N642AE

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 54,791 hrs · 51,811 cycles

EMERGENCY LIGHT STRIP AT ROW 15 IS INOP. RAR STRIP IAW AMM33-50-08

Part: CONTROLLER — DEFECTIVE (CABIN PRESSURE) · airframe 54,309 hrs · 51,259 cycles

ON CLIMB UP UNTIL 8000 FT IN AUTO MODE. A/C DID NOT PRESSURIZE. FACT 22FEB25 03:36 ROA R&R'D DIGITAL CONTROLLER IRW AMM 21-31-01 DUE TO CODE A016 ON DIGITAL CONTROLLER. OPS CK GOOD

Part: LIGHT — FAULTED (ZONE 200) · airframe 54,235 hrs · 51,189 cycles

ON CLIMB AROUND 10,000 FT FA EMERGENCY LIGHTS CAME ON AND STAYED ON. OPERATIONALLY CHECKED THE EMERGENCY LIGHTING SYSTEM IAW WC 33-70-17. NO DEFECT FOUND. EMS LIGHTS OPS CHECK GOOD

Part: SENSOR — FAULTED (FUEL QTY) · airframe 53,972 hrs · 50,909 cycles

TANK 2 & TOTAL FUEL INDICATION NOT SHOWING. MEL 24DEC24 10:05 CLT B35905 28-9 WING TANK FUEL QTY INDC EICAS MFE FACT 28DEC24 06:31 SBY T/S FUEL INDICATION ISSUE USING FIM. CHANGED FCU IAW AMM 28-41-01 DOES NOT CHOW DASHES ANYMORE OPS CHECK GOOD..PROBLEM RETURNED,REINSTALLED ORIGINAL FCU IAW AMM 28-41-01 ( SHORT SIGNED) R&R'D RH FUEL TANK UNIT 2 IAW AMM 28-41-02 OPS CHECK GOOD CLEAR MEL 28-9

Part: CONTROL PANEL — MALFUNCTIONED (CABIN PRESSURE) · airframe 52,745 hrs · 49,493 cycles

AT 18K ALTITUDE, CABIN ALTITUDE CLIMBED TO 10K FEET. MEL APPLIED. PRESS CONTROL AUTO AND MANUAL FACT 23MAY24 04:15 ALB T/S IRW EMB-145 FIM 21-31-00-810-805-A, BLOCKS 1-2. R&R CPAM IRW EMB-145 AMM 21-32-01. LEAK AND OPS CHECK PASSED. THIS CLEARS MEL 21-12-3

Part: UNKNOWN — UNKNOWN (UNKNOWN)

PRESSURIZATION AUTOMATIC MODE FAILURE AT 13,000 FT CABIN ALT PRESENTED RED HISTORY: YES MEL 21NOV23 10:06 MDT C32507 21-12-3 PRESS CONTROL AUTO AND MANUAL. TROUBLESHOT PER FIM TASK 21-31-00-810-809-A. FOUND RELAY K0412 INOP. R/R'D K0412 RELAY IAW AMM 20-13-02 OPS CHECKS GOOD. CLEAR MEL 21-12-3.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,724 hrs · 48,336 cycles

E993888 SHEAR CLIP CRACKED AT FR 8 BTW STGR 9L AND WINDSHIELD LOWER FRAME. ACCOMPLISHED REPAIR OF FR 8 STGR 9L TO LOWER WINDSHIELD FRAME SHEAR CLIP IAW ETD# ETD2023-145-021990 AND EO1-53-23-0271.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,724 hrs · 48,336 cycles

E992717 RH WING UPPER WING TIP ATTACHMENT FLANGE HAS AN ELONGATED NUTPLATE HOLE. : RAR R/H WING UPPER WING TIP RIB IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,724 hrs · 48,336 cycles

E992227 CABIN L/H #4 FLOORBOARD SUPPORT HAS CORROSION. : REMOVED AND REPLACED CABIN L/H #4 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,724 hrs · 48,336 cycles

E992224 CABIN R/H #2 FLOORBOARD SUPPORT HAS CORROSION. : RAR R/H #2 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,724 hrs · 48,336 cycles

E992226 CABIN L/H #3 FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED CABIN L/H #3 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,724 hrs · 48,336 cycles

E992242 L/H FLOOR BEAM HAS CORROSION BETWEEN FRAMES 36 AND 39. RAR L/H FLOOR BEAM GUSSET BETWEEN FRAMES 36 AND 39 IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,724 hrs · 48,336 cycles

E992234 CABIN L/H FLOOR BEAM BETWEEN FRAME 29 AND 31 HAS CORROSION. REMOVED AND REPLACED GUSSET ON CABIN L/H FLOOR BEAM BETWEEN FRAME 29 AND 31 IAW EMB 145 SRM 51-40-02. SEE TASK AND WIPS FOR FURTHER DETAILS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,742 hrs · 48,336 cycles

E992228 CABIN R/H #3 FLOORBOARD SUPPORT HAS CORROSION. RAR R/H #3 CABIN FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,724 hrs · 48,336 cycles

E991923 RUDDER II HAS AN EXTERNAL REPAIR DOUBLER ON LH SIDE ABOVE ACCESS PANEL#327CL NO REPAIR INFO FOUND. RE-ACCOMPLISHED REPAIR FOR DTI FCD: RUDDER II HAS AN EXTERNAL REPAIR DOUBLER ON LH SIDE ABOVE ACCESS PANEL #327CL IAW EO1-55-23-0259.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,724 hrs · 48,336 cycles

E992217 CABIN L/H #2 FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED CABIN L/H #2 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,724 hrs · 48,336 cycles

E991951 GALLEY TRIANGLE GUSSET AT WARDROBE AREA HAS CORROSION. : REMOVED AND REPLACED GALLEY TRIANGLE GUSSET AT WARDROBE AREA IAW EMB145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,724 hrs · 48,336 cycles

E992002 RUDDER 2 LIGHTNING HOLE AT UPPER CONTROL ROD ATTACH POINT CRACKED. REMOVED AND REPLACED RIB ON RUDDER 2 AT LIGHTNING HOLE AT UPPER CONTROL ROD ATTACH POINT IAW EMB145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,724 hrs · 48,336 cycles

E991999 RUDDER 1 LOWER HINGE FITTING WORN. REMOVED WORN RUDDER 1 LOWER HINGE FITTING AND INSTALLED SERVICEABLE RUDDER 1 LOWER HINGE FITTING ASSEMBLY IAW EMB145 SRM 51-40-02 AND AMM 20-10-01.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,724 hrs · 48,336 cycles

E992197 R/H #5 FLOORBOARD SUPPORT HAS CORROSION. : REMOVED AND INSTALLED NEW R/H #5 FLOORBOARD SUPPORT IAW EMB 145 SRM51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,724 hrs · 48,336 cycles

E991959 AFT FLOOR BOARD SUPPORT AT PAX DOOR ENTRENCE HAS CORROSION. RAR AFT FLOOR BOARD SUPPORT AT PAX DOOR ENTRENCE IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,724 hrs · 48,336 cycles

E992000 RUDDER 2 UPPER HINGE FITTING ELONGATED AT HAT BUSHING. REMOVED AND INSTALLED SERVICEABLE RUDDER 2 UPPER HINGE FITTING IAW EMB145 SRM 55-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,724 hrs · 48,336 cycles

E991907 : FUSELAGE EXTERNAL SKIN PREVIOUS REPAIR DOUBLER BETWEEN FR 6/7 AND STR 2L/2R HAS NO REPAIR INFORMATION. RE-ACCOMPLISHED REPAIR ON FWD FUSELAGE II SKIN FR 6-7 STGR 2L-2R IAW ETD2023-145-021605 REV. A, EO1-53-23-0276

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,724 hrs · 48,336 cycles

E991690 FRAME 65 L-SHAPE ANGLE IS CORRODED BETWEEN STRG. 17L-18L. RE-ACCOMPLISHED SPLICE REPAIR AT FRAME 65 L-SHAPE ANGLE BETWEEN STRG. 17L-18L IAW EMB 145 SRM 53-31-04RE, ITEM4D, FIGURE 212, AND EO1-53-23-0285

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,724 hrs · 48,336 cycles

E991802 : BAGGAGE DOOR EXTERNAL SKIN PREVIOUS CIRCULAR REPAIR DOUBLER BETWEEN VB4/VB5 AND HB3/HB4 AND DOUBLER AT EXTERNAL HANDLE REQUIRE DAMAGE TOLERANCE ANALYSIS DUE TO PROXIMITY. : RE-ACCOMPLISHED BAGGAGE DOOR EXTERNAL SKIN CIRCULAR REPAIR DOUBLER BETWEEN VB4/VB5. AND HB3/HB4 AND OBTAINED DTI INFORMATION FOR CIRCULAR REPAIR AND DOUBLER AT EXTERNAL HANDLE IAW ETD2018-145-103153, ETD2023-145-022433, EO1-52-23-0260 AND EO1-05-23-0261.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,724 hrs · 48,336 cycles

E990709 DENT ON RH #1LEADING EDGE APPROXIMATELY 22 INCHES FROM INBD EDGE AND 19 INCHES FROM LOWER TRAILING EDGE. : PERFORMED REPAIR TO RH #1 LEADING EDGE APPROXIMATELY 22 INCHES FROM INBD EDGE AND 19 INCHES FROM LOWER TRAILING EDGE. IAW EMB 145 SRM 57-40-00 RE (2. A PATCH TYPE REPAIR PROCEDURE FOR THE WING LEADING EDGE SKIN TABLE 201, FIGURE 201, FIGURE 202), AND EO1-57-23-0275

