N867RW

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 34,867 hrs · 23,113 cycles

CORRODED SHEAR CLIP, FR 87, STGR 27R-28R, AFT OF DRAIN FITTINGS. REMOVED AND REPLACED SHEAR CLIP AFT OF DRAIN FITTING BETWEEN FR 87 STGR 27R-28R. REF EMB SRM 51-40-08.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 34,867 hrs · 23,113 cycles

CORRODED SHEAR CLIP, FR 82, STGR 28L-29L. REMOVED AND REPLACED SHEAR CLIP AT FR 82 BETWEEN STGR 28L-29L. REF EMB SRM 51-40-08.

Part: FILLER — CORRODED (ZONE 100) · airframe 34,867 hrs · 23,113 cycles

CORROSION AND TOOLING MARKS - RH CROSSBEAM FR14. REMOVED DAMAGE SECTION BY CUT-OUT, FABRICATED AND INSTALLED REPAIR PARTS FOR CROSSBEAM FRAME 14 REFER SRM 53-00-10/REPAIR 03P.

Part: FILLER — CORRODED (ZONE 100) · airframe 34,867 hrs · 23,113 cycles

CORROSION - RH CROSSBEAM FR17. REMOVED CORROSION AND PERFORMED PERMANENT REPAIR ON RH CROSSBEAM FR 17. REF EMB SRM 53-00-10/REPAIR 03P.

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 34,113 hrs · 22,582 cycles

L1 DOOR SLIDE PARTIALLY DEPLOYED. R&R SLIDE. TROUBLESHOT AND R&R FLEXBALL CABLE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,540 hrs · 21,408 cycles

FWD LAV EXIT SIGN DOES NOT WORK AND THE EMERGENCY LIGHTS ON CEILING PANELS 1, 3, FWD LT ENTRANCE CEILING PANEL ARE DIM. ALL THOSE LIGHTS ARE POWERED BY ELPU 2. R & R ELPU 2.

Part: SEAL DEPRESSOR — CRACKED (L1 DOOR) · airframe 30,688 hrs · 19,918 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, L1 DOOR UPPER SEAL DEPRESSOR CRACKED.

Part: ANGLE — CRACKED (FRAME 12) · airframe 30,688 hrs · 19,918 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, ANGLE CRACKED BELOW COCKPIT FLOOR.

Part: ANGLE — CRACKED (FRAME 12) · airframe 30,688 hrs · 19,918 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, CLIP CRACKED BELOW COCKPIT FLOOR.

Part: SKIN — CRACKED (LT WING) · airframe 30,688 hrs · 19,918 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, L/H WING L/E SKIN AT SLAT TRACK #4 CUTOUT IS CRACKED. REMOVED CRACK IAW SRM 57-49-01 R06.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 30,688 hrs · 19,918 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, LEVEL II CORROSION WAS FOUND @ CENTER FUSELAGE III FLOOR STRUCTURE GUSSET PLATE. GUSSET PLATE REPLACED IAW SRM 51-40-02.AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SUPPORT — CORRODED (FRAMES 89-90) · corrosion level 2 · airframe 30,688 hrs · 19,918 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND @ CENTER FUSELAGE III FLOOR STRUCTURE SUPPORT. SUPPORT WAS REPLACED IAW SRM 51-43-03, AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SEAT TRACK — CORRODED (FRAMES 74-85) · corrosion level 2 · airframe 30,688 hrs · 19,918 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, LEVEL II CORROSION WAS FOUND @ CENTER FUSELAGE III SEAT TRACK. SEAT TRACK REPLACED IAW SRM 51-43-03. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SKIN — CORRODED (FRAME 88) · corrosion level 2 · airframe 30,688 hrs · 19,918 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND @ EXTERNAL FUSELAGE SKIN WASTE SERVICING CUTOUT. REPAIR WORK DONE IAW SRM 51-70-03 AND ETD 2019-170-067922. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: FLOORBEAM — CRACKED (FRAME 86) · airframe 30,688 hrs · 19,918 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, FLOOR SUPPORT BRACKET FOUND CRACKED AT CENTER FUSELAGE III.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 30,688 hrs · 19,918 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND @ CENTER FUSELAGE III GUSSET PLATE. GUSSET PLATE REPLACED IAW SRM 51-40-02. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 30,688 hrs · 19,918 cycles

