N900AE

Part: O-RING — FAILED (BLEED LINE) · airframe 45,551 hrs · 41,702 cycles

MOMENTARY MUSTY/MOLDY ODOR WHEN SWITCHING FROM ENG BLEED TO APU BLEED WITH PACKS RUNNING. CURRENT CREW DESCRIBED SMELL AS MUSTY/MOLDY. PREV CREW DESCRIBED IT AS A FUEL SMELL. INSPECTED APU BLEED VALVE, FOUND BAD O-RINGS ON BLEED LINE. R & R O-RINGS IAW AMM 36-12-03. RAN PACKS OFF APU BLEED, NO SMELLS NOTED. OK FOR SERVICE.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,346 hrs · 41,464 cycles

F081154 LH OMEGA BEAM CRACKED AT THE FR27 SUPPORT. PERFORMED PERMANENT REPAIR OF CRACKED LH OMEGA BEAM AT THE FRAME 27 SUPPORT IAW PIEDMONT EO1-53-25-0384 AND ETD2025-145-931299.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,346 hrs · 41,464 cycles

LH OMEGA BEAM CRACKED AT THE FR26 SUPPORT. REPAIRED THE LH OMEGA BEAM CRACKED AT THE FR26 SUPPORT IAW EMBRAER ETD2025-145-931300 REV A AND PIEDMONT EO1-53-25-0383.

Part: BULKHEAD — CHAFED (ZONE 200) · airframe 45,346 hrs · 41,464 cycles

F078881 LH COCKPIT AFT BULKHEAD GUIDE PIN HOLE UPPER OTBD IS CHAFED. ACCOMPLISHED REPAIR OF LH COCKPIT AFT BULKHEAD UPPER GUIDE PIN OUTBD PLATE IAW EMB145 SRM 53-21-02 ITEM 4 FIGURE 204 AND EO1-53-25-0405.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,346 hrs · 41,464 cycles

F078880 SHEAR CLIP IS CRACKED AT FR15 BETWEEN STRGS 15R-16R. RAR SHEAR CLIP AT FR15 BETWEEN STRGS 15R-16R IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,346 hrs · 41,646 cycles

LEFT FLOOR SUPPORT NR 2 IS CORRODED. R & R LT FLOOR SUPPORT IAW SRM 51-40-02.

Part: STRINGER — CRACKED (ZONE 200) · airframe 45,346 hrs · 41,464 cycles

STRINGER 3L AT FR20 IS CRACKED. REMOVED AND REPLACED MACHINED STGR 3L BTW FR 19-20 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,346 hrs · 41,464 cycles

FWD GALLEY RT CENTER FLOOR SUPPORT HAS CORROSION AROUND NUTPLATE HOLES. PERFORMED PERMANENT REPAIR ON FWD GALLEY RT CENTER FLOOR SUPPORT IAW EO1-53-25-0387 AND SRM 53-21-02, ITEM 2, FIG 201.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,346 hrs · 41,464 cycles

FRAME 79 SHEAR CLIP INBD OF STR 3L CRACKED. REMOVED AND REPLACED FRAME 79 SHEAR CLIP INBD OF STR 3L IAW EMB145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,346 hrs · 41,464 cycles

F078897 FRAME 80 SHEAR CLIP BETWEEN STR 5R/7R CRACKED. REMOVED AND REPLACED CRACKED FRAME 80 SHEAR CLIP BETWEEN STR 5R-7R IAW EMB 145 SRM 51-40-02 AND EMB 145 SRM 51-40-03.

Part: STRINGER — CRACKED (ZONE 200) · airframe 45,346 hrs · 41,464 cycles

STRINGER 6R IS CRACKED AT FR13. REMOVED AND REPLACED STRINGER 6R BTW FR 12A-14 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,346 hrs · 41,464 cycles

CENTER FUSELAGE III INTERNAL CENTER LT FLOOR GUSSET BETWEEN FR 35 - 39 CORRODED. R & R CENTER FUSELAGE III INTERNAL CENTER LT FLOOR GUSSET BETWEEN FR 35 - 39 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,346 hrs · 41,464 cycles

LEFT OMEGA BEAM GUSSET NR 3 IS CORRODED. R & R LT OMEGA BEAM GUSSET IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,346 hrs · 41,464 cycles

RIGHT FLOOR SUPPORT NR 2 IS CORRODED. REMOVED AND REPLACED THE RT FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,346 hrs · 41,646 cycles

LEFT FLOOR SUPPORT NR 3 IS CORRODED. R & R THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,346 hrs · 41,464 cycles

CENTER FUSELAGE III INTERNAL CENTER RT FLOOR GUSSET BETWEEN FR 38 & 45 CORRODED. R & R CENTER RT FLOOR GUSSET BTW FR38-45 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,346 hrs · 41,464 cycles

CENTER FUSELAGE III INTERNAL CENTER LT FLOOR GUSSET BETWEEN FR 38 - 45 CORRODED. R & R CENTER FUSELAGE III INTERNAL CENTER LT FLOOR GUSSET BETWEEN FR 38 - 45 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,346 hrs · 41,464 cycles

CENTER FUSELAGE III INTERNAL CENTER LT FLOOR GUSSET BETWEEN FR 45 / 53 CORRODED. R & R CENTER FUSELAGE III INTERNAL CENTER LT FLOOR GUSSET BETWEEN FR 45 / 53 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,346 hrs · 41,464 cycles

CENTER OMEGA BEAM GUSSET NR 1 HAS CORROSION. R & R CENTER OMEGA BEAM GUSSET IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,346 hrs · 41,464 cycles

CARGO SHEAR CLIP AT FRAME 73 BETWEEN STGR 8R AND 9R HAS POSSIBLE CRACKS AT HI LOCS. REMOVED AND REPLACED CRACKED SHEAR CLIP IN CARGO AT FRAME 73 BETWEEN STGR 8R AND 9R WITH 3PC SHEAR CLIP IAW EMB145 SRM 53-31-04RE, ITEM 2, FIG 208.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,346 hrs · 41,464 cycles

CARGO AT FRAME 65 THE SHEAR CLIP BETWEEN 1L AND 1R HAS TOOLING DAMAGE FROM BUCKING BAR. FABRICATED AND INSTALLED NEW SHEAR CLIP AT FR 65 BETWEEN STR 1L-1R IAW EMB145 SRM 51-40-02 AND EO1-53-25-0388.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,346 hrs · 41,464 cycles

CABIN LT FLOOR GUSSET BETWEEN FR 52 / 59 CORRODED. R & R CABIN LT FLOOR GUSSET BETWEEN FR 52 / 59 IAW EMB145 SRM 51-40-02, 51-40-08, & 51-40-09.

Part: BEAM — CRACKED (ZONE 800) · airframe 45,346 hrs · 41,464 cycles

F078457 LH ESCAPE HATCH BEAM 3 HAS A POSSIBLE CRACK AT AFT EDGE. REMOVED AND REPLACED LH ESCAPE HATCH BEAM 3 IAW EMB 145 SRM 51-40-02.

Part: SKIN — CRACKED (ZONE 200) · airframe 45,346 hrs · 41,464 cycles

POSSIBLE SKIN CRACK AT RIVET ON LH REAR FUSELAGE 2 AT FR 79, STGR 3L-4L. ACCOMPLISHED SKIN BUSHING REPAIR AT RIVET ON LH REAR FUSELAGE 2 AT FR 79 BETWEEN STGR 3L-4L IAW EMB145 SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-25-0396.

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 45,346 hrs · 41,464 cycles

F077360 VERTICAL STABILIZER LH DRAG ANGLE HAS POSSIBLE CRACK AT FR 76. REMOVED CRACKED VERTICAL STABILIZER LH DRAG ANGLE AT FR 76 IAW EMB145 SRM 51-40-02 AND SRM 51-20-03 AND INSTALLED SERVICEABLE VERTICAL STABILIZER LH DRAG ANGLE AT FR 76. IAW EMB 145 SRM 53-31-01RE. & SRM 51-40-02.

Part: FIRE DETECTOR — FAILED (NR 2 ENGINE) · airframe 43,418 hrs · 39,307 cycles

E2 FIRE DET FAIL ON TAKEOFF. T/S IRW FIM 26-11-00-810-804A TO STEP 8 E2 FIRE LOOP DETERMINED TO BE FAULTY. R & R E2 FIRE DETECTOR IAW AMM 26-11-01. OPS CHK GOOD. A/C OK FOR SERVICE

Part: SOLENOID VALVE — FAILED (MLG)

ON GEAR UP SELECTION INSTANTLY L/G DIS DISPLAYED- GEAR DID NOT RETRACT- FACT 16APR24 15:29 PHL R/R LG SOLENOID VLV IAW AMM 32-33-04. OPS CHECK GOOD LEAK CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: FLAP SYSTEM — BINDING

DURING CLIMB FLAPS WERE SELECTED FROM 9 TO 0 AND WHEN FLAPS INDICATED 0, FLAP FAIL EICAS MESSAGE DISPLAYED WITH CMC OF FLAP JAMBED. INSPECTED FLAPS FOR OBVIOUS DEFECTS NONE FOUND. PERFORMED ZERO RIGGING OF LH &RH FLAPS PER AMM 27-53-04 OPERATED FLAPS FROM 0-45 DEGREES 20 TIMES OPS CHECK GOOD AT THIS TIME.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,158 hrs · 37,864 cycles

DURING CLIMB OUT LOUD AIR RUSHING COMING FROM NOSE GEAR WELL. NO EICAS MSG OR ABNORMAL. FOUND RADOME LATCHES LOOSE AND READJUSTED AND TIGNTENED LATCHES AS REQ,SWING GEARS MULTIPLE TIMES AND FOUND R/H NOSE GEAR DOOR OUT OF ALIGNMENT,READJUSTED R/H NOSE GEAR DOOR ACTUATOR IRW AMM 32-33-03 A/C OKAY FOR SERVICE AT THIS TIME

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,078 hrs · 37,780 cycles

LOUD NOISE AND VIBRATION ON CLIMBOUT FROM NOSE GEAR AREA. FOUND #1 DOOR ACTUATOR ASSY HAS TOO MUCH PLAY WHEN THE DOOR MOVES UP AND DOWN. R/R'D DOOR ACTUATOR IAW AMM 32-33-03. OPS CHECKS GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,420 hrs · 37,037 cycles

AT ALTITUDE LEFT FUEL QUNTY DROPED AT FASTER RATE OF FUEL BURN THEN CACULATED, DIVERTED TO MDT AS PRECAUTION. MEASURE STICKS CONFIRMED LEFT INDICATION FAULTY MEL 23JUL23 12:39 MDT B20412 28-9 WING TANK FUEL QTY INDC EICAS MFE FACT 24JUL23 03:33 PHL R&R FUEL CONDITIONING UNIT IAW AMM 28-41-01. RAN BOTH ENGINES, FUEL QUANTITY GOOD, OK FOR SERVICE. CLEARED MEL 28-9.

