N11113

Part: SWITCH — OUT OF ADJUST (LT MLG WOW) · airframe 45,044 hrs · 28,113 cycles

LG AIR/GROUND FAIL ON EICAS MESSAGE IN FLIGHT. FOUND MLG STRUT WOW SWITCH (LT) OUT OF RIG. FOUND RT MLG STRUT WOW SWITCH BRACKET LOOSE. SECURED RT MLG STRUT SWITCH BRACKET AND ADJUSTED BOTH MLG STRUT WOW SWITCHES. OPERATIONS CHECK GOOD. GEAR SWINGS GOOD.

Part: DOUBLER — NOT REPORTED (FRAMES 19-20) · airframe 44,956 hrs · 28,031 cycles

REPAIR DOUBLER ON LT CENTER FUSE 1, BETWEEN FR 19-20 AND BETWEEN STR 14L-16L. REPAIRED DOUBLER ON LT CENTER FUSE 1, BETWEEN FR 19-20 AND BETWEEN STR 14L-16L REPAIR SKIN.

Part: WIRE — FAILED (SMOKE DETECTOR) · airframe 44,648 hrs · 27,765 cycles

BAG SMOKE EICAS MSG, BAG BOTTLES DISCHARGED---R&R BOTH BAGGAGE FIRE BOTTLES(HIGH RATE AND METERING). ADDITIONAL MX- REPLACED WIRING FROM SG4313 TO SMOKE DETECTORS 1 AND 2 DUE TO WIRES READING 200 OHMS( TEST RESULT WHEM WIRES MEGGERED) PERFORMED BAGG SMOKE TEST AND FOUND NOT DEFECTS

Part: PARTITION — CORRODED (FRAME 61) · airframe 44,569 hrs · 27,700 cycles

FR 61 R/H SIDE PARTITION HAS CORROSION UNDER CARBON FIBER RING....R&R R/H SIDE PARTITION AT FR 61.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 44,569 hrs · 27,700 cycles

SHEAR CLIP CORRODED AR FRAME 65 BETWEEN STR 21L & 21R. REMOVED AND REPLACED THE SHEAR CLIP.

Part: SHEAR TIE — CORRODED (FRAME 61) · airframe 44,569 hrs · 27,700 cycles

FRAME 61, STRINGER 19R, RBL 20 SHEAR TIE FASTENER CORRODED. R & R THE SHEAR TIE.

Part: PLATE — CORRODED (FRAME 18) · airframe 44,569 hrs · 27,700 cycles

AFT DIGITAL PLATE AT FR 18 IS CORRODED....R&R AFT DIGITAL PLATE AT FR 18.

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,569 hrs · 27,700 cycles

LOWER SKIN OF FUSELAGE ABOVE VENTRAL FUEL TANK HAS POSSIBLE CORROSION- REMOVED CORROSION FROM BELLY EXTERIOR AT FUSELAGE DRAIN BETWEEN FR 53-54, STR 21L & 21R & REMOVED THE DRAIN MOUNTING PLATE, AWAITING ULTRASOUND SKIN THICKNESS MEASUREMENT. DAMAGE TO BE ALLOWER A1 IS PER ETD 2019-145-164595 PERFORMED UNTRASOUND AND REMAINING THICKNESS US 0.123". REPAIRED LOWER SKIN FUSELAGE ABOVE VENTRAL TANK.

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,569 hrs · 27,700 cycles

LOWER SKIN OF FUSELAGE ABOVE VENTRAL FUEL TANK HAS POSSIBLE CORROSION- REMOVED CORROSION FROM BELLY EXTERIOR AT FUSELAGE DRAIN BETWEEN FR53-54, STR 21L & 21R & REMOVED THE DRAIN MOUNTING PLATE. AWAITING ULTASOUND SKIN THICKNESS MEASUREMENT. DAMAGE TO BE ALLOWED A1 IS PER ETD2019-145-164595 PERFORMED UNTRASOUND AND REMAINING THICKNESS IS 0.123". REPAIRED LOWER SKIN FUSEALAGE ABOVE VENTRAL TANK.

Part: FLOOR SUPPORT — CORRODED · airframe 44,569 hrs · 27,700 cycles

LEFT LAVATORY FLOOR SUPPORT HAD CORROSION AROUND AFT NUT PLATE HOLES. R & R THE FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED · airframe 44,569 hrs · 27,700 cycles

R/H LAV FLOOR SILL HAS CORROSION AROUND AFT NUT PLATE HOLE....R&R R/H LAV FLOOR SILL.

Part: SHEAR TIE — CRACKED (FRAME 65) · airframe 44,569 hrs · 27,700 cycles

SHEAR TIE WAS CRACKED AT FRAME 65, STRINGER 18L. R&R THE SHEAR TIE.

Part: GUSSET — CORRODED (LAVATORY) · airframe 44,569 hrs · 27,700 cycles

RIGHT GUSSET IN LAVATORY HAS CORROSION AROUND NUT PLATE HOLES. R&R RT GUSSET IN LAV

Part: FRAME ANGLE — CORRODED (CARGO DOOR) · airframe 44,569 hrs · 27,700 cycles

CARGO DOOR LOWER FRAME ANGLE HAS CORROSION AROUND NUTPLATE HOLES- R/R CARGO DOOR LOWER FRAME ANGLE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 22-23) · airframe 44,569 hrs · 27,700 cycles

R/H FLOOR SILL HAS CORROSION AT FR 23 & 22 AFT OF SERVICE DOOR....R&R R/H FLOOR SILL AT FR 23 & 22 AFT OF SERVICE DOOR.