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,724 hrs · 48,336 cycles

E988431 ACCOMPLISH PERMANENT REPAIR PER FCD1-54-21-0017 RH PYLON - REPLACEMENT OF FWD PYLON LINKAGE FITTINGS AND BUSHINGS. ACCOMPLISHED PERMANENT REPAIR PER FCD1-54-21-0017 RH PYLON - REPLACEMENT OF FWD PYLON LINKAGE FITTINGS AND BUSHINGS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,648 hrs · 48,248 cycles

IN CRUISE FLT, STRONG BURNING ODOR DETECTED IN CABIN & FLIGHT DECK. INSPECTED ACFT FOUND PACK 1 TO HAVE OVERTEMPED & MELTED ALL OF SLEEVES ASSOCIATED WITH PACK. RAN PACK 2 WITH APU & BOTH ENG BLEEDS WITH NO SMELLS NOTED. RAN ENGINES 2 TIMES AT MAX POWER ON PACK 2 NO ISSUES NOTED OR ANY SMELLS. ACFT OK FOR SERVICE. FOUND PACK 1 TO HAVE OVER TEMPED AND ALL ASSOCIATED SLEEVES TO BE MELTED MEL 31JUL23 05:02 GSO C21201 21-15-11 AIR COND PACK ELECTRO/MECH N600-N649 FACT 01AUG23 06:45 MDT R&R'D DUCT PN:C143123-6 BETWEEN DCV AND PACK VALVE R&R'D DCV AND ALL ASSOCIATED SLEEVES IRW 21-60-01. R&R'D #100 ACM AND ASSOCIATED SLEEVES IRW 21-51-03 AND PB 21-05. FINAL OPS CHECKS OK AT THIS TIME.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,638 hrs · 48,236 cycles

ON T/O ROLL #1 ENG OIL PSI PASSED THROUGH 120PSI. REF RR FIM 79-37-00-810-805 GRND RAN ENG 1 REF 71-00-00-810-804 RESULTS ACCEPTABLE PER FIG 201 A/C OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,474 hrs · 48,050 cycles

LIGHTNING NEAR CAPT WINDOW FACT 25JUN23 01:02 PHL PERFORMED LIGHTNING STRIKE INSPECTION IAW AMM 05-50-01-200-801-A. NO FURTHER DAMAGE NOTED. OK FOR SERVICE

Part: NONE — NONE · airframe 49,564 hrs · 45,919 cycles

OIL LEAK COMING FROM THE #1 ENGINE. ALSO HAD FAINT OIL BURNING SMELL AT T/O POWER. CLEANED OIL FROM LOWER COWL AND GROUND RAN ENGINE WITH CREW. NO LEAKS NOTED IN LOWER COWL OR EXHAUST SECTION OF ENGINE. SUSPECT OIL IN COWLING IS FROM SERVICING. HOWEVER, OIL BURNING SMELL REMAINED WITH #1 ENG RUNNING AND PACKS ON SEE SEQ #3 OF THIS LP FOR MEL OF #1 PACK.

Part: SHEAR TIE — CORRODED (FRM 65 S16-17L) · airframe 47,987 hrs · 44,165 cycles

E867937 - SHEAR CLIP AT FR 65 BTW STR 16L-17L CORRODED. ... PERFORMED PERMANENT REPAIR OF FR 65 SHEAR CLIP BTW STR 16-17L IAW EMB 145 SRM 53-31-04 ITEM 4 AND EO1-53-21-0168.

Part: SEAT TRACK — CORRODED (FRM 46) · airframe 47,987 hrs · 44,165 cycles

E867911 - RH UPPER SEAT TRACK SUPPORT CORRODED AT FR 46. ... PERFORMED PERMANENT REPAIR ON RH UPPER SEAT TRACK SUPPORT AT FRAME 46 AREA IAW EMB 145 SRM 53-00-11 ITEM 5 FIG 207 AND EO1-05-21-0176.

Part: RIB — CRACKED (RT WING) · airframe 47,987 hrs · 44,165 cycles

E867865 - RH WING RIB #21 CRACKED INSIDE PANEL 651CB. ... FURTHER INVESTIGATION OF SERVICE DOOR LOWER FRAME SHOWS TO HAVE 3 NUTPLATES WITH CORROSION. REMOVED CORROSION AROUND 3 NUTPLATES AND FOUND THE FWD 2 AREAS WITHIN ALLOWABLE LIMITS IAW EMB 145 SRM 52-43-06. PERFORMED PERMANENT REPAIR OF AFT DAMAGE IAW EO1-52-21-0169.

Part: ANGLE — CHAFED (CARGO DOOR) · airframe 47,987 hrs · 44,165 cycles

E868234 - CARGO DOOR AFT LOWER EDGE OTBD ANGLE IS CHAFED. ... RAR CARGO DOOR AFT EDGE OTBD ANGLE IAW EMB 145 SRM 51-40-02.

Part: SKIN — CRACKED (FRM 78 S3-8L) · airframe 47,987 hrs · 44,165 cycles

E867325 - EXTERNAL FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND 14 RIVETS ON FR 78 BTW STR 3L-8L. ... FURTHER INVESTIGATION OF EXTERNAL FUSELAGE SKIN POSSIBLE CRACKS AROUND 14 RIVETS ON FR 78 BTW STR 3L-8L FOUND ONLY 1 CRACK. SEE WIPS AND TASKS FOR NDT DETAILS. REFER TO NRTC E867324 FOR REPAIR IAW EO1-53-21-0174 AND ETD2021-145-021446.

Part: SKIN — CRACKED (FRM 79 S3-8R) · airframe 47,987 hrs · 44,165 cycles

EXTERNAL FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND 13 RIVETS ON FR 79 BTW STR 3R-8R. .... REPAIRED EXTERNAL FUSELAGE SKIN CRACK AROUND 1 RIVET ON FR 79 BETWEEN STRINGERS 8R AND 9R. 12 RIVETS WERE FOUND NOT TO HAVE CRACKS AROUND THEM, SEE TASK 1.

Part: SKIN — CRACKED (FRM 79 S3-9L) · airframe 47,987 hrs · 44,165 cycles

E867326 - EXTERNAL FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND 13 RIVETS ON FR 79 BTW STR 3L-9L. ... FURTHER INVESTIGATION OF THE 13 POSSIBLE EXTERNAL FUSELAGE SKIN CRACKS ON FR 79 BTW STR 3L-9L, ONLY 2 EA. CRACKS WERE FOUND. SEE TASK ENTRY #1 FOR NDT RESULTS. 1 EA. CRACK LOCATED BTW STR 4L-5L AND 1 EA. BTW STR 5L-6L. REPAIRED 2 EA. CRACKS WITH BUSHINGS IAW EO1-53-21-0181 STEPS 2 AND 3.

Part: SKIN — CRACKED (FRM 77 S2-8R) · airframe 47,987 hrs · 44,165 cycles

EXTERNAL FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND 26 RIVETS ON FR 77 BTW STR 2R-8R. ... REPAIRED EXTERNAL FUSELAGE SKIN CRACKS AROUND 3 RIVETS ON FR 77 BETWEEN STRINGERS 04R AND 08R IAW PIEDMONT EO1-53-21-0178 (BUSHING REPAIRS), REPAIRED EXTERNAL FUSELAGE SKIN CRACK AROUND 1 RIVET ON FR 77 IAW PIEDMONT EO1-53-21-0177(DOUBLER REPAIR). 22 RIVETS WERE FOUND NOT TO HAVE CRACKS AROUND THEM, SEE TASK 1.

Part: SKIN — CRACKED (FRM 77 S4-8R) · airframe 47,987 hrs · 44,165 cycles

EXTERNAL FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND 26 RIVETS ON FR 77 BTW STR 2R-8R. REPAIRED EXTERNAL FUSELAGE SKIN CRACKS AROUND 3 RIVETS ON FR 77 BETWEEN STRINGERS 04R AND 08R IAW PIEDMONT EO1-53-21-0178 (BUSHING REPAIRS), REPAIRED EXTERNAL FUSELAGE SKIN CRACK AROUND 1 RIVET ON FR 77 IAW PIEDMONT EO1-53-21-0177(DOUBLER REPAIR). 22 RIVETS WERE FOUND NOT TO HAVE CRACKS AROUND THEM, SEE TASK 1.

Part: BRACKET — BENT (RT NACELLE) · airframe 47,987 hrs · 44,165 cycles

E867564 - RH PYLON RIB 5 INTERNAL BRACKET BENT (RIVET INCORRECTLY INSTALLED MISSED BRACKET). REMOVED AND INSTALLED R/H PYLON RIB 5 INTERNAL BRACKET AND R/H PYLON UPPER AFT SKIN IAW EMB 145 SRM 51-40-02.

Part: SUPPORT — CORRODED (THRESHOLD) · airframe 47,987 hrs · 44,165 cycles

E869218 - L/H OTBD #3 FLOOR BOARD SILL IS CORRODED. ... REMOVED AND REPLACED SERVICE DOOR THRESHOLD IAW EMB 145 AMM 25-24-01.

