N633RW

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 46,266 hrs · 28,854 cycles

RUDDER AND VERTICAL STABLIZER DAMAGED BETWEEN RIB 10 AND RIB 13 AT TRAILING EDGE. REMOVED AND REPLACED THE RUDDER AND REPAIRED VERTICAL STABLIZER IAW EMB 170/175 ETD170-001452 AND AERNNOVA T1-170-22-001. ALSO REF VP-001581-2022 N/R 1 C1 THRU C6.

Part: SPAR — CRACKED (ZONE 600) · airframe 43,741 hrs · 27,218 cycles

(MAJOR) RT WING STUB SPAR 3 FOUND CRACKED. REPAIRED PER ETD2016-170-048482 REV D.

Part: WEB — CORRODED (FRAME 85-86) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

CENTER FUSELAGE III, CORROSION FOUND ON WEB UNDER DOOR SILL BETWEEN FR 85-86 AT STR 19 L. REPLACED IAW SRM 51-41-01.

Part: SEAL REST — CORRODED (FRAMES 25-26) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

AFT CARGO C/OUT AT LOWER DOOR SILL, CORROSION FOUND ON MID SEAL REST. REPLACED IAW SRM 51-41-01.

Part: SEAT TRACK — CORRODED (FRAMES 43-59) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

CF II, FLOOR STRUCTURE, CORROSION FOUND ON RT INBOARD SEAT TRACK CROWN AREA BETWEEN FR 43-59 AT MULTIPLE PLACES. REPLACED IAW SRM 51-41-02.

Part: NUT PLATE — CORRODED (FRAMES 24-27) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

FWD CARGO DOOR SURROUND LOWER SILL BEAM, CORROSION FOUND ON 2 SUPPORT BRACKETS BETWEEN FR 24-26. REPLACED IAW SRM 51-41-01.

Part: LOUVER — CRACKED (ANTI-ICE DUCT) · airframe 43,741 hrs · 27,218 cycles

ENG 1 INTAKE COWL, ANTI-ICE DUCT EXHAUST PANEL MIDDLE LOUVRE CRACKED. REPAIRED IAW ETD2020-170-02724.

Part: SHEAR TIE — CORRODED (FRAME 78) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

CORROSION FOUND ON CENTER FUSELAGE III AFT CARGO SHEAR CLIP HALF AT FR 78 AND STR 28R. REPLACED IAW SRM 51-41-01.

Part: DOOR SILL — CORRODED (FRAMES 26-27) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

CORROSION FOUND ON FWD CARGO DOOR SURROUND, LOWER SILL BEAM. REPAIRED IAW ETD2020-170-027672.

Part: SEAT TRACK — CORRODED (FRAME 17) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

LEVEL 2 CORROSION FOUND ON CENTER FUSELAGE 1 RT INBOARD SEAT TRACK BEAM AT FR 17. REPLACED SEAT TRACK, IAW SRM 51-43-01 AND 51-41-02.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

FWD LOWER FUSELAGE, CORROSION FOUND ON SHEAR CLIP AT FR 17 BETWEEN STR 27-28 LT. REPLACED IAW SRM 51-41-01.

Part: SCOOP — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

ENG NR 1 AFT STRUT STRUCTURE AREA, INBOARD AIR SCOOP CORRODED. REPLACED IAW SRM 51-41-02.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

FWD LOWER FUSELAGE, CORROSION FOUND ON SHEAR CLIP AT FR 17 BETWEEN STR 27-28 RT. REPLACED IAW SRM 51-41-01.

Part: CROSSBEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

CORROSION FOUND ON CENTER FUSELAGE FLOOR STRUCTURE CROSSBEAM UPPER FLANGE AT FR 16 RT SIDE. REPAIRED IAW SRM 53-00-10.

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

FWD LOWER FUSELAGE, CORROSION FOUND ON SHEAR CLIP AT FR 16 BETWEEN STR 27-28 RT. REPLACED IAW SRM 51-41-01.

Part: ROD END — CORRODED (MLG) · airframe 43,741 hrs · 27,218 cycles

ROD END ON MLG LANDING GEAR FREEFALL CONECTING ROD (RT MLG WHEEL WELL) CORRODED. REPLACED AND ADJUSTED, IAW AMM 32-34-17.

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

FWD LOWER FUSELAGE, CORROSION FOUND ON SHEAR CLIP AT FR 16 BETWEEN STR 27-28 LT. REPLACED IAW SRM 51-41-01.

