N690AE

Part: INLET — CORRODED (RT ENGINE) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

RIGHT ENGINE INLET HAS CORROSION ON THE INTERNAL LWR SIDE WHERE THE GENERATOR INLETS ARE LOCATED. RAR RH ENGINE INLET IAW EMB 145 AMM 71-60-01,

Part: ATTACH FITTING — WORN (ZONE 600) · airframe 45,986 hrs · 43,361 cycles

RIGHT AILERON DAMPER ATTACHMENT FITTING HOLE IS WORN. R & R RT AILERON DAMPER ATTACHMENT FITTING IAW EMB 145 SRM 51-40-02.

Part: BRACKET — CRACKED (ZONE 200) · airframe 45,986 hrs · 43,361 cycles

COCKPIT LH LATERAL BRACKET IS CRACKED. REMOVED AND INSTALLED NEW SERVICEABLE LH LATERAL BRACKET IN COCKPIT IAW EMB 145 SRM 51-20-03, 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,986 hrs · 43,361 cycles

SHEAR CLIP IS CRACKED AT FRAME 16 BETWEEN STRINGERS 15R-16R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 16 BETWEEN STRINGERS 15R-16R IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,986 hrs · 43,361 cycles

SHEAR CLIP IS CRACKED AT FRAME 15 BETWEEN STRINGERS 15R-16R. R & R SHEAR CLIP AT FRAME 15 BETWEEN STRINGERS 15R-16R. IAW EMB 145 SRM 51-40-02 AND PDT EO1-53-25-0454

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION ON PASSENGER DOOR ENTRY AFT FLOORBOARD SUPPORT. RAR SUPPORT IAW SRM 51-40-02

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

LAV WASTE BUCKET IS CORRODED AT AFT OF THE WASTE DRAIN VALVE. REMOVED AND REPLACED LAV WASTE BUCKET IAW EMB 145 SRM 51-40-02.

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION ON SERVICE DOOR CUT-OUT FWD SILL. R & R THE SERVICE DOOR CUTOUT FWD SILL IAW EMB 145 SRM 51-40-02.

Part: GUSSET — CORRODED (ZONE) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION ON LH NR 1 BEAM GUSSET. R & R L/H # 1 BEAM GUSSET IAW EMB-145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION IN GALLEY AREA ON FWD DIGITAL. REPAIRED WITH DOUBLER IAW EMB-145 SRM 53-21-10

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION IN GALLEY AREA ON LT CROSS FLOORBEAM AT FRAME 18. R & R LT CROSS FLOORBEAM AT FRAME 18 IAW EMB145 SRM 51-40-02

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION IN GALLEY AREA ON RT FLOORBEAM GUSSET AT FRAME 18. REMOVED AND REPLACED GUSSET ON GALLEY AREA RT FLOORBEAM GUSSET AT FRAME 18 IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION ON RT OTBD NR 2 SEAT TRACK. REMOVED AND REPLACED RT NR 2 OTBD SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION ON SIDE OF STEP-UP CROSS FLOORBEAM AT FRAME 23 BETWEEN STRINGERS 21R-21L. R & R STEP-UP CROSS FLOORBEAM AT FR23 BTWN STGRS 21R-21L IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION ON LT OTBD NR 1 FLOOR SILL. R & R L/H OUTBD # 1 FLOOR SILL IAW EMB145 SRM 51-40-02.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION IN LAV AREA ON RH FLOORBEAM GUSSET. RAR RH FLOORBEAM GUSSET IN LAV IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION ON RH INBD NR 4 SEAT TRACK. REMOVED AND REPLACED RT INBD NR 4 SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION ON LT OTBD #2 FLOOR SILL. R & R L/H OTBD #2 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION IN LAV AREA ON LH FLOORBEAM GUSSET. RAR LH FLOORBEAM GUSSET IN LAV IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,986 hrs · 43,361 cycles

SHEAR CLIP IS CRACKED AT FRAME 24 BETWEEN STRINGERS 15R-16R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 15R-16R IAW EMB 145 SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,986 hrs · 43,361 cycles

SHEAR CLIP IS CRACKED AT FRAME 25 BETWEEN STRINGERS 15R-16R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 25 BETWEEN STRINGERS 15R-16R IAW EMB 145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION ON LT NR 2 FLOORBEAM ISLE AREA AT FRAME 29. REMOVED CORROSION ON LT NR 2 FLOORBEAM ISLE AREA AT FRAME 29 IAW EMB 145 SRM 51-10-03. BLEND OUT IS ACCEPTED AS PERMANENT REPAIR IAW ETD2025-145-933947 AND EO1-05-26-0006.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION IN LAV AREA ON CENTER FLOORBEAM GUSSET. R & R CENTER FLOORBEAM GUSSET IN LAV IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION ON CARGO DOOR CUT-OUT SHEAR CLIP AT FRAME 65. PERFORMED SPLICE REPAIR OF SHEAR CLIP AROUND CARGO DOOR CUTOUT AT FRAME 65 IAW EMB 145 SRM 53-31-04 ITEM 4D FIG 212 AND EO1-53-25-0445.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,986 hrs · 43,361 cycles

SHEAR CLIP IS CRACKED AT FRAME 61 BETWEEN STRINGERS 6R-7R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 61 BETWEEN STRINGERS 6R-7R IAW EMB 145 SRM 51-40-02.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CORROSION ON CARGO DOOR CUTOUT LOWER SILL. REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW EMB 145 SRM 51-40-02.

Part: SPAR — CRACKED (ZONE 600) · airframe 45,986 hrs · 43,361 cycles

RIGHT WING SPAR I LOWER FLANGE AT RIB 9 IS CRACKED. PERFORMED REPAIR OF RH WING SPAR I AT RIB 9 REPAIR PARTS IAW EMB 145 SRM 57-20-05 ITEM3, ETD2025-145-934133 AND EO1-57-25-0455.

Part: SPAR — CRACKED (ZONE 500) · airframe 45,986 hrs · 43,361 cycles

LEFT WING SPAR I LOWER FLANGE AT RIB 9 IS CRACKED. PERFORMED REPAIR ON LT WING SPAR I LOWER FLANGE AT RIB 9 IAW EMB 145 SRM 57-20-05 ITEM 3, ETD2025-145-933843 AND EO1-57-25-0446.

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,986 hrs · 43,361 cycles

CARGO DOOR CORRODED AROUND FWD MOST 2 SCREW HOLES ON INBD LOWER FRAME PROFILE. R & R CARGO DOOR INBD LOWER FRAME PROFILE IAW EMB 145 SRM 51-40-02

Part: ACCESS DOOR — CRACKED (ZONE 200) · airframe 45,986 hrs · 43,361 cycles

COCKPIT UNDER FLOOR ACCESS HATCH CRACKED UNDER HINGE PIN ATTACH RING (HATCH SIDE). REPAIRED IAW EMB145 SRM 52-42-02-RE & 51-40-02, CPM 51-21-04 & 51-21-05.

