N203JQ

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 14,366 hrs · 8,408 cycles

RIGHT FLOOR SILL PLATE CORRODED OUT OF LIMITS AT FR 14. REMOVED AND REPLACED SILL.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,925 hrs · 19,771 cycles

CFIII, FLOOR STRUCTURE, CORROSION FOUND ON PANEL SUPPORT RT AT FR 84. REPLACED IAW SRM 51-41-02 & 51-41-01.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 27,925 hrs · 19,771 cycles

CFIII, FLOOR STRUCTURE, CORROSION FOUND ON RT GUSSET PLATE AT FR 90. CRIII, FLOOR STRUCTURE RT GUSSET PLATE AT FR 90 REPLACED IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,925 hrs · 19,771 cycles

FWD FUSELAGE, FLOOR STRUCTURE, CORROSION FOUND ON RT INBD SEAT TRACK BETWEEN FR 12-17. REPLACED IAW SRM 51-41-01, 51-43-03 & 51-43-04.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,925 hrs · 19,771 cycles

CFIII, FLOOR STRUCTURE, CORROSION FOUND ON RT FLOOR SUPPORT PANEL BTWN FR 88-90. CRIII, FLOOR STRUCTURE ON RT FLOOR SUPPORT PANEL BET FR 88-90 REPLACED IAW SRM 57-42-01 AND SRM 51-43-03.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,925 hrs · 19,771 cycles

CFIII, FLOOR STRUCTURE, CORROSION FOUND ON LT DOUBLER AT SHEAR PANEL BETWEEN FR 87-88. CFIII, FLOOR STRUCTURE, LT DOUBLER AT SHEAR PANEL BTWN FR 87-88 HAS BEEN REPLACED IAW SRM 51-42-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,925 hrs · 19,771 cycles

FWD FUSELAGE, FLOOR STRUCTURE, CORROSION FOUND ON FLOOR SUPPORT WINDSCREEN LT SIDE AT FR19. REPLACED IAW SRM 51-43-03.

Part: SHEAR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,925 hrs · 19,771 cycles

CFIII, FLOOR STRUCTURE, CORROSION FOUND ON MID - SHEAR PANEL BETWEEN FR 87-88. CFIII FLOOR STRUCTURE MID SHEAR PANEL BET FR 87-88 REPLACED IAW SRM 51-42-01.

Part: RIB — CRACKED (ZONE 300) · airframe 27,925 hrs · 19,771 cycles

DURING HEAVY CHECK MAINTENANCE FOUND RH HORIZONTAL STAB RIB 11A CRACKED. RH HORIZONTAL STAB RIB 11A REPLACED WITH A NEW RIB IAW TASK# 170EO-55-10-0004-1.

Part: POST — CRACKED (ZONE 100) · airframe 27,925 hrs · 19,771 cycles

FWD AVIONICS COMPARTMENT, CRACK FOUNDON LH FWD POST AVIONICS RACK. FWD AVIONICS COMPARTMENT L/H FWD POST AVIONICS RACK REPAIRED UNDER TASK CARD 170EO-53-12-0000

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 27,925 hrs · 19,771 cycles

DURING HEAVY CHECK MAINTENANCE FOUND R2 DOOR SURROUND EMERGENCY LIGHT ONLY LIGHTS UP ON TOP HALF. INOPERATIVE EMERGENCY EXIT LIGHT ON R2 DOOR SURROUND REPLACED IAW AMM 33-50-15-400-801A.

Part: CONNECTOR — DISCONNECTED (COCKPIT) · airframe 22,569 hrs · 15,756 cycles

COCKPIT EMERGENCY LIGHT INOP. TROUBLESHOT TO DISCONNECTED PLUG TO COCKPIT EMERGENCY LIGHT ASSEMBLY. RECONNECTED IAW AMM 35-50-00-710-801-11500.

