N650AE

Part: SENSOR — FAULTED (BRAKE TEMP) · airframe 52,705 hrs · 50,264 cycles

AT ABOUT 85 TO 90 KTS, BRAKE OVER HEAT EICAS MESSAGE WITH LEFT INBD BRAKE INDICATION HIGHER. ON GROUND LEFT INBD TEMP FLUXUATES MEL 10AUG25 12:12 PHL C22214 32-2-2 BRAKE TEMPERATURE INDICATIONS FACT 12AUG25 12:37 SBY RAR BRAKE TEMP SENSOR #200 IAW AMM 32-47-01. OPS CHECK GOOD.

Part: NONE — NONE (NONE) · airframe 52,160 hrs · 49,637 cycles

AT LEAST TWO LIGHTNING STRIKES IN FLIGHT, FLIGHT CREW AND CABIN BOTH REPORTED ELECTRICAL FUMES. (NO LOSS OF AVIONICS, NO EICAS MSGS) FACT 15MAY25 03:04 PHL PERFORMED LIGHTNING STRIKE INSPECTION IAW AMM REF. 05-50-01 AND FOUND NO DEFECTS NOTED AT THIS TIME. A/C OKAY FOR SERVICE.

Part: NONE — NONE (NONE) · airframe 52,160 hrs · 49,637 cycles

AT LEAST TWO LIGHTNING STRIKES IN FLIGHT FLIGHT CREW AND CABIN BOTH REPORTED ELECTRICAL FUMES(NO LOSS OF AVIONICS, NO EICAS MSGS) FACT 15MAY25 03:04 PHL PERFORMED LIGHTNING STRIKE INSPECTION IAW AMM REF. 05-50-01 AND FOUND NO DEFECTS NOTED AT THIS TIME. A/C OKAY FOR SERVICE.

Part: DISPLAY — ODOR (ZONE 200) · airframe 51,626 hrs · 49,027 cycles

ON DESCENT BURNING SMELL NOTICED IN FLT DECK FOR APROX 1 MIN BEFORE SMELL DISSIPATED. DU 4 O/H MSG DISPLAYED FOR APROX 3SECS. ENGINE BLEEDS AND PACK NORMAL OPERATION FACT 13FEB25 09:12 CLT R/R DISPLAY UNIT 4 IAW AMM 34-22-01. EFIS OPS CHECK GOOD. NO ABNORMAL SMELLS NOTED. AIRCRAFT GOOD FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSERS) · airframe 51,264 hrs · 48,653 cycles

E2 THRUST REVERSER REVERSE DISAGREE REJECTED TAKE OFF 80 KNOTS. FACT 04DEC24 05:21 PHL COULD NOT DUPLICATE. R/R RELAY K0378 K0264 K0400 IRW AMM 20-13-02 FOR POSITIVE MAINTENANCE. OPS CHECK GOOD IRW AMM 78-31-01. OK FOR SERVICE AT THIS TIME.

Part: ENGINE — FAILED (NR 1) · airframe 51,094 hrs · 48,468 cycles

CLIMBING THROUGH 3000FT HEARD A BANG AND NO. 1 ENGINE SUDDENLY FAILED. LOST ITT INDICATION. N1 CONTINUED TO SPIN AT 13 PRESENT. OIL PRESSURE ZERO. FACT 04NOV24 08:34 PHL R/R #100 ENGINE PER W/C 71-00-00

Part: STUB FRAME — CRACKED (FUSELAGE) · airframe 50,357 hrs · 47,585 cycles

00153 L/H STUB FRAME ABOVE WINDSHIELD POST CRACK AT LOWER CORNER. RAR L/H STUB FRAME PN: 123-07751-005 ABOVE WINDSHIELD POST IAW EMB 145 SRM 51-40-02

Part: STUB FRAME — CRACKED (COCKPIT) · airframe 50,357 hrs · 47,585 cycles

00154 R/H STUB FRAME ABOVE WINDSHIELD POST CRACK AT LOWER CORNER. RAR R/H STUB FRAME PN: 123-07751-006 ABOVE WINDSHIELD POST IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (FRM 20) · corrosion level 2 · airframe 50,357 hrs · 47,585 cycles

00161 RH FLOOR SILL IS CORRODED AT FS. 20. REPAIRED IAW PIEDMONT EO1-53-24-0320.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,357 hrs · 47,585 cycles

00139 CENTER FUSELAGE I - SMALL DENT LOCATED AFT OF MAIN DOOR REQUIRES PERMANENT REPAIR. PAIRED PERMANENTLY ON CENTER FUSELAGE 1 - SMALL DENT LOCATED AFT OF MAIN DOOR IAW EMB 145 SRM 53-21-01

Part: SKIN — DAMAGED (RUDDER) · airframe 50,357 hrs · 47,585 cycles

00105 TOP RH AFT CORNER OF RUDDER 1 DAMAGED. REMOVED DAMAGE IAW EMB 145 51-10-05 STEP #3 DAMAGE DID NOT PENETRATE CLAD LAYER.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,357 hrs · 47,585 cycles

00105 CENTER FUSELAGE I - SMALL DENT LOCATED AFT OF MAIN DOOR REQUIRES PERMANENT REPAIR. REPAIRED PERMANENTLY ON CENTER FUSELAGE 1 - SMALL DENT LOCATED AFT OF MAIN DOOR IAW EMB 145 SRM 53-21-01

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,588 hrs · 45,538 cycles

DURING CLIMB AT 16,000 FT F/A REPORTED LOUD AIR RUSHING NOISE AND BURNING SMELL. FACT 09MAY23 00:57 CLT R&R RECIRC FAN #1 IAW AMM 21-24-01 (SHORT SIGN) R&R FUSE F0059 AND CONTACTOR K0189. FAN BLEW NEW FUSE. SEE LP 286540-1 FOR FUSE REPLACEMENT AND FAN OPS CHECK

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,516 hrs · 45,438 cycles

LOUD NOISE FROM NLG AREA FLY BY TOWER SHOWED NLG DOOR OPEN. UNSURE OF NLG POSITION. FLIGHT WAS AT 310K WHEN NOISE ORIGINATED. HISTORY: NO FACT 25APR23 16:38 MDT R&R NLG DOOR SOLENOID VALVE OPS CHECK GOOD. OK FOR SERVICE. REF AMM 32-33-02.......NOTE: FAULT DUPLICATED ON GROUND MULTIPLE TIMES AND ONCE REPAIRED. OPS CHECK GOOD MULTIPLE TIMES

Part: NONE — NONE · airframe 46,414 hrs · 43,026 cycles

MDIS 650 26-15 2594831 18FEB22 RIC CLOSE BAGGAGE BAY FIRE PUSHBUTTON DOES NOT ILLUMINATE WHILE PRESSING FIRE DET PUSH BUTTON FACT 18FEB22 08:49 RIC R+R'D #200 BAG BAY SMOKE DETECTOR IN REF. TO AMM TASK 26-15-01-000/400-801-A OPS CHECK GOOD OK FOR SERVICE

Part: NOT REPORTED — NOT REPORTED · airframe 46,298 hrs · 42,881 cycles

PDIS 650 78-30 2594602 24JAN22 CHO CLOSE E2 REV DISAGREE MSG ON EICAS DURING TAKEOFF ROLL FACT 26JAN22 16:45 ROA REMOVED AND REPLACED #2 THRUST REVERSER ASSY PER W/C 78-31-01. REMOVED AND REPLACED WIRING HARNESS W408 PER AMM 78-35-01. SEE HA-300 SEQ# 4, 9 & 10 FOR SIGN OFFS. OPS & LEAK CHECKS GOOD, CLEAR MEL. RE-ACTIVATED #2 T/R PER AMM 78-31-01. P/N ON/OFF 145-77751-615 S/N ON TR0360, S/N OFF TR136.

Part: NONE — NONE · airframe 46,267 hrs · 42,846 cycles

PDIS 650 78-33 2598492 12JAN22 CLT ASSGN ENG 2 REV DISAGREE ON TAKE OFF ROLL. 31933 00 AKR HISTORY: . MEL 12JAN22 19:07 CLT C01206 78-2 ENG 1(2) REV DISAGREE MESS CURRENTLY ON THE MEL R&R RELAY K0640 AS REQ OPS CHECK GOOD NO CMC OR EICAS MSG OK FOR SERVICE AT THIS TIME.REACTIVATED #2 T/R.NO FADEC MSG.

Part: NONE — NONE · airframe 46,266 hrs · 42,843 cycles

PDIS 650 78-33 2598471 10JAN22 PHL CLOSE ENG 2 REV DISAGREE ON TAKEOFF ROLL FACT 11JAN22 07:10 PHL REMOVED AND REPLACED #2 TR ICU IAW AMM 78-33-01 OPS CHECK LEAK CHECK GOOD OK FOR SERVICE

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893076 - CENTER CABIN FLOOR BEAM SEAT TRACK #3 IS CORRODED ... REMOVED CORRODED SEAT TRACK AND INSTALLED SERVICEABLE CENTER SEAT TRACK #3 IAW EMB 145 AMM 53-01-06

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E892909 - RH CABIN #1 FLOOR SILL CORRODED. ... RAR RH CABIN #1 FLOOR SILL IAW EMB1145 SRM 51-40-02

Part: NONE — NONE · airframe 46,263 hrs · 42,841 cycles

E892626 - DENT ON BAGGAGE DOOR LOWER FRAME ... UPON FURTHER INVESTIGATION FOUND DENT TO BE ON BAGGAGE DOOR LOWER OUTBD "L" PROFILE. RAR "L" PROFILE ON LOWER BAGGAGE DOOR IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E892893 - CARGO DOOR SILL CORRODED ...REMOVED DRILLED AND INSTALLED SERVICEABLE CARGO DOOR LRW CENTER SILL IAW EMB 145 SRM 51-20-03 AND SRM 51-40-02.

