N868RW

Part: BYPASS VALVE — FAULTED (HYD SYS) · airframe 33,936 hrs · 25,088 cycles

HYD 2 OVR TEMP MSG. RAN QRH SAW 100 DEGRESS C AND PSI OF 3100. ROUGHLY 30 MINUTES LATER HYD 2 HI TEMP EICAS MESSAGE REAPPEARED EXACTLY ONE MINUTE LATER HYD 2 OVERHEAT EICAS MESSAGE SAW TEMP PEAK AT 200 DEGREES C AND PSI WAS ZERO RAN QRH EHG PUMP SHUTOFF WAS PRESSED TEMPS REMAINED CONSTANTLY HIGH AND LASTED ROUGHLY 15-20 MINUTES DECLARED EMERGENCY COMPLIED WITH THE EMERGENCY CHECK LISTS LANDED-C/A-REMOVED AND REPLACED #2 HYD SYS HEAT EXCHANGER THERMAL BY-PASS VALVE PER EMB-170 MM 29-11-14 OPS AND LEAK CHECK GOOD AT THIS TIME

Part: BATTERY — UNSERVICEABLE · airframe 33,606 hrs · 24,824 cycles

UPON SHUTIMG DOWN AIRCRAFT. THE CEILING PANEL EMERGENCY LIGHTS #4 AND #6 COME ON AND STAY ON WITH A /C POWER OFF-C/A-RAR #4 AFT O/B EMERGENCY LIGHT POWER UNIT IAW MM 33-50-01 OPS CHECK GOOD

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,955 hrs · 23,628 cycles

FLIGHT CREW REPORTED THE EMERGENCY LIGHT AT ROW 5 WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK IN ACCORDANCE WITH AMM 33-50-01, WITH NO FURTHER DEFECTS NOTED.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,955 hrs · 23,625 cycles

EMERGENCY LIGHT ROW 5 NOT WORKING. R & R NR 2 EMERGENCY LIGHT BATTERY, IAW AMM 33-50-01.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 31,476 hrs · 23,255 cycles

DURING HEAVY CHECK. CORROSION FOUND ON TWO SHEAR CLIPS ON FR17 BETWEEN STR28 RH AND 25 RH. SHEAR CLIPS WERE REPLACED IAW SRM 51-41-01, 51-41-02 AND 51-43-01. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR TIE — CORRUPTED (FRAME 16) · corrosion level 2 · airframe 31,476 hrs · 23,255 cycles

DURING HEAVY CHECK. CORROSION FOUND ON SHEAR CLIP AT FR16 BETWEEN STR28 RH AND 27RH. SHEAR CLIP WAS REPLACED IAW SRM 51-41-01 AND 51-41-02. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 31,476 hrs · 23,255 cycles

DURING HEAVY CHECK. FLOOR SUPPORT STRUCTURE CENTER SHEAR PANEL BETWEEN FR87 AND FR88 HAS CORROSION. SHEAR PANEL WAS REPLACED IAW SRM 51-42-02. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: ROD END — CORRODED (SELECTOR VALVE) · corrosion level 2 · airframe 31,476 hrs · 23,255 cycles

DURING HEAVY CHECK. EMERGENCY EXTENSION SELECTOR VALVE ROD END CORRODED. REPLACED ROD END IAW AMM 32-34-17/400. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: FLOOR SUPPORT — CORRODED (FRAMES 88-99) · corrosion level 2 · airframe 31,476 hrs · 23,255 cycles

DURING HEAVY CHECK. FLOOR SUPPORT ANGLE BETWEEN FR88 AND FR90 HAS CORROSION. REPLACED SUPPORT ANGLE IAW SRM 51-42-01 AND 51-43-03. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: FLOORBEAM — CORRODED (FRAME 86) · corrosion level 2 · airframe 31,476 hrs · 23,255 cycles

DURING HEAVY CHECK. FLOOR PANEL SUPPORT CLIP ON FLOOR BEAM AT FR86 HAS CORROSION. REPLACED SUPPORT CLIP IAW SRM 51-41-01. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 31,476 hrs · 23,255 cycles

DURING HEAVY CHECK. FLOOR SUPPORT STRUCTURE RH SHEAR PANEL BETWEEN FR87-FR88 HAS CORROSION. SHEAR PANEL REPLACED IAW SRM 51-42-01 AND SRM 51-42-02. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK.