Part: FLOOR SUPPORT — CORRODED (FRAME 89) · corrosion level 2 · airframe 22,504 hrs · 15,711 cycles

FOUND THE FLOOR SUPPORT FRAME 89, RBL 10 CORRODED. MX REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-08, AND 51-27-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 89-90) · corrosion level 2 · airframe 22,504 hrs · 15,711 cycles

FOUND PAX CABIN FLOOR SUPPORT, FRAMES 89 TO 90, RBL 10 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-08, AND 51-27-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 89) · corrosion level 2 · airframe 22,504 hrs · 15,711 cycles

FOUND THE CABIN FLOOR SUPPORT, FRAME 89, RBL 10 CORRODED. REMOVED AND REPLACED IAW SRM 51-25-16, 51-40-08, AND ETD2011-1901/013330, REV C.

Part: SHEAR WEB — CORRODED (FRAME 87) · corrosion level 2 · airframe 22,504 hrs · 15,711 cycles

FOUND PAX CABIN SHEAR WEB, FRAME 87, RBL 10 - RBL 40 CORRODED. MX REMOVED AND REPLACED SHEAR WEB IAW SRM 51-40-03, 51-40-08, AND ETD2011-190/01333, REV C.

Part: FLOORBEAM — CORRODED (FRAME 87) · corrosion level 2 · airframe 22,504 hrs · 15,711 cycles

FOUND PAX CABIN AFT WET AREA FLOORBEAM AT FRAME 87, RBL 10 WAS CORRODED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 53-23-10, 51-40-08, ETD2011-190/01333, REV C,

Part: FLOORBEAM — CORRODED (FRAME 87) · corrosion level 2 · airframe 22,504 hrs · 15,711 cycles

FOUND PAX CABIN FLOORBEAM, FRAME 87, LBL 10 HAD CORROSION. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 53-23-10, 51-40-08, AND 51-27-02.

Part: MOUNT — CORRODED (FRAME 90) · corrosion level 2 · airframe 22,504 hrs · 15,711 cycles

FOUND PAX CABIN FLOOR, FRAME 90, RBL 23, AFT GALLEY MOUNT PLATE HAD CORROSION . MX REMOVED AND REPLACED MOUNT PLATE IAW SRM 51-75-16, 51-40-08, 51-27-02.

Part: WEB — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 22,504 hrs · 15,711 cycles

FOUND THE AFT CABIN WET AREA WEB, FRAMES 87 - 88, LBL 10 CORRODED. MX REMOVED AND REPLACED THE WEB IAW SRM 53-23-10, 51-40-08, AND ETD 2011-190/01333, REV C.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,504 hrs · 15,711 cycles

WHILE PERFORMING HEAVY CHECK MAINT FOUND PASSENGER CABIN FLOOR FR 89 RBL 36, SIDE SKIRT ANGLE WITH GALLEY MOUNT POINT CORRODED ON UPPER SURFACE. REMOVED AND REPLACED ANGLE AT FR89, RBL 36 IAW SRM 51-10-03, SRM 51-75-16 AND SRM 51-40-08. A/C REMAINS IN HEAVY CHECK UNTIL COMPLETION PN-170-86181-005.

Part: WEB — CORRODED (FRAME 87) · corrosion level 2 · airframe 22,504 hrs · 15,711 cycles

FOUND THE PAX CABIN FLOOR WEB AT FRAME 87, LBL 10 TO 40 HAD CORROSION. MX REMOVED AND REPLACED THE WEB IAW SRM 51-40-08, AND ETD2011-190/01333, REV C.

Part: ANGLE — CORRODED (FRAME 89) · corrosion level 2 · airframe 22,504 hrs · 15,711 cycles

FOUND THE PAX CABIN FLOOR SIDE SKIRT ANGLE AT FRAME 89, LBL 36 HAD CORROSION. MX REMOVED AND REPLACED PAX CABIN FLOOR SIDE SKIRT ANGLE IAW SRM 51-75-16, AND 51-27-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,504 hrs · 15,711 cycles

WHILE A/C WAS IN HEAVY MAINT FOUND PASSENGER CABIN AFT WET AREA FR87 RBL 10 FLOORBEAM CORRODED. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40-08. PN- 170-65669-004. A/C REMAINS IN HEAVY CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,504 hrs · 15,711 cycles

WHILE IN HEAVY CHECK FOUND SHEAR TIE CORRODED AT FR88 INBD OF S-28R. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-40-08. PN- 170-66531-001. A/C REMAINS IN IND HEAVY CHECK FOR COMPLETION.