Part: NONE — NONE · airframe 46,263 hrs · 42,841 cycles

E892890 - CARGO FR 68 GOUGED AT NUTPLATE HOLES (6EA) BETWEEN STGRS 01L/08L .... INSTALLED 3 EA DOUBLER REPAIRS FOR FR 68 NUTPLATE REPAIR POSITION #3, #4 AND #6 IAW ETD2021-145-042792 REV. B AND PIEDMONT EO1-53-21-0366.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893029 - CORROSION IN GALLEY AREA ON SERVICE DOOR CENTER SILL ... INSTALLED INTERNAL DOUBLER AT GALLEY SERVICE DOOR CENTER SILL AT FWD NUTPLATE HOLE IAW EMB 145 SRM 53-21-02 RE, ITEM 2, FIG. 201 AND PIEDMONT EO1-53-21-0362.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E892910 - RH CABIN #2 FLOOR SILL CORRODED ... REMOVED AND REPLACED RH CABIN #2 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893072 - CENTER FLOOR BEAM SEAT TRACK GUESSET #3 IS CORRODED. ... REMOVED AND INSTALLED SERVICEABLE CENTER FLOOR BEAM SEAT TRACK GUSSET #3 IAW EMB145 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893018 - CORROSION ON LH OTBD #2 SEAT TRACK ... RAR LH OUTBD#2 SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: NONE — NONE · airframe 46,263 hrs · 42,841 cycles

E893451 - FUSELAGE SKIN IS CRACKED BETWEEN FR 80-81 NEAR STR 13R ... COMPLETED REPAIR OF FUSELAGE SKIN BTW FR 80-81 STGR 13R-15R IAW ETD# ETD2021-145-041044 AND PIEDMONT EO1-53-21-0356.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893576 - LH AILERON TO DAMPER FITTING OTBD HAT BUSHING MIGRATED ... RAR LH AILERON DAMPER FITTING IAW EMB 145 SRM 51-40-02, ETD2021-145-041146 AND PIEDMONT EO1-05-21-0365

Part: NONE — NONE · airframe 46,263 hrs · 42,841 cycles

E892012 - LH SIDE FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND FASTENERS ON FRAME 79 (1) EA ... REPAIRED LH SIDE FUSELAGE SKIN AROUND FASTENERS ON FRAME 79 (1) EA IAW EMB 145 SRM 53-32-01-RE, ITEM 9, FIG 213 AND PIEDMONT EO1-53-21-0360.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893071 - L/H CABIN FLOOR SILL #4 IS CORRODED ... RAR LH #4 CABIN FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893014 - CORROSION ON LH OTBD #5 SEAT TRACK ... REMOVED AND REPLACED LH OTBD #5 SEAT TRACK IAW EMB 145 AMM 53-01-06

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E892916 - RH FLOOR SEAT TRACK PITTED BETWEEN FR27-28 ... RAR RH FLOOR SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893033 - CORROSION IN GALLEY AREA ON CENTER GUSSET AT FRAME 22 ... REMOVED AND REPLACED CENTER GUSSET AT FRAME 22 IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · airframe 46,263 hrs · 42,841 cycles

E891808 - LIGHTNING STRIKE ON FUSELAGE SKIN AT FR 24-25 AND STR 17R-18R ... PERFORMED REPAIR ON FUSELAGE SKIN AT FR 24-25 AND STR 17R-18R. IAW EMB 145 SRM 53-22-01 FIG 204 SHEET 1 AND PIEDMONT EO1-53-21-0369.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893075 - L/H CABIN FLOOR BEAM SEAT TRACK #4 IS CORRODED ... RAR L/H CABIN FLOOR BEAM SEAT TRACK #4 IAW EMB 145 AMM 53-01-06

Part: NONE — NONE · airframe 46,263 hrs · 42,841 cycles

E892937 - RH AILERON INBD HINGE ATTACHMENT BOLT HOLE GOUGED ... REMOVED AND INSTALLED SERVICEABLE RH AILERON INBD HINGE FITTING IAW EMB145 SRM 51-40-02 AND ETD2021-145-040901 AND PIEDMONT EO1-05-21-0365.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893015 - CORROSION ON LH OTBD #4 SEAT TRACK ... COMPLETED INSTALLATOIN OF LH OUTB #4 SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893034 - CORROSION IN GALLEY AREA ON CROSS BEAM AT FRAME 20 ... REMOVED CORRODED CROSSBEAM, DRILLED UP AND INSTALLED NEW FLOOR CROSS BEAM AT FRAME 20 IN GALLEY AREA IAW EMB 145 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893044 - CORROSION IN GALLEY AREA ON CROSS FLOOR BOARD SUPPORT AT FRAME 19 ... REMOVED AND REPLACED CROSS FLOOR BOARD SUPPORT AT FRAME 19 IN GALLEY AREA IAW EMB145 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893042 - CORROSION ON PASSENGER DOOR ENTRY AFT FLOOR BOARD SUPPORT ... REMOVED DAMAGED SUPPORT AND INSTALLED SERVICEABLE PASSENGER DOOR ENTRY AFT FLOOR BOARD SUPPORT IAW EMB 145 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E892967 - CORROSION ON RH OTBD #3 SEAT TRACK ... RAR RH OUTBD #3 SEAT TRACK IAW EMB 145 AMM 53-01-06. TORQUE WRENCH #4401

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E892912 - LH CABIN #3 FLOOR SILL CORRODED. ... RAR LH #3 CABIN FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · airframe 46,263 hrs · 42,841 cycles

E892865 - L/H WING RIB 21 IS CRACKED ...INSTALLED SERVICEABLE REPAIR DOUBLER, FILLER, AND SHIM ON LH WING RIB 21 IAW EMB145 SRM 57-20-07 AND PIEDMONT EO1-57-21-0357.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893043 - CORROSION IN GALLEY AREA ON HAT BEAM AT FRAME 18 PREVIOUS REPAIR ... ACCOMPLISHED REPAIR DOUBLER ON R/ H HAT BEAM AT FRAME 18 IAW ETD2021-145-041321 AND PIEDMONT EO1-53-21-0348.

Part: NONE — NONE · airframe 46,263 hrs · 42,841 cycles

E892891 - FR 68 SHEAR CLIP CRACKED BETWEEN STGRS 06L/07L .... COMPLETED INSTALLATION OF SHEAR CLIPS REPAIR FOR FR 68 BETWEEN STGRS 06L/07L IAW EMB 145 SRM 53-31-04-RE, ITEM #2 AND TABLE 203 AND TABLE 205 AND PIEDMONT EO1-53-21-0367.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E892968 - CORROSION ON RH OTBD #2 SEAT TRACK ... RAR RH OTBD #2 SEAT TRACK DUE TO CORROSION IAW EMB-145 AMM 53-01-06.

Part: NONE — NONE · airframe 46,263 hrs · 42,841 cycles

E893647 - FR 73 CRACKED AT STR 17R ... REMOVED AND REPLACED FR-73 (LWR SECTION) IAW EMB 145 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E892969 - CORROSION ON RH OTBD #1 SEAT TRACK ... REMOVED AND REPLACED R/H OUTBD #1 SEAT TRACK IAW EMB 145 AMM 53-01-06, REINSTALLED RISER DUCT BETWEEN FR 29 AND FR 30 AFTER MTX IAW EMB 145 AMM 21-20-04

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893017 - CORROSION ON LH OTBD #3 SEAT TRACK ... RAR LH OTBD #3 SEAT TRACK IAW EMB 145 AMM 53-01-06

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E892915 - LH FLOOR SEAT TRACK PITTED BETWEEN FR29-30 ... REMOVED AND REPLACED LH FLOOR SEAT TRACK AT FR 29-30 IAW EMB 145 AMM 53-01-06. TQW USED EASI# 4401.

Part: NONE — NONE · airframe 46,263 hrs · 42,841 cycles

E892657 - BAGGAGE DOOR WEBBING IS GOUGED 5 EACH ONE ON PREVIOUS REPAIR ... NO. 4 AND 5 GOUGES FOUND TO BE WITHIN ALLOWABLE LIMITS, MATERIAL REMAINING AFTER BLEND OUT IAW EMB 145 SRM 52-30-01. REPAIRED 1, 2 AND 3 DOUBTERS ON CARGO DOOR INNER WEB IAW ETD2021-145-041226 AND PIEDMONT EO1-52-21-0353

Part: NONE — NONE · airframe 46,263 hrs · 42,841 cycles

E894729 - #3 R/H OVER WING BRACKET HAS MISSED DRILLED HOLE ON SKIN BETWEEN FR 49-50 STRINGER 14R-13R ... REPAIRED #3 R/H OVER WING BRACKET HOLE ON SKIN BETWEEN FR 49-50 STRINGER 14R-13R BY INSTALLING BUSHING IAW ETD2021-145-042169 AND PIEDMONT EO1-53-21-0354.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893041 - CORROSION ON PASSENGER DOOR ENTRY FWD FLOOR BOARD SUPPORT ... REMOVED DAMAGED SUPPORT AND INSTALLED SERVICEABLE PASSENGER DOOR ENTRY FWD FLOOR BOARD SUPPORT IAW EMB 145 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893012 - CORROSION ON LH OTBD #6 SEAT TRACK ... REMOVED CORROSION ON LH OUTD #6 SEAT TRACK IAW EMB145 SRM 51-10-03, FOUND TO BE OUTSIDE ALLOWABLE LIMITS IAW EMB145 SRM 53-00-11. CALIPERS EASI# 7496. REMOVED AND INSTALLED SERVICEABLE LH OTBD #6 SEAT TRACK IAW EMB 145 53-01-06.

