N693AE

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 41,904 hrs · 37,198 cycles

F012102 LH OMEGA BEAM CRACKED ON SIDE WALL AT FR29. REMOVED DAMAGE AND PERFORMED DOUBLER FILLER REPAIR IAW ETD2024-145-032096 AND EO-1-53-24-0724.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 41,904 hrs · 37,198 cycles

F012133 LH OMEGA BEAM SIDE WALL CRACKED AT FR31. PERFORMED REPAIR OF CRACK ON LH OMEGA BEAM SIDE WALL AT FR31 IAW ETD2024-145-032466 AND EO1-53-24-0728.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 41,904 hrs · 37,198 cycles

F011500 L/H OMEGA BEAM AT FR-21 HAS CRACK. PERFORMED CUT OUT, DOUBLER AND FILLER REPAIR ON L/H OMEGA BEAM AT FR-21 IAW ETD2024-145-032095 AND EO1-53-24-0723

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 41,904 hrs · 37,198 cycles

F011503 L/H OMEGA BEAM FR-22 HAS CRACK. REPAIRED THE LH OMEGA BEAM AT FR22 IAW EMB ETD2024-145-032094 AND EO1-53-24-0726

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,904 hrs · 37,198 cycles

F011176 L/H FLOOR SILL #3 HAS CORROSION AT MULTIPLES AREAS. REMOVED AND REPLACED L/H FLOOR SILL #3 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,904 hrs · 37,198 cycles

F011175 L/H OMEGA GUSSET #3 HAS CORROSION IN MULTIPLES AREAS. RAR L/H OMEGA GUSSET #3 IAW EMB-145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,904 hrs · 37,198 cycles

F011310 SERVICE DOOR LOWER CENTER FLOOR SILL HAVE CORROSION. REMOVED CORROSION AT CENTER HOLE OF THE SERVICE DOOR LOWER CENTER FLOOR SILL AND FOUND IT WITHIN ALLOWABLE LIMITS IAW EMB 145 SRM 53-21-02AD. PERFORMED PERMANENT REPAIR (INTERNAL DOUBLER REPAIR) TO FORWARD HOLE IAW EMB 145 SRM 53-21-02RE, ITEM 2, FIG 201 AND EO1-53-24-0731.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,904 hrs · 37,198 cycles

F011194 L/H OMEGA GUSSET #2 HAS CORROSION IN MULTIPLES AREAS. RAR L/H OMEGA GUSSET #2 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,904 hrs · 37,198 cycles

F011193 CENTER OMEGA BEAM GUSSET #1 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED CENTER OMEGA BEAM GUSSET #1 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,904 hrs · 37,198 cycles

F011174 CENTER OMEGA BEAM GUSSET #2 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED CENTER OMEGA BEAM GUSSET #2 IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,904 hrs · 37,198 cycles

F010824 RH CENTER FLOOR GUSSET CORRODED BETWEEN FR 35 / 39. RAR R/H CENTER FLOOR GUSSET FR 35/39 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,904 hrs · 37,198 cycles

F010813 CABIN LH CENTER FLOOR GUSSET CORRODED BETWEEN FR 45 / 53. R A R CABIN L/H FLOOR GUSSET FR 45/53 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,904 hrs · 37,198 cycles

F010835 LH #4 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED LH #4 FLOOR SUPPORT IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,904 hrs · 37,198 cycles

F010812 CABIN RH CENTER FLOOR GUSSET CORRODED BETWEEN FR 45 / 53. REMOVED AND REPLACED RH CENTER FLOOR GUSSET BETWEEN FR 45 / 53 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,904 hrs · 37,198 cycles

F010822 RH CENTER FLOOR GUSSET CORRODED BETWEEN FR 38 / 45. REMOVED AND REPLACED RH CENTER FLOOR GUSSET BETWEEN FR 38 / 45 IAW EMB 145 SRM 51-40-02

Part: FRAME — CRACKED (ZONE 100) · airframe 41,904 hrs · 37,198 cycles

CARGO FR 73 CRACKED BETWEEN STGR 16R/17R. RAR CARGO FR73 IAW EMB 145 SRM 51-40-02

Part: DOOR FRAME — CHAFED (ZONE 100) · airframe 41,904 hrs · 37,198 cycles

F010194 CARGO DOOR FRAME LOWER EDGE CHAFED. REMOVED AND REPLACED CARGO DOOR FRAME LOWER EDGE PROFILE IAW EMB 145 SRM 51-20-01 AND 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 41,904 hrs · 37,198 cycles

CARGO SHEAR CLIP AT FR66 BETWEEN STGR 6L / 7L CRACKED. REMOVED AND REPLACED SHEAR CLIP AT FR66 BETWEEN STGR 6L / 7L IAW EMB-145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 41,904 hrs · 37,198 cycles

F010566 CARGO UNDER FLOOR SHEAR CLIP AT FR 73 BETWEEN STGR 16L / 17L CRACKED. REMOVED AND REPLACED CARGO UNDER FLOOR SHEAR CLIP AT FR 73 BETWEEN STGR 16L / 17L IAW EMB145 SRM 51-40-02.

Part: RIB — CRACKED (ZONE 500) · airframe 41,904 hrs · 37,198 cycles

F009620 LH WING RIB 21 IS CRACKED AT AFT END. PERFORMED REPAIR OF LH WING RIB 21 AT AFT END IAW EMB 145 ETD2024-145-031113 AND EO1-57-24-0727

Part: RIB — CRACKED (ZONE 600) · airframe 41,904 hrs · 37,198 cycles

F009621 RH WING RIB 21 IS CRACKED AT FWD AND AFT END. PERFORMED PERMANENT REPAIR OF RH WING RIB 21 AFT END IAW EMB 145 ETD2024-145-033676 AND EO1-57-24-0730. NDT INDICATED NO CRACK ON RH WING RIB 21 FWD END

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,904 hrs · 37,198 cycles

F008493 LAVATORY BUCKET EXTERNAL SKIN AROUND WASTE VALVE CORRODED. REMOVED AND REPLACED LAVATORY BUCKET IAW EMB145 SRM 51-40-02

Part: SKIN — CRACKED (ZONE 200) · airframe 41,904 hrs · 37,198 cycles

F008527 THE EXTERNAL SKIN OF THE FUSELAGE IS CRACKED AT FRAME 75 BETWEEN STRINGERS 1L AND 2L. PERFORMED REPAIR ON EXTERNAL SKIN OF THE FUSELAGE AT FRAME 75 BETWEEN STRINGERS 1L AND 2L. IAW EMB 145 SRM53-31-01 ITEM 11 FIGURE 219 SHEET 1 AND TABLE 27 AND EO1-53-24-0729.

Part: NONE — INOPERATIVE (FA) · airframe 41,901 hrs · 37,195 cycles

FA FORWARD FLASHLIGHT INOP-C/A-SPARE FLASHLIGHT PROVIDED TO FLIGHT ATTENDANT. FLASHLIGHT DEFERRED PER EMB145 MEL 25-32. M PROCEDURES C/W

Part: NONE — BROKEN (FA) · airframe 41,624 hrs · 36,836 cycles

REAR FA EMERGENCY FLASHLIGHT CLIP BROKEN-C/A-REMOVED AND REPLACED BROKEN CLIP ON REAM FA FLASHLIGHT IAW ASTRONICS DME CMM 25-60-14.

