N652RS

Part: WIRE — BROKEN (ZONE 200) · airframe 53,394 hrs · 50,726 cycles

FOUND BROKEN WIRE AT ROW 9 IN FLOOR PROXIMITY EMERGENCY SWITCH . REPAIRED BROKEN WIRE AT FLOOR PROXIMITY STRIP IN REF TO SWPM 20-21-00. OP CK GOOD. OK FOR SERVICE.

Part: GLIDE SLOPE — UNKNOWN · airframe 53,229 hrs · 50,537 cycles

RECIEVED FULL DEFLECTION OF 1.5 ON BOTH SIDE OF GLIDESLOPE IN EWN, DIVERTED TO ILM DEFLECTION HAPPENED 700 FT, AND RA WAS INTERMITTANT GOING INTO EWN. CAPTAIN DIVERTED TO ILM. PERFORMED OPS CHECK OF VOR & ILS SYSTEM IAW AMM 34-32-00-700-801-A. REF T30D TEST PROCEDURE FOR T30D TEST BOX, OPS CHECKED GOOD. GLIDE SLOPE AND LOC BEHAVE WITHIN EXPECTED PARAMETERS. OK FOR SERVICE.

Part: FAN — ODOR (ZONE 200) · airframe 52,566 hrs · 49,782 cycles

ELECTRICAL BURNING SMELL COMING FROM GASPER VENT. FACT 16JUN25 09:53 ROA DETERMINED GASPER FAN TO BE CREATING BURNING SMELL. R/R GASPER FAN IAW AMM 21-23-03-00/400-801-A. OPS CHECK GOOD. NO BURNING SMELL AT THIS TIME

Part: DAU — FAULTED (ZONE 200)

AT FL220 CABIN PRESSURIZATION INDICATIONS ALL WENT DASHED. AIRCRAFT DID NOT RAPIDLY DECOMPRESS. DESCENDED TO 10000 AND DECLAIRED AN EMERGENCY. FACT 06JUN25 04:40 ROA R&R DAU 2 DUE TO POSSIBLE SKYDROL CONTAMINATION IAW AMM 31-41-01

Part: FAN — OBSTRUCTED (ZONE 200) · airframe 52,094 hrs · 49,241 cycles

SMOKE AND BURNING SMELL IN FLIGHT DECK SITTING AT GATE. HEARD FANS FOR FWD AVIONICS BAY KICK ON. FACT 27MAR25 16:13 CLT UPON INSPECTION FOUND INSULATION CAUGHT IN LH FWD FAN. REMOVED INSULATION. FAN OPERATES AS INTENDED. NO FURTHER DEFECTS OR FUMES NOTED AT THIS TIME. A/C OK FOR SERVICE

Part: WARNING MESSAGE — ILLUMINATED (NR 1 THRUST REV) · airframe 51,595 hrs · 48,689 cycles

E1 REV DISAGREE ON DURING TAKEOFF AROUND 80KTS DEACTIVED NO.1 TR IAW AMM 78-31-01 MEL 22DEC24 15:00 MDT C35721 78-2 ENG 1 OR 2 REV DISAGREE MESSAGES. FACT 01JAN25 09:50 SBY RE-RIGGED IAW W/C 78-70-06. . OC FOR SERVICE. CLOSE MEL 78-2.

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSERS) · airframe 51,595 hrs · 48,689 cycles

E1 REV DISAGREE ON DURING TAKEOFF AROUND 80KTS. DEACTIVED NO.1 TR IAW AMM 78-31-01 MEL 22DEC24 15:00 MDT C35721 78-2 ENG 1 OR 2 REV DISAGREE MESSAGES

Part: DAU — FAULTED (THRUST REVERSERS) · airframe 51,525 hrs · 48,605 cycles

E1 REV DISAGREE ON TAKEOFF ROLL BETWEEN 70 AN 90 KIAS. MEL 09DEC24 17:29 BGR C34420 78-2 ENG 1 OR 2 REV DISAGREE MESSAGES ROA DEINHIBITED #100 ICU AND #100 T/R. OPERATED T/R'S SEVERAL TIMES CND FAULT. T/R ICU FAIL ON CMC, T/S IAW FIM 78-30-00-810-802. R/R'D DAU2 AS PERCAUTION IAW MM 31-41-01-04, OPS CK GOOD CLEAR MEL.

Part: DAU — FAULTED (NR 2) · airframe 50,934 hrs · 47,963 cycles

DAU 2A FAIL EICAS MESSAGE DURING CLIMBOUT, INDICATIONS INTERMITTENT WITH REVERSION ON AND OFF. R & R DAU NR 2 IRT AMM 31-41-01, OPS CHK GOOD. OK FOR SERVICE AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (DAU 2A)

DAU 2A FAIL EICAS MESSAGE DURING CLIMB OUT, INDICATIONS INTERMITTENT WITH REVERSION ON & OFF.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT BRAKE TEMP) · airframe 50,330 hrs · 47,256 cycles

BRAKE DEGRADED EICAS MESSAGE, LH IB BRAKE NO TEMP RISE AND LACK OF BRAKING FACT 30APR24 16:25 LYH CYCLED CBS A7, A27, E16, AND E19. VERIFIED BRAKING OPERATIONS. PERFORMED TAXI CHECK WITH CREW. NO DEFECTS NOTED. A/C OK FOR SERVICE.

Part: ANTI-ICE VALVE — FAILED (NR 2) · airframe 50,106 hrs · 47,006 cycles

WING ANTI ICE FAILED IN ICING DURING CLIMB OUT. FOUND WING2 LOW PRESS MESSAGE ON CMC.C/W STEPS 1-4 OF FIM TASK30-11-00-810-811A AND VERIFIED PRESSURES AT PICOLLO DROP & MANIFOLD WERE GOOD, NO HISTORY. R&R #2 WING A/I VALVE PER AM/M 30-11-01.//GRND RAN A/C PERFORMED A/I TEST OPS & LEAK CHECK GOOD AT THIS TIME.

Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 50,046 hrs · 46,945 cycles

AT 27K FT ENCOUNTERED ICING OBSERVED BLEED VALVE 2 FAIL, OBSERVED 3K FT PER MINUTE IN RATE OF CLIMB. WING ANTI ICE MESSAGE ICE CONDITION ANTI ICE WARNING. RAN QRH FOR A/I INOP QRH FOR WING A/I FAIL LNDED 44,100 LBS 25O FT PER MIN WAS RUNNING LOW FUEL DFRL 08MAR24 01:19 DAY REMOVED AND REPLACED #2 ENGINE PRESSURE TRANSDUCER IAW AMM 30-21-06-000-801-A AND 30-21-06-400-801-A. SHORT SIGN FACT 09MAR24 08:56 DAY PERFORMED RUN UP WITH CREW IAW AMM 30 21 00 700 803A 500 AND 30 00 00 700 802 A. OPS CHECK GOOD. OK FOR SERVICE

Part: VALVE — SURGES (THRUST REVERSERS) · airframe 50,025 hrs · 46,921 cycles

ON TAKE OFF ROLL, ENG 1 REV DISAGREE MSG. ABORTED TAKEOFF. FACT 02MAR24 01:38 RIC FOUND EVIDENCE OF SMALL LEAK ON #100 ICU. RAN OPS CHECK FOUND VALVE SURGING WHILE DEPLOYING T/R'S. REMOVED AND REPLACED #100 ICU IN REFERENCE TO AMM 78-33-01-000/400-801-A OPS CHECK GOOD NO REV DISAGREE OR CMC MESSAGES. LEAK CHECK GOOD OK FOR SERVICE

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSERS)

IRREGULARITY, DURING T/O ROLL E1 REV DISAGREE MESSAGE, ABORTED T/O AT ABOUT 70 KTS. CREW PERFORMED TR ACUATION CHECK WITH NO DEFECTS NOTED. IRREGULARITY CLEARED USING NORMAL CREW PROCEDURES.

Part: COMPUTER — FAULTED (NR 2) · airframe 50,019 hrs · 46,915 cycles

BLEED 2 VALVE FAIL DURING ICING DISPLAYED ON EICAS. R/R INTEGRATED COMPUTER IC600 NO. 2 IAW AMM 31-42-01 OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: FLOOR SUPPORT — CRACKED (FRMS 28-29) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2371 CTR OMEGA BEAM #2 HAS CORROSION ON LH FLANGE BTW FR28-29. REPAIRED IAW EO 1-53-24-0097

Part: SHEAR TIE — CRACKED (FRM 48 S13-14L) · airframe 50,017 hrs · 46,913 cycles

53-2365 SHEAR CLIP CRACKED AT FR48 BTW STR13L-14L. R&R'D IAW SRM51-40-02

Part: NACELLE — NONE · airframe 50,017 hrs · 46,913 cycles

UNDOCUMENTED REPAIR ON LH NACELLE UPPER COWLING. R&R'D REAIR IAW EO1-05-24-0050

Part: NACELLE — NONE (RT) · airframe 50,017 hrs · 46,913 cycles

71-2255 UNRECORDED REPAIR ON RH NACELLE UPPER COWLING AFT OF XN1046.5 NEAR IB EDGE. R&R'D REPAIR IAW EO1-05-24-0050

Part: ATTACH FITTING — CRACKED (LT AILERON PCA) · airframe 50,017 hrs · 46,913 cycles

27-2185 SUSPECT CRACK IN LH AILERON PCA ATTACH FITTING. R&R'D FITTING IAW SRM 51-40-02.