Part: WEB — GOUGED (PAX DOOR) · airframe 47,987 hrs · 44,165 cycles

E867975 - MAIN PASSENGER DOOR INNER WEB GOUGED JUST ABOVE THE CENTER TORSION BAR. ... FABRICATED AND INSTALLED NEW SHEAR CLIP ON FR 66 STR 6L-7L IAW EMB 145 SRM 53-31-04 ITEM 2, FIG. 203 AND EO1-53-21-0183.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 47,987 hrs · 44,165 cycles

E867936 - BAGGAGE DOOR CUTOUT LOWER SILL CORRODED IN MULTIPLE AREAS. ... RAR CARGO DOOR CUTOUT LOWER SILL IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 47,987 hrs · 44,165 cycles

E868054 - LH OUTBD UPPER SEAT TRACK #1 IS CORRODED AT NUMEROUS AREA'S. ... REMOVED AND REPLACED LH OUTBD UPPER SEAT TRACK IAW EMB 145 AMM 53-01-06

Part: ATTACH FITTING — CORRODED (THRESHOLD) · airframe 47,987 hrs · 44,165 cycles

E868044 - PAX DOOR CUT-OUT LOWER THRESHOLD ATTACHMENT FITTING IS CORRODED. ... REMOVED AND INSTALLED SERVICEABLE PAX DOOR CUTOUT LOWER THRESHOLD ATTACHMENT FITTING IAW EMB 145 SRM 51-40-02

Part: ANTI-ICE VALVE — FAILED (NR 2 ENGINE) · airframe 47,376 hrs · 43,515 cycles

NR 2 ENGINE ANTI ICE FAILED AFTER TAKEOFF. R & R THE NR 2 ENGINE ANTI-ICE VALVE IAW AMM 30-21-01-000/400-801A. PERFORMED OPS CHECK IN REF TO AMM 30-00-70-700-802A. OPS CHECKED GOOD OK FOR SERVICE CLEAR MEL.

Part: PLATE — CRACKED (FLOOR SUPPORT) · airframe 47,085 hrs · 43,188 cycles

CENTER FUSELAGE DIGITAL PLATE IS CRACKED ON THE LEFT OMEGA FLOOR BEAM NEAR THE MAIN CABIN DOOR (IN-LINE WITH FRAME 21). ACTION TAKEN: PERFORMED HFEC OF AREA SURROUNDING THE CRACK INCLUDING THE OTHER SIDE OF THE NUT-PLATE THE CRACK ENDS AT. NO FURTHER DAMAGE DETECTED ON EITHER SIDE OF THE CRACK AND IT DOES NOT EXTEND BEYOND THE NUT-PLATE. AFTER CLEANING AND PREPARING THEY PERFORMED A 2ND HFEC AND FOUND CRACK TO EXTEND BEYOND THE NUT-PLATE HOLE BY .25". REPAIRED IAW EO1-53-20-0392. SEE EO AND ASSOCIATED HA-300'S FOR WORK PERFORMED.

Part: SLEEVE — BLOWN (NR 2 A/C PACK) · airframe 46,934 hrs · 43,023 cycles

BLEED 2 LEAK EICAS MESSAGE. TROUBLESHOT IAW FIM 36-20-00-810-802-A TO BLOCK 9. FOUND BLOWN OUT BLEED SLEEVE FROM PACK 2 VALVE TO HEAT EXCHANGER. REPLACED THE SLEEVE COUPLING AND CLAMPS AS REQUIRED. OPERATED THE PACK NR 2, NO DEFECTS NOTED. OK FOR SERVICE.

Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 46,775 hrs · 42,838 cycles

ON TAXI AND WHILE SITTING SPOILER FAIL MSG INTERMITTENT. R & R SCU IAW AMM 27-63-02, OPS CHECK GOOD. TAXIED AIRCRAFT, RAN ENGINES, NO DEFECTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 46,600 hrs · 42,638 cycles

PDIS 642 78-33 2216421 21MAR20 PHL ASSGN E2 REV DISAGREE MSG ON TAKEOFF . MEL 21MAR20 12:45 PHL C08106 78-2 ENG 1 OR 2 REV DISAGREE MESSAGES - DEACTIVATED AND STOWED TR1, INHIBITED ICU 1 FACT 20MAR20 20:52 PHL PERFORMED TR OPS CHECK IAW AMM 78-31-01. OPS CHECK G OOD. PERFORMED HIGH SPEED TAXI WITH CREW, NO E1 REV DISAGREE MESSAGE. CLEAR MEL 78-2. OK FOR SERVICE

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 46,600 hrs · 42,638 cycles

PDIS 642 78-34 2216403 20MAR20 PHL CLOSE E2 DISAGREE DURING T/O ROLL AT ABOUT 40KTS AND CLEARED DURING TAXI. CMC MESSAGE OF E2 ICU VALVE FAI FACT 20MAR20 02:09 PHL R&R DAU #2 AFT AVIONICS BAY AS PER AMM 31-31-07 OPS CHECK GOOD OK FOR SERVICE. CLEAR MEL 78-2 MEL ENG 1(2) REV DISAGREE MESS FACT 20MAR20 19:57 PHL TROUBLESHOT IAW FIM 78-30-00-810-814-A UP TO STEP 2.FOUND CONTINUITY ON A38. LOCKED E2 TR IAW AMM 78-31-01.REACTIVATED #1 TR FOR TROUBLESHOOTING PURPOSES (SHORT SIGN). MX ACTION COMPLETED. CLEAR MEL

Part: INVERTER — INOPERATIVE (COCKPIT) · airframe 45,463 hrs · 41,341 cycles

COCKPIT STEP EMERGENCY LIGHT INOP. R&R #100 EMERGENCY LIGHT INVERTER IAW 33-50-11-00/400-801-A. OKAY FOR SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 44,781 hrs · 40,574 cycles

NDIS 642 33-51 0004570 30APR19 RIC CLOSE EMERGENCY EXIT SIGN WILL NOT ILLUMINATE_IN FRONT OF SEAT 3B. 28713 00 NGR FACT 0APR19 06:47 RIC R/R'D 300 EMERGENCY LIGHT DC/AC INVERTER IAW AMM 33-50-11-000/400-801-A. OK FOR SERVICE. P/N ON INVERTER_P/N :7824-1 P/N OFF INVERTER_P/N :7824-1.

Part: CONNECTOR — DIRTY (CABIN) · airframe 44,577 hrs · 40,335 cycles

NDIS 642 33-51 0003890 24MAR19 RIC CLOSE EMERGENCY LIGHT AT SEAT 3B WILL NOT ILLLUMINATE FACT 24MAR19 09:39 RIC CLEANED AND RESECURED EMERGENCY LIGHT CONNECTORS FOR EMERGENCY LIGHT AT SEAT 3B IN REF TO AMM 32-50-14-000-701/400-801-A. OPS CHECK GOOD OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,233 hrs · 39,950 cycles

DIS 642 33-51 0002620 17JAN19 RIC CLOSE COCKPIT CEILING EMERGENCY LIGHT DOES NOT ILLUMINATE. FACT 17JAN19 08:11 RIC R/R LAMP FOR COCKPIT CEILING EMERGENCY LIGHT IN REF TO AMM 33-50-05-000/400-801-A. OPS CHECK GOOD OK FOR SERVICE. P/N ON LAMP, 1317 P/N OFF LAMP, 1317

Part: SIGN — INOPERATIVE (CABIN) · airframe 44,178 hrs · 39,883 cycles

PDIS 642 33-51 1861662 04JAN19 CLT CLOSE EMERGENCY EXIT SIGN AT ROW 2 IS INOP. FACT 04JAN19 10:19 CLT. REINSTALLED SIGN ON AFT GALLEY WALL, RESEATED CONNECTOR ON NR 2 BATTERY. OPS CHECK GOOD OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (ROW 3) · airframe 44,111 hrs · 39,807 cycles

NDIS 642 33-51 0002280 24DEC18 SBY CLOSE EMEGENCY LIGHT IN FRONT OF ROW 3 INOP FACT 24DEC18 09:44 SBY R&R EMERGENCY LIGHT IN FRONT OF ROW 3, SECURED WITH RETAINED HARDWARE PART INSTALLED/REMOVED SIGN 1013835

Part: RELAY — BURNED · airframe 43,845 hrs · 39,586 cycles

FOUND WIRE W102-0268-16 BURNT ON RELAY K0058 AND RELAY BASE XK0058. RE-TERMINATED WIRE W102-0268-16. R&R RELAY K0058 AND RELAY BASE K0058.

Part: BULB — INOPERATIVE (EMEGENCY LIGHT) · airframe 43,842 hrs · 39,484 cycles

LH OVER WING EMERGENCY LIGHT IS INOP.-C/A-COMPLETE:REMOVED AND REPLACED L/H OVER WING EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. OPC GOOD.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 43,842 hrs · 39,484 cycles

BAGGAGE DOOR EXTERNAL SKIN IS CRACKED NEAR HANDLE-C/A-COMPLETE:REPAIRED BAGGAGE DOOR EXTERNAL SKIN CRACKED NEAR HANDLE IAW ENVOY ERS-EM-52MR-916. SEE TASK AND WIPS FOR DETAILS.

Part: FRAME — CRACKED (FRM 23) · airframe 43,842 hrs · 39,484 cycles

FR 23 IS CRACKED AT RH OUTBD FLOOR SILL LOWER RIVET.-C/A-COMPLETE:REPAIRED FRAME 23 AT STRINGER 15R-16R AREA. IAW WITH EO# EM-53MR-1808.

Part: O-RING — DAMAGED (NR 3 BRAKE) · airframe 43,796 hrs · 39,429 cycles

CREW REPORTS FLUID LEAKING AT NR 3 BRAKE. FOUND ORING ON NR 3 BRAKE SHUTTLE VALVE QUICK DISCONNECT LEAKING. REMOVED AND REPLACED SHUTTLE VALVE QUICK DISCONNECT ORING IAW MM 32-49-03-400-802-A (PT) SUB TASK 42-003-A STEP (1) (I) THROUGH & INCLUDE (M) OPS & LEAK CHECK GOOD.

