N844HK

Part: SKIN — DISTORTED (FRM19-20 S11-12L) · airframe 29,924 hrs · 27,714 cycles

DISCREPANCY - LEFT HAND SIDE FUSELAGE JUST AFT OF ENTRY DOOR AND FORWARD OF REPAIR HAS "OIL CANNING" AND DISTORTION THAT IS APPROXIMATELY 2 INCH'S SQUARE. CORRECTIVE ACTION - REPAIRED LEFT HAND SIDE FUSELAGE JUST AFT OF ENTRY DOOR IN ACCORDANCE WITH EMB 145 SRM 51-75-00. THE DAMAGE REPAIR WAS CLASSIFIED AS A MAJOR REPAIR AND IS LOCATED ON THE CENTER FUSELAGE I, LEFT HAND FUSELAGE SKIN BETWEEN FRAMES FR19L & FR20L AND STRINGERS STR11L & STR12L.

Part: COUPLING — DISCONNECTED (TEMP CONTROLLER) · airframe 28,943 hrs · 26,827 cycles

PAC #1 VALVE CLOSED IN FLIGHT. FOUND DISCONNECTED COUPLING AT DUEL TEMP CONTROLLER. RECONNECTED COUPLING AND PERFORMED OPS CHECK. LEAK CHECK OF PACK 1 OPS CHECK GOOD AT THIS TIME.

Part: SEAL — DAMAGED (WINDSHIELD) · airframe 28,404 hrs · 26,343 cycles

RETURN FROM FLIGHT DUE TO BANGING ON OUTSIDE OF AIRCRAFT. POSSIBLE CAPT WINDSHIELD SEAL TORN. INSPECTED AND FOUND BANGING TO BE COMING FROM CAPT'S HUMPSEAL. DEFERED HUMPSEAL. MORE INFORMATION PROVIDED WHEN AVAILIBLE. SUPPLIMENTAL INFORMATION FROM FIRST ENTRY. REPAIRED CAPT'S HUMP SEAL. DMI CLEARED.

Part: CONTROL SWITCH — FAILED (O2 SYSTEM) · airframe 27,886 hrs · 25,894 cycles

PAX 02 MASK DO NOT DEPLOY DURING FUNCTION CHECK. R&R ALTITUDE PRESSURE SWITCH.

Part: FIREWALL — CRACKED (APU BAY) · airframe 27,886 hrs · 25,894 cycles

APU FIREWALL IS CRACKED @ RT SIDE @ 2:00 O'CLOCK POSITION- FOUND SMALL CRACK IN RT APU FIREWALL AREA AND STOP DRILLED CRACK. FABRICATED DOUBLER TO BE INSTALLED OVER STOP DRILLED CRACK ON APU, INSTALLED DOUBLER.

Part: FLOOR SUPPORT — CORRODED (FRAMES 36-38) · airframe 27,886 hrs · 25,894 cycles

CENTER OMEGA BEAM UPPER RH MATING FLANGE HAS CORROSION FROM FRAME 36 THRU 38- REMOVED CORROSION FROM CENTER OMEGA BEAM GUSSET FROM FR36 TO FR38, IT IS BEYOND ALLOWABLE LIMITS. .022" WAS REMOVED. R&R CENTER OMEGA BEAM GUSSET AT FR36-38.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,886 hrs · 25,894 cycles

AFT FUSELAGE RT SIDE AT FR 78 BELOW STG 3R SHOWS SIGNS OF A CRACK. PERFORMED HFEC INSPECTION OF INDICATED AREA CRACK CONFIRMED. REMOVED DAMAGED AREAS AROUND CRACKED RIVET ON RT SIDE AT FR 78 BELOW STR 3R AND STARTED MAKING BUSHING. REPAIRED CRACKED AREA ON RT SIDE AT FR 78 BELOW STR 3R.

Part: FIREWALL — CRACKED (APU BAY) · airframe 27,886 hrs · 25,894 cycles

APU FIREWALL IS CRACKED AT RT SIDE AT 1:00 O'CLOCK POSITION. FOUND CRACKED AREA AROUND RIVET IN PROFILE AREA. FABRICATED DOUBLER AND FILLER TO MAKE FINAL REPAIR. REMOVED CRACKED AREA AROUND UPPER PROFILE RIVET AREA. INSTALLED FILLER AND DOUBLER FOR FINAL REPAIR OF DAMAGED AREA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,886 hrs · 25,894 cycles

MAIN CABIN FRAME 58 LT SHEAR CLIP IS CRACKED AT STR 15L. REMOVED CRACKED SHEER CLIP AT FR 58 LT & STR 15L. INSTALLED NEW SHEAR CLIP AT FRAME 58 LT STRINGER 15.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,886 hrs · 25,894 cycles

AFT FUSELAGE LT SIDE AT FR 79 STR 3L SHOWS SIGNS OF A CRACK. PERFORMED KF EC INSPECTION OF INDICATED AREA. CRACK CONFIRMED. REMOVED DAMAGED AREAS AROUND RIVETS AT FR 79 STR 3L AND MADE BUSHING. REPAIRED CRACKED AREAS ON AFT FUSELAGE LT SIDE AT FR 79 STR 3L.

Part: FLOOR SUPPORT — CORRODED (FRAMES 48-49) · airframe 27,886 hrs · 25,894 cycles

CENTER OMEGA BEAM LH LOWER MATING FLANGE HAVE CORROSION FROM FRAME 48 TO 49- BEGAN REMOVING FASTENERS FROM CENTER OMEGA BEAM BY FR48-FR49. REMOVED OMEGA BEAM, CENTER, BY FR48-FR49 & BEGAN DRILLING HOLES. FINISHED INSTALLING THE NUTPLATES ON CENTER OMEGA BEAM FROM FR48-49.

Part: FLOOR SUPPORT — CORRODED (FRAMES 69-71) · airframe 27,886 hrs · 25,894 cycles

CARGO BAY L/H AFT SILL FROME FRAMES 69-71 HAS CORROSION....REMOVED AND REPLACED CARGO L/H SILL AT FR 69-71.

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-68) · airframe 27,886 hrs · 25,894 cycles

CARGO BAY R/H SILL AT FRAMES 65-68 HAS CORROSION....REMOVED AND REPLACED R/H CARGO SILL AT FR 65-68.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 27,886 hrs · 25,894 cycles

L/H WING I/B UPPER SURFACE AT L/E BELLY FAIRING NUTPLATE SUPPORT ANGLE AT FR 39 IS CRACKED....REMOVED & REPLACED SUPPOT ANGLE AT FR 39.

