N691AE

Part: DAU — ABNORMAL (ZONE 200) · airframe 45,948 hrs · 43,026 cycles

ON T/O ROLL #2 ENG REV DISAGREE MSG DISPLAYED--STOWED E2 TR AS REQUIRED MEL 11NOV25 12:50 ALB C31507 78-2 ENG 1 OR 2 REV DISAGREE MESSAGES. RAR #2 DAU IAW AMM 31-41-01. OPS CHECK GOOD. CLEAR MEL

Part: FLAP SYSTEM — ABNORMAL (ZONE 600)

EVAL FLIGHT UNSATISFACTORY DUE TO "FLAP FAIL" EICAS MESSAGE DURING FINAL APPROACH WHEN TRANSITIONING FLAPS FROM 22 DEG TO 45 DEG. STUCK AT 36 DEG. MX HEARD GRINDING NOISE FROM RH FTB AND FFS OUTBOARD OF FTB. R+R FTB IAW AMM 27-51-01

Part: CONTROL UNIT — FAULTED (ZONE 200)

SPOILER OPEN INDICATION IN CRUISE FLIGHT FOLLOWED BY SPOILER FAIL EICAS MESSAGE. C/E FLIGHT CREW PROCEDURE. MESSAGE REMAINED UNTIL GEAR WAS EXTENDED. FACT 25OCT25 15:40 PHL COMPLIED WITH SB145-27-0121 & R&R SPOILER CONTROL UNIT IRW AMM 27-63-02. OPS CHECK GOOD.

Part: BEARING CAP — CORRODED (ZONE 700) · corrosion level 2 · airframe 45,920 hrs · 41,922 cycles

F072285 RH MAIN LANDING GEAR LEG AFT BEARING CAP IS CORRODED. RH MAIN LANDING GEAR LEG AFT BEARING CAP IS CORRODED

Part: STRINGER — CRACKED (ZONE 200) · airframe 45,920 hrs · 41,992 cycles

F072376 STRINGER 6R IS CRACKED AT FRAME 14. RAR STRINGER 6R AT FRAME 14 IAW EMB 145 SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,920 hrs · 41,992 cycles

F072027 FR 61 SHEAR CLIP AT STR 7L HAS POSSIBLE CRACK. RAR SHEAR CLIP ON FRAME 61 AT STR 7L IAW EMB-145 SRM 51-40-02.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,920 hrs · 42,992 cycles

CORROSION ON CARGO DOOR CUT-OUT LOWER SILL. RAR CARGO DOOR CUT-OUT LOWER SILL IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,920 hrs · 42,992 cycles

F072008 LAV LH OTBD FLOOR SILL AFT END HAS 1 SPOT OF CORROSION. REMOVED & REPLACED LAV LH OTBD FLOOR SILL IAW EMB-145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,920 hrs · 41,992 cycles

F072219 LH UPPER #2 SEAT TRACK HAS CORROSION IN MULTIPLE AREAS. RAR LH UPPER #2 SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,920 hrs · 42,992 cycles

F072070 CORROSION ON LH OTBD #1 SEAT TRACK. REMOVED AND REPLACED LH OTBD #1 SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,920 hrs · 41,992 cycles

F072225 LH FLOOR SILL #3 HAS CORROSION IN MULTIPLE AREAS. RAR LH FLOOR SILL #3 IAW EMB 145 SRM 51-40-02.

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 45,920 hrs · 41,992 cycles

F070244 VERTICAL STABILIZER LH DRAG ANGLE HAS POSSIBLE CRACK AT FR 76. RAR VERTICAL STABILIZER LH DRAG ANGLE AT FR 76. IAW EMB 145 SRM 53-31-01RE DET B FIG 219 SH1 AND SRM 51-40-02.

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 45,920 hrs · 41,992 cycles

F070245 VERTICAL STABILIZER RH DRAG ANGLE HAS POSSIBLE CRACK AT FR 76. REPAIRED VERTICAL STABILIZER RH DRAG ANGLE AT FR 76. IAW EMB 145 SRM 53-31-01RE DET B FIG 219 SH1 AND SRM 51-40-02.

Part: STRUCTURE — CORRODED (RT MLG WW) · corrosion level 2 · airframe 45,920 hrs · 42,992 cycles

F069855 RH MLG BAY LOWER SKIN FWD OF MAIN SIDE BRACE AT SPAR II HAS CORROSION, BLENDED AREA ON RH MLG BAY. DAMAGE ACCEPTED AS IS IAW ETD2025-145-928499 AND PIEDMONT EO1-05-25-0363.

Part: STRUCTURE — CORRODED (LT MLG WW) · corrosion level 2 · airframe 45,920 hrs · 42,992 cycles

F069854 LH MLG BAY LOWER SKIN FWD OF MAIN SIDE BRACE AT SPAR II INTERNAL HAS CORRODED AREA. RAR LH MLG BAY LOWER SKIN FWD OF MAIN SIDE BRACE AT SPAR II IAW EMB 145 SRM 51-40-02.

Part: SKIN — DENTED (ZONE 100) · airframe 45,920 hrs · 410,992 cycles

F069895 FUSELAGE EXTERNAL SKIN HAS A PROTRUSION BETWEEN FR 77/80 STR 18R/19R. INSTALLED FABRICATED REPAIR DOUBLER AND FILLER ON FUSELAGE EXTERNAL SKIN BETWEEN FR. 77-80, STRG. 18R-19R IAW ETD2025-145-928508 AND PIEDMONT EO1-05-25-0363.

Part: CONTACTOR — BURNED (FAN) · airframe 45,456 hrs · 42,476 cycles

ELECTRICAL -SOLDERING SMELL IN PASSENGER DOOR/FLIGHT DECK DOOR AREA OF AIRCRAFT. INSPECTED AND FOUND RECIRC FAN 2 CONTACTOR K0190 AND RING TERMINAL OF W746-0239-10 TO BE SCORCHED. RAR CONTACTOR AND RIN TERMINAL REFERING TO SWPM 20-21-00 AND AMM21-24-03-000/400-801A

Part: RADIO ALTIMETER — ABNORMAL (ZONE 100) · airframe 45,024 hrs · 41,973 cycles

ON DESCENT FROM 15,000FT HAD MULTIPLE CONSTANT GPWS CALL OUT S THAT WOULD NOT STOP. DID NOT CLEAR UNTIL ROUGHLY 2,000FT WITH GEAR DOWN. FACT 16MAR25 14:21 PHL REMOVED AND REPLACED RADIO ALTIMETER IAW AMM 34-31-01. OPS CHECK GOOD. A/C OK FOR SERVICE

Part: RADIO ALTIMETER — ABNORMAL (ZONE 100) · airframe 45,024 hrs · 41,973 cycles

ON DESCENT FROM 15,000FT HAD MULTIPLE CONSTANT GPWS CALLS OUT THAT WOULD NOT STOP. DID NOT CLEAR UNTIL ROUGHLY 2,000FT WITH GEAR DOWN. FACT 16MAR25 14:21 PHL REMOVED AND REPLACED RADIO ALTIMETER IAW AMM 34-31-01. OPS CHECK GOOD. A/C OK FOR SERVICE

Part: CONTROL VALVE — ABNORMAL (ZONE 400) · airframe 44,944 hrs · 41,892 cycles

BLD 2 VLV FAIL MSG ON EICAS ON T/O ROLL FACT 01MAR25 17:18 CLT R/R NO.2 BLD VLV IRT AMM 36-11-05 OPS CHECK GOOD OK FOR SERVICE

Part: UNKNOWN — ODOR (CABIN) · airframe 44,830 hrs · 41,768 cycles

IN CRUISE FLIGHT CREW HAD BURNING SMELL IN FLIGHT DECK IN CABIN WITH PACKS RUNNING. FACT 08FEB25 20:51 PHL PERFORMED PACK 1 AND 2 TEST ON THE APU BLEED SYSTEM AND ENG 1 AND 2 IN REF TO MX GROUND RUN UP CHECKLIST ON IDLE. NO ABNORMAL SMELLS NOTED DURING TEST. OK FOR SERVICE AT THIS TIME.