Part: FRAME — CRACKED (FRM 25 S15-16R) · airframe 50,017 hrs · 46,913 cycles

53-2197 FR 25 CRACKED BTW STR15R-16R. REPAIRED IAW EO 1-53-24-0057

Part: FLOOR SUPPORT — CORRODED (FRMS 18-20) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2212 LH OMEGA BEAM IB SIDE CORRODED AT EXISTING REPAIR OF FR18-20. REPAIRED IAW EO1-53-24-0062

Part: SHEAR TIE — CRACKED (FRM 73- S9-10L) · airframe 50,017 hrs · 46,913 cycles

53-2163 SHEAR CLIP CRACKED AT FR73 BTW STR9L-10L. R&R'D IAW SRM 51-40-02

Part: SUPPORT — CORRODED (FRMS 19-34) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2167 UNDERFLOOR, CTR OMEGA BEAM BTW FR19-34 CORRODED. R&R'D IAW SRM51-40-02

Part: STRUCTURE — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2164 CORROSSION ON CARGO DOOR CUTOUT AT L SHAPE OF LWR EDGE. REPAIRED IAW EO1-53-24-0054

Part: SHEAR TIE — CRACKED (FRMS 62 S6-7R) · airframe 50,017 hrs · 46,913 cycles

53-2162 SHEAR CLIP CRACKED AT FR62 BTW STR6R-7R. R&R'D IAW SRM51-40-02

Part: SUPPORT — CORRODED (UNKNOWN) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2143 LH SILL #3 CORRODED. R&R'D IAW SRM51-40-02

Part: PANEL — CRACKED (FRM 47-48) · airframe 50,017 hrs · 46,913 cycles

57-2137 LH OVERWING PANEL CRACKED AT LWR FLANGE BTW FR47-48. R&R'D IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2102 UNDERFLOOR, AFT DIGITAL CORRODED. R&R'D IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (FRM 25 S16-17R) · airframe 50,017 hrs · 46,913 cycles

53-2117 SHEAR CLIP CRACKED AT FR25 BTW STR16R-17R. R&R'D IAW SRM 51-40-02

Part: BEAM — CRACKED (FRM 33) · airframe 50,017 hrs · 46,913 cycles

53-2124 CTR OGA BEAM CRACKED AT FR33. REPAIRED IAW EO 1-53-24-0060

Part: SUPPORT — CORRODED (UNKNOWN) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2089 RH SILL #3 CORRODED. R&R'D SILL IAW SRM 51-40-02

Part: FLANGE — CORRODED (FRMS 23-29) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2112 LH OMEGA BEAM #2 IB FLANGE CORRODED BTW FR23-29 AND CRACKED AT FR24 AND 27. R&R'D IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (FRM 28 S15-16R) · airframe 50,017 hrs · 46,913 cycles

53-2120 SHEAR CLIP CRACKED AT FR 28 STR15R-16R. R&R'D IAW SRM51-40-02

Part: SHEAR TIE — CRACKED (FRM 24 S16-17L) · airframe 50,017 hrs · 46,913 cycles

53-2113 SHEAR CLIP CRACKED AT FR24 BTW STR16L-17L. R&R'D IAW SRM51-40-02

Part: SHEAR TIE — CRACKED (FRM 26- S16-17R) · airframe 50,017 hrs · 46,913 cycles

53-2118 SHEAR CLIP CRACKED AT FR26 STR16R-17R. R&R'D IAW SRM51-40-02

Part: FLOOR SUPPORT — CRACKED (FRMS 20-21) · airframe 50,017 hrs · 46,913 cycles

53-2096 SUPPORT CRACKED AT CTR OMEGA BEAM BTW FR20-21. R&R"D IAW SRM 51-40-02

Part: SUPPORT — CRACKED (FRMS 29-35) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2122 RH #2 SILL CORRODED BTW FR29-35. R&R'D IAW SRM51-40-02

Part: SUPPORT — CORRODED (FRMS 23-29) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2119 RH SILL #1 BTW FR23-29 CORRODED. R&R'D SILL IAW SRM 51-40-02

Part: GUSSET — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2088 RH GUSSET #3 CORRODED. R&R'D IAW SRM 51-40-02

Part: SUPPORT — CORRODED (FRMS 29-35) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2125 LH SILL #3 CORRODED BTW FR29-35. R&R'D IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (FRMS 21-22) · airframe 50,017 hrs · 46,913 cycles

53-2095 UNDERFLOOR, LH OMEGA BEAM HAS CRACKS AT FR21-22. R&R"D IAW SRM 51-40-02

Part: SUPPORT — CRACKED (FRM 23-29) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2111 LH SILL #2 CORREDE BTW FR23-29. R&R'D IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (FRM 47) · airframe 50,017 hrs · 46,913 cycles

53-2105 CTR OMEGA BEAM WING STUB LH ANGLE IS CRACKED AT FR47. R&R'D IAW SRM 51-400-02 AND EO1-53-24-0104

Part: GUSSET — CORRODED (FRMS 19-23) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2094 UNDERFLOOR, CTR GUSSET AT FR19-23 CORRODED. R&R'D IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (NOT REPORTED) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2098 UNDERFLOOR, LH SILL #1 IS CORRODED. R&R"D IAW SRM51-40-02

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

UNDERFLOOR: FWD DIGITAL FOUND CORRODED. REPAIED IAW EO1-53-24-0134

Part: SUPPORT — CORRODED (UNKNOWN) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2107 RH SILL #5 CORRODED. R&R"D IAW SRM51-40-02

Part: FLOOR SUPPORT — CRACKED (FRSM 19-20) · airframe 50,017 hrs · 46,913 cycles

53-2097 UNDERFLOOR, LH OMEGA BEAM AGLE SUPPORT IS CRACKED BTW FR19-20

Part: BEAM — CORRODED (FRMS 29-35) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2127 LH OMEGA BEAM CORRODED AT FR29-35 AND CRACKED AT FR30 AND 33. R&R'D IAW SRM51-40-02

Part: ANGLE — CRACKED (FRM 47) · airframe 50,017 hrs · 46,913 cycles

53-2106 CTR OMEGA BEAM WING STUB RH ANGLE CRACKED ON FWD SIDE OF FR47

Part: SHEAR TIE — CRACKED (FRM 46 S15-16R) · airframe 50,017 hrs · 46,913 cycles

53-2116 SHEAR CLIP CRACKED AT FR46 STR15R-16R. R&R"D IAW SRM 51-40-02

Part: DOUBLER — CORRODED (FRMS 57-58) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2061 CORROSION ON WATWR WASTE DOUBLER AT FR57-58 STR19R-20R. REPAIRD IAW EO1-53-24-00109

Part: RIVET — LOOSE (FRM 80 S6-7L) · airframe 50,017 hrs · 46,913 cycles

53-2049 LOOSE RIVET ON LH SIDE SKIN AT FR80 BTW STR6L-7L. REPAIRED IAW EO1-53-24-0053

Part: SUPPORT — CORRODED (WASTE VALVE) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2023 CORROSION ON TOILET WASTE VALVE SUPPORT, TOILET CUP. R&R'D IAW SRM51-40-02

Part: SKIN — CORRODED (FRM 24 S21L) · corrosion level 2 · airframe 50,017 hrs · 46,913 cycles

53-2019 CORROSION STR21L BTW SKIN JUNCTION 3 AND FR24. REPAIRED IAW EO1-53-24-0056

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,938 hrs · 46,821 cycles

E1 A/I FAIL ON EICAS DURING TAKE OFF ROLL. MEL 18DEC23 20:52 CLT C35217 30-8-1. ENGINE ANTI-ICING VALVES. R & R 100 ENGINE A/I VALVE IAW EMB-145 AMM 30-21-01. OPS CHECK GOOD. CLEAR MEL 30-8-1.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,802 hrs · 46,654 cycles

STRONG BURNING SMELL AFTER LIGHTNING STRIKE. RAN AIRCRAFT, NO SMELLS NOTED. PERFORMED TAXI CHECK WITH HIGH POWERED ENGINE RUN, NO SMELLS NOTED. ISOLATED + CHECKED BLEED 1, APU BLEED, BLEED 2 WITH NO DEFECTS NOTED. FURTHER UNABLE TO DUPLICATE SMELL WITHING REALM OF MAINTENANCE. AIRCRAFT OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,294 hrs · 46,074 cycles

CREW CALLED WITH REJECTED T/O. AT 80 KTS THEY GOT A STEER INOP MSG WITH A "NO CONFIG" MSG. IRREGULARITY CLEARED USING NORMAL CREW PROCEDURES

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,250 hrs · 46,032 cycles

T/O CONFIG SPOILER REJECTED TAKEOFF. MX PERFORMED SPOILER OPERATIONAL TEST. OPS CHECK GOOD NO DEFECTS NOTED, AIRCRAFT RETURN TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,045 hrs · 45,809 cycles

GROUND CREW DIECONNECTED GROUND POWER WITHOUT CREW APROVAL SMOKE SEEN AT CENTER PEDESTAL. UPON INSPECTION FOUND DIGITAL CONTROLLER TO BE INOP. INSPECTED PRESS CONTROLLER AND FOUND IT TO BE SOURCE OF SMOKE. INSPECTED WIRING OF CONTROLLER NO DEFECTS NOTED. R&R'D DIGITAL PRESS CONTROLLER IAW AMM 21-31-01. OPS CHECK GOOD. A/C OK FOR SERVICE AT THIS TIME

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,441 hrs · 45,208 cycles

REJECTED TAKE OFF DUE TO TAKE OFF CONFIG WARNING ON EICAS WARNING CAME ON AT ABOUT 10 KNOTS AT THE START OF ROLL AND REJECTED ALMOST IMMEDIATELY MESSAGE DID CLEAR AND HAD NOTICED THAT THE BRAKE LIGHT HAD COME ON LIGHT HAD EXTIGUSHED AFTER CYCLED BRAKES HISTORY: FACT 10JUN23 08:34 PHF INRREGULARITY CLEARED USING NORMAL CREW PROCDURES NO MESSAGES OR LIGHT ON AT THIS TIME

Part: A/C PACK — ODOR (NR 1) · airframe 47,901 hrs · 44,575 cycles

AFTER GEAR DOWN NOTED BURING PLASTIC SMELL ON FLIGHT DECK WITH MINOR SMELL NOTED IN CABIN. RAN PACK 1 AND PACK 2 AND OPERATED FLAPS, TRIMS GUST LOCK, WINDSHIELD HEAT, LIGHTS AND RADIOS. FOUND OIL SMELL PRESENT WHILE ONLY OPERATING PACK 1. PAC 1 CURRENTLY ON THE MEL.