Part: FLOOR SUPPORT — CORRODED (FRAMES 20-23) · airframe 27,886 hrs · 25,894 cycles

L/H OMEGA BEAM UPPER DIGITAL SUPPORT HAVE CORROSION FROM FRAME 20 THRU 23....REMOVED AND REPLACED L/H OMEGA BEAM UPPER DIGITAL SUPPORT AT FRAME 20 THRU 23.

Part: FLOOR SUPPORT — CORRODED (FRAMES 30-36) · airframe 27,886 hrs · 25,894 cycles

CENTER OMEGA BEAM UPPER GUSSET HAVE CORROSION FROM FRAME 30 THRU 36....REMOVED AND REPLACED CENTER OMEGA BEAM UPPER GUSSET AT FRAME 30 THRU 36

Part: FLOOR SUPPORT — CRACKED (FRAME 52) · airframe 27,886 hrs · 25,894 cycles

FLOOR SUPPORT IS CRACKED AT FRAME 52 BETWEEN CENTER AND R/H OMEGA BEAM....REMOVED AND REPLACED FLOOR SUPPORT AT FRAME 52 BETWEEN CENTER AND R/H OMEGA BEAM.

Part: FLOOR SUPPORT — CORRODED (FRAMES 23-24) · airframe 27,886 hrs · 25,894 cycles

L/H FLOOR SILL SPLICE BETWEEN FR 23 & 24 IS CRACKED....REMOVED AND REPLACED L/H FLOOR SILL SPLICE AT FR 23 & 24

Part: FLOOR SUPPORT — CORRODED · airframe 27,886 hrs · 25,894 cycles

L/H OMEGA BEAM RAMP ANGLE SUPPORT ABOVE OMEGA BEAM REPAIR DOUBLER HAVE CORROSION....REMOVED AND REPLACED L/H OMEGA BEAM RAMP ANGLE SUPPORT ABOVE OMEGA BEAM REPAIR DOUBLER.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 27,886 hrs · 25,894 cycles

RT ELEVATOR UPPER SKIN IS CRACKED AROUND HINGE NR 2 CUTOUT AT YH-1310. REPAIRED CRACKED SKIN ON RT ELEVATOR AT YH-1310.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 27,886 hrs · 25,894 cycles

LT ELEVATOR UPPER SKIN IS CRACKED AROUND HINGE NR 2 CUTOUT AT YH-1310. REPAIRED CRACK SKIN AT YH-1310.

Part: FLOOR SUPPORT — CRACKED (FRAMES 20-21) · airframe 27,886 hrs · 25,894 cycles

CENTER OMEGA BEAM BETWEEN FR 20 & 21 L ANGLE IS CRACKED. R&R CENTER OMEGA BEAM BETWEEN FR 20 & 21.

Part: ANGLE — CRACKED (FRAME 47) · airframe 27,886 hrs · 25,894 cycles

R/H OVERWING FAIRING "L" ANGLE IS CRACKED AT FRAME 47....REMOVED AND REPLACED "L" ANGLE AT FRAME 47.

Part: FLOOR SUPPORT — DAMAGED (FRAMES 48-49) · airframe 27,886 hrs · 25,894 cycles

L/H CENTER OMEGA BEAM LOWER SUPPORT ANGLE IS DAMAGED AT FR 48 & 49....REMOVED AND REPLACED L/H CENTER OMEGA BEAM LOWER SUPPORT AT FR 48 & 49.

Part: FITTING — CORRODED (FUSELAGE) · airframe 27,886 hrs · 25,894 cycles

L ANGLE CLIP HAS SIGN OF CORROSION UNDER RAMP ON FRAME 20. R&R L ANGLE CLIP.

Part: FLOOR SUPPORT — CRACKED (FRAMES 15-16) · airframe 27,886 hrs · 25,894 cycles

L/H OMEGA BEAM UPPER DIGITAL SUPPORT HAVE CRACKED BETWEEN FRAME 15 & 16....REMOVED AND REPLACED L/H OMEGA BEAM UPPER DIGITAL SUPPORT AT FRAME 15 & 16.

Part: CAP — CORRODED (LT MLG TRUNNION) · airframe 27,886 hrs · 25,894 cycles

LT MLG FWD TRUNION LOWER CAP HAS SIGNS OF CORROSION. R&R LT MLG FWD TRUNION CAP.

Part: CAP — CORRODED (RT MLG TRUNNION) · airframe 27,886 hrs · 25,894 cycles

RT MLG AFT TRUNION LOWER CAP HAS SIGNS OF CORROSION. R&R LT MLG FWD TRUNION CAP.

Part: FLOOR SUPPORT — CORRODED (FRAMES 30-36) · airframe 27,886 hrs · 25,894 cycles

CENTER OMEGA BEAM UPPER RH MATING FLANGE HAVE CORROSION FROM STA 30 THRU 36. R&R GUSSET AT FRAME 30 TO 36.

Part: FLOOR SUPPORT — CORRODED (FRAME 29) · airframe 27,886 hrs · 25,894 cycles

CENTER OMEGA BEAM UPPER RH MATING FLANGE HAVE CORROSION AT FRAME 29. R&R CENTER OMEGA BEAM GUSSET.

Part: FLOOR SUPPORT — CORRODED (FRAMES 36-39) · airframe 27,886 hrs · 25,894 cycles

L/H OMEGA BEAM R/H LOWER MATING FLANGE HAVE CORROSION FROM FRAME 36 THRU 39....REMOVED AND REPLACED L/H OMEGA BEAM AT FRAME 36 THRU 39

Part: FLOOR SUPPORT — CRACKED (FRAME 47) · airframe 27,886 hrs · 25,894 cycles

R/H OMEGA BEAM LOWER SUPPORT IS CRACKED AT FRAME 47....REPAIRED FWD AND AFT ANGLES AT FRAME 47.

Part: SEAT TRACK — WORN (FRAMES 36-46) · airframe 27,886 hrs · 25,894 cycles

L/H SIDEWALL SEAT TRACK FROM FRAME 36 THRU 46 WORN....REMOVED AND REPLACED L/H SIDEWALL SEAT TRACK FROME FRAME 36 THRU 46.

Part: FLOOR SUPPORT — CORRODED (FRAMES 25-29) · airframe 27,886 hrs · 25,894 cycles

RH FLOOR SILL HAVE CORROSION ON UPPER SURFACE FROM FRAME STA 25 THRU 29. R&R RH FLOOR SILL FROM FRAME 25 THRU 29.

Part: FLOOR SUPPORT — CORRODED (FRAMES 36-38) · airframe 27,886 hrs · 25,894 cycles

L/H OMEGA BEAM UPPER L/H MATING FLANGE IS CORRODED FROM FRAME 36 THRU 38....REMOVED AND REPLACED L/H OMEGA BEAM UPPER L/H MATING FLANGE.