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893326 - RH FUSELAGE DRAG ANGLE FWD SECTION AFT AREA HAS POSSIBLE CRACKS AT FASTENER HOLE AREAS MARKED ... COMPLETED INSTALLATION OF SERVICEABLE FWD DRAG ANGLE, AND PREVIOUS REPAIR ANGLE AND SHIMS AT FRAME 75 STRINGER 2R IAW EMB145 SRM 51-40-02, 53-31-01 ITEM 11, FIGURE 219, SHEETS 1-2 AND PIEDMONT EO1-53-21-0372.

Part: NONE — NONE · airframe 46,263 hrs · 42,841 cycles

E892866 - R/H WING RIB 21 IS CRACKED. ... COMPLETED FABRICATION, POSITIONING, AND DRILLING OF REPAIR DOUBLER, FILLER, AND SHIM FOR RH WING RIB 21 REPAIR IAW EMB145 SRM 57-20-07 AND PIEDMONT EO1-57-21-0358

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E892911 - LH CABIN #2 FLOOR SILL CORRODED ... REMOVED AND REPLACED LH CABIN #2 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893073 - L/H FLOOR BEAM SEAT TRACK GUESSET #4 IS CORRODED ... REMOVED AND REPLACED L/H FLOOR BEAM SEAT TRACK GUSSET #4 IAW EMB-145 SRM 51-40-02.

Part: NONE — NONE · airframe 46,263 hrs · 42,841 cycles

E895330 - LH PLYON YOKES SPAR II UPPER FLANGE FASTENER HOLE PREVIOUSLY OVERSIZED ... ACCOMPLISHED REPAIR OF LH PYLON YOKE SPAR II UPPER FLANGE FASTENER HOLE IAW ETD# ETD-2021-145-042799 REV. A. AND PIEDMONT EO1-54-21-0364

Part: NONE — NONE · airframe 46,263 hrs · 42,841 cycles

E891811 - LIGHTNING STRIKE ON FUSELAGE SKIN AT FR 26-27 AND STR 17R-16R ... ACCOMPLISHED RIVET REPAIR OF LIGHTNING STRIKE ON FUSELAGE SKIN AT FR 26-27 AND STR 17R-16R IAW EMB 145 SRM 53-00-01 ITEM 2B AND PIEDMONT EO1-53-21-0368.

Part: NONE — NONE · airframe 46,263 hrs · 42,841 cycles

E893582 - RH AILERON TO DAMPER FITTING LUG WORN ... REMOVED AND INSTALLED SERVICEABLE RH AILERON DAMPER FITTING IAW EMB145 SRM 51-40-02 AND ETD2021-145-041149 AND PIEDMONT EO1-05-21-0365

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893519 - CORROSION ON LH OTBD #1 SEAT TRACK - RAR LH OUTBD#1 SEAT TRACK IAW EMB 145 AMM 53-01-06

Part: NONE — NONE · corrosion level 2 · airframe 46,263 hrs · 42,841 cycles

E893062 - L/H CABIN FLOOR SILL #7 IS CORRODED ... RAR CABIN FLOOR SILL #7 IAW EMB 145 SRM 51-40-02.

Part: WARNING MESSAGE — FALSE INDICATION · airframe 46,231 hrs · 42,809 cycles

ON REJECTED T/O EICAS WARNING T/O NO CONFIG APPEARED WITH NO AURAL CALLOUT. T/S PERFORMED FIM TASK 31-51-00-810-804-A BLOCK 1 THROUGH BLOCK 7 R&R RELAY K0212 IAW AMM 20-13-02 OPS CHECK PERFORMED IAW AMM 31-51-00 OPS CHECK GOOD A/C OK FOR SERVICE AT THIS TIME.

Part: PUMP — FAILED (NR 1 HYD SYSTEM) · airframe 45,894 hrs · 42,426 cycles

HYD SYS 1 LOW QTY IN FLT ( HYD SYS 2 REMAIN FULL) R&R NR 1 ENG DRIVEN PUMP IAW EMB 145 AMM 29-10-03. OPS CHECK GOOD NO FURTHER LEAKS DETECTED A/C OK FOR SERVICE

Part: EICAS — FAULTY (COCKPIT) · airframe 45,136 hrs · 41,621 cycles

PDIS 650, 31-41, 13APR21 PHL CLOSE, 300 FEET AFTER ROTATION, EICAS DISPLAY FLASHED BRIGHTLY AND WENT BLANK MOMENTARILY FOLLOWED BY AN ELECTRICAL ODOR. R&R'D EICAS DISPLAY UNIT AS REQUIRED PER AMM 34-22-01-400-801-A, OPS CHECK IAW 34-22-00-700-801A GOOD ON GROUND AT THIS TIME, OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 44,744 hrs · 41,197 cycles

AFTER T/O FUMES WERE SMELLED, SIMILAR TO A WET MUSTY SOCK ODOR. GROUND RAN AIRCRAFT ENGINE NR 1 AND NR 2 ALSO OPERATIONS CHECKED AIRCRAFT AIR CONDITION SYSTEM. NO DEFECTS OR ABNORMAL SMELLS FOUND, IN REF TO FIM TASK 21-20-00-810-801-A. A/C OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 44,231 hrs · 40,618 cycles

SPOILER FAIL EICAS MESSAGE DISPLAYED ON TAKE OFF.CW FIM 27-63-00-810-802A STEPS 1-9, DETERMINED TO BE TRANSITORY. R+R SCU IAW 27-63-02 AND 27-63-01 FOR POSITIVE MAIN ACTION . OPS CHECK GOOD. OK FOR SERVICE

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 44,231 hrs · 40,618 cycles

SPOILER FAIL EICAS MESSAGE DISPLAYED ON TAKE OFF. CW FIM 27-63-00-810-802A STEPS 1-9, DETERMINED TO BE TRANSITORY. R & R SCU IAW 27-63-02 AND 27-63-01 FOR POSITIVE MAIN ACTION . OPS CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,836 hrs · 40,173 cycles

PDIS 650 21-01 2289391 11FEB20 PHL CLOSE CREW NOTICED FUMES DURING TAKE OFF. THEN WENT AWAY. FUMES CAME BACK IN CRUISE FLIGHT AND GOT STRONGER TH ROUGH DESCENT FACT 11FEB20 18:43 PHL EVALUATION FLIGHT REQUIRED. RAN BOTH PACKS TOGETHER AND SEPERATELY ON FULL COLD AND FULL HOT IN AUTO AND MANUAL MODE. DID SAME SEQUENCE WITH APU BLEED AND ENGINE BLEED. RAN HYD PUMPS AS WELL TO SEE IF A SMELL COULD BE SMELT IN COCKPIT. ACFT WAS AT 90% N2 FOR AFEW MOMENTS AS WELL. NO SMELL EVER NOTED

Part: UNKNOWN — ODOR (COCKPIT) · airframe 43,829 hrs · 40,167 cycles

OIL FUME SMELL-VERY APPARENT IN COCKPIT- WHEN BOTH PACKS ARE ACTIVATED THROUGHOUT WHOLE FLIGHT. FOUND LOOSE DUCT IN #1 PACK. OPERATED APU AND BOTH ENGINES AFTER TIGHTENING DUCTS WITH BOTH PACKS ON AND FULL HEAT, NO SMELL PRESENT. OK FOR SERVICE AT THIS TIME.

Part: RELAY — FAULTED (RUDDER SYS) · airframe 43,793 hrs · 40,126 cycles

EICAS CT MESS, RUDDER SYS 2 INOP, IN FLT (TAKE-OFF). R+R RUDDER #2 PRESSURE SWITCH IAW AMM 27-23-04. OPS CHECK GOOD OK FOR SERVICE. EICAS MESS, RUDDER SYS 2 INOP, IN FLT. T/S IAW FIM TASK 27-23-00-810-802-A. FOUND RUDDER PRIORITY RELAY K0384 TO AT FAULT. R/R'D RELAY IAW MM 20-13-02/400, OPS CK GOOD TO 160 KTS.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 43,772 hrs · 40,104 cycles

STRONG FUMY SMELL IN FLT DECK DURING ALL PHASES OF FLIGHT.MORE NOTICEABLE ON GROUND....FIX:PERFORMED HIGH POWER ENGINE RUNS WITH CREW. COULD NOT DUPLICATE ANY SMELLS WHILE ON APU,ENGINES AND WITH BOTH PACKS ON. A/C OK FOR SERVICE AT THIS TIME

Part: COMPUTER — INOPERATIVE (STALL PROTECTION) · airframe 43,655 hrs · 39,980 cycles

PDIS 650 27-36 2289051 05JAN20 PHL CLOSE SPS 2 INOP AND SPS ADVANCED DURING REJECTED TAKEOFF FACT 05JAN20 20:15 PHL PERFORMED OPS CHECK IAW AMM 27-26-00. DETERMINED FAU LT ON STALL PROTECTION COMPUTER. R&R SPC COULDN'T DU PLICATE FAULT ON GROUND. A/C OK FOR SERVICE.

Part: A/C PACK — ODOR (NR 1) · airframe 43,274 hrs · 39,565 cycles

PDIS 650 21-50 1891911 27OCT19 DCA CLOSE BURNING RUBBER SMELL NOTICED IN CABIN AND COCKPIT. S MELL WENT WHEN PACK 1 WAS TURNED OFF. FACT 27OCT19 02:33 ALB MX INSP AND DETERMINED SMELL IS ONLY ASSOCIATED WITH PACK 1. OPERATED BOTH PACK SYSTEMS FOR 30 MINUTES FROM COLD TO HOT AND FOUND NO IRREGULAR SMELLS. WORK WAS DONEIAW E145 AMM 21-00-00 OPS CHECK GOOD MEL 21-13-2 CLOSED.