Part: DAU — FAULTED (THRUST REVERSERS) · airframe 44,542 hrs · 41,460 cycles

E1 REV DISAGREE ON TAKE OFF ROLL. ENG 1 OR 2 REV DISAGREE MESSAGES. TROUBLESHOT IAW FIM TASK 78-30-00-810-802A, FOUND DAU 2 WITH NO CONTINUITY BETWEEN PIN A-36 TO A/C GROUND. R&R DAU 2 IAW AMM 31-41-01, OPS CHECK GOOD, CLEAR MEL 78-2. RE-ACTIVATED #100 T/R IAW AMM 78-31-01.

Part: THRUST REVERSER — INTERMITTENT (ZONE 400) · airframe 44,498 hrs · 41,415 cycles

E1 REV DISAGREE INTERMITTENT ON TAXI AND WITH TAKEOFF THRUST MEL 13DEC24 08:56 ALB C34809 78-2 ENG 1(2) REV DISAGREE MESS H T.O. THRUST DFRL 15DEC24 03:39 PHL REACTIVATED #1 T/R, INSPECTED MICRO SWITCHES AND CANON PLUGS, NO DEFECTS NOTED. ACTVATED #1 T/R SEVERAL TIMES IAW AMM 78-31-01-700-801-A. CND MESSAGE. DEACTIVATED AND STOWED #100 T/R. RETAIN MEL 78-2. TRANSCRIBED TO LP 345343-1 FACT 18DEC24 06:17 SBY RIGGED BOTH UPPER AND BOTH LOWER STOW SWITCHES IAW 145 AMM 78-31-01. REACTIVATED #100 T/R PLUGS INSTALLED. BOLTS STOWED. RAN AT POWER AND TAXIED AIRCRAFT. OPS CHECK GOOD. CLEAR MEL 78-2

Part: CLAMP — LOOSE (BLEED SYSTEM) · airframe 43,514 hrs · 40,271 cycles

BLEED 1 VALVE FAIL MFD MESSAGE ON TAKE OFF ROLL. FOUND BROKEN WIRE ON BLD 1 PUSH BUTTON ON A/C PANEL R & R PANEL PER AMM 20-13-10 NO FIX. R/R'D RELAY K0537 PER STANDARD PROC. NO FIX. INSPECTED NR 1 ENGINE BLEED DUCTS AND FOUND THE CLAMPS SECURING THE CHECK VALVES IN PLACE LOOSE & GASKETS INCORRECTLY PLACED CAUSING LEAKS. REPLACED THE GASKETS & RETORQUED THE CLAMPS IAW 361101. LEAK CHECKED GOOD, OPS CHECKED BLEED VALVE, NO DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,377 hrs · 39,018 cycles

IN CRUISE FLIGHT AT ABOUT 24K, FLIGHT DECK HAD SMOKE ACCUMULATION FROM DUCTS NEAR DV WINDOWS ON BOTH SIDES. MASKS WERE PUT ON, NO LOSS OF PRESSURIZATION, SMOKE STARTED TO DISAPATE, STARTED DESCENT AND SELECTED DUMP. FACT 09NOV23 03:37 BHM INSPECTED AND FOUND PACK 1 AT FAULT. #1 ACM IS SWELLED OUT AND LOCKED UP. SEE 306033-3 FOR #1 ACM WRITE UP AND MEL INFO

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 37,999 cycles

E970627 LH OUTBD FLOOR SILL #3 IS PITTED AT NUMEROUS AREAS. R&R'D LH OUTBD FLOOR SILL #3 IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 31,999 cycles

E970811 WASTE SERVICE BUCKET (LAV BUCKET) REINFORCMRNT BRACKETS ARE CORRODED (LEVEL2) AND CRACKED. R&R'D REINFORCEMENT BRACKETS IAW EMB145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 37,999 cycles

E970636 LH OMEGA BEAM GUSSET IS CORRODED BETWEEN FR 35-37. R&R'D LH OMEGA BEAM GUSSET IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 37,999 cycles

E970629 RH OUTBD FLOOR SILL #2 IS PITTED AT NUMEROUS AREAS. R&R'D RH OUTBD FLOOR SIL #2 IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 37,999 cycles

E970658 LAV LH BEAM GUSSET IS CORRODED (LEVEL 2). R&R'D LAV LH BEAM GUSSET IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 37,999 cycles

E970608 #6 LH OMEGA GUSSET IS CORRODED (LEVEL 2). R&R'D GUSSET IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 37,999 cycles

E970607 #5 LH OMEGA BEAM GUSSET IS CORRODED. R&R'D #5 OMEGA BEAM GUSSET IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 37,999 cycles

E970489 SSI 53-20-11 LAVATORY RH BEAM GUSSET HAS NUMEROUS SPOTS OF CORROSION. R&R'D GUSSET IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 37,999 cycles

E970510 SSI 53-20-11 CABIN RH OMEGA GUSSET BETWEEN FRAMES 35-42 HAS NUMEROUS SPOTS OF CORROSION. R&R'D GUSSET IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 37,999 cycles

FR73 IS CRACKED BETWEEN STR17R AND 16R. R&R'D FR73 BETWEEN STR14R-17L IAW EMB145 SRM 51-40-20.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 37,999 cycles

E969827 R/H WING RIB 5 CRACKED AT LOWER FWD END. REPAIRED IAW PIEDMONTEO1-57-23-0122

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 37,999 cycles

E969778 POSSIBLE CRACK ON EXTERNAL FUSELAGE AT FR77 BETWEEN STR4R AND 5R. REPAIRED IAW PIEDMONT EO1-53-23-0117

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,484 hrs · 37,999 cycles

E969647 WASTE SERVICE BUCKET (LAV BUCKET) IS CORRODED (LEVEL 2). R&R'D BUCKET IAW EMB145 SRM051-40-02. REPAIRED IAW PIEDMONT EO1-53-23-0117

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,484 hrs · 37,999 cycles

E969788 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AT FR78 BETWEEN STR5R AND 6R. REPAIRED IAW PIEDMONT EO1-53-23-0117

Part: CLAMP — WORN (BLEED VALVE)

BLEED 2 LEAK AT 4000 FEET DURING CLIMB

Part: NONE — NONE · airframe 41,171 hrs · 37,652 cycles

UPON APU START BURNING SMELL IN FLIGHT DECK AND CABIN.

Part: DAU — FAULTED (NR 1) · airframe 40,660 hrs · 37,049 cycles

EMERGENCY DECLARED LH FUEL TANK WENT TO ZERO DURING CRUISE FUEL IMBALANCE EICAS PRESENTED SUSPECTED FUEL LEAK. VERIFIED MEL CONDITIONS ARE MET USING SPR PANEL. R/R'D FOR MAINT CONVENIENCE DAU #1 IAW 31-41-01-000/ 400-801-A AND REPEATER IAW 28 23-08-000/400-801-A. SEE HA-300 SEQ#4 FOR TROUBLESHOOTING. T/S IAW FIM TAS K 28-41-00-810-914-A. OPS CHECKS GOOD, CLEAR MEL 28-9.

