N635AE

Part: SLEEVE — FAILED (NR 2 PACK DUCT) · airframe 49,035 hrs · 46,423 cycles

BLD 2 LEAK EICAS MSG IN FLT. R+R DUCT SLEEVE FROM PACK 2 HEAT EXCHANGER IN REF TO AMM 21-51-02. PACK 2 SYS OPS CHECK SATISFACTROY NO EICAS MESSAGES PRESENT AT THIS TIME. OK FOR SERVICE AT THIS TIME

Part: WARNING LIGHT — FALSE ACTIVATION (BLEED AIR SYSTEM) · airframe 48,710 hrs · 46,055 cycles

ON CLIMB OUT BLEED 1 LEAK DISPLAYED ON EICAS. RAN QRH AND MESSAGE EXTINGUISHED. MAINTENANCE: FOLLOWED FIM TASK 36-20-00-810-801-A. RAN AMM TASK 36-00-00-700-803-A/500. NO LEAKS NOTED. NO DEFECTS FOUND IN BLEED SYSTEM. A/C OK FOR SERVICE.

Part: NONE — NONE · airframe 48,470 hrs · 45,793 cycles

PDIS 635 21-31 2592341 24APR22 PHL CLOSE CLIMBING THROUGH FL 250 CABIN ALTITUDE SLOWLY INCREASED UP TO 10000 (RED INDICATION) IN AUTO MODE FACT 24APR22 17:10 PHL REMOVED AND REPLACED CABIN PRESSURE AQUISITION MODULE IAW EMB AMM 21-32-01, OPERATIONAL CHECK / LEAK TEST GOOD OK FOR SERVICE.

Part: NONE — NONE · airframe 48,470 hrs · 45,793 cycles

PDIS 635 21-31 2592311 21APR22 MDT CLOSE CLIMBING THROUGH FL 230 CABIN ATTITUDE SLOWLY INCREASED UP TO 10,000 (RED INDICATION) IN AUTO MODE. ( C/W AMM TASK 21-31-03-040-801-A SUB TASK 040-002) FACT 23APR22 03:24 PHL TROUBLESHOT IAW FIM 21-31-00-810-809A. R&R DIGITAL CONTROLLER IAW AMM REF 21-31-01 OPS CHECK GOOD OK FORSERVICE AT THIS TIME CLEAR MEL 21-12-3

Part: NONE — NONE · airframe 48,415 hrs · 45,731 cycles

PDIS 635 34-15 2592212 12APR22 EVV CLOSE NO AIRSPEED INDICATION ON CA'S SIDE ON TAKE OFF ROLL FACT 12APR22 22:01 EVV T/S IN REF TO FIM TASK 34-22-00-810-812-A STEPS 8-11 SWAPPED IC 600S TO ORIGINAL POSITION.R/R IC600 100 IAW AMM 31-42-01.OPS CHECK GOOD.A/C OK FOR SERVICE.

Part: NONE — NONE · airframe 48,316 hrs · 45,626 cycles

PDIS 635 30-21 2696461 24MAR22 PHL CLOSE E2 AI FAIL MESSAGE DISPLAYED C/W AMM 30-21-01-040-801-A FACT 27MAR22 06:15 PHL T/S FIM TASK 30-21-00-810-806-A BLOCK 5. REMOVED + REPLACED E2 A/I PRESSURE TRANSDUCER IAW AMM 30-21-06. NO FIX. FOLLOWED STEP 7. REMOVED + REPLACED E2 A/I VALVE IAW AMM 30-21-01. OPS CHECK GOOD. NO LEAKS. OK FOR SERVICE. CLEAR MEL 30-8-1.

Part: NONE — NONE · airframe 48,145 hrs · 45,428 cycles

PDIS 635 05-50 2696123 19FEB22 CLT CLOSE FLAP OVERSPEED AT 150 KTS FOR 1-2 SECONDS AT 2500 TO 3000FT WITH FLAPS AT 45 FACT 19FEB22 13:56 CLT INSPECTED A/C IAW AMM 05-50-07. NO MAINTENANCE ACTION IS NEEDED AT THIS TIME. A/C OK FOR SERVICE

Part: NOT REPORTED — NOT REPORTED · airframe 48,145 hrs · 45,428 cycles

PDIS CLT 19FEB22 DURING FLIGHT LOST RMU 1 PFD1 NAV 1 FMS 1 AND MFD2 AND REMAINED OFF THROUGHOUT FLIGHT FACT 19FEB22 15:11 UPON MX ARRIVAL TO A/C THE AVIONICS MASTER 1 PB WAS IN THE OFF POSITION. SUSPECT SWITCH FAILURE FROM TURBULENCE IN SEQ 1 THIS LP. R&R AVIONICS 1 MASTER PB IAW AMM 20-13-04-00-801-A AND 20-13-04-400-801-A. TURNED ON AVIONICS MASTER 1 PB AND ALL RELATED SYSTEMS POWERED ON. PERFORMED OPS CHECKS IAW AMM 34-22-00, 34-62-00, 23-81-00, 34-51-00, 34-53-00, 34-32-00

Part: NOT REPORTED — NOT REPORTED · airframe 48,145 hrs · 45,428 cycles

PDIS 635 05-50 2606121 19FEB22 CLT CLOSE DURING DESCENT A/C EXPERIENCED SEVERE TURBULENCE FACT 19FEB22 14:48 CLT PERFORMED SEVERE TURBULENCE INSP/ CHECK IAW AMM 05-50-27NO DAMAGE FOUND. OPS CHECK GOOD. A/C OK FOR SERVICE

Part: BLEED VALVE — FAULTED · airframe 47,283 hrs · 44,445 cycles

BLEED 1 VALVE FAIL CAUTION AND BLEED 1 VALVE CLOSED IN ICING CONDITION DURING CLIMB OUT. PERFORMED OPS CHECK TO BLD 1 VALVE IAW AMM 36-11-05 FOUND TO BE TRANSITORY CONDITION OPS CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: WARNING MESSAGE — FALSE INDICATION (PITCH TRIM) · airframe 47,029 hrs · 44,186 cycles

DURING LANDING WHEN SELECTING FLAPS TO 45 MAIN PITCH TRIM AND BACK UP PITCH TRIM INOP BOTH APPEARED ON EICAS. PER FIM TASK 27-43-00-810-820-A FIM PROCEDURES BLOCK DIAGRAM BLOCKS 3&8 HORIZONTAL STAB ELECTRNIC OPERATIONAL TEST AMM TASK 27-40-00-802-A/500 TRANSITORY CONDITION OF THE HSCU EXISTS. OPS CHECK GOOD RETURN TO SERVICE

Part: SPAR — DAMAGED (LT WING) · airframe 47,003 hrs · 44,155 cycles

LH WING SPAR 1 RIB 9 AREA HAS RELEVANT INDICATION AT LOWER FLANGE FWD OF SCREW HOLE ... ACCOMPLISHED REPAIR OF LH SPAR I AT RIB 9 IAW EMB 145 SRM 57-20-05 ITEM 2, FIG 201 SHEET 1 AND PIEDMONT EO1-57-21-0121. PERFORMED LEAK CHECK ON LH WING SPAR 1 RIB 9 IAW EMB 145 AMM 28-11-00, LEAK CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (FRM 20) · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CORROSION ON INBD SIDE LT OMEGA BEAM AT FRAME 20 ... REMOVED, FABRICATED AND INSTALLED REPAIR PARTS ON LH OMEGA BEAM AT FR 20 IAW EMB145 SRM 53-00-10 ITEM #2 FIG. 201 SHEET 1 AND PIEDMONT EO1-53-21-0128

Part: DOOR SILL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

SSI 53-30-48: CARGO DOOR FRAME CUTOUT SILL CORRODED ... COMPLETED REMOVAL AND INSTALLATION OF SERVICEABLE CARGO DOOR CENTER SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CARGO COMPARTMENT LH #3 FLOOR SILL CORRODED ... REMOVED CORRODED CARGO COMPARTMENT LH #3 FLOOR SILL AND POSTIONED, DRILLED, AND INSTALLED SERVICEABLE CARGO COMPARTMENT LH #3 FLOOR SILL IAW EMB 145 SRM 51-40-02 AND SRM 51-20-03

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CARGO COMPARTMENT LH #2 FLOOR SILL CORRODED ... REMOVED CORRODED CARGO COMPARTMENT LH #2 FLOOR SILL AND POSTIONED, DRILLED, AND INSTALLED SERVICEABLE CARGO COMPARTMENT LH #2 FLOOR SILL IAW EMB 145 SRM 51-40-02 AND SRM 51-20-03

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CORROSION ON RH INBD # 5 SEAT TRACK GUSSET ... REMOVED AND INSTALLED SERVICEABLE RH INBD #5 SEAT TRACK GUSSET IAW EMB145 SRM 51-40-02.

