N656RW

Part: HINGE FITTING — ELONGATED (ZONE 300) · airframe 45,106 hrs · 28,220 cycles

***********MAJOR******** RH ELEVATOR #3 HINGE FITTING IB BUSHING OVERSIZED. REPAIRED PN 170-62073-407 IAW ETD 2022-028564******MAJOR*******

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

LEVEL 2 CORROSION FOUND ON WING TO FUSELAGE FAIRING SUPPORT STRUCTURE FRAME WEB AT FR52. FRAME WEB REPLACED IAW SRM 51-41-01

Part: RIB — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND CORROSION FOUND ON MID WING TO BODY SUPPORT RIB FR47 BL 0. REPLACED PN 170-14708-007 IAW SRM 51-43-03 AC RTS'ED

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

LEVEL 2 CORROSION FOUND ON RH MLG UPLOCK FITTING AFT LOWER HOLE. REPLACED MLG UPLOCK FITTING IAW SRM 51-43-04

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

LEVEL 2 CORROSION FOUND ON CENTER FUSELAGE 2 RH IB SEAT TRACK FR43-59. REPLACED RT INBD SEAT TRACK IAW SRM 51-43-05

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND FWD CARGO COMPT CORROSION FOUND ON SHEAR CLIP AR FR16 BTWN STR 27L-28L. REPLACED PN 170-03859-001 IAW SRM 51-41-01, 51-41-02.- AC WAS RTS

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

LEVEL 2 CORROSION FOUND ON FWD CARGO COMPARTMENT SHEAR CLIP AT FR16 BETWEEN STR 27L-28L. REPLACED SHEAR CLIP IAW SRM 51-41-01

Part: ANGLE — CORRODED (ZONE 100) · airframe 45,106 hrs · 28,220 cycles

LEVEL 2 CORROSION FOUND ON AFT CARGO DOOR CUTOUT LOWER SEAL DEPRESSOR ANGLE. DEPRESSOR REPLACED IAE SRM 51-40-02

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

LEVEL 2 CORROSION FOUND ON CENTER FUSELAGE 3 LH IB SEAT TRACK FR 74-84. REPLACED SEAT TRACK IAW SRM 51-43-03

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

LEVEL 2 CORROSION FOUND ON FORWARD FUSELAGE LT IB SEAT TRACK. REPLACED SEAT TRACK IAW SRM 51-41-02

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

LEVEL 2 CORROSION FOUND ON CENTER FUSELAGE 2 RH IB SEAT TRACK FR43-59. REPLACED LT INBD SEAT TRACK IAW SRM 51-42-02

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

LEVEL 2 CORROSION FOUND ON CENTER FUSELAGE 1 RH IB SEAT TRACK FR23-34. REPLACED SEAT TRACK IAW SRM 51-43-03

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND CORROSION FOUND ON FWD FUSE FLOOR STRUCTURE SHEAR WEB BTWN FR 13 FR16 LH SIDE OF L1 DOOR. REPLACED PN 170-12118-001 IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND. FORWARD FUSE CORROSION FOUND ON RH IB SEAT TRACK FR12-20. REPLACED PN 170-03263-001 IAW SRM 51-41-02, 51-43-03 AC WAS RTS

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

LEVEL 2 CORROSION FOUND ON CENTER FUSELAGE 3 RT IB SEAT TRACK FR 74-84. REPLACED SEAT TRACK IAW SRM 51-43-03

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND CORROSION FOUND ON FWD FUSE FLOOR STRUCTURE SHEAR WEB BTWN FR12-14 RH SIDE FWD OF R1 DOOR. REPLACED PN 170-05663-003 IAW SRM 51-43-02, 51-41-02. AC WAS RTS

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND.-CORROSION FOUND ON FWD FUSE FLOOR STRUCTURE SHEAR WEB BTWN FR19-20 LH SIDE AFT OF L1 DOOR. REPLACED PN 170-07311-001 IAW SRM 51-41-02, 51-43-04. AC WAS RTS

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND. CENTER FUSE 3 CORROSION FOUND ON RH SUPPORT PANEL AT FR84. REPLACED PN 170-92908-001 IAW SRM 51-41-02. AC WAS RTS

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND CORROSION FOUND ON FWD FUSE FLOOR STRUCTURE LAV FITTING FR 15LH. REPLACED PN 170-13633-003 IAW SRM 51-43-03 AC RTS'ED

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND AFT CARGO COMPT. CORROSION FOUND ON SHEAR CLIP AT FR 84 BTWN STR 29R-28R. REPLACED PN 170-91908-001 IAW SRM 51-43-03.. AC RTS'ED

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND CENTER FUSE 3 CORROSION FOUND ON SHEAR CLIP FR 85 BTWN STR 29R-28R. REPLACED PN 170-66064-001 IAW SRM 51-41-02. AC RTS'ED

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND -CORROSION FOUND ON CF 3 FLOOR STRUCTURE GUSSET PLATE AT BL0 AND FR90. REPLACED PN 170-86119-003 IAW SRM 51-43-01. AC WAS RTS

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND CORROSION FOUND ON CF3 CABIN FLOOR SUPPORT RH OB SIDE BTWN FR 88 AND 90. REPLACED PN 170-86181-005IAW SRM 51-42-01, 51-43-01 AC RTS'ED

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND -CORROSION FOUND ON CF3 FLOOR STRUCTURE CENTER SHEAR WEB BTWN FR 87-88. REPLACED PN 170-65928-001 IAW SRM 51-42-01 AC WAS RTS

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND CORROSION FOUND CF3 FLOOR STRUCTURE GUSSET PLATE INBD SIDE FR 90. REPLACED PN 170-60257-001 IAW SRM 51-41-02. AC RTS'ED

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND CORROSION FOUND ON REAR FUSELAGE CABIN FLOOR SUPPORT INTERCOSTAL BTWN FR90 AND 92 RBL 11.REPLACED IAW PN 170-61041-402 SRM 51-41-01, 51-43-03 AC RTS'ED

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND -.CORROSION FOUND ON CF3 FLOOR SUPPORT UPPER SHEET AFT OF RH INBD CABIN SEAT TRACK BTWN FR85-86. REPLACED PN 170-86101-001 IAW SRM 51-43-03. AC WAS RTS

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND CORROSION FOUND ON CF3 FLOOR SUPPORT UPPER SHEET AFT OF LH INBD CABIN SEAT TRACK BTWN FR 85-86. REPLACED PN 170-86101-001 IAW SRM 51-43-03. AC WAS RTS

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND -CORROSION FOUND ON CF3 FLOOR STRUCTURE RH SHEAR WEB BTWN FR87-88.REPLACED PN 170-91919-001 IAW SRM 51-43-01, 51-42-01.. AC WAS RTS

Part: RIB — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,106 hrs · 28,220 cycles

WHILE AC WAS IN FOR HVY CK FOUND -LH GEAR WELL FR52 CRACK . REPLACED PN 171-19903-401 IAW SRM 51-43-03, 51-41-01.. AC WAS RTS

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 42,333 hrs · 26,339 cycles

STEER FAIL WHEN GEAR EXTENDED. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. UNABLE TO STEER AFTER LANDING. PERFORMED FIM TASK 45-45-00-810-973-A, MESSAGE CLEARED. OPS CHECK GOOD.