DURING FUNCTIONAL CHECK THE PILOT (CAPT) OXYGEN MASK DID NOT BREATHE OUT. MASK ASSY WAS REPLACED IAW AMM 35-10-10-10-400-801A. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SIGN — INOPERATIVE (R2 DOOR AREA) · airframe 30,688 hrs · 19,918 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, R2 DOOR EMERGENCY EXIT IDENTIFIER AT R2 DOOR FOUND NOT COMPLETELY ILLUMINATED. EXIT IDENTIFIER REPLACED IAW AMM 33-50-15. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,621 hrs · 18,405 cycles

EMERGENCY LIGHT INOP. R&R EMERGENCY LIGHT POWER UNIT BATTERY IAW AMM 33-50-01. OPS CHECK GOOD.

Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 25,566 hrs · 16,433 cycles

CORROSION ON FWD CARGO DOOR HORIZONTAL BEAM. REMOVED AND REPLACE THE BEAM IAW SRM 51-41-01 AND 51-41-02.

Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 25,566 hrs · 16,433 cycles

CORROSION ON AFT CARGO DOOR HORIZONTAL BEAM REMOVED AND REPLACED THE BEAM IAW SRM 51-41-01 AND 51-41-02.

Part: SEAL REST — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 25,566 hrs · 16,433 cycles

NUT PLATE BRACKETS AT FWD CARGO CENTER SEALREST CORRODED REMOVED AND REPLACE FWD CARGO DOOR CENTER SEALREST REF. E170 SRM 51-41-01 AND 51-41-02 PN: 170-66804-403 SEE EAMS WO H5450 SN 487 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA

Part: RETAINER — CORRODED (WASTE BOX) · corrosion level 2 · airframe 25,566 hrs · 16,433 cycles

CORROSION ON WASTE SERVICE BOX FWD RETAINER. REMOVED AND REPLACED THE RETAINERS IAW EO-53-10-0020.

Part: FLOOR SUPPORT — CORRODED (FRAME 18) · corrosion level 2 · airframe 25,566 hrs · 16,433 cycles

FLOOR SUPPORT AT FRAME 18 LBL 30 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FRAMES 83-84) · corrosion level 2 · airframe 25,566 hrs · 16,433 cycles

RIGHT OTBD FLOOR SUPPORT CORRODED FRAMES 83 - 84. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01 & 02.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 25,566 hrs · 16,433 cycles

RIGHT OTBD GUSSET CORRODED FRAME 90 REMOVED AND REPLACED THE GUSSET IAW SRM 51-41-02

Part: FLOOR SUPPORT — CORRODED (FRAMES 83-84) · corrosion level 2 · airframe 25,566 hrs · 16,433 cycles

RIGHT OUTBOARD FLOOR SUPPORT CORRODED FRAMES 83 - 84. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01 AND 02.

Part: SHEAR TIE — CORRODED (FRAME 83) · corrosion level 2 · airframe 25,566 hrs · 16,433 cycles

AFT CARGO SHEAR TIE CORRODED AT FR 83, STRINGER 27 - 28R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01 & 51-41-02.

Part: INDICATOR — OUT OF ADJUST (L1 DOOR) · airframe 24,748 hrs · 15,863 cycles

L1 PASSENGER GREEN INDICATOR ON THE LEFT SIDE OF DOOR TO SHOW LOCKED UNABLE TO SEE GREEN COMPLETELY. ADJUSTED L1 PAX DOOR GREEN INDICATOR LH SIDE OF DOOR IAW CMM 52-11-22. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 23,273 hrs · 14,816 cycles

EMERGENCY LIGHT BATTERY FAULT EICAS MESSAGE. PERFORMED FIM TASK EMB 33-50-00-810-801-A. EMERGENCY LIGHTS OPS TEST NORMAL AT THIS TIME.