Part: FLOOR SUPPORT — CORRODED (FRAMES 37-38) · airframe 44,569 hrs · 27,700 cycles

L/H FLOOR SILL HAS CORROSION ON UPPER SURFACE BETWEEN FR 37 & 38....R&R L/H FLOOR SILL BETWEEN FR 37 & 38.

Part: FLOOR SUPPORT — CORRODED (FRAMES 19-20) · airframe 44,569 hrs · 27,700 cycles

L/H FLOOR SILL HAS CORROSION ON UPPER SURFACE FROM FR 19 THRU 20....R&R THE L/H FLOOR SILL AT FR 19 & 20.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · airframe 44,569 hrs · 27,700 cycles

AFT LAV R/H FLOOR SIL HAS CORROSION AROUND FASTNER HOLES AT FR 59 & 61....R&R LAV R/H FLOOR SILL AT FR 59 & 61

Part: FLOOR SUPPORT — CORRODED (FRAME 15) · airframe 44,569 hrs · 27,700 cycles

MAIN CABIN CENTER OMEGA BEAM UPPER DIGITAL SUPPORT HAS CORROSION AROUND FASTENER HOLE AT FR 15- PERFORMED REPAIR FOR THE CORRODED NUTPLATE HOLE AT FR15 AT CENTER OMEGA BEAM ON THE UPPER DIGITAL PLATE.

Part: ANGLE — CORRODED (THRESHOLD) · airframe 44,569 hrs · 27,700 cycles

PASSENGER DOOR LOWER THRESHOLD 2EA NUTPLATE 'Z' ANGLES HAVE CORROSION AROUND FASTENER HOLES- R&R 2EA PASSENGER DOOR COVER THRESHOLD 'Z' ANGLES.

Part: NUT PLATE — CORRODED (ANTENNA HOUSING) · airframe 44,569 hrs · 27,700 cycles

MAIN CABIN LOWER BELLY DME1 ANTENNA HOUSING HAS CORROSION BETWEEN FRAME 19 & 20 @ STR 12 & 20 LH- R/R THE DME1 NUTPLATE ATTACH ASSEMBLY PLATE BETWEEN FR19 & 20 BY STR20L.

Part: SEAT TRACK — CORRODED (FRAMES 19-24) · airframe 44,569 hrs · 27,700 cycles

MAIN CABIN LH OMEGA BEAM SEAT TRACKS HAVE LIGHT CORROSION FROM FR 19 THRU 24. REMOVED THE SEAT TRACK AND INSTALLED A NEW SEAT TRACK.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · airframe 44,569 hrs · 27,700 cycles

AFT LAV RH OMEGA BEAM UPPER DIGITAL SUPPORT HAS CORROSION AT FRAME 59 & 61- PERFORMED CUT-OUT OF CORROSION AROUND THE NUTPLATE AT FR 59 ON RIGHT OMEGA BEAM. MANUFACTURED DOUBLER FOR THE RIGHT OMEGA BEAM REPAIR AT FR 59 & INSTALLED, NUTPLATE STILL NEEDS INSTALLED. INSTALLED UPPER DIGITAL SUPPORT ON THE RH OMEGA BEAM FROM FR58-FR62, ALL NUTPLATES STILL NEED TO BE INSTALLED. INSTALLED NUTPLATES ON AFT LAV RH OMEGA BEAM UPPER DIGITAL AT FR 59 & 61.

Part: SHEAR TIE — CORRODED (FRAME 61) · airframe 44,569 hrs · 27,700 cycles

AFT LAV FRAME 61 SHEER CLIP HAS CORROSION ON FWD SIDE BETWEEN STR 19 & 20 RH, AFT OF DUMP VALVE HOUSING- SHEER CLIP HAD 100% MATERIAL LOSS AROUND FASTENER, FOUND OUT OF LIMITS, REMOVED DEFECTIVE SHEER CLIP. LOCATED, DRILLED UP. INSTALLED NEW SHEER CLIP.

Part: FLOORBEAM — CORRODED (FRAME 59) · airframe 44,569 hrs · 27,700 cycles

CENTER OMEGA BEAM HAS CORROSION AT FR 59 BETWEEN UPPER DIGITAL & FLOOR BEAM AROUND NUTPLATE HOLE- PERFORMED CUT OUT OF CORROSION AROUND THE NUTPLATE AT FR 59 ON THE CENTER OMEGA BEAM. MANUFACTURED DOUBLER FOR THE CENTER OMEGA BEAM REPAIR AT FR 59 & INSTALLED IT, NEEDS NUTPLATE INSTALLED. INSTALLED NUTPLATES ON CENTER OMEGA BEAM AT FR 59, INSTALLED UPPER DIGITAL AT FR 59 CENTER OMEGA BEAM.

Part: SEAT TRACK — CORRODED (FRAMES 28-38) · airframe 44,569 hrs · 27,700 cycles

RH SIDEWALL SEAT TRACKS HAVE CORROSION BETWEEN FRAME 28 THRU 38- REMOVED CORROSED SEAT TRACKS THAT WERE MARKED WITH RED MARKER ON RH SIDEWALL BETWEEN FRAMES 28 THRU 38. INSTALLED SEAT TRACKS ON RH SIDEWALL, REMAINING 4 SEAT TRACKS TO BE INSTALLED. INSTALLED REMAINING 4 SEAT TRACKS.

