N692AE

Part: HOT WATER POT — ODOR (ZONE 900) · airframe 46,766 hrs · 43,622 cycles

IN FLIGHT FA REPORTS AN ELECTRICAL BURNING SMELL IN GALLEY AREA. CONFIRMED HOT JUG OFF. NO C/B POPPED. SLAVED IN HOT JUG. OPS CHECK GOOD. LEFT HOT JUG ON FOR 20MINS WITH NO BURNING SMELL OBSERVED. REMOVED DEFECTIVE HOT JUG FROM A/C.

Part: CONTROL MODULE — ODOR (ZONE 200)

LH SIDEWALL LIGHTS AFT OF 2A INOP. WITH ELECTRICAL BURNING SMELL. R & R CONTROL MODULE ASY IAW AMM 33-21-01 OPS CHECK IAW AMM 33-21-01A/C OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,212 hrs · 42,908 cycles

RH OUTBD FLOOR SILL #2 HAS PITTING IN MULTIPLE SPOTS. BLENDED TO REMOVE PITTING ON RH OUTBD FLOOR SILL #2 IAW EMB 145 SRM 51-10-03 RAR RH FLOOR SILL #2 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

LH FLOOR SILL #2 HAS CORROSION IN MULTIPLE SPOTS. BLENDED TO REMOVE CORROSION ON LH FLOOR SILL #2 IAW EMB 145 SRM 51-10-03. RAR THE LH #2 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

LH UPPER #2 SEAT TRACK HAS CORROSION IN MULTIPLE SPOTS. REMOVED AND REPLACED LH UPPER #2 SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

LH FLOOR CROSSBEAM AT FR 31 HAS CORROSION. RAR LH FLOOR CROSSBEAM AT FR31 IAW EMB 145 SRM 51-40-02

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

GALLEY FLOOR R/H BEAM DIAMOND GUSSET AT FR-22 HAS CORROSION. REMOVED AND REPLACED GALLEY FLOOR R/H BEAM DIAMOND GUSSET AT FR-22 IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

F058356 GALLEY FLOOR FWD DIGITAL BETWEEN FR-16/17 NEXT TO PAX DOOR AROUND A NUT-PLATE HOLE HAS CORROSION. REPAIRED CORRODED AREA ON GALLEY FLOOR FWD DIGITAL BETWEEN FR-16/17 NEXT TO PAX DOOR AROUND A NUT-PLATE HOLE IAW PIEDMONT EO1-05-25-0264 AND EMB 145 SRM 53-21-10RE ITEM 2 FIGURE 201 SHEET 5.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

LH FLOOR SILL #3 HAS CORROSION IN MULTIPLE SPOTS. REMOVED AND REPLACED LH FLOOR SILL #3 IAW EMB 145 SRM 51-40-02

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

F058237 LH UPPER #3 SEAT TRACK HAS PITTING IN MULTIPLE SPOTS. REMOVED PITTED LH UPPER #3 SEAT TRACK AND INSTALLED SERVICEABLE LH UPPER #3 SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

RH LOWER #1 SEAT TRACK HAS CORROSION IN MULTIPLE SPOTS. REMOVED AND REPLACED RH LOWER SEAT TRACK #1 IAW EMB 145 AMM 53-01-06

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

F058242 RH UPPER #1 SEAT TRACK HAS CORROSION IN MULTIPLE SPOTS. REMOVED AND REPLACED RH UPPER #1 SEAT TRACK IAW EMB 145 AMM 53-01-06

Part: ANGLE — CORRODED (ESCAPE HATCH) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

F058407 RH ESCAPE HATCH LOWER L ANGLE HAS SURFACE CORROSION AT AFT GROUND PLATE. REMOVED AND REPLACED RH ESCAPE HATCH LOWER "L" ANGLE IAW EMB145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

F058236 LH LOWER #3 SEAT TRACK HAS PITTING IN MULTIPLE SPOTS. REMOVED AND REPLACED L/H LOWER #3 SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

F058251 LH OMEGA BEAM IS CORRODED BETWEEN FR33 AND FR34. REMOVED CORROSION ON LH OMEGA BEAM BETWEEN FR33 AND FR34 IAW EMB 145 SRM 51-10-03 AND BLENDED AREA ACCEPTED IAW PIEDMONT EO1-05-25-0264 AND ETD2025-145-925337.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,121 hrs · 42,908 cycles

F057577 CABIN SHEAR CLIP IS CRACKED AT FR-61 BETWEEN STR 6R/7R. REMOVED AND REPLACED CABIN SHEAR CLIP AT FR-61 BETWEEN STR 6R/7R IAW EMB145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

LH UPPER SEAT TRACK #5 IS GOUGED AND CORRODED IN NUMEROUS AREAS ALONG ENTIRE LENGTH ON INSIDE AND OUTSIDE OF TRACK. RAR LH UPPER SEAT TRACK #5 IAW EMB 145 AMM 53-01-06

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,121 hrs · 42,908 cycles

F057576 CABIN SHEAR CLIP IS CRACKED AT FR-61 BETWEEN STR 6L/7L. REMOVED AND REPLACED CABIN SHEAR CLIP AT FR-61 BETWEEN STR 6L/7L IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

LH CABIN FLOOR SILL #6 HAS CORROSION ALONG THE ENTIRE LENGTH INCLUDING NUMEROUS PREVIOUSLY BLENDED AREAS. REMOVED AND REPLACED LH CABIN FLOOR SILL #6 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

RH CABIN FLOOR SILL #5 CORRODED IN NUMEROUS AREAS. BLENDED TO REMOVE CORROSION ON RH CABIN FLOOR SILL #5 IAW EMB 145 SRM 51-10-03. RH CABIN FLOOR SILL #5 IS WITHIN ALLOWABLE LIMITS IAW EMB 145 SRM 53-23-10 AD.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

F057498 CENTER FLOOR OMEGA BEAM GUSSET BETWEEN FR-54/55 HAS CORROSION. REMOVED AND REPLACED CENTER FLOOR OMEGA BEAM GUSSET BETWEEN FR-54/55 IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

LH CABIN FLOOR SILL #4 HAS CORROSION ALONG THE ENTIRE LENGTH INCLUDING NUMEROUS PREVIOUSLY BLENDED AREAS. REMOVED AND REPLACED CABIN FLOOR SILL #4 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

LH CABIN FLOOR SILL #5 HAS CORROSION ALONG THE ENTIRE LENGTH. PERFORMED HFEC INSPECTION IAW EASI NDTM SECTION 4-01, NO RELEVANT INDICATIONS NOTED. PERFORMED UT THICKNESS INSPECTION IAW EASI NDTM SECTION 4-02, THICKNESS MARKED FOR EVALUATION.- .043" TO .049". EASI S/N 8958 AND EASI S/N 8389 USED. COMPLETED REMOVAL OF CORROSION ON LH CABIN FLOOR SILL #5 IAW EMB 145 SRM 51-10-03. FURTHER INVESTIGATION AFTER NDT SHOWS FLOOR SILL TO BE WITHIN ALLOWABLE LIMITS IAW EMB 145 SRM 53-23-10AD.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

LH UPPER SEAT TRACK #4 IS GOUGED AND CORRODED IN NUMEROUS AREAS ALONG ENTIRE LENGTH ON INSIDE AND OUTSIDE OF TRACK. RAR LH UPPER SEAT TRACK #4 IAW EMB 145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

F057484 L/H FLOOR SILL #7 HAVE CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED L/H FLOOR SILL #7 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

RH CABIN FLOOR SILL #3 CORRODED BTWN FR 35-39 IN PREVIOUSLY BLENDED AREAS. REMOVED AND REPLACED RH CABIN FLOOR SILL #3 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,121 hrs · 42,908 cycles