Part: NONE — NONE · airframe 40,041 hrs · 36,375 cycles

PDIS 691 27-21 2618561 18MAY22 CLT CLOSE RUDDER SYSTEM 1-2 FAIL MESSAGE DISPLAYED CREW FOLLOWED QRH RUDD 2 WAS SELECTED OUT AND RUDD 1 SYSTEM RETURNED W/O EICAS MESSAGE. 25550 00 SMK FACT 18MAY22 16:05 CLT R/R #2 RUDDER PRESS SWITCH PER AMM 27-23-04.LEAK CK GOOD.REQUIRES OPS CHECK.PERFORMED OPS CHECK IAW AMM 27-2300-700-804-A.OPS CHECK GOOD.A/C OK FOR SERVICE.

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 38,653 hrs · 34,799 cycles

PRESS AUTO FAIL ON TAKE OFF ROLL. MAINTENANCE R&R'D DIGITAL CONTROLLER PER AMM 21-31-01 OPS CHECK GOOD PER AMM TASK 21-31-00-700-802-A OK FOR SERVICE

Part: VALVE — FAILED (NLG STRUT) · airframe 38,021 hrs · 34,082 cycles

SHORTLY AFTER TAKEOFF EICAS DISPLAYED LG AIR GRND FAIL AND LANDING GEARS WOULD NOT RETRACT. TROUBLESHOT USING FIM 32-63-00-810-802-A STEP 1 2 AND 14, FOUND NLG TO BE IMPROPERLY SERVICED. REPLACED FILLING PORT CHARGING VALVE ON NLG SERVICED NLG IAW AMM TASK 32-20-01-600-801-A.

Part: VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 37,703 hrs · 33,765 cycles

PDIS 691 21-31 2381531 20FEB21 PHL CLOSE AT 24K FEET. CABIN PRESSURIZATION IN AUTO MODE STARTED TO RAPIDLY RISE. FACT 20FEB21 21:48 PHL R & R GROUND CONNECTION VALVE IAW AMM 21-22-04 NEEDS OPS CHECK. PERFORMED PRESSURIZATION, OPS CK FOR GROUND CONNECTION VALVE IAW 21-31-00 OPS CK GOOD OK FOR SERVICE AT THIS TIME.

Part: BALLAST — ODOR (SEAT 1A) · airframe 37,620 hrs · 33,674 cycles

DURING DECENT AT 11000 FEET F/A SMELT PLASTIC, RUBBER BURNING SMELL LOCALIZED IN GALLEY. MAINTENANCE PERFORMED: TROUBLESHOT, PER EMB145 FIM 21-20-00-810-803. REMOVED AND REPLACED BALLAST FOR LIGHTS AT SEAT 1A, PER EMB 145 AMM 33-21-03. OPERATIONS CHECK GOOD. REMOVED TWO SIDE WALL LIGHTS AT SEAT 1A, PER EMB 145 AMM 33-21-06. OPERATIONS CHECK GOOD OPERATIONS CHECK WITH BOTH PACKS AND LIGHTS AND DID NOT FIND ANY ABNORMAL SMELLS.

Part: ENGINE — HAZE · airframe 37,233 hrs · 33,236 cycles

FLIGHT ATTENDANT REPORTS HAZE LIKE SMOKE IN CABIN DURING CLIMBOUT CLEARED AT CRUISE. AIRCRAFT 691 IS CURRENTLY IN WORK, ENGINE IS BEING R&R IN RIC.

Part: INTERCOM — MALFUNCTIONED (CAPTAIN'S) · airframe 36,791 hrs · 32,725 cycles

AFTER T/O, LOST LIGHTS AND AUDIO ON CAPT INTERCOM ASSOCIATED W/ SMOKE AND ODOR. CLEAR AFTER APPROX 4 MINUTES. AFTER T/O, LOST LIGHTS AND AUDIO ON CAPT SIDE ASSOC W/ SMOKE AND ODOR. CLEARED AFTER APPROX 4 MINUTES, CAPT AUDIO RETURNED TO NORMAL. R&R CAPTAINS DAP REF EMB 145 AMM 23-51-00. PERFORMED OPS TEST REF AMM 23-51-00. CHECK GOOD. (THIS IS A SDR ITEM)

Part: PRESSURE SWITCH — FAILED (PARKING BRAKE) · airframe 36,608 hrs · 32,517 cycles

PDIS 691 32-49 2249601 03JAN20 CLT CLOSE TAKEOFF CONFIG, BRAKES ARE STICKING. ATTEMPTED 6 TIMES. FACT 03JAN20 18:02 CLT REMOVED AND REPLACED EMERGENCY PARKING BRAKE PRESSUR E SWITCH IAW AMM 32-44-07-400-801-A. PERFORMED OPS CHECK IAW AMM 31-51-00-700-801-A. OPS CHECK GOOD . LEAK CHECK GOOD. OK FOR SERVICE.

Part: VALVE — MALFUNCTIONED (BLEED AIR) · airframe 36,340 hrs · 32,177 cycles

BLEED 2 LOW TEMP IN ICING CONDITIONS WITH N1 ABOVE 85%....FIX: REMOVED AND REPLACED FAN AIR VALVE IAW EMB AMM 36-11-03. OPS CHK GOOD

Part: A/C PACK — WARNING LIGHT · airframe 36,244 hrs · 32,066 cycles

NDIS 691 21-99 0015370 28OCT19 BGR CLOSE **** THIS DISCREPANCY CREATED FOR MIR PURPOSES **** AIRCRAFT ABORTED TAKEOFF DUE TO A PACK ISSUE WHICH S ELF CLEARED. CREW PERFORMED SYSTEM CHK AND ALL SYSTE MS OPS NORM THROUGH NORMAL CREW PROCEDURES WITH NO H ISTORY OR DISCREPANCY REQUIRED. FACT 28OCT19 16:58 BGR THIS DISCREPANCY CLOSED. MIR CREATED.

Part: CONTROL UNIT — FAILED (THRUST REVERSER) · airframe 34,545 hrs · 30,091 cycles

ON TAKEOFF WHEN FULL POWER APPLIED E1 TR DISAG EICAS MESSAGE DISPLAYED. ABORTED TAKEOFF. DISCOVERED E1 TR ICU VLV FAIL MSG IN CMC. R&R NR 1 ICU IAW 78-33-01. NO DEFECTS NOTED OPS CHECK GOOD AT THIS TIME. OK FOR SERVICE

Part: THRUST REVERSER — WARNING MESSAGE (NR 1) · airframe 34,425 hrs · 29,956 cycles

NR 1 ENGINE THRUST REVERSER DISAGREE MESSAGE. THE ACFT HAD SAME HISTORY IN JULY WITH SAME FAILURE. ICU VALVE FAILURE. UPPER ACTUATOR WAS REPLACED. POSSIBLE FAILURE OF THE LOWER ACTUATOR OR MAYBE UPPER. ACTUATOR.