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 44,569 hrs · 27,700 cycles

MAIN CABIN FR 24 SHEAR CLIP IS CRACKED AT STR 15 LH- REMOVED AND REPLACED SHEAR CLIP AT FR 24.

Part: FLOOR SUPPORT — CORRODED (FRAME 47) · airframe 44,569 hrs · 27,700 cycles

RIGHT FLOOR SUPPORT HAD CORROSION AT FRAME 47 ON UPPER SURFACE. R & R THE RT FLOOR SUPPORT AT FRAME 47.

Part: FLOOR SUPPORT — CORRODED (FRAMES 38-41) · airframe 44,569 hrs · 27,700 cycles

RH FLOOR SILL HAS CORROSION ON UPPER SURFACE BETWEEN FR 38 THRU 41- REMOVED DAMAGED FLOOR SILL. INSTALLED NEW RH FLOOR SILL BETWEEN FR 36 & FR 41

Part: FLOOR SUPPORT — CORRODED (FRAMES 32-35) · airframe 44,569 hrs · 27,700 cycles

LH FLOOR SILL HAS CORROSION ON UPPER SURFACE FROM STA 32 THRU 35 LH- R/R LH FLOOR SILL AT FR 32 THRU 35.

Part: FLOOR SUPPORT — CORRODED (FRAMES 48-50) · airframe 44,569 hrs · 27,700 cycles

R/H FLOOR SILL HAS CORROSION AT FR 48, 49 & 50 ON UPPER SURFACE....R&R R/H FLOOR SILL AT FR 48, 49 & 50.

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 44,569 hrs · 27,700 cycles

MAIN CABIN FR 24 SHEER CLIP IS CRACKED AT STR 15 LH- REMOVED AND REPLACED SHEER CLIP AT FR 24.

Part: FLOOR SUPPORT — CORRODED (FRAME 59) · airframe 44,569 hrs · 27,700 cycles

AFT LAV LH OMEGA BEAM UPPER DIGITAL SUPPORT HAS CORROSION AROUND FASTENER HOLE AT FRAME 59- R/R LH AFT LAV OMEGA BEAM UPPER DIGITAL SUPPORT AT FRAME 59.

Part: FLOOR SUPPORT — CORRODED (FRAMES 20-23) · airframe 44,569 hrs · 27,700 cycles

CENTER OMEGA BEAM UPPER DIGITAL HAS CORROSION FROM FR 20 TRU 23....R&R CENTER OMEGA BEAM GUSSET FROM FR 18 THRU 23.

Part: FLOOR SUPPORT — CORRODED (FRAMES 29-30) · airframe 44,569 hrs · 27,700 cycles

MAIN CABIN RH FLOOR SILL HAS CORROSION BETWEEN FRAME 29 & 30- R&R RH FLOOR SILL AT FR 29 & 30.

Part: SEAT TRACK — CORRODED (FRAMES 44-51) · airframe 44,569 hrs · 27,700 cycles

LH SIDEWALL SEAT TRACKS HAVE CORROSION FROM FR 44 THRU 51- R/R LH SIDEWALL SEAT TRACKS THAT HAVE CORROSION FROM FRAME 44 THRU 51.

Part: FLOOR SUPPORT — CORRODED (FRAMES 48-50) · airframe 44,569 hrs · 27,700 cycles

L/H FLOOR SILL HAS CORROSION BETWEEN FR 48 & 50 ON UPPER SURFACE....R&R L/H FLOOR SILL BETWEEN FR 48 & 50

Part: FLOOR SUPPORT — CORRODED (FRAMES 29-30) · airframe 44,569 hrs · 27,700 cycles

MAIN CABIN L/H FLOOR SILL HAS CORROSION ON UPPER SURFACE BETWEEN FR 29 & 30....R&R L/H FLOOR SILL AT FR 29 & 30.

Part: SEAT TRACK — CORRODED (FRAMES 45-51) · airframe 44,569 hrs · 27,700 cycles

RH SIDEWALL SEAT TRACKS HAVE CORROSION AT FRAME 45, 46, 47, 48 & 51- R/R RH SIDEWALL SEAT TRACKS THAT HAVE CORROSION AT FRAME 45, 46, 47, 48 AND 51.

Part: FLOOR SUPPORT — CORRODED (FRAME 46) · airframe 44,569 hrs · 27,700 cycles

L/H FLOOR SILL HAS CORROSION BETWEEN FR 46 ON UPPER SURFACE....R&R L/H FLOOR SILL BETWEEN FR 46.

Part: HOUSING — CORRODED (DME ANTENNA) · airframe 44,569 hrs · 27,700 cycles

MAIN CABIN LOWER BELLY DME 2 ANTENNA HOUSING HAS CORROSION BETWEEN FR 27 & 28 @ STR 20 & 21RH- R/R MAIN CABIN LOWER BELLY DME 2 ANTENNA HOUSING AT FR 27 & 28.

