N922AE

Part: CLAMP — LOOSE (BLEED AIR SYS)

BLEED 1 LEAK DISPLAYED DURING TAKE OFF. (FERRY PERMIT ISSUED WITH BLEED 1 VALVE SECURED CLOSED). FACT 19DEC25 22:10 RIC RE-SEATED AND TIGHTENED Y-DUCT CLAMPS AND ENGINE BLEED VALVE CLAMPS ON #100 SIDE. R&R CROSSBLEED COUPLING BOOT THAT WAS DAMAGED IN REFERENCE TO AMM 36-11-05-400-801-A AND AMM 36-11-09-000/400-802-A. OPS CHECK GOOD. LEAK CHECK GOOD. OK FOR SERVICE

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,914 hrs · 41,736 cycles

53-2069 LH OMEGA BEAM #1 IB FLANGE CRACKED AT FR21, FR22, FR23. REPAIRED OMEGA BEAM IAW ETD2025-145-928523 AND EO1-53-25-0336

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,914 hrs · 41,736 cycles

SHEAR CLIP CRACKED AT FR80 BTW STR5-7L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 45,914 hrs · 41,736 cycles

CARGO DOOR ENTRANCE AT FR67 POST CRACKED. RAR POST IAW SRM 51-40-02

Part: BEAM — CORRODED (ZONE 100) · airframe 45,914 hrs · 41,736 cycles

53-2127 RF1 CARGO DOOR ENTRANCE AT FR66 POST CRACKED. RAR POST IAW SRM 51-40-02

Part: ANGLE — CRACKED (ZONE 100) · airframe 45,914 hrs · 41,736 cycles

CARGO DOOR ENTRANCE AT FR67 ANGLE ON TOP OF LWR BEAM CRACKED. RAR ANGLE IOAW SRM 51-40-02

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,914 hrs · 41,736 cycles

RIGHT GUSSET AT BTW FR 59-61 IS CORRODED. R & R GUSSET IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,914 hrs · 41,736 cycles

53-2141 SHEAR CLIP CRACKED AT FR62 BTW STR6-8L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: BEAM — CORRODED (ZONE 100) · airframe 45,914 hrs · 41,736 cycles

53-2130 RF1 CARGO DOOR ENTRANCE AT FR66 ANGLE ON TOP OF LWR BEAM CRACKED. RAR ANGLE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,914 hrs · 41,736 cycles

SHEAR CLIP CRACKED AT FR 71 BTW STR 6-10R. R & R SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,914 hrs · 41,736 cycles

LEFT SHEAR CLIP CRACKED AT FR66 BTW STR6-7L. R & R SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,914 hrs · 41,736 cycles

53-2172 LH SHEAR CLIP CRACKED AT FR61 BTW STR18-19L. REPAIRED IAW ETD 2025-145-929206

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,914 hrs · 41,736 cycles

53-2157 CF4 BTW FR59-61, LH GUSSET CORRODED

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,914 hrs · 41,736 cycles

SHEAR CLIP CRACKED AT FR62 BTW STR6-8R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: ANGLE — CRACKED (WINDOW FRAME) · airframe 45,914 hrs · 41,736 cycles

LEFT ANGLE CRACKED AT FR10 BELOW COCKPIT SIDE WINDOW. R & R ANGLE IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,914 hrs · 41,736 cycles

SHEAR TIE CRACKED AT FR40 BTW STR 9-10R. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IAW ETD2025-145-929204, EO1-53-25-0355, AND SRM 51-40-02.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,914 hrs · 41,736 cycles

53-2123 RF1 CARGO DOOR ENTRANCE LWR BEAM CORRODED. RAR BEAM IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,914 hrs · 41,736 cycles

53-2099 RH OMEGA BEAMIB STUB ANGLE IS CRACKED. RAR STUB ANGLE IAW SRM 51-40-02

Part: ANGLE — CRACKED (ZONE 100) · airframe 45,914 hrs · 41,736 cycles

LEFT OMEGA BEAM STUB ANGLE OB IS CRACKED. RAR ANGLE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,914 hrs · 41,736 cycles

SHEAR CLIP CRACKED AT FR15 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,914 hrs · 41,736 cycles

LEFT GUSSET NR 3 CORRODED. R & R GUSSET IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,914 hrs · 41,736 cycles

LEFT OMEGA BEAM IB VERT FLANGE CRACKED AT FR28. REPAIRED IAW ETD2025-145-928525 AND EO1-53-25-0337

Part: CHANNEL — CORRODED (ZONE 800) · corrosion level 2 · airframe 45,914 hrs · 41,736 cycles

CF1 SERVICE DOOR CHANNEL CORRODED. R & R CHANNEL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,914 hrs · 41,736 cycles

53-2087 CTR OMEGA BEAM #3 CRACKED AT FR31 IB VERT FLANGE. REPAIRED IAW ETD2025-145-928527 AND EO1-53-25-0238

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,914 hrs · 41,736 cycles

53-2087 CTR OMEGA BEAM #3 CRACKED AT FR31 IB VERT FLANGE. REPAIRED IAW ETD2025-145-928527 AND EO1-53-25-0238

Part: CUP — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,914 hrs · 41,736 cycles

53-2049 TIOLET WASTE CUP CORRODED ON EXTRNAL SIDE. REPAIRED IAW SRM 51-10-05

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,914 hrs · 41,736 cycles

53-2058 EXTERNAL SKIN CORROSION AT HEATED WATER DRAIN BTW FR60-61, BTW STR19-20L. REPAIRED IAW ETD2025-145-928591 AND SRM 51-40-02

Part: STIFFENER — CRACKED (NLG WW) · airframe 45,914 hrs · 41,736 cycles

NLG BAY WHEEL STOPPER AT FR 2, INTERTNAL STIFFENER CRACKED. R & R STIFFENER IAW SRM 51-40-02.

Part: PLATE — CORRODED (ZONE 100 WW) · corrosion level 2 · airframe 45,914 hrs · 41,736 cycles

NLG CEILING PLATE CORRODED AT BTW FR4-7. R & R PLATE IAW SRM 51-40-02

Part: DISPLAY — FAILED (ZONE 200)

DURING APPR FO MFD STARTED FLICKERING FOLLOWED BY SLIGHT ELECTRICAL ODOR DISAPATED AFTER FO MFD DIMMED TO BLACK. R&R #2 MFD IN REF TO AMM 34-22-01-000/400-801-A OPS CHECK GOOD OK FOR SERVICE.

Part: ELEC CONNECTOR — LOOSE (ZONE 100) · airframe 44,883 hrs · 40,585 cycles

HS2 VALVE FAIL MESSAGE DURING TAKE OFF. FACT 08MAR25 22:23 ORD MX FOUND HS2 VALVE CANNON PLUG BACKSHELL LOOSE TIGHTENED BACK SHELL IAW AS REQ. OPS CHECKED IAW AMM 36-11-02. OPS CHECK GOOD A/C OK FOR SERVICE AT THIS TIME

Part: CONTROL VALVE — ABNORMAL (ZONE 400) · airframe 44,850 hrs · 40,541 cycles

HS2 VALVE FAIL MESSAGE DURING T/O, ABORT. R&R #2 HSV IAW AMM 36-11-02 OPS CHECK GOOD

Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 44,021 hrs · 39,650 cycles

HS VLV 2 FAIL ON T/O ROLL MEL 04OCT24 18:37 EWN C27818 36-1-3 RIGHT ENG BLEED INOP DFRL 04OCT24 22:55 EWN C/W MEL PROCEDURE. E2 BLD VLV SECURED CLOSED.