Part: LONGERON — CORRODED (LT NACELLE) · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CORROSION ON LH ENGINE UPPER COWLING OTBD LONGERON UNDER AFT HINGE FITTING ... SEE NRTC# E862591 FOR REPLACEMENT OF LH ENGINE UPPER COWLING OUTBD LONGERON.

Part: LONGERON — CORRODED (LT NACELLE) · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CORROSION ON LH ENGINE UPPER COWLING OTBD LONGERON UNDER CENTER HINGE FITTING ... SEE NRTC # E862591 FOR REMOVAL AND REPLACEMENT OF LH UPPER ENGINE COWLING OUTBOARD LONGERON

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CORROSION ON LH OTBD #5 FLOOR SILL ... REMOVED AND INSTALLED NEW LH OTBD #5 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FRM 65) · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

SSI 53-30-48: CARGO DOOR FRAME CUTOUT FR65 SHEAR CLIP CORRODED (MARKED). ... REPAIRED CARGO DOOR FRAME CUTOUT FR65 SHEAR CLIP IAW EMB 145 SRM 53-31-04RE ITEM 4 AND EO1-53-21-0124

Part: FLOOR SUPPORT — CORRODED (CARGO) · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CARGO COMPARTMENT RH #4 FLOOR SILL CORRODED ... REMOVED AND REPLACED CORRODED CARGO COMPARTMENT RH #4 FLOOR SILL IAW EMB 145 SRM 51-40-02 AND SRM 51-20-03.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 47,003 hrs · 44,155 cycles

POTABLE WATER SERVICE/ OVERFILL PORTS SUPPORT DOUBLER HAS CORROSION. AREA APPEARS TO HAVE BEEN PREVIOUSLY BLENDED ... REMOVED AND REPLACED THE POTABLE WATER SERVICE/ OVERFILL PORTS SUPPORT DOUBLER IAW EMB-145 SRM 51-40-02

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CORROSION ON LH INBD # 2 SEAT TRACK GUSSET...REMOVED UN-SERVICEABLE, POSITIONED, DRILLED AND INSTALLED SERVICEABLE LH INBD # 2 SEAT TRACK GUSSET IAW EMB 145 SRM 51-40-02 AND EMB 145 SRM 51-20-03.

Part: GUSSET — CORRODED (FRM 28) · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CORROSION ON DIAMOND GUSSET AT FRAME 28 ... REMOVED AND INSTALLED SERVICEABLE DIAMOND GUSSET AT FRAME 28 IAW EMB 145 SRM 51-40-02 AND EMB 145 SRM 51-20-03.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CORROSION ON LH INBD # 2 SEAT TRACK ... RAR L/H INBD #2 SEAT TRACK IAW EMB 145 AMM 53-01-06. TQW EASI# 7336

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CORROSION ON PASSENGER DOOR ENTRY FWD FLOOR BOARD SUPPORT ... RAR PAX DOOR ENTRY FWD FLOOR SUPPORT IAW EMB-145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED · airframe 47,003 hrs · 44,155 cycles

CORROSION ON LH INBD # 3 SEAT TRACK GUSSET ... REMOVE AND INSTALLED SERVICEABLE LH INBD SEAT TRACK GUSSET IAW EMB 145 SRM 51-40-02 AND EMB 145 SRM 51-20-03.

Part: FLOOR SUPPORT — CORRODED (FRM 18) · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CORROSION ON CROSS FLOOR BOARD SUPPORT AT PASSENGER DOOR ENTRY AT FRAME 18 ... REMOVED AND INSTALLED SERVICEABLE CROSSBEAM AT FR 18 IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CORROSION ON RH INBD # 2 SEAT TRACK GUSSET...REMOVED AND INSTALLED SERVICEABLE RH INBD #2 SEAT TRACK GUSSET IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CORROSION ON RH OTBD #3 FLOOR SILL ... REMOVED AND INSTALLED SERVICEABLE RH OTBD #3 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: NUT PLATE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

E859712 CARGO DOOR LWR EDGE AROUND NUT PLATE HOLES CORRODED ... REMOVED AND REPLACED CARGO DOOR LWR FRAME INNER L-PROFILE IAW EMB 145 SRM 51-40-02.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CARGO DOOR LWR EDGE AROUND NUT PLATE HOLES CORRODED ... REMOVED AND REPLACED CARGO DOOR LWR FRAME INNER L-PROFILE IAW EMB 145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FRM 20) · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CORROSION IN GALLEY AREA ON CENTER RAMP FLOOR BOARD SUPPORT AT FRAME 20 ... REMOVED AND REPLACED CENTER RAMP FLOOR BOARD SUPPORT AT FRAME 20 IAW EMB145 SRM 51-40-02. NO FURTHER ACTION REQUIRED.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 47,003 hrs · 44,155 cycles

CARGO COMPARTMENT RH #2 FLOOR SILL CORRODED ... REMOVED CORRODED CARGO COMPARTMENT RH #2 FLOOR SILL AND POSTIONED, DRILLED, AND INSTALLED SERVICEABLE CARGO COMPARTMENT RH #2 FLOOR SILL IAW EMB 145 SRM 51-40-02 AND SRM 51-20-03

Part: ECS — ODOR (COCKPIT) · airframe 46,886 hrs · 44,030 cycles

PDIS 635, FOUL ODOR IN COCKPIT ON TAKE OFF AND LANDING. SMELL DISSIPATED AFTER 2 OR 3 MINUTES. - CAPTAIN SAID SMELL ONLY IN COCKPIT AND FLIGHT ATTENDANT DIDN'T SMELL ANYTHING IN CABIN. FACT 11APR21 16:14 PERFORMED VISUAL INSPECTION OF ENGINES, NO OIL LEAK OR ODOR NOTED. PERFORMED VISUAL INSPECTION OF PACK 1 AND 2 NO EXTERNAL LEAKS OR ODORS NOTED. RAN ENGINES TO T/O POWER WITH PACKS 1 AND 2 ON WITH CREW. NO ABNORMAL ODORS NOTED. AC OK FOR SERVICE AT THIS TIME.

Part: UNKNOWN — ODOR · airframe 46,862 hrs · 44,000 cycles

PDIS 635 21-01 2441972 06APR21 SBY CLOSE BURNING SMELL NOTED DURING TAKEOFF, WITH PACKS AND BLEED TURNED ON. SMELL DISAPPEARS AFTER 2-3 MINUTES. FACT 06APR21 05:15 SBY DUE TO PREVIEWS DISCREPANCY ON 05APR21 COMPLIED WITH MAINT FOLLOW UP TASK HA-300 SEQ#3.MAINT REQUESTED EVALUATION FLIGHT TO DETERMING IF FURTHER ACTION IS REQUIRED.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,862 hrs · 44,000 cycles

PDIS 635 21-01 2441961 05APR21 ROA CLOSE STRONG FOUL SMELL ON TAKE OFF AND LANDING. SMELLED LIKE BURNT OIL. SMELL DIMINISHED IN FLIGHT FACT 05APR21 03:22 ROA RAN BOTH ENGINE BLEEDS ON AND APU, NO FOUL SMELLS NOTED. INSPECTED ENGINE EXHAUST FOR SIGNS OF OIL. NO WETNESS NOTED.

Part: POTENTIOMETER — FAILED (NLG STEERING) · airframe 46,154 hrs · 43,194 cycles

STEERING INOP MESSAGE APPEARED AFTER HAND WHEEL RELEASED 5 ATTEMPTS AND MESSAGE STILL CAME UP. R&R LOAD POTENTIOMETER IN COCKPIT MX PANEL IAW AMM 32-50-05. OPS CHECK GOOD. OK FOR SERVICE.

