYS. PERFORMED OPERATIONAL CHECKS OF ANTI-ICING SYS IAW AMM 30-00-00 & AMM 30-21-00. FOUND NO DEFECTS NOTED ON ANTI-ICING SYS & DIDN’T SMELL ANY UNUSUAL ODOR WHEN SYS RUNNING.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 34,625 hrs · 31,301 cycles

MAIN CABIN DOOR IS GETTING STUCK & HARD TO OPEN. LUBED MAIN CABIN DOOR. OPERATIONS CHECKED GOOD IAW STANDARD PRACTICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 34,454 hrs · 31,153 cycles

DURING HMBV INSPECTION FOUND CARGO DOOR SILL IS CORRODED IN SEVERAL SPOTS. R & R CARGO DOOR SILL IAW SRM CHAPTER 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 34,454 hrs · 31,153 cycles

DURING HMBV INSPECTION FOUND THE SERVICE DOOR SILL HAS AREAS OF CORROSION BETWEEN FRAMES 20 - 22. R & R SERVICE DOOR SILL IAW SRM 51-40-02.

Part: FIREWALL — CRACKED (APU BAY) · airframe 34,454 hrs · 31,153 cycles

DURING HMBV INSPECTION FOUND APU FIREWALL LOWER RT SIDE JUST ABOVE THE MOUNTING BRACKET HAS A 1 INCH CRACK BY A RIVET. COMPLIED WITH REPAIR OF THE APU FIREWALL LOWER RT SIDE IAW EO-EM-53AD-1883 PART C STEP 5.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 34,454 hrs · 31,153 cycles

DURING HMBV INSPECTION FOUND THE RT MLG BAY AFT FAIRING SUPPORT PLATE IS CRACKED. R & R BRACKET IAW AMM CHAPTER 20-10-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,454 hrs · 31,153 cycles

DURING HMBV INSPECTION FOUND SHEAR CLIP CRACKED AT FRAME 24 AT STRINGER 15RT. R & R SHEAR CLIP AT FRAME 24 AT STRINGER 15RT IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 34,454 hrs · 31,153 cycles

DURING HMBV INSPECTION FOUND LT COCKPIT FRAME 10 FWD SUPPORT BRACKET IS CRACKED BENEATH THE DV WINDOW. R & R LT COCKPIT FRAME 10 FWD SUPPORT BRACKET IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,454 hrs · 31,153 cycles

DURING HMBV INSPECTION FOUND SHEAR CLIP CRACKED AT FRAME 24 BETWEEN STRINGER 15RT & 16RT. R & R SHEAR CLIP AT FRAME 24 AT STRINGER 15RT & 16RT IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 34,454 hrs · 31,153 cycles

DURING HMBV INSPECTION FOUND FRAME 68 CARGO DOOR HOLD OPEN STRUT RETAINER CUP. AFT SIDE SUPPORT BRACKET IS CRACKED. R & R FRAME 68 CARGO DOOR HOLD OPEN STRUT RETAINER CUP, AFT SIDE SUPPORT BRACKET IAW SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,454 hrs · 31,153 cycles

DURING HMBV INSPECTION FOUND RT COCKPIT FRAME 10 IS CRACKED ON THE TOP END AT THE RIVET HOLES. REMOVED & INSTALLED NEW FRAME IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 34,454 hrs · 31,153 cycles

DURING HMBV INSPECTION FOUND RT COCKPIT FRAME 10 FWD SUPPORT BRACKET CRACKED BENEATH THE DV WINDOW. R & R RT COCKPIT FRAME 10 FWD SUPPORT BRACKET IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,454 hrs · 31,153 cycles

DURING HMBV INSPECTION FOUND FRAME 73 HAS CRACKED SHEAR CLIP & FRAME SUPPORT BETWEEN STRINGERS 15L & 16L. R & R FRAME 73 SHEAR CLIP & FRAME SUPPORT BETWEEN STRINGERS 15L & 16L IAW SRM 51-40-02.

Part: LIGHT — CRACKED (CABIN) · airframe 34,454 hrs · 31,153 cycles

LEFT FLOOR EMERGENCY LIGHT STRIP NR 5 IS CRACKED. REPLACED LIGHT STRIP IAW AMM 33-50-12.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,454 hrs · 31,153 cycles

FRAME 72 IS CRACKED AT FLOOR & WALL SUPPORT BETWEEN STRINGERS 15L & 16L. COMPLIED WITH ERS-EM-53MR-439.