Part: SHEAR TIE — CORRODED (FRAME 88) · corrosion level 2 · airframe 22,504 hrs · 15,711 cycles

FOUND THE SHEAR TIE CORRODED AT FRAME 88 INBD OF STRINGER 28R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-08.

Part: PLATE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 22,504 hrs · 15,711 cycles

WHILE PERFORMING HEAVY CHECK MAINTENANCE FOUND FWD CARGO CLOSING PLATE TO BE CORRODED BEYOND LIMITS. REPLACED CLOSING PLATE PN-170-67451-001 IAW SRM 51-75-16.

Part: ANGLE — CORRODED (FRAME 89) · corrosion level 2 · airframe 22,504 hrs · 15,711 cycles

FOUND THE PAX CABIN FLOOR, FRAME 89, RBL 36, SIDE SKIRT ANGLE MOUNT POINT CORRODED. REMOVED AND REPLACED THE SKIRT ANGLE IAW 51-10-03, 51-75-16, 51-40-08, AND ETD 2011-190/01333.

Part: LENS — CRACKED (EXIT SIGN) · airframe 22,172 hrs · 15,490 cycles

AFT RT EXIT SIGN LENS CRACKED. R&R EXIT SIGN LENS COVER IAW AMM 33-50-17.

Part: DETECTOR — MALFUNCTIONED (L1 DOOR) · airframe 19,654 hrs · 13,902 cycles

L1 DOOR SHOWS OPEN ON EICAS. R & R SHAFT ROLLER DETECTOR ON L1 DOOR IAW AMM 53-10-21. OPERATIONAL CHECKED GOOD.

Part: INDICATOR — INOPERATIVE (L1 DOOR) · airframe 17,906 hrs · 12,817 cycles

L1 DOOR WILL NOT SHOW ARMED AND LOCKED ON EICAS STATUS PAGE WHEN DOOR IS ACTUALLY ARMED AND LOCKED. R&R VISUAL LOCK INDICATOR ON L1 DOOR.

Part: PIN — BROKEN (L2 DOOR) · airframe 17,585 hrs · 12,631 cycles

F/A REPORTS DOOR PASSENGER AFT OPEN AT FL350. FOUND ELASTIC PIN BROKEN ON FWD COMMAND RAMP L2 DOOR. R & R PIN IAW AMM 53-23-21.

Part: SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 17,580 hrs · 12,629 cycles

DOOR PAX AFT OPEN EICAS MESSAGE 3 TIMES DURING FLIGHT. TROUBLESHOOT TO L2 DOOR WARNING SENSOR OUT OF ADJUSTMENT TO SPEC IN AMM 52-12-21 AND IAW 52-72-21 AND OPS CHECK OF L2 DOOR WARNING SYSTEM IAW 52-72-21. OPS CHECK GOOD.

Part: FLOOR PANEL — CORRODED (FRAME 89) · corrosion level 2 · airframe 17,532 hrs · 12,598 cycles

FRAME 89, RT FLOOR PANEL AT FASTENER HOLE CORRODED. R & R FRAME 89 RT FLOOR PANEL AND APPLIED TOPCOAT REF SRM 51-23-06, 51-42-03.

Part: GUSSET — CORRODED (FRAME) · airframe 17,532 hrs · 12,598 cycles

CORROSION, FRAME 90 RT CENTER GUSSET. R & R FRAME 90 RT CENTER GUSSET REF SRM 51-41-02.

Part: STRUCTURE — CORRODED (FRAME 90) · airframe 17,532 hrs · 12,598 cycles

FRAME 90 AFT GALLEY CORROSION AROUND FASTENER HOLE ON GUSSET, TEXAS PATCH. REMOVED RIVETS, R & R SILL PANEL IAW SRM 51-41-02.