Part: MANIFOLD — FAILED (NLG STEERING) · airframe 46,154 hrs · 43,194 cycles

NWS WILL NOT ENGAGE. R+R STEERING MANIFOLD IAW 32-50-04. OPS CHECK IAW AMM 32-50-00. OPS AND LEAK CHECK GOOD. OK FOR SERVUCE

Part: RELAY — FAILED (NR 2 STARTER) · airframe 46,149 hrs · 43,189 cycles

E2 ATS SOV OPEN ON EICAS IN FLIGHT. R+R RELAY K0114 IAW AMM 20-13-02. RAN #2 ENGINE WITH #2 BLEED ON ABOVE 54% N2 FOR 20 MINUTES. MESSAGE DID NOT SHOW ON EICAS. OPS CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: START VALVE — FAILED · airframe 46,148 hrs · 43,186 cycles

#2 ATS SOV OPN MESSAGE APPEARED AFTER SMELLING AN UNKNOWN FUME FOR 2 MINUTES. (SMELL PERSISTED AFTER FOLLOWING QRH AND WOULD INCREASE AS THROTTLE INCREASED. OCCURED IN CRUISE) FOLLOWED THE FIM TASK 80-10-00-810-803-A AND R&R'D STARTER CONTROL VAVLE ASSY AS REQUIRED PER AMM 80-10-02. GROUND RAN #2 ENGINE OPS NORMAL AT THIS TIME.

Part: PDU — MALFUNCTIONED (TE FLAP) · airframe 44,558 hrs · 41,380 cycles

FLAP FAIL MSG DURING FLIGHT, HANDLE MOVED TO 9 DEGREES, AFTER LANDING FLAP OBSERVED TO BE AT 0 DEGREES. FIX: FOUND FLAP POSITION TRANSDUCER UNIT TO BE ROTATED IN HOUSING. R&R D FLAP POWER DRIVE UNIT IN REF TO AMM 27-53-04. OPS CHECK GOOD. OK FOR SERVICE. NOTE: FLAPS FAILED DURING DEPLOYMENT GOING INTO MDT. EMERGENCY DECLARED.AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE UNDER ITS OWN POWER.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,374 hrs · 41,187 cycles

EMERGENCY LIGHT ON RH FWD DOOR INOPERATIVE. REMOVED AND REPLACED BULB, OPS CHECKED GOOD

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 44,097 hrs · 40,872 cycles

PDIS 635 32-42 1917502 05MAY19 CLE CLOSE BRAKE ON LIGHT CAME ON DURING FLIGHT. LANDING ROLL OUT WAS NORMAL WITH NO PARK BRAKE ACTUALLY ON. CW DEACTIVATION PROCEDURE FOR EMERGENCY PARKING BRAKE PRESSURE SWITCH. FACT 06MAY19 01:42 PHL COULD NOT DUPLICATE ISSUE. R&R RELAY K0212 AS PROGRESSIVE ACTION IAW 20-13-02-04. BRAKE ON LIGHT OPERATES NORMAL. OK FOR SERVICE AT THIS TIME. CLEAR MEL 32-5-1.

Part: SENSOR — MALFUNCTIONED (AOA SYSTEM) · airframe 43,374 hrs · 40,043 cycles

SPS2 INOP WARNING AND SPS ADVANCED ON EICAS DURING TAKE OFF ROLL. R&R NR 2 AOA SENSOR IAW AMM 27-36-01. PERFORMED SPS OPS CHECK IAW AMM 27-36-00, OPS CHECK GOOD, NO DEFECTS FOUND, OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,092 hrs · 39,724 cycles

NDIS 635 33-51 0018250 14OCT18 SBY CLOSE EMERGENCY EXIT LIGHT ABOVE SERVICE DOOR INOP. 31254 00 SPE FACT 14OCT18 10:42 SBY R&R EMERGENCY EXIT LIGHT ABOVE SERVICE DOOR & RESET CIRCUIT BREAKER. OPS CHECK GOOD CEILING PANEL RESECURED. P/N ON/OFF 7444-1

Part: POTENTIOMETER — DEFECTIVE (NLG STEERING) · airframe 43,087 hrs · 39,717 cycles

ON LANDING AS NOSE WHEELS TOUCHED DOWN A/C SWERVED HARD RIGHT. RUDDER AND REVERSE INEFFECTIVE. KEPT ON RUNWAY WITH STEERING HANDLE. ALSO A LOUD GRINDING WHILE STEERING TILLER IS ENGAGED. R&R STEERING MANIFOLD IAW AMM32-50-04, NO FIX. R&R FEEDBACK POTENTIOMETER IAW AMM 32-50-07. ADJUSTED FEEDBACK UNIT POTENTIATE IAW AMM 32-50-00 OPS AND TAXI CHECK GOOD NO DEFECTS NOTED AT THIS TIME OK FOR SERVICE.

Part: DAU — MALFUNCTIONED (NR 1) · airframe 42,921 hrs · 39,524 cycles

DAU 1B FAIL OK TAKEOFF ROLL AT 90KTS REJECTED TAKEOFF AND RETURN TO GATE. R&R NR 1 DAU. OPS CHECK GOOD AT THIS TIME REF AMM 31-41-01. OKAY FOR SERVICE.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 42,842 hrs · 39,439 cycles

VERTICAL STAB DRAG ANGLE ON THE LEFT SIDE OF FRAME 75 REPAIR DOUBLER WAS CRACKED AFT OF DOUBLER. R & R THE LT VERTICAL STABILIZER FWD LOWER DRAG ANGLE IAW SRM 51-40-02, AND 53-31-01, ITEM 11, AND FIGURE 219.

Part: SPAR — CRACKED (RT WING) · airframe 42,842 hrs · 39,439 cycles

RT WING SPAR NR 1 LOWER FLANGE AT RIB 9 HAD A CRACK AT FASTENER. REPAIRED THE WING SPAR IAW SRM 57-20-05, ITEM 2.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 42,506 hrs · 39,072 cycles

BLEED 2 VALVE FAIL MSG IN FLIGHT WITH ICING CONDITIONS. CREW RAN QRH. GROUND RAN AC AND PERFORMED OPS CHECK OF BLEED VALVES IAW AMM 36-11-05. OPERATIONAL CHECK GOOD. OK FOR SERVICE.

Part: AOA — OUT OF ALIGNMENT · airframe 42,395 hrs · 38,951 cycles

ABORTED TAKEOFF DUE TO A SPS FAIL MESSAGE. INSPECTED AND FOUND AOA SENSORS NOT PROPERLY ALIGNED. ALIGNED THE SENSORS TO MATCH AND PERFORMED AN OPS CHECK IAW AMM 27-36-00-700-801-A. SYSTEM OPS CHECKED GOOD. OKAY FOR SERVICE.

Part: PROXIMITY SWITCH — FAILED (MLG) · airframe 42,267 hrs · 38,804 cycles

ON LIFTOFF, MLG AIR GROUND FAILED AND THE NR 1 & 2 ENGINE REVERSER DISAGREE EICAS MESSAGES APPEARED AND REMAINED ON UNTIL TOUCHDOWN. R & R THE WOW PROXIMITY SWITCH HARNESS, R & R THE NOSE GEAR UPLOCK HARNESS. R & R THE NLG WOW PROXIMITY SWITCH.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,420 hrs · 37,923 cycles

SERVICE DOOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-10, OPS CHECKED GOOD.

Part: SWITCH — MALFUNCTIONED (TRIM) · airframe 41,271 hrs · 37,750 cycles

IMMEDIATELY AFTER TAKEOFF, LG AIR/GRD FAIL CAUTION MESSAGE DISPLAYED ON EICAS AND PITCH TRIM MAIN INOPERATIVE WARNING MESSAGE. PITCH TRIM RUN AWAY TO NOSE DOWN. R & R THE BACKUP TRIM SWITCH AND OPS CHECKED IAW AMM 20-13-05. OPS CHECKED GOOD. COULD NOT DUPLICATE. R & R LGEU AS PRECAUTIONARY MEASURE.

