N644AE

Part: RETAINER — CRACKED (ZONE 600 FLAP) · airframe 56,272 hrs · 53,417 cycles

410 RH IB FLAP AERODYNAMIC SEAL SHROUD RETAINER CRACKED. RAR RATAINER IAW 51-40-02

Part: DOOR — NO DISCREPANCY (ZONE 800) · airframe 54,839 hrs · 51,739 cycles

DURING CLIMB OUT BAGG OPEN IND PRESENTED WITH CABIN RATE CLIMB 2000 FT PER MIN. OPENED AND CLOSED DOOR SEVERAL TIMES DOOR OPS NORMALLY AS REQ

Part: FAIRING — DAMAGED (RT ELEVATOR) · airframe 53,853 hrs · 50,655 cycles

LIGHNING DAMAGE TO RH ELEVATOR TIP FAIRING. RAR TIP FAIRING IAW AMM 55-20-01

Part: SKIN — CRACKED (ZONE 500) · airframe 53,721 hrs · 38,373 cycles

LH LWR SKIN PANEL PN 145-66205-005 HAS 3" CRACK AT TR-4374.44 BTW RIBS11-12, SPAR II. REPAIRED IAW EO1-57-24-0510

Part: SKIN — CRACKED (ZONE 600) · airframe 53,721 hrs · 38,373 cycles

RH WING LWR SKIN CRACKED BTW RIB 11-12, SPAR II. REPAIRED IAW EO1-57-24-0511

Part: UPLOCK — FAULTED (NLG) · airframe 52,792 hrs · 49,445 cycles

DURING CLIMB AT 6000-1000FT AND ON DECENT AT 8,000 FT LOUD BANGING SOUND COMING FROM NOSE GEAR AREA. VIBRATION FELT IN FLT DECK FLOOR. R&R NLG UPLOCK BOX IAW EMB AMM 32-33-07 UP TO STEP (1) ON SUBTASK 842-002-A. INSTALL NEW PROXIMITY SWITCHES IN REF TO AMM 36-61-01. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN)

DURING T/O PACK 1-2 OVHT DISPLAYED WITH STRONG FUME SMELL IN FLT DECK FOLLOWED QRH RESET PACKS MESSAGE CLEARED SMELL DISSIPATED FACT 31OCT23 14:09 CLT PERFORMED GROUND RUNS, NO DEFECTS NOTED. A/C OK FOR SERVICE. UPON FURTHER INSPECTION, FOUND 2 TORN PACK SLEEVES ON #2 PACK Y-DUCT. R&R BOTH PACK SLEEVES, OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN)

PACK 1 OVERHEAT DISPLAYED PRIOR TO ROTATION. COULD NOT DUPLICATE FAULT OF PACK #1 OVERHEAT. PERFORMED PACK #1 OVERHEAT TEST IAW AMM REF 21-51-09. OK FOR SERVICE AT THIS TIME. CLEAR MEL 21-15-1

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,177 hrs · 48,771 cycles

SUSPECTED FUEL LEAK FROM LH WING IN FLIGHT. MX INSPECTED LH WING FOR FUEL LEAK.FOUND LOOSE FASTENERS RESECURED FASTENERS AS REQUIRED, NO FUEL LEAK EVIDENCE FOUND. A/C OK FOR SERVICE. INSPECTED MAGNA STICKS AND OVER WING FUEL CAP. INSPECTED LEFT WING SPOILER AND SPEED BRAKE FOR LEAKS. NO LEAKS NOTED. R/R OVER WING FUEL CAP IAW AMM 28-11-06. OK FOR SERVICE.

Part: FLOORBEAM — CORRODED (UNKNOWN) · corrosion level 2 · airframe 51,851 hrs · 48,416 cycles

LAV CENTER FLOORBEAM GUSSSET HAS LEVEL 1 CORROSION. BLENDED CORROSION ON LAV FLOORBEAM GUSSET IAW EMB145 SRM 511003. UPON INVESTIGATION LAV CENTER FLOORBEAM GUSSET ORIGINAL THICKNESS SHOWN IN SRM 53-24-10AD SHOWS TO HAVE NOMINAL THICKNESS=.040". REMAINING THICKNESS AT BLENDED AREA ON LAV CENTER FLOORBEAM GUSSET FOUND TO BE WITHIN LIMITS IAW EMB145 SRM 53-24-10AD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,851 hrs · 48,416 cycles

E986248 REAR FUSELAGE SKIN BUSHING REPAIRS AT FR 77 STGR 4R-5R (LOWER BUSHING), AND STGR 8R-9R. REQUIRE DT INSPECTION IAW EMB 145 SRM 53-32-01, ITEM 10. ACCOMPLISHED DVI ON REAR FUSELAGE SKIN BUSHING REPAIRS AT FR 77 STGR 4R-5R (LOWER BUSHING), AND STGR 8R-9R IAW EMB 145 SRM 53-32-01, ITEM 10. RECEIVED PIEDMONT EO1-05-23-0208 FOR 500 HOUR DMT DTA.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,851 hrs · 48,416 cycles

E986166 EXTERNAL FUSELAGE REPAIR FRAME 7-8 STR 13L-15L HAS NO DTI INFO. : RECEIVED PIEDMONT EO1-05-23-0186 FOR EXISTING EXTERNAL FUSELAGE REPAIR AT FR 7-8 AND BTW STR 13L-15L. EO ACCEPTS REPAIRED AREA AS IS AND HAS INSTRUCTIONS FOR DTI

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,851 hrs · 48,416 cycles

UNDER AFT BELLY PANEL EXTERNAL FUSELAGE STGR 19R REPAIR BTW FR 52--53 NO REPAIR INFO. REMOVED PREVIOUS REPAIR UNDER AFT BELLY PANEL EXTERNAL FUSELAGE STR 19R BTW FR 52-53 WITH NO REPAIR INFORMATION AND REPAIRED STR 19R IAW PIEDMONT EO EO1-53-23-0211 AND EMB 145 SRM 53-24-02RE ITEM 2, FIG 201.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,851 hrs · 48,416 cycles

UNDER AFT BELLY PANEL EXTERNAL FUSELAGE STGR 19L PREVIOUS REPAIR IS CHAFED BTW FR 52-53. REMOVED CHAFED PREVIOUS REPAIR UNDER AFT BELLY PANEL EXTERNAL FUSELAGE STR 19L BTW FR 52-53 AND REPAIRED STR 19L IAW PIEDMONT EO1-53-23-0210 AND EMB 145 SRM 53-24-02RE ITEM 2, FIG 201.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,851 hrs · 48,416 cycles

E985328 L/H WINDSHIELD LATERAL POST UPPER ATTACH POINT SKIN CRACKED JUST FWD OF SPEAKER. RAR L/H WINDSHIELD LATERAL POST IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,851 hrs · 48,416 cycles

E985348 STRINGER 6R CRACKED BEHIND FRAME 13 R/H SIDE OF COCKPIT. EMOVED AND REPLACED STRINGER 6R BEHIND FRAME 13 R/H SIDE OF COCKPIT IAW EMB145 SRM 51-40-02.