Part: NONE — NONE · airframe 41,008 hrs · 36,137 cycles

BLEED 1 LEAK ON CLIMBOUT DECLARED EMERGENCY. REF ITEM #1 WHILE PERFORMING BLEED LEAK INSPECTION FOUND WARNING ELEMENT IN ENG 1 DISCONNECTED AND CHAFFING ON FITTING.-C/A-FOUND LOOSE CLAMPS ON PRE-COOLER #1. RESECURED CLAMPS, RAN APU FOR HOURS, GROUND RAN ENG 1 AND ENG 2, COULD NOT DUPLICATE IAW EMB 145 MM 36-00-00.RESECURD #1 FIRE LOOP CLAMPS AS REQUIRED AND REPOSITIONED FIRE LOOP TO PREVENT ANY MORE CHAFFING. PERFORMED OPERATIONAL CHECK OF ENG 1 FIRE LOOP IAW EMB-145 AMM 26-10-00. OPS CHECK GOOD

Part: NONE — NONE · airframe 40,577 hrs · 35,649 cycles

FA EMERGENCY FLASHLIGHT HOLDER BRACKET CRACKED-C/A-RAR FA FLASHLIGHT HOLDER BRACKET IAW EMB 145 CMM 25-60-14.

Part: NONE — NONE · airframe 40,026 hrs · 35,031 cycles

FA REPORTS REAR CABIN FLASHLIGHT HOLDER BROKEN.-C/A-RAR AFT CABIN FLASHLIGHT HOLDER ASSY IAW ETN-EM-33-059.

Part: COMPRESSOR — DAMAGED (NR 1 ENGINE) · airframe 39,508 hrs · 34,417 cycles

ENG 1 FAILURE ON CLIMBOUT, AFTER T/O CHECK COMPLETE, PASSING 5,500 FT LOUD BANG ENG 1 FAIL MESSAGE ON EICAS E1 FAILURE / DECLARED EMERGENCY / EQP SWAP FLT CONT. ENG #1 INSP REVIELED HEAVY DAMAGE TO COMPRESSOR, PERFORMED ENGINE REPLACEMENT OF #1 ENGINE AS PER ENVOY W/C 71-000-00 OPS CHECK AND LEAK CHECK GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 39,453 hrs · 34,362 cycles

EMERGENCY LIGHT NOT ARMED CAUTION MESSAGE AFTER TAKEOFF. RAN QRH AND DIDN?T FIX PROBLEM. C19 CRCT BRKR POPPED AND EMER LGTS LASTED 20 MIN-C/A-RAR EMERGENCY LIGHT POWER SUPPLIES IAW WC 33-700-19. FOUND SIGNIFICANT EXCEPT AS NOTED IN FOLLOW ON ITEMS, OPS CHECK GOOD. EMER LT CB C19 DOES NOT POP ANYMORE

Part: CRADLE — BROKEN (FWD FLASHLIGHT) · airframe 39,047 hrs · 33,955 cycles

FA EMETRGENCY FLASHLIGHT HOLDER BROKEN-C/A- RAR FWD FA EMERGENCY FLASHLIGHT ASSY IAW ETN-EM-33-059

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,795 hrs · 33,710 cycles

MAIN DOOR HINGE COVER EMERGENCY LIGHT INOPERABLE. C/A: R & R MAIN DOOR HINGE COVER EMERGENCY LIGHT, IAW EMB 145 AMM 33-50-10 2J(3) AND 3I(3). OPERATIONS CHECK GOOD.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 38,642 hrs · 33,536 cycles

COCKPIT EMERGENCY FLASH LIGHT MISSING ABOVE PBE. C/A: FLIGHT CREW PLACARDED, PER MEL2553 AUTH120078-C MOC 135181.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,426 hrs · 33,316 cycles

MAIN DOOR EMERGENCY LIGHT INOPERABLE. C/A: R & R MAIN DOOR EXTERNAL EMERGENCY LIGHT, IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. OPERATIONS CHECK GOOD.

Part: HINGE FITTING — DAMAGED (RUDDER) · airframe 37,784 hrs · 32,629 cycles

RUDDER 1 UPPER HINGE POINT FOR RUDDER 2 BALL BEARING REQUIRES REPLACEMENT DUE TO BOLT FAILING DIMENSIONAL CHECK.-C/A-REMOVED AND REPLACED RUDDER 1 UPPER HINGE FITTING IAW EMB SRM 51-40-02.

Part: BUSHING — MIGRATED (LT AIERON) · airframe 37,784 hrs · 32,629 cycles

LH AILERON DAMPER FITTING HAS MIGRATING HAT BUSHINGS-C/A-LH AILERON DAMPER FITTING REPLACEMENT IAW EO-EM-27MR-112.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 37,784 hrs · 32,629 cycles

CROSSBEAM JUST BEHIND NOSE UPLOCK BOX IS CRACKED.-C/A-INSTALLED NEW CROSSBEAM BEHIND NOSEE UPLOCK BOX IAW SRM 51-40-02.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 37,784 hrs · 32,629 cycles

CARGO DOOR SKIN HAS APPROXIMATELY A 1" CRACK ON UPPER AFT SIDE OF HANDLE CUT OUT.-C/A-COMPLIED WITH REPAIR IAW ERS-EM-52MR-1064.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 37,784 hrs · 32,629 cycles

LEFT AFT UPPER FUSELAGE SKIN PANEL HAS NUMEROUS CRACKS AROUND RIVETS.-C/A-INSTALLED REPAIR BUSHINGS 4EA ON L/H AFT FUSELAGE SKIN ON FRAME 77 AND RESTORED PAINT FINISH IAW SPM 53-32-01 ENTERED INTO DT EM-53-1281 AND ACL 6930042. INSTALLED REPAIR BUSHINGS 2EA ON L/H AFT FUSELAGE SKIN ON FRAME 78 AND RESTORED PAINT FINISH IAW SRM 53-32-01 ENTERED INTO DET EM-53-1281 AND ADL 6930042. INSTALLED REPAIR BUSHINGS 3EA ON L/H AFT FUSELAGE SKIN ON FRAME 79 AND RESTORED PAINT FINISH IAW SRM 53-32-01 ENTERED INT DET EM 53-1281 AND ADI 6930042.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 37,784 hrs · 32,629 cycles

RIGHT AFT UPPER FUSELAGE SKIN PANEL HAS NUMEROUS CRACKS AROUND RIVETS.-C/A-INSTALLED REPAIR BUSHING ON RH AFT FUSELAGE FRAME 77 AND RESTORED PAINT FINISH IAW SRM 53-32-01. ENTERED INTO DET-EM-53-1282 AND ADI#6930041. INSTALLED REPAIR BUSHINGS 3EA ON R/H AFT FUSELAGE SKIN ON FRAME 78 AND 79 AND RESTORED PAINT FINISH IAW SRM 53-32-01 AND ENTERED INTO DET EM-53-1282 AND ADL 6930041

Part: RIB — CRACKED (FUSELAGE) · airframe 37,784 hrs · 32,629 cycles

RIGHT SIDE OF THE UPPER FUSELAGE WINDSHIELD CUTOUT IS CRACKED BY THE NUT PLATE.-C/A-REPAIRED RH SIDE WHINSHIELD CUT-OUT GRAB HANDLE IAW ERS-EM-5300-4064.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 37,784 hrs · 32,629 cycles

FRAME 60 HAS A TOOLING MARK BETWEEN STRINGERS 4L-5L.-C/A-REPAIRED FRAME 60, BETWEEN STRS 4L-5L IAW SRM 53-00-04 ENTERED INTO DET-EM-53-972.