Part: WIRE — BROKEN (CABIN) · airframe 34,454 hrs · 31,153 cycles

FORWARD EMERGENCY FLOOR LIGHT STRIP FOUND WIRES BROKEN TO LIGHT STRIP. R & R FWD EMERGENCY FLOOR LIGHT STRIP IAW AMM 33-50-12.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 34,454 hrs · 31,153 cycles

WEB SUPPORT BENEATH THE LT SIDE COCKPIT AILERON TORQUE TUBE IS CRACKED AT THE LIGHTENING HOLE, APPROXIMATELY 1/2 INCH IN LENGTH. REPAIRED DAMAGED AREA IAW ERS-EM-53MR-421.

Part: ANTENNA — FAULTY (ELT) · airframe 34,454 hrs · 31,153 cycles

ELT FAILED BIT TEST, THREE FLASHES SHOWS A 406.025 MHZ TRANSMITTER PROBLEM. R & R ELT ANTENNA IAW AMM 25-61-03 & ETN GN-34-013. OPERATIONS CHECKED GOOD IAW AMM 25-61-00.

Part: TRUNNION — CRACKED (RT MLG) · airframe 34,454 hrs · 31,153 cycles

RIGHT WING MLG AFT TRUNNION FITTING IS CRACKED. R & R RT WING MLG AFT TRUNNION IAW ERS-EM-57MR-141.

Part: CONNECTOR — BROKEN (CABIN) · airframe 34,454 hrs · 31,153 cycles

EMERGENCY LIGHT STRIP NR 2 HAS A CONNECTOR BROKEN OFF OF WIRE, OLD CONNECTOR TAPED TO WIRE. R & R SPLICE ON NR 2 LIGHT STRIP IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: BRACKET — DEBONDED (EMERGENCY EXIT) · airframe 34,454 hrs · 31,153 cycles

RIGHT EMERGENCY EXIT INNER LINING HAS BROKEN SECURING POINT. INSPECTED RT EMERGENCY EXIT INNER LINING FOUND THAT IT WAS NOT BROKEN, JUST BRACKET WAS DE-BONDED FROM PANEL. RE-BONDED BRACKET TO PANEL IAW AMM 25-00-00.

Part: LIGHT — BROKEN (CABIN) · airframe 34,454 hrs · 31,153 cycles

RIGHT NR 1 CTR AISLE PROX STRIP BROKEN. R & R RT NR 1 CTR AISLE PROX STRIP IAW AMM 33-50-12.

Part: BRACKET — UNSECURE (EMERGENCY EXIT) · airframe 34,454 hrs · 31,153 cycles

LEFT EMERGENCY EXIT DOOR LINING HAS 3 BRACKETS THAT CAME UNGLUED THAT HOLDS LINING ONTO DOOR. RE-BONDED 3 BRACKETS ON TO LT EMERGENCY EXIT DOOR LINING IAW AMM 25-00-00.

Part: LIGHT — CRACKED (CABIN) · airframe 34,454 hrs · 31,153 cycles

LEFT FLOOR EMERGENCY LIGHT SWITCH NR 7 IS CRACKED. REPLACED EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: CONNECTOR — BROKEN (CABIN) · airframe 34,454 hrs · 31,153 cycles

FLOOR PROXIMITY STRIP LIGHTS WIRE CONNECTOR BROKEN, PAX CTR FLOOR PANEL JUST FWD OF LAVATORY ENTRANCE. R & R FLOOR PROXIMITY STRIP LIGHTS WIRE CONNECTOR AT PAX CTR FLOOR PANEL JUST FWD OF LAVATORY ENTRANCE IAW SWPM 20-50-01. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,386 hrs · 31,089 cycles

LEFT HAND OVERWING EMERGENCY LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT BULB IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.