Part: PRESSURE SWITCH — FAULTED (PARKING BRAKE)

WHILE ATTEMPTING TAKEOFF "NO TAKE OFF CONFIG" EICAS MESSAGE APPEARED. R+R PARKING BRAKE PRESSURE SWITCH PER AMM 32-44-07. OPS AND LEAK CHECK GOOD. C/W AWU OPS CHECK PER AMM 31-51-00. OPS CHECK GOOD. SET A/C TO T/O CONFIGURATION CYCLED THRUST LEVERS FROM IDLE TO THRUST SET AND FULLY FWD POSITION MANY TIMES. "NO TAKEOFF CONFIG" EICAS MESSAGE WAS NOT DISPLAYED. OPS CHECK GOOD. OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,875 hrs · 37,192 cycles

ABNORMAL CABIN ALTITUDE INDICATION AT 30000 FT. CABIN ALTITUDE INDICATION READ UP TO 14,800 FT. FOUND ECS SLEEVE ON #1 CONDENSER MIXER LEAKING. R/R'D IAW AMM 21-51-04. R/R'D DIGITAL CONTROLLER IAW AMM 21-31-01. OPS CHECKS GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,542 hrs · 36,820 cycles

AROUND 900 FEET, LOUD NOISE HEARD, FOLLOWED WHITE SMOKE OBSERVED IN CABIN BETWEEN ROW 7 AND 9, NO ABNORMAL INDICATIONS SHOWN IN FLT DECK. FACT 14JUN23 16:01 PHL FOUND BLOWN DUCT BETWEEN ROW 7,8,9, REINSTALLED DUCT AND SECURED WITH NEW CLAMP. RAN PACK 1 FOR FIVE MINUTES. NO LEAKS NOTED. OPS CHECK GOOD ACFT OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,538 hrs · 36,816 cycles

E968646 PILOT SIDE BULHEAD OUTB GUIDE PIN HOLE ELONGATED. REPAIRED IAW EMB148 SRM 53-21-02 ITEM 4 FIGURE 204 AND PIEDMONT EO1-53-23-0105

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,538 hrs · 36,816 cycles

E968665 FRAME 68 IS CRACKED JUST BELOW CARGO DOOR HOLD OPEN CUP. REPAIRD IAW EMBREAR ETD2023-145-009411 AND PIEDMONT EO 1-*53-23-0106.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,538 hrs · 36,816 cycles

E968631 LEVEL 2 CORROSION ON CENTER #3 OMEGA BEAM GUSSET. REMOVED AND REPLACED IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,538 hrs · 36,816 cycles

E968620 LEVEL 2 CORROSION IN LAV AREA ON CENTER FLOOR GUSSET. REPAIRED IAW EMB145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,538 hrs · 36,816 cycles

E968626 LEVEL 2 CORROSION ON CENTER #4 OMEGA BEAM GUSSET. REPAIRED IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,538 hrs · 36,816 cycles

E968625 COROSSION ON LH #5 OMEGA BEAM GUSSET. REPAIRED IAW EMB145 SRM 51-10-03, 53-23-10, AND 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,538 hrs · 36,816 cycles

E968627 LEVEL 2 CORROSION ON CENTER #5 OMEGA BEAM GUSSET. REPAIRED IAW EMB145 SRM 51-10-03, 53-23-10, AND 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,538 hrs · 36,816 cycles

E968586 SSI LEVEL 2 CORROSION ON CARGO DOOR FLOOR SILL REPAIRED IAW EMB145 SRM51-10-03, 51-40-02,51-40-03,51-40-06 AND 51-40-09

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,538 hrs · 36,816 cycles

E968619 LEVEL 2 CORROSION IN LAV AREA ON RH FLOOR GUSSET REPAIRED IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,538 hrs · 36,816 cycles

E968624 LEVEL 2 CORROSION ON LH #6 OMEGA BEAM GUSSET. REPAIRED IAW EMB145 SRM 51-10-03, 53-23-10, AND 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,538 hrs · 36,816 cycles

E968313 RH WING RIB 21 CRACKED. REPAIRED IAW EMB145 SRM 57-20-07-RE AND PIEDMONT EO1-57-23-0103

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,538 hrs · 36,816 cycles

E968314 LH WING RIB 21 IS POSSIBLE OF BEING CRACKED REPAIRED IAW EMB145 SRM 57-20-07RE AND PIEDMONT EO1-57-23-0104

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,538 hrs · 36,816 cycles

E968207 RH ENGINE YOKE ASSY HAS POSSIBLE CRACK AT FWD OTBD LOWER CORNER. REPAIRED IAW PIEDMONT FCD1-54-21-0017 REV D, REPLACEMENT OF RH FWD YOKE LINKAGE FITTINS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,583 hrs · 36,816 cycles

E968006 POSSIBLE SKIN CRACK AT 2 RIVETS AT FR79 BETWEEN STR3R AND 4R. REPAIRED IAW EMB145 SRM 53-20-01RE9 C,2 D-F FIG213 SHEET 2-3 AND PIEDMONT EO1-53-23-0101

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,538 hrs · 36,816 cycles

E967852 POSSIBLE SKIN CRACKS AROUND FASTENER (1EA) AT FRAME 77 BETWEEN STR 08L AND 09L. REPAIRED IAW EMB145 SRM 53-32-01 RE9 C,2 D-F FIG 213 SHEET 2-3 AND PIEDMONT EO1-53-23-0102

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,538 hrs · 36,816 cycles

E967855 POSSIBLE CRACKS AROUNDFASTENER (4EA) AT FR77 BETWEEN STR 05R-07R. REPAIRED IAW ETD2023-145-008966 AND PIEDMONT EO1-53-23-0107.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,538 hrs · 36,816 cycles

E967854 POSSIBLE SKIN CRACKS AROUND FASTENER (3EA) AT FR77 BETWEEN STR03R AND 05R. REPAIRED IAW EMB145 SRM 53-32-01 RE 9 C,2 D-F FIG 213 SHEET 2-3 AND PIEDMONT EO1-53-23-0101

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,538 hrs · 36,816 cycles

E967856 POSSIBLE CRACKS AROUNF FASTENER (1EA) AT FR77 BTWEEN STR08R AND 09R. REPAIRED IAW EMB145 SRM 53-32-01 RE 9 C,2 D-F FIG 213 SHEET2-3 AND PIEDMONT EO1-53-23-0101

Part: UNKNOWN — ODOR (CABIN) · airframe 41,296 hrs · 36,579 cycles

AFTER LANDING, SMELL OF BURNING APPROX 5 MINS INTO TAXI I CALLED FOR STANDARD TAXI SINGLE ENGINE. 1-2 MINS AFTER STICK SHAKER ACTIVATION AS WELL AS MFD INOP. PRESSURE BEGAN TO CLIMB & WE RESET PACKS, DID NOT WORK & KEPT PACKS OFF, SMELL OF BURNING AS WELL. REF AML 4960091 ITEM 1. PERFORMED ENG ODOR EVENT TROUBLESHOOTING IAW ETN-EM-72-034. NO ODOR NOTED.

Part: CONNECTOR — LOOSE (NLG PROX SWITCH) · airframe 41,176 hrs · 36,452 cycles

LG AIR GND FAIL AFTER TAKE OFF. CAN?T ENTER ICING CONDS. EMERGENCY DECLARED.-C/A-FOUND NLG PROX SWITCH CONNECTOR LOOSE, RESECURED IAW AMM 32-63-02/ETN-EM-32-176 OPC GOOD IAW AMM 32-63-00-700-801

Part: INVERTER — INOPERATIVE (CP) · airframe 40,820 hrs · 36,055 cycles

COCKPIT STEPUP EMERGENCY EXIT SIGN INOP-C/A-RAR INVERTER #1 IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A NO FIX, INVERTER BAD FROM STOCK. INSTALLED NEW INVERTER OPS CHECK GOOD.

Part: ACM — INTERMITTENT (CABIN) · airframe 40,351 hrs · 35,502 cycles

ON CLIMB AIRCRAFT DID NO PRESSURIZE. TRIED MANUAL PRESSURIZATION. DID NOT WORK. RAN QRH PRSN AUTO FAIL CHECKLIST. RETURNED TO DFW DID NOT DECLARE EMERGENCY.-C/A-RAR GROUND CONNECTION VALVE COVER IAW AMM 21-22-04.PERFORMED OPERATIONAL CHECK FOR PRESSURIZATION IAW AMM 21-31-00, IN AUTO AND MANUAL MODES.OPC GOOD. NO DEFECTS NOTED.

Part: INVERTER — UNSERVICEABLE (#6) · airframe 40,152 hrs · 35,284 cycles

FWD OVERWING EMER LIGHT INDICATOR INOP.-C/A-T/S AND FOUND INVERTER #6 INOP. RAR'D #6 INVERTER PER AMM 33-50-11. OPS CHECK IS GOOD.