Part: UNKNOWN — UNKNOWN (UNKNOWN)

POSSIBLE LIGHTNING STRIKE. SAW FLASH NEAR NOSE, HEARD LOUD BANG. C/W W/C 05-20-00 LIGHT STRIKE INSPECTION (CAT II) SEE HA300'S FOR WORK PERFORMED. RH ELEVATOR TIP FAIRING HAS LIGHNING DAMAGE. R&R'D RH ELEVATOR TIP IN REFERENCE TO AMM SECTION 55-20-01

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

FR 62 CRACKED BEHIND CARGO LH FLOOR SILL #1. REPAIRED IAW EO1-53-23-0063

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

LH CARGO DOOR SILL #1 CORRODED (LEVEL2). REPAIRED IAW SRM 51-20-03, 51-20-03, AND 51-21-06

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

FR 23 HAS ELONGATED RIVET HOLES WHERE LH OUTBOARD #1 FLOOR SILL ATTACHES. REPAIRED IAW SRM 51-40-02 AND 53-00-04

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

SSI 53-20-11 R/H OUTBD SEAT TRACK SUPPORT CORRODED AT RIVET FR-50 MARKED. REPAIRED IAW EO1-53-23-0058.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

CROSSBEAM AT FR 20 IS CORRODED (LEVEL 2). REPAIRED IAW SRM51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

CARGO DOOR EXTERIOR HOUSING IS GOUGED WITH CHUNK OF METAL MISSING AT HOLE FOR HANDLE. REPAIRED IAW EMB145 SRM 51-40-02 WITH REPLACEMENT OF DOOR HANDLE HOUSING

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

RH CARGO FLOOR SILL #4 CORRODED (LEVEL 2). REPAIRED IAW SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,937 hrs · 36,463 cycles

SERVICE DOOR CUTOUT CORRODED (LEVEL 2) AT AFT LOWER DOOR STOP. REPAIRED IAW SRM51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

RH BANANA PANEL BETWEEN LAV/CARGO IS CORRODED (LEVEL 2) AROUND LOWER FASTENER. REPAIRED IAW SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

AREA AROUND LOWER FASTENER ON LH BANANA PANEL BETWEEN LAV/CARGO IS CORRODED (LEVEL 2). REPAIRED IAW SRM51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

PAX DOOR CUTOUT, THE FWD PAX DOOR FLOOR TRIM BRACKET IS CORRODED (LEVEL 2). REPAIRED IAW EMB145 SRM 51-10-03 AND 53-21-02AD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

PAX DOOR CUTOUT, THE AFT PAX DOOR FLOOR TRIM BRACKET IS CORRODED (LEVEL 2). REPAIRED IAW SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

FR 59 STRAP CHAFFED AT STR 8L. REPAIRED IAW SRM51-40-02 AND 51-20-01

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

RH CARGO FLOOR SILL #3 CORRODED (LEVEL 2). REPAIRED IAW SRM51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

LH CARGO FLOOR SILL #2 CORRODED(LEVEL 2). REPAIRED IAW SRM51-20-03 AND 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

CARGO DOOR LOWER SILL CORRODED. REPAIRED IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

RH CARGO FLOOR SILL CORRODED (LEVEL 2). REPAIRED IAW SRM51-20-03 AND 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

FR 65 CORRODED (LEVEL2) AT STR18L. REPAIRED IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

FR 65 SHEAR CLIP IS CORRODED (LEVEL 2). REPAIRED IAW SRM51-10-03, 53-31-04, 51-20-03, AND 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

L/H EXTERNAL FUSELAGE SKIN CRACKED AROUND 1 RIVET FR79 BETWEEN STR5L AND STR6L. REPAIRED IAW EO1-53-23-0060.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

EXTERNAL FUSELAGE SKIN HAS BURN MARK BETWEEN FR 14 AND FR 15 BETWEEN STR3R AND STR4R. REPAIRED IAW EO1-53-23-0069

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,935 hrs · 36,463 cycles

R/H EXTERNAL FUSELAGE SKIN CRACKED AROUND 2 RIVETS AT FR77 BETWEEN STR3R AND STR4R. REPAIED IAW PIEDMONT EO1-53-23-0061.

Part: THERMOSTAT — FAULTED (ANTI-ICE SYSTEM) · airframe 40,881 hrs · 36,405 cycles

BLEED 2 OVERTEMP WARNING ON ICAS DURING CLIMBOUT IN ICING CONDITIONS. R & R FAN AIR CONTROL THERMOSTAT IAW AMM 36-11-06. DURING RAR OF THERMOSTAT, FOUND HOSE LEADING TO THERMOSTAT CRACKED. R & R HOSE IAW AMM 36-11-06. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: TARGET — OUT OF ALIGNMENT (PROXIMITY SENSOR) · airframe 40,781 hrs · 36,298 cycles

LG AIR/GND FAIL MESSAGE AFTER TAKEOFF. GEAR WOULD NOT RETRACT EMERGENCY DECLARED. FOUND NLG AIR/GROUND (WOW) PROX SWITCH TARGET TO BE OUT OF ALIGNMENT. ADJUSTED TARGET IAW EMB 145 AMM 32-63-05. OPC GOOD.

Part: TRANSDUCER — UNSERVICEABLE ([0000] [RH 2]) · airframe 40,606 hrs · 36,074 cycles

BRAKE DEGRADE CAUTION ILLUMINATED ON FINAL DESCENT AT GEAR DROP. RIGHT INBOARD BRAKE APPEARS TO HAVE NOT ENGAGED." DURING TROUBLESHOOTING AND READING NVM, SUSPECT #3 BRAKE PRESSURE TRANDUCER TO BE FAULTY AND CAUSING THE PRESSURE PULSE TEST TO FAIL IN FLIGHT.-C/A-RAR #3 BRAKE PRESSURE TRANSDUCER IAW EMB 145 AMM 32-41-08. OPS CHECK LEAK CHECK GOOD.

Part: LAMP — INOPERATIVE (LH) · airframe 40,503 hrs · 35,971 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. NO FIX. RAR LH OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: NONE — UNSERVICEABLE ([0000] [-] [) · airframe 40,485 hrs · 35,947 cycles

BRAKE DEGRADED EICAS MESSAGE. LITTLE TO NO BRAKING NO RIGHT HAD SIDE #3 BRAKE NO TEMP RISE-C/A-RAR BRAKE CONTROL UNIT IAW AMM 32-41-02 OPC GOOD, BRAKE SYSTEM AND #3 BRAKE TEMP INDICATION TEST GOOD IAW AMM 32-41-00

Part: APU — FUMES (CABIN) · airframe 40,305 hrs · 35,736 cycles

STRONG FUME SMELL ON TAKEOFF. PACKS WERE RUNNING ON APU BLEED UNTIL AFTER T/O CHECK LIST. FUMES SLOWLY SUBSIDED THOUGH OUT FLIGHT. NO SMELL NOTICED ON TAXI OUT WHILE IN SAME PACK/BLEED CONFIGURATION. EMEREGNCY NOT DECLARED "TRANSFERRED TO NRWC 900-ORD-05856"-C/A-PERFORMED ETN-EM-72-034. TRANSFERRED FROM NRWC 900-ORD-05856. REF NRWC#S 900-ORD-05857, 05858, 05859, AND 05860 FOR INSPECTIONS AND FIM TASKS. NO DEFECTS NOTED. NO ODOR, NO SMOKE.

Part: TIRE — DAMAGED (#2 MAIN WHEEL) · airframe 40,245 hrs · 35,664 cycles

ON LANDING NUMBER 2 TIRE TREAD FAILED -C/A-REMOVED AND REPLACED #2 MLG TIRE PER W/C 32-700-11

Part: CABIN PRESSURE — FAILED (COCKPIT) · airframe 40,058 hrs · 35,442 cycles

A/I LCH ACCT AUTO/MAN PRESSURIZATION FAIL. EMERGENCY NOT DECLARED. REF NRWC 900-DFEW-05773 MEL 2122 - AUTH# 06-152DM-C LOG PG 4848122 ITEM AUTO & MANUAL PRESSURAZIATION FAILED IN FLIGHT. CABIN RATE WAS OVER 2000FT /MIN AFTER PACKS AND BLEED WAS RESET ON INITIAL CLIMB-C/A-FOUND PRESSURAZIATION DIGITAL CONTROLLER PUSHBUTTONS STICKY AND RAR DIGITITAL CONTROLLER IAW AMM 31-14-00. REF ITEM 2 THIS NRWC 900-FW-05774 FOR OPERATIONAL CHECK

Part: NONE — DAMAGED (FA) · airframe 39,939 hrs · 35,303 cycles

CREW REPORTS FA EMERGENCY FLASH LIGHT C/B POPPING-C/A-FOUND FWD FA EMERGENCY FLASH LIGHT TO HAVE DAMAGE WIRE RAR FLASH LIGHT ASSY IAW EMB 145 AMM 33-51-01. OPC GOOD NO DEFETS NOTED.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,672 hrs · 35,006 cycles

SERVICE DOOR EMGERGENCY LIGHT INOP. REF AML PAGE 4861345, ITEM #1. MEL 33-22, AUTH #030228D-C.-C/A-RAR EXTERNAL EMERGENCY LIGHT ON SERVICE OOR IAW EMB 145 AMM 33-50-10 AN RAR #2 BATTERY POWER SUPPLY FOR EMERGENCY LIGHTS IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. MEL ITEM RESTORED

Part: NONE — NONE · airframe 39,668 hrs · 35,003 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A- "TRANSFERRED TO AML PAGE 4861345 ITEM 1"

Part: NONE — NONE · airframe 39,560 hrs · 34,884 cycles

DURING PS-2 CHECK FOUND, EMEERGENCY EXIT SIGN LOCATOR AFT GALLEY AND FLOOR PROX LIGHT 3 INOP-C/A-RAR #2 EMERGENCY LIGHT SYS BATT AND POWER CHARGER IAW W/C 33-700-19 AND AFT GALLEY EXIT MARKING SIGN IAW AMM 33-50-14 OPS CHECK

Part: NONE — NONE · airframe 39,508 hrs · 34,822 cycles

AFT CABIN EMERGENCY FLASHLIGHT MISSING ORG LOG PAGE 4799117 ITEM #1 REF MEL 25-32 AUTH # 010400M-C/A-INSTALLEED EMERGENCY FLASHLIGHT IAW AML 33-50-16 OPS CHECK GOOD MEL RESTORED

Part: NONE — NONE · airframe 39,490 hrs · 34,802 cycles

AFT CABIN EMERGENCY FLASHLIGHT MISSING-C/A-FLIGHT CREW PLACARDED MISSINGCABIN EMERGENCY FLASHLIGHT "M PROCEDURES C/W" MEL 2532 AUTH# 010400M MOC 680820

Part: NONE — NONE · airframe 39,325 hrs · 34,606 cycles

GALLEY EMERGENCY LIGHT INOP-C/A-RAR GALLEY EMERGENCY LIGHT IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECK GOOD. NO DEFECTS NOTED. END.

Part: NONE — NONE · airframe 39,325 hrs · 34,606 cycles

EMERGENCY LIGHT OVER 12BC INOP-C/A-RAR EMERGENCY LIGHT OVER 12BC IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPS CHECK GOOD. NO DEFECTS NOTED. END.

Part: NONE — NONE · airframe 39,235 hrs · 34,498 cycles

MAIN DOOR EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EMERGENCY LIGHT IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. NO DEFECTS NOTED. END

Part: NONE — NONE · airframe 39,166 hrs · 34,415 cycles

FWD F/A FLASH LIGHT HOLDER BROKEN-C/A-DEFERRED F/A FLASH LIGHT HOLDER M PROCEDURES C/W

Part: NONE — NONE · airframe 39,142 hrs · 34,385 cycles

DURING PS-1 CHECK FOUND LH OVERWING EMERGENCY LIGHT TO BE INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPS CHECK GOOD.