Part: MUFFLER — UNSECURE (AC BAY) · airframe 34,095 hrs · 30,878 cycles

UPON CLIMB OUT AT 1500' FLIGHT ATTENDANT ADVISED OF CABIN IN FUMES & SMOKE, WHITE. SMOKE TAPERED OFF SLIGHTLY UPON LEVEL OFF & RETURNED DURING DESCENT. PERFORMED TROUBLESHOOTING IAW FIM TASK 21-20-00-810-801-A, UP TO TASK OR STEP NR 7. FOUND RECIRCULATION MUFFLER OFF FROM JOINING DUCT, SECURED IAW AMM 21-24-02, RAN ACFT IAW 21-10-00 & AMM72-00-00, OPERATIONS CHECKED GOOD, NO FAULTS NOTED.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 33,736 hrs · 30,621 cycles

ON DESCENT APPROACH & LANDING HAD STRONG ELEC ODOR IN THE COCKPIT, NO SMOKE. REPLACED FLASHLIGHT ASSEMBLY BEHIND CAPTAIN`S SEAT IAW AMM 33-50-16. NO OTHER DEFECTS FOUND OR OBSERVED.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 33,215 hrs · 30,234 cycles

F/O FLASHLIGHT CRADLE BROKEN. R & R FLASHLIGHT CRADLE IAW AMM 33-50-16.

Part: STRINGER — DAMAGED (6 RIGHT) · airframe 32,982 hrs · 30,033 cycles

STRINGER 6R BIRD STRIKE DAMAGE. REPAIRED STRINGER 6R IAW EO EM-53MR-2205 DAMAGE FOUND AFTER FLT WITH A BIRD STRIKE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,982 hrs · 30,033 cycles

FORWARD FUSELAGE 1 RT AFT SKIN BIRD STRIKE DAMAGE. REPAIRED FWD FUSLEAGE 1 RT AFT SKIN IAW EO EM-53MR-2206. DAMAGE FOUND AFTER FLT WITH A BIRD STRIKE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,973 hrs · 30,026 cycles

FRAME 4 IS CRACKED NEAR TO THE STRINGER, DUE TO BIRD STRIKE. REPAIRED FRAME 4 IAW EO EM-53MR-2206.

Part: PROXIMITY SENSOR — INOPERATIVE (LT MLG UPLOCK) · airframe 32,952 hrs · 30,010 cycles

THE CREW REPORTED JUST AFTER LEVELING AT FL 360 THEY HEARD & FELT A LOUD THUMP UNDER THE COCKPIT FLOORBOARD. THE ACFT DID NOT GIVE ANY AN INDICATION OF A MALFUNCTION , BUT THE CREW HEARD THE THUMP AGAIN. THE CREW DIVERTED SO THAT MX COULD INSPECT THE ACFT. THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 2 PROX SWITCH ON RT MLG UPLOCK IAW AMM 32-61-01. THE FUNCTIONAL CHECK WAS GOOD IAW AMM 32-63-05. THE ACFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 31,420 hrs · 28,785 cycles

ON FLIGHT 3368 THE CREW REPORTED A STRONG SMELL AFTER INCREASING AND DECREASING THRUST LEVERS (ARCH OR RUBBER /ODOR). THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ODOR EVENT TROUBLESHOOTING ETN EM 72-034 NO ODOR DETECTED, BRIGHT LT OF ENGINE APU & ACM INLET FOR SERVICE IAW GNC. THE FUNCTIONAL CHECK FLIGHT WAS FOUND SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — PEELING (WINDSHIELD) · airframe 30,455 hrs · 28,028 cycles

ON FLIGHT 2807 THE CREW REPORTED THAT ON TAKEOFF ACCELERATING TO 180 KNOTS THE CREW NOTICED A COCKPIT NOISE RESEMBLING STATIC OR CRACKING EMINATING FROM THE OVERHEAD PANEL ON THE CAPTAIN’S SIDE. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED INSPECTION OF CAPTTAIN’S FORWARD WINDOW AND FOUND CAPTAIN’S HUMP SEAL PEELING OFF (2"). DEFERRED PER TDMI #647560759. GOOD FOR 100 FH REF EMB 145 AMM 56-10-01. REPAIRED CAPTAIN’S WINDSHIELD HUMPSEAL IAW EMB 145 MM 56-10-01 TDMI RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 30,285 hrs · 27,895 cycles

ON FLIGHT 2775 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (APU COWLING) · airframe 30,070 hrs · 27,719 cycles