Part: ACM — SMOKE (RIGHT) · airframe 43,254 hrs · 39,539 cycles

SMOKE FOUND IN CABIN DURING FLIGHT....FIX: R&RD RH ACM, MAINT FOUND FROZEN, IAW AMM 21-51-03. OPS AND LEAK CHECK GOOD.OK FOR SERVICE. NO SMOKE FOUND WITH ENGINES RUNNING. NOTE: CREW REPORTED EMERGENCY, NO EVACUATION, NO EMERGENCY EQUIPMENT USED

Part: RELAY — BURNED (PITOT) · airframe 42,252 hrs · 38,420 cycles

NDIS 650 05-50 0001550 24APR19 RIC CLOSE PITOT NR 3 RELAY K0058 AND BASE VISIBLY BURNT AND DEFORMED RELAY K0057 WAS PHYSICALLY DAMAGED AND SILICONE GASKET WAS STICKING AND NOT RETAINING ORIGINAL FORM 34793 00 SJU FACT 24APR19 10:50 RIC RR RELAY K0058 AND K0057 AND RELAY BASE K0058 IAW FCD 1-30-16-0276 PITOT NR 3 RELAYS CONFORMITY.

Part: FLOOR SUPPORT — DENTED (FRAMES 49-50) · airframe 42,248 hrs · 38,418 cycles

DENT ON RH OMEGA BEAM BETWEEN FR. 49-50-C/A-ACCOMPLISHED REPAIR ON RH OMEGA BEAM BETWEEN FR49 AND 50 IAW ERS-EM-5300-3734 AND EMB145 SRM 53-23-10

Part: CHANNEL — OUT OF LIMITS (FRAME 22) · airframe 42,248 hrs · 38,418 cycles

SERVICE DOOR CUT-OUT FRAME 22 AFT LOWER CORNER OUT OF LIMITS.-C/A-ACCOMPLISHED SERVICE DOOR CUTOUT FR22 REPAIR IAW ERS-EM-53MR-3728

Part: FIREWALL — CANNING (APU BAY) · airframe 42,248 hrs · 38,418 cycles

APU FIREWALL AT RH UPPER CORNER IS OIL CANNING-C/A-REPAIRED APU FIREWALL IAW ERS-EM-49MR-141

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 42,248 hrs · 38,418 cycles

#8 EMERGENCY LIGHT STRIP WIRE BROKEN-C/A-REMOVED AND REPLACED # 8 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 42,248 hrs · 38,418 cycles

CENTER AISLE CROSSMEMBER AT FRAME 25 IS CORRODED. C/A-COMPLETE:REMOVED AND REPLACED CENTER AISLE CROSSMEMBER AT FRAME 25 IAW SRM 53-22-10, ETN-EM-53-139R4, AND ETN-EM-53-150R2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,248 hrs · 38,418 cycles

PREVIOUS REPAIR IS CORRODED ON CENTER OMEGA BEAM BETWEEN FRAMES 24-25. C/A-COMPLETE:REMOVED CORROSION ON PREVIOUS REPAIR ON CENTER OMEGA BEAM BETWEEN FRAMES 24-25 VIA BLENDING IAW SRM 51-10-03.

Part: TRANSDUCER — FAILED (RT ENGINE) · airframe 40,925 hrs · 37,170 cycles

DIVR STL E2 A/I ICE FAIL IN ICING CONDITIONS / EMER DECL. DEFERRED E2 A/I VLV M PROCEDURES C/W. FOUND CMC MSG E2 A/ICE VALVE FAIL, E2 A/ICE LOW PRESS, AND A/ICE OVERPRESS REMOVED AND REPLACED RT A/ICE VALVE IAW AMM 30-21-01 AND REMOVED AND REPLACED TRANSDUCER IAW AMM 30-21-06 OPC GOOD NO DEFECTS NOTED AT THIS TIME MEL RESTORED END. ENGINE ANTICE/VALVE P/N C146009-4 S/N 1397.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 40,880 hrs · 37,124 cycles

ON DESENT TO LANDING PASSING THROUGH FL 240, AURAL ALERT CABIN AND CABIN ALT REACHED 11,000 FT. TS PRESN AUTO FAIL MSG PER FIM 21-31-00-810-801-Z. R&R DIGITAL CONTROLLER IAW AMM 21-31-01-000-801-A/21-31-01-400-801-A FNC TASK 21-31-00-700-802-A GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 40,845 hrs · 37,096 cycles

ON DESCENT TO LANDING AUTO MODE PRESS FAIL. TS PRESN AUTO FAIL MSG PER FIM 21-31-00-810-801-Z. REMOVED AND REPLACED DIGITAL CONTROLLER IAW AMM 21-31-01-000-801-A/21-31-01-400-801-A FNC TASK 21-31-00-700-802-A.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 39,502 hrs · 35,926 cycles

AFT FA FLASHLIGHT HOLDER BROKEN. R&R AFT FA'S FLASHLIGHT HOLDER BRACKET IAW AMM 33-50-16 OPS CHK GOOD AT THIS TIME LED LIGHT IS ON.

Part: RHEOSTAT — FAILED (FLOODLIGHT PANEL) · airframe 39,143 hrs · 35,548 cycles

ELECTRICAL BURNING ODOR ENROUTE, DESCENT & LANDING, ODOR IN COCKPIT AND NEAR F/A JUMPSEAT. INSPECTED AND FOUND THE CAPTAIN'S FLOODLIGHT RHEOSTAT TO BE AT FAULT. REMOVED AND REPLACED THE INSTRUMENT AND CONTROL PANEL LIGHT PANEL ASSEMBLY IAW AMM 20-13-10 AND OPS CHECKED GOOD IAW 33-12-00, RAN BOTH BLEEDS, PACKS, WINDSHIELD HEAT, ALL COCKPIT LIGHTS & SYSTEMS, NO SMOKE OR BURNING ELECTRICAL ODOR NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,862 hrs · 34,352 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-50-10-000-801-A, & 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 37,545 hrs · 34,064 cycles

MAIN DOOR HARD TO OPEN AND CLOSE. REMOVED BRACKET AND BELLCRANK BOLT IAW AMM 52-18-02 ALL WORK ACCOMPLISHED ON NRWC 650-DFW-03000, 03001, AND 03002. PERFORMED OPERATIONAL CHECK IAW AMM 52-18-00 ON MAIN CABIN DOOR. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 37,510 hrs · 34,030 cycles

FLIGHT ATTENDANT FORWARD FLASHLIGHT RED CHARGING LIGHT NOT ILLUMINATING. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 33-50-16 OPS CHECKED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 37,349 hrs · 33,872 cycles

NR 3 FLOOR PROX LIGHT STRIP BROKEN. REMOVED AND REPLACED NR 3 FLOOR PROX LIGHT STRIP IAW AMM 33-50-12. OPS CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 37,349 hrs · 33,872 cycles

LT NR 5 EMERGENCY LIGHT STRIP BROKEN. REMOVED AND REPLACED LT NR 5 EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECK GOOD.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 37,349 hrs · 33,872 cycles

POSSIBLE CRACK LOCATED APPROX 1" BELOW CARGO DOOR HANDLE CUTOUT. INSTALLED REPAIR DOUBLER, CARGO DOOR IAW ERS-EM-52MR-661.

Part: FRAME — CHAFED (FUSELAGE) · airframe 37,349 hrs · 33,872 cycles

CHAFE ON FR 61 BETWEEN STGRS 4R-5R. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-2442. DOUBLER P/N 145-64146-001.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,349 hrs · 33,872 cycles

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

Part: TRUNNION — CRACKED (RT MLG) · airframe 37,349 hrs · 33,872 cycles

RT AFT UPPER TRUNNION CRACKED. INSTALLED SERVICEABLE RT MLG AFT UPPER TRUNNION IAW ERS-EM-57MR-731.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,349 hrs · 33,872 cycles

CORROSION IN GALLEY AREA ON RT OMEGA BEAM FRAME 23 AT PREVIOUS REPAIR. INSTALLED DOUBLER AT RT OMEGA BEAM AT FR 23 IAW ERS-EM-53MR-2447.

Part: TRUNNION — CRACKED (LT MLG) · airframe 37,349 hrs · 33,872 cycles

WHILE PERFORMING HFEC INSPECTION ON LT MLG AFT UPPER TRUNNION, FOUND TRUNNION TO BE CRACKED. FREQUENCY 400KHZ,ANGLE 130 DEGREES, H-GAIN 63.6,V-GAIN 77.6. USED EASI 6581. INSTALLED SERVICEABLE LT MLG AFT UPPER TRUNNION IAW ERS-EM-57MR-722.

Part: FITTING — CRACKED (LT ENGINE) · airframe 37,349 hrs · 33,872 cycles

LT ENGINE FWD LOWER YOKE CRACKED. REMOVED AND REPLACED LT FWD PYLON LOWER YOKE IAW EO EM-54MR-386.