Part: NONE — NONE · airframe 39,068 hrs · 34,304 cycles

OVERWING EMERGENCY EXIT FORWARD CEILING LIGHT IS INOP.-C/A-TROUBLE SHOT IAW WM 33-50-50 FOUND EMERGENCY LIGHT INVERTER TO BE BAD. RAR EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPC GOOD.

Part: NONE — NONE · airframe 39,012 hrs · 34,243 cycles

ROW 13 TO 18 EMERGENCY LIGHT STRIPS INOP-C/A-RAR #4 BATTERY IAW EMB AMM 33-50-04-000-802-A AND 33-50-04-400-802-A. AND #4 CHARGER IAW EMB AMM 33-50-04-000-801-A AND 33-50-04-400-801-A. NO FIX. FOUND INVERTER TO BE BAD.

Part: CONNECTOR — CORRODED (FLASHLIGHT) · airframe 38,741 hrs · 33,913 cycles

FOUND EMERGENCY FLASHLIGHT C/B (J19) POPPED WHILE SECURING A/C FOR THE NIGHT.-C/A-PERFORMED TROUBLESHOOTING ON EMERGENCYFLASHLIGHT ASSY. FOUND CORROSSION ON PIN CONNECTOR AT AFT CLOSET. CLEANED CORROSION IAW SWPM 20-50-00. REINSTALLED FLASHLIGHT ASSY IAW AMM 33-50-16. FUNCTIONAL CHECK IAW 33-51-01. FUNC CK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,719 hrs · 33,887 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCT LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD. END.

Part: LIGHT — INOPERATIVE (LT WING) · airframe 38,652 hrs · 33,810 cycles

L WING EMERGENCY LIGHT INOP-C/A-R&R L WING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10 OP'S CHECK GOOD NO OTHER DEFECT NOTED AT THIS TIME

Part: CONNECTOR — LOOSE (PROXIMITY SWITCH) · airframe 38,645 hrs · 33,803 cycles

ON ROTATION DURING TAKE OFF LG AIR/GND FAIL ILLUMINATED QRH PROCEDURE COMPLIED WITH - GEAR RETRACTION ISSUE DECLARED EMERGENCY FLT DLYD AM -C/A-DURING INITIAL EVALUATION OF NOSE LANDING GEAR WHEEL WELL, FOUND CANNON PLUG J0775 LOOSE FROM THE UP/LOCK PROXIMITY SWITCH, RESECURED IAW AMM 32-63-05. REQ. GEAR SWING.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 38,581 hrs · 33,742 cycles

FA FLASHLIGHT FOUND NOT CHARGING-C/A-RAR FA FLASHLIGHT IAW EMB AMM 33-50-16-000-801 AND 33-50-16-400-801. OPS CHECK GOOD. NO DEFECTS NOTED. END.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 38,310 hrs · 33,433 cycles

SERVICE DOOR EXTERNAL EMERGENCY LGIHT INOP-C/A-FOUND SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOP. RAR LAMP IN REF WITH EMB 145 AMM 33-50-10. OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 38,276 hrs · 33,404 cycles

FWD AISLE STRIP LIGHTS AND LOWER SERVICED DOOR EMERGENCY LIGHTS INOP-C/A-T/S FWD AISLE STRIP LIGHTS AND LOWER SERVICED DOOR EMERGENCY LIGHTS IAW FIM TASK 33-50-00-810-804-A DISCONNECTED AND CLEANED #2 BATTERY HOLDER CANNON PLUG IN REF WITH EMB AMM 33-50-04-000-801-A AND 33-50-04-400-801-A OPS CHECK GOOD

Part: INVERTER — FAILED (COCKPIT EMER LT) · airframe 38,019 hrs · 33,154 cycles

COCKPIT STEP AND FWD AISLE CEILING PANEL EMERGENCY LIGHTS ARE INOP-C/A-REMOVED AND REPLACED THE INVERTER FOR THE COCKPIT STEP AND FWD AISLE CEILING PANEL LIGHTS IAW EMB 145 AMM 33-50-11. OPC GOOD

Part: LANDING GEAR — MALFUNCTIONED · airframe 37,812 hrs · 32,950 cycles

LANDING GEAR FAIL UNABLE TO RETRACT. EMERGENCY DECLARED-LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF IN QV. AIR/GROUND FAIL EICAS MESSAGE, COMPLIED WITH QRH. DEVERTED TO SGF. LANDED AT 43,500 LBS, SOFT TOUCHDOWN. COMPLIED W/OVERWEIGHT LANDING PROCEDURES.-C/A-UPON INSP FOUND LG AIR/GND - PROX SW FAIL MSG ON CMC. PERFORMED PROXIMITY SWITCH FNC - ALTERNATIVE PROCEDURE WITH BREAK OUT BOX PER AMM 32-63-05-700-802-A. FNC GOOD. PERFORMED MULTIPLE LANDING GEAR EXTENSION AND RETRACTION OPC PER AMM 32-30-00-700-801-A. OPC GOOD. CND FAULT.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 37,566 hrs · 32,694 cycles

DURING REPLACING NR 3 EMERGENCY LIGHTING BATTERY CHARGER, LIGHTS WOULDN'T TURN OFF, REF NRWC 900-ORD-04750. C/A: SUSPECTED BATTERY CHARGER IS BAD STOCK. REMOVED AND REPLACED NR 3 EMERGENCY LIGHTING BATTERY CHARGER, REF EMB 145 AMM 33-50-04. OPERATIONS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 37,024 hrs · 32,114 cycles

ACCESS DOOR OPEN ON DESCENT ON EICAS FWD ELECTRONIC HATCH. PERFORMED OPS CHECK ON FWD ELECTRONIC DOOR IAW AMM 52-71-00. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. MEL ITEM RESTORED. M PROCEDURES REVERSED.

Part: SPAR — CRACKED (LT WING) · airframe 36,956 hrs · 32,067 cycles

LH WING SPAR 1 HAS A RELEVANT CRACK INDICATION AT RIB 9AREA. SETTINGS: FREQ. 400KHZ, ANGLE: 291.1 DEG. H GAIN: 61.3DB. V GAIN 77.6DB. LO PASS FILTER: 500HZ. PERFORMED PERMANENT REPAIR ON LH WING SPAR 1 LOWER FLANGE AND SPAR 1 WEB CRACK INBD OF RIB 9 IAW ERS-EM-57MR-1245. SEE ATTACHED PAGE 2 OF ERS-EM-57MR-1245 FOR PARTS AND MATERIALS LIST

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 36,956 hrs · 32,067 cycles

DURING HMBV INSPECTION, QA FOUND THE RH VERTICAL DRAG ANGLE FWD SECTION CRACKED-C/A-REMOVED AND REPLACED THE RH VERTICAL DRAG ANGLE FWD SECTION IAW EMB 145 SRM 51-40-02

Part: PROFILE — CORRODED (CARGO DOOR) · airframe 36,956 hrs · 32,067 cycles

DURING HMBV INSPECTION, QC FOUND CORROSION ON THE BAGGAGE DOOR LOWER PROFILE-C/A-REMOVED AND REPLACED THE BAGGAGE DOOR LOWER INBD PROFILE IAW EMB 145 SRM 51-40-02

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,956 hrs · 32,067 cycles

DURING HMBV INSPECTION, QC FOUND A CRACK AROUND RIVETS ON RH REAR FUSELAGE I SKIN AT FR 75 BETWEEN STGR 1R AND 3R.-C/A-PERFORMED PERMANENT REPAIR TO CRACK ON RH REAR FUSELAGE I SKIN AT FR 75 BETWEEN STGR 1R AND 3R IAW EMB 145 SRM 53-31-01-RE REPAIR #11. (REPAIR MATERIALS: DOUBLER ALCLAD 2024-T3, 0.080?, FILLER: ALCLAD 2024-T3, 0.063?, ANGLE: ALCLAD 2024-T3, 0.050?, SHIM ALCLAD 2024-T3, 0.032?)

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 36,956 hrs · 32,067 cycles

DURING HMBV INSPECTION, QC FOUND THE BAGGAGE DOOR FWD FRAME CORRODED AROUND NUTPLATE HOLES-C/A-ACCOMPLISHED A PERMANENT REPAIR ON THE BAGGAGE DOOR FWD FRAME IAW ERS-EM-52MR-1076. REPAIR MATERIAL: L SHAPED DOUBLER- AL 2024T3 (0.063) FILLER: AL2024-T3 (0.050) SHIM- AL2024-T3 THICKNESS AS REQUIRED

Part: SKIN — DENTED (FUSELAGE) · airframe 36,956 hrs · 32,067 cycles

AIRCRAFT CAME IN WITH TDMI 900T5355 TO ACCOMPLISH PERMANENT REPAIR OF REAR FUSELAGE I SKIN DENT BETWEEN FR 72-73A AND STRINGER 13R-14R IAW ERS-EM-53DF-3460 PART C-C/A-ACCOMPLISHED PERMANENT REPAIR OF REAR FUSELAGE 1 SKIN DENT BETWEEN FR 72-73A AND STGR 13R-14R IAW ERS-EM-53MR-4110 AND ERS-EM-53DF-3460 PART C

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 36,956 hrs · 32,067 cycles

DURING HMBV INSPECTION, QC FOUND CORROSION ON THE CARGO DOOR FRAME LOWER BEAM (SILL)-C/A-REMOVED AND REPLACED THE CARGO DOOR FRAME LOWER BEAM (SILL) IAW EMB 145 SRM 51-40-02

Part: DOUBLER — CHAFED (CARGO DOOR) · airframe 36,956 hrs · 32,067 cycles

DURING HMBV INSPECTION, QC FOUND THE BAGGAGE DOOR WEBBING CHAFED IN 2 PLACES ON PREVIOUS DOUBLER REPAIR-C/A-REMOVED AND REPLACED THE BAGGAGE DOOR WEBBING PREVIOUS REPAIR DOUBLER IAW EMB 145 SRM 52-30-01 AND ETN-EM-52-043. REPAIR DOUBLER :AL2024-T3 (0.050)

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 36,956 hrs · 32,067 cycles

DURING HMBV INSPECTION, QC FOUND THE BAGGAGE INTERNAL LOWER L-SHAPE ANGLE WHERE SEAL ATTACHES TO IS BENT AND CRACKED-C/A-REMOVED AND REPLACED THE BAGGAGE DOOR FWD CONTINUOUS STOP (LOWER FWD L-ANGLE) IAW EMB 145 SRM 51-40-02

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 36,956 hrs · 32,067 cycles

DURING HMBV INSPECTION, QC FOUND THE SERVICE DOOR CENTER SILL CORRODED AROUND NUTPLATE HOLES-C/A-ACCOMPLISHED PERMANENT REPAIR ON SERVICE DOOR CENTER SILL CORROSION AROUND NUTPLATE HOLES IAW EMB 145 SRM 53-21-02RE REPAIR 2 FIG 201. REPAIR DOUBLER AL CLAD 2024-T3 (0.063)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,956 hrs · 32,067 cycles

LH OMEGA BEAM ISLE FLOOR SUPPORT PITTED AT CROSSBEAM AT FR 38-C/A-ACCOMPLISHED REPAIR ON LH OMEGA BEAM ISLE FLOOR SUPPORT AT CROSSBEAM AT FR 38 IAW EMB 145 SRM 53-00-10 ITEM 3 FIG 202 SHEET 1

Part: RIB — CRACKED (LT WING) · airframe 36,956 hrs · 32,067 cycles

DURING HMBV INSPECTION, QA FOUND THE LH WING RIB 21 CRACKED -C/A-PERFORMED PERMANENT REPAIR ON LH WING RIB 21 IAW EMB 145 SRM 57-20-07 REPAIR 4. MATERIALS; FILLER- AL 2024T3 (0.040) DOUBLER; AL7475 T761 (0.050) SHIM; AL2024T3 (0.032)

Part: FITTING — CRACKED (LT PYLON) · airframe 36,956 hrs · 32,067 cycles

DURING HMBV INSPECTION, QC FOUND LH PYLON FWD LOWER YOKE FITTING CRACKED.-C/A-REMOVED AND REPLACED YOKE FITTING IAW ERS-EM-54MR-698.