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 45,986 hrs · 43,361 cycles

CARGO DOOR LWR OUTBD FRAME PROFILE IS CHAFED AND CRACKED AT FWD END. REMOVED AND REPLACED CHAFED AND CRACKED CARGO DOOR LWR OUTBOARD FRAME PROFILE IAW EMB 145 SRM 51-40-02, 51-20-01, 51-20-03, 51-40-04, 51-40-06

Part: SKIN — CRACKED (ZONE 200) · airframe 45,986 hrs · 43,361 cycles

POSSIBLE SKIN CRACK AT FR 77 BTWN STGRS 3L-4L. REPAIRED SKIN CRACK AT FR 77 BTWN STGRS 3L-4L WITH INSTALLATION OF SKIN BUSHING IAW EMB145 SRM 53-32-01RE, ITEM 9, FIG. 213 AND EO1-53-26-0005.

Part: SKIN — DENTED (ZONE 600 LE) · airframe 45,986 hrs · 43,361 cycles

RIGHT WING LEADING EDGE NR 2 HAS A DENT APPROX. 13" FROM OTBD EDGE. REPAIRED RH WING LEADING EDGE #2 DENT APPROX. 13" FROM OTBD EDGE IAW PIEDMONT EO1-57-25-0461, ETD2025-145-934265 AND EMB 145 SRM 57-40-00RE.

Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,847 hrs · 43,206 cycles

AREA OF CORROSION AT FR22, STR16R. REPAIRED IAW EO1-53-25-0364

Part: SENSOR — FAULTED (NR 1 ENGINE) · airframe 44,794 hrs · 40,336 cycles

N THE CLIMB FROM CLT E1 OIL TEMPERATURE WENT INTO THE RED FOR APPROXIMATELY 1 MINUTE THEN RETURNED TO NORMAL 20 PSI INCREASE INDICATION OIL PRESSURE, OIL TEMPERATURE WAS MAXED OUT AT 138 DEGREES TOP OIL TEMPERATURE. FACT 02APR25 19:28 CLT R+R'D #1 ENG OIL TEMP/PRESS SENSOR IAW RR MM 79-31-10 OPS+LEAK CHECK GOOD. A/C GOOD FOR SERVICE.

Part: WINDOW — NO DISCREPANCY (ZONE 200)

BIRD STIRKE FO DV WINDOW DURING LANDING. CLEANED AREA, PERFORMED BIRD STRIKE INSPECTION IAW AMM 05-50-08. NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE.

Part: HEATER — INOPERATIVE (ZONE 200) · airframe 43,833 hrs · 40,954 cycles

TAT 2 HEAT INOP ON CLIMB OUT. FACT 26OCT24 10:33 ALB FOUND TAT 2 CB OPENED PERFORMED OPS CHECK IAW EMB 145 AMM TASK 30-33-00 AFTER CLOSING CB. BOTH TAT 1&2 SENSOR BECAME HOT OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 43,808 hrs · 40,930 cycles

EMERGENCY LIGHT ON SERVICE DOOR HINGE INOP. RAR LAMP ASSY WITH RETAINED HARDWARE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,807 hrs · 38,653 cycles

MULTIPLE BIRDSTRIKES ON TAKE OFF. RETURNED TO FIELD. MX INSPECTED A/C FOR BIRDSTRIKE AND CLEANED AREA IAW AMM 05-50-25 NO DEFECTS NOTED AND ENGINE AND INLET INGESTION NOTED AT THIS TIME. A/C OK FOR SERVICE AT THIS TIME

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,581 hrs · 38,394 cycles

HN00103352 CORROSION FOUND ON "0" FLOOR BEAM CAP BETWEEN FRM 36-26 REMOVED CORRODED FLOOR BEAM CAP AND INSTALLED NEW FLOOR GUSSET/ FLOOR BEAM CAP AT "0" BEAM FRM 26 TO FRM 36 IAW EMB 145 SRM 51-40-02-PR.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,581 hrs · 38,394 cycles

CORROSION FOUND ON RH FLOOR SILL BETWEEN FRM 59-52. INSTALLED NEW SERVICEABLE RH FLOOR SILL PN: 145-29495-005 IAW EMB-145 SRM 51-40-02-PR.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,581 hrs · 38,394 cycles

HN00104071 UPON DVI OF THE RH MLG FWD BEARING LOWER HALF CORROSION WAS FOUND REPLACEMENT OR REPAIR REQUIRED. REPLACED RH MLG FWD BEARING HOUSING LOWER HALF WITH SERVICEABLE UNIT IAW EMB 145 AMM 32-10-01-400-801-A

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,581 hrs · 38,394 cycles

HN00103367 CORROSION FOUND ON L/H OMEGA BEAM TOP CAP. FROMFR53-FR58. : INSTALLED NEW L/H OMEGA BEAM TOP CAP P/N 145-30635-001 BETWEEN FR53 TO FR58 IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,581 hrs · 38,394 cycles

HN00103366 CORROSION FOUND ON L/H OMEGA BEAM TOP CAP FROM FR45-FR53. : REMOVED AND REPLACED FLOOR BEAM GUSSET (P/N: 145-30634-009) ON L/H OMEGA BEAM FROM FR45-FR53 IAW EMB145 51-40-02-PR.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,581 hrs · 38,394 cycles

HN00103267 CENTER FLOOR BEAM CAP HAS CORROSION BETWEEN FRM 14 AND FRM 18. INSTALLED NEW SERVICABLE GUSSET P/N 145-22460-015 IAW ERJ-145 SRM 51-40-02-PR

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,581 hrs · 38,394 cycles

HN00103350 CORROSION FOUND ON "0" FLOOR BEAM CAP BETWEEN FRM 46-39. INSTALLED NEW SERVICEABLE Y0 FLOORBEAM CAP PN 145-30634-007 BETWEEN FRM39 - FRM47 IAW EMB145 SRM 51-40-08-PR.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,581 hrs · 38,394 cycles

HN00103364 CORROSION FOUND ON L/H OMEGA BEAM TOP CAP FROM FR35-FR38. : REMOVED UNSERVICEABLE CAP AND INSTALLED NEW SERVICEABLE LH FLOORBEAM TOP CAP (P/N: 145-30634-001) BETWEEN FRM35 - FRM38 IAW EMB-145 SRM 51-40-02-PR.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,581 hrs · 38,394 cycles

HN00103353 CORROSION FOUND ON "0" FLOOR BEAM CAP BETWEEN FRM 29-22 : INSTALLED NEW SERVICEABLE FLOOR BEAM. CAP (P/N: 145-30633-003) ON "0" BETWEEN FRM 22-29 IAW EMB145 SRM 51-40-02-PR.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,581 hrs · 38,394 cycles

