N908AE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,967 hrs · 37,466 cycles

MAIN PTRIM INOP DISPLAYED AFTER TAKEOFF. R/R CAPT PTRIM SWITHC IAW AMM 27-40-02 OPS CHK GOOD. A/C OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,805 hrs · 37,275 cycles

WING A ICE FAIL MSG WITH WING ANTI ICE INOP MSG IN ICING CONDITIONS. TS IN REF TO FIM 30-11-00-810-810-A DIAGRAM 003 UP TO BLOCK 6.R/R RH WING ANTI-ICING PICCOLO BURST PRESSURE TRANSDUCER IAW AMM 30-11-12. OPS CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,801 hrs · 37,272 cycles

LAV CENTER FLOOR BEAM CORRODED AT AFT NUTPLATE HOLE, BETWEEN FR 60-61. (UNDER FLOOR BEAM GUSSET.) PERFORMED CUTOUT, FABRICATED, AND INSTALLED DOUBLER AT LAV CENTER BEAM AT AFT NUTPLATE HOLE BETWEEN FR 60-61 IAW EMB 145 ETD2023-145-023088, EO1-53-23-0292 AND SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,801 hrs · 37,272 cycles

E994107 R/H OMAGA BEAM IS CORRODED AT FR 23. INSTALLED REPAIR DOUBLER ON R/H OMAGA BEAM AT FR 23 IAW EMBRAER ETD2023-145-024679 AND PIEDMONT EO1-53-23-0304

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,801 hrs · 37,272 cycles

LH OMEGA BEAM HAS CORROSION BETWEEN FRAMES 33 AND 34. INSTALLED REPAIR DOUBLER ON R/H OMAGA BEAM AT FR 23 IAW EMBRAER ETD2023-145-024663 REV "A" AND PIEDMONT EO1-53-23-0306.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,801 hrs · 37,272 cycles

E993554 INTERNAL DOUBLER IS CORRODED BETWEEN FRAMES 61-62 STRINGERS 19L-20L. FABRICATED AND INSTALLED SERVICEABLE INTERNAL DOUBLER FOR INSTALLATION BTW FR 61-62 STGR 19L-20L IAW ETD# ETD2023-145-023886AND EO1-53-23-0290.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,801 hrs · 37,272 cycles

E993572 CARGO DOOR CUTOUT SILL IS CORRODED. REMOVED AND REPLACED CARGO DOOR CUTOUT SILL IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,801 hrs · 37,272 cycles

E993573 CARGO DOOR CUTOUT SHEAR CLIP AT FRAME 65 IS CORRODED. : REMOVED AND REPLACED CARGO DOOR CUTOUT FRAME 65 SHEAR CLIP IAW EMB 145 SRM 53-31-04 ITEM 4D FIG. 212 AND PIEDMONT EO1-53-232-0294.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,801 hrs · 37,272 cycles

E993556 ; INTERNAL DOUBLER IS CORRODED BETWEEN FRAMES 62-62A STRINGERS 19L-20L. : FABRICATED AND INSTALLED SERVICEABLE INTERNAL DOUBLER FOR INSTALLATION BTW FR 62-62A STGR19L-20L IAW ETD# ETD2023-145-023886 AND EO1-53-23-0290

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,801 hrs · 37,272 cycles

E993553 FRAME 66 IS CRACKED AT STRINGER 16R. PERFORMED CUTOUT AS REQUIRED TO REMOVE DAMAGED SECTION OF FR 66 AT STGR 16R AND FABRICATED AND INSTALLED REPLACEMENT SECTION AND REPAIR SPLICE IAW EMB-145 SRM 53-00-04 SECTION 4 AND FIG. 201. CUTOUT PERFORMED BETWEEN STGR 16R-17R. FRAME REPLACED FROM CUT LINE TO FACTORY SPLICE BETWEEN STGR 15R-16R AND EO1-53-23-0296

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,801 hrs · 37,272 cycles

LH ENGINE FWD YOKE ASSEMBLY CRACKED AT LOWER OTBD CORNER. : REFER TO NRTC E998758 FOR REMOVAL AND REPLACEMENT OF LH ENGINE FWD YOKE LINKAGE FITTINGS.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,801 hrs · 37,272 cycles

E990366 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AT FRAME 79 BETWEEN STRINGERS 4L-5L. REMOVED CRACKS FROM RIVET HOLE ON FR 79 BETWEEN STGR 4L-5L AND INSTALLED FABRICATED REPAIR BUSHING IAW EMB 145 SRM 53-32-01-RE STEP 9.E, 53-23-01-RE ITEM 9 AND EO1-53-23-0307

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,801 hrs · 37,272 cycles

E990365 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AT FRAME 78 BETWEEN STRINGERS 4L-5L. : REMOVED CRACKS FROM RIVET HOLE ON FR 78 BETWEEN STGR 4L-5L AND INSTALLED FABRICATED REPAIR BUSHING IAW EMB 145 SRM 53-32-01-RE STEP 9.E, 53-23-01 RE ITEM 9 AND EO1-53-23-0307.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,801 hrs · 37,272 cycles

COCKPIT UNDERFLOOR ACCESS HATCH INTERNAL OUTER RING MOLDING IS CRACKED. FABRICATED DOUBLER AND FILLER CUTOUT DAAMAGE AND INSTALLED DOUBLER AND FILLER ON COCKPIT UNDERFLOOR ACCESS HATCH INTERNAL OUTER RING MOLDING IAW EMB 145 SRM 52-42-02 FIG201 AND EO1-52-23-0299

Part: FAN — ODOR (RECIRCULATION) · airframe 41,295 hrs · 36,784 cycles

SMELLED BURNING PLASTIC/SMOKE IN THE COCKPIT AT GATE. DURING T/S OF COCKPIT ODOR, HEARD LOUD NOISE COMING FROM PACK 2. -C/A-REF. NRWC#908-ORD-06501 AND 908-ORD-06503. C/W FIM TASK 21-20-00-810-801 REPLACED R/H CABIN RECIRCULATION FAN IAW EMB-145 M/M 21-24-01 OPS CHECKS GOOD, NO BURNING SMELLS NOTED.