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 41,694 hrs · 25,943 cycles

EMERGENCY LIGHT BATTERY FAULT. CHARGED EMERGENCY POWER LIGHT UNIT.

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 41,430 hrs · 25,759 cycles

PHOTOLUMINESCENT STRIP BROKEN IN FRONT OF SEAT 1C. R & R SEGMENT OF STRIP.

Part: LIGHT — MISSING (SEAT 7B) · airframe 40,664 hrs · 25,226 cycles

FLOOR LEVEL EXIT PATH STRIP MISSING AT SEAT 7B. INSTALLED PHOTOLUMINESCENT INDICATOR STRIP LIGHT AT SEAT 7B IAW AMM 33-50-21.

Part: SHEAR TIE — CORRODED (FRAME 82) · corrosion level 2

**WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK**MAINTENANCE FOUND 633-57 CF III INTERNAL LOWER STRUCTURE FR82 STR 27-28R, SHEAR CLIP FOUND CORRODED. REPLACED SHEAR CLIP IAW SRM 51-41-01 / 51-41-02. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 40,117 hrs · 24,887 cycles

**WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** MAINTENANCE FOUND 633-21 FWD FUSELAGE WET AREA FLOOR STRUCTURE FR16 LBL45" SILL WEB FOUND CORRODED. REPLACED SILL WEB IAW SRM 51-41-02 / 51-43-04. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR TIE — CORRODED (FRAME 82) · corrosion level 2

**WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** MAINTENANCE FOUND 633-58 CF III INTERNAL LOWER STRUCTURE FR82 STR 28 - 29R. SHEAR CLIP FOUND CORRODED. REPLACED SHEAR CLIP IAW SRM 51-41-01, 5141-02, 51-43-03. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR TIE — CORRODED (FRAME 83) · corrosion level 2 · airframe 40,117 hrs · 24,887 cycles

***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** CF III INTERNAL LOWER STRUCTURE FR83 STGR27-28R, SHEAR CLIP FOUND CORRODED. REPLACED SHEAR CLIP IAW SRM 51-41-01/51-41-02/51-43-03. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR TIE — CORRODED (FRAME 83) · corrosion level 2 · airframe 40,117 hrs · 24,887 cycles

***WHILE A/C WAS OUT OF SERVICE FOR HEAVY CHECK*** CF III INTERNAL LOWER STRUCTURE FR83 STGR28-29R, SHEAR CLIP FOUND CORRODED. REPLACED SHEAR CLIP IAW SRM 51-41-01/51-41-02/51-43-03. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 40,117 hrs · 24,887 cycles

***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** FWD FUSELAGE LOWER STRUCTURE FR16 STGR27-28R, SHEAR CLIP CORRODED. REPLACED SHEAR CLIP IAW SRM 51-41-01 & 51-41-02. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: COUPLING — MISSING (FUEL VENT) · airframe 40,117 hrs · 24,887 cycles

***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** UPON INSPECTION OF RH WING FUEL TANK, VENT PIPING INSIDE ACC. PNL. 631EB WAS FOUND MISSING ONE O-RING AND CLAM-SHELL SLEEVE. REPLACED IAW AMM 20-10-13-400-801-A. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 40,117 hrs · 24,887 cycles

***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** FWD FUSELAGE LOWER STRUCTURE FR17 STGR 27-28L, SHEAR CLIP CORRODED. REPLACED SHEAR CLIP IAW SRM 51-41-01 & 51-41-02. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: DOUBLER — CORRODED (FRAMES 19-20) · corrosion level 2 · airframe 40,117 hrs · 24,887 cycles

***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** FWD FUSELAGE LOWER STRUCTURE FR19-20 STR26-27L, ANTENNA INTERNAL DOUBLER FOUND CORRODED. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 40,117 hrs · 24,887 cycles

***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** FWD FUUSELAGE LOWER STRUCTURE FR 17 STGR27-28R, SHEAR CLIP CORRODED. REPLACED SHEAR CLIP IAW SRM 51-41-02 & 51-41-01. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SKIN — DENTED (FRAMES 1-2) · airframe 40,117 hrs · 24,887 cycles

***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** FWD FUSELAGE EXTERNAL SKIN FR1-2, STGR20-22L, 4 PROTRUDING DENTS AT RVSM AREA. 4 EA DENTS IN LH RVSM AREA WERE FOUND TO BE WITHIN LIMITS IAW ETD2019-170-157004. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SKIN — NONE (FRAMES 19-20) · airframe 40,117 hrs · 24,887 cycles

***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** "MAJOR REPAIR" FWD FUSELAGE EXTERNAL SKIN FR19-20 STGR23-24, 17 UNRECORDED FLUSH RIVETS FOUND. FWD FUSELAGE SKIN REPAIRED IAW SRM 53-10-01 REPAIR 12P. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SKIN — CRACKED (RT WING) · airframe 40,117 hrs · 24,887 cycles

R/H WING, SLAT TRACK #5 FIXED LEADING EDGE CUTOUT CRACKED. REPAIRED PER SRM 57-49-01 REPAIR #6

Part: FLOORBEAM — CRACKED (FRAME 12) · airframe 40,117 hrs · 24,887 cycles

FWD FUSELAGE FLOOR STRUCTURE ANGLE FOUND CRACKED. R&R'D ANGLE IAW 51-41-02

Part: FLOORBEAM — CRACKED (FRAME 12) · airframe 40,117 hrs · 24,887 cycles

FWD FUSELAGE FLOOR STRUCTURE AT FR 12 BL 0, CROSSBEAM ANGLE FOUND CRACKED. R&R'D ANGLE I.A.W. SRM 51-41-02

Part: DOUBLER — CORRODED (FRAME 19) · corrosion level 2 · airframe 40,117 hrs · 24,887 cycles

**WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** MAINTENANCE FOUND 633-22 FWD FUSELAGE WET AREA FLOOR STRUCTURE FR19 LBL36"DOUBLER UPPER SURFACE FOUND CORRODED. REPLACED DOUBLER IAW SRM 51-41-02 / 51-43-04. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SEAT TRACK — CORRODED (FRAMES 17-19) · corrosion level 2 · airframe 40,117 hrs · 24,887 cycles

**WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** MAINTENANCE FOUND 633-23 FWD FUSELAGE WET AREA FLOOR SRUCTURE FR17/18/19 LHIB SEAT TRACK BEAM UPPER FLANGE FOUND CORRODED. REPLACED TRACK BEAM UPPER FLANGE IAW SRM 53-10-10 AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SKIN — DAMAGED (FRAMES 23-24) · airframe 40,117 hrs · 24,887 cycles

***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** "MAJOR REPAIR" CF I EXTERNAL SKIN FR23-24 STGR16-17L, UNRECORDED RIVET FOUND. REPAIRED SKIN IAW ETD2019-170-158221. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,117 hrs · 24,887 cycles

** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** LH HORIZONTAL STAB RIBS 10 AND 11 BETWEEN FRONT SPAR AND MIDDLE SPAR SUSPECT CRACK. C/A REPLACED RIBS 10-11-12 PER SB 170-55-0014. RIB 12 REPLACED AS PART OF THE SB. WEB RIB 10 PN 170-62567-003 RIB 11 ASSY PN 170-62611-401. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 40,117 hrs · 24,887 cycles

***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** ELPU #2 FAILED EMERGENCY LIGHTS FUNCTIONAL CHECK. EIPU #2 REPLACED IAW AMM 33-50-01-400-801-A. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: STRUT — NOT REPORTED (NLG) · airframe 39,889 hrs · 24,736 cycles

LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FERRIED TO CMH. R&R NLG STRUT ASSEMBLY.