Part: ANGLE — CORRODED (FRAME 84) · airframe 43,741 hrs · 27,218 cycles

CORROSION FOUND ON CENTER FUSELAGE III FRAME STABILIZER CLIP AT FR 84 AND STR 19L. REPLACED IAW SRM 51-41-01.

Part: SHEAR PANEL — CORRODED (FRAMES 88) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

CORROSION FOUND ON CENTER FUSELAGE III FLOOR STRUCTURE RT SHEAR PANEL AT FR 88. REPLACED IAW SRM 51-42-01.

Part: ANGLE — CORRODED (FRAME 85) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

CORROSION FOUND ON CENTER FUSELAGE III FRAME STABILIZER CLIP AT FR 85 AND STR 19L. REPLACED IAW SRM 51-43-01.

Part: FLOOR SUPPORT — CORRODED (FRAMES 86-89) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

CORROSION FOUND ON CENTER FUSELAGE III FLOOR STRUCTURE RT LONGITUDINAL BEAM FR 86-89. REPLACED IAW SRM 51-43-01.

Part: SHEAR PANEL — CORRODED (FRAME 88) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

CORROSION FOUND ON CENTER FUSELAGE III FLOOR STRUCTURE, MID SHEAR PANEL. AT FR 88. REPLACED IAW SRM 51-42-01.

Part: SEAT TRACK — CORRODED (FRAME 17) · corrosion level 2 · airframe 43,741 hrs · 27,218 cycles

CORROSION FOUND ON FWD FUSELAGE FLOOR SUPPORT STRUCTURE LT INBOARD SEAT TRACK BEAM ON UPPER CAP FR 17. REPLACED IAW SRM 51-43-03.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 43,741 hrs · 27,218 cycles

(MAJOR) RT HORIZONTAL STAB RIB 11A CRACKED. REPLACED IAW 170EO-55-10-0004.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 43,741 hrs · 27,218 cycles

(MAJOR) LT HORIZONTAL STAB RIBS 10A,11A,12A FOUND CRACKED. REPLACED IAW 170EO-55-10-0004.

Part: POWER UNIT — FAILED (CABIN) · airframe 43,521 hrs · 27,035 cycles

AFT RT OUTBOARD EMERGENCY LIGHT POWER UNIT FAILED. R&R AFT OUTBOARD EMERGENCY LIGHT POWER UNIT.

Part: POWER UNIT — FAILED (CABIN) · airframe 43,521 hrs · 27,035 cycles

AFT RT INBOARD EMERGENCY LIGHT POWER UNIT FAILED. R&R AFT RT IB EMERGENCY LIGHT POWER UNIT.

Part: POWER UNIT — FAILED (CABIN) · airframe 43,521 hrs · 27,035 cycles

FWD RT EMERGENCY LIGHT POWER UNIT FAILED. PERFORMED FULL CHARGE OF FWD RT EMERGENCY LIGHT POWER UNIT.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 39,214 hrs · 24,447 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. SEAT TRACK AT FRAME 23 LBL 29 WAS FOUND GOUGED. SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-08. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: BOLT — CORRODED (TE FLAP) · corrosion level 2 · airframe 39,214 hrs · 24,447 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. LEVEL 2 CORROSION WAS FOUND AT RT WING NR 2 FLAP TRACK SUPPORT ACTUATOR FITTING FASTENERS . FASTENERS WERE REMOVED AND REPLACED IAW AMM 57-54-21-000-801A. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,214 hrs · 24,447 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. LEVEL 2 CORROSION WAS FOUND AT PASSENGER CABIN AFT WET AREA FRAME 90 RBL 22 STIFFENER. STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-40-08. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,214 hrs · 24,447 cycles

*** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** LEVEL 2 CORROSION WAS FOUND AT PASSENGER CABIN AFT WET AREA FRAME 89 RBL 36 DOOR SILL BEAM. SILL BEAM WAS REMOVED AND REPLACED IAW SRM 51-40-08 AND ETD 2011-190/01333. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,214 hrs · 24,447 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. LEVEL 2 CORROSION WAS FOUND AT PASSENGER CABIN AFT WET AREA FRAME 90 LBL 5 STIFFENER. STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-40-08 AND SRM 53-23-10. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,214 hrs · 24,447 cycles

*** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** "MAJOR" LEVEL 2 CORROSION WAS FOUND AT LOWER FUSELAGE AFT WASTE TUBE ACCESS PANEL CUT OUT AROUND HINGE AREA. REPAIRS DONE IAW SRM 53-23-01, 53-23-60 AND 51-23-06. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 37,426 hrs · 23,330 cycles

MAIN CABIN DOOR GUST LOCK FAILS TO LATCH. ADJUSTED AND LUBED DOOR LATCH AND DOOR SURROUND IAW AMM 52-11-22.

