N636AE

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 54,067 hrs · 52,165 cycles

MAIN DOOR EMERGENCY LIGHT INOP. RAR LIGHT ASSY IAW AMM 33-50-06

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 53,913 hrs · 51,965 cycles

EMERGENCY LIGHT SYSTEM NOT ILLUMINATING. R & R THE EMERGENCY LIGHT BATTERY PACK IAW AMM33-50-04-000/400-801-19.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 53,913 hrs · 51,965 cycles

EMERGENCY LIGHT SYS NOT ILLUMINATING. R & R EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-04-000/400-801-A.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 53,913 hrs · 51,965 cycles

EMERGENCY LIGHT SYS NOT ILLUNINATING. R & R THE BATTERY IAW AMM 33-50-04-000/400-801-A.

Part: DOOR — NICKED (ZONE 100) · airframe 53,913 hrs · 51,965 cycles

NICK ON AFT AVIONICS DOOR. REPAIRED IAW EO 1-53-24-0332

Part: REPAIR — NONE · airframe 53,913 hrs · 51,965 cycles

TEMP REPAIR INSTALLED ON AFT FUSELAGE PER EO1-53-25-0319. R & R REPAIR IAW EO 1-53-25-0325

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 53,306 hrs · 51,251 cycles

CABIN AISLE ROW 12 CIELING EMERGENCY EXIT LIGHT INOP ON FWD SIDE. RAR LIGHT ASSY IAW AMM 33-50-15

Part: NONE — NONE (NONE) · airframe 51,994 hrs · 49,788 cycles

UNRECORDED REPAIR FOUND ON L/H OMEGA BEAM BTW FR 22-23.

Part: NONE — NONE (NONE) · airframe 51,994 hrs · 49,788 cycles

UNRECORDED REPAIR FOUND ON L/H OMEGA BEAM BTW FR 49-50.

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

ELEVATOR INNER LEADING EDGE UPPER SKIN BTW YH=1280.0 AND AT HINGE CUT OUT FOUND DENTED.

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

AT FR61 LH DOUBLER UNDER CARBON FRAME FOUND CORRODED.

Part: SKIN — CRACKED (ZONE 200)

RF1, LH SIDE OF FR68 FOUND CRACKED UNDER CARGO DOOR HOLDER FITTING.

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

GOUGE IN HOLE OF L/H WING LOWER SKIN, AT SPLICE ANGLE XIV, RIB #9, 6.5 FROM FWD SKIN EDGE.

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

FOLLOWING NDT INSPECTION, CRACK INDICATION FOUND IN R/H WING TORQUE BOX #1 AT SPAR 3, FORMOST OUTBD INNER HOLE.

Part: TRUNNION — CRACKED (ZONE 700) · airframe 51,994 hrs · 49,788 cycles

LH MLG AFTUPPER TRUNION CRACKED.

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

RF1, L/H SILL BTW FR60-63 CORRODED.

Part: BRACKET — CRACKED (ZONE 200) · airframe 51,994 hrs · 49,788 cycles

FWD FUSELAGE II, BRACKET LATERAL UPPER MOUNTING FOUND CRACKED.

Part: REPAIR — NOT ENTERED (ZONE 100) · airframe 51,994 hrs · 49,788 cycles

UNRECORDED PATCH BTW FR24-25 AND BTW STR18L-20L.

Part: REPAIR — NOT ENTERED (ZONE 100) · airframe 51,994 hrs · 49,788 cycles

AT FR 10, BTW STR 20L-21L UNRECORDED ROUND PATCH FOUND.

Part: SUPPORT — CRACKED (ZONE 200) · airframe 51,994 hrs · 49,788 cycles

CENTER FUSELAGE I, RH SILL BTW FRAME 20-18 FOUND CORRODED.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 51,994 hrs · 49,788 cycles

CENTER FUSELAGE I, LH OMEGA BEAM, INBD ANGLE SPLICE BTW AFT AND FWD DIGITAL FOUND CRACKED.

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

BOTTOM OF VERT STAB FWD OF FRONT SPAR 1, BOTH LIPS CHAFED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 51,994 hrs · 49,788 cycles

RH SIDE ON BULKHEAD 80, SHEAR CLIP CRACKED BETWEEN STR 5 & STR 7.

Part: SKIN — CRACKED (ZONE 300) · airframe 51,994 hrs · 48,788 cycles

VERT STAB AFT OF SPAR 3 LH SKIN UPPER PROFILE CRACKED.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 51,994 hrs · 49,788 cycles

CENTER FUSELAGE I, LH OMEGA BEAM, INBD FLANGE CRACKED FRAME 23-22-21.

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

CENTER FUSE IV, RH GUSSET BTW FRAME 59-61 FOUND CORRODED.

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

CENTER FUSELAGE IV, SHEAR CLIP CRACKED AT FRAME 58 BTW STR 15L-16L.

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

LH SIDE AT FRAME 46 CLOSING ANGLE BRACKET FOUND CRACKED JUST UNDER FLOOR LEVEL.

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

CF3, WING TO FUSELAGE FAIRING RH AFT WHEELWELL RIB FOUND CRACKED.

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

RF1 BTW FR65-68, BEAM LOWER FRAME CARGO DOOR, FOUND CORRODED.

Part: ANTI-ICE SYSTEM — FAILED (NR 2 ENGINE) · airframe 51,861 hrs · 49,646 cycles

E2 ANTI ICE FAIL. CW MX PROCEDURE. MEL 25MAY24 10:25 PHL C14602 30-8-1 ENGINE ANTI-ICE. FACT 28MAY24 02:00 PHL T/S IRW FIM 30-21-00-810-804-A, FOUND CONNECTOR P0973 WOULD NOT SEAT, HAD DAMAGED SHIELDING. R&R CONNECTOR IRW SWPM 20-50-00. RAN E2 AND PERFORMED OPS CHECK. OPS CHECK GOOD, OK FOR SERVICE. CLEAR MEL 30-8-1

Part: SUPPORT BRACKET — CRACKED (ZONE 100)

784- TEMP REPAIR IAW EO1-53-21-0254 & ETD2021-145-030320 PERFORMED AT TAT:47747 & TAC: 44977 REQUIRES REPLACE OF PART (145-21873-007) AT FRAME 73 SUPPORT BRACKET AT STR 16R AT OR BEFORE 5000FC.

Part: PUMP — FAILED (NR 1) · airframe 51,560 hrs · 49,301 cycles

E1 HYD PUMP FAIL ON EICAS. R&R'D #1 EDP IAW AMM 29-10-04. OPS CHECK GOOD. LEAK CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,060 hrs · 47,605 cycles

MAIN PTRIM INOP ON EICAS ON CLIMBOUT. FOUND HSCU FAULT ON CMC. FOLLOWED FIM 27-43-00-810A STEP 6. R+R HSCU IAW AMM 27-40-01. OPS CHECK IAW AMM 27-40-00-700-802A. OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: ANTI-ICE SYSTEM — FAULTED (NR 2 ENGINE) · airframe 49,602 hrs · 47,102 cycles

RETURN TO FIELD DUE TO ENG 2 ANTI ICE FAIL AT APPROX 14,000 FT WITH BLEED 1 OVERTEMP MESSAGE AND THEN SHORTLY AFTER WING ANTI ICE FAIL MESSAGE. R & R ENGINE PRESSURE TRANSDUCER IAW AMM 30-21-06-04. OPS CHECK IAW AMM 30-21-00-700-803-A. ENGINE THERMAL A/I SYSTEM OPERATIONAL CHECK, SB 145-30-0022. NO CMC MESSAGES PRESENT AT THIS TIME. A/C OK FOR SERVICE AT THIS TIME.

