N865RW

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 49,541 hrs · 31,479 cycles

AFT RH EMERGENCY LIGHT BATTERY FAILED FUNCTIONAL CHECK. REPLACED AFT RH EMERGENCY LIGHT BATTERY.

Part: STRINGER — MECHANIC ERROR (ZONE 100) · airframe 49,541 hrs · 31,479 cycles

MISDRILLED HOLES AND DAMAGED DRAIN HOLE ON STG 21L BETWEEN FR30 AND FR31. REPAIRED DAMAGED STG 21L BY INSTALLING SPLICE BUILD-UP AS PER ETD2025-170-929580. REPAIR IS PERMANENT AND NO FURTHER ACTION REQUIRED.

Part: STRINGER — MECHANIC ERROR (ZONE 100) · airframe 49,541 hrs · 31,479 cycles

MISDRILLED HOLES AND DAMAGED DRAIN HOLE ON STG21L BETWEEN FR30 AND FR31. REPAIRED DAMAGED STG 21L BY INSTALLING SPLICE BUILD-UP AS PER ETD2025-170-929580. REPAIR IS PERMANENT AND NO FURTHER ACTION REQUIRED.

Part: CONNECTOR — DAMAGED (WORK LIGHT) · airframe 47,431 hrs · 29,140 cycles

DURING AGEING AIRCRAFT INSPECTION. DAR FINDING #15 AFT AVIONICS WORK LIGHT CONNECTORS DAMAGED/BURNT, EWIS. AFT AVIONICS WORK LIGHT CONNECTORS HOUSING R&R IAW IPC 33-32-01-05.

Part: SEAL — DAMAGED (E/E BAY) · airframe 47,431 hrs · 29,140 cycles

DURING AGEING AIRCRAFT INSPECTION. DAR FINDING#19 A SPOT CHECK OF THE AFT AVIONICS SMOKE SEAL DISCOVERED TE L/H SMOKE SEAL IS DAMAGED.SEAL REPAIRED IAW AMM 25-84-01-801-A.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII FR89 STR27-28 RH, FOUND CORRODED SHEAR TIE. CFIII FR89 STR27-28 RH, SHEAR-TIE HAS BEEN REPLACED IAW ERJ 170 SRM 51-41-02, SRM 51-43-03.

Part: ACCESS PANEL — CORRODED (ZONE 600) · airframe 46,337 hrs · 28,808 cycles

RH WING, INBD. MAIN FLAP, LOWER MID #2 ACCESS PANEL HAS CORROSION IN ONE CORNER, REPLACEMENT IS REQUIRED. RH WING, INBD. MAIN FLAP, LOWER MID #2 ACCESS PANEL HAS BEEN REPLACED WITH 'MADE' REPAIR PART IN REFERENCE WITH DRAWING 170-39117-001 AND CARS 571. PANEL INSTALLED IAW AMM 20-10-01-910-801-A.

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

FWD CARGO DOO CUT-OUT FOUND CORROSION ON TRIM BRACKETS (QTY 3) AT LOWER BEAM BETWEEN FR25-27. REMOVED AND REPLACED TRIM BRACKETS (3X) ON FWD CARGO DOOR CUT-OUT AT LOWER BEAM BETWEEN FR25-27 IAW EMBRAER 170 SRM 51-41-01.

Part: SUPPORT — CRACKED (ZONE 500) · airframe 46,337 hrs · 28,808 cycles

DURING HEAVY CHECK, LOWER AILERON CABLE FAIRLEAD SUPPORT AT FRAME 31 IN FWD CARGO CRACKED. CRACKED LOWER AILERON CABLE FAIRLEAD SUPPORT AT FRAME 31 IN FORWARD CARGO REMOVED & REPLACED WITH NEW PART IAW ERJ 170/175 SRM 51-41-01.

Part: BEAM — CORRODED (ZONE 200) · airframe 46,337 hrs · 28,808 cycles

CFIII FR85-87, STR.17L, FOUND TO HAVE CORROSION ON L2 DOOR CUT-OUT LWR. MID BEAM. CFIII, FR 85-87, STR.L7L, L2 DOOR CUT-OUT, CORRODED. LWR. MID BEAM, REMOVED AND REPLACED IAW EMB. 170/175 SRM 51-43-03 AND 51-43-04.