Part: UNKNOWN — ODOR (CABIN) · airframe 41,212 hrs · 37,695 cycles

ACFT WAS IN ROUGH AIR WHEN CREW AND PAX SMELLED AN ELECTICAL BURNING ODOR. NO SMOKE WAS SEEN. ODOR DISSIPATED AS FLIGHT CONTINUED. INSPECTED THE AIRCRAFT FOR OBVIOUS DEFECTS REGUARDING THE ELECTRICAL ODOR. FOUND NO OBVIOUS DEFECTS OR ORIGIN OF SUSPECT ODOR. OK FOR SERVICE.

Part: HANDSET — FAILED · airframe 41,157 hrs · 37,638 cycles

ELECTRICAL BURNING ODOR COMING FROM FWD FA HANDSET AREA.AFTER LOSING INTERPHONE AND PA ON ALL STATIONS. R & R FWD HANDSET AND CRADLE AND PA AMP. OPS CHECKED GOOD IAW MM 23-31-00-700-801-A.

Part: RELAY — BURNED · airframe 40,743 hrs · 37,200 cycles

DURING INSPECTION OF PIVOT, NR 3 RELAYS AND SOCKET CIRCURITY, FOUND WIRE W102027016 BURNED ALONG WITH SOCKET IN RECEPTICLE WIRE W102-0288-16 WAS BURNED ALONG WITH SOCKET 2 IN RECEPTICLE, RELAY SHOWED EVIDENCE OF BURNING, MELTING, AND DISCOLORATION, ALL WIRES MENTIONED ABOVE WERE BURNED WITH INSULATION MISSING AND THE RECEPTICAL SOCKETS 2 AND 3 OF K0058. REMOVED AND REPLACED K0058 AND K1237, REMOVED AND REPLACED RELAY BASE XK0058 AND XK1237. REMOVED AND REPLACED WIRE W1102-0283-16, AND REPAIRED WIRE W102-027-16 USING M227/59/16 16AWG WIRE AND MPN M 81824-1-6 SPLICE. OPS CHECKED GOOD IAW 30-31-00-700-801-A.

Part: AOA — MALFUNCTIONED (STALL WARNING) · airframe 40,438 hrs · 36,861 cycles

TAKE OFF AT 75 KNOTS ABORTED DUE TO MULTIPLE 1 CAUTION AND 2 WARNING MESSAGES. CMC SHOWED AOA FAILED, PERFORMED STALL PROTECTION OPS CHECK IAW AMM 27-36-00-700-801-A/500 AND 2 HIGH SPEED RUN OPS AT 80 KNOTS NO DEFECTS NOTED AT THIS TIME OK FOR SERVICE.

Part: CONTROL UNIT — FAILED (PITCH TRIM) · airframe 39,483 hrs · 35,826 cycles

PITCH TRIM MAIN INOPERATIVE EICAS MESSAGE ILLUMINATED IN FLIGHT AT FLIGHT LEVEL 230. R & R THE HSCU AND PERFORMED OPS CHECK IAW MM 27-40-01. NO OTHER DEFECTS NOTED. OK FOR SERVICE.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 39,216 hrs · 35,522 cycles

STRONG ELECTRICAL ODOR IN CABIN COMING FROM ROW 2A AND 3A OVERHEAD. INSPECTED AND FOUND LIQUID CONTAINER TO BE CAUSE OF ODOR. UNPLUGGED LIQUID CONTAINER. R & R HOT JUG RECEPTACLE IAW AMM 25-30-02-04. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 39,110 hrs · 35,385 cycles

DURING T/O ROLL NO TAKEOFF CONF EICAS WARNING MESSAGE. T/O ABORTED, F/O REPORTED SPOILER OPEN MOMENTARILY. AFTER SPOILER CLOSED EICAS MESSAGE EXTINGUISHED. C/W SPOILER TEST IAW 27-63-01. OPS CHECK GOOD. NO DEFECTS NOTED. NO EICAS OR CMC CODES. OK FOR SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,955 hrs · 35,192 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED AT FRAME 75, ABOVE STRINGER 2R. REPAIRED RT UPPER FUSELAGE SKIN CRACK IAW ERS-EM-53MR-1984.

Part: SKIN — CORRODED (FUSELAGE) · airframe 38,955 hrs · 35,192 cycles

INTERNAL FUSELAGE SKIN CORRODED ON FRAME 67 FWD & AFT SIDES, BETWEEN STRINGER 21L - 21R. REPAIRED FUSELAGE I SKIN IAW ERS-EM-53MR-1971.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,955 hrs · 35,192 cycles

LEFT UPPER FUSELAGE SKIN CRACKED AFT FRAME 75 ABOVE STRINGER 2L. REPAIRED LT UPPER FUSELAGE SKIN CRACK IAW ERS-EM-53MR-1984.

Part: SUPPORT — CORRODED (LAVATORY) · airframe 38,955 hrs · 35,192 cycles

SSI 53-20-29 TOILET WASTE VLV SUPPORT, LAVATORY BUCKET, IS CORRODED. R & R LAVATORY BUCKET IAW SRM 51-40-02

Part: RIB — CHAFED (LT WING) · airframe 38,955 hrs · 35,192 cycles

LEFT AIL PCA SYS NR 1 RETURN BLUE FLEXIBLE HOSE IS CHAFING ON LOWER RIB INSIDE 551CB. REPAIRED LT WING 21 CHAFE IAW ERS-EM-57MR-594.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,955 hrs · 35,192 cycles

DENT BETWEEN FRAME 77 - 80 & STRINGER 17L. REPAIRED DENT IAW ERS-EM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 38,951 hrs · 35,190 cycles

EMERGENCY LIGHT STRIP NR 5 HAS BROKEN CONNECTOR AT FLOOR. REPLACED CONNECTOR ON EMER LIGHT STRIP NR 5 IAW SWPM 20-21-00. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.

Part: STRUT — LOW (NLG) · airframe 38,835 hrs · 35,099 cycles

ENG 1 - 2 REV DISAGREE & LG AIR & GND FAILED AFTER GEAR RETRACTION AFTER LIFTOFF. DURING LG EXTENSION FOR LANDING, MSG WENT AWAY. SERVICED NOSE STRUT, POST MOD, IAW MM 32-20-01. LEAK CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 38,439 hrs · 34,735 cycles

AFT CABIN FLASHLIGHT IS INOPERATIVE. R & R AFT CABIN FLASHLIGHT IAW AMM 33-50-00.

Part: UPLOCK — FAILED (RT MLG) · airframe 38,391 hrs · 34,696 cycles

AFTER TAKEOFF & GEAR RETRACT, HEARD A LOUD CONTINUOUS THUMPING UNDER ACFT & RT MAIN GEAR LIGHT CHANGING FROM GREEN TO AMBER. RETURNED TO FIELD FOR LANDING. TRANSFERRED TO NRWC 635-ABI-02482. R & R RT UPLOCK BOX IAW AMM 32-33-10. OPERATIONS & LEAK CHECKED GOOD.

Part: FLASHLIGHT — BURNED (COCKPIT) · airframe 37,950 hrs · 34,277 cycles

SMELL OF SOMETHING BURNT IN THE COCKPIT. R & R FIRST OFFICERS FLASHLIGHT & BASE IAW AMM 33-51-01.