DURING MAINTENANCE INSPECTION FOUND THE APU COWLING FORWARD FRAME CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. FABRICATED AND INSTALLED FILLER, DOUBLER AND SHIM. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 30,101 hrs · 27,750 cycles

DURING MAINTENANCE INSPECTION FOUND A BROKEN EMERGENCY LIGHT STRIP WIRE AT FLOOR PANEL 24DF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE BROKEN CONNECTOR AT THE FLOOR EMERGENCY LIGHT STRIP AT FLOORBOARD 242DF IAW EMB145 SWPM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,101 hrs · 27,750 cycles

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

Part: STRUCTURE — CRACKED (E/E BAY DOOR) · airframe 30,070 hrs · 27,719 cycles

AFT ELECTRONICS DOOR INNER STRUCTURE IS CRACKED AT BOTH RIVETS OF RETAINER PIN EYELET. REPAIRED AFT ELECTRONICS DOOR 272DR INNER STRUCTURE IS CRACKED AT BOTH RIVETS OF RETAINER PIN EYELET IAW AEA EM-52MR-324.

Part: LIGHT — UNSERVICEABLE (OVERWING) · airframe 30,052 hrs · 27,704 cycles

DURING MAINTENANCE INSPECTION, FOUND EMERGENCY EXTERIOR OVERWING AFT LIGHT INOPERATIVE. AIRCRAFT REMOVE FROM SERVICE. REPLACED LEFT AFT EXTERIOR EMERGENCY LIGHT ASSY IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.

Part: CRADLE — INOPERATIVE (FLASHLIGHT) · airframe 30,046 hrs · 27,700 cycles

DURING MAINTENANCE INSPECTION, FOUND CAPTS FLASHLIGHT HOLDER FINGERS CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT BASE IAW AMM 33-50-16. OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED. THE AIRCRAFT RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,046 hrs · 27,700 cycles

DURING MAINTENANCE INSPECTION, FOUND EMERGENCY EXTERIOR OVERWING AFT LIGHT ON BOTH SIDE ARE OUT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND INSTALLED NR 4 BATTERY POWER CHARGER IAW AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,780 hrs · 27,508 cycles

DURING B INSPECTION, FOUND THE LAST ROW EMERGENCY LIGHT STRIP INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAST ROW EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD IAW AE WC 33-700-17. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — DAMAGED (COCKPIT) · airframe 29,435 hrs · 27,275 cycles

FLIGHT 4260, CREW REPORTED THE COCKPIT FLASHLIGHT BEHIND THE CAPTAIN IS MISSING RED CHARGE INDICATOR. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT IAW SMP. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,547 hrs · 26,650 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT AND RIGHT AFT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY ASSEMBLY AND BATTERY CHARGER. THE OPERATIONAL CHECK WAS GOOD IAW WC 33-700-19. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,472 hrs · 26,596 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT OVERWING EXTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY AND EMERGENCY POWER SUPPLY CHARGER IAW WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,467 hrs · 26,591 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT AND LEFT OVERWING EXTERIOR EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHTING BATTERY CHARGER AND BATTERY IAW AE MTX WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE INDICATION (CARGO BAY) · airframe 282,228 hrs · 26,411 cycles

ON FLIGHT 3450 THE CREW REPORTED THAT WHILE ON TAXI THEY RECEIVED A BAGGAGE SMOKE INDICATION MESSAGE. THE CREW ELECTED TO ABORT THE TAKE OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BAGGAGE COMPARTMENT FIRE EXTINGUISHER BOTTLES IAW AMM 26-23-01. THE OPS CHECKED GOOD IAW AMM 26-10-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,117 hrs · 26,337 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FLOOR PROXIMITY STRIP LIGHT AT ROW 5-7 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY STRIP AT ROW 5-7. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 27,900 hrs · 26,192 cycles

ON FLIGHT 3347 THE CREW REPORTED THAT AFTER LANDING THEY RECEIVED A BAGGAGE SMOKE MESSAGE MOMENTARILY ON EICAS ALONG WITH ILLUMINATION OF BAGGAGE EXTINGUISHIER LIGHT ON OVERHEAD. EICAS MESSAGE EXTINGUISHED AND LIGHT REMAINED. NO OTHER VISUAL INDICATIONS. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL TEST AND FUNCTIONAL CHECK OF BAGGAGE SMOKE DETECTION SYSTEM IAW EMB 145 AMM 26-15-00. NO DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 27,876 hrs · 26,177 cycles