Part: RIB — CRACKED (ZONE 300) · airframe 46,337 hrs · 28,808 cycles

DURING HEAVY CHECK H-STAB LH TIP FAIRING RIB FOUND CRACKED. H-STAB LH TIP FAIRING RIB REPLACED IAW SRM 51-46-02

Part: RIB — CRACKED (ZONE 400) · airframe 46,337 hrs · 28,808 cycles

RH PYLON AFT FAIRING FOUND TO HAVE 3X CRACKED ANGLE RIB ON HEAT SHIELD. REMOVED & REPLACED 3X ANGLE RIBS ON HEAT SHIELD AT R/H PYLON AFT FAIRING IAW EMB 170/175 SRM 51-42-03.

Part: SEAL REST — CORRODED (UNKNOWN) · airframe 46,337 hrs · 28,808 cycles

DURING HEAVY CHECK, CFIII FR85-87, STR.17L FOUND TO HAVE CORRODED MID SUPPORT SEAL REST. CFIII FR85-87, STR. 17L, CORRODED MID SUPPORT SEAL REST, REMOVAL AND REPLACED IAW EMB 170/175 SRM 51-41-01.

Part: STRINGER — CORRODED (ZONE 200) · airframe 46,337 hrs · 28,808 cycles

DURING HEAVY CHECK, CFIII FR 86-87, STR. 27R FOUND TO HAVE CORRODED STRINGER.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII FR90, STR27R-28R FOUND TO HAVE CORRODED SHEAR CLIP. CFIII FR90, STR27R-28R SHEAR CLIP HAS BEEN REPLACED IAW SRM 51-41-02 AND 51-43-03.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII FR90 STR28R-29R FOUND TO HAVE CORRODED SHEAR CLIP. CFIII FR90, STR28R-29R, CORRODED SHEAR CLIP REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-41-02 AND 51-43-03.

Part: SUPPORT FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

FWD FUSE FR16 LBL47 FOUND TO HAVE CORRODED FLOOR SUPPORT FITTING. REMOVED AND REPLACED FLOOR SUPPORT FITTING ON FWD FUSE AT FR16 LBL47 IAW EMBRAER 175 SRM 51-41-02 AND 51-43-01.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII FR88-90 STR25R-29R FOUND TO HAVE CORRODED WASTE INTERNAL DOUBLER. CFIII FR88-90, STR25R-29R INTERNAL DOUBLER HAS BEEN REPLACED IAW ERJ-170SRM 51-41-02 AND SRM 51-21-01.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII FR90 STR29R-29L FOUND TO HAVE CORRODED SHEAR CLIP. CFIII FR90 STR 29R-29L SHEAR CLIP HAS BEEN REPLACED IAW ERJ-170- SRM 51-41-02, SRM 51-41-01, SRM 51-21-01.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII FR89 STR28R-29R FOUND TO HAVE CORRODED SHEAR CLIP. CFIII FR89 STR28R-29R SHEAR CLIP HAS BEEN REPLACED IAW ERJ-170-SRM 51-41-01 AND 51-41-02.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII FR87 BETWEEN STR25L-26R FRAME FOUND TO BE CORRODED. CFIII FR87 BETWEEN STR 25L-26R, CORRODED FRAME REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-41-01.

Part: SKIN — CRACKED (ZONE 500) · airframe 46,337 hrs · 28,808 cycles

LH WING FLE BET RIB 19-20, L/E SLAT CUT OUT REPAIR C/OUT IAW EMB 170/175 SRM 57-49-01. L/H WING FLE BTW RIB 19 TO 20 L/E SLAT CUT OUT REPAIR C/O IAW 170/175 SRM 57-49-01. HFEC C/OUT, NO FAULTS FOUND, SEE REPORT TW040160.12 FOR DETAILS.

Part: RIB — CRACKED (ZONE 500) · airframe 46,337 hrs · 28,808 cycles

DURING HEAVY CHECK R/H WING FLE RH RIB 23 FOUND TO BE CRACKED. R/H WING F.L.E. RIB 23 REPLACED & INSTALLED IAW 170/175 SRM 51-41-02.

Part: RIB — CRACKED (ZONE 500) · airframe 46,337 hrs · 28,808 cycles

DURING HEAVY CHECK RH WING FLE RH RIB31 FOUND TO BE CRACKED. RH WING F.L.E. RH RIB 31 REPLACED & INSTALLED IAW 170/175 SRM 51-41-02.