Part: LAMP — INOPERATIVE (LH) · airframe 39,976 hrs · 35,273 cycles

L/H OVER WING EMERGENCY LIGHT INOP-C/A-RAR L/H OVER WING EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPERATIONAL CHECK GOOD.

Part: NONE — NONE · airframe 39,557 hrs · 34,787 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOP-C/A-RAR AFT CABIN EMERGENCY FLASHLIGHT ASSY IAW EMB 145 33-50-16. OPC GOOD.

Part: NONE — NONE · airframe 39,521 hrs · 34,744 cycles

FA AFT FLASHLIGHT INOP-C/A-DEFERRED PER MEL 25-32. AUTH # 010222M-C. EXPIRES 01/25/22. M PROCEDURES C/W

Part: NONE — NONE · airframe 39,490 hrs · 34,710 cycles

AFT EMERGENCY CABIN FLASHLIGHT INOP-C/A-REPLACED AFT EMERGENCY FLASHLIGHT BATTERY AS REQUIRED

Part: NONE — NONE · airframe 39,448 hrs · 34,663 cycles

AFT CABIN FLASHLIGHT HOLDER BROKEN-C/A-RAR AFT CABIN FLASHLIGHT HOLDER IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECK GOOD. END.

Part: PANEL — UNSECURE (NR 1 NACELLE) · airframe 38,915 hrs · 34,061 cycles

ENG VIBRATION AFTER TAKEOFF. A/I EMERGENCY DECLARED. IN FLIGHT AIRFRAME BEGAN TO SHAKE/VIBRATE. NO ENGINE VIBRATION NOTED. CLEAN CONFIGURATION. NO OVERWEIGHT LANDING. NO EXCESSIVE SINK RATE ON LANDING. UPON POST FLIGHT INSPECTION FOUND E1 PRE-COOLER EXHAUSE PANEL WAS FOUND PEELING BACK.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 38,842 hrs · 33,982 cycles

FWD F/A EMERGENCY FLASHLIGHT WONT CHARGE-C/A-RAR FWD EMERGENCY FLASHLIGHT IAW ETN-33-059 OPS CHECK GOOD

Part: DOOR FRAME — DEFORMED (CARGO DOOR) · airframe 37,851 hrs · 32,956 cycles

FRAME 67 HAS 1 OBLONG HOLE BENEATH THE CARGO DOOR SILL. C/A REPAIRED FRAME 67 BENEATH THE CARGO DOOR SILL IAW SRM 53-00-04.

Part: DOOR FRAME — DEFORMED (CARGO DOOR SILL) · airframe 37,851 hrs · 32,956 cycles

FRAME 66 HAS 2 OBLONG HOLES BENEATH THE CARGO DOOR SILL. C/A-REPAIRED FRAME 66 BENEATH THE CARGO DOOR SILL IAW SRM 53-00-04.

Part: ATTACH FITTING — CHAFED (AILERON ACTUATOR) · airframe 37,851 hrs · 32,956 cycles

LT AILERON ACTUATOR ATTACH POINT (ON AILERON) FITTING IS CHAFFED. C/A: R & R LT AILERON PCU ATTACH FITTING, IAW EO EM-27MR-112.

Part: BUSHING — MIGRATED (PCU FITTING) · airframe 37,851 hrs · 32,956 cycles

RT AILERON OUTBD PCU ATTACH FITTING HAS MIGRATED HAT BUSHINGS ON INBOARD AND OUTBOARD LUGS. C/A: R & R RT AILERON PCA ATTACH FITTING ASSEMBLY, IAW EO-EM-27MR-112.

Part: FITTING — DAMAGED (LT AIL DAMPER) · airframe 37,851 hrs · 32,956 cycles

LT AILERON DAMPER FITTING HAS TOOLING MARKS. C/A: COMPLIED WITH EO EM-27MR-112.

Part: SUPPORT BRACKET — CRACKED (FUELAGE) · airframe 37,851 hrs · 32,956 cycles

RT LATERAL PANEL OVERWING SUPPORT SPLICE BRACKET CRACKED. C/A: R & R RT LATERAL PANEL OVERWING SUPPORT BRACKET, IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 37,851 hrs · 32,956 cycles

LT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 41-48 HAS MULTIPLE SPOTS OF CORROSION. CORROSION LEVEL 1. C/A: REPLACED LT OUTBOARD FLOOR SUPPORT BETWEEN FR 41-48, IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 37,851 hrs · 32,956 cycles

RT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 48-52 HAS MULTIPLE SPOTS OF CORROSION. CORROSION LEVEL 1. C/A: R & R LT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 48-52, IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 37,851 hrs · 32,956 cycles

RT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 29-35 HAS MULTIPLE SPOTS OF CORROSION. CORROSION LEVEL 1. C/A: R & R RT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 29-35, IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 37,851 hrs · 32,956 cycles

RT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 34-40 HAS MULTIPLE SPOTS OF CORROSION. CORROSION LEVEL 1. C/A: REPLACED RT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 34-40, IAW SRM 51-40-02.