Part: PIN — BACKED OUT (CONNECTOR) · airframe 43,340 hrs · 38,997 cycles

FA EXIT MARKING SIGN ASSEMBLY INOP. FOUND PIN 4 ON CONNECTOR J8030 PUSH BACKED. RESECURED PIN IN SOCKET IAW SWPM 20-21-00. C/W OPS CHECK OF EMERGENCY LIGHTING SYSTEM IAW AMM 33-50-00 OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 43,240 hrs · 38,925 cycles

AFT FA FLASHLIGHT INOP. REMOVED AND REPLACED AFT FA FLASHLIGHT IAW AMM 25-60-11. OPS CHECK GOOD.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 42,882 hrs · 38,621 cycles

EMERGENCY LIGHT SWITCH NOT FUNCTIONING AS EXPECTED, LIGHTS COME ON WHEN OFF SELECTED. REMOVED AND REPLACED THE SWITCH IAW WC 33-700-17. ALL CHECKS PASSED.

Part: SWITCH — BROKEN (EMERGENCY LIGHTS) · airframe 42,879 hrs · 38,620 cycles

SWITCH FOR OVERHEAD PANEL EMERGENCY LIGHTS BROKE OFF. REPLACED THE LIGHT SWITCH IAW AMM 20-13-03 & OPS CHECKED IAW AMM 33-50-00. SYSTEM WORKING PROPERLY.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 42,654 hrs · 38,420 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,523 hrs · 38,285 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LT EXTERNAL OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: PRESSURE SWITCH — FAILED (FUREL SYSTEM) · airframe 42,189 hrs · 37,964 cycles

EICAS DISPLAYED E1 FUEL LOW PRESSURE FAIL IN FLIGHT. DECLARED EMERGENCY RESCUE MSN FLT DELAYED TILL AM. FOLLOWED QRH, CABIN PRESSURE ALTITUDE READING 10100 IN DESCENT AT 1300, RISING IN CLIMB AND CONTINUED RISING IN DESCENT UNTIL LEVEL AT 8000 THEN REMAINED AT AIRCRAFT ALTITUDE. FLIGHT CREW PLACARDED E1 FUEL LOW PRESS MESSAGE REF 28-13. REMOVED AND REPLACED E1 LOW PRESSURE SWITCH IAW AMM 28-45-01, OPS AND LEAK CK GOOD, MEL RESTORED. REMOVED AND REPLACED DIGITAL CONTROLLER PER AMM 21-31-01. OPC GOOD PER AMM 21-31-00. AIRCRAFT PRESSURIZES IN AUTO AND MANUAL MODES NORMALLY AT THIS TIME. DIGITAL CONTROLLER P/N 22250N030301 S/N 187.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,187 hrs · 37,963 cycles

FLIGHT ATTENDANT FRONT HEADSET HAS EMERGENCY LIGHT ON , ALL FLASHLIGHTS NOT CHARGING AND CD PLAYER NO WORKING. GPU ATTACHED AND SELECTED. REMOVED EXTERNAL POWER, INSTALLED A GPU, OPS CHECKED GOOD IAW AMM 24-40-00

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 40,907 hrs · 36,767 cycles

FA'S FLASHLIGHT DISCHARGED. FOUND STOWED SWITCHED ON. REMOVED AND REPLACED THE FA FLASHLIGHT. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,860 hrs · 36,725 cycles

LEFT FWD EXTERNAL EMERGENCY LIGHT LAMP INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,860 hrs · 36,725 cycles

AFT CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-08-000-801-A, AND 33-50-08-400-801-A. OPS CHECKED GOOD.

Part: SENSOR — MALFUNCTIONED (PITOT SYS) · airframe 40,037 hrs · 36,001 cycles

PITOT NR 1 INOPERATIVE EICS MESSAGE ILLUMINATED ON & OFF ON FOR ONE OR ONE OR MORE MINUTES OFF FOR 30 SECONDS. NO MESSAGE DURING GROUND OPS PITOT 1 APPEARED TO BE WORKING AS AIRSPEEDS MATCHED. REMOVED AND REPLACED STATIC PORT CURRENT SENSOR S0335 AND PITOT 1 CURRENT SENSOR K0056 IAW EMB 145 AMM 30-31-02 AND 30-31-01. OPS CHECK GOOD. REF NRWC 642-ORD-02916 FOR ALL WORK PERFORMED.

Part: TRUNNION — CRACKED (LT MLG) · airframe 39,742 hrs · 35,689 cycles

LT AFT UPPER MLG TRUNNION CRACKED OUTBD AFT SIDE. REMOVED AND REPLACED LT MLG AFT TRUNNION IAW ERS-EM-57MR-714.

Part: SPAR — CRACKED (RT WING) · airframe 39,742 hrs · 35,689 cycles

RT WING SPAR I LOWER FLANGE CRACKED AT SCREW HOLE AT RIB 9 AREA. REPAIRED RT WING SPAR I IAW ERS-EM-57MR-712.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 39,742 hrs · 35,689 cycles

LT OMEGA BEAM IS CORRODED BETWEEN FR58-59 AT LAV FLOORBOARD CROSSMEMBER. REPAIRED LT OMEGA BEAM IAW ERS-EM-53MR-2326.

Part: TRUNNION — CRACKED (RTMLG) · airframe 39,742 hrs · 35,689 cycles

RT AFT UPPER MLG TRUNNION CRACKED OUTBD AFT SIDE. REMOVED AND REPLACED RT MLG AFT TRUNNION IAW ERS-EM-57MR-707.

Part: STRIP — DAMAGED (CABIN) · airframe 39,697 hrs · 35,646 cycles

NR 1 PANEL STRIP IS DAMAGED. REMOVED AND REPLACED NR 1 PANEL STRIP IAW 145 AMM 33-50-12.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 39,308 hrs · 35,276 cycles

FORWARD CABIN FLASHLIGHT INOPERATIVE. REPLACED FWD CABIN FLASHLIGHT.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 39,074 hrs · 35,065 cycles

AFT OVERWING EMERGENCY LIGHT INOPERATIVE. R&R 4 EMERGENCY LIGHT INVERTER, OPC GOOD IAW AMM 33-50-11.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 38,915 hrs · 34,928 cycles

CENTER AISLE EMER EXIT REAR OF SIGN INOPERATIVE. FOUND CONNECTOR UNPLUGGED, SECURED CONNECTOR IAW AMM 33-50-15-400-801. OPERATIONS CHECKED GOOD.

Part: BRAKE — OVERHEATED (MLG) · airframe 37,805 hrs · 33,926 cycles

AFTER LANDING & PARKED AT THE RAMP, WE HAD AN INDICATION OF BRAKE OVERHEAT ON THE EICAS. ALSO THE MFD INDICATION OF THE LT OTBD & INBD WENT TO THE TOP OF THE YELLOW ARC. THE RAMP PERSONNEL REPORTED SMOKE COMING FROM THE LT MAIN GEAR. AFTER THE POST FLIGHT SOME UNUSUAL & UNKNOWN CONDITION OF BOTH LT TIRES. CONTACTED MOC & SENT PICTURES OF THE TIRES & THEY AGREE WITH THE UNUSUAL. PERFORMED TAXI CHECK WITH THE CREW & BRAKE OPERATIONAL CHECK IAW AMM 32-41-00. INSPECTED TIRES & FOUND TO BE WITHIN LIMITS IAW AMM 32-49-01. ACFT OKAY FOR SERVICE.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 37,783 hrs · 33,904 cycles

PASSENGER DOOR SKIN 3" SCRATCH & TWO SMALL GOUGES. REQUIRE REINSPECT IAW ERS-EM-52DF-463 PT B. ACCOMPLISHED PERMANENT REPAIR TO PAX DOOR SKIN IAW ERS-EM-52DF-463 PT D.

Part: LIGHT — DEFECTIVE (EXIT SIGN) · airframe 37,410 hrs · 33,543 cycles

OVERHEAD EMER EXIT LIGHT HARD TO SEE WHEN SET TO ON. R & R AFT CEILING EMER EXIT SIGN LIGHT IAW AMM 33-50-15. OPERATIONS CHECKED GOOD.

Part: PITOT SYSTEM — CONTAMINATED · airframe 35,519 hrs · 31,950 cycles

DURING CRUISE AT FL 360 CAPTAIN`S AIRSPEED DECREASED 10KT COMPARED TO STANDBY & FIRST OFFICERS AIRSPEED THEN CAPTAINS AIRSPEED DECREASED 30KT IN DESCENT. DRAINED MOISTURE FROM PITOT SYS IAW AMM 34-13-00. PERFORMED OPERATIONAL CHECK OF ADC SYS IAW AMM 34-15-00. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE. AMT IS NOT AUTHORIZED FOR CAT II. ACFT IS NOT CAT II OPERATIONS.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 35,380 hrs · 31,847 cycles

FLIGHT ATTENDANT FLASHLIGHT WILL NOT STAY CHARGING. R & R EMER FLASHLIGHT ASSEMBLY ABOVE FLIGHT ATTENDANT SEAT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 35,307 hrs · 31,786 cycles

CENTER AISLE AFT EMER EXIT LIGHT INOPERATIVE. R & R NR 4 INVERTER FOR CTR AISLE AFT EMER EXIT LIGHT IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 35,082 hrs · 31,583 cycles

AFT EMER FLASHLIGHT IS INOPERATIVE, CABIN. R & R AFT FLASHLIGHT ONLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: VALVE — FAILED (BLEED AIR SYS) · airframe 35,065 hrs · 31,566 cycles

DURING TAKEOFF ROLL HIGH STAGE 2 VLV FAIL MSG CAME ON TWICE. ABORTED TAKEOFF & RETURNED TO GATE. TRANSFERRED FROM LOG PAGE 3693766 ITEM NR 1 MEL 36-3. PERFORMED TROUBLESHOOTING IAW FIM 36-11-00. R & R NR 2 HIGH STAGE VLV IAW AMM 36-11-02. OPERATIONS CHECKED GOOD MEL RESTORED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,007 hrs · 31,509 cycles

FLIGHT ATTENDANT REPORTS FWD COURTESY LIGHT INOPERATIVE. FOUND FWD EMER, MAIN DOOR, LIGHT INOPERATIVE. RE LAMPED IAW AMM 33-50-06. USED BULB FROM SPARE BULB KIT.