Part: ANGLE — CRACKED (LT WING) · airframe 37,784 hrs · 32,629 cycles

LEFT WING UPPER SURFACE "L" ANGLE AT WING ROOT IS CRACKED, ANGLE SUPPORT FOR 193EL.-C/A-REMOVED AND REPLACED LT WING UPPER SURFACE L ANGLE AT WING ROOT IAW SRM 51-40-02. REF E778729 FOR LEAK CHECK.

Part: ANGLE — CRACKED (RT WING) · airframe 37,784 hrs · 32,629 cycles

RIGHT WING FORWARD UPPER "L" ANGLE AT WING ROOT IS CRACKED, ANGLE SUPPORT FOR PANEL 194ER.-C/A-REMOVED AND REPLACED RT WING UPPER SURFACE WING L ANGLE AT WING ROOT IAW SRM 51-40-02. REF NRTC E778731 FOR LEAK CHECK.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,784 hrs · 32,629 cycles

CARGO DOOR CUTOUT SILL IS CORRODED.-C/A-REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02. RESTORED SURFACE PROTECTION IAW CPM 51-21-06.

Part: SUPPORT BRACKET — CRACKED (CARGO BAY) · airframe 37,784 hrs · 32,629 cycles

BAGGAGE DOOR LIFTING/LOWERING MECH AFT LOWER SUPPORT BRACKET IS CRACKED.( APPROX 1" LONG) -C/A-REPLACED BAGGAGE DOOR LIFTING/LOWERING MECH AFT LOWER SUPPORT BRACKET IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,784 hrs · 32,629 cycles

CENTER SERVICE DOOR SILL IS CORRODED-C/A-COMPLETED INSTALLATION OF SERVICE DOOR SILL IAW SRM 51-40-02, RESTORED SURFACE PROTECTION IAW CPM 51-21-06.

Part: CHARGER — MALFUNCTIONED (CABIN) · airframe 37,784 hrs · 32,629 cycles

EMERGENCY LIGHTS FOR BATTERY PACK #3 CAME ON UN COMMANDED.-C/A-COMPLETE:REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY #3 IAW EMB AMM 33-50-04, OPS CHECK GOOD I.A.W. EMB145 A.M.M. 33-50-00-700-801-A.

Part: WIRE — BROKEN (CABIN) · airframe 37,784 hrs · 32,629 cycles

EMERGENCY FLOOR LIGHT STRIP #4 HAS A BROKEN WIRE.-C/A-REMOVED AND REPLACED #4 PROX LIGHT STRIP IAW AMM 33-50-12. OPS CK GOOD

Part: WIRE — BROKEN (LIGHT STRIP) · airframe 37,784 hrs · 32,629 cycles

EMERGENCY LIGHT STRIPS #2 AND #3 HAVE BROKEN WIRES.-C/A-REMOVED AND REPLACED THE EMERGENCY LIGHT STRIPS #2 AND #3. IAW AMM 33-50-12.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,762 hrs · 32,614 cycles

DURING PS-2 CHECK, FOUND EMERGENCY FLOOR LIGHTS SEGMENTS 6 THRU 8 INOP-C/A-REPLACED BATTERY, CHARGER AND INVERTER IAW 33-50-04. OPS CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 83000; INVERTER P/N 7824-1

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,550 hrs · 32,416 cycles

LH OVER WING EMERGENCY LIGHT INOP-C/A-RAR LH OVER WING EEL POWER SUPPLY AND EMERGENCY EXIT SIGN LH OVER WING IAW AMM 33-50-11 OPS CHECK GOOD

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,354 hrs · 32,223 cycles

FOUND OVERWING EMERGENCY LIGHTS INOP.-C/A-REMOVED AND REPLACED #4 EMERGENCY LIGHTING POWER SUPPLY AND BATTERY IAW WORKCARD 33-700-19, OPS CHK GOOD. WORKCARD 33-700-17. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 82530

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,278 hrs · 32,169 cycles

LH FWD OVERWING EMERGENCY LIGHT INOP.-C/A-RELAMPED LH FWD OVERWING EMERGENCY LIGHT IAW EMB-145 AMM 33-50-07. TESTED SATISFACTORY.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 37,004 hrs · 31,977 cycles

OVERHEAD AISLE LIGHT NR 4 INOPERATIVE. -REMOVED AND REPLACED FUSE ON BATTERY CHARGER #4 IAW CMM 25-60-03. OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,805 hrs · 31,780 cycles

DURING PS1 FOUND LT FORWARD EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT LAMP IAW AMM-33-50-10. OPS CHECK GOOD.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 36,466 hrs · 31,537 cycles

LT OVERWING EMER EXIT MARKER INOP. C/A-RESET LT OVERWING EMER EXIT MARKER CONNECTORS SP9126 AND SP9127 IAW WM 33-50-50. OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 35,800 hrs · 31,010 cycles

FA REPORTED THAT THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN- LATCHES WERE STICKING. C/A-C/W MAIN CABIN DOOR FRAME ROLLERS LUBE IAW AMM 53-21-02. FOUND SATISFACTORY AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,976 hrs · 30,261 cycles

E1 FIRE DET FAIL MSG INTERMITTENT DURING CLIMB. PERFORMED OPERATIONAL TEST OF NR 1 ENG FIRE DET GOOD NO MESSAGE NOTED IAW AMM 26-10-00.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 34,482 hrs · 29,780 cycles

DURING PS-1 CHECK FOUND EMERGENCY OVERWING DOOR LT EXIT SIGN INOP, INSIDE CABIN. REMOVED AND REPLACED LT EMERGENCY DOOR EXIT SIGN LIGHT ASSY IAW AMM 33-50-14 OPS CHECK GOOD.

Part: ESCAPE ROPE — UNSERVICEABLE (COCKPIT) · airframe 34,443 hrs · 29,749 cycles

PILOT ESCAPE ROPE UNTIED-C/A-REMOVED AND REPLACED PILOT ESCAPE ROPE IAW AMM 25-60-07.

Part: CONTROLLER — FAILED (WINDOW HEAT) · airframe 34,227 hrs · 29,534 cycles

WINDSHIELD 2 HEAT FAIL EICAS MESSAGE WITH SLIGHT ELECTRICAL BURNING SMELL, DESELECTED W/S 2 HEAT AND DID NOT RESET. REMOVED AND REPLACED NR 2 W/S TEMPERATURE CONTROLLER IAW AMM-30-42-01. OPS CHECK GOOD. BURNING SMELL ASSOCIATED WITH PART REMOVED.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 34,077 hrs · 29,391 cycles

LEFT EMERGENCY EXIT ROW UPPER EXIT IDENTIFIER SIGN INOPERATIVE. FOUND THE SPLICE CONNECTOR LOOSE. CONNECTED THE CONNECTOR IAW SWPM.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,391 hrs · 28,660 cycles

SECTION 6, 7, 8 EMERGENCY LIGHTS INOPERATIVE. TROUBLE SHOT IAW FIM 33-50-00-810-804-A. REMOVED AND REPLACED NR 6 INVERTER IAW AMM 33-50-11-000-801-A, AND 33-50-11-400-801-A, OPS CHECKED GOOD.

Part: ROLLER — NOT REPORTED (PAX DOOR) · airframe 33,368 hrs · 28,633 cycles

DIFFICULT TO OPEN MAIN CABIN DOOR. SERVICED MAIN PAX DOOR FRAME ROLLERS IAW MM 53-21-02.