Part: FLOOR SUPPORT — CORRODED (FRAMES 24-29) · airframe 44,569 hrs · 27,700 cycles

MAIN CABIN LH FLOOR SILL HAS CORROSION ON UPPER SURFACE AT FR 24 & 29- STARTED REMOVING LH SILL TO GAIN ACCESS TO SHEER CLIP AT FR 25. FINISHED REMOVING AND REPLACED SILL.

Part: FLOOR SUPPORT — CORRODED (FRAMES 54-57) · airframe 44,569 hrs · 27,700 cycles

R/H FLOOR SILL HAS LIGHT CORROSION AT FR 54 & 57 ON UPPER SURFACE....R&R R/H FLOOR SILL AT FR 54 & 57.

Part: FLOOR SUPPORT — CORRODED (FRAME 22) · airframe 44,569 hrs · 27,700 cycles

R/H OMEGA BEAM UPPER STOP SIGN HAS CORROSION AT FR 22....R&R R/H OMEGA BEAM STOP SIGN AT FR 22.

Part: FLOOR SUPPORT — CORRODED (FRAMES 32-35) · airframe 44,569 hrs · 27,700 cycles

RH FLOOR SILL HAS CORROSION ON UPPER SURFACE FROM STA 32 THRU 35 RH- R&R RH FLOOR SILL AT FR 32 & 35.

Part: SHEAR TIE — CRACKED (FRAME 67) · airframe 44,569 hrs · 27,700 cycles

AFT CARGO FRAME 67 SHEAR CLIP WAS CRACKED BETWEEN STRINGERS 6 & 7LT ABOVE CARGO DOOR CUT OUT. R & R THE CRACKED SHEAR CLIP.

Part: SUPPORT ANGLE — CORRODED (FRAME 66) · airframe 44,569 hrs · 27,700 cycles

AFT CARGO DOOR LOWER THRESHOLD T PROFILE AT FR 66 LOWER ANGLE SUPPORT IS CRACKED....R&R AFT CARGO DOOR LOWER THRESHOLD T PROFILE AT FR 66.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 44,569 hrs · 27,700 cycles

AFT CARGO DOOR TORSION BAR AFT UPPER SUPPORT BRACKET IS CRACKED AT HI-LOC: REMOVED TORSION BAR QUADRANT TO FACILITATE MAINTENCE. REMOVED AND STARTED INSTALLATION OF SUPPORT. FINISHED INSTALLING SUPPORT. INSTALLED TORSION BAR LIFT AND LOWERING MECHANISM, REQUIRES TENSIONING. PERFORMED REQUIRED TENSION ON THE CARGO BAY.

Part: SHEAR TIE — CRACKED (FRAME 71) · airframe 44,569 hrs · 27,700 cycles

AFT CARGO FR 71 R/H SHEAR TIE IS CRACKED AT STRINGER 8R. R & R AFT CARGO FR 71 RT SHEAR TIE AT STR 8 R/H.

Part: SHEAR TIE — CRACKED (FRAME 25) · airframe 44,569 hrs · 27,700 cycles

MAIN CABIN FRAME 25 LH SHEER CLIP IS CRACKED AT STR 15 LH- REMOVED & REPLACED SHEER CLIP AT FR 25 LH SIDE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 61-64) · airframe 44,569 hrs · 27,700 cycles

AFT CARGO LEFT FLOOR SILL HAD CORROSION AROUND FASTENER HOLE FROME FRAMES 61 - 64. R & R AFT CARGO LEFT FLOOR SILL.

Part: FLOOR SUPPORT — CORRODED (FRAMES 61-65) · airframe 44,569 hrs · 27,700 cycles

AFT CARGO RT FLOOR SILL HAS CORROSION AROUND FASTNER HOLES FROM FR 61 THRU 65 R/H. R&R AFT CARGO RT FLOOR SILL AT FR 61 THRU 65.

Part: FLOOR SUPPORT — CORRODED (FRAME 65-68) · airframe 44,569 hrs · 27,700 cycles

AFT CARGO RH FLOOR SILL HAS CORROSION FROM FRAME 65 THRU 68 ON UPPER SURFACE- REMOVE DAMAGED FLOOR SILL, LOCATED AND DRILLED NEW RH FLOOR SILL, INSTALLED NEW FLOOR SILL.

Part: SHEAR TIE — CORRODED (FRAME 61) · airframe 44,569 hrs · 27,700 cycles

AFT LAV FRAME 61 SHEAR CLIP HAS CORROSION ON FWD SIDE BETWEEN STRINGERS 19 & 20 RT AFT OF DUMP VALVE HOUSING. R&R SHEAR CLIP AT FR 61 BETWEEN STR 19 & 20 R/H.

Part: SHEAR TIE — CRACKED (FRAME 72) · airframe 44,569 hrs · 27,700 cycles

AFT CARGO FRAME 72 SHEER CLIP IS CRACKED AT STR 15 LH- REMOVED & REPLACED SHEER CLIP AT FR 72.

Part: SEAT TRACK — CORRODED (FRAMES 56-57) · airframe 44,569 hrs · 27,700 cycles

POSSIBLE CORROSION FOUND ON UPPER SEAT TRACKS AT RT FR 56 LT FR 56 & FR 57. R&R SEAT TRACKS AT RT FR 56 AND LT FR 56 AND FR 57.

Part: SHEAR TIE — CRACKED (FRAME 65) · airframe 44,569 hrs · 27,700 cycles

AFT CARGO FRAME 65 SHEER CLIP IS CRACKED AT STR 17 LH- REMOVED CRACKED SHEER CLIP. LOCATED, DRILLED & INSTALLED NEW SHEER CLIP.