Part: FITTING — CRACKED (RT PYLON) · airframe 36,956 hrs · 32,067 cycles

DURING HMBV INSPECTION, QC FOUND RH PYLON FWD LOWER YOKE FITTING CRACKED.-C/A-REMOVED AND REPLACED YOKE FITTING IAW ERS-EM-54MR-698

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 36,956 hrs · 32,067 cycles

TWO PROXIMITY LIGHTS WITHOUT ARROWS AND ONE PROXIMITY LIGHT WITH ARROWS HAS BROKEN WIRES. REMOVED AND REPLACED TWO LIGHTS WITHOUT ARROWS AND ONE LIGHT WITH ARROWS IAW AMM 33-50-12. INSTALLED AND OPS CHECKED.

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 36,956 hrs · 32,067 cycles

AFT CABIN FLASHLIGHT HOLDER BROKEN.-C/A-COMPLETE:REMOVED AND REPLACED AFT CABIN FLASHLIGHT HOLDER IAW EMB 145 AMM 33-51-01.

Part: FRAME — CRACKED (FRM 73) · airframe 36,956 hrs · 32,067 cycles

FRAME 73 CRACKED BETWEEN STRINGERS 15R AND 16R. REMOVED AND REPLACED THE FRAME LOWER SECTION IAW SRM 51-40-02.

Part: HOLDER — BROKEN (EMERGENCY LIGHTS) · airframe 36,956 hrs · 32,067 cycles

FIVE PROXIMITY LIGHT HOLDERS AND FIVE RT SIDEWALLS ARE BROKEN. R & R THE LIGHT HOLDERS AND THE RH SIDEWALLS IAW AMM 33-50-12.

Part: WIRE SPLICE — DAMAGED (EMERGENCY LIGHT) · airframe 36,956 hrs · 32,067 cycles

SERVICE DOOR LOWER LH EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED REMOVABLE SPLICE SP9043 ON SERVICE DOOR LOWER EMERGENCY LIGHT IAW SWPM 20-21-00, WM 33-50-50 AND AMM 33-50-00. OPS CHECK GOOD.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 36,847 hrs · 31,958 cycles

SUPPLEMENTAL PACK #2 HAS A VERY UNUSUAL NOISE AND WAS FILLING THE CABIN WITH A BURNING TYPE ODOR-C/A-VERIFIED NOISE COMING FROM PACK #2 PERFORMED ENGINE RUN WITH CREW INDICATING PACK #1 NO SMELL NOTED. DEFERRED PACK #2 SYSTEM AUTH 030559D-C REF 21-30. COMPLIED WITH EO EM-2100-048. REMOVED AND REPLACED RH ACM AND RH DUAL HEAT EXCHANGER. PERFORMED OPERATIONAL TEST OF COOLING PACK SYSTEM IAW EMB 145 AMM 21-51-00. OPS/LEAK TEST GOOD. NO DEFECTS NOTED. MEL ITEM RESTORED.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 36,846 hrs · 31,956 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 36,612 hrs · 31,728 cycles

AFT CREW FLSHLIGHT INOP-C/A-FLIGHT CREW PLACARDED AFT CREW FLASHLIGHT MEL AUTH# 020105-C REF# 25-53 MOC# 628765. REMOVED AND REPLACED AFT CREW FLASHLIGHT AS REQUIRED. FUNCTION CHECK GOOD. MEL ITEM RESTORED.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 36,304 hrs · 31,532 cycles

RH EXT UPPER (OVER WING) EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED EXT UPPER (OVER WING) EMERGENCY LIGHT ASSY IAW AMM 33-50-07. OPC GOOD.

Part: INVERTER — INOPERATIVE (EXTERIOR LIGHT) · airframe 36,277 hrs · 31,503 cycles

DURING PS-1 CHECK, FOUND RH OVERWING EXTERNAL EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED #6 EMERGENCY LIGHT DC/AC INVERTER IAW AMM 33-50-11. OPC GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,256 hrs · 31,480 cycles

FOUND RH EXTERNAL UPPER WING EMERGENCY LIGHT INOP.-C/A-REMOVED AND REPLACED RH EXTERNAL UPPER WING EMERGENCY LAMP IAW EMB AMM 33-50-10. OPC GOOD.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 36,230 hrs · 31,445 cycles

RH EMERGENGY LIGHT OVER WING INOP DURING PS-1 CHECK-C/A-REMOVED AND REPLACED RH EMERGENCY LIGHT OVER WING IAW AMM 33-50-10 OPS CHECK GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,999 hrs · 31,257 cycles

ROW 17 CEILING EMERGENCY LIGHT INOP-C/A-RAR ROW 17 CEILING EMERGENCY LAMP IAW AMM TASK 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD. END.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,780 hrs · 31,046 cycles

DURING PS-2 CHECK, FOUND RH EXTERIOR EMERGENCY LIGHT ABOVE WING INOP-C/A-REMOVED AND REPLACED RH EXTERIOR ABOVE WING EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. SEE NRWC 900-ORD-04100 FOR CURE CHECK.

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 34,094 hrs · 29,275 cycles

SUPPLEMENTAL ENG A/I FAIL IN FLIGHT (EMERGENCY NOT DECLARED). FLT CONT. C/A-DEFERRED E1 A/I VLV M PROCEDURES C/W REF MEL 30-11AUTH 121065DM-C. REMOVED AND REPLACEDEN E1 ANTI-ICE VALVE IAW AMM 30-21-01 OPS CHECK GOOD MEL RESTORED.

Part: SCREW — MISSING (PAX DOOR) · airframe 33,986 hrs · 29,166 cycles

PASSENGER DOOR HARD TO OPEN AND SCREWS MISSING FROM PANELING.-C/A-REPLACED SCREWS AS REQUIRED AND OPS CHECKED PAX DOOR REF. AMM 52-10-01. OPS CHECK GOOD.

Part: STRUT — DISCHARGED (NLG) · airframe 33,979 hrs · 29,159 cycles

L/G AIR GROUND FAIL EICAS MSG IN FLIGHT-WENT AWAY WHEN GEAR SELECTED DOWN-C/A-FOLLOWING FIM 32-63-00 INTERROGATED CMC NO MSG NOTED AT THIS TIME. PERFORMED NLG SHOCK ABSORBER SERVICING AND CHRGING NO LEAKS NOTED IAW EMB 145 AMM 32-20-01

Part: RESTRICTOR — MISINSTALLED (ANTI ICE SYSTEM) · airframe 33,979 hrs · 29,159 cycles

BLD 2 LOW TEMP W/CLB PWR 88% N2, DURING CHECKLIST WE GOT ICE COND-A/I INOP, WG A/ICE FAIL, STAB A/ICE FAIL "TRANSFERRED TO NRWC 900-DFW-03528"-C/A-FOUND RESTRICTOR TO BE POSITIONED BACKWARDS ON RH BLEED-AIR SERVO LINE AND DRAIN LINE OF FAN-AIR CONTROL THERMOSTAT B-NUT TO BE LOOSE. REPOSITION RESTRICTOR ON RH BLEED-AIR SERVO LINE TO CORRECT DIRECTION AND TIGHTEN DRAIN LINE OF FAN-AIR CONTROL THERMOSTAT B-NUT IAW EMB145 AMM TASK 36-11-11. OPS CHECK GOOD IAW EMB145 AMM TASK 36-00-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,149 hrs · 28,391 cycles

FWD CABIN FLASHLIGHT NOT WORKING. REMOVED & REPLACED FWD CABIN FLASHLIGHT IAW AMM 33-50-16 STEP 3 H (H).

Part: SKIN — DENTED (FRAMES 19-20) · airframe 32,910 hrs · 28,163 cycles

FOUND A LARGE DENT BETWEEN STRINGERS 15L & 16L, FRAMES 19 & 20, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-01. REPAIRED THE SKIN IAW ERS-EM-53MR-3325.

Part: SKIN — CRACKED (FRAME 75) · airframe 32,870 hrs · 28,124 cycles

CRACK APPROXIMATELY 0.25 LONG FOUND IN FUSELAGE SKIN BY HFEC, AT FRAME 75, APPROXIMATELY 1 INCH BELOW STRINGER 2L. CUT OUT THE CRACK IAW SRM 53-31-01, ITEM 11, FIG 219, SHEET 2. PERFORMED HFEC INSPECTION ALONG AREAS OF DAMAGE REMOVAL IAW NDTM 51-00-00-916-801-AOO, NO DEFECTS NOTED. FABRICATED A REPAIR IAW SRM 53-31-01. ALODINED, AND PRIMED THE REPAIR IAW CPM 51-21-04, AND 51-21-05. INSTALLED THE REPAIR IAW SRM 53-31-01.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · corrosion level 2 · airframe 32,870 hrs · 28,124 cycles

CORROSION UNDER GUSSET AT FRAME 20 AND RT OMEGA BEAM. REMOVED CORROSION UNDER THE GUSSET IAW SRM 51-10-03, FOUND TO BE OUT OF LIMITS PER SRM 53-21-10, SI FIG 10, ITEM 15. CUT OUT DAMAGED AREA IAW SRM 53-21-10. PERFORMED HFEC INSP OF CUT OUT IAW NDTM 51-00-00-916-801-A00, NO DEFECTS NOTED. INSTALLED A REPAIRED IAW SRM 53-21-10, ITEM 3, FIG 202, SHEET 2, SRM 51-20-03, CPM 51-21-04, 51-21-05.

Part: DOUBLER — DAMAGED (PYLON) · airframe 32,870 hrs · 28,124 cycles

REPAIR PYLON DOUBLER AT FRAME 73 BETWEEN STRINGERS 8 L AND 9L. REMOVED PYLON DOUBLER AT FRAME 70 TO 74 IAW SRM 51-40-02 FABRICATED DOUBLER FROM 2024 T3 0.063 IAW ENGINEERING DRAWING 145-25898. LOCATED, DRILLED, ALODINED AND PRIMED DOUBLER IAW SRM 51-20-03, 51-40-06, 51-30-01 AND CPM 51-21-04 AND 51-21-05. FABRICATED L ANGLE FOR FRAME 73 FROM 6013 T4 0.050 ETD 2018-145-057749 AND NCR EM-54-130. APPLIED SURFACE PROTECTION TO L ANGLE IAW CPM 51-21-04, 51-21-05 AND ETN EM-51-091 AND INSTALLED IAW ETD 2018-145-057749 AND NCR EM-54-130. INSTALLED DOUBLER IAW SRM 51-40-02 AND NCR EM-54-130. FABRICATED SHEAR CLIP AND REPAIR DOUBLER FOR FRAME 73 FROM 7475 T761 0.050 IAW SRM 53-31-04. ALODINED AND PRIMED SHEAR CLIP AND DOUBLER IAW CPM 51-21-04 AND 51-21-05. INSTALLED SHEAR CLIPS AT FRAMES 71,72,73, DOUBLER AT FRM 73.