Part: WIRE HARNESS — DAMAGED (SLAT SYSTEM) · airframe 36,556 hrs · 22,710 cycles

AT 15,000 FEET, SLATS FAILED. DECLARED EMERGENCY, AND LANDED WITHOUT INCIDENT. TROUBLESHOT TO THE LT SLAT 2/3 HARNESS. R & R THE HARNESS IAW MM 27-83-07. AS A PRECAUTION, MOC REQUESTED RH SLAT 3/4 HARNESS BE REPLACED, R & R HARNESS.

Part: LIGHT — UNSECURE (CABIN) · airframe 35,153 hrs · 21,864 cycles

PART OF EMERGENCY LIGHT STRIP PEELED UP IN FIRST CLASS SECTION.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 34,798 hrs · 21,654 cycles

MAINTENANCE REPORTED LEVEL 2 CORROSION IN THE AFT WET AREA FLOOR SPLICE PLATE AT FR90 RBL24. MAINTENANCE REMOVED AND REPLACED THE AFT WET AREA FLOOR SPLICE GUSSET PLATE AT FR90 RBL24 IAW E170 SRM 51-41-02, 51-23-06 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 89-90) · corrosion level 2 · airframe 34,798 hrs · 21,654 cycles

MAINTENANCE REPORTED LEVEL 2 CORROSION IN THE AFT WET AREA, FLOOR SUPPORT INTERCOSTAL AT FR89-FR90, RBL10. MAINTENANCE REMOVED AND REPLACED THE AFT WET AREA INTERCOSTAL PANEL SUPPORT AT FR89-FR90, RBL10 IAW E170 SRM 51-43-03, 51-40-02 AND 51-40-03.

Part: SPLICE PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 34,798 hrs · 21,654 cycles

MAINTENANCE REPORTED CORROSION IN THE AFT WET AREA, LT SHEAR PANEL OUTBOARD SPLICE PLATE AT FRAMES 87-88. REMOVED AND REPLACED THE SHEAR PANEL OUTBOARD SPLICE PLATE IAW SRM 51-40-08, 51-75-16, 51-23-06 AND 51-40-02.

Part: SUPPORT — CORRODED (FRAMES 17-22) · corrosion level 2 · airframe 34,798 hrs · 21,654 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION AT THE FORWARD CARGO DOOR CUTOUT 6EA LOWER KICK PLATE BRACKETS. MAINTENANCE REMOVED AND REPLACED 6EA LOWER KICK PLATE BRACKETS (SUPPORTS) AT THE FORWARD CARGO DOOR CUTOUT (P/N'S 170-67032-401 & 170-67176-403) IAW E170 SRM 51-12-01, 51-10-03, 51-41-01, 51-40-02 AND 51-75-16. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 34,798 hrs · 21,654 cycles

MAINTENANCE REPORTED LEVEL 2 CORROSION IN THE AFT WET AREA, FLOOR SPLICE PLATE AT FR90 RBL12. MAINTENANCE REMOVED AND REPLACED THE AFT WET AREA, FLOOR SPLICE GUSSET PLATE AT FR90 RBL12 IAW E170 SRM 51-41-02, 51-40-02 AND 51-23-06.

Part: FLOOR SUPPORT — CORRODED (FRAMES 88-90) · corrosion level 2 · airframe 34,798 hrs · 21,654 cycles

MAINTENANCE REPORTED LEVEL 2 CORROSION IN THE AFT WET AREA LH FLOOR SUPPORT WEB IN MULTIPLE AREAS BETWEEN FR88 AND FR90 MAINTENANCE REMOVED AND REPLACED THE AFT WET AREA LH FLOOR PANEL SUPPORT WEB BETWEEN FR88 AND FR90 IAW E170 SRM 51-41-01, 51-43-03 AND 51-42-03.

Part: DOUBLER — CORRODED (FRAMES 84-85) · corrosion level 2 · airframe 34,798 hrs · 21,654 cycles

MAINTENANCE REPORTED LEVEL 2 CORROSION IN THE AFT WET AREA RH INBOARD SEAT TRACK BEAM AT FR84-FR85. MAINTENANCE REMOVED DAMAGE AND PERFORMED REPAIR WITH FABRICATED FILLER AND DOUBLER ON THE RH INBOARD SEAT TRACK BEAM AT FR84-FR85 IAW E170 SRM 53-23-10, 51-43-03 AND 51-41-01.

Part: FILLER — CORRODED (FRAMES 84-85) · corrosion level 2 · airframe 34,798 hrs · 21,654 cycles

MAINTENANCE REPORTED LEVEL 2 CORROSION IN THE AFT WET AREA LT INBOARD SEAT TRACK BEAM AT FR84-FR85. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED REPAIR WITH FABRICATED DOUBLER AND FILLER USING 7475T761, .080 IAW SRM 53-23-10, 51-43-03 AND 51-41-01.

Part: SPLICE PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 34,798 hrs · 21,654 cycles

***WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION IN THE AFT WET AREA, RH SHEAR PANEL SPLICE PLATE AT FR87-FR88. MAINTENANCE REMOVED AND REPLACED THE AFT WET AREA, RH SHEAR PANEL SPLICE PLATE AT FR87-FR88 IAW E170 SRM 51-40-08, 51-75-16, 53-23-06 AND 51-40-02. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: DOOR — CORRODED (WASTE SERVICE) · corrosion level 2 · airframe 34,798 hrs · 21,654 cycles

MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE WASTE SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED THE WASTE SERVICE DOOR IAW AMM 20-10-01, 11-21-03 & 51-24-06.