Part: CLOSEOUT PANEL — CORRODED (FRAME 65) · airframe 44,569 hrs · 27,700 cycles

AFT CARGO DOOR CUT OUT LOWER CLOSE OUT PANEL AT FRAME 65 AT LOWER FWD CORNER HAS CORROSION AROUND FASTENER HOLES- BLENDED CORROSION ON RIB AT FR 65, RIB WAS FOUND TO BE OUT OF LIMITS. REMOVED DEFECTIVE RIB, LOCATED AND DRILLED UP NEW RIB. INSTALLED NEW RIB.

Part: DOOR FRAME — CORRODED (FRAME 68) · airframe 44,569 hrs · 27,700 cycles

AFT CARGO DOOR CUT OUT LOWER AFT CORNER PANEL AT FR 68 AT LOWER AFT CORNER HAS CORROSION AROUND FASTNER HOLE....R&R CARGO DOOR LOWER AFT CORNER PANEL.

Part: SUPPORT ANGLE — CORRODED (THRESHOLD) · airframe 44,569 hrs · 27,700 cycles

AFT CARGO DOOR LOWER THRESHOLD Z ANGLE SUPPORT HAS CORROSION ON UPPER SURFACE....R&R AFT CARGO DOOR LOWER THRESHOLD Z ANGLE SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-73) · airframe 44,569 hrs · 27,700 cycles

AFT CARGO RT FLOOR SILL CORRODED FROM FRAMES 68 - 73 ON UPPER SURFACE. R & R THE FLOOR SILLS.

Part: SUPPORT ANGLE — CRACKED (FRAME 66) · airframe 44,569 hrs · 27,700 cycles

AFT CARGO DOOR LOWER THRESHOLD 'T' PROFILE AT FRAME 66 LOWER ANGLE SUPPORT IS CRACKED-REMOVED DAMAGED ANGLE, LOCATED AND DRILLED AND INSTALLED NEW ANGLE.

Part: ALTIMETER — CORRODED (RADIO) · airframe 44,569 hrs · 27,700 cycles

CORROSION UNDER AFT RADIO ALTIMETER AFT OF WING....PREFORMED REPAIR ON AFT RADIO ALTIMETER SKIN I/A/W EO-EMB145-53-068-O.

Part: ALTIMETER — CORRODED (RADIO) · airframe 44,569 hrs · 27,700 cycles

CORROSION UNDER FWD RADIO ALTIMETER AFT OF WING....PREFORMED REPAIR ON FWD RADIO ALTIMETER SKIN I/A/W EO-EMB145-53-069-O.

Part: STRUCTURE — CRACKED (E/E BAY DOOR) · airframe 44,569 hrs · 27,700 cycles

AFT AVIONICS DOOR 272DR IS CRACKED UNDER HINGE BRACKET- CUT OUT DAMAGED AREA, FABRICATED FILLER, SHIM AND DOUBLER.LOCATED AND DRILLED UP ALL NEW PARTS. INSTALLED ALL NEW PARTS.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 44,569 hrs · 27,700 cycles

R/H WING I/B UPPER SURFACE AT FR 41 BELLY FAIRING L ANGLE SUPPORT BRACKET IS CRACKED....R&R R/H UPPER WING L ANGLE AT FR 41

Part: HINGE BRACKET — CRACKED (FLOOR HATCH) · airframe 44,569 hrs · 27,700 cycles

COCKPIT UNDER FLOOR HATCH 123BL IS CRACKED UNDER HINGE BRACKET- REPAIRED HATCH DOOR.

Part: WHEEL — OUT OF ADJUST (NLG) · airframe 43,523 hrs · 26,858 cycles

NOSE WHEEL PULLS HARD TO RIGHT ON TAKE OFF. MADE ADJUSTMENT TO THE LOAD POT AND CENTERED NLG TIRES. TAXI CHECKED WITH CREW. OPS CHECK GOOD.

Part: FILTER — DIRTY (BLEED AIR SYS) · airframe 41,224 hrs · 24,963 cycles

BLD 2 OVERTEMP IN ICING CONDITIONS FOLLOWED QHR AND THEN A BLD 1 OVER TEMP. CLEANED E2 FAN AIR VALVE FILTER. PERFORMED ENG RUNS WITH CREW. OPS CHECK NORMAL.

Part: FILTER — DIRTY (FAN AIR VALVE) · airframe 41,206 hrs · 24,945 cycles

BLEED NR 2 OVERTEMP IN FLIGHT. CLEANED FAN AIR VALVE FILTER. NO FURTHER DEFECTS NOTED AT THIS TIME. FLT 4616.

Part: YOKE — CRACKED (LT NACELLE) · airframe 40,366 hrs · 24,246 cycles

LH ENG FWD MOUNT LOWER YOKE FITTING IS CRACKED. R & R LH ENG FWD MOUNT LOWER YOKE FITTING.

Part: YOKE — CRACKED (RT NACELLE) · airframe 40,366 hrs · 24,246 cycles

RH ENG FWD MOUNT LOWER YOKE FITTING IS CRACKED. R & R RH ENG FWD MOUNT LOWER YOKE FITTING.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,393 hrs · 23,428 cycles

PAX DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE BULB, OPS CHECKED GOOD.