HN00103339 CORROSION FOUND ON RH FLOOR SILL BETWEEN FRM 52-48. REMOVED RH FLOOR SILL BETWEEN FRM 52-48 IAW EMB145 SRM 51-40-02-PR. LOCATED AND DRILLED NEW SERVICEABLE R/H FLOOR SILL (P/N: 145-25800-016) BETWEEN FR 48 & 52 FRM 22-29 IAW EMB 145 51-20-03-PR. INSTALLED RH FLOOR SILL BETWEEN FRM 52-48 IAW EMB145 SRM 51-40-02-PR.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,581 hrs · 38,394 cycles

HN00103354 CORROSION FOUND ON CROSSBEAM BETWEEN -479 AND + 479 AT FRM 25. BLENDED CORROSION ON LH CROSSBEAM AT FRM28 BETWEEN Y-479 AND LH FLOOR SILL AS PER STEPS 1 - 5.A.(6) IAW EMB-145 SRM 51-10-03-PR. FOUND TO BE WITHIN LIMITS IAW EMB-145 SRM 53-22-10-AD. (ORIGINAL THK - .050", REMOVED - .015", REMAINING THK - .035")

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 39,789 hrs · 36,369 cycles

CABIN RATE DURING CLIMB WENT TO 1800 FT PER MIN, THEN GOT TO 9000 FT WITH A/C AT 10,000 FT. R/R PRESSURIZATION CONTROLLER IAW MM 21-31-02. OPS CHECK GOOD. OK FOR SERVICE.

Part: NONE — NONE · airframe 38,895 hrs · 35,361 cycles

FO'S DAP INOP, NOTICED SMOKE EMITTING FROM PANEL. SWAPPED FO'S DAP WITH OBSERVER'S, INSPECTED AND FOUND NO DEFECTS, OPS CHECK GOOD OK FOR SERVICE.

Part: TUBE — DISCONNECTED (CONTROL VALVE) · airframe 37,080 hrs · 33,405 cycles

PDIS 690 36-21 2337261 30SEP20 ALB CLOSE. DURING CRUISE BLD 1 LEAK MESSAGE ON EICAS, CREW C/W QRH MSG GONE. FACT 01OCT20 03:28 ALB. FOUND TUBE TO BE DISCONNECTED ON DUAL TEMP CONTROL VALVE. INSTALLED TUBE AND R & R CLAMP, IAW EMB 145 AMM 21-60-01. PERFORMED AIR BLEED LEAK AND OPERATIONS CHECK IAW EMB 145 AMM 36-00-00. LEAK AND OPERATIONSS CHECK GOOD.

Part: SKIN — DAMAGED (FRAME 78) · airframe 37,071 hrs · 33,398 cycles

MULTIPLE RIVETS ON FR 78 BETWEEN STR 5L-8L HAVE POSSIBLE CRACKS (2 TOTAL). PERFORMED DYE PENETRANT INSPECTION, IAW EA SI NDTM 1. RELEVANT INDICATION NOTED SKIN CRACK ENDS, MARKED, RADIOMETER EASI 0452. COMPLETE: CUTOUT DAMAGE AREA ON FR 78 BETWEEN STR 6L-7L. FABRICATED REPAIR BUSHING. INSTALLED 1 BUSHING ON FR 78 BETWEEN STR 6L-7L, IAW EMB 145 SRM 53-32-01 AND PIEDMONT EO1-53-20-0344.

Part: SHEAR TIE — CORRODED (DOOR FRAME) · airframe 37,071 hrs · 33,398 cycles

SSI 53-30-48 FR 68 SHEAR CLIP IS CORRODED AT CARGO DOOR CUT-OUT LOWER END, MARKED. COMPLETE: BLENDED FR 68 SHEAR CLIP AT CARGO DOOR CUTOUT. FOUND TO BE OUT LIMITS. REMOVED PREVIOUS REPAIR. INSTALLED SHEAR CLIP AT FR 68, IAW EMB 145 SRM 53-31-04 ITEM 4 AND PIEDMONT EO1-53-20-0338.

Part: WEB — DAMAGED (CARGO DOOR) · airframe 37,071 hrs · 33,398 cycles

CARGO DOOR INNER WEB HAS TOOLING MARK AT HB 4 BETWEEN VB 2-4. COMPLETE: BLENDED AREA FOUND TO BE OUTSIDE ALLOWABLE LIMITS. CUT OUT BLENDED AREA ON CARGO DOOR INNER WEB HB4 BETWEEN VB2. ACCOMPLISHED REPAIR OF CARGO DOOR INNER WEB AT HB4 BETWEEN VB2, IAW EMB 145 SRM 52-30-01 AND PIEDMONT EO1-52-20-0335.

Part: GUIDE — DAMAGED (COCKPIT BULKHEAD) · airframe 37,071 hrs · 33,398 cycles

PILOT'S BULKHEAD UPPER OUTBOARD GUIDE PIN HOLE ELONGATED. COMPLETE: REMOVED PILOTS OUTBOARD GUIDE PIN DOUBLER. FABRICATED REPAIR PARTS; ONE DOUBLER AND SACRIFICAL PLATE. ACCOMPLISHED REPAIR ON PILOTS OUTBOARD GUIDE PIN HOLE, IAW EMB 145 SRM 53-21-02 ITEM 4 AND PIEDMONT EO1-25-20-0333.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 37,071 hrs · 33,398 cycles

SERVICE DOOR CENTER SILL CORRODED. FABRICATED REPAIR PARTS FOR REPAIR AT SERVICE DOOR CENTER SILL, IAW EMB 145 SRM 53-21-02 ITEM 2 FIGURE 201. COMPLETE: PERFORMED REPAIR AT SERVICE DOOR CENTER SILL, IAW EMB 145 SRM 53-21-02 ITEM 2 FIGURE 201 AND EO1-05-20-0340, SEE TURNOVER FOR DETAILS.

Part: NUT PLATE — CORRODED (PAX DOOR LINER) · airframe 37,071 hrs · 33,398 cycles

PAX DOOR LINER LOWER NUTPLATES (4) ON THE BOTTOM OF THE DOOR HAVE CORROSION. COMPLETE: BLENDED AREA 3 FWD NUTPLATES ON PAX DOOR LOWER FRAME. FOUND TO BE WITHIN ALLOWABLE LIMITS. CUT OUT AFT NUTPLATE PAX DOOR LOWER FRAME. REPAIR ACCOMPLISHED, IAW EMB 145 SRM 52-10-04 AND PIEDMONT EO1-52-20-0356.

Part: SHEAR TIE — CORRODED (DOOR FRAME) · airframe 37,071 hrs · 33,398 cycles

SSI 53-30-48 FR 65 SHEAR CLIP IS CORRODED AT CARGO DOOR CUT-OUT LOWER END. COMPLETE: BLENDED FR 65 SHEAR CLIP AT CARGO DOOR CUTOUT. FOUND TO BE OUT LIMITS. REMOVED PREVIOUS REPAIR. INSTALLED SHEAR CLIP AT FR 65, IAW EMB 145 SRM 53-31-04 ITEM 4 AND EO1-53-20-0339.