Part: SOLENOID — FAILED (PSU) · airframe 33,084 hrs · 28,392 cycles

FLIGHT ATTENDANT REPORTED A STRANGE ODOR BEHIND THE EXIT ROW IN THE CABIN. THE LIGHTS CAUSED A SPARK WHEN TURNED ON. INSPECTED WIRING FOR SIGNS OF DAMAGE, FOUND OXYGEN DOOR RELEASE SOLINOID SMELLED OF BURNED ELECTRICAL. REMOVED AND REPACED THE PSU PANEL AT SEAT 14A IAW AMM 25-22-05, PERFORMED AN OPS CHECK OF CABIN SIDEWALL LIGHT LIGHTS, OPS CHECKED GOOD IAW AMM 33-21-00.

Part: CONNECTOR — LOOSE (MLG) · airframe 32,726 hrs · 28,071 cycles

LG/AIR GROUND FAIL. INTERROGATED CMC, LG/AIR / GND LGEU FAIL MESSAGE ON CMC. PERFORMED FAULT ISOLATION IAW FIM 32-63-00. DISCONNECTED LGEU CONNECTORS. FOUND BACKSHELL LOOSE ON LEFT CONNECTOR. SECURED THE BACKSHELL, RECONNECTED CONNECTORS IAW AMM 32-32-01. OPS CHECKED GOOD

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,687 hrs · 28,045 cycles

CORROSION IN STRINGER 21R ACROSS CIRCUMFRENTIAL SPLICE BETWEEN FRAME 60 AND 61. -C/A-REMOVED AND REPLACED STRINGER 21R SPLICE ACROSS CIRCUMFRENTIAL SKIN SPLICE AT FRAME 60-61 IAW EMB 145 SRM 51-40-02. AND RESTORED SURFACE PROTECTION IAW CPM 51-21-04 AND 51-21-05.

Part: FLOOR SUPPORT — CORRODED (FRAME 27) · corrosion level 2 · airframe 32,687 hrs · 28,045 cycles

CORROSION ON THE FLOOR SUPPORT LT SIDE OF CENTER OMEGA BEAM AT FRAME 27 AT SCREW HOLE. REMOVED CORROSION, CUTOUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER , NO DEFECTS NOTED DURING NDT. IAW SRM 53-22-10, HFEC IAW NDTM 51-00-00-916-801-A00 AND DYE PEN IAW NDTM SECTION D.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 32,687 hrs · 28,045 cycles

LAST EMERGENCY LIGHT LEAD DAMAGED. REPAIRED THE WIRING CONNECTOR IAW SWPM 20-21-00 OPS CHECKED GOOD IAW AMM 33-50-00

Part: DOUBLER — CORRODED (FRAME 59) · airframe 32,686 hrs · 28,044 cycles

CORROSION IN REPAIR DOUBLER I/B SIDE OF L/H OMEGA AT FRAME 59 CROSS MEMBER-C/A-REMOVED CORRODED DOUBLER, PERFORMED HFEC INSPECTION, NO DEFECTS NOTED. FABRICATED AND INSTALLED NEW DOUBLER IAW NCR -EM-53-046, EMB 145 SRM 53-24-10, NTM 51-00-00-916-801-A00 AND ETD 2017-145-10897

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,686 hrs · 28,044 cycles

CORROSION ON LT OMEGA AT FRAME 60 AROUND NUTPLATE. BLENDED CORROSION AND DETERMINED TO BE OUT OF LIMITS, CUT OUT DAMAGE, PERFORMED NDT, FABRICATED AND INSTALLED REPAIR DOUBLER AND RESTORED PROTECTIVE COATING IAW SRM 51-10-03, 53-24-10,CPM 51-21-04, 51-21-05 AND NIM 51-00-00-916-801-A00.

Part: SHEAR TIE — CRACKED (FRAME 27) · airframe 32,686 hrs · 28,044 cycles

CRACK IN SHEAR CLIP AT FRAME 27 BETWEEN STRINGERS 15 R -16 R-C/A-REMOVED AND REPLACED SHEAR CLIP AT FRAME 27 BETWEEN STRINGERS 15R AND 16 R APPLIED PRIMER AND TOP COAT IAW EMB 245 SRM 51-40-02 AND CPM 51-21-05 , 51-21-06

Part: SHEAR TIE — CRACKED (FRAME 26) · airframe 32,686 hrs · 28,044 cycles

CRACK IN THE SHEAR TIE AT FRAME 26, BETWEEN STRINGERS 16 AND 17R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 32,686 hrs · 28,044 cycles

CRACK IN SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 16 R -17 R-C/A-REMOVED AND REPLCED SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 16 R AND 17 R IAW EMB 145 SRM 51-40-02

Part: FRAME — GOUGED (FUSELAGE) · airframe 32,686 hrs · 28,044 cycles

GOUGE IN FRAME 60 BETWEEN STRINGER 4L AND 5L. BLENDED GOUGE, PERFORMED NDT, FABRICATED AND INSTALLED REPAIR DOUBLER AND RESTORED SURFACE PROTECTION IAW NCR EM-53-045 AND ETD 2017-145-107262.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,686 hrs · 28,044 cycles

CRACK IN SHEAR CLIP AT FRAME 25 BETWEEN STRINGERS 15 R AND 16 R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 35 AND BETWEEN STRINGERS 15 R AND 16 R IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRAME 26) · airframe 32,686 hrs · 28,044 cycles

CRACK IN SHEAR CLIP AT FRAME 26 BETWEEN STRINGER 15L AND 16L-C/A-REMOVED AND REPLACED SHEAR CLIP AT FRAME 26 BETWEEN STRINGERS 15-16 L IAW EMB 145 SRM 51-40-02

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 32,686 hrs · 28,044 cycles

CRACK IN SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 15 R -16 R-C/A-REMOVED AND REPLCED SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 15 R AND 16 R IAW EMB 145 SRM 51-40-02

Part: STRINGER — CRACKED (FUSELAGE) · airframe 32,686 hrs · 28,044 cycles

CRACK IN STRINGER AT FRAME 20 STRINGER 3L. REMOVED AND REPLACED STRINGER 3L AT FRAME 20 IAW SRM 51-40-02 AND TOPCOATED FASTENERS, EXTERIOR AND INTERIOR IAW CPM 51-21-06.

Part: SHEAR TIE — CRACKED (FRAME 26) · airframe 32,686 hrs · 28,044 cycles

CRACK IN SHEAR CLIP AT FRAME 26 BETWEEN STRINGERS 15 R -16 R-C/A-REMOVED AND REPLCED SHEAR CLIP AT FRAME 26 BETWEEN STRINGERS 15 R AND 16 R IAW EMB 145 SRM 51-40-02

Part: WEB — CRACKED (NLG UPLOCK) · airframe 32,686 hrs · 28,044 cycles

NLG UPLOCK BOX CRACKED ON BOTH SIDES. REMOVED AND REPLACED NLG UP LOCK BOX WEBS IAW SRM 51-40-02, PERFORMED LEAK CHECKS AND GEAR SWINGS IAW AMM 32-30-00. NO DEFECTS NOTED

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,567 hrs · 27,938 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-50-05-000-801-A, AND 33-50-05-400-801-A. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,108 hrs · 27,489 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE IAW PS-2 INSPECTION. R & R LAMP ON MAIN DOOR EXTERNAL EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 31,262 hrs · 26,765 cycles

INTERIOR EMERGENCY LIGHTS, SERVICE DOOR EXTERIOR LIGHT, AND GALLEY AFT BULKHEAD EMERGENCY LIGHT WILL NOT ILLUMINATE. FOUND A DEFECTIVE SERVICE DOOR EXTERNAL EMERGENCY LIGHT ASSEMBLY. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,215 hrs · 26,723 cycles

NR 2 AND 3 FLOOR EMERGENCY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED BATTERY AND CHARGER ASSEMBLY IAW 33-700-19. OPS CHECKED GOOD IAW 33-700-17. NO DEFECTS FOUND.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,117 hrs · 26,637 cycles

FLOOR EMERGENCY LIGHT STRIPS NR 2 AND 3 INOPERATIVE. REMOVED AND REPLACED THE THE CHARGER ASSY AND BATTERY PACK.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 31,097 hrs · 26,615 cycles

EMERGENCY LIGHTS FOR SERVCIE DOOR, SEAT 3B, EXIT SIGN, AND FLOOR ROW 3 TO 7 INOPERATIVE. R & R THE NR 2 EMERGENCY LIGHT BATTERY AND CHARGER IAW W/C 33-700-19, OPS CHECKED GOOD.