Part: DUCT — UNSECURE (A/C PACK) · airframe 39,173 hrs · 23,242 cycles

RAPID CABIN DEPRESSURIZATION, WHILE CLIMBING OUT OF FL 180. SECURED SEVERAL DUCTS ON BOTH PACKS AND PERFORMED A PRESURIZATION CHECK IAW AMM 21-31-00. OPS CHECKED GOOD.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 38,591 hrs · 22,774 cycles

UNABLE TO CONTROL CABIN ALTITUDE WITH MANUAL CONTROLLER. TIGHTENED LINES AND CLAMP TO ELEC PNEUM VALVE IAW AMM 21-31-03. OPS CHECK GOOD AT THIS TIME.

Part: COUPLING — DAMAGED (CABIN PRESSURE) · airframe 37,445 hrs · 21,811 cycles

CABIN DEPRESSURIZED IN FLIGHT, LOST MANUAL PRESSURIZATION CONTROL AT 28,000 FT. INSPECTED AND FOUND BLOWN COUPLING ON PACK 2. RESECURED COUPLING AND PERFORMED PRESURIZSATION CHECK. PRESSURE CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,967 hrs · 21,413 cycles

EMERGENCY EXIT AISLE FLOOD LIGHT AT ROW 3, LIGHT 16A IS INOPERATIVE. R & R EMERGENCY EXIT AISLE FLOOD LIGHT BULB AT ROW 3. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,830 hrs · 21,281 cycles

PASSENGER DOOR EMEGENCY FLOOD LIGHT NR 1 INOPERATIVE. R & R PASSENGER DOOR EMERGENCY FLOOD LIGHT BULB. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,830 hrs · 21,281 cycles

R & R BULB ON SERVICE DOOR, EMERGENCY FLOOD LIGHT. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,578 hrs · 21,073 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED MAIN DOOR EXTERNAL EMERGENCY LIGHT BULB, OPS CHECK GOOD.

Part: SEAL — WORN (PAX DOOR) · airframe 36,329 hrs · 20,876 cycles

LOUD SQUEAL FROM PAX DOOR WITH ABNORMAL PRESSURIZATION. R & R MAIN CABIN DOOR SEAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,298 hrs · 20,851 cycles

SERVICE DOOR EMERGENCY LIGHT, NR 2 IS INOPERATIVE. R & R SEVICE DOOR EMERGENCY LIGHT NR 2. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,140 hrs · 20,712 cycles

SERVICE DOOR EMERGENCY FLOOD LIGHT NR 2 INOPERATIVE. R & R SERVICE DOOR EMERGENCY FLOOD LIGHT BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,140 hrs · 20,712 cycles

PAX DOOR EMERGENCY FLOOD LIGHT NR 1 INOPERATIVE. R & R PAX DOOR EMERGENCY FLOOD LIGHT BULB. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,936 hrs · 20,555 cycles

PAX DOOR EMERGENCY FLOOD LIGHT NR 1 INOPERATIVE. MAINTENANCE REPLACED LIGHT, OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,877 hrs · 20,506 cycles

SERVICE DOOR EMERGENCY FLOOD LIGHT NR 2 INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,479 hrs · 20,228 cycles

PASSENGER DOOR FLOOD LIGHT NR 1 IS INOPERATIVE. MAINTENANCE REPLACED LIGHT, OPS CHECK GOOD.

Part: WIRE HARNESS — SHORTED (MLG) · airframe 34,696 hrs · 19,628 cycles

LANDING GEAR AIR GROUND FAIL MSG DURING CLIMB, RETURNED TO BLOCK. MAINTENANCE REPLACED NOSE LANDING GEAR WOW HARNESS W019, OPS CHECK GOOD. PERFORMED MAINTENANCE CHECK FLIGHT, NO DEFECTS NOTED.

Part: PROXIMITY SWITCH — INOPERATIVE (MLG) · airframe 34,696 hrs · 19,628 cycles

LANDING GEAR FAIL IN FLT DURING CLIMB, RETURN TO BLOCK. MAINTENANCE REPLACED NOSE WOW PROXIMITY SWITCH, OPS CHECK GOOD AND LANDING GEAR EXTENSION/RETRACTION OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (PITCH TRIM) · airframe 34,696 hrs · 19,628 cycles

PITCH TRIM MAIN INOPERATIVE IN FLIGHT DURING CLIMB, RETURNED TO BLOCK. MAINTENANCE PERFORMED OPS CHECK OF PITCH TRIM SYS, NO DEFECTS NOTED, OPS CHECK GOOD.

Part: ACTUATOR — INOPERATIVE (HORIZONTAL STAB) · airframe 34,696 hrs · 19,628 cycles

MAIN PITCH TRIM INOP EICAS MSG DURING CLIMB, RETURNED TO BLOCK. MAINTENANCE REPLACED HORIZONTAL STABILIZER ACTUATOR, OPS CHECK GOOD. PERFORMED MAINTENANCE FLIGHT CHECK, NO DEFECTS NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,695 hrs · 19,626 cycles

NR 4 EMERGENCY BATTERY INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECK GOOD.