Part: SUPPORT BRACKET — CRACKED (FRAME 43) · airframe 27,886 hrs · 25,894 cycles

MAIN CABIN FRAME 46 LOWER SUPPORT BRACKET IS CRACKED BELOW L/H SIDE FLOOR SILL....REMOVED AND REPLACED LOWER SUPPORT BRACKET BELOW L/H FLOOR SILL AT FS 46.

Part: FLOOR SUPPORT — CORRODED (FRAMES 45-46) · airframe 27,886 hrs · 25,894 cycles

L/H FLOOR SILL HAVE CORROSION ON UPPER SURFACE FROM FRAME 45 TO 46....REMOVED AND REPLACED L/H FLOOR SILL FROM FRAME 45 TO 46

Part: FLOOR SUPPORT — CORRODED (FRAME 50) · airframe 27,886 hrs · 25,894 cycles

LH OMEGA BEAM LOWER O/B SUPPORT HAVE CORROSION @ AFT END AT FRAME 50. R&R LH OMEGA BEAM O/B SUPPORT AT FRAME 50.

Part: DOOR SILL — CORRODED (CABIN) · airframe 27,886 hrs · 25,894 cycles

LT FLOOR SILL IS CORRODED ON UPPER SURFACE FROM FR 36 THRU 41. REMOVED AND REPLACED LT FLOOR SILL AT FR 36 THRU 41.

Part: SUPPORT BRACKET — CRACKED (FRAME 46) · airframe 27,886 hrs · 25,894 cycles

MAIN CABIN FRAME 46 LOWER SUPPORT BRACKET IS CRACKED BELOW LH SIDE FLOOR SILL. R & R LOWER SUPPORT BRACKET.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 27,886 hrs · 25,894 cycles

FRAME 24 RT SHEAR CLIP IS CRACKED AT STR 15R. R&R SHEAR CLIP.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 27,886 hrs · 25,894 cycles

RT FLOOR SILL HAVE CORROSION ON UPPER SURFACE FROM FRAME 36 THRU 41. REMOVED AND REPLACED FLOOR SILL AT FR 36 THRU 41 RT.

Part: FLOOR SUPPORT — CORRODED (FRAMES 30-35) · airframe 27,886 hrs · 25,894 cycles

LH FLOOR SILL HAVE CORROSION ON UPPER SURFACE FROM FRAME 30 THRU 35. R&R LH FLOOR SILL

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 27,886 hrs · 25,894 cycles

RT FLOOR SILL HAVE CORROSION ON UPPER SURFACE FROM FRAME 28 THRU 36. REMOVED AND REPLACED RT FLOOR SILL AT FR 28 THRU 36.

Part: FLOOR SUPPORT — CORRODED (FRAMES 30-36) · airframe 27,886 hrs · 25,894 cycles

L/H OMEGA BEAM UPPER L/H MATING FLANGE HAVE CORROSION FROM FRAME 30 THRU 36....REMOVED AND REPLACED L/H OMEGA BEAM UPPER L/H MATING FLANGE

Part: FLOOR SUPPORT — CORRODED (FRAMES 48-52) · airframe 27,886 hrs · 25,894 cycles

L/H FLOOR SILL HAVE CORROSION ON UPPER SURFACE FROM FRAME 48 THRU 52....REMOVED AND REPLACED L/H FLOOR SILL FROM FRAME 48 THRU 52.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,886 hrs · 25,894 cycles

CENTER OMEGA BEAM RT UPPER MATING FLANGE HAVE CORROSION FROM FRAME 38 TO 45. R&R CENTER OMEGA BEAM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 27,886 hrs · 25,894 cycles

FRAME 25 RT SHEAR CLIP IS CRACKED AT STR 15R. R&R SHEAR CLIP.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 27,886 hrs · 25,894 cycles

RT FLOOR SILL HAVE CORROSION ON UPPER SURFACE AT FR 53 THRU 55. REMOVED AND REPLACED FLOOR SILL AT FR 53 THRU 55 RT.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,886 hrs · 25,894 cycles

LT OMEGA BEAM RAMP ANGLE SUPPORT IS CRACKED AT FR 19. REMOVED AND REPLACED LT OMEGA BEAM ANGLE AT FR 19.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · corrosion level 2 · airframe 27,886 hrs · 25,894 cycles

RH FLOOR SILL AT FRAME 20 FWD OF SERVICE DOOR HAVE CORROSION AROUND FASTNER HOLES. R&R FLOOR SILL AT FR 20 RH.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 27,886 hrs · 29,894 cycles

LAV LT GUSSET BETWEEN FRAMES 58-61 HAS CORROSION. R&R LT GUSSET.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 27,886 hrs · 29,894 cycles

LAV CENTER GUSSET BETWEEN FRAMES 58-61 HAS CORROSION. R&R LT GUSSET.

Part: SUPPORT — CORRODED (FRAMES 61-65) · airframe 27,886 hrs · 25,894 cycles

CARGO BAY LH FWD SILL FROM FRAME 61-65 HAS CORROSION. R&R CARGO BAY LH FWD SILL @ FR 62-65.

Part: ANGLE — CORRODED (THRESHOLD) · airframe 27,886 hrs · 25,894 cycles

AFT CARGO DOOR LOWER THRESHOLD Z ANGLE HAVE CORROSION AROUND FASTNER HOLES. R&R AFT CARGO DOOR LOWER THRESHOLD Z ANGLE.

Part: SHEAR TIE — CRACKED (FRAME 65) · airframe 27,886 hrs · 25,894 cycles

AFT CARGO COMPARTMENT ABOVE CARGO DOOR FRAME 65 SHEER CLIP IS CRACKED BETWEEN STR 7 & 8....REMOVED AND REPLACED CRACKED SHEER CLIP BETWEEN STR 7 & 8.

Part: ATTACH BRACKET — CRACKED (FRAME 66) · airframe 27,886 hrs · 25,894 cycles

AFT CARGO DOOR LOWER THRESHOLD T PROFILE AT FRAME 66 LOWER L ANGLE BRACKET IS CRACKED UNDER DRILL HOLES....REMOVED AND REPLACE LOWER L ANGLE BRACKET AT FRAME 66.

Part: FLOOR SUPPORT — CORRODED (FRAMES 24-25) · airframe 27,886 hrs · 25,894 cycles

CENTER OMEGA BEAM UPPER SURFACE HAVE CORROSION FROM FRAME 24 THRU 25. R&R CENTER OMEGA BEAM GUSSET.

Part: FLOOR SUPPORT — CORRODED (FRAMES 18-23) · airframe 27,886 hrs · 25,894 cycles

CENTER OMEGA BEAM UPPER DIGITAL SUPPORT HAVE CORROSION FROM FRAME 18 THRU 23. R&R CENTER OMEGA BEAM UPPER DIGITAL SUPPORT.