RH CABIN FLOOR SILL #4 CORRODED BTWN FR 44-48 INCLUDING A PREVIOUSLY BLENDED AREA. BLENDED TO REMOVE CORROSION ON RH CABIN FLOOR SILL #4 IAW EMB 145 SRM 51-10-03. COMPLETED REMOVAL OF CORROSION ON RH CABIN FLOOR SILL #4 IAW EMB 145 SRM 51-10-03. FURTHER INVESTIGATION AFTER NDT SHOWS FLOOR SILL TO BE WITHIN ALLOWABLE LIMITS IAW EMB 145 SRM 53-23-10AD

Part: VALVE — FAILED (ANTI-ICE SYS) · airframe 45,309 hrs · 42,033 cycles

IN ICING CONDITIONS ICE COND A/I INOP, WING A/ICE FAIL, STAB A/ICE FAIL EICAS MESSAGES DISPLAYED DFRL 12FEB25 06:02 CLT R/R'D #2 FAN AIR VALVE IAW EMB AMM 36-11-03. OPS CHECK AND LEAK CHECK STILL REQ'D. FACT 12FEB25 08:08 CLT RAN A/C, OPS CHECK IRT AMM 36-00-00. OPS CHECK/LEAK CHECK GOOD. A/C OK FOR SERVICE AT THIS TIME

Part: THERMOSTAT — FAULTED (NR 2 ENGINE) · airframe 45,309 hrs · 42,033 cycles

BLEED 2 OVERTEMP MESSAGE IN FLIGHT, INDICATED IN RED ZONE DFRL 12FEB25 06:04 CLT R/R'D BLEED #2 FAN AIR VALVE CONTROL THERMOSTAT. STILL REQ'S OPS CHECK AND LEAK CHECK. FACT 12FEB25 08:10 CLT OPS AND LEAK CHECK COMPLETE. GOOD IAW AMM 36-11-06.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 44,606 hrs · 41,290 cycles

LH FWD EXTERNAL EMERGENCY LIGHT INOP. RAR #1 EMER LIGHT BATTERY IAW AMM 33-50-54

Part: WIRE — BROKEN (THERMAL SWITCH)

AFTER T/O BLEED 2 LEAK EICAS MSG. RAN QRH AND MSG EXTINGUISHED. T/S IAW FIM 36-20-00-810-801-A TO STEP 9, FOUND WIRE BROKEN ON THERMAL SWITCH S0157. R/R'D SWITCH S0157 IAW MM 36-20-02. OPS CK GOOD LEAK CK GOOD

Part: WARNING UNIT — FAULTED (TE FLAPS) · airframe 43,727 hrs · 40,289 cycles

AFTER T/O AND FLAPS RETRACTED TO ZERO. T/O CONFIG ANNUNCIATED "FLAPS" IN FLIGHT. FACT 07MAY24 PERFORMED AURAL WARNING OPS CHECK IAW AMM 31-51-00. NO DEFECTS FOUND,R&R AURAL WARNING UNIT AS A PRECAUTIONG IAW AMM 31-51-01. OPS CHECK GOOD, OK FOR SERVICE AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,505 hrs · 40,041 cycles

PAX DOOR EMERGENCY LIGHT INOP. SBY R & R PAX DOOR EMERGECNY LIGHT LAMP NO FIX.R+RED PAX DOOR EMERGENCY LIGHT ASSY AND SECURED WITH RETAINING HARDWARE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,694 hrs · 38,003 cycles

E966678 L/H OMEGA BEAM AT FRAME 28 HAS ELONGATED SEAT TRACK SCREW HOLE. REPAIRED IAW PIEDMONT EO 1-53-23-0080

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,694 hrs · 38,003 cycles

E965760 CORROSION (LEVEL2) ON DIAMOND GUSSET IN GALLEY AT FRAME 22. REMOVED AND REPLACED DIAMOND GUSSET IAW EMB145 SRM 51-20-03, AND 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,694 hrs · 38,003 cycles

E965758 COROSSOIN (LEVEL 2) ON LH IB #1 SEAT TRACK. REMOVED AND REPLACED SEAT TRACK IAW EMB145 AMM 53-01-06TQW #2081

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,694 hrs · 38,003 cycles

E965753 CORROSION (LEVEL 2)ON LH FWD DIGITAL AT PREVIOUS REPAIR. REPAIRED IAW PIEDMONT EO 1-53-23-0091

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,694 hrs · 38,003 cycles

E965774 CORROSION (LEVEL 2) ON LH OTBD #1 SEAT TRACK. REMOVED AND REPLACED LH OTBD #1 SEAT TRACK IAW EMB144 AMM 53-01-06

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,694 hrs · 38,003 cycles

E965460 PAX DOOR BOTTOM FRAME 1 SCREW HOLE CORRODED (LEVEL 2), REPAIRED IAW PIEDMONT EO 1-52-23-0090

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,694 hrs · 38,003 cycles

E965394 L/H SIDE OF FUSELAGE HAS POSSIBLE CRACKS AT TWO FASTENERS AT FRAME 77 BETWEEN STRINGERS 5L AND 7L. REPAIRED IAW PIEDMONT EO 1-53-23-0088.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,694 hrs · 38,003 cycles

E965745 CABIN LH #2 FLOOR BEAM GUSSET HAS AREAS WITH SIGNS OF CORROSION (LEVEL 2). REPAIRED IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,694 hrs · 38,003 cycles

E965262 TOILET WASTE VALVE BUCKET EXTERNAL SKIN CORRODED (LEVEL 2) REPAIRED IAW PIEDMONT EO 1-53-23-0081

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,694 hrs · 38,003 cycles

RH VERTICAL DRAG ANGLE HAS 2 POSSIBLE CRACKS BETEEN FRAMES 76 AND 77. REPAIRED IAW EO1-53-23-0087

Part: UNKNOWN — UNKNOWN · airframe 41,689 hrs · 38,000 cycles

CAME TO AIRCRAFT AND POWERED IT UP WITH APU. DID FIRE DETECTION TEST, BAG LIGHT REMAINED ON. DID FIRE DETECT AGAIN AGAIN, LIGHT REMAINED ON. TOLD FIRST OFFICER TO CHECK PEEP HOLE, TOLD FIRST OFFICER TO LOOK AT BAG BAY. 1ST OFFICER SAID IT LOOKED LIKE SMOKE IN BAG BAY, EXTINGUISHING BOTTLE PUSHED, MADE CALL TO CFR.

Part: CONTROL UNIT — FAULTED (HORIZONTAL STAB) · airframe 41,109 hrs · 37,378 cycles

PITCH TRIM MAIN INOP DISPLAYED ON EICAS DURING INITIAL CLIMBOUT. R/R HSCU IAW AMM 27-40-01.OPS CHECK GOOD.A/C OK FOR

Part: MODULE — FAULTED (PITCH TRIM) · airframe 41,109 hrs · 37,378 cycles

PITCH TRIM MAIN INOP EICAS MESSAGE DISPLAYED ON T/O. R AND R PITCH TRIM MODULE ASSY AS REQUIRED OPS CHECK GOOD ACFT OK FOR SERVICE

Part: NONE — NONE · airframe 40,356 hrs · 36,523 cycles

PDIS 692 05-50 2708471 27MAY22 ROA CLOSE SEVERE TURBULENCE ENCOUNTERED IN FLIGHT. (CAPTAIN ANSWERED 1.SEVERE 2. AUTOPILOT WAS ON 3. A/C OUT OF CONTROL - NO 4. CHNG IN ALT OR ATT - NO 5. VARIA IN AIRSPD - +/- 10 KNOTS 6. ANYTHING ELSE - NO 7. YES SHE REPORTED IT TO ATC. 27014 00 WO FACT 27MAY22 20:31 ROA INSPECTED AIRCRAFT IAW AMM 05-50-27, NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE

Part: NONE — NONE · airframe 40,197 hrs · 36,321 cycles

PDIS 692 30-14 2708031 22APR22 MDT CLOSE AOA HEAT 2 INOP ON EICAS. FACT 22APR22 03:47 ROA R&R'D #200 AOA IAW AMM 27-36-01. OPS CHECK GOOD IAW AMM 30-12-00. NO DEFECTS NOTED AT THIS TIME.