Part: PRESSURE DECK — CRACKED (COCKPIT) · corrosion level 2 · airframe 51,851 hrs · 48,416 cycles

COCKPIT UNDERFLOOR MAINTENANCE HATCH CUTOUT LH BRACKED HAS LEVEL 1 CORROSION BETWEEN BRACKET AND SKIN. BLENDED AREA ON COCKPIT UNDERFLOOR BETWEEN BRACKET AND SKIN IA ACCEPTED PERMANENT REPAIR IAW ETD2023-145-017636

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,851 hrs · 48,416 cycles

E985174 PAX DOOR ENTRENCE AFT FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED PAX DOOR ENTRANCE AFT FLOORBOARD SUPPORT IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,851 hrs · 48,416 cycles

E985210 R/H #2 FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED WITH SERVICABLE R/H #2 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,851 hrs · 48,416 cycles

E985209 R/H #1 FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED WITH SERVICEABLE R/H #1 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02

Part: DOOR SEAL — LEAKING · airframe 51,025 hrs · 47,526 cycles

CABIN PRESSURE ERRATIC ON CLIMB. REACHED 14400'. FOUND SEAL ON GROUND CONNECTION DOOR TO BE WORN R&R SEAL IN REF TO AMM 21-22-04-000/400-802-A PERFORMED OPS CHECK IN REF TO AMM 21-31-00-700-808-A LEAK CHECK GOOD CLEAR MEL 21-12-3

Part: NONE — NONE · airframe 49,689 hrs · 46,042 cycles

PDIS 644 34-11 2574541 22APR22 PHL CLOSE STANDBY ALTITUDE IND IS UNRELIABLE. JUMP FROM 100-400 FT RANDOMLY FACT 22APR22 13:21 PHL R&R STBY ALTIMETER IAW AMM34-13-00 PERFORMED OPS CK IAW AMM 34-11-00. OPS LEAK CK GOOD. OK FOR SERVICE.

Part: NONE — NONE · airframe 48,713 hrs · 44,964 cycles

MULTIPLE BIRD STRIKES ON A/C ON NOSE, TOP OF FLIGHT DECK & ON HORIZONTAL STAB. CLEANED AND INSPECTED A/C FOR BIRD STRIKES. FOUND 2 BIRD STRIKES ABOVE COCKPIT WINDOWS WITH NO DEFECTS NOTED. INSPECTED IAW AMM 05-50-08-200-802-A. NO DEFECTS NOTED ON HORIZONTAL STAB. A/C OK FOR SERVICE.

Part: UNKNOWN — ODOR (LAVATORY) · airframe 48,026 hrs · 44,206 cycles

PILOT WAS DOING HIS PRE FLIGHT WALK AROUND IN THE CABIN AND NOTICED A SMELL IN THE LAVATORY. WILL MONITER

Part: DOOR SILL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 48,017 hrs · 44,199 cycles

SSI 53-30-48: CARGO DOOR CUTOUT LWR SILL CORRODED. REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW EMB145 SRM 51-40-02.

Part: SKIN — DAMAGED (FRM 19 S2-4R) · airframe 48,017 hrs · 44,199 cycles

PREVIOUS REPAIR OF FR 19 BETWEEN STGR. 2R-4R IS DAMAGED. RE-ACCOMPLISHED REPAIR OF FR19 BETWEEN STRINGER 2R - 4R IAW PIEDMONT EO1-53-21-0107.

Part: BULKHEAD — DAMAGED (FRM 15) · airframe 48,017 hrs · 44,199 cycles

PILOTS BULK HEAD LOWER GUIDE PIN HOLE IS ELONGATED AT FR15. REPAIRED PILOTS BULK HEAD LOW-ER GUIDE PIN ELONGATED HOLE AT FR 15 IAW PIEDMONT EO1-53-21-0108.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 48,017 hrs · 44,199 cycles

SERVICE DOOR CENTER SILL IS CORRODED. REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW EMB-145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 48,017 hrs · 44,199 cycles

R/H #4 FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED RH #4 FLOORBOARD SUPPORT IAW EMB145 SRM 51--40-02.

Part: FLOOR SUPPORT — CORRODED (LAVATORY) · corrosion level 2 · airframe 48,017 hrs · 44,199 cycles

LAV L/H FLOORBOARD SUPPORT AT POTABLE WATER PULL HANDLE MOUNT HAS CORROSION. REMOVED AND REPLACED LAV L/H FLOORBOARD SUPPORT POTABLE WATER PULL HANDLE MOUNT IAW EMB 145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FRM 54) · corrosion level 2 · airframe 48,017 hrs · 44,199 cycles

SSI 53-20-11 L/H FLOOR BEAM HAS CORROSION AT CROSS BEAM AT FRAME 54. REPAIRED LH CABIN OMEGA BEAM AFT OF FR 54 CROSS MEMBER IAW ETD2021-145-012775 AND EO1-53-21-0105

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 48,017 hrs · 44,199 cycles

L/H #4 FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED L/H #4 FLOORBOARD SUPPORT IAW EMB 145 SRM51-20-03 AND SRM 51-40-02

Part: DOOR FRAME — FAILED (FRM 67) · airframe 48,017 hrs · 44,199 cycles

FR 67 BROKE ABOVE CARGO DOOR CUTOUT. REPAIRED FRAME 67 ABOVE CARGO DOOR CUTOUT IAW PIEDMONT EO1-53-21-0109.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 48,017 hrs · 44,199 cycles

R/H #3 FLOORBOARD SUPPORT HAS CORROSION. REMOVED UNSERVICEABLE R/H #3 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02.POSITIONED, DRILLED AND INSTALLED SERVICEABLE R/H #3 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02 AND 51-20-03.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 48,017 hrs · 44,199 cycles

LAV R/H FLOORBOARD SUPPORT HAS CORROSION AT POTABLE WATER ATTACH ELBOWS. REMOVED AND REPLACED LAV R/H FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02.

Part: WEB — CHAFED (CARGO DOOR) · airframe 48,017 hrs · 44,199 cycles

BAGGAGE DOOR INNER WEBBING FRAME HAS TWO CHAFE SPOTS. REPAIRED BAGGAGE DOOR INNER WEBBING FRAME CHAFES IAW PIEDMONT EO-1-52-21-0106.

Part: BUMPER — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 48,017 hrs · 44,199 cycles

L/H EMERGENCY EXIT HAS CORROSION AT LOWER AFT BUMPER. REMOVED AND INSTALLED SERVICEABLE L/H EMERGENCY EXIT LOWER AFT BUMPER PROFILE "L" IAW EMB145 SRM 51-40-02.

Part: YOKE — CRACKED (LT ENGINE) · airframe 48,017 hrs · 44,199 cycles

LH ENGINE LWR FWD YOKE CRACKED. REMOVED AND REPLACED L/H FORWARD LOWER YOKE FITTING AND GUSSET PLATE IAW ETD2021-145-012599 AND EO1--54-21-0104.

Part: DRAG ANGLE — CRACKED (FUSE TO VERTICAL) · airframe 48,017 hrs · 44,199 cycles

RH FUSELAGE TO VERTICAL STAB DRAG ANGLE IS CRACKED AT FWD FITTING AFT END. REMOVED AND REPLACED FWD RH FUSELAGE TO VERTICAL STABILIZER DRAG ANGLE IAW EMB 145 SRM 51-40-02.