Part: NONE — NONE · airframe 46,419 hrs · 42,929 cycles

PDIS 652 05-51 2143691 14JAN22 SBY CLOSE BIRD STRIKE ON T/O ON RIGHT SIDE OF AIRCRAFT. AIRCRAFT ABORTED T/O FACT 14JAN22 07:43 SBY INSP'D A/C FOR BIRD STRIKE IAW AMM 05-50-08. NO DAMAGE FOUND. AIRCRAFT OK FOR SERVICE.

Part: PROFILE — CORRODED (EMERGENCY EXIT) · airframe 45,619 hrs · 42,006 cycles

E869338 - SSI 52-21-06 CORROSION ON PASSENGER RH CABIN ESCAPE HATCH LOWER PROFILE .... REMOVED AND INSTALLED SERVICEABLE R/ H CABIN ESCAPE HATCH LOWER FRAME AROUND LOWER STOP IAW EMB 145 SRM 51-40-02 SRM 51-20-03 SRM 51-40-09.

Part: PROFILE — CORRODED (PAX DOOR) · airframe 45,619 hrs · 42,006 cycles

E869336 - SSI 52-21-06 CORROSION ON PASSENGER LH CABIN ESCAPE HATCH LOWER PROFILE ... REMOVED AND INSTALLED OF SERVICEABLE L/ H CABIN ESCAPE HATCH LOWER PROFILE IAW EMB 145 SRM 51-40-02 SRM 51-20-03 SRM 51-40-06 SRM 51-40-09.

Part: PROFILE — DENTED (CARGO DOOR) · airframe 45,619 hrs · 42,006 cycles

E869386 - DENT ON BAGGAGE DOOR LOWER L PROFILE. ... REMOVED AND REINSTALLED BAGGAGE DOOR INTERNAL LOWER " L " PROFILE IAW EMB 145 SRM 51-40-02

Part: SHEAR TIE — CRACKED (LT WING) · airframe 45,619 hrs · 42,006 cycles

E870635 - LH WING, THE LOWER SHEAR CLIP AT RIB 18 HAS A CRACK .... REMOVED AND INSTALLED LH WING RIB 18 LOWER SHEAR CLIP IAW EMB-145 SRM 51-40-02. LEAK CHECKED GOOD SEE TURNOVER FOR DETAILS

Part: SKIN — CRACKED (FRM 79) · airframe 45,619 hrs · 42,006 cycles

E869171 - FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 2 FASTNERS FR 79 RH SIDE BELOW VERTICAL STAB. ... INSTALLED REPAIR BUSHING FOR (1 EACH ) ( MARKED ) ON FUSELAGE EXTERNAL SKIN AT FR 79 RH SIDE BELOW VERTICAL STAB IAW EMB 145 SRM 53-32-01, ITEM #9 AND EO1-53-21-0196. UPON FURTHER INVESTIGATION NO DAMAGE WAS FOUND AT LOWER FASTENER

Part: SKIN — CRACKED (FRM 77) · airframe 45,619 hrs · 42,006 cycles

E869173 - FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 1 FASTNER FR 77 RH SIDE BELOW VERTICAL STAB ... REMOVED DAMAGE AT (1 EACH ) ( MARKED) FASTENER & INSTALLED REPAIR BUSHING FOR (1 EACH) ( MARKED) ON FUSELAGE EXTERNAL SKIN AT FR 77 RH SIDE BELOW VERTICAL STAB IAW EMB 145 SRM 53-32-01, ITEM #9 AND EO1-53-21-0196

Part: SHEAR TIE — CRACKED (FRM 73- S16-17L) · airframe 45,619 hrs · 42,006 cycles

E870195 - SHEAR CLIP IS CRACKED IN CARGO COMPARTMENT BETWEEN AT FRAME 73 BETWEEN STRINGERS 16L-17L ... REMOVED AND REPLACED SHEAR CLIP AT FR 73 STGR 16-17L IAW EMB145 SRM 51-40-02

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 45,619 hrs · 42,006 cycles

E869837 - SSI 53-30-48 CORROSION ON CARGO DOOR SILL ... REMOVED AND REPLACED CARGO DOOR LOWER SILL IAW EMB145 SRM 51-40-02.

Part: BUSHING — WORN (RT AILERON PCA) · airframe 45,619 hrs · 42,006 cycles

E869840 - R/H AILERON PCA FITTING OUTBD HAT BUSHING HOLES WORN ... REMOVED & REPLACED R/H AILERON PCA FITTING IAW EMB 145 SRM 51-40-02 & 51-20-03.

Part: FLOOR SUPPORT — DAMAGED (FRMS 58-59) · corrosion level 2 · airframe 45,619 hrs · 42,006 cycles

E870099 - L/H OMAGA BEAM FLOOR SUPPORT IS DAMAGED BETWEEN FR 58-59 ... BLENDED AS REQUIRED TO REMOVE CORROSION FROM LH OMEGA BEAM LOWER FLANGE BETWEEN FR 58-59 IAW EMB-145 SRM 51-10-03. UT CHECK INDICATES 0.037" REMAINING THICKNESS, NOMINAL THICKNESS 0.050", DAMAGE IS WITHIN ALLOWABLE LIMITS IAW EMB-145 SRM 53-24-10 AD.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 45,619 hrs · 42,006 cycles

E869889 - LH #3 FLOORBOARD SILL CORRODED. ... RAR LH #3 FLOORBOARD SILL IAW EMB145 SRM 51-40-02

Part: SUPPORT BRACKET — CRACKED (FRMS 45-46) · airframe 45,619 hrs · 42,006 cycles

E870110 - R/H OMEGA BEAM INBD SUPPORT BRACKET IS CRACKED BETWEEN 45 - 46 .... RAR R/H OMEGA BEAM INBD SUPPORT BRACKET BETWEEN 45 -46 IAW EMB 145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FRM 31) · corrosion level 2 · airframe 45,619 hrs · 42,006 cycles

E869886 - LH CROSSBEAM AT FR 31 CORRODED ... REMOVED AND REPLACED LH CROSSBEAM AT FR 31 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 45,619 hrs · 42,006 cycles

E869893 - LH #4 FLOORBOARD SILL CORRODED. ... REMOVED AND REPLACED LH #4 FLOOR SILL IAW EMB 145 SRM 51-40-02, SRM 51-20-03, AND SRM 51-40-09.

Part: WEB — GOUGED (CARGO DOOR) · airframe 45,619 hrs · 42,006 cycles

E869387 - BAGGAGE DOOR WEBBING IS GOUGED. 4 EACH WITH 1 AT PREVIOUS REPAIR ... ACCOMPLISHED REPAIR OF 3 BLENDED AREAS AND REMOVED AND REPLACED EXISTING DOUBLER ON BAGGAGE DOOR INTERNAL WEB IAW EMB 145 SRM 52-30-01 ITEM 12 FIGURE 213 AND EO1-52-21-0192

Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 45,619 hrs · 42,006 cycles

E870107 - L/H FLOOR SILL #6 IS CORRODED. ... REMOVED AND INSTALLED NEW LH #6 FLOORBOARD SILL IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 45,619 hrs · 42,006 cycles

E870108 - L/H FLOOR SILL #5 IS CORRODED ... REMOVED AND INSTALLED NEW LH #5 FLOORBOARD SILL IAW EMB 145 SRM 51-40-02.

Part: RIB — CRACKED (LT WING) · airframe 45,619 hrs · 42,006 cycles

E870644 - LH WING, THE UPPER SHEAR CLIP AT RIB 21 IS CRACKED....PERFORMED REPAIR AT L/H WING RIB 21 IAW EMB 145 SRM 57-20-07 ITEM #4 FIGURE 203 DET.C AND EO1-57-21-0191

Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · airframe 45,619 hrs · 42,006 cycles

E870109 - R/H FLOOR SILL #4 IS CORRODED .... RAR R/H FLOOR SILL #4 IAW EMB145 SRM 51-40-02

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,619 hrs · 42,006 cycles

E869905 - LH #3 OMEGA BEAM UPPER GUSSET CORRODED ... REMOVED AND REPLACED LH #3 OMEGA BEAM UPPER GUSSET IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (RIGHT) · corrosion level 2 · airframe 45,619 hrs · 42,006 cycles

E869884 - RH #1 FLOORBOARD SILL CORRODED ... RAR RH #1 FLOORBOARD SILL IAW EMB 145 SRM 51-40-02. SEE NRTC FOR DETAILS

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 45,619 hrs · 42,006 cycles

E869890 - RH #2 FLOORBOARD SILL CORRODED. ... RAR RH #2 FLOORBOARD SILL IAW EMB145 SRM 51-40-02

Part: GUSSET — CORRODED · airframe 45,619 hrs · 42,006 cycles

E869892 - CENTER #2 OMEGA BEAM UPPER GUSSET CORRODED ... RAR #2 CENTER OMEGA BEAM GUSSET IAW EMB 145 SRM 51-40-02 AND SRM 51-40-09.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 45,619 hrs · 42,006 cycles

LEFT NR 4 OMEGA BEAM UPPER GUSSET CORRODED . REMOVED AND REPLACED NR 4 OMEGA BEAM UPPER GUSSET IAW SRM 51-40-02.

Part: GUSSET — CORRODED (NR 1) · corrosion level 2 · airframe 45,619 hrs · 42,006 cycles

E869881 - CENTER #1 OMEGA BEAM UPPER GUSSET CORRODED. ... REMOVED AND REPLACED CENTER #1 OMEGA BEAM UPPER GUSSET IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 45,619 hrs · 42,006 cycles

E869885 - LH #2 OMEGA BEAM UPPER GUSSET CORRODED ... REMOVED AND REPLACED LH #2 OMEGA BEAM UPPER GUSSET IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 45,619 hrs · 42,006 cycles

E870053 - BOTH FLOOR SUPPORTS CORRODED/GOUGED (BELOW THE PAX DOOR CUTOUT) ... REMOVED AND REPLACED BOTH FLOOR SUPPORTS BELOW THE PAX DOOR CUTOUT IAW EMB 145 SRM 51-40-02.