DURING MAINTENANCE VISIT FOUND THE GALLEY OVERHEAD EMERGENCY BULB NOT INSTALLED. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED GALLEY OVERHEAD EMERGENCY LAMP IAW EMB AMM TASK 33-50-09-400-801A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POTENTIOMETER — BROKEN (RUDDER PEDAL) · airframe 27,768 hrs · 26,091 cycles

FOR FLIGHT 4176 THE CREW REPORTED THE NOSE WHEELS PRESENTED ERRATIC BEHAVIOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND RUDDER PEDAL POTENTIOMETER STUD BROKEN. REMOVED AND REPLACED POTENTIOMETER IAW EMB 145 AMM 32-50-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INDICATION SYS — ACTIVATED (COCKPIT) · airframe 27,106 hrs · 25,592 cycles

ON FLIGHT 2959 DISPATCH REPORTED THE CREW BLEW THE CARGO FIRE BOTTLES DUE TO A SMOKE INDICATION. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO METERING FIRE EXTINGUISHER BOTTLE IAW EMB 145 AMM 26-23-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 26,700 hrs · 25,302 cycles

ON FLIGHT 2901 THE CREW REPORTED, RECEIVED A BAGGAGE SMOKE INDICATION MESSAGE DURING THE TAKEOFF ROLL AT APPROXIMATELY 100 KNOTS. THE CREW WAS ABLE TO SLOW THE AIRCRAFT USING NORMAL BRAKING. BY THE TIME THE CREW SLOWED TO TAXI SPEED THE EICAS WARNING HAD DISSAPPEARED. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED BAGGAGE COMPARTMENT SMOKE DETECTION SYSTEM. OPERATIONAL CHECK MULTIPLE TIMES NO DEFECT NOTED AFTER. REMOVED AND REPLACED THE AFT BAGGAGE SMOKE DETECTOR IAW EMB AMM 26-15-01. THE OPERATIONAL CHECK DONE IAW EMB AMM 26-15-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,507 hrs · 25,139 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT OVERWING EMERGENCY LT IAW 33-50-06. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,369 hrs · 25,035 cycles

FOR FLIGHT 2885 DURING THE PREFLIGHT INSPECTION FOUND THE RIGHT OVERWING AFT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT BULB. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,083 hrs · 24,010 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT AFT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT EXTERNAL OVERWING EMERGENCY LIGHT IAW EMB AMM TASK 33-50-07-000-802-AAND 33-50-07-440-802-A. THE OPERATIONAL CHECK WAS NORMAL AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 25,074 hrs · 23,999 cycles

DURING MAINTENANCE BASE INSPECTION FOUND FRAME 65 ON THE RIGHT TOOL DAMAGE BEYOND LIMITS OF THE SRM. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH REPAIR OF Z-FRAME 65 RIGHT IAW EO EM-53MR-1673. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 25,074 hrs · 23,999 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND FRAME 70 RIGHT SIDE HAS TOOLING MARKS. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE CORRECTIVE ACTION INFORMATION IS PENDING.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 25,074 hrs · 23,999 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND STRINGER 19 LEFT IS CHAFED BETWEEN FRAMES 52 AND 53. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED STRINGER 19 LEFT BETWEEN FRAMES 52 AND 53 IAW EMB SRM 53-24-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 25,074 hrs · 23,999 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND STRINGER 19 RIGHT CHAFED BETWEEN FRAMES 52 AND 53. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED STRINGER 19 RIGHT BETWEEN FRAMES 52 AND 53 IAW EMB SRM 53-24-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 24,939 hrs · 23,891 cycles

DURING MAINTENANCE BASE VISIT ALL EMERGENCY LIGHTS ON BATTERY PACK NR 1 WERE FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY POWER SUPPLY AND CHARGER. THE OPERATIONAL CHECK WAS GOOD IAW WC 33-700-19. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,482 hrs · 23,520 cycles