Part: CONNECTOR — BROKEN (CABIN) · airframe 37,349 hrs · 33,872 cycles

UNDER FLOOR BOARD PANEL 251DF BROKEN OFF SPLICE ON AIRCRAFT SIDE FOR LIGHT STRIP. REPLACED CONNECTOR ON AIRCRAFT SIDE FOR LIGHT STRIP UNDER FLOOR BOARD PANEL 251DF IAW SWPM 20-21-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,349 hrs · 33,872 cycles

RT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 AND ABOVE STRINGER 2R, APPROX 3/8' LONG. INSTALLED REPAIR DOUBLER, FILLER, SHIM DRAG ANGLE ON RT UPPER FUSELAGE AFT OF FRAME 75 AND ABOVE STRINGER 2R IAW SRM 53-31-01. SEE WIPS AND TASKS FOR DETAILS.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 37,349 hrs · 33,872 cycles

POSSIBLE CRACK LOCATED APPROX 1'' BELOW CARGO DOOR HANDLE CUTOUT. INSTALLED REPAIR DOUBLER, CARGO DOOR IAW ERS-EM-52MR-661. SEE TASKS AND WIPS FOR DETAILS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,060 hrs · 32,700 cycles

EMERGENCY MAIN DOOR LIGHT INOPERATIVE. R & R EMER MAIN DOOR LAMP IAW AMM 33-50-10. OPERATIONS CHECK WAS GOOD AT THIS TIME.

Part: CONTROL MODULE — FAULTY (CABIN) · airframe 35,956 hrs · 32,615 cycles

CABIN COVE LIGHTS WILL NOT TURN ON. FLIGHT ATTENDANT SMELLED SOMETHING. R & R WITH SERVICEABLE SIDEWALL LIGHT CONTROL MODULE IAW AMM 33 21 01. OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,285 hrs · 32,023 cycles

MAIN DOOR EMER LIGHT INOPERATIVE. RELAMPED MAIN DOOR EXTERNAL EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: TARGET — OUT OF ADJUST (NLG) · airframe 35,195 hrs · 31,934 cycles

AFTER TAKEOFF & AFTER LG AIR & GND FAIL MSG RECEIVED, THRUST 1 - 2 REVERSER DISAGREE CAUTION MSG ON EICAS. AFTER LANDING MSG WENT AWAY, FOUND MSG RELATED TO AFOREMENTIONED NLG WOW SWITCH TARGET ADJUSTMENT, REF THIS AML PAGE ITEM 1. MSG NO LONGER IN VIEW AFTER NLG WOW TARGET WAS ADJUSTED. COMPLIED WITH OPERATIONS CHECK OF THRUST REVERSERS IAW AMM 78-31-01-700-801-A. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,975 hrs · 31,700 cycles

MAIN DOOR HINGE, EMER LIGHT INOPERATIVE. R & R EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,932 hrs · 31,658 cycles

LEFT FWD LOWER FAIRING, EMER LIGHT INOPERATIVE. R & R LT FWD LOWER FAIRING EMER LIGHT LAMP IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 34,676 hrs · 31,415 cycles

INITIALLY AFTER TAKEOFF VERY LOUD NOISE COMING FROM FWD NOSE SECTION, ACCESS DOOR OPEN ON EICAS. PERFORM APPROPRIATE CHECKLIST, DECLARED EMER. PERFORMED GEAR SWING & FOUND NOSE GEAR DOORS DID NOT CLOSE. FOUND BAD NOSE GEAR SEQUENCE PROX SWITCH WITH GSE212. R & R NOSE GEAR DOOR SEQUENCE PROX SWITCH IAW AMM 32-63-03. OPERATIONS CHECKED GOOD. SEE ITEM 2 BELOW FOR ACCESS DOOR OPEN. FWD ELEC COMPARTMENT DOOR INDICATION CHECKED GOOD IAW AMM 52-71-00.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 34,498 hrs · 31,237 cycles

AFT EMER FLASHLIGHT STAYS ON ALL THE TIME. R & R AFT EMER FLASHLIGHT IAW AMM 33-50-16 STEPS 2 J 1, 3 I 4. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,250 hrs · 31,013 cycles

AFT FLIGHT ATTENDANT EMER FLASHLIGHT INOPERATIVE. REPLACED AFT FLIGHT ATTENDANT EMER FLASHLIGHT IAW AMM 25-60-01. CHECKED GOOD.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 33,790 hrs · 30,572 cycles

ON TAXI OUT SMOKE IN COCKPIT & CABIN FOLLOWED BY APU FAIL CAUTION ON EICAS. INSPECTED & COMPLIED WITH ETN-EM-72-034. FOUND APU TO BE SOURCE FOR THE SMELL. DEFERRED APU IAW MEL 49-1. R & R APU REF WC 49-800-05. OPERATIONS CHECKED GOOD AT THIS TIME & MEL RESTORED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,769 hrs · 30,545 cycles

FLIGHT ATTENDANT`S EMER FLASHLIGHT INOPERATIVE. R & R FLIGHT ATTENDANT`S EMER FLASHLIGHT IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,532 hrs · 30,291 cycles

RIGHT AFT OVERWING EXTERNAL EMER LIGHT INOPERATIVE. R & R RT AFT OVERWING EXTERNAL EMER LIGHT LAMP IAW AMM 33-50-07-000-801-A & 33-50-07-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,381 hrs · 30,133 cycles

RIGHT EXTERNAL OVERWING EMER LAMP INOPERATIVE. R & R RT EXTERNAL OVERWING EMER LIGHT LAMP IAW AMM 33-50-07-000-801-A & 33-50-07-400-801-A. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 33,211 hrs · 29,999 cycles

AFTER ENG'S WERE AT IDLE FOR A LONG PERIOD, THE THRUST WAS BROUGHT UP & WE SMELLED AN OIL BURNING SMELL. REPEAT WRITE UP TRANSFERRED TO NRWC 650-DFW-01922. IAW NRWC 650-DFW-01922, R & R LT ENG IAW WC 71-000-00. OPERATIONS CHECKED GOOD. NO LEAKS DETECTED.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 33,209 hrs · 29,997 cycles

OILY BURNING SMELL COMING THRU PACK SYS WITH TAKEOFF THRUST & CLIMB THRUST SET. SEEMED TO GET WORSE IN THE DESCENT WITH LOW THRUST SETTINGS. NO VISIBLE SMOKE. SUSPECT PACK NR 1 SYS. TRANSFERRED TO NRWC 650-DFW-01912. IAW NRWC 650-DFW-01917, COMPLIED WITH. R & R E1 NR 0 CARBON SEAL. ENG RUN PERFORMED FOR ODOR CONFIRMATION, NO SMELL NOTED IAW ETN-EM-72-034.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,680 hrs · 29,524 cycles

LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. INSTALLED FILLER, REPAIR DOUBLER, REPAIR ANGLE & REPAIR ANGLE FILLER IAW ERS -EM-53MR-712.

Part: DOOR FRAME — CRACKED (ACCESS HATCH) · airframe 32,665 hrs · 29,514 cycles

COCKPIT UNDERFLOOR ACCESS HATCH 123BL FRAME IS CRACKED UNDER THE RETAINER RING EYELET. PERFORMED REPAIR TO COCKPIT UNDERFLOOR ACCESS HATCH IAW ERS EM-5200-199.

Part: FUEL LINE — CRACKED (FUEL SYSTEM) · airframe 32,665 hrs · 29,514 cycles

LEFT FUEL SOV PRESS REFERENCE LINE CRACKED. R & R CRACKED LT FUEL SOV PRESS IAW EMB 145 AMM 28-00-01.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 32,665 hrs · 29,514 cycles

LEFT MLG WW AFT LOWER BULKHEAD CRACKED INBD OF PREVIOUS REPAIR. R & R LT MLG WW AFT BULKHEAD IAW SRM 51-20-03, 51-40-06, 51-40-02 & 51-40-09. SEE WIP ENTRIES FOR DETAILS.

Part: CHECK VALVE — FAILED (BRAKE SYSTEM) · airframe 32,665 hrs · 29,514 cycles

NUMBER 2 MAIN BRAKE SYS RETURN LINE CHECK VLV FAILED OPERATIONAL CHECK. R & R NR 2 MAIN BRAKE SYS RETURN LINE CHECK VLV IAW AMM 32-41-09. LEAK & OPERATIONAL CHECKED GOOD.

Part: FIREWALL — CRACKED (APU BAY) · airframe 32,665 hrs · 29,514 cycles

APU FIREWALL CRACKED AT APPROX 6 O'CLOCK POSITION. REPAIR IAW EO EM-53AD-1883 PART C, REPAIRED APU FIREWALL.

Part: CRADLE — LOOSE (FLASHLIGHT) · airframe 32,625 hrs · 29,477 cycles

FLIGHT ATTENDANTS FLASHLIGHT CRADLE IS LOOSE. FLASHLIGHT WILL NOT CHARGE. REPLACED FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: SPLICE — DAMAGED (CABIN) · airframe 32,467 hrs · 29,301 cycles

DURING PS 1 INSPECTION FOUND SECTION 4 FLOOR PROXIMITY EMER LIGHT ASSEMBLY INOPERATIVE. ITEM DEFERRED IAW MEL 33-30. INSTALLED NEW SPLICES AT SECTION 4 FLOOR STRIP IAW WM CH 20-50-01. OPERATIONS CHECKED GOOD IAW MM CH 33-50-00. MEL ITEM RESTORED.

Part: FIRE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 32,230 hrs · 29,032 cycles

CARGO SMOKE WARNING DURING CRUISE AT FL 250. FIRE BOTTLE FIRED, CFR REPORTED NO FIRE. CVR PULLED DUE TO POSSIBLE FIRE.