Part: SUPPORT — CORRODED (FRAME 61) · airframe 27,886 hrs · 25,894 cycles

RH FLOOR SUPPORT BETWEEN RH OMEGA BEAM AND FUSELAGE AT FRAME 61 HAS CORROSION. R&R RH FLOOR SUPPORT BETWEEN RH OMEGA BEAM AND FUSELAGE @ FR 61.

Part: TEE FITTING — CRACKED (FRAME 66) · airframe 27,886 hrs · 25,894 cycles

AFT CARGO DOOR LOWER THRESHOLD T PROFILE AT FRAME 66 IS BENT AND CRACKED....REMOVED AND REPLACED CARGO DOOR LOWER THRESHOLD T PROFILE AT FRAME 66.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 27,886 hrs · 29,894 cycles

CENTER OMEGA BEAM RAMP SUPPORT ANGLE HAVE CORROSION AT FRAME 20. R&R CENTER OMEGA BEAM RAMP SUPPORT ANGLE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 23-29) · airframe 27,886 hrs · 25,894 cycles

L/H OMEGA BEAM UPPER SURFACE HAS CORROSION UNDER SEAT TRACK FROM FRAME 23 THRU 29....REMOVED AND REPLACED L/H OMEGA BEAM GUSSET FROM FRAME 23 THRU 29

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 27,886 hrs · 29,894 cycles

MAIN CABIN FRAME 16 SHEAR CLIP IS CRACKED AT STR 15R. R&R FRAME SHEAR CLIP.

Part: SHEAR TIE — CRACKED (FRAME 67) · airframe 27,886 hrs · 25,894 cycles

AFT CARGO COMPARTMENT L/H SIDE ABOVE CARGO DOOR AT FR 67 SHEER CLIP IS CRACKED AT STR 7 L/H....REMOVED AND REPLACED SHEER CLIP AT FS 67.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 27,886 hrs · 25,894 cycles

LT FLOOR SILL HAVE CORROSION ON UPPER SURFACE FROM 25 THRU 29. REMOVED AND REPLACED FLOOR SILL LT FROM 25 THRU 29.

Part: TEE FITTING — CRACKED (FRAME 67) · airframe 27,886 hrs · 25,894 cycles

AFT CARGO THRESHOLD LOWER T PROFILE AT FRAME 67 IS CRACKED....REMOVED AND REPLACED CARGO THRESHOLD LOWER T PROFILE AT FRAME 67.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 27,886 hrs · 25,894 cycles

LH FLOOR SILL HAVE CORROSION AT FRAME 20 ON UPPER SURFACE. R&R SILL AT FRAME 20

Part: SHEAR TIE — CRACKED (FRAME 68) · airframe 27,886 hrs · 25,894 cycles

AFT CARGO COMPARTMENT L/H SIDE ABOVE CARGO DOOR AT FR 68 SHEER CLIP IS CRACKED AT STR 7.... REMOVED AND REPLACED CRACKED SHEER CLIP AT FS68 STG 7 L/H.

Part: FLOOR SUPPORT — CORRODED (FRAMES 60-64) · airframe 27,886 hrs · 25,894 cycles

CARGO BAY RH SILL BETWEEN FRAMES 60-64 HAS CORROSION. R&R SILL.

Part: ATTACH BRACKET — BENT (FRAME 67) · airframe 27,886 hrs · 25,894 cycles

AFT CARGO DOOR TRESHOLD LOWER T PROFILE LOWER L ANGLE BRACKET AT FRAME 67 IS BENT WITH 4 OPEN UNDRILLED HOLES....REMOVED AND REPLACED LOWER L ANGLE AT FRAME 67.

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-68) · airframe 27,886 hrs · 25,894 cycles

AFT CARGO L/H OMEGA BEAM UPPER DIGTAL SUPPORT HAVE CORROSION BETWEEN 65 THRU 68....REMOVED AND REPLACED L/H OMEGA BEAM UPPER DIGITIAL SUPPORT AT 65 THRU 68.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 27,886 hrs · 25,894 cycles

MAIN CABIN FRAME 25 SHEAR CLIP IS CRACKED AT STR 15L. REMOVED AND REPLACED SHEAR TIE AT FR 25 STR 15L.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,886 hrs · 29,894 cycles

FWD CABIN STR 3 LT MACHINE FITTING END FINGER IS CRACKED AT FRAME 20. CUT OUT CRACKED EDGE. PERFORMED NDT. INSTALLED REPAIR ELEMENTS.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 27,886 hrs · 25,894 cycles

MAIN CABIN FRAME 24 SHEAR CLIP IS CRACKED AT STR 15L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 24 STR 15L.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 27,886 hrs · 25,894 cycles

L/H OMEGA BEAM HAS CORROSION ON PREVIOUS REPAIR DOUBLER AT FRAME 20....REMOVED AND REPLACED L/H DOUBLER AT FRAME 20.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 27,886 hrs · 25,894 cycles

L/H WING I/B UPPER SURFACE NUTPLATE SUPPORT "L" ANGLE BRACKET IS CRACKED AT FRAME 47....REMOVED AND REPLACED "L" ANGLE BRACKET ON L/H WING AT FR 47.

Part: SKIN — CRACKED (RT WING) · airframe 27,886 hrs · 25,894 cycles

R/H WING UPPER I/B SURFACE AT FRAME 48 NUTPLATE SUPPORT ON TOP OF WING IS CRACKED....REMOVED & REPLACED R/H UPPER I/B SURFACE ANGLE SUPPORT AT FRAME 48 ON TOP OF WING.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 27,886 hrs · 25,894 cycles

L/H WING UPPER SURFACE AT FR 46 NUTPLATE "L" ANGLE SUPPORT BRACKET IS CRACKED....REMOVED & REPLACED L/H "L" ANGLE AT FR 46 ON UPPER WING.

Part: SUPPORT BRACKET — CRACKED (PAX DOOR) · airframe 27,886 hrs · 25,894 cycles

PASSENGER DOOR INTERIOR DOOR HANDLE SUPPORT BRACKET IS CRACKED. R&R DOOR HANDLE BRACKET.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,886 hrs · 25,894 cycles

PASSENGER DOOR CUTOUT FWD LOWER CORNER UPPER DIGITAL FLOOR SUPPORT END ANGLE IS CRACKED AT FR 15 &STR 15L. REMOVED & REPLACED FLOOR SUPPORT ANGLE AT FR15 & STR 15L.

Part: SUPPORT BRACKET — CRACKED (NLG) · airframe 27,886 hrs · 25,894 cycles

NLG UPLOCK SUPPORT BRACKET IS CRACKED. R&R CRACKED SUPPORT BRACKET.