Part: NONE — BROKEN (AFT) · airframe 40,152 hrs · 35,284 cycles

AFT EMERGENCY FLASHLIGHT HOLDER IS BROKEN-C/A-RAR AFT EMERGENCY FLASHLIGHT HOLDER IAW AMM 33-50-16. OPS CHECK GOOD

Part: NONE — NONE · airframe 39,786 hrs · 34,892 cycles

AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT/HOLDER INOP.MEL 25-32 - AUTH# 02-224M-C - LOG PAGE 4768660 ITEM #1 --C/A-REMOVED AND REPLACED AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT ASSY PER AMM 33-50-16. OPS CHECK GOOD. MEL RESTORED.

Part: NONE — NONE · airframe 39,765 hrs · 34,872 cycles

FORWARD CABIN FA EMERGENCY FLASHLIGHT CRADLE BROKEN-C/A-DEFERRED PER MEL 25-32 MAINT PROCEDURE C\W

Part: NONE — NONE · airframe 39,654 hrs · 34,739 cycles

LAV SMOKE EICAS MESSAGE RECEIVED AT GATE-C/A-RESET LAV SMOKE CB AND PERFORMED LAV SMOKE OPS CHECK IAW EMB 145 AMM 26-14-00-700-801-A. OPS CHECK GOOD

Part: NONE — NONE · airframe 39,506 hrs · 34,572 cycles

ALL EMERGENCY LIGHTS POWERED BY NO.3 EMERGENCY POWER SUPPLY INOP-C/A-RAR NO.3 BATTERY AND POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPC GOOD

Part: NONE — NONE · airframe 39,130 hrs · 34,141 cycles

#2 AND #3 FLOOR PROXIMITY STRIP LIGHTS INOP-C/A-RAR #2 EMERGENCY LIGHTING POWER SUPPLY BATTERY AND CHARGER IAW ENVOY WC 33-700-19. DID NOT FIX. REMOVED #2 FLOOR PROXIMITY STRIP LIGHT IAW EMB AMM 33-50-12-000-801-A AND FOUND SPLICE DISCONNECTED. RECONECTED AND REINSTALLED #2 FLOOR PROXIMITY STRIP LIGHT IAW EMB AMM 33-50-12-400-801-A. OPS CHECK GOOD. END.

Part: NONE — NONE · airframe 39,109 hrs · 34,118 cycles

CLIP ON F/A'S FWD EMERGENCY FLASHLIGHT BROKEN-C/A-RAR F/A EMERGENCY FLASH LIGHT ASSEMBLY IAW AMM 33-50-16 OPERATIONAL CHECK GOOD

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 39,076 hrs · 34,075 cycles

PASSENGER EMERGENCY LIGHT STRIP #1 HAS A WIRE BROKEN-C/A-REPAIRED EMERGENCY LIGHT STRIP #1 WIRE SPLICE CONNECTOR IAW EMB 145 SWPM 20-21-00 AND 20-50-01. OPS CHECK GOOD.

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 39,067 hrs · 34,064 cycles

MEL 2532 AUTH 09-59M-C AML 4798735 ITEM 1. AFT EMERGENCY FLASHLIGHT HOLDER BROKEN, WILL NOT HOLD FLASH LIGHT-C/A-REMOVED AND REPLACED EMERGENCY FLASHLIGHT ASSEMBLY AT AFT POSITION IAW EMB 145 AMM 33-50-16 OPERATIONAL CHECK IS GOOD MEL RESTORED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,784 hrs · 33,723 cycles

MAIN DOOR INTERIOR EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR INTERIOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECK GOOD.

Part: FLAP SYSTEM — OVERSPEED · airframe 37,952 hrs · 32,904 cycles

FLAP OVER SPEED ON TAKEOFF 270 KNTS 2 MINUTES GEAR WAS UP ONE TIME. DAMAGE FLP OVRSPD, MTX EVALUATING C/A-REF. NRWC 922-ORD-05079 FOR DFDR DOWNLOAD INFO. ACCOMPLISHED EMB WC 05-200-06 AS REQUIRED. NO DEFECTS NOTED AT THIS TIME.

Part: NUT PLATE — CORRODED (CARGO DOOR) · airframe 37,667 hrs · 32,632 cycles

CARGO DOOR AFT NUT PLATE HOLES HAVE SURFACE CORROSION. C/A: FABRICATED DOUBLER, FILLER AND SHIM FOR REPAIR OF NUTPLATE HOLE ON CARGO DOOR AFT NUTPLATE HOLES, IAW EMB-145 SRM 52-30-04 RE.

Part: LINER — CHAFED (CARGO DOOR) · airframe 37,667 hrs · 32,632 cycles

CARGO DOOR BACK LINER WEBBING HAS ONE CHAFED SPOT. C/A: REPAIRED THE CARGO DOOR BACK LINER WEBBING, IAW EMB 145 SRM 52-30-01 ETN-EM-52-043.

Part: BRACKET — CRACKED (FRAMES 18-20) · airframe 37,667 hrs · 32,632 cycles

PASSENGER DOOR REINFORCEMENT FRAME BRACKET IS CRACKED BETWEEN FR 18-20, STGR 3L. C/A: REMOVED AND REPLACED PASSENGER DOOR REINFORCEMENT FRAME BRACKET, IAW EMB 145 SRM 51-40-02.

Part: RIB — CRACKED (LT ELEVATOR) · airframe 37,667 hrs · 32,632 cycles

LT ELEVATOR INBOARD HINGE INBOARD RIB HAS POSSIBLE CRACKS AROUND LEADING EDGE DRAIN HOLE. C/A: REMOVED AND REPLACED LT ELEVATOR INBOARD HINGE INBOARD RIB, IAW EMB 145 SRM 51-40-02.

Part: BUSHING — WORN (LT AILERON) · airframe 37,667 hrs · 32,632 cycles

LT AILERON PCA ROD FITTING (ON AILERON) OUTBOARD LUG HAT BUSHING HOLE WORN. C/A: REMOVED AND REPLACED LT AILERON PCA FITTING, IAW EO EM-27MR-112.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 37,667 hrs · 32,632 cycles

LATERAL UPPER MOUNTING BRACKET P/N 123-07551-006 IS CRACKED, RT SIDE OF THE COCKPIT CROWN. C/A: INSTALLED LATERAL UPPER MOUNTING BRACKET RT SIDE OF THE COCKPIT CROWN, IAW EMB 145 SRM 51-40-02.

Part: WEB — GOUGED (FRAME 19A-20) · airframe 37,667 hrs · 32,632 cycles

SERVICE DOOR CUTOUT REINFORCING WEB IS GOUGED JUST ABOVE THE DOOR HINGE. C/A: INSTALLED FABRICATED FILLER, SHIM, AND INTERNAL DOUBLER ON SERVICE DOOR REINFORCING WEB, IAW ENVOY ERS-EM-53MR-4214.

Part: DOOR SILL — CORRODED (FRAMES 65-68) · airframe 37,667 hrs · 32,632 cycles

CARGO DOOR LOWER SILL IS CORRODED. C/A: INSTALLED SERVICABLE CARGO DOOR LOWER SILL, IAW EMB145 SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FRAME 68) · airframe 37,667 hrs · 32,632 cycles

FRAME 68 SHEAR CLIP IS CORRODED AT CARGO DOOR LOWER SILL. C/A: INSTALLED SERVICEABLE FR 68 SHEAR CLIP REPAIR SECTION AT CARGO DOOR LOWER SILL, IAW EMB145 SRM 53-31-04, ETN-EM--53-272.

Part: SHEAR TIE — CORRODED (FRAMES 65) · airframe 37,667 hrs · 32,632 cycles

FRAME 65 SHEAR CLIP IS CORRODED AT CARGO DOOR SILL. C/A: INSTALLED SERVICEABLE FR 65 SHEAR CLIP REPAIR SECTION, IAW EMB145 SRM 53-31-04, ETN-EM-53-272.