Part: WARNING LIGHT — FALSE ACTIVATION (SERVICE DOOR)

DURING TAKE OFF ROLL AT 30 KNOTS SERVICE DOOR WARNING APPEARED. VERIFIED SERVICE DOOR CLOSED AND LATCHED. C/W FLT CREW PROCEDURE. 00 FACT 09MAY21 00:33 MDT. INSPECTED SERVICE DOOR AND RAN TEST IRT AMM 52-74-00 CND DISCREPANCY. OPS CHECK GOOD AND OK FOR RETURN TO SERVICE AT THIS TIME.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 45,155 hrs · 41,501 cycles

EMERGENCY LIGHT AT ROW 18A AND 17A INOP. REMOVED ROW 18A AND 17A EMERGENCY LIGHT STRIP AND FOUND BROKEN WIRE ON WIRE APLICE CONNECTOR. REMOVED FLOOR PANEL 261BF TO ACCESS BROKEN WIRE REPLACED CONTACT PIN AND THE RECEPTACLE OF THE WIRE SPLICE CONNECTOR. PERFORM OPS CHECK INSTALL PANEL 261BF AND ROW 18A AND 17A EMERGENCY LIGHT STRIP ALL. MAINTENANCE PERFORM WAS IAW ALL 33-50-12, 53-01-02 AND 20-21-00 AT THE AIRCRAFT STANDARD WIRING MANUAL

Part: WARNING SYSTEM — MALFUNCTIONED · airframe 44,978 hrs · 41,285 cycles

PDIS 652 31-50 2379262 01MAR21 CLT CLOSE. DURING T/O ROLL AT ABOUT 40 KTS, GPWS, TCAS, TERRAIN INOP EICAS MESSAGES WITH TAKEOFF CONFIG WARNING WITH NO RELATED AURAL WARNING. FACT 02MAR21 09:27 CLT R&R AURAL WARNING UNIT IAW AMM 31-51-400-801-A OPS CHECK IAW 31-51-00-700-801-A.

Part: RELAY — FAILED (GPWS/TCAS) · airframe 44,978 hrs · 41,285 cycles

DURING T/O ROLL AT ABOUT 30KTS, GPWS, TCAS, TERRAIN INOP EICAS MESSAGES WITH T/O CONFIG WARN WITH NO RELATED ORAL WARNING FACT 01MAR21 17:03 CLT C/N/D, R&R'D RELAY K0212 FOR PRECAUTION. C/W SELF TEST OF GPWS, TCAS AND T/O CONFIG. ALL TESTS PASS. OPS CHECK GOOD. A/C OK FOR SERVICE

Part: HANDLE — FAILED (PARKING BRAKE) · airframe 44,565 hrs · 40,834 cycles

PDIS 652 32-44 2174051 04OCT20 CLT. CLOSE PARKING BRAKE WILL NOT DISENGAGE, HANDLE WILL NOT MOVE DOWN. FACT 04OCT20 17:09 CLT. R & R PARKING BRAKE HANDLE/CABLE ASSY, IAW AMM 32-44-11. OPERATIONS CHECK GOOD, OK FOR SERVICE.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 44,558 hrs · 40,825 cycles

PDIS 652 21-31 2174011 27SEP20 LEX CLOSE. CABIN WOULD NOT AUTO PRESSURIZE AFTER TAKEOFF. IN MANUAL, CABIN ALT INDICATION FAILED AFTER 10 MINS. INDICATION CAME BACK AFTER LANDING. FACT 27SEP20 13:30 LEX. INSPECTED CPAM AND CB FOR PROPER OPERATION, NO DEFECTS FOUND. PERFORMED PRESSURE CONTROL SYSTEM OPERATIONS CHECKS MANUAL AND AUTO MODES, IAW AMM 21-31-00-700-801-A AND 21-31-00-700-802-A, NO DEFECTS NOTED. OPS CHECKS GOOD, OK FOR SERVICE.

Part: SPOILER SYS — MALFUNCTIONED · airframe 44,493 hrs · 40,752 cycles

DURING TAKEOFF ROLL AT ABOUT 70 KTS MASTER WARNING LIGHT ILLUMINATED, SPOILER INDICATED OPEN, AND AURAL WARNING TAKEOFF SPOILERS. SPOILERS CLOSED AFTER T/L RETURNED TO FLIGHT IDLE. NO RELATED CMC MESSAGES FOR TODAY. RESET SPOILER SYSTEM. OPERATIONS CHECK SPOILERS IAW AMM 27-63-01 OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 44,325 hrs · 40,563 cycles

DURING CRUISE/APPROACH GOT STRONG ELECTRICAL SMELL IN COCKPIT. NO ASSOCIATED EICAS MESSAGES. SMELL CLEARED WHEN ON GROUND. (OUTSIDE OF ICING CONDITIONS WHEN SMELL OCURRED). MAINTENANCE: T/S ELECTRICAL SMELL IAW FIM 21-20-00-810-801-A. NO ABNORMAL SMELLS NOTED. PERFORMED COOLING SYSTEM OPS CHECK IN REF TO AMM 21-51-00. OPS CHECK GOOD. INSPECTED FWD AVIONICS BAY, NO ABNORMAL SMELLS/DEFECTS NOTED. A/C OK FOR SERVICE AT THIS TIME.

Part: SENSOR — FAILED (NR 1 SPS) · airframe 43,528 hrs · 39,685 cycles

SPS 1 INOP MSG ON T/O ROLL...FIX:R&RD #1 AOA SENSOR IAW EMB AMM 27-36-01-04 OPS CHECK GOOD. OK FOR SERVICE

Part: TRIM SYSTEM — LACK OF LUBE (FIRST OFFICER'S) · airframe 43,411 hrs · 39,546 cycles

FO YOKE PITCH TRIM INOP IN FLIGHT. ON GROUND PITCH TRIM UP OK, PITCH RIM DOWN INOP.....FIX:LUBED FOS PITCH TRIM ON YOKE IAW AMM 27-40-03-640-801A.OPS CHECK GOOD.GOOD FOR SERVICE.CLEARED MEL.

Part: FLASHLIGHT — ODOR (COCKPIT) · airframe 42,291 hrs · 38,217 cycles

PDIS 652 05-50 2016771 26APR19 CLT CLOSE WHEN SWITCHING FROM F/A CONTROL TO F/D DECK CONTROL ON PACK 2 SLIGHT ODOR NOTICED. ODOR DISSIPATED SHORTLY AFTER. 29363 00 CVS HISTORY: NONE FACT 26APR19 08:01 CLT INSPECTED A/C AND DETERMINED TO BE F/D FLASHLIGHT CAUSING ODOR. R&R'D FLASHLIGHT ON CA'S REAR WALL AS REQ'D OPS CHK GOOD OK FOR SERVICE.

Part: FLAP SYSTEM — STUCK · airframe 42,259 hrs · 38,183 cycles

PDIS 652 05-50 2016731 21APR19 FAY CLOSE REF LP 201672 ITEM 3, DURING GO AROUND WITH FLAPS ST UCK AT 45 DEGREES A/C REACHED 173 KTS FACT 22APR19 08:57 FAY INSP FLAP IAW AMM 05-50-07-212-004-A NO DEFECTS NOTE D AT THIS TIME. DVI FLAP FOR DAMAGE NO DEFECTS NOTED AT THIS OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 42,081 hrs · 37,974 cycles

PDIS 652 52-40 1931872 18MAR19 PHL CLOSE ON TAKEOFF ROLL SERVICE DOOR OPEN EICAS MSG DISPLAYED. HISTORY: FACT 18MAR19 22:17 PHL INSP SERVICE DOOR FOR DEFECTS W NONE NOTED. SERVICE DOOR OPERATES NORMALLY AT THIS TIME OKAY FOR SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 41,832 hrs · 25,394 cycles

NDIS 652 33-51 0003030 14JAN19 SBY CLOSE FWD CEILING EMERGENCY LIGHT AT ROW 12 INOP. FACT 14JAN19 10:37 SBY R&R NR 6 EMERGENCY LIGHT INVERTER IAW 33-50-11-04. P/N ON INVERTER 1330312 P/N OFF INVERTER 1330312

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 41,770 hrs · 37,617 cycles

PDIS 652 27-38 1735201 01JAN19 MKE CLOSE PTRIM MAIN INOP EICAS MESSAGE ON TAKEOFF. HISTORY: YES FACT 01JAN19 17:08 MKE REST MAIN CHANNEL IN REFERENCE TO FIM 27-43-00-810-801-A OPS CK GOOD IAW AMM 27-40-00-700-802-A NO FAULTS NOTED OK FOR SERVICE.

Part: TRIM SYSTEM — MALFUNCTIONED (HORIZ STAB) · airframe 41,660 hrs · 37,492 cycles

ON CLIMB OUT FO PITCH TRIM FAILED FOLLOWED BY PTRIM MAIN INOP AND PTRIM BACK UP INOP. RAN QRH BACK SYS MOMENTARY CAME BACK ONLINE CYCLED MAIN AND BACK UP CUT OUT. CND DISCREPANCY ON GROUND. R&R HSCU AS MX PRECAUTION OPS CHECK GOOD REF AMM 27-40-00 AND 27-40-01. READY FOR SERVICE.