Part: RIB — CRACKED (LT WING) · airframe 32,870 hrs · 28,124 cycles

CRACK IN THE LT RIB 5 OTB OF THE MLG. REPAIRED IAW EO EM-57MR-594, REV 1.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 32,870 hrs · 28,124 cycles

PAX DOOR OUTER SKIN LOWER AFT EDGE WAS GOUGED AND CHAFED. REMOVED GOUGE AND CHAFE BY MEANS OF MECHANICAL BLENDING IAW SRM 51-10-03. DAMAGE WAS LESS THAN 4D MIN DISTANCE FROM RIVET LINE . PERFORMED HFEC INSPECTION OF BLENDED AREA IAW NDTM 51-00-00-916-801-A00, NO DEFECTS NOTED. REMOVED DAMAGE BY CUTTING IAW SRM 52-10-01. PERFORMED HFEC INSPECTION ALONG AREA OF DAMAGE REMOVAL IAW NDTM 51-00-00-916-801-A00, NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER AND FILLER. LOCATED, DRILLED AND ALODINED THE REPAIR AND ALODINED DOOR SKIN IAW SRM 52-10-01 AND CPM 51-21-04.APPLIED PRIMER TO REPAIR PIECES AND INSTALLED IAW CPM 51-21-05, AND SRM 52-10-01. APPLIED TOP COAT TO REPAIR AREA IAW CPM 51-10-06 AND ETN GN-51-017.

Part: SKIN — CRACKED (FRAME 79) · airframe 32,870 hrs · 28,124 cycles

FOUR WORKING RIVETS AT FRAME 79 BETWEEN STRINGERS 4R TO 7R. REMOVED PAINT AT 4 EACH WORKING RIVETS IAW SRM 51-10-05. PERFORMED FPI TO AFFECTED FASTENERS IAW NDTM INTRODUCTION SECTION D.FIRST HOLE ABOVE STRINGER 4 FOUND TO BE CRACKED. REMOVED EXISTING RIVET AND ENLARGED HOLE TO .518 INCH IAW SRM 53-32-01. PERFORMED HFEC INSPECTION OF HOLE CUT OUT IAW NDTM 51-00-00-916-801-A00, NO DEFECTS NOTED. FABRICATED FILLER AND DOUBLER IAW SRM 53-32-01 FIG 204, AND FIG 205. LOCATED, DRILLED ALODINE, AND PRIMED THE FILLER AND DOUBLER IAW SRM 53-32-01 AND CPM 52-21-04 AND 51-21-05. INSTALLED THE FILLER AND DOUBLER IAW SRM 53-32-01 AND INSTALLED ALL OTHER WORKING RIVETS IAW SRM 51-40-02. RESTORED SURFACE PROTECTION IAW CPM 51-21-06 AND ETN GN-51-017.

Part: SKIN — CRACKED (FRAME 79) · airframe 32,870 hrs · 28,124 cycles

FOUR WORKING RIVETS AT FRAME 79 BETWEEN STRINGERS 4R TO 7R. REMOVED PAINT AT 4 EACH WORKING RIVETS IAW EMB 145 SRM 51-10-05. PERFORMED FPI TO AFFECTED FASTENERS IAW NDTM INTRODUCTION SECTION D.FIRST HOLE ABOVE STRINGER 6 FOUND TO BE CRACKED. REMOVED EXISTING RIVET AND ENLARGED HOLE TO .656 INCH IAW SRM 53-32-01. PERFORMED HFEC INSPECTION OF HOLE CUT OUT IAW NDTM 51-00-00-916-801-A00, NO DEFECTS NOTED. FABRICATED A FILLER AND DOUBLER IAW SRM 53-32-01 FIG 204, AND FIG 205. LOCATED, DRILLED, ALODINE, AND PRIMED THE FILLER AND DOUBLER IAW SRM 53-32-01, CPM 52-21-04, AND 51-21-05. INSTALLED FILLER AND DOUBLER IAW SRM 53-32-01, AND INSTALLED ALL OTHER WORKING RIVETS IAW SRM 51-40-02.

Part: SKIN — CRACKED (FRAME 78) · airframe 32,870 hrs · 28,124 cycles

FIVE WORKING RIVETS AT FRAME 78 BETWEEN STRINGERS 5R AND 8R. REMOVED PAINT AT FIVE WORKING RIVETS IAW SRM 51-10-05. PERFORMED FPI TO AFFECTED FASTENERS IAW NDTM INTRODUCTION SECTION D.FIRST HOLE BELOW STRINGER 6 FOUND TO BE CRACKED. REMOVED EXISTING RIVET AND ENLARGED HOLE TO .721 INCH IAW SRM 53-32-01. PERFORMED HFEC INSPECTION OF HOLE CUT OUT IAW NDTM 51-00-00-916-801-A00, NO DEFECTS NOTED. FABRICATED FILLER AND DOUBLER IAW SRM 53-32-01, FIG 204, AND FIG 205. LOCATED, DRILLED, ALODINE, AND PRIMED FILLER AND DOUBLER IAW SRM 53-32-01, CPM 52-21-04, AND 51-21-05. INSTALLED FILLER AND DOUBLER IAW SRM 53-32-01, AND INSTALLED ALL OTHER WORKING RIVETS IAW SRM 51-40-02.

Part: SKIN — CRACKED (FRAMES 77-81) · airframe 32,870 hrs · 28,124 cycles

THE AFT UPPER SKIN HAD NUMEROUS CRACKS. REMOVED THE AFT UPPER SKIN IAW SRM 51-40-02. LOCATED, DRILLED, COUNTERSUNK, TRIMMED AND ALODINED THE NEW SKIN IAW SRM 51-20-03, 51-40-06, AND CPM 51-21-04. INSTALLED THE SKIN IAW SRM 51-40-02.

Part: CONNECTOR — MISSING (CABIN) · airframe 32,870 hrs · 28,124 cycles

NUMBER 1 EMERGENCY LIGHT STRIP WIRE MISSING END CONNECTOR. REPLACED MISSING LIGHT STRIP WIRE CONNECTOR IAW SWPM 20-21-00, PERFORMED OPS CHECK IAW AMM 33-50-00, OPS CHECK GOOD. CONNECTOR PIN P/N M39029/31-228.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,870 hrs · 28,124 cycles

CRACK IN SHEAR CLIP FRAME 79 BETWEEN STRINGER 7L AND 8L. REMOVED SHEAR CLIP IAW SRM 51-40-02. LOCATED, DRILLED AND ALODINED FASTENER HOLES IAW SRM 51-20-03,AND CPM 51-21-04.INSTALLED NEW SHEAR CLIP IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,870 hrs · 28,124 cycles

CRACK IN SHEAR CLIP AT FRAME 62 BETWEEN STRINGERS 4 R AND 5 R. INSTALLED EWIS PROTECTION IAW SWPM 21-20-00 REMOVED CARGO DOOR FWD TORSION BAR SUPPORT AND CARGO DOOR LIFTING CABLE TO FOM IAW AMM 52-32-00. REMOVED TORSION BAR SUPPORT FITTING BETWEEN FRAMES 61 AND 62 AND REMOVED L ANGLE SUPPORT BRACKET IAW SRM 51-40-02. REMOVED SHEAR CLIP, LOCATED, DRILLED AND ALODINED FASTENER HOLES IAW SRM 51-40-02, 51-20-03 AND CPM 51-21-04.INSTALLED NEW SHEAR CLIP IAW SRM 51-40-02. REINSTALLED PREVIOUSLY REMOVE L ANGLE AND TORSION BAR SUPPORT FITTING IAW SRM 51-40-02. REINSTALLED CARGO DOOR LIFTING CABLE AND FWD TORSION BAR SUPPORT IAW AMM 52-32-00. REMOVED EWIS PROTECTION IAW SWPM 20-21-00. APPLIED TOP COAT TO EXTERNAL FASTENERS IAW CPM 51-21-06 AND ETN GN-51-017. OPS CHECK OF LIFTING AND LOWERING MECHANISM AND OPS CHECK OF CARGO DOOR GOOD, IAW AMM 52-32-00.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,870 hrs · 28,124 cycles

CRACK IN SHEAR CLIP AT FRAME 71 BETWEEN STRINGERS 16L AND 17L. INSTALLED EWIS PROTECTION IAW SWPM 20-21-00. REMOVED CRACKED SHEAR CLIP IAW SRM 51-40-02. LOCATED, DRILLED ALODINED AND PRIMED FASTENER HOLES IN NEW SHEAR CLIP IAW SRM 51-20-03, AND CPM 51-21-04 AND 51-21-05.INSTALLED NEW SHEAR CLIP IAW SRM 51-40-02. APPLIED CIC IAW CPM 51-61-00. APPLIED TOP COAT TO EXTERNAL RIVETS IAW CPM 51-21-06 AND ETN GN-51-017.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,870 hrs · 28,124 cycles

CORROSION IN SERVICE DOOR THRESHOLD BEAM BETWEEN FRAMES 20 AND 22. INSTALLED EWIS PROTECTION IAW SWPM 20-21-00. REMOVED SERVICE DOOR THRESHOLD TRIM AND DISPLACED DOOR SEAL IAW AMM 20-10-01AND 53-21-11.REMOVED CROSSBEAM, 2EA LOWER ANGLES AND SCUFF PLATE TO FOM IAW SRM 51-40-02.BLENDED CORROSION AND DETERMINED TO BE BEYOND SRM 53-21-02 LIMITS. REMOVED THRESHOLD BEAM IAW SRM 51-40-02. LOCATED , DRILLED AND ALODINE NEW THRESHOLD BEAM IAW SRM 51-20-03 AND CPM 51-21-04.INSTALLED NEW BEAM IAW SRM 51-40-02.REINSTALLED 2EA LOWER ANGLES IAW SRM 51-40-02 AND APPLIED TOP COAT IAW CPM 51-21-05, 51-21-06 AND ETN GN -51-017. REINSTALLED CROSSBEAM AND SCUFF PLATE IAW SRM 51-40-02. REINSTALLED THRESHOLD TRIM IAW AMM 20-10-01 AND SRM 51-20-01. REINSTALLED DOOR FRAME SEAL IAW AMM 53-21-11. REMOVED EWIS PROTECTION IAW SWPM 20-21-00

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,870 hrs · 28,124 cycles

CRACK IN SHEAR CLIP AT FRAME 61 BETWEEN STRINGERS 6L AND 7L. REMOVED SHEAR CLIP AT FRAME 61 IAW SRM 51-40-02. LOCATED, DRILLED AND ALODINED FASTENER HOLES ON NEW SHEAR CLIP IAW SRM 51-20-03 AND CPM 51-21-04. INSTALLED NEW SHEAR CLIP IAW SRM 51-40-02, RESTORED SURFACE PROTECTION IAW CPM 51-21-05, 51-21-06 AND ETN GN-51-017.

Part: FLOOR SUPPORT — CORRODED (FRAMES 52-62) · airframe 32,870 hrs · 28,124 cycles

CORROSION ON THE RT OMEGA BEAM BETWEEN FRAMES 52 AND 62. BLENDED CORROSION IAW SRM 51-10-03, FOUND TO BE CRACKED ON THE INBD SIDE. 0.25 IN LENGTH.DETERMINED TO BE OUT OF LIMITS PER EMB 145 SRM 53-24-10.CUT OUT CRACK IAW EMB 145 SRM 53-24-10, PERFORMED HFEC INSPECTION OF BLENDED AREAS AND AROUND CUT OUT IAW NDTM 51-00-00-916-801-A00, NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER IAW SRM 53-24-10. INSTALLED THE DOUBLER IAW SRM 53-24-10.