Part: SKIN — DAMAGED (FRAME 77) · airframe 37,071 hrs · 33,398 cycles

MULTIPLE RIVETS ON FR 77 BETWEEN STR 3L-9L HAVE POSSIBLE CRACKS (6 TOTAL). PERFORMED DYE PENETRANT INSPECTION, IAW EASI NDTM 3. RELEVANT INDICATION NOTED SKIN CRACK ENDS, MARKED, RADIOMETER EASI 0452. COMPLETE: CUTOUT DAMAGED AREA ON FR 77 BETWEEN STR. 4L-9L. FABRICATED REPAIR BUSHINGS, INSTALLED 3 BUSHING ON FR 77 BETWEEN STR 4L-9L, IAW EMB 145 SRM 53-32-01 AND PIEDMONT EO1-53-20-0343.

Part: SKIN — DAMAGED (FRAME 78) · airframe 37,071 hrs · 33,398 cycles

MULTIPLE RIVETS ON FR 78 BETWEEN STR 5R-7R HAVE POSSIBLE CRACKS (3 TOTAL). PERFORMED DYE PENETRANT INSPECTION, IAW EASI NDTM 1. RELEVANT INDICATION NOTED SKIN CRACK ENDS MARKED RADIOMETER EASI 0452. COMPLETE: CUTOUT DAMAGED AREA ON FR 78 BETWEEN STR 5R-6R. FABRICATED REPAIR BUSHINGS. INSTALLED BUSHING ON FR 78 BETWEEN STR 5R-6R, IAW EMB 145 SRM 53-32-01 AND PIEDMONT EO1-53-20-0341.

Part: SKIN — CRACKED (FRAME 79) · airframe 37,071 hrs · 33,398 cycles

MULTIPLE RIVETS ON FR 79 BETWEEN STR 5L-7L HAVE POSSIBLE CRACKS (2 TOTAL). PERFORMED DYE PENETRANT INSPECTION, IAW EASI NDTM 1 RELEVANT INDICATION NOTED SKIN CRACK ENDS MARKED RADIOMETER EASI 0452. COMPLETE: CUTOUT DAMAGED AREA ON FR 79 BETWEEN STR 6L-7L. FABRICATED REPAIR BUSHINGS. INSTALLED BUSHING ON FR 79 BETWEEN STR 6L-7L, IAW EMB 145 SRM 53-32-01 AND PIEDMONT EO1-53-20-0342.

Part: CONNECTOR — UNSECURE (CONTROL PANEL) · airframe 36,210 hrs · 32,428 cycles

PDIS 690 21-31 2248721 27NOV19 PHL CLOSE PACK 2 VALVE CLOSED MSG ON CLIMBOUT WITH PACK 1 VALV E CLOSED MSG AFTER APPOX 2 MINS. BOTH UNABLE TO CLEA R WITH QRH. PACK 1 CLEARED BELOW 100K FACT 27NOV19 10:06 PHL WHEN TROUBLESHOOTING FOUND BEHIND AC/PNEUMATIC PANEL CONNECTOR J7128 NO PROPERLY CONNECTED. RESECURED AS REQUIRED AND PERFORMED #1 AND #2 COOLING PACK OPS CHECK GOOD IAW 21-51-00, OK FOR SERVICE

Part: LIGHT — LOOSE · airframe 34,723 hrs · 30,754 cycles

NDIS 690 33-40 0008520 13MAR19 SBY CLOSE RT OVER WING EMERGENCY LIGHT IS INOP. 35719 00 SMC FACT 13MAR19 09:25 SBY R&R LIGHT BULB FOR RT EMERGENCY OVER WING LIGHT, NO FIX. INSPECTED ASSEMBLY AND FOUND LIGHT BULB TO BE LOOSE IN CONNECTOR. R&R OVER WING EMERGENCY LIGHT ASSEMBLY IAW AMM TASKS 33-50-10-020-005-A AND 33-50-10-420-005-A. OPS CHECK GOOD P/N OFF AND ON 30-2510-3.

Part: SIGN — INOPERATIVE (CABIN) · airframe 33,300 hrs · 29,107 cycles

EMERGENCY LIGHT ABOVE SERVICE DOOR WILL NOT ILLUMINATE. R&R EMERGENCY EXIT MARKING SIGN IN REF TO AMM 33-50-14-000/400-801-A. P/N ON EXIT SIGN 1013834, P/N OFF EXIT SIGN 1013834.

Part: STUD — BURNED (LANDING LIGHT) · airframe 33,278 hrs · 29,081 cycles

DURING DESCENT, AT APPROXIMATELY 25,000 FEET, A STRONG ELECTRICAL ODOR IN THE COCKPIT, REMAINED FOR 5 MINUTES AND DISSIPATED. R & R THE LANDING LIGHTS CONTACTOR K0233 DUE TO BURNED ON TERMINAL STUDS. GROUND RAN ACFT WITH NO ELECTRICAL ODOR PRESENT, OPS CHECKED GOOD IAW 33-41-03. OK FOR SERVICE.

Part: CONNECTOR — CONTAMINATED (SPOILER ACTUATOR) · airframe 32,724 hrs · 28,450 cycles

EICAS SPOILER FAILED MESSAGE WITH SPOILER DEPLOYMENT, DURING CLIMB OUT. HAPPENED AROUND 3000 FEET, SPOILERS FELT DEPLOYED, CIRCUIT BREAKERS WERE PULLED IAW QRH. TROUBLESHOT IAW FIM 27-63-00-810-802-A AND DETERMINED TO BE TRANSITORY CONDITION. PERFORMED INSPECTION OF ALL SPOILER PROXIMITY SENSORS AND FOUND GLYCOL INSIDE FOUR CONNECTOR PLUGS FOR THE PROXIMITY SENSORS. CLEANED THE CONTAMINATION AND PERFORMED A SPOILER SYSTEM OPERATIONAL CHECK IAW AMM 27-63-01. OPS CHECKED GOOD.

Part: YOKE — CRACKED (LT ENGINE) · airframe 32,702 hrs · 28,429 cycles

LEFT ENGINE FORWARD YOKE I RADIUS CRACKED. COMPLIED WITH EO-EM-54MR-386.

Part: ATTACH ANGLE — CRACKED (FRAME 47) · airframe 32,702 hrs · 28,429 cycles

RIGHT WING TO FUSELAGE LATERAL FAIRING LOWER ATTACH ANGLE CRACKED AT FRAME 47, 4TH ONE AFT. REMOVED AND REPLACED THE ATTACH ANGLE IAW ETN-EM-53-142.

Part: ATTACH ANGLE — CRACKED (FRAME 48) · airframe 32,702 hrs · 28,429 cycles

RIGHT WING TO FUSELAGE LATERAL FAIRING LOWER ATTACH ANGLE CRACKED AT FRAME 48, 5TH ONE AFT. INSTALLED A NEW ATTACH ANGLE BETWEEN FRAMES 48 AND 49 IAW ETN-EM-53-142, AND SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FRAMES 47-48) · airframe 32,702 hrs · 28,429 cycles

RIGHT HAT BEAM ATTACH ANGLE CRACKED BETWEEN FRAMES 47 AND 48. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 53-23-02.

