N699AE

Part: SWITCH — FAULTED (ZONE 800) · airframe 45,338 hrs · 42,460 cycles

DURING TAKEOFF AT 4000 FT BAG DOOR INDICATION INDICATED OPEN. RETURNED TO FIELD. OPERATED DOOR MULTIPLE TIMES. DOOR OPERATES NORMALLY. PERFORMED GENERAL VISUAL INSPECTION OF BAGGAGE DOOR AREA. NO DEFECTS NOTED. DETERMINED TO BE AN INDICATION ISSUE. INSTALLED BOTH BAGGAGE DOOR MICROSWITCHES IAW AMM 52-76-01-04, ADJUSTED AND TESTED BOTH MICROSWITCHES IAW AMM 52-7601-05. OPS CHECK GOOD. USED MULTIMETER TO CHECK FOR CONTINUITY OHMS AND PROPER VOLTAGE FOR SHORTS, NO DEFECTS TO NOTE. OK FOR SERVICE AT THIS TIME.

Part: LOCK — LACK OF LUBE (ZONE 800) · airframe 45,337 hrs · 42,459 cycles

ENROUTE BAGGAGE DOOR OPEN INDICATION DISPLAYED. ON GROUND RAMP CONFIRMED DOOR NOT FULLY LATCHED. COMPLIED WITH BAGGAGE DOOR ACTUATING AND LOCKING MECHANISM OPS CHECK IAW AMM 52-31-00-700-801. NO DEFECTS NOTED. LUBED DOOR ACTUATING AND LOCKING MECHANISM IAW AMM 52-31-00-600-801. PERFORMED OPERATION OF BAGGAGE DOOR AND NO DEFECTS NOTED. OPS CHECKED GOOD

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 44,995 hrs · 42,051 cycles

EMERGENCY FLOOR STRIP 2 & 3 DIM AND THE SECOND CEILING EMERGENCY LIGHT IS INOP. R & R EMERGENCY BATTERY 200; FLOOR PROX STRIP 2 &3, OPS CHECKED GOOD. FOUND CONNECTOR PLUG FOR SECOND EMERGGENCY CEILING LIGHT UNPLUGGED; RECONNECTED CONNECTOR AND OPS CHECK GOOD. ALL WORK DONE PER AMM 33-50-04 AND AMM 33-50-05.

Part: O-RING — FAILED (BLEED SYS) · airframe 44,598 hrs · 41,578 cycles

BLD 1 LEAK IN FLIGHT DURING CLIMB. R & R FOUR O-RINGS ON BLEED AIR DUCT COUPLING IN AFT AVIONICS BAY AT L/H FWD FIREWALL IAW AMM 36-11-09. LK CHECK & OPS CHECKS GOOD.

Part: EXHAUST DUCT — LEAKING (NR 2 A/C PACK) · airframe 44,593 hrs · 41,570 cycles

BLD 1 LEAK DURING AT 7000FT MSG EXTINGUISH AFTER TURNING OFF BLDS. FOUND PACK 2 EXHAUST DUCT AND SLEEVE AT HEAT EXCHANGER LEAKING. R+R EXHAUST DUCT AND SLEEVE AS REQUIRED.

Part: DOOR — STUCK (MAIN) · airframe 43,926 hrs · 40,855 cycles

CANNOT GET MAIN PAX DOOR OPEN FACT 03MAR25 00:45 PHL FOUND CIRCLIP ON INTERMEDIATE TORQUE TUBE UNSEATED. RE-SEATED CIRCLIP IRW AMM 52-18-01. OPS CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 900) · airframe 43,067 hrs · 39,929 cycles

LAV SMOKE IND CONTINUESLY ALERTED. NO ACTUALLY SMOKE WAS OBSERVED. FACT 24SEP24 02:17 PHL INSPECTED & OPS CHECKED LAV SMOKE DET IRW AMM 26-14-00. OPS CHECK GOOD. NO DEFECTS NOTED, A/C OK FOR SERVICE.

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 42,837 hrs · 39,647 cycles

ON CLIMBOUT CABIN DID NOT PRESSURIZE REACHED 10,000 FT AND RETURNED TO FIELD----CREW DID NOT SPECIFY IF THEY TRIED BOTH AUTO AND MANUAL MODE BECAUSE THERE WAS TOO MUCH GOING ON "THEIR WORDS" THEY JUST RTF. MEL 10AUG24 18:20 CLT C22321 21-12-3 PRESS CONTROL AUTO AND MANUAL FACT 12AUG24 04:41 SBY TROUBLESHOT UTILIZONG FIM TASK 21-31-00-810-809-A R&R'D DIGITAL CONTROLLER IAW AMM 21-31-01. OPS CHECK GOOD A/C OK FOR SERVICE CLEAR MEL 21-12-3

Part: DISPLAY — ODOR (COCKPIT) · airframe 42,257 hrs · 38,990 cycles

EGREGIOUS SMELL IN COCKPIT FACT 28APR24 13:02 CLT UPON INSPECTION FOUND FO PFD TO BE THE EGREGIOUS SMELL. R/R F/O PFD IAW EMB AMM 34-22-01. OPS CHECK GOOD. A/C OK FOR SERVICE. SPRAYED A/C WITH AIR FRESHENER.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 38,103 cycles

53-2079 CF3 LH SILL #4 BTW FR 36-42 CORRODED. R&R'D SILL #4 IAW SRM 51-40-42, 51-20-03, AND 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 38,103 cycles

53-2087 CF3 LH GUSSET #4 BTW FR 36-42 IS CORRODED. R&R'D GUSSET IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 38,103 cycles

53-2101 CF1, CORROSION FOUND ON RH DOUBLER FLOOR STRUCTURE AT FR22. R&R'D DOUBLER FLOOR STRUCTURE IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 38,103 cycles

23-2092 CF2 RH GUSSET #2 BTW FR 30-36 IS CORRODED. R&R'D GUSSET IAW SRM 51-22-10, 51-20-03, AND 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 38,103 cycles

53-2085 CF2 LH GUSSET #2 BTW FR23-29 CORRODED. R&R'D #2 GUSSET IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 38,103 cycles

53-2086 CF2 LH GUSSET #3 BTW FR 29-35 CORRODED. R&R'D GUSSET #3 IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 38,103 cycles

53-2131 CF1 RH OMEGA BEAM UNDER FLOOR DOUBLER AT FR 22 CORRODED. R&R'D OMEGA BEAM IAW SRM51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2073 LH OMEGA BEAM VERTICAL FLANGE CRACKED AT FR36. REPAIRED IAW PIEDMONT EO1-53-53-0317

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2041 LIGHTNING STRIKE ON FUSELAGE SKIN AT 6INCHES FWD OF FR34 AND 7TH RIVET FWD OF STR2R. REPAIRED IAW SRM51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 38,103 cycles

53-2102 CORROSION FOUND ON MIDDLE GUSSET FLOOR STRUCTURE BTW FR18-22. R&R'D GUSSET IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2106 RH OMEGA BEAM OB AFT ANGLE TO WHEEL WELL BTW FR46-50 CRACKED. R&R'D OMEGA BEAM ANGLE IAW SRM 53-23-02 AND PIEDMONT EO1-53-23-0328.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2108 RH OMEGA BEAM IB ANGLE TO WHEEL WELL CRACKED BTW FR46-50. R&R'D RH OMEGA BEAM IB ANGLE IAW SRM 53-23-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2314 ELONGATED HOLE ON OMEGA BEAM BTW FR20-21. REPAIRED IAW PIEDMONT EO1-53-23-0323

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2326 NLG WHEEL WELL DRAG BRACE RH HOUSING BEARING WORN. REPAIRED IAW PIEDMONT EO1-53-23-0335

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

52-2323 UNDOCUMENTED REPAIR ON PAX DOOR SKIN .6" AFT OF HANDLE 1.2" BELOW STR10L. R&R'D REPAIR IAW PIEDMONT EO1-52-23-0321