Part: NONE — NONE · corrosion level 3 · airframe 47,747 hrs · 44,977 cycles

E879831 - RH ENGINE PYLON FWD YOKE UPPER AFT JO-BOLT HOLE DAMAGED. (LOCATED AT OUTBD EDGE OF PYLON UPPER SKIN). .... REPAIRED RH ENGINE PYLON FWD YOKE UPPER AFT JO-BOLT HOLE IAW SB 145-54-0008 AND EO1-54-21-0258. SEE WIPS AND TASKS FOR DETAILS.

Part: NONE — NONE · corrosion level 2 · airframe 47,747 hrs · 44,977 cycles

E881864 - FOUND ADDITIONAL CORROSION ON L/H #1 CABIN FLOOR SILL (MARKED. .... RAR L/H #1 CABIN FLOOR SILL IAW EMB145 SRM 51-40-02.

Part: NONE — NONE · airframe 47,747 hrs · 47,747 cycles

E878508 - INVESTIGATE POSSIBLE SKIN CRACKS AROUND FASTENERS (2EA) AT FR 78 BETWEEN STGRS 04R/07R .... PERFORMED DYE PENETRANT INSPECTION IAW EASI NDTM RELEVANT INDICATION NOTED .... FURTHER INVESTIGATION FOUND 1 CRACK LOCATED ON FR 78, 1" BELOW STR 06R. REPAIRED CRACK IAW EMB SRM 53-32-01 AND EO1-53-21-0260.

Part: NONE — NONE · corrosion level 2 · airframe 47,747 hrs · 44,977 cycles

E879830 - LH ENGINE PYLON FWD YOKE UPPER AFT JO-BOLT HOLE DAMAGED. (LOCATED AT OUTBD EDGE OF PYLON UPPER SKIN). .... LH ENGINE PYLON FWD YOKE UPPER AFT JO-BOLT HOLE DAMAGED. (LOCATED AT OUTBD EDGE OF PYLON UPPER SKIN)

Part: NONE — NONE · corrosion level 2 · airframe 47,747 hrs · 44,977 cycles

E879601 - LH AND RH SERVO TAB FAIL SAFE ROD FWD PIN RETENTION DEVICE CORRODED (AT ELEVATOR INTERNAL SIDE). .... RAR LH AND RH SERVO TAB FAIL SAFE ROD FWD PIN RETENTION TAB IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 47,747 hrs · 44,977 cycles

E879384 - RH CABIN FLOOR SILL #6 CORRODED .... REMOVED AND REPLACED : RH CABIN FLOOR SILL #6 IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 47,747 hrs · 44,977 cycles

E879338 - DIAMOND GUSSET HAS CORROSION AT FRAME 20 .... REMOVED AND REPLACED DIAMOND GUSSET AT FRAME 20 IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 47,747 hrs · 44,977 cycles

E879397 - RH CABIN FLOOR SILL #5 CORRODED .... REMOVED AND REPLACED R/H #5 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · airframe 47,747 hrs · 47,747 cycles

E879260 - RFR 66 HAS CRACK ON INBD RADIUS AT STR 16R. .... REPAIRED FR 66 ON INBD RADIUS AT STR 16R IAW EO1-53-21-0249.

Part: NONE — NONE · corrosion level 2 · airframe 47,747 hrs · 44,977 cycles

E879381 - LAVATORY RH GUSSET CORRODED .... RAR LAVATORY RH GUSSET IAW EMB 145 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 47,747 hrs · 44,977 cycles

E879335 - GALLEY FWD DIGITAL HAS CORROSION .... PERFORMED DOUBLER REPAIR OF GALLEY FWD DIGITAL IAW EMB 145 SRM 53-21-10RE, ITEM 2, FIG 201 SHEET 5 AND EO1-53-21-0263.

Part: NONE — NONE · corrosion level 2 · airframe 47,747 hrs · 44,977 cycles

E879385 - LH CABIN FLOOR SILL #7 CORRODED .... REMOVED AND REPLACED : LH CABIN FLOOR SILL #7 IAW EMB 145 SRM 51-40-02.

Part: NONE — NONE · airframe 47,747 hrs · 47,747 cycles

E879334 - PAX DOOR AFT ENTRANCE FLOORBOARD SUPPORT HAS CORROSION. .... REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE PAX DOOR AFT ENTRANCE FLOORBOARD SUPPORT IAW EMB145 SRM 51-40-02.

Part: NONE — NONE · airframe 47,747 hrs · 47,747 cycles

E879202 - RIGHT HAND VERTICAL STABILIZER SPHERICAL BEARING HOLE IS ENLARGED PAST ORIGINAL DIAMETER NEED TO BE ENLARGED TO FIRST OVERSIZE. .... RIGHT HAND VERTICAL STABILIZER SPHERICAL BEARING HOLE IS ENLARGED TO FIRST OVERSIZE IAW PIEDMONT EO1-55-21-0248.

Part: NONE — NONE · airframe 47,747 hrs · 47,747 cycles

E878917 - STRINGER 19R GOUGED AFT OF FRAME 52 .... REPAIRED STRINGER 19R AFT OF FRAME 52 IAW PIEDMONT EO1-53-21-0256

Part: NONE — NONE · airframe 47,747 hrs · 47,747 cycles

E878971 - BAGGAGE DOOR WEBBING IS GOUGED 6 EACH AT PREVIOUS REPAIRS. .... COMPLIED WITH PIEDMONT EO1-52-21-0250 FOR 1 GOUGE AT FORWARD LOWER CORNER AND FOUND OTHER 5 WITHIN ALLOWABLE LIMITS IAW EMB 145 SRM 52-30-01

Part: NONE — NONE · airframe 47,747 hrs · 47,747 cycles

E878978 - SSI 52-30-08 CORROSION BAGGAGE DOOR LOWER FWD WEBBING PREVIOUS REPAIR. .... INSTALLED AND EDGE SEALED REPAIR DOUBLER IAW EO1-52-21-0251.

Part: COMPRESSOR — MAKING METAL (NR 2 ENGINE) · airframe 47,600 hrs · 44,825 cycles

DURING CLIMB OUT WITH N1 AROUND 91%. LOUD BANG HEARD FROM ENGINE #1 FOLLOWED QUICKLY BY ENGINE SHUTDOWN. PERFORMED GVI OF #1 ENGINE. FOUND METAL FOD IN FIRST STAGE COMPRESSOR SECTION, WITH DAMAGE TO MULTIPLE INLET GUIDE VANES. NO OBVIOUS DAMAGE OR BIRD STRIKE OCCURRENCE TO WING OR FUSELAGE... ENGINE CHANGE IN PROGRESS

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (WING) · airframe 45,780 hrs · 42,844 cycles

WG A/ICE FAIL FOR 10 SECONDS EVERY TIME ENTERING ICE CONDITION. PERFORMED ANTI ICING SYSTEM FUNCTIONAL CHECK IN REF TO AMM 30-00-00-800-804A FOUND #1 ANTI ICE VALVE TO BE FAULTY.R/R #1 ANTI ICE VALVE IN REF TO AMM 30-11-01-000/400-801A. PERFORMED ANTI ICING SYSTEM CHECK IN REF TO AMM 30-00-00-700-802A OPS CHECK GOOD AT THIS TIME OK FOR SERVICE CLEAR MEL.