Part: CHECK VALVE — LEAKING (BLEED AIR SYS) · airframe 32,229 hrs · 29,031 cycles

CLIMBING THROUGH FL 180, WHILE PERFORMING THE ANTI-ICE TEST, BLD 1 LEAK WARNING. EA PROCEDURE COMPLIED WITH & RESOLVED ISSUE. DURING TROUBLESHOOTING, FOUND LEAK AT O & L ABOVE NR 1 BLEED AIR CHECK VLV. R & R BLEED AIR CHECK VLV & UPPER DUCT ASSEMBLY. ADJACENT TO CHECK VLV IAW AMM 36-11-09-000-002-A & 36-11-09-400-802-A. LEAK CHECKED & PERFORMED OPERATIONAL TEST OF THE BLEED AIR SYS IAW AMM 36-00-00-700-803A. NO LEAKS NOTED & NO FAULTS INDICATED. ACFT OK FOR SERVICE.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 32,217 hrs · 29,019 cycles

TRANSFERRED FROM AML PAGE 3527007 ITEM 1, BLEED 1 LEAK EICAS WARNING & BUTTON INSCRIPTION DURING CLIMB FL 190. EPC & AOM PROCEDURES COMPLIED WITH. EICAS MSG & BUTTON INSCRIPTION EXTINGUISHED WITH CLOSURE OF ASSOCIATED BLEED VLV & CROSSBLEED CLOSED. REMAINED BELOW FL 250, NO FURTHER INDICATIONS PRESENTED. R & R AIR BLEED LINE O RINGS JOINT NR 28 AFT PRESS BULKHEAD IAW AMM 36-11-10. OPERATIONS CHECKED LEAK, CHECKED GOOD. NO OTHER DEFECTS NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,134 hrs · 28,948 cycles

PAX DOOR EMERGENCY LIGHT, OVERHEAD BY COCKPIT DOOR EMERGENCY LIGHT & LT WING LATERAL PANEL EMERGENCY LIGHT INOPERATIVE. R & R BATTERY POWER SUPPLY & BATTERY FOR NR 1 EMERGENCY SYS IAW AMM 33-50-04 & REPLACED LT WING EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: RVDT — OUT OF ADJUST (NR 2) · airframe 31,801 hrs · 28,631 cycles

FDR PARAMETERS REPORTED OUT OF LIMITS. NR 2 ELEVATOR FAILED OUT OF TOLERANCE. ADJUSTED ELEVATOR NR 2 RVDT IAW AMM 31-31-06 OPS CHECKED GOOD.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 31,579 hrs · 28,456 cycles

WHEN ON THE APPROACH THE AP DID A HARD RT TURN & THEN A HARD LT TURN. FLIGHT CREW PLACARDED IAW MEL 22-01.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 30,933 hrs · 27,954 cycles

EXIT SIGN ON GALLEY BULKHEAD IN FRONT OF SEAT 3BC IS INOPERATIVE. R & R NR 3 DC/AC INVERTER IAW EMB 145 AMM 33-50-11. R & R EMERGENCY LIGHTS BATTERY SUPPLY NR 2 IAW EMB 145 AMM 33-50-04, OPERATION CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGT) · airframe 30,905 hrs · 27,935 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,645 hrs · 27,718 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD END.

Part: HANDLE — BINDING (PAX DOOR) · airframe 30,622 hrs · 27,698 cycles

MAIN CABIN DOOR INTERIOR HANDLE IS DIFFICULT TO OPERATE. WHEN CLOSING HANDLE DOES NOT COMPLETELY LATCH DOWN. CLEANED DOOR SEAL AND LUBED TOP ROLLERS IN REF TO AMM 52-18-06. OPS CHECKED GOOD IAW AMM 52-18-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,148 hrs · 27,336 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM TASK 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 29,712 hrs · 26,971 cycles

DURING CRUISE, RECEIVED AN EICAS BAGGAGE SMOKE INDICATION AND OVERHEAD, AUROL WARNING. PERFORMED THE EMERGENCY CHECKLIST AND THE BAGGAGE SMOKE LIGHT EXTINGUISHED & THEN CAME BACK ON. BOTTLE WAS DISCHARGED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R CARGO REAR SMOKE DETECTOR IAW MM 26-15-01. OPT CHECK FOUND SATISFACTORY IAW MM 26-15-00. PERFORMED CARGO SMOKE DETECTOR, INSPECTION CHECK IAW AMM 26-15-01. FOUND OK. NO EVIDENCE OF SMOKE. FOUND BAGGAGE TEST SWITCH S7265 ON MAINT PANEL BAD. CARTRIDGE LOWER, PN: M30903870. CARTRIDGE UPPER, PN: M30903870. FIREX BOTTLE-630 CU. IN., PN: 346000731, SN: 1959F1. FIREX BOTTLE-630 CU.IN., PN: 346000731. SN: 1959F1. SWITCH, PN: M83731/10-271. CARGO AREA SMOKE DETECTOR, PN: 473597-13. SN: 1059. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,577 hrs · 26,859 cycles

DURING B INSPECTION, FOUND THE 12C INTERIOR OVERWING EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE RT OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: RELAY — FAILED (LANGING GEAR) · airframe 29,217 hrs · 26,582 cycles

ON FLIGHT 3996 THE CREW REPORTED THAT AFTER TAKEOFF THEY COULD NOT RAISE THE LANDING GEAR NORMALLY, RECEIVED NUMEROUS CONFIG WARNINGS FOR FLAPS & TRIM VIA AURAL WARNING- NO EICAS MESSAGES DISPLAYED. THE CREW PERFORMED AOM VOL 1 PROCEDURE FOR LANDING GEAR AND IT COULD NOT BE RAISED. GOT GEAR UP AND MOC ADVISED AND TOLD THEM TO RETURN TO ORD. THE CREW DECLARED AN EMERGENCY AND LANDED NORMALLY. DURING THE ROLLOUT THE CREW BEGAN TO RECEIVE MANY EICAS WARNING AND CAUTIONS INCLUDING LG. AIR/GND FAIL AND IC 1-2 WOW INOP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RELAYS K0025, K0024, AND K0453. NO DEFECTS NOTED. GEAR SWING GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR · airframe 29,062 hrs · 26,437 cycles

DURING MAINTENANCE INSPECTION NOTICED A STRONG FUEL SMELL AFTER APU START-UP REF LOG PAGE 3199769. COMPLIED WITH ETN-EM-72-034 PERFORMED PACKS WITH ENGINES AND APU RUNS. THE OPERATIONAL CHECK WAS GOOD NO FUEL SMELL NOTED DURING ECF FLIGHT 9808. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (AILERONS) · airframe 28,999 hrs · 26,379 cycles

FLIGHT 9806. CREW REPORTED ACFT BANKS HARD TO RIGHT WITH AILERON TRIM AT ZERO. TO KEEP WINGS LEVEL 1/4 ROLL TRIM IS REQUIRED. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT AND RIGHT AILERON ACTUATORS IAW AMM 27-21-01. OPS AND & LEAK CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 28,999 hrs · 26,379 cycles

FOR FLIGHT 9806 THE CREW REPORTED STRONG FUEL SMELL AFTER STARTING APU. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH ETN-EM-72-034. PERFORMED ENGINE RUNS AND APU RUNS NO FUEL SMELL NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POTENTIOMETER — UNSERVICEABLE (NLG STEERING) · airframe 28,952 hrs · 26,344 cycles

ON FLIGHT 3596 THE CREW REPORTED THAT WHILE DOING HIGH SPEED TAXI THE AIRCRAFT OCCASIONALLY JERKS TO THE LEFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED LOAD POTENTIOMETER IAW EMB 145 AMM 32-00-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

FWD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT AREA 2 BATTERY AND CHARGER ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,404 hrs · 25,921 cycles

DURING B INSPECTION FOUND THE MAIN DOOR CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR CEILING EMERGENCY LIGHT IAW EMB AMM TASK 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 28,250 hrs · 25,799 cycles

DURING B INSPECTION FOUND THE ROW 3 EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND FOUND CONNECTORS LOOSE. RECONNECTED LAMP IAW EMB AMM 33-50-14-000-801-A AND 33-50-14-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,099 hrs · 25,677 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT AT MID-CABIN LEFT SIDE EMERGENCY EXIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP AT THE LEFT EMERGENCY EXIT PER EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 27,976 hrs · 25,576 cycles

BACKSIDE FRAME 80 BURNED/CORRODED. ACCOMPLISHED EM-53MR-2024.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 27,982 hrs · 25,581 cycles

DURING B INSPECTION FOUND THE RIGHT CROSS MEMBER OUTBOARD GUSSET CORRODED AT FRAME 23. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT CROSS MEMBER OUTBOARD GUSSET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 27,982 hrs · 25,581 cycles

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

Part: GUSSET — CORRODED (FUSELAGE) · airframe 27,982 hrs · 25,581 cycles

DURING B INSPECTION FOUND THE RIGHT BEAM GUSSET CORRODED BETWEEN FRAMES 60-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT BEAM GUSSET BETWEEN FRAMES 60-61 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 27,982 hrs · 25,581 cycles

DURING B INSPECTION FOUND THE RIGHT BEAM GUSSET CORRODED AT FRAME 31. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT BEAM GUSSET IAW EMB SRM 51-40-02, EMB SRM 51-20-03, EMB SRM 51-40-06 AN EMB SRM 51-40-09. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 27,982 hrs · 25,581 cycles

DURING B INSPECTION FOUND THE RIGHT BEAM GUSSET CORRODED AT FRAME 28. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT BEAM GUSSET IAW EMB SRM 51-40-02, EMB SRM 51-20-03, EMB SRM 51-40-06 AN EMB SRM 51-40-09. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 27,982 hrs · 25,581 cycles

DURING B INSPECTION FOUND THE CENTER BEAM GUSSET CORRODED BETWEEN FRAMES 59-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CENTER BEAM GUSSET BETWEEN FRAMES 59-61 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 27,982 hrs · 25,581 cycles

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

Part: SEAL — TORN (CABIN DOOR)

DURING B INSPECTION FOUND THE MAIN CABIN DOOR SEAL TORN IN TWO PLACES ON DOOR FLAP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN CABIN DOOR SEAL IAW EMB 145 AMM 52-18-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,976 hrs · 25,576 cycles

LEFT OMEGA BEAM IS CORRODED BETWEEN FRAMES 58-59. REPAIRED LEFT OMEGA BEAM CORROSION BETWEEN FR 58-59 IAW AEA EO-EM-53MR-2027.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 27,976 hrs · 25,576 cycles

BACK SIDE OF FRAME 80 IS BURNED/CORRODED WHERE APU SHUNT IS ATTACHED. REPAIRED BACK SIDE OF FR 80 BURNED/CORRODED WHERE APU SHUNT IS ATTACHED IAW AEA EO-EM-53MR-2024.