Part: DOOR FRAME — CORRODED (CARGO DOOR SILL) · airframe 37,851 hrs · 32,956 cycles

CARGO DOOR SILL IS CORRODED. CORROSION LEVEL 1. C/A-R & R CARGO DOOR SILL IAW SRM 51-40-02. REFER TO NON-ROUTINE E840095 FOR ADDING MATERIAL TO CARGO DOOR INTERNAL LOWER . CARGO DOOR SILL IS CORRODED. CORROSION LEVEL 1. C/A-R & R CARGO DOOR SILL IAW SRM 51-40-02. REFER TO NON-ROUTINE E840095 FOR ADDING MATERIAL TO CARGO DOOR INTERNAL LOWER CORNERS.

Part: SKIN — CRACKED (RUDDER FWD SPAR) · airframe 37,851 hrs · 32,956 cycles

RUDDER II FWD SPAR SKIN APPEARS TO HAVE A CRACK PROTRUDING FROM A HIGH LOCK FOR THE MIDDLE LOWER ATTACH POINT. VIEWED THREW ACCESS PANEL 327 BL. C/A: R & R RUDDER, IAW AMM 27-20-02, REF NON-ROUTINES E839469, E839910 AND E839976 FOR GAP CHECKS, FCF AND BACKLASHES. OPERATIONS AND DEFLECTION CHECKS GOOD.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 37,851 hrs · 32,956 cycles

RT CABIN OMEGA BEAM SUPPORT ANGLE IS CRACKED, ON TOP SIDE OF WING DECK BETWEEN FR 47 AND 48, INBOARD SIDE OF OMEGA BEAM. C/A: REMOVED AND REPLACED SUPPORT, IAW SRM 53-23-02.

Part: BRACKET — CRACKED (FRAME 68) · airframe 37,851 hrs · 32,956 cycles

CARGO BAY, RT WALL, CARGO DOOR TORSION BAR AFT END BRACKET IS CRACKED AT RT FR 68 BENEATH SINGLE HI LOCK. C/A: INSTALLED BRACKET, IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (RT OVERWING) · airframe 37,851 hrs · 32,956 cycles

RT OVER-WING LATERAL PANEL LOWER NUTPLATE SUPPORT (NR 3 FROM FWD EDGE) IS CRACKED. C/A: R & R RT OVER-WING LATERAL PANEL LOWER NUTPLATE SUPPORT (NR 3 FROM THE FWD EDGE), IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (LT OVERWING) · airframe 37,851 hrs · 32,956 cycles

LT OVER-WING LATERAL PANEL LOWER NUTPLATE SUPPORT (NR 2 FROM FWD EDGE) IS CRACKED. C/A: R & R LT OVER WING LATERAL PANEL LOWER NUTPLATE SUPPORT, IAW SRM 51-40-02 AND 51-40-04.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 37,851 hrs · 32,956 cycles

FLOOR EMERGENCY LIGHTING CONNETOR AT FR 20 LEFT HAS A BROKEN WIRE-C/A-COMPLETE:INSTALLED NEW PIN AND SPLICE IAW SWPM 20-21-00, REF BOW 351666 TASK #1 FOR OPTS CHECK

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,851 hrs · 32,956 cycles

#1 LH EMERGENCY EXIT LIGHT STRIP HAS A BROKEN WIRE/TERMINAL END CONNECTION ON THE LIGHT STRIP SIDE.-C/A-COMPLETE:REPLACED #1 L/H EMERGENCY EXIT LIGHT STRIP DISCONNECTABLE SPLICE ON THE LIGHT STRIP SIDE I.A.W. EMB145 S.W.P.M. 20-21-00.

Part: LIGHT — TORN (CABIN) · airframe 37,851 hrs · 32,956 cycles

CABIN FLOOR RH #1 EMERGENCY EXIT LIGHT STRIP ESCUTCHEON IS TORN.-C/A-COMPLETE:RAR THE CABIN FLOOR RH #1 EMERGENCY EXIT LIGHT STRIP EXTRUSION IAW AMM 33-50-12

Part: WIRE — FRAYED (EMERGENCY LIGHTS) · airframe 37,851 hrs · 32,956 cycles

#3 EMERGENCY EXIT LIGHT FLOOR STRIP HAS EXPOSED AND FRAYED WIRES ON STRIP SIDE.-C/A-COMPLETE:INSTALLED NEW FLOOR PROXIMITY LIGHT IAW EMB145 AMM 33-50-12.

Part: LIGHT — BROKEN (CABIN) · airframe 37,851 hrs · 32,956 cycles

#8 RIGHT HAND CABIN EMERGENCY EXIT FLOOR LIGHT ESCUTCHEON IS BROKEN.-C/A-COMPLETE:INSTALLED NEW FLOOR SIDEWALL EXTRUSION IAW EMB145 AMM 33-50-12.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 37,538 hrs · 32,626 cycles

RT OVERWING EMERGENCY LIGHT INOPERABLE. C/A: R & R RT OVERWING EMERGENCY LIGHT, IAW EMB AMM33-50-07-000-801-A AND 33-50-07-400-801-A. NO FIX, FOUND CANNON PLUG LOOSE. RETIGHTENED CANNON PLUG. OPERATIONS CHECKED GOOD.