Part: POTENTIOMETER — FAILED (FEEDBACK UNIT) · airframe 44,959 hrs · 41,945 cycles

WITH TILLER ENGAGED UNCOMMANDED STEERING TO LEFT AND RIGHT WITH NOTED CLICKING AND GRINDING SOUND HEARD. REPLACED FEEDBACK UNIT (POTENENTIOMETER) IAW 30-50-07 PERFORMED COMPLETE ADJUSTMENT IAW AMM 32-50-00-700-804/500. TAXI CHECK NO FIX. REPLACED STEERING HANDLE WHEEL IAW 32-50-01 OPS CHECK GOOD,OPS CHECK TAXI CHECK GOOD. RETURN TO SERVICE

Part: CONTROL VALVE — MALFUNCTIONED (DUEL TEMP) · airframe 44,169 hrs · 41,021 cycles

PDIS 636 21-60 1938091 29MAR19 PWM CLOSE PACK 2 AUTO TEMP CONTROL UNRESPONSIVE TO PILOT CONTR OLS. MANUAL DOES NOT PROPERLY CONTROL TEMP. MANUAL O NLY EFFECTIVE AT 9 OCLOCK OR LESS POSITION. FACT 30MAR19 11:19 PHL R&R DUAL TEMP CONTROL VALVE IAW AMM 21-60-01 OPS CHE CK GOOD CLEAR MEL 21-15-3

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 44,047 hrs · 40,892 cycles

NDIS 636 22-99 0023230 09MAR19 PHL CLOSE **** THIS DISCREPANCY CREATED FOR MIR PURPOSES **** CREW PREVIOUSLY HAD ISSUE WITH OH BIN PRIOR TO DEPARTURE. CREW C/W MEL PROCEDURE. THEN CREW ABORTED T/O FOR AUTOPILOT MSG AT TAKEOFF, CREW RESET SYSTEM ALL SYSTEMS OPS NORM AND CONTINUE W/NO ISSUES. FACT 09MAR19 18:31 PHL THIS DISCREPANCY CLOSED. MIR CREATED.

Part: INVERTER — FAULTY (CABIN) · airframe 40,866 hrs · 27,625 cycles

NDIS 636 33-51 0022920 04MAR19 RIC CLOSE SERVICE DOOR EXIT IDENTIFIER EMERGENCY LIGHT, ROW 1+ 2 FLOOR PROXIMITY EMERGENCY LIGHT STRIP AND COCKPIT STEP EMERGENCY EXIT IDENTIFIER EMERGENCY LIGHT INOP 27625 00 NGR FACT 04MAR19 10:14 RIC R/R #200 INVERTER IAW 33-50-11-00/400-801-A.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 43,763 hrs · 40,569 cycles

DIS 636 33-51 0021500 13JAN19 SBY CLOSE EMERG. LIGHT FLOOR 1 AND LOWER SERVICE DOOR EXIT SIGN INOP. FACT 13JAN19 12:48 SBY RESEATED BATT NR 2 CONNECTOR. RESECURED GALLEY CEILING PANEL WITH RETAINED HARDWARE.

Part: FRAME — CHAFED (FRM 64) · airframe 43,593 hrs · 40,365 cycles

DISCREPANCY: DURING HEAVY CHECK MAINTENANCE FOUND RH SIDE FRAME 64 IN CARGO CHAFED. CORRECTIVE ACTION: REPAIRED RH SIDE FRAME 64 IN CARGO IAW ETD2018-145-119894

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 43,593 hrs · 40,365 cycles

DISCREPANCY: DURING HEAVY CHECK MAINTENANCE FOUND BAGGAGE DOOR ENTRENCE SILL TO BE CORRODED. CORRECTIVE ACTION: R&R BAGGAGE DOOR ENTRENCE SILL WITH P/N 145-25480-603 IAW EMB 145 SRM 51-40-02

Part: RIB — CRACKED (RT WING) · airframe 43,593 hrs · 40,365 cycles

DURING HEAVY CHECK MAINTENANCE FOUND RT WING RIB 5 CRACKED AT AFT LIGHTNING HOLE. R&R RT WING RIB 5 WITH P/N 145-67083-602 IAW ETD2018-145-118003 AND TI-145-14-306.

Part: SUPPORT — CORRODED (TOILET VALVE) · airframe 43,593 hrs · 40,365 cycles

DISCREPANCY: DURING HEAVY CHECK MAINTENANCE FOUND TOILET VALVE SUPPORT BUCKET CORRODED. CORRECTIVE ACTION: R&R TOILET VALVE SUPPORT BUCKET WITH P/N 145-25599-001 IAW EMB 145 SRM 51-40-02.

Part: FRAME — CHAFED (CARGO DOOR) · airframe 43,593 hrs · 40,365 cycles

DISCREPANCY: DURING HEAVY CHECK MAINTENANCE FOUND CARGO DOOR INTERIOR WEB FRAME HAS MULTIPLE CHAFES. CORRECTIVE ACTION: REPAIRED CARGO DOOR INTERIOR WEB FRAME P/N 145-23918-001 IAW EMB 145 SRM 52-30-01.

Part: BRACKET — BENT (FWD SEAL) · airframe 43,593 hrs · 40,365 cycles

DISCREPANCY: DURING HEAVY CHECK MAINTENANCE FOUND CARGO FWD SEAL ANGLE BRACKET BENT ON LOWER CORNER. CORRECTIVE ACTION: R&R CARGO FWD ANGLE SEAL BRACKET WITH P/N 145-29610-003 IAW EMB 145 SRM 51-20-03 AND 51-40-02

Part: WARNING MESSAGE — FALSE ACTIVATION (DAU) · airframe 43,585 hrs · 40,356 cycles

DAU 2A FAILURE MESSAGE DISPLAYED. CYCLED THE CIRCUIT BREAKERS, PDPU, OPS CHECKED GOOD. OK FOR SERVICE.

Part: FILTER — DIRTY (NR 1 ENGINE) · airframe 43,313 hrs · 40,034 cycles

E1 FUEL IMP BYPASS ADVISORY MESSAGE ON EICAS. REMOVED AND REPLACED NR 1 ENGINE FUEL FILTER IN REFERENCE TO EMM 73-21-10. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: LIGHT — BROKEN (ROW 7) · airframe 42,134 hrs · 38,742 cycles

ROW 7 CEILING EMERGENCY LIGHT CALL LOCATER LIGHT BROKEN. R & R THE ZONAL ATTENDANT CALL LIGHT AT ROW 7 IAW AMM 33-25-05-000/400-801-A. OPS CHECKED GOOD. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,134 hrs · 38,742 cycles

FWD GALLEY CEILING EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-50-06-000/400-801-A. OPS CHECK GOOD. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (BRAKES) · airframe 40,973 hrs · 37,532 cycles

BRAKE DEGRADED EICAS MESSAGE DISPLAYED FOUR TIMES DURING TAXI, NR 3 BRAKE INDICATES NO TEMP. BRAKE DEGRADED MESSAGE CLASSIFIED AS TRANSITORY CONDITION IAW TASK 32-41-00-810-831-A. NR 3 BRAKE TEMP, OPS NORMAL AND MATCH OTHER BRAKE TEMPS AFTER BLEEDING BRAKE LINE.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS) · airframe 40,856 hrs · 29,257 cycles

COCKPIT STAIR EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. RESEATED THE CONNECTOR ON THE LIGHT.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,856 hrs · 29,257 cycles