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2095 CTR OMEGA BEAM LH ANGLE TO WHEEL WELL CRACKED BTW FR46-50. REPAIRED IAW PIEDMONT EO1-53-23-0328

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

55-2244 LH VERTICAL STAB LWR STRAP FUSELAGE FASTENERS LOOSE. REPAIRED IAW ETD2023-145-025934

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2029 2 CRACKS AT FR79 1 RIVET BELOW AND ABOVE STR8R. REPAIRED IAW PIEDMONT EO1-53-23-0338

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2105 LH OMEGA BEAM OB ANGLE TO WHEEL WELL CRACKED BTW FR46-50. R&R'D OB OMEGA BEAM ANGLE IAW SRM53-23-02 AND PIEDMONT EO1-53-23-0328

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2174 LIGHTNING STRIKE ON LH CENTER FUSE 3 UPPER SKIN, 4.7" AFT OF FR45 AND .8" BELOW STR4L. REPAIRED IAW PIEDMONT EO1-53-23-0341

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 38,103 cycles

32-2320 BOTH NLG TRUNNION FITTINGS ARE CORRODED. REPAIRED IAW PIEDMONT EO1-53-23-0335

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2045 LIGHTNING STRIKE ON RH TOP SKIN AT 2.8INCHES FWD OF FR27 AT STR2R 3RD RIVET FWD. REPAIRED IAW SRM51-40-02 AND ETD2023-145-027072

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2097 LH OMEGA BEAM IB ANGLE TO WHEEL WELL SKIN CRACKED AT FR46-50. R&R'D OMEGA BEAM IAW SRM 53-23-02 AND PIEDMONT EO1-53-23-0328

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2024 CRACKS(2) ON SKIN AT FR79 AT STR4L AND 5L. REPAIRED IAW PIEDMONT EO1-53-23-0338

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2044 LIGHTNING STRIKE ON FUSELAGE SKIN AT 4.5 INCHES FWD OF FR29 ON STR2R 5TH RIVET FWD. REPAIRED IAW PIEDMONT EO1-53-23-0344

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

57-2312 OVERSIZED HOLES ON LH AND RH WING RIBS 01A LOWWER SURFACE. REPAIRED IAW PIEDMONT EO 1-57-23-0343

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2331 UNRECORDED REPAIR AT FWD FUSELAGE BTW FR6-7 STR15L. R&R'D DOUBLER IAW PIEDMONT EO1-53-23-0339

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2069 CTR OMEGA BEAM IB VERTICAL FLANGE CRCKED AT FR33. REPAIRED IAW ETD2023-145-025187 AND PIEDMONT EO 1-53-23-0318

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,484 hrs · 38,103 cycles

53-2028 CRACK ON SKIN AT FR77 1 RIVET BELOW STR4R. REPAIRED IAW PIEDMONT EO1-53-23-0338

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2070 LH OMEGA BEAM IB VERTICAL FLANGE CRACKED AT FR21, FR22, FR23. R&R'D LH OMEGA BEAM IAW SRM51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 38,103 cycles

53-2254 FLOOR LEVEL CORRODED AT BTW FR14-18 Y479. REPAIRED IAW SRM 53-21-10

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2072 LH OMEGA BEAM (#3) IB VERTICAL FLANGE IS CRACKED AT FR31, FR33, FR34, ANFR35. R&R'D OMEGA BEAM IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2040 LIGHTNING STRIKE ON TOP SKIN SPLICE AT 5.3INCHES AFT OF FR35 AND 3.5 INCHES ABOVE STR2R. REPAIRED IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 38,103 cycles

53-2098 CORROSSION FOUND ON PREVIOUS REPAIR OF RH SERVICE DOOR AFT SILL FRAME AT FR22-23 AT FLOOR STRUCTURE AREA. REPAIRED IAW SRM 53-21-10

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

TWO ANGLES SUPPORT UNDER MIDDLE GUSSET BTW FR18-23 ARE CRACKED. R&R'D ANGLES IAW SRM51-40-02TWO ANGLES SUPPORT UNDER MIDDLE GUSSET BTW FR18-23 ARE CRACKED. R&R'D ANGLES IAW SRM51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2326 NLG WHEEL WELL DRAG BRACE RH HOUSING BEARING WORN. REPAIRED IAW PIEDMONT EO1-53-23-0335

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2071 LH OMEGA BEAM (#2) IB VERTICAL FLANGE CRACKED AT FR24, FR26, FR27, AND FR28. R&R'D LH OMEGA BEAM 2 IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2332 UNRECORDED REPAIR DOUBLER AT FWD FUSELAGE LEFT UPPER SKIN BTW FR6-7 AND BTW STR9L-11L. R&R'D DOUBLER IAW PIEDMONT EO1-53-23-0340

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2042 LIGHTNING STRIKE ON FUSELAGE SKIN AT 2.7 INCHES AFT OF FR32 AND 2R 3RD RIVET AFT. REPAIRD IAW SRM51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2030 LIGHTNING STRIKE ON SKIN AT FR77 1 RIVET ABOVE STR7R REPAIRED IAW SRM 51-10-07, 51-20-08, AND 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

27-2271 ANCHOR NUT MISSING FROM RUDDER 2. REPAIRED IAW PIEDMONT EO1-27-23-0332

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2050 LIGHTNING STRIKE ON FUSELAGE SKIN AT 6.5INCES FWD OF FR17 ON STR4R 7TH RIVET FWD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

55-2327 RH VERTICAL STAB AT SPAR 3 VF63.3 ON CLOSING ANGLE, 1 COUNTERSINK DAMAGED. REPAIRED IAW ETD2023-145-025921, ETD 2023-145-019907, AND PIEDMONT EO1-53-23-0333

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 38,103 cycles

53-2068 CF2 CENTER OMEGA BEAM IB VERTICAL FLANGE CRACKED AT FR25 AND FR27. REPAIRED IAW ETD2023-145-024919

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,966 hrs · 37,499 cycles

DURING T/O ROLL, BOTH FUEL QUNTY INDICATORS WENT TO DASHED LINES. UPON INSP FOUND BATT SWITCH ON SPR PANEL IN AN UNSEATED INTERMEDIATE POSITION. CYCLED SWITCH, INDICATIONS RETURNED AND PANEL FUNCTIONS AS INTENDED. OK FOR SERVICE AT THIS TIME

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,846 hrs · 37,346 cycles

SUDDEN ENGINE #1 FAILURE AT FLIGHT LEVEL 290, SPEED WAS MACH .76. ( CAPTAIN SAID IT WAS ABRUPT SHUTDOWN AND EICAS MESSAGES WERE ENG 1 SHORT DISP, ENG 1 OUT, RUDDER HARDOVER PROTECTION FAIL.

Part: NONE — NONE · airframe 40,510 hrs · 36,969 cycles

MAIN PITCH TRIM INOP EICAS MESSAGE DURING CLIMBOUT, AUTO PILOT NOT SELECTED, FO FLYING FACT 03MAR23 10:36 PHL INSP CMC FOUND HSCU FAILURE. R&R'D HSCU IAW EMB 145 MM 27-40-01 OPS CHECK GOOD OK FOR SERVICE

Part: CONTROLLER — FAULT MESSAGE · airframe 40,096 hrs · 36,539 cycles

PDIS 699 21-31 2796581 14DEC22 CLT CLOSE PRESSURIZATION AUTO FAILED ON EICAS. ACCOM. OPER. PROC. APP 1 21-12. PRESS THE DUMP BUTTON FACT 14DEC22 01:57 ROA T/S PER FIM TASK 21-31-00-810-801-A. FOUND DIGITAL CONTROLLER TO BE BAD. R/R'D DIG CONTROLLER IAW MM 21-31-01-000-801-A/400. OPS CK GOOD PER MM 21-31-00-700-801-A AND 802A, CLEAR MEL.