Part: LAMP — INOPERATIVE (ETERIOR LIGHT) · airframe 37,484 hrs · 32,565 cycles

EXTERNAL EMERGENCY LIGHT ON RT SIDE CENTER FAIRING INOPERABLE. C/A: REMOVED AND REPLACED LAMP TO EXTERNAL EMERGENCY LIGHT ON RT SIDE CENTER FAIRING, IAW EMB145 AMM 33-50-10. OPERATIONS CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,189 hrs · 32,218 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RT OVERWING EMERGENCY LIGHT LAMP IAW 33-50-10-000-801-A, AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,994 hrs · 32,029 cycles

RIGHT EXTERNAL EMERGENCY AFT LIGHT IS INOPERATIVE. REMOVED AND REPLACED RT EXTERNAL EMERGENCY AFT LIGHT LAMP IAW AMM 33-50-10. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,870 hrs · 31,894 cycles

DURING PS-1 CHECK EXTERNAL EMERGENCY LIGHT RH UPPER FAIRING DID NOT FUNCTION-C/A-REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT RH UPPER FAIRING LAMP IAW EMB AMM 35-50-10

Part: CONTROLLER — FAILED (COCKPIT) · airframe 36,519 hrs · 31,546 cycles

IN TO CLIMB AT AROUND 7,000FT WE LOST CAB ALT INDICATIONS ON TO PRESSURIZATION. SHORTLY AFTER WE LOST DELTAP AND CAB RAT INDICATIONS AS WELL-C/A-MEL 21-17 CHANGED TO MEL 21-19. M PROCEDURES C/W. A/C OK FOR SERVICE. REMOVED AND REPLACED DIGITAL CONTROLLER IAW EMB 145 AMM 21-31-01. OPS CHECK GOOD. MEL ITEM RESTORED. M PROCEDURES REVERSED.

Part: WARNING MESSAGE — FALSE ACTIVATION (WING ANTI-ICE) · airframe 36,491 hrs · 31,516 cycles

ICE CONDITION-A/I INOP WG A/ICE FAIL.DECLARED EMERGENCY.-C/A-PERFORMED OPERATIONAL TEST OF THE ANTI-ICEING SYSTEM IAW EMB 145 AMM 30-00-00-700-802-A. SYSTEM OPERERATES NORMALLY. AIRCRAFT OKAY FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,952 hrs · 31,038 cycles

EXTERIOR RH UPPER EMERGENCY LIGHT INOP. REMOVED AND REPLACED EXTERIOR RH UPPER EMERGENCY LAMP IAW AMM 33-50-10 OPC GOOD

Part: TIRE — WORN (NLG) · airframe 35,839 hrs · 30,919 cycles

WHEN EXITING RUNWAY (RIGHT TURN) GRINDING NOISE FROM NOSE AREA, BELOW FLIGHT DECK. BURNING SMELL IN FLIGHT DECK SHORT TIME LATER. BURNING RUBBER SMELL. "TRANSFERRED TO NRWC 908-ORD-04440" PERFORM ETN-EM-72-034 PER MOC FOR BURNING RUBBER SMELL IN COCKPIT. C/A-REF NRWC 908-ORD-04440. UPON FURTHER T/S FOUND RT NLG TIRE TO HAVE CONCENTRATED WEAR ON RT SIDE ONLY. R&R RT AND LT NLG WHEEL AND TIRE ASSY. NO GRINDING NOTED. BURNING RUBBER SMELL ATTRIBUTED TO SKIDDING TIRE. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 35,407 hrs · 30,484 cycles

CABIN ALTITUDE CLIMBED AS HIGH AS 9.800' AND MSL WAS 10,000'. ALSO IN MLI. THE MAIN CABIN DOOR WAS SHUT AND THE GROUND PERSONAL FAILED TO TAKE OFF THE PCA. C/A-REMOVED AND REPLACED DIGITAL CONTROLLER IAW AMM 21-31-01. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,635 hrs · 29,738 cycles

SERVICE DOOR EMERGENCY LIGHT INOP. C/A-RAR EXTERNA EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,550 hrs · 29,639 cycles

SUPPLEMENTAL CABIN ALTITUDE PRESS AND CABIN RATE HAVE YELLOW DASHES. C/A-FLIGHT CREW PLACARDED CPAM M PROCEDURES C/W MEL 21-23 AUTH 030249DM-C MOC 056048. CPAM INDICATION OPC GOOD, NO DEFECTS NOTED AT THIS TIME, IAW AMM 21-31-00 MEL RESTORED.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 34,475 hrs · 29,550 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RESEATED RH OVERWING EMERGENCY LIGHT IAW EMB145 AMM 33-50-10 OPC GOOD

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,317 hrs · 29,433 cycles

HYD SYS 2 PRESSURE FLUCTUATED IN FLIGHT SAW 2100 THEN 0 AND ENG 2 HYD PUMP FAIL. PERFORMED OPS CHECK OF EDP IAW AMM 29-10-03. OPS CHECK GOOD. NO FURTHER DEFCTS NOTED.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 33,495 hrs · 28,559 cycles

FOUND GALLEY AISLE CEILING PANEL EMERGENCY EXIT SIGN INOP. FOUND CONNECTOR P8525 DISCONNECTED AND BAGGED. REMOVED BAG AND INSTALLED CONNECTOR TO GALLEY AISLE CEILING PANEL EMERGENCY LIGHT, OPC GOOD IAW AMM 33-50-00.

Part: STRAP — UNSECURE (CARGO DOOR) · airframe 33,302 hrs · 28,362 cycles

DURING INITIAL CLIMB AT 3500 MSL, THE CARGO DOOR OPEN INDICATION DISPLAYED, ON RETURN, OPS FOUND A STRAP IN THE DOOR FRAME. PERFORMED AN OPS CHECK OF THE CARGO DOOR WARNING, OPS CHECKED GOOD IAW AMM 52-76-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,233 hrs · 28,284 cycles

FLOOR PROXIMITY LIGHTING STRIPS 6, 7 8 NOT LIT. R&R NR 4 EMERGENCY LIGHTING BATTERY ASSEMBLY AND R&R NR 6 LIGHT STRIP ONTO PANEL COVER IAW AMM 33-50-04. OPS CHECK GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 33,233 hrs · 28,284 cycles

1A CEILING PANEL EMERGENCY LIGHT LOOSE. REBONDED 1A CEILING PANEL EMERGENCY LIGHT IAW AMM 33-50-15.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 32,948 hrs · 28,016 cycles

DURING A FIRE DETECTOR TEST, THE CARGO SMOKE FAIL. REMOVED AND REPLACED CARGO BAY FWD SMOKE DETECTOR IAW AMM 26-15-01. OPS CHECKED GOOD IAW AMM 26-15-00.