SEAT 12A LT SIDE MAIN EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. REMOVED AND INSTALLED A NEW INVERTER IAW AMM 33-50-11-04.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHT) · airframe 40,856 hrs · 29,257 cycles

COCKPIT STAIR EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. RESEATED THE CONNECTOR ON THE EMERGENCY LIGHT.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 40,620 hrs · 37,156 cycles

EMERGENCY LIGHT UNDER COCKPIT DOOR IN INOPERATIVE. CLEANED THE CONNECTOR IAW MM 33-50-13-000-801-A, AND 33-50-13-500-801-A. OPS CHECKED GOOD.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 40,396 hrs · 36,915 cycles

AT 10,000 FEET, CABIN ALTITUDE INDICATED 200 FEET. CABIN PRESSURE WAS NOT CLIMBING. PERFORMED A CABIN PRESSURIZATION OPS CHECK. PNEUMATIC VALVE OPS CHECKED IAW MM 21-31-00. OPS CHECKED GOOD. OKAY FOR SERVICE.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 39,821 hrs · 36,301 cycles

LEFT FORWARD EXTERIOR OVERWING EMERGENCY LIGHT DIMMING OUT. REMOVED AND REPLACED BULB IAW MM 33-50-10-04. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,786 hrs · 36,261 cycles

LEFT EMERGENCY EXIT UPPER SIDEWALL LIGHT IS INOPERATIVE. R & R LT EXIT UPPER SIDEWALL LIGHT ASSY IAW MM 33-50-14. OPS CHECKED GOOD.

Part: SPAR CAP — CRACKED (LT WING) · airframe 39,220 hrs · 35,622 cycles

LEFT WING SPAR 1 RIB 9 AREA, FASTENER HOLE AT LOWER FLANGE HAS A CRACK. REPAIRED LT WING SPAR 1 LOWER CAP AT RIB 9 AREA IAW ERS-EM-57MR-617.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,220 hrs · 35,622 cycles

LEFT FUSELAGE FRAME 75 ABOVE STRINGER 2 SKIN CRACKED. REPAIRED LT UPPER FUSELAGE SKIN AT FRAME 75, ABOVE & BELOW STRINGER 2L IAW ERS-EM-53MR-2085.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,220 hrs · 35,622 cycles

FRAME 22 IS CORRODED BELOW SERVICE DOOR LOWER FRAME STOP. REPAIRED FRAME 22 IAW ERS-EM-53MR-2053.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 39,216 hrs · 35,620 cycles

SSI 53-20-07 FRAME 22 IS CORRODED BELOW SERVICE DOOR LOWER FRAME STOP. REPAIRED CORROSION BELOW SERVICE DOOR LOWER FRAME STOP AT CTR FUSELAGE I IAW ERS-EM-53MR-2053. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.

Part: CONTROL PANEL — FAULTY (SMOKE DETECTION) · airframe 38,372 hrs · 34,840 cycles

LAVATORY SMOKE PRESENTED ON EICAS. R & R SMOKE DETECTOR PANEL IAW 26-14-02. OPERATIONS CHECKED GOOD.

Part: TIRE — SEPARATED (MLG) · airframe 38,010 hrs · 34,547 cycles

ON POST FLIGHT FOUND TREAD MISSING ON NR 3 MAIN WHEEL & TIRE. LOOKS LIKE HIT UNDER FLAP, SIDE ENG NACELLE ON FUSELAGE SIDE BEHIND ANTI-ICE LIP & AGAINST EMPENNAGE AT AFT ENG NACELLE. EMAILED PICTURES TO MOC. R & R NR 3 TIRE IAW WC 32-700-11, GVI UNDER FLAP, ENG NACELLE, ENG INTAKE & FUSELAGE IAW AMM 05-50-00. NO DAMAGE NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (NLG) · airframe 37,875 hrs · 34,405 cycles

NOSE GEAR LANDING LIGHT INOPERATIVE. R & R NOSE GEAR LANDING LIGHT IAW 33-41-02. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,875 hrs · 34,405 cycles

LEFT AFT EMER DOOR LIGHT INOPERATIVE. R & R EXIT IDENTIFIER SIGN IAW AMM 33-50-13. OPERATIONS CHECKED GOOD.

Part: TIRE — DAMAGED (NR 4) · airframe 37,874 hrs · 34,404 cycles

NUMBER 4 MAIN TIRE DAMAGED, MISSING TREAD ON INNER HOLE. R & R NR 4 MLG WHEEL ASSEMBLY IAW WC 32-700-11 & WC 32-700-18.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 37,579 hrs · 34,114 cycles

AFT CABIN EMER FLASHLIGHT BASE 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.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,061 hrs · 33,628 cycles

AISLE EMER LIGHT AT ROW 7 INOPERATIVE. R & R ROW 7 AISLE EMER LIGHT LAMP IAW AMM 33-50-08-000-801-A & 33-50-08-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: PITOT SYSTEM — CONTAMINATED (NR 2) · airframe 36,789 hrs · 33,350 cycles

DURING CRUISE AT FL 280 ICAS CAUTION SPC ADVANCED LIGHT CAME ON. DRAINED WATER FROM NR 2 PITOT DRAIN SYS IAW AMM CH34-13-00. PERFORMED PITOT STATIC SYS ADJUSTMENT TEST. PITOT STATIC SYS CHECKED GOOD. ALL WORK PERFORMED IAW AMM CH 34-13-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,786 hrs · 33,348 cycles

FLOOR PROXIMITY LIGHT 6A INOPERATIVE. R & R FLOOR PROXIMITY LIGHT AT 6A IAW AMM 33-50-12. OPERATION CHECKED GOOD.

Part: CIRCUIT BOARD — DEFECTIVE (COCKPIT) · airframe 36,722 hrs · 33,292 cycles

EMERGENCY PARK BRAKE PANEL BACKLIGHTING INOPERATIVE ON CTR PEDESTAL. R & R EMER PARK BRAKE PANEL BACKLIGHTING CIRCUIT BOARD ON CTR PEDESTAL IAW SWPM 20-30-00 & AMM 33-12-00. OPERATIONAL CHECKED GOOD.

Part: ACTUATOR — FAILED (RT SPOILER) · airframe 36,682 hrs · 33,262 cycles

UPON DESCENT, THE SPEED BRAKES WERE OPENED WHEN COMMANDED TO CLOSE. THE ACFT EXHIBITED A PRONOUNCED BUT CONTROLLABLE ROLL TO THE RT, FOLLOWED BY SPOILER FAIL MSG ON EICAS. AFTER 15 - 20 SECS THE ACFT RETURNED TO NORMAL CONFIG & THE SPOILER FAIL MSG EXTINGUISHED. PROBLEM REOCCURRED DURING LANDING ROLL OUT ALSO. R & R SPEED BRAKE ACCUMULATOR ON RT SIDE IAW AMM 27-62-02. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 36,623 hrs · 33,216 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. R & R CAPTAIN`S FLASHLIGHT IAW 25-60-00.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 36,600 hrs · 33,198 cycles

CAPTAIN`S FLASHLIGHT NOT WORKING. REPLACED FLASHLIGHT IAW MM 25-60-00.