Part: NONE — NONE · airframe 39,005 hrs · 35,328 cycles

PDIS 699 52-71 2708702 29APR22 CLT CLOSE DURING TAKEOFF BAGG DOOR OPEN EICAS MSG DISPLAYED FACT 30APR22 02:17 ROA FOUND MICROSWITCH ROLLER TO BE WORN. R&R'D MICROSWITCH ROLL IN REF W/AMM 52-76-01. OPS CK GOOD IN REF W/AMM 52-76-01-700-801-A. CLEAR MEL 52-3-2.

Part: NONE — NONE · airframe 38,043 hrs · 34,241 cycles

PDIS 699 36-11 2600211 23OCT21 PHL CLOSE BLEED 2 OVERTEMP DISPLAYED ON EICAS. FACT 23OCT21 16:02 PHL R+R E2 AIR VAILVE FILTER IAW AMM EMB 145 36-11-03, R+R E2 HSV FILTER IAW AMM EMB 145 36-11-02. OPS CHECK IAW AMB AMM 145 36-00-00-700-803A. OPS CHECK GOOD AT THIS TIME. OK FOR SERVICE

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,954 hrs · 34,198 cycles

EMERGENCY EXIT SIGN OVER FA SEAT INOP. REMOVED AND REPLACED #100 EMERGENCY LIGHT DC/AC INVERTER IN REF. TO AMM TASK 33-50-11-000/400-801-A. OPS CHECK GOOD.

Part: INDICATOR — FAULTED (FUEL QTY) · airframe 37,540 hrs · 33,695 cycles

DURING TAXI FUEL QTY LOW MASTER WARNING APPEARED WITH FUEL INDICATION GOING TO DASHES ON EICAS. (HAPPENED AS A/C RECEIVED PERMISSION TO ENTER RWY). PERFORMED OPS CHECK IAW AMM 28-41-00. OPS CHECK GOOD. OK FOR SERVICE. ALL FUEL QUANTITY INDICATIONS NORMAL AND NO MESSAGES PRESENT.

Part: SKIN — CRACKED (ZONE 200) · airframe 37,090 hrs · 33,184 cycles

LH UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L, CRACK IS APPROX. 3/8" LONG. (MARKED) EASI #8071 USED, 100-500 KHZ PROBE, FREQ= 400KHZ, V-GAIN=76.0, H-GAIN =64.0, LPF=100....INSTALLED SERVICEABLE REPAIR PARTS (REPAIR DOUBLER, FILLER, ANGLE AND SHIM) ON LH UPPER FUSELAGE SKIN AT FR 75 AT STR 2L IAW EMB 145 SRM 53-31-01, ITEM 11, FIG. 219 SHEET 1, EO1-53-21-0039.

Part: SKIN — CRACKED (ZONE 200) · airframe 37,090 hrs · 33,184 cycles

POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FR 77 BTW STR 4L-5L....PERFORMED PT INSPECTION IAW EASI NDTM. EASI 0452. CRACK ENDS MARKED.REMOVED THE CRACK AREA ON FUSELAGE SKIN AND INSTALLED SKIN BUSHING ON EXTERNAL FUSELAGE SKIN AT RIVET AT FR 77 BTW STR 4L-5L IAW EMB145 SRM 53-32-01RE ITEM 9, EO1-53-21-0040. SEE TASK AND WIPS FOR FURTHER DETAIL

Part: SKIN — CRACKED (ZONE 200) · airframe 37,090 hrs · 33,184 cycles

POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FR 77 BTW STR 8L-9L... PERFORMED PT INSPECTION IAW EASI NDTM. EASI 0452. CRACK ENDS MARKED....REMOVED CRACKED AREA ON EXTERNAL FUSELAGE SKIN AND INSTALLED SKIN BUSHING ON EXTERNAL FUSELAGE SKIN AT RIVET AT FR 77 BTW STR 8L-9L IAW EMB145 SRM 53-32-01RE ITEM 9, EO1-53-21-0040.

Part: SKIN — CRACKED (ZONE 200) · airframe 37,090 hrs · 33,184 cycles

POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FR 77 BTW STR 8R-9R....PERFORMED PT INSPECTION IAW EASI NDTM. EASI 0452. CRACK ENDS MARKED....REMOVED THE CRACK AREA ON FUSELAGE SKIN AND INSTALLED SKIN BUSHING ON EXTERNAL FUSELAGE SKIN AT RIVET AT FR 77 BTW STR 8R-9R IAW EMB145 SRM 53-32-01RE ITEM 9, EO1-53-21-0040. SEE TASK AND WIPS FOR FURTHER DETAIL

Part: SKIN — CRACKED (ZONE 200) · airframe 37,090 hrs · 33,184 cycles

POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FR 79 BTW STR 6L-7L....PERFORMED PT INSPECTION IAW EASI NDTM. EASI 0452. CRACK ENDS MARKED....REMOVED THE CRACK AREA ON FUSELAGE SKIN AND INSTALLED SKIN BUSHING ON EXTERNAL FUSELAGE SKIN AT RIVET AT FR 79 BTW STR 6L-7L IAW EMB145 SRM 53-32-01RE ITEM 9, EO1-53-21-0040. SEE TASK AND WIPS FOR FURTHER DETAIL

Part: BEAM — CORRODED (LT OVERWING EXIT) · airframe 37,090 hrs · 33,184 cycles

CORROSION ON HARDWARE ON LH CABIN ESCAPE HATCH AT LOWER RUBBER STOP....UPON FURTHER INVESTIGATION FOUND LH OVERWING EMERGENCY EXIT BEAM #4 TO BE CORRODED, REMOVED AND REPLACED THE BEAM IAW EMB145 SRM 51-40-02. SEE TASK AND WIP ENTRIES FOR DETAILS.

Part: ATTACH BRACKET — GOUGED (BULKHEAD) · airframe 37,090 hrs · 33,184 cycles

PILOTS BULKHEAD OTBD UPPER ATTACHMENT BRACKET IS GOUGED....REPAIRED PILOTS BULKHEAD OUTBOARD UPPER ATTACHMENT BRACKET IAW PIEDMONT EO1-53-21-0038. SEE TASK AND WIP ENTRIES FOR DETAILS

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 37,090 hrs · 33,184 cycles

SSI 53-20-29 TOILET WASTE VALVE SUPPORT IS CORRODED....RAR LAV BUCKET IAW EMB 145 SRM 51-20-03 AND 51-40-02. SEE TURNOVER FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (FRAME 19) · airframe 37,090 hrs · 33,184 cycles

RH OMEGA BEAM CORRODED AROUND NUT PLATE HOLE AT FR 19....REPAIRED R/H OMEGA BEAM ON NUTPLATE HOLE AT FRAME 19 IAW EO1-53-21-0031. SEE WIPS AND TASKS FOR DETAILS

Part: CROSSBEAM — CORRODED (FRM 20) · airframe 37,090 hrs · 33,184 cycles

CROSSBEAM AT FR 20 CORRODED.....REMOVED AND REPLACE THE CROSS BEAM AT FR20 IAW EMB 145 SRM'S 51-40-02, 53-21-10 AND PIEDMONT BULLETIN 53-3 R1.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 37,090 hrs · 33,184 cycles

RH OMEGA BEAM DIAMOND GUSSET AT FR20 CORRODED AROUND NUT PLATE HOLES....REMOVED AND REPLACED THE RH OMEGA BEAM DIAMOND GUSSET AT FR20 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 37,090 hrs · 33,184 cycles

RH #4 CABIN FLOOR SILL CORRODED....REMOVED AND REPLACED THE RH #4 CABIN FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 37,090 hrs · 33,184 cycles

RH #5 CABIN FLOOR SILL CORRODED....REMOVED AND REPLACED RH #5 CABIN FLOOR SILL IAW EMB145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 37,090 hrs · 33,184 cycles

LH #5 CABIN FLOOR SILL CORRODED....REMOVED AND REPLACED LH #5 CABIN FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 37,090 hrs · 33,184 cycles