Part: SPAR — CRACKED (LT WING) · airframe 34,957 hrs · 31,473 cycles

LEFT WING SPAR 3 CRACKED AT MLG PROXIMITY HARNESS ROUTING HOLE. ACCOMPLISHED LT WING SPAR III PERMANENT REPAIR IAW ERS-EM-57MR-222.

Part: SPAR — CRACKED (RT WING) · airframe 34,957 hrs · 31,473 cycles

RIGHT WING SPAR 3 CRACKED AT MLG PROXIMITY HARNESS ROUTING HOLE. ACCOMPLISHED RT WING SPAR III PERMANENT REPAIR IAW ERS-EM-57MR-219.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,957 hrs · 31,473 cycles

LEFT FUSELAGE SKIN CRACKED AFT OF FRAME 75, ABOVE STRINGER 2L. CRACK APPROX LENGTH 3/8 INCHES. PERFORMED REPAIR AFT OF FRAME 75 ABOVE STRINGER 2L IAW ERS-EM-53MR-698.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,957 hrs · 31,473 cycles

RIGHT FUSELAGE SKIN CRACKED AFT OF FRAME 75 ABOVE STRINGER 2R. CRACK APPROX LENGTH 9/16 INCHES. PERFORMED REPAIR TO RT FUSELAGE SKIN AFT FRAME 75 & STRINGER 2R IAW ERS-EM-53MR-697.

Part: WIRE — BROKEN (CABIN) · airframe 34,957 hrs · 31,473 cycles

LEFT NR 1 EMER PROXIMITY LIGHT STRIP HAS BROKEN WIRE, FOUND DURING INSTALL. R & R LT NR 1 EMER PROXIMITY LIGHT STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: FRAME — GOUGED (FUSELAGE) · airframe 34,957 hrs · 31,473 cycles

FRAME 70 HAS 2 GOUGES BETWEEN STRINGER 12R - 13R. REPAIRED IAW ERS-EM-53MR-679.

Part: LIFE VEST — UNKNOWN (COCKPIT) · airframe 34,957 hrs · 31,473 cycles

A121 OVERHEAD CREW LIFE VEST CMM 25-60-06, CMM 25-64-02 CAPTAIN SN US1002840. R & R CAPTAIN`S LIFE VEST IAW ELL-08-12.

Part: LIFE VEST — UNKNOWN (CABIN) · airframe 34,957 hrs · 31,473 cycles

A32 RESTORE INFANT LIFE VEST IAW CMM 25-60-15 G1 SN C58691. R & R INFANT LIFE VEST SN C58691 IAW ELL-08-12.

Part: LIFE VEST — UNKNOWN (CABIN) · airframe 34,957 hrs · 31,473 cycles

A32 RESTORE INFANT LIFE VEST IAW CMM 25-60-15 G1 SN C64904. R & R INFANT LIFE VEST SN C64904 IAW ELL-08-12.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 34,957 hrs · 31,473 cycles

VERIFY CORRECT REPAIR ON SKIN BETWEEN FRAME 27 - 28 STRINGER 13R - 14R. NO FILLER INSTALLED. PERFORMED REPAIR IAW ERS-EM-53MR-693. R & R DOUBLER.

Part: LIGHT — CRACKED (CABIN) · airframe 34,957 hrs · 31,473 cycles

LIGHT STRIP NR 4 EXTRUSION IS CRACKED. REPLACED LIGHT STRIP NR 4 EXTRUSION IAW AMM 33-50-08. SEE BOW 161234 FOR FINAL INSTALL.

Part: RELIEF VALVE — FAILED (BRAKE SYSTEM) · airframe 34,957 hrs · 31,473 cycles

EMERGENCY & PARKING BRAKE SYS THERMAL RELIEF VLV FAILED FUNCTIONAL CHECK. R & R EMER & PARKING BRAKE SYS THERMAL RELIEF VLV IAW AMM 32-44-06. LEAK CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,957 hrs · 31,473 cycles

LEFT FUSELAGE SKIN CRACKED AT FRAME 75, 1ST FASTENER BELOW STRINGER 2L. CRACK APPROX LENGTH 1/2 INCHES. SEE NRWC E400943 FOR CORRECTIVE ACTION FOR REPAIR.

Part: WINDOW FRAME — CORRODED (COCKPIT) · airframe 34,957 hrs · 31,473 cycles

PILOT'S WINDSHIELD INNER FRAME CORRODED ALONG LOWER SURFACE NEAR FASTENERS HOLES. BLENDED AREAS ALONG LOWER SURFACE FASTENER HOLES ON PILOT'S WINDSHIELD & ACCEPTED AS IS IAW ERS-EM-5600-041.

Part: COVER — CRACKED (LT WING) · airframe 34,957 hrs · 31,473 cycles

LEFT WING NR 2 TORQUE BOX COVER CRACKED. REPAIRED LT WING NR 2 TORQUE BOX COVER IAW ERS-EM-5700-216.

Part: SPLICE — DAMAGED (CABIN) · airframe 34,957 hrs · 31,473 cycles

EMERGENCY LIGHTING, EXIT LOCATOR, FWD INDICATOR ON CEILING PANEL INOPERATIVE. REPAIRED SPLICES SP 9208 & SP 9209 ON EMER LIGHTING IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: LIGHT — CRACKED (CABIN) · airframe 34,957 hrs · 31,473 cycles

LIGHT STRIP NR 1 EXTRUSION IS CRACKED. REPLACED LIGHT STRIP IAW AMM 33-50-08. SEE BOW 161234 FOR FINAL INSTALL.

Part: LIGHT — CRACKED (CABIN) · airframe 34,957 hrs · 31,473 cycles

LIGHT STRIP NR 5 EXTRUSION IS CRACKED. REPLACED LIGHT STRIP IAW AMM 33-50-08. SEE BOW 161234 FOR FINAL INSTALL.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 34,957 hrs · 31,473 cycles

RIGHT BEAM INBD SUPPORT CRACKED AT FRAME 47. REMOVED CRACKED RT BEAM INBD SUPPORT AT FRAME 47, PREPPED & INSTALLED SERVICEABLE BEAM SUPPORTS IAW SRM 53-23-02.

Part: WIRE — BROKEN (CABIN) · airframe 34,957 hrs · 31,473 cycles

LIGHT STRIP NR 5 HAS BROKEN WIRE AT STRIP. REPLACED NR 5 EMER LIGHT STRIP IAW AMM 33-50-08. SEE BOW 161234 FOR FINAL INSTALL & OPERATIONAL CHECK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,957 hrs · 31,473 cycles

RIGHT FUSELAGE SKIN CRACKED AT FRAME 75, 1ST FASTENER BELOW STRINGER 2R. CRACK APPROX LENGTH 3/8 INCHES. SEE NRWC E400940 FOR CORRECTIVE ACTION OF REPAIR FOR RT FUSELAGE SKIN.

Part: REVEAL — CRACKED (CABIN) · airframe 34,957 hrs · 31,473 cycles

RIGHT EMER EXIT WINDOW REVEAL ASSEMBLY IS CRACKED. R & R RT EMER EXIT WINDOW REVEAL ASSEMBLY IAW AMM 25-23-09.

Part: LIGHT — CRACKED (CABIN) · airframe 34,957 hrs · 31,473 cycles

LIGHT STRIP NR 3 EXTRUSION IS CRACKED. REPLACED LIGHT STRIP IAW AMM 33-50-08. SEE BOW 161234 FOR FINAL INSTALL.

Part: WIRE — DAMAGED (CABIN) · airframe 34,957 hrs · 31,473 cycles

EMERGENCY LIGHTING, EXIT MARKER, AFT OF RT OVERWING EXIT INOPERATIVE. REPAIRED WIRE ON EMER LIGHTING IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD.

Part: PANEL — CRACKED (RAM AIR INTAKE) · airframe 34,957 hrs · 31,473 cycles

LEFT & RIGHT RAM AIR PANEL INTAKES ARE CRACKED NEXT TO ACTUATORS. REPAIRED LT & RT RAM AIR PANEL INTAKES IAW ERS-EM-5300-695 OVEN 6132 GAGE 3337.

Part: LIGHT — CRACKED (CABIN) · airframe 34,957 hrs · 31,473 cycles

LIGHT STRIP NR 6 EXTRUSION IS CRACKED. REPLACED LIGHT STRIP IAW AMM 33-50-08. SEE BOW 161234 FOR FINAL INSTALL.

Part: ACTUATOR — FAILED (RAM AIR VALVE) · airframe 34,847 hrs · 31,345 cycles

RAM AIR VLV FAIL. R & R LT RAM AIR LINEAR ACTUATOR IAW AMM 21-25-03. OPERATIONS CHECKED GOOD.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 34,692 hrs · 31,212 cycles

ACFT PRIMARY AIRSPEED INDICATORS ON BOTH FIRST OFFICER & CAPTAIN SIDES UNRELIABLE. WHILE CLIMBING FROM FL360 TO 370, PRIMARY IND'S 265 KIAS WITH A HIGH SPEED WARNING. ACTUAL AIRSPEED WAS 230 KIAS VIA THE STBY IND. DECLARED EMER & DESCENDED. DURING DESCENT PRIMARY AIRSPEED SLOWLY DECREASED TO 90 KIAS WHILE ACTUAL WAS 230 KIAS. UNRELIABLE AIRSPEED CHECKLIST COMPLIED IAW AOM VOL 1, WHILE DESCENDING THRU FL1. INSPECTED PITOT LINES & FOUND WATER, DIRT & DEBRIS. DRAINED WATER & PERFORMED CLEANING OF THE PITOT LINES IAW AMM 34-13-00. PERFORMED ADJUSTMENT TEST OF ADC SYS OPERATIONS & LEAK CHECK GOOD IAW AMM 34-15-00. ALSO PERFORMED A FINAL PITOT STATIC SYS LEAKAGE TEST NO LEAKS FOUND & WORKING PROPERLY IAW AMM 34-13-00. ACFT REMAINS RVSM ELIGIBLE. .