Part: ATTACH FITTING — DAMAGED (LT AILERON) · airframe 32,702 hrs · 28,429 cycles

LEFT AILERON PCA ATTACH FITTING IS DAMAGED. REPAIRED IAW EO EM-27MR-112

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 32,702 hrs · 28,429 cycles

CARGO BAY DOOR HOLD OPEN STRUT SUPPORT IS CRACKED ON THE BACK SIDE IN 2 PLACES, REPLACED THE DOOR HOLD OPEN STRUT SUPPORT IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FRAMES 48-49) · airframe 32,702 hrs · 28,429 cycles

RIGHT WING TO FUSELAGE LATERAL FAIRING LOWER ATTACH ANGLE CRACKED BETWEEN FRAMES 48 AND 49, 6TH ONE AFT. FABRICATED A NEW ATTACH ANGLE IAW ETN-EM-53-142, AND SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (LT WING TO FUSE) · airframe 32,702 hrs · 28,429 cycles

LEFT WING TO FUSELAGE LATERAL FAIRING LOWER ATTACH ANGLE 4TH ONE AFT OF FRAME 48 CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW ETN-EM-53-142, AND SRM 51-40-02.

Part: STRUCTURE — CORRODED (LT WING TE FLAP) · airframe 32,702 hrs · 28,429 cycles

LEFT OTBD FLAP, OTBD ROLLER BUSHING BORE IS CORRODED. REMOVED AND REPLACED THE LT OTBD FLAP ASSY IAW AMM 27-50-00.

Part: TERMINAL — DETACHED (EMERGENCY LIGHT) · airframe 32,702 hrs · 28,429 cycles

AFT EMERGENCY LIGHT STRIP INOPERATIVE. FOUND ONE TERMINAL END LOOSE ON STRIP SIDE, INSTALLED A NEW TERMINAL END IAW SWPM 20-13-01. OPS CHECKED GOOD.

Part: CHARGER — UNKNOWN (EMERGENCY LIGHTS) · airframe 32,431 hrs · 28,162 cycles

REPLACE EPSU CHARGER-C/A-REMOVED & REPLACED EPSU BATTERY #1 IAW WC 33-700-19 OPS CHECK GOOD IAW WC 33-700-17

Part: VALVE — FAILED (CABIN PRESSURE) · airframe 32,425 hrs · 28,158 cycles

CLIMBING THROUGH 11,000 FT CABIN WARNING. WOULD NOT WORK IN AUTO OR MAN MODE. RETURN TO AIRPORT. PERFORMED INSTALL NEW GROUND CONNECTION VALVE IAW AMM 21-22-04 OPS AND PRESSURIZATION CHECK GOOD. INSTALL BOTH ESCAPE HATCHES IAW AMM 52-21-00 OPS AND PRESSURE CHECK GOOD.

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 31,974 hrs · 27,732 cycles

AFT CABIN FLASHLIGHT CHARGING CRADLE BROKEN. REMOVED AND REPLACED THE FLASHLIGHT CRADLE IAW AMM 33-50-16-000-801-A, AND 33-50-16-400-801-A. OPS CHECKED GOOD.

Part: PRESSURE SWITCH — INOPERATIVE (HYD SYSTEM) · airframe 31,306 hrs · 27,110 cycles

RUDDER SYS 1 - 2 INOPERATIVE WITH Y/D, CLIMBING THRUGH 3000 FT. REMOVED AND REPLACED THE NR 2 PRESSURE SWITCH IAW AMM TASK 27-23-04. OPS CHECKED GOOD. NO LEAK NOTED.

Part: SIGN — ABNORMAL (CABIN) · airframe 30,980 hrs · 26,783 cycles

DURING PS-1 INSPECTION, FOUND LT EMERGENCY EXIT MARKING SIGN INOP. REMOVED AND REPLACED LT EMER EXIT MARKING SIGN IAW EMB145 AMM 33-50-14. OPS CHECK GOOD.

Part: SLEEVE — BLOWN (NR 2 PACK) · airframe 30,670 hrs · 26,514 cycles

AFTER TAKE OFF, CLIMBING THRU 11,000, PACK 1 VALVE CLOSED. RESET IAW AOM 1, WOULD NOT RESET. CONTINUED CLIMBING TO REVIEW PROCEEDURE, THEN RECEIVED A BLEED 1 LEAK, CLOSED CROSS BLEED, DECLARED EMERGENCY, RETURNED TO DEPARTURE. PERFORMED AN OPS CHECK OF THE NR 1 PACK IAW MM 21-51-00, OPS CHECKED GOOD. FOUND BLOWN SLEEVE ON NR 2 PACK DUCTING. REMOVED & REPLACED THE SLEEVE IAW MM 21-51-14 OPS & LEAK CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,034 hrs · 25,927 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (SERVICE DOOR) · airframe 29,836 hrs · 25,749 cycles

SERVICE DOOR SEAL AFT LOWER CORNER REQUIRES PRESSURIZATION LEAK CHECK DUE TO DISPLACEMENT AND REINSTALLATION OF SEAL. PERFORMED PRESSURIZATION OF LEAK CHECK OF SERVICE DOOR SEAL IAW AMM 52-43-04. NO DEFECTS NOTED AT THIS TIME.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,563 hrs · 25,501 cycles

DAMAGED SKIN PANEL. REMOVED AND REPLACED DAMAGED THE SKIN PANEL IAW SRM 51-40-02. MAJOR REPAIR.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,563 hrs · 25,501 cycles

ALL EMERGENCY LIGHT BATTERIES ARE DEAD. R & R ALL EMERGENCY LIGHT BATTERY ASSEMBLIES IAW WC 33-700-19, OPS CK GOOD. BATTERY CHARGER ASSY, PN 11-0049, SN 18284, NR 4; SN 13704, NR 3; SN 20134, NR 2; PN BA5-0933-901, SN C02557, NR 1 EMERGENCY LIGHTING BATTERY, PN 2013-1A, SN 70938, NR 3; SN 105202, NR 2; PN 2013-1ASMI, SN 62620.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,557 hrs · 25,497 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. DISCONNECTED AND CONNECTED EMERGENCY LIGHT FROM BATTERY HARNESS IAW 33-26-05-400-801-A. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,378 hrs · 24,433 cycles

NUMBER 8 EMER FLOOR PROXIMITY LIGHT STRIP INOPERATIVE. R & R NR 8 EMER FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: FITTING — CHAFED (LT AILERON) · airframe 28,354 hrs · 24,413 cycles

INBOARD LUG ON THE LT AILERON DAMPENER FITTING IS CHAFED ON THE INBD SIDE. DAMPENER FITTING REPLACED IAW EO EM-27MR-112.