Part: SKIN — CRACKED (FRM 78 S4-5L) · airframe 48,017 hrs · 44,199 cycles

REAR FUSELAGE II SKIN HAS POSSIBLE CRACKS AROUND 1 RIVET AT FR 78 BTW STRINGERS 4L-5L.REPAIRED REAR FUSELAGE II SKIN CRACKS AROUND 1 RIVET AT FR 78 BETWEEN STRINGERS 4L-5L IAW PIEDMONT EO1-53-21--0110.

Part: SKIN — CRACKED (FRM 78 S6-7L) · airframe 48,017 hrs · 44,199 cycles

REAR FUSELAGE II SKIN HAS POSSIBLE CRACKS AROUND 1 RIVET AT FR 78 BTW STRINGERS 6L-7L. REPAIRED REAR FUSELAGE II SKIN CRACKS AROUND 1 RIVET AT FR 78 BETWEEN STRINGERS 6L-7L IAW PIEDMONT EO1-53-21--0110.

Part: SKIN — CRACKED (FRM 77 S8-9L) · airframe 48,017 hrs · 44,199 cycles

REAR FUSELAGE II SKIN HAS POSSIBLE CRACKS AROUND 1 RIVET AT FR 77 BTW STRINGERS 8L-9L. REPAIRED REAR FUSELAGE II SKIN CRACKS AROUND 1 RIVET AT FR 77 BETWEEN STRINGERS 8L-9L IAW PIEDMONT EO1-53-21--0110.

Part: A/C PACK — FAILED (NR 1) · airframe 47,820 hrs · 43,978 cycles

PDIS 644 21-51 2139501 28FEB21 TRI ASSGN #1 PACK FAIL WITH BURNING SMELL MEL 28FEB21 10:56 TRI C05904 21-13-1 1 AIR CON PACK ELECTRO/MECH N600-N649 SMOKE REPORT HAS BEEN FILLED OUT, SDR SUPPLEMENTAL INFO WILL FOLLOW, CURRENTLY ON THE MEL

Part: INDICATOR — FAILED (COCKPIT) · airframe 47,726 hrs · 43,873 cycles

PDIS 644 36-11 2139201 31JAN21 ALB CLOSE. DURING CLIMB IN ICING CONDITIONS, EICAS DISPLAYED BL, EED 1 LOW TEMP MULTIPLE TIMES WITH N1 AT 85% FACT 31JAN21 07:08 ALB. R+R BLEED 1 PUSH BUTTON REF. EMB 145 AMM 20-13-04. OPS CHECK GOOD.

Part: SENSOR — FAULTED (NR 1 TEMP) · airframe 47,637 hrs · 43,770 cycles

BLD 1 OVTEMP MESSAGE DURING ICE TEST IN FLIGHT, MESSAGE EXTINGUISHES AFTER TURNING OFF ICE PROTECTION. MX TROUBLESHOT, PER FIM 36-11-00-810-803-A. R & R CHANGED NR 1 AIR FILTER AND NR 1 TEMP SENSOR ON PYLON. PERFORMED BLEED SYSTEMS OPERATIONS CHECK SEVERAL TIMES. OPERATIONS CHECK GOOD, REF AMM36-00-00-05 AND 36-20-01-05 PN OFF 0132 ADT SN OFF E5273. PN ON 0132ADT SN ON P1190.

Part: DOOR — OPEN (GPU) · airframe 46,683 hrs · 44,706 cycles

IN MODERATE TURBULENCE HEARD A THUD BY CAPTAIN LEFT HAND SIDE FOLLWED BY A VIBRATION. THEY DECREASED SPEED AND NOISE DIMINISHED....FIX: UPON A/C TAXING IN FOUND GPU DOOR OPEN, INSPECTED AREA NO FURTHER DAMAGE NOTED. PERFORMED GEAR SWING IAW EMB 145 AMM, NO DEFECTS OR NOISES HEARD AT THIS TIME.OK FOR SERVICE.

Part: WARNING MESSAGE — ACTIVATED (NR 1 ENGINE) · airframe 46,605 hrs · 42,628 cycles

AIRCRAFT RECEIVED LIGHTENING STRIKE. E1 OUT MASTER CAUTION FOLLOWED BY A HIGH SPIKE OF ITT ON ENG#1. THEN ENGINE 1 ROLL BACK AND SHUT OFF. AFTER LANDING E1 EXCEDANCE MESSAGE....FIX:PERFORMED ENG LIGHTENING INSP IAW BR 05-50-00-200-806. NO DEFECTS NOTED.PERFORMED LIGHTENING STRIKE INSPECTION IAW EMB 05-50-01.FOUND RT WING TIP DAMAGED SEE SEQ 2 FOR DESCREPENCY.PERFORMED PERFORMANCE RUN OF #1 ENGINE IAW 72-00-00-700-801.NO DEFECTS NOTED.OK FOR SERVICE

Part: RELAY — FAILED (THRUST REVERSER) · airframe 46,117 hrs · 42,069 cycles

ON T/O E2 REV DISAGREE EICAS MSG....FIX:(PHL)MELD T/R.... (SBY)REACTIVATED #2 TR IAW AMM 78-31-01-980-801. SEE HA300 SEQ 5 FOR T/S.R&RD RELAY K0398.OPS CHECK GOOD IN HANGAR. GROUND RAN AND TAXIED A/C.NO DEFECTS NOTED.NO EICAS OR CMC MESSAGES.CLEAR MEL

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 46,051 hrs · 42,000 cycles

PDIS 644 78-33 1997531 02NOV19 ROC ASSGN ENG 2 REV DISAGREE AFTER TAKE OFF EDGAR HISTORY: NONE MEL 02NOV19 16:17 ROC C30609 78-2 ENG 1 OR 2 REV DISAGREE MESSAGES

Part: THERMAL SWITCH — DEFECTIVE (BLEED AIR SYS) · airframe 45,004 hrs · 40,767 cycles

NDIS 644 36-21 0006270 05MAY19 ROA CLOSE LOG PAGE 203016 SEQ #1 "BLEED 1 LEAK EICAS WARNING". REMOVED PANEL 191EL AND 191KL TO CHECK FO BLEED AIR LEAKS FOUND TUBE ASSY WITH LLOSE CLAMP REPLACE TUBE ASSY AND TIGHTEN CLAMP RAON ENGINE AT TAKE OFF POWER FOR 1 MINUTE 29 SECONDS. MESSAGE CAME BACK "BLEED 1 LEAKS" ON EICAS WAS A NO FIX. PERFORMED FIM TASK 36-20-00-810-801-A STEPS 1, 2, 12 AND 23. R&R THERMAL SWITCH S0153 CCN: 1210022 PER AMM MOO 36-20-02/400 AND WM 36-21-50. RAN ENGINE AT TAKE OFF POWER FOR5 MINUTES NO FAIL MESSAGE ON EICAS. AIRCRAFT OK FOR SERVICE A THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,933 hrs · 40,669 cycles

NDIS 644 33-51 0005660 21APR19 SBY CLOSE PAX SIDE HINGED MAIN DOOR EMERGENCY LIGHT IS INOP 29192 00 BRA FACT 21APR19 09:24 SBY R&R'ED PAX SIDE HINGED MAIN DOOR EMERGENCY LIGHT LAM P IAW AMM 33-50-10

Part: NONE — NONE (NONE) · airframe 44,056 hrs · 39,653 cycles

PDIS 644 05-50 1925362 06NOV18 SYR CLOSE FLAP OVERSPEED NOTED 45 DEG A7 157 KTS 28482 00 RNR FACT 06NOV18 14:22 SYR FLAP OVERSPEED NOTED AND WITH-IN LIMITS OF AMM 05-50 -07, NO INSPECTION REQUIRED