Part: STRUCTURE — SECONDARY DAMAGE (BY TIRE) · airframe 36,537 hrs · 33,148 cycles

RIGHT INBOARD FLAP DAMAGED BY TIRE TREAD SEPARATION. TEARS IN SKIN 5 INCHES & 2 INCHES LONG. R & R RT INBD FLAP IAW AMM 27-50-00. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 36,286 hrs · 32,885 cycles

FIRST OFFICER`S FLASHLIGHT IS INOPERATIVE. R & R FLASHLIGHT WITH SERVICEABLE FLASHLIGHT AS REQUIRED. OPERATIONS CHECKED GOOD.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 36,118 hrs · 32,715 cycles

AFTER TAKEOFF APPROX 16000 FT ADVISORY MSG HYD 2 LO QTY HYD QTY NEEDLE AMBER TOP OF SCALE PSI AT 3000 WITHIN 10 MIN HYD 2 QTY NEEDLE AT BOTTOM OF SCALE PSI SHOWED 2100. R & R NR 2 ENG DRIVEN HYD PUMP & SERVICED NR 2 HYD QTY. OPERATIONS & LEAK CHECKED GOOD IAW AMM CH 29-10-03.

Part: LEVER — FAILED (SPEED BRAKE) · airframe 35,904 hrs · 32,516 cycles

DESCENDING THROUGH FL 160, 250KTS TRIED TO OPEN SPEED BRAKES 3 TIMES. SPEED BRAKE FAIL MSG ON EICAS NO APPARENT DEPLOYMENT OF SPEED BRAKES. R & R SPEED BRAKE LEVER IAW AMM 27-63-03. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,796 hrs · 32,410 cycles

SEAT 12A EMER EXIT LIGHT INOPERATIVE. R & R EMER EXIT LIGHT AT 12 A IAW AMM 35-50-13. OPERATIONS CHECKED GOOD.

Part: CONDITIONER — FAULTY (FUEL SYSTEM) · airframe 34,686 hrs · 31,438 cycles

DURING TAKEOFF MC FUEL IMBALANCE & MASTER WARNING FUEL 1 LOW LEVEL LIGHTS ILLUMINATED AS SOON AS THE GEAR RETRACTED. RESET FUEL CONDITION UNIT IAW AMM 28-41-01, OPERATIONS CHECKED GOOD, FUEL INDICATOR OK.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 34,663 hrs · 31,417 cycles

DURING HMBV INSPECTION FOUND LT & RT PULLEY SUPPORTS IN THE BELLY NEAR STRINGER 21 AT FRAME 16 ARE CRACKED ON THE FWD END. REMOVED CRACK ON RT PULLEY SUPPORT NEAR STRINGER 21 & FRAME 16 IAW ERS-M-5300-636. RESTORED TOP IAW CPM 51-21-06 & ETN EM-51-091. REMOVED CRACK ON LT PULLEY SUPPORT NEAR STRINGER 21 & FRAME 16 IAW ERS-EM-5300-636. RESTORED TOP IAW CPM 51-21-06 & ETN EM-51-091.

Part: FITTING — DAMAGED (LT SPOILER) · airframe 34,663 hrs · 31,417 cycles

DURING HMBV INSPECTION FOUND LT AILERON PCA FITTING DAMAGED & BENT, WHILE REMOVING SEIZED ATTACHING HARDWARE. R & R LT AILERON PCA FITTING IAW EO EM-27MR-112.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,663 hrs · 31,417 cycles

DURING HMBV INSPECTION FOUND CLIP FROM FIRST OFFICER`S DV WINDOW CUT OUT TO FRAME 10 ON THE LOWER SIDE OF CUT OUT HAS A 2" CRACK. R & R CLIP IAW SRM 51-40-02.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 34,663 hrs · 31,417 cycles

RIGHT SIDE OF FRAME 64 HAS DAMAGE ON A PREVIOUS REPAIR DOUBLER. COMPLIED WITH EO EM-53MR-1972.

Part: FIREWALL — CRACKED (APU BAY) · airframe 34,663 hrs · 31,417 cycles

DURING HMBV INSPECTION FOUND THE APU FIREWALL CRACKED AT THE TOP RT MOUNTING POINT & ABOVE THE TOP RIVET ON THE RT SIDE RIVET ROW. COMPLETED FABRICATION & INSTALLED NEW DOUBLER AT TOP RT MOUNTING POINT IAW EO EM-53AD-1883 & ETN EM-53-244. COMPLETED REPAIR OF APU FIREWALL IAW EO EM-53AD-1883 PART C STEPS 81 THRU 1.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 34,663 hrs · 31,417 cycles

DURING HMBV INSPECTION FOUND RT WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE IS CRACKED BETWEEN FRAMES 47 - 48. CRACK APPROXIMATELY 1 INCH LONG. INSTALLED NEW ANGLE IAW SRM CH 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 34,663 hrs · 31,417 cycles

DURING HMBV INSPECTION FOUND LT WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE IS CRACKED BETWEEN FRAMES 45 - 46 & AT FRAME 46. THIS REPAIR IS LOCATED ON THE SAME ANGLE & IS FARTHER AFT THAN THE CRACK AT FRAME 45 - 46. IAW NRWC E374048 FOR THE AFT SECTION OF THE DRAG ANGLE TO BE REPLACED THAT COVERS THIS CRACK & THE OTHER CRACK AS WELL.

Part: SUPPORT FRAME — CRACKED (NLG WW) · airframe 34,663 hrs · 31,417 cycles

DURING HMBV INSPECTION FOUND THE NLG BAY AFT UPLOCK BOX SUPPORT FRAME IS CRACKED ON THE LT SIDE. R & R NLG BAY, AFT UPLOCK BOX SUPPORT FRAME IAW SRM 51-40-02.

Part: WIRE — BROKEN (CABIN) · airframe 34,663 hrs · 31,417 cycles

PAX CABIN NR 8 EMERGENCY LIGHT STRIP WIRES BROKEN. R & R PAX CABIN NR 8 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 34,663 hrs · 31,417 cycles

RIGHT PULLEY SUPPORT IN BELLY NEAR STRINGER 21 AT FRAME 16 IS CRACKED 1/8 INCH ON THE FWD END. REMOVED CRACK ON RT PULLEY SUPPORT NEAR STRINGER 21 & FRAME 16 IAW ERS-EM-5300-636. RESTORED TOP IAW CPM 51-21-06 & ETN-EM-51-091.

Part: SUPPORT FRAME — CRACKED (NLG WW) · airframe 34,663 hrs · 31,417 cycles

NLG BAY, AFT UP LOCK BOX SUPPORT FRAME IS CRACKED ON THE LT SIDE. R & R NLG BAY, AFT UP LOCK BOX SUPPORT FRAME IAW SRM 51-40-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,663 hrs · 31,417 cycles

ACFT INTERIOR SKIN LOCATED BETWEEN FRAMES 13 - 14, STRINGERS 21R - 19R IS CORRODED. COMPLIED WITH ERS-EM-53MR-383.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 34,663 hrs · 31,417 cycles

PAX DOOR BRACKET FOR INNER HANDLE TORQUE BOX HAS A 3/8 INCH CRACK ON AFT UPPER CORNER. REPAIRED PAX DOOR BRACKET FOR INNER HANDLE TORQUE BOX IAW EO-EM-52MR-250.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,663 hrs · 31,417 cycles

RIGHT OTBD CLIP FROM AFT SVC DOOR SILL TO FRAME 23 FLOORBEAM HAS A 3/4 INCH CRACK. R & R CLIP IAW SRM 51-40-02.