Part: ICU — MALFUNCTIONED (THRUST REVERSER) · airframe 34,267 hrs · 29,780 cycles

ENG 1 REV DISAGREE MSG ON T/O ROLL, C/W TASK 78-31-01-980-801-A. DOWNLOADED CMC. MESSAGE ENG 1 T/R ICU VALVE FAI ON CMC. CW FIM TASK 78-30-00-810-814-A BLOCKS 1 & 4. REMOVED AND REPLACED NR 1 ICU PER 78-33-01. OPS CHECKS GOOD.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 34,233 hrs · 29,736 cycles

691 36-21 1659701 28SEP18 CHS CLOSE BLEED 1 LEAK EICAS WARNING MESSAGE. THROUGH 3000 FT ON CLIMB OUT. 27147 00 JBU HISTORY: . MEL 28SEP18 21:21 CHS C27111 21-13-2 AIR CONDITIONING PACKS FACT 29SEP18 03:25 RIC FOUND LOOSE V BAND CLAMP AT FWD SIDE OF NR 1 BLEED VALVE TIGHTENED CLAMP IN REF TO AMM 20-10-10-910-801A OPS AND LEAK CHECK GOOD NO DEFECTS NOTED AT THIS TIME OK FOR SERVICE. CLEAR MEL.

Part: VALVE — CRACKED (BLEED DUCT) · airframe 34,194 hrs · 29,700 cycles

NDIS 691 36-21 0006440 22SEP18 PHL CLOSE BLEED 1 LEAK MSG IN CLIMB OUT C/W QRH LIGHT WENT OUT (AT 17K HAD NUMEROUS ICE CONDITION WARNINGS CAPT HAD STATED SYS NOT WORKING-NO HISTORY) 31575 00 CFG FACT 22SEP18 19:58 PHL MX INSP FOUND DUCT AT PACK 1 VALVE TO BE CRACK AT WE LD JOINT RNR DUCT 1360004 REF EMB 145 AMM 21-51-01 O PS AND LEAK GOOD PERFORMED ANTI ICE TEST IAW AMM 30- 00-00 TESTED OK FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 34,044 hrs · 29,544 cycles

FOUND THE EMERGENCY LIGHT STRIP WITH A BROKEN WIRE. R & R THE EMERGENCY LIGHT BETWEEN ROWS 8 & 9 IAW AMM 33-50-12-000/400-801-A. OPS CHECKED GOOD, OK FOR SERVICE.

Part: UNKNOWN — FIRE (LT ENGINE) · airframe 34,049 hrs · 29,544 cycles

PDIS 691 05-50 1610351 20AUG18 ORF CLOSE GND CREW REPORTS LF ENG EXHAUST FIRE AT GATE 25440 00 MS HISTORY: . FACT 20AUG18 16:13 ORF INSPECTED, FOUND NO EVIDENCE OF FIRE, NO OIL POOLING GND RAN RESULTING IN CLEAN SHUT DOWN AND NO SMOKE.

Part: ACTUATOR — DEFECTIVE (THRUST REVERSER) · airframe 33,928 hrs · 29,401 cycles

ON TAKE OFF SET THRUST, E1 REV DISAGREE CAUTION WITH TAKE OFF CONFIG MSG. REJECTED TAKE OFF. REACTIVATED NR 1 T/R. CHECKED RIGGING OF T/R MICROSWITCHES. NO DEFECTS NOTED. R&R UPPER T/R DOOR ACTUATOR PER AMM 78-32-01. OPERATED T/R'S. OPS CHECK GOOD AT THIS TIME.

Part: VALVE — FAILED (THRUST REVERSER) · airframe 33,881 hrs · 29,336 cycles

E1 TR DISAGREE EICAS MESSAGE ON TAKEOFF ROLL. E1 TR ICU VALVE FAIL IN CMC. CREW LONG TAXI THEN RETURN TO GATE. MX TO DEACTIVATE, LATE BACK ON GATE 0925L. REINSTALLED PANELS 416AB, 416BB, 416CB, 416HT, 416JT, 416PR, AND 416QL USING RETAINED HARDWARE.

Part: RELAY — FAILED (THRUST REVERSER) · airframe 33,871 hrs · 29,323 cycles

NR 1 T/R DISAGREE MESSAGE ON TAKEOFF. TAKEOFF ABORTED. CHECKED CMC NO MESSAGES PRESENT DUE TO PRIOR HISTORY FOLLOWED FIM 78-34-00-810-803-A BLOCK DIAGRAM AS STEPS 1-4, 11 AND 12 INSPECTED WIRES TO THRUST LEVELS DEPLOY MICROSWITCHES AND ICU FOR SIGNS OF CHAFFING NONE FOUND TESTED CONTINUITY FROM P1269 PIND TO K0641 PIN X1, K0641 X2 TO GROUND AND K0641 A2 TO P1250 PIN 4. TESTED FOR CONTINUITY FROM J1269 PIN D TO PIN F CHECKED GOOD ALSO CHECKED FOR CONTINUITY FORM PIN D, TO PIN G CHECKED GOOD THRUST LOWER SWITCH (ENG 1) CHECKED GOOD. R&R RELAY K0401, K0403, K0405, AND K0407 AS A MAINTENACE PROGRAM IN REF FIM 7 8-34-00-801-803-A ALL 4 RELAY PART NUMBERS ARE M83536-7-024M. CHECKED A2 (RELAYK0641) TO GROUND CHECK GOOD CHECKED PIN D1 TO PIN D3 FOR RESTIANCE CHECK GOOD. REF WIRING DIAGRAM 79-31-50 MEASURED REISTANCE ON THE NR 1 RESISTAS MODULE. OPS CHECKED T/R WITH ELECTRIC PUMPS NO FAULTS PERFORMED T/O POWER RUN WITH AIRCRAFT IN T/O CONFIG NO EICAS MESSAGES.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 33,831 hrs · 29,276 cycles

ENG 1 T/R DISAGREE MESSAGE DISPLAYED ON TAKEOFF ROLL. C/W AMM 78-31-01-980-801-A. ENG 1 OR 2 REV DISAGREE MESSAGES.

Part: ICU — MALFUNCTIONED (THRUST REVERSER) · airframe 33,820 hrs · 29,264 cycles

UPON REACHING TO POWER E1 REV DISAGREE EICAS MESSAGE DISPLAYED WITH NO TO CONFIG AND SPOILERS DEPLOYED. ABORTED TAKEOFF. E1 TR ICU VLV FAIL DISPLAYED IN CMC. R&R NR 1 ICU IAW AMM 78.33.01. OPS CK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (NR 2 BLEED VALVE) · airframe 33,215 hrs · 28,590 cycles

BLEED 2 VALVE CLOSED MESSAGE DISPLAYED ON EICAS DURING FLIGHT, CREW FOLLOWED QRH MESSAGE AND RETURNED.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPS) · airframe 33,199 hrs · 28,569 cycles

ON TAKEOFF ROLL SPS1 INOPERATIVE AND SPS FAILED MESSAGE DISPLAYED AND SPOILERS INDICATED OPEN. COMPLIED WITH AN OPERATIONAL TEST OF THE SPS IAW 27-36-00. OPS CHECKED NORMAL, NO DISCREPANCIES NOTED.

Part: HEATER — INOPERATIVE (PITOT) · airframe 33,196 hrs · 28,567 cycles

NR 3 PITOT WILL NOT HEAT. R & R PITOT 3 SENSOR SWITCH IAW AMM 20-13-04-000-400-801-A. R & R PITOT STATIC SENSOR NR 3 IAW AMM 34-13-02-000-400- 801-A. OPS CHECKED GOOD. OKAY FOR SERVICE.