Part: GUST LOCK — LACK OF LUBE (PAX DOOR) · airframe 35,317 hrs · 21,997 cycles

MAIN CABIN DOOR GUST LOCK INOPERATIVE. REPOSITIONED TRIM AND LUBED DOOR GUST LOCK IAW AMM 25-23-04. OPS CHECKED GOOD.

Part: FLASHLIGHT — DIM (CABIN) · airframe 34,892 hrs · 21,717 cycles

MAINTENANCE REPORTED THAT THE FORWARD CABIN JUMPSEAT FLASHLIGHT WAS VERY DIM. MAINTENANCE OPS CHECKED FORWARD CABIN JUMPSEAT FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (L2 DOOR) · airframe 34,824 hrs · 21,676 cycles

CREW REPORTED THAT WHEN THE L2 DOOR WAS CLOSED, THE EICAS SHOWED A YELLOW CIRCLE WITH A BLACK X. MAINTENANCE REMOVED AND REPLACED L2 INDICATOR HARNESS IAW AMM AND OPS CHECKED GOOD.

Part: BELLCRANK — DAMAGED (GIRT BAR) · airframe 34,376 hrs · 21,388 cycles

CREW REPORTED THAT THE L2 DOOR GIRT BAR INDICATOR FLAG WAS ONLY COMING HALF INTO VIEW. MAINTENANCE REMOVED AND REPLACED L2 DOOR AFT GIRT BAR BELLCRANK IAW AMM AND OPS CHECKED GOOD.

Part: BRACKET — LOOSE (L2 DOOR) · airframe 33,999 hrs · 21,152 cycles

CREW REPORTED THAT THE L2 DOOR WOULD NOT DISARM. MAINTENANCE FOUND AFT END BRACKET MISALIGNED AND LOOSE. SECURED BRACKET IAW AMM AND OPS CHECKED GOOD.

Part: SPRING — LACK OF LUBE (CABIN DOOR) · airframe 33,898 hrs · 21,087 cycles

CREW REPORTED THAT THE MAIN CABIN DOOR GUST LOCK WAS NOT LATCHING. MAINTENANCE LUBED GUST LOCK LATCH SPRING IAW AMM AND OPS CHECKED. GOOD.

Part: GUST LOCK — DIRTY (L1 DOOR) · airframe 33,547 hrs · 20,853 cycles

L1 DOOR GUST LOCK WILL NOT ENGAGE. CLEANED DEBRIS FROM L1 DOOR GUST LOCK MECHANISM AND PERFORMED OPS CHECK. OPS CHECK GOOD IAW AMM 52-11-00.

Part: TRIM PANEL — OUT OF ADJUST (CABIN DOOR) · airframe 33,424 hrs · 20,770 cycles

GUST LOCK ON MAIN CABIN DOOR WILL NOT ENGAGE. FOUND DOOR HINGE TRIM TO BE INTERFERING WITH GUST LOCK. ADJUSTED TRIM, OPS CHECK GOOD REF CMM 52-11-22.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 33,223 hrs · 20,631 cycles

MAJOR REPAIR, LT HORIZONTAL STAB TIP RIB CRACKED. RIB 14 WAS R & R IAW SRM 51-40-02.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 33,223 hrs · 20,631 cycles

MAJOR REPAIR - RT HORIZONTAL STABILIZER RIB 10 CRACKED AT TOP. THE RT HORIZONTAL STAB RIB 10A WAS REPAIRED IAW ETD2016-170-048141.

Part: SEAT TRACK — CORRODED (FRAME 19) · corrosion level 2 · airframe 33,223 hrs · 20,631 cycles

CORROSION ON REPAIR DOUBLER ON LT SEAT TRACK AT FRAME 19. R & R THE SEAT TRACK IAW 51-40-02, 51-41-02, 51-43-02.

Part: SHEAR TIE — CORRODED (FRAME 87) · airframe 33,223 hrs · 20,631 cycles

MAJOR REPAIR, CORROSION ON SHEAR CLIP AT FRAME 87 BETWEEN STR 27R AND 28R. R & R CORRODED SHEAR CLIP AT FR 87 BETWEEN STR 27R AND 28R.

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,223 hrs · 20,631 cycles

CORROSION ON SHEAR PLATE FWD OF R1 DOOR CUT-OUT BETWEEN FRAME 13 AND FRAME 14. R&R SHEAR PLATE IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,223 hrs · 20,631 cycles

RT SEAT TRACK EXTENSION SHOWS EVIDENCE OF POSSIBLE CORROSION. REINSTALLED SHEER PLATE THAT WAS REMOVED TO FOM IAW SRM 51-42-01.