Part: SLAT TRACK — CRACKED (LT WING) · airframe 31,476 hrs · 23,255 cycles

DURING HEAVY CHECK...LH WING LEADING EDGE SLAT 2 BOTH TRACK CUTOUTS CRACKED. REPAIRED IAW SRM 57-49-01 REPAIR 6. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: TORQUE MOTOR — INOPERATIVE (ZONE 600) · airframe 30,794 hrs · 22,707 cycles

BLEED 2 FAIL EICAS MESSAGE, PACK 2 FAIL EICAS MESSAGE AFTER TAKEOFF. RAN QRH, PACK 2 FAIL 5 MINUTES LATER. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITH NO FURTHER INCIDENT. R&R RT TMC IAW AMM 170 36-11-06, OPS AND LEAK CHECK GOOD. COUND NOT DUPLICATE PACK 2 FAULTS, OPS CHECK GOOD.

Part: SIGN — CRACKED (CABIN) · airframe 30,314 hrs · 22,335 cycles

EXIT SIGN ABOVE R2 DOOR CRACKED. R&R EXIT SIGN ABOVE R2 DOOR IAW AMM 33-50-17.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,341 hrs · 21,570 cycles

R1 DOOR EMERGENCY EXIT SIGN INOP. R&R R1 DOOR EMERGENCY EXIT SIGN IAW AMM 33-50-15.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 28,446 hrs · 20,904 cycles

FWD EMERGENCY LIGHTS WILL NOT TEST FROM FA PANEL. R&R FWD LH EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,028 hrs · 20,649 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND CORROSION FWD OF FR 87 BETWEEN STR 27R-28R INTERCOSTAL JUST AFT OF WATER DRAIN MAST CORRODED. MX REMOVED AND REPLACED PN 170-87562-001 IAW SRM 51-40-08, 51-40-02, 53-23-01. AC REMAINS IN IND FOR COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,028 hrs · 20,649 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND AFT CARGO FR 82 STR12R-28R SHEAR CLIP HAS CORROSION. MX REMOVED AND REPLACED AFT CARGO FR 82 STR 12R-28R SHEAR CLIP PN 170-66674-001 IAW SRM 51-40-08, ETD2018-170-078410. AC REMAINS IN IND FOR COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,080 hrs · 20,649 cycles

DURING HEAVY CHECK MAINTENANCE FOUND A SHEAR CLIP CORRODED AT FR83 BETWEEN STR27R AND 28R. OUT OF LIMITS IAW SRM 53-23-04. MAINTENANCE REMOVED AND REPLACED THE SHEAR CLIP IAW SRM 51-40-08,51-41-02. A/C REMAINS IN IND FOR CHECK COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,080 hrs · 20,649 cycles

WHILE IN HEAVY CHECK MAINTENANCE FOUND SHEAR CLIP CORRODED AT FR87 BETWEEN STR 27R AND 28R. FOUND OUT OF LIMITS IAW SRM 53-23-04. REMOVED AND REPLACED SHEAR CLIP IAW SRM 51-40-08. A/C REMAINS IN IND FOR CHECK COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,028 hrs · 20,649 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND AFT FUSELAGE FR88 BETWEEN STR 27R AND 28R SHEAR CLIP IS CORRODED. MX REMOVED AND REPLACED AFT FUSELAGE FR88 BETWEEN STR 27R AND 28R SHEAR CLIP PN 170-66531-001 IAW SRM 51-40-02, 51-40-08, SRMI 53-23-04. AC REMAINS IN IND FOR COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,028 hrs · 20,649 cycles