Part: SKIN — PUNCTURED (RUDDER) · airframe 32,938 hrs · 28,285 cycles

FOUND A PUNCTURE IN THE RUDDER ON THE RIGHT SIDE 20 MM FROM BOTTOM AND 45MM FROM AFT EDGE. PERFORMED A PERMANENT REPAIR TO THE RUDDER IAW ERS-EM-55MR-614

Part: ATTACH FITTING — DAMAGED (RT AILERON) · airframe 32,938 hrs · 28,285 cycles

RIGHT HAND AILERON PCA ATTACH FITTING OUTBOARD LUG HAT BUSHING MIGRATING OUT OF FITTING. -C/A-REMOVED AND REPLACED R/H AILERON PCA FITTING ASSY IAW EO EM-27MR-112.

Part: ATTACH FITTING — DAMAGED (LT AILERON) · airframe 32,938 hrs · 28,285 cycles

LEFT HAND AILERON PCA ATTACH FITTING OUTBOARD LUG HAT BUSHING MIGRATING OUT OF FITTING. -C/A-REPLACED AILERON WITH NEW. SEE NRWC E609824 FOR INSTALLATION AND E611839 FOR FCF

Part: SUPPORT — WORN (RT AILERON) · airframe 32,938 hrs · 28,285 cycles

RT AILERON #4 HINGE OUTBOARD LUG BORE IS WORN-C/A-REMOVED AND REPLACED HINGE FITTING #4 ON R/H AILERON IAW EO EM-27MR-112.

Part: FITTING — WORN (LT AILERON) · airframe 32,938 hrs · 28,285 cycles

LT AILERON DAMPER FITTING OUTBOARD LUG BORE IS WORN-C/A-REPLACED AILERON WITH NEW. SEE NRWC E609824 FOR INSTALLATON AND E611839 FOR FCF.

Part: SUPPORT — WORN (RT AILERON) · airframe 32,938 hrs · 28,285 cycles

RT AILERON #3 HINGE INBOARD LUG BORE IS WORN-C/A-REMOVED AND REPLACED THE RH AILERON #3 HINGE IAW EM-27MR-112.

Part: SUPPORT BRACKET — CRACKED (CARGO DOORWAY) · airframe 32,938 hrs · 28,285 cycles

BAGGAGE DOOR LIFTING AND LOWERING FWD TORSION BAR SUPPORT BRACKET IS CRACKED. -C/A- REMOVED AND REPLACED BAGGAGE DOOR LIFTING AND LOWERING FWD TORSION BAR SUPPORT BRACKET IAW SRM 51-40-02

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 32,938 hrs · 28,285 cycles

SERVICE DOOR UPPER BEAM HAS A 3/8" CRACK BETWEEN TWO FWD VERTICAL BEAMS. -C/A-COMPLIED WITH REPAIR OF SERVICE DOOR BEAM IAW ERS-EM-52MR-835.

Part: BRACKET — CRACKED (CARGO DOORWAY) · airframe 32,938 hrs · 28,285 cycles

AFT CARGO DOOR HOLD OPEN ROD SUPPORT INNER BRACKET IS CRACKED IN TWO SPOTS. -C/A- INSTALLED NEW SUPPORT IAW SRM 51-40-02

Part: ATTACH ANGLE — CRACKED (FRAME 47) · airframe 32,938 hrs · 28,285 cycles

RH WING LATERAL PANEL LOWER ATTACH ANGLE CRACKED AT FRAME 47-C/A-INSTALLED NEW RH WING LATERAL PANEL LOWER ATTACH ANGLE AT FRAME 47 IAW ETN-EM-53-142.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 32,116 hrs · 27,531 cycles

DURING TAKEOFF ROLL STRONG BURNING ODOR WAS SMELLED BY BOTH PILOTS, THE TAKEOFF WAS ABORTED. FOLLOWING FIM TASK 21-20-00-810-801-A AND 21-20-00-810-803-A, PERFORMED ALL RELEVANT TASK AND FOUND NO SMOKE SMELL IN COCKPIT AT THIS TIME.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 31,439 hrs · 26,960 cycles

EMERGENCY LIGHTS AND NR 2 EPSU INOPERATIVE. R & R NR 2 EMERGENCY LIGHT POWER SUPPLY INVERTER IAW AMM 33-50-11-000-801-A, & 33-50-11-400-801-A, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,471 hrs · 26,075 cycles

EMERGENCY LIGHT ON LOWER LEFT SIDE SERVICE DOOR FAIRING WILL NOT PROPERLY ILLUMINATE. R & R THE EMERGENCY LIGHT, OPS CHECKED GOOD IAW AMM 33-50-13

Part: ROLLER — DEFECTIVE (FUSELAGE) · airframe 30,138 hrs · 25,760 cycles

F/A REPORTS MAIN CABIN DOOR BINDING, DIFFICULT TO OPERATE. REPLACED AFT UPPER ROLLER IAW AMM 53-21-02. OPS CHECK GOOD, ACFT OK FOR SERVICE.

Part: SHUTOFF VALVE — FAILED (NR 2 A/C PACK) · airframe 30,124 hrs · 25,748 cycles

NR 2 A/C PACK CIRCUIT BREAKER TRIPPED DURING CLIMB OUT, AROUND 10000FT. NR 2 VALVE PRESSURE REGULATOR AND SHUTOFF VALVES REPLACED IAW AMM 21-51-01 OPS CHECKED GOOD.

Part: CONTROL MODULE — FAILED (CABIN LIGHTS) · airframe 29,933 hrs · 25,578 cycles

FOUND STRONG ELECTRICAL ODOR COMING FROM CABIN LIGHTING CONTROL MODULE. REPLACED CABIN CONTROL LIGHT MODULE & CHECK OK IAW MM 33-21-01.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 29,539 hrs · 25,217 cycles

AFT EXIT LOCATING SIGN INOPERATIVE. R & R NR 4 EMER LIGHT AC & DC INVERTER IAW 33-50-11. OPERATIONS CHECKED GOOD.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 28,774 hrs · 24,499 cycles

THROUGH 22000 FT CAB RATE ABNORMAL FLUCTUATIONS. THE CAB RATE DASHED INDICATIONS CAB AP HOLD 8-21 PSI & CAB ALT INITIAL HOLDING AT 2500 FT, THEN SLOWLY DECREASING. RUN AOM 1 PROCEDURES ON AUTO PESS LAND ELEV, NO MSGS BUT THE LANDING ALT INDICATIONS. DEFERRED PRESSURIZATION CONTROL SYS AUTO & MANUAL M PROCEDURES COMPLIED WITH IAW 21-18. REMOVED AND REPLACED ELECTROPNEUMATIC OUTFLOW VALVE IAW EMB AMM 21-31-03. OPC GOOD REF AMM 21-31-00-700-801-A. MEL RESTORED.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 28,601 hrs · 24,329 cycles

GALLEY FLOOR CROSSBEAM CORRODED AT FRAME 20. R & R CORRODED CROSSBEAM GALLEY FLOOR AT FRAME 20 IAW SRM 51-40-02 & ETN-EM-53-139.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,601 hrs · 24,329 cycles

LEFT UPPER FUSELAGE SKIN HAS 2 CRACKS, CRACK 1 IS AT FRAME 75 & ABOVE STRINGER 2L, CRACK IS 1" LONG. CRACK 2 IS AT FRAME 75 OFF OF THE FIRST FASTENER BELOW STRINGER 2L, CRACK IS APPROX 1/4" LONG, EASI 8071 USED, 100-500 KHZ PROBE, FREQ= 400KHZ, V-GAIN= 77.0, H-GAIN=65.0, LPF=-100. SATISFACTORY ACCOMPLISHED THE REPAIR OF 2 CRACKS ON LT UPPER FUSELAGE SKIN AT FRAME 75 ABOVE STRINGER 2L, & OFF OF THE FIRST FASTENER BELOW STRINGER 2L IAW ERS-EM-53MR-1828. SEE WIP & TASK ENTRIES FOR DETAILS.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,601 hrs · 24,329 cycles

LEFT FWD EMER LIGHT RAMP EXTRUSION DAMAGED. R & R LT FWD EMER LIGHT RAMP EXTRUSION AS REQUIRED, SEE NRTC BOW206193 FOR INSTALL.