Part: CONTACT — DIRTY (EMERGENCY LIGHT) · airframe 41,533 hrs · 37,321 cycles

NDIS 652 33-51 0001970 13NOV18 SBY CLOSE ROW 12 EMERGENCY LIGHT ON CEILING IS INOP 33384 00 SPE FACT 13NOV18 07:48 SBY REMOVED CEILING HEADLINER AT ROW 12 IAW AMM 25-22-04-000-801-A. TESTED VOLTAGE OF EMERGENCY LIGHT AND FOUND NO DESCREPANCY. CLEANED CONTACTS WITH ELECTRICAL CONTACT CLEANER. RETESTED LIGHT SATISFACTORY. EMERGENCY LIGHT IS GOOD FOR SERVICE. INSTALLED HEADLINER AT ROW 12 IAW AMM 25-22-04-400-801-A

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 41,464 hrs · 37,229 cycles

COCKPIT FLASHLIGHT INOP. C/A-REMOVED AND REPLACED COCKPIT FLASHLIGHT IAW AMM 33-50-16 OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 41,464 hrs · 37,229 cycles

AFT CABIN FLASHLIGHT INOP. C/A-REMOVED AND REPLACED AFT CABIN FLASHLIGHT IAW AMM 33-50-16 OPS CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,463 hrs · 37,228 cycles

SKIN CRACKED AROUND RIVETS ON FRAME 80. C/A-ACCOMPLISHED REPAIR IAW SRM 53-32-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,463 hrs · 37,228 cycles

NUMBER NR 4 EMERGENCY LIGHT STRIP INOP. C/A-REMOVED AND REPLACED NR 4 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: STRUCTURE — DENTED (SERVICE DOOR) · airframe 41,463 hrs · 37,228 cycles

SERVICE DOOR LOWER EDGE IS DENTED. C/A-REPAIRED SERVICE DOOR LOWER EDGE IAW ERS-EM-52MR-911.

Part: WEB — GOUGED (CARGO DOOR) · airframe 41,463 hrs · 37,228 cycles

CARGO DOOR WEBBING HAS SEVERAL GOUGES. C/A-REPAIRED BAGGAGE DOOR INNER WEB CHAFES IAW SRM 52-30-01 AND ETN-EM-52-043.

Part: WIRE — BROKEN (CABIN) · airframe 41,463 hrs · 37,228 cycles

LT NR 2 FLOOR PROXIMITY EMERGENCY LIGHT WIRES BROKEN. C/A-REMOVED AND REPLACED LT NR 2 FLOOR PROXIMITY EMERGENCY LIGHT IAW AMM 33-50-12.

Part: FITTING — CRACKED (LT ENGINE) · airframe 41,463 hrs · 37,228 cycles

LT ENG FWD YOKE LOWER FWD FITTING CRACKED. C/A-COMPLETE:ERS-EM-54MR-698 FOR CRACKED LT ENGINE FORWARD YOKE LOWER FORWARD FITTING SATISFACTORILY ACCOMPLISHED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 41,307 hrs · 37,047 cycles

DURING A PS-1 CHECK, FOUND AN EXTERNAL EMERGENCY LIGHT ON THE LT CENTER FAIRING, BURNED OUT. REMOVED AND REPLACED THE BULB IAW AMM 33-50-10. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 40,812 hrs · 36,582 cycles

FUMES IN COCKPIT & FORWARD CABIN SIMILAR TO DIRTY GYM BAG WITH HINT OF OIL NO EICAS INDICATIONS DURING DESCENT AND LEVEL OFF WHILE INCREASING POWER TO MAINTAIN SPEED GOT WORSE WITH INCREASE IN POWER BOTH PACKS POWERED BY THEIR RESPECTIVE BLEED NOTHING ASSOCIATED WITH ICING SYSTEM APPEARED IN DESCENT NO PRIOR INDICATION FOR HOUR & THIRTY MINUTE FLIGHT NOT AN ELECTRICAL SMELL NO APU AIR OR POWER.-C/A-PERFORMED CONDITIONED AIR DUCT DECONTAMINATION IAW AMM 21-20-00-100-805 AND PERFORMED ODOR EVENT T/S IAW ETN-EM-72-034. NO EVIDENCE OF SMELL OR FUMES FOUND IN COCKPIT OR CABIN. REF NRWC 625-ORD-03627, 625-ORD-03621, 625-ORD-03624 FOR ADDITIONAL INSPECTIONS PERFORMED OPS CHECK GOOD.

Part: FLASHLIGHT — ODOR (COCKPIT) · airframe 40,660 hrs · 36,426 cycles

ODOR OF SMOKE IN THE COCKPIT. PERFORMED AN ENGINE RUN IAW MM 72-00-00, AND APU RUNS. FOUND THE ODOR COMING FROM FIRST OFFICER`S SIDE FLASHLIGHT. REMOVED AND REPLACED THE FLASHLIGHT. NO ODOR NOTED

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,539 hrs · 36,305 cycles

FLOOR EMERGENCY LIGHT AT SEAT 18A FOUND INOPERAIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT CONNECTOR IAW SWPM 20-50-01. OPS CHECKED GOOD.

Part: BULB — NOT SEATED (EMERGENCY LIGHT) · airframe 40,150 hrs · 35,937 cycles

RIGHT AFT OVERWING EXIT LIGHT INOPERATIVE. REMOVED, RESEATED AND REINSTALLED THE BULB IAW AMM 33-50-10 . OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 40,126 hrs · 35,913 cycles

COCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE COCKPIT EMEGENCY LIGHT IAW AMM 33-50-05-000-801, AND 33-50-05-400-801. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,094 hrs · 35,882 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE BULB AND OPS CHECKED GOOD IAW AMM 33-50-06.

Part: ACM — FAILED (LEFT) · airframe 39,864 hrs · 35,698 cycles

STRONG ODOR OF BURNING, NO INDICATION OF ANY FIRE. THE ODOR WAS WITH THE NR 2 PACK. COMPLIED WITH ETN-EM-72-034, THE NR 2 PACK OVERHEATT MESSAGE NOTED. NO DEFECTS NOTED ON THE NR 1 PACK. REMOVED AND REPLACED THE NR 2 ACM IAW AMM 21-51-03, OPS CHECKED GOOD, NO BURNING ODOR NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,730 hrs · 35,586 cycles

RH WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED THE RH WING EXTERNAL EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10, OPS CHECK GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,269 hrs · 35,179 cycles

LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: CRADLE — INOPERATIVE (FLASHLIGHT) · airframe 38,788 hrs · 34,791 cycles

PREVIOUS CREW REPORTED STRONG BURNING ODOR IN THE CABIN WHILE FLYING THROUGH THUNDERSTORMS, FOUND BURNING ODOR ON FED FLASHLIGHT CRADLE. REMOVED AND REPLACED FWD CABIN EMERGENCY FLASHLIGHT ASSY IAW AMM 33-50-16.

Part: SENSOR — FALSE INDICATION (BRAKE TEMP) · airframe 38,434 hrs · 34,511 cycles

ON ROTATION A BRAKE OVERHEAT ILLUMINATED ON EICAS. THE LEFT INBOARD DETECTOR TOP OF SCALE. FA REPORTED ODD NOISE WHEN RETRACTING GEAR, ALL OTHER INDICATORS FOR BRAKE TEMP GREEN. ALL MTX PROCEDURES COMPLIED WITH. REPLACED THE LT, INBD BARKE TEMP SENSOR IAW AMM 32-47-01. OPS CHECKED GOOD.

Part: CONNECTOR — MISINSTALLED (BRK TEMP SENSOR) · airframe 38,420 hrs · 34,497 cycles

AFTER TAKE OFF, A BRAKES OVERHEAT ON EICAS. PERFORMED THE CHECKLIST, UNABLE TO RESTORE. REMOVED AND REPLACED THE NR 1 BRAKE TEMPERATURE SENSOR IAW AMM 32-47-01. OPS CHECKED GOOD. DURING TROUBLESHOOTING, FOUND THE NR 1 AND 2 BRAKE TEMP SENSOR CONNECTORS SWITCHED. PROPERLY CONNECTED THE NR 1 AND 2 BRAKE TEMP SENSORS IAW CMM 32-10-01 AND WM 32-47-50. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,533 hrs · 33,701 cycles

ROW 12 CIELING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACEDTHE EMERGENCY LIGHT. OPS CHECKED GOOD IAW AMM 33-50-07.

Part: CHARGER — FAILED (CABIN) · airframe 37,511 hrs · 33,675 cycles

RT & LT EXTERIOR OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 BATTERY CHARGER. OPS CHECKED GOOD IAW AMM 33-50-04.

Part: SWITCH — OBSTRUCTED (MLG DOOR) · airframe 37,359 hrs · 33,543 cycles

AFTER ROTATION AND DURING GEAR RETRACTION, RECEIVED "ACCESS DOORS OPEN" CAUTION MESSAGE AND FOWARD AVIONICS ACCESS HATCH OPEN INDICATION ON MFD DOORS PAGE-C/A-UPON FURTHER INVESTIGATION FOUND SEAL OBSTRUCTING SWITCH. RESEATED DOOR AND OPS CHECK GOOD IAW EMB 145 AMM 52-71-00. OPS CHECK GOOD

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,338 hrs · 33,517 cycles

RIGHTT AFT UPPER OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: ENGINE — FAILED (LEFT) · airframe 37,254 hrs · 33,419 cycles

STRONG FUMES IN THE COCKPIT & CABIN DIRING FLIGHT. DECLARED EMERGENCY, DIVERTED TO MKE. C/W ETN-EM-72-034 AND FIM TASK 21-20-00-810-801A. NO FURTHER DEFECTS NOTED AT THIS TIME. REMOVED AND REPLACED LT ENGINE IAW WC 71-000-00 OPC AND LEAK CHECK GOOD PERFORMED ODOR EVENT IAW ETN-EM-72-034. NO FUTHER ODORS AT THIS TIME END.

Part: STRINGER — CRACKED (FRAME 13) · airframe 37,188 hrs · 33,358 cycles

DURING HMBV INSPECTION, QA FOUND STRINGER 6R CRACKED AT FRAME 13. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CRACKED (FRM 66) · airframe 37,188 hrs · 33,358 cycles

DURING HMBV INSPECTION, QA FOUND FRAME 66 CRACKED AT CARGO DOOR SILL. AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE FRAME IAW ERS-EM-53MR-2302. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CRACKED (FRM 10) · airframe 37,188 hrs · 33,358 cycles

DURING HMBV INSPECTION, QA FOUND FR 10 CRACKED AT UPPER END. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02 AND 51-20-03. AIRCRAFT RETURNED TO SERVICE.