Part: INDICATOR — OUT OF ADJUST (L1 DOOR) · airframe 23,240 hrs · 14,789 cycles

L1 DOOR TOP, LT INDICATOR SHOWING CLEAR, NOT GREEN WHEN ARMED. ADJUSTED L1 DOOR TOP LT INDICATOR AND LINING IAW AMM 25-23-04, NO DEFECTS NOTED. OPEN AND CLOSED L1 DOOR SEVERAL TIMES, THE INDICATOR SHOWED GREEN. NO DEFECTS NOTED.

Part: SWITCH — DIRTY (PAX DOOR) · airframe 23,202 hrs · 14,756 cycles

DOOR PAX FWD OPEN EICAS MESSAGE IN FLIGHT, PRESSURE NORMAL. CLEANED SWITCHES ON MAIN DOOR AND OPS CHECK IAW AMM 52-70-00. OPS CHECK GOOD.

Part: SEAL REST — CORRODED (SERVICE DOORWAY) · corrosion level 2 · airframe 21,948 hrs · 13,913 cycles

AFT SERVICE DOOR LOWER CENTRAL SEAL REST IS CORRODED. R & R AFT SERVICE DOOR LOWER CENTER SEAL REST IAW SRM 51-41-01.

Part: BEAM — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 21,948 hrs · 13,913 cycles

AFT SERVICE DOOR LOWER BEAM CORRODED FRAMES 85-86. R & R AFT SERVICE DOOR LOWER BEAM 51-43-03.

Part: BEAM — CORRODED (FRAMES 16-19) · corrosion level 2 · airframe 21,984 hrs · 13,913 cycles

FWD PAX DOOR LOWER BEAM HAS BUBBLED PAINT AROUND THE AFT SLIDE FITTING AND PAINT DAMAGE IN THE CENTER OF THE BEAM BETWEEN FRAMES 16 AND 19. COMPLIED WITH ETD2015-170-039331.

Part: CROSSBEAM — CORRODED (FRAME 13) · corrosion level 2 · airframe 21,984 hrs · 13,913 cycles

FRAME 13 CROSSBEAM IS CORRODED AT RBL 13 TO 35. COMPLIED WITH ETD2015-170-039511. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FRAME 84) · airframe 21,948 hrs · 13,913 cycles

FRAME 84 CROSSBEAM IS CORRODED AT RBL 15" TO 30". C/W ETD2015-170-041290.

Part: SEAT TRACK — CORRODED (FRAMES 84-85) · corrosion level 2 · airframe 21,948 hrs · 13,913 cycles

RT SEAT TRACK CORRODED FRAME 84-85, RBL 12". REPAIRED IAW ETD2015-170-039933.

Part: CLOSEOUT PANEL — CORRODED (FWD CARGO BAY) · corrosion level 2 · airframe 21,984 hrs · 13,913 cycles

CORROSION FOUND ON FWD CARGO CLOSEOUT PANEL. R & R THE CLOSEOUT PANEL IAW AMM 20-10-07.

Part: STRAP — CORRODED (FRAME 85-86) · airframe 21,948 hrs · 13,913 cycles

AFT PASSENGER DOOR LOWER BEAM FWD STRAP HAS CORROSION FRAME 85-86. R & R STRAP.

Part: STRUCTURE — CORRODED (FRAMES 12-14) · airframe 21,948 hrs · 13,913 cycles

FWD RT SILL BETWEEN FRAMES 12 AND 14 RT BUTTLINE 36" TO 49" IS CORRODED. R & R SILL.

