N686AE

Part: DOUBLER — MECHANIC ERROR (ZONE 200) · airframe 51,994 hrs · 49,788 cycles

53-2524 - TOOL MARK ON REAR FUSELAGE UPPER SKIN AT FRAME 75 AND LH STR #2. REPAIRED IAW SRM 53-31-01 & EO1-53-24-0515.

Part: DOUBLER — CRACKED (ZONE 100) · airframe 51,994 hrs · 49,788 cycles

2 CRACKS FOUND ON SKIN AT FR75 BETWEEN STR 1R-1L UNDER REPAIR DOUBLER. PERMANENTE REPAIR PERFORMED AS PER ETD2024-145-019639.

Part: RIB — CRACKED (ZONE 300) · airframe 51,994 hrs · 49,788 cycles

VERTICAL STAB AFT OF SPAR 3 LOWER RIB CRACKED. INSTALLED NEW RIB IAW SRM 51-40-02.

Part: PLATE — CRACKED (ZONE 400) · airframe 51,994 hrs · 49,788 cycles

78-2176- FOUND LOOSE RIVETS ON INBD KICKER PLATE AND ACTUATION SYSTEM WARNING PLATE DAMAGED ON OUTBD KICKER PLATE AT LH ENGINE UPPER T/R DOOR.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 51,994 hrs · 49,788 cycles

AFT FUSELAGE BETWEEN THE FRAMES 57-58 ON RH, THE SKIN IS CORRODED FROM THE EXTERNAL AROUND THE POTABLE REFILL TUBE. REPAIRED IAW ETD2024-145-019512.

Part: ANGLE — CORRODED (RT TE FLAP) · airframe 51,994 hrs · 49,788 cycles

57-2177 - RH WING INBD FLAP LOWER SKIN, ROOT SPARE ANGLE CORRODED.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 51,994 hrs · 49,788 cycles

53-21388- CENTER FUSE III, LH OMEGA BEAM CRACKED FRAME 36 AND 37.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 51,994 hrs · 49,788 cycles

CENTER FUSE II, SHEAR CLIP CRACKED AT FRAME 27 BETWEEN STR 15R-16R.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 51,994 hrs · 49,788 cycles

CENTER FUSE II, LH OMEGA BEAM CRACKED AT FRAME 30 & 33.

Part: SUPPORT — CORRODED (ZONE 100)

53-2067- CENTER FUSELAGE II, LH SILL 3 BTW FRAME 29-35 FOUND CORRODED. REMOVED & REPLACED SILL 3 IAW SRM 51-40-02.

Part: GUSSET — CRACKED (ZONE 400) · airframe 51,994 hrs · 49,788 cycles

71-2109 - A GUSSET CRACKED ON RIGHT BESIDE AIR STARTER VALVE ACCESS DOOR AT R/H ENGINE LOWER COWLING.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 51,994 hrs · 49,788 cycles

53-2136 - WING STUB, CENTER OMEGA BEAM OUTBD ANGLE FOUND CRACKED.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 51,994 hrs · 49,788 cycles

CENTER FUSE II, LH OMEGA BEAM CRACKED AT FRAME 27 & FRAME 28.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 51,994 hrs · 49,788 cycles

CENTER FUSE II, SHEAR CLIP AT FRAME 24 BETWEEN STR 15R-16R FOUND CRACKED.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 51,994 hrs · 49,788 cycles

53-2082- CENTER FUSE II, CENTER OMEGA BEAM CRACKED AT FRAME 33.

Part: GUSSET — CORRODED (ZONE 100) · airframe 51,994 hrs · 49,788 cycles

CENTER FUSE II, LH GUSSET 3 BETWEEN FRAME 29-35 FOUND CORRODED.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 51,994 hrs · 49,788 cycles

CENTER FUSE II, CENTER OMEGA BEAM CRACKED AT FRAME 33.

Part: RIB — CRACKED (ZONE 600) · airframe 51,994 hrs · 49,788 cycles

53-2023 - RH WING AT RIB 9 LOWER SPLICE XIV CRACKED BTW TWO H-LOCK. REPAIRED IAW ETD2024-145-018993 & EO1-57-24-0423.

Part: SKIN — CRACKED (ZONE 500) · airframe 51,994 hrs · 49,788 cycles

57-222 - CRACK INDICATION FOUND IN TWO HOLES OF SPLICE ANGLE # XIV AT RIB #9 OF LH WING LOWER SKIN. REPAIRED IAW ETD2024-145-018999 & EO1-57-24-0424.

Part: UNKNOWN — ODOR (CABIN)

STRANGE ODOR REPORTED IN FWD CABIN BY FA IN DESCENT. ODOR DISAPPATED BUT RETURNED ON GROUND FACT 18MAY24 16:52 PHL RAN BOTH PACKS TO TRY AND DUPLICATE ODOR. COULD NOT DUPLICATE. UPON INSPECTION FOUND FWD 2 PAX L/H CABIN CEILING LIGHTS WERE BURNT ALONG WITH CORRESPONDING HARNESS. RAR LAMP, BALAST, AND HARNESS PER AMM 33-21-06

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,070 hrs · 40,081 cycles

ICE COND A/I INOP MSG ON EICAS ON RUNWAY. IAW EMB SNL 145-30-0009 PERFORMED A/I VLV OPS CHECK IAW EMB AMM 300000700803A OPS CHECK GOOD OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,045 hrs · 40,054 cycles

CA MFD INTERMITTENT IN FLIGHT. ABLE TO DUPLICATE PROBLEM BY TAPPING ON LIGHT CONTROL PANEL. FOUND BROKEN WIRE IN MFD DIMMER SWITCH. R & R CA LIGHT CONTROL PANEL IAW EMB 145 AMM 20-13-10 OPS CHECK GOOD. CA MFD NO LONGER INTERMITTENT A/C OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,045 hrs · 40,054 cycles

CA MFD INTERMITTENT ON TAKE OFF ROLL. R & R 200 CA MFD DISPLAY PER AMM 34-22-01 OPS CHECK GOOD PER AMM 34-22-00 A/C OK FOR SERVICE.