DURING MAINTENANCE INSPECTION FOR FLIGHT 4219 THE RIGHT AFT EXIT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EXIT EMERGENCY LIGHT IAW EMB-145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — FAILED (CABIN) · airframe 23,809 hrs · 22,990 cycles

ON FLIGHT 2721 THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT OVER THE FLIGHT ATTENDANT’S SEAT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 POWER INVERTER IAW EMB 145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,644 hrs · 21,151 cycles

DURING PERIODIC SERVICE 1 CHECK, MAINTENANCE FOUND EMERGENCY LIGHT ABOVE SERVICE DOOR TO BE INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REPLACED WITH NEW EXIT MARKING SIGN ASSEMBLY, OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (MLG) · airframe 17,962 hrs · 17,916 cycles

ON FLIGHT 3719, THE CREW NOTED AFTER TAKEOFF AFTER LANDING GEAR HANDLE SELECTED UP GEAR NEVER MOVED. LANDING GEAR LEVER DISAGREE ON EICAS AT APPROX 700' AGL FOLLOWED ALL AOM PROCEDURES SEVERAL TIMES GEAR WOULD NOT COME UP LANDED OVER WEIGHT AT 44,600 LBS RATE OF DESCENT LESS THAN 50'/MIN NORMAL ROLL OUT NO PROBLEMS WITH GEAR AFTER LANDING. DOWNLOADED CMC AND FOLLOWED FIM 32-61-00-810-807. FOUND PROBLEM IN LGEU REMOVED AND REPLACED LGEU IAW EMB 145 AMM 32-32-01. PERFORMED LDG GEAR EXTENSION/RETRACTION IAW EMB 145 AMM EMB 145 AMM 32-30-00. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL LEVER — MALFUNCTIONED (MLG) · airframe 17,962 hrs · 17,916 cycles

ON FLIGHT 3619, THE CREW NOTED AFTER TAKEOFF WHEN SELECTED GEAR HANDLE UP GEAR SHOWS IN TRANSIT LIGHT LONGER THAN NORMAL. LANDING GEAR DISAGREE AND CREW NOTED THAT IT SOUNDED LIKE THE GEAR DID NOT RAISE. CREW SELECT GEAR HANDLE DOWN 3 GREEN CREW ELECTED TO RETURN TO DFW. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB 145 AMM 32-32-02. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,173 hrs · 17,174 cycles

EMERGENCY FLOOR LIGHT STRIP ROW 7 THROUGH 12 INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOOR PROXIMITY STRIP LIGHT IAW EMB AMM 33-50-12. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY EXIT) · airframe 16,273 hrs · 16,404 cycles

EMERGENCY EXIT LIGHT ABOVE SERVICE DOOR INOPERATIVE. RESECURED LOOSE CONNECTOR ABOVE GALLEY CEILING PANEL IAW EMB AMM 20-00-00. OPERATIONAL CHECK GOOD IAW EMB AMM 33-50-11. RETURNED AIRCRAFT TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 15,408 hrs · 15,663 cycles

EMERGENCY BATTERIES DEAD. REMOVED AND REPLACED BATTERY PACK AT LOCATION BT8501, BT8502, BT503 AND BT8526 IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 15,248 hrs · 15,537 cycles

RIGHT VERTICAL TO FUSELAGE DRAG ANGLE CRACKED. FABRICATED ANGLE, CLEANED TREATED AND INSTALLED FABRICATED ANGLE IAW EMB IC2006-145-9432 AND SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,248 hrs · 15,537 cycles

FOUND PREVIOUS REPAIR ON LEFT OMEGA BEAM CORRODED AT FRAME 20. FABRICATED DOUBLER, CLEANED, TREATED AND INSTALLED DOUBLER IAW EMB SRM 53-00-10. AIRCRAFT RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,248 hrs · 15,537 cycles

LEFT OMEGA BEAM FOUND CORRODED AT FRAME 58 AND 59. FABRICATED REPAIR ANGLE, CLEANED, TREATED AND INSTALLED ANGLE IAW EMB SRM 53-21-10 EMB IC2006-145/9434.