Part: RIB — BENT (RUDDER) · airframe 28,354 hrs · 24,413 cycles

RUDDER 1 HAS 2 BENT RIBS. 1 NEAR THE UPPER CTR HINGE POINT & 1 BY THE LOWER CTR HINGE POINT. INSTALLED RIB IAW SRM 51-40-02.

Part: BEAM — CORRODED (FUSELAGE) · airframe 28,354 hrs · 24,413 cycles

RIGHT HAT BEAM AT FRAME 23 IS CORRODED. REPAIRED RT HAT BEAM AT FRAME 23 IAW SRM 53-21-10.

Part: ANGLE — CRACKED (LT WING) · airframe 28,354 hrs · 24,413 cycles

LEFT OVERWING TO FUSELAGE PANEL LOWER NUTPLATE SUPPORT FLANGE IS CRACKED AT FRAME 49. REPLACED OVERWING ANGLE IAW SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 28,354 hrs · 24,413 cycles

STRINGER 21L IS CORRODED, BETWEEN FRAMES 20 & 21. REMOVED DAMAGED SECTION OF STRINGER 21L & INSTALLED NEW SECTION IAW SRM 51-40-02.

Part: ANGLE — CRACKED (LT WING) · airframe 28,354 hrs · 24,413 cycles

LEFT OVERWING TO FUSELAGE PANEL LOWER NUTPLATE SUPPORT FLANGE IS CRACKED AT FRAME 47. REPAIRED LT OVERWING SUPPORT FLANGE IAW ETN-EM-53-142. REF NRTC E485066 FOR LEAK CHECK.

Part: ANGLE — CRACKED (LT WING) · airframe 28,354 hrs · 24,413 cycles

LEFT OVERWING TO FUSELAGE PANEL LOWER NUTPLATE SUPPORT FLANGE IS CRACKED AT FRAME 50. REPLACED OVERWING ANGLE IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,354 hrs · 24,413 cycles

SERVICE DOOR CTR SILL IS CORRODED. COMPLETED REMOVAL & INSTALLATION OF SERVICE DOOR SILL IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (CARGO BAY) · airframe 28,354 hrs · 24,413 cycles

FORWARD SUPPORT BRACKET CRACKED FOR THE BAGGAGE DOOR LIFTING & LOWERING TORSION BARS. R & R BAGGAGE DOOR LIFTING & LOWERING TORSION BARS FWD SUPPORT BRACKET ANGLE IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,354 hrs · 24,413 cycles

BELLY FAIRING LOWER SUPPORT FLANGE IS CRACKED ON RT SIDE NEAR FRAME 51. R & R BAGGAGE DOOR LIFTING & LOWERING TORSION BARS FWD SUPPORT BRACKET ANGLE IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 28,354 hrs · 24,413 cycles

STRINGER CLIP ON FRAME 80, BETWEEN STRINGERS 6L - 7L, APPEARS TO HAVE A 1/2" CRACK. R & R STRINGER CLIP ON FRAME 80, BETWEEN STRINGERS 6L - 7L IAW SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,354 hrs · 24,413 cycles

RIGHT AFT UPPER FUSELAGE APPEARS TO BE CRACKED, BETWEEN FRAMES 73 & 74, JUST BELOW DRAG ANGLE. DURING EVALUATION FOUND DAMAGE TO BE AT FRAME 75 LOCATION & NOT BETWEEN FRAMES 73 - 74, REPAIRED IAW ERS-EM-53MR-1842.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,354 hrs · 24,413 cycles

LEFT AFT UPPER FUSELAGE APPEARS TO BE CRACKED, BETWEEN FRAMES 73 & 74, JUST BELOW DRAG ANGLE. DURING EVALUATION FOUND DAMAGE TO BE AT FRAME 75 LOCATION & NOT BETWEEN FRAMES 73 - 74. COMPLETED REPAIR IAW ERS-EM-53MR-1841.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 28,344 hrs · 24,402 cycles

DURING PS 1 FOUND BATTERY & POWER SUPPLY 2 INOPERATIVE. R & R NR 2 BATTERY & POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. EMER LIGHTING BATTERY PN 2013-1ASMI & SN 82630.

Part: PROXIMITY SENSOR — FAILED (LT SPOILER) · airframe 28,344 hrs · 24,402 cycles

SPOIL FAIL ON TAKEOFF ROLL JUST BEFORE V1 AT ABOUT 120 KTS SPOILER INDICATED OPEN WARNING. SPOILER CB INDICATION POPPED. R & R LT INBD SPOILER PROX SENSOR IAW AMM 27-63-04 & LT INBD SPOILER PROX SENSOR CONNECTOR IAW AMM SWPM 20-50-01. OPERATIONAL CHECK OF THE SPOILER SYS GOOD IAW AMM 27-63-01.

Part: LIGHT — INOPERATIVE (BLEED AIR SYS) · airframe 28,082 hrs · 24,161 cycles

BLEED 2 PUSH BUTTON LIGHTS INOPERATIVE. R & R BLEED 2 PUSH BUTTON LIGHT LAMP IAW AMM 20-13-04-000-801-A & 20-13-04-400-801-A. OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 27,778 hrs · 23,875 cycles

CAPTAINS EMER FLASHLIGHT HOLDER BROKEN. R & R CAPTAINS EMER FLASHLIGHT HOLDER IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 26,444 hrs · 22,651 cycles

UPON ENTERING THE AIRPLANE TRIPLE CHIME HEARD & LAVATORY SMOKE ON EICAS OBSERVED. OPERATIONS CHECK LAVATORY SMOKE. OPERATIONS CHECKED GOOD 26-14-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,173 hrs · 22,433 cycles

LEFT AFT EXTERNAL OVERWING EMER LIGHT INOPERATIVE. R & R LT EXTERNAL OVERWING EMER LIGHT IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 25,540 hrs · 21,804 cycles

FIRST FLIGHT OF THE DAY TESTING FIRE THE BAGG EXTINGUISHER FAILED TO LIGHT UP. R & R FWD CARGO SMOKE DETECTOR IAW AMM 26-15-0. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,277 hrs · 21,588 cycles

REAR FLOOR PROX STRIP AT ROW 18A INOPERATIVE. REPAIRED EMERGENCY LIGHT FLOOR STRIP I.A.W SWPM 20-21-00 OPS CHECK GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 25,029 hrs · 21,380 cycles

DURING PREFLIGHT FLIGHT ATTENDANT FOUND CABIN'S REAR FLASHLIGHT HOLDER BROKEN. REAR FLASHLIGHT HOLDER DEFERRED IAW MEL 25-53. R & R AFT FLIGHT ATTENDANT FLASHLIGHT & HOLDER IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,996 hrs · 21,352 cycles

EMERGENCY OVERWING LIGHTS INOPERATIVE. R & R NR 4 EMER LIGHT BATTERY & CHARGER IAW AMM33-50-04. OPERATIONS CHECKED GOOD. EMER LIGHT BATTERY PN 2013-1A SN 112872.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,996 hrs · 21,352 cycles

BOTH LT & RT EXTERIOR OVERWING EMER LIGHTS INOPERATIVE. R & R BOTH BATTERY CHARGER & BATTERY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. CHARGER ASSEMBLY BATTERY PN BAS0933901, SN 001596.