Part: SKIN — CRACKED (FRM 77 S6-7R) · airframe 41,169 hrs · 37,942 cycles

E949304 - EXTERNAL FUSELAGE SKIN IS CRACKED AT FRAME 77 STRINGERS 6R-7R .... PERFORMED SKIN BUSHING (.4375" BUSHING) REPAIR AT RIVET LOCATION ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 6R-7R IAW EMB-145 SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-22-0266.

Part: SKIN — CRACKED (FRM 77 S6-7L) · airframe 41,169 hrs · 37,942 cycles

EXTERNAL FUSELAGE SKIN IS CRACKED AT FRAME 77 STRINGERS 6L-7L. PERFORMED SKIN BUSHING (.4375" BUSHING) REPAIR AT RIVET LOCATION ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 6L-7L IAW SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-22-0267.

Part: SKIN — CRACKED (FRM 78 S3-4L) · airframe 41,169 hrs · 37,942 cycles

EXTERNAL FUSELAGE SKIN IS CRACKED AT FRAME 78 STRINGERS 3L-4L. PERFORMED SKIN BUSHING (.4375" BUSHING) REPAIR AT RIVET LOCATION ON EXTERNAL FUSELAGE SKIN AT FRAME 78 BETWEEN STRINGERS 3L-4L IAW SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-22-0267.

Part: SKIN — CRACKED (FRM 78 S3-4L) · airframe 41,169 hrs · 37,942 cycles

E949306 - EXTERNAL FUSELAGE SKIN IS CRACKED AT FRAME 78 STRINGERS 3L-4L .... PERFORMED SKIN BUSHING (.4375" BUSHING). REPAIR AT RIVET LOCATION ON EXTERNAL FUSELAGE SKIN AT FRAME 78 BETWEEN STRINGERS 3L-4L IAW EMB-145 SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-22-0267

Part: SKIN — CRACKED (FRM 77 S6-7L) · airframe 41,169 hrs · 37,942 cycles

E949305 - EXTERNAL FUSELAGE SKIN IS CRACKED AT FRAME 77 STRINGERS 6L-7L ....PERFORMED SKIN BUSHING (.4375" BUSHING) REPAIR AT RIVET LOCATION ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 6L-7L IAW EMB-145 SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-22-0267

Part: SKIN — CRACKED (FRM 77 S6-7R) · airframe 41,169 hrs · 37,942 cycles

EXTERNAL FUSELAGE SKIN IS CRACKED AT FRAME 77 STRINGERS 6R-7R. PERFORMED SKIN BUSHING (.4375" BUSHING) REPAIR AT RIVET LOCATION ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 6R-7R IAW SRM 53-32-01RE ITEM 9 FIGURE 213 AND EO1-53-22-0266.

Part: SKIN — DENTED (FRMS9-10 S20-21L) · airframe 41,169 hrs · 37,942 cycles

ACCOMPLISH PERMANENT REPAIR OF FUSELAGE SKIN DENT BETWEEN FR9 - 10, SL20L - 21L. ACCOMPLISHED PERMANENT REPAIR OF FUSELAGE SKIN DENT BETWEEN FR9 - 10, STR 20L - 21L IAW EMB 145 SRM 53--10-01RE, ITEM 6, FIG. 206 AND EO1-53-22-0265

Part: SUPPORT — CORRODED (GALLEY) · corrosion level 2 · airframe 41,169 hrs · 37,942 cycles

GALLEY, CORROSION FOUND ON THE RT FWD SILL AT 3 LOCATIONS BETWEEN FRAMES 18 - 20. R & R GALLEY SILL IAW SRM 51-40-02.

Part: SUPPORT — CORRODED (GALLEY) · corrosion level 2 · airframe 41,169 hrs · 37,942 cycles

E950007 - GALLEY, CORROSION FOUND ON THE RH FWD SILL AT 3 LOCATIONS BETWEEN FR18 - 20 .... RAR GALLEY RH FWD SILL IAW EMB145 SRM 51-40-02.

Part: YOKE — CRACKED (LT NACELLE) · airframe 41,169 hrs · 37,942 cycles

LEFT PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE HAS A RELEVANT INDICATION DURING HFEC ROTOR TEST INSPECTION. FREQ. 500KHZ, ANGLE 151.0 DEGREES, H-GAIN 86.7 DB, V-GAIN 66.1 DB, HP FILTER 400 HZ, LP FILTER 1600 HZ. EASI S/N 8958, 9081 .... INSTALLED SERVICEABLE REPAIR BUSHINGS AND PREPPED AND INSTALLED SERVICEABLE FASTENER AND WASHER ON LH PYLON FWD YOKE UPPER FLANGE AFT HOLE IAW ETD2022-145-036593 AND EMB SB145-54-0008. COMPLIED WITH EO1-54-22-0263

Part: GUSSET — CORRODED · corrosion level 2 · airframe 41,169 hrs · 37,942 cycles

CORROSION ON NR 1 CENTER BEAM GUSSET. REMOVED AND INSTALLED A SERVICEABLE GUSSET IAW SRM 51-40-02.