Part: SKIN — CRACKED (ZONE 500) · airframe 46,337 hrs · 28,808 cycles

RH WING FLE BET RIB 19-20 FOUND TO HAVE CRACK ON L.E. ON SLAT CUR OUT. RH WING FLE BET RIB 19 TO 20 L.E. SLAT CUT OUT REPAIR C/O IAW 170/175 SRM 57-49-01. HFEC C/OUT, NO FAULTS FOUND. SEE NDT REPORT TW040160.11 FOR DETAILS.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII AFT CARGO FR76 STR28R-29R, FOUND TO HAVE CORRODED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIP ON CFIII AT FR76 BETWEEN STR28R-29R IAW EMBRAER 175 SRM 51-41-01, 51-41-02 AND 51-21-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII AFT CARGO FR88 STR27R-28R FOUND TO HAVE CORRODED SHEAR CLIP. CFIII AFT CARGO FR88 STR27R-28R, CORRODED SHEAR CLIP REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-41-01 AND 51-41-02.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII AFT CARGO FR87, STR27R-28R CORRODED INTERCOSTAL. CFIII AFT CARGO FR87, STR27R-28R CORRODED INTERCOSTAL REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-41-01 AND 51-41-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII AFT CARGO FR83 STR28R-29R FOUND CORRODED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIP ON CFIII AT FR83 STR28R-29R IAW EMBRAER 175 SRM 51-41-01, 51-41-02 AND 51-21-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII AFT CARGO FR79 STR27L-28L FOUND TO HAVE CORRODED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIP ON CFIII AT FR79 STR27L-28L IAW EMBRAER 175 SRM 51-41-01, 51-41-02 AND 51-21-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII AFT CARGO FR87 STR27R-28R FOUND TO HAVE CORRODED SHEAR CLIP. CFIII AFT CARGO FR87 STR27R-28R , CORRODED SHEAR CLIP REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-41-01 AND 51-41-02.

Part: SEAL REST — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

AFT CARGO DOOR CUT-OUT, FOUND CORROSION ON LOWER FWD CORNER SEAL REST BETWEEN FR 77-78. AFT CARGO DOOR CUT-OUT LOWER FWD SEAL REST REPLACED IAW AMM 20-10-01.

Part: SHEAR TIE — CORRODED (UNKNOWN) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII AFT CARGO FR79 STR28L-29L FOUND TO HAVE CORRODED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIP ON CFIII AT FR79 BETWEEN STR28L-29L IAW EMBRAER 51-41-01, 51-41-02 AND 51-21-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII AFT CARGO FR76 STR28L-29L, FOUND CORRODED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIP ON CFIII AT FR76 BETWEEN STR28L-29L IAW EMBRAER 175 SRM 51-41-02 AND 51-21-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII AFT CARGO FR86 STR28R-29R FOUND TO HAVE CORRODED SHEAR CLIP. CFIII AFT CARGO FR86 STR28R-29R CORRODED SHEAR CLIP REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-41-01 AND 51-41-02.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII AFT CARGO FR86 STR27R-28R FOUND TO HAVE CORRODED INTERCOSTAL. CFIII AFT CARGO FR86 STR27R-28R CORRODED INTERCOSTAL REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-41-01 AND 51-41-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII AFT CARGO FR86 STR27R-28R FOUND TO HAVE CORRODED SHEAR CLIP. CFIII AFT CARGO FR86 STR27R-28R, CORRODED SHEAR CLIP REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-41-01 AND 51-41-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII AFT CARGO FR84 STR27R-28R FOUND TO HAVE CORRODED SHEAR CLIP. CFIII AFT CARGO FR84 STR27R-28R, CORRODED SHEAR CLIP REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-41-01 AND 51-41-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII AFT CARGO FR84 STR28R-29R FOUND TO HAVE CORRODED SHEAR CLIP. CFIII AFT CARGO FR84 STR28R-29R, CORRODED SHEAR CLIP REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-41-01 AND 51-41-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII AFT CARGO FR77 STR28L-29L FOUND TO HAVE CORRODED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIP ON CFIII AT FR77 BETWEEN STR28L-29L IAW EMBRAER 175 SRM 51-41-01, 51-41-02 AND 51-21-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII AFT CARGO FR78 STR27L-28L FOUND TO HAVE CORRODED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIP ON CFIII AT FR78 BETWEEN STR27L-28L IAW EMBRAER 175 SRM 51-41-01, 51-42-01 AND 51-21-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,337 hrs · 28,808 cycles

CFIII AFT CARGO FR80 STR28L-29L FOUND TO HAVE CORRODED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIP ON CFIII FR80 STR28L-29L IAW EMBRAER SRM 51-41-01, 51-41-02 AND 51-21-02.