Part: SEAL REST — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,532 hrs · 12,598 cycles

CORROSION ON THE FORWARD CARGO DOOR OPENING AFT SEAL REST. R & R FWD CARGO DOOR SURROUND STRUCTURE, AFT DOOR SEAL REST IAW AMM 51-40-00, 53-21-00.

Part: SEAL REST — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,532 hrs · 12,598 cycles

CORROSION ON THE FWD CARGO DOOR OPENING CENTER SEAL REST. R & R FWD CARGO DOOR CENTER SEAL REST IAW SRM 51-40-00 AND 51-41-01.

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 17,532 hrs · 12,598 cycles

CORROSION PITTING ON SPLINES OF RT WING FLAP TORQUE TUBE F6. R & R RT F6 FLAP TQ TUBE REF AMM 27-51-03.

Part: MOUNT — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 17,532 hrs · 12,598 cycles

FRAME 87-88 AT AFT GALLEY MOUNT OTBD AND INBD FASTENER HOLES IN SHEAR PLATE. R & R SHEAR PANEL FRAME 87-88 IAW SRM 51-42-03 AND 51-42-04.

Part: SKIN — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 17,532 hrs · 12,598 cycles

CHAFE AND CORROSION ON FWD SERVICE DOOR INTERIOR SKIN STRUCTURE JUST FWD OF SLIDE ATTACH POINT FITTING, AREA PREVIOUSLY BLENDED/REPAIRED. R & R GUSSET FROM INTERIOR STRUCTURE OF FWD SERVICE DOOR REF SRM 51-41-02, 51-42-03, 51-23-06.

Part: SEAT TRACK — CORRODED (FRAMES 20-23) · corrosion level 2 · airframe 17,532 hrs · 12,598 cycles

RT INBD SEAT TRACK HAS SEVERAL AREAS OF CORROSION AND GOUGES FROM FRAME 20 TO FRAME 23. REPAIRED CORROSION DAMAGE TO SEAT TRACK SPLICE FRAME 20/23, REF SRM 51-40-02, 51-23-04, 51-41-02, 51-43-03.

Part: SEAT TRACK — CORRODED (FRAMES 23-32) · corrosion level 2 · airframe 17,532 hrs · 12,598 cycles

RIGHT INBD SEAT TRACK HAS SEVERAL AREAS OF CORROSION AND GOUGES FROM FRAMES 23 TO 32. R & R RT INBD SEAT TRACK, PN CH170-67861-005.

Part: SEAT TRACK — CORRODED (FRAMES 20-23) · corrosion level 2 · airframe 17,532 hrs · 12,598 cycles

RT INBD SEAT TRACK HAS SEVERAL AREAS OF CORROSION AND GOUGES FROM FRAME 20 TO FRAME 23. REPAIRED CORROSION DAMAGE TO SEAT TRACK SPLICE FRAME 20/23, REF SRM 51-40-02, 51-23-04, 51-41-02, 51-43-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,950 hrs · 11,014 cycles

1ST LT AND 1ST AND 2ND RT PHOTOLUMINESCENT STRIPS INOPERATIVE. R & R 1ST LT AND 1ST AND 2ND RT PHOTOLUMINESCENT STRIPS IAW AMM 33-50-21.

Part: LOCK SENSOR — MALFUNCTIONED (PAX DOOR) · airframe 14,934 hrs · 11,005 cycles

DOOR PASSENGER AFT OPEN ON EICAS IN FLIGHT. R & R L2 DOOR LOCK SENSOR, ON DOOR FRAME, IAW AMM 52-72-21. OPS CHECK GOOD.

Part: STOP FITTING — OUT OF ADJUST (L2 DOOR) · airframe 14,923 hrs · 10,997 cycles

L2 DOOR OPEN INDICATION DURING CRUISE, WENT AWAY DURING DESCENT. ADJUSTED L2 DOOR STOPS IAW AMM 52-12-23. OPS CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (DOOR) · airframe 14,919 hrs · 10,995 cycles

LEFT REAR DOOR INDICATED OPEN WITH EICAS MESSAGE AS WELL AS MFD STATUS PAGE INDICATIONS IN FLIGHT. MESSAGE APPEARED IN CLIMB APPROXIMATELY AT 30K FT AND DISAPPEARED APPROXIMATELY AT 25K IN DESCENT. PERFORMED OPS CHECK OF L1 "AFT PASSENGER DOOR" AND OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED, REF CMM 52-12-22.