Part: SLEEVE — LOOSE (AC PACK) · airframe 34,280 hrs · 19,355 cycles

THE CREW REPORTED THAT THE NR 2 PACK AUTO SHUTOFF NUMEROUS TIMES DURING FLIGHT, AND A BURNING ODOR. THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT, SECURED A LOOSE SLEEVE ON THE NR 2 PACK, OPS TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,234 hrs · 19,325 cycles

DURING MAINTENANCE INSPECTION THE LT OVERWING EXIT IDENTIFIER ON THE EXIT DOOR SHROUD WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 5 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 33,052 hrs · 18,554 cycles

F/A REPORTED A LAV SMOKE DETECTOR ALARM DURING APPROACH. MX RESET THE LAV SMOKE DETECTION SYS AND PERFORMED THE LAV SMOKE TEST. OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (NLG DOORS) · airframe 27,895 hrs · 15,225 cycles

CREW REPORTED THE NLG DOORS ATTEMPTED TO OPEN TWICE DURING CRUISE FLIGHT. MX R & R THE RT MLG NR 1 UPLOCK PROXIMITY SWITCH WITH OPS CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — UNKNOWN (NLG DOORS) · airframe 27,883 hrs · 15,216 cycles

CREW REPORTED NOSE GEAR DOORS ATTEMPTED TO OPEN ON APPROACH TWO TIMES WITH GEAR SELECTED IN UP POSITION. SOUND ONLY, NO INDICATION. MX PERFORMED GVI OF NLG AREA AND PERFORMED LANDING GEAR EXTENSION AND RETRACTION. OPS CHECKED SUCCESSFUL WITH NO FAULTS FOUND. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (NR 2) · airframe 27,869 hrs · 15,206 cycles

THE CREW REPORTED SMOKE VISIBLE IN CABIN AT 6000 FT. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX REPLACED THE NR 2 ENGINE, OPS CHECKED GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 27,785 hrs · 15,150 cycles

ON DEPARTURE AT 3000FT, SMOKE IN CABIN BETWEEN ROW 3 & 4 REPORTED. MX DROPPED PSU PANELS INSPECTED AREA, ELECTRICAL WIRING, BALLASTS, LIGHTS AND FOUND NO EVIDENCE OF ARCING OR ELECTRICAL SHORTS. PERFORMED SUCCESSFUL OPS CHECKS OF CABIN LIGHTNING WITH NO EVIDENCE OF HEAT OR SMOKE AND COULD NOT DUPLICATE. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 27,491 hrs · 14,953 cycles

CREW REPORTED A BAGGAGE SMOKE INDICATION IN FLIGHT. BOTTLES WERE DISCHARGED AND ACFT PERFORMED AIR RETURN WITHOUT INCIDENT. NO EVIDENCE OF SMOKE OR FIRE NOTED BY FIRE PERSONNEL AFTER LANDING. MX R & R THE NR 1 BAGGAGE SMOKE DETECTOR WITH OPS CHECKS SUCCESSFUL. ALSO BOTH THE MAIN AND METERED BAGGAGE FIRE BOTTLES WERE REPLACED SINCE BOTH WERE DISCHARGED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 26,944 hrs · 14,601 cycles

DURING ROUTINE MX THE EMERGENCY EXIT SIGN ON CEILING WAS INOPERATIVE. MX REPLACED THE EXIT SIGN AND OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,692 hrs · 14,447 cycles

MX REPORTED THE SERVICE DOOR EMERGENCY LIGHT WAS INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT BULB. OPS CHECKS WERE GOOD.

Part: CONTACTOR — INOPERATIVE (FUEL SYSTEM) · airframe 20,552 hrs · 10,911 cycles

IAH - FLIGHT 2288, THE CREW REPORTED THAT FUEL PUMP 2B STAYED ON EVEN WHEN CROSSFEED LOW 2, 2A, OR 2C WERE SELECTED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FUEL PUMP 2B CONTACTOR K0121, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANTENNA — MALFUNCTIONED (WEATHER RADAR) · airframe 18,957 hrs · 10,043 cycles

MCI - FLIGHT 2848, THE CREW REPORTED THAT THE WEATHER RADAR WAS INTERMITTENT. THE AIRCRAFT DIVERTED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RADAR ANTENNA, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MOUNT FLANGE — CORRODED (NACELLE) · airframe 18,600 hrs · 9,842 cycles

TYS - AIRCRAFT CURRENTLY IN A C-CHECK STATUS, INSPECTION FOUND CORROSION IN BOTH LEFT AND RIGHT INLET MOUNTING FLANGES. MAINTENANCE REAMED THE HOLES AND REPLACED BUSHINGS IAW EC 5420-01158. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FUEL CONTROL — FAULTY

IAH - FLIGHT 2187 - THE CREW REPORTED A "FUEL XFER INOP" MESSAGE ON THE EICAS IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RELEASED THE AIRCRAFT IAW MEL 28-21-12. MAINTENANCE REPLACED THE VENTRAL FUEL CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD. (A)

Part: NONE — NONE · airframe 15,769 hrs · 8,374 cycles

FLIGHT 1245 - EWR - FLIGHT CREW REPORTED SPS FAIL DURING PRE-FLIGHT TEST AND SMELLED SMOKE AFTER TEST. EWR MX PERFORMED OPERATIONAL CHECK OF SPS SYSTEM AND NO ABNORMALITIES WERE FOUND. FURTHER TROUBLESHOOTING FOUND EXTERNAL AIR CONDITIONING CART BAD. MX THEN PERFORMED OPERATIONAL CHECK OF AIR CONDITIONING SYSTEM SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 14,429 hrs · 7,696 cycles

RIC: DURING A ROUTINE MX INSPECTION, SEAT 12A LOWER SIDEWALL EMERGENCY EXIT LIGHT FOUND INOP. REPAIR SECURED SEAT 12A LOWER SIDEWALL EMERGENCY EXIT LIGHT CONNECTOR IAW EMB145XR AMM 33-50-13. OPS CHECK GOOD. A/C APPROVED FOR RETURN TO SERVICE.