Part: GUSSET — GOUGED (FRAME 68) · airframe 37,188 hrs · 33,358 cycles

DURING HMBV INSPECTION, QA FOUND FRAME 68 GUSSET WAS GOUGED AROUND NUMEROUS SCREW HOLES. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GUSSET IAW SRM 51-40-02, 51-40-06 AND 51-20-03. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CRACKED (FRM 67) · airframe 37,188 hrs · 33,358 cycles

DURING HMBV INSPECTION, QA FOUND FRAME 67 CRACKED AT CARGO DOOR SILL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE FRAME IAW ERS-EM-53MR-2312. AIRCRAFT RETURNED TO SERVICE.

Part: ACCESS PANEL — CHAFED (FRAMES 77-80) · airframe 37,188 hrs · 33,358 cycles

DURING HMBV INSPECTION, QA FOUND ACCESS PANEL 312AR CUT OUT CAM LOCK RECEPTICAL OPENINGS CHAFED. AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE ACCESS PANEL IAW ERS-EM-53MR-2314. AIRCRAFT RETURNED TO SERVICE.

Part: TRUNNION — CRACKED (LT MLG) · airframe 37,188 hrs · 33,358 cycles

DURING HMBV INSPECTION, QA FOUND LT MLG AFT UPPER TRUNNION CRACKED IN UPPER RADIUS. AIRCRAFT WAS REMOVED FROM SERVICE. -C/A-REMOVED AND REPLACED LH MLG AFT UPPER TRUNION IAW ERS-EM-57MR702. AIRCRAFT RETURNED TO SERVICE.

Part: TRUNNION — CRACKED (RT MLG) · airframe 37,188 hrs · 33,358 cycles

DURING HMBV INSPECTION, QA FOUND RT MLG AFT UPPER TRUNNION CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RT MLG AFT UPPER TRUNNION IAW ERS-EM-57MR-697. THE AIRCRAFT RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FRAMES 60-61) · airframe 37,188 hrs · 33,358 cycles

DURING HMBV INSPECTION, QA FOUND THE TOILET WASTE VALVE SUPPORT CORRODED. AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED REPAIR DOUBLER IAW ERS-EM-53MR-2300. THE AIRCRAFT RETURNED TO SERVICE.

Part: TEE FITTING — CRACKED (FRAME 65) · airframe 37,188 hrs · 33,358 cycles

DURING HMBV INSPECTION, QA FOUND CARGO DOOR CUTOUT SILL FWD TEE BRACKET CRACKED. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CARGO DOOR CUTOUT SILL FWD TEE BRACKET IAW SRM 51-20-03 AND 51-40-02. AIRCRAFT WILL BE RETURNED TO SERVICE.

Part: FILLER — CORRODED (FRAMES 64-65) · airframe 37,188 hrs · 33,358 cycles

DURING HMBV INSPECTION, QA FOUND PREVIOUS REPAIR FILLER BETWEEN FR 64 - 65, STGR 21L-21R CORRODED. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED PREVIOUS REPAIR CORRODED FILLER IAW SRM 53-31-01RE ITEM 2. AIRCRAFT WILL BE RETURNED TO SERVICE.

Part: FRAME — CRACKED (FRM 10) · airframe 37,188 hrs · 33,358 cycles

DURING HMBV INSPECTION, QA FOUND FRAME 10 CRACKED AT UPPER END. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02 AND 51-20-03. AIRCRAFT WILL BE RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 37,188 hrs · 33,358 cycles

DURING HMBV INSPECTION, QA FOUND THE CARGO DOOR CUTOUT FWD LWR SHEAR TIE ON FRAME 65 CORRODED. AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION. REPAIRED THE CARGO DOOR CUTOUT FWD LWR SHEAR TIE IAW SRM 53-31-04 RE STEP 4F. AIRCRAFT WILL BE RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,693 hrs · 32,916 cycles

GALLEY OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R LAMP IN GALLEY OVERHEAD EMERGENCY LIGHT IAW AMM 33-50-09. OP CHECKED GOOD IAW AMM 33-50-00.

Part: FCU — MALFUNCTIONED (FUEL SYSTEM) · airframe 36,260 hrs · 32,499 cycles

AT CRUISE RECEIVED FUEL IMBALANCE EICAS MSG. LT WING TANK INDICATED ZERO POUNDS FUEL, FUEL FLOW MATCHED RT SIDE FUEL FLOW. INSPECTED ACFT FOR LEAKS, NO LEAKS NOTED. FOUND LT FUEL QTY INDICATION INTERMITTENT. FOUND FCU LT FAIL FAULT CODE ON REPEATER PANEL. R & R FCU IAW MM 28-41-01. OPERATIONS CHECKED GOOD IAW MM 28-41-00.

Part: LIGHT — BROKEN (EXTERIOR) · airframe 36,259 hrs · 32,498 cycles

RIGHT EXTERIOR EMER LIGHT ABOVE PACK PANEL IS BROKEN. R & R RT EXTERIOR EMER LIGHT ABOVE PACK PANEL IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 35,813 hrs · 32,103 cycles

CABIN FWD EMER FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: ENGINE — SHUTDOWN (NR 1) · airframe 35,391 hrs · 31,735 cycles

NR 1 ENGINE SHUTDOWN DURING CLIMB OUT BELOW 2000 FT. R & R LT ENGINE IAW WC 71-000-00. GROUND RAN ACFT. OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: EPSU — INOPERATIVE (CABIN) · airframe 34,989 hrs · 31,378 cycles

NUMBER 4 & 5 EMER FLOOR PROX LIGHT & OTHER EXIT SIGNS NEAR EMER ESCAPE HATCHES ASSOCIATED WITH NR 3 EPSU ARE INOPERATIVE. R & R NR 3 EPSU ASSEMBLY. OPERATIONS CHECKED GOOD IAW AMM 33-50-04.

Part: TIRE — BLOWN (LANDING GEAR) · airframe 34,684 hrs · 31,105 cycles

NUMBER 2 LT INBD BLOWN ON TAKEOFF, CONTROL REPORTED ENROUTE DID NUMEROUS ACFT DAMAGE. LANDING GEAR TIRE TREAD FAILURE IAW AMM 5-50-15 IAW LOG PAGE 3892894, 3892895, 3892896, 3892897 & 3892898 FOR DISCREPANCIES OF DAMAGE FOUND. COMPLIED WITH LG TIRE TREAD FAILURE INSPECTION & CHECK IAW AMM 05-50-15, SEE LOG PAGE 3892895 ALSO. COMPLIED WITH ETN-GN-32-009 THROWN TIRE TREAD ETN. R & R NR 2 MLG TIRE ASSEMBLY IAW WC 32-700-11. COMPLIED WITH CARBON BRAKE INSPECTION IAW WC 32-700-18.

Part: RELAY — INOPERATIVE (RUDDER SYS) · airframe 33,729 hrs · 30,297 cycles

DURING INITIAL CLIMB OUT RUDDER SYS 2 INOPERATIVE MSG ON EICAS. COMPLIED WITH AOM PROCEDURE. REPLACED PRIORITY RELAY K0387 IAW MM 20-13-02. OPERATIONS CHECKED GOOD IAW MM 27-23-00 J 2.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 33,725 hrs · 30,294 cycles

HAIL DAMAGE EVENT, REPLACE RT ELEVATOR OTBD UPPER SKIN TIP. R & R IAW SRM 55-20-01, 51-20-01, 51-40-02, ETN-EM-55-073R2 & ETN-EM-55-076.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,725 hrs · 30,294 cycles

HAIL DAMAGE EVENT, RT CFI NEW SKIN HAS HOLE DRILLED ON CHEM MILL EDGE. ACCOMPLISHED REPAIR IAW ERS-EM-53MR-1080.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,725 hrs · 30,294 cycles

HAIL DAMAGE EVENT, REPLACE REAR FUSELAGE I SKIN. R & R REAR FUSELAGE I SKIN IAW SRM 51-40-02, 51-40-06, 51-20-01, 51-20-03, 51-40-03, ETN-EM-51-118, ETN-EM-53-266 & 53-31-01-SI.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 33,725 hrs · 30,294 cycles

HAIL DAMAGE EVENT, SCRATCH AT FRAME 23 BETWEEN STRINGER 1 - 2R. ACCOMPLISHED REPAIR IAW ERS-EM-53MR-1091.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,725 hrs · 30,294 cycles

HAIL DAMAGE EVENT, RT CFI HAS 8 PILOT HOLES ON NEW SKIN THAT DO NOT ALIGN WITH TEAR STRAP. ACCOMPLISHED REPAIR IAW ERS-EM-53MR-1081.

Part: RIB — DAMAGED (HORIZ STAB) · airframe 33,725 hrs · 30,293 cycles

HORIZONTAL STAB RIB 8 HAS ELONGATED HOLE. ACCOMPLISHED REPAIR OF RIB 8 IAW ERS-EM-55MR-235.

Part: RIB — DAMAGED (HORIZ STAB) · airframe 33,725 hrs · 30,294 cycles

HAIL DAMAGE EVENT, HORIZONTAL STAB RIB 8 HAS ELONGATED HOLE. ACCOMPLISHED REPAIR OF RIB 8 IAW ERS-EM-55MR-235.