Part: CRADLE — DEFECTIVE (FLASHLIGHT) · airframe 34,628 hrs · 31,171 cycles

FLASHLIGHT IN REAR OF ACFT WILL NOT STAY SECURED IN THE CRADLE. R & R THE AFT CABIN FLASHLIGHT CRADLE IAW AMM TASKS 33-50-16-000-801-A33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 34,205 hrs · 30,824 cycles

DURING FINAL APPROACH, BAGGAGE SMOKE WARNING ON EICAS. DURING INSPECTION, FOUND NO INDICATION OF FIRE OR SMOKE. R & R HIGH RATE BAGGAGE FIRE BOTTLE BECAUSE IT WAS DISCHARGED IAW AMM 26-23-01, OPS CHECKED GOOD. R & R AFT CARGO SMOKE DETECTOR IAW AMM 26-15-01, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,156 hrs · 30,786 cycles

EMERGENCY LIGHTING SYS FAILED OPERATIONAL CHECK. R & R NR 1 EMERGENCY BATTERY & POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 34,156 hrs · 30,786 cycles

EMERGENCY LIGHTING SYS FAILED OPERATIONAL CHECK. R & R NR 1 EMERGENCY BATTERY & POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 34,156 hrs · 30,786 cycles

SEVERAL DAMAGED FASTENER HOLES BETWEEN FRAME 18 & FRAME 19 & BETWEEN STRINGER 5L & 6L. PERFORMED REPAIR TO DAMAGED FASTENER HOLES IAW AEA ERS-EM-53MR-333 PART A.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 34,156 hrs · 30,786 cycles

PASSENGER DOOR FRAME INNER WEB CRACKED BETWEEN FRAME 16 & FRAME 17 ABOVE DOOR CUT OUT AT FWD LIGHTNING HOLE. PERFORMED REPAIR PAX DOOR FRAME INNER WEB BETWEEN FRAME 16 & FRAME 17 ABOVE DOOR CUT OUT AT FWD LIGHTNING HOLE IAW AEA ERS-EM-53MR-334 PART A.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 34,156 hrs · 30,786 cycles

MULTIPLE HAIL DAMAGE EVENT REPLACE RT ELEVATOR LE. R & R RT ELEVATOR LE IAW SRM 51-40-02 & AEA ETN-EM-55-073.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,156 hrs · 30,786 cycles

MULTIPLE HAIL DAMAGE EVENT REPLACE CTR FUSELAGE II SKIN. R & R UPPER CTR FUSELAGE II SKIN IAW SRM 51-40-02 & ETN-EM-53-263.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 34,156 hrs · 30,786 cycles

MULTIPLE HAIL DAMAGE EVENT REPLACE RT ELEVATOR ROOT SKIN. R & R RT ELEVATOR ROOT SKIN IAW SRM 51-40-02 & AEA ETN-EM-55-073.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 34,156 hrs · 30,786 cycles

MULTIPLE HAIL DAMAGE EVENT REPLACE RT ELEVATOR TIP SKIN. R & R RT ELEVATOR TIP SKIN IAW SRM 51-40-02 & AEA ETN-EM-55-073.

Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 34,156 hrs · 30,786 cycles

MULTIPLE HAIL DAMAGE EVENT REPLACE RT STABILIZER SKIN. R & R RT HORIZONTAL STAB TOP SKIN IAW SRM 51-40-02 & AEA ETN-EM-55-073.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 34,156 hrs · 30,786 cycles

MULTIPLE HAIL DAMAGE EVENT REPLACE LT ELEVATOR ROOT SKIN. R & R LT ELEVATOR ROOT SKIN IAW SRM 51-40-02 & AEA ETN-EM-55-073.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 34,156 hrs · 30,786 cycles

MULTIPLE HAIL DAMAGE EVENT REPLACE LT STABILIZER SKIN. R & R LT HORIZONTAL STAB TOP SKIN IAW SRM 51-40-02 & AEA ETN-EM-55-073.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,156 hrs · 30,786 cycles

MULTIPLE HAIL DAMAGE EVENT REPLACE CTR FUSELAGE I LT SKIN. R & R CTR FUSELAGE I LT SKIN IAW SRM 51-40-02 & ETN-EM-53-262.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,156 hrs · 30,786 cycles

MULTIPLE HAIL DAMAGE EVENT REPLACE CTR FUSELAGE I RT SKIN. R & R CTR FUSELAGE I RT SKIN IAW SRM 51-40-02 & AEA ETN-EM-53-262.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,156 hrs · 30,786 cycles

FOUR EMERGENCY LIGHTS COME ON WHEN POWER IS REMOVED FROM ACFT. R & R NR 3 EMERGENCY LIGHT POWER SUPPLY & BATTERY PACK IAW AMM 33-50-04, OPS CHECKED GOOD.

Part: HOLDER — FAILED (CABIN) · airframe 34,156 hrs · 30,786 cycles

BATTERY HOLDER ASSEMBLY 2013-1A SN 103136 FAILED OPERATIONAL CHECK. REMOVED BATTERY HOLDER ASSEMBLY 2013-1A SN 103136, FAILED OPERATIONAL CHECK.

Part: HOLDER — DEFECTIVE (CABIN) · airframe 34,156 hrs · 30,786 cycles

BATTERY HOLDER ASSEMBLY LIGHT IS ALWAYS ON, PN 2013-1A & SN 67592. REMOVED BATTERY HOLDER ASSEMBLY LIGHT PN 2013-1A & SN 67592.

Part: DOOR — STUCK (LAVATORY) · airframe 33,901 hrs · 30,585 cycles

FLIGHT ATTENDANT CANNOT OPEN DOOR IN LAVATORY TO CHECK THE FIRE EXTINGUISHER. C/A FREED STUCK DOOR, IAW AMM 26-25-01, NO FURTHER DEFECTS NOTED.

Part: A/C PACK — MALFUNCTIONED (AC BAY) · airframe 33,866 hrs · 30,560 cycles

PACK 1 OVERLOAD CAUTION MESSAGE CYCLING ON & OFF AT 24,000 FT WITH A LIGHT BURNING SMELL WHICH WENT AWAY AFTER PACK 1 WAS DESELECTED.

Part: APU — ODOR · airframe 33,371 hrs · 30,168 cycles

LAVATORY SMOKE WARNING ON EICAS DURING CLIMBOUT THROUGH 1000 FT, PASSENGER REPORTED SLIGHT ODOR OF ELECTRICAL BURNING. ACCOMPLISHED ETN EM-72-034 R4 TWICE. FOUND ODOR TO BE RESIDUAL OIL FROM APU REMOVAL & REPLACEMENT. NO ODORS NOTED AT THIS TIME.

Part: CARBON SEAL — LEAKING (RT ENGINE) · airframe 33,371 hrs · 30,169 cycles

WHILE INVESTIGATING SMOKE ODOR IN CABIN, FOUND RT ENGINE ZERO CARBON SEAL LEAKING. R & R RT ENGINE ZERO CARBON SEAL IAW MM 72-25-25. OPS CHECKED GOOD. ACCOMPLISHED ETN EM-72-034 R4. NO DEFECTS NOTED.

Part: DOOR — LACK OF LUBE (MAIN CABIN) · airframe 33,177 hrs · 30,010 cycles

THE MAIN CABIN DOOR IS HARD OPEN. LUBRICATED MAIN CABIN CABIN DOOR FRAME ROLLERS IAW AMM 53-21-02. TESTED SATISFACTORY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,314 hrs · 29,361 cycles

DURING B-INSPECTION, FOUND THE CEILING EMERGENCY LIGHT AT ROW 7 INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE BULB IN CEILING EMERGENCY LIGHT AT ROW 7 IAW AMM33-50-08. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 31,688 hrs · 28,867 cycles

ON FLIGHT 3415 THE CREW REPORTED A STRONG OIL SMELL IN THE COCKPIT AT LOW THRUST SETTINGS AND LOW ALTITUDES NOT NOTICABLE IN CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LEFT ENGINE REQUIRED INSPECTION FOR VIBRATION OF THE TURBINE SECTION DUE TO REINSTALLATION OF FAN BLADES. INSPECTED LEFT ENGINE FAN AND NR 0 CARBON SEAL AREAS FOR OIL LEAKAGE PER RR MM 72-00-00 AND NO LEAKS WERE FOUND. THE LEFT ENGINE LP VIBRATION WAS WITH IN LIMITS IAW RR MM 72-50-00. NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED TO FUNCTIONAL CHECK FLIGHT PER TECH SERVICES AND RR TECH REP RECOMENDATION. THE FUNCTIONAL CHECK FLIGHT WAS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (MAIN DOOR) · airframe 30,779 hrs · 28,140 cycles

ON FLIGHT 2915 THE CREW REPORTED THE MAIN DOOR WAS HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED ROLLERS ON MAIN PASSENGER DOOR IAW EMB 145 AMM 52-10-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,646 hrs · 28,025 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT AT SEAT 12 B/C OVERHEAD INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB AT SEAT 12 B/C IAW EMB 145 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: LIGHT — INOPERATIVE (CABIN) · airframe 30,497 hrs · 27,902 cycles