Part: WARNING LIGHT — FALSE ACTIVATION (L2 DOOR) · airframe 14,918 hrs · 10,994 cycles

CAS L2 DOOR SHOWED OPEN AT FL300. CABIN ALT 5400', DELTA P 7.7 PSI. ALL DOOR INDICATIONS SHOWED GREEN. DOOR SHOWED CLOSED AT FL180, DELTA P 5.5 PSI, CABIN ALT 2500 FEET. INSPECTED L2 DOOR, FOUND NO DEFECTS. PRESSURIZED ACFT TO DELTA P 7.8 PSI, NO DOOR MESSAGE. INDICATION SHOWED GREEN. PERFORMED FIM TASK 52-72-00-810A. OPS CHECK GOOD.

Part: SENSOR — FALSE INDICATION (L2 DOOR) · airframe 14,922 hrs · 10,996 cycles

LEFT REAR DOOR EICAS MFD STATUS INDICATION IN FLIGHT ABOVE FL240. LOCK AND PRESSURIZATION INDICATIONS NORMAL. R & R L2 DOOR HANDLE SENSOR IAW AMM 52-72-21. OPS CHECK GOOD AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 14,456 hrs · 10,754 cycles

3 SEGMENTS OF EMERGENCY LIGHTS INOPERATIVE NEAR FRONT OF FIRST CLASS CABIN. CLEANED AND RECHARGED ESCAPE LIGHTING.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,662 hrs · 10,283 cycles

COCKPIT EMERGENCY LIGHT DOES NOT TURN ON DURING TEST. R & R EMERGENCY LIGHT NR 1 BATTERY, OPS CHECKED GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 12,271 hrs · 9,287 cycles

R1 DOOR EXIT MARK SIGN LENS BROKEN. R & R R1 DOOR EXIT MARK SIGN LENS IAW AMM 33-50-17.

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON LT SPLICE FR90 Y=-10.748. R & R SPLICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON LT FWD SEAT TRACK. R & R FWD SEAT TRACK.

Part: DOUBLER — CORRODED (SEAL DEPRESSOR) · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON NUTPLATE DOUBLERS FWD CARGO CENTER SEAL DEPRESSOR. REMOVED, FABRICATED AND REPLACED ALL NUTPLATE DOUBLERS.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 11,599 hrs · 8,828 cycles

LEVEL 2 CORROSION - RT FLOOR SUPPORT FRAMES 84-85. R & R FLOOR SUPPORT.

Part: FINGER DOUBLER — CORRODED (CARGO DOOR) · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON FWD CARGO DOOR FWD FINGER DOUBLER. R & R FINGER DOUBLER.

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON RT SHEAR PANEL SPLICE PLATE. REMOVED, FABRICATED AND INSTALLED SHEAR PANEL.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON FRAME16 FLOOR SUPPORT. R & R SUPPORT.

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON LT SHEAR PLATE AT FRAMES 87-88. R & R SHEAR PLATE.

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON LT SHEAR PLATE SPLICE AT FRAMES 87-88. R & R SHEAR PLATE SPLICE, .

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON DOUBLER AT FRAME 19. R & R DOUBLER.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON RT FLOOR SUPPORT BETWEEN FRAMES 84-85. R & R FLOOR SUPPORT.

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON GUSSET PLATE FRAME 90 RT SIDE. R & R GUSSETT.

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON GUSSET PLATE FRAME 90 LT SIDE. R & R GUSSETT.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON RT FLOOR SUPPORT FRAMES 84-85. R & R FLOOR SUPPORT.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON RT BEAM AROUND FASTENER HEAD AND NUT PLATE. R & R BEAM.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION ON FWD LT SILL AT FRAME 16. R & R SILL.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON RT FWD SEAT TRACK. R & R SEAT TRACK.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON LT AFT SILL FRAME 19. R & R SILL.