Part: ANCHOR — CORRODED (GALLEY) · corrosion level 2 · airframe 33,223 hrs · 20,631 cycles

FWD SECTION OF AFT GALLEY OTBD FWD FLOOR ANCHOR CORRODED. R & R BRACKET IAW CMM 25-33-97.

Part: ATTACH FITTING — CORRODED (AFT GALLEY) · corrosion level 2 · airframe 33,223 hrs · 20,631 cycles

AFT GALLEY FWD SECTION 2 ATTACHMENT FITTINGS CORRODED. R & R BRACKETS IAW CMM 25-33-97.

Part: SEAL REST — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,223 hrs · 20,631 cycles

AFT CARGO DOOR CUTOUT CENTER SEAL REST CORRODED. R & R LUMBER CENTER SEAL REST, FOUND GAUGE WAS CORRODED AND 8 TOTAL AREAS OF CORROSION BEYOND LIMITS IAW SRM 53-23-11. MATCH DRILLED AND INSTALLED NEW SEAL REST IAW SRM 51-40-02 AND 51-41-01.

Part: SHEAR TIE — CORRODED (FRAME 88) · airframe 33,223 hrs · 20,631 cycles

SHEAR TIE LOCATED ON FRAME 88 BETWEEN STR 26-27R IS CORRODED. R & R SHEAR TIE IAW SRM 51-41-02 AND 51-41-01.

Part: HINGE — CORRODED (WASTE BOX) · corrosion level 2 · airframe 33,223 hrs · 20,631 cycles

WASTE BOX DOOR HINGE HAS SIGNS OF CORROSION. R & R HINGE IAW SRM 51-41-02 AND 51-43-02.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,223 hrs · 20,631 cycles

SIGNS OF CORROSION AROUND SCREW HOLES AND GOUGE IN LOWER CHANNEL OF AFT LOWER CORNER SEAL REST OF AFT CARGO DOOR CUTOUT. CORROSION BEYOND BLENDOUT LIMITS. R & R SEAL REST.

Part: SPAR — CRACKED (ZONE 600) · airframe 33,223 hrs · 20,631 cycles

MAJOR REPAIR, CRACK INDICATION IN FASTENER HOLE IN SPAR 3 WING STUB ON RT SIDE. THE RT SPAR 3 AND CF 2 BULKHEAD WAS REPAIRED IAW ETD2016-170-048482, REV B.

Part: SEAL — PINCHED (R2 DOOR) · airframe 31,703 hrs · 19,626 cycles

CABIN CREW REPORTED FLAPPING NOISE DURING CRUISE FROM R2 DOOR. INSPECTED R2 DOOR, FOUND SEAL PINCHED ON INTERIOR TOP FLAPPER PANEL. ADJUSTED SEAL REF AMM 52-12-00. OPS CHECK GOOD.

Part: LINE — DAMAGED (HYD SYSTEM) · airframe 30,884 hrs · 19,059 cycles

LEFT DEPARTURE AIRPORT WITH HYDRAULIC SYSTEM 1 QUANTITY AT 32 PERCENT. ABOUT 150 MILES EAST, HYDRAULIC SYSTEM 1 LOW QUANTITY. DECLARED EMERGENCY, DIVERTED, OVER AIRPORT, 12 PERCENT. LANDED WITH 6 PERCENT AND WENT TO 2 PERCENT WITH REVERSERS. LANDED WITHOUT INCIDENT. AT GATE, WITH PUMPS OFF, SHOWS 10 PERCENT. ON WALK AROUND, FOUND HYDRAULIC FLUID LEAKING FROM NR 1 ENGINE. INSPECTED AND FOUND HYDRAULIC 1 LINE DAMAGED INSIDE E1 PYLON. R & R HYDRAULIC LINE IN E1 PYLON REF MM 54-50-23/20-10-03. OPS AND LEAK CHECK GOOD. SERVICED E1 HYDRAULICS IAW MM 12-12-01.

Part: LIGHT — UNSECURE (CABIN) · airframe 30,860 hrs · 19,047 cycles

PHOTOLUMINESCENT STRIP MISSING BETWEEN FIRST CLASS AND COACH CABIN. SECURED THE STRIP IAW AMM 33-50-21.