Part: FLAP TRACK — DEFECTIVE (TE FLAP) · airframe 32,596 hrs · 27,699 cycles

FLAP FAIL AFTER TAKEOFF CLIMBING THROUGH 2500' AND DECELERATING THROUGH 200 KTS AOM 1 PROC APPLIED. REMOVED AND REPLACED RT I/B FLAP ROOT MOVABLE TRACK IAW AMM 57-52-01. INSTALLED NEW RT I/B FLAP SHROUD IAW AMM 57-56-01. REMOVED AND REPLACED RT I/B FLAP TIP MOVABLE TRACK IAW AMM 57-52-01. REPLACED LT I/B FLAP OUTB TRACK IAW AMM57-52-01. INSTALLED LT INBD FLAP IAW AMM27-50-00. PERFORM OPERATIONAL CHECK.

Part: ELECTRONIC UNIT — FAILED (TE FLAPS) · airframe 32,596 hrs · 27,698 cycles

FLAPS FAILED MESSAGE DURING CLIMBOUT. PERFORMED CMC DOWNLOAD. NOTED FECU FAIL MESSAGE. COMPLIED WITH FIM 27-51-00-810-803-A. REMOVED AND REPLACED FLAP ELECTRONIC UNIT IAW AMM 27-53-02. OPS CHECKED GOOD, NO FAULTS FOUND.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,553 hrs · 27,655 cycles

LEFT EMERGENCY LIGHT EXIT SIGN INOPERATIVE, BY THE LT OVERWING EMERGENCY DOOR IAW PS-1 CHECK. FOUND EMERGENCY LIGHT DC - AC INVERTER NR 4 TO BE BAD. R & R EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 32,508 hrs · 27,612 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. AFTER PERFORMING A VISUAL INSPECTION, A WIRE WAS FOUND BROKEN. SPLICED THE WIRE IAW SWPM-2430-20-21-00. OPS CHECKED GOOD.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 32,233 hrs · 27,321 cycles

AIRCRAFT FAILED TO PRESSURIZED AFTER TAKE OFF. ALL THE CONTROLS WERE SET UP CORRECTLY. RETURNED TO DEPARTURE. REMOVED AND REPLACED THE DIGITAL CONTROLLER IAW AMM 21-31-01. PERFORMED AN OPS CHECK IAW AMM 21-31-00, CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,087 hrs · 27,167 cycles

LH EMERGANCY EXIT EMERGANCY LIGHT AND LAST CEILING PANEL EMERGANCY LIGHT INOP-C/A-REPLACED CEILING PANEL LIGHT BULB IAW AMM 33-50-08 AND RESET CANNON PLUG ON #4 INVERTER IAW AMM 33-50-11. PERFORMED OPERATIONAL CHECK OF THE EMERGANCY LIGHTING SYSTEM IAW AMM 33-50-00-700-801. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,272 hrs · 26,478 cycles

SERVICE DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT BULB IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A OPC GOOD END.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,967 hrs · 26,207 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,962 hrs · 26,201 cycles

SERVICE DOOR ARM EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EXTERIOR EMERGENCY LIGHT IAW AMM 33-50-10-000-801 AND 33-50-10-400-801. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,549 hrs · 25,859 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 1 INVERTER IAW AMM 33-50-11 OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,487 hrs · 25,805 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A. OPS CHECKED GOOD

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,230 hrs · 25,583 cycles

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

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 29,064 hrs · 24,509 cycles

COCKPIT EMERGENCY LIGHT LAMP BURNED OUT. R & R COCKPIT EMERGENCY LIGHT LAMP. OPC GOOD IAW 33-50-05.

Part: WIRE — DAMAGED (CABIN) · airframe 29,060 hrs · 24,506 cycles

NR 1 EMEGENCY LIGHT STRIP WIRES TORN OFF. FOUND ON CLOSE-UP. R & R NR 1 EMERGENCY LIGHT STRIP IAW AMM 33-50-12

Part: SKIN — CRACKED (FRAME 75) · airframe 29,060 hrs · 24,506 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R, CRACK IS APPROX. 3/8" LONG. REPAIRED THE SKIN IAW SRM 53-31-01 REV 54.

Part: STRUCTURE — CORRODED (LAV BUCKET) · airframe 29,060 hrs · 24,506 cycles

THE LAV BUCKET IS CORRODED. REMOVED AND REPLACED THE LAV BUCKET IAW SRM 51-40-02.

Part: SKIN — CRACKED (FRAME 75) · airframe 29,060 hrs · 24,506 cycles

LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L, CRACK IS APPROX. 3/8" LONG. REPAIRED THE SKIN IAW SRM 53-31-01 REV 54.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 29,060 hrs · 24,506 cycles

EMERGENCY LIGHT INOPERATIVE. REPAIRED THE WIRE IAW SWPM 20-21-00 AND AMM 33-50-12. OPS CHECKED GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 29,060 hrs · 24,506 cycles

LOWER CARGO DOOR SILL HAS CORROSION. R & R CARGO DOOR CUTOUT LOWER SILL IAW SRM 51-40-02.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,953 hrs · 24,404 cycles

FOUND EMERGENCY EXIT SIGN ABOVE F/A SEAT INOPERATIVE. REPLACED INVERTER NR 1. OPC IS GOOD IAW AMM 33-50-11.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,916 hrs · 24,368 cycles