Part: NONE — NONE · airframe 40,174 hrs · 36,297 cycles

PDIS 692 28-21 2704993 18APR22 CHS CLOSE AT MAX THRUST ON TAKE OFF HAD E2 FUEL LOW PRESSURE CAUTION DISPLAYED. REJECTED TAKEOFF. C/W MAINT PROCEDURE. PUMP 2A IS ON THE MEL FACT 23APR22 10:26 ROA T/S FIM 28-45-00-810-802-A THRU BLOCK 42 SHORTSIGNED RNR FUEL PUMP 2A IRW AMM 28-21-00 SHORT SIGNED OPS CHECK IAW AMM 28-45-00-700-801-AG GOOD OK FOR SERVICE CLEAR MEL 28-3

Part: NONE — NONE · airframe 39,585 hrs · 35,667 cycles

NDIS 692 30-10 0029390 19DEC21 ORF CLOSE CREW REPORTED MOMENTARY WING A/ICE FAIL MSG DURING TAKEOFF. ABORTED TAKEOFF RAN QRH AND ICE PROTECTION TEST (PNEUMATIC) ON GROUND, NO FURTHER DEFECTS NOTED. FACT 19DEC21 09:21 RIC NO RELATED CMC MESSAGES FOUND INSPECTED PACK DUCTS FOR PROPER CONNECTIONS FOUND NUMEROUS DUCT SLEEVES NOT PROPERLY CONNECTED ON #100 AND #200PACK SYSTEMS RECONNECTED DUCT SLEEVES PROPERLY AS REQUIRED LEAK CHECK GOOD PERFORMED AIRFOIL ANTI-ICING SYSTEM OPERATIONAL TEST IN REF TO AMM 30-10-00-700-801-A OPS CHECK GOOD OK FOR SERVICE AT THIS TIME

Part: NONE — NONE · airframe 39,580 hrs · 35,661 cycles

PDIS 692 30-10 2472263 18DEC21 YYZ CLOSE WING A/ICE FAIL ON CLIMB SHORTLY AFTER TAKEOFF. RESOLVED AFTER FOLLOWING QRH FACT 18DEC21 21:46 PHL VISUALLY INSP L/H WING ANTI ICE VALVE AND DUCT WEAR NO DEFECTS NOTED. PERFORMED OPS CHECK OF WING ANTI ICE SYSTEM AND ANTI ICE VALVES IAW AMM 30-00-00-05 OPS CHECK GOOD OK FOR SERVICE

Part: DUCT — LEAKING (WING ANTI-ICE) · airframe 38,916 hrs · 34,915 cycles

WING ANTI ICE FAIL DURING PNEUMATIC TEST ON CLIMB. R & R Y DUCT IN PACK AREA THAT WAS LEAKING. R+R BULBS FOR WING OPEN LIGHT IAW AMM 20 13 04. OPS CHECK GOOD IAW AMM 30 00 00 700 802 A. OKAY FOR SERVICE CLEAR MEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,759 hrs · 34,743 cycles

EMERGENCY EXIT LIGHT IS INOP JUST AFT OF R/H EMERGENCY EXIT HATCH AT SEAT 12BC. R & R EMERGENCY EXIT LIGHT ASSY JUST AFT OF R/H EMERGENCY EXIT HATCH AT SEAT 12BC IAW AMM 33-50-14.

Part: TERMINAL BLOCK — DAMAGED (EMERGENCY LIGHTS) · airframe 38,743 hrs · 34,718 cycles

EMERGENCY LIGHT BETWEEN ROW 8 AND 9 IS INOP CENTER FLOOR LIGHT STRIP. REPAIRED WIRING AT TERMINAL BLOCK IAW SWPM 20-30-00 ON LIGHT STRIP FLOOR BETWEEN ROW 8 AND 9.

Part: WARNING BELL — FALSE ACTIVATION (CONFIGURATION) · airframe 37,785 hrs · 33,667 cycles

TRIPPLE CHIME TAKE OFF WARNING OBSERVED WITH A/C CONFIGURED NORMALLY. REJECTED TAKE OFF AND RETURNED TO GATE. R&R HSCU, IAW EMB 145 AMM 27-40-01. OPERATIONS CHECK GOOD, OK FOR SERVICE AT THIS TIME.

Part: A/C PACK — ODOR (NR 1) · airframe 37,361 hrs · 33,192 cycles

DURING PUSH BACK, WITH PACK 1 ON, SMOKE BEGIN TO ACCUMULATE IN THE COCKPIT. WAS ACCOMPANIED BY AN ELECTRICAL SMELL. SEEMED TO COME FROM FO SIDE. COULD NOT DUPLICATE PRESENCE OF WHITE SMOKE. FOUND NO VISUAL SIGN OF BURNING. NOTICED BURNING SMELL WITH PACK 1 ON. R & R NR 1 ACM IAW AMM 21-51-03. OPS CHECKED GOOD. NO PRESENCE OF BURNING SMELL. OK FOR SERVICE AT THIS TIME

Part: A/C PACK — ODOR · airframe 36,452 hrs · 32,157 cycles

PDIS 692 21-01 2094012 27OCT19 SYR CLOSE SMELL OF SMOKE ON DESCENT COMING FROM FO'S VENT. SM ELL WAS STRONGEST DURING HEAVY PRECIP. FACT 27OCT19 11:41 SYR INSPECTED AND FOUND A/C IN ELE BACKUP MODE. REMOVED ALL PWR FROM A/C. C/W TASK 24-60-00-810-820-A. CREW PWR'D UP A/C. ALL SYSTEMS CHECK NORMAL WITH NO ABNORMAL EICAS MSG'S. CREW GRD RAN BOTH ENG'S WITH NO ABNORMAL INDICATIONS. NO SMOKE OR FUME SMELLS. A/C OK FOR SERVICE. -PCS-

Part: INDICATION SYS — FALSE ACTIVATION (RT MLG) · airframe 45,983 hrs · 43,133 cycles

AFTER GEAR RETRACTION, A THUMPING NOISE, AND INTERMITTENT INDICATION FROM RT GEAR, FOR 10 SECONDS. AFTER 10 SECONDS EVERYTHING WAS NORMAL. CYCLED LANDING GEAR MULTIPLE TIMES WITH NO ISSUES, CONDUCTED PROXIMITY SWITCH FUNCTIONAL CHECK IAW 32-63-05. OPS CHECKED GOOD, NO FAULTS ON CMC DOWNLOAD, OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSER) · airframe 36,308 hrs · 31,990 cycles

SHORTLY AFTER TAKEOFF, THE L/G AIR GROUND FAIL MESSAGE DISPLAYED, FOLLOWED BY ENGINE 1/2 REVERSE DISAGREE MESSAGES. INSPECTED NOSE AND MAIN WOW SWITCHES, ALL PASSED ELECTRICAL CHECK. R & R RELAYS K0352, K0353, AND K0453, OPS CHECKED GOOD IAW AMM 32-63-05-05. OPERATED BOTH THRUST REVERSERS, NO EICAS MESSAGES, OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 36,266 hrs · 31,932 cycles

SPOILER FAIL MESSAGE ON TAXI OUT. FIX: T/S PER FIM 27-63-00-810-802-A. NO RELEVANT MESSAGES DISPLAYED AT THIS TIME. SUSPECT A TRANSITORY CONDITION. OK FOR SERVICE.