Part: PROFILE — CRACKED (APU BAY) · airframe 34,663 hrs · 31,417 cycles

APU COWL LOWER RT FWD PROFILE CRACKED 4 INCHES INBD OF LOWER RT MOUNT POINT. REPAIRED PROFILE IAW EM-4900-011.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 34,663 hrs · 31,417 cycles

LEFT PULLEY SUPPORT IN BELLY NEAR STRINGER 21 AT FRAME 16 IS CRACKED 3/8 INCH ON THE FWD END. REMOVED CRACK ON LT PULLEY SUPPORT NEAR STRINGER 21 & FRAME 16 IAW ERS-EM-5300-636. RESTORED TOP IAW CPM 51-21-06 & ETN-EM-51-091.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,663 hrs · 31,417 cycles

CLIP FROM FWD DIGITAL TO FWD PAX DOOR CUT OUT AT FRAME 15 HAS A 1 INCH CRACK. R & R CLIP IAW SRM CH 51-40-02.

Part: BRACKET — CRACKED (RT WING) · airframe 34,663 hrs · 31,417 cycles

RIGHT WING ANGLE BRACKET THAT IS ATTACHED TO TORQUE BOX NR 1 HAS 1/2 INCH CRACK ON THE TE. REPAIRED RT WING ANGLE BRACKET THAT IS ATTACHED TO TORQUE BOX NR 1 IAW ETN-EM-53-142.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 34,663 hrs · 31,417 cycles

CARGO DOOR LIFTING & LOWERING MECHANISM FWD BRACKET HAS A CRACK APPROX 1/4 INCH LONG. R & R CARGO DOOR LIFTING LOWER MECHANISM FWD BRACKET IAW SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,663 hrs · 31,417 cycles

IAW NRTC E373524 FOR PERMANENT REPAIR 636T5314 TO LATERAL POST SKIN CRACK. COMPLIED WITH ERS-EM-53MR-187 R1 PART C, IAW STEP 4 FOR COMPLIANCE WITH EO EM-5300-2232.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 34,663 hrs · 31,417 cycles

RIGHT WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE IS CRACKED AT FRAME 47 CRACK APPROXIMATELY 1 INCH LONG. INSTALLED NEW ANGLE IAW SRM CH 51-40-02.

Part: APU — CONTAMINATED (APU BAY) · airframe 34,593 hrs · 31,355 cycles

SHORTLY AFTER APU START STRONG BURNING ODOR IN COCKPIT. APU BLEED CLOSED PACKS WERE OFF VISUAL INSPECTION SHOWED SMOKE COMING OUT OF APU AIR INLET & EXHAUST. TROUBLESHOT BURNING SMELL TO RESIDUAL DE-ICE FLUID IN THE APU AREA. NO DEFECTS OR SMELL NOTED, CLEANED RESIDUAL FLUID.

Part: CARBON SEAL — FAILED (NR 2 ENGINE) · airframe 34,534 hrs · 31,304 cycles

FIFTEEN MINUTES AFTER TAKEOFF OF ABOUT FP 270 E2 OIL QTY 5 QT AFTER CHECKED SHUT DOWN MODE SINGLE ENGINE LANDING. ENGINE REPLACED DUE TO NR 7 CARBON SEAL REPLACEMENT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,358 hrs · 31,168 cycles

CRACK DAMAGE FOUND ON FWD FUSELAGE SKIN II AT UPPER PORTION OF WINDSHIELD LATERAL POST BETWEEN PILOT WINDOW & DV WINDOW. PERFORMED TEMPORARY STRUCTURAL REPAIR IAW ERS-EM-53MR-187 PART A.

Part: EXTINGUISHER — MALFUNCTIONED (CARGO BAY) · airframe 33,629 hrs · 30,620 cycles

DURING START OF DESCENT, RECEIVED A BAGGAGE EXTINGUISHER WARNING. FOLLOWED APPROPRIATE PROCEDURES AND LANDED. R & R BAGGAGE COMPARTMENT FIRE EXTINGUISHER BOTTLES IAW AMM-26-23-01. OPS CHECKED GOOD. R & R THE CARGO AREA SMOKE DETECTOR. PERFORMED ELECTRICAL ACFT RESET AND OPS CHECK IAW AMM 26-15-00. OPS CHECKED GOOD.

Part: SWITCH — BROKEN (FLASHLIGHT) · airframe 33,411 hrs · 30,445 cycles

F/O FLASHLIGHT HAS A BROKEN SWITCH. R & R F/O FLASHLIGHT AND BATTERY IAW AMM TASK 33-50-16-000-801-A AND TASK 33-50-16-400-801-A. OPS CHECKED NORMAL.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,948 hrs · 30,044 cycles

DURING PS-2 CHECK, FOUND SERVICE DOOR EMERGENCY EXIT SIGN INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — UNKNOWN (CABIN) · airframe 32,880 hrs · 29,982 cycles

DURING MX INSPECTION, FOUND THE GALLEY EMERGENCY LIGHTS INOPERATIVE. ACFT REMOVED FROM SERVICE. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-50-00. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED. ACFT RETURNED TO SERVICE.

Part: BLEED VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 32,080 hrs · 29,396 cycles

FOR FLIGHT 2710 THE CREW REPORTED THAT WITH APU RUNNING BLEED OPEN PACK NR 2 MADE NON-REGULAR RUNNING SOUNDS AFTER CYCLING PACK NR 2 AND ODORLESS SMOKE/VAPOR WAS SEEN AROUND THE AIRCRAFT AND FILLED UP THE CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE E1 BLEED VALVE IAW EMB 145 AMM 36-11-05, OPC GOOD, MEL 36-01 RESTORED. PART NUMBER 3215886-2, S/N 354. REMOVED AND REPLACED RIGHT ACM IAW EMB 145 AMM 21-51-03 OPS CHECK GOOD, NO LEAKS NOTED AND ETN EM 21-056. PART NUMBER 8152403, S/N 9908264. REMOVED AND REPLACED RIGHT DUCT TEMP SENSOR IAW EMB 145 AMM 21-60-03, OPS CHECK GOOD. PART NUMBER 8152892, S/N 06455. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONDITIONER — INOPERATIVE (FUEL SYSTEM) · airframe 31,245 hrs · 28,724 cycles

ON FLIGHT 4197 THE CREW REPORTED THAT FROM BNA TO JFK THEY WERE HOLDING OVER LENDY FIX ON THE ARRIVAL. EFC OF 20:45, 45 MINUTES FROM THE PRESENT TIME OF THE EVENT. THEY HAD 25 MINUTES OF HOLDING FUEL TIME. THE CREW SENT A MESSAGE TO DISPATCH WITH THE EFC AND FUEL ON BOARD. THE CREW DECLARED MINIMUM FUEL WHILE DOWN WING FROM THE LANDING RUNWAY 31L VISUAL. THE CONTROLLER ADVISED THEM TO EXPECT A LONG FINAL DUE TO TRAFFIC. THE CREW WAS FORCED TO DECLARE A FUEL EMERGENCY WITH 1600 LBS FOB. THE AIRCRAFT LANDED SAFELY WITH 1450 LBS FOB. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FUEL CONDITIONING UNIT IAW EMB AMM 28-41-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,117 hrs · 28,636 cycles

DURING B INSPECTION FOUND THE EMERGENCY FLOOR LIGHTING STRIP 2ND ONE FROM THE AFT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY FLOOR LIGHTING STRIP IAW EMB-145 MM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,072 hrs · 28,600 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT AFT OVERWING LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 30,972 hrs · 28,523 cycles