RH FLOORBOARD SILL #3 CORRODED....REMOVED AND REPLACED THE RH FLOORBOARD SUPPORT SILL #3 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 37,090 hrs · 33,184 cycles

RH #6 CABIN FLOOR SILL CORRODED....REMOVED AND REPLACED RH #6 CABIN FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (MAIN CABIN) · airframe 37,090 hrs · 33,184 cycles

LH #3 CABIN FLOOR SILL CORRODED....REMOVED AND REPLACED THE LH #3 CABIN FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED · airframe 37,090 hrs · 33,184 cycles

PAX DOOR FWD FLOORBOARD SUPPORT CORRODED AROUND NUT PLATE HOLES....REMOVED AND REPLACED DEFECTIVE PART IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · airframe 37,090 hrs · 33,184 cycles

PAX DOOR AFT FLOORBOARD SUPPORT CORRODED AROUND NUT PLATE HOLES....REMOVED AND REPLACED PAX DOOR AFT FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02

Part: STRINGER — GOUGED (ZONE 200) · airframe 37,090 hrs · 33,184 cycles

STRINGER 2L IS GOUGED BETWEEN FRAMES 20-21....COMPLETED CENTER FUSELAGE I STRINGER 2L BETWEEN FRAME 20-21 GOUGE IAW PIEDMONT EO NO E01-53-21-0042.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 36,403 hrs · 32,414 cycles

CLIMBING THRU 600FT HEARD LOUD PO FOLLOWED BY E1 AUTO SHUT DOWN. ATTEMPTED RESTART TO NO AVAIL....FIX: R&RD #1 ENG IAW W/C 71-00-00. OPS CHECK/LEAK CHECK GOOD.

Part: ENGINE — SHUTDOWN (NR 1) · airframe 35,916 hrs · 31,868 cycles

#1 ENG SHUT DOWN ON ITS OWN PASSING THRU FLT LEVEL 330. FOLLOWED QRH ATTEMPTED RESTART FAILED. ENG OUT EICAS MSG DISPLAYED. FIX ENGINE IS REMOVED AND REPLACED.

Part: SCREW — MISSING (STOP BRACKET) · airframe 33,853 hrs · 29,428 cycles

NDIS 699 52-10 0003740 21NOV18 MDT CLOSE MAIN CABIN ENTRANCE DOOR- FWD LWR DOOR STOP BRAKET H AS 1 SCREW MISSING 26739 00 HSM FACT 21NOV18 08:52 MDT INSTALLED SCREW NUT AND WASHER TO FWD LOWER DOOR STO P SUPPORT BRACKET IRT EMB145 MM 52-18-00

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 33,530 hrs · 29,037 cycles

PDIS 699 27-51 1724322 25SEP18 CHA CLOSE FLAP FAIL MESSAGE IN FLIGHT NO FLAP INDICATION ON EICAS. CMC SHOWS FLAP ELECTRONIC UNIT FAIL. 24934 00 JDJ HISTORY: YES. #1 CHANNEL ALREADY ON MEL.ROA MX HISTORY: ROADTRIP ETD 2230. A/C OUT OF POSITION. FACT 26SEP18 07:31 PHF R/R EFCU IAW AMM 27-53-02-04. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 33,446 hrs · 28,945 cycles

EMERGENCY LIGHT ON SERVICE DOOR INOP. REPAIRED BROKEN WIRE, OPS CHECK GOOD.

Part: BATTERY — OVERTEMP (MAIN) · airframe 33,278 hrs · 28,752 cycles

BATT 1 OV/TEMP MSG INFLT 258 DEG 79 DEG ON GATE. REMOVED AND REPLACED NR 1 BATTERY IAW AMM 24-36-01. OPS CHECK GOOD OK FOR SERVICE.

Part: BATTERY — OVERTEMP (MAIN) · airframe 33,278 hrs · 28,752 cycles

BATT 1 OV/TEMP MSG INFLT 258 DEG 79 DEG ON GATE. REMOVED AND REPLACED NR 1 BATTERY IAW AMM 24-36-01. OPS CHECK GOOD OK FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 33,228 hrs · 28,680 cycles

CREW NOTICED ELECTRICAL SMELL DURING CRUISE PHASE OF FLIGHT IN COCKPIT AND FWD CABIN. LASTED FOR 10 MINS AND DISSIPATED. RAN ENGINES AND PACKS FOR 30 MIN AND RAN ELECTRICAL SYSTEMS NO ODOR NOTICED IN CABIN OR COCKPIT. INSPECTED FWD CABIN FOR ANY ELECTRICAL ANOMOLIES. NO DEFECTS NOTED, OK FOR SERVICE.

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 33,160 hrs · 28,609 cycles

ENROUTE NR 1 HYD SYS WENT INTO YELLOW WITH HYD LOW QTY EICAS. SERVICED NR 1 HYD SYS IAW AMM 12-13-01 OK FOR SERVICE.

Part: YOKE — CRACKED (LT PYLON) · airframe 33,156 hrs · 28,607 cycles

LT PYLON ENGINE FORWARD LOWER YOKE CRACKED. (BEHIND LOWER FWD ENG MOUNT). REMOVED UNSERVICEABLE AND INSTALLED NEW LT PYLON ENGINE FORWARD LOWER YOKE IAW EO EM-54MR-386.

Part: YOKE — CRACKED (RT PYLON) · airframe 33,156 hrs · 28,607 cycles

RT PYLON ENGINE FORWARD LOWER YOKE CRACKED. (BEHIND LOWER FWD ENG MOUNT). REMOVED AND REPLACED RT PYLON ENGINE FORWARD LOWER YOKE IAW EO EM-54MR-386.

Part: FITTING — CRACKED (EXIT LIGHT) · airframe 33,156 hrs · 28,607 cycles

NR 1-2-3-5 LT ISLE FLOOR LIGHT EXTRUSION CRACKED. REMOVED AND REPLACED NR 1,2,3, AND 5 LT ISLE FLOOR LIGHT EXTRUSIONS IAW AMM 33-50-12.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,156 hrs · 28,607 cycles

RT AFT FUSELAGE HAS A SKIN CRACK AT FRAME 75 ABOVE STRINGER 2R. RAI SERVICEABLE DOUBLER FOR SKIN REPAIR AT FR 75R IAW SRM 53-31-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,156 hrs · 28,607 cycles

NR 2 EMERGENCY LIGHT BATTERY INOP. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY AND CHARGER IAW WC 33-700-19. OP CHECK GOOD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,156 hrs · 28,607 cycles

FR22 AND STR15R HAS CORROSION. PERFORMED FR22 STR15 REPAIR IAW ERS-EM-53MR-3332.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,060 hrs · 28,498 cycles

FLOOR EMERGENCY LIGHT STRIPS AT ROWS 8 - 9 AND ROWS 10 - 11, AND RT AND LT OVERWING EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED THE INVERTER ASSY NR 5 IAW MM 33-50-11. OPS CHECKED GOOD .

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,921 hrs · 28,345 cycles

EMERGENCY EXIT SIGN AT SEAT 12C WAS FOUND INOPERATIVE. REMOVED AND REPLACED SEAT 12C UPPER SIDEWALL EXIT SIGN IAW AMM 33-50-14-000-801-A, AND 33-50-14-400-801-A. OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,894 hrs · 28,311 cycles

DOOR EMERGENCY LIGHTS AND ONE PROXIMITY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY AND CHARGER IAW AMM 33-50-04, OPS CHECKED GOOD.