Part: WIRE HARNESS — FAILED (L1 DOOR) · airframe 29,557 hrs · 18,220 cycles

L1 DOOR INDICATOR INTERMITTENT UNSAFE IN FLIGHT. R & R L1 DOOR WARNING HARNESS IAW AMM 52-72-21. ALL OPS CHECKED GOOD.

Part: MECHANISM — DIRTY (R2 DOOR) · airframe 29,178 hrs · 18,017 cycles

R2 DOOR DIFFICULT TO ARM & DISARM. CLEANED R2 DOOR ARMING MECHANISM IAW CMM 52-12-22. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (FRAME 87) · corrosion level 2 · airframe 29,044 hrs · 17,935 cycles

LEFT CENTER SEAT TRACK EXTENSION AT FRAME 87 CORRODED. R & R THE SEAT TRACK.

Part: SHEAR WEB — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 29,044 hrs · 17,935 cycles

SHEAR WEB CORRODED FRAMES 87-88. R & R CENTER SHEAR WEB.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,044 hrs · 17,935 cycles

LEFT HORIZONTAL STAB RIB 12 CRACKED FWD OF MID SPAR. REMOVED DAMAGE AND FABRICATED REPAIR ANGLES.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,044 hrs · 17,935 cycles

RT HORIZONTAL STABILIZER RIB 11 CRACKED FWD OF MID SPAR. REMOVED DAMAGE AND FABRICATED REPAIR ANGLES.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,044 hrs · 17,935 cycles

RIGHT HORIZONTAL STAB RIB 12 CRACKED FWD OF MID SPAR. REMOVED DAMAGE AND FABRICATED REPAIR ANGLES.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,044 hrs · 17,935 cycles

LEFT HORIZONTAL STABILIZER RIB 11 CRACKED FWD OF MID SPAR. REMOVED DAMAGE AND FABRICATED NEW REPAIR ANGLES.

Part: BEAM — CORRODED (DOOR FRAME) · airframe 29,044 hrs · 17,935 cycles

DOOR CUTOUT LOWER BEAM CORRODED. R & R DOOR LOWER BEAM AND CTR SEAL REST.

Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 29,044 hrs · 17,935 cycles

LEFT SHEAR PLATE ALONG FRAME 87 CORRODED. R & R THE SHEAR PLATE.

Part: SEAT TRACK — DAMAGED (FRAMES 74-84) · corrosion level 2 · airframe 29,044 hrs · 17,935 cycles

LEFT INBD SEAT TRACK DAMAGED FROM FRAMES 74-84. R & R THE SEAT TRACK.

Part: SEAT TRACK — DAMAGED (FRAMES 22-34) · corrosion level 2 · airframe 29,044 hrs · 17,935 cycles

RIGHT INBD SEAT TRACK DAMAGED FROM FRAMES 22-34. R & R THE SEAT TRACK.

Part: SEAT TRACK — DAMAGED (FRAMES 74-84) · corrosion level 2 · airframe 29,044 hrs · 17,935 cycles

RIGHT INBD SEAT TRACK DAMAGED FRAMES 74-84. R & R THE SEAT TRACK.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 29,044 hrs · 17,935 cycles

CRACKED LT MLG WHEEL WELL FWD BULKHEAD ATTACH ANGLE CRACKED. R & R ATTACH ANGLE.

Part: CABLE — OUT OF ADJUST (R2 DOOR SLIDE) · airframe 26,967 hrs · 16,703 cycles

R2 DOOR SLIDE INDICATOR NOT SHOWING GREEN "DISARM" INDICATION. ADJUSTED CABLE FOR R2 DOOR SLIDE INDICATOR, OPS CHECKED GOOD IAW AMM 52-42-20.

Part: LINKAGE — OUT OF ADJUST (R2 DOOR) · airframe 26,609 hrs · 16,511 cycles

R2 DOOR SLIDE INDICATOR INOPERATIVE. ADJUSTED MECHANICAL LINKAGE ON R2 DOOR VISUAL INDICATOR IAW AMM 52-42-00, OPS CHECKED GOOD.

Part: INDICATOR — UNSECURE (R2 DOOR) · airframe 26,599 hrs · 16,505 cycles

R2 DOOR DOES NOT SHOW DISARMED. SECURED DISARM INDICATOR IAW AMM 52-12-40, OPS CHECKED GOOD.

Part: GIRT BAR — UNSECURE (L1 DOOR) · airframe 25,553 hrs · 15,865 cycles

L1 GIRT BAR HANGING FROM DOOR. REINSTALLED GIRT BAR FOR L1 DOOR IAW AMM 52-11-41.