EMERGENCY FLOOR PROXIMITY LIGHT STRIP INOPERATIVE AT ROW 18. R&R FLOOR PROXIMITY LIGHT STRIP LT AFT IAW AMM 33-50-12. OPS CHECK GOOD.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 27,885 hrs · 23,467 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN. MAIN CABIN DOOR LUBRICATED & OPERATIONS CHECKED FOR OPENING & CLOSING, GOOD IAW AMM52-18-06.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,871 hrs · 23,457 cycles

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

Part: MODULE — FAILED (COCKPIT) · airframe 27,513 hrs · 23,145 cycles

BACKLIGHT AROUND EMER LIGHT SWITCH & BRIGHTNESS KNOB INOPERATIVE. R & R EMER LIGHT OVERHEAD MODULE IAW AMM 33-12-00. OPERATIONS CHECK FOUND OK.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,258 hrs · 22,898 cycles

RIGHT FWD BULKHEAD, PAX COMPARTMENT EMER LIGHT INOPERATIVE. R & R NR 3 EMER LIGHT INVERTER IAW AMM 33-50-11. LIGHT CHECKED GOOD.

Part: CONTROL PANEL — FAULTY (SMOKE DETECTION) · airframe 26,471 hrs · 22,194 cycles

ON DESCENT CREW RECEIVED EICAS LAVATORY SMOKE WARNING. THE FLIGHT ATTENDANT FOUND NO TRACES OF FIRE OR SMOKE IN THE LAVATORY. CREW COMPLIED WITH AOM VOL 1 PROCEDURES, DECLARED AN EMER & LANDED WITHOUT INCIDENT. CFR CLEARED THE ACFT TO TAXI. LAVATORY SMOKE INDICATION INFLIGHT. NO ORDER NOTED. R & R SMOKE DETECTION PANEL IAW AMM 26-14-02. OPERATIONS CHECKED GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 25,997 hrs · 21,769 cycles

LEFT OVERWING EMER EXIT SIGN INOPERATIVE. R & R EXIT SIGN. OPERATIONS CHECKED GOOD IAW AMM 37-50-14.

Part: CONNECTOR — UNSECURE (EXIT SIGN) · airframe 25,405 hrs · 21,212 cycles

EMERGENCY EXIT SIGN LIGHT ON A SIDE DOOR DOES NOT WORK. SECURED ELEC CONNECTORS IAW AMM 33-50-13. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: CONNECTOR — UNSECURE (EXIT SIGN) · airframe 25,405 hrs · 21,212 cycles

EMERGENCY EXIT SIGN LIGHT ON WALL 3 BC DOES NOT WORK. SECURED CONNECTORS IAW AMM 33-50-13. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 25,288 hrs · 21,094 cycles

RIGHT OVERWING EMER LIGHT IS INOPERATIVE. R & R RT OVERWING EMER LIGHT BULB IAW AMM 33-50-10.

Part: ANGLE — CRACKED (E&E DOOR) · airframe 24,309 hrs · 20,250 cycles

REAR ELECT COMPARTMENT DOOR UPPER INNER STRUCTURE REPAIR ANGLE IS CRACKED. REPAIRED IAW ERS-EM-52MR-152.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,270 hrs · 19,447 cycles

LEFT EXIT & FRONT RT BULKHEAD EMERGENCY LIGHTS INOPERATIVE. R & R LT EXIT & FRONT RT BULKHEAD EMERGENCY LIGHTS IAW AMM 33-50-13, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 23,008 hrs · 19,249 cycles

CREW REPORTED EMERGENCY FLASHLIGHT INOPERATIVE IN COCKPIT. REPLACED COCKPIT FLASHLIGHT IAW AMM 25-60-00.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,790 hrs · 19,095 cycles

EMERGENCY LIGHT PANEL MUST BE PUSHED FOR BACKLIGHTING TO WORK. R & R EMERGENCY LIGHT AT GALLEY BULKHEAD IAW AMM 33-50-14.

Part: LAMP — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 21,920 hrs · 18,334 cycles

DURING MX INSPECTION, FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R LAMP IAW AMM 33-50-09. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 21,772 hrs · 21,772 cycles

DURING B INSPECTION, FOUND THE COCKPIT CEILING EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE COCKPIT CEILING EMERGENCY LIGHT LAMP IAW AMM 33-50-05-000-801-A AND 33-50-05-400-801-A. THE OPS CHECK WAS GOOD. NO DEFECTS NOTED. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,702 hrs · 18,157 cycles

DURING B-INSPECTION, FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE MAIN DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — FUMES (COCKPIT) · airframe 21,332 hrs · 17,843 cycles

FOR FLIGHT 2898 THE CREW REPORTED A STRONG SMELL OF FUMES WITH APU ON AND APU BLEED OFF WITH BOTH ENGINES RUNNING AND BOTH ENGINE BLEEDS ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. RAN ENGINES AN APU WITH ENGINES ABOVE 85%, TRIED VARIOUS BLEED AIR SETTINGS IAW AMM 36-00-00. COULD NOT DUPLICATE SMELL OR RECREATE FUMES. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 21,136 hrs · 17,685 cycles

FLIGHT 2785. CAPTAIN’S FLASHLIGHT WOULD NOT CHARGE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT ASSEMBLY. OPS CHECKED GOOD WAS IAW AMM 33-50-16. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 20,930 hrs · 17,528 cycles

DURING B INSPECTION FOUND THE EMERGENCY EXIT SIGN AT ROW 3BC WILL NOT COME ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY EXIT SIGN AT ROW 3BC IAW EMB145 AMM 33-50-13. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,762 hrs · 17,391 cycles