Part: CUP — CORRODED (TOILET DRAIN) · airframe 27,886 hrs · 25,894 cycles

AFT FUSELAGE INSIDE ACCESS 272AR TOILET DRAIN VALVE HAVE CORROSION BETWEEN DRAIN VALVE AND HOUSING & CORRODED HARDWARE. R&R TOILET DRAIN CUP AND HARDWARE.

Part: WEB — CRACKED (RT MLG WW) · airframe 27,886 hrs · 25,894 cycles

RH WHEEL WELL AFT WEB IS CRACKED IN 2 PLACES. R&R RH WHEEL WELL AFT WEB.

Part: BRACKET — CRACKED (FAIRING) · airframe 27,886 hrs · 25,894 cycles

CENTER BELLY FAIRING RH AFT L ANGLE BRACKET CRACKED. R&R L ANGLE BRACKET.

Part: BRACKET — CRACKED (RT OVERWING) · airframe 27,886 hrs · 25,894 cycles

RH OVERWING FAIRING L ANGLE BRACKET CRACKED. R&R BRACKET.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,811 hrs · 25,818 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,622 hrs · 25,628 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,634 hrs · 29,029 cycles

BOTH OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BULB, OPS CHECK GOOD.

Part: CLAMP — FAILED (BLEED DUCT) · airframe 24,117 hrs · 22,461 cycles

AFTER TAKEOFF, AT 500FT, NR 1 BLEED LEAK APPEARED ON EICAS, ACFT RETURNED. MAINTENANCE INSPECTED AND REPLACED DUCT CLAMPS, OPS AND LEAK CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,541 hrs · 21,925 cycles

RIGHT AFT WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,541 hrs · 21,925 cycles

LEFT AFT WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECKED GOOD.

Part: WIRE HARNESS — SHORTED (MLG) · airframe 23,406 hrs · 21,805 cycles

LANDING GEAR, AIR GROUND FAIL AFTER GEAR RETRACTION DURING CLIMB OUT, RETURN BLOCK. MAINTENANCE REPLACED NLG WIRING HARNESS AND OPS CHECK GOOD.

Part: WIRE — BROKEN (WOW SWITCH) · airframe 23,406 hrs · 21,804 cycles

LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS AFTER GEAR RETRACTION DURING CLIMB OUT, RETURN TO BLOCKS. MAINTENANCE INSPECTED AND REPAIRED WIRES IN THE LT FORWARD MLG WOW SWITCH CONNECTOR PLUG AND REPLACED THE SAME LOCATION CONNECTOR PLUG, OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,237 hrs · 21,652 cycles

RIGHT WING FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED RT WING FORWARD EMERGENCY EXIT BULB, OPS CHECKED GOOD.

Part: PROXIMITY SWITCH — FAILED (MLG) · airframe 23,054 hrs · 21,487 cycles

LANDING GEAR AIR GROUND FAIL AFTER TAKEOFF, GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED AND REPLACED NOSE WHEEL PROXIMITY SWITCH, RT MLG AFT PROXIMITY SWITCH AND THE LGEU, OPS CHECK GOOD.

Part: BUSS — FAILED (ESS) · airframe 22,839 hrs · 21,290 cycles

ESS BUSS 1 FAILED DURING CRUISE, EMERGENCY LANDING.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,760 hrs · 21,220 cycles

LEFT FWD WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT INOPERATIVE. MAINTENANCE REPLACED BULB AND OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,504 hrs · 20,994 cycles

AISLE FLOOD LIGHTS 16C AND 16D INOPERATIVE. MX REPLACED BULBS, OPS CHECKED GOOD.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 21,137 hrs · 19,800 cycles

THE CREW REPORTED RECEIVING A NR 2 ENGINE BLEED LEAK EICAS MESSAGE IN FLIGHT. MAINTENANCE FOUND THREE CLAMPS BLOWN OFF AND RE-SECURED THE CLAMPS. FOLLOW ON OPERATIONAL CHECKS OF THE BLEED SYSTEM WERE GOOD.

Part: SWITCH — MALFUNCTIONED (RT MLG) · airframe 20,810 hrs · 19,514 cycles

DURING CRUISE FLIGHT THE FLIGHT CREW GOT A LANDING GEAR AIR GROUND FAIL MESSAGE. AIRCRAFT MADE AN EMERGENCY LANDING AT STL. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE RIGHT MLG NR 2 WOW SWITCH. SYSTEM OPS CHECKED GOOD.

Part: SWITCH — FAULTY (RT MLG) · airframe 20,817 hrs · 19,518 cycles

DURING CRUISE, THE FLIGHT CREW RECEIVED A LANDING GEAR AIR GROUND FAILURE MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG NR 2 WOW SWITCH. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,796 hrs · 18,574 cycles

DURING MAINTENANCE INSPECTION, FOUND PASSENGER ENTRY CEILING EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE BULB IN THE PASSENGER ENTRY CEILING LIGHT, OPS CHECK GOOD.

Part: SCREW — MISSING (PAX DOOR) · airframe 19,566 hrs · 18,369 cycles

CREW COULD NOT OPEN MAIN PASSENGER DOOR DURING POST FLIGHT. MAINTENANCE INSPECTED AND FOUND A MISSING SCREW FROM A DOOR PANEL AND INSTALLED SCREW FOR DOOR PANEL AND OPS CHECK GOOD, DEFERRED PANEL DUE TO CRACKING FROM DOOR OPENING.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 18,910 hrs · 17,739 cycles

DURING CLIMB THE AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO STL. MAINTENANCE INSPECTED AND REPLACED THE PNEUMATIC OUTFLOW VALVE. SYSTEM OPS CHECKED GOOD.

Part: FASTENER — MISSING (PAX DOOR) · airframe 18,419 hrs · 17,305 cycles

DURING POST-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR WAS HARD TO OPEN. MAINTENANCE INSPECTED AND FOUND THE DOOR WAS BINDING ON THE MAIN DOOR LT SIDE PANEL. PANEL WAS LOOSE AND MISSING HARDWARE. MAINTENANCE RE-SECURED THE PANEL AND INSTALLED HARDWARE AS REQUIRED. DOOR OPS CHECKED GOOD.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE RAMP SUPPORT ANGLE ON CENTER BEAM FRAME 18-20 CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP SUPPORT ANGLE ON CENTER BEAM FRAME 18-20.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR SILL FROM FRAME 18-23 CORRODED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR SILL FROM FRAME 18-23.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE GUSSET ON RT BEAM IN LAV CORRODED. MAINTENANCE REMOVED AND REPLACED THE GUSSET ON RT BEAM IN LAV.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE CENTER GUSSET IN LAV CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER GUSSET IN LAV.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE CENTER BEAM BETWEEN FRAMES 59-60 CORRODED. MAINTENANCE REPAIR THE CENTER BEAM BETWEEN FRAMES 59-60.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE LT "T" PROFILE UNDER COMPOSIT RING CORRODED. MAINTENANCE REMOVED AND REPLACED THE LT "T" PROFILE UNDER COMPOSIT RING.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE GUSSET ON LT BEAM IN LAV CORRODED. MAINTENANCE REMOVED AND REPLACED THE GUSSET ON LT BEAM IN LAV.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE AFT ANGLE ON AFT SERVICE DOOR SILL AT FRAME 24 CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT ANGLE ON AFT SERVICE DOOR SILL AT FRAME 24.