Part: GUSSET — CORRODED (CABIN) · corrosion level 2 · airframe 41,169 hrs · 37,942 cycles

E949912 - CORROSION ON # 1 CENTER BEAM GUSSET .... REMOVED AND INSTALLED SERVICEABLE #1 CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-02

Part: SEAT TRACK — CORRODED (FRMS 18-20) · corrosion level 2 · airframe 41,169 hrs · 37,942 cycles

GALLEY, CORROSION FOUND ON THE LT NR 1 LOWER SEAT TRACK, BETWEEN FR 18-20. REMOVED AND REPLACED THE SEAT TRACK AND SCREWS AND INSTALLED WASHERS WHERE THEY WERE MISSING IAW AMM 53-01-06.

Part: SEAT TRACK — CORRODED (FRMS 18-20) · corrosion level 2 · airframe 41,169 hrs · 37,942 cycles

GALLEY, CORROSION FOUND ON LH # 1 LOWER SEAT TRACK, BETWEEN FR 18-20 .... REMOVED AND REPLACED L/H #1 SEAT TRACK AND SCREWS AND INSTALLED WASHERS WHERE THEY WERE MISSING ON L/ H #1 SEAT TRACK IAW EMB 145 AMM 53-01-06. EASI# 7236

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 41,169 hrs · 37,942 cycles

CORROSION ON LT OTBD NR 2 FLOOR SILL. R & R THE FLOOR SILL IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 41,169 hrs · 37,942 cycles

E949909 - CORROSION ON LH OTBD # 2 FLOOR SILL .... RAR LH OUTBD #2 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 41,169 hrs · 37,942 cycles

CORROSION ON LH OTBD # 3 FLOOR SILL .... REMOVED AND REPLACED LH OUTBOARD #3 FLOOR SILL IAW EMB 145 SRM 51-20-03, 51-40-02 AND 51-40-09.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 41,169 hrs · 37,942 cycles

LEFT CABIN FLOOR SUPPORT NR 7 WAS CORRODED. R & R THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 41,169 hrs · 37,942 cycles

LEFT CABIN FLOOR SUPPORT NR 7 IS CORRODED. R & R LT CABIN FLOOR SUPPORT NR 7 IAW SRM 51-40-02.

Part: SPLICE — CORRODED (FRMS 23-24) · corrosion level 2 · airframe 41,169 hrs · 37,942 cycles

GALLEY, CORROSION FOUND ON THE CROSSBEAM SPLICE, BETWEEN FR 23- 24. R & R THE CROSSBEAM SPLICE, BETWEEN FR 23- 24 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 41,169 hrs · 37,942 cycles

CORROSION ON LT OTBD NR 3 FLOOR SILL. REMOVED AND REPLACED THE FLOOR SILL IAW SRM 51-20-03, 51-40-02 AND 51-40-09.

Part: SPLICE — CORRODED (FRMS 23-24) · corrosion level 2 · airframe 41,169 hrs · 37,942 cycles

GALLEY, CORROSION FOUND ON THE CROSSBEAM SPLICE, BETWEEN FR 23- 24 .... RAR GALLEY, CROSSBEAM SPLICE, BETWEEN FR 23- 24 IAW EMB 145 SRM 51-40-02.

Part: NOT REPORTED — NOT REPORTED · airframe 39,792 hrs · 36,273 cycles

PDIS 686 30-21 2573953 24JAN22 CLT ASSGN E1 A/I FAIL MSG FACT 22JAN22 01:20 ROA FOUND E1 A/I OVERPRESS MESSAGE ON CMC. R&R'D E1 PRES SURE TRANSDUCER IAW AMM 30-21-06-000/400-801-A. OPS CK SATISFACTORY. OK FOR SERVICE AT THIS TIME. CLEAR MEL.

Part: NONE — NONE · airframe 39,433 hrs · 35,838 cycles

PDIS 686 27-41 2395231 15NOV21 CLT CLOSE DECENTING THROUGH 12000 FEET. SPEED BRAKES DEPLOYED. TCS BUTTON PRESSED. IDLE THRUST. PTRIM MAIN INOP MSG WITH MATER CAUTION DISPLAYED. C/W QRH PTRIM MAIN MSG REMAINED. FACT 15NOV21 14:04 CLT REMOVED AND REPLACED HORIZONTAL STAB CONTROL UNIT I/A/W AMM 27-40-01. OPS CHECKS GOOD I/A/W AMM 27-40-00-700-802-A/500. NO MESSAGES ON EICAS AIRCRAFT OKAY FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (PITCH TRIM) · airframe 38,546 hrs · 34,864 cycles

PDIS 686 27-41 2396533 31MAY21 CLT CLOSE ON FINAL PITCH TRIM MAIN INOP MESSAGE APPEARED ON EICAS FACT 31MAY21 20:17 CLT PDPU CND C/W TASK 27-40-00-700-802-A AND 27-40-00-700-803-A NO DEFECTS NOTED OPS CHECK GOOD A/C OK FOR SERVICE

Part: WARNING MESSAGE — ILLUMINATED (ANTI-ICE SYSTEM) · airframe 38,531 hrs · 34,837 cycles

ON TAXI, ICE COND, NO ICE -A/ICE ON, ICE COND - A/I INOP, AND ENG REF A/I DISAGREE MESSAGES APPEARED ON EICAS WHILE A/I SET TO AUTO. C/W R&R FIM 73-25-00-810-836 FOUND TAKE OFF DATA A/ICE CONDITION ENTERED WAS NOT THE SAME AS A/ICE SWITCH POSITION. C/W A/ICE OPS CHECK IAW AMM 30-00-00 OK FOR SERVICE

Part: RELAY — MALFUNCTIONED (NR1 BLEED) · airframe 38,398 hrs · 34,690 cycles

BLEED 1 LOW TEMP AT CLIMB THRUST IN ICING CONDITIONS. R & R RELAYS K0537, K0173, K0528, AND K0552 IAW AMM 20-13-02. PERFORMED OPS CHECK IAW AMM 36-00-00. OPS CHECK GOOD AT THIS TIME. OK FOR SERVICE.