WHILE A/C WAS IN HEAVY CHECK FOUND SHEAR CLIP CORRODED AFT FUSELAGE FR89 BETWEEN STR 27R AND 28R. FOUND TO BE CORRODED THROUGH 100% AND OUT OF LIMITS IAW SRM 53-23-04. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP IAW SRM 51-40-08. A/C REMAINS IN IND FOR CHECK COMPLETION.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,028 hrs · 20,649 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND PAX CABIN FLOOR STRUCTURE AT AFT WET AREA SUPPORT CHANNEL AT FR 87-88 AND RBL 25 HAS CORROSION ON UPPER SURFACE AREA. MX REMOVED AND REPLACED AFT WET AREA SUPPORT CHANNEL AT FR 87-88 AND RBL 25 PN 170-86131-001. IAW SRM 51-40-02, 51-43-01. AC REMAINS IN IND FOR COMPLETION.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,028 hrs · 20,649 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND PAX CABIN FLOOR STRUCTURE AT AFT WET AREA CENTER SHEAR PANEL HAS CORROSION ON UPPER SURFACE BETWEEN FR87-88 LBL 23-33. MX REMOVED AND REPLACED CENTER SHEAR PANEL PN 170-65927-007 IAW SRM 51-75-16, ETD2011-190/013330REV C, SRM 51-40-08.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,028 hrs · 20,649 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND PASSENGER CABIN FLOOR STRUCTURE AT AFT WET AREA SKIRT ANGLE HAS CORROSION AT FR 89, RBL 36. MX REMOVED AND REPLACED FLOOR STRUCTURE AT AFT WET AREA SKIRT ANGLE PN 170-86181-005, IAW SRM 51-40-02 , SRM 71-40-08. AC REMAINS IN IND FOR COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,028 hrs · 20,649 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND PAX CABIN FLOOR STRUCTURE AT AFT WET AREA RIGHT SHEAR CLIP HAS CORROSION ON UPPER SURFACE BETWEEN FR87-88 AND RBL 24. MX REMOVED AND REPLACED AFT WET AREA RIGHT SHEAR CLIP PN 170-19191-001 IAW SRM 51-40-08, 53-23-1051-40-08. AC REMAINS IN IND FOR COMPLETION.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,028 hrs · 20,649 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND PAX CABIN FLOOR STRUCTURE AT AFT WET AREA PLATE SHOWS SIGNS OF PREVIOUS CORROSION AND BLEND OUT AT FR90 RBL25. MX REMOVED AND REPLACED GUSSET PLATE PN 170-60259-001 IAW SRM 51-75-16, 51-40-08. AC REMAINS IN IND FOR COMPLETION.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,028 hrs · 20,649 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND PAX CABIN FLOOR STRUCTURE AT AFT WET AREA LEFT SHEAR PANEL HAS CORROSION ON UPPER SURFACE BETWEEN FR 87-88 AND LBL 3.5. MX REMOVED AND REPLACED LEFT SHEAR PANEL PN 170-65928-001. IAW SRM 51-40-08, 51-75-16, ETD2011-190/01333 REV C. AC REMAINS IN IND FOR COMPLETION.

Part: SUPPORT — CORRODED (FLAP TRACK) · corrosion level 2 · airframe 28,028 hrs · 20,649 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND RT WING IN BOARD MAIN FLAP INMOST FLAP TRACK SUPPORT HAS CORROSION. MX REMOVED CORROSION FLAP TRACK FAIRING SUPPORT PN 170-14654-404. IAW ETD2018-170-076715. AC REMAINS IN IND FOR COMPLETION.

Part: SLIDE — PARTIAL DEPLOY (L2 DOOR) · airframe 25,820 hrs · 19,273 cycles

L2 DOOR SLIDE PARTIALLY DEPLOYED. R & R THE L2 DOOR SLIDE IAW AMM 25-61-01.

Part: SENSOR — OUT OF ADJUST (L2 DOOR) · airframe 22,601 hrs · 17,053 cycles

L2 DOOR INDICATION SHOWED UP ON TAKEOFF. ADJUSTED L2 DOOR WARNING SENSOR IAW AMM 52-72-21. OPS CHECKED GOOD.

Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 22,524 hrs · 16,985 cycles

CORROSION ON AFT CABIN CENTER SHEAR PANEL FRAME 87. R & R CENTER SHEAR PANEL, PN 170-65928-001.

Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 22,524 hrs · 16,985 cycles

CORROSION ON AFT CABIN CENTER SHEAR PANEL FRAME 87. R & R CENTER SHEAR PANEL, PN 170-65928-001.

Part: GUSSET — CORRODED (FRAME 80) · corrosion level 2 · airframe 22,524 hrs · 16,985 cycles

AFT CARGO DOOR CUTOUT STRUCTURE FRAME 80, STR 26R SUPPORT GUSSET CORRODED. R & R GUSSET, PN 17085667-001.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 22,524 hrs · 16,985 cycles

CORROSION ON AFT CABIN RT SHEAR PANEL FRAME 87-88, RBL 41.5". R & R SHEAR PANEL.

Part: FLOORBEAM — CORRODED (FRAME 87) · corrosion level 2 · airframe 22,524 hrs · 16,985 cycles

AFT CABIN RT PANEL SUPPORT FRAME 87. R & R THE FLOORBEAM.

Part: SEAL REST — CORRODED (ZONE 100) · airframe 22,524 hrs · 16,985 cycles

AFT CARGO DOOR FWD SEAL REST HAS CORROSION. R & R SEAL REST.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 22,524 hrs · 16,985 cycles

FLOOR PANEL SUPPORT AT FRAME 16, RBL 25" IS CORRODED. R & R SUPPORT, PN 170-04071-001.