Part: STRUT — UNDERSERVICED (NLG) · airframe 27,558 hrs · 23,322 cycles

AFTER TAKEOFF RECEIVED LG AIR & GND FAIL ON EICAS, FOLLOWED BY ENG 1, 2 REV DISAGREE. RETURNED FOR NORMAL LANDING. PERFORMED FIM TASKS 32-63-00-810-804-A & 32-63-00-810-805-A. FOUND NLG STRUT UNDERSERVICED. SERVICED NLG STRUT IAW AMM 32-20-01. PERFORMED LG RETRACTION IAW AMM 32-30-00. NO DEFECTS NOTED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,584 hrs · 23,344 cycles

DURING ROUTINE MX, DAMAGE TO RT REAR FUSELAGE SKIN WAS DISCOVERED TO BE BEYOND LIMITS OF THE MANUAL. RECONTOURED AFFECTED AREA IAW ERS-EM-53MR-1114.

Part: PITOT LINE — CONTAMINATED (NR 1&2) · airframe 27,406 hrs · 23,170 cycles

AT FL 360 & FLYING THROUGH MOD RAIN REC EICAS, SPS ADVANCED, PLUS THE IAS ON THE CAPTAINS SIDE HAD A DIFFERENCE OF 40 KTS FROM FIRST OFFICERS SIDE. ALSO FIRST OFFICERS SIDE TO CAPTAINS SIDE WAS OFF BY 200 FT. CAPTAINS & STANDBY WAS CORRECT. DESCENDING THROUGH FL 200, FIRST OFFICER AIRSPEED & ALT RETURNED TO NORMAL. DRAINED WATER FROM PITOT STATIC SYS 1 & 2 IAW AMM 34-13-00. ADC SYS OPERATIONS CHECKS GOOD IAW AMM 34-15-00. STALL PROTECT SYS OPERATIONS CHECK GOOD IAW AMM 27-36-00.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 26,947 hrs · 22,800 cycles

COCKPIT STEP LIGHT, EMER LIGHT INOPERATIVE. R & R NR 1 EMER LIGHT DC & AC INVERTER. OPERATIONS CHECKED GOOD IAW AMM 33-50-11.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 26,879 hrs · 22,747 cycles

DURING DESCENT OUT OF FL 230, CAPTAIN’S PFD HAD RED X 'S OVER AIRSPEED ALTIMETER VSI VFR CONDITIONS. EMER DECLARED, NO OVERWEIGHT LANDING & NO CFR. INSPECTED PITOT STATIC DRAINS, FOUND ADEQUATE MOISTURE IN ADC 1 LINE. REMOVED MOISTURE IAW AMM 34-13-00. WATER REMOVED FROM SYS.

Part: CRADLE — INOPERATIVE (FLASHLIGHT) · airframe 26,497 hrs · 22,432 cycles

CAPTAIN`S FLASHLIGHT BOTTOM CLIP ON CRADLE INOPERATIVE. R & R CAPTAIN`S BASE ASSEMBLY IAW AMM 33-51-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,873 hrs · 21,887 cycles

EMER LIGHT OVER RT EMER EXIT ROW INOPERATIVE. R & R EMER LIGHT LAMP AT RT EXIT ROW IAW AMM 33-50-08. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — ODOR · airframe 25,481 hrs · 21,520 cycles

STRONG SMELL OF FUEL ON TAKEOFF ROLL. PERFORMED VISUAL INSPECTION OF NR 1 & 2 ENG IAW 72-00-00-200-802. NO LEAKS NOTED. PERFORMED ETN-EM72-034 NO FUEL SMELL NOTED.

Part: EPSU — INOPERATIVE (CABIN) · airframe 24,755 hrs · 20,935 cycles

EMERGENCY LIGHTS LEFT ON. FOUND MULTIPLE EMERGENCY LIGHTS INOPERATIVE. R & R NR 1 & NR 3 EPSU IAW WC 33-700-19. OPERATIONS CHECKED GOOD IAW WC 33-700-17, NO FURTHER DEFECTS NOTED.

Part: CONNECTOR — LOOSE (CABIN) · airframe 24,700 hrs · 20,901 cycles

AFT SIDE OF CTR ISLE CEILING EMERGENCY EXIT LIGHT PANEL DOES NOT ILLUMINATE. UPON FURTHER INSPECTION FOUND LOOSE CONNECTOR, RECONNECTED IAW AMM 33-50-15, OPERATIONS CHECKED GOOD.

Part: STRUT — LOW (NLG) · airframe 24,534 hrs · 20,771 cycles

IMMEDIATELY AFTER TAKEOFF LG AIR & GND FAIL MSG APPEARED ON EICAS & REMAINED UNTIL LG EXTENDED. SERVICED NOSE STRUT IAW AMM WC 62-600-06 DUE TO IMPROPERLY SERVICED NOSE STRUT. PERFORMED GEAR SWING IAW AMM 32-30-00 OPERATIONS CHECKED GOOD.

Part: FITTING — CRACKED (RT NACELLE) · airframe 24,503 hrs · 20,741 cycles

DURING MBV INSPECTION, QC FOUND RT ENG FWD LOWER YOKE FITTING CRACKED. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER INSPECTION. PERFORMED PERMANENT REPAIR ON RT ENG FWD LOWER YOKE FITTING IAW EO-EM-54MR-386.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 24,503 hrs · 20,741 cycles

RT OTBD OMEGA BEAM SUPPORT AT FRAME 47 IS CRACKED. R & R RT OTBD OMEGA BEAM SUPPORT IAW SRM 51-40-02. SEE WIPS & TASK FOR ADDITIONAL INFORMATION.

Part: HOUSING — LOOSE (CABIN) · airframe 24,503 hrs · 20,741 cycles

AFT CEILING EMERGENCY LIGHT HOUSING LOOSE. REPAIRED AFT CEILING EMERGENCY LIGHT LENS IAW AMM 25-00-00.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 24,503 hrs · 20,741 cycles

LT OTBD OMEGA BEAM SUPPORT HAS POSSIBLE CRACK AT FRAME 47. R & R LT OTBD OMEGA BEAM SUPPORT IAW SRM 51-40-02.

Part: CONNECTOR — BROKEN (CABIN) · airframe 24,503 hrs · 20,741 cycles

CEILING PANEL 253 CLC FWD EMERGENCY EXIT LIGHT WIRE CONNECTOR END BROKEN. REPAIRED CEILING PANEL 253 CLC FWD EMERGENCY EXIT LIGHT WIRE CONNECTOR IAW SWPM 20-21-00 STEP 6.

Part: WIRE — EXPOSED (CABIN) · airframe 24,503 hrs · 20,741 cycles

EMERGENCY PROXIMITY LIGHT STRIPS NR 1, NR 2 & NR 5 HAVE EXPOSED WIRES. R & R PROXIMITY LIGHT STRIP NR 1, NR 2 & NR 5 INTO LIGHT STRIP COVER PANEL AS REQUIRED. SEE BOW 149832 FOR INSTALLATION OF PROXIMITY LIGHT STRIP COVER PANEL & OPERATIONS CHECK.