Part: PROXIMITY SWITCH — FAILED (MLG) · airframe 38,182 hrs · 34,455 cycles

AFTER T/O, LANDING GEAR WOULD NOT RETRACT. EICAS LG AIR/GND FAIL DISPLAYED. MESSAGE APPEARED FOLLOWING ROTATION. FOUND NLG WOW PROX SWITCH BAD. R&R'D PROX SWITCH IAW AMM 32-63-02. T/S IAW FIM 32-63-00-810-801-A. SWUNG GEAR SEVERAL TIMES. OPS CHECK GOOD. OKAY FOR SERVICE AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPS2) · airframe 37,900 hrs · 34,118 cycles

DURING T/O ROLL, SPS2 INOPERABLE EICAS WARNING MESSAGE. T/S IAW FIM 27-36-00-810-807A TO STEP 3. R & R SPC IAW 27-36-02/400. OPERATIONS CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,327 hrs · 33,454 cycles

LEFT HAND AFT FUSELAGE SKIN HAS POSSIBLE CRACK AROUND FASTENER AT FRAME 79 BETWEEN STR 6L-7L. REPAIRED IAW EO1-53-20-0152.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 37,327 hrs · 33,454 cycles

STRINGER 2L CRACKED AT RIVET HOLE JUST AFT OF FR 75. REPAIR IAW ETD2020-145-010123 AND EO1-53-20-0146.

Part: RIB — CRACKED (RT WING) · airframe 37,327 hrs · 33,454 cycles

RIGHT HAND WING RIB 21 IS CRACKED. REPAIRED IAW SRM 57-20-07 AND EO1-57-20-0159.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,327 hrs · 33,454 cycles

LEFT HAND AFT FUSELAGE SKIN HAS CRACK AROUND FASTENER AT FRAME 79 BETWEEN STR 3L-4L. REPAIRED IAW EO1-53-20-0152.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,327 hrs · 33,454 cycles

LEFT AFT FUSELAGE SKIN HAS CRACK AROUND FASTENER AT FRAME 79 BETWEEN STRINGER 4L AND 5L. REPAIRED IAW EO1-53-20-0152.

Part: FITTING — CRACKED (LT PYLON) · airframe 37,327 hrs · 33,454 cycles

LEFT HAND ENGINE PYLON FORWARD YOKE LOWER FORWARD FITTING CRACKED. REPAIRED IAW ETD2020-145-009605 AND EO1-54-20-0147.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 37,327 hrs · 33,454 cycles

SSI 53-30-03. FRAME 65 SHEAR CLIP CORRODED. REPAIRED IAW EO1-53-20-0138.

Part: DOOR FRAME — CHAFED (CARGO DOOR) · airframe 37,327 hrs · 33,454 cycles

CARGO DOOR WEB FRAME HAS 2 CHAFES AND ONE HOLE. REPAIRED IAW EO1-52-20-0141.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,327 hrs · 33,454 cycles

FRAME 73 IS CRACKED BETWEEN STR 17R-16R. REMOVED AND REPLACED FRAME 73 LOWER SECTION IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,327 hrs · 33,454 cycles

SSI 53-20-11 SERVICE DOOR CENTER SILL IS CORRODED AROUND FORWARD AND CENTER SCREW HOLES. INSTALLED NEW SERVICEABLE SERVICE DOOR CENTER SILL IAW SRM 51-40-02.

Part: HOUSING — CORRODED · airframe 37,327 hrs · 33,454 cycles

SPHERICAL BEARING HOUSING ON LH AND RH SIDES HAS CORROSION. REPAIRED SPHERICAL BEARING HOUSING CORROSION ON LH AND RH SIDES IAW PIEDMONT EO1-55-20-0131.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,327 hrs · 33,454 cycles

SSI 53-30-48. CARGO DOOR LOWER SILL CORRODED. REMOVED AND REPLACED CARGO LOWER SILL IAW SRM 51-40-02 AND 51-20-01.

Part: WIRE — BURNED (PITOT HEAT) · airframe 36,695 hrs · 32,758 cycles

PDIS 686 30-31 2088311 29OCT19 TRI CLOSE PITOT 3 INOP MESSAGE. FACT 29OCT19 03:29 TRI REPAIRED BURNT WIRE IAW IAW SWPM 20-21-00. INSTALLED NEW #3 PITOT-STATIC TUBE IAW AMM 34-13-02. LEAK CHE CK GOOD. HEATING OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,677 hrs · 32,734 cycles

NDIS 686 33-50 0016490 25OCT19 SBY CLOSE ROW 12BC EMERGENCY EXIT LIGHT ON SIDEWALL INOP 21611 00 CRH FACT 25OCT19 08:20 SBY R&R'ED EMERG LT. INVERTOR IRW AMM 33=50=11

Part: FAN — FAILED (CABIN AIR) · airframe 36,520 hrs · 32,549 cycles

PDIS 686 21-01 1894001 27SEP19 PHL CLOSE ODOR DETECTED IN COCKPIT AND CABIN WHILE IN FLIGHT FACT 27SEP19 17:20 PHL WHILE TROUBLESHOOTING ISSUES WITH FIM TASK 21-20-00- 810-801-A, NOTED ABNORMAL SMELL AND SOUND UNDER FLOO R AT ROW 15 AND AFT. R+R GASPER FAN IN REF TO AMM 21 -23-03. RAN PACK WITH APU AND ENGINES. NO STRANGE SM ELL OR ODOR NOTED. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,396 hrs · 32,410 cycles