Part: WINDOW — OUT OF POSITION (COCKPIT) · airframe 31,074 hrs · 26,598 cycles

CA DV WINDOW TOO FAR FORWARD OF SECURE POSITION. YELLOW TAB SLIGHTLY SHOWING RETURN TO DEPARTURE. PRESURIZED ACFT AND FOUND NO LEAKS IAW AMM 21-31-00. OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,012 hrs · 26,540 cycles

NR 2 AND 3 EMERGENCY LIGHTS AND AFT GALLEY EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY AND CHARGER IAW W/C 33-700-19. OPS CHECKED GOOD IAW W/C 33-700-17.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 30,897 hrs · 26,462 cycles

FOUND NR 4 AND 5 EMERGENCY LIGHT STRIPS INOPERATIVE. REMOVED AND REPLACED NR 3 BATTERY AND CHARGER IAW W/C 33-700-19. OPS CHECKED GOOD, NO FURTHER DEFECTS FOUND.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 30,897 hrs · 26,462 cycles

FOUND NR 2 AND 3 EMERGENCY LIGHT STRIPS INOPERATIVE. REMOVED AND REPLACED DC/AC INVERTER IAW AMM 33-50-11. REMOVED AND REPLACED THE NR 2 BATTERY PACK AND HOLDER ASSY IAW W/C 33-700-19. OPS CHECEDK GOOD. NO FURTHER DEFECTS FOUND.

Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 30,762 hrs · 26,348 cycles

SPOILER FAIL MESSAGES PRESENTED ON ICAS AFTER TAKEOFF MESSAGE EXTINGUISHED AFTER LANDING GEAR EXTENSION. TROUBLESHOOTED PER FIM 27-63-00. REMOVED AND REPLACED RELAY K0030 AND K0031 IAW AMM 20-13-02. NO FIX. REMOVED AND REPLACED SPOILER CONTROL UNIT IAW AMM 27-63-02. OPS CHECK SPOILER IAW AMM 27-63-01. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,736 hrs · 26,324 cycles

EXTERIOR LEFT LOWER EMERGENCY LIGHT ASSEMBLY INOPERATIVE. REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW 33-50-10. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,736 hrs · 26,324 cycles

EMERGENCY LIGHT STRIP 2 AND 3 AS WELL AS EXIT SIGN ON BACK OF GALLEY WILL NOT ILLUMINATE. REMOVED AND REPLACED THE NR 2 BATTERY PACK AND POWER SUPPLY IAW AMM 33-50-04 AND CHANGED THE NR 2 AND 3 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: BATTERY — FAILED (FLASHLIGHT) · airframe 30,722 hrs · 26,311 cycles

WAITING FOR TAKEOFF A SUDDEN AND STRONG NOXIOUS ODOR AS NOTED BY 3 CREW MEMBERS AS WELL AS MULTIPLE PASSENGERS CREW (3) REPORTED NOT FEELING WELL AS RESULT. INSPECTED AC FOR SOURCE OF ODOR, REMOVED AND REPLACED FORWARD FA FLASHLIGHT BATTERY IAW CMM 25-60-11. OPS CHECK GOOD. NO SMELL NOTICED.

Part: ACM — FAILED (AC BAY) · airframe 30,010 hrs · 25,616 cycles

SMOKE IN CABIN DURING DESCENT THROUGH FL200 WENT AWAY WITH PACK SHUTOFF. R & R RT ACM IAW AMM 21-51-03, OPS GOOD, NO SMOKE NOTED, NO LEAKS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,668 hrs · 25,302 cycles

OVERHEAD MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-06. OPS CHECKED GOOD

Part: TORQUE LINK — NOT REPORTED (NLG) · airframe 29,177 hrs · 24,847 cycles

NOSE WHEEL HAS BAD SHIMMY AT HIGH SPEED. SERVICED NOSE GEAR TORQUE LINKS IAW 32-34-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,150 hrs · 24,828 cycles

FLOOR EMER LIGHTS INOPERATIVE FROM ROW 3A - 7A. TROUBLE SHOT & FOUND SERVICE DOOR EXTERNAL EMER LIGHT SHORTED. R & R SERVICE DOOR EXTERNAL EMER LIGHT IAW EMB 145 AMM 33-50-10-000-801 & 33-50-10-400-801. ALSO FOUND NR 2 BATTERY POWER SUPPLY BAD R & R NR 2 BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04-000-801 & 33-50-04-400-801. OPERATION CHECK GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 17641.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 28,850 hrs · 24,558 cycles

EMERGENCY LIGHT STRIP INOPERATIVE AT SEAT 4A. R & R THE NR 2 BATTERY & POWER SUPPLY IAW AMMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,816 hrs · 24,522 cycles

NUMBER 2 & 3 EMER LIGHT FLOOR STRIPS INOPERATIVE. R & R THE NR 2 EMER BATTERY PACK & THE POWER SUPPLY IAW AMM 33-50-04-000-801-A & 33-50-04-400-801-A. COMPLIED WITH OPERATIONAL CHECK IAW AMM 33-50-00-700-801-A. OPERATIONS CHECKED GOOD. END BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 24504.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,473 hrs · 24,208 cycles

GALLEY CEILING PANEL EMER LAMP INOPERATIVE. R & R GALLEY CEILING PANEL EMER LIGHT LAMP IAW AMM 33-26-05-000-802-A & 33-26-05-400-802-A.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 28,266 hrs · 24,017 cycles

RIGHT WING LOWER LATERAL FAIRING ATTACHMENT ANGLE, 3RD FROM THE AFT IS CRACKED. REPLACED ANGLE IAW SRM 51-40-02.

Part: HINGE FITTING — GOUGED (RUDDER) · airframe 28,266 hrs · 24,017 cycles

RUDDER 2 TO RUDDER 1, UPPER HINGE FITTING, UPPER LUG IS GOUGED. INSTALLED NEW RUDDER 2 UPPER HINGE FITTING IAW SRM 55-40-02 & ETN EM-55-070.