Part: SPLICE — DAMAGED (PAX DOOR) · airframe 37,848 hrs · 34,207 cycles

PASSENGER DOOR EMER LIGHT INOPERATIVE. REPLACED SPLICE SP7426 AT MAIN PAX DOOR EXTERNAL LIGHT IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 37,824 hrs · 34,186 cycles

FIRST OFFICERS FLASHLIGHT IS VERY DIM WITH NEW BATTERY. R & R FIRST OFFICER`S FLASHLIGHT ASSEMBLY. OPERATIONS CHECKED GOOD IAW AMM 33-50-16.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 37,398 hrs · 33,826 cycles

REFERENCE ITEM NR 2 OF THIS LOG PAGE, COCKPIT FLASHLIGHT INOPERATIVE. R & R COCKPIT FLASHLIGHT BEHIND CAPTAIN IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: BULB — BURNED OUT (FLASHLIGHT) · airframe 37,308 hrs · 33,762 cycles

FIRST OFFICERS FLASHLIGHT BULB IS BURNED OUT. REPLACED LIGHT BULB. OPS CHECKED GOOD IAW AMM 33-51-01.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,265 hrs · 33,726 cycles

LEFT SIDE CTR FAIRING EMER LIGHT INOPERATIVE. R & R LT SIDE CTR FAIRING EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,081 hrs · 33,589 cycles

ROW 12 AISLE EMER LIGHT INOPERATIVE. R & R ROW 12 EMER LIGHT LAMP IAW AMM 33-50-08-000-801-A & 33-50-08-400-801-A. OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 36,853 hrs · 33,395 cycles

FIRST OFFICER'S EMER FLASHLIGHT HOLDER BROKEN. R & R FIRST OFFICER`S EMER FLASHLIGHT HOLDER IAW TASK 33-50-16-000-801-A & TASK 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — MISSING (CABIN) · airframe 36,838 hrs · 33,381 cycles

FOUND EMER LIGHT AFT CABIN CEILING INOPERATIVE DUE TO PULLED WIRE. INSPECTED & FOUND CONNECTOR GONE. INSTALLED NEW CONNECTOR IAW SWPM 20-13-02. OPERATIONAL CHECKED GOOD.

Part: CONTROLLER — FAILED (WINDOW HEAT) · airframe 35,240 hrs · 32,017 cycles

ENROUTE IN ICING CONDITIONS, WS HEAT NR 1 FAIL EICAS CAUTION MSG PRESENTED. AOM 1 EMER & ABNORMAL PROCEDURE COMPLIED WITH & MSG RESET. HOWEVER, AFTER TWO MINUTES THE SAME HEAT NR 1 FAIL EICAS CAUTION MSG PRESENTED AGAIN. REMOVED & INSTALLED SERVICEABLE NR 1 WS HEAT TEMP CONTROLLER IAW AMM 30-42-01. FUNCTION CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 35,119 hrs · 31,910 cycles

FWD GALLEY CEILLING EMER EXIT SIGN INOP. RECONNECT CONNECTOR & PERFORM OPT CHECK GOOD IAW EMB 145 AMM 33-50-00.

Part: AUDIO PANEL — DEFECTIVE (COCKPIT) · airframe 35,086 hrs · 31,879 cycles

FIRST OFFICER`S DIGITAL AUDIO PANEL EMER LIGHT INOPERATIVE. R & R FIRST OFFICER`S DIGITAL AUDIO PANEL IAW AMM 23-51-01. OPERATIONAL CHECKED OK IAW AMM 23-51-00, SUB TASKS 23-51-00-700-801-1 & 23-51-00-700-802-A.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 34,805 hrs · 31,641 cycles

MAIN CABIN DOOR HANGS UP ON SOMETHING WHEN OPENING. LUBRICATED MAIN CABIN DOOR ROLLERS, OPERATIONS CHECKED GOOD IAW AMM 52-10-01.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 34,779 hrs · 31,611 cycles

SMOKE IN THE COCKPIT WHEN NR 1 PACK TURNED ON FROM APU SOURCE. TRANSFERRED TO NRWC 635-DFW-01735. AFTER FOLLOWING FIM TASK 21-20-00-810-801-A & SERVICE NEWSLETTER 145-49-0005, FOUND EVIDENCE OF OIL LEAK DUE TO APU OIL OVER SERVICE. CORRECTED APU OIL QTY IAW AMM 49-96-00. LEAK CHECKED GOOD, NO FURTHER SMOKE OR ODOR IN COCKPIT IAW AMM 21-00-00.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 34,754 hrs · 31,594 cycles

MAIN CABIN DOOR CATCHES WHILE OPENING, HARD TO OPEN. PERFORMED ADJUSTMENT & TEST OF PAX DOOR IAW AMM 52-18-00. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 34,753 hrs · 31,593 cycles

NR 1 ENGINE OIL LEVEL DEPLETED TO 3 QTS DURING FLIGHT. SERVICED NR 1 ENGINE OIL IAW WC. REMOVED AND REPLACED LT ENGINE IAW WC 71-000-00. OPS AND LEAK CHECKED GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,747 hrs · 31,586 cycles

DURING HMBV INSPECTION, QA FOUND ON FRAME 65, TWO CORRODED NUTPLATE HOLES JUST ABOVE LT FLOOR SUPPORT. ACFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. PERFORMED PERMANENT REPAIR ON TWO CORRODED NUTPLATE HOLES ON FRAME 65 JUST ABOVE LT FLOOR SUPPORT IAW ERS-EM-53MR-327. REPAIR DOUBLER AL 2024 T3, 0.050 INCHES.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,747 hrs · 31,586 cycles

CO-PILOTS RT FLOOR SUPPORT CORRODED AROUND YOKE MOUNTING BASE. BLENDED OUT CORROSION ON CO-PILOTS RT FLOOR SUPPORT AROUND YOKE MOUNTING BASE IAW CPM 51-14-00. MAPPED DAMAGE IAW AE ETN-GN-51-013R2. ACCEPTED AS IS IAW ERS-EM-5300-313.

Part: WIRE — EXPOSED (CABIN) · airframe 34,747 hrs · 31,586 cycles

NR 6 EMERGENCY PROXIMITY LIGHT STRIP WIRES EXPOSED. R & R NR 6 EMERGENCY PROXIMITY LIGHT STRIP AS REQUIRED SEE BOW151123 FOR INSTALLATION OF EMERGENCY PROXIMITY LIGHT STRIPS.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 34,747 hrs · 31,586 cycles

CARGO DOOR FWD FRAME HAS CORROSION AROUND SEVERAL NUTPLATE HOLES. CARGO DOOR FWD FRAME CORROSION AROUND SEVERAL NUTPLATE HOLES ACCEPTED IAW ERS-EM-5200-098.

Part: BATTERY PACK — DAMAGED (EMERGENCY LIGHTS) · airframe 34,747 hrs · 31,586 cycles

EMERGENCY LIGHTS BATTERY HOLDER ASSEMBLY NOT OPERATING. EMERGENCY LIGHTS REMOVED BATTERY HOLDER ASSEMBLY.

Part: CONNECTOR — BROKEN (CABIN) · airframe 34,747 hrs · 31,586 cycles

EMERGENCY LIGHT STRIP AT SEAT 10A HAS A BROKEN CONNECTOR, AIRFRAME SIDE. INSTALLED CONNECTOR ON EMERGENCY LIGHT STRIP WIRE AT SEAT 10A IAW SWPM 20-21-00. SEE NRTC BOW151123 TASK NR 2 FOR OPERATIONAL CHECK.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 34,747 hrs · 31,586 cycles

LEFT OVERWING UPPER BRACKET AFT SUPPORT IS CRACKED. R & R LT OVERWING UPPER BRACKET AFT SUPPORT IAW SRM 51-40-02 & 51-20-03.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 34,747 hrs · 31,586 cycles

NUMEROUS INTERIOR EMERGENCY LIGHTS NOT FUNCTIONING. R & R BATTERY POWER SUPPLY 2 IAW AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,747 hrs · 31,586 cycles

FUSELAGE EXTERNAL SKIN CRACKED AROUND 1 FASTENER RT SIDE FRAME 79 BELOW VERTICAL STABILIZER. CUT OUT DAMAGED AREA TO 0.375" IAW ERS-EM-5300-319. INSTALLED REPAIR BUSHING ON EXTERNAL SKIN AT RT SIDE FRAME 79 BELOW VERTICAL STABILIZER IAW ERS-EM-5300-319.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,747 hrs · 31,586 cycles

BATTERY CHARGER EMERGENCY LIGHT NOT OPERATING. REMOVED BATTERY CHARGER.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 34,747 hrs · 31,586 cycles

FWD RT PULLEY SUPPORT CORRODED BETWEEN FRAME 16 & FRAME 17 AT STRINGER 21R. R & R FWD RT PULLEY SUPPORT BETWEEN FRAME 16 & 17 & STRINGER 21L - 21R IAW SRM 51-40-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,371 hrs · 31,270 cycles

DURING PS 2 INSPECTION EMERGENCY LIGHT FLOOR STRIP AT 3A - 4A INOPERATIVE. ACFT WAS REMOVED FROM SERVICE. R & R EMERGENCY LIGHT FLOOR STRIP 3A - 4A IAW AMM 33-50-12. OPERATIONAL CHECKED OK.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 34,350 hrs · 31,251 cycles

ON FLIGHT 3158 CREW REPORTED HYD 1 FAIL, DECLARED EMERGENCY & LANDED WITHOUT INCIDENT AT MSN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 HYD PUMP IAW EMB 145 AMM 29-10-03 OPS CHECK LEAK CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,325 hrs · 31,232 cycles

AFT BULKHEAD EMERGENCY FLASHLIGHT IS INOPERATIVE. R & R AFT BULKHEAD EMERGENCY FLASHLIGHT IAW AMM 33-51-01.