Part: FLASHLIGHT — UNSERVICEABLE (COCKPIT) · airframe 27,948 hrs · 25,557 cycles

ON FLIGHT 3266 THE CREW REPORTED THE FLASHLIGHT CRADLE BEHIND THE CAPTAIN SEAT WAS BROKEN. (FLASHLIGHT FALLS OUT) DEFERRED PER MEL 25-53 AUTH 090679-C FOR CAPT'S FLASHLIGHT. SECURED IN PLACE. COMPLIED WITH (M) PRODGERS FOR MEL. REMOVED AND REPLACED THE CAPTAIN’S EMERGENCY FLASHLIGHT ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-16. MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 27,941 hrs · 25,551 cycles

ON FLIGHT 3401 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 27,543 hrs · 25,227 cycles

DURING MAINTENANCE INSPECTION, FOUND THE ROW NR 8 FLOOR EMERGENCY LIGHT CONNECTOR WIRE BROKEN. AIRCRAFT REMOVED FROM SERVICE. REPAIRED ROW NR 8 FLOOR EMERGENCY LIGHT CONNECTOR IAW WM 20-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 27,533 hrs · 25,218 cycles

DURING B INSPECTION, FOUND THE FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT BATTERY. OPS CHECKED GOOD IAW CMM 25-60-11. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — SHUTDOWN (NR 2 ENGINE FUEL) · airframe 27,209 hrs · 24,963 cycles

FLIGHT 4050 - ON ARRIVAL AT GATE WITH NR 2 ENGINE RUNNING, PARKING BRAKE ON, NO APU OR GPU, HAD NR 2 ENGINE FLAMEOUT, SHUTDOWN UNCOMMANDED WITH ECAS MESSAGE. AIRCRAFT REMOVED FROM SERVICE. PERFORMED CMC AND FDR DOWNLOAD, FOUND THAT NR 2 ENGINE FUEL PUMP WAS TURNED OFF PRIOR TO ENGINE SHUTDOWN CAUSING FLAMEOUT. GROUND RAN AIRCRAFT IAW FIM TASK 72-00-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: COVER — DEFECTIVE (PAX DOOR) · airframe 26,943 hrs · 24,735 cycles

ON FLIGHT 4291 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN FROM THE INSIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN CABIN DOOR HANDLE COVER PER STANDARD MTX PROCEDURES. THE OPERATIONAL CHECK WAS GOOD PER EMB-145 MM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 26,522 hrs · 24,441 cycles

ON FLIGHT 4200 THE LIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN CABIN DOOR FRAME ROLLERS IAW EMB MM 53-21-00. NO DEFECTS NOTED, DOOR OPENING WITH NO DIFFICULTY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,340 hrs · 24,330 cycles

DURING B-INSPECTION FOUND THE MAIN DOOR MOUNTED EMERGENCY LIGHT INOP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED MAIN CABIN DOOR MOUNTED EMERGENCY LAMP IAW EMB 145 AMM TASK 33-50-10-000-801-A & 33-50-10-400-801-A OPERATIONAL CHECK GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL CABLE — OUT OF ADJUST (AILERON) · airframe 26,180 hrs · 24,190 cycles

ON FLIGHT 4391 THE CREW REPORTED AN UNCOMMANDED ROLL TO THE RIGHT AFTER TAKEOFF. THE FLAPS WERE AT 9 DEGREES. THE CREW RETURNED TO ORD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND AILERON CONTROL CABLES BELOW SPECIFICATION. ADJUSTED THE WING AND FUSELAGE SECTORS OF THE AILERON CONTROL SYSTEM IAW EMB-145 AMM 27-11-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 26,031 hrs · 24,090 cycles

DURING MAINTENANCE INSPECTION FOUND THE FORWARD BAGGAGE SMOKE DETECTOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FORWARD BAGGAGE SMOKE DETECTOR IAW EMB AMM 26-15-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,569 hrs · 23,723 cycles

FOR FLIGHT 3541 THE CREW REPORTED THE AFT CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT AND CHARGER ASSY IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,475 hrs · 23,656 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT IAW EMB MM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,211 hrs · 22,645 cycles

DURING MAINTENANCE CHECK FOUND EMERGENCY LIGHT STRIPS 4 AND 5 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DC/AC INVERTER NR 5 IAW EMB 145 AMM 33-50-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,728 hrs · 21,523 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — FUMES (COCKPIT) · airframe 22,642 hrs · 21,449 cycles

ON FLIGHT 3209 THE CREW REPORTED UPON DESCENT TO LANDING SMELLED A BURNING ODOR IN THE COCKPIT ONLY. DETECTED FUMES ONLY, NO SMOKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED GENERAL VISUAL INSPECTION OF THE COCKPIT AND HAD CREW RUN ENGINES WITH PACKS ON WITH MAINTENANCE PRESENT. NO FURTHER ODORS WERE NOTED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,584 hrs · 21,407 cycles

FOR FLIGHT 2875 DURING MAINTENANCE CHECK FOUND THE LIGHT STRIP FOR EMERGENCY LIGHTING ON THE LEFT OVERWING EMERGENCY EXIT WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT STRIP ON THE LEFT SIDE OVERWING EMERGENCY EXIT IAW AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LINE — DISCONNECTED (BRAKES) · airframe 22,277 hrs · 21,171 cycles

ON FLIGHT 4318 CREW REPORTED ON LANDING, RECEIVED A "BRAKE DEGRADED" & FELT ASYMMETRIC THRUST ON LAST PORTION OF LANDING ROLLOUT. TOWER REPORTED SMOKE COMING FROM LT MLG. ON TURN INTO GATE TOWER REPORTED MORE SMOKE FROM LT MLG AND FLUID SPILLING OUT, AT THAT MOMENT LOST HYD NR 2 QTY & PRESSURE. HAD MINIMAL BRAKING. POST FLT INSPECTION REVEALED HYD FLUID LEAKING FROM LT MLG & INBOARD BRAKE PIN MISSING. NO FIRE AT ANYTIME. ACFT REMOVED FROM SERVICE. INSPECTED LT MLG ASSY. FOUND NR 2 HYD BRAKE LINE DISCONNECTED CAUSING HYD NR 2 QTY DEPLETION & SUBSEQUENT BRAKE DEGRADING & EMERGENCY LOW PRESSURE MESSAGE ON EICAS. NO CMC MSG. R & R NR 2 MLG BRAKE ASSY IAW W/C 32-600-14. ALSO R & R NR 2 BRAKE TEMP SENSOR IAW AMM 32-47-01. OPS & LEAK CHECK GOOD. ACFT RETURNED TO SERVICE.

Part: BALLAST — BURNED OUT (CABIN) · airframe 22,078 hrs · 21,043 cycles

ON FLIGHT 3648 THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE GALLEY. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BURNED LIGHT BALLAST AT SEAT 3 B & C. REPLACED THE BALLAST IAW EMB AMM 33-21-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,468 hrs · 20,580 cycles

DURING MAINTENANCE BASE VISIT FOUND THE GALLEY EMERGENCY EXIT LIGHTS TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY AND BATTERY CHARGER ASSEMBLY ASSY IAW EMB AMM TASK 33-50-04-000-801-A & 33-50-04-400-801-A . THE OPERATIONAL CHECK WAS NORMAL AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,321 hrs · 20,466 cycles

DURING MAINTENANCE BASE VISIT FOUND THE PASSENGER DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IAW EMB 145 AMM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,321 hrs · 20,466 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT EXIT EMERGENCY OVERWING LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB SB 145-33-0013R1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — FAILED (CABIN) · airframe 21,217 hrs · 20,390 cycles

DURING P2-2 CHECK THE FORWARD CENTER OVERWING INTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 INVERTER FOR THE EMERGENCY LIGHT IAW EMB145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD IAW 33-50-00-700-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FIRE BOTTLE — MALFUNCTIONED (NR 1 ENGINE) · airframe 21,074 hrs · 20,269 cycles

ON FLIGHT 3892 THE CREW REPORTED, RECEIVED A MESSAGE THAT NR 1 ENGINE FIRE BOTTLE WAS INOPERABLE. THE CREW ELECTED TO RETURN TO MIA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET SYSTEM. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD PER AMM 26-21-00. NO DEFECTS NOTED, OK FOR SERVICE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — LEAKING (LEFT) · airframe 16,745 hrs · 16,444 cycles

ON FLIGHT 4348, CREW REPORTED THAT ATOMIZED TURBINE OIL FUMES WERE INTRODUCED INTO THE CABIN CONDITIONED AIR WHEN USING ENG 1 BLEED AS SUPPLY SOURCE. WHEN USING BLEED 2 OR APU TO SUPPLY A/C PACKS CONDITIONED AIR IS GOOD. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR1 ENGINE IAW WORK CARD 71-00-00. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 14,436 hrs · 14,488 cycles

EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REMOVED AND REPLACED NUMBER TWO BATTERY PACK AND CHARGER IAW EMB AMM. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