Part: LATCH — OPEN (FUEL DOOR) · airframe 24,523 hrs · 20,914 cycles

AFTER TAKEOFF FUELING PANEL DOOR LIGHT ON & MSG ON EICAS. FOUND FUEL DOOR LATCH OPEN, CLOSED LATCH. FUEL DOOR INDICATION OPERATIONS CHECKED GOOD IAW AMM 52-78-00.

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 24,249 hrs · 20,712 cycles

HYD SYS NR 1 LOW QTY AT FL 350 GEAR & FLAPS UP MACH 72 NO ICE. COMPLIED WITH HYD SYS TRANSFER IAW ETN EN-27-023, CHECKED GOOD, OK FOR SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · airframe 24,096 hrs · 20,593 cycles

FRAME 68 SHEAR CLIP CORRODED. PERFORMED PERMANENT REPAIR OF FRAME 68 SHEAR CLIP IAW EO EM-53MR-1129.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 24,096 hrs · 20,593 cycles

RIGHT FLOOR BEAM INBD SUPPORT CRACKED BETWEEN FRAME 47 & 48. REMOVED CRACKED SUPPORT & INSTALLED NEW SUPPORTS ON RT INBD FLOOR BEAM BETWEEN FRAMES 46 - 50 IAW SRM 51-40-02, 53-23-02.

Part: STRAP — CORRODED (FUSELAGE) · airframe 24,096 hrs · 20,593 cycles

FRAME 65 AT STRINGER 17L TOP STRAP CORRODED. REMOVED & INSTALLED NEW FABRICATED PART 145-25518-003 AT FRAME 65 AT STRINGER 17L IAW SRM 51-40-02.

Part: SWITCH — BROKEN (EMERGENCY EXIT) · airframe 24,096 hrs · 20,593 cycles

RIGHT EMERGENCY EXIT STOW SWITCH BROKEN. R & R RT OVERWING ESCAPE HATCH MICRO SWITCH ACTUATOR LEVER IAW AMM 52-75-01, OPERATIONS CHECKED GOOD.

Part: CONTROL VALVE — FAILED (A/C PACK) · airframe 23,262 hrs · 19,904 cycles

SITTING AT GATE TURNED ON BOTH PACKS AND NOTICED STRANGE BURNING ODOR. R & R NR 1 DUAL TEMP CONTROL VALVE. OPS CHECKED GOOD IAW AMM 21-60-01.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,185 hrs · 19,839 cycles

THE CREW REPORTED A BURNING ODOR ON DESCENT THROUGH FT 280 AND AGAIN AROUND FT 180. THE ACFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. COMPLIED WITH ETN EM-72-034R4. NO ODOR NOTED AT THIS TIME. THE ACFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,920 hrs · 19,614 cycles

OVERWING EXIT LOCATOR FWD SIDE INOPERATIVE. R & R EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,592 hrs · 19,342 cycles

DURING MX INSPECTION, FOUND EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,081 hrs · 18,175 cycles

DURING MAINTENANCE INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT ASSEMBLY INOPERABLE. ISSUED MEL 25-53 AUTH 120668. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — UNSECURE (COCKPIT) · airframe 21,043 hrs · 18,145 cycles

ON FLIGHT 3205 THE CREW REPORTED THE CAPTAIN'S FLASHLIGHT DOES NOT STAY TIGHTLY IN RECHARGING RECEPTICLE. DEFERRED PER MEL 25-53 AUTH 120668-C FOR CAPTAIN’S FLASHLIGHT/HOLDER. SECURED FLASHLIGHT. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAPPER VALVE — DEFECTIVE (LT WING) · airframe 20,442 hrs · 17,666 cycles

ON FLIGHT 2956 THE CREW REPORTED THAT WHILE AT FLIGHT LEVEL 300 A PASSENGER NOTICED A POSSIBLE FUEL LEAK ON THE LEFT WING SLIGHTLY INBOARD OF INBOARD EDGE OF LEFT AILERON. THE CREW COMPLETED THE AOM VOL 1 PROCEDURES, CONTACTED SOC/DISPATCH AND DECLARED AN EMERGENCY AND ELECTED TO DIVERT TO JAN. THE AIRCRAFT LANDED WITHOUT INCIDENT. CFR FOUND NO EVIDENCE OF AN IMMEDIATE LEAK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT WING FUEL FLAP VALVE AT RIB 19 IAW EMB 145 AMM 28-11-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 19,848 hrs · 17,163 cycles

DURING B INSPECTION, FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT INTERIOR OVERWING EMERGENCY LAMP IAW AMM 33-50-07-000-801/33-50-07-400-801. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,691 hrs · 17,042 cycles

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

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 19,577 hrs · 16,938 cycles

DURING B INSPECTION, FOUND THE RIGHT FLOOR SUPPORT CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR SUPPORT . AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — UNSECURE (CABIN) · airframe 19,577 hrs · 16,938 cycles

DURING B INSPECTION, FOUND THE AFT MOST EMERGENCY LIGHT STRIP NOT PROPERLY SECURED. AIRCRAFT REMOVED FROM SERVICE. SECURED THE AFT MOST EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 19,577 hrs · 16,938 cycles

DURING B INSPECTIONS, FOUND THE LEFT FLOOR SUPPORT IS CORRODED BETWEEN FRAMES 61-65. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FLOOR SUPPORT FOR FRAMES 61-65, IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 19,539 hrs · 16,909 cycles

ON FLIGHT 3235 THE CREW REPORTED THAT DURING TAXI IN THEY NOTICED FUMES IN THE COCKPIT AND CABIN. APU BLEED ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ENGINE RUN IAW RRMM 72-00-00 WITH BLEEDS AND PACKS ON. COULD NOT DUPLICATE PROBLEM AT THIS TIME. FUNCTIONAL CHECK FLIGHT FOUND SATISFACTORY, NO FUMES NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — INOPERATIVE (RECIRCULATION) · airframe 19,359 hrs · 16,759 cycles

FLIGHT 2906, CREW REPORTED DURING PUSHBACK THERE WAS A SUDDEN DECREASE OF AIR FLOW FROM GASPERS WHILE ON APU, TRIED TO START ENGINES AND TAXI BUT PROBLEM PERSISTED IN AUTO AND MANUAL. A PASSENGER IN ROW 4 REPORTED A BURNING ODOR ON TAXI. IN COCKPIT TEMP 37C CABIN REACHED 30C. AIRCRAFT REMOVED FROM SERVICE. FOUND RECIRCULATION FAN 1 AND 2 FAILED REMOVED AND REPLACED NR 1 AND 2 RECIRCULATION FANS IAW AMM 21-24-01. OPS CHECKED GOOD IAW AMM TASK 21-20-00-700-801-A. AIRCRAFT RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT ASSY) · airframe 19,279 hrs · 16,681 cycles

DURING MAINTENANCE INSPECTION FOUND THE CAPTAINS FLASHLIGHT HOLDER BROKEN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT HOLDER IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,157 hrs · 15,846 cycles

LT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LT OVERWING UPPER EMERGENCY LIGHT IAW EMB AMM 33-50-07, OPS CHECK GOOD.