Part: STRIP — LOOSE (CABIN) · airframe 14,410 hrs · 7,685 cycles

CLE FLIGHT NR 2297, THE CREW REPORTED THE EMERGENCY LIGHT STRIP AT THE GALLEY WAS LOOSE. MAINTENANCE INSPECTED AND RESECURED LIGHT STRIP AT THE GALLEY IAW FCD 3350-01003. OPERATIONAL CHECKS WERE GOOD.

Part: PANEL — DEBONDED · airframe 13,904 hrs · 7,419 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND PANEL 197 DR WITH DEBONDED BONDING PLATE. MAINTENANCE REPAIRED PANEL 197 DR BONDING PLATE IAW EC5750-01315 REV E. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PANEL — DEBONDED · airframe 13,904 hrs · 7,419 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND PANEL 197CL WITH DEBONDED BONDING PLATE. MAINTENANCE REPAIRED PANEL 197CL IAW EC 5750-01315 REV E. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SELECTOR — INOPERATIVE (COCKPIT) · airframe 13,846 hrs · 7,390 cycles

BJX - FLIGHT 2193, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE, AND THE GEAR WAS STUCK DOWN AFTER T/O. THE AIRCRAFT RETURNED TO BJX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND IT WAS FERRIED TO IAH WHERE IT LANDED WITHOUT INCIDENT. IAH MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR LEVER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (MLG) · airframe 13,846 hrs · 7,390 cycles

BJX - FLIGHT 2193, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE, AND THE GEAR WAS STUCK DOWN AFTER T/O. THE AIRCRAFT RETURNED TO BJX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND IT WAS FERRIED TO IAH WHERE IT LANDED WITHOUT INCIDENT. IAH MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, (LGEU), OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — FAULTY (CABIN) · airframe 13,706 hrs · 7,310 cycles

DURING ROUTINE MAINTENANCE THE AFT OVERHEAD EXIT SIGN WAS ONLY PARTIALLY ON. MAINTENANCE INSPECTED AND REPLACED THE NR 6 INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — FAULTY (EMERGENCY LIGHTS) · airframe 13,706 hrs · 7,310 cycles

DURING ROUTINE MAINTENANCE THE RIGHT EMERGENCY EXIT SIGN DID NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE NR 5 INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,439 hrs · 7,172 cycles

FLT 2246 - CHS - CREW REPORTED EMERGENCY EXIT LIGHT OVER SEAT 12C NOT WORKING. MX REMOVED AND REPLACED LIGHT BULB IAW EMB145 AMM 33-50-14 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 11,955 hrs · 6,372 cycles

MKE FLIGHT NR 2745 THE CREW REPORTED A ELECTRICAL BURNING SMELL IN THE COCKPIT AND CABIN UPON LANDING. MAINTENANCE INSPECTED CIRCUIT BREAKERS AND RELAYS AND FOUND NO DEFECTS. RAN THE ENGINES WITH BLEEDS ON AND NO ODOR WAS DETECTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACTUATOR — INOPERATIVE (PITCH TRIM) · airframe 10,902 hrs · 5,816 cycles

IAH - FLIGHT 2422, THE CREW REPORTED A MAIN PITCH TRIM INOP DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER ACTUATOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 7,653 hrs · 4,098 cycles

CLE FLIGHT NR 2468, THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHT STRIP WAS MISSING AT GALLEY. MAINTENANCE INSPECTED AND REPLACED THE LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 7,092 hrs · 3,786 cycles

THE CREW REPORTED SMOKE IN THE CABIN AT FL 200 FOLLOWED BY A LAV SMOKE WARNING. THEY ALSO REPORTED SMOKE IN THE COCKPIT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD. THE NR 4 CARBON SEAL WAS FOUND DETERIORATED CAUSING OIL TO LEAK BY.

Part: THERMOSTAT — INOPERATIVE (NR 2 ENGINE) · airframe 6,215 hrs · 3,322 cycles

DURING CLIMBING, BLEED 2 OVERTEMP LIT UP, THEN BLEED 1 OVERTEMP LIT UP TOO. ICE COND MSG ON EICAS, A/I INOP (ANTI ICE)IN EICAS TOO. CREW PERFORMED AIR RETURN TO RIC. RIC MX PERFORMED TROUBLESHOOTING AND FOUND THERMOSTAT INOP. MX REMOVED AND REPLACED FAN AIR CONTROL THERMOSTAT AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 5,567 hrs · 2,982 cycles

CLE - THE CREW REPORTED THE AISLE PATH LIGHTING STRIP WAS MISSING. MAINTENANCE INSPECTED AND INSTALLED THE AISLE PATH LIGHTING STRIP COVER. OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 4,775 hrs · 2,548 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 4,775 hrs · 2,548 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145XR SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.