Part: SUPPORT — CORRODED (FRAMES 17-22) · corrosion level 2 · airframe 34,798 hrs · 21,654 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION AT THE FORWARD CARGO DOOR CUTOUT 6EA LOWER KICK PLATE BRACKETS. MAINTENANCE REMOVED AND REPLACED 6EA LOWER KICK PLATE BRACKETS (SUPPORTS) AT THE FORWARD CARGO DOOR CUTOUT (P/N'S 170-67032-401 & 170-67176-403) IAW E170 SRM 51-12-01, 51-10-03, 51-41-01, 51-40-02 AND 51-75-16. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: WEB — CORRODED (FRAMES 13-14) · corrosion level 2 · airframe 34,798 hrs · 21,654 cycles

MAINTENANCE REPORTED LEVEL 2 CORROSION AT THE FORWARD WET AREA IN MULTIPLE AREAS AT THE FLOOR WEB BETWEEN FRAMES 13 AND 14 JUST INBOARD OF R1 DOOR. MAINTENANCE REMOVED AND REPLACED THE FLOOR WEB IAW SRM 51-75-16, 51-41-02, 51-43-04, 51-40-02, 51-23-06 AND ETD2017-170-105765.

Part: PROFILE — CRACKED (FRAME 52) · airframe 34,798 hrs · 21,654 cycles

MAINTENANCE REPORTED A CRACK ON THE FRAME 52 FLANGE FOR THE RECEPTACLES IN THE LT WHEEL WELL. MAINTENANCE REMOVED AND REPLACED THE FLANGE (PROFILE L) FOR THE RECEPTACLES AT FRAME 52 IN THE LT WHEEL WELL IAW SRM 51-41-01, 51-40-02 AND 51-45-00.

Part: BEAM — CORRODED (FRAMES 13-14) · corrosion level 2 · airframe 34,798 hrs · 21,654 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION IN THE FORWARD WET AREA AROUND THE GALLEY MOUNT HOLE AT FR13-FR14, RBL10. MAINTENANCE REMOVED CORROSION AND REPAIRED DAMAGED IN THE FORWARD WET AREA AROUND THE GALLEY MOUNT HOLE AT FR13-FR14, RBL10 WITH FABRICATED DOUBLER FROM 2024T3 .080 (REF PREMIER AVIATION PO# P4125C364) AND FILLER FROM 2024T3 .071 (REF PREMIER AVIATION PO# PS-1611068) IAW E170 SRM 53-10-10, 51-41-01, 51-41-02 AND EMBRAER ETD2017-170-105762. AIRCRAFT IS CURRENTLY STILL OUR OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: DOUBLER — CORRODED (FRAMES 13-16) · corrosion level 2 · airframe 34,798 hrs · 21,654 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION IN THE FORWARD WET AREA AROUND THE LAVATORY MOUNT HOLE FORWARD OF FR16, LBL12. MAINTENANCE REMOVED AND REPLACED THE SHEAR WEB FLOOR DOUBLER IN THE FORWARD WET AREA AROUND THE LAVATORY MOUNT HOLE FORWARD OF FR16, LBL12. IAW E170 SRM 51-75-16, 51-41-02, 51-40-02, 51-40-04 AND 51-23-06. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: INLET — CRACKED (APU) · airframe 34,798 hrs · 21,654 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED THE APU INTAKE RIBS ARE CRACKED (2 TOTAL). MAINTENANCE REMOVED AND REPLACED THE APU AIR INLET ASSEMBLY IAW AMM 49-16-01. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: RIB — CORRODED (FRAME 52) · airframe 34,798 hrs · 21,654 cycles

MAINTENANCE REPORTED A CRACK AT FRAME 52 RIB ASSY. IN THE LT WHEEL WELL. MAINTENANCE REMOVED AND REPLACED THE RIB ASSY. AT FRAME 52 IN THE LT WHEEL WELL IAW E170 SRM 51-41-01 AND 51-40-02.

Part: LAVATORY — LEAKING · corrosion level 2 · airframe 33,681 hrs · 20,917 cycles

CORROSION ON SHEAR TIE AT FRAME 86 BETWEEN STRINGERS 27R AND 28R DUE TO LAVATORY LEAK. R & R SHEAR TIE.

Part: SHEAR TIE — CORRODED (FRAME 87) · corrosion level 2 · airframe 33,681 hrs · 20,917 cycles

CORROSION ON SHEAR TIE AT FRAME 87 BETWEEN STRINGERS 27R AND 28R. R&R SHEAR TIE.

Part: ROD — UNKNOWN (COUNTERBALANCE) · airframe 33,152 hrs · 20,592 cycles

L1 DOOR HAS NO TENSION IN THE HANDLE WHEN CLOSED FROM INSIDE. R & R THE FWD COUNTERBALANCE ROD IAW AMM 52-11-20. OPS CHECKED GOOD.

Part: HANDLE — LACK OF LUBE (L1 DOOR) · airframe 32,851 hrs · 20,377 cycles

L1 DOOR IS DIFFICULT TO OPEN FROM OUTSIDE THE AIRCRAFT. LUBRICATED OUTSIDE DOOR HANDLE. OPS CK GOOD REF AMM 52-11-00.

Part: HYDRAULIC LINE — WORN (HYDRAULIC SYS) · airframe 32,745 hrs · 20,308 cycles

FLYING RDU - LGA, CREW RECEIVED A HYD 2 LO QTY MESSAGE, FOLLOWED BY A HYD SYS 2 FAIL MESSAGE. CREW DECLARED AN EMERGENCY, USED THE ALTERNATE GEAR EXTENSION LEVER TO LOWER THE GEAR AND DIVERTED TO EWR WHERE THEY LANDED WITHOUT INCIDENT. AIRCRAFT WAS PULLED VIA TUG INTO GATE WHERE PASSENGERS DEPLANED. MAINTENANCE FOUND LINE IN LEFT HAND PYLON TO HAVE BROKEN CLAMP AND RUB THRU. MAINTENANCE REMOVED AND REPLACED PRESSURE RETURN LINE PER AMM AND OPS CHECKED GOOD.

Part: DIAPHRAGM — DAMAGED (ASSI ST BOTTLE) · airframe 32,666 hrs · 20,267 cycles

CREW REPORTED THAT THE L1 DOOR ASSIST BOTTLE PRESSURE WAS ZERO. MAINTENANCE FOUND THE DIAPHRAM DAMAGED. REMOVED AND REPLACED THE L1 DOOR ASSIST BOTTLE DIAPHRAM AND SHEAR PIN, SERVICED BOTTLE IAW AMM AND OPS CHECKED GOOD.

Part: INDICATOR — OUT OF ADJUST (L1 DOOR) · airframe 32,655 hrs · 20,260 cycles

CREW REPORTED THAT THE L1 DOOR LATCH INDICATOR DID NOT FULLY SHOW. MAINTENANCE ADJUSTED L1 DOOR LATCH INDICATOR PER AMM AND OPS CHECKED GOOD.

Part: UNKNOWN — UNKNOWN (R2 DOOR) · airframe 32,325 hrs · 20,056 cycles

CREW REPORTED THAT THE R2 DOOR WOULD NOT ARM. MAINTENANCE CHECKED DOOR IAW AMM AND OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (LE SLATS) · airframe 32,270 hrs · 20,025 cycles

DURING FLIGHT, CREW RECEIVED A SLAT FAIL MESSAGE. CREW EXECUTED A MISSED APPROACH TO RUN QRH. CREW THEN RECEIVED FLAP/SLAT FAIL MESSAGE, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, FOUND RIGHT INBOARD SKEW SENSOR CONNECTOR LOOSE. MAINTENANCE RESECURED AND SAFETIED PER EMB AMM AND OPS CHECKED GOOD.