DURING B INSPECTION FOUND THE FORWARD CABIN EMERGENCY CEILING LIGHT AT 3B INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN EMERGENCY CEILING LIGHT AT 3B. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-08. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,497 hrs · 27,902 cycles

DURING B INSPECTION FOUND THE RIGHT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT OVERWING EMERGENCY LIGHT BULB. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,254 hrs · 27,707 cycles

DURING B INSPECTION FOUND THE RIGHT NR 2 FLOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT NR 2 FLOOR SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRIP — DAMAGED (CABIN) · airframe 30,254 hrs · 27,707 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT EMERGENCY LIGHT STRIP EXTRUSION NR 1, 8 AND 7 DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EMERGENCY LIGHT STRIP EXTRUSION NR 1, 8 AND 7 IAW EMB 145 ZMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 30,254 hrs · 27,707 cycles

DURING B INSPECTION FOUND FRAME 67 T-PROFILE SUPPORT ANGLE CRACKED AT CARGO DOOR SILL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FRAME 67 T-PROFILE SUPPORT ANGLE AT CARGO DOOR SILL IAW EMB SRM 51-40-02,CPM 51-21-05, 51-21-06, AEA ETN-EM-51-075, AND ETN-GN-51-016. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 30,254 hrs · 27,707 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 30,254 hrs · 27,707 cycles

DURING B INSPECTION FOUND FRAME 66 T-PROFILE SUPPORT ANGLE IS CRACKED AT CARGO DOOR SILL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FRAME 66 T-PROFILE SUPPORT ANGLE AT CARGO DOOR SILL IAW EMB SRM 51-40-02, CPM 51-21-05, CPM 51-21-06, AEA ETN# EM-51-075, AND ETN# GN-51-016. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 30,254 hrs · 27,707 cycles

DURING B INSPECTION FOUND THE RIGHT FLOORBEAM GUSSET CORRODED BETWEEN FRAMES 59-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FLOORBEAM GUSSET BETWEEN FRAMES 59-61. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,254 hrs · 27,707 cycles

DURING B INSPECTION FOUND THE RIGHT FLOOR SILL CORRODED BETWEEN FRAMES 35-40. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FLOOR SILL BETWEEN FRAMES 35-40 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,254 hrs · 27,707 cycles

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

Part: WIRE — BROKEN (CABIN) · airframe 30,254 hrs · 27,707 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP NR 7 HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP NR 7 IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 30,254 hrs

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

Part: STRIP — CRACKED (CABIN) · airframe 30,254 hrs · 27,707 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP FORWARD RAMP PANEL EXTRUSION CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP FORWARD RAMP PANEL EXTRUSION IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,254 hrs · 27,707 cycles

DURING B INSPECTION FOUND THE LEFT OUTBOARD FLOOR SILL CORRODED BETWEEN FRAMES 19-22. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OUTBOARD FLOOR SILL, BETWEEN FRAME 19-20 IAW EMB SRM 51-40-02 NR 1 SILL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 30,254 hrs · 27,707 cycles

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

Part: WIRE — BROKEN (LIGHT PANEL) · airframe 30,254 hrs · 27,707 cycles

DURING MAINTENANCE INSPECTION FOUND THE SERVICE DOOR FORWARD EMERGENCY LIGHT PANEL HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY EXIT SIGN/LIGHT ON SERVICE DOOR FORWARD LINER IAW EMB 145 AMM 33-50-13. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: O-RING — FAULTY (BLEED SYSTEM) · airframe 30,237 hrs · 27,687 cycles

FLIGHT 2800 THE CREW REPORTED THAT CLIMBING THROUGH AT 6000 FEET THEY RECEIVED A BLEED 1 LEAK MESSAGE ON EICAS. THE CREW COMPLIED WITH EPC +AOM VOL 1 AND DECLARED AN EMERGENCY. THE CREW RETURNED TO DFW AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED O-RINGS AT JOINTS 1, 3, 5, 7, 9, 16, 17, 19, 25, 28. THE OPERATIONAL CHECK WAS GOOD ALSO REFERNCE NRWC 642-DFW-00960 THRU 00966. NO OTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DISPLAY — FAILED (COCKPIT) · airframe 29,222 hrs · 26,885 cycles

ON FLIGHT 2795, THE CREW REPORTED THAT WHILE ON DESCENT THE CAPTAIN’S PFD WENT OUT HAD A LIGHT BURNING ODOR, THEN WENT AWAY. THE AIRCRAFT LANDED WITHOUT INCIDENT. INTERNAL COOLING FAN IN CAPT'S PFD BURNED OUT MAKING PFD OVERHEAT, THEN SHUT OFF. REMOVED AND REPLACED CAPTAINS SERVICEABLE MULT FUNCTION DISPLAY UNIT IAW EMB AMM 34-22-01.THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 2,942 hrs · 26,871 cycles

DURING B-INSPECTION FOUND THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHT IAW EMB 145 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: HOLDER — BROKEN (CABIN) · airframe 29,205 hrs · 26,871 cycles

DURING B-INSPECTION FOUND THE FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,807 hrs · 26,569 cycles

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

Part: STRAP — DETACHED (SMOKE GOGGLES)

FOR FLIGHT 4314 DURING PREFLIGHT INSPECTION MAINTNANCE FOUND THE FIRST OFFICER’S SMOKE GOGGLE STRAP OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-ATTACHED FIRST OFFICER’S SMOKE GOGGLES RETAINING STRAP IAW STANDARD MAINTENANCE PRACTICES. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN)

TWICE DURING FLIGHT EXPERIENCED AN ODOR IN COCKPIT AND FWD PART OF CABIN - SMELLED LIKE INDUSTRIAL PLASTIC. NO VISUAL CLUES JUST ODOR. PERFORMED ETN EM 72-034R4. DVI OF AIRDUCTS, COCKPIT LIGHTING AND PANELS, PASSENGER CABIN AND GALLEY LIGHTING AND RELATED EQUIPMENT INCLUDING DVI OF RELAY PANELS AND RELATED AREAS. GROUND RAN AIRCRAFT WITH NO OCCURANCES OF PLASTIC SMELL IN COCKPIT OR CABIN.

Part: UNKNOWN — ODOR (CABIN) · airframe 27,484 hrs · 25,572 cycles

PLASTIC SMELL IN COCKPIT AND FORWARD PART OF CABIN. SMELL DID GO AWAY ONCE AND CAME BACK 20 MIN LATER. DID NOT DECLARE EMERGENCY. LANDED WITHOUT INCIDENT. DID NOT SMELL LIKE A BURNING SMELL. COULD NOT DUPLICATE. PASSED FCF. TRIAD RELEASED AIRCRAFT TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,254 hrs · 25,380 cycles

ON FLIGHT 3932 THE FLIGHT ATTENDANT REPORTED THE FORWARD FLASHLIGHT WAS NOT CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE FORWARD FLIGHT ATTENDANT FLASH LIGHT ASSEMBLY PER EMB 135AMM 33-50-16 . THE OPERATIONAL CHECK WAS GOOD PER EMB 135 AMM 33-51-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INTERMITTENT (EXTERIOR) · airframe 26,475 hrs · 24,787 cycles

FOR FLIGHT 3641 DURING PRE FLIGHT INSPECTION FOUND THE EXTERNAL RIGHT LOWER FORWARD FAIRING EMERGENCY LIGHT TO WORK INTRMITTENTLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT LOWER FORWARD FAIRING EMERGENCY LIGHT. THE OPERATIONAL TEST WAS OK. REF EMB AMM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: AHRS — MALFUNCTIONED (COCKPIT) · airframe 25,944 hrs · 24,405 cycles

ON FLIGHT 3605 DURING CRUISE THE CREW REPORTED, RECEIVED AN ATTITUDE HEADING REFERENCE SYSTEM FAIL EICAS MESSAGE. THE CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TO SAV. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 ATTITUDE HEADING REFERENCE SYSTEM IAW EMB AMM 34-21-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,254 hrs · 23,853 cycles

ON FLIGHT 2789 DURING INSPECTION FOUND THE AFT EXTERNAL OVERWING EMERGENCY LIGHTS ON THE LEFT AND RIGHT SIDE TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY AND CHARGER IAW AMM 33-50-0. ALSO REMOVED AND REPLACED THE LEFT AFT EXIT EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — MALFUNCTIONED (PAX DOOR) · airframe 24,128 hrs · 23,000 cycles

ON FLIGHT 2705 THE CREW REPORTED THE MAIN PASSENGER DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK PER EMB AMM AND THE DOOR CHECKED GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: THERMOSTAT — INOPERATIVE (BLEED AIR SYS) · airframe 23,245 hrs · 22,237 cycles

DURING FLIGHT 3489 THE CREW REPORTED A NUMBER 2 BLEED LOW TEMPERATURE MESSAGE IN ICING CONDITIONS. THE CREW DECLARED AND EMERGENCY AND DUE TO THE WEATHER DIVERTED TO XNA. THE AIRCRAFT LANDED WITHOUT INCIDENT. NO OTHER PROBLEMS WERE NOTED BY THE CREW. REMOVED AND REPLACED THE NUMBER 2 FAN AIR THERMOSTAT IAW AMM 36-11-06. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUT — FAULTY (NLG) · airframe 22,532 hrs · 21,690 cycles

ON FLIGHT 3816 THE CREW REPORTED THAT AFTER TAKEOFF AND UPON SELECTING GEAR UP, GOT A LANDING GEAR "AIR /GROUND FAIL" MESSAGE. THE LANDING GEAR DID NOT RETRACT. THE CREW DIVERTED TO TUL TO BURN FUEL WITH THE GEAR DOWN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NOSE LANDING GEAR STRUT ASSEMBLY IAW EMB-145 AMM 32-22-01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,449 hrs · 19,883 cycles