Part: FRAME — CHAFED (FRM 68) · airframe 43,876 hrs · 39,456 cycles

Z-FRAME FR-68 CHAFED AT CARGO LINER NUTPLATES -C/A-REPAIRED Z-FRAME AT FR 68 IAW ERS-EM-53MR-3427

Part: SKIN — CRACKED (CARGO DOOR) · airframe 43,875 hrs · 39,455 cycles

BAGGAGE DOOR ACTUATING HANDLE CUTOUT AFT END CRACKED-C/A-PERFORMED PERMANENT REPAIR IAW ENVOY ERS-EM-52MR-795

Part: SKIN — CRACKED (FRAME 75) · airframe 43,875 hrs · 39,455 cycles

LH AFT FUSELAGE FR 75 HAS A SKIN CRACKS AT FASTENER ABOVE STRINGER 2L-C/A-PERFORMED PERMANENT REPAIR OF LH REAR FUSELAGE I SKIN AT FRAME 75 IAW SRM 53-31-01

Part: FRAME — CRACKED (FRM 73) · airframe 43,875 hrs · 39,455 cycles

FR 73 IS CRACKED BETWEEN STR 15R AND 16R-C/A-REMOVED AND REPLACED FR 73 LWR SECTION IAW EMB 145 SRM 51-40-02

Part: FRAME — CRACKED (FRM 10) · airframe 43,875 hrs · 39,455 cycles

RH FRAME 10 CRACKED JUST BELOW CO-PILOTS DV WINDOW-C/A-REMOVED AND REPLACED RH FRAME 10 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (FRAME 23) · airframe 43,875 hrs · 39,455 cycles

R/H OMEGA BEAM CORRODED AT PREVIOUS BLEND FR 23-C/A-REPAIRED R/H OMEGA BEAM CORRODED AT PREVIOUS BLEND FRAME 23 IAW EMB145 SRM 53-21-10

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,875 hrs · 34,955 cycles

LT OMEGA BEAM CORRODED AT CROSS BEAM BETWEEN FR-33 AND FR-34. REPAIRED LT OMEGA BEAM CORROSION BETWEEN FRAMES 33 AND 34 IAW SRM 53-00-10, FIGURE 202, SHEET 2.

Part: YOKE — CRACKED (RT ENGINE) · airframe 43,875 hrs · 39,455 cycles

R/H ENGINE FWD LOWER YOKE CRACKED. -C/A-REMOVED AND INSTALLED SERVICEABLE YOKE IAW EO EM-54MR-386

Part: FRAME — CRACKED (FRM 66) · airframe 43,875 hrs · 39,455 cycles

FR 66 CRACKED ON INNER RADIUS AT RH FLOOR SUPPORT-C/A-RAR FR 66 LOWER HALF IAW EMB 145 SRM 51-40-02

Part: BUSHING — MIGRATED (RT AILERON) · airframe 43,875 hrs · 39,455 cycles

RT AILERON OTBD PCA ATTACHMENT LUG OTBD HAT BUSHING MIGRATED-C/A-REMOVED AND REPLACED RH AILERON PCA FITTING IAW EO EM-27MR-112.

Part: PLACARD — DAMAGED (EMERGENCY EXIT) · airframe 43,875 hrs · 39,455 cycles

COCKPIT DOOR EMERGENCY EXIT FWD SIDE HAS VINYL DAMAGE-C/A-COMPLETE:REMOVED AND REPLACED VINYL TO COCKPIT DOOR EMERGENCY EXIT FWD SIDE IAW EMB 145 AMM 25-00-00 AND ETN EM-25-182R1.

Part: LIGHT — DAMAGED (CABIN) · airframe 43,875 hrs · 39,455 cycles

LH EMERGENCY LIGHT EXTRUSION RAMP, 1,2,3,7 AND LAV DAMAGED-C/A-COMPLETE:RAR LH EMERGENCY LIGHT EXTRUSION RAMP, 1,2,3,7 AND LAV IAW EMB145 AMM 33-50-12-04. SEE NRTC BOW300444 FOR INSTALLATION AND OPERATIONAL CHECK

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,862 hrs · 38,506 cycles

EMERGENCY LIGHT EXIT LOCATOR OVERWING FWD CEILING, INOPERATIVE IAW A PS-1 CHECK. FOUND EMERGENCY LIGHT DC/AC INVERTER NR 6 SUSPECTED TO BE BAD. R & R THE INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,716 hrs · 38,342 cycles

DURING PS-1 INSPECTION, FOUND THE MID CEILING EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-15. OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,145 hrs · 37,850 cycles

FWD EMERENCY EXIT SIGN ASSEMBLY INOPERATIVE. REMOVED AND REPLACED THE SIGN IAW AMM 33-50-15, OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 41,346 hrs · 37,066 cycles

FWD FACING EMERGENCY EXIT SIGN IN MID CABIN INOPERATIVE. REMOVED AND REPLACED AND OPS CHECKED GOOD IAW AMM 33-50-15.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,144 hrs · 36,898 cycles

MID CABIN FWD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED MID CABIN FWD EMERGENCY LIGHT ASSY IAW AMM 33-50-15. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,794 hrs · 36,591 cycles

MAIN DOOR EMERGENCY LIGHT INOP. SEE IPC 33-50-10 FIGURE 25 FOR LOCATION. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT IAW AMM 25-23-04. OPS CK GOOD.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 40,666 hrs · 36,452 cycles

CREW REPORTED FA FLASHLIGHT BROKEN. R & R THE FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: DOOR — UNSECURE (ESCAPE ROPE) · airframe 40,047 hrs · 35,887 cycles

CAPTAIN`S ESCAPE ROPE DOOR CAME OFF DURING TAKEOFF AND WILL NOT STAY SECURED. SECURED ESCAPE ROPE DOOR IAW STANDARD MAINTENANCE PROCEDURES.

Part: TRUNNION — WORN (NLG) · airframe 39,549 hrs · 35,446 cycles

RIGHT NLG TRUNION WORN BEYOND LIMITS. REMOVAL AND REPLACED THE TRUNION FITTING IAW EO EM-53MR-2242

Part: INVERTER — INOPERATIVE (CABIN) · airframe 39,544 hrs · 35,442 cycles

NR 3 EMERGENCY FLOOR LIGHT STRIP INOPERATIVE. R & R EMERGENCY LIGHT DC/AC INVERTER NR 2 IAW AMM 33-50-11. OPC GOOD.

Part: TRUNNION — CRACKED (LT MLG) · airframe 39,544 hrs · 35,442 cycles

LEFT UPPER AFT TRUNION CRACKED. REMOVED AND REPLACED THE UPPER AFT TRUNION IAW ERS-EM-57MR-680.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 39,544 hrs · 35,442 cycles

RIGHT WING LEADING EDGE LOWER ATTACH FLANGE IS CRACKED AT RIB 9. REPAIRED ATTACH FLANGE IAW ERS ERS-EM-57MR-684.

Part: TRUNNION — WORN (NLG) · airframe 39,544 hrs · 35,442 cycles

NLG DAMAGE TO THE FITTING HOUSING BEARING TRACKS. REMOVED AND REPLACED THE LT AND RT NLG TRUNION FITTINGS IAW ERS-EM-53DF-2002 PT C AND ERS-EM-53MR-2242.