Part: REPAIR — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE PREVIOUS REPAIR ON BEAM Y-479 FROM FRAMES 18-20 CORRODED. MAINTENANCE REMOVED AND REPLACED THE PREVIOUS REPAIR ON BEAM Y-479 FROM FRAMES 18-20.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE DOUBLER AT FRAME 22 ON BEAM Y-479 CORRODED. MAINTENANCE REMOVED AND REPLACED THE DOUBLER AT FRAME 22 ON BEAM Y-479.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE FWD SHEAR CLIP IN CARGO DOOR CUTOUT AT FRAME 65 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FWD SHEAR CLIP IN CARGO DOOR CUT OUT AT FRAME 65.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE SERVICE DOOR SILL PLATE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR SILL PLATE.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE PASSENGER DOOR ENTRY WAY U-SHAPES CORRODED. MAINTENANCE REMOVED AND REPLACED PASSENGER DOOR ENTRY WAY U-SHAPES.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE GUSSET ON CENTER BEAM AT FRAME 20-23 CORRODED. MAINTENANCE REMOVED AND REPLACED THE GUSSET ON CENTER BEAM AT FRAME 20-23.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE SPLICE ANGLE CONNECTING CENTER 1 FUSELAGE FLOOR SILL AND CENTER 2 FUSELAGE SILL CORRODED. MAINTENANCE REMOVED AND REPLACED THE SPLICE ANGLE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE FWD DIGITAL FRAMES 14-18 CORREDED. MAINTENANCE REMOVED AND REPLACED FWD DIGITAL FRAMES 14-18.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE DOUBLER AT FRAME 20 ON BEAM Y-479 CORRODED. MAINTENANCE REMOVED AND REPLACED THE DOUBLER AT FRAME 20 ON BEAM Y-479.

Part: SILL — CORRODED (AFT SERVICE DOOR) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION, MAINTENANCE FOUND THE AFT SERVICE DOOR SILL CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT SERVICE DOOR SILL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE LEFT DIGITAL ON FRAMES 19-23 CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT DIGITAL ON FRAMES 19-23.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE RAMP SUPPORT ANGLE FROM FRAMES 18-19 CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP SUPPORT ANGLE FROM FRAMES 18-19.

Part: MOUNT — CORRODED (LAVATORY) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE LAV FLOOR TO PEDESTAL HAS 4 EACH MOUNTS CORRODED. MAINTENANCE REMOVED AND REPLACED THE LAV FLOOR TO PEDESTAL MOUNTS.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE AFT SHEAR CLIP IN CARGO DOOR CUT OUT AT FRAME 68 CORRODED. MAINTENANCE REPAIRED THE AFT SHEAR CLIP IN CARGO DOOR CUTOUT AT FRAME 68.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,306 hrs · 17,196 cycles

DURING HEAVY CHECK INSPECTION MAINTENANCE FOUND THE CARGO DOOR CUTOUT LOWER BEAM CORREDED. MAINTENANCE REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER BEAM.

Part: PACKING — FAILED (NLG STRUT) · airframe 16,524 hrs · 15,566 cycles

LANDING GEAR AIR/GND FAIL MESSAGE ON EICAS. MAINTENANCE TROUBLESHOT, DISCOVERED NLG STRUT NOT CENTERING. REPACKED NLG STRUT, OPS CHECK GOOD IAW EMB 145 AIRCRAFT MAINTENANCE MANUAL PROCEDURE.

Part: CONNECTOR — MALFUNCTIONED (NLG) · airframe 16,523 hrs · 15,564 cycles

DURING CLIMB THE EICAS HAD A AIR GROUND MESSAGE. AIRCRAFT RETURNED FROM FLIGHT. AIRCRAFT DID A FERRY FLIGHT TO STL. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE NLG WOW PROX SWITCH CONNECTOR. SYSTEM OPS CHECKED GOOD.

Part: SENSOR — MALFUNCTIONED (LT MLG) · airframe 16,523 hrs · 15,564 cycles

DURING CLIMB THE FLIGHT CREW GOT AN EICAS LANDING GEAR AIR FAIL MESSAGE. AIRCRAFT RETURNED FROM FLIGHT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE LT MLG WOW SENSOR. SYSTEM OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 16,390 hrs · 15,436 cycles

DURING CRUISE THE FLIGHT CREW REPORTED A STRONG SMELL OF BURNING WIRES COMING FROM THE COCKPIT RADOME AREA. MAINTENANCE INSPECTED WIRING AND HARNESSES THROUGH ACCESS PANELS FOR RADOME ZONE LT FORWARD ELECTRONIC BAY PANEL, 113CZ BELOW COCKPIT AREA ZONE 123 PANELS 123BL FLOOR COCKPIT 123 PANEL 221, NO ODOR OR DEFECTS DETECTED.

Part: INVERTER — MALFUNCTIONED (CABIN) · airframe 16,096 hrs · 15,173 cycles

DURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED EMERGENCY LIGHT INOP. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 4 INVERTER. SYSTEM OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 16,003 hrs · 15,092 cycles

DURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE OVERWING EMERGENCY EXIT LIGHT INOP. MAINTENANCE INSPECTED AND RESET THE SYSTEM. LIGHT OPS CHECKED GOOD.

Part: BOLT — BENT (PAX DOOR) · airframe 15,934 hrs · 15,035 cycles

DURING POST-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR WOULD NOT OPEN. MAINTENANCE INSPECTED AND FOUND THE PASSENGER DOOR HANDLE BOLT BENT. MAINTENANCE REMOVED AND REPLACED THE BOLT. SYSTEM OPS CHECKED GOOD.

Part: SOLENOID VALVE — FAULTY (LANDING GEAR) · airframe 15,700 hrs · 14,815 cycles

DURING LANDING APPROACH, THE CREW REPORTED THAT THE NOSE LANDING GEAR DID NOT EXTEND. MANUAL EXTENSION WAS REQUIRED. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SOLENOID VALVE IAW AMM PROCEDURES. FOLLOW ON EXTENSION AND RETRACTION CHECKS WERE GOOD.