EMERGENCY LIGHTS OVERWING ON LT AND RT SIDES AND EMERGENCY LIGHTS ON FLOOR STRIPS FROM SEATS 12A BACK TO 18A WILL NOT TURN ON. FIX: REMOVED AND REPLACED #400 BATTERY ASSY IAW AMM 33-50-04-04. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 36,396 hrs · 32,410 cycles

AFT F/A FLASHLIGHT IS NOT WORKING. FIX: REPLACED OLD BATTERY WITH NEW ONE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 36,188 hrs · 32,185 cycles

COCKPIT EMERGENCY LIGHT WONT ILLUMINATE. FIX: REMOVED AND REPLACED BULB IAW AMM TASK 33-50-05-000/400-801-A. OK FOR SERVICE.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 35,649 hrs · 31,549 cycles

686 33-20 0010830 09APR19 RIC CLOSE EMERGENCYH LIGHT AT SEAT 12C INOP 27625 00 NGR FACT 09APR19 08:42 RIC CLEANED AND RESEATED CONNECTORS ON EMERGENCY LIGHT A T SEAT 12C. OP CHECK GOOD. OK FOR SERVICE

Part: ANTI-ICE VALVE — FAILED (NR 2 ENGINE) · airframe 34,972 hrs · 30,774 cycles

PDIS 686 30-21 2096021 29NOV18 PHL ASSGN NO.2 ENGINE A/ICE FAILED INFLIGHT. SECURED E2 ANTI ICE VALVE IN LOCKED POSITION IAW 30-21-01-040-801-A VCTR HISTORY: NO HISTORY: FLT4860 SWAPPED TO 655 WHICH TOOK A 46 HISTORY: MINUTE DELAY. MEL 29NOV18 20:10 PHL C33316 30-8-1 ENGINE ANTI-ICING VALVES

Part: SIGN — INOPERATIVE (CABIN) · airframe 34,561 hrs · 30,291 cycles

EMERGENCY SIGN AT 18 ROW 15 RT SIDEWALL LITE OUT. R&R RT OVERWING EMERGENCY EXIT SIGN AT ROW 12. OPS CHECK GOOD COVER RESECURED W/ RETAINED HARDWARE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 34,555 hrs · 30,285 cycles

LARGE ILLUMINATED EMERGENCY EXIT PLACARD AT SEATS 12BC IS INOP. REMOVED LIGHT FRAME, REMOVED LIGHT ASSY. RE-SEATED ELECTRICAL CONNECTORS. VERIFIED CORRECT VOLTAGE FROM CONNECTORS AND REINSTALLED LIGHT ASSY. OPS CHECK GOOD.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 34,346 hrs · 30,029 cycles

INOP EMERGENCY EXIT LIGHT ON SIDEWALL AFT OF RT FUSELAGE EXIT. RESEATED CONNECTOR SP9104 AND S99105 FOR EMERGENCY LIGHT.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 34,342 hrs · 30,025 cycles

INOP EMERGENCY EXIT LIGHT ON SIDEWALL AFT OF RT FUSELAGE EXIT. RESEATED CONNECTOR SP9104 AND S99105 FOR EMERGENCY LIGHT.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,322 hrs · 30,003 cycles

E1 ANTI ICE FAIL EICAS MESSAGE ILLUMINATED AT 15000 FT ABOVE 10 DEGREES CELSIUS FOLLOWED BY NO ICE-A/ICE ON MESSAGE. COMPLIED WITH ENG TERMAL ANTI ICING SYSTEM AND ENG ANTI ICING VALVE OPS CHECK. OPS GOOD. NO DEFECTS NOTED IAW AMM 30-21-00-700-803A AND 30-21-00-700-804A.

Part: RELAY — FAILED (WARNING SYSTEM) · airframe 34,160 hrs · 29,814 cycles

T/O CONFIG WARNING, ABORT T/O. R&R RELAY K0212 IAW 21-51-00-810-804-1.

Part: PRESSURE SWITCH — MALFUNCTIONED (PARK BRAKE) · airframe 34,162 hrs · 29,815 cycles

TAKE OFF CONFIG WARNING ON ROLL OUT. NO AURAL WARNINGS. NO OTHER EICAS OR CMC MESSAGE. TROUBLESHOT THE TAKE OFF CONFIGURATION WARNING DISCREPANCY. R & R THE AWU IAW 31-51-01-000-801A AND R & R THE EMERGENCY PARK BRAKE PRESSURE SWITCH IAW 32-44-07-00-801A.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 32,973 hrs · 28,564 cycles

EMERGENCY LIGHT ON THE LT SIDE OF FUSELAGE JUST ABOVE PANEL 191EL INOPERATIVE. TROUBLESHOOTING THROUGH IAW FIM 33-50-00-810-804-A, FOUND A FAILURE OF THE BATTERY CHARGER. REPLACED THE BATTERY CHARGER, REPLACED THE POWER SUPPLY. BATTERY POWER SUPPLY TESTED GOOD IAW AMM 33-50-04.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,973 hrs · 28,564 cycles

EMERGENCY LIGHT ON CEILING PANEL 243ALC INOPERATIVE. R & R THE NR 1 POWER SUPPLY. THE POWER SUPPLY TESTED GOOD IAW AMM 33-50-04-700-801-A.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,970 hrs · 28,561 cycles

A DENT WAS NOTED ON THE RIGHT SIDE BEHIND SERVICE DOOR. -FABRICATED AND INSTALLED A REPAIR IAW SRM 53-21-01-RE, FIG 202,

Part: SUPPORT — CRACKED (FRAMES 47-48) · airframe 32,970 hrs · 28,561 cycles

RIGHT OTBD HAT BEAM, OTBD SUPPORT HAS A 1/2 INCH CRACK BETWEEN FRAMES 47 AND 48. COMPLIED WITH A AFT SUPPORT REPLACEMENT AW SRM 53-23-02.