Part: LIGHT — UNKNOWN (CABIN) · airframe 32,779 hrs · 28,196 cycles

MIDDLE SECTION OF FLOOR EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT PLACED ONTO APU POWER. OP TESTED THE EMERGENCY LIGHTS IAW 33-50-00. OP CHECKED GOOD. NO FURTHER FAULTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (WING ANTI ICE) · airframe 32,413 hrs · 27,950 cycles

WING ANTI ICE FAILED WHEN OVERRIDE KNOB IN THE ALL POSITION, FAULT CODE 301M0200. FOLLOWING FIM 30-11-00-810-803-A, ITEM 1, PERFORMED AN OPS CHECK IAW AMM 30-00-00. OPS CHECKED GOOD. NO MESSAGE NOTED.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,061 hrs · 27,619 cycles

RH FWD OVERWING EMERG, AND OVRHD ISILE EMERG LIGHTS ARE OUT.-C/A-REMOVED AND REPLACED #2 EMER POWER SUPPLY AND CHARGER IAW EMB-145 AMM 33-50-04. OPS CHK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 105196

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,390 hrs · 27,015 cycles

WHILE PERFORMING PS-1 INSPECTION FOUND NR 4 AND NR 5 FLOOR PROXIMITY EMERGENCY LIGHT STRIPS INOP. REMOVED AND REPLACED NR 3 EMERGENCY BATTERY POWER SUPPLY IAW AMM 33-50-04. OPS CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 79752.

Part: LIGHT — INOPERATIVE (OVERWING) · airframe 30,562 hrs · 26,301 cycles

RT OVER WING EMERGENCY LAMP INOP. RELAMPED IAW AMM 33-50-10 OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,043 hrs · 25,849 cycles

ROW 12 AISLE EMERGENCY LIGHT INOP. REMOVED AND REPLACED ROW 12 AISLE EMERGENCY LIGHT IAW AMM 33-50-08. OPC GOOD.

Part: MODULE — FAILED (CABIN PRESSURE) · airframe 29,846 hrs · 25,689 cycles

CABIN AUTO PRESSURIZATION FAIL CABIN STARTED CLIMBING DID NOT TRY MANUAL OPER. REMOVED AND REPLACED CPAM IAW AMM 21-32-01 REF ITEM NR 2 AND NR 3 THIS PAGE FOR OP CHECK.

Part: BLEED VALVE — FAILED (LT ENGINE) · airframe 29,475 hrs · 25,354 cycles

AFTER TAKE-OFF, RECEIVED BLEED 1 LEAK EICAS MESSAGE. RAN THE CHECK LIST AND RETURNED TO DEPARTURE. FOUND ENGINE BLEED VALVE TO BE BAD. REMOVED AND REPLACED LT ENGINE BLEED VALVE IAW AMM 36-11-05-000-801-A AND 36-11-05-400-801-A. OPS CHECKED GOOD NO DEFECTS NOTED AT THIS TIME. END

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,464 hrs · 25,344 cycles

F/A REPORTS THAT CABIN FLOOR EMERGENCY LIGHT MID CABIN ARE INOPERATIVE. R & R THE NR 3 BATTERY IAW WORK CARD 33-700-19.

Part: SIGN — INOPERATIVE (CABIN) · airframe 29,292 hrs · 25,181 cycles

RT OVERWING INTERIOR EXIT SIGN WILL NOT ILLUMINATE. R & R RT OVERWING INTERIOR EXIT SIGN IAW AMM 33-50-14. OPS CK GOOD.

Part: INDICATION SYS — FAULTY (FUEL SYSTEM) · airframe 28,678 hrs · 24,585 cycles

DVT INDICATION DUE ERRONEOUS FUEL INDICATIONS ON RT FUEL TANK, DECLARED EMER. FLIGHT CREW PLACARDED RT FUEL QTY INDICATIONS INOPERATIVE MEL 28-09. REMOVED AND REPLACED TU R-4 IAW EMB 145 AMM 28-41-02. REFERENCE NRWC 699-CMH-02573. MEL RESTORED

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 28,678 hrs · 24,585 cycles

BAGG EXT LIGHT & BAGG SMOKE EICAS WARNING AT GATE, THEN EICAS WARNING IMMEDIATELY EXTINGUISHED. R & R BOTH FWD & AFT SMOKE DETECTOR FROM THE CARGO COMPARTMENT IAW AMM 26-15-01. PERFORMED OPERATIONAL TEST IAW AMM 26-15-00. OPERATIONS CHECKED GOOD, NO MSG NOTED.

Part: FIRE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 28,673 hrs · 24,580 cycles

CREW RECEIVED A CARGO FIRE DETECTION WARNING. BAGGAGE COMPARTMENT SMOKE DETECTION SYS ALERTED & WAS RESET, FIRE DEPT CALLED. REMOVED BAGS. NO FURTHER ISSUES. INSPECTED CARGO COMPARTMENT AS REQUIRED & PERFORMED CARGO COMPARTMENT SMOKE DETECTOR OPERATIONS CHECK IAW AMM 26-15-01. OPERATIONS CHECKED NORMAL, NO DEFECTS NOTED. ARFT OK FOR SERVICE

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 28,616 hrs · 24,539 cycles

ATTACH CLIP FOR CARGO RAMP SUPPORT AT FRAME 66 IS CRACKED. R & R ATTACH CLIP FOR CARGO RAMP SUPPORT AT FRAME 66 IAW SRM 51-40-02.

Part: FITTING — CHAFED (RT AILERON) · airframe 28,616 hrs · 24,539 cycles

RIGHT AILERON DAMPER FITTING HAS CHAFES. REPLACED DAMPER FITTING IAW EO-EM-27MR-112.

Part: FITTING — WORN (LT AILERON) · airframe 28,616 hrs · 24,539 cycles

LEFT AILERON PCA FITTING OTBD LUG BUSHING BORE WORN. LT AILERON DAMPER FITTING IS DAMAGED. INSTALLED PCA FITTING IAW EO 3M-27MR-112. FITTING PN 145-69382-609.

Part: SKIN — CHAFED (RUDDER) · airframe 28,616 hrs · 24,539 cycles

RUDDER 1 IS CHAFED 5.75" FROM UPPER HINGE LOWER CUT OUT & 5.75" FROM RT EDGE OF LE PANEL. REPAIRED DAMAGE IAW ERS-EM-55MR-426.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,616 hrs · 24,539 cycles

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

Part: SUPPORT BRACKET — CRACKED (CARGO BAY) · airframe 28,616 hrs · 24,539 cycles

CARGO DOOR LIFT & LOWER MECHANISM FWD SUPPORT BRACKET AT FRAME 61 IS CRACKED. R & R CARGO DOOR LIFT & LOWERING MECHANISM FWD SUPPORT BRACKET AT RT FRAME 61 IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 28,616 hrs · 24,539 cycles

FRAME 72 SHEAR CLIP UNDER LT FLOOR & WALL SUPPORT IS CRACKED. R & R FRAME 72 SHEAR CLIP UNDER THE FLOOR & WALL SUPPORT IAW SRM 51-40-02.

Part: CLEAT — CRACKED (FUSELAGE) · airframe 28,616 hrs · 24,539 cycles

SHEAR CLEAT AT FRAME 80R, STRINGER 7R, IS CRACKED APPROX 1/2 INCH. R & R SHEAR CLEAT AT FRAME 80RT, STRINGER RT IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,616 hrs · 24,539 cycles

FLOORBEAM AT FRAME 65, RIB IS CORRODED JUST ABOVE CARGO DOOR SILL. R & R FLOORBEAM IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 28,616 hrs · 24,539 cycles

RIGHT OMEGA BEAM L ANGLE SUPPORT IS CRACKED, BETWEEN FRAMES 47R & 48R. INSTALLED NEW FWD & AFT L ANGLE SUPPORTS FOR RT OMEGA BEAM IAW SRM 53-23-02 & 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 28,616 hrs · 24,539 cycles

FRAME 71 SHEAR CLIP UNDER LT FLOOR & WALL SUPPORT IS CRACKED. R & R SHEAR CLIP IAW SRM CH 51-40-02.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 28,616 hrs · 24,539 cycles

CARGO DOOR LIFTING & LOWERING MECHANISM SUPPORT IS CRACKED. R & R CARGO DOOR LIFTING & LOWERING MECHANISM SUPPORT IAW AMM 52-32-00.