Part: SENSOR — MALFUNCTIONED (LAVATORY) · airframe 15,577 hrs · 14,699 cycles

DURING TAKEOFF CREW GOT A LAV SMOKE INDICATION. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE LAV SMOKE DETECTOR SENSOR. SYSTEM OPS CHECKED GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 15,577 hrs · 14,699 cycles

DURING CRUISE THE FLIGHT CREW GOT A LAV SMOKE INDICATION. FLIGHT CREW CHECKED LAV AND FOUND NO SMOKE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE SMOKE DETECTION PANEL. SYSTEM OPS CHECKED GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 15,445 hrs · 14,571 cycles

DURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE EMERGENCY LIGHT STRIP AT SEAT 1A CAME LOOSE. MAINETNANCE INSPECTED AND RE-SECURED THE EMERGENCY LIGHT STRIP. SYSTEM OPS CHECKED GOOD.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 15,301 hrs · 14,431 cycles

DENT IN REAR FUSELAGE 1 BETWEEN FRAME 66 AND 69, STRINGER 20L AND 20R. REFER TO LOG PAGE 418087 DISC 1 FOR ORIGINAL DISCREPANCY. MAINTENANCE PERFORMED A TEMPORARY REPAIR BETWEEN FRAME 66 AND 69 IAW EMBRAER ETD 2010-145/09044. REPAIR WAS PAINTED. TEMPORARY REPAIR IS DMI 61852, RE-INSPECT EVERY 2,000 FC.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 14,842 hrs · 13,986 cycles

DURING TAKEOFF AIRCRAFT HAD A BIRD STRIKE. FERRY FLIGHT AIRCRAFT TO A REPAIR STATION. REMOVED AND REPLACED FRAME 4, FRAME 5 AND REPAIRED FRAME 6. REMOVED AND REPLACED LEFT AND RIGHT NOSE SKIN.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 14,492 hrs · 13,653 cycles

DURING PRE-FLIGHT THE FLIGHT CREW REPORTED THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND ADJUSTED THE PASSENGER DOOR. DOOR OPS CHECKED GOOD.

Part: CLAMP — OUT OF POSITION (LT PYLON) · airframe 14,454 hrs · 13,613 cycles

THE CREW REPORTED RECEIVING A BLEED LEAK MESSAGE ON THE EICAS DURING CLIMB. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEAK TO BE AT THE NR 1 ENGINE PRE-COOLER. THE CLAMP WAS REPOSITIONED AND THE SYSTEM WAS OPS CHECKED WITH NO ADDITIONAL ISSUES.

Part: PIN — CORRODED (LANDING GEAR) · airframe 14,352 hrs · 13,510 cycles

THE CREW REPORTED RECEIVING A LANDING GEAR DISAGREE MESSAGE ON THE EICAS AFTER TAKEOFF AND THAT THE EICAS INDICATED THAT THE LANDING GEAR WAS DOWN AND RED WITH THE HANDLE IN THE UP POSITION. MAINTENANCE INSPECTED AND REPAIRED A CORRODED PIN AT THE LANDING GEAR SOLENOID VALVE CONNECTOR. FOLLOW-ON SYSTEM CHECK PROVED A SATISFACTORY FIX AT THAT TIME.

Part: ENGINE — LEAKING (NR 2) · airframe 14,284 hrs · 13,450 cycles

WHILE IN CRUISE, THE CREW REPORTED THAT THE LAVATORY SMOKE DETECTOR WENT OFF AND THAT A STRONG SMELL WAS COMING FROM PACK NR 2. INITIALLY, THE NR 2 PACK WAS DEFERRED AND THE SMOKE DETECTOR WAS OPERATIONALLY CHECK GOOD. THE DEFERRAL WAS CORRECTED WHEN MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FOR LEAKING OIL INTERNALLY WHICH WAS CAUSING THE SMELL AND POSSIBLY THE SMOKE.

Part: A/C PACK — ODOR (NR 2) · airframe 14,281 hrs · 13,447 cycles

DURING THE LANDING, THE CREW REPORTED A LAV SMOKE WARNING AND THE F/A REPORTED THAT THE NR 2 PACK WAS BLOWING WARM AIR AND HAD ODOR. MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED AN OPERATIONAL CHECK OF THE LAV SMOKE WITH NO DEFECTS NOTED. MAINTENANCE DEFERRED THE NR 2 PACK AS THE SOURCE OF THE ODOR.

Part: O-RING — WORN (BLEED AIR SYS) · airframe 14,140 hrs · 13,314 cycles

WHILE IN CRUISE, THE CREW REPORTED RECEIVING A BLEED 1 LEAK MESSAGE ON THE EICAS. MAINTENANCE INSPECTED THE AIRCRAFT AND PRIOR TO RELEASING IT BACK INTO SERVICE. REMOVED AND REPLACED THE BLEED O-RING SEALS AT THE AFT CARGO BAY. AN OPERATIONAL CHECK OF THE BLEED SYSTEM WAS PERFORMED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — BINDING (MAIN PAX) · airframe 14,088 hrs · 13,271 cycles

AFTER FLIGHT, THE CREW REPORTED THAT THE MAIN DOOR WAS DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE MAIN DOOR PRIOR TO THE NEXT FLIGHT AND LUBED THE DOOR OPERATING MECHANISM. OPERATIONAL CHECK OF THE DOOR DID NOT REVEAL ADDITIONAL DEFECTS.

Part: FAIRING — VIBRATION (HORIZ STAB) · airframe 13,891 hrs · 13,103 cycles

CREW REPORTED THAT THE AIRCRAFT EXHIBITED SOME VIBRATIONS IN THE FLOORBOARD WHILE IN FLIGHT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE LT AND RT HORIZONTAL STABILIZER FAIRING TIPS. ALSO REMOVED AND REPLACED THE LT AND RT ELEVATOR TIPS. THE RIGHT LANDING GEAR WHEEL FAIRING WAS ALSO FOUND TO HAVE A CRACK. IT WAS REMOVED AND PLACED ON CDL. NO OTHER DEFECTS NOTED AT THE TIME.

Part: ROLLER — LACK OF LUBE (MAIN DOOR) · airframe 13,780 hrs · 13,003 cycles

THE CREW REPORTED THE MAIN DOOR AS BEING DIFFICULT TO OPEN FROM THE INSIDE. MAINTENANCE LUBED THE DOOR ROLLERS. OPS CHECKED GOOD.