Part: SUPPORT — CRACKED (WNG TO BDY) · airframe 32,970 hrs · 28,561 cycles

LEFT WING TO FUSELAGE UPPER SUPPORT CRACKED BETWEEN FRAMES 50 AND 51. REPAIRED THE FAIRING SUPPORT IAW SRM 53-23-12

Part: ANGLE — CRACKED (LT WING) · airframe 32,970 hrs · 28,561 cycles

LEFT WING TO FUSELAGE FAIRING LOWER FORWARD SUPPERT CRACKED-C/A-REPAIRED LH WING TO FUSELAGE FWD LOWER SUPPORT IAW ETN-EM-53-142, REF NRWC E600132 FOR LEAK CHECK OF FASTNERS INTO FUEL TANK.

Part: STRINGER CLIP — CRACKED (FRAME 61) · airframe 32,970 hrs · 28,561 cycles

FRAME 61, STRINGER CLIP 7R HAS A CRACK, 1/2 INCH LONG. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02, 51-30-02, AND 53-31-04

Part: FITTING — DAMAGED (RUDDER) · airframe 32,970 hrs · 28,561 cycles

RUDDER MID UPPER HINGE FITTING, LOWER HAT BUSHING BORE DIMENSIONAL CHECKED BAD. REPLACED THE FITTING IAW SRM 55-40-02, AND ETN EM-55-070

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,957 hrs · 28,544 cycles

AFT CABIN CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED AFT INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 32,688 hrs · 28,268 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 32,527 hrs · 28,105 cycles

FLASHLIGHT CRADLE CRACKED. REMOVED AND REPLACED AFT FLASHLIGHT AND CRADLE ASSEMBLY IAW AMM 33-50-16-04. OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 31,088 hrs · 26,850 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY, OPS CHECKED GOOD, IAW AMM 33-50-10

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 31,088 hrs · 26,850 cycles

EMERGENCY LIGHTS INOPERATIVE AT ROW 17 AND 18. REPAIRED THE LIGHT WIRE SPLICE SP9212 IAW SWPM 20-21-00. OPS CHECKED GOOD IAW AMM 33-50-00

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 30,180 hrs · 26,063 cycles

COCKPIT FLASHLIGHT INOPERATIVE. R & R CAPTAIN FLASHLIGHT IAW AMM 33-50-06.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,104 hrs · 25,986 cycles

1 FLOOR EMER LIGHT STRIP, BETWEEN 3A & 4A IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOOR PROX FLOOR STRIP IAW EMB 145 AMM 33-50-12 CW EMERGENCY FLOOR PROXIMITY FLOOR STRIP OPS CHECK IAW W/C 33-700-17 OPS CHECK GOOD RESTORED MEL.

Part: WIRE — BROKEN (CABIN) · airframe 30,005 hrs · 25,899 cycles

EMERGENCY LIGHT INOPERATIVE ON SERVICE DOOR. REPAIRED BROKEN WIRES ON SERVICE DOOR EMERGENCY LIGHT ASSEMBLY IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: CHARGER — FAILED (CABIN) · airframe 29,886 hrs · 25,801 cycles

DURING PS 1 INSPECTION, FOUND FWD EMER LIGHTS INOPERATIVE. R & R NR 2 EMER BATTERY & CHARGER IAW AMM 33-50-04. OPERATIONS CHECK FAILED ON ONE EMER FLOOR STRIP IAW MEL 33-30. EMER LIGHTING BATTERY PN 2013-1A & SN 109939.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 28,846 hrs · 24,793 cycles

FIRST OFFICERS FLASHLIGHT CHARGING CRADLE IS BROKEN, WILL NOT HOLD FLASHLIGHT IN PLACE. REPLACED FLASHLIGHT ASSEMBLY IAW 33-50-16.

Part: GENERATOR — MALFUNCTIONED (NR 3) · airframe 28,794 hrs · 24,741 cycles

AFTER STARTING ENG 2, ON TAXI OUT EICAS DISPLAYED GEN 3 OFF BUS, GEN 3 INDICATED 32.5V & 0 AMPS. TROUBLESHOT NR 3 GEN OFF BUSS EICAS MSG IAW FIM 24-31-00-810-807-A. R & R NR 3 MAIN GEN IAW WC 24-800-00. OPERATIONS CHECK & LEAK CHECKED GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,389 hrs · 24,339 cycles

DURING IMBV INSPECTION, QA FOUND THE SERVICE DOOR CTR SILL CORRODED. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. R & R THE SERVICE DOOR CTR SILL IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,389 hrs · 24,339 cycles

DURING IMBV INSPECTION, QA FOUND THE CARGO DOOR SILL CORRODED. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. R & R THE CARGO DOOR SILL IAW SRM 51-40-02.