Part: FLOOR SUPPORT — CORRODED (FRAME 29) · corrosion level 2 · airframe 32,870 hrs · 28,124 cycles

CORROSION ON THE CENTER OMEGA AT CARBON CROSSMEMBER, FRAME 29. BLENDED THE CORROSION IAW SRM 51-10-03, FOUND TO BE OUT OF LIMITS IAW SRM 53-22-10. CUT OUT THE DAMAGE IAW SRM 53-22-10. PERFORMED HFEC INSPECTION OF CUT OUT AND BLENDED AREAS IAW NDTM 51-00-00-916-801-A00, NO DEFECTS NOTED. FABRICATED A DOUBLER IAW SRM 53-22-10, ITEM 4, FIGURE 203, SHEET 3. PERFORMED FPI OF FABRICATED PARTS IAW NDTM INTRODUCTION SECTION D, NO DEFECTS NOTED. LOCATED, DRILLED, AND COUNTERSUNK THE REPAIR IAW SRM 51-20-00, 51-20-03, AND 51-40-06. INSTALLED IAW SRM 51-40-02, AND 53-22-10 FIG 203 SHEET 3.

Part: BRACKET — CRACKED (FRAME 14) · airframe 32,870 hrs · 28,124 cycles

CRACKED BRACKET AT FRAME 14, STRINGER 2L. REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-04, AND 51-20-01.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · corrosion level 2 · airframe 32,870 hrs · 28,124 cycles

CORROSION ON THE CENTER OMEGA BEAM FROM FRAME 52 TO 62 -C/A-REMOVED CORROSION FROM CENTER OMEGA AT FRAME 59 AND FRAME 60 IAW EMB 145 SRM 51-10-03, DAMAGE AT FRAM E 60 FOUND TO BE OUT OF SRM 53-24-10 LIMITS.CUT OUT CORROSION DAMAGE AT FRAME 60 IAW EMB SRM 53-24-10FABRICATED REPAIR DOUBLER FROM 2024-T3 0.080 IAW EMB 145 SRM 53-24-10. PERFORMED FPI OF FABRICATED REPAIR DOUBLER IAW NDTM INTRODUCTION SECTION D AND ASTM E 1417, NO DEFECTS NOTED . PERFORMED HFEC INSPECTION OF CUT OUT IAW EMB NDTM 51-00-00-916-801-A00 NO DEFECTS NOTED . ALODINED PRIMED DOUBLER IAW EMB CPM 51-21-04 AND 51-21-05. INSTALLED DOUBLER IAW EMB 145 SRM 51-40-02 AND 53-24-10. APPLIED TOP COAT TO REPAIR AREA IAW CPM 51-21-06

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,870 hrs · 28,124 cycles

CRACK IN SHEAR CLIP AT FRAME 62 BETWEEN STRINGERS 6R AND 8R. C/A-INSTALLED EWIS PROTECTION IAW SWPM 20-21-00. REMOVED 4 EACH BONDING TABS ON SHEAR CLIP TO FOM IAW SWPM 20-13-05. REMOVED SHEAR CLIP IAW SRM 51-40-02. LOCATED, DRILLED AND ALODINED NEW SHEAR CLIP IAW SRM 51-20-03, AND CPM 51-21-04. INSTALLED NEW SHEAR CLIP IAW SRM 51-40-02, APPLIED PRIMER AND TOP COAT IAW CPM 51-21-05 AND 51-21-06 AND ETN GN-51-017. INSTALLED 4 EA BONDING TABS TO NEW SHEAR CLIP AND REMOVED EWIS PROTECTION IAW SWPM 20-13-05 AND 20-21-00.

Part: SHEAR TIE — CRACKED (FRAME 62) · airframe 32,870 hrs · 28,124 cycles

SHEAR TIE AT FRAME 62, BETWEEN STRINGERS 6L AND 8L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-04, CPM 51-21-05, 51-21-06, AND ETN GN-51-017.

Part: SHEAR TIE — CRACKED (FRAME 61) · airframe 32,870 hrs · 28,124 cycles

SHEAR TIE AT FRAME 61, BETWEEN STRINGERS 6 R AND 7R WAS CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, AND CPM 51-20-04.

Part: SHEAR TIE — CRACKED (FRAME 72) · airframe 32,870 hrs · 28,124 cycles

SHEAR TIE AT FRAME 72, BETWEEN STRINGERS 17 L AND 18L WAS FOUND CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-04 AND 51-21-05.

Part: SHEAR TIE — CRACKED (FRAME 26) · airframe 32,870 hrs · 28,124 cycles

SHEAR TIE AT FRAME 26, BETWEEN STRINGERS 15R AND 16R WAS FOUND CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-04, AND 51-20-01.

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 32,870 hrs · 28,124 cycles

CRACKED SHEAR TIE AT FRAME 24 BETWEEN STRINGERS 16R AND 17R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-04, AND 51-20-01.

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 32,870 hrs · 28,124 cycles

CRACKD SHEAR TIE AT FRAME 24 BETWEEN STRINGERS 15R AND 16R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02. SRM 51-20-03, CPM 51-21-04, AND 51-20-01

Part: SHEAR TIE — CRACKED (FRAME 25) · airframe 32,870 hrs · 28,124 cycles

SHEAR TIE AT FRAME 25 BETWEEN STRINGER 15R AND 16R WAS FOUND CRACKED. REMOVED THE SHEAR TIE IAW SRM 51-40-02. LOCATED, DRILLED, AND ALODINE A NEW SHEAR TIE IAW SRM 51-20-03, AND CPM 51-21-04. INSTALLED IAW SRM 51-40-02, AND 51-20-01.

Part: SHEAR TIE — CRACKED (FRAME 67) · airframe 32,870 hrs · 28,124 cycles

SHEAR TIE AT FRAME 67, BETWEEN STRINGERS 6L AND 7L WAS CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-40-10, FIG 1, SRM 51-20-03, CPM 51-21-04, 51-21-05. CPM 51-21-06, AND ETN GN-51-017.

Part: RIB — CRACKED (LT WING) · airframe 32,870 hrs · 28,124 cycles

CRACKED, LEFT RIB 5, OTBD OF MLG. REPLACED THE LT WING RIB IAW EO EM-57MR-594.

Part: UNKNOWN — MALFUNCTIONED (TRIM SYSTEM) · airframe 32,267 hrs · 27,573 cycles

ON SHORT FINAL MASTER WARNING ON EICAS PTRIM MAIN INOP AND PTRIM BACKUP INOP. STAYED ON A COUPLE SECONDS THEN WENT AWAY. FOUND MSG CTRL WHEEL TRIM SW FAIL 3 OCCURENCES. PERFORMED A/C RESET AND STAB ELECTRONIC OPS CHECK IAW AMM 27-40-00. OPS CHECK GOOD. FOUND TO BE TRANSITORY

Part: CHARGER — FAILED (CABIN) · airframe 32,233 hrs · 27,541 cycles

LT FWD OVER WING EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 1 EMERGENCY BATTERY AND CHARGER IAW MTX WC 33-700-19. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 108512.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,421 hrs · 26,847 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-50-06-000-801-A, AND 33-50-06-400-801-A. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,368 hrs · 26,791 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 31,212 hrs · 26,641 cycles

EMERGENCY LIGHT STRIPS AT SEATS 7-11 ARE INOPERATIVE. TROUBLESHOT AND FOUND THE P8031/J8031 CONNECTOR LOOSE, RECONNECTED THE CONNECTION IAW SWMP 20-50-00, OPS CHECKED GOOD IAW WC 33-700-17.

Part: CRADLE — CRACKED (FA FLASHLIGHT) · airframe 30,859 hrs · 26,341 cycles

FA FLASHLIGHT CRADLE CRACKED. R & R THE FLASHLIGHT CRADLE IAW AMM 33-50-16-000-801-A, AND 33-50-16-400-801-A. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,622 hrs · 26,106 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,679 hrs · 25,282 cycles

FA FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT IAW 33-50-16. OPS CHECKED GOOD.

Part: DISPLAY — FAILED (COCKPIT) · airframe 28,960 hrs · 24,626 cycles

FO'S MFD WENT DARK ENROUTE AND THEN SMELLED AN ACRID ELECTRICAL ODOR THAT LASTED A FEW MINUTES. AFTER 15 MINS FO'S MFD CAME BACK ON-C/A-REMOVED AND REPLACED FOS MFD OPC GOOD IAW EMB AMM 31-22-01

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,369 hrs · 24,065 cycles

EMERGENCY LIGHT, BETWEEN ROW 8 - 11 INOPERATIVE. R & R TWO FLOOR PROXIMITY LIGHTING STRIPS AT ROWS 8 -11 IAW MM CH 33-50-12. R & R DAMAGED FEMALE CONNECTOR AT ROW 11 IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — FUMES (COCKPIT) · airframe 28,368 hrs · 24,064 cycles

10 - 15 MINS AFTER TAKEOFF ELEC FUMES CAME INTO THE COCKPIT. THE SMELL WOULD COME THEN DISSIPATE DIVERTED, LANDED UNDERWEIGHT CAN STILL SMELL FUMES IN THE COCKPIT. NO SMOKE OBSERVED, NO FUMES WERE SMELLED IN THE CABIN, COCKPIT ONLY. COMPLIED WITH RECIRCULATION FAN OPERATIONS & INSPECTION CHECK FOUND OK IAW AMM 21-24-02. COMPLIED WITH LT & RT AIR COND SYS INSPECTION & OPERATIONS CHECK, FOUND OK IAW AMM 21-51-03. COMPLIED WITH COCKPIT ELEC EQUIP & DISPLAYS VISUAL CHECK, FOUND OK IAW AMM 33-15-00. COMPLIED WITH ETN-EM-72-034-R9, FOUND OK & FOUND FIRST OFFICERS FLOOD RT KNOB & SWITCH LOOSE. REPOSITIONED & ADJUSTED KNOB IAW AMM 33-15-00. OPERATIONS CHECKED GOOD, NO ABNORMALLY OR ODOR NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,316 hrs · 24,022 cycles

MAIN DOOR EXTERNAL EMER LIGHT INOPERATIVE. RELAMPED MAIN DOOR EXTERNAL EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,880 hrs · 23,628 cycles

SHEAR CLIP AT FRAME 65, BETWEEN STRINGER 17L & 18L IS CRACKED. R & R SHEAR CLIP AT FRAME 65 IAW SRM 51-40-02.

Part: FITTING — GOUGED (RT AILERON) · airframe 27,880 hrs · 23,628 cycles

RIGHT AILERON DAMPENER FITTING IS GOUGED. REPLACED IAW EO EM-27MR-112.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,880 hrs · 23,628 cycles

RIGHT OMEGA BEAM ATTACH ANGLE APPEARS CRACKED, BETWEEN FRAMES 47 & 48. R & R RT OMEGA BEAM ATTACH ANGLE IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,880 hrs · 23,628 cycles

SHEAR CLIP AT FRAME 68, BETWEEN STRINGERS 6 & 7L HAS A 1 INCH CRACK. INSTALLED NEW SHEAR CLIP IAW SRM 51-40-02 & ERS-EM-5300-1885.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,880 hrs · 23,628 cycles

SHEAR CLIP AT FRAME 73, BETWEEN STRINGERS 8 & 9L, HAS A 1/4 INCH CRACK. R & R SHEAR CLIP AT FRAME 73, STRINGERS 8L & 9L IAW SRM 53-31-04.