Part: DUCT — INOPERATIVE (ZONE 100) · airframe 43,065 hrs · 26,263 cycles

BLEED 1 LEAK IN FLIGHT FOLLOWED BY CABIN ALTITUDE HIGH INDICATION. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R RH PACK OUTLET DUCT.

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 41,891 hrs · 25,457 cycles

WHEN DOOR CLOSED AT CUSTOMS, THEY KNOCKED AND I OPENED. THE SLIDE FELL OUT OF THE DOOR AND DID NOT DEPLOY. THEY KNOCKED TO TELL ME A PIN WAS HANGING OUTSIDE THE DOOR. R&R L1 FWD PAX DOOR EMERGENCY EVAC SLIDE ASSY.

Part: RIB — CRACKED (RT WING) · airframe 41,891 hrs · 25,456 cycles

WHILE AC WAS IN FOR HVY CK FOUND RH WING FIXED LEADING EDGE RIB 31 CRACKED AT UPPER FLANGE. REPAIRED RIB 31 PN 170-31281-001. IAW EMB ETD2021-170-019996. SEE AAR NRC# 4500917-6000-0046 FOR DETAILS OF WORK PERFORMED. AC RTS'ED.

Part: SHEAR ANGLE — CORRODED (FLOORBEAM) · corrosion level 2 · airframe 41,891 hrs · 25,456 cycles

WHILE AC WAS IN FOR HVY CKCORROSION FOUND ON CENTER FUSELAGE 3 AFT CARGO FLOOR SUPPORT SHEAR CLIP AT FR 81 AND STR 29R-29L. REPLACED SUPPORT PN 170-66354-002 IAW SRM 51-41-01. SEE AAR NRC# 4500917-1000-0102 FOR DETAILS OF WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.

Part: FLOORBEAM — CORRODED (FRM 80 S29R*L) · corrosion level 2 · airframe 41,891 hrs · 25,456 cycles

WHILE AC WAS IN FOR HVY CK FOUND CORROSION FOUND ON CENTER FUSELAGE 3 AFT CARGO FLOOR SUPPORT AT FR 80 AND STR 29R-29L. REPLACED SUPPORT PN 170-66353-001 IAW SRM 51-41-01 SEE AAR NRC# 4500917-1000-0103. FOR DETAILS OF WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.

Part: FLOORBEAM — CORRODED (FRM 79 S29L-R) · corrosion level 2 · airframe 41,891 hrs · 25,456 cycles

WHILE AC WAS IN FOR HVY CK CORROSION FOUND ON CENTER FUSELAGE 3 AFT CARGO FLOOR SUPPORT AT FR 79 AND STR 29L-29R. REPLACED SUPPORT PN 170-65912-001 IAW SRM 51-41-01, SEE AAR NRC# 4500917-1000-0104. AC REMAINS IN YQG FOR COMPLETION.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,891 hrs · 25,456 cycles

************THIS WAS A DUPLICATE SDR THAT WAS FILED TWICE BY MISTAKE #517 USED TWICE.**********WHILE AC WAS IN FOR HVY CK CORROSION FOUND ON CENTER FUSELAGE 3 AFT CARGO FLOOR SUPPORT SHEAR CLIP AT FR 81 AND STR 29R-29L. REPLACED SUPPORT PN 170-66354-002 IAW SRM 51-41-01. SEE AAR NRC# 4500917-1000-0102 FOR DETAILS OF WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.

Part: FLOORBEAM — CORRODED (FRM 77 29L-R) · corrosion level 2 · airframe 41,891 hrs · 25,456 cycles

WHILE AC WAS IN FOR HVY CK CORROSION FOUND ON CENTER FUSE 3 AFT CARGO FLOOR SUPPORT AT FR 77 AND STR 29L-29L. REPLACED FLOOR SUPPORT PN 170-66350-002 IAW SRM 51-41-01, 51-41-02. SEE AAR NRC# 4500917-1000-0105 FOR DETAILS OF WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 41,891 hrs · 25,456 cycles

WHILE AC WAS IN FOR HVY CK CRACK FOUND ON VERTICAL STABILIZER TRAILING EDGE RIB 9/10. REPLACED RIB 9/10 PN 170-63629-005 IAW SRM 51-41-01, 51-41-02. SEE AAR NRC# 4500917-3000-0037 FOR DETAILS OF WORK PERFORMED. AC RTS'ED.