Part: WARNING LIGHT — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 23,817 hrs · 20,214 cycles

EMERGENCY LIGHT INDICATION CAME ON THE ICU PANEL AND WONT GO OUT. RESET ELECTRICAL POWER ON ACFT IAW WM-24-31-00, OPS CHECKED GOOD. NO FAULTS NOTED IAW MM-35-50-00.

Part: DOOR — DIRTY (MAIN PAX) · airframe 23,408 hrs · 19,836 cycles

F/A REPORTS MAIN CABIN DOOR IS DIFFICULT TO OPERATE. CLEANED, LUBED AND PERFORMED OPS CHECK OF MAIN DOOR IAW AMM 52-10-01. CLEANED AND LUBED DOOR ROLLERS, REQUIRED 30LBS ON FISH SCALE TO OPEN.

Part: ROLLER — LACK OF LUBE (MAIN DOOR) · airframe 23,164 hrs · 19,610 cycles

F/A REPORTS PASSENGER DOOR IS HARD TO OPEN. LUBRICATED FRAME ROLLERS IAW AMM 53-21-02, OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 23,053 hrs · 19,520 cycles

F/A REPORTS MAIN PAX DOOR HANDLE GET STUCK AND DOOR HARD TO CLOSE AND OPEN. LUBRICATED MAIN CABIN DOOR FRAME ROLLERS IAW AMM 52-18-00. TESTED SATISFACTORY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,891 hrs · 19,379 cycles

DURING MX INSPECTION, FOUND RT UPPER WING EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R THE RT UPPER WING EMERGENCY LIGHT ASSY IAW AMM 33-50-10. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: MODULE — INOPERATIVE (INTERCOM) · airframe 22,798 hrs · 19,301 cycles

CREW REPORTED COCKPIT AND CABIN EMERGENCY INTERCOM LIGHTS SELF ILLUMINATED AND COULD NOT BE RESET. BACKUP DID NOT FUNCTION. ACFT REMOVED FROM SERVICE. R & R THE ICU MODULE IAW AMM 23-31-02. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 22,062 hrs · 18,711 cycles

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

Part: LIGHT — NOT SEATED (EXTERIOR) · airframe 21,399 hrs · 18,181 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT HAND OVER WING EXT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESEATED THE RIGHT HAND EXTERNAL OVERWING EMERGENCY LAMP IAW EMB145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 21,281 hrs · 18,092 cycles

ON FLIGHT 2921 THE CREW REPORTED THE FLIGHT ATTENDANTS FLASHLIGHT ABOVE JUMPSEAT HAS BROKEN HOLDER. THE FLASHLIGHT WOULD NOT STAY IN OR CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLASHLIGHT. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,279 hrs · 18,091 cycles

DURING B INSPECTION FOUND THE AFT CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CEILING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 20,949 hrs · 17,817 cycles

ON FLIGHT 2723 THE FLIGHT ATTENDANT REPORTED THE FORWARD FLASHLIGHT DID NOT WORK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,868 hrs · 17,750 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 145 AMM TASK 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 20,539 hrs · 17,476 cycles

DURING B INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM TASK: 33-50-07-000-801-A, AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 20,274 hrs · 17,261 cycles

FLIGHT 3214, FOUND EMERGENCY LIGHT ON FLOOR BY LEFT OVERWING EXIT DOES NOT CONFORM TO GUIDANCE ON PG 2-24 OF THE INFLIGHT MANUAL. AIRCRAFT REMOVED FROM SERVICE. REPOSITIONED EXIT ROW EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 19,408 hrs · 16,572 cycles

ON FLIGHT 3461, CREW REPORTED MAIN CABIN DOOR WAS HARD TO OPEN AND CLOSE. AIRCRAFT REMOVED FROM SERVICE. LUBRICATED MAIN CABIN DOOR IAW AMM 52-18-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 19,408 hrs · 16,572 cycles

ON FLIGHT 3461, CREW REPORTED CAPTAIN'S FLASHLIGHT NOT CHARGING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 18,894 hrs · 16,162 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLASHLIGHT WILL NOT STAY IN HOLDER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT AND CHARGER IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,805 hrs · 16,096 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LAST EMERGENCY LIGHT IN CEILING INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 18,278 hrs · 15,733 cycles

ON FLIGHT 3335 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED MAIN DOOR ROLLERS IAW EMB 145 AMM 53-21-02. THE OPERATIONAL CHECK WAS GOOD IAW AMM 52-00-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — SMOKE (NR 1) · airframe 17,702 hrs

AFTER LANDING AND PARKING AT GATE, OBSERVED EXCESSIVE AMOUNT OF SMOKE COMING FROM FRONT AND REAR OF ENGINE NR 1. OIL LEVEL OK. PERFORMED ENGINE RUN OF NR 1 ENGINE IAW EMB 145 AMM 71-00-01. FOUND SMOKE COMING FROM INTAKE AND EXHAUST UPON SHUTDOWN. NO ENGINE OIL LEAKS DETECTED AT THIS TIME.

Part: UNKNOWN — SMOKE (NR 1 ENGINE) · airframe 17,702 hrs

AFTER LANDING AND PARKING AT GATE, OBSERVED EXCESSIVE AMOUNT OF SMOKE COMING FROM FRONT AND REAR OF ENGINE NR 1 . OIL LEVEL OK. PERFORMED ENGINE RUN OF NR 1 ENGINE IAW AMM 71-00-01. FOUND SMOKE COMING FROM INTAKE AND EXHAUST UPON SHUTDOWN. NO ENGINE OIL LEAKS DETEDTED AT THIS TIME.

Part: PROXIMITY SENSOR — DIRTY (NLG) · airframe 17,123 hrs · 14,902 cycles

ON FLIGHT 2915 ON DESCENT THE CREW REPORTED, RECEIVED AN AIR/ GROUND FAIL MESSAGE ON ECIAS FOR A FEW SECONDS AFTER GEAR EXTENSION AND THEN CLEARED. A CORRESPONDING THRUST INCREASE WAS NOTED WITH AIR / GROUND AND THE ECIAS MESSAGE DID NOT APPEAR TO GO AWAY. THE CREW PERFORMED THE CHECKLIST FOR AIR / GROUND FAIL MESSAGES AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT IAW EMB FIM 32-63-00 NO CENTRAL MAINTENANCE COMPUTER MESSAGE FOUND, THE NOSE LANDING GEAR PROXIMITY SWITCH WAS VERY DIRTY. CLEAND AND PERFORMED OPERATIONAL CHECK IAW AMM 32-60-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRESSURE SWITCH — INOPERATIVE (RUDDER) · airframe 16,525 hrs · 14,492 cycles

ON FLIGHT 3649 THE CREW REPORTED THAT DURING THE CLIMB AT 2,000 FEET RECEIVED A "RUDDER SYS 1-2 INOP" AND YAW DAMPER FAIL MESSAGES. A 'THUD' AND RUDDER PEDAL MOVEMENT NOTED WITH THE INITIAL FAILURE AND WITH SYSTEM 1 DURING THE AIRCRAFT OPERATIONS MANUAL CHECKLIST. AN EMERGENCY WAS DECLARED AND THE CREW ELECTED TO RETURN TO MIA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT T/S AS PER FIM 27-22-00-810-804-A PAGE 202 STEP 1 AND 3. REPLACED RUDDER PRESSURE SWITCH AS PER EMB AMM 27-23-04 OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BUSHING — WORN (SERVICE DOOR) · airframe 13,812 hrs · 12,366 cycles

PRIOR TO FLIGHT 3376 THE SERVICE DOOR WAS DIFFICULT / IMPOSSIBLE TO CLOSE, THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BUSHINGS ON SUPPORT ASSEMBLY AND ACTUATION ROD WORN. REPLACED AND ADJUSTED BUSHINGS ON SUPPORT ASSEMBLY AND ACTUATION ROD. THE SERVICE DOOR FUNCTIONS NORMALLY AT THIS TIME IAW EMB 145 AMM 52-43-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 11,803 hrs · 10,729 cycles

CREW REPORTED A ELECTRICAL ODOR IN GALLEY COMING FROM THE COFFEE POT MOVED CONTAINER TO ALTERNATE POSITION AND ODOR WENT AWAY DEACTIVATED RT PLUG IAW MEL 2550 AND ISSUED MEL AWAITING FOLLOW UP.