Part: GIRT BAR — UNSECURE (L1 DOOR SLIDE) · airframe 25,419 hrs · 15,786 cycles

L1 DOOR EVACUATION SLIDE INOPERATIVE. SECURED L1 DOOR SLIDE GIRT BAR IN PLACE IAW AMM 25-65-01, NO DEFECTS NOTED.

Part: GIRT BAR — LACK OF LUBE (L1 DOOR) · airframe 25,379 hrs · 15,765 cycles

L1 DOOR GIRT BAR INDICATOR NOT ALIGNED AND WON'T SHOW ARMED. LUBED DOOR AND SECURED GIRT BAR IAW AMM 52-11-22.

Part: GIRT BAR — UNSECURE (CABIN DOOR) · airframe 24,766 hrs · 15,392 cycles

AFTER MAIN CABIN DOOR WAS CLOSED, F/A NOTICED GIRT BAR HANGING AT BOTTOM RT OF DOOR. RESECURED GIRT BAR IAW AMM 52-11-41, OPS CHECK GOOD.

Part: GIRT BAR — LOOSE (CABIN DOOR) · airframe 24,756 hrs · 15,387 cycles

PRIOR TO DEPARTURE F/A ATTEMPTED TO CLOSE MAIN CABIN DOOR AND ARMING LEVER WOULD NOT GO ALL THE WAY DOWN. FOUND GIRT BAR AND BAG PIN LOOSE ON ONE SIDE, INSTALLED IAW AMM 25-65-01.

Part: GIRT BAR — OBSTRUCTED (R2 DOOR) · airframe 24,102 hrs · 14,988 cycles

AFT SERVICE DOOR R2 WILL NOT OPEN. INSPECTION FOUND DEBRIS UNDER GIRT BAR AND DOOR ROLLER MARKS. OPENED DOOR AND OPS CHECK IAW AMM 52-42-20.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,225 hrs · 14,448 cycles

LEVEL 2 CORROSION WASTE BOX DOUBLERS. REMOVED CORRODED DOUBLERS AND PERFORMED WORK IAW SB 170-53-0095.

Part: STRUCTURE — CRACKED (LT WING) · airframe 23,225 hrs · 14,448 cycles

MAJOR REPAIR - DURING PROCESS OF REMOVING FASTENERS FOR SB170-57-10-0053, FOUND A BUSHING ALREADY INSTALLED IN THE LEFT A3 FASTENER HOLE. FOUND CRACK IN LEFT A3 AND REPAIRED IAW ETD2012-170-015358 REV C.

Part: MECHANISM — OUT OF ADJUST (R2 DOOR) · airframe 22,963 hrs · 14,299 cycles

L2 DOOR ARMING HANDLE MOVES TOO FAR WHEN DISARMING DOOR. ADJUSTED R2 DOOR EMERGENCY EVAC SLIDE MECH IAW EMB 170 AMM 52-42-40-5. REMOVED AND REPLACED R2 DOOR LINING IAW EMB 170 AMM 25-23-07-04. OPS CHECK GOOD.

Part: CABLE ASSY — BROKEN (R2 DOOR) · airframe 22,919 hrs · 14,271 cycles

R2 DOOR INDICATION UNCLEAR. T/S TO BROKEN R2 DOOR EMERGENCY EVAC SLIDE MECHANISM FLEXBALL CABLE BROKEN. REMOVED AND REPLACED FLEXBALL CABLE ASSY IAW EMB 170 MM 52-42-40. OPS CHECK GOOD IAW EMB 170 MM 52-42-400-700-802A.

Part: INDICATOR — OUT OF ADJUST (R2 DOOR) · airframe 20,641 hrs · 12,833 cycles

R2 DOOR ARM/DISARM SIGN NOT VISIBLE THROUGH DISPLAY WINDOW. ADJUSTED R2 SLIDE INDICATION IAW EMB 170 MM 52-42-40. OPS CHECK GOOD.

Part: WIRE — LOOSE (BRAKE SYSTEM) · airframe 20,090 hrs · 12,439 cycles

DURING FLIGHT PARKING EMERGENCY BRAKE LIGHT CAME ON INTERMITTENTLY WITH THE PARK BRAKE NOT RELEASED MESSAGE COMING ON INTERMITTENTLY. DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT. CLEANED AND RESECURED RT AND LT EMERGENCY PARKING BRAKE PRESSURE SWITCHES, OPS CHECK GOOD IAW MM 32-44-00. MESSAGE RETURNED ON TAXI OUT, RETURNED TO GATE. REMOVED AND REPLACED EMERGENCY PARKING BRAKE VALVE, OPS CHECK GOOD. TWO FLIGHTS LATER THE MESSAGE RETURNED ON TAXI. REMOVED AND REPLACED NR 2 PARKING BRAKE PRESSURE SWITCH IAW EMB 170 MM 33-44-09, OPS CHECK GOOD. TWO FLIGHTS AFTER THAT THE MESSAGE RETURNED AGAIN ON TAXI. AIRCRAFT WAS FERRIED TO IND. SECURED WIRES FROM PARK BRAKE MICROSWITCH TO TERMINAL BLOCK 2503 AND GROUND STUD 0408. OPS AND TAXI CHECK GOOD IAW EMB SWPM 20-64-00.