Part: SHEAR TIE — CORRODED (LWR CNTR FUS) · corrosion level 2 · airframe 41,891 hrs · 25,456 cycles

WHILE AC WAS IN FOR HVY CK CORROSION FOUND ON CENTER FUSELAGE 3 LOWER FUSELAGE SHEAR CLIP AT FR83 BTWN STR 27-28R. REPLACED SHEAR CLIP PN 170-66868-001 IAW SRM 51-41-01, 51-41-02.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,891 hrs · 25,456 cycles

WHILE AC WAS IN FOR HVY CK CORROSION FOUND ON FWD FUSELAGE FLOOR STRUCTURE RH INBD SEAT TRACK. REPLACED SEAT TRACK PN 170-03263-001 IAW SRM 51-21-01, 51-41-01. SEE AAR NRC# 4500917-1000-0037 FOR DETAILS OF WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.

Part: PLATE — CORRODED (CABIN FLOOR) · corrosion level 2 · airframe 41,891 hrs · 25,456 cycles

WHILE AC WAS IN FOR HVY CK CORROSION FOUND ON FWD FUSELAGE FLOOR STRUCTURE DOUBLER PLATE AT FR13 RH SIDE. REPLACED DOUBLER PLATE PN 170-05663-003 IAW SRM 51-41-02, 51-43-04.

Part: SEAT TRACK — CORRODED (FRM 19) · corrosion level 2 · airframe 41,891 hrs · 25,456 cycles

WHILE AC WAS IN FOR HVY CK CORROSION FOUND ON FWD FUSELAGE FLOOR STRUCTURE LH INBD SEAT TRACK AT FR19. REPLACED SEAT TRACK PN 170-03264-001 IAW SRM 51-21-01, 51-41-01, 51-41-02, 51-43-03, 51-43-04. AC REMAINS IN YQG FOR COMPLETION.

Part: SEAT TRACK — CORRODED (FRAMES 43-59) · corrosion level 2 · airframe 41,891 hrs · 25,456 cycles

WHILE AC WAS IN FOR HVY CK CORROSION FOUND ON CENTER FUSELAGE 2 LH LATERAL SEAT TRACK BTWN FR43 AND 59 ON UPPER CROWN. REPLACED SEAT TRACK PN 170-02056-007 IAW SRM 51-21-01, 51-41-01, 51-43-03, 51-43-04. SEE AAR NRC# 4500917-1000-0040 FOR DETAILS OF WORK PERFORMED. AC RTS'ED.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 41,891 hrs · 24,556 cycles

LH H-STAB RIB 11A FOUND CRACKED. LH H-STAB 170EO-55-10-0004_1 ALL REPAIRS CARRYED OUT ON REPUBLIC 170EO-55-10-0004_1. CARRIED OUT ON AAR NRC# 4500916-3000-0065. THIS NRC WAS FOR TRACKING ONLY!! CRACK LENGTH 17.78MM OR 0.7" SEE AAR ROUTINE CARD # 4500916-3000-0065, AND 170EO-55-10-0004_1 FOR DETAILS OF WORK PERFORMED. MAJOR

Part: DOOR — BINDING (R2) · airframe 40,414 hrs · 24,502 cycles

R2 DOOR STICKING. CLEANED AND INSPECTED R2 DOOR, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,860 hrs · 22,896 cycles

**WHILE IN HEAVY CHECK** MAINTENANCE FOUND EMERGENCY EXIT SIGN ON FORWARD LAVATORY DOES NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED #2 EMERGENCY BATTERY REF AMM 33-50-01.

Part: POWER UNIT — INOPERATIVE (CABIN) · airframe 37,860 hrs · 22,896 cycles

**WHILE IN HEAVY CHECK** MAINTENANCE FOUND AFT SERVICE DOOR SURROUND EXIT LIGHT DOES NOT WORK. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER UNIT REF AMM 33-21-00, 33-50-01, AND 33-50-15.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 37,860 hrs · 22,896 cycles

MAINTENANCE FOUND RH HORIZONTAL RIB 10A CRACKED BETWEEN FRONT SPAR AND MID SPAR JUST AFT OF 6TH RIVET UPPER ROW FROM FRONT SPAR. MAINTENANCE REMOVED AND REPLACED RH HORIZONTAL RIB 10A, AND PREPPED, PRIMED, AND PAINTED RH HORIZONTAL REF EMB SRM 51-23-04, SRM 51-23-05, SRM 51-23-06.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 37,860 hrs · 22,896 cycles