Part: FLOOR SUPPORT — CORRODED (FRAMES 87-90) · airframe 22,524 hrs · 16,985 cycles

CORROSION ON AFT CABIN LT PANEL SUPPORT FRAME 87-90, LBL 44". R & R SUPPORT PN CH170-86139-005.

Part: CONTROL UNIT — SMOKE (CABIN) · airframe 22,434 hrs · 16,918 cycles

SMOKE IN CABIN. AGCU KEEPS BURNING IN RICC. DECLARED EMERGENCY, RETURNED TO GATE. R & R AGCU IAW AMM 24-22-03.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,242 hrs · 16,087 cycles

EMERGENCY EXIT LIGHTS OVER L1 DOOR INOPERATIVE. R & R EMERGENCY LIGHT BATTERY 1 IAW AMM 33-50-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,242 hrs · 16,087 cycles

EMERGENCY EXIT LIGHTS OVER R1 DOOR INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-01. OPS CHECK GOOD.

Part: DOUBLER — DAMAGED (FRAMES 9-11) · airframe 21,242 hrs · 16,087 cycles

4 FASTENER HOOKS IN SKIN SPLICE DOUBLER BETWEEN FRAMES 9-11 AND STR 19 - 20L ARE DAMAGED. REPAIRED THE LOWER SKIN SPLICE IAW ETD2015-170-043278, REV B.

Part: SKIN — DENTED (FRAMES 11-12) · airframe 21,242 hrs · 16,087 cycles

LARGE DENT TO THE LT FORWARD FUSELAGE SKIN BETWEEN FR 11 AND 12, STRINGERS 12 - 15L. R & R LT FWD FUSELAGE SKIN IAW SRM 51-40-02, 51-41-00, 51-43-04, AND 51-21-03.

Part: BOTTLE — LOW PRESSURE (SERVICE DOOR) · airframe 20,895 hrs · 15,886 cycles

AFT RT SERVICE DOOR PNEUMATIC BOTTLE ASSEMBLY LOW PRESSURE. FOUND AFT RT SERVICE DOOR PNEUMATIC BOTTLE LEAKING NITROGEN. R & R DIAPHRAGM AND O-RINGS. SERVICED AFT RT SERVICE DOOR PNEUMATIC BOTTLE ASSY TO 2350 PSI AT 20 DEGREES C, 160 BAR REF AMM 52-42-53 AND 52-42-51.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,850 hrs · 15,858 cycles

R1 DOOR EMERGENCY EXIT IDENTIFIER SIGN ON R1 DOOR SIDE SURROUND PARTIALLY ILLUMINATED. R & R R1 DOOR EMERGENCY EXIT IDENTIFIER SIGN REF AMM 33-50-15. OPS TEST SATISFACTORY.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,850 hrs · 15,858 cycles

EXIT LOCATOR SIGN ON AFT CENTER CEILING INOPERATIVE. R & R ELPU NR 3 REF AMM 33-50-01. OPS TEST SATISFACTORY.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,850 hrs · 15,858 cycles

L1 DOOR EMERGENCY EXIT IDENTIFIER SIGN ON FWD LAVATORY PARTIALLY ILLUMINATED. R & R THE L1 DOOR EMERGENCY EXIT IDENTIFIER SIGN ON THE FWD LAVATORY REF AMM 33-50-15. OPS TEST SATISFACTORY.

Part: SIGN — CRACKED (EMERGENCY LIGHT) · airframe 20,850 hrs · 15,858 cycles

EXIT MARKING SIGN LENS ABOVE THE R1 DOOR CRACKED. R & R THE EXIT MARKING SIGN LENS ABOVE THE R1 DOOR REF AMM 33-50-17. OPS TEST SATISFACTORY.

Part: PIN — UNSECURE (L2 DOOR SLIDE) · airframe 19,236 hrs · 14,852 cycles

TWO PINS FROM L2 SLIDE HANGING OUT. SECURED L2 SLIDE PINS IAW AMM 52-12-40.

Part: GIRT BAR — OUT OF ADJUST (R2 DOOR) · airframe 19,168 hrs · 14,813 cycles

R2 DOOR INDICATION OUT OF ALIGNMENT. RIGGED THE ARM AND DISARM CABLE, AND DOOR LOCKING MECHANISM. ADJUSTED FINE, BUT FLAG AT RT BOTTOM CORNER KEPT DRIFTING AWAY. FERRIED. ADJUSTED FWD AND AFT GIRT BAR FLOOR FITTINGS ON R2 DOOR REF AMM 53-23-25. OPS CHECK GOOD.