Part: HANDLE — OUT OF ADJUST (R1 DOOR) · airframe 31,670 hrs · 19,626 cycles

CREW REPORTED THAT THE ARMING HANDLE FOR THE R1 DOOR DID NOT AGREE WITH THE INDICATION ON THE SLIDE AND THE HANDLE WAS NOT GOING FULL UP WHEN DISARMED. AIRCRAFT WAS FLOWN VIA MAINTENANCE FERRY TO PIT WHERE MAINTENANCE FOUND ARM/DISARM VIEWING WINDOW CONE DISPLACED. MAINTENANCE REATTACHED CONE PER EMB AMM AND OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,600 hrs · 19,581 cycles

CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT WAS UNABLE TO HOLD A CHARGE. MAINTENANCE R & R FORWARD F/A BATTERIES IAW AMM AND OPS CHECKED GOOD.

Part: ROLLER — DIRTY (L1 DOOR) · airframe 31,260 hrs · 19,365 cycles

CREW REPORTED THAT THE L1 DOOR WAS HARD TO OPEN AND THE FORWARD UPPER CORNER WAS BINDING. MAINTENANCE CLEANED DOOR ROLLERS IAW AMM AND OPS CHECKED GOOD.

Part: STOP FITTING — OUT OF ADJUST (L1 DOOR) · airframe 31,261 hrs · 19,366 cycles

CREW REPORTED THAT THE L1 DOOR WAS HARD TO OPEN. MAINTENANCE ADJUSTED FORWARD UPPER DOOR FRAME STOP IAW AMM AND OPS CHECKED GOOD.

Part: INDICATOR — OUT OF ADJUST (R2 DOOR) · airframe 31,257 hrs · 19,362 cycles

CREW REPORTED THAT THE R2 DOOR LOCK INDICATORS WERE NOT SHOWING GREEN. MAINTENANCE ADJUSTED THE DOOR LOCK INDICATORS IAW AMM AND OPS CHECKED GOOD.

Part: DOOR — OUT OF ADJUST (MAIN CABIN) · airframe 31,182 hrs · 19,310 cycles

CREW REPORTED THAT THE MAIN CABIN DOOR WOULD NOT CLOSE. MAINTENANCE ADJUSTED MAIN CABIN DOOR IAW AMM AND OPS CHECKED GOOD.

Part: CONTROL PANEL — BROKEN (L1 DOOR) · airframe 29,962 hrs · 18,539 cycles

L1 DOOR ARM/DISARM PANEL BROKEN. R & R L1 DOOR LINING IAW AMM 25-23-04.

Part: HANDLE — LACK OF LUBE (R1 DOOR) · airframe 29,701 hrs · 18,368 cycles

R1 DOOR NOT SHOWING ARMED ON STATUS PAGE OR ON DOOR. CLEANED AND LUBED R1 DOOR HANDLE REF AMM 52-41-22.

Part: RIB — CORRODED (HORIZONTAL STAB) · airframe 29,687 hrs · 18,361 cycles

RIB 12 HAS UPPER CRACK AND 1 LOWER CRACK ON RT HORIZONTAL STABILIZER. REPAIRED RT HORIZONTAL RIB 12 FCBS 55-10-00-005 IAW ETD2015-170-117101.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 29,687 hrs · 18,361 cycles

HORIZONTAL STABILIZER UPPER SKIN DENT BETWEEN RIBS 9 AND 10 AND STR 5. REPAIRED DAMAGE TO RT HORIZONTAL STABILIZER UPPER SKIN IAW SRM 55-10-01.

Part: SUPPORT BEAM — DAMAGED (ZONE 100) · airframe 29,687 hrs · 18,361 cycles

FOUND HOLE IN AFT CARGO DOOR CUTOUT LOWER SUPPORT BEAM AT AFT BOTTOM CORNER. REPAIRED AFT CARGO DOOR CUTOUT LOWER SUPPORT BEAM, FCBS 53-23-00-008 IAW ETD2015-170-117475.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,687 hrs · 18,361 cycles

RIGHT HORIZONTAL STABILIZER L/E RIB 4 IS CRACKED. CUT OUT DAMAGE ON RT HORIZONTAL STABILIZER L/E RIB 4 AND FABRICATED DOUBLER AND FILLER. INSTALLED IAW ETD 2015-170-117099.

Part: SEAL REST — CORRODED (AFT CARGO) · corrosion level 2 · airframe 29,687 hrs · 18,361 cycles

FWD SEAL REST CORNER FOR AFT CARGO DOOR HAS CORROSION AROUND SCREW HOLES AND ON THE TOP LEDGE. R & R CORRODED PART IAW SRM 51-40-02.

Part: RIB — CORRODED (HORIZONAL STAB) · airframe 29,687 hrs · 18,361 cycles

RIB 10 CRACKED ON UPPER MIDDLE AND LOWER FRONT OF RT HORIZONTAL STABILIZER. REPAIRED RT HORIZONTAL RIB 10 FCBS 55-10-00-005 IAW ETD2015-170-117101.

Part: RIB — CORRODED (HORIZONTAL STAB) · airframe 29,687 hrs · 18,361 cycles

RIB 11 CRACKED UPPER ON RT HORIZONTAL STABILIZER. REPAIRED RT HORIZONTAL RIB 11 FCBS 55-10-00-005 IAW ETD2015-170-117101.

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,687 hrs · 18,361 cycles

CORROSION ON AFT WET AREA SHEAR PLATE RT AT RIVETS. REMOVED DAMAGED SHEAR PLATE AND DRILLED NEW SHEAR PLATE IAW SRM 51-40-02. INSTALLED NEW SHEAR PLATE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 87-88) · airframe 29,687 hrs · 18,361 cycles

GALLEY FLOOR SUPPORT RT IB INTERCOSTAL AT FRAMES 87-88 HAS CORROSION AROUND INBD GALLEY MOUNT HOLE. R & R CORRODED GALLEY FLOOR SUPPORT RHIB FR87-88 AS REQUIRED IAW SRM 51-43-01.

Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 29,687 hrs · 18,361 cycles

CORROSION ON FRAME 87 SHEAR PLATE AT LAV MOUNTING. R & R SHEAR PLATE IAW SRM 51-42-01.

Part: SUPPORT — CORRODED (FRAME 89) · corrosion level 2 · airframe 29,687 hrs · 18,361 cycles

CORROSION ON RT SIDE PLATE AFT WET AREA AT FRAME 89. R & R SUPPORT IAW SRM 51-42-01 AND SRM 51-43-01.

Part: SEAL REST — CORRODED (FWD CARGO) · corrosion level 2 · airframe 29,687 hrs · 18,361 cycles

LOWER FWD AND AFT SEAL REST SHOW SIGNS OF CORROSION ON FWD CARGO DOOR CUT OUT. R & R FWD CARGO SEAL REST IAW 53-21-29.