Part: PROXIMITY SENSOR — MALFUNCTIONED (NLG) · airframe 34,225 hrs · 31,151 cycles

ON FLIGHT 3621 IMMEDIATELY AFTER TAKEOFF CREW REPORTED LANDING GEAR AIR GROUND FAIL CAUTION MESSAGE APPEARED ON EICAS. DECLARED EMERGENCY & IMMEDIATELY RETURNED TO THE AIRPORT & LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NLG AIR GROUND WOW PROXIMITY SWITCH IAW NRWC 635-ORD-01605 IAW EMB AMM 32-63-02. THE ACFT RETURN TO SERVICE.

Part: MECHANISM — LACK OF LUBE (DOOR LOCKING) · airframe 33,647 hrs · 30,699 cycles

F/A REPORTS MAIN CABIN DOOR HANDLE IS HARD TO OPERATE. LUBRICATED MAIN CABIN DOOR LOCKING MECHANISM IAW AMM 52-18-00. OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 33,194 hrs · 30,326 cycles

MAIN CABIN DOOR HARD TO OPEN AND CLOSE. LUBED FRAME DOOR ROLLERS REF AMM 53-21-02 AND OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 33,161 hrs · 30,302 cycles

AFT F/A EMERGENCY FLASHLIGHT INOPERATIVE. R & R AFT FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 33,087 hrs · 30,246 cycles

DURING MX INSPECTION, FOUND AFT F/A FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW AMM 33-50-16 OPS CHECKED GOOD.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 32,940 hrs · 30,117 cycles

DURING B INSPECTION, FOUND CABIN FORWARD FLASHLIGHT HOLDER CRACKED. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT HOLDER ASSEMBLY IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 32,782 hrs · 29,981 cycles

DURING B-INSPECTION FOUND THE FWD CABIN EMERGENCY FLASHLIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE FLASHLIGHT MOUNTED ABOVE THE F/A`S SEAT AT THE FWD CABIN IN REF WITH AMM TASK 33-50-16-000-801-A AND TASK 33-50-16-400-801-A. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DAMAGED (CAPTAIN’S) · airframe 32,389 hrs · 29,642 cycles

FLIGHT 2907, CAPTAIN’S FLASHLIGHT WAS DAMAGED. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 31,785 hrs · 29,191 cycles

DURING MAINTENANCE INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IAW 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 31,719 hrs · 29,138 cycles

DURING B INSPECTION FOUND THE 2ND EMERGENCY LIGHT FLOOR STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT INVERTER. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 31,689 hrs · 29,112 cycles

DURING MAINTENANCE INSEPCTION FOUND THE EMERGENCY FLASHLIGHT HOLDER BEHIND THE CAPTAINS SEAT HAD A CRACKED IN THE UPPER ARM WHICH SUBSEQUENTLY BROKE OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT HOLDER IAW EMB145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 30,874 hrs · 28,473 cycles

DURING B INSPECTION FOUND THE FIRST OFFICER’S EMERGENCY FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S EMERGENCY FLASHLIGHT BRACKET ASSEMBLY PER EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 30,874 hrs · 28,473 cycles

DURING B INSPECTION FOUND THE AFT CABIN CEILING EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED AFT CABIN EXIT IDENTIFIER IN REFERENCE WITH EMB AMM TASKS 25-24-01-000-801-A & 25-24-01-400-801-A. THE OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,547 hrs · 28,156 cycles

DURING MAINTENANCE INSPECTION, FOUND MOST AFT OVERHEAD AISLE EMERGENCY LIGHT BURNED OUT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY EXIT CEILING LIGHT ASSEMBLY IAW AMM 33-50-08. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,371 hrs · 28,016 cycles

DURING B INSPECTION, FOUND THE RIGHT EXTERIOR EMERGENCY LIGHT FORWARD OF WING INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT EXTERIOR EMERGENCY LIGHT FORWARD OF WING IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — OBSTRUCTED (MAIN CABIN) · airframe 30,349 hrs · 27,997 cycles

FLIGHT 3388, FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CURTAIN STRAP FROM DOOR. CLEAN AND LUBE ROLLS IAW AMM 52-18-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: TRUNNION — CORRODED (LT MLG) · corrosion level 2 · airframe 30,196 hrs · 27,868 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT MAIN LANDING GEAR UPPER BEARING HALF TRUNNION HAS CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. ACCOMPLISHED EO EM-57MR-631. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,214 hrs · 27,884 cycles

DURING B INSPECTION FOUND THE CARGO DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NEW SERVICEABLE CARGO DOOR SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (RT WING) · airframe 30,196 hrs · 27,868 cycles

RT WING NR 5 RIB CRACKED AT AFT LARGE LIGHTNING HOLE. R & R RT WING RIB 5 IAW EO EM-57MR-629.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,214 hrs · 27,884 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR AFT SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT SERVICE DOOR SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,214 hrs · 27,883 cycles

DURING B INSPECTION FOUND THE LEFT NR 1 FLOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED THE LEFT NR 1 FLOOR SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 30,214 hrs · 27,883 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 8 EMERGENCY LIGHT STRIP HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 8 EMERGENCY PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 30,214 hrs · 27,884 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 5 EMERGENCY LIGHT STRIP HAS BROKEN WIRES. SPLICED THE NR 5 EMERGENCY LIGHT STRIP BROKEN WIRES IAW EMB 145 WM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,214 hrs · 27,883 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR FORWARD SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED THE SERVICE DOOR FORWARD SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,214 hrs · 30,214 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT EXTERNAL FORWARD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT EXTERNAL FORWARD EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 30,214 hrs · 27,884 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 4 EMERGENCY LIGHT STRIP HAS BROKEN WIRES. SPLICED THE NR 4 EMERGENCY LIGHT STRIP BROKEN WIRES IAW EMB 145 WM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,090 hrs · 27,785 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT FORWARD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB FOR THE RIGHT FORWARD EMERGENCY LIGHT IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,049 hrs · 27,754 cycles

DURING B-INSPECTION FOUND THE RIGHT HAND OVER WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW AMM TASK 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: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 29,982 hrs · 27,695 cycles

ON FLIGHT 4101 THE CREW REPORTED THE FLASHLIGHT ABOVE THE CAPTAIN’S SEAT DOES NOT WORK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT IAW EMB 145 MM CH 33-50-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 29,968 hrs · 27,684 cycles

ON FLIGHT 4078 THE CREW REPORTED THE CAPTAIN'S FLASHLIGHT WAS INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT ON CAPTAIN'S SIDE IAW EMB-145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,737 hrs · 27,485 cycles

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

Part: INVERTER — INOPERATIVE (CABIN) · airframe 29,405 hrs · 27,217 cycles

DURING B-INSPECTION FOUND THE EMERGENCY LIGHTS INOPERABLE AT COCKPIT STEP, COCKPIT BULKHEAD AND GALLEY AISLE CEILING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD IAW AE W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,634 hrs · 26,649 cycles

FOR FLIGHT 2882 DURING PREFLIGHT INSPECTION MAINTENANCE FOUND THE OVERHEAD GALLEY EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW BULB IAW AMM 33-50-09. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,636 hrs · 26,651 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE OVERHEAD GALLEY EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW BULB IAW AMM 33-50-09. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DEFIBRILLATOR — UNSERVICEABLE (CABIN) · airframe 28,174 hrs · 26,289 cycles