Part: TORQUE BOX — CRACKED (PAX DOOR) · airframe 28,616 hrs · 24,539 cycles

PASSENGER DOOR INNER HANDLE TORQUE BOX HAS A 1/8" CRACK BY THE NUTPLATE ON AFT UPPER CORNER. R & R PAX DOOR INNER HANDLE TORQUE BOX IAW SRM 51-40-02.

Part: CLEAT — CRACKED (FUSELAGE) · airframe 28,616 hrs · 24,539 cycles

SHEAR CLEAT AT FRAME 80L, STRINGER 7L IS CRACKED APPROX 1 INCH. R & R SHEAR CLEAT IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (CARGO BAY) · airframe 28,616 hrs · 24,539 cycles

CARGO DOOR LIFT & LOWER MECHANISM FWD SUPPORT BRACKET AT FRAME 68 RT IS CRACKED. SHOULD READ AFT SUPPORT BRACKET. R & R CARGO DOOR LIFT & LOWER MECHANISM AFT SUPPORT BRACKET IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 28,616 hrs · 24,539 cycles

RIGHT WING TO FUSELAGE PANEL 194ER, LOWER ANGLE SUPPORT 3 IS CRACKED APPROX 1". R & R RT WING TO FUSELAGE PANEL 194ER, LOWER ANGLE SUPPORT 3 IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,616 hrs · 24,539 cycles

RIGHT WING TO FUSELAGE PANEL 194ER UPPER SUPPORT, BETWEEN FRAMES 48 - 49 IS CRACKED APPROX 1/4". REMOVED DAMAGED SECTION OF LOWER ANGLE SUPPORT 4 & CUT TO FIT & INSTALLED NEW SECTION OF ANGLE IAW SRM 51-40-02 & ETN-EM-53-142.

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 28,616 hrs · 24,539 cycles

APU FIRE WALL HAS A 1/4" CRACK BY RIVET, JUST ABOVE LOWER RT APU MOUNTING POINT. COMPLIED WITH APU FIREWALL REPAIR IAW PART C OF EO-EM-53AD-1883.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 28,616 hrs · 24,539 cycles

RIGHT WING TO FUSELAGE PANEL 194ER, LOWER ANGLE SUPPORT 4 IS CRACKED APPROX 2". REMOVED DAMAGED SECTION OF LOWER ANGLE SUPPORT 4 & CUT TO FIT & INSTALLED NEW SECTION OF ANGLE IAW SRM 51-40-02 & ETN-EM-53-142.

Part: PANEL SUPPORT — CRACKED (FUSELAGE) · airframe 28,251 hrs · 24,217 cycles

RT WING FUSELAGE LATERAL FAIRING, UPPER SUPPORT CRACKED AT FS 16783.5, 6.25" LENGTH. INSTALLED NEW OVERWING LATERAL UPPER PANEL SUPPORT IAW SRM 51-40-02.

Part: ROLLER — OUT OF ADJUST (SERVICE DOOR) · airframe 27,924 hrs · 23,903 cycles

SERVICE DOOR NOT OPENING FROM INSIDE OR CLOSING FROM INSIDE, LOTS OF FREE PLAY AT TOP DOOR HINGE. TRANSFERRED TO NRWC 699-DFW-02424. FOR SERVICE DOOR FOUND UPPER AFT ROLLER & LOWER FWD ROLLER OUT OF ADJUSTMENT. ADJUSTED UPPER AFT ROLLER & LOWER FWD ROLLER IAW STEP 2 & AMM 52-43-06. SERVICE DOOR OPENS & CLOSES GOOD IAW AMM 52-43-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,394 hrs · 23,433 cycles

FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R FWD FLIGHT ATTENDANT FLASHLIGHT IAW AMM 33-50-16.

Part: BRACKET — CRACKED (FLASHLIGHT) · airframe 26,008 hrs · 22,194 cycles

FLIGHT ATTENDANT FLASHLIGHT BRACKET IS CRACKED. R & R FLIGHT ATTENDANTS FLASHLIGHT BRACKET & FLASHLIGHT IAW EEL 08-12.

Part: WIRE — BROKEN (CABIN) · airframe 25,458 hrs · 21,701 cycles

DURING PS 2 CHECK FOUND SERVICE DOOR EMER LIGHT INOPERATIVE. REPAIRED BROKEN SERVICE DOOR EMER LIGHT WIRE IAW SWPM 20-21-00 & MM 25-23-05.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,307 hrs · 21,542 cycles

SERVICE DOOR EXTERNAL EMER LAMP INOPERATIVE. R & R SVC DOOR EXTERNAL EMER LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: BRAKE ASSY — FAILED (NR 2) · airframe 25,186 hrs · 21,413 cycles

NUMBER 2 MLG BRAKE FAILED CARBON BRAKE INSPECTION. R & R NR 2 BRAKE IAW WC 32600-14.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,031 hrs · 20,424 cycles

DURING MBV INSPECTION, QA FOUND LT OMEGA BEAM CORRODED AROUND NUTPLATE HOLE ON LOWER FLANGE BETWEEN FRAME 22 & 23. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR ON LT OMEGA BEAM NUTPLATE HOLE ON LOWER FLANGE BETWEEN FRAME 22 & 23 IAW ERS-EM-53MR-458. REPAIR DOUBLER AL CLAD 2024-T3, 0.050 INCHES. ACFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION.

Part: WIRE — DAMAGED (CABIN) · airframe 24,031 hrs · 20,424 cycles

FOUND DURING CLEAR TO CLOSE. FLOOR PROXIMITY LIGHT STRIP WIRE DAMAGED AT FLOOR PANEL 251BF. REPAIRED FLOOR PROXIMITY LIGHT STRIP WIRE AT FLOOR PANEL 251BF IAW SWPM 20-21-00. SEE BOW 155932 FOR OPERATIONS CHECK.

Part: SWITCH — FAULTY (ANTI-ICE SYS) · airframe 23,551 hrs · 20,028 cycles

CHRONIC REPEAT DISCREPANCY E2 ANTI-ICE VLV FAIL ON EICAS WITH E2 ENG AIR INLET LIGHT CLOSED ENTIRE FLIGHT. EMERGENCY DECLARED IAW LOG PAGE 35275881. DEFERRED IAW MEL 30-11 AUTH 030061DM C M PROCEDURES COMPLIED WITH. R & R ENG 2 ANTI-ICE SWITCH, PUSH BUTTON, IAW AMM 20-13-04. PERFORMED OPERATIONS CHECK OF ENG THERMAL ANTI-ICING SYS, NO DEFECTS NOTED. M PROCEDURE COMPLIED WITH MEL 30-11 RESTORED.

Part: LIGHT — INOPERATIVE (MAIN DOOR) · airframe 23,538 hrs · 20,018 cycles

MAIN DOOR MOUNTED EMERGENCY LIGHT INOPERATIVE. R & R MAIN DOOR MOUNTED EMERGENCY LIGHT LAMP IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A, OPERATIONS CHECKED GOOD.

Part: UNKNOWN — ODOR · airframe 23,462 hrs · 19,948 cycles

ABORTED TAKEOFF DUE TO A STRONG ODOR. TROUBLE SHOT ODOR IAW EMB FIM 21-20-00 & ETN EM-72-034, NO NOXIOUS ODORS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,450 hrs · 19,938 cycles

NUMBER 2 EMERGENCY LIGHT INOPERATIVE, FLOOR PROXIMITY STRIP. DEFERRED IAW MEL 33-30 AUTH 020586-C. ACFT WAS REMOVED FROM SERVICE. R&R NR 2 EMERGENCY FLOOR PROX STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD, MEL RESTORED & PLACARD REMOVED.