Part: BOLT — SHEARED (GIRT BAR) · airframe 19,171 hrs · 14,815 cycles

R2 DOOR HARD TO ARM AND DEARM. INSPECTED AND FOUND A SHEARED BOLT AT THE END OF THE GIRT BAR. ADJUSTED R2 DOOR CABLE, OPS CHECK GOOD.

Part: CABLE — OUT OF ADJUST (R2 DOOR) · airframe 19,168 hrs · 14,813 cycles

AFT R2 DOOR DIFFICULT TO OPEN. GIRT BAR NOT ARMING, INDICATOR SHOWS CLEAR, NOT RED. ADJUSTED R2 DOOR PAX SERVICE DOOR FLEX BALL CABLE AND DOOR ACTUATING AND LOCKING MECHANISM REF AMM 52-42-22. NO DEBRIS NOTED, WORKS AND LOCKS FINE.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 19,166 hrs · 14,812 cycles

L1 DOOR GIRT BAR INDICATION ONLY SHOWS PARTIALLY IN WINDOW. ADJUSTED AFT GIRT BAR FLOOR FITTING IAW AMM 53-10-21. OPS CHECKED GOOD.

Part: GIRT BAR — OUT OF ADJUST (R2 DOOR) · airframe 19,166 hrs · 14,812 cycles

R2 DOOR GIRT BAR WILL NOT GO ALL THE WAY DOWN WHEN ARMING. INDICATOR IS SHOWING HALF RED AND HALF CLEAR. R & R R2 DOOR BUSTLE IAW 52-42-20 AND ADJUSTED LOCK LATCH AND GIRT ATTACHMENT. OPS CHECKED GOOD.

Part: THRESHOLD — CORRODED (R2 DOORWAY) · corrosion level 2 · airframe 19,165 hrs · 14,811 cycles

CORROSION FOUND AROUND RIVET HEADS ON R2 DOOR THRESHOLD. R & R THRESHOLD. MAJOR REPAIR.

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,165 hrs · 14,811 cycles

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

Part: CROSSBEAM — CORRODED (FRAME 84) · corrosion level 2 · airframe 19,165 hrs · 14,811 cycles

CORROSION FOUND ON CROSSBEAM AT FRAME 84. INSTALLED ANGLE REPAIR ON CENTER SECTION OF CROSSFRAME. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 19,165 hrs · 14,811 cycles

CORROSION FOUND ON LEFT SEAT TRACK AT FRAME 84. REPAIRED SEAT TRACK IAW ETD2014-170-042950, MAJOR REPAIR.

Part: THRESHOLD — CORRODED (L2 DOORWAY) · corrosion level 2 · airframe 19,165 hrs · 14,811 cycles

CORROSION FOUND AROUND RIVET HEADS ON L2 DOOR THRESHOLD. R & R THRESHOLD. MAJOR REPAIR.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 19,165 hrs · 14,811 cycles

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

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · airframe 19,165 hrs · 14,811 cycles

CORROSION FOUND ON RT SHEAR PLATE SPLICE FRAMES 87-88. R & R SHEAR PLATE SPLICE.

Part: CROSSBEAM — CORRODED (FRAME 84) · corrosion level 2 · airframe 19,165 hrs · 14,811 cycles

CORROSION FOUND ON CROSSBEAM AT FRAME 84. INSTALLED ANGLE REPAIR ON CENTER SECTION OF CROSSBEAM. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 19,165 hrs · 14,811 cycles

CORROSION FOUND ON RT FWD FLOOR SUPPORT FRAMES 12-14. R & R FLOOR SUPPORT.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,165 hrs · 14,811 cycles

CORROSION FOUND ON BOTTOM FLANGE OF 191 TO 192 FAIRING. R & R CENTER RIB SUPPORTS, MAJOR REPAIR.

Part: GUSSET — CORRODED (FRAME 90) · airframe 19,165 hrs · 14,811 cycles

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

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-20) · corrosion level 2 · airframe 19,165 hrs · 14,811 cycles

CORROSION FOUND ON RT FLOOR SUPPORT FRAMES 12-20. R & R RT FLOOR SUPPORT.

Part: CROSSBEAM — CORRODED (FRAME 14) · corrosion level 2 · airframe 19,165 hrs · 14,811 cycles

CORROSION FOUND ON CROSSBEAM A FRAME 14 AND Y=+10.748. REMOVED CORROSION, REPAIRED CROSSBEAM IAW ETD2014-170-042963. MAJOR REPAIR

Part: CROSSBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 19,165 hrs · 14,811 cycles

CORROSION FOUND ON CROSSBEAM FRAME 17 Y=+10.748. REMOVED CORROSION, REPAIRED CROSSBEAM IAW ETD2014-170-042963. MAJOR REPAIR

Part: FLOOR SUPPORT — CORRODED (FRAME 86) · corrosion level 2 · airframe 19,165 hrs · 14,811 cycles

CORROSION FOUND ON FLOOR SUPPORT RT AT FRAME 86. R & R FLOOR SUPPORT.