Part: STRUCTURE — CORRODED (CARGO DOOR) · airframe 37,667 hrs · 32,632 cycles

CARGO DOOR FWD NUT PLATE HOLES HAVE SURFACE CORROSION. C/A: UPON FURTHER INVESTIGATION FOUND 3 NUTPLATE HOLES TO BE OUT OF ALLOWABLE LIMITS ON CARGO DOOR FWD FRAME, IAW EMB-145 SRM 52-30-04 RE. PERFORMED 3 CUTOUTS TO REMOVE DAMAGE AND FABRICATED AND INSTALLED DOUBLERS AND FILLERS, IAW EMB-145 SRM 52-30-04 RE. ALL OTHER BLENDED AREAS ARE WITHIN ALLOWABLE LIMITS, IAW EMB-145 SRM 52-30-04 AD.

Part: SKIN — DAMAGED (RUDDER) · airframe 37,667 hrs · 32,632 cycles

RUDDER 2 AFT LOWER EDGE DAMAGED (CHAFED, SEPARATED AND RT SKIN CRACKED). C/A: INSTALLED DOUBLER AND FILLER ON RUDDER 2 RT AFT LOWER EDGE, IAW ERS-EM-55MR-866.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 37,667 hrs · 32,632 cycles

ALL LT RT CENTER AISLE CARPET AND EMERGENCY LIGHT STRIP SUPPORTS DAMAGED. C/A COMPLETE: REPLACED ALL LT/RT CENTER ISLE CARPET EMERGENCY LIGHT STRIP SUPPORT COVERS, IAW EMB145 AMM 33-50-12 SEE NRTC BOW348179 FOR AIRCRAFT INSTALLATION.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 37,667 hrs · 32,632 cycles

EMERGENCY LIGHT STRIPS NR 1, 3, 5, 6, 7, 8 CONNECTOR WIRING DAMAGED/BROKEN. C/A COMPLETE: REPLACED EMERGENCY LIGHT STRIPS 1, 3, 5, 6, 7, AND 8, IAW EMB145 AMM 33-50-12 SEE NRTC BOW348179 FOR AIRCRAFT INSTALLATION AND OPERATIONAL CHECK

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,147 hrs · 31,177 cycles

DURING PS-1 CHECK, FOUND FORWARD AMBER EMERGENCY LIGHT FLOOR PROXIMITY STRIP AND SERVICE DOOR SMALL EXIT IDENTIFIER SIGN INOP. C/A-R&R FWD AMBER EMERGENCY LIGHT FLOOR PROXIMITY STRIP, OPC BAD, IAW AMM 33-50-12. REF ITEM 2 OF THIS NRWC

Part: ACM — FAULTY (AC BAY) · airframe 36,145 hrs · 31,176 cycles

IN CRUISE FLT FL240, FA REPORTED SMOKE IN THE CABIN, FOLLOWED AOM EMERGENCY PRECEDURES, LANDED SAFELY IN TPA. UPON CABIN INSPECTION FOUND SMOKE MARKS BY SEATS 4C, 5C. FA REPORTS SMOKE CAME OUT BY SEATS 3A, 4A.PAX REPORTS VIBRATION BY SEAT 11A. C/A-DURING INSPECTION OF #2 PACK FOUND ACM NOT TURNING. REMOVED AND REPLACED ACM OPS CHECK GOOD IAW AMM 21-51-03. NO SMOKE IN THE CABIN NOTED.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 36,142 hrs · 31,172 cycles

SMOKE IN FLIGHT DECK LEVEL AT FL250 DIVR JAX ACCT SMOKE IN COCKPIT. EMER DECL. C/A-PERFORMED FIM TASK 21-20-00-810-801-A AND FOUND PACK 1 ACM NOT CYCLING PROPERLY. REF ITEM 2 THIS LG PG FOR PACK 1 DEFERRAL AND PERFORMED ETN-EM-72-034.

Part: FITTING — DEFECTIVE (BRAKE SYSTEM) · airframe 35,103 hrs · 30,303 cycles

PARKING BRAKE WILL NOT REMAIN ENGAGED. "TRANSFERRED TO NRWC 922-DFW-04012". C/A-TRANSFERRED FROM NRWC 922-DFW-04012. REMOVED AND REPLACED EMERGENCY/PARKING BRAKE FITTING ASSY IAW AMM TASK 32-44-11. OPS CHECK GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 34,882 hrs · 30,088 cycles

EMERGENCY LIGHT STRIP AT ROW 1-3 INOP. C/A-REPAIRED EMERGENCY LIGHT STRIP WIRING IAW SWPM 20-21-00. OPS CHECK GOOD NO FURTHER DEFECTS FOUND.

Part: HOSE — DAMAGED (AC BAY) · airframe 34,772 hrs · 30,014 cycles

SUPPLEMENTAL CABIN ALT WAS 9000' AND CLIMBING AS WE STARTED DESCENT THROUGH FL240. WE BEGAN RAPID DESCENT TO 10,000'. CABIN ALT WAS MAXED AT 11,300' THE BEGAN DESCENDING. C/A-DEFERRED ELECTROPNUEMATIC AND PNEUMATIC OUTFLOW VLVS. M PROCEDURES C/W MEL 21-22 AUTH 030207DMC. PERFORMED FIM T/S 21-31-00-810-808A THRU STEP 9. FOUND AIR LEAKAGE FROM MAIN DOOR UPPER FLAP, NR 1 DUAL TEMP VALVE COUPLING AND CARGO DOOR SEAL. ALL ITEMS HAVE BEEN REPAIRED AS PER AMM 52-18-04, AMM 21-60-01, AND AMM 52-00-04. PERFORMED CABIN LEAKAGE TEST I/A/W AMM 21-31-00-700-808 A/500. LEAKS CHECK OK. MEL RESTORED. RESECURED MAIN DOOR UPPER FLAP SEAL WITH RTV 157 IAW AMM 52-18-04. APPLIED RTV AT 2PM. REMOVED AND REAPPLIED SEALANT BETWEEN BAGGAGE DOOR PROTECTOR STRIP AND ALUMINUM SKIN AS PER AMM 53-31-09. SEALANT APPLIED AT 9:45 PM. REMOVED AND REPLACED RUBBER HOSE FOR PACK 1 DUAL TEMP CONTROL VALVE AND Y-DUCT AS PER AMM 21-60-01. OPC AND LEAK CHECK GOOD.

Part: FLASHLIGHT — OUT OF POSITION (CABIN) · airframe 34,763 hrs · 30,008 cycles

AFT FA FLASHLIGHT MISSING. C/A-FLIGHT CREW PLACARDED AFT FA FLASHLIGHT AUTH # 030160-C MEL 25-53. AFTER INSPECTION FOUND F/A AFT FLASHLIGHT, INSTALLED AS REQUIRED. OPS CK GOOD. IAW AMM 33-51-01. MEL RESTORED / MOC # 607040.

Part: PRESSURE SWITCH — INOPERATIVE (RUDDER) · airframe 33,968 hrs · 29,377 cycles

RUD DER SYS 1-2 INOP OVER 180 KNOTS.EMERGENCY DECLARED DID NOT HAVE AN OVERWEIGHT LANDING.FLT CONT.-C/A-REF FIM 27-22-00-810-804-A, RPL'D SYS 2 RUDDER PERSSURE SW IN REF TO / AMM 27-23-04 & OPS CHKED RUDDER SYS OK IN REF TO AMM 27-23-00. NO FAULT & LEAK FOUND.NO COMPONENT RAR.

Part: NOT REPORTED — MALFUNCTIONED (FLIGHT CONTROL) · airframe 33,932 hrs · 29,340 cycles

SPS 2 INOP DURING LEVEL CRUISE FLIGHT. NO CMC MSG. TROUBLESHOT SAPS IAW FIM 27-36-00-810-802-A BLOCKS 1 & 10. OPS CHECK GOOD. CONDITION CONSIDERED TRANSITORY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,745 hrs · 29,121 cycles

MAIN DOOR EXTERNAL EMERGENCY LT INOP. -C/A-R&R MAIN DOOR EXTERNAL EMERGENCY LT LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD.

Part: BEAM — CORRODED (FRAMES 65 - 66) · corrosion level 2 · airframe 32,680 hrs · 28,115 cycles

CORROSION ON THE CARGO DOOR CUTOUT THRESHOLD BEAM BETWEEN FRAMES 65 AND 66. BLENDED THE CORROSION ON THE CARGO DOOR CUT OUT THRESHOLD BEAM, FOUND TO BE OUT OF LIMITS IAW SRM 53-31-15. REMOVED THRESHOLD BEAM IAW SRM 51-40-02. LOCATED, DRILLED AND ALODINED A NEW THRESHOLD BEAM IAW SRM 51-20-03, AND CPM 51-21-04. INSTALLED A NEW THRESHOLD BEAM AND RESTORED PROTECTIVE COATING IAW SRM 51-40-02, CPM 51-21-04, 51-21-05, AND 51-21-06.