Part: TEAR STRAP — DAMAGED (FUSELAGE) · airframe 33,725 hrs · 30,293 cycles

TEAR STRAP HAS ELONGATED HOLE AT FRAME 56 ABOVE STRINGER 5R. ACCOMPLISHED REPAIR OF TEAR STRAP AT FRAME 56 ABOVE STRINGER 5R IAW ERS-EM-53MR-1054.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 33,725 hrs · 30,293 cycles

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

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,725 hrs · 30,294 cycles

HAIL DAMAGE EVENT, REPLACE RT CTR FUSELAGE I. R & R PN 145-20552-003 IAW SRM 51-21-01 SI, 51-40-02, 51-20-03, 51-20-01, 51-40-06, ETN-EM-51-118 & ETN-EM-53-262R1.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 33,725 hrs · 30,293 cycles

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

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 33,725 hrs · 30,293 cycles

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

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 33,725 hrs · 30,294 cycles

HAIL DAMAGE EVENT, REPLACE RT ELEVATOR OUTER LE. R & R IAW SRM 51-40-02, 51-40-06PR, 51-20-01, 51-20-03, SRM 55-20-01, ETN-EM-55-073R2, ETN-EM-55-076 & ERS-EM-5500-233.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,725 hrs · 30,294 cycles

HAIL DAMAGE EVENT, REPLACE LT CTR FUSELAGE I. R & R LT CTR FUSELAGE I IAW SRM 51-40-03, 51-20-01, 051-20-03, 53-21-01 SI, 51-40-02, 51-40-06, ETN-EM-51-118, ETN-EM-53-263 R1 & ETN-EM-51-092.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,725 hrs · 30,294 cycles

HAIL DAMAGE EVENT, REPLACE CTR FUSELAGE II SKIN TOP. R & R IAW SRM 53-22-01-SI, 51-40-03, 51-20-01, 51-20-03, 51-40-06, 51-40-02, ETN EM-53-263 R1, ETN-EM-51-118 & ETN-EM-51-092.

Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 33,725 hrs · 30,294 cycles

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

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 33,725 hrs · 30,294 cycles

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

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,725 hrs · 30,293 cycles

HAIL DAMAGE EVENT, REPLACE FWD FUSELAGE I SKIN, LT FWD. R & R IAW SRM 51-20-01, 51-40--02, 51-20-03, 51-40-06, 53-11-01-SI & ETN-EM-51-118, ETN-EM-53-235 & ERS-EM--5300-1072.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,725 hrs · 30,294 cycles

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

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 33,725 hrs · 30,293 cycles

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

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 33,725 hrs · 30,293 cycles

HAIL DAMAGE EVENT, REPLACE LT ELEVATOR UPPER CTR SKIN. REMOVED & INSTALLED LT ELEVATOR UPPER CTR SKIN IAW SRM 51-20-01, 51-20-03 & ETN-EM-55-076.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,725 hrs · 30,293 cycles

HAIL DAMAGE EVENT, REPLACE FWD FUSELAGE I SKIN, RT FWD. R & R IAW SRM 51-40-02, 51-20-03, 51-40--06, 51-20-01, ETN-EM-51-118, ETN-EM-53-235 & ERS-EM-5300-1072.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 33,725 hrs · 30,294 cycles

HAIL DAMAGE EVENT, REPLACE RT ELEVATOR INBD LE. R & R RT ELEVATOR INBD LE IAW SRM 51-40-06, 51-40-02, 51-20-01, 51-20-03, 55-20-01, ETN-EM-55-073R2 & ETN-EM-55-076.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,725 hrs · 30,293 cycles

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

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 33,725 hrs · 30,293 cycles

HAIL DAMAGE EVENT, REPLACE LT ELEVATOR LE ON TIP. R & R LT ELEVATOR LE ON TIP IAW SRM 51-20-03, 51-20-06 & 51-20-01.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 33,725 hrs · 30,294 cycles

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

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 33,725 hrs · 30,294 cycles

HAIL DAMAGE EVENT, REPLACE RT ELEVATOR LE ON TIP. R & R IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-06, 55-20-01-SI, ETN EM-55-073R2 & ETN-EM-55-076.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 33,725 hrs · 30,293 cycles

HAIL DAMAGE EVENT, REPLACE LT ELEVATOR INBD LE. R & R LT ELEVATOR INBD LE IAW SRM 51-20-01, -03 & 51-40-02, -06.

Part: ADC — FAILED (NR 1) · airframe 33,419 hrs · 30,053 cycles

ADC 1 FAIL. R & R NR 1 ADC IAW AMM 34-15-01. OPERATIONS CHECKED GOOD, LEAK CHECKED GOOD IAW AMM 34-13-00, NO LEAKS. ACFT IS COMPLIANT FOR CONTINUED CAT II OPERATIONS.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 32,894 hrs · 29,608 cycles

FLIGHT ATTENDANT FLASHLIGHT OPERATES INTERMITTENTLY. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 32,856 hrs · 29,570 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN. CLEANED & LUBED MAIN PAX DOOR ROLLERS IAW AMM 52-18-00. OPERATIONS CHECKED GOOD.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 32,859 hrs · 29,573 cycles

WHILE AT FC 360 IN ICING CONDITIONS WE RECEIVED IAS MSG ON BOTH PFD'S. IT APPEARED THAT THE CAPTAIN`S SIDE & STANDBY WERE IN AGREEMENT. WE CONCLUDED THE FIRST OFFICER'S SIDE WAS INACCURATE. AT ONE POINT DURING A DESCENT CAPTAIN`S SIDE SPEED INCREASED NORMALLY WHILE FIRST OFFICER`S SIDE DECREASED SPEEDS INDICATING AT THAT TIME. CA-245 KNOTS FO 219 KNOTS. FIRST OFFICER`S SPEED RETURNED TO NORMAL UPON EXITING ICING CONDITIONS & USING ALL MODE POSITION FOR THE ICE DETECTION OVERRIDE. WE ALSO SAW GPS 2 NOT NAV ON FMS SPS ADVANCE IN AMBER, NO BLUE SPS SPEEDS MSG. PERFORMED PITOT STATIC SERVICING, FOUND WATER IN TUBES. PERFORMED ADC OPERATIONAL TEST CHECKS OK IAW AMM 34-13-00 & 34-15-00. ACFT IS COMPLIANT FOR CAT II & RVSM OPERATIONS.

Part: LIGHT — DAMAGED (CABIN) · airframe 32,661 hrs · 29,410 cycles

LEFT EMER LIGHT STRIP NR 3 LIGHT STRIP DAMAGED. R & R EMER LIGHT STRIP NR 3 IAW AMM 33-50-12. FOUND DURING ACFT OPEN UP.

Part: LIGHT — DAMAGED (CABIN) · airframe 32,661 hrs · 29,410 cycles

LEFT EMER LIGHT STRIP NR 8 LIGHT STRIP DAMAGED. R & R EMER LIGHT STRIP NR 8 IAW AMM 33-50-12. FOUND DURING ACFT OPEN UP.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 32,626 hrs · 29,383 cycles

FLIGHT ATTENDANT REAR FLASHLIGHT WILL NOT STAY SECURE IN HOLDER. REPLACED AFT FLASHLIGHT ASSEMBLY IAW MM 33-50-16. OPERATIONS CHECKED GOOD.

Part: CRADLE — DEFECTIVE (FLASHLIGHT) · airframe 32,545 hrs · 29,289 cycles

FLIGHT ATTENDANT EMER FLASHLIGHT NOT BEING HELD PROPERLY BY BRACKET CRADLE. R & R FLASHLIGHT & CRADLE ASSEMBLY IAW AMM 25-61-01.

Part: BATTERY — OVERTEMP (NR 2) · airframe 32,441 hrs · 29,215 cycles

BATTERY 2 OVTMP ACCOMPANIED BY ELEC BURNING ODOR. R & R NR 1 & 2 MAIN BATTERIES IAW AMM 24-36-00. OPERATIONS CHECK OF BATTERIES COMPLIED WITH NORMALLY IAW AMM 24-36-00. NO EVIDENCE OF BURNING ELEC ODOR NOTED. PERFORMED AIR CONDITIONING SYS PURGE IAW AMM TASK 21-20-00-100-805A. PERFORMED ENG RUNS & OPERATED ALL GENERATORS NO EVIDENCE OF ELEC BURNING ODOR. INSPECTED FLIGHT DECK INSTRUMENT LIGHTING & PAX CABIN LIGHTING SYS FOR ANOMALIES. NO DEFECTS OR BURNING ELEC ODOR NOTED. PN AML 3591977-1 SN 32248-0012.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 31,480 hrs · 28,417 cycles

CAPTAIN`S FLASHLIGHT SWITCH BROKEN OFF. R & R CAPTAIN`S FLASHLIGHT, OPERATIONS CHECKED GOOD IAW 33-51-01 AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 31,147 hrs · 28,161 cycles

ON FLIGHT 3191 CREW FOUND AFT LIGHT EMERGENCY FLOOR STRIP & OVERWING LIGHTS ON WHEN IN THE ARMED POSITION. THE ACFT WAS REMOVED FROM SERVICE. R & R NR 4 EMERGENCY BATTERY CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD, THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE WARNING — ACTIVATED (LAVATORY) · airframe 30,729 hrs · 27,833 cycles

FLIGHT 5215, CREW REPORTED CLIMBING THROUGH 1000 FEET, RECEIVED A LAVATORY SMOKE WARNING. NO FIRE OR SMOKE NOTICED. FOLLOWED AOM PROCEDURES AND DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. OPEN

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,503 hrs · 27,654 cycles

AFT TWO FLOOR PROXIMITY LIGHTS INOPERATIVE. R & R NR 4 EMERGENCY POWER SUPPLY IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: FLASHLIGHT ASSY — CRACKED (FWD CABIN) · airframe 29,927 hrs · 27,193 cycles

DURING B INSPECTION, FOUND THE F/A EMERGENCY FLASHLIGHT ASSY CRACKED. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT ASSY IAW WC 33-700-20. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 28,032 hrs · 25,694 cycles

FOUND 2 CRACKS APPROX 3/8 " LONG EA ON STRINGER 2L JUST AFT OF FR 75. REPAIRED STRINGER 2L AT FRAME 75 IAW SRM 53-00-03 FIG. 202 AND ETA-EM-5300-2534. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,032 hrs · 25,694 cycles

DURING IMBV INSPECTION FOUND CARGO DOOR AFT ANGLE AT FRAME 68 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED INSTALLATION OF FRAME 68 SHEAR CLIP IAW EO EM-53MR-1129. THE AIRCRAFT WAS RETUNRED TO SERVICE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 28,032 hrs · 25,694 cycles