Part: SPAR — CRACKED (LT WING) · airframe 39,544 hrs · 35,442 cycles

LT WING LEADING EDGE LOWER ATTACHMENT FLANGE IS CRACKED AT RIB 9. REPAIRED THE WING LEADING EDGE LOWER ATTACHMENT FLANGE IAW ERS ERS-EM-57MR-685.

Part: SWITCH — LACK OF LUBE (SERVICE DOOR) · airframe 39,490 hrs · 35,388 cycles

SERVICE DOOR INDICATION SHOWS OPEN WHEN CLOSED. DEFERRED SERVICE DOOR WARNING SYSTEM REF MEL 52-04, AUTH 070580-B. ACCOMPLISHED CLEANING AND LUBRICATION OF SERVICE DOOR MICROSWITCHES, OPS CHECK GOOD IAW AMM 52-74-00.

Part: MECHANISM — DEFECTIVE (CARGO DOOR) · airframe 39,259 hrs · 35,177 cycles

FCF CLOSING ACTION FOR TRANSFERRED FROM NRWC 644-SGF-02450. ITEM 1, BAGGAGE DOOR HARD TO OPEN, BROKEN GEAR AND SUPPORT ASSY. R & R BAGGAGE DOOR LIFTING AND LOWERING MECHANISM ASSY IAW AMM 52-32-00.

Part: SIGN — INOPERATIVE (CABIN) · airframe 39,131 hrs · 35,057 cycles

FOUND FWD FACING EMER EXIT CEILING LIGHT INOPERATIVE. R & R FWD FACING EMER EXIT CEILING LIGHT IAW AMM 33-50-15.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 37,996 hrs · 34,078 cycles

AT FL 360 CABIN ALT BEGAN TO RISE UP TO 8700 FT. ROSE UP APPROX 100 FT PER SEC. TRANSFERRED TO NRWC 644-DFW-02165. TROUBLE SHOT IAW FIM 21-31-00. R & R ELECTRO PNEUMATIC OUT FLOW CONTROL VLV IAW MM CH 21-31-03. COMPLIED WITH FUNCTIONAL TEST. ALL CHECKS GOOD, LEAK CHECKED GOOD, WITHIN RATE. REF NRWC 664-DFW 02165 FOR OTHER WORK PERFORMED. DAMAGED FITTING FOUND ON OUT FLOW VLV.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 37,794 hrs · 33,865 cycles

ON DEPARTURE, EXPERIENCED AN AUTO PRESSURIZATION FAILURE. PERFORMED AOM 1 PROCEDURE & SWITCH TO MANUAL MODE. MANUAL MODE REQUIRED EXCESSIVE MOVEMENT & WAS DIFFICULT TO CONTROL. PERFORMED AOM 1 PROCEDURE FOR MANUAL CONTROL FAILURE. PERFORMED GVI OF LINES AT BOTH OUTFLOW LINES & AT PCA FLAPPER. OPERATIONS CHECKED GOOD WITH NO EICAS OR CMC MSGS IN BOTH AUTO & MANUAL MODES IAW AMM 21-31-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,333 hrs · 33,421 cycles

RIGHT EXTERNAL OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RIGHT EXTERNAL OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: PRESSURE SWITCH — FAILED (LT ACM) · airframe 36,647 hrs · 32,864 cycles

CLIMBING OUT THRU 25,000, RECEIVED A, NR 1 PACK OVERLOAD MESSAGE, WITH A STRONG BURNED ODOR. RESET IAW CHECKLIST & WAS OK FOR REMAINDER OF FLIGHT. R & R PACK 1 OVER PRESSURE SWITCH IAW AMM 21-51-06. OPS CHECKED OK.

Part: BATTERY PACK — UNSECURE (CABIN) · airframe 36,149 hrs · 32,445 cycles

EMERGENCY LIGHT IN COCKPIT & LT EXTERNAL WING INOPERATIVE. FOUND BATTERY PACK NR 1 UNSECURED. REINSTALLED IAW AMM 33-50-04. OPERATIONS CHECKED GOOD OF ALL EMER LIGHTS IAW AMM 33-50-00.

Part: SEAL — FAILED (WINDOW) · airframe 35,151 hrs · 31,474 cycles

ON INITIAL CLIMB THROUGH 200 AN EXTREMELY LOUD AIR SQUEAL STARTED ON POST FLIGHT. THE FIRST OFFICERS DV WINDOW SEAL WAS FOUND OUTSIDE THE WINDOW FAILED. REPAIRED FIRST OFFICERS DV WINDOW IAW 56-112-02. OPERATIONS CHECK & LEAK CHECKED GOOD. NO LEAKS NOTED.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 35,151 hrs · 31,474 cycles

UNABLE TO TUNE ILS OR GS ON NAV 1 RED X ON PFD X ON BOTH DISSAPPERAD WITHIN 8.0 NM OF RUNWAY. NO FAULT FOUND PERFORMED OPERATIONS CHECK OF VOR, ILS & GS IAW AMM 34-32-00. OPERATIONS CHECKED GOOD COULD NOT DUPLICATE PROBLEM AT THIS TIME.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,921 hrs · 31,269 cycles

DURING HMBV INSPECTION, QA FOUND TWO CRACKED FASTENER HOLES ON FRAME 75 BETWEEN STRINGERS 2R & 3R. ACFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. PERFORMED PERMANENT REPAIR ON TWO CRACKED FASTENER HOLES ON FRAME 75 BETWEEN STRINGERS 2R & 3R IAW ERS-EM-53MR-523.

Part: PLATE — CORRODED (FUSELAGE) · airframe 34,921 hrs · 31,269 cycles

DURING HMBV INSPECTION, QC FOUND CORROSION BETWEEN FRAME 13 - 14, STRINGER 19L - 19R. ACFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. CUT OUT DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW ERS-EM-53MR-539.

Part: REPAIR — CHAFED (FUSELAGE) · airframe 34,921 hrs · 31,269 cycles

DURING HMBV INSPECTION, QA FOUND A CHAFE ON A PREVIOUS REPAIR TO FRAME 19 BETWEEN STRINGERS 3R & 4R. ACFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. R & R PREVIOUS REPAIR ON FRAME 19 BETWEEN STRINGERS 3R & 4R IAW ERS-EM-53MR-526.

Part: DECK PLATE — CRACKED (NLG WW) · airframe 34,921 hrs · 31,269 cycles

DURING HMBV INSPECTION, QA FOUND A CRACK ON NLG BAY UPPER DECK AT UPLOCK BOX SUPPORT RT SIDE AFT OF BRACE. ACFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. INSTALLED FILLER & DOUBLER REPAIR ON NLG BAY UPPER DECK IAW ERS-EM-53MR-509. REPAIR FILLER & DOUBLER MATERIAL 2024T3 040. ACFT WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION.