Part: SHEAR TIE — CRACKED (FRAME 25) · airframe 32,680 hrs · 28,115 cycles

CRACKED SHEAR TIE AT FRAME 25 BETWEEN STRINGERS 15L AND 16L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, CPM 51-21-04, 51-21-05, AND 51-21-06.

Part: TEE FITTING — CORRODED (FRAME 65) · corrosion level 2 · airframe 32,680 hrs · 28,115 cycles

CORRODED TEE FITTING AT FRAME 65 THRESHOLD. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-05. DRILLED, LOCATED AND ALODINED A NEW TEE FITTING IAW SRM 51-20-03 AND CPM 51-21-04. INSTALLED THE NEW TEE FITTING AND RESTORED TOP COAT TO FASTENERS IAW SRM 51-40-02, AND ETN EM-51-091.

Part: FRAME — GOUGED (FRM 60) · airframe 32,680 hrs · 28,115 cycles

GOUGE IN FRAME 60 AT PREVIOUS REPAIR BETWEEN STRINGERS 4L AND 5L. REMOVED PREVIOUS REPAIR AND ENLARGED THE CUT OUT. REMOVE DAMAGE, INSTALLED A NEW REPAIR IAW SRM 53-00-04.

Part: SHEAR TIE — CRACKED (FRAME 25) · airframe 32,680 hrs · 28,115 cycles

CRACK IN SHEAR TIE AT FRAME 25, BETWEEN STRINGERS 15R AND 16R. 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 AMM 20-10-01.

Part: FLOOR SUPPORT — CORRODED (FRAME 29) · corrosion level 2 · airframe 32,680 hrs · 28,115 cycles

CORROSION ON THE LT OMEGA AT CROSSMEMBER, FRAME 29. REMOVED CROSS MEMBER AT FRAME 29 TO FOM AND INSTALLED EWIS PROTECTION IAW SRM 51-40-02 AND SWPM 20-21-00. BLENDED CORROSION ON LEFT OMEGA AND FOUND TO BE OUT OF LIMITS OF SRM 53-22-10. CUT OUT DAMAGED AREA IAW SRM 53-00-10. PERFORMED HFEC INSPECTION OF CUT OUT AREA IAW NDTM 51-00-00-918-801-A00. LOCATED DRILLED ALODINED AND PRIMED REPAIR PIECES IAW SRM 51-20-03 AND CPM 51-21-04 AND 51-21-05. INSTALLED DOUBLED IAW SRM 51-40-02 AND 53-00-10. REINSTALLED PREVIOUSLY REMOVED CROSS MEMBER IAW SRM 51-40-02 AND REMOVED EWIS PROTECTION IAW SWPM 20-21-00

Part: SHEAR TIE — CRACKED (FRAME 27) · airframe 32,680 hrs · 28,115 cycles

CRACKED SHEAR TIE AT FRAME 27 BETWEEN STRINGERS 15R AND 16R. REMOVED AND REPLACED THE SHEAR IAW SRM 51-40-02. LOCATED, DRILLED AND ALODINED IAW SRM 51-20-03 AND CPM 51-21-04, SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FRAME 59) · airframe 32,680 hrs · 28,115 cycles

LEFT OMEGA BEAM HAS A CRACK AT THE NUTPLATE HOLE, FRAME 59. CUT OUT DAMAGE IAW SRM 53-24-10. PERFORMED HFEC INSPECTION ALONG AREA OF DAMAGE REMOVAL IAW NDTM 51-00-00-916-801-A00, NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER IAW SRM 53-24-10, AND 51-30-01. PERFORMED FPI OF REPAIR DOUBLER, NO DEFECTS NOTED IAW NDTM INTRODUCTION SECTION D. LOCATED, DRILLED, ALODINED, AND PRIMED THE DOUBLER IAW SRM 53-24-10, FIG 203, CPM 51-21-04, AND 51-21-05. INSTALLED THE DOUBLER IAW SRM 53-24-10, FIG 203, CPM 51-21-05, AND 51-21-06.

Part: FLOOR SUPPORT — CRACKED (FRAME 61) · airframe 32,680 hrs · 28,115 cycles

RIGHT OMEGA BEAM HAS A CRACK AT THE NUTPLATE HOLE AT FRAME 61. CUT OUT DAMAGE IAW SRM 53-24-10. PERFORMED HFEC INSPECTION ALONG AREA OF DAMAGE REMOVAL IAW NDTM 51-00-00-916-801-A00, NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER IAW SRM 53-24-01 AND 51-30-01. PERFORMED FPI OF REPAIR DOUBLER , NO DEFECTS NOTED IAW NDTM INTRODUCTION SECTION D. LOCATED , DRILLED, ALODINED, AND PRIMED THE DOUBLER IAW SRM 51-20-03, CPM 51-21-04, AND 51-21-05. INSTALLED THE DOUBLER IAW SRM 51-20-01, 51-40-02, CPM 51-21-05, AND 51-21-06

Part: SHEAR TIE — CRACKED (FRAME 28) · airframe 32,680 hrs · 28,115 cycles

CRACK IN SHEAR TIE AT FRAME 28 BETWEEN STRINGER 15R AND 16R. REMOVED THE SHEAR TIE IAW SRM 51-40-02. LOCATED, DRILLED AND ALODINED A NEW SHEAR TIE IAW SRM 51-20-03 AND CPM 51-21-04. INSTALLED IAW SRM 51-40-02, CPM 51-21-04, 51-21-05, AND 51-21-06.

Part: FLOOR SUPPORT — CORRODED (FRAME 29) · corrosion level 2 · airframe 32,680 hrs · 28,115 cycles

CORROSION ON THE LT OMEGA BEAM AT CROSSMEMBER, FRAME 29. BLENDED THE CORROSION IAW SRM 53-22-10, DETERMINED TO BE OUT OF ALLOWABLE LIMITS. CUT OUT DAMAGE IAW SRM 53-00-10. PERFORMED HFEC INSPECTION OF CUT OUT AREA IAW NDTM 51-00-00-918-801-A00, NO DEFECTS NOTED. FABRICATED A SHIM , FILLER, AND EXTERNAL ANGLE. LOCATED, DRILLED, ALODINED AND PRIMED THE REPAIR IAW SRM 51-20-03, CPM 51-21-04, AND 51-21-05. INSTALLED THE REPAIR IAW SRM 51-40-02 AND 53-00-10.

Part: SHEAR TIE — CRACKED (FRAME 65) · airframe 32,680 hrs · 28,115 cycles

CRACKED SHEAR TIE, FRAME 65, BETWEEN STRINGERS 18L, AND 19L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02. LOCATED, DRILLED AND ALODINED NEW SHEAR CLIP IAW SRM 51-20-03, CPM 51-21-04, SRM 51-40-02, CPM 51-21-06, AND ETN GN-51-017.

Part: FLOOR SUPPORT — CRACKED (FRAME 59) · airframe 32,680 hrs · 28,115 cycles

RIGHT OMEGA BEAM HAS A CRACK AT THE NUTPLATE HOLE, FRAME 59. CUT OUT DAMAGE IAW SRM 53-24-10. PERFORMED HFEC INSPECTION ALONG AREA OF DAMAGE REMOVAL IAW NDTM 51-00-00-916-801-A00, NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER IAW SRM 53-24-10, AND 51-30-01. PERFORMED FPI OF REPAIR DOUBLER, NO DEFECTS NOTED IAW NDTM INTRODUCTION SECTION D. LOCATED, DRILLED, ALODINED, AND PRIMED THE DOUBLER IAW SRM 51-20-03, CPM 51-21-04, AND 51-21-05. INSTALLED THE DOUBLER IAW SRM 51-20-01, 51-40-02, CPM 51-21-05, AND 51-21-06

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 32,323 hrs · 27,796 cycles

BAG SMOKE MESSAGE RAN PROCEDURES IN AOM BAGG EXT BTL INOP MESSAGE. REMOVED AND REPLACED AFT BAGGAGE BAY NR 2 SMOKE DETECTOR IAW AMM TASK 26-15-01. OPS CHECK GOOD IAW AMM 26-15-00.