Part: ROLLER — OUT OF ADJUST (MAIN DOOR) · airframe 13,764 hrs · 12,989 cycles

THE FLIGHT ATTENDANT REPORTED THAT THE MAIN DOOR WAS DIFFICULT TO OPEN. MAINTENANCE ADJUSTED THE MAIN DOOR ROLLERS AND OPS CHECKED THE DOOR GOOD.

Part: LATCH — DIRTY (MAIN DOOR) · airframe 13,764 hrs · 12,989 cycles

DURING GROUND HANDLING, THE CREW REPORTED THAT THE MAIN DOOR LATCH WAS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE CLEANED AND LUBRICATED THE MAIN DOOR TRACKS AND HANDLE. OPERATIONAL CHECK OF THE DOOR WAS GOOD.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 13,561 hrs · 12,807 cycles

CREW REPORTED RECEIVING A BLEED 1 LEAK MESSAGE ON THE EICAS DURING FLIGHT. MAINTENANCE INSPECTED AND FOUND THE CLAMP AT THE DUAL TEMP CONTROL VALVE LOOSE. THE CLAMP WAS TIGHTENED AND AN OPERATIONAL CHECK OF THE SYSTEM WAS PERFORMED WITH NO LEAKS FOUND.

Part: SMOKE DETECTOR — DIRTY (LAVATORY) · airframe 13,404 hrs · 12,655 cycles

THE CREW REPORTED THAT THE LAVATORY SMOKE DETECTOR WAS PRODUCING INTERMITTENT FAILURES WHILE IN FLIGHT. MAINTENANCE CLEANED THE SMOKE DETECTOR AND CONNECTOR AND PERFORMED A OPERATIONAL CHECK OF THE SMOKE DETECTOR. OPS CHECKED GOOD.

Part: SWITCH — MALFUNCTIONED (NR 1 BATTERY) · airframe 12,963 hrs · 12,239 cycles

CREW REPORTED, RECEIVED A ELECTRICAL EMERGENCY ABNORMAL INDICATION ON THE EICAS DURING CRUISE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 1 BATTERY SWITCH IAW AMM PROCEDURES. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 12,457 hrs · 11,763 cycles

POST FLT - ORD - CREW REPORTED AN ELECTRICAL SMELL IN THE CABIN NEAR ROW 3. MAINTENANCE INSPECTED THE AIRCRAFT AND DEFERRED THE INTERIOR LIGHTING AT ROW 3.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,592 hrs · 10,115 cycles

DURING PRE FLIGHT INSPECTION, THE LT OVERWING EMERGENCY EXIT FLOOD LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE AFFECTED LIGHT. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 10,090 hrs · 9,652 cycles

PRE-FLT 7878-STL - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE LIGHT ASSEMBLY AND PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WITH NO DEFECTS NOTED. (S)

Part: BATTERY — MALFUNCTIONED (NR 1) · airframe 24,194 hrs · 20,818 cycles

FLT 5506 - ATL - CREW RECEIVED A BATTERY NR 1 OVERHEAT MESSAGE ON THE EICAS DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE NR 1 MAIN BATTERY ASSEMBLY. NO OTHER DEFECTS NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 9,242 hrs · 8,889 cycles

PRE FLT 7936 - MSN - SEVERAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. SYSTEM OPS CHECKED GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 9,150 hrs · 8,808 cycles

PRE FLT 7922 IAD - EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY. SYSTEM OPS CHECKED GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 9,074 hrs · 8,739 cycles

PRE FLT 8018 - IAD - EMERGENCY LIGHT FLOOR STRIP AT SEAT 17A INOPERATIVE. MAINTENANCE SECURED EMERGENCY LIGHT STRIP. SYSTEM OPS CHECKED GOOD.

Part: BLEED AIR SYS — MALFUNCTIONED (NR 1 & NR 2) · airframe 9,052 hrs · 8,718 cycles

FLT 7910 - CVG - BLEED NR 1 AND NR 2 OVERTEMP MESSAGE ON THE EICAS. MAINTENANCE PERFORMED A BLEED SYSTEM OPERATIONAL CHECK OF BOTH THE BLEED SYSTEM AND THE ANTI-ICING SYSTEM WITH NO DEFECTS NOTED.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 8,820 hrs · 8,510 cycles

FLT 7971 - IAD - MAIN PITCH TRIM INOP DURING CLIMB. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT. OPS CHECKED GOOD.

Part: WIRE — BROKEN (NLG) · airframe 8,576 hrs · 8,301 cycles

FLT 8018-STL - GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE REPAIRED WIRES AT THE NLG WOW PROXIMITY SWITCH CONNECTOR. OPS CHECKED GOOD.

Part: ARM — OUT OF SEQUENCE (PAX DOOR) · airframe 8,488 hrs · 8,224 cycles

PRE FLT NR 7885 - EWR - PAX DOOR HARD TO OPEN. MAINTENANCE FOUND DOOR LOCK ARMS OUT OF SEQUENCE, RELEASED ARMS OPERATED DOOR 3 TIMES LOCK MECHANISM, OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 7,374 hrs · 7,152 cycles

PRE FLT NR FLMX - RIC - EMERGENCY LIGHT LEFT FORWARD WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT INOP. MAINTENANCE DEFERRED PER MEL.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 7,311 hrs · 7,089 cycles

PRE FLT 7947 - STL - VARIOUS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY.

Part: RELAY — FAILED (BLEED AIR SYS) · airframe 6,712 hrs · 6,513 cycles

FLT NR 7982 - ALB - BLEED 2 LO TEMP EICAS MESSAGE DOES NOT APPEAR DURING TEST. MAINTENANCE REMOVED AND REPLACED BLEED TEST RELAY, OPS CHECK GOOD.

Part: INU — MALFUNCTIONED (NR 1) · airframe 6,287 hrs · 6,109 cycles

FLT NR 8095 - IAD - LOST NAV 1 /NAV 2 ON ILS APPROACH TO IAD. MAINTENANCE REMOVED AND REPLACED NR 1 INU, OPS CHECK GOOD AT THIS TIME.

Part: BATTERY — DISCHARGED (CABIN) · airframe 5,513 hrs · 5,331 cycles

PRE FLT NR 7971 - EWR - VARIOUS EMERGENCY LIGHTS INOP. MAINTENANCE CHARGED THE EMERGENCY LIGHT BATTERIES. OPS CHECKED GOOD.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 5,194 hrs · 5,024 cycles

FLT NR 7978 - ORD - MAIN CABIN DOOR STUCK CLOSED. MAINTENANCE RELEASED THE PASSENGER DOOR HANDLE AND LUBRICATED BOTH THE HANDLES AND ROLLERS. OPS CHECKED NORMAL.

Part: CONTROLLER — MALFUNCTIONED (SPOILERS) · airframe 195 hrs · 168 cycles

EWR - SPOILER FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED SPOILER CONTROL UNIT.