Part: CARBON SEAL — FAILED (NR 1 ENGINE) · airframe 23,388 hrs · 19,881 cycles

ON POST FLIGHT NR 1 ENG SMOKING AFTER SHUTDOWN FOR 15 MINUTES. IAW ETN-EM-79-015 REV 5 SHAFT PLUG WAS CHANGED 22.13 HRS AGO. IAW ETN STEP 13 THE RTBS & THE THIRD STAGE BLADES ARE DRY. R&R THE ENGINE DUE TO A NR 7 CARBON SEAL. REMOVED AND REPLACED LT ENG S/N CAE312737 IAW W/C 71-000-00 SEE NRWC 699-CMI-01626 FOR OPC /LEAK CHECK TDMI RESTORED. END

Part: UNKNOWN — SMOKE (NR 1 ENGINE) · airframe 23,342 hrs · 19,848 cycles

NUMBER 1 ENG INDICATES 7 QTS OF OIL AFTER START. ON POST FLIGHT INSPECTION A LOT OF SMOKE WAS COMING OUT OF TAIL PIPE ON ENG. PERFORMED OIL CHECK IAW OIL CHECK WORK CARD. SEE ITEM 2 FOR CORRECTIVE ACTION OF SMOKE ON SHUTDOWN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,491 hrs · 19,179 cycles

EMERGENCY LIGHT INOPERATIVE BETWEEN SEATS 8A - 9A. R & R EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 22,325 hrs · 19,043 cycles

ELECTRICAL BURNING ODOR IN COCKPIT AND CABIN. R & R EMERGENCY FLASHLIGHT IN FLIGHT DECK, BEHIND CAPTAINS SEAT IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: DISPLAY — FAILED (COCKPIT) · airframe 22,288 hrs · 19,011 cycles

STRONG ODOR OF FUMES IN COCKPIT WHILE PARKED AT THE GATE. SMELLS LIKE ELECTRICAL BURNING. TROUBLESHOT IAW FIM 21-20-00-810-801A. R & R PFD2 AND OPS CHECKED GOOD IAW MM 34-22-01 AND FIM 34-22-00-810-835-A.

Part: ACM — FAILED (RIGHT) · airframe 22,125 hrs · 18,851 cycles

CREW REPORTED, WHEN NR 2 PACK IS RUNNING THERE IS CLUNKING NOISE AND BAD ODOR. WHEN NR 2 PACK IS TURNED OFF, NOISE AND ODOR GOES AWAY. PERFORMED FIM TASK 21-51-00-810-824-A BLOCK 1 THRU 7 AND R & R NR 2 PACK VALVE IAW AMM 21-51-01 AND R & R OVER TEMPERATURE SWITCH IAW AMM 21-51-08. REMOVED AND REPLACED AIR CYCLE MACHINE IAW AMM 21-51-03-000-801-A AND 21-51-03-400-801-A. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,779 hrs · 18,564 cycles

DURING B-INSPECTION FOUND THE LT OVER WING EMERGENCY LIGHT LAMP INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LT OVER WING EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,658 hrs · 18,450 cycles

DURING B-INSPECTION, FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R LAMP AT MAIN DOOR EMERGENCY LIGHT IAW AMM TASK 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,419 hrs · 18,267 cycles

DURING B INSPECTION FOUND THE MAIN CABIN DOOR MOUNTED EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN CABIN DOOR MOUNTED EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 21,122 hrs · 18,022 cycles

ON FLIGHT 4030 THE CREW REPORTED THE AFT FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,121 hrs · 18,021 cycles

DURING MAINTENANCE INSPECTION, FOUND LEFT & RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE DURING PS1 CHECK. REMOVED AND REPLACED THE BATTERY POWER SUPPLY IAW MM 33-50-04 AND EXTERNAL EMERGENCY LIGHT ON RIGHT SIDE IAW MM 33-50-10. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 20,958 hrs · 17,885 cycles

DURING B INSPECTION FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY NR 4 BATTERY POWER SUPPLY ASSEMBLY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 20,831 hrs · 17,788 cycles

DURING B INSPECTION FOUND THE AFT CABIN AND FIRST OFFICER’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH FLASHLIGHTS IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,810 hrs · 17,773 cycles

DURING B INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT BATTERY AND BATTERY CHARGER IAW WC 33-700-19 AND PERFORMED OPERATIONAL CHECK IAW WC33-700-17. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,219 hrs · 17,289 cycles

DURING B INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW EMB AMM TASK: 33-50-07-000-801-A, AND 33-50-07-400-801-A. PART NUMBER 1317. NO FIX REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY AND CHARGER IAW W/C: 33-700-19 AND W/C: 33-700-17. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,191 hrs · 17,263 cycles

ON FLIGHT 4249 THE CREW REPORTED THE EMERGENCY EXIT LIGHTS ROW 1-7 GALLEY EXIT LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 BATTERY AND CHARGER PER W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 19,377 hrs · 16,570 cycles

DURING B INSPECTION, FOUND THE RIGHT LAVATORY GUSSET BEAM CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED GUSSET IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — WRONG PART (CABIN) · airframe 19,377 hrs · 16,570 cycles

DURING B INSPECTION, FOUND LIGHT INCORRECT PART. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — CRACKED (CABIN) · airframe 19,377 hrs · 16,570 cycles

DURING B INSPECTION, FOUND THE NR 3 PROXIMITY LIGHT TO BE CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-12. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,178 hrs · 16,426 cycles

DURING B INSPECTION FOUND THE LEFT FORWARD WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FORWARD FUSELAGE EXTERNAL EMERGENCY LAMP IAW EMB AMM 33-50-00-000-801/33-50-10-400-801. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 18,724 hrs · 16,058 cycles

ON FLIGHT 2779 THE CREW REPORTED THE BAGGAGE SMOKE WARNING LIGHT AND EICAS (FIRED BAGG EXT AS REQUIRED BY AOM-1) THE CREW REPORTED THE FORWARD AND AFT SMOKE DETECTOR IN BAGGAGE COMPARTMENT NEED TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPALCED THE AFT AND FORWARD BAGGAGE COMPARTMENT SMOKE DETECTORS IAW EMB AMM 26-15-01 IAW AMM 26-15-00. REMOVED AND REPLACED THE BAGGAGE COMPT HIGH STAGE FIRE BOTTLE IAW EMB 145 AMM 26-23-01. PART NUMBER CARTRIDGE 30903870. PART NUMBER FIREX BOTTLE-224 CU. IN. 337000271, SERIAL NUMBER 32588D1. THE OPERATIONAL CHECK WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 18,691 hrs · 16,037 cycles

ON FLIGHT 3239 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED ROLLERS ON MAIN CABIN DOOR. THE OPERATIONAL CHECK WAS GOOD AMM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,238 hrs · 15,705 cycles

ON FLIGHT 4374 CREW FOUND AFT CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED AFT CABIN FLASHLIGHT IN REFERENCE TO EMB 145 AMM33-50-16-000-801-A AND 33-50-16-400-801-A OPERATIONAL WAS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,099 hrs · 15,606 cycles

DURING UNSCHEDULED MAINTENANCE THE RAMP REPORTED THE EMERGENCY LIGHTS INOPERABLE, AND THE LEFT WING INSPECTION LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPILED WITH OPERATIONAL TEST OF THE EMERGENCY LIGHTS IAW EMB 145 MM 33-50-00. THE SYSTEM CHECK WAS GOOD AT THIS TIME. REMOVED AND REPLACED THE LEFT WING INSPECTION LIGHT AS PER EMB145 AMM 33-44-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — FUMES (COCKPIT & CABIN) · airframe 17,854 hrs · 15,414 cycles

FUNCTIONAL CHECK FLIGHT REQUIRED DUE TO FUMES IN BOTH COCKPIT AND CABIN. AIRCRAFT RELEASED FOR FCF PURPOSES ONLY. FCF FOUND SATISFACTORY.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 17,853 hrs · 15,413 cycles