Part: BULB — INOPERATIVE (FLASHLIGHT) · airframe 32,250 hrs · 27,743 cycles

COCKPIT FLASHLIGHT INOPERATIVE. R & R THE BULB IAW AMM 33-50-16, OPS CHECKED GOOD.

Part: ENGINE — FAILED (NR 2) · airframe 32,050 hrs · 27,559 cycles

#2 ENGINE FAILED IN FLIGHT APPROXIMATELY 2 MIN AFTER TAKEOFF. FAILURE WAS ABRUPT, CREW FELT A THUMP THROUGH THE FLOOR. FO REPORTS HEARING A BANGING SOUND. N2 WENT TO 0.0%IMMEDIATELY E2 NO DISP AND HS VLV 2 FAIL ON SHUTDOWN, E2 NO DISP DISAPPEARED WHEN SWITCHING TO GPU AT GATE EICAS MOMENTARY FAILURE. REMOVED AND REPLACED #2 ENGINE IAW AE WORK CARD 71-00-00. OPS CHECK GOOD. LEAK CHECK GOOD

Part: RELAY — MALFUNCTIONED (DE ICE PRESSURE) · airframe 30,852 hrs · 26,408 cycles

DURING CLIMB AT 1700 FT, PERFORMED ICE TEST AND PRESSURE CLIMBED AT A RATE OF 2000 FPM, CANCELLED THE ICE TEST AND RETURNED TO NORMAL. PERFORMED QRH PROCEDURES. REMOVED AND REPLACED THE RELAY K0412 IAW AMM 20-13-02, AND WM 21-30-50. PERFORMED AND OPS CHECK OF THE PRESSURIZATION CONTROL SYSTEM IAW AMM 21-31-00. OPS CHECKED GOOD.

Part: SEAL — MISSING (PAX DOOR) · airframe 30,851 hrs · 26,407 cycles

ON REACHING FL 350, PRESSURE NORMAL DURING CLIMB & CRUISE. SHORTLY AFTER NOTICED CABIN RATE AND CABIN ALTITUDE INCREASING UP TO 8600 AND RISING. SWITCHED TO MANUAL MODE WITH NO RESPONSE IN FULL DOWN POSITION. STARTED DESCENT TO 10,000 FT. CABIN ALTITUDE STILL WAS CLIMBING AND REACHED 10,000 CABIN ALTITUDE. PASSING FL 240 STARTED TO REGAIN MANUAL CONTROL OF PRESSURIZATION SYSTEM. DIVERTED. RUBBER SEAL RING AT GROUND CONNECTION DOOR MISSING. INSTALLED GROUND CONNECTION SEAL IAW 21-22-04. PERFORMED OPS CHECKED IAW 21-31-00-700-808. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: CHARGER — FAILED (CABIN) · airframe 30,765 hrs · 26,335 cycles

EMERGENCY FLOOR PROX LIGHT 1 WILL NOT ILLUMINATE. REMOVED AND REPLACED 2 EMERGENCY LIGHT CHARGER AND BATTERY IAW AMM 33-50-04 OPS CK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 85712

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 29,809 hrs · 25,474 cycles

FWD FLIGHT ATTENTDANT FLASHLIGHT INOPERATIVE. REMOVED & REPLACED THE FLASHLIGHT. OPS CHECKED GOOD IAW AMM 33-50-16.

Part: HYDRAULIC SYSTEM — MALFUNCTIONED (NR 1) · airframe 29,516 hrs · 25,223 cycles

DURING CLIMBOUT RECEIVED NR 1 HYDRAULIC LOW QTY MESSAGE. QUANTITY CONTINUED TO DECREASE THROUGH THE AMBER, DECLARED EMERGENCY AND LANDED. HYDRAULIC FLUID STABILIZED IN AMBER AFTER LANDING. SERVICED THE NR 1 HYD FLUID IAW AMM 12-13-01. INSPECTED AIRCRAFT FOR LEAKS IAW AMM 29-10-00. NO LEAKS NOTED. AIRCRAFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,260 hrs · 24,117 cycles

AFT CEILING EMER LIGHT INOPERATIVE. R & R AFT CEILING EMER LIGHT LAMP. OPERATIONS CHECKED GOOD IAW AMM 33-50-08.

Part: ROLLER — LACK OF LUBE (DOOR FRAME) · airframe 28,095 hrs · 23,972 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN & CLOSE. SERVICED MAIN DOOR FRAME ROLLERS IAW 53-21-02.

Part: FITTING — GOUGED (RT AILERON) · airframe 27,990 hrs · 23,871 cycles

RIGHT AILERON DAMPENER FITTING IS GOUGED. R & R DAMPENER FITTING ON THE RT AILERON IAW EO EM-27MR-112.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,990 hrs · 23,871 cycles

RIGHT OMEGA BEAM, BETWEEN FRAME 18 & 18 IS CORRODED. REPAIRED RT OMEGA BEAM AT FRAME 18 NUTPLATE IAW ERS-EM-53MR-1906.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 27,990 hrs · 23,871 cycles

SERVICE DOOR AFT SILL HAS CORROSION. R & R SERVICE DOOR AFT SILL IAW SRM 51-40-02.

Part: CROSSMEMBER — CORRODED (FUSELAGE) · airframe 27,990 hrs · 23,871 cycles

CENTER AISLE CROSS MEMBER, BETWEEN FRAME 24 & 25 IS CORRODED. R & R CTR AISLE CROSS MEMBER, BETWEEN FRAME 24 & 25 IAW SRM 53-21-10 & ETN EM-53-139 R4.

Part: FITTING — GOUGED (RT AILERON) · airframe 27,989 hrs · 23,870 cycles

RIGHT AILERON DAMPENER FITTING IS GOUGED. R & R DAMPENER FITTING ON THE RT AILERON IAW EO EM-27MR-112.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 27,990 hrs · 23,871 cycles

CARGO DOOR CUT OUT CTR SILL CORRODED. R & R CARGO DOOR CUT OUT CTR SILL IAW SRM 51-40-02.

Part: CONNECTOR — CORRODED (CABIN) · airframe 27,990 hrs · 23,871 cycles

CONNECTOR P8528 AT FRAME 20 - 21, STRINGER 3R - 4R HAS MINOR SURFACE CORROSION. R & R CONNECTOR P8528 IAW SWPM 20-21-00 & 20-50-00.

Part: FITTING — CORRODED (FUSELAGE) · airframe 27,990 hrs · 23,871 cycles

FRAME 68 L SHAPE CORROSION ON LOWER PORTION, ABOVE CARGO DOOR SILL. REPAIRED FRAME 68 SHEAR CLIP IAW EO EM-53MR-1129 PART B, FOUND DURING INSPECTION IAW WC 53-200-69.

Part: WIRE — BROKEN (CABIN) · airframe 27,989 hrs · 23,870 cycles

NUMBER 2 EMER LIGHT STRIP WIRES BROKEN. R & R EMER LIGHT STRIP NR 2 IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 27,989 hrs · 23,870 cycles

EMERGENCY LIGHT STRIP NR 2 TORN ALONG EDGE. R & R EMER LIGHT STRIP NR 2 FLOOR SIDEWALL ASSEMBLY IAW AMM 33-50-12.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,070 hrs · 23,042 cycles

EXTERNAL EMER LIGHT ON SERVICE DOOR INOPERATIVE. R & R EXTERNAL EMER LIGHT ASSEMBLY ON SERVICE DOOR IAW AMM 33-50-09. OPERATIONS CHECKED GOOD.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 26,620 hrs · 22,644 cycles

LAVATORY SMOKE ON EICAS, WE GOT NW COURSE AS WELL. PERFORMED A 10 MIN ENG RUN AT IDLE IAW GND HANDLING CHECKLIST, NO SMOKE NOTED AT THIS TIME & AMM 26-14-00.