Part: RELAY — FAILED (SPOILER SYS) · airframe 36,266 hrs · 31,932 cycles

ON TAXI OUT, SPOILER FAIL EICAS MESSAGE. FIX: R&RD TWO RELAYS AND SPC UNIT, REF FIM TASK 27-63-00-810-806-1 AND AMM 27-63-02. TAXIED AIRCRAFT ABOVE 19 KNTS, NO SPOILER MESSAGE ON EICAS OR CMC. OPS CHECK GOOD. OK FOR SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 35,865 hrs · 31,457 cycles

EMERGENCY EXIT DIRECTION LIGHT ON WALL AT ROW3 INOP. FIX: R&RD EMERGENCY LIGHT SIGN.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 35,739 hrs · 31,318 cycles

EMERGENCY EXIT SIGN ON AFT SIDE OF GALLEY AFT BULKHEAD WAS INOPERATIVE. REMOVED THE EXIT SIGN, CLEANED THE WIRE CONNECTIONS AND REINSTALLED SIGN USING RETAINED HARDWARE,OPS CHECKED GOOD

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 35,557 hrs · 31,109 cycles

NDIS 692 33-51 0010370 09MAY19 SBY CLOSE EMERGENCY LIGHT ON BULKHEAD AT ROW 2 INOP 30155 00 SJU FACT 09MAY19 10:29 SBY REMOVED TRIM PANEL OF SAID EMERGENCY LIGHT RESEATED ELECTRICAL CONNECTOR OF SAID EMERGENCY LIGHT AND REINSTALLED TRIM PANEL USING RETAINED HARDWARE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 35,524 hrs · 31,075 cycles

PDIS 692 30-80 1877141 05MAY19 PHL CLOSE ICE CONDITION ON EICAS WITH NO ICING CONDITION, FOLLOWED BY WARNING MESSAGE A/I INOP. PERFORMED QRH PROCEDURE. HAPPENED 3 MORE TIMES THIRD TIME ON TAKE OFF. FACT 05MAY19 21:11 PHL T/S WITH FIM 30-80-00-810-801-A UP TO BLOCK17, FOUND TO BE TRANSITORY CONDITION OF ANTIICE SYSTEM. OPS CHECK ANTIICE SYSTEM IAW AMM 30-00-00 NO DEFECTS NOTED. OK FOR SERVICE.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 35,484 hrs · 31,025 cycles

NDIS 692 33-51 0010160 27APR19 RIC CLOSE EMERGENCY EXIT LIGHT IS FRONT OF SEAT 3B INOP 27625 00 BRA FACT 27APR19 10:27 RIC REMOVED EMERGENCY EXIT LIGHT IN FRONT OF SEAT 3B CLEANED CONNECTORS AND RESET LIGHT PERFORMED OPS CHECK OF LIGHT IN REF TO AMM 33-50-00-700-801A OPS CHECK GOOD. INSTALLED EMERGENCY EXIT LIGHT IN FRONT OF SEAT 3B IN REF TO AMM 33-50-14-800-801-A OP CHECK GOOD OK FOR SERVICE

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 35,070 hrs · 30,703 cycles

PDIS 692 22-10 1874591 10MAR19 PHL CLOSE UNCOMMANDED AUTO PILOT FAIL IN FLIGHT WITH ASSOC. EICAS MSGS FACT 10MAR19 08:20 PHL FUNCTIONAL TESTED AUTO PILOT AIW AMM 22-11-00-700-803-A FUNCTIONAL TEST GOOD WITH NO DEFECTS NOTED, OK FOR SERVICE AT THIS TIME.

Part: SENSOR — MALFUNCTIONED (BRAKE TEMP) · airframe 34,817 hrs · 30,283 cycles

DISCREPANCY: BRAKE HOT INDICATION AFTER T/O, EXTINGUISH AFTERLANDING ACTION TAKEN: MX ISOLATED TO #3 BRAKE TEMP SENSOR, R&R'D #3 BRAKE TEMP SENSOR IAW AMM 32-47-01.

Part: INDICATOR — INACCURATE (STBY ATTITUDE) · airframe 34,580 hrs · 30,001 cycles

PDIS 692 34-22 1640842 05NOV18 MDT CLOSE IN STRAIGHT AND LEVEL FLIGHT ISIS STAND BY ATTITUDE INDICATOR SHOWS BETWEEN 20-30 DEG NOSE UP PITCH AND 20 DEG OF RIGHT BANK FACT 06NOV18 01:31 MDT R/R INTEGRATED STANDBY INSTRUMENT IN REF TO EMB M/M 34-01-01. OPS CHECK AND LEAK CHECK GOOD A THIS TIME.

Part: CONTROL MODULE — FAULTY · airframe 34,550 hrs · 29,966 cycles

PDIS 692 33-51 1640791 30OCT18 TRI CLOSE EMERGENCY LIGHT NOT ARMED EICAS MSG DISPLAYED. PDPU AND CYCLED C/B'S AND SWITCHS WITH NO FIX. 24137 00 RNR FACT 30OCT18 16:21 CLT RNR UNIT CONTROL MODULE IAW AMM 33-21-01-04 OPS CHECK GOOD IAW AMM 33-21-01-05 A/C OK FOR SERVICE.

Part: PITOT TUBE — DENTED (NR 2) · airframe 34,099 hrs · 29,431 cycles

AIRSPEED DISAGREE AT APPROXIMATELY 30-40 KTS, DURING TAKEOFF ROLL. ABORTED TAKEOFF. PERFORMED AN ADC OPS CHECK IAW AMM 34-15-00. NO DEFECTS NOTED. FOUND A SLIGHT DENT AT THE 4 O'CLOCK POSITION ON THE NR.2 PITOT TUBE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,084 hrs · 29,414 cycles

LEFT EMERGENCY EXIT, EMERGENCY LIGHT WAS INOPERATIVE. R & R THE NR 4 INVERTER IAW AMM 33-50-11-04.

Part: FIREWALL — CRACKED (APU BAY) · airframe 33,152 hrs · 28,365 cycles

APU FIREWALL IS CRACKED APPROX .500 INCHES AT THE CANNON PLUG J0274 INBOARD UPPER MOUNT BOLT AND REINFORCEMENT CLIP ON FORWARD SIDE OF THE APU FIREWALL IS CRACKED .500 INCHES AT STRINGER 11R-C/A-REPAIRED FIREWALL IAW EO EM-53AD-1883 PART C STEP 9. AND REMOVED AND REPLACED REINFORCEMENT CLIP AT APU FIREWALL STRINGER 11R IAW SRM 51-40-02

Part: FITTING — DAMAGED (RT AILERON) · airframe 33,152 hrs · 28,365 cycles

DAMPNER FITTING ON THE RIGHT AILERON IS DAMAGED. REMOVED AND REPLACED THE DAMPNER FITTING IAW EO EM-27MR-112.

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · airframe 33,152 hrs · 28,365 cycles

CARGO DOOR SILL CORRODED AND MISSING PAINT AT THE PROTECTIVE PLATE ATTACHMENT HOLES FRAMES 64 - 68. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,152 hrs · 28,365 cycles

PAX DOOR FUSELAGE CUTOUT HAS A CRACKED "L" ANGLE AT FLOOR LEVEL, FRAME 17. CRACK IS APPROX 1/4 INCH IN LENGTH. REMOVED AND REPLACED PAX DOOR FUSELAGE LOWER "L" ANGLE AT FR 17 IAW SRM 51-40-02, AND CPM 51-21-05.