Part: SUPPORT ANGLE — CRACKED (CARGO DOOR) · airframe 34,921 hrs · 31,269 cycles

CARGO DOOR RAMP SUPPORT ANGLE IS CRACKED AT FRAME 65. R & R CARGO DOOR RAMP SUPPORT ANGLE AT FRAME 66 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,921 hrs · 31,269 cycles

GALLEY FWD DIGITAL HAS CORROSION. REPAIRED GALLEY FWD DIGITAL IAW ERS-EM-5300-512.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 34,921 hrs · 31,269 cycles

CENTER AISLE CROSSBEAM AT FRAME 20 HAS CORROSION. R & R CTR AISLE CROSSBEAM AT FRAME 20 IAW ETN-EM-53-139R3 & SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,921 hrs · 31,269 cycles

LEFT OMEGA BEAM HAS CORROSION FWD & UNDER CROSSBEAM AT FRAME 29. PERFORMED REPAIR ON LT OMEGA BEAM UNDER CROSSBEAM AT FRAME 29 IAW SRM 53-00-10 ITEM 3.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 34,921 hrs · 31,269 cycles

COPILOTS RT FLOOR SUPPORT FWD CROSSBEAM CORRODED. BLENDED TO REMOVE CORROSION FROM MARKED AREAS ON COPILOTS RT FLOOR SUPPORT FWD CROSSBEAM IAW SRM 51-10-03. ACCEPTED AS IS IAW ERS-EM-5300-522. SEE WIPS & TASK FOR DETAILS.

Part: WIRE — SHORT (EXTERIOR LIGHT) · airframe 34,921 hrs · 31,269 cycles

SERVICE DOOR EXTERIOR EMER LIGHT WIRE CONNECTOR P7198 TO SHORT FOR CONNECTION. EXTENDED WIRES ON CONNECTOR P7198 FOR SERVICE DOOR EXTERIOR EMER LIGHT IAW SWPM 20-21-00. SEE NRTC BOW 157123 FOR OPERATIONS CHECK. SEE TASK & WIP ENTRIES FOR DETAILS.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 34,921 hrs · 31,269 cycles

PILOTS RT SEAT TRACK SUPPORT CORRODED ADJACENT TO CONTROL COLUMN. BLENDED TO REMOVE CORROSION FROM MARKED AREAS ON PILOTS RT SEAT TRACK SUPPORT ADJACENT TO CONTROL COLUMN IAW SRM 51-10-03. PILOTS RT SEAT TRACK SUPPORT CORROSION ADJACENT TO CONTROL COLUMN ACCEPTED AS IS IAW ERS-EM-5300-521. SEE WIPS & TASKS FOR DETAILS.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 34,921 hrs · 31,269 cycles

COPILOTS RT SEAT TRACK SUPPORT CORRODED ADJACENT TO CONTROL COLUMN. BLENDED TO REMOVE CORROSION FROM MARKED AREAS ON COPILOTS RT SEAT TRACK SUPPORT ADJACENT TO CONTROL COLUMN IAW SRM 51-10-03. COPILOTS RT SEAT TRACK SUPPORT CORROSION ADJACENT TO CONTROL COLUMN MARKED ACCEPTED AS IS IAW ERS-EM-5300-518. SEE WIPS & TASKS FOR DETAILS.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 34,921 hrs · 31,269 cycles

EMERGENCY LIGHT NORMAL ON BUTTON ON FLIGHT ATTENDANT CONTROL PANEL INOPERATIVE. SECURED CONNECTOR ON FLIGHT ATTENDANT CONTROL PANEL IAW AMM 25-27-09. OPERATIONS CHECKED GOOD.

Part: PIN — BROKEN (FLASHLIGHT) · airframe 34,921 hrs · 31,269 cycles

PIN BROKEN OFF WIRE FOR AFT CABIN RT BULKHEAD FLASHLIGHT REMOVABLE SPLICE. R & R PIN & REMOVABLE SPLICE FOR AFT CABIN RT BULKHEAD FLASHLIGHT IAW SWPM 20-00-03 & WM 91-10-02. OPERATIONS CHECKED GOOD.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 34,921 hrs · 31,269 cycles

RT FLOORBEAM INBD SUPPORT IS CRACKED BETWEEN FRAMES 47 - 48. PREVIOUSLY MARKED AS CRACKED. REMOVED & INSTALLED SERVICEABLE RT FLOORBEAM INBD SUPPORT BETWEEN FRAMES 47 - 48 IAW SRM 53-32-02.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 34,731 hrs · 31,072 cycles

AIRCRAFT WOULD NOT PRESSURIZE ON TAKEOFF. RETURNED FOR EMERGENCY LANDING. CABIN ALTITUDE REMAINED WITH AMBIENT RETURNED FOR LANDING AT 6000' ALTITUDE. ACCOMPLISHED PRESSURIZATION FUNCTIONAL TEST OF AUTOMATIC & MANUAL MODE IAW AMM 21-31-00, FOUND NO DISCREPANCIES AT THIS TIME, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,578 hrs · 30,935 cycles

CEILING EMERGENCY LAMP AT ROW 7 INOPERATIVE. R & R AISLE EMERGENCY LIGHT LAMP AT ROW 7 IAW AMM 33-50-08-000-801-A & 33-50-08-400-801-A, OPERATIONS CHECKED GOOD.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 34,119 hrs · 30,555 cycles

FIRST OFFICER`S FLASHLIGHT CRADLE CRACKED. R & R FIRST OFFICER`S FLASHLIGHT BRACKET IAW MM 25-60-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,126 hrs · 30,561 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (LOCALIZER) · airframe 34,078 hrs · 30,513 cycles

ON FLIGHT 3266 DURING APPROACH CREW REPORTED LOST BOTH LOCALIZER SIGNALS & BOTH GPS SIGNALS FOR LATERAL GUIDANCE. THE ACFT WAS REMOVED FROM SERVICE. BOTH NR 1 AND NR 2 LOCALIZERS OPERATIONAL CHECK GOOD IAW EMB145 AMMK 34-32-00.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,483 hrs · 30,057 cycles

EMERGENCY LIGHT AT ROW 1 AND SERVICE DOOR LOWER RT EXIT SIGN FAILED TO ILLUMINATE. R & R NR 2 EMERGENCY LIGHTING INVERTER IAW AMM 33-50-11. OPS GOOD AT THIS TIME.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,353 hrs · 29,951 cycles

EMERGENCY LIGHT SEGMENTS 6,7 AND 8 INOPERATIVE. R & R NR 6 INVERTER ASSY IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (FLASHLIGHT) · airframe 31,964 hrs · 28,860 cycles

FLIGHT 4256. AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. RELAMPED FLASHLIGHT IAW CMM 25-60-11. OPS CHECKED GOOD IAW AMM 33-51-01. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 31,845 hrs · 28,760 cycles

ON FLIGHT 3924 THE CREW REPORTED THAT ON DESCENDING FROM 370 TO 350 THE CABIN ALTTITUDE STARTED INCREASING THRU 8500. THE CREW RAN CAB ALT AMBER AOM AND AT THE SAME TIME CABIN ALT CLIMBED THRU 10.5 THE CREW RAN RAPID DECOMPRESSION CHECK LIST. DEC. DWN TO 8000 RAN CAB ALT AMBER AGAIN, AT THAT POINT THEY NOTICED AUTO PRESS AT 14000. THEY RESET TO 700 AND CABIN PRESS VERY SLOWLY CAME BACK DOWN. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DIGITAL CONTROLLER IAW 21-31-01. THE OPERATIONAL CHECK WAS GOOD IAW 21-31-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