Part: TIRE — FAILED (MLG) · airframe 17,458 hrs · 15,307 cycles

ON FLIGHT 2779 THE CREW REPORTED THAT UPON LANDING, BLEW ALL FOUR TIRES, WITH DAMAGE TO ALL BRAKES, GEAR DOORS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACE TIRE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 15,525 hrs · 13,890 cycles

FOR FLIGHT 3633 DURING PRE FLIGHT FOUND AFT FLIGHT ATTENDANT FLASHLIGHT TO BE INOPERABLE. THE FLASHLIGHT WOULD NOT CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED THE REAR CABIN FLIGHT ATTENDANT FLASHLIGHT IAW EMB MM 33-50-15. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CART — ODOR (GALLEY) · airframe 15,213 hrs · 13,645 cycles

ON FLIGHT 3222 DURING THE DESCENT THE FLIGHT ATTENDANT REPORTED FUMES OF A GASOLINE NATURE COMING FROM THE GALLEY CART IN THE FORWARD GALLEY. THE CAPTAIN DECLARED AN EMERGENCY. NO OTHER ODORS OR FUMES WERE NOTED. FIRE, CRASH AND RESCUE WAS CALLED FOR THE LANDING. THE AIRCRAFT LANDED SAFELY WITH NO INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOLLOWED EPC PROCEDURES FOR CABIN FUMES. THE FIRE DEPARTMENT CONFIRMED THE GASOLINE ODOR IN THE GALLEY CART AND NO WHERE ELSE ON THE AIRCRAFT. REMOVED AND REPLACED THE RIGHT GALLEY CART AS REQUIRED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — LEAKING (NR 4) · airframe 22,211 hrs · 21,121 cycles

FOR FLIGHT 4322 DURING INSPECTION FOUND AN OIL SMELL IN THE COCKPIT WITH THE NUMBER 1 BLEED AND PACK ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 ENGINE IAW 71-000-00. THE OPERATIONAL CHECK WAS GOOD. NO LEAKS NOTED. THE CAUSE OF THE SMOKE WAS DETERMINED TO BE FROM A FAULTY NR 4 CARBON SEAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — DIRTY (CARGO DOOR) · airframe 13,957 hrs · 12,627 cycles

ON FLIGHT 3218 THE CREW REPORTED THE BAGGAGE DOOR WARNING ILLUMINATED ON CLIMBOUT. THE CREW REPORTED, NEVER LOST PRESSURE AT 1500 FEET. THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBRICATED THE BAGGAGE DOOR MICRO SWITCHES AND PERFORMED MULTIPLE OPERATIONAL CHECKS OF THE BAGGAGE DOOR WARNING SYSTEM. NO PARTS REMOVED OR REPLACED. ALL CHECKS GOOD PER EMB AMM 52-76-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRAKE — FAILED (NR 3) · airframe 11,531 hrs · 10,479 cycles

ON FLIGHT 3686, CREW REPORTED UPON LANDING A "GIVE" IN THE BRAKING. THIS WAS FOLLOWED BY "BRAKE DEGRADED" EICAS CAUTION MESSAGE. AIRCRAFT TOOK LONGER TO SLOW AND ATC INFORMED THE CREW THEY SAW A "PUFF" OF SMOKE FROM THE RIGHT WHEEL. CREW CALLED FOR CFR AIRCRAFT WAS TOWED BACK TO GATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BRAKE NUMBER 3 AND 4, WHEEL ASSY 3 AND NR 3 BRAKE LINE. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — MALFUNCTIONED (FUEL VENT) · airframe 8,393 hrs · 7,611 cycles

ON FLIGHT 4207, CREW REPORTED ON CLIMB-OUT THERE WAS SOME FUEL VENTING FROM THE RIGHT WING VENT VALVE. SERVICED TANKS TO 10600 LBS AND WAS UNABLE TO DUPLICATE LEAK. OK PER EMB AMM 28-12-00 OVERWEIGHT LANDING. AIRCRAFT REMOVED FROM SERVICE. DESCENT WAS UNDER 300 FPM, NO MAINTENANCE ACTION REQUIRED FOR OVERWEIGHT LANDING. INSPECTED AIRCRAFT, NO ACTION REQUIRED PER EMB AMM 28-12-00 AND NR 8194; AND NR 8194; AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — FAILED (RUDDER PRESSURE) · airframe 8,047 hrs · 7,275 cycles

RUDDER SYS 1 AND 2 INOP DURING FLIGHT. REMOVED AND REPLACED NUMBER 2 RUDDER PRESSURE SWITCH IAW EMB 145 AMM 27-23-04. OPS CHECK GOOD IAW EMB 145 AMM 27-23-00, AIRCRAFT RETURNED TO SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 6,793 hrs · 6,130 cycles

HUMMING NOISE INFLIGHT WITH FLAPS IN UP POSITION, NOISE GOES AWAY WITH FLAPS DEPLOYED. REMOVED AND REPLACED PCA AND COMPLIED WITH LEFT INBOARD FLAP SEAL PLATE MOD IAW EMB AMM 27-12-01. OPERATIONAL CHECKED GOOD WITH NO DEFECTS NOTED, RETURNED AIRCRAFT TO SERVICE.

Part: SKIN — DAMAGED (ZONE 200) · airframe 6,752 hrs · 6,102 cycles

LEFT LOWER FUSELAGE SKIN DAMAGED BETWEEN FRAMES 63 AND 65 AT STRINGER 19L, 20L AND 21L. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB IC2004-145/03857A, IC2007-145-03878 AND IC2007-145/03912. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (ZONE 300) · airframe 6,584 hrs · 5,970 cycles

PITCH TRIM INOP MESSAGE AT 37,000 FEET, BACKUP SYSTEM WORKED NORMAL. REMOVED AND REPLACED HORIZONTAL STABLIZER ACTUATOR IAW EMB AMM 27-40-02. OPERATIONAL CHECK GOOD, PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.

Part: COMPUTER — FAILED (ZONE 300) · airframe 6,581 hrs · 5,968 cycles

PITCH TRIM MAIN INOP WARNING MESSAGE, RETURNED TO DFW. REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT IAW EMB AMM 27-40-01. OPERATIONAL CHECKED GOOD, PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE.

Part: TIRE — FAILED (MLG)

BLOWN TIRE ON TAKEOFF. RETURN TO ORD DID NOT LAND OVERWEIGHT. REPLACED NR 2 MAIN LANDING GEAR WHEEL ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (M)