Part: LIGHT — DAMAGED (CABIN) · airframe 18,901 hrs · 14,624 cycles

EMERGENCY LIGHT BETWEEN FIRST CLASS ROWS, SEAT 1 TO 3 FADED AND DIM. R & R LIGHT IAW AMM 33-50-21. OPS CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 17,634 hrs · 13,719 cycles

R1 DOOR PRESSURE OBSERVED OUT OF NORMAL RANGE. SERVICED R1 DOOR ASSIST BOTTLE IAW AMM 52-11-51 TO 2200PSI.

Part: HINGE — LACK OF LUBE (L2 DOOR) · airframe 16,038 hrs · 12,549 cycles

L2 IS VERY HARD TO ARM AND DISARM. LUBRICATED HINGES IAW AMM 52-10-00.

Part: HANDLE — DIRTY (L2 DOOR) · airframe 16,017 hrs · 12,522 cycles

L2 DOOR HANDLE STICKS WHEN OPENING, ARMING HANDLE STICKS WHEN DISARMING. CLEANED AND PERFORMED OPS CHECK OF L2 DOOR HANDLE IAW AMM 52-12-40. OPS CHECK GOOD.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,550 hrs · 11,548 cycles

LEVEL 2 CORROSION RT SHEAR WEB AT FR87 TO FR88. REMOVED, MATCH DRILLED, AND INSTALLED REPLACEMENT SHEAR PANEL IAW EMB 170 SRM 51-40-02, 51-42-01, 51-42-02, AND 51-43-03.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 14,550 hrs · 11,548 cycles

LEVEL 2 CORROSION LT UPPER SHEET AT LT SEAT TRACK BEAM. REMOVED, MATCH DRILLED, AND INSTALLED REPLACEMENT UPPER SHEET LT IAW EMB 170 SRM 51-41-01 AND 51-43-03.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,550 hrs · 11,548 cycles

LEVEL 2 CORROSION LT SHEAR WEB AT FR87 TO FR88. REMOVED, MATCH DRILLED, AND INSTALLED NEW LT SHEAR PANEL IAW EMB 170 SRM 51-40-02, 51-42-01, 51-42-02, AND 51-43-03.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,550 hrs · 11,548 cycles

LEVEL 2 CORROSION RT UPPER SHEET AT RT SEAT TRACK BEAM. REMOVED, MATCH DRILLED, AND INSTALLED NEW RT UPPER SHEET IAW EMB 170 SRM 51-40-02, 51-41-01, AND 51-43-03.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,550 hrs · 11,548 cycles

LEVEL 2 CORROSION - RIGHT I/B GUSSET AT FR90. REMOVED AND REPLACED RIGHT I/B GUSSET AT FR90 IAW EMB 170 SRM 51-40-02 AND 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,550 hrs · 11,548 cycles

LEVEL 2 CORROSION RIGHT SEAT TRACK BEAM ON UPPER SURFACE AT FR87 TO FR88. REMOVED AND REPLACED SEAT TRACK BEAM IAW EMB 170 SRM 51-41-01 AND 51-43-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,550 hrs · 11,548 cycles

LEVEL 2 CORROSION RT FWD FUSELAGE SEAT TRACK BEAM AT FR16 TO FR19. REMOVED CORRODED SEAT TRACK BEAM AND INSTALLED SERVICEABLE LIKE BEAM PER EMB 170 SRM 51-41-00 AND 51-43-00.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,550 hrs · 11,548 cycles

LEVEL 2 CORROSION CENTER GUSSET AT FR90, SURFACE CORROSION. REMOVED AND REPLACED GUSSET AT FR90 IAW EMB 170 SRM 51-43-01.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,550 hrs · 11,548 cycles

LEVEL 2 CORROSION - RIGHT O/B GUSSET AT FR90. REMOVED AND REPLACED O/B GUSSET AT FR90 IAW EMB 170 SRM 51-40-02 AND 51-41-02.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,550 hrs · 11,548 cycles

LEVEL 2 CORROSION CENTER SHEAR WEB AT FR87 TO FR88. REMOVED, MATCH DRILLED, AND INSTALLED NEW SHEAR PANEL CENTER IAW EMB 170 SRM 51-40-02 AND 51-42-01.