MAINTENANCE FOUND RH HORIZONTAL RIB 12A CRACKED BETWEEN FRONT SPAR AND MID SPAR JUST AFT OF 4TH RIVET UPPER ROW FROM FRONT SPAR. MAINTENANCE REMOVED AND REPLACED RH HORIZONTAL RIB 12A BETWEEN FRONT SPAR AND MID SPAR REF: SRM 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FRAMES 89) · corrosion level 2 · airframe 37,860 hrs · 22,896 cycles

DURING HEAVY CHECK MAINTENANCE FOUND RH AFT WET AREA PANEL SUPPORT AT FR89 HAS CORROSION. FOUND OUT OF LIMITS AND REMOVED AND REPLACED PANEL SUPPORT AT FR89 R/H PER SRM51-40-08. A/C REMAINS IN CHECK.

Part: FLOOR SUPPORT — CORRODED (FRAME 89) · corrosion level 2 · airframe 37,860 hrs · 22,896 cycles

DURING HEAVY CHECK MAINTENANCE FOUND RH AFT WET AREA PANEL SUPPORT AT FR89 HAS CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED PANEL SUPPORT AT FR89 R/H PER SRM51-40-08. A/C REMAINS IN CHECK.

Part: SEAT TRACK — CORRODED (FRAME 48) · corrosion level 2 · airframe 37,860 hrs · 22,896 cycles

MAINTENANCE FOUND LEVEL 2 CORROSION AT RH IB SEAT TRACK FR 43-59 HAS CORROSION @ FR 48. MAINTENANCE REMOVED AND REPLACED RH INBD SEAT TRACK FR 43-59 REF EMB SRM 51-40-08. RESTORED SURFACE PROTECTION TO R/H INB SEAT TRACK REF: SRM 51-23-06 CPM 51-25-00.

Part: FLOOR SUPPORT — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 37,860 hrs · 22,896 cycles

DURING HEAVY CHECK MAINTENANCE, FOUND AFT WET AREA FLOOR SUPPORT HAS CORROSION BETWEEN CENTER AND RT SHEAR PANELS AT FRAMES 87 - 88. BLENDED AND FOUND OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-08.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 37,860 hrs · 22,896 cycles

DURING HEAVY CHECK MAINTENANCE FOUND AFT WET AREA CORROSION AT GUSSET PLATE AT FR90 RH SIDE. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED GUSSET PLATE AT FR90 RH PER SRM 51-40-08. A/C REMAINS IN CHECK.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,860 hrs · 22,896 cycles

MAINTENANCE FOUND LEVEL 2 CORROSION 3 EA LOWER ANGLE AND 1 CRACK RECEPTACLE ON PANEL 1441FR. MAINTENANCE REMOVED AND REPLACED 1EA LOWER ANGLE AND NUTPLATES FROM PANEL 1441FR. REF SRM 51-40-08. ALODINED, PRIMED AND TOPCOATED OTHER TWO LOWER ANGLES ON PANEL 1441FR. REF SRM 51-23-04,51-23-05, 51-23-06. AIRCRAFT REMAINS IN HEAVY CHECK FOR DURATION OF THE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 33-34) · corrosion level 2 · airframe 37,860 hrs · 22,896 cycles

MAINTENANCE FOUND LEVEL 2 CORROSION AT RH IB SEAT TRACK FR 21-34 HAS CORROSION BETWEEN FR 33-34. MAINTENANCE REMOVED AND REPLACED RH IB SEAT TRACK FR 21-34 REF EMB SRM 51-40-08. RESTORED SURFACE PROTECTION TO RH IB SEAT TRACK REF EMB SRM 51-23-06,CPM 51-25-00.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,860 hrs · 22,896 cycles

MAINTENANCE FOUND LEVEL 2 CORROSION AT 3 EA LOWER ANGLE AND 4 CRACK RECEPTACLE ON PANEL 1431DL. MAINTENANCE REMOVED AND REPLACED 1 EA LOWER ANGLE AND 4 CRACK RECEPTACLE ON PANEL 1431DL REF. EMB SRM 51-40-08, 51-40-02. RESTORED SURFACE PROTECTION TO 2 EA LOWER ANGLE ON PANEL 1431DL REF. EMB SRM 51-23-04, 51-23-05, 51-23-06. AIRCRAFT REMAINS IN HEAVY CHECK FOR DURATION OF THE CHECK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,992 hrs · 21,758 cycles

**DURING MAINTENANCE HEAVY CHECK** MAINTENANCE FOUND 2 OF 3 EMERGENCY LIGHTS NOT WORKING IN CEILING PANEL 227BLC AT L1 DOOR. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY IAW AMM 33-50-01-400-802A, OPS CHECK GOOD.