FOR FLIGHT 3931 THE CREW NOTICED THE SEAL WAS MISSING FORM THE DEFIBRILLATOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW DEFIBRILLATOR AS REQUIRED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TIRE — DAMAGED (NLG) · airframe 27,946 hrs · 26,106 cycles

ON FLIGHT 4261 THE CREW REPORTED THE RIGHT NOSE LANDING TIRE DAMAGED UPON LANDING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AND RIGHT NOSE WHEEL ASSEMBLY IAW WK CD 32-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,783 hrs · 25,975 cycles

DURING PS-2 MAINTENANCE BASE VISIT WHILE ACCOMPLISHING OPERATIONAL CHECK OF EMERGENCY LIGHTS DURING INSPECTION FOUND THE NR 3 EMERGENCY CEILING LIGHT FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BULB. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,211 hrs · 24,742 cycles

FOR FLIGHT 2773 DURING PREFLIGHT CHECK FOUND THE RIGHT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT EMERGENCY LIGHT. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HYDRAULIC LINE — DEFECTIVE (RT MLG) · airframe 25,566 hrs · 24,226 cycles

ON FLIGHT 3948 DURING CRUISE THE CREW REPORTED, RECEIVED A HYDRAULIC 1 LOW QUANTITY MESSAGE FOLLOWED BY E1 HYDRAULIC PUMP FAIL AND THE ELECTRIC HYDRAULIC PUMP CYCLED ON AND OFF. AT GEAR EXTENSION RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED AT ORD WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN LANDING GEAR (RIGHT) ACTUATOR HOSE ASSEMBLY IAW EMB 145 MM CH 32-33-08. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (BS 89.134-105.39) · airframe 25,503 hrs · 24,183 cycles

FLT 3610 SHORT FINAL, A BIRD STRIKE BELOW CAPTAINS WINDSHIELD. ACFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. ACFT GROUNDED FOR TEMP REPAIR & RELEASED FOR A FERRY FLT. LARGE DENT BETWEEN SKIN PANELS AT BUTT SPLICE. SEVERAL SHEARED RIVETS AT BUTT SPLICE. LT FWD LATERAL PANEL IS CRACKED & LIFTING. SPLICE STRAP ALSO DAMAGED. DENT LOCATED BETWEEN FRAMES 7 & 8 S6 & 8L. DENT MEASURES APPROX 11 " BY 12 " & 0.75 " AT ITS DEEPEST POINT. R & R LT SKIN & UPPER CENTER SKIN IN FRONT OF WINDSHIELD IAW SRM 51-40-02. R & R WINDSHIELD FRONT STRAP IAW SRM 51-40-02, 51-40-04, 51-40-06, 51-40-05, 51-40-09 & 51-20-03. INSTALLED WINDSHIELD CENTER POST & LOWER MOUNT IAW AMM 53-12-01. ACFT RETURNED TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (CARGO BAY) · airframe 24,807 hrs · 23,660 cycles

FOR FLIGHT 3546 CREW REPORTED, WHILE PARKED AT THE GATE RECEIVED AN EICAS BAGGAGE SMOKE MESSAGE ALONG WITH A TRIPLE CHIME WARNING WHEN THE RAMP OPENED THE CARGO DOOR. THE EICAS MESSAGE WENT AWAY AND NO SIGN OF SMOKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH VISUAL INSPECTION OF SMOKE DETECTORS IAW AMM 26-15-01-200-802-A. COMPLIED WITH OPERATIONAL TESTS IAW AMM 26-15-00-700-804-A, NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,382 hrs · 23,316 cycles

DURING A MAINTENANCE CHECK THE CLEANING CREW REPORTED THAT THE EMERGENCY LIGHTS WERE CYCLING ON AND OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 4 BATTERY PACK AND REMOVED AND REPLACED THE NUMBER 4 CHARGER. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BALLAST — UNSERVICEABLE (CABIN LIGHTS) · airframe 22,145 hrs · 21,180 cycles

ON FLIGHT 3890, CREW REPORTED STRONG ODOR BY MAIN CABIN DOOR SMELLS LIKE NAIL POLISH REMOVER. AIRCRAFT REMOVED FROM SERVICE. REPLACED LIGHT BALLAST ABOVE SEAT BACK 1A IAW AMM 33-21-03. AIRCRAFT RETURNED TO SERVICE.

Part: BALLAST — FAULTY (CABIN) · airframe 21,257 hrs · 20,400 cycles

FLIGHT 3982 - CREW NOTICED A BURNING SMELL IN GALLEY. AIRCRAFT REMOVED FROM SERVICE. FOUND CEILING BALLAST FOR ROW 2 AND 3 TO BE THE SOURCE OF THE SMELL. REMOVED AND REPLACED ROW 2 AND 3 CEILING BALLASTS AND ASSOCIATED HARNESS IAW EMB 145 MM 33-21-05. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: THERMAL SWITCH — FAILED (HYD OVERHEAT)

ON FLIGHT 3839 CREW REPORTED AT CRUISE NUMBER 2 HYDRAULIC SYSTEM OVERHEAT FOLLOWED BY NUMBER 2 HYDRAULIC SYSTEM FAIL. AFTER AOM COOL DOWN PERIOD INITIALLY WOULD NOT TURN ON WITH EICAS SYSTEM OVER HEAT MESSAGE GONE. CREW TRIED 5 MIN LATER AND SYSTEM CAME ON. CREW DECLARED EMERGENCY AND LANDED WITH OUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED HYDRAULIC SYSTEM RESERVOIR 2 THERMAL SWITCH IAW EMB 145 AMM 29-30-05. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. (A)

Part: O-RING — BROKEN (BLEED SYSTEM) · airframe 19,263 hrs · 18,604 cycles

CREW GOT A BLEED 1 LEAK MESSAGE IN FLIGHT WHILE PASSING THROUGH 10,000 FEET. CREW FOLLOWED AOM PROCEDURES AND MESSAGE WENT AWAY. CREW DECIDED TO RETURN TO ORD. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND O-RING IN CARGO AREA, BOTTOM PANEL BY DOOR WAS BROKEN. REMOVED AND REPLACED O-RINGS IAW EMB 145 AMM 36-11-10, OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: SHUTOFF VALVE — FAILED (ZONE 700) · airframe 18,456 hrs · 17,919 cycles

ABORTED TAKEOFF, BRAKE OVERHEAT WARNING MESSAGE. REMOVED AND REPLACED INBOARD BRAKE SHUTOFF VALVE IAW EMB AMM 32-41-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: A/C PACK — ODOR · airframe 18,046 hrs · 17,580 cycles

BURNING SMELL FROM PACKS WITH NO SMOKE. INSPECTED AND FOUND APU INTAKE SCREEN COVERED WITH CICADAS. REMOVED CICADAS. PERFORMED OPERATIONAL CHECK OF PACK SYSTEM WITH NO BURNING SMELL NOTED. RETURNED AIRCRAFT TO SERVICE.