Part: DOOR FRAME — CRACKED (ACCESS DOOR) · airframe 28,266 hrs · 24,017 cycles

ACCESS DOOR 123BL HAS A 1 INCH CRACK ON THE FRAME UNDER THE IPI PIN BRACKET. R & R FRAME UNDER ACCESS DOOR 123BL, PIP PIN BRACKET IAW SRM 51-10-02.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 28,266 hrs · 24,017 cycles

BAGGAGE DOOR FWD TORSION SPRING BRACKET IS CRACKED. R & R BAGGAGE DOOR FWD TORSION SPRING BRACKET IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,266 hrs · 24,017 cycles

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

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 28,266 hrs · 24,017 cycles

WHILE PERFORMING EO EM53AD-1883 PART B, FOUND ONE EACH .500 INCH CRACK ON THE APU FIREWALL AROUND THE J0274 ELEC CONNECTOR. COMPLIED WITH EO EM-53AD-1883 PART B.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,266 hrs · 24,017 cycles

LEFT SIDE OVERWING FAIRING, UPPER SUPPORT IS CRACKED AFT OF FRAME 41 LOCATION. REPAIRED IAW SRM 53-2312.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,266 hrs · 24,017 cycles

RIGHT OMEGA BEAM OTBD LT ANGLE SUPPORT IS CRACKED, BETWEEN FRAMES 47 & 48. REPAIRED IAW SRM 53-23-02. CHANNEL PN 140-04213-607.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,266 hrs · 24,017 cycles

RIGHT SIDE OVERWING FAIRING, UPPER SUPPORT IS CRACKED AFT OF FRAME 41 LOCATION. COMPLIED WITH REPAIR AT AFT OF FRAME 41 RT SIDE IAW SRM 53-23-12.

Part: FITTING — CRACKED (FUSELAGE) · airframe 28,266 hrs · 24,017 cycles

FRAME CLIP CRACKED 1/2 INCH AT FRAME 73, STRINGER 8L. REPLACED CLIP IAW SRM 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,266 hrs · 24,017 cycles

LEFT OMEGA BEAM LT ANGLE IS CRACKED, BETWEEN FRAMES 47 & 48. COMPLETED REPAIR OF LT OMEGA BEAM LT ANGLE IAW SRM 53-23-02. CHANNEL PN 140-04213-611, SHEAR CLIP PN 140-04214-605 & 140-04214-611.

Part: FITTING — CRACKED (FUSELAGE) · airframe 28,266 hrs · 24,017 cycles

FRAME CLIP CRACKED 1/2 INCH AT FRAME 67, STRINGER 6R. R & R CLIP AT FRAME 67, STRINGER 6R IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 28,266 hrs · 24,017 cycles

FRAME CLIP CRACKED 1 INCH AT FRAME 68, STRINGER 6L. R & R SHEAR CLIP AT FRAME 68, STRINGER 6L IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,266 hrs · 24,017 cycles

RIGHT OMEGA BEAM INBD LT ANGLE SUPPORT IS CRACKED, BETWEEN FRAMES 47 & 48. REPAIRED IAW SRM 53-23-02. SHEAR CLIP PN 140-04213-609.

Part: FITTING — CRACKED (FUSELAGE) · airframe 28,266 hrs · 24,017 cycles

LEFT STRINGER 7, CLIP AT LT FRAME 80 IS CRACKED IN THE AFT UNPRESSURIZED TAIL COMPARTMENT. R & R SHEAR CLIP IAW SRM 51-40-02 & 51-20-03.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 28,266 hrs · 24,017 cycles

RIGHT STRINGER 7 CLIP AT RT FRAME 80 IS CRACKED IN THE AFT UNPRESSURIZED TAIL COMPARTMENT. R & R RT STRINGER 7 CLIP IAW SRM 51-40-02.

Part: ACM — FAILED (AC BAY) · airframe 27,426 hrs · 23,180 cycles

AT CRUISE AT FL 250, WITH POWER IN CLIMB THRUST GOT SMOKE IN COCKPIT & CABIN. SMOKE DISSIPATED AFTER 2 MINUTES. R & R NR 2 ACM IAW AMM 21-51-03. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,341 hrs · 23,114 cycles

FLOOR EMER LIGHT STRIP ON ROW 7 - 9 INOPERATIVE. R & R FLOOR EMER LIGHT STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,892 hrs · 22,718 cycles

FWD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-6011. OPERATIONS CHECKED GOOD.

Part: HOLDER — DEFECTIVE (FLASHLIGHT) · airframe 26,631 hrs · 22,494 cycles

FLIGHT ATTENDANT'S FLASHLIGHT HOLDER IS FALLING OFF THE WALL. R & R FWD FLASHLIGHT HOLDER IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,600 hrs · 22,467 cycles

SEVERAL FWD CABIN CEILING EMER LIGHTS ARE INOPERATIVE. REPLACED NR 1 EMER LIGHT BATTERY POWER SUPPLY WITH BATTERY IAW 33-50-04. EMER LIGHTS OPERATIONS CHECK GOOD IAW 33-50-00. EMER LIGHTING BATTERY PN 2013-1A SN 104872.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,450 hrs · 22,307 cycles

COCKPIT STEP & FLIGHT ATTENDANT SEAT EMER EXIT IDENTIFIER INOPERATIVE. R & R NR 1 BATTERY PACK IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — SMOKE · airframe 26,270 hrs · 22,122 cycles

SMOKE IN COCKPIT OR CABIN AFTER PACK NR 2 SELECTED ON. USING APU PERFORMED OPERATIONS CHECK OF NR 2 PACK IAW AMM 21-51-00. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED AT THIS TIME. COMPLIED WITH FIM TASK 21-20-00, NO DEFECTS NOTED.

Part: FLASHLIGHT — UNSECURE (COCKPIT) · airframe 26,262 hrs · 22,116 cycles

COCKPIT FLASHLIGHT IS FALLING FROM ITS HOLDER. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.

Part: ANTENNA — FAILED (RADIO ALTIMETER) · airframe 26,081 hrs · 21,990 cycles

DURING CLIMB, RECEIVED TOO LOW TERRAIN AURAL WARNINGS FOLLOWED BY RADAR ALTIMETER FAIL GPWS ON OPERATIONAL & WINDSHEAR INOPERATIVE. REMOVED AND REPLACED RADIO ALTIMETER ANTENNAS IAW AMM 34-31-02. OPS CHECKED GOOD.

Part: FLASHLIGHT ASSY — INOPERATIVE (AFT CABIN) · airframe 25,870 hrs · 21,760 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT & CRADLE ASSEMBLY IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: PRINTER — FAILED (COCKPIT) · airframe 25,868 hrs · 21,759 cycles

PRINTER STARTED SMOKING & STOPPED PRINTING. R & R ACARS PRINTER IAW AMM 23-22-02. OPS CHECKED GOOD IAW AMM 23-22-02-700-801-A.

Part: CONNECTOR — UNSECURE (EXTERIOR LIGHT) · airframe 25,286 hrs · 21,245 cycles

BOTH SIDES AFT OVERWING EXTERIOR EMER LIGHTS INOPERATIVE. SECURED WIRE CONNECTION LT OVERWING EXTERIOR EMER LIGHT IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,172 hrs · 21,146 cycles

LEFT & RIGHT EXTERIOR OVERWING EMER LIGHTS INOPERATIVE. R & R NR 4 BATTERY CHARGER & BATTERY ASSEMBLY IAW WC 33-700-19. OPERATIONS CHECKED GOOD IAW WC 33-700-17. CHARGER ASSEMBLY BATTERY PN BA5-0933-901 & SN C02382.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 25,097 hrs · 21,064 cycles

LEFT EXTERIOR OVERWING EMER LAMP INOPERATIVE. R & R NR 4 EPSU IAW WC 33-700-19. OPERATIONS CHECKED GOOD AT THIS TIME. END BATTERY CHARGER ASSEMBLY PN 11-0049, SN 19000.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,062 hrs · 21,026 cycles

LT & RT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 BATTERY CHARGER IAW AMM 33-50-04, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,038 hrs · 21,000 cycles