Part: FUEL SYS — LEAKING (APU)

MSN - FLT 3922 - FUEL LEAKING FROM APU AND FUEL SMELL IN CABIN. (M)

Part: CONTROL MODULE — BURNED (CABIN LIGHTS)

REPORTED AN ELECTRICAL ODOR IN THE CABIN DURING FLIGHT. ODOR WAS COMING FROM AREA AROUND FIRST ROW OF SEATS. REMOVED AND REPLACED CABIN LIGHT CONTROL MODULE, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DAMAGED (FUSELAGE)

HAIL DAMAGE BETWEEN FRAMES 30-31 AND STRINGER 21L AND 21R. PERFORMED CUT OUT OF DAMAGE. FABRICATED A DOUBLER AND FILLER. REPAIR DONE IAW SRM. (K)

Part: SKIN — DENTED (FUSELAGE)

DENT IN THE FUSELAGE BETWEEN STRINGER 20R AND 21R AT FRAME 15. REMOVED THE DENT BY MAKING CUTOUT. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K)

Part: WINDOW — FAILED (COCKPIT)

DURING CRUISE FLIGHT, CREW REPORTED THE CAPTAINS WINDSHIELD SHATTERED. AIRCRAFT WAS DIVERTED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW MFG MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406966)

Part: CHARGER — INOPERATIVE (CABIN)

ORD - FLT 4240 - CREW REPORTED THE AFT HALF OF THE CABIN EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

SWF - FLT 4133 - CREW REPORTED SEVERAL EMERGENCY LIGHTS IN THE AFT CABIN TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTEYR IN THE NR 4 POWER SUPPLY UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - FOUND GALLEY FLOOR CENTER BEAM CORRODED AT FRAME 20. REPAIRED GALLEY FLOOR CENTER BEAM CORROSION AT FRAME 20 IAW EMB145 REPAIR STATEMENT GST 3215/01. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - FOUND SERVICE DOOR AFT SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE AFT SILL AT SERVICE DOOR IAW EMB145 SRM 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND FORWARD DIGITAL CORRODED. REPAIRED FORWARD DIGITAL IAW EMB145 SRM. (M)

Part: GUSSET — CORRODED (FUSELAGE)

FOUND CENTER BEAM GUSSET CORRODED. INSTALLED NEW SERVICEABLE CENTER BEAM GUSSET IAW EMB145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL TWO FINDING ON A CORROSION REPAIR ITEM CARD NR 23851. SERVICE DOOR CENTER SILL CORRODED. BLENDED CORROSION SERVICE DOOR CENTER SILL IAW EMB145 CP 51-14-02. REPAIRED SERVICE DOOR CENTER. SILL IAW EMB GST-3215/01. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN MBV INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA FLOORBEAM AT FRAME 20. REMOVED CORROSION BY CUTOUT. FABRICATED A FILLER AND DOUBLER ANGLE. A PLATE AND TWO SHIMS IAW EMB145 (SRM 145/1142 CHAPTER 53 REV 14) 53-21-10, PG 204, FIG 201, SHEET 1 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING A MBV INSPECTION, CORROSION WAS FOUND ON THE GALLEY FLOOR FORWARD DIGITAL. REMOVED CORROSION BY BLENDING OUT. PERFORMED NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER IAW EMB GST-3215/01 AND STANDARD SRM PRACTICES. (M)

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

THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 23846. PAX DOOR THRESHOLD SUPPORTS CORRODED. BLENDED CORROSION IAW EMB CPM 51-14-02. PERFORMED THICKNESS TEST AND EDDY CURRENT. NO DEFECTS. REPAIRED PAX DOOR THRESHOLD SUPPORT IAW EMB GST-3215/01. (M)

Part: GUSSET — CORRODED (FUSELAGE)

ABI - THIS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 23843. CENTER BEAM GUSSET CORRODED. REMOVED CORROSION IAW EMB SRM 51-10-02. INSTALLED NEW SERVICEABLE CENTER BEAM GUSSET IAW EMB145 SRM 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3

ABI - THIS IS A LEVEL 3 FINDING ON A CORROSION REPAIR ITEM CARD NR 23803. LEFT OMEGA BEAM CORRODED AT FRAME 20. REPAIRED LEFT OMEGA BEAM AT FRAME 20 IAW EMB 145 SRM 53-21-10 FIG 201, PAGE 20. (M)