Part: UNKNOWN — UNKNOWN (NLG)

LBB - FLT 3638 - DURING CLIMB, HEARD LOUD AIR NOISE FROM THE NOSE GEAR AREA GOT LOUDER AS THE AIRCRAFT CLIMBED. AIRCRAFT RETURNED TO LBB. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING HMBV INSPECTION, THE FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED AREA BY MAKING A CUT OUT, PREPARED STRAP AND THREE SHIMS OF VARIOUS SIZES. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 33, CHAPTER 53-21-10 FIG 201. RETURNED AIRCRAFT TO SERVICE. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING HMBV INSPECTION, STRINGER 19L WAS FOUND TO BE CHAFED AT THE AFT BELLY PANEL. BLENDED THE DAMAGED AREA AND PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A DOUBLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM145/1142 REV 33, CHAPTERS 53-24-02. RETURNED AIRCRAFT TO SERVICE. (M)

Part: SILL — CORRODED (CARGO DOORWAY)

DURING HMBV INSPECTION, FOUND CARGO DOOR CUTOUT LOWER SILL CORRODED. REMOVED THE CORRODED DOOR SILL AND CLEANED THE AREA. INSTALL NEW DOOR SILL. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 33, 51-20-01, 03, 51-40-04, 06 AND CPM, CMP-145/1132 REV 13 CHAPTER 51-21-04. RETURNED AIRCRAFT TO SERVICE. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 12,044 hrs · 12,275 cycles

DURING AN MBV INSPECTION, A LIGHTNING STRIKE WAS FOUND ON THE LT SIDE OF THE FUSELAGE BETWEEN FRAMES 32 AND 33 AT STRINGER 6L. REMOVED THE DAMAGE BY MAKING A CUT OUT. FABRICATED A FILLER, OUTER DOUBLER AND AN INNER DOUBLER. REPAIR DONE IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 12,044 hrs · 12,275 cycles

THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER, TWO SHIMS AND PLATE. REPAIR DONE IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 12,044 hrs · 12,275 cycles

THE GALLEY CENTER BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORRODED GALLEY CENTER BEAM. INSTALLED NEW BEAM IAW SRM. (K)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 11,781 hrs · 12,000 cycles

LIGHTNING STRIKE DAMAGE FOUND ON SKIN AT FRAME 20 BETWEEN STRINGERS 3L AND 4L. MAINTENANCE COMPLETED A PATCH REPAIR IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501814) (K)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

LIGHTNING STRIKE DAMAGE FOUND ON SKIN AT FRAME 16788.5 STRINGER 6L. MAINTENANCE COMPLETED A PATCH REPAIR IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501815) (K)

Part: SMOKE — DETECTED (CABIN)

DURING DECENT, CREW REPORTED A BURNING ELECTRICAL SMELL IN THE COCKPIT FOR ABOUT 30 SECONDS WITH PAINT SMOKE BEING SEEN FOLLOWED QRH PROCEDURES. THERE WERE NO ALARMS, WARNING MESSAGES OR SMOKE IN CABIN. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS INSPECTED FOR SMOKE IN COCKPIT. NO DEFECTS WERE NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501211)

Part: CONTROL UNIT — INOPERATIVE (SPOILERS)

CREW NOTED AFTER ROTATION SPOILER OPEN INDICATION ACCOMPANIED WITH EICAS MESSAGE SPOILER FAIL AND TAKEOFF CONFIGURATION WARNING. REPLACED SPOILER CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

DISC - FWD OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. RESECURED CONNECTOR. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406984)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

CMH - REARE CABIN EMERGENCY LIGHTS INOPERATIVE. RAI NR 4 EMERGENCY BATTERY, OPS CHECK GOOD. (M)

Part: CONTROLLER — INOPERATIVE (COCKPIT)

PIT - FLT 4345 - CREW REPORTED DURING CLIMB THROUGH 17,000 FT, CABIN ALTITUDE EXCEEDED 14,500 FT, OXYGEN MASK DEPLOYED IN MAIN CABIN. THE FLT CREW PERFORMED EMERGENCY DESCENT OT 10,000 FT REGAINED CONTROL OF CABIN ALTITUDE AND DIFFERENTIAL PRESS. THE FLT CREW THEN CLIMBED BACK TO 15,000, SYSTEM OPERATED MANUALLY ON DESCENT, APPROACH AND LANDING. THE AUTO PRESSURIZATION SYSTEM IS ALREADY ON MEL. MAINTENANCE REMOVED AND REPLACED THE PRESSURE DIGITAL CONTROLLER IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — GOUGED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, A GOUGE WAS FOUND ON REAR FUSELAGE 1 BETWEEN FRAMES 65 AND 66 AND STRINGERS 20L AND 21L. REMOVED DAMAGE BY MAKING A 2.25 INCH BY 3.12 INCH CUTOUT. FABRICATED A REPAIR FILLER. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 20) 53-31-01 PARA 2 FIG 201, AND GST 3655/02. (M)

Part: SILL — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION, RIGHT SILL CORRODED BETWEEN FRAMES 23-27, 32-36, 40, 46-47, 50 AND 53-54. REMOVED RIGHT SILL AND INSTLALED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02, 51-20,03 AND 51-40-06. (M)

Part: BEAM — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION, CENTER BEAM RAMP FOUND CORRODED. REMOVED AND INSTALLED SERVICEABLE RAMP IAW EMB 145 SRM 51-40-02, 51-20-03. (M)

Part: SKIN — CORRODED (WINDSHIELD FRAME)

ABI - DURING AN IMBV INSPECTION, THE THIRD SCREW HOLE ON THE RIGHT WINDSHIELD FRAME WAS FOUND TO BE CORRODED BELOW LIMITS. REAMED FASTENER HOLE OT .313 INCH AND PERFORMED AN NDT INSPECTION WITH NO DEFECTS FOUND. FABRICATED A REPAIR BUSHING. REPAIR DONE IAW EMB REPAIR STATEMENT GAST-3637/02 AND GST-1587/02B. (M)

Part: BEAM — CORRODED (GALLEY)

ABI - DUIRNG AN IMBV INSPECTION, THE GALLEY FLOOR CENTER BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS AT FRAME 23. BLENDED THE CORRODED AREA AND PERFORMED NDT INSPECTION APPLIED ALODINE AND EPOXY PRIMER TO THE BLENDED AREA. FILLED THE BLENDED AREA WITH EPOXY RESIN. FABRICATED A REINFORCEMENT DOUBLEF FOR REPAIR. REPAIR DONE IAW EMB 145 SRM (SRM EMB 145/1142 REV 20) CHAPTER 53-21-10 FIGURE 207. (M)

Part: SILL — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION, LEFT PROFILE AT FRAME 23 CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)

Part: SILL — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION, LEFT FLOOR SILL BETWEEN FRAMES 19 TO 23 CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)

Part: SILL — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTIONS, AFT SERVICE DOOR SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE AFT SILL IAW EMB 145 SRM 51-40-02, 51-20-03. (M)

Part: SILL — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION, SERVICE DOOR FORWARD SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

DFW - FLT 3479 - AFTER TAKEOFF, CREW NOTED E2 OIL IMPENDING BYPASS MESSAGE ON EICAS. AFTER 10 MINUTES NOTED 200 DEGREE ITT INCREASE ACCOMPANIED BY VIBRATION. ENGINE POWER WAS REDUCED TO IDLE AND CREW RETURNED TO FIELD. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - FOUND LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 20. REPAIRED FRAME IAW EMBRAER SRM 145/1142 REV 12 CHAPTER 53-21-10 PAGE 208. (M)

Part: HEATER — FAILED (WINDSHIELD)

ORD - FLT 4114 - IN CRUISE WINDSHIELD 1 HEAT FAILED. RETURN TO ORD FOR MAINTENANCE REPAIR. MAINTENANCE COMPLIED WITH ENGINEERING ORDER EM 3000-018, WINDSHIELD HEATING IMPROVEMENT. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SWITCH — FAILED (PITCH TRIM)

CID - FLT 4236 - CREW REPORTED PITCH TRIM 1 FAIL ON APPROACH. MAINTENANCE REMOVED AND REPLACED CAPTAIN AND FIRST OFFICERS PITCH TRIM YOKE SWITCHES AND THE HSCU. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — FAILED (HORIZONTAL STAB)

CID - FLT 4236 - CREW REPORTED PITCH TRIM 1 FAIL ON APPROACH. MAINTENANCE REMOVED AND REPLACED CAPTAIN AND FIRST OFFICERS PITCH TRIM YOKE SWITCHES AND THE HSCU. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200101804. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ORD - FLT 4401 - EMERGENCY LIGHTS OVER SERVICE DOOR INOPERATIVE. FOUND CANNON PLUG DISCONNECTED. RECONNECTED SAME. OPS CHECK GOOD. (M)

Part: SWITCH — FAILED (RT MLG)

ORD - FLT 4387 - LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED TWO RIGHT MAIN LANDING GEAR PROXIMITY SWITCHES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR 2000ZZZX167. (X)

Part: SWITCH — FAILED (RT MLG)

ORD - FLT 4387 - LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED TWO RIGHT MAIN LANDING GEAR PROXIMITY SWITCHES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA99298-1.