Part: SUPPORT BRACKET — CRACKED (CARGO BAY) · airframe 33,152 hrs · 28,365 cycles

CARGO DOOR HOLD OPEN ROD SUPPORT BRACKET IS CRACKED AT FRAME 68. BOTH UPPER AND LOWER ATTACHMENT POINTS APPROX 1/2" LONG EACH. R&R CARGO DOOR HOLD OPEN ROD SUPPORT BRACKET THAT WAS CRACKED AT FRAME 68. BOTH UPPER AND LOWER ATTACHMENT IAW SRM 51-40-02.

Part: SIDEWALL SUPPORT — DAMAGED (FRAMES 48-49) · airframe 33,152 hrs · 28,365 cycles

RT SIDE LATERAL SIDE PANEL SUPPORT HAS 2 RIVETS PULLED THRU. AND IS ALSO CRACKED APPROX. 2 INCHES BETWEEN FRAMES 48 AND 49. REPAIRED PANEL SUPPORT IAW SRM 53-23-12. REFERENCE E616435 FOR PAINT FINISH.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 33,152 hrs · 28,365 cycles

LATERAL SIDE PANEL, THIRD ONE AFT ATTACH L ANGLE ON RIGHT WING IS CRACKED APPROX. 2 INCHES. COMPLETED A REPAIR IAW ETN-EM-53-142.

Part: RIB — CRACKED (NLG WW) · airframe 33,152 hrs · 28,365 cycles

RIB IN THE NOSE WHEEL WELL ABOVE AND AFT OF THE UPLOCK BOX IS CRACKED APPROX 3 INCHES. REMOVED AND REPLACED RIB IN THE NOSE WHEEL WELL ABOVE AND AFT OF THE UPLOCK BOX IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 33,152 hrs · 28,365 cycles

LATERAL SIDE PANEL, FORTH ONE AFT, ATTACH ANGLE ON LEFT WING HAS TWO CRACKS 1.5 INCHES. INSTALLED A NEW ATTACH ANGLE IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRAME 61) · airframe 33,152 hrs · 28,365 cycles

FRAME 61 SHEAR TIE BETWEEN STRINGERS 6L AND 7L IS CRACKED .500 INCHES. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,152 hrs · 28,365 cycles

RT FRAME 80, SHEAR CLIP AT STRINGER 7 IS CRACKED APPROX 1/2". COMPLETED INSTALLATION OF RT FR 80 SHEAR CLIP AT STR 7 IAW SRM 51-40-02 AND CPM 51-21-06.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 33,152 hrs · 28,365 cycles

LT WING TO FUSELAGE UPPER SUPPORT IS CRACKED. COMPLETED REPAIR TO DAMAGED LT WING TO FUSELAGE SUPPORT IAW SRM 53-23-12

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 33,152 hrs · 28,365 cycles

LATERAL SIDE PANEL, MOST FWD ATTACH L ANGLE ON LEFT WING IS CRACKED APPROX .500 INCHES. PERFORMED REPAIR TO LATERAL SIDE PANEL MOST FWD ATTACH "L" ANGLE ON LT WING IAW ETN-EM-53-142.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 33,152 hrs · 28,365 cycles

FRAME 80, SHEAR TIE AT STRINGER 7L IS CRACKED .5 INCH. REPAIRED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.

Part: BUSHING — MIGRATED (RT AILERON) · airframe 33,152 hrs · 28,365 cycles

INBOARD ATTACH FITTING ON THE RIGHT AILERON HAS A MIGRATING HAT BUSHING. REMOVED REPLACED THE ATTACH FITTING IAW EO EM-27MR-112.

Part: NUT PLATE — TORN (RUDDER) · airframe 33,152 hrs · 28,365 cycles

RIGHT SIDE OF RUDDER ATTACH POINT NR 3 ACCESS PANEL NUT PLATE ATTACHMENT FITTING TORN. REMOVED AND REPLACED THE NUT PLATE IAW SRM 51-40-02.

Part: ENGINE — FAILED (LEFT) · airframe 33,150 hrs · 28,363 cycles

DURING DECENT AT 5000 FT, STARTED SMELLING OIL, ALSO DURING ENTIRE FLIGHT. CHECKED OIL PRESSURE, WENT FROM 63 LBS TO 88 FLUXUATION THE ENTIRE FLIGHT. AFTER DESELECTING THE NR 1 PACK. THE ODOR WENT AWAY. RESELECTED PACK AND ODOR CONTINUED. AT ALL OTHER ALTITUDES NO ODOR, JUST OIL PRESSURE ISSUE. REMOVED AND REPLACED THE LT ENGINE IAW WC 71-000-00 , PERFORMED NRWC 692-CMI-03269 FOR DUCT DECONTAMINATION AND ODOR EVENT. TROUBLESHOT COMPLIANCE IAW ETN-EM-72-034. OPS & LEAK CHECKED GOOD, NO ODOR NOTED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 33,149 hrs · 28,362 cycles

DECENDING THROUGH 11000, AN OIL ODOR, PACK 2 FAIL BLEED 2. PERFORMED OPS CHECK OF THE PACK 2 FOR TWO HOURS IAW AMM 21-51-01. OPS CHECKED GOOD. PERFORMED OPS CHECK OF BLEED 2 VALVE IAW AMM 36-11-05. OPS CHECKED GOOD. PERFORMED ETN-EM-72-034 FOR OIL ODOR IN COCKPIT. NO DEFECTS NOTED.

Part: ENGINE — ODOR · airframe 33,097 hrs · 28,313 cycles

LEVEL @ 16000' BOTH ACS ON BUILDING CHEMICAL LIKE SMELL WAS DETECTED BY BOTH FLIGHT CREW MEMBERS AND ALSO THE F/A WHEN SHE CAME TO THE FORWARD CABIN. THE SMELL WAS IRRITATING TO THE THROAT. "TRANSFERRED TO NRWC 692-CMI-03243"-C/A-TRANSFERRED FROM NRWC 692-CMI-03243 FOUND ODOR EVENT TO BE CAUSED BY RESIDUAL GLYCOL INGESTION INTO L/H ENG, AFTER CLEANING L/H ENG INLET AND PERFORMING SATISFACTORY ETN-EM-72-034 WITH NO ODORS PRESENT TRIAD GROUP APPROVES RETURN TO SERVICE OF THIS A/C - END PERFORMED ETN-EM-72-034. ODOR APPEARS TO BE COMING FROM ENGINE #1. STRONGEST ODOR NOTICED WHILE OPERATING PACK 1 OFF OF #1 ENGINE BLEED BUT DISSIPATED THROUGHOUT THE DURATION OF THE HIGH POWER ENGINE RUN. HAD TO STOP ENGINE RUNS AFTER STEP 6 TO HAVE MORE FUEL PUT ON TO CONTINUE RUNS. WHILE WAITING FOR REFUELING, INSPECTED ENGINE 1 INLET AREA AND FOUND WHAT APPEARED TO BE GLYCOL WICKING FROM THE ACOUSTIC LINER OF THE INTAKE. THE BOTTOM OF THE INTAKE WAS VERY WET. AFTER FUELING, THE REMAINDER OF THE REQUIRED ENGINE RUNS WERE COMPLETED AND SMELLS SEEMED TO DISSIPATE THROUGHOUT THE RUNS. INSPECTED THE #1 INLET AGAIN AND FOUND IT TO BE CONSIDERABLY DRIER THAN PREVIOUSLY NOTED. SUSPECT ODOR EVENT WAS CAUSED BY GLYCOL WICKING FROM THE INTAKE ACOUSTIC LINER AND BEING SUCKED INTO THE INLET OF THE ENGINE. SUGGEST PERFORMING ETN-EM-72-034 AGAIN TO SEE IF NO FURTHER SMELLS ARE NOTED. PER GENERAL MAINTNENANCE KNOWLEDGE CLEANED INTAKE BEFORE PERFORMING RUNS, C/W ETN-EM-72-034 FOR SECOND TIME FOUND N

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,595 hrs · 27,855 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. R & R THE BULB IAW AMM 33-50-05-000-801-A, AND 33-50-05-400-801-A. OPS CHECKED GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 31,549 hrs · 26,883 cycles

EMERGENCY LIGHTS AT LT FWD WING TO FUSELAGE AND ISLE LIGHT ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY, OPS CHECKED GOOD IAW AMM 33-50-04.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,452 hrs · 26,805 cycles

RIGHT FWD WING TO FUSELAGE FAIRING EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-10-000-801, AND 33-50-10-400-801. OPS CHECKED GOOD.