FOUND 2 CRACKS APPROX 3/8 " LONG EA ON STRINGER 2R JUST AFT OF FR 75. REPAIRED STRINGER 2R AT FRAME 75 IAW SRM 53-00-03 AND ETA-EM-5300-2534. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — DAMAGED (RT AILERON) · airframe 28,032 hrs · 25,694 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT AILERON DAMPNER ATTACHMENT FITTING HAS SEVERAL NICKS AND GOUGES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DAMPNER FITTING ON RIGHT AILERON IAW EO EM-27MR-112. THE AIRCRAFT WAS RETUNRED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 28,032 hrs · 25,694 cycles

DURING IMBV INSPECTION FOUND CARGO DOOR SILL CORRODED. REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 28,072 hrs · 25,729 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY LIGHT STRIP (ON AIRCRAFT SIDE NEAT CONNECTOR) HAS BROKEN INSULATION. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING IAW AMM 33-50-00, AND THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 27,768 hrs · 25,482 cycles

ON FLIGHT 4304 THE CREW ABORTED TAKEOFF, LOW SPEED (40 KNOTS) DUE TO VISABLE SMOKE AND OIL SMELL IN COCKPIT. SMOKE ALSO VISABLE IN CABIN AS REPORTED BY FLIGHT ATTENDANT. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE AIRCRAFT WAS INSPECTED TO THE EXTENT NECESSARY FOR A FERRY FLIGHT AND FOUND TO BE IN A SAFE CONDITION FOR A FERRY FLIGHT. ISOLATED SMOKE EVENT TO THE NR 1 ENGINE PER ETN EM-72-034-R4. REMOVED AND REPLACED THE LEFT ENGINE IAW W/C 71-000-00 OPC/LEAK CHECK GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,361 hrs · 25,444 cycles

DURING B INSPECTION FOUND THE LEFT PSU FILLER PANEL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT PSU FILLER PANEL EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-5-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 27,593 hrs · 25,329 cycles

ON FLIGHT 4078, THE CREW REPORTED THE MAIN CABIN DOOR WAS OCCASIONALLY HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED THE MAIN CABIN DOOR ROLLERS. NO FURTHER DEFECTS NOTED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED · airframe 27,298 hrs · 25,125 cycles

FLIGHT 3928, THE CREW REPORTED THAT PRIOR TO LEVELING OFF AT 10,000 FT AFTER DEPARTURE, RECEIVED A PITCH TRIM MAIN INOPERATIVE WARNING MESSAGE ON EICAS. AIRCRAFT DIFFICULT TO CONTROL. CAPTAIN REQUESTED PTRIM MAIN INOPERATIVE CHECKLIST IN AOM VOL 1. AOM PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY WAS DECLARED. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. VISUALLY INSPECTED EXTERIOR FOR ANY ABNORMALITIES OR DAMAGE, NONE REPORTED. AIRCRAFT REMOVED FROM SERVICE. PERFORMED FIRST OFFICER’S YOKE PITCH TRIM SERVICING IAW AMM 27-40-03. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — FAILED (NR 1 ENGINE) · airframe 24,436 hrs · 23,029 cycles

ON FLIGHT 3368 THE CREW REPORTED HYDRAULIC 1 LOW QUANTITY MESSAGE ON CLIMBOUT OF LIT, QUANTITY WAS AMBER TOP OF RANGE, AS FLIGHT PROGRESSED QUANTITY CONTINUED TO DROP. ENGINE HYDRAULIC PUMP NR 1 FAILED AND SYSTEM NR 1 FAILED, COMPLIED WITH ABNORMAL PROCEDURES, HYDRAULIC 1 FAIL AND ABNORMAL GEAR EXTENSION. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW EMB 145 AMM 29-10-03. THE OPERATIONAL AND LEAK CHECK WERE GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RUB STRIP — DAMAGED (PAX DOOR)

F/A REPORT PASSENGER DOOR IS HARD TO OPEN. SMOOTHED SHARP EDGE FROM UPPER DOOR RUB STRIP AS REQUIRED. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: ROLLER — LACK OF LUBE (CABIN DOOR)

MAIN CABIN DOOR HARD TO OPEN. LUBED ROLLERS.

Part: DOOR — BINDING (CABIN) · airframe 24,099 hrs · 22,782 cycles

FOR FLIGHT 3989 CONTRACT MAINTENANCE HAD A DIFFICULT TIME OPENING TO CABIN DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. OPEN AND CLOSED THE MAIN DOOR IAW EMB AMM 52-18-00 NO DEFECTS NOTED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WASHER — WORN (CABIN DOOR) · airframe 23,541 hrs · 22,369 cycles

FOR FLIGHT 3242 THE CREW REPORTED THE FLIGHT ATTENDANT COULD NOT OPEN THE MAIN DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED WASHERS BETWEEN ARM LOWER FITTING NR 1 AND FITTING NR 2 IAW ETN EM 52-013R1. THE DOOR OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 22,090 hrs · 21,315 cycles

DURING FLIGHT NUMBER 4188 LOW SPEED ABORT DUE TO BAGG DOOR OPEN INDICATION ON EICAS AS THRUST LEVERS WERE ADVANCED. THE AIRCRAFT WAS NOT REMOVED FROM SERVICE. RE-ADJUSTED BAGGAGE DOOR FORWARD MICROSWITCH IAW EMB 145 AMM 52-76-01. OPC GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 19,762 hrs · 19,413 cycles

DURING FLIGHT 4379, THE CREW REPORTED A FAINT ELECTRICAL ODOR IN THE CABIN AND COCKPIT. AIRCRAFT REMOVED FROM SERVICE. INSPECTED GPU, CABIN AND FLIGHT DECK LIGHTING, FLASHLIGHTS AND HOT JUGS. NO DEFECTS NOTED. OPERATIONAL CHECKS OF PACKS ARE GOOD IAE AMM 21-20-00. NO ABNORMAL OR ELECTRICAL SMOKE ODORS NOTED AT ANY TIME. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,322 hrs · 13,506 cycles

AFT SERVICE DOOR SILL CORRODED. REPAIRED DOOR SILL BY CUTTING OUT DAMAGE AND INSTALLED DOUBLER IAW SRM 53-21-10. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,322 hrs · 13,506 cycles

LT FWD IB SEAT TRACK CORRODED FROM FRAME 17 TO 24. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE

Part: CLAMP — OUT OF ADJUST (RADOME) · airframe 13,188 hrs · 13,380 cycles

NOSE VIBRIBATION IN FLIGHT. READJUSTED RADOME ATTACHMENT CLAMPS, PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED, RETURNED AIRCRAFT TO SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

CID - FLT 4309 - FLAP FAIL MESSAGE ON APPROACH, FLAPS REMAINED AT 0 DEGREES. (M)

Part: UNKNOWN — ODOR (COCKPIT)

DURING CRUISE AT FL 370, CREW NOTED PITOT HEAT 3 FAIL. CREW FOLLOWED AOMM AND UPON RESETTING SYSTEM NOTED ELECTRICAL ODOR IN COCKPIT AND SHORTLY NOTED A HAZE AROUND FLOOR LIGHTS. AIRCRAFT DIVERT TO JAX AND DECLARED EMERGENCY LANDING. AIRCRAFT LANDED SAFELY. DUE TO HAZE AND ODOR IN THE CABIN, PASSENGERS DEPLANED BY STAIRS AT TAXI WAY. ALSO, GOT RUDDER 1 SYSTEM FAIL. REMOVED AND INSTALLED SERVICEABLE RIGHT CONSOLE, IAW EMB 145 AMM 25-12-08, OPS CHECKED GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: STRINGER — CHAFED (FUSELAGE)

DURING INSPECTION, 652 STRINGER 19R WAS FOUND TO BE CHAFED AT AFT FAIRING CUTOUT. BLENDED THE CHAFE AND PERFORMED EDDY CURRENT INSPECTION WITH NO CRACKS NOTED. FABRICATED A DOUBLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 53-24-02. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING INSPECTION STRINGER 19L WAS FOUND TO BE CHAFED AT AFT FAIRING CUTOUT. BLENDED THE CHAFE AND PERFORMED EDDY CURRENT INSPECTION WITH NO CRACKS NOTED. FABRICATED A DOUBLER, TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 53-24-02. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, A PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED REPAIR. FABRICATED AN EXTERNAL ANGLE, FABRICATED A FILLER AND THREE SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 53-21-10 FIG 201. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING INSPECTION, FOUND STRINGER 19L WAS FOUND TO BE CHAFED AT AFT FAIRING CUT OUT. BLENDED THE CHAFE AND PERFORMED EDDY CURRENT INSPECTION WITH NO CRACKS NOTED. FABRICATED A DOUBLER, TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 53-24-02. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER SILL. INSTALLED SERVICEABLE SILL IAW EMB SRM, SRM EMB 145/1142 REV 28 CHAPTERS 51-20-01, 51-20-03, 51-40-02, 51-40-04 AND 51-40-06. (M)

Part: ACM — SEIZED (CABIN COOLING)

ORD - FLT 4023 - AFTER RETURNING TO THE GATE, THE CREW REPORTED THE CABIN FILLING WITH SMOKE. MAINTENANCE FOUND AN AIR CYCLE MACHINE SEIZED. THE AIR CYCLE MACHINE WAS REMOVED AND REPLACED IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: DRAIN LINE — LOOSE (APU)

AFTER TAKE OFF CREW REPORTED THE LAVATORY SMOKE WARNING CAME ON FOR 5 MINUTES. FLIGHT ATTENDANT ALSO REPORTED AN MIST IN THE AIR WITH A BURNING SMELL. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO FIELD WITH NO FURTHER INCIDENTS REPORTED. CONTRACT MAINTENANCE ISOLATED SMELL TO APU. MAINTENANCE FOUND A LOOSE OIL DRAIN LINE WAS TIGHTENED AND AN OPERATIONAL CHECK WAS COMPLIED WITH. AIRCRAFT WAS THEN RETURNED TO SERVICE.