Part: CONTROL UNIT — FAILED (HORIZ STAB) · airframe 26,441 hrs · 22,455 cycles

ON CLIMB OUT THROUGH 5,000 HAND FLYING THE ACFT WE GOT A PTRIM MAIN INOPERATIVE. FOLLOWED AOM VOL 1 ABNORMAL PROCEDURE. R & R HSCU IAW AMM 27-40-01. OPERATIONS CHECKED GOOD. SEE ITEM NR 2 THIS LP.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 26,400 hrs · 22,407 cycles

RIGHT OVERWING EMER LIGHT INOPERATIVE. R & R RT OVERWING EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,319 hrs · 22,337 cycles

LEFT OVERWING EMER LIGHT INOPERATIVE. R & R LT EXTERNAL OVERWING EMER LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 25,356 hrs · 21,493 cycles

SERVICE DOOR EMER LIGHT INOPERATIVE. R & R SERVICE DOOR EMER LIGHT LAMP IAW AMM 33-50-09-000-801-A & 33-50-09-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: DOOR — OPEN (COMM) · airframe 24,383 hrs · 20,571 cycles

COM HATCH POPPED OPEN IN FLIGHT OR WAS NOT CLOSED ON GND. CLOSED DOOR & PERFORMED GVI OF DOOR & SURROUNDING AREA. NO DAMAGE NOTED.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 23,712 hrs · 20,022 cycles

LAVATORY SMOKE WARNING INDICATION DURING CRUISE FLIGHT. NO EVIDENCE OF SMOKE OR FIRE FOUND BY THE FLIGHT ATTENDANT OR CRASH, FIRE & RESCUE. DEFERRED IAW MEL 26-2 AUTH 040356DM C M PROCEDURES, COMPLIED WITH CORRECTIVE ACTION. PERFORMED OPERATIONAL ON POST OD SMOKE DETECTOR FOR LAVATORY IAW AMM 26-14-00-700-801-A. LAVATORY SMOKE DETECTOR, OPERATIONS CHECKED GOOD. MEL RESTORED

Part: FRAME — CRACKED (DOOR) · airframe 23,643 hrs · 19,970 cycles

272DR OUTER FRAME CRACKED AT RELEASE PIN RECEPTACLE. REPAIRED CRACKED AREA ON 272DR OUTER FRAME AT RELEASE PIN RECEPTACLE IAW AEA ERS-EM-52MR-109.

Part: PBE — UNSERVICEABLE (COCKPIT) · airframe 23,643 hrs · 19,970 cycles

COCKPIT PBE HAS A HOLE IN BAG. R & R COCKPIT PBE & BOX IAW AMM 20-10-01 & 35-30-03. FOUND DURING REMOVAL OF EMERGENCY EQUIPMENT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,643 hrs · 19,970 cycles

NR 4 FLOOR EMERGENCY LIGHT STRIP INOPERATIVE. R & R NR 4 FLOOR EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: SHEAR TIE — CRACKED (FRAME 65) · airframe 23,643 hrs · 19,970 cycles

FRAME 65 SHEAR TIE BETWEEN STRINGERS 7 & 9 LEFT CRACKED. R & R SHEAR TIE IAW SRM 53-31-04.

Part: ATTACH FITTING — CRACKED (RT WING) · airframe 23,643 hrs · 19,970 cycles

RIGHT UPPER OVERWING ATTACHMENT FLANGE BETWEEN FRAME 50 - 51 IS CRACKED APPROX 5 INCHES. ACCOMPLISHED REPAIR OF RT UPPER OVERWING ATTACHMENT FLANGE BETWEEN FRAME 50 - 51 IAW SRM 53-23-12.

Part: WINDOW FRAME — CORRODED (COCKPIT) · airframe 23,643 hrs · 19,970 cycles

COPILOTS WINDSHIELD HAS CORROSION ON LOWER INBD SIDE OF THE OUTER FRAME. BLENDED AREAS FOR CORROSION ON COPILOTS WINDSHIELD LOWER INBD SIDE OF THE OUTER FRAME ACCEPTED IAW ERS-EM-5600-024.

Part: WINDOW FRAME — CORRODED (COCKPIT) · airframe 23,643 hrs · 19,970 cycles

PILOTS WINDSHIELD HAS CORROSION ON LOWER INBD SIDE OF THE OUTER FRAME. BLENDED AREAS FOR CORROSION ON PILOTS WINDSHIELD LOWER INBD SIDE OF OUTER FRAME ACCEPTED IAW ERS-EM-5600-023.

Part: SHEAR TIE — CRACKED (FRAME 67) · airframe 23,643 hrs · 19,970 cycles

CARGO BAY FRAME 67 SHEAR TIE CRACKED BETWEEN STRINGER 7 & 8 LEFT. REPAIRED IAW SRM 53-31-04.

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 23,643 hrs · 19,970 cycles

SERVICE DOOR CUT OUT LOWER SILL CORRODED. R & R SILL IAW SRM 51-40-02.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,495 hrs · 19,852 cycles

FLIGHT ATTENDANT FLASHLIGHT INTERMITTENT. R & R FLIGHT ATTENDANT FLASHLIGHT IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,053 hrs · 19,500 cycles

SERVICE DOOR HINGE EMERGENCY LAMP INOPERATIVE. R & R SERVICE DOOR HINGE EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. R & R EMERGENCY BATTERY NR 2 IAW AMM 33-50-04-000-802-A & 33-50-04-400-802-A. OPERATIONS CHECKED GOOD IAW WC 33-700-17.

Part: WIRE — DAMAGED (CABIN) · airframe 22,946 hrs · 19,418 cycles

DURING REMOVAL OF FLOOR PANEL 261BF FOUND DAMAGED WIRE ON FLOOR PROX STRIP EMERGENCY LIGHT AT ROW 18. R & R FLOOR PROX STRIP EMERGENCY LIGHT AT ROW 18 IAW AMM 33-50-12, OPERATION GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LAV SMOKE) · airframe 22,529 hrs · 19,073 cycles

CREW REPORTED AFTER TAKEOFF, A LAVATORY SMOKE INDICATION ON EICAS AND RECEIVED A CALL FROM THE F/A REPORTING SMOKE IN REAR SECTION OF THE CABIN AND SMOKE ALARM ACTIVATED. NO FIRE OF SMOKE SOURCE WAS FOUND BY F/A. AIR RETURN, SMOKE ODOR IN CABIN GONE AT DESCENT STARTED. ACFT WAS MET ON THE TAXI WAY AND INSPECTED THE EXTERIOR OF ACFT. NO FIRE OR SMOKE DAMAGE FOUND. ACFT REMOVED FROM SERVICE. COMPLIED WITH EM-72-034 R4. NO ODORS WERE NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 22,338 hrs · 18,927 cycles

CAPTAIN FLASHLIGHT HOLDER BROKEN. R & R CAPTAINS FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,484 hrs · 18,233 cycles

DURING B INSPECTION, FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE SERVICE DOOR EMERGENCY LIGHT IAW TASK 33-50-09-000-801-A AND 33-50-09-400-801-A. THE OPS CHECK WAS GOOD AT THIS TIME. THE ACFT WAS RETURNED TO SERVICE.

Part: CHARGER — DEFECTIVE (CABIN) · airframe 21,059 hrs · 17,867 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY LIGHT BATTERY CHARGER NEEDS TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY CHARGER IAW EMB AMM 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — WEAK (CABIN) · airframe 21,059 hrs · 17,867 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY LIGHT BATTERY WEAK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BATTERY IAW EMB AMM 33-50-04. REF ITEM 1 LOG PG 3084360. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,018 hrs · 17,836 cycles

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

Part: CONTROLLER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 20,894 hrs · 17,732 cycles

ON FLIGHT 3570 THE CREW REPORTED AN ELECTRICAL ODOR FROM THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. VERIFIED STRONG ELECTRICAL BURNT SMELL FROM THE FLIGHT GUIDANCE CONTROLLER. REMOVED AND REPLACED THE FLIGHT GUIDANCE CONTROLLER IAW AMM II CH 22-11-01. THE OPERATIONAL CHECK WAS GOOD IAW AMM II CH 22-11-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

AFT CEILING EMERGENCY LIGHT INOP. REPLACED LAMP.