FORWARD FLOOR EMERGENCY LIGHT INOP. REPLACED LIGHT STRIP.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 31,077 hrs · 28,155 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLIGHT ATTENDANT’S FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED SERVICEABLE FLASHLIGHT HOLDER. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — UNSERVICEABLE (COCKPIT) · airframe 30,873 hrs · 27,990 cycles

ON FLIGHT 2914 THE CREW REPORTED THE CAPTAIN'S FLASHLIGHT WAS LOOSE IN THE BRACKET. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN'S FLASHLIGHT BASE AND FLASHLIGHT IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CHAFED (FUSELAGE) · airframe 30,536 hrs · 27,738 cycles

DURING INSPECTION QC DISCOVERED A CHAFE ON FRAME 65 BETWEEN STRINGERS 12R AND 13R. THE AIRCRAFT WAS REMOVED FROM SERVICE. DOUBLER INSTALLED IAW EO EM-53MR-2020. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,537 hrs · 27,739 cycles

DURING MAINTENANCE INSPECTION FOUND THE FOLLOWING EMERGENCY LIGHTS FAILED THE EMERGENCY LIGHTING SYSTEM OPERATIONAL TEST: COCKPIT FLOOD LIGHT, AISLE LIGHT NR 1 AND THE LEFT WING FUSELAGE FRONT FAIRING EXTERNAL LIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY & POWER SUPPLY CHARGER NR 1 IAW EMB 145 AMM 33-50-04. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,376 hrs · 27,615 cycles

DURING MAINTENANCE INSPECTION, FOUND 12C OVERHEAD EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. RELAMPED. NO FURTHER DEFECTS, FOUND OPS CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 29,755 hrs · 27,182 cycles

ON FLIGHT 3549, AFTER CLIMB OUT, CREW REPORTED THEY RECEIVED HYD 1 LOW QUANTITY MESSAGE AND THEN RECEIVED AN E1 HYD PUMP FAIL MESSAGE. THE CREW DECLARED AN EMERGECNY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ENGINE NR 1 HYD PUMP AND PRESSURE HOSE IAW AMM 29-10-03. OPS CHECKED GOOD. NO LEAKS FOUND. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,663 hrs · 27,122 cycles

DURING B INSPECTION FOUND THE RIGHT OVERWING AFT EMERGENCY EXIT LAMP INOPERABLE AND FOUND THE FORWARD SIDE OVERWING OVERHEAD EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING AFT EMERGENCY EXIT LAMP IAW EMB 145 AMM 33-50-07 AND REMOVED AND REPLACED THE INTERIOR FORWARD SIDE OVERWING OVERHEAD EMERGENCY EXIT SIGN IAW EMB 145 AMM 33-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 29,651 hrs · 27,107 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT EXIT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED LAMP OF RIGHT EXIT OVERWING EMERGENCY LIGHT IAW EMB AMM 33-50-10. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — UNSERVICEABLE (COCKPIT) · airframe 29,528 hrs · 27,011 cycles

ON FLIGHT 2914 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT CHARGING INDICATOR WAS MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S EMERGENCY FLASHLIGHT IAW EMB-145 MM 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,510 hrs · 26,991 cycles

DURING B-INSPECTION FOUND THE EMERGENCY EXIT LIGHT AT CEILING CENTER FUSELAGE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT PER AMM 33-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 29,472 hrs · 26,958 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT EXIT ROW EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 INVERTER IAW EMB 145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PUMP — FAILED (NR 1 ENGINE) · airframe 4,127 hrs · 26,695 cycles

ON FLIGHT 4127 THE CREW REPORTED THAT WHILE EN ROUTE TO YUL RECEIVED AN E1 HYDRAULIC PUMP FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND HYDRAULIC LEAK ON EDP 1 FLANGE. REPLACED HYDRAULIC 1 EDP IAW EMB 145 AMM 29-10-03. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME AND NO LEAK NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (COCKPIT) · airframe 28,931 hrs · 26,562 cycles

ON FLIGHT 4076 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT CRADLE WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT AND BASE IAW EMB-145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,911 hrs · 26,549 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT OVERWING LOWER EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING LOWER EMERGENCY LIGHT IAW EMB145 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (CABIN PRESSURE) · airframe 28,856 hrs · 26,516 cycles

ON FLIGHT 3509 THE CREW REPORTED THAT ON THE CLIMB THROUGH AT 10000 FEET THEY RECEIVED "CABIN" AURAL WARNING AND RED CABIN ALTITUDE INDICATION ON EICAS. RECEIVED NORMAL INDICATIONS WHILE DESCENDING. THE CREW DECLARED AN EMERGENCY AND LANDED WTHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. OPERATIONALLY CHECKED PRESSURIZATION CONTROL SYSTEM IN MANUAL AND AUTOMATIC MODE IAW EMB 145 AMM 21-31-00. UNABLE TO DUPLICATE CONDITIONS AIRCRAFT OK TO RETURN TO SERVICE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,759 hrs · 26,442 cycles

DURING MAINTENANCE BASE CHECK FOUND LEFT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT OVERWING EMERGENCY LIGHT REF EMB 145 AMM TASK 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,872 hrs · 25,787 cycles

ON FLIGHT 4287 THE CREW REPORTED THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SOCKET — OUT OF POSITION (CABIN) · airframe 27,679 hrs · 25,645 cycles

ON FLIGHT 3560 THE CREW REPORTED AN ODOR OF ELECTRICAL BURNING AND LIGHT SMOKE OBSERVED NEAR SEATS 4 B & C AND THE AFT GALLEY AREA. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPOSITIONED LATERAL LIGHT SOCKET AT ROW 4A-B/C. THE OPERATIONAL TEST CHECK WAS GOOD IAW EMB 145 AMM 20-13-02. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FCU — MALFUNCTIONED (TE FLAP) · airframe 27,352 hrs · 25,387 cycles

ON FLIGHT 3990 DURING THE DESCENT THE CREW REPORTED, RECEIVED A FLAP FAIL AND SPS ADVANCE MESSAGES. THE CREW RAN THE APPROPRIATE CHECKLIST. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLAP ELECTRICAL CONTROL UNIT IAW EMB-145 AMM 27-53-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 26,346 hrs · 24,631 cycles

ON FLIGHT 3314 ON APPROACH TO DFW THE CREW REPORTED, RECEIVED A CARGO SMOKE WARNING ON EICAS. THE CREW FOLLOWED AOM PROCEDURES AND USED FIRE BOTTLES. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT AND TAXIED TO RAMP. NO FIRE OR SMOKE NOTED IN CARGO BAY AFTER INSPECTION ON THE GROUND. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CARGO SMOKE DETECTORS IAW EMB 145 AMM 26-15-01. THE OPERATIONAL CHECK WAS GOOD. REMOVED AND REPLACED THE AFT CARGO SMOKE DETECTORS IAW EMB 145 AMM 26-15-01. THE OPERATIONAL CHECK WAS GOOD. REMOVED AND REPLACED THE CARGO FIRE BOTTLES IAW EMB 145 AMM 26-23-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 25,455 hrs · 23,984 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT OVERWING ESCAPE HATCH EMERGENCY ESCAPE IDENTIFIER SIGN TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EMERGENCY HATCH EXIT SIGN IDENTIFIER. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,104 hrs · 22,108 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THAT THE FORWARD EMERGENCY LIGHTS WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 POWER SUPPLY, BATTERY IAW 33-700-19 AND INVERTER IAW EMBRAER 145 AMM 33-50-11. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 23,104 hrs · 22,108 cycles