ON FLIGHT 4180 THE CREW REPORTED THE CABIN AFT FLASHLIGHT WAS MISSING. FLIGHT CREW PLACARD PER MEL 25-53 AUTH 101125-C MOC ID 373623 CABIN AFT MISSING FLASHLIGHT. FOUND FLASHLIGHT, MEL RESTORED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,680 hrs · 28,296 cycles

DURING B INSPECTION FOUND SEAT 12A OVERHEAD PANEL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT 12A OVERHEAD PANEL EMERGENCY LIGHT BULB IAW EMB 145 AMM 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: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 30,043 hrs · 27,793 cycles

DURING B INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT AND INSTALLED NEW BATTERY AND BULB IAW EMB AMM TASK: 33-51-01-700-802-A. BULB PART NUMBER:A1-14-0001-002. BATTERY PART NUMBER: P4-01-1003-001. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRUNNION — CRACKED (RIGHT WING) · airframe 29,973 hrs · 27,728 cycles

DURING MAINTENANCE INSPECTION, FOUND THE RIGHT MAIN LANDING GEAR AFT UPPER TRUNNION SUPPORT CRACKED AT THE LOWER RADIUS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-57MR-625. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 29,973 hrs · 27,728 cycles

DURING MAINTENANCE BASE INSPECTION, FOUND SERVICE DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED SILL YAW EMBRACER STRUCTURAL REPAIR MANUAL 53-21-02. REPAIRED SILL YAW EMBRACER STRUCTURAL REPAIR MANUAL 53-21-02.

Part: SILL — CORRODED (FUSELAGE) · airframe 29,973 hrs · 27,728 cycles

DURING MAINTENANCE BASE INSPECTION, FOUND THE CARGO DOOR SILL HAS CORROSION AND IS CHAFED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — BROKEN (CABIN) · airframe 30,025 hrs · 27,774 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT NR 2, 5 AND 6 SIDEWALL EXTRUSIONS FOR THE EMERGENCY PROXIMITY LIGHTS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT NR 2, 5 AND 6 SIDEWALL EXTRUSIONS IAW AMM 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 30,025 hrs · 27,774 cycles

DURING B INSPECTION FOUND THE FLOORBOARD 251BF EMERGENCY LIGHTING STRIP HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FLOORBOARD 251BF EMERGENCY LIGHTING STRIP IAW EMB145/SWPM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 30,025 hrs · 27,774 cycles

DURING B INSPECTION FOUND THE FLOORBOARD 261BF EMERGENCY LIGHTING STRIP HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FLOORBOARD 261BF EMERGENCY LIGHTING STRIP AW EMB145/SWPM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 30,025 hrs · 27,774 cycles

DURING B INSPECTION FOUND THE FLOORBOARD 251DF EMERGENCY LIGHTING STRIP HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FLOORBOARD 251DF EMERGENCY LIGHTING STRIP IAW EMB145/SWPM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FILLER — DAMAGED (CABIN) · airframe 30,025 hrs · 27,774 cycles

DURING MAINTENANCE INSPECTION FOUND SEVERAL EMERGENCY LIGHT STRIPS FILLERS MISSING OR DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED MISSING AND DAMAGED EMERGENCY LIGHT STRIPS FILLERS STRIPS IAW AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TIRE — WORN (MLG) · airframe 29,620 hrs · 27,447 cycles

DURING B-INSPECTION, FOUND THE NR 3 TIRE WORN OUT OF LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 3 TIRE IAW CARD 32-700-11. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: TIRE — CUT (MLG) · airframe 29,577 hrs · 27,421 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 2 MAIN LANDING GEAR TIRE CUT OUT OF LIMITS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 WHEEL ASSEMBLY IAW W/C 32-700-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN & COCKPIT) · airframe 29,359 hrs · 27,248 cycles

ON FLIGHT 2839 THERE WAS SMOKE IN COCKPIT AND CABIN AFTER TAKEOFF AOM 1 PROEDURE. SMOKE STOPPED AFTER BLEEDS WERE CLOSED AIR TURNBACK AND LANDING OVERWEIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED INSPECTION OF COCKPIT, GALLEY, CABIN LIGHTING, A/C DISTRIBUTION DUCTS AND ENGINE BLEEDS FOR SMOKE ODOR IAW ETN EM-77-034R4 NO DEFECTS NOTED AT THIS TIME REFER TO ITEMS NR 3 AND NR 4 THIS LOGPAGE FOR NR 1 PACK INOPERABLE AND NR 2 PACK DUCT LOOSE. OPERATIONAL WAS CHECK GOOD. THE AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN DOOR) · airframe 27,953 hrs · 26,199 cycles

ON FLIGHT 3365 THE RAMP CREW REPORTED THE MAIN CABIN DOOR WILL NOT CLOSE ALL THE WAY, THE RED HANDLE OF THE DOOR WAS NOT FLUSH. THE FLIGHT ATTENDANT ALSO REPORTED THE HANDLE WAS NOT MOVING TO A FULL CLOSED POSITION. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPEN AND CLOSING OF THE PASSENGER DOOR AND THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 52-00-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — PULLED (CABIN) · airframe 28,377 hrs · 26,214 cycles

ON FLIGHT 4226 THE CREW REPORTED THE EMERGENCY LIGHT STRIP NEAR EXIT ROW 15 LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND WIRE PULLED FROM CONTACT AT SPLICE 9115 REPLACED CONTACT IAW EMB WPM 20-00-03. THE EMERGENCY LIGHT OPERATIONAL CHECK WAS GOOD IAW EMB MM 33/50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,672 hrs · 25,297 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY EXIT LIGHTS/PLACARDS INOPERABLE AT OVERWING EMERGENCY EXITS AND FLOOR PROXIMITY LIGHTS AT EMERGENCY EXIT ROW. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 BATTERY ASSEMBLY AND CHARGER ASSEMBLY IAW EMB 145 AMM 33-50-04 OPC GOOD IAW EMB 145 AMM 33-50-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRIM SWITCH — FAILED (COCKPIT) · airframe 26,331 hrs · 25,737 cycles

ON FLIGHT 2841 DISPATCH REPORTED THAT IMMEDIATELY AFTER TAKEOFF THE FIRST OFFICER STARTED TRIMMING AND GOT NO RESPONSE. SEVERAL SECONDS LATER, GOT A PITCH TRIM MAIN INOPERABLE EICAS MESSAGE. THE CREW ELECTED TO RETURN TO DFW AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERS YOKE PITCH TRIM SWITCH IAW EMB-145 AMM 27-40-03. THE OPERATIONAL TEST WAS OK. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — WORN (AILERON) · airframe 25,024 hrs · 23,996 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE LEFT POWER CONTROL ACTUATOR ATTACH FITTING OUTBOARD BUSHING TO BE MIGRATING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AILERON POWER CONTROL ACTUATOR FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,024 hrs · 23,996 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE EXTERIOR FUSELAGE SKIN WITH A 1 INCH CRACK AT FRAME 75 BETWEEN STRINGERS 01 RIGHT AND 02 RIGHT; APPROXIMATELY 4 INCHES RIGHT OF THE VERTICAL STABILIZER; ALSO ALONG WITH STRINGER 02 RIGHT WAS FOUND TO BE CRACKED AT THE INTERSECTION OF FRAME 75. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED SKIN IAW ETA EM-5300-1412, REPAIRED STRINGER IAW EMBRAER SRM 53-00-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 17,644 hrs · 17,674 cycles