Part: TRACK — LACK OF LUBE (L1 DOOR) · airframe 35,989 hrs · 21,755 cycles

MAIN CABIN DOOR L1 IS DIFFICULT TO OPEN FROM THE OUTSIDE. DOOR FREQUENTLY GETS CAUGHT ON FRAME. LUBRICATED DOOR TRACKS, OPS CHECK OF L1 DOOR GOOD IAW AMM 52-11-00.

Part: POWER SUPPLY — BURNED (ZONE 100) · airframe 32,331 hrs · 19,508 cycles

SPDA FAIL MESSAGE, PACK 1 AND 2 MESSAGE, FLAP LOW RATE MESSAGE, BLEED 1 FAIL MESSAGE, RECEIVED AN ELECTRICAL SMOKE ODOR IN THE COCKPIT AND CABIN. DIVERTED. R & R SPDA NR 2 POWER SUPPLY MODULE IAW AMM 24-61-11.

Part: FASTENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,306 hrs · 19,488 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND CORROSION AFT CARGO PIT SHEAR CUP/BRACKET FR77 BL TO FUSELAGE SKIN. MX REMOVED AND REPLACED AFT CARGO PIT SHEAR CLIP RIVETS IAW SRM 51-10-03, 51-23-05. AC REMAINS IN RME FOR COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,306 hrs · 19,488 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND SHEAR CLIP AT STR 25L AND 26L FR17 HAS CORROSION. MX REMOVED AND REPLACED SHEAR CLIP AT STR 25L AND 26L FR17 PN 170-03868-001 IAW SRM 51-41-01, 51-41-02, 51-10-03, 51-75-16. AC REMAINS IN RME FOR COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,306 hrs · 19,488 cycles

WHILE AC IS IN FOR HEAVY CHECK FOUND STR 28R 27R FR 16 SHEAR CLIP CORROSION. MX REMOVED AND REPLACED SHEAR CLIP AT STR 28R 27R FR 16 IAW SRM 51-41-01, 51-41-02, 51-10-03. AC REMAINS IN RME FOR COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,306 hrs · 19,488 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND SHEAR CLIP BETWEEN STR 27R AND 26R AT FR17 HAS CORROSION. MX REMOVED AND REPLACED SHEAR CLIP BETWEEN STR 27R AND 26R AT FR17 PN 170-03869-002 IAW SRM 51-41-01, 51-41-02. AC REMAINS IN RME FOR COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,306 hrs · 19,488 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND SHEAR CLIP BETWEEN STR 28R AND 27R AT FR 17 HAS CORROSION. MX REMOVED AND REPLACED SHEAR CLIP BETWEEN STR 28R AND 27R AT FR 17 PN 170-03335-001 IAW SRM 51-10-02, 51-41-01, 51-41-02. AC REMAINS IN RME FOR COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2

WHILE A/C WAS IN FOR HEAVY CHECK FOUND SHEAR CUP BETWEEN STR 28L AND 27L HAS CORROSION. MX REMOVED AND REPLACED SHEAR CUP BETWEEN STR 28L AND 27L FR17, PN 170-03870-001 IAW SRM 51-41-02, 51-41-01, 51-40-02 AC REMAINS IN RME FOR COMPLETION.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,306 hrs · 19,488 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND AFT GALLEY MOUNT FR89 RT SIDE SHEAR PANEL SHOWING SIGNS OF CORROSION. MX REMOVED AND REPLACED SHEAR PANEL AT AFT GALLEY MOUNT FR89 RT SIDE IAW E170 SRM 51-43-01, SRM 51-40-02, 51-23-06. AC REMAINS IN RME FOR COMPLETION.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,306 hrs · 19,488 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND CENTER SHEAR PANEL AT FR 87 HAS CORROSION. MX REMOVED AND REPLACED CENTER SHEAR PANEL AT FR 87 PN 170-65928-001 IAW SRM 53-23-10, 51-42-01. AC REMAINS IN RME FOR COMPLETION.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,306 hrs · 19,488 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND FR87-FR88 SIDE SUPPORT PANEL SHOWING POSSIBLE CORROSION. MX REMOVED AND REPLACED SHEAR SUPPORT PANEL PN 170-91919-001 IAW SRM 51-75-16, 51-40-02, 51-40-03, 51-42-01, 51-42-02. AC REMAINS IN RME FOR COMPLETION.