Part: DOOR — OUT OF SEQUENCE (CABIN) · airframe 13,848 hrs · 11,185 cycles

MAIN CABIN DOOR HARD TO CLOSE. RESEQUENCED DOOR AND PERFORMED FUNCTION CHECK IAW EMB MM 52-11-23. OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 13,365 hrs · 10,896 cycles

EMERGENCY LIGHTS NOT WORKING ABOVE R2 DOOR. FOUND CONNECTOR DISCONNECTED FOR EMERG LIGHTS ABOVE R2 DOOR. RECONNECTED PLUG IAW EMB 170 MM 33-50-01. OPS CHECK GOOD.

Part: DOOR — OUT OF SEQUENCE (L1) · airframe 11,061 hrs · 9,316 cycles

CREW REPORTED L-1 DOOR WOULDN'T CLOSE. MAINTENANCE RESET L-1 DOOR SEQUENCE PER EMB AMM AND REPORTED, OPS CHECK GOOD.

Part: DOOR — LACK OF LUBE (L1) · airframe 10,016 hrs · 8,582 cycles

CREW REPORTED L-1 DOOR WAS DIFFICULT TO CLOSE. MAINTENANCE LUBED THE L-1 DOOR PER EMB AMM, AND OPS CHECK WAS GOOD. A/C WAS THEN RETURNED TO SERVICE.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 9,090 hrs · 7,944 cycles

WHILE AC WAS IN FOR HEAVY CHECK, A MAJOR REPAIR WAS ACCOMPLISHED. WHILE PERFORMING SB 170-53-0050 A DRILL SART WAS FOUND UNDER THE LT FITTING. MAINTENANCE REQUESTED EMB ENGINEERING SUPPORT AND RECEIVED ETD2010-170/01719. MAINTENANCE REPAIRED PER ETD AND SRM. AC STILL OUT OF SERVICE FOR HEAVY CHECK.

Part: SKIN — DENTED (FUSELAGE) · airframe 9,090 hrs · 7,944 cycles

WHILE AC WAS IN FOR HEAVY CHECK, A MAJOR REPAIR WAS ACCOMPLISHED. DENT WAS FOUND ON LT FUSELAGE AT FR 27 TO FR 28, STR 20L TO STR 21L. MAINTENANCE REQUESTED EMB ENGINEERING SUPPORT AND RECEIVED ETD2010-170/01697 AND ETD2010-170/01112 FOR REPAIR. MAINTENANCE REPAIRED PER ETD'S AND EMB SRM. AC STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SKIN — DENTED (FUSELAGE) · airframe 9,090 hrs · 7,944 cycles

WHILE AC WAS IN FOR HEAVY CHECK, A MAJOR REPAIR WAS ACCOMPLISHED. DENT WAS FOUND ON LT FUSELAGE AT FR 25, STR 21L. MAINTENANCE REQUESTED EMB ENGINEERING SUPPORT AND RECEIVED ETD2010-170/01692. MAINTENANCE REPAIRED PER ETD AND SRM. AC STILL OUT OF SERVICE FOR HEAVY CHECK.

Part: SKIN — DENTED (FUSELAGE) · airframe 9,090 hrs · 7,944 cycles

WHILE AC WAS IN FOR HEAVY CHECK, A MAJOR REPAIR WAS ACCOMPLISHED. DENT WAS FOUND ON LT FWD FUSELAGE AT FR 26 AND FR 27, STR 20L AND STR 21L. MAINTENANCE REQUESTED EMB ENGINEERING SUPPORT AND RECEIVED ETD2010-170/01697 AND ETD2010-170/01711 FOR REPAIR. MAINTENANCE REPAIRED PER ETD'S AND SRM. AC STILL OUT OF SERVICE FOR HEAVY CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,089 hrs · 7,944 cycles

WHILE AC WAS IN FOR HEAVY CHECK, A MAJOR REPAIR WAS ACCOMPLISHED ON THE RT SEAT TRACK BEAM BETWEEN FR 14 AND FR 17. MAINTENANCE REQUESTED EMB ENGINEERING SUPPORT AND RECEIVED ETD2010-170/01723. MAINTENANCE REPAIRED AS REQUIRED, AC STILL OUT OF SERVICE FOR HEAVY CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,089 hrs · 7,944 cycles

WHILE AC WAS IN FOR HEAVY CHECK, A MAJOR REPAIR WAS ACCOMPLISHED ON THE LT SEAT TRACK BEAM BETWEEN FR 16 AND FR 19. MAINTENANCE REQUESTED EMB ENGINEERING SUPPORT AND RECEIVED ETD2010-170/01723. MAINTENANCE REPAIRED AS REQUIRED, AC STILL OUT OF SERVICE FOR HEAVY CHECK.