Part: STIFFENER — CRACKED (VERTICAL STAB) · airframe 27,880 hrs · 23,628 cycles

LEFT LOWER VERTICAL STABILIZER TE SKIN STIFFENER ANGLE IS CRACKED. REPAIRED LT LOWER VERTICAL STABILIZER TE SKIN STIFFENER IAW ETN-EM-55-047R1. SEE BOW 209341 FOR PAINT TOUCH UP.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,880 hrs · 23,628 cycles

LEFT WING TO FUSELAGE FAIRING, LOWER ATTACH ANGLE NR 2 IS CRACKED. REPLACED ATTACH ANGLE IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,880 hrs · 23,628 cycles

RIGHT WING TO FUSELAGE FAIRING, LOWER ATTACH ANGLE NR 4 CRACKED AT THE AFT END. INSTALLED NEW SECTION ANGLE IAW ETN-EM-53-142 & SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,880 hrs · 23,628 cycles

LEFT WING TO FUSELAGE UPPER ATTACH ANGLE CRACKED, BETWEEN FRAMES 48 & 49. REPAIRED IAW SRM 53-23-12.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 27,880 hrs · 23,628 cycles

RIGHT WING TO FUSELAGE FAIRING, UPPER SUPPORT CRACKED. REPAIRED IAW SRM 53-23-12.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 27,880 hrs · 23,628 cycles

RIGHT WING TO FUSELAGE PANEL, LOWER FWD SUPPORT CRACKED. COMPLETED REPAIR IAW ETN-EM-53-142 R2. SEE NRTC E488775 FOR LEAK CHECK.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,880 hrs · 23,628 cycles

RIGHT WING TO FUSELAGE FAIRING, LOWER ATTACH ANGLE NR 2 CRACKED AT AFT END. REPLACED ATTACH ANGLE IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 27,880 hrs · 23,628 cycles

CARGO DOOR SILL IS CORRODED. REPLACED CARGO DOOR SILL IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 27,880 hrs · 23,628 cycles

LEFT WING TO FUSELAGE PANEL LOWER FWD SUPPORT CRACKED. REPAIRED IAW ETN-EM-53-142 R2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,402 hrs · 23,159 cycles

MAIN DOOR EMER LIGHT INOPERATIVE. R & R LAMP IN MAIN DOOR EMER LIGHT ASSEMBLY IAW AMM 33-50-06-000-801 & 33-50-06-400-801. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 27,383 hrs · 23,137 cycles

AT 360 CABIN PRESS BEGAN TO RISE, SLOW BUT STEADY, TO EXTENDED LIMITS. HAD TO DESCEND TO 10000 FT. DEFERRED PRESSURIZATION CONTROL SYS M PROCEDURES COMPLIED WITH REF 21-18. PERFORMED OPERATIONS CHECK OF MANUAL PRESSURIZATION IAW AMMM 21-31-00. OPERATIONS CHECKED GOOD IAW ITEM 3 FOR AUTO MODE. MEL REMAINS OPEN. R & R ELECTRO PNEUMATIC OUTFLOW VLV IAW AMM 21-31-03. OPERATIONS CHECKED GOOD, MEL RESTORED IAW NRWC 900-DFW-02107.

Part: SKIN — CRACKED (RUDDER) · airframe 26,840 hrs · 22,593 cycles

RUDDER II SKIN CRACKED. REPAIRED IAW ERS-EM-55MR-325.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 26,012 hrs · 21,904 cycles

FLIGHT ATTENDANT`S EMER FLASHLIGHT CRADLE BROKEN. NO PARTS AT CMI, TRANSFERRED TO AML PAGE 3713135 ITEM 4. R & R FWD FLIGHT ATTENDANT`S FLASHLIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-50-16. MEL ITEM RESTORED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,850 hrs · 21,756 cycles

ABOVE RT WING EMER LIGHT INOPERATIVE. R & R, OPERATIONS CHECKED GOOD ABOVE RT WING EMER LIGHT BULB IAW AMM 33-50-10.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 25,722 hrs · 21,625 cycles

WHILE PERFORMING PS 1 INSPECTION FOUND RT FWD EXTERNAL EMER LIGHT INOPERATIVE & NR 2 AISLE EMER LIGHT INOPERATIVE. R & R THE NR 2 BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. CHARGER ASSEMBLY BATTERY PN BA5-0933-901 SN C02279.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,417 hrs · 21,370 cycles

RIGHT EXTERIOR FWD FUSELAGE EMER LIGHT & OVERHEAD AISLE LIGHTS INOPERATIVE. R & R N 2 EPSU BATTERY & CHARGER. OPERATIONS CHECKED GOOD IAW WC 33-700-19.

Part: SMOKE DETECTOR — FAILED (AFT) · airframe 25,313 hrs · 21,278 cycles

AFT SMOKE DETECTOR FAILED TEST IAW WC-26-200-06. R & R AFT SMOKE DETECTOR IAW AMM-26-15-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SWITCH — UNSECURE (COCKPIT) · airframe 25,146 hrs · 21,146 cycles

ON CLIMB OUT NR 1 BLEED VLV SWITCH FELL OUT OF OVERHEAD PANEL, NR 1 BLEED VLV CLOSE, UNABLE TO OPEN. SECURED PUSH BUTTON AS REQUIRED IAW SP 23-1304. OPERATIONS CHECKED NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT REPLACE CTR FUSELAGE 1 RT SKIN. R & R IAW SRM 51-40-02, ETN EM-53-262 R1, ETN-EM-51-118 & ERS-EM-5300-759.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT REPLACE LT CTR FUSELAGE SKIN. R & R IAW SRM 51-40-02, ETN-EM-53-262 & ETN-EM-51-118.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT REPLACE FWD FUSELAGE 1 RT SKIN PANEL. R & R IAW SRM 51-40-02, ETN-EM-53-206 & ETN-EM-53-262.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 25,141 hrs · 21,142 cycles

RIGHT LOWER OTBD ELEVATOR WING TIP SKIN HAS ELONGATED HOLES. PERFORMED REPAIR ON RT ELEVATOR LOWER OTBD WING TIP SKIN IAW ERS-EM-55MR-161.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT REPLACE CTR FUSELAGE IV TOP SKIN. R & R CTR FUSELAGE IV TOP SKIN IAW SRM 51-40-02, 51-20-01, ETN EM-53-265 & ETN-EM-51-118.

Part: CONNECTOR — BROKEN (CABIN) · airframe 25,141 hrs · 21,142 cycles

EMERGENCY LIGHT STRIP CONNECTOR BROKEN AT SEAT 9A. REPAIRED EMER LIGHT STRIP CONNECTOR AT SEAT 9A IAW SWPM 20-21-00 STEP 5.

Part: SKIN — DENTED (RT HORIZ STAB) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT REPLACE RT STAB SKIN. R & R RT STAB TOP SKIN IAW SRM 51-40-02 & ETN EM-55-073.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT REPLACE LT ELEVATOR OTBD UPPER SKIN TIP. R & R LT ELEVATOR OTBD UPPER SKIN TIP IAW SRM 51-40-02 & ETN EM-55-073.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT-REPLACE RT ELEVATOR OTBD UPPER SKIN TIP. R & R RT ELEVATOR OTBD UPPER SKIN TIP IAW SRM 51-40-02, ETN EM-55-073.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT REPLACE LT ELEVATOR UPPER CTR SKIN. R & R LT ELEVATOR UPPER CTR SKIN IAW SRM 51-40-02 & ETN EM-55-073.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT REPLACE LT ELEVATOR MID SKIN TIP. R & R LT ELEVATOR MID SKIN TIP IAW SRM 51-40-02, ETN EM-55-073 & ERS-EM-55-073.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT REPLACE CTR FUSELAGE II SKIN PANEL. R & R CTR FUSELAGE II SKIN IAW SRM 51-40-02, ETN-EM-53-263 & ETN-EM-51-118.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT REPLACE RT ELEVATOR MID SKIN TIP. R & R RT ELEVATOR MID SKIN TIP IAW SRM 51-40-02 & ETN EM-55-073.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT REPLACE RT ELEVATOR INBD LE. R & R RT ELEVATOR INBD LE SRM 51-40-02 & ETN EM-55-073.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT REPLACE RT ELEVATOR UPPER CTR SKIN. R & R RT ELEVATOR UPPER CTR SKIN IAW SRM 51-40-02 & ETN EM-55-073.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT REPLACE REAR FUSELAGE I SKIN. R & R REAR FUSELAGE I SKIN IAW SRM 51-40-02 & ERS-EM-5300-615, ETN-EM-53-266R3 & ETN-EM-51-118.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT REPLACE LT STAB SKIN. R & R LT STAB TOP SKIN IAW SRM 51-40-02, 51-40-06 & ETN EM-55-073.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT REPLACE FWD FUSELAGE II SKIN PANEL, CROWN. R & R FWD FUSELAGE II SKIN IAW SRM 51-40-02, ETN-EM-53-206, ETN-EM-51-118 & ERS-EM-5300-707.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,141 hrs · 21,142 cycles

HAIL DAMAGE EVENT REPLACE FWD FUSELAGE II SKIN WIPER PANEL. R & R FWD FUSELAGE II SKIN IAW SRM 51-40-02, ETN EM-53-206 & ETN-EM-51-118.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,068 hrs · 21,068 cycles

MAIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN DOOR EMER LIGHT LAMP IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: HOLDER — DAMAGED (FLASHLIGHT) · airframe 24,626 hrs · 20,728 cycles

FLIGHT ATTENDANT`S FLASHLIGHT HOLDER DAMAGED. R & R FLASHLIGHT BASE IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,712 hrs · 20,022 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOPERATIVE. R & R AFT CABIN EMERGENCY FLASHLIGHT IAW AMM 33-50-16-000-801-A & 33-50-16-0400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SILL — CORRODED (FUSELAGE) · airframe 23,675 hrs · 19,993 cycles

DURING MBV INSPECTION FOUND CARGO DOOR SILL CORRODED. R & R CARGO DOOR SILL IAW SRM 51-40-02.

Part: LIGHT — BROKEN (CABIN) · airframe 23,675 hrs · 19,993 cycles

NUMBER 1 EMERGENCY LIGHT STRIP RT REQUIRES REPLACEMENT. ACQUIRED THE NR 1 EMERGENCY LIGHT STRIP FROM CPH, REMOVED BROKEN STRIP & ATTACHED THE NEW LIGHT STRIP TO THE NR 1 PROFILE.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 23,675 hrs · 19,993 cycles

RIGHT OTBD OMEGA BEAM INBD SUPPORT ANGLE IS CRACKED BETWEEN FRAMES 47 - 48. R & R RT OTBD OMEGA BEAM INBD SUPPORT ANGLE IAW SRM 53-23-02 & SRM 51-40-02.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 23,675 hrs · 19,993 cycles

FLASHLIGHT ON FWD SIDE OF CAPTAIN'S BULKHEAD WILL NOT LIGHT. R & R FLASHLIGHT ON FWD SIDE OF CAPTAIN'S BULKHEAD AS REQUIRED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,614 hrs · 19,945 cycles

MAIN DOOR EMERGENCY LAMP INOPERATIVE. R & R THE MAIN CABIN DOOR EXTERNAL EMERGENCY LAMP IAW AMM TASKS 33-50-10-000-801-A 33-50-10-400-801-A, OPERATIONS CHECKED CHECK GOOD.