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON CENTER SHEAR PLATE BETWEEN FRAMES 87-88. R & R SHEAR PLATE.

Part: BEAM — CORRODED (ZONE 100) · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON RT BEAM AROUND FASTENER HEAD AND NUT PLATE. R & R RT SHEAR PLATE.

Part: SPLICE — CORRODED (ZONE 100) · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON RT SPLICE AT FRAME 90. R & R SPLICE.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON FWD RIGHT THREE HOLE DOUBLER. R & R DOUBLER.

Part: FINGER DOUBLER — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON FWD CARGO DOOR AFT FINGER DOUBLER. R & R DOUBLER.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON RT AFT SILL. R & R SILL.

Part: UPPER SHEET — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON UPPER SHEET LEFT FRAMES 85-86. R & R UPPER SHEET.

Part: UPPER SHEET — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON UPPER SHEET RIGHT FRAMES 85-86. R & R UPPER SHEET.

Part: BEAM — CORRODED (ZONE 100) · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON BEAM FRAME 87 AROUND RIVET HEAD. R & R BEAM.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON RT FLOOR SUPPORT FRAMES 88-90. R & R FLOOR SUPPORT.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON RT INTERCOSTAL BETWEEN FRAMES 89-90. R & R INTERCOSTAL.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,599 hrs · 8,828 cycles

CORROSION FOUND ON RT AFT FLOOR SUPPORT, FRAMES 88-90. R & R FLOOR SUPPORT.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 10,246 hrs · 7,827 cycles

CAPT REPORTED AT FL200, WINDSHIELD CRACKED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CAPTAIN WINDSHIELD.

Part: WIRE HARNESS — FAULTY (L2 DOOR) · airframe 9,545 hrs · 7,348 cycles

L2 DOOR AMBER "X" INDICATED ON MFD STATUS PAGE. REMOVED AND REPLACED L2 DOOR ELECTRICAL HARNESS PER EMB 170 MM 52-72-21. OPS CHECK GOOD.

Part: POWER UNIT — DEFECTIVE (CABIN) · airframe 9,355 hrs · 7,218 cycles

AFT GALLEY EMERGENCY EXIT LIGHT AND OVERHEAD EMERGENCY LIGHT OVER ROW 12 WILL NOT GO OUT, EMERGENCY LIGHT BATTERY FAULT EICAS MESSAGE. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT 3 IAW AMM 33-50-01. OPS CHECK GOOD.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 8,941 hrs · 6,874 cycles

ILLUMINATION TAPE PEELING IN ROW 1 ON RIGHT SIDE OF AISLE. RE-SECURED PHOTOLUMINESCENT FLOOR TRIM IAW EMB 170 MM 33-50-21.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 8,776 hrs · 6,743 cycles

PHOTOLUMINESCENT STRIP AT 1C IS NOT ADHERED TO FLOOR. RE-SECURED PHOTO LUMINESCENT STRIP IAW EMB 170 MM 33-50-21.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 7,915 hrs · 6,055 cycles

EMERGENCY LIGHT BATT FAULT ON START UP. REPOWERED A/C IAW AMM 24-42-02 AND OPS CHECK OF EMERGENCY LIGHTS GOOD IAW 33-50-01.

Part: LIGHT — UNSECURE (CABIN) · airframe 6,523 hrs · 4,976 cycles

EMERGENCY LIGHT FLOOR STRIP CAME OFF IN FIRST CLASS SECTION. RE-SEUCRED EMERGENCY LIGHT FLOOR STRIP IN FIRST CLASS SECTION IAW EMB 170 MM 33-50-21.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 3,396 hrs · 2,609 cycles

EMERGENCY LIGHT FAULT MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED THE AFT OUTBOARD EMERGENCY LIGHT POWER SUPPLY PER EMB 175 MM 33-50-01.