Part: ROLLER — DAMAGED (FUSELAGE) · airframe 28,131 hrs · 24,090 cycles

MAIN DOOR IS DIFFICULT TO OPEN & CLOSE. REMOVED & REPAIRED UPPER AFT MAIN DOOR FRAME ROLLER IAW AMM 53-21-02. OPERATIONS CHECKED GOOD IAW AMM 52-10-01.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 28,133 hrs · 24,092 cycles

MAIN DOOR IS STILL DIFFICULT TO OPEN & CLOSE. APPEARS TO STICK, HANDLE, LAST PART OF CLOSING. ADJUSTED TOP ROLLERS IAW AMM 52-18-00-820-805-A.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 27,046 hrs · 23,128 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW 33-50-16. OPERATIONS CHECKED GOOD.

Part: HOLDER — DAMAGED (FLASHLIGHT) · airframe 26,743 hrs · 22,891 cycles

CAPTAIN'S FLASHLIGHT HOLDER IS DAMAGED. R & R CAPTAIN'S FLASHLIGHT HOLDER BASE. OPERATIONS CHECKED GOOD IAW AMM 33-50-16.

Part: PROXIMITY SWITCH — FAILED (LT MLG) · airframe 26,069 hrs · 22,338 cycles

ON GEAR RETRACT, LT GEAR DID NOT SHOW IN TRANSIT & WENT IMMEDIATELY TO UP. RETURNED GEAR LEVER TO DOWN & VERIFIED ALL GEAR SHOWED NORMAL TRANSITION. LEFT MAIN WAS MUCH SHORTER TRANSIT TO DN INDICATION. PERFORMED FLYBY & GEAR CONFIRMED DOWN. LANDED & TAXIED IN WITH NO ISSUES. R & R LT LG UPLOCK PROXIMITY SWITCH NR 1 & 2 IAW AMM 32-61-01. OPERATIONS CHECKED GOOD. EXTENSION & RETRACTION FOUND SATISFACTORY IAW AMM 32-30-00. PROXIMITY SENSOR PN 80-057-01 SN 35145.

Part: BATTERY PACK — FAILED (CABIN) · airframe 24,998 hrs · 21,314 cycles

REPLACE BATTERY PACK NR 4 AE WC 33-700-19 DUE IAW BOW. R & R BATTERY PACK NR 4 IAW AE WORK CARD 33-700-19, OPERATIONS CHECKED GOOD.

Part: VHF COMM — FAILED (NR 1) · airframe 24,736 hrs · 21,122 cycles

AFTER ITEM NR 1 RTG WITH MTX ON BOARD APU RUNNING. STRONG SMELL OF ELEC BURNING, SMELL IN COCKPIT, CABIN ON JET BRIDGE. R & R NR 1 COMMUNICATION UNIT IAW AMM 23-00-01, OPERATIONS CHECKED GOOD SEE ABOVE ITEM NR 1 OF THIS LOG PAGE FOR CORRECT ACTION.

Part: PROXIMITY SWITCH — FAULTY (LT MLG) · airframe 24,547 hrs · 20,976 cycles

NUMBER 12K' LEVEL 310 KTS BOTH CAPTAIN & FLIGHT OFFICER FELT & HEARD LOUD THUD. ALL INDICATIONS NORMAL, DECLARED EMERGENCY. R & R UPPER & LOWER LT MLG UP LOCK PROXIMITY SWITCH IAW AMM 32-61-01.

Part: LIGHT — CRACKED (CABIN) · airframe 24,138 hrs · 20,648 cycles

RT CABIN EMERGENCY LIGHT CRACKED. REPLACED IAW AMM 33-50-12.

Part: LIGHT — BROKEN (CABIN) · airframe 24,138 hrs · 20,648 cycles

CABIN FLOOR EMERGENCY LIGHT BROKEN. R & R EMERGENCY LIGHT IAW AMM 33-50-12 AND 20-10-01.

Part: LIGHT — CRACKED (CABIN) · airframe 24,138 hrs · 20,648 cycles

CABIN EMERGENCY LIGHTS CRACKED. R & R LIGHT IAW AMM 33-50-12.

Part: LIGHT — FAILED (SEATS 4C & 4B) · airframe 23,999 hrs · 20,523 cycles

DURING MX INSPECTION, OVERHEAD LIGHT HAD ELECTICAL ODOR AND WENT AWAY AFTER TURNING LIGHTS OFF. PERFORMED OPS CHECK OF CABIN LIGHTS AND READING FOR 40 MINUTES, NO ODOR OR SMOKE NOTED. FOUND READING LIGHTS AT 4C AND 4B INOPERATIVE. R & R CIRCUIT BOARD FUSES AT 4C IAW AMM 33-25-04, OPS CHECKED GOOD. R & R THE READING LIGHT ASSY, FOUND THAT REFLECTOR WAS BURNED IAW AMM 25-28-48. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,981 hrs · 20,503 cycles

LINGERING ODOR OF SMOKE IN CABIN. UNSURE OF SOURCE. INSPECTED CABIN LIGHT UPPER NO SMOKE ODOR.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,980 hrs · 20,502 cycles

OVERHEAD LIGHTS HAD ELECTRICAL ODOR, WENT AWAY AFTER TURNING LIGHTS OFF. NR 1 BALLEST IS ENERGIZE AND WORKING. INSPECTED CABIN LIGHTS, NO SMOKE ODOR IN CABIN. PERFORMED GVI OF CABIN LIGHTING, NO SHORTING OR ARCHING PRESENT NO ELECTRICAL ODOR NOTED CABIN LIGHTING.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 23,929 hrs · 20,452 cycles

DURING CLIMBOUT, CABIN PRESSURE CLIMBED RAPIDLY. SWITCHED TO MANUAL PRESSURE MODE ACFT STILL DIDN`T PRESSURIZE. DECLARED EMERGENCY AND LANDED WITHOUT EVENT. FOUND DIGITAL PRESSURE CONTROLLER TO READ ERRATICALLY AND MANUAL BUTTON WOULD NOT STAY DEPRESSED. R & R DIGITAL PRESSURE CONTROLLER IAW AMM 21-31-01, OPC GOOD IN MANUAL AND AUTO IAW AMM 21-31-00-700-801-A AND 21-31-00-700-802-A.