Part: LENS — CRACKED (FLASHLIGHT) · airframe 23,465 hrs · 19,823 cycles

CAPTAIN'S FLASHLIGHT LENS COVER CRACKED. REPLACED CAPTAIN`S FLASHLIGHT IAW AMM 25-60-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,293 hrs · 19,688 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R MAIN DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,189 hrs · 19,598 cycles

RIGHT FWD FAIRING EMERGENCY LIGHT INOPERATIVE. C/A R & R NR 2 EMERGENCY LIGHT BATTERY & CHARGER ASSEMBLY IAW EMB WC 33-700-19, OPERATIONS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 23,180 hrs · 19,591 cycles

AFT CABIN FLASHLIGHT CRADLE IS BROKEN. REPLACE AFT CABIN FLASHLIGHT CRADLE IAW MM 33-50-16.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,734 hrs · 19,215 cycles

MAIN DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R MAIN DOOR OVERHEAD EMERGENCY LIGHT LAMP IAW AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,407 hrs · 18,164 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP AT SERVICE DOOR CEILING EMERGENCY LIGHT IAW EMB AMM TASK 33-50-09-000-801-A AND 33-50-09-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,407 hrs · 18,164 cycles

DURING B INSPECTION FOUND THE CABIN CENTER AISLE CEILING EMERGENCY LIGHT 2ND FROM FRONT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN CENTER AISLE CEILING EMERGENCY LIGHT LAMP 2ND FROM FRONT IAW EMB AMM TASK 33-50-08-000-801-A AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DAMAGED (CABIN) · airframe 21,373 hrs · 18,140 cycles

DURING B INSPECTION FOUND THE FORWARD FLIGHT ATTENDANT FLASHLIGHT SWITCH BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 20,619 hrs · 17,560 cycles

ON FLIGHT 4359 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN PASSENGER DOOR IAW EMB-145 M/M 52-18-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,586 hrs · 17,535 cycles

DURING B INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. DID NOT FIX. FOUND GROUNDING PROBLEM WITH LAMP ASSEMBLY. RE-SECURED GROUND TO LAMP ASSEMBLY IAW EMB 145 AMM 20-13-21. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,402 hrs · 17,381 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,336 hrs · 17,335 cycles

DURING B INSPECTION FOUND THE EMERGENCY EXIT LIGHT ON THE MAIN DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP AT MAIN DOOR EMERGENCY LIGHT PER EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — LOOSE (COCKPIT) · airframe 20,103 hrs · 17,169 cycles

ON FLIGHT 3570 THE CREW REPORTED THE FIRST OFFICER’S SIDE WINDOW HAD A LOUD AIR LEAK AND LOOSE WINDOW SEAL. THE CREW DECLARED AN EMERGENCY AND RETURNED TO MIA UNDER MAX LANDING WEIGHT. TOUCHDOWN LESS THAN 300 MIN. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT WINDOW SEAL IAW AMM 56-11-02. THE LEAK CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 19,939 hrs · 17,040 cycles

DURING B INSPECTION FOUND THE NR 1 EMERGENCY POWER SUPPLY UNIT BATTERY INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY POWER SUPPLY UNIT BATTERY IAW W/C: 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,939 hrs · 17,040 cycles

DURING B INSPECTION FOUND THE LEFT LOWER EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EMERGENCY LIGHT BULB 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 — BROKEN (CABIN) · airframe 19,815 hrs · 16,936 cycles

DURING B INSPECTION FOUND THE AFT CABIN FLASHLIGHT RECEPTACLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,313 hrs · 16,555 cycles

DURING HMBV INSPECTION FOUND CARGO DOOR SILL CORRODED AROUND FASTENER HOLES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CARGO DOOR SILL IAW STRUCTUAL REPAIR MANUAL 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 19,313 hrs · 16,555 cycles

DURING HEAVY MAINTENANCE INSPECTION FOUND THE CENTER OMEGA BEAM GUSSET CORRODED BETWEEN FRAMES 59 AND 61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED GUSSET IAW EMBRAER SRM 51-40-02. THE AIRCRAFT RETURN TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 19,313 hrs · 16,555 cycles

DURING HEAVY MAINTENANCE INSPECTION FOUND RIGHT OMEGA BEAM GUSSET CORRODED BETWEEN FRAMES 59 AND 61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED GUSSET IAW EMBRAER SRM 51-40-02. THE AIRCRAFT RETURN TO SERVICE.

Part: ANGLE — CRACKED (RT WING) · airframe 19,313 hrs · 16,555 cycles

DURING HEAVY MAINTENANCE INSPECTION FOUND THE RIGHT OVERWING TO FUSELAGE ATTACH ANGLE CRACKED ON THE AFT END OF NR 1 SECTION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED RIGHT OVERWING ANGLE IAW ETN-EM-53-142. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,313 hrs · 16,555 cycles

DURING HEAVY MAINTENANCE INSPECTION FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 59. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT HAND OEMGA BEAM IAW EO EM-53MR-1518. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 19,313 hrs · 16,555 cycles

DURING HEAVY MAINTENANCE INSPECTION FOUND THE SHEAR CLIP IS CRACKED AT FRAME 73 BETWEEN STRINGERS 8L AND 9L. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SHEAR CLIP IAW EMB STRUCTUAL REPAIR MANUAL 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 9,808 hrs · 16,631 cycles

DURING MAINTENANCE INSPECTION, FOUND A WIRE FOR THE EMERGENCY LIGHT AT FRAME 49 TO HAVE A BROKEN END. AIRCRAFT REMOVED FROM SERVICE. REPAIRED EMERGENCY LIGHT CONNECTOR 49 IAW SWPM 20-21-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN DOOR) · airframe 18,893 hrs · 16,170 cycles

DURING B-INSPECTION FOUND THE EMERGENCY LIGHT ON MAIN CABIN ENTRY DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RELAMPED EMERGENCY LIGHT ON MAIN CABIN DOOR IAW EMB 145 AMM 33-50-06. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — TORN (MAIN DOOR) · airframe 18,720 hrs · 16,021 cycles

ON FLIGHT 3394 THE CREW REPORTED THE MAIN DOOR HAS A 2 INCH TEAR IN SEAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED MAIN DOOR SEAL IAW AMM CH 52-00-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ADC — MALFUNCTIONED (COCKPIT) · airframe 15,701 hrs · 13,768 cycles

ON FLIGHT 2771 DURING CRUISE THE CREW REPORTED THE COCKPIT HAD A BURNING ODOR IN ICING CONDITIONS AND WINDSHIELDS WERE ICED OVER. THE CAPTAIN DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AIR DATA COMPUTER IAW AMM 34-15-01. THE OPERATIONAL TEST AND THE LEAK CHECK WAS GOOD IAW 34-13-00. ALSO REMOVED AND REPLACED THE CAPTAINS WINDSHIELD HEAT TEMPERATURE CONTROLLER IAW AMM CH. 30-42-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LANDING GEAR — MALFUNCTIONED (RIGHT) · airframe 11,180 hrs · 10,090 cycles

CREW REPORTED AFTER GEAR EXTENSION RT MLG IN-TRANSIENT LIGHT WITH ASSOCIATED LANDING GEAR DISAGREE MESSAGE. CREW DECLARED EMERGENCY AND PERFORMED GO AROUND. CREW CYCLED GEAR IAW AOM AND ALL INDICATIONS WERE NORMAL. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE.

Part: ACTUATOR — FAILED (RT MLG) · airframe 11,180 hrs · 10,090 cycles

CREW REPORTED AFTER GEAR EXTENSION RT MLG IN-TRANSIENT LIGHT WITH ASSOCIATED LANDING GEAR DISAGREE MESSAGE. CREW DECLARED EMERGENCY AND PERFORMED GO AROUND. CREW CYCLED GEAR IAW AOM AND ALL INDICATIONS WERE NORMAL. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATOR IAW EMB 145 AMM 32-33-08. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR UNLOCKING ACTUATOR IAW EMB 145 AMM 32-33-09. OPERATION AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 8,514 hrs · 7,563 cycles

ON FLIGHT 4401, CREW REPORTED OVER HEAD EMERGENCY LIGHT INOPERATIVE IN CABIN AIRCRAFT FROM SERVICE. FOUND COCKPIT FLOODLIGHT AND LT FORWARD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT POWER SUPPLY AND BATTERY. FOUND WIRING SPLICE SP9003 BROKEN. REPAIRED SPLICE AND FOUND NR 1 EMERGENCY LIGHT POWER SUPPLY INOPERATIVE AGAIN DUE TO NO FAULT PROTECTION ON THIS CIRCUIT. REMOVED AND REPLACED NR 1 EMERGENCY POWER SUPPLY. OPERATIONAL CHECK GOOD. ALL LIGHTS WORKING NORMALLY. AIRCRAFT RETURNED TO SERVICE.

Part: BUTTON — FAILED (BLEED SYS) · airframe 7,607 hrs · 6,667 cycles

EMERGENCY DECLARED, RIGHT AFTER TAKEOFF AT ABOUT 2000 FEET WING AND STAB FAIL CAUTION CAME ON FOLLOWED BY ICE CONDITION A/I INOP WARNING ON EICAS. RETURNED FOR LANDING AT ORD. VISUALLY INSPECTED PRESSURE SWITCH MANIFOLD, WING ANTI ICE VALVES, AND SENSE LINES AT WING TO FUSE FAIRING FOR SECURITY AND ABNORMALITIES. NO DEFECTS NOTED. REMOVED AND REPLACED BOTH ENGINE BLEED PUSHBUTTONS IAW EMB 145 20-13-04. OPS CHECK NUMEROUS TIMES IAW EMB 145 30-00-00. OPS CHECK GOOD, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: ANTI-ICE SYSTEM — FAILED (WING)

WING ANTI ICE SYSTEM FAILED ON CLIMB-OUT. CREW CALLED MOC AND ELECTED TO RETURN BACK TO ORD DUE TO WEATHER.

Part: FITTING — UNKNOWN (CABIN PRESSURE) · airframe 5,889 hrs · 5,174 cycles

AIRCRAFT WOULD NOT PRESSURIZE IN BOTH AUTO OR MANUAL. REMOVED OUTFLOW VALVES HOLD OPEN CLIPS AND PERFORMED OPERATIONAL TEST OF PRESSURIZATION CONTROL SYSTEM IN BOTH MODES WITH NO DEFECTS.

Part: LIGHT — BURNED (COCKPIT) · airframe 5,035 hrs · 4,447 cycles

VISIBLE SMOKE AND BURNING SMELL FROM FIRST OFFICERS CHART HOLDER LIGHT. REMOVED AND REPLACED CHART HOLDER DUE TO CHAFED WIRE IAW EMB AMM 25-12-11. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DUCT — CRACKED (BLEED AIR SYS)

ORD - FLT 4402 - LAVATORY SMOKE WARNING CAME ON DURING TAXI AND WENT OUT. INSPECTED CUSTOMER SERVICE MANIFOLD ON LEFT ENGINE AND FOUND HIGH STAGE BLEED TUBE CRACKED. REPLACED BLEED TUBE. PERFORMED FUNCTIONAL TEST FLIGHT AND PASSED. OPERATIONAL TEST OF SMOKE DETECTOR GOOD. AIRCRAFT RETURNED TO SERVICE. (M)