CID - FLT 3570 - FLOOR EMERGENCY LIGHTS FROM ROW 8 TO 12 OUT AND OVERWING EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED NR 3 BATTERY PACK, IAW EMB 145, AMM 33-50-04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: TRIM SWITCH — FAILED (COCKPIT)

CMH - FLT 3589 - ON TAKEOFF, FIRST OFFICERS TRIM SWITCH WAS IN USE AND IT STARTED TO SMOKE. STOP USING THE FIRST OFFICERS TRIM SWITCH AND CAPTAIN TRIM WORKED NORMAL, RETURNED TO FIELD NO OTHER PROBLEMS NOTED. RAI FIRST OFFICERS TRIM SWITCH, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: RELAY — FAILED (SPOILER SYS)

MKE - FLT 4095 - ABORTED TAKEOFF FOR TAKEOFF CONFIGURATION WARNING WITH SPOILER OPEN EICAS MESSAGE. RAI RELAY K0212, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ALL EMERGENCY LIGHTS FAILED TO TEST DURING PREFLIGHT. REPLACED NR 2 BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)

Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHTS)

ORD - FLT 4435 - FOUND EMERGENCY LIGHT CIRCUIT BREAKER POPPED. WOULD NOT RESET. EMERGENCY LIGHT NO ARMED EICAS MESSAGE ILLUMINATED. REPLACED NR 3 EMERGENCY BATTERY AND CHARGER IAW EMB 145 MM 33-50-04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. CHARGER P/N OFF 11-0049 S/N OFF 14855, BATTERY P/N OFF 20131 S/N OFF 67338. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS WILL NOT EXTINGUISH. REPLACED NR 1, 2, 3 AND 4 EMERGENCY LIGHT BATTERY POWER SUPPLIES AND NR 2 EMERGENCY LIGHT CHASSIS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. EMERGENCY LIGHT BATTERIES OFF P/N 2-131A. POWER SUPPLY SERIAL NUMBERS OF AS FOLLOWS 1-66089, 2-69701, 3-67880, 4-74123. (M)

Part: RELAY — FAULTY (CABIN)

CVG - FLT 3971 - EMERGENCY LIGHTING CIRCUIT BREAKER POPPED. REPLACED CIRCUIT BREAKER 8500 AND RELAY K0275. OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM GOOD PER EMB AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE. C/B PN IS REBC4105-200003. (M)

Part: CONNECTOR — LOOSE (BATTERY PACK)

EMERGENCY LIGHT ARM CIRCUIT BREAKER POPPED. FOUND LOOSE CONNECTOR ON BATTERY PACK. RESECURED CONNECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS)

THE EMERGENCY LIGHTS ILLUMINATED IN THE COCKPIT AND CABIN. SHORTLY AFTERWARDS THE EMERGENCY LIGHTS NOT ARMED MESSAGE APPEARED ON THE EICAS. REPLACED EMERGENCY BATTERIES NR 1 AND NR 3 IAW EMB 145 MM 33-50-04. BOTH BATTERIES HAD LOW VOLTAGE. PERFORMED EMERGENCY LIGHTING TEST IAW EMB-145 MM 33-50-00. NO DEFECTS NOTED. A/C RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 8,459 hrs · 8,903 cycles

DURING CPCP INSPECTION, FOUND THE FLOOR DIGITAL CORRODED IN SEVERAL AREAS REMOVED AND REPLACED FLOOR DIGITAL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)

Part: SILL — CORRODED (FUSELAGE) · airframe 8,459 hrs · 8,903 cycles

DURING CPCP INSPECTION, FOUND THE FORWARD CABIN FLOOR RT SILL HAS CORROSION AROUND NUTPLATE. REMOVED AND REPLACED SILL ASSY IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)

Part: ANGLE — CORRODED (FUSELAGE) · airframe 8,459 hrs · 8,903 cycles

DURING CPCP INSPECTION FOUND ANGLE CORRODED THROUGH AFT END. REMOVED AND REPLACED FORWARD CABIN FLOOR ANGLE WITH A NEW ANGLE IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501) (K)

Part: SKIN — DENTED (FUSELAGE) · airframe 8,459 hrs · 8,903 cycles

DURING MBV INSPECTION, A DENT WAS FOUND AFT OF RADOME FRAME 1 AND STRINGER 13 R. REPLACED DAMAGED SECTION OF SKIN IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)

Part: SILL — CORRODED (FUSELAGE) · airframe 8,459 hrs · 8,903 cycles

DURING CPCP INSPECTION FOUND FORWARD CABIN LT SILL CORRODED. REMOVED AND REPLACED SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 8,459 hrs · 8,903 cycles

DURING CPCP INSPECTION, FOUND THE SUPPORT CORRODED UPPER AFT END. REMOVED AND REPLACED FLOOR SUPPORT BETWEEN FRAME 19 AND FRAME 20 IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 8,459 hrs · 8,903 cycles

DURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR OMEGA SHAPE CORRODED. REPAIRED FORWARD LT CABIN OMEGA SHAPE AT FRAME 20 CROSSBEAM ATTACH JUNCTION IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)

Part: ANGLE — CORRODED (FUSELAGE) · airframe 8,459 hrs · 8,903 cycles

DURING CPCP INSPECTION, FOUND THE MAIN DOOR SILL ANGLES ARE CORRODED. REMOVED AND REPLACED MAIN DOOR SILL ANGLES IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)

Part: DOUBLER — CORRODED (CABIN FLOOR) · airframe 8,459 hrs · 8,903 cycles

DURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR DOUBLERS HAVE CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOOR DOUBLERS IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)

Part: SILL — CORRODED (FUSELAGE) · airframe 8,459 hrs · 8,903 cycles

DURING CPCP INSPECTION, FOUND THE SERVICE DOOR SILL CORRODED AROUND NUTPLATES UPPER SURFACE. REMOVED AND REPLACED SERVICE DOOR SILL PLATE IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)

Part: SILL — CORRODED (FUSELAGE) · airframe 8,459 hrs · 8,903 cycles

DURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR SILL ASSEMBLY HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED FORWARD SILL ASSEMBLY IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)

Part: GUSSET — CORRODED (FUSELAGE) · airframe 8,459 hrs · 8,903 cycles

DURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR GUSSET HAS CORROSION ON UPPER SURFACE. INSTALLED NEW GUSSET IAW SRM. AC RETURNED TO SERVICE. (SW21200501985) (K)

Part: PDU — FAILED (TE FLAPS)

ON FINAL APPROACH, FLAPS SELECTED TO MOVE FROM 22 TO 45 DEGREES. FLAPS STUCK AT 41 DEGREES WITH ACCOMPANYING FLAP FAIL AND FLAP CAUTION MESSAGES ON EICAS. REPLACED PDU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ODOR — DETECTED (COCKPIT)

ORD - FLT 4431 - CREW REPORTED A HEAVY OZONE ODOR IN COCKPIT AFTER LIGHTNING STRIKE. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION IAW WORK CARD 05-200-00. NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ACTUATOR — LEAKING (RI WING)

ORD - FLT 4333 - DURING CLIMB, CREW REPORTED HYDRAULIC 1 QTY MESSAGE ON EICAS. QUANTITY DROPPED TO BOTTOM OF GAUGE AND A E1 HYDRAULIC PUMP FAIL MESSAGE SHOWED ON EICAS. CREW DECLARED AN EMERGENCY. AFTER GEAR WAS SELECTED DOWN PUMP FAIL MESSAGE WENT AWAY. AIRCRAFT WAS LANDED AND TAXIED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE FOUND AND REPLACED A SPOILER ACTUATOR FOR THE RIGHT SPOILER IAW EMB MM. OPERATIONAL AND LEAK CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN MBV INSPECTION LEFT STRINGER 19 WAS FOUND TO BE CHAFED AT FRAME 52. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB SRM (EMB SRM 145/1142 REV 20) CHAPTER 53-24-02. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, THE RIGHT STRINGER 19 WAS FOUND TO BE CHAFED AT FRAME 52. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM (EMB 145/1142 REV 20) CHAPTER 53-24-02. (M)

Part: FLOORBEAM — CORRODED (GALLEY)

ABI - DURING AN MBV INSPECTION, THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS. PERFORMED A CUT OUT OF THE DAMAGED SECTION OF THE LEFT FLOORBEAM. FABRICATED AN EXTERNAL ANGLE, FILLER AND SHIMS. REPAIR DONE IAW EMB 145 SRM (SRM 145/1142 REV 20) CHAPTER 53-21-10 FIGURE 201 SHEET 1. (M)

Part: GUSSET — CORRODED (GALLEY)

ABI - THIS LEVEL 2 FINDING FOUND DURING MBV INSPECTION REFERENCE CRIC NR 27870. FORWARD DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M)

Part: SILL — CORRODED (GALLEY)

ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN MBV INSPECTION REFERENCE CRIC NR 27872 SERVICE DOOR AFT SILL CORRODED. INSTALLED NEW AFT SERVICE DOOR SILL IAW EMB 145 SRM 51-40-02. (M)

Part: GUSSET — CORRODED (GALLEY)

ABI - THIS LEVEL 2 FINDING FOUND DURING MBV INSPECTION REFERENCE CRIC NR 27875, CENTER BEAM GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-02. (M)

Part: GUSSET — CORRODED (GALLEY)

ABI - THIS LEVEL 2 FINDING FOUND DURING MBV INSPECTION REFERENCE CRIC NR 27871, AFT DIAMOND GUSSET CORRODED. REMOVED CORRODED GUSSET AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M)

Part: SILL — CORRODED (GALLEY)

ABI - THIS LEVEL 2 FINDING FOUND DURING MBV INSPECTION REFERENCE CRIC NR 27873. SERVICE DOOR FORWARD SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)