Part: STRAP — CORRODED (FRAMES 85-86) · airframe 21,948 hrs · 13,913 cycles

AFT SERVICE DOOR LOWER BEAM FWD STRAP HAS CORROSION FRAME 85-86. R & R AFT SERVICE DOOR LOWER BEAM FWD STRAP. MAJOR REPAIR.

Part: CROSSBEAM — CORRODED (FRAME 14) · airframe 21,984 hrs · 13,913 cycles

FRAME 14 CROSSBEAM IS CORRODED AT RBL 13 TO 35. COMPLIED WITH ETD2015-170-039511. MAJOR REPAIR.

Part: SEAL REST — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 21,984 hrs · 13,913 cycles

CORROSION FOUND ON AFT CARGO DOOR LOWER CENTER SEAL REST. R &R THE CENTER SEAL REST IAW SRM 51-41-01.

Part: UPPER SHEET — CORRODED (FRAMES 84-85) · corrosion level 2 · airframe 21,984 hrs · 13,913 cycles

AFT WET RT UPPER SHEET CORRODED FRAME 84-85, RBL 12". R & R UPPER SHEET WITH NEW, SRM 53-23-10, FIGURE 55B, ITEM 60.

Part: SEAT TRACK — CORRODED (FRAMES 86-87) · corrosion level 2 · airframe 21,948 hrs · 13,913 cycles

RIGHT SEAT TRACK CORRODED FRAMES 86-87 RBL 12. BLENDED CORROSION IAW SRM 51-10-03. TRIMMED AND CUTOUT DAMAGE, NDT HFEC INSPECTION OF CUTOUT DAMAGE. FABRICATED DOUBLER AND INSTALLED IAW ETD 2015-170-039960.

Part: SEAT TRACK — CORRODED (FRAMES 12-20) · corrosion level 2 · airframe 21,984 hrs · 13,913 cycles

RT SEAT TRACK IS CORRODED BETWEEN FRAMES 12 AND 20, RT BUTTLINE 12. R & R SEAT TRACK.

Part: SUPPORT — CORRODED (FRAME 89) · airframe 21,984 hrs · 13,913 cycles

AFT WET RT PANEL SUPPORT CORRODED FRAME 89, RBL 38. R & R PANEL SUPPORT.

Part: SEAT TRACK — CORRODED (FRAMES 86-87) · airframe 21,984 hrs · 13,913 cycles

RT SEAT TRACK CORRODED, FRAME 86-87, RBL 12". BLENDED CORROSION RBL 11", 1" X 1" X .0521" AREA DAMAGE, REF SRM 51-10-03. TRIMMED AND CUTOUT DAMAGE, NDT HFEC INSPECTION OF CUTOUT DAMAGE. FABRICATED DOUBLER AND INSTALLED IAW ETD 2015-170-039960.

Part: LEVER — LACK OF LUBE (R2 DOOR) · airframe 21,533 hrs · 13,659 cycles

R2 DOOR ARMING LEVER HARD TO MOVE. LUBED, OPS CHECK R2 DOOR IAW AMM 52-42-20. CHECKS GOOD.

Part: LINER — UNSECURE (L2 DOOR) · airframe 20,008 hrs · 12,743 cycles

L2 DOOR WON'T OPEN. SECURED L2 DOOR LINER IAW AMM 25-23-09. OPS CHECK OK, NO FURTHER DAMAGE AT THIS TIME.

Part: SHEAR TIE — CORRODED (FRAME 86) · corrosion level 2 · airframe 19,643 hrs · 12,478 cycles

CORROSION FOUND ON FRAME 86 SHEAR TIE BETWEEN STRINGERS 28-87R. R & R SHEAR TIE. MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (FRAME 88) · corrosion level 2 · airframe 19,643 hrs · 12,478 cycles

CORROSION FOUND ON SHEAR TIE AT FRAME 88, S28-29R. R & R SHEAR TIE.