Part: SEAL REST — CORRODED (FWD CARGO BAY) · corrosion level 2 · airframe 29,687 hrs · 18,361 cycles

FWD CARGO DOOR CUTOUT LOWER CENTER SEAL REST SHOWS SIGNS OF CORROSION. R & R FWD CARGO DOOR CENTER DOOR SEAL REST IAW SRM 51-40-02 AND 51-41-02.

Part: SEAL REST — CORRODED (AFT CARGO) · corrosion level 2 · airframe 29,687 hrs · 18,361 cycles

EVIDENCE OF CORROSION BENEATH NUT PLATES ON AFT CARGO DOOR CUTOUT LOWER CENTER SEAL REST. R & R AFT CARGO DOOR CENTER SEAL REST IAW SRM 51-40-02 AND 51-41-02.

Part: ATTACH FITTING — MISSING (EMERGENCY LIGHT) · airframe 28,829 hrs · 17,767 cycles

AFT GALLEY CEILING EXIT SIGN NOT SECURE, MISSING THREE TABS THAT HOLD IT IN PLACE. R & R AFT GALLEY CEILING EXIT SIGN COVER IAW AMM 33-50-19. OPS CHECK GOOD.

Part: LIGHT — UNSECURE (SEAT 7 CD) · airframe 28,354 hrs · 17,437 cycles

EMERGENCY LIGHT STRIP, SEAT 7CD, IS UNSECURE. SECURED THE STRIP IAW AMM 33-50-21.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 27,766 hrs · 17,035 cycles

R1 DOOR HANDLES DON'T MOVE SIMULTANEOUSLY. REMOVED DEBRIS FROM THE R1 DOOR GIRT BAR FLOOR ENGAGEMENT POINT AS REQUIRED. OPS CHECK NORMAL OF THE R1 DOOR IAW CMM 52-41-22.

Part: GUST LOCK — INOPERATIVE (PAX DOOR) · airframe 27,451 hrs · 16,837 cycles

MAIN CABIN DOOR GUST LOCK WILL NOT ENGAGE. RESECURED L1 DOOR HANDLE BUSSEL AS REQUIRED. L1 DOOR GUST LOCK OPERATES NORMALLY.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 27,117 hrs · 16,628 cycles

EMERGENCY EXIT OVERHEAD SIGN COVER FELL OFF ON TAKEOFF. ATTACHED EMERGENCY SIGN AS REQUIRED IAW AMM 33-50-019.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 26,791 hrs · 16,445 cycles

EXIT MARKER LENS CRACKED ABOVE R2 DOOR. R & R THE LENS IAW AMM 33-50-17.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 26,043 hrs · 15,983 cycles

FWD GALLEY AREA EMERGENCY EXIT SIGN COVER IS LOOSE. R & R FWD GALLEY EXIT COVER, LENS, REF AMM 33-50-19. OPS CHECK NORMAL.

Part: LOCK — DIRTY (PAX DOOR) · airframe 25,733 hrs · 15,804 cycles

MAIN CABIN DOOR DOES NOT LOCK. CLEANED LOCKING DEVICE IAW AMM 12-22-01. OPS CHECKED GOOD IAW AMM 52-11-00.

Part: GIRT BAR — CONTAMINATED (SERVICE DOOR) · airframe 25,304 hrs · 15,549 cycles

FWD SERVICE DOOR HARD TO ARM AND DISARM. FOUND STICKY STUFF IN GIRT BAR LOCK AND CLEANED OUT STICKY STUFF, OPS CHECK GOOD IAW AMM 52-11-22.

Part: GUST LOCK — LACK OF LUBE (PAX DOOR) · airframe 25,216 hrs · 15,495 cycles

MAIN CABIN DOOR GUST LOCK NEEDS LUBE. CLEANED AND REMOVED DIRT AND DEBRIS FROM L1 DOOR LATCH ASSY, OPS CHECKED IAW CMM 52-11-22.

Part: HANDLE — LACK OF LUBE (R2 DOOR) · airframe 24,211 hrs · 14,918 cycles

R2 AFT SERVICE DOOR, ARMING HANDLE IS HARD, IMPOSSIBLE, TO MOVE. CLEANED AND LUBED R2 ARMING HANDLE, OPS CHECKED GOOD IAW AMM 52-42-00. OK FOR SERVICE.

Part: INDICATOR — OUT OF POSITION (GIRT BAR) · airframe 24,100 hrs · 14,850 cycles

R1 GIRT BAR INDICATOR MISSING. REPOSITIONED R1 GIRT BAR INDICATOR IAW AMM 52-11-41, INDICATOR NOT MISSING.

Part: STRUCTURE — DAMAGED (ZONE 100) · airframe 23,813 hrs · 14,674 cycles

AFT SEAT REST HAS TWO ELONGATED HOLES AT LOWER CORNER. REAMED HOLES UP TO .191 FOR .3125 RIVETS IAW SRM 51-41-01. MAJOR REPAIR

Part: THRESHOLD — CORRODED (L1 DOORWAY) · airframe 23,813 hrs · 14,674 cycles

L1 DOOR THRESHOLD HAS CORROSION AT FASTENERS INSIDE POCKETS FOR THE EVAC SLIDE FITTINGS. R & R L1 DOOR THRESHOLD IAW SRM 591-40-02. MAJOR REPAIR

Part: SEAL DEPRESSOR — GOUGED (L1 DOOR FRAME) · airframe 23,813 hrs · 14,674 cycles

L1 DOOR CUTOUT STRUCTURE GOUGED ON LOWER AFT SIDE UNDER LOWER AFT OF COMMAND RAMP. R & R AFT SEAL REST IAW SRM 51-41-01 AND 51-43-01. EDGE SEALED AND PAINTED AFT L1 DOOR CUTOUT STRUCTURE IAW SRM 51-21-00, 51-23-06. INSTALLED LOWER AFT DOOR STOP IAW AMM 52-11-23. MAJOR REPAIR.

Part: CROSSBEAM — CORRODED (ZONE 100) · airframe 23,813 hrs · 14,674 cycles

CORROSION FOUND ON CROSSBEAM FRAME 84. REMOVED CORROSION . FABRICATED AND REPAIRED REPAIRED ANGLE, FILLER AND SHIM IAW 2013-170-055123.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 23,813 hrs · 14,674 cycles

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

Part: STRUCTURE — GOUGED (PAX DOOR) · airframe 23,813 hrs · 14,674 cycles

FWD PASSENGER DOOR FWD EDGE METAL SEAL PROFILE GOUGED. REMOVED FWD PAX DOOR FWD EDGE METAL SEAL PROFILE, MATCH DRILLED NEW ONE AND INSTALLED IAW SRM 51-40-02, 51-43-03, 51-41-01.

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 22,596 hrs · 13,909 cycles

HEAVY ODOR OF WET SOCKS IN COCKPIT DURING FLIGHT. ODOR ESPECIALLY INTENSE AT LOWER ALTITUDES. RAN NR 1 AND 2 PACKS AT POWER WITH CREW, COULD NOT DUPLICATE. OPS CHECKED GOOD AT THIS TIME IAW AMM 21-00-00. MX LATER REPLACED NR 1 ENGINE DUE TO OIL LEAK.