LT & RT OVERWING EMER LIGHTS INOPERATIVE. R & R NR 4 EMER LIGHT BATTERY CHARGER & BATTERY IAW WC 33-700-19. OPERATIONS CHECKED GOOD. CHARGER ASSEMBLY BATTERY PN BA5-0933-901 SN C01194.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,011 hrs · 20,976 cycles

RIGHT AFT OVERWING EMERGENCY LIGHT IS INOPERATIVE. R & R AFT BATTERY ASSEMBLY IAW AMM 33-50-04. PERFORMED OPERATIONS CHECK IAW AMM 33-50-00 OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 24,887 hrs · 20,883 cycles

LT & RT OVER THE WING EMERGENCY LIGHT INOPERATIVE. R & R NR 4 EMERGENCY LIGHT POWER SUPPLY ASSEMBLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,852 hrs · 20,847 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R NR 4 EMER BATTERY & CHARGER IAW WC 33-700-19. OPERATIONS CHECK OF RT & LT EMER LIGHTS GOOD AT THIS TIME.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,807 hrs · 20,801 cycles

BOTH AFT WING EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 EMERGENCY BATTERY & CHARGER ASSEMBLY IAW WC 33-700-19. OPERATIONS CHECKED GOOD IAW WC 33-700-17.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,647 hrs · 20,679 cycles

OVERWING EMERGENCY LIGHTS ON LT & RT WINGS ARE INOPERATIVE. R & R BATTERY CHARGER NR 4 IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,590 hrs · 20,633 cycles

LT & RT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 CHARGER & BATTERY ASSEMBLY IAW WC 33-700-19 & OPERATIONS CHECK PERFORMED USING WC 33-700-17.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,560 hrs · 20,604 cycles

BOTH OVER THE WING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY CHARGER & BATTERY IAW WC 33-700-19. OPERATIONS CHECKED PERFORMED IAW WC 33-700-17. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,531 hrs · 20,576 cycles

LT & RT OVERWING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 EPSU BATTERY & CHARGER ASSEMBLY IAW AMM 33-50-04, OPERATIONS CHECKED GOOD IAW AE WC 33-700-17.

Part: HOLDER — DEFECTIVE (FLASHLIGHT) · airframe 24,503 hrs · 20,557 cycles

R & R FLASHLIGHT HOLDER OVER FLIGHT ATTENDANT'S SEAT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 24,499 hrs · 20,552 cycles

BOTH LT & RT WING UPPER EMERGENCY LIGHTS ARE INOPERABLE. R & R NR 4 EMERGENCY BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,392 hrs · 20,479 cycles

RT EXTERIOR EMERGENCY LIGHT OVER WING INOPERATIVE. R & R NR 4 EMERGENCY BATTERY PACK & CHARGER IAW AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,392 hrs · 20,479 cycles

LT EXTERIOR EMERGENCY LIGHT OVERWING INOPERATIVE. R & R BATTERY PACK & CHARGER IN POSITION NR 4 IAW AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,328 hrs · 20,430 cycles

NUMBER 4 EPSU INOPERATIVE. R & R NR 4 EPSU BATTERY & CHARGER IAW WC 33-700-19, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: ACCELEROMETER — FAILED (NR 2 ENGINE) · airframe 24,082 hrs · 20,244 cycles

DURING CLIMB THROUGH FL260 TGE NR 1 ENG BEGAN TO SURGE. CREW TURNED THEN ENG IGNITION ON & THE N1 SURGING WENT AWAY. CREW DECLARED AN EMERGENCY & DIVERTED TO IND. DURING MAINTENANCE INSPECTION ON FLIGHT 3745 FOUND ALT TO 1 AT SJT RIGHT HP WENT TO THE BOTTOM OF THE AMBER RANGE IN CLIMB WENT TO TOP OF GREEN RANGE VIBERATION INCREASES RAPID ABOVE 90 % N2. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVE AND REPLACE NR 2 ENGINE ACCELEROMETER SENSOR IAW RRMM - OPS CHECK GOOD.

Part: STRIP — CRACKED (CABIN) · airframe 23,937 hrs · 20,116 cycles

LEFT NR 5 & NR 2 EMERGENCY LIGHT STRIP EXTRUSIONS ARE CRACKED. RE-INSTALLED LT NR 5 & NR 2 EMERGENCY LIGHT STRIP EXTRUSIONS IAW AMM 33-50-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,937 hrs · 20,116 cycles

EMERGENCY LIGHT ON COCKPIT STEP INOPERATIVE. R & R EMERGENCY LIGHT ON GALLEY CEILING WHICH WAS AFFECTING EMERGENCY LIGHT ON COCKPIT STEP IAW AMM 33-50-14. EMERGENCY LIGHT, OPERATIONS CHECKED GOOD.

Part: ATTACH BRACKET — CRACKED (PAX DOOR) · airframe 23,937 hrs · 20,116 cycles

PASSENGER DOOR INNER HANDLE ATTACH BRACKET IS CRACKED. R & R CRACKED PAX DOOR INNER HANDLE ATTACH BRACKET IAW SRM 51-40-02 & SRM 51-20-03.

Part: HOLDER — FAILED (FLASHLIGHT) · airframe 23,937 hrs · 20,116 cycles

FLIGHT ATTENDANT HAND HELD FLASHLIGHT HAS NO CHARGE. REMOVED & INSTALLED SERVICEABLE FLIGHT ATTENDANT FLASHLIGHT BASE IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: CRADLE — DAMAGED (FLASHLIGHT) · airframe 23,578 hrs · 19,802 cycles

F/O FLASHLIGHT DOES NOT FIT TIGHTLY IN CRADLE. RED CHARGING LAMP WILL NOT ILLUMINATE UNLESS PRESSED AND HELD FLASHLIGHT IN PLACE. R & R F/O'S FLASHLIGHT ASSY IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD, NO DEFECTS NOTED AT THIS TIME.

Part: CART — ODOR (GALLEY) · airframe 23,314 hrs · 19,582 cycles

F/A REPORTS THAT ONE OF THE GALLEY CARTS SMELLS LIKE A DEAD ANIMAL. CLEANED INSIDE OF BOTH GALLEY CARTS. NO DEFECTS OR ODORS NOTED. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,091 hrs · 19,387 cycles

INTERIOR EMERGENCY LIGHT OVER RT WING DOOR INOPERATIVE. R & R BULB IAW MM 33-50-07, OPS CHECKED GOOD IAW MM 33-50-00.