Part: ENGINE — LEAKING (LEFT) · airframe 20,031 hrs · 12,401 cycles

STRONG SMELL OF TURBINE OIL IN CABIN DURING TAKEOFF CLIMBOUT. FOUND A SUMP LEAKING, REPLACED DRAIN LINE O-RINGS, OIL SMELL STILL PRESENT, OIL CONSUMPTION WITHIN LIMITS. REMOVED AND REPLACED LT ENGINE IAW SHUTTLE JOB CARD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 20,005 hrs · 12,387 cycles

CREW REPORTS FOUL ODOR FROM PACKS AIR SYSTEM BELOW 5000FT ON DESCENT, FA COMPLAINED OF AN IMMEDIATE HIGH CABIN TEMP, UNCONTROLLABLE BY TEMP KNOB. PERFORMED OPS CHECK OF CABIN TEMP CONTROL, NO DEFECTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (CABIN) · airframe 17,343 hrs · 10,744 cycles

EMERGENCY LIGHT BATTERY FAULT MESSAGE. CYCLED AIRCRAFT POWER AND FAULT CLEARED.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,310 hrs · 9,844 cycles

LEVEL 2 CORROSION ON GUSSET RT FLOORBEAM AT FR90. REMOVED AND INSTALLED GUSSET AT RT FLOORBEAM BRAKE 90 IAW EMB 170 SRM 51-40-02, 51-23-04, 51-23-05, 51-23-06 AND 51-41-02.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,310 hrs · 10,724 cycles

LEVEL 2 CORROSION RT FLOOR PLATE FWD OF R1 DOOR. REMOVED AND INSTALLED RT FLOOR SILL PLATE FORWARD OF R1 DOOR IAW EMB 170 SRM 51-40-02, 51-41-02, 51-43-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,310 hrs · 10,724 cycles

LEVEL 2 CORROSION RT OMEGA BEAM, FR 86-90. REMOVED AND REPLACED OMEGA BEAM IAW EMB 170 SRM 51-40-00.

Part: STRUCTURE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 17,310 hrs · 10,724 cycles

LEVEL 2 CORROSION FORWARD CARGO DOOR, AFT SEAL REST. REMOVED AND REPLACED FORWARD CARGO DOOR AFT SEAL IAW EMB 170 MM 51-41-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,310 hrs · 10,724 cycles

LEVEL 2 CORROSION AT FR 90 FLOORBEAM LT BEAM AND LT INTERCOSTAL GUSSET PLATES. REMOVED AND REPLACED GUSSETS ON FR 90 IAW EMB 170 SRM 51-41-02.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,310 hrs · 10,724 cycles

LEVEL 2 CORROSION ON TOP SURFACE OF SHEAR PLATE BETWEEN CENTER RIGHT FLOORBEAM AND RIGHT SILL AT FR 87-88. REMOVED AND REPLACED SHEAR PLATE IAW EMB 170 SRM 57-40-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,310 hrs · 10,724 cycles

LEVEL 2 CORROSION ON RT CENTER FLOOR SUPPORT AT FR 17 CROSS BEAM. REMOVED AND REPLACED RT CENTER FLOORBEAM IAW EMB 170 SRM 51-42-02.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,311 hrs · 10,725 cycles

LEVEL 2 CORROSION LAV SERVICE DOOR ON INSIDE OF PANEL. INSTALLED SERVICEABLE DOUBLER IAW EMB 170 SRM 51-43-02.