WHILE AT SYR THE AIRCRAFT WAS HIT BY A BELT LOADER NEAR THE CARGO DOOR. THE GASH WAS APPROXIMATELY 8 INCHES LONG LOCATED AT THE REAR FUSELAGE BETWEEN FRAMES 65 AND 67, BETWEEN STRINGERS 17L AND 21L. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE AIRCRAFT WAS FERRIED TO MQT FOR REPAIRS. THE DAMAGE WAS REPAIRED WITH DOUBLER IAW AEAI EO-EM-53MR-1436. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — ODOR (RECIRCULATION) · airframe 19,463 hrs · 18,791 cycles

ON FLIGHT 4409, CREW REPORTED WHILE CRUISING FL 270 A VERY STRONG ELECTRIC ODOR EMANATED FROM THE VENTS SUPPLIED PACK 1 IN CABIN. AIRCRAFT REMOVED FROM SERVICE. FOUND SOURCE OF ODOR TO BE FAILED LEFT RECIRCULATION FAN. REMOVED AND REPLACED LEFT RECIRCULATION FAN IAW EMB-145 AMM 21-24-01; OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RELAY — FAILED · airframe 19,061 hrs · 18,394 cycles

ON FLIGHT 3957, CREW REPORTED DURING TAKEOFF AFTER ROTATION RECEIVED L/G AIR GRND FAIL AMBER EICAS MESSAGE. GEAR HANDLE WOULD NOT MOVE ONCE TRIM WENT OUT OF TAKEOFF RANGE. BEGAN RECEIVING TAKEOFF TRIM AND TAKEOFF FLAPS AURAL WARNING AFTER APPROX 4 MINUTES THE LG AIR GRND FAIL WENT AWAY ALONG WITH AURAL WARNING LEFT GEAR DOWN AND RETURNED TO ORD WITHOUT INCIDENT. CMC MSG LGEU FAIL. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RELAY. PERFORMED RETRACTION TEST OF LANDING GEAR. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,826 hrs · 17,219 cycles

NOTIFIED BY THE CREW VIA TELESIS. FORWARD EMERGENCY EXIT SIGN ACROSS FROM GALLEY INOP AND EMERGENCY EXIT LIGHT IN COCKPIT STEP INOP. REMOVED AND REPLACED BATTERY PACK AT POS NR 1 IAW AMM 33-50-04. OPS CK GOOD AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,834 hrs · 15,421 cycles

LEFT OMEGA BEAM AT FRAME 20 FOUND TO BE CORRODED. REMOVED PREVIOUS REPAIR, FABRICATED DOUBLER AND FILLER. INSTALLED AND RESTORED SURFACE PROTECTION IAW EMB SRM 53-10-00 AND 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 15,834 hrs · 15,421 cycles

MAIN PASSENGER DOOR INTERIOR HANDLE ACTUATION BRACKET CRACKED. STOP DRILLED AND FABRICATED DOUBLER, INSTALLED IAW EMB IC2006-145/9020. RETURNED AIRCRAFT TO SERVICE.

Part: TRANSDUCER — FAILED (WHEEL SPEED)

RECEIVED AMBER SPOILER FAIL MESSAGE ON EICAS DURING TAKEOFF ROLL, EICAS = SPOILERS OPEN, HANDLE = CLOSE. RAI NR 3 WHEEL SPEED TRANSDUCER IAW EMB 145 AMM 32-41-03, OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (FUSELAGE)

FWD AND AFT EMERGENCY FLOOR LIGHT STRIPS INOPERATIVE. REPLACED AFT BATTERY PACK WITH OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE PREVIOUS REPAIR. FABRICATED AN EXTERNAL ANGLE, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28 CHAPTER 53-21-10. (M)

Part: PDU — INOPERATIVE (TE FLAPS)

DURING CRUISE FLIGHT CREW REPORTED A FLAP FAIL MESSAGE ON EICAS. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE FLAP POWER DRIVE UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION, THE FORWARD DIGITAL WAS FOUND CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND TREATED THE BARE METAL SURFACE. FABRICATED A REPAIR DOUBLER AND INSTALLED. REPAIR DONE IAW EMB STATMENT IC2003-145/1604, PARA 12. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 24 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT A 1.1250 BY 1.5625 SECTION OF DAMAGE OMEGA BEAM. FABRICATED ONE FILLER, EXTERNAL ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 21, CHAPTER 53-21-10 FIG 202. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SILL AND INSTALLED SERVICEABLE SILL IAW EMB-1459 SRM 145/1142, REV 21, 51-20-01/03, 51-40-02/04/06 EMB CPM (CPM-145/1132 REV 8) 51-21-04, 51-21-05, 51-21-06 AND STANDARD SRM PRACTICES. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE SHEAR TIE AT FRAME 68 AND THE CARGO DOOR CUTOUT WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORROSION BY PERFORMING AN CUT OUT OF THE LOWER PORTION OF THE SHEAR TIE. FABRICATED A REPLACEMENT SPLICE. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/1615 AND STANDARD EMB SRM, SRM 145/1142 REV 21, PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19L BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS NOTED. FABRICATED A REPAIR ANGLE, AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 21, CHAPTERS 53-24-02 FIGURE 201. (M)

Part: STRINGER — CHAFED (FUSELAGE)

DURING AN IMBV INSPECTION, STRINGER 19R BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS NOTED. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 21, CHAPTERS 53-24-02 FIGURE 201. (M)

Part: ELEMENT — FAILED (COCKPIT)

DURING CLIMB CREW REPORTED A SMOKE SMELL IN THE AIRCRAFT. CREW ELECTED TO RETURN TO ORD AND LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND THE CAUSE OF THE SMELL TO BE FROM THE CAPTAINS WINDSHIELD HEATING ELEMENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD HEATING ELEMENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION, FOUND GALLEY CENTER BEAM AT FRAME 20 CORRODED. REMOVED CORROSION ON GALLEY CENTER BEAM AT FRAME 20 AND REPAIRED IAW EMB 145 SRM AND REPAIR STATEMENT GST 2977/01. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION FROM LEFT OMEGA BEAM AT FRAME 20 AND REPAIRED IAW EMB 145 SRM. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

HRL - FLT 3724 - ON CLIMB-OUT, CREW NOTED SPARKS CAME FROM FIRST OFFICERS WINDSHIELD SIDE AREA THEY THEN TURNED WINDSHIELD HEAT OFF. AT THAT TIME THE WINDSHIELD CRACKED ALL OVER, SO THE CREW COMPLETED A EMERGENCY LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: RELAY — INOPERATIVE (THRUST REVERSER)

ORD - FLT 4255 - DURING TAKEOFF, CREW NOTED THRUST REVERSER 1 FAIL. TAKEOFF ABORTED AND AIRCRAFT WAS RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED RELAY K0352. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SWITCH — INOPERATIVE (NR 1 ENGINE)

NR 1 ENGINE OIL PRESSURE HIGH CREW ABORTED TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE OIL PRESSURE SWITCH IAW EMB MM. OPERATIONAL AND LEAK CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 481 hrs · 539 cycles

ORD - FLT 4039 - FIRST ONE-THIRD OF EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY PACK. OPS CHECK GOOD. (M)