Part: HOSE — SPLIT (LANDING GEAR) · airframe 31,261 hrs · 26,634 cycles

ON DEPARTURE THE GEAR DID NOT RETRACT AND CREW RECEIVED HYD SYS 1 FAIL MESSAGE. CREW COMPLIED WITH AOL VOL1 PROCEDURES, DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. FOUND LT GEAR ACTUATOR RETRACT HOSE SPLIT. REMOVED AND REPLACED RETRACT HOSE IAW EMB AMM 32-33-08. LEAK CHECKED GOOD. REF ITEM 2 THIS LOG PAGE FOR GEAR SWING. FOUND PRESSURE HOSE FROM ENGINE DRIVEN PUMP SPLIT. RAR HOSE IAW EMB AMM 29-10-03. OPS CHECK GOOD. LEAK CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 31,204 hrs · 26,589 cycles

AFT CABIN FLASHLIGHT INOP. REMOVED AND REPLACED AFT CABIN FLASHLIGHT IN REF TO AMM 33-50-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,953 hrs · 26,376 cycles

SERVICE DOOR CEILING EMERGENCY LT INOP. R&R SERVICE DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-09-000-801-A & 33-50-09-400-801-A. OPS CHECK GOOD AT THIS TIME.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT) · airframe 30,825 hrs · 26,241 cycles

FOUND REAR LT DOOR EMERGENCY EXIT SIGN INOPERATIVE DURING PS-1 CHECK. REMOVED AND REPLACED THE SIGN IAW AMM 33-50-13. OPS CHECKED GOOD.

Part: ANTENNA — DAMAGED (RADAR ALTIMETER) · airframe 30,485 hrs · 25,890 cycles

RADIO ALTIMETER FAILED AT GATE. REMOVED AND REPLACED BOTH RADAR ALTIMETER ANTENNAS IAW AMM 34-31-02. RADIO ALTIMETER SYS. OPS TESTED GOOD IAW AMM 34-31-00.

Part: PRESSURE SWITCH — FAILED (BLEED AIR SYS) · airframe 30,359 hrs · 25,781 cycles

CLIMB THROUGH 7,000' WE GOT RED WARNING E2 BLEED LEAK, RAN EPC CHECKLIST ISOLATED AND LANDED. FOUND NR 2 ENGINE HIGH STAGE VALVE PRESSURE SWITCH BROKEN. REPLACED NR 2 ENGINE HIGH STAGE VALVE PRESSURE SWITCH IAW AMM 36-11-07-400-801-A. OPS CHECK SATISFACTORY IAW AMM 36-11-07-700-801-A.

Part: GPWS — UNKNOWN (COCKPIT) · airframe 29,677 hrs · 25,130 cycles

MECHANICS GPWS FAIL. WINDSHEAR INOPERATIVE DUE TO MEL 34-21. OPERATIONS CHECK OF GPWS GOOD IAW AML 4008481 ITEM 3. MEL RESTORED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 29,421 hrs · 24,922 cycles

LEFT WING FWD FAIRING EXTERNAL EMER LIGHT INOPERATIVE. R & R BT8500 NR 1 BATTERY POWER SUPPLY. OPERATES OK IAW AMM 33-50-04.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,313 hrs · 24,815 cycles

LEFT FWD EMER LIGHT INOPERATIVE. R & R NR 1 EMER BATTERY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD ON LT FWD EMER BATTERY. EMER LIGHT BATTERY PN 2013-1A & SN 124556.

Part: SKIN — DENTED (LT HORIZ STAB) · airframe 28,774 hrs · 24,333 cycles

ORIGINAL LOG PAGE 3700827-TDMI 692T5514. FIRST OFFICERS NOTICED DENT ON LT HORIZONTAL STAB. PERFORMED MAJOR REPAIR TO LT HORIZONTAL STABILIZER IAW ERS-EM-55MR-395 PART A. REF AML PAGE 3932954 ITEM 3 TDMI ITEM RESTORED.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 28,774 hrs · 24,333 cycles

RIGHT OVERWING PAX ESCAPE HATCH BOTTOM FRAME IS CORRODED. R & R BEAM NR 4, BOTTOM FRAME, IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 28,774 hrs · 24,333 cycles

SHEAR CLIP AT FRAME 62, BETWEEN STRINGER 4R & 5R IS CRACKED. REPLACED SHEAR CLIP IAW SRM 51-40-02.

Part: MOUNT BRACKET — CRACKED (RT WING) · airframe 28,774 hrs · 24,333 cycles

RIGHT WING FUEL TANK VENT PIPE NEAR RIB 3 HAS 2 EACH CRACKED MOUNT BRACKETS. REMOVED BROKEN BRACKETS ON REFUEL PIPE AT RIB 3 IN RT WING & REPLACED WITH NEW UNITS IAW AMM 20-10-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,774 hrs · 24,333 cycles

CRACK LIKE INDICATION NOTED ON THE RT SIDE EXTERIOR SKIN AT FRAME 75, ABOVE STRINGER 2R APPROX .75 " IN LENGTH. REPAIRED CRACK AT FRAME 75, ABOVE STRINGER 2R IAW ERS-EM-53MR-1826.

Part: HINGE FITTING — WORN (RUDDER) · airframe 28,774 hrs · 24,333 cycles

RUDDER NR 2 LOWER HINGE FITTING BORES ARE WORN. R & R FITTING IAW SRM 55-40-02 & ETN EM-55-070.

Part: DOOR FRAME — CRACKED (ACCESS DOOR) · airframe 28,774 hrs · 24,333 cycles

MAINTENANCE DOOR FRAME IS CRACKED AT FWD OTBD CORNER. REPLACED DOOR FRAME IAW SRM 51-40-02.

Part: HINGE FITTING — WORN (RUDDER) · airframe 28,774 hrs · 24,333 cycles

RUDDER NR 2 UPPER HINGE FITTING BORES ARE WORN. R & R FITTING IAW SRM 55-40-02 & ETN EM-55-070.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 28,774 hrs · 24,333 cycles

RIGHT OMEGA BEAM SUPPORT ANGLE IS CRACKED, BETWEEN FRAMES 47 & 48. RT INBD SIDE OF THE OMEGA BEAM. REPAIRED IAW SRM 53-23-02 & SRM 51-40-02.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 28,255 hrs · 23,822 cycles

AFT CABIN EMER FLASHLIGHT CRADLE BROKEN. R & R AFT CABIN EMER FLASHLIGHT CRADLE IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: DOOR — BROKEN (ESCAPE ROPE) · airframe 27,579 hrs · 23,150 cycles

FIRST OFFICER`S ESCAPE ROPE DOOR BROKEN. R & R FIRST OFFICER`S ESCAPE ROPE HATCH IAW 20-10-00.