DURING A MBV INSPECTION. THE LT OMEGA BEAM AT FRAME 29 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE LT OMEGA BEAM TO REMOVE THE DAMAGE. PREPARED A REPAIR DOUBLE, FILLER AND TWO SHIMS. MARKED, DRILLED, CLEANED AND TREATED REPAIR PART. REPAIR DONE IAW SRM 53-00-10, FIGURE 202. ACFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,449 hrs · 19,883 cycles

DURING A MBV INSPECTION THE CARGO DOOR SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CARGO DOOR SILL. POSITIONED NEW SILL AND DRILLED. REPAIR DONE IAW EMB SRM (SRM EMB-145/1142 REV 40) CHAPTERS 51-20-03 AND 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: ACM — MALFUNCTIONED (A/C BAY) · airframe 19,018 hrs · 18,573 cycles

ON FLIGHT 3653, CREW REPORTED DURING TAXI OUT WITH APU BLEED SUPPLYING THE PACKS A HAZE IN THE COCKPIT AND CABIN WAS NOTED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LT HEAT EXCHANGER AND LEFT ACM IAW EMB AMM 21-51-02 AND 21-51-03. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: A/C PACK — ODOR · airframe 19,018 hrs · 18,573 cycles

ON FLIGHT 3653, CREW REPORTED DURING TAXI OUT WITH APU BLEED SUPPLYING THE PACKS A "HAZE" IN THE COCKPIT AND CABIN. ALSO DETECTED A BURNING SULFUR ODOR.

Part: FRAME — DAMAGED (ZONE 100) · airframe 17,161 hrs · 16,911 cycles

DAMAGE BETWEEN FRAME 67 AND STRINGERS 15R AND 16R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB IC2007-145/04150. RETURNED AIRCRAFT TO SERVICE.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 16,456 hrs · 16,371 cycles

SEVERAL OVERHEAD CABIN LIGHTS INOPERATIVE ABOVE ROWS 16 AND 17A, SMOKE SMELL REPORTED. REMOVED AND REPLACED BALLAST FOR CEILING LIGHTS AT 16 AND 17A IAW EMB AMM 33-21-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND LEFT INBOARD SEAT TRACK FROM FRAME 30 TO 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND OUTBOARD SEAT TRACK FROM FRAME 36 TO 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND LEFT INBOARD SEAT TRACK FROM FRAME 18 TO 21 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND RIGHT OUTBOARD SEAT TRACK FROM FRAME 24 TO 30 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,942 cycles

DISC - FOUND RIGHT INBOARD SEAT TRACK FROM FRAME 24 TO 30 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND LEFT OUTBOARD SEAT TRACK FROM FRAME 24 TO 30 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB SRM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND RIGHT INBOARD SEAT TRACK FROM FRAME 30 TO 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND RIGHT OUTBOARD SEAT TRACK FROM FRAME 30 TO 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND RIGHT INBOARD SEAT TRACK FROM FRAME 36 TO 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND LEFT INBOARD SEAT TRACK FROM FRAME 36 TO 47 CORRODED. REMOVED AND REPLACED IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND LEFT OUTBOARD SEAT TRACK FROM 47 TO 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND RIGHT OUTBOARD SEAT TRACK FROM FRAME 47 TO 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND RIGHT OUTBOARD SEAT TRACK FROM FRAME 53 TO 59 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND LEFT OUTBOARD SEAT TRACK FROM FRAME 36 TO 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND LEFT OUTBOARD SEAT TRACK FROM FRAME 17 TO 24 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND LEFT INBOARD SEAT TRACK FROM FRAME 24 TO 30 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND LEFT OUTBOARD SEAT TRACK FROM FRAME 53 TO 59 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: RECEPTACLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND LAVATORY RECEPTICLE CORRODED ON SKIN ATTACHMENT. REMOVED AND REPLACED CUP ASSEMBLY IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,547 hrs · 15,492 cycles

DISC - FOUND LEFT OUTBOARD SEAT TRACK FROM FRAME 30 TO 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB SRM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB)

ORD - FLT 4142 - DURING APPROACH CREW REPORTED A DUAL PITCH TRIM FAILURE WITH AUTO PILOT ON AFTER SELECTING FLAPS TO 9 DEGREES. IAS WAS 210 KNOTS IN SMOOTH AIR IN VMC CONDITIONS LEVELING OFF AT 5000 FEET. NO CONTROL COLUMN FORCE WAS FELT DUE TO AUTO PILOT BEING ON. REPLACED HSCU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

FOUND FLOOR EMERGENCY LIGHTING INOPERATIVE FROM ROWS 7-12 INCLUDING EXIT ROW LIGHTS. REPLACED NR 3 POWER SUPPLY. OPS CHECK GOOD. (M)

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

DURING SCHEDULED MAINTENANCE CHECK, THE EXIT LIGHT AT ROWS 12C WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 5 INVERTER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

DURING PRE-FLIGHT, THE CREW NOTED EMERGENCY EXIT LIGHTS AT ROW 12 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AC/DC INVERTER IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RAI EXIT MARKER ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

EMERGENCY LIGHT AT EXIT 12 C INOPERATIVE. CLEANED CONNECTORS ON THE EMERGENCY LIGHT AT EXIT 12C. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SUPPORT — CORRODED (PAX DOOR FRAME)

ABI - DURING AN IMBV INSPECTION, THE PASSENGER DOOR LOWER SEALING SUPPORT FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED THE LOWER SEALING SUPPORT AND ATTACHED STRUCTURE. FABRICATED A REPLACEMENT SUPPORT. FABRICATION AUTHORITY CONTAINED IN EMB STATEMENT IC2003-145/1435. REPAIR DONE IAW EMB STATEMENT IC2003-145/1435, EMB SRM, SRM 145/1142 REV 21, 51-20-03, 51-40-02, 51-40-06, EMB CPM, CPM 145/1132 REV 8, 51-21-04, 51-21-05, 51-21-06, AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (GALLEY)

ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR LOWER CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED THE CENTER SILL AND INSTALLED NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 21, CHAPTERS 51-40-02, 51-40-06, 51-20-03. (M)

Part: SILL — CORRODED (SERVICE DOOR)

ABI - DURING AN IMBV INSPECTION, THE SERVIE DOOR CENTER SILL WAS FOND TO BE CORRODED BEYOND SRM LIMITS. REMOVED EXISTING SERVICE DOOR CENTER SILL AND INSTALLED NEW SILL IAW EMB SRM, SRM EMB-145/1142 REV 21, CHAPTERS 51-40-02, 51-40-03, 51-40-06 AND CPM 51-21-04. (M)

Part: SILL — CORRODED (GALLEY)

THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, GALLEY AREA RIGHT AFT SILL HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02/06, 51-20-03. (M)

Part: GUSSET — CORRODED (CARGO BAY)

THIS IS A LEVEL 2 FINDING, FOUND ON AN IMBV INSPECTION CARGO ENTRY GUSSET HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02/06, 51-20-03. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION SERVICE DOOR SILL HAS CORROSION. REMOVED DAMAGED SILL AND INSTALLED NEW SERVICE DOOR SILL IAW EMB 145 SRM 51-20-03, 51-40-02/06 AND EMB CPM 5-21-04. (M)

Part: ANGLE — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION GALLEY CROSSBEAM AND PROFILE CORRODED. REMOVED AND REPLACED CROSSBEAM AND PROFILE IAW EMB 145 SRM 51-40-02/04, 51-20-03. (M)

Part: SILL — CORRODED (SERVICE DOOR)

ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION SERVICE DOOR FORWARD SILL CORRODED. REMOVED CORRODED FORWARD SILL AND INSTALLED SERVICEABLE SILL IAW EMB SRM 51-40-02. (M)

Part: BEAM — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, GALLEY CENTER BEAM GUSSET CORRODED. REMOVED AND INSTALLED NEW CENTER BEAM IAW EMB 145 SRM 51-40-02/04/06, 51-20-03. (M)

Part: STRINGER — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON STRINGER 21R BETWEEN FRAMES 12 AND 13. CUT OUT 2 DAMAGED AREAS OF STRINGER LOWER FLANGE BETWEEN FRAMES 12 AND 13. FABRICATED 2 FILLERS, 1 REINFORCEMENT, REPAIR DONE IAW EMB GST-2763/02 PARA 2B, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE GALLEY FLOOR FORWARD DIGITAL. CORROSION WAS REMOVED AND AREA WAS REPAIRED IAW EMB GST-2713/01 AND SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. CORROSION WAS REMOVED AND AREA WAS REPAIRED IAW EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)

Part: SWITCH — REVERSED (CAPTAIN YOKE) · airframe 2,871 hrs · 3,076 cycles

DURING CLIMB-OUT, CAPTAIN NOTED HIS PITCH TRIM SWITCH DOING THE OPPOSITE OF WHAT WAS COMMANDED. FIRST OFFICER AND STAND BY SWITCHES OPERATED NORMAL. AIRCRAFT WAS RETURNED TO CRP SAFELY WITH NO FURTHER INCIDENTS REPORTED. C/A- MAINTENANCE REMOVED AND REPLACED THE PILOTS TRIM SWITCH IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — FAILED (RT MLG BRAKE)

OMA - FLT 4174 - NR 2 BRAKE TEMP INDICATION WENT HIGH ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. INDICATION RETURNED TO NORMAL. ISSUED MEL 3202 AUTH 040027. REMOVED AND REPLACED NR 1 BRAKE TEMP SENSOR IAW AMM OPS CHECK GOOD. (M)