Part: ACTUATOR — FAILED (TE FLAP) · airframe 22,962 hrs · 19,682 cycles

THE CREW REPORTED THAT WHILE OPERATING FLAPS, FLAPS FROZE AT 27 DEGREES WITH SIMULTANEOUS "FLAP FAIL" MFD MESSAGE AND "FLAP RT TRANSMISSION FAIL" CMC MESSAGE. LOUD GRINDING NOISE WHEN DEPLOYING FLAPS FROM 9 TO 22 DEGREES, APPROX 180 KTS. THE ACFT WAS REMOVED FROM SERVICE. R & R THE RT WING OTBD FLAP TIP ACTUATOR. R & R THE VELOCITY SENSOR IAW AMM 27-51-12, PN 3633501003, SN 05565. REPLACED RETAINING RING: PN CA18203 AND COTTER PIN, PN MS24665-151. THE OPS CHECK WAS GOOD IAW 27-51-10. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 22,876 hrs · 19,609 cycles

DURING UNSCHEDULED MAINTENANCE INSPECTION FOUND THE ELT BATTERY REQUIRES REPLACEMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ELT BATTERY IAW EMB145 AMM CHAPTER 25-61-04. NEW BATTERY EXPIRATION DATE IS APR/2018. THE BATTERY CHECK WAS GOOD IAW WC#: 25-700-07. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 22,325 hrs · 19,165 cycles

ON FLIGHT 3354 THE CREW REPORTED THAT A FEW SECONDS AFTER ROTATION THE FLIGHT ATTENDANT CALLED TO SAY SHE THOUGHT THERE WAS SMOKE IN THE CABIN AS SHE CALLED THE CREW GOT LAV SMOKE WARNING. COMPLETED THE CHECK LIST SHORTLY AFTER LANDING EICAS WARNING WENT OUT AND THE FLIGHT ATTEDNANT CALLED TO SAY SMOKE HAD CLEARED. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NR 2 ENGINE IAW WORKCARD 71-000-00 AND ACCOMPLISHED ETN-EM-72-034. LEAK AND OPS CHECK NORMAL, NO ABNORMAL SMELLS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 20,980 hrs · 18,122 cycles

ON FLIGHT 2731 THE CREW REPORTED THE FLIGHT ATTENDANT’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT’S FLASHLIGHT ASSEMBLY IAW GENERAL MAINTENANCE PRACTICES. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (ROW 9) · airframe 20,748 hrs · 17,947 cycles

DURING MAINTENANCE INSPECTION, FOUND ROW 9 FLOOR EMERGENCY LIGHT STRIP INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ROW 9 FLOOR PROXIMITY LIGHT STRIP IAW AMM TASK 33-50-12-000-801-A AND 33-50-12-400-801-A. AIRCRAFT RETURN TO SERVICE.

Part: HOLDER — INOPERATIVE (COCKPIT) · airframe 20,163 hrs · 17,480 cycles

DURING B INSPECTION, FOUND THE CAPTAIN’S FLASH LIGHT HOLDER INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASH LIGHT HOLDER ASSEMBLY IAW EMB AMM TASKS 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS NORMAL AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUT — LOW (NLG) · airframe 19,460 hrs · 16,918 cycles

FOR FLIGHT 2963 MAINTENANCE REPORTED THAT DURING APPROACH THE CREW RECEIVED A LANDING GEAR/AIR GROUND FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AICRAFT WAS REMOVED FROM SERVICE. SERVICED NOSE LANDING GEAR STRUT IN ACCORDENCE WITH EMB 145 AMM 32-20-01. REMOVED GEAR PINS IAW EMB 145 AMM 32-00-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,005 hrs · 16,557 cycles

DURING MAINTENANCE BASE VISIT FOUND THE GALLEY CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY CEILING EMERGENCY LIGHT IAW AMM TASKS 33-50-09-000-801-A AND 33-50-09-400-801-A. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (CABIN) · airframe 18,940 hrs · 16,509 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FORWARD FLIGHT ATTENDANT FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT’S FLASHLIGHT CRADLE ASSY IAW EMB 145 AMM TASKS 33-50-16-000-801-A & 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,620 hrs · 13,373 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE WASTE DRAIN VALVE SUPPORT INSIDE ACCESS DOOR 272AR TO BE CORRODED. THE ACFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DRAIN SUPPORT IAW SRM51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — LEAKING (RT ENGINE) · airframe 8,492 hrs · 8,035 cycles

ON FLIGHT 4111, CREW REPORTED LAV SMOKE DETECTOR AND SMOKE ODOR DURING CLIMB-OUT. REMOVED AND REPLACED "0" CARBON SEAL ON RT ENG IAW MM 72-25-25. PERFORMED SEVERAL HIGH POWER RUN IAW MM 72-00-00. RAN PACKS NR 1 AND 2 OFF BLEED ALL CHECK GOOD. NO SMOKE OR ODOR WITNESSED. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — ODOR (NR 1)

STRONG OIL ODOR IN CABIN WITH BOTH PACKS ON. MAINTENANCE FOUND OIL IN THE NR 1 ENGINE EXHAUST. REPLACED NR 1 ENGINE IAW W/C 72-000-00. OPS CHECK GOOD, LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)