Part: PITOT SYSTEM — CONTAMINATED (LT & RT) · airframe 27,358 hrs · 22,964 cycles

IAS COMPARATOR CAUTIONS ON PFD'S LOSS OF 10 KTS ON CAPTAINS SIDE WITH GAIN OF 15KTS. FIRST OFFICERS IAS LOST AIRSPEED. BOTH CAPTAIN & FIRST OFFICER AIRSPEED BEGAN TO DECREASE. ACFT WAS IMC AT FL 370, SAT -55. ACFT ANTI-ICING WAS SELECTED TO ALL. AIRSPEED INDICATIONS CONTINUED TO DECREASE. CLEANED LT & RT PITOT MAST MOISTURE DRAINS & DRAINED WATER FROM P1 & P2 LOW POINT DRAINS. NR 1 & 2 ADC'S OPERATIONS CHECKED OK IAW AMM CH 34-15-00.

Part: HOLDER — DEFECTIVE (FLASHLIGHT) · airframe 26,553 hrs · 22,251 cycles

CAPTAIN`S FLASHLIGHT HOLDER WON’T HOLD THE FLASH LIGHT. R & R CAPTAIN`S FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECK IS GOOD.

Part: HOLDER — LOOSE (FLASHLIGHT) · airframe 26,552 hrs · 22,250 cycles

CAPTAIN`S FLASHLIGHT HOLDER ATTACHMENT IS LOOSE, FLASHLIGHT FALLS OUT. DEFERRED CAPTAIN`S FLASH LIGHT IAW MEL 25-53. R & R CAPTAIN`S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. REF NRWC 692-XNA-01828. MEL RESTORED.

Part: TRANSDUCER — FAULTY (ANTI-ICE SYSTEM) · airframe 26,382 hrs · 22,122 cycles

IAW MEL 30-11, OPEN INSCRIPTION ON ENG AIR INLET BUTTON SHOULD REMAIN OPEN WHENEVER ENGINE IS RUNNING, ON CLIMB OUT THE OPEN WENT AWAY. R & R ENG ANTI-ICE NR 1 PRESS TRANSDUCER/. OPERATIONS CHECKED GOOD IAW AMM 30-21-06. OPERATIONS CHECKED OK IAW ER 30-00-00.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 25,978 hrs · 21,706 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR IS HARD TO OPEN & CLOSE MAY NEED LUBRICATION. ACCOMPLISHED LUBE OF MAIN CABIN DOOR IAW SMP. OPERATIONS CHECKED GOOD.

Part: COUPLING — DEFECTIVE (AC BAY) · airframe 25,484 hrs · 21,271 cycles

DURING CLIMB OUT AT ABOUT 20,000 FT RECEIVED BLD 2 LEAK EICAS MSG THAT WAS ABOUT 5*C. AFTER COMPLETING AOM 1 PROCEDURES, THE MSG EXTINGUISHED. R & R BOTH AFT BIG & SMALL DTCV COUPLINGS ON RT PACK SYS IAW AMM 21-60-01. LEAK CHECK & OPERATIONS CHECKED GOOD. ALSO NRWC 692-ORD-01647. PERFORMED AIR BLEED SYS OPERATIONS CHECK IAW AMM 36-00-00-700-803A, OPERATIONS CHECKED GOOD. R & R AFT V BAND CLAMP OF RT PACK VLV IAW AMM 20-10-10 USING THE TORQUE SPECIFIED IN AMM 21-51-01. LEAK CHECKED GOOD

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 25,482 hrs · 21,269 cycles

WHILE IN ROUTE GOT BLD 2 LEAK. R & R O RINGS IN COUPLING NR 20 IN LWR REAR OF BAGGAGE IAW 36-11-10. OPERATIONS CHECKED GOOD, NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,354 hrs · 20,308 cycles

DURING NR 2 ENG BLEED AIR OPERATION CHECK, SMOKE NOTICED IN THE CABIN WITH STRONG ODOR. RAN ENGS FOR 30 MINUTES AT 90 PERCENT IAW GHC-10-13 WITH AIR GND CBS PULLED, NO ODOR NOTED. SUSPECT THAT THE SMELL WAS FROM THE NEWLY INSTALLED BLEED AIR O RINGS. NIGHT SHIFT TURNOVER STATED THAT THE SMELL DISSIPATED BEFORE ENG RUNS WERE COMPLETED BY THEM LAST NIGHT. OPERATIONS CHECKED GOOD.

Part: LIGHT — INTERMITTENT (RT OVERWING) · airframe 23,940 hrs · 19,987 cycles

RT OVERWING EMERGENCY LIGHT INTERMITTENT. R & R EMERGENCY LIGHT ASSY IAW MM 33-50-10. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 23,828 hrs · 19,894 cycles

F/A AFT FLASHLIGHT INOPERATIVE. R & R AFT FLASHLIGHT ASSY IAW AMM 33-50-16, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR)

LEFT AFT EXTERIOR OVERWING EMERGENCY LIGHT INOP. REPLACED LEFT AFT EXTERIOR OVERWING EMERGENCY LIGHT LAMP.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,371 hrs · 17,885 cycles

DURING B INSPECTION FOUND THE RIGHT OVER WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT CHARGER AND BATTERY IAW EMB W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,371 hrs · 17,885 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 ASSEMBLY IAW EMB AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GRIP — OUT OF ADJUST (CABIN DOOR) · airframe 21,336 hrs · 17,856 cycles

ON FLIGHT 3322 THE CREW REPORTED THE MAIN CABIN DOOR HANDLE GRIP CAME OFF MAKING IT DIFFICULT TO OPERATE. DEFERRED MAIN DOOR RUBBER HANDGRIP IAW CDL 52-1, AUTH. NO.111334CDL-D. NO DEFECTS NOTED WITH DOOR OPERATION WITH GRIP FULLY REMOVED. INSTALLED MAIN DOOR HAND GRIP AS REQUIRED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,327 hrs · 17,847 cycles

DURING B INSPECTION FOUND THE RIGHT AND LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY POWER SUPPLY AND BATTERY HOLDER ASSEMBLY IAW EMB145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,300 hrs · 17,822 cycles

DURING B INSPECTION FOUND THE EXTERIOR AFT OVERWING EMEGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHTS BATTERY AND CHARGER ASSEMBLY IAW EMB145 MTX W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,006 hrs · 17,599 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY AND CHARGER IAW AMM 33-50-04. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 20,780 hrs · 17,425 cycles

DURING B INSPECTION FOUND THE LOWER SERVICE DOOR AND FIRST FLOOR STRIP EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 INVERTER IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD IAW W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,280 hrs · 17,017 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LEFT AND RIGHT EXTERIOR LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CORRODED (RT ENGINE) · corrosion level 2 · airframe 19,736 hrs · 16,625 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT ENGINE FRONT FRAME FORWARD FLANGE HAS MULTIPLE ENLARGED FLANGE HOLES DUE TO EXCESIVE CORROSION. ENGINE REQUIRES CHANGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT ENGINE IAW W/C 71-000-00. THE OPERATIONAL CHECK WAS GOOD, NO LEAKS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 19,669 hrs · 16,567 cycles

DURING B-INSPECTION FOUND THE RIGHT WINDSCREEN EMERGENCY EXIT LOCATOR LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — DISCONNECTED (CABIN) · airframe 19,648 hrs · 16,544 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RECONNECTED EMERGENCY EXIT SIGN IAW EMB 145 AMM 33-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (E&E DOOR) · airframe 19,647 hrs · 16,543 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT AVIONICS DOOR 272DR IS CRACKED UNDER HANGER BRACKET. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED AFT AVIONICS DOOR 272DR IAW EO EM-52MR-309. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 19,648 hrs · 16,544 cycles

DURING B-INSPECTION FOUND THE NR 1, 4, 5 AND 6 FLOOR PROXIMITY LIGHT STRIP WIRING DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERIVCE. REPAIRED THE NR 1 BROKEN WIRE, IAW EMB 145 SWPM 20-21-00 AND SWPM 20-50-00. REMOVED AND REPLACED THE NR 4, 5 AND 6 PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 19,647 hrs · 16,543 cycles

FRAME DAMAGED. REPAIRED FRAME 68 LT HALF IAW EO EM-53MR-1590, PART B.