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

ABI - THIS IS A LEVEL TWO FINDING ON A CORROSION REPAIR ITEM CARD NR 23844. RIGHT GALLEY AFT GUSSET PLATE CORRODED. BLENDED CORROSION. INSTALLED SERVICEABLE RIGHT GALLEY AFT GUSSET PLATE IAW EMB145 SRM 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION AIRCRAFT 647AE CORROSION WAS FOUND ON THE GALLEY FLOOR CENTER BEAM AT FRAME 20. REMOVED CORROSION BY BLENDING AND CUT OUT DAMAGED AREA. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTION INDICATED. FABRICATED A FILLER, AND DOUBLER IAW EMB GST-3215/01 AND STANDARD SRM PRACTICES. (M)

Part: LIGHT — MALFUNCTIONED (CABIN)

MSN - FLT 3426 - FOUND FLOOR EMERGENCY PROX LIGHTS FROM ROWS 12 AFT CAME ON THEN EXTINGUISHED. PERFORMED OPS CHECK TO SYSTEM IAW AMM, OPS CHECK GOOD. NO DEFECTS NOTED. (M)

Part: ENGINE

ON TAKEOFF, E1 ATTS NO MARGIN. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGNIE IAW WC 05-50-00-400-801-A RUN AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — INOPERATIVE (HORIZ STAB)

ORD - FLT 4366 - CREW REPORTED A PITCH TRIM 1 INOPERATIVE MESSAGE ON EICAS AND BOTH MAIN SWITCHES INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SOCKET — FAILED (COCKPIT)

CRW - FLT 4020 - FOUND CREW REPORTED NR 2 PITOT FAIL ON EICAS AND THAN HAD AN ELECTRICAL SMELL THROUGHOUT CABIN AND COCKPIT. CREW MADE AN EMERGENCY LANDING WITHOUT INCIDENT IN CRW. MAINTENANCE REMOVED AND REPLACED RELAY AND SOCKET. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: RELAY — FAILED (COCKPIT)

CRW - FLT 4020 - CREW REPORTED NR 2 PITOT FAIL ON EICAS AND THAN HAD AN ELECTRICAL SMELL THROUGHOUT CABIN AND COCKPIT. CREW MADE AN EMERGENCY LANDING WITHOUT INCIDENT IN CRW. MAINTENANCE REMOVED AND REPLACED RELAY AND SOCKET. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

LBB - FLT 9734 - FLOOR PROXIMITY EMERGENCY LIGHTS IN BACK OF CABIN ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SWITCH — FAILED (NR 2 ENGINE)

FWA - FLT 3432 - ON TAKEOFF ROLL, CREW NOTED THRUST REVERSER DISAGREE MESSAGE ON EICAS. TAKEOFF WAS ABORTED AND AIRCRAFT RETURND TO GATE. MAINTENANCE FOUND THE NR 2 OUTBOARD STOW SWITCH INOPERATIVE. SWITCH REMOVED AND REPLACED IAW EMB MM. OPERATIONAL CHECK WAS SATISFACTORY, AICRAFT RETURNED TO SERVICE. NOTE: PREVIOUSLY SUBMITTED CLOSED, BUT WAS ON MEL STILL CORRECTIVE ACTION WAS THE STOW MICROSWITCHES WERE ADJUSTED BY ADDING SHIMS TO STRIKER PLATE ASSYS IAW EMB MM. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (X)

Part: CONTROL VALVE — INOPERATIVE (THRUST REVERSER)

FWA - FLT 3432 - DURING TAKEOFF ROLL, CREW HAD AN E1 TR DISAGREE ON EICAS. TAKEOFF WAS ABORTED AND AIRCRAFT WAS RETURNED TO GATE. THRUST REVERSERS WERE PUT ON MEL AT THIS TIME. MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL VALVE IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: MODULE — FAILED (NR 2 ENGINE) · airframe 545 hrs · 596 cycles

ORD - FLT 4055 - ON TAKEOFF ROLL. CREW REPORTED AN E2 FIRE WARNING INDICATION. ABORTED TAKEOFF. RETURNED TO GATE AND NO FIRE WAS NOTED. REMOVED AND REPLACED NR 2 FIRE CONTROL MODULE IAW EMB MM 26-11-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)