Part: FLANGE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,089 hrs · 7,944 cycles

WHILE AC WAS IN FOR HEAVY CHECK, LEVEL TWO CORROSION WAS FOUND INSIDE THE ATTACH FLANGE ON THE LAV SERVICE PANEL. MAINTENANCE REMOVED AND REPLACED INSIDE ATTACH FLANGE PER EMB SRM. AC STILL OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 9,089 hrs · 7,944 cycles

***A/C IS CURRENTLY OUT OF SERVICE IN HEAVY CHECK*** THIS MAJOR REPAIR WRITE-UP WAS GENERATED WHILE A/C IS IN HEAVY CHECK, MAINTENANCE REPORTED DENT ON LT FWD FUSELAGE AT FR26 - FR27 STR 20L - STR 21L AND LT FWD FUSELAGE AT FR27-FR28 AND STR 20L-21L. RECEIVED EMB ETD 2010-170-01697, A/C IS CURRENTLY OUT OF SERVICE AWAITING FINAL REPAIR.

Part: CONTROL LEVER — INOPERATIVE (ZONE 200) · airframe 7,777 hrs · 6,399 cycles

ON CLIMB AT 3000 FT GEAR WAS STUCK DOWN. CLIMBED TO 10000 FT, FOLLOWED QRH, NO FIX. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. MX CLEANED PROX SENSORS ON ALL 3 GEAR, SERVICED NLG STRUT AND PERFORMED GEAR SWINGS. COULD NOT DUPLICATE. THE LANDING GEAR CONTROL LEVER WAS LATER REPLACED AS PRECAUTIONARY.

Part: PROXIMITY SENSOR — INOPERATIVE (NLG) · airframe 7,115 hrs · 4,969 cycles

AFTER GEAR RETRACTION, LG WOW SYS FAIL MESSAGE APPEARED. THE QRH INSTRUCTS THE PILOT TO LAND AT THE NEAREST SUITABLE AIRPORT. RETURNED TO HNL. UPON GEAR EXTENSION THE MESSAGE WENT AWAY. MAINTENANCE CLEANED THE PROX SENSOR FOR THE NLG. THE ISSUE REAPPEARED 4/3/09, FLIGHT NUMBER 159, SAME CIRCUMSTANCES, AND THE CREW DECLARED AN EMERGENCY. MAINTENANCE SERVICED THE NLG STRUT IAW EMB MM 12-12-09-03.

Part: FITTING — CHAFED (HYDRAULIC SYSTEM) · airframe 3,886 hrs · 2,207 cycles

FLIGHT 6496 DFW TO JFK IN CRUISE, CREW HAD A HYDRAULIC 2 LOW QUANTITY EICAS MESSAGE FOLLOWED BY LOSS OF HYDRAULIC 2 SYSTEM PRESSURE. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND A UNION FITTING CHAFED AND LEAKING AT NR 2 ENGINE HYDRAULIC PUMP HIGH PRESSURE LINE. REMOVED AND REPLACED FITTING. NR 2 ENGINE HYDRAULIC PUMP WAS REPLACED AS A PRECAUTIONARY MEASURE DUE TO LOSS OF SYSTEM 2 PRESSURE.

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL FEED) · airframe 325 hrs · 135 cycles

FLIGHT 6441 SLC TO IND IN CRUSE THE CREW RECEIVED A "FUEL FEED 1 FAULT" ON THE EICAS FOLLOWED BY A CAUTION MESSAGE "ENG 1 FUEL LO PRESS". THE CREW RAN THE QRH PROCEDURE FOR "ENG 1 FUEL LO PRESS." THE FUEL FLOW ON THE NR 1 ENGINE APPEARED NORMAL. THE MESSAGE "ENG 1 FUEL LO PRESS" DID NOT GO AWAY FROM THE EICAS. WITH THE NR 1 ENGINE AT IDLE THE CREW DIVERTED TO MCI AND LANDED WITH NOW INCIDENT. MAINTENANCE REPLACED THE E1 LOW PRESSURE SWITCH, NO FIX. MEL’D E1 ENGINE LOW FUEL PRESSURE MESSAGE. MAINTENANCE INSTALLED CUSTOM IN & OUT MODULE, NO HELP, THEN RECONNECTED LOOSE CANNON PLUGS. OPS CHECK GOOD.