Part: FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 19,647 hrs · 16,543 cycles

CARGO BAY FRAME 68 IS CORRODED AT LOWER END. REPAIRED FRAME 68 IAW AE EO EM-53MR-1129, PART B.

Part: FRAME — CORRODED (CARGO BAY) · airframe 19,647 hrs · 16,543 cycles

DURING HEAVY CHECK, FOUND CARGO FRAME 65 CORRODED AT LOWER END. REPAIRED FRAME IAW AE EO EM-53MR-1129, PART A.

Part: WIRE — BROKEN (CABIN) · airframe 19,648 hrs · 16,544 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP MOST AFT WIRE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT AFT EMERGENCY LIGHT WIRE IAW EMB 145 SWPM 20-21-00 AND EMB 145 SWPM 20-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRIM PANEL — DAMAGED (CABIN) · airframe 19,648 hrs · 16,544 cycles

DURING B-INSPECTION FOUND THE NR 1, 3, 5 AND 6 AISLE LEFT FLOOR PROXIMITY LIGHT TRIM EXTRUSIONS DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1, 3, 5 AND 6 LEFT FLOOR PROXIMITY LIGHT TRIM EXTRUSIONS IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PLUG — DEFECTIVE (NR 1 ENGINE) · airframe 19,490 hrs · 16,427 cycles

ON FLIGHT 4201 THE CREW REPORTED SMOKE COMING OUT OF EXHAUST ON SHUT DOWN OF NR 1 ENGINE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 ENGINE SHAFT PLUG IAW RR MM 72-59-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — DIRTY (CARGO DOOR) · airframe 17,813 hrs · 15,193 cycles

HIGH SPEED ABORT TAKEOFF FOR BAG DOOR OPEN WARNING INDICATION ON EICAS. CLEANED AND LUBED MICROSWITCHES.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 17,301 hrs · 14,843 cycles

ON FLIGHT 2840 ON THE FINAL APPROACH THE CREW REPORTED A FUEL ODOR IN THE COCKPIT. THE FUEL TANK 2 QUANTITY ON EICAS AND THE MULTI FUNCTION DISPLAY SHOWED AMBER DASHES UNTIL GATE ARRIVAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE SYSTEMS WERE FOUND TO BE WORKING GOOD AND UNABLE TO DUPLICATE THE PROBLEM IAW 28-40. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 17,030 hrs · 14,655 cycles

ON FLIGHT 4237 THE CREW NOTICED THE FORWARD CABIN EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND LOOSE CONNECTIONS SP9220 & SP9223 SECURED IAW EMB WM 20-50-00 EMERGENCY LIGHTS OPERATIONAL CHECK GOOD IAW EMB-145 M/M 33-50-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 15,830 hrs · 13,801 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE FORWARD EMERGENCY CEILING LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 EMERGENCY LIGHT DC/AC INVERTER IAW EMB AMM 33-50-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 14,864 hrs · 13,061 cycles

DURING MAINTENANCE BASE VISIT FOUND THE INTERIOR EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY EXIT SIGN ASSEMBLY IAW EMB 145 AMM 33-50-15. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (RT MLG) · airframe 13,399 hrs · 11,887 cycles

ON FLIGHT 3267 UPON LANDING THE TOWER REPORTED SEEING SMOKE TRAIL FROM THE RIGHT MAIN LANDING GEAR WHILE EXITING THE RUNWAY. CRASH, FIRE AND RESCUE FOLLOWED THE AIRCRAFT TO THE GATE. NO INCIDENT HAPPENED AT THE GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED THE RIGHT MAIN LANDING GEAR. NO LEAKS OR DEFECTS WERE NOTED IAW EMB AMM 32-10-02 AND 32-49-02. NO PARTS WERE REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DISPLAY — INOPERATIVE (COCKPIT) · airframe 13,209 hrs · 11,738 cycles

CAPTAIN REPORTED THAT RIGHT AFTER TAKEOFF THE MULTI FUNCTION DISPLAY UNIT WENT BLANK. NO ASSOCIATED EICAS MESSAGES FOLLOWED. A MOMENTARY BURNING SMELL WAS REPORTED. THE CREW ELECTED TO RETURN TO DEPARTURE. THE ACFT LANDED WITHOUT INCIDENT. ACFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S MULTI FUNCTION DISPLAY UNIT IAW AMM 34-22-01. OPS CHECKS WERE GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 11,462 hrs · 10,224 cycles

ON FLIGHT 3986, ON GROUND MAINTENANCE REPORTED EMERGENCY EXIT SIGN OVER FLIGHT ATTENDANTS SEAT WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT IAW AMM 33-15-14. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FR 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. PREPARED A DOUBLER, FILLLER, TWO SHIMS AND BACK PLATE. CLEANED AND TREATED ALL REPAIR PARTS. REPAIR DONE IAW EMB 145 SRM (SRM EMB-145/1142 REV 40) CHAPTER 53-00-10 FIGURE 201. ACFT RETURNED TO SERVICE. (S)

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 6,870 hrs · 6,134 cycles

EMERGENCY EXIT LIGHT OVER FLIGHT ATTENDANT SEAT BURNED OUT. RESCURED NUMBER ONE AC/DC INVERTER CONNECTOR IAW EMB AMM. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED CORROSION BY MAKING A CUTOUT. PREPARED A DOUBLER, FILLER, PLATE AND SHIMS. REPAIR DONE IAW EMB SRM (145/1142 REV 34) CHAPTER 53-00-10, FIG 201 SHEET 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED THE AREA TO REMOVE CORROSION AND PERFORMED NDT INSPECTION WITH NO REJECT ABLE INDICATIONS. CLEANED AND TREATED THE BLENDED AREA INCLUDING TOP COAT. FABRICATED 3 DOUBLERS, REPAIR DONE IAW EMB SRM (145/1142 REV 34) CHAPTERS 53-53-21-02 FIG 2 AND EMB IC2006-145/6943. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — LEAKING (RT ENGINE)

CREW REPORTED SHORTLY AFTER ROTATION, RECEIVED A LAV SMOKE LIGHT AND RETURNED TO FIELD. RAI NUMBER 2 ENGINE. (M)

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY)

AFTER TAKEOFF CREW REPORTED A LAVATORY SMOKE INDICATION. FLIGHT ATTENDANT FOUND LAVATORY HAZY AND THE LIGHT WAS INOPERATIVE. REPLACED LAVATORY SMOKE DETECTOR AND PERFORMED CHECK FLIGHT. PASSED CHECK FLIGHT AND TRIAD RELEASED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WARNING LIGHT — FALSE ACTIVATION (LAVATORY)

LAVATORY SMOKE EICAS MESSAGE ILLUMINATED AFTER TAKEOFF. FOUND BLUE WATER SPILL ON BLEED DUCT IN LAVATORY. CLEANED BLUE WATER SPILL AND PERFORMED OPERATIONAL CHECK OF AIR CONDITIONING SYSTEM. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DISCREPANCIES NOTED. AC RETURNED TO SERVICE. (K)