Part: CRADLE — BROKEN (CABIN) · airframe 20,071 hrs · 17,097 cycles

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

Part: UNKNOWN — ODOR (COCKPIT) · airframe 19,960 hrs · 16,997 cycles

ON FLIGHT 4302 THE CREW REPORTED AN OVERPOWERING TUNA FISH ODOR. MAINTENANCE ACCEPTED THE AIRCRAFT TO FIND AN OVERPOWERING TUNA FISH ODOR IN THE FLIGHT DECK. SPRAYED AIR FRESHENER FOR FLIGHT CONTINUOUSLY BUT AIRCRAFT STILL SMELLED LIKE A DEAD FISH BAKING IN THE SUN. TREATED COCKPIT WITH ODOR ELIMINATING SPRAY AS REQUIRED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 19,277 hrs · 16,505 cycles

DURING MAINTENANCE INSPECTION, FOUND THE AFT FLIGHT ATTENDANT FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED AFT FLIGHT ATTENDANT FLASHLIGHT ASSY, OPS CHECKED GOOD. THE AIRCRAFT RETURN TO SERVICE.

Part: BULB — INOPERATIVE (FLASHLIGHT) · airframe 19,260 hrs · 16,490 cycles

FLIGHT 4215, FOUND CABIN REAR FLASHLIGHT BULB BURNED OUT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED AFT FLT ATTENDANT FLASHLIGHT ASSEMBLY. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,034 hrs · 16,311 cycles

DURING B INSPECTION FOUND THE SMALL EMERGENCY LIGHT ON LEFT CABIN SIDE WALL BY OVERWING EXIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SMALL EMERGENCY LIGHT ON LEFT CABIN SIDEWALL BY OVERWING EXIT IAW EMB 145 AMM 33-50-13.

Part: WIRE — BROKEN (CABIN) · airframe 19,034 hrs · 16,311 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP NR 5 HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP NR 5 IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — CRACKED (CABIN) · airframe 19,034 hrs · 16,311 cycles

DURING B INSPECTION FOUND THE CABIN FLOOR EMERGENCY LIGHT STRIP HOLDERS NR 1, 2, 5, 6 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN FLOOR EMERGENCY LIGHT STRIP HOLDERS NR 1, 2, 5, 6 IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,034 hrs · 16,311 cycles

DURING B INSPECTION FOUND THE RIGHT EXTERIOR FORWARD EMERGENCY LIGHT INOPERABLE ABOVE ACM PANEL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT EXTERIOR FORWARD EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,179 hrs · 15,654 cycles

DURING MAINTENANCE INSPECTION, FOUND AFT CABIN FLASHLIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT IAW SMP. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — DEFECTIVE (CABIN PRESSURE) · airframe 17,115 hrs · 14,825 cycles

ON FLIGHT 3382 THE CREW REPORTED THAT AT 37000 FEET LOST BOTH AUTOMATIC AND MANUAL MODE PRESSURIZATION CONTROL. THE CREW DECLARED AN EMERGENCY AND LANDED AT DESTINATION WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DIGITAL CONTROLLER IAW EMB AMM 21-31-01. THE OPERATIONAL CHECK OF AUTO AND MANUAL MODES WERE GOOD PER EMB AMM 21-31-00-700-801-A AND 21-31-00-700-802-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRUNNION — CORRODED (RT MLG) · airframe 16,944 hrs · 14,695 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT MAIN LANDING GEAR FORWARD UPPER TRUNNION PITTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE TRUNNION WAS REPAIRED IAW EO-EM-57MR-503 PT C. THIS IS CONSIDERED TO BE A PERMANENT REPAIR IAW PT D OF THIS EO. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRUNNION — CORRODED (LT MLG) · airframe 16,944 hrs · 14,695 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT MAIN LANDING GEAR AFT UPPER TRUNNION PITTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE TRUNNION WAS REPAIRED IAW EO-EM-57MR-503 PT C. THIS IS CONSIDERED TO BE A PERMANENT REPAIR IAW PT D OF THIS EO. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,294 hrs · 12,701 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY EXIT SIGN/PLACARD DIRECTLY AFT OF THE RIGHT OVERWING ESCAPE HATCH TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 BATTERY AND BATTERY CHARGER. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,124 hrs · 12,561 cycles

DURING MAINTENANCE BASE VISIT FOUND THAT THE LEFT OMEGA BEAM HAS CORROSION UNDER AND AROUND CROSS-BEAM BETWEEN FRAMES 24 AND 25. REPAIRED LEFT OMEGA BEAM WITH DOUBLER IAW SRM 53-00-10 FIGURE 202 SHEET 1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,764 hrs · 12,266 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT WING EMERGENCY EXIT LIGHT (UPPER) TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT. THE OPERATIONAL CHECK WAS IN ACCORDANCE WITH EMBRAER AMM 33-50-13. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 12,860 hrs · 11,591 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FLIGHT ATTENDANT’S EMERGENCY FLASHLIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD, NO OTHER PROBLEMS FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STATIC INVERTER — ODOR · airframe 11,524 hrs · 10,380 cycles

ON FLIGHT 4439, DURING CRUISE THE CREW REPORTED THAT A 115 VAC BUS VOLT WENT OFF. THE CREW RESET PER AMO PROCEDURES AND THE EICAS MESSAGE WAS EXTINGUISHED. THE CREW DETECTED AN ELECTRICAL BURNING ODOR. THE AC POWER WAS TURNED OFF AND THE CREW REPORTED THAT THE ELECTRICAL BURNING ODOR DISSIPATED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AC STATIC INVERTER I/W EMB-145 AMM 24-20-01. OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (ELECTRICAL SYS) · airframe 11,524 hrs · 10,380 cycles

ON FLIGHT 4439 DURING CRUISE THE CREW REPORTED A 115 AC VOLT WENT OFF. THE CREW RESET AS PER AOM PROCEDURES AND THE EICAS MESSAGE WAS EXTINGUISHED. THE CREW DETECTED AN ELECTRICAL BURNING ODOR. THE AC POWER WAS TURNED OFF AND THE CREW REPORTED THAT THE ELECTRICAL BURNING SMELL DISSIPATED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE AC STATIC INVERTER IAW EMB-145 AMM 24-20-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 9,605 hrs · 8,629 cycles

ON A IMBV INSPECTION REPAIRED A DEFERRED DISCREPANCY. A GOUGE AND DENT ON FUSELAGE SKIN BETWEEN FRAMES 21 AND 22 AND BETWEEN STRINGERS 17L AND 18L. PERFORMED A CUT OUT OF THE FUSELAGE SKIN TO REMOVE THE DAMAGE. FABRICATED. A FILLER AND REPAIR DOUBLER. MARKED, DRILLED, CLEANED AND TREATED REPAIR PARTS. REPAIR DONE IAW EMB 145 SRM (SRM-145/1142 REV 40) CHAPTERS 53-21-01 AND 51-75-04. AIRCRAFT RETURNED TO SERVICE.

Part: FIRE LOOP — MALFUNCTIONED (NR 2) · airframe 78,567 hrs · 7,229 cycles

ON FLIGHT 3609, CREW REPORTED DURING TAXING OUT FOR TAKEOFF THEY GOT ENGINE NR 2 FIRE WARNING ON EICAS (ENGINE NOT RUNNING) FIRE BELL AND NR 2 FIRE HANDLE RED. COMPLIED WITH ENGINE FIRE FAILURE EPC CHECKLIST. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ENGINE NR 2 FIRE DETECTION LOOP IAW EMB 145 AMM 26-11-09. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — FAILED (ZONE 500) · airframe 4,895 hrs · 4,769 cycles

FLUID STREAMING FROM LEFT WING, RETURNED TO CHA. POST INSPECTION LEFT OUTBOARD WING WET FROM FLUID AND REVEALED FUEL STRAINED AROUND VENT VALVE AND FLAME ARRESTOR. FERRIED AIRCRAFT TO CMI FOR REPAIR. REMOVED AND REPLACED VENT VALVE IAW EMB AMM. OPERATIONAL AND LEAK CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 4,867 hrs · 4,743 cycles

LEFT OMEGA BEAM CORRODED AT FRAME 20. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN)

ORD - FLT 4289 - WHEN THE GPU WAS DISCONNECTED FROM THE AIRCRAFT, THE EMERGENCY LIGHTS CAME ON AND DRAINED THE POWER SUPPLIES. ALL FOUR BATTERY POWER SUPPLIES FOR EMERGENCY CABIN LIGHTING. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)