WHEN PERFORMING ICE TEST IN THE AIR, ICE TEST KNOB IN ALL AFTER 14 SECONDS FUMES WERE DETECTED IN BOTH COCKPIT AND CABIN. TURNED SWITCH BACK TO AUTO AND FUMES DISAPPEARED. PERFORMED ANTI ICING SYSTEM OP TEST IAW AMM 30-00-00, NO FUMES NOTED

Part: FLASHLIGHT — MISSING (CABIN) · airframe 17,838 hrs · 15,405 cycles

AFT FA FLASHLIGHT MISSING. REPLACED AFT FLIGHT ATTENDANT FLASHLIGHT. OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 17,729 hrs · 15,328 cycles

FOR FLIGHT 2755 DURING THE PRE FLIGHT INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT 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: BATTERY — DISCHARGED (CABIN) · airframe 17,409 hrs · 15,097 cycles

FOR PS -1 MAINTENANCE CHECK FOUND SEAT ROW 1-6 FLOOR EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY SUPPLY BATTERY AND HOLDER ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD IAW W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,373 hrs · 15,073 cycles

FOR PS -1 MAINTENANCE CHECK FOUND THE AFT EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY AND CHARGER ASSEMBLY IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD IAW W/C 33-70-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — CRACKED (SMOKE DETECTOR) · airframe 17,338 hrs · 15,043 cycles

DURING MAINTENANCE INSPECTION FOUND THE SMOKE DETECTOR DOOR ASSEMBLY CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SMOKE DETECTOR DOOR ASSEMBLY IAW CMM 25-31-55. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — ODOR (COCKPIT) · airframe 16,625 hrs · 14,512 cycles

FOR FLIGHT 2763 THE CREW REPORTED THAT DURING TAXI TO TL16 RUNWAY, SMELLED A BURNING PLASTIC ODOR LIKE HOT ELECTRICAL WIRING. THE ODOR WAS FAIRLY STRONG FOR A FEW MINUTES THEN DISSIPATED. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED WINDSHIELD HEAT POST. REINSTALLED GLARESHIELD IAW 25-12-07. INSPECTED MAP LIGHTS NO DEFECTS NOTED. FOUND STRONG PLASTIC ELECTRICAL ODOR FROM THE CAPTAIN’S FLASHLIGHT. REPLACED FLASHLIGHT AND CRADLE. FOUND STRONG PLASTIC AND ELECTRICAL SMELL FROM FLIGHT ATTENDANT’S FLASHLIGHT REPLACED THE BATTERY IAW 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 14,988 hrs · 13,279 cycles

DURING CLIMB AROUND 15000 FT GOT A PRONOUNCED ELECTRICAL BURNING ODOR. SHORTLY AFTER ELECTRICAL ODOR DISSIPATED AND BURNING ODOR CONTINUED FOR ABOUT 15 MINUTES FROM COCKPIT DOOR AREA AS WELL AS REAR OF CABIN AFTER ASKING FLIGHT ATTENDANT TO INVESTIGATE CLOSET AND GALLEY AREA, F/A ADVISED BOTH TRASHCAN AREAS TO BE ABNORMALLY WARM. NO LIQUIDS HAD BEEN POURED AND ALL GALLEY EQUIPMENT WAS ALREADY OFF. ALL ODORS DISSIPATED AFTER 15-20 MIN, NO EICAS MESSAGES NON-ICING CONDITION. THE CREW ELECTED TO DIVERT TO TPA AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED CEILING LIGHTS AND WINDOW LIGHTS IAW EMB 145 CHAPTER 33-21-02 OPS CHECK GOOD NO DEFECTS NOTED. INSPECTED CABIN LIGHT BALLAST IAW CHAPTER 33-21-00 OPS CHECK GOOD NO DEFECTS NOTED. INSPECTED LIGHT LT AND RT RELAYS SUPPORT IAW CHAPTER 20-13-02 NO DEFECTS NOTED. INSPECTED COCKPIT DISPLAY UNITS IAW CHAPTER 34-22-00 NO DEFECTS NOTED. INSPECTED WINDSHIELD CONTROLLER AND HEATING SENSORS IAW CHAP. SUSPECT OF ODOR IS BURNT COFFEE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 14,835 hrs · 13,159 cycles

ON FLIGHT 3999 THE CREW REPORTED AN ABNORMAL ELECTRICAL PROBLEM. THE BATTERIES ON THE AIRCRAFT WENT INTO AN ESSENTIAL TRANS MODE. (IE- PLANE GOES DARK AND EICAS ONLY). THE CAPTAIN ELECTED TO RETURN TO FAR. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BAD BATTERY 1 SWITCH. REMOVED AND REPLACED THE ELECTRICAL CONTROL PANEL IAW EMB-145 AMM 24-00-01. THE OPERATIONAL CHECK WAS GOOD PER EMB-145 AMM 24-60-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 11,392 hrs · 10,317 cycles

ON MAINTENANCE CHECK FOUND EMERGENCY LIGHT STRIP AT ROW 8/9 WRONG FOR LOCATION CHART. REMOVED INCORRECT STRIP AND INSTALLED CORRECT EMERGENCY LIGHT STRIP. AIRCRAFT RETURNED TO SERVICE.

Part: CARBON SEAL — WORN (LT ENGINE) · airframe 8,190 hrs · 7,310 cycles

ON FLIGHT 9811, CREW REPORTED CABIN ODOR DURING TAKEOFF IN COCKPIT. ODOR DISAPPEARED DURING CLIMB. ODOR RE-EXPERIENCED ON APPROACH BELOW 7000 MSL. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE ZERO CARBON SEAL IAW EMB 145 AMM 72-25-25. AIRCRAFT RETURNED TO SERVICE.

Part: A/C PACK — ODOR · airframe 8,189 hrs · 7,309 cycles

ON FLIGHT 3856, CREW REPORTED DURING DESCENT, PACKS PRODUCED ODD ODOR (POSSIBLY OIL) FOLLOWED BY PACK 2 OVERHEAT, AIRCRAFT REMOVED FROM SERVICE. PERFORMED VISUAL INSPECTION OF OIL LEAKAGE AND ALSO PERFORMED BOROSCOPE INSPECTION FOR OIL LEAKAGE. NO EVIDENCE OF OIL FOUND. GROUND RUN A/C AND NO ABNORMAL OIL SMELL DETECTED. AIRCRAFT RETURNED TO SERVICE.

Part: FADEC — FAILED (APU) · airframe 6,087 hrs · 5,536 cycles

APU IN OPERATION TO COMPLY WITH MEL 24-5. APU FAILED DURING CLIMB-OUT. REPLACED APU FADEC. OPERATIONAL CHECKS GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: BOOT — DETACHED (LT WING) · airframe 4,881 hrs · 4,532 cycles

LOUD NOISE HEARD FROM LEFT SIDE OF AIRCRAFT AROUND ROW 8. REATTACHED BOOT ON NACA DUCT IAW EMB AMM 36-10-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: ENGINE — LEAKING (LT/RT ENGINES)

CREW NOTED LAV SMOKE ON EICAS. REPLACED BOTH ENGINES, LEFT ENG P/N OFF AE3007A1/3, S/N CAE312729. RIGHT ENGINE P/N OFF AE3007A 1/3, S/N OFF CAE312756. (M)

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY)

CREW RECEIVED LAV SMOKE DETECTION INDICATION ON EICAS. PERFORMED OPERATIONAL CHECKS OF THE LAVATORY SMOKE DETECTION SYSTEM WITH NO DISCREPANCIES NOTED. AC RETURNED TO SERVICE. (K)

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY)

LAV SMOKE INDICATION ON EICAS AFTER TAKEOFF. NO VISIBLE SMOKE WAS NOTED. REPLACED LAVATORY SMOKE DETECTOR PANEL AND LAVATORY SMOKE DETECTOR IAW EMB AMM 26-14-02 AND 26-14-01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE, P/N FOR PANEL IS FAU-751A-4 S/N IS 043477. (M)