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,643 hrs · 12,478 cycles

CORROSION FOUND ON LAVATORY PAN UPPER STIFFENER. R & R STIFFENER.

Part: CLOSEOUT PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,643 hrs · 12,478 cycles

CORROSION FOUND ON FWD CARGO CLOSEOUT PANEL IN MULTIPLE AREAS. R & R CLOSEOUT PANEL.

Part: RIB — CRACKED (RT WING) · airframe 16,764 hrs · 10,429 cycles

MAJOR REPAIR - RT WING RIB 10 IS CRACKED ON UPPER FLANGE AFT OF SPAR II. REMOVED AND REPLACED RT WING RIB 10 PANEL IAW SRM 51-43-01 AND 51-43-02.

Part: HANDLE — DIRTY (L1 DOOR) · airframe 16,141 hrs · 9,990 cycles

L1 DOOR ARMING LEVER DOESN'T ENGAGE EVERY TIME. CLEANED AND LUBRICATED L1 DOOR HANDLE (ARMING). PERFORMED OPS CHECK IAW EMB 170 MM 52-11-00. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 16,062 hrs · 9,947 cycles

UPON POWER UP EICAS MESSAGE "EMER LT BATT FAULT". REPOWERED A/C IAW AMM, NO FAULTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 16,042 hrs · 9,934 cycles

UPON POWER UP EICAS MESSAGE "EMER LT BATT FAULT." REPOWERED A/C IAW AMM 49-00-00, NO FAULTS NOTED AT THIS TIME.

Part: SLIDE — DEFECTIVE (L2 DOOR) · airframe 14,740 hrs · 9,200 cycles

THE 2L DOOR NOT CLOSING. REMOVED AND REPLACED EMERGENCY EVACUATION SLIDE ASSY IAW EMB 170 MM 25-65-01. OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (L1 DOOR) · airframe 13,754 hrs · 8,625 cycles

L1 DOOR DIFFICULT TO OPEN. OUTER HANDLE DROPS UNLESS HELD UP. DOOR SEEMS TO BE HITTING LOW ON CAMS. OPERATED L1 DOOR WITH NO DEFECTS NOTED IAW EMB 170 MM 52-11-01.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,402 hrs · 7,033 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE LONGITUDINAL BEAM AT FRAME 17. MAINTENANCE PERFORMED MAJOR REPAIR ON THE LONGIUDINAL BEAM AT FRAME 17 IAW EMBRAER ETD 2010-170/09724, EMB 170 SRM 51-10-02, 51-21-00 & 51-41-02. REF MATERIAL USED. 2024-T3 .080 PO 320478 AND 2024-T3 .071 PO 000587-2010. A/C IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,402 hrs · 7,033 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND IN NUMEROUS AREAS OF THE RIGHT LONGITUDINAL BEAM FROM FRAME 12 TO FRAME 17. MAINTENANCE PERFORMED MAJOR REPAIR TO RIGHT LONGITUDINAL BEAM FROM FRAME 12 TO FRAME 17 IAW EMBRAER ETD 2010-170/09724, EMB 170 SRM 51-40-02 & 51-10-02. REF MATERIAL USED, 2024-T3 .080 PO 320478 AND 2024-T3 .071 PO 000587-2010.

Part: FASTENER — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 11,402 hrs · 7,033 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL TWO CORROSION ON THE FASTENERS FOR THE WASTE SERVICE DOOR HINGE. MX REPLACED THE FASTENERS IAW EMB 170 SRM 51-43-02. P/N MS14218AD4 A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.

Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 10,287 hrs · 6,271 cycles

CREW REPORTED THE COCKPIT EMERGENCY LIGHT WAS INOP. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK PER EMB AMM, OPS CHECK GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 8,798 hrs · 5,366 cycles

MAJOR REPAIR: LOWER LT FORWARD FUSELAGE SKIN FOUND 5.25 INCH LONG CRACK; REPAIRED IAW EMBRAER IC2009-170/07387.