DURING B INSPECTION FOUND THE LEFT WING AFT EMERGENCY LIGHT BULB INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT WING AFT EMERGENCY LIGHT LAMP. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-07. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 20,700 hrs · 17,342 cycles

ON FLIGHT 2788 THE CREW REPORTED THE FLASHLIGHT OVER THE FLIGHT ATTENDANT’S JUMP SEAT HAD A BROKEN HOLDER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 20,667 hrs · 17,316 cycles

ON FLIGHT 3431 THE CREW REPORTED A STRONG ODOR OF FUEL AFTER THE CABIN DOOR WAS CLOSED AND AIRCRAFT SLIGHTLY PRESSURIZED. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED APU FOR FUEL LEAKS WITH NONE NOTED AND NO FAULTS LOGGED TO APU FADEC IAW EMB-145 AMM 49-30-00. PURGED BLEED LINES WITH BOTH PACKS NO ODOR NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 19,953 hrs · 16,745 cycles

ON FLIGHT 3578 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IN THE FIRST OFFICER’S EMERGENCY FLASHLIGHT IAW DME CORPORATION CMM 25-60-02. NO OTHER DEFECTS NOTED AT THIS TIME. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — DEFECTIVE (CABIN PRESSURE) · airframe 19,740 hrs · 16,580 cycles

ON FLIGHT 4023 THE CREW REPORTED THEY LOST CABIN PRESSURE GRADUALLY AT FLIGHT LEVEL 330, CABIN PRESSURE WENT 12000. THE CREW DECLARED AN EMERGECNY AND LANDED WITHOUT INCIDENT THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DIGITAL CONTROLLER PER EMB-145 MM 21-31-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED · airframe 19,682 hrs · 16,537 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LEFT OMEGA BEAM CORRODED AT CARBON CROSS MEMBER AT FRAME 59. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED OMEGA BEAM IAW EO EM-53MR-1518. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CRACKED (LAV DRAIN DOOR) · airframe 19,682 hrs · 16,537 cycles

DURING MAINTENANCE INSPECTION, FOUND THAT THE LAV DRAIN DOOR HINGE APPEARS TO BE CRACKED. AIRCRAFT REMOVED FROM SERIVCE. REMOVED AND REPLACED THE DRAIN HINGE IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 19,682 hrs · 16,537 cycles

DURING MAINTENANCE INSPECTION, FOUND CARGO DOOR CUT OUT SHEAR TIE AT FRAME 68 CORRODED NEAR SILL. ACFT REMOVED FROM SERVICE. REPAIRED SHEAR TIE IAW EO EM-53MR-1129 PART B. ACFT RETURNED TO SERVICE.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 19,682 hrs · 16,537 cycles

DURING MAINTENANCE INSPECTION, FOUND STRINGER CLIP AT FRAME 80 S7L HAS A 5/8 INCH CRACK. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 19,682 hrs · 16,537 cycles

DURING MAINTENANCE INSPECTION, FOUND THE CARGO DOOR SILL IS CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 19,682 hrs · 16,537 cycles

DURING MAINTENANCE INSPECTION, FOUND CARGO DOOR CUT OUT SHEAR TIE AT FRAME 65 CORRODED NEAR SILL. AIRCRAFT REMOVED FROM SERVICE. REPAIRED SHEAR TIE IAW EO EM-53MR-1129 PART A. AIRCRAFT RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 19,683 hrs · 16,537 cycles

CARGO DOOR CUT-OUT SHEAR TIE AT FR. 65 CORRODED NEAR SILL. REPAIRED SHEAR TIE IAW EO EM-53MR-1129, PART A.

Part: SHEAR TIE — CORRODED (FRAME 68) · airframe 19,683 hrs · 16,537 cycles

CARGO DOOR CUT-OUT SHEAR TIE AT FR 68 CORRODED NEAR SILL. REPAIRED SHEAR TIE IAW EO EM-53MR-1129, PART B.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,683 hrs · 16,537 cycles

LT OMEGA BEAM IS CORRODED AT CARBON CROSS MEMBER AT FR 59. REPAIRED OMEGA BEAM IAW EO EM-53MR-1518.

Part: WIRE — EXPOSED (CABIN) · airframe 19,684 hrs · 16,538 cycles

DURING MAINTENANCE INSPECTION FOUND MOST AFT EMERGENCY FLOOR PROXIMITY LIGHT STRIPS ON THE LEFT SIDE OF CABIN HAS TORN INSULATION AND EXPOSED WIRES WHERE WIRING ENTERS STRIP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MOST AFT EMERGENCY FLOOR PROXIMITY LIGHT STRIPS ON THE LEFT SIDE OF CABIN IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,684 hrs · 16,538 cycles

DURING B INSPECTION FOUND THE CARGO DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW CARGO DOOR SILL IAW SRM 51-40-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT BRACKET — CORRODED (LAVATORY) · airframe 19,683 hrs · 16,537 cycles

LAVATORY SHROUD/SEAT SUPPORT BRACKET IS CORRODED BEYOND LIMITS. INSTALLED NEW SEAT SUPPORT BRACKET IAW AMM 38-32-01.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,665 hrs · 16,523 cycles

DURING MAINTENANCE INSPECTION, FOUND SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. THE AIRCRAFT WAS REMOVE FROM SERVICE. REMOVED AND REPLACED SERVICE EMERGENCY LIGHT BULB IAW AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. THE AIRCRAFT RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 18,278 hrs · 15,494 cycles

DURING B-INSPECTION FOUND THE RIGHT AFT EMERGENCY EXIT LIGHT ON EMERGENCY EXIT DOOR WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 5 EMERGENCY LIGHT DC/AC INVERTER IAW EMB AMM 33-50-11. OPERATIONAL CHECK GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,900 hrs · 15,224 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT FORWARD WING TO FUSELAGE FAIRING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY AND CHARGER IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,321 hrs · 14,003 cycles