Part: POWER UNIT — INOPERATIVE (CABIN) · airframe 21,045 hrs · 12,980 cycles

COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE TURNED ON. REMOVED AND REPLACED EMERGENCY POWER UNIT IAW AMM 33-50-01, OPS CHECK GOOD.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 19,398 hrs · 12,005 cycles

COCKPIT OVERHEAD EMERGENCY FLOOR LIGHT DOES NOT COME ON DURING ORIGINATING LIGHT TEST. RESEATED ELEC CONNECTOR ON B-LIGHT BATTERY PACK, LIGHT IN COCKPIT OVERHEAD OPS CHECK GOOD IAW EMB 170 MM 33-50-01.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 18,682 hrs · 11,559 cycles

EMERGENCY LIGHT IN COCKPIT INOP. REMOVED AND REPLACED LIGHT ASSY IAW EMB 170 MM 33-50-03. OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (COCKPIT) · airframe 18,581 hrs · 11,497 cycles

COCKPIT EMERGENCY LIGHT INOP. CLEANED ELECTRIC CONNECTION AND RE-SECURED COCKPIT EMERGENCY LIGHT. OPS CHECK GOOD.

Part: FLAP — OUT OF ADJUST (R1 DOOR) · airframe 18,473 hrs · 11,420 cycles

R1 DOOR DIFFICULT TO DISARM AFTER LANDING. ADJUSTED VENT FLAP PER AMM 52-41-25. OPS CHECK GOOD.

Part: FLAP — MALFUNCTIONED (R1 DOOR) · airframe 18,468 hrs · 11,416 cycles

R1 DOOR VENT FLAP AND SLIDE HANDLE WON'T DISARM. PERFORMED OPS CHECK OF R1 DOOR IAW EMB 170 MM 52-41-00. NO DEFECTS NOTED.

Part: HANDLE — LACK OF LUBE (R1 DOOR) · airframe 18,468 hrs · 11,416 cycles

DOOR 1R VENT FLAP HANDLE DIFFICULT TO MOVE. LUBED R1 VENT HANDLE, PERFORMED OPS CHECK IAW EMB 170 MM 52-11-00. OPS CHECK GOOD.

Part: FLAP — DIRTY (SERVICE DOOR) · airframe 18,441 hrs · 11,396 cycles

FRONT SERVICE DOOR WILL NOT OPEN. CLEANED AND LUBED DOOR VENT FLAP, OPS CHECK GOOD IAW EMB 170 MM 52-41-25.

Part: FLAP — MALFUNCTIONED (SERVICE DOOR) · airframe 18,443 hrs · 11,397 cycles

FRONT SERVICE DOOR VENT FLAP WON'T OPEN USING HANDLE INSIDE CABIN. OPERATED FWD SERVICE DOOR, OPS CHECK GOOD IAW EMB 170 MM 52-41-00.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 18,424 hrs · 11,384 cycles

COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY IAW EMB 170 AMM 33-50-03. OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (COCKPIT) · airframe 18,412 hrs · 11,377 cycles

COCKPIT EMERGENCY LIGHT INOP. RECONNECTED ELECTRICAL CONNECTOR ON THE COCKPIT EMERGENCY LIGHT IAW EMB 170 AMM 33-50-03. OPS CHECK GOOD.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,848 hrs · 11,017 cycles

LEVEL 2 CORROSION ON SEAL REST. REMOVED AND REPLACED SEAL REST WITH NEW SEAL, NEW NUT PLATES INCLUDED, IAW EMB 170 SRM 51-41-01 AND 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,848 hrs · 11,017 cycles

MAJOR REPAIR - RIB 52 ANGLE AT WING STUB LT SIDE CRACKED. REMOVED RIB 52 ANDLE AT WING STUB IAW EMB SRM 51-40-02. MATCH DRILLED NEW ANGLE IAW EMB 170 SRM 51-41-01, 51-42-01, AND 51-43-03. INSTALLED RIB 52 ANGLE IAW EMB SRM 51-41-01, 51-42-01, AND 51-43-03.

Part: RIB — CRACKED (FUSELAGE) · airframe 17,911 hrs · 11,087 cycles

MAJOR REPAIR - RIB 52 CENTER SPLICE CRACKED (CENTER BELLY). REMOVED RIB 52 IAW EMB SRM 51-41-01. STOP DRILLED CRACK IAW EMB SRM 51-10-04. PERFORMED HFEC ON STOP DRILL, NO FURTHER DEFECTS NOTED. MATCH DRILLED SERVICEABLE DOUBLER SPLICE IAW EMB 170 SRM 51-20-00. INSTALLED DOUBLER IAW EMB 170 SRM 51-41-01 AND ETD 2011-170-108328.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,848 hrs · 11,017 cycles

LEVEL 2 CORROSION FLOORBEAM FWD OF CFI AREA ON RT SIDE. REMOVED AND REPLACED RT LWR FWD CFI SEAT TRACK EXTENSION IAW EMB 170 SRM 51-40-02, 51-40-04, 51-41-01, 51-41-02, 51-43-01, AND 51-43-02.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,848 hrs · 11,017 cycles

LEVEL 2 CORROSION SHEAR PLATE IN FWD LAV AREA. REMOVED AND REPLACED CORRODED SHEAR PLATE IN FWD LAV AREA IAW EMB 170 SRM 51-40-02 AND 51-41-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,848 hrs · 11,017 cycles

LEVEL 2 CORROSION L FLOORBEAM IN FRONT OF CF I IN SEVERAL AREAS. REMOVED AND REPLACED CF I LT FLOORBEAM IAW EMB 170 SRM 51-41-02, 51-43-01, AND 51-43-02.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,848 hrs · 11,017 cycles

LEVEL 2 CORROSION ON U-SHAPED BRACKETS FOR WATER SERVICE BOX. REMOVED, MATCH DRILLED, AND INSTALLED NEW U-SHAPE RETAINERS ON WATER SERVICE BOX IAW EMB SRM 51-40-02 AND 51-43-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,848 hrs · 11,017 cycles

LEVEL 2 CORROSION FOUND ON SEAT TRACK EXTENSION ON LT SIDE AT FR87. REMOVED AND REPLACED CORRODED SEAT TRACK EXTENSION BEAM ON LT SIDE AT FR87 IAW EMB 170 SRM 51-40-01, 51-42-01, AND 51-43-01.