Part: SOCKET — DEFECTIVE (GALLEY)

ON FLIGHT 3411 CREW REPORTED A ELECTRICAL ODOR IN GALLEY COMING FROM THE COFFEE POT MOVED CONTAINER TO ALTERNATE POSITION AND ODOR WENT AWAY DEACTIVATED RT PLUG IAW MEL 2550 AND ISSUED MEL. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT HOT CONTAINER SOCKET IAW CRD AEROSPACE CMM. OPERATIONAL CHECK GOOD. MEL RESTORED. AIRCRAFT RETURNED TO SERVICE.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 114,860 hrs · 10,401 cycles

ON FLIGHT 4361, CREW ELECTED TO RETURN TO ORD DUE TO ELECTRICAL ODOR IN CABIN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BALLASTS OPERATIONAL CHECK GOOD. PERFORMED A FUNCTIONAL CHECK FLIGHT WHICH PASSED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL MODULE — ODOR (PSU) · airframe 11,405 hrs · 10,399 cycles

ON FLIGHT 4199, CREW REPORTED THAT THE FA DETECTED A BURNING ODOR IN THE GALLEY AREA ON TAXI. MAINTENANCE LATER FOUND ODOR TO BE ORIGINATING FROM SEAT 1A PSU AREA. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CONTROL MODULE ASSEMBLY FOR PASSENGER CABIN LIGHTS IAW AMM 33-21-01. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL MODULE — FAILED (CABIN LIGHTS) · airframe 11,405 hrs · 10,399 cycles

ON FLIGHT 4199, CREW REPORTED THAT THE FA DETECTED A BURNING ODOR IN THE GALLEY AREA ON TAXI. MAINTENANCE LATER FOUND ODOR TO BE ORIGINATING FROM SEAT 1A PSU AREA. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CONTROL MODULE ASSEMBLY FOR PASSENGER CABIN LIGHTS IAW AMM 33-21-01. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — LEAKING (FUEL VENT) · airframe 10,069 hrs · 9,101 cycles

ON FLIGHT4222 CREW REPORTED DURING CLIMBOUT NOTICED A CLEAR FLUID LEAKING OUT OF THE RIGHT WING. CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO THE FIELD. AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED VENT VALVE, NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — LEAKING (FUEL VENT) · airframe 9,183 hrs · 8,305 cycles

ON FLIGHT 3456 AFTER TAKEOFF, TOWER REPORTED A FUEL LEAK COMING FROM ONE OF THE WINGS. CREW DID NOT NOTICED ANY ABNORMALITY. AT FL130 HE DID NOTICED A NORMAL FUEL BURN AND NO FUEL QUANTITY CHANGES. CREW ELECTED TO RETURN TO THE BLOCK. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT WING FUEL VENT VALVE. LEAK CHECKED GOOD AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 8,753 hrs · 7,926 cycles

ON FLIGHT 4371, CREW REPORTED ABNORMAL SMELL IN THE COCKPIT ON CLIMB-OUT FROM, ODOR WAS INTERMITTENT SMELLED LIKE A COMBINATION DIRTY SOCK AND CHEMICAL. CREW PERFORMED APPROPRIATE PROCEDURE IN AOM 1 DECLARED PRECAUTIONARY (NOT AN EMERGENCY). RETURNED TO MDT. ALSO, LATER GOT PACK 1 OVLD AND PACK 1 OVHT AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF PACK SYSTEM IAW EMB 145 AMM 21-31-00-700-802. NOTED DIRTY SOCK SMELL WHILE RUNNING NR 1 PACK ALSO RECEIVED PACK 1 OVLD MESSAGE MEL'D NR 1 PACK PER MEL 21-29 AUTH 031085D-C. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — WORN (MLG) · airframe 8,525 hrs · 7,696 cycles

ON FLIGHT 3973, CREW REPORTED LANDING GEAR CLUNKING NOISE. DURING LANDING GEAR RETRACTION CLUNKING LOUD BANG AT RETRACTION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NOSE LANDING GEAR DOOR ACTUATOR IAW EMB 145 AMM 32-33-03. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED AND NR 8194; AIRCRAFT RETURNED TO SERVICE.

Part: HOLDER — SMOKE (COCKPIT) · airframe 8,310 hrs · 7,484 cycles

ON FLIGHT 4302, CREW REPORTED SHUTDOWN ENGINE AT THE GATE. A LITTLE BIT OF SMOKE WAS SEEN FROM UNDER THE F/O'S GLARE SHIELD. AIRCRAFT REMOVED FROM SERVICE. FOUND F/O`S CHART HOLDER SHORTING OUT AGAINST CHART ASSEMBLY CAUSING CIRCUIT BREAKER NR 2 COCKPIT READING TO TRIP. REMOVED AND REPLACED FIRST OFFICES CHART HOLDER ASSY IAW EMB145 25-12-11. OPS CHECK GOOD. NO DEFECTS NOTED, AIRCRAFT RETURNED TO SERVICE.

Part: FAN — BURNED (CABIN) · airframe 8,064 hrs · 7,271 cycles

PAX COMPLAINING OF NOXIOUS VAPORS LOCATED MID CABIN. VERIFIED BY DEAD HEADING CREW MEMBERS. UNABLE TO LOCATE SOURCE. REMOVED AND REPLACED BOTH RECIRCULATION FANS THAT WERE FOUND TO HAVE BURNED, AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 7,470 hrs · 6,708 cycles

STRONG BURNING RUBBER ODOR COMBINED WITH MUSKY DIRTY SOCK ODOR. BURNING ODOR WENT AWAY AFTER TWO MINUTES, BUT MUSKY ODOR PERSISTED. NO SMOKE NOTICED. LANDED AT ORD. NO EMER DECLARED. C/A-REMOVED AND REPLACED ENGINE 2 OPS & LEAK CHECKS GOOD AIRCRAFT RETURN TO SERVICE.

Part: GASPER FAN — OVERHEATED (CABIN)

CMH - FLT 4154 - CREW GOT A LAV SMOKE DETECTOR INDICATION WITH ASSOCIATED SMOKE AND RETURNED BACK TO CMH. REPLACED GASPER FAN WITH OPERAITONAL. CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)

EICAS LAVATORY SMOKE INDICATION DURING CLIMB OUT. INSPECTED LAVATORY FOUND NO EVIDENCE OF SMOKE. REPLACED LAVATORY SMOKE DETECTOR IAW AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW21200501195)