Part: MANIFOLD — INOPERATIVE (HYD SYSTEM) · airframe 23,018 hrs · 19,335 cycles

AFTER TAKEOFF AT ABOUT 600 AGL, HYD SYS 1 LOW QTY, HYD 1 SYS LOW PRESSURE HYD 1 SYS 1 FAIL, RUDDER SYS 1 INOPERATIVE AND AILERON 1 SYS 1 PRESSURE DROPPED TO ZERO, SYS 1 QTY DROPPED TO ZERO. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R THE LT HYD MANIFOLD ASSY IAW AMM 29-10-07. NO LEAKS NOTED. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT — CRACKED (CABIN) · airframe 22,756 hrs · 19,132 cycles

DURING B INSPECTION, FOUND F/A EMERGENCY FLASHLIGHT CRACKED. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT IAW AMM TASKS 33-50-16-000-801-A/33-50-16-400-801-A. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,886 hrs · 18,435 cycles

ON FLIGHT 2917 - THE CREW REPORTED THE EMERGENCY LIGHTS WERE FOUND ON. THE BATTERY WAS DISCHARGING. THE EMERGENCY LIGHT SWITCH IN THE COCKPIT WAS FOUND "OFF". THE AIRCRAFT WAS REMOVED FROM SERVICE. CHARGED EMERGENCY LIGHT BATTERY USING APU FOR 6 HRS IAW RADIANT CMM 25-60-03. MAINTENANCE PERFORMED EMERGENCY LIGHT CHECK OK AND PER EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 21,840 hrs · 18,397 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FLOOR LIGHTING SECTIONS NR 4 AND NR 5 INOPERABLE ALONG WITH BOTH RIGHT AND LEFT EMERGENCY EXIT IDENTIFIER SIGNS. THE AIRCRAFT WAS REMOVED FROM SERVICE REMOVED AND REPLACED THE NR 5 EMERGENCY LIGHT DC/AC INVERTER IAW EMB 145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHT FLOOR STRIPS 5 AND 6 AND LT AND RT WING EMERGENCY EXIT LIGHTS ARE INOP. REPLACED NR 3 EMERGENCY BATTERY POWER SUPPLY AND CHARGER.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,472 hrs · 17,329 cycles

DURING B INSPECTION, FOUND THE LEFT AFT EXTERIOR OVERWING EMERGENCY LIGHT IS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LAMP IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 20,266 hrs · 17,178 cycles

FLIGHT 3522, FLIGHT ATTENDANT REPORTED FLASHLIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT IAW 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,033 hrs · 16,999 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT BULB AT THE SERVICE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EXTERNAL EMERGENCY LIGHT BULB AT SERVICE DOOR IAW EMB 145 AMM 33-50-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — BROKEN (CABIN) · airframe 18,718 hrs · 15,933 cycles

FWD FLIGHT ATTENDANT FLASHLIGHT CHARGER LATCH BROKEN. REMOVED AND REPLACED FWD FLIGHT ATTENDENT FLASHLIGHT CHARGER IAW EMB AMM 33-50-16. OPC GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 18,149 hrs · 15,512 cycles

ON FLIGHT 2998 THE CREW REPORTED THAT CLIMBING AT FL370 FLYING AROUND WEATHER, GOT AN UPDRAFT THAT SHOT THEM UP TO 37,500. THE CREW HEARD A LOUD POP AND NOTICED THE CAPTAINS OUTER WINDSHIELD HAD CRACKED. THE CREW DECLARED AN EMERGECNY AND DIVERTED TO ABI. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW EMB 145 AMM 56-10-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PLUG — DEFECTIVE (NR 1 ENGINE) · airframe 17,337 hrs · 14,868 cycles

ON POST FLIGHT OF 2935 THE CREW REPORTED THE NR 1 ENGINE SMOKING FROM INTAKE, 18 MIN AFTER LANDING AND SHUTDOWN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SHAFT PLUG OF NR 1 ENGINE IAW RR MM 72-59-15-400-801 UP TO AND INCLUDING STEP J (I)(A) PERFORMED ENGINE RUN IAW RR MM 72-00-00-710-801. THE OPERATIONAL CHECK WAS GOOD NO DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 15,580 hrs · 13,595 cycles

FOR FLIGHT 3251 THE RAMP REPORTED THAT WHILE CLEANING THE AIRCRAFT EMERGENCY LIGHTS FROM ROW 10 AND AFT AND OVERWING EMERGENCY LIGHTS WERE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 CHARGER AND BATTERY IAW EMB AMM 33-50-04. REMOVED AND REPLACED THE NR 4 CHARGER AND BATTERY IAW EMB AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 14,330 hrs · 12,578 cycles

ON FLIGHT 3546 WHILE DESCENDING INTO DFW THE CREW RECEIVED AN EICAS HYDRAULIC E1 PUMP FAIL ADVISORY MESSAGE. THE CREW COMPLIED WITH THE AIRCRAFT OPERATING MANUAL PROCEDURES. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE E1 HYDRAULIC PUMP IAW EMB-145 AMM 29-10-03. THE LEAK CHECK AND OPERATIONAL CHECK WERE OK. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 23,403 hrs · 21,677 cycles

ON FLIGHT 3374, CREW REPORTED FORWARD EMERGENCY EXIT LIGHTS INTERMITTENT AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 BATTERY SUPPLY AND BATTERY HOLDER ASSY IAW AMM EMB 33-50-04. OPERATIONAL CHECK GOOD AS THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — DISCHARGED (EMERGENCY LIGHTS) · airframe 10,920 hrs · 9,790 cycles

ON FLIGHT 9804 CREW REPORTED HALF OF EMERGENCY FLOOR LIGHTING STRIPS ARE INOPERATIVE AND SERVICE DOOR EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED INVERTER NR 2 IAW 33-50-50, OPERATIONS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — FUMES (COCKPIT) · airframe 8,593 hrs · 7,602 cycles

ON FLIGHT 4064, CREW REPORTED THAT ON APPROACH TO ORD ELECTRICAL FUMES IN COCKPIT. EMERGENCY DECLARED. AIRCRAFT LANDED WITH OUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. COULD NOT ISOLATE PROBLEM AT THIS TIME. A/C DID 2510 CHECK FLIGHT AND PASSED. AIRCRAFT RETURNED TO SERVICE.

Part: ANTENNA — FAILED (WX RADAR SYS) · airframe 7,638 hrs · 6,790 cycles

DIVERTED TO DFW WEATHER RADAR FAILED EN ROUTE TO MCI WHEN RADAR TESTED IT DISPLAYED RADAR FAIL CODE J TILT UNCALIBRATED POC O EL POSITION. REMOVED AND REPLACED WEATHER RADAR ANTENNA ASSEMBLY. OPS CK GOOD IAW AMM 34-42-00. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (FIRE DETECTION) · airframe 7,282 hrs · 6,495 cycles

INFLIGHT RECEIVED APU FIRE INDICATION WITH FIRE DETECT FAIL MESSAGE. DIVERTED TO SAT. REMOVED AND REPLACED FIRE TEST PANEL IAW EMB AMM 26-00-01. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: FIRE DETECTOR — ACTIVATED (APU BAY) · airframe 7,252 hrs · 6,485 cycles

RECEIVED APU FIRE WARNING AND APU FIRE DET FAIL AT 12,000 FEET, FIRED APU EXTINGUISHER BOTTLE, POST INSPECTION FOUND NO EVIDENCE OF FIRE. ISSUED AMERICAN EAGLE MEL 26-01, 26-05 AND 49-01. REPLACED FIRE BOTTLE IAW AMERICAN EAGLE WORK CARD 26-200-01. RESTORED MEL, RETURNED AIRCRAFT TO SERVICE.

Part: CLAMP — MISSING (LEFT ENGINE) · airframe 6,483 hrs · 5,908 cycles

RECEIVED ENGINE ONE ATTCS NO MARGAIN AND EXCEEDANCE ON TAKEOFF, LOW SPEED ABORT. INSTALLED NEW V-BAND CLAMP ON LEFT UPPER COMPRESSOR BLEED LINE IAW ROLLS ROYCE MM 75-31-00. LEAK CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SKIN PANEL — GOUGED (FUSELAGE)

DURING REPAIR OF TDMI 53003E, FOUND 2 SCRATCHES ON RT SIDE OF AIRCRAFT BELOW PASSENGER WINDOW BETWEEN FRAMES 24 AND 25 AND STRINGERS 13R AND 12R. MAINTENANCE APPLIED PATCH IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200505707) (K)