FIRST 5 ROWS OF EMERGENCY LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED NUMBER TWO BATTERY AND CHARGER IAW EMB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: POWER SUPPLY — DEFECTIVE (EMERGENCY LIGHT)

FLT 3459 - LEFT EMERGENCY OVERWING EXIT LIGHT INOPERATIVE. RAI NR 4 BATTERY POWER SUPPLY, OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MID ROW OVERHEAD EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. RAI MID ROW OVERHEAD EMERGENCY EXIT LIGHT ASSY, OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: FIXTURE — CORRODED (LAVATORY)

DURING A HMBV INSPECTION, LAVATORY SERVICE AREA BUCKET WAS FOUND TO BE CORRODED. REMOVED THE CORRODED LAV BUCKET AND INSTALLED SERVICEABLE BUCKET. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 33, CHAPTERS 51-40-02, 51-20-03, 51-40-06, 51-40-09 AND 51-20-01. RETURNED AIRCRAFT TO SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING A HMBV INSPECTION, THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND TO BE CORRODED. REMOVED AND REPLACED LOWER SILL, IAW EMB SRM, SRM 1454/1142 REV 33, CHAPTER 51-40-02, 03, 51-40-06, 51-20-01 AND EMB CPM, (CPM-145/1132 REV 13) CHAPTERS 51-21-05, 51-14-02, 51-20-03 AND 51-21-03, RETURNED AIRCRAFT TO SERVICE. (M)

Part: SIGN — INOPERATIVE (CABIN)

SHV - FLT 3782 - EMERGENCY EXIT CEILING LIGHT AFT OF ROW 12 INOPERATIVE. RAI EXIT SIGN IAW EMB 145 AMM 33-50-15. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY)

BAGGAGE SMOKE INDICATION ON EICAS. EXAMINATION OF BAGGAGE COMPARTMENT ON POSTFLIGHT REVEALED NO EVIDENCE OF FIRE OR SMOKE. PERFORMED OPERATIONAL CHECK OF BAGGAGE SMOKE INDICATION SYSTEM NO DEFECTS FOUND. AIRCRAFT RETURNED TO SERVICE. (K)

Part: POWER SUPPLY — DISCHARGED (CABIN)

EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY NR 3. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FRAME — CHAFED (FUSELAGE)

FOUND FRAME 81 CHAFED THROUGH AT THE 6 O`CLOCK POSITION CAUSED BY APU COWLING BRACKET. REPLACED BOTTOM HALF OF FRAME 81 IAW SRM 51-23-01. INSPECTED APU COWLING BRACKET WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FIRE BOTTLE — DISCHARGED (CARGO BAY)

CARGO FIRE EXTINGUISHER LIGHT ILLUMINATED IN FLIGHT, FIRE BOTTLES WERE DISCHARGED. MAINTENANCE FOUND NO EVIDENCE OF FIRE OR SMOKE. MAINTENANCE REPLACED BOTH FIRE BOTTLES. OPERATION CHECK OF FIRE DETECTION, GOOD. AC RETURNED TO SERVICE. (K)

Part: LEVER — INOPERATIVE (MLG)

ORD - FLT 4204 - ON APPROACH TO ORD LANDING GEAR RECEIVED AIR/GND FAIL MESSAGE. CREW USED EMERGENCY EXTENSION PROCEDURES TO LOWER LANDING GEAR. REPLACED LANDING GEAR SELECTOR LEVER. OP CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - THE CENTER OMEGA BEAM AT FRAME 24 WAS FOUND TO BE CORRODED. PERFORMED A CUT OUT OF THE CENTER OMEGA BEAM TO REMOVE CORROSION. FABRICATED FILLER, TWO SHIMS AND DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/1180 PARA 2 DATED MARCH 15, 2005. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

THE LEFT OMEGA BEAM AFT OF FRAME 24 WAS FOUND CORRODED. PERFORMED A NINE INCH CUT OUT OF THE OMEGA BEAM TO REMOVE THE CORROSION. FABRICATED A FILLER, EXTERNAL ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/1180 PARA 1 DATED MARCH 15, 2005. (M)

Part: SILL — CORRODED (FUSELAGE)

THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER SILL AND INSTALLED NEW SERVICEABLE SILL IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 51-40-02, IC2003-145/0818 DATED MARCH 6, 2003 AND AEA ETN EM-53-013 DATED AUGUST 28, 2001. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - FLT 3358 - DURING POSTFLIGHT, CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 7 THROUGH 10 APPEARS TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

ORD - FLT 4238 - TWO AISLE EMERGENCY LIGHT STRIPS ARE INOPERATIVE. REPLACED NR 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING PREFLIGHT, CREW FOUND THE EMERGENCY LIGHTS AFT OF ROW 12 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER PACK IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (GALLEY)

ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR CENER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED CENTER SILL. INSTALLED SERVICEABLE SILL IAW EMB 145 SRM (145/1142 REV 20) CHAPTERS 51-40-02, 51-20-03, 51-40-06 AND EMB 145 CPM 51-21-04 THROUGH 51-21-06. (M)

Part: SILL — CORRODED (GALLEY)

ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS IN THREE AREAS. COMPLETELY REMOVED CORROSION FROM AREAS BY BLENDING. PERFORMED AN EDDY CURRENT INSPECTION OF BLENDED AREA. NO DEFECTS NOTED. FABRICATED TWO REPAIR DOUBLERS. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 20) CHAPTERS 51-40-02, 51-20-03, 51-40-06 EMB IC2003-145/0137 AND INFORMATION CONTAINED IN AEAI ETN NR EM 53-0361 PAGE 7 FIG 5 ITEM 3. (M)

Part: FLOORBEAM — CORRODED (GALLEY)

ABI - DURING A IMBV INSPECTION, THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT A 16.5 BY 21 SECTION OF THE DIGITAL. FABRICATED A REPLACEMENT STRAP. FABRICATED TWO REPAIR DOUBLERS, AND SHIMS. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 20) CHAPTER 53-21-10. (M)

Part: WINDSHIELD — FAILED (COCKPIT)

ORD - FLT 4145 - DURING FLIGHT, CREW REPORTED THE FIRST OFFICERS WINDSHIELD ARCED FOLLOWED BY WINDOW OUTER PANE SHATTERING. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PSU — MALFUNCTIONED (CABIN)

ORD - FLT 4173 - DURING TAXI, FLIGHT CREW REPORTED SMOKE COMING FROM PASSENGER READING LIGHT AT SEAT 7A. MAINTENANCE REMOVED AND REPLACED THE PASSENGER SERVICE UNIT PCB ASSEMBLY AT ROW 7 IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ACM — FAILED (NR 2)

DISC- FLIGHT CREW NOTED VISIBLE SMOKE IN CABIN DURING FLIGHT. C/A NR 2 PACK ACM IAW SRM. OPS CHECK GOOD

Part: BATTERY — DISCHARGED (CABIN)

AZO - FLT 4266 - EMERGENCY LIGHTS INOPERATIVE ROWS 8 THROUGH 12. REPLACED LIGHT BATTERY AND HOLDER, OPS CHECKS GOOD. (M)

Part: LIGHT — INOPERATIVE (EMERGENCY DOOR)

FLT 4080 - ORD - GROUND FLOOR LIGHT ON MAIN EMERGENCY DOOR IS INOPERATIVE. REMOVED AND REPLACED FLOOD LIGHT ON MAIN EMERGENCY DOOR. OPERATIONAL CHECK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)