FOR FLIGHT 4368 DURING THE PREFLIGHT INSPECTION FOUND BOTH LEFT AND RIGHT EXTERIOR OVERWING LIGHTS AND INTERIOR EMERGENCY EXIT LIGHTS AT ROW 12 TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLE SHOT SYSTEM AND FOUND EMERGENCY LIGHT BATTERIES TO BE LOW. STARTED APU AND ALLOWED BATTERIES TO CHARGE AS NEEDED. THE OPERTIONAL CHECK WAS GOOD IAW EMERGENCY LIGHTING SYSTEM POWER SUPPLIES FUNCTIONAL CHECK WORK CARD 33-700-19. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACCESS DOOR — CRACKED (FUSELAGE) · airframe 14,883 hrs · 12,841 cycles

DURING MAINTENANCE BASE VISIT FOUND ACCESS DOOR 272DR FRAME CRACKED UNDER DOOR PIN GUIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED ACCESS DOOR 272DR IAW EO EM-52MR-264. CRACK LENGTH 0.25 INCH TO APPROXIMATELY 0.75 INCH. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 14,920 hrs · 12,874 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHT STRIP AT 15A INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BROKEN WIRE FROM THE CONNECTOR AT 15A. REPAIRED THE BROKEN WIRE USING STANDARD PRACTICES. THE OPERATIONAL CHECK WAS GOOD PER AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,105 hrs · 12,186 cycles

ON FLIGHT 908 THE FLIGHT CREW REPORTED THE FORWARD OVERWING EMERGENCY LIGHT AND EMERGENCY LIGHT SIGN ADJACENT TO THE FLIGHT ATTENDANT SEAT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT SUPPLY AND BATTERY IAW EMB AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD NO FURTHER DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RUDDER PEDAL — DEFECTIVE (COCKPIT) · airframe 13,749 hrs · 11,897 cycles

ON FLIGHT 2838 DURING CRUISE THE CREW REPORTED DURING THE FLIGHT CONTROL CHECK THE RIGHT RUDDER WAS BINDING. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED RIGHT RUDDER PEDAL IAW EMB AMM 27-21-03. THE OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 12,811 hrs · 11,142 cycles

ON TAXI OUT FOR FLIGHT 4042 THE CREW REPORTED A SMOKE SMELL IN THE COCKPIT AND CABIN WITH THE APU ON AND PACK 1 OR 2 SELECTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 RECIRCULATION FAN IAW EMB 145 AMM 21-24-01. OPERATIONAL CHECK AND LEAK CHECK WAS GOOD. NO ODOR OR SMOKE SMELL NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — FAILED (CABIN LIGHTS) · airframe 10,101 hrs · 8,924 cycles

ON FLIGHT 4375, CREW REPORTED UPON PARKING, SMOKE AND FUMES, NO VISIBLE SMOKE FROM CABIN ROW 7 TO THE COCKPIT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SIDEWALL LIGHTS AT PAX ROW 7A OPERATION CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,855 hrs · 8,507 cycles

DURING AN IMBV INSPECTION. THE BAGGAGE DOOR LOWER CENTER SILL WAS FOUND TO BE CORRODED. REMOVED CORRODED CENTER SILL. INSTALLED NEW SILL 145-25480-603. REPAIR DONE IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 7,080 hrs · 6,397 cycles

PITCH TRIM INOP. REMOVED AND REPLACED HSCU IAW AMM 27-10-01-000-801-A AND 27-40-01-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (HORIZONTAL STAB) · airframe 7,081 hrs · 6,398 cycles

MAIN PITCH TRIM FAILED. CAPT ELECTED TO RETURN TO THE FIELD IAW AMM 27-40-02 REF NRWC 2004864. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR IAW AMM 27-40-03-000-801. OPS CHECK GOOD AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DAMAGED (ZONE 200) · airframe 6,201 hrs · 5,601 cycles

FUSELAGE SKIN BETWEEN FRAME 7 AND 8 GOUGED. REPAIRED SKIN IAW EMB SRM 53-10-01. RETURNED AIRCRAFT TO SERVICE.

Part: MANIFOLD — FAILED (ZONE 700) · airframe 6,200 hrs · 5,600 cycles

UNABLE TO STEER AIRCRAFT AFTER LANDING, AIRCRAFT VEERED STRIKING RUNWAY INFORMATION SIGN. REMOVED AND REPLACED NOSE STRUT ASSEMBLY AND NOSE WHEEL STEERING MANIFOLD IAW EMB AMM 32-20-01 AND 32-50-04. OPERATIONAL CHECK GOOD - AIRCRAFT RETURNED TO SERVICE

Part: FRAME — BIRD STRIKE (COCKPIT WINDOW)

CREW REPORTED BIRD STRIKE ABOVE THE FIRST OFFICERS WINDOW. AIRCRAFT REPOSITIONED TO ABI FOR REPAIR. PERFORMED A 19.5 INCH CUT OUT OF FRAME 6 TO REMOVE FRAME DAMAGE RECONTOURED DENT ON SKIN AT FRAME 7. PREPARED A 19.5 INCH FRAME FILLER, A 8 INCH LOWER FRAME SPLICE AND AN 8.5 INCH UPPER FRAME. FABRICATED 3 SKIN REINFORCEMENT ANGLES AND 2.5 INCH STRAPS FOR FRAME 6 SPLICE. REPAIR ACCOMPLISHED IAW EMB REPAIR STATEMENT IC2005-145/5730A DATED 10/26/2005 AND IC 2005-145/6219 DATED 10/30/2005. AIRCRAFT RETURNED TO SERVICE. (M)