Part: RIB — CRACKED (RT WING) · airframe 17,848 hrs · 11,017 cycles

MAJOR REPAIR - RT WING RIB 10 CRACKED AT THIRD FROM AFT END UPPER FASTENER. REMOVED AND REPLACED RIB 10 IAW EMB 170 SRM 51-40-02, 51-43-01, AND 51-43-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,848 hrs · 11,017 cycles

LEVEL 2 CORROSION RT UPPER CFI SEAT TRACK AT FR26, AND HAS SCRATCHES AND PAINT DAMAGE. BLENDED OUT CORROSION AT FR26 IAW EMB 170 SRM 51-10-03 AND IS WITHIN ALLOWABLE DAMAGE LIMITS IAW ETD 2011-170/01766 REV C. PERFORMED HFEC TO EFFECTIVE AREAS IAW NDR MANUAL, NO FURTHER INDICATIONS OR CRACKS NOTED. RESTORED TOP COAT IAW EMB 170 SRM 51-23-06.

Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 17,848 hrs · 11,017 cycles

LEVEL 2 CORROSION RT LOWER CFI SEAT TRACK 5 INCHES FWD FRAME 23, 9" AFT FRAME 23, 2" AFT FRAME 26, 1" AFT FRAME 29, 4" AFT FRAME 31, 2" AFT FRAME 32, 8" AFT FRAME 33, SCRATCHES AND PAINT DAMAGE. REMOVED AND REPLACED CFI SEAT TRACK IAW EMB 170 SRM 51-43-01 AND 51-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,848 hrs · 11,017 cycles

LEVEL 2 CORROSION LT LOWER CFI SEAT TRACK, 4 INCHES AFT FRAME 26, 3 INNCHES AFT FRAME 24, SCRATCHES AND PAINT DAMAGE. BLENDED OUT AREAS OF CORROSION IAW EMB 170 SRM 51-10-03 AND IS WITHIN ALLOWABLE DAMAGE LIMITS IAW ETD 2011-170/01766 REV C. PERFORMED HFEC TO EFFECTIVE AREA IAW NDT MANUAL, NO FURTHER CRACK LIKE INDICATIONS NOTED. RESTORED TOP COAT IAW EMB 170 SRM 51-23-06.

Part: SEAL DEPRESSOR — GOUGED (L1 DOOR) · airframe 17,848 hrs · 11,017 cycles

MAJOR REPAIR - L1 DOOR SEAL GOUGED IN SEVERAL PACES. DAMAGE IS WITHIN LIMITS IAW IC 2008-170-04854J. PERFORMED HFEC TO FWD PROFILE IAW NDTM, NO CRACK LIKE INDICATIONS NOTED. CUT OUT DAMAGED SECTION, MATCH DRILLED NEW L1 DOOR SEAL DEPRESSOR SPLICE, AND INSTALLED L1 DOOR SEAL DEPRESSOR IAW IC 2008-170/04854J AND EMB SRM 51-43-01 AND 51-41-01.

Part: STRUCTURE — MISREPAIRED (FUSELAGE) · airframe 17,848 hrs · 11,017 cycles

MAJOR REPAIR - PERFORMED INSPECTION OF LT CG III REPAIR BETWEEN FR82 AND FR83, STR 23L AND 22L, AND FOUND REPAIR TO NOT CONFORM TO THE CRITERIA IN EMB 170 SRM 53-23-01. STRIPPED PAINT, REMOVED DOUBLER AND FILLER, STRIPPED PAINT BENEATH DOUBLER, FABRICATED REPAIR DOUBLER, ALODINE AND PRIMED SKIN AND DOUBLER, AND INSTALLED FILLER AND DOUBLER IAW EMB 170 SRM 51-41-01 AND 51-41-02.

Part: GUST LOCK — MALFUNCTIONED (L1 DOOR) · airframe 17,367 hrs · 10,706 cycles

GUST LOCK ON L1 DOOR (MAIN CABIN ENTRANCE DOOR) DOES NOT SPRING TO LOCKED POSITION WHEN DOOR IS OPENED. GUST LOCK ON L1 DOOR PERFORMED ADJUSTMENT TEST IAW EMB 170 MM 52-11-00. OPS CHECK GOOD.

Part: RETAINER — LOOSE (GIRT BAR) · airframe 16,415 hrs · 10,134 cycles

L1 DOOR WON'T CLOSE ALL THE WAY AND A PART OF THE SLIDE (STRING) IS LOOSE. INSPECTED AND RE-SECURED L1 DOOR GIRT BAR RETAINER, OPS CHECK GOOD IAW EMB MM 52-11-41.

Part: GIRT BAR — OBSTRUCTED (R2 DOOR) · airframe 15,714 hrs · 9,701 cycles

R2 DOOR WILL NOT ARM/DISARM. MAINTENANCE REMOVED FOD FROM GIRT BAR ATTACHMENT TO AIRFRAME. OPS CHECK GOOD IAW EMB 170 MM 52-50-01.

Part: UNKNOWN — DETECTED (BLEED AIR SYS) · airframe 14,840 hrs · 9,166 cycles

CREW REPORTED BLEED 1 PRODUCING 'DIRTY SOCK' SMELL WHEN SELECTED. ACCOMPLISHED FIM TASK, REPRODUCED SMELL AND FOUND IT COMING FROM BLEED 1. DEFERRED BLEED 1 SYSTEM.

Part: PROCESSOR — UNSERVICEABLE (COCKPIT) · airframe 13,817 hrs · 8,536 cycles

DURING DESCENT, AVNX MAU 3A FAIL MESSAGE APPEARED. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. MAINTENANCE RESET PER FIM 45-45-00. ON 8/4/10 MAINTENANCE REMOVED AND REPLACED NIC PROC 5 IAW MM 31-41-04 AND POWER SUPPLY 1 IN MAU 3 IAW MM 31-41-02.

Part: SENSOR — INOPERATIVE (TE FLAP) · airframe 9,741 hrs · 6,068 cycles

FLAP FAIL EICAS MESSAGE SHORTLY AFTER REACHING CRUISE ALTITUDE. DECLARED AN EMERGENCY, LANDED ZERO FLAPS OR SLATS WITHOUT INCIDENT. MAINTENANCE REPLACED THE SF-ACE NR 1 AND T3 AND T4 LT O/B SKEW SENSORS. THERE HAVE BEEN NO WRITE UPS SINCE.

Part: CONTROL LEVER — INOPERATIVE · airframe 9,706 hrs · 6,046 cycles

AFTER MOVING FLAP LEVER TO FLAPS 3, RECEIVED A MASTER CAUTION AND AN EICAS ANNUNCIATION OF SLAT-FLAP LVR DISAG. CONTINUED APPROACH AND RAN QRH PROCEDURE. DECLARED AN EMERGENCY. LANDING UNEVENTFUL. MAINTENANCE CLEARED INHIBITS AND CHANGED NIC PROC 5 AS A PRECAUTION. THE SLAT FLAP CONTROL LEVER WAS LATER REPLACED.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 2,352 hrs · 1,528 cycles

FLIGHT 7519 DFW TO IAD. CREW REPORTED LOSS OF HYD IN FLIGHT REACHED 0 PERCENT, DIVERTED TO MEM. ON WALKAROUND FOUND LEAK AT NR 1 ENG. ON CALL MTX REPORTS THAT THE ENGINE DRIVEN PUMP IS LEAKING AT THE CASING HALF. REMOVED AND REPLACED NR 1 ENG HYP PUMP.