Part: POSITION SENSOR — UNSERVICEABLE (ZONE 500) · airframe 15,836 hrs · 9,844 cycles

DURING APPROACH, RECEIVED MULTIPLE MASTER CAUTION MESSAGES WHEN FLAPS SELECTED TO 1; AOA LIMIT FAIL, SHAKER ANTICIPATED, AND SLAT FAIL WERE AMONG THEM. ALL MESSAGES EXCEPT SLAT FAIL CLEARED. CONTINUED APPROACH AND RAN QRH CHECKLIST. NO EMERGENCY DECLARED BUT FIRE TRUCKS WERE AVAILABLE TO OBSERVE BRAKES DURING LANDING. LANDING WAS UNEVENTFUL. RHOB AND RHIB BRAKES DID GET HOT CAUSING A BRAKE OVERHEAT MASTER CAUTION, BUT THEN QUICKLY COOLED OFF. MX CLEARED SF-ACE INHIBITS AND OPS CHECKED THE SYS. MESSAGE RETURNED ON NEXT FLIGHT. AGAIN THERE WAS NO EMERGENCY DECLARED BUT FIRE TRUCKS WERE PRESENT. MX R & R THE LT NR 3 AND NR 4 SLAT SKEW SENSORS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 12,103 hrs · 7,586 cycles

DURING DESCENT TO APPROACH PHASE, SLOWED TO 210KTS AND SELECTED FLAPS 1, RECEIVED EICAS MESSAGES: SLAT FAIL, SHAKER ANTICIPATED, AOA LIMIT FAIL, SPOILER FAULT. CREW CYCLED FLAPS WITH THE SAME RESULTS. CREW FOLLOWED QRH PROCEDURES AND DECLARED AN EMERGENCY. LANDED WITHOUT EVENT. MAINTENANCE CLEARED INHIBITS, RELEASED BRAKE, AND MESSAGE CLEARED AND DID NOT RETURN.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,594 hrs · 6,089 cycles

RIGHT SILL LEVEL 2 CORROSION AT FWD FUSELAGE BETWEEN FR 12 AND FR 14. RIGHT SILL REPLACED AT FWD FUSELAGE BETWEEN FR 12 AND FR 14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,594 hrs · 6,089 cycles

FOUND LEVEL 2 CORROSION ON RT FLOORBEAM BETWEEN FR 86 AND 89. RT FLOORBEAM BETWEEN FR 86 AND 89 REPLACED IAW EMB 170 SRM 51-41-01 AND 51-43-04.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,594 hrs · 6,089 cycles

RT GUSSET LEVEL 2 CORROSION AT FR 90. RT GUSSET REPLACED BY FABRICATED GUSSET IAW EMB 170 SRM 51-41-02.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,594 hrs · 6,089 cycles

MID SHEAR PLATE LEVEL 2 CORROSION BETWEEN FR 87 AND FR 88. MID SHEAR PLATE REPLACED BY NEW SHEAR PLATE IAW EMB 170 SRM 51-41-01, 51-42-01, AND 51-43-01.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,594 hrs · 6,089 cycles

RT SIDE SHEAR PLATE LEVEL 2 CORROSION BETWEEN FR 87 AND FR 88. RT SHEAR PLATE REPLACED BY FABRICATED SHEAR PLATE IAW EMB 170 SRM 51-41-01, 51-42-01, AND 51-43-01.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,594 hrs · 6,089 cycles

LEVEL 2 CORROSION FOUND AT JUNCTION OF RT FLOORBEAM AT FR 89. GUSSET REPLACED BY NEW GUSSET IAW EMB 170 SRM 51-43-01 AND 51-42-01.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,594 hrs · 6,089 cycles

LT SHEAR PLATE LEVEL 2 CORROSION BETWEEN FR 87 AND 88. LT SHEAR PLATE BETWEEN FR 87 AND 88 CORROSION REPLACED IAW EMB 170 SRM 51-41-01, 51-42-01, AND 51-43-01.

Part: SLIDE — DEPLOYED (CABIN) · airframe 59 hrs · 32 cycles

AFTER ARRIVING AT THE GATE ON FLIGHT 7702 FROM IAH TO IAD, THE FLIGHT ATTENDANT COULD NOT OPEN THE EXIT DOOR. THE GIRT BAR WOULD NOT FULLY DISENGAGE FROM THE ACTIVATED POSITION. WHEN THE DOOR WAS OPENED FROM THE OUTSIDE, THE SLIDE DID NOT DISCONNECT FROM THE AIRCRAFT AND THE SLIDE PULLED OUT OF THE CONTAINER AT THE BASE OF THE DOOR. THE DOOR SLIDE ASSEMBLY DEPLOYED UPON ARRIVAL AT THE GATE BY THE MECHANICS. MAINTENANCE PERFORMED AND INSPECTION OF THE FORWARD PASSENGER DOOR EMERGENCY MECHANISM IAW EMB 170 AMM 52-11-40. REMOVED AND REPLACED EMERGENCY SLIDE ON FORWARD PASSENGER DOOR IAW WMB 170 AMM 52-11-40.