Part: GAUGE — OUT OF POSITION (L2 DOOR SLIDE) · airframe 31,935 hrs · 19,257 cycles

L2 DOOR SLIDE GAUGE HARD TO SEE. REPOSITIONED L2 DOOR BUSTLE IAW AMM 25-23-05.

Part: UNKNOWN — ODOR (CABIN) · airframe 31,488 hrs · 18,961 cycles

CREW REPORTED A STRONG ODOR OF OIL COMING FROM THE VENTILATION SYSTEM. AN EMERGENCY WAS NOT DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED PACK AIR SYSTEM IAW AMM WITH NO OIL RESIDUES OR OIL ODORS FOUND. AIRCRAFT IS GOOD FOR SERVICE.

Part: CONNECTOR — DETACHED (EMERGENCY LIGHTS) · airframe 31,412 hrs · 18,908 cycles

MAINTENANCE REPORTED THAT THE AFT CABIN EMERGENCY LIGHTS FAILED TO ILLUMINATE. MAINTENANCE FOUND THE CONNECTOR PLUG DETACHED FROM AFT CABIN EMERGENCY LIGHT ASSEMBLY. MAINTENANCE REINSTALLED CANNON PLUG IAW AMM AND OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 30,296 hrs · 18,099 cycles

FOUND MAIN DOOR EXIT IDENTIFIED LIGHT NOT WORKING WHEN EMERGENCY PLACE ON. R & R SIGN, EXIT ID IAW MM 33-50-15.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 30,286 hrs · 18,093 cycles

EMERGENCY LIGHT BATTERY FAULT EICAS MESSAGE. R & R FWD LT EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01-000801A ADJUSTMENT TEST IAW AMM 33-50-01-710-801-A. OPS TEST, MESSAGE CLEARED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,286 hrs · 18,093 cycles

EMERGENCY LIGHT BATTERY FAULT EICAS MESSAGE APPEARED FOR 30 MINUTES, CLEARED, AND REAPPEARED AGAIN INTERMITTENTLY. THE MESSAGE APPEARS RANDOMLY WITH THE EMERGENCY LIGHT SWITCH IN THE ARMED POSITION. R & R EMERGENCY BATTERY NR 2 IAW AMM 33-50-01.

Part: CONTROL PANEL — MALFUNCTIONED (EMERENCY LIGHTS) · airframe 30,284 hrs · 18,092 cycles

EMERGENCY LIGHT BATTERY FAULT MESSAGE. R & R PASSENGER SIGN PANEL IAW AMM 33-23-07. RAN ACFT APU FOR 10 MINUTES, NO MESSAGE PRESENT.

Part: WARNING MESSAGE — FALSE INDICATION (COCKPIT) · airframe 30,283 hrs · 18,091 cycles

EMERGENCY LIGHT BATTERY FAULT MESSAGE. RESET ACFT POWER IAW FIM 33-50-00-810-802-A. FAULT CLEARED.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 30,117 hrs · 17,983 cycles

EMERGENCY LIGHT BATTERY FAULT ON AND OFF. R & R EMERGENCY LIGHT LT FWD BATTERY UNIT IAW AMM 33-50-01. OPS CHECKED GOOD.

Part: DETECTOR — DEFECTIVE (R2 DOOR) · airframe 29,959 hrs · 17,866 cycles

R2 LATCH INDICATOR NOT SHOWING OPEN. R & R ROLLER DETECTOR ON AFT SERVICE DOOR FWD GUIDE RAMP DUE TO SHEARED ROLL PIN. OPS CHECK GOOD REF AMM 53-23-25.

Part: SENSOR — MALFUNCTIONED (NLG STEERING) · airframe 29,935 hrs · 17,852 cycles

STEER FAIL MESSAGE IN FLIGHT WHEN GEAR WAS EXTENDED. DECLARED EMERGENCY, DIVERTED, AND LANDED WITHOUT INCIDENT. R & R NR 2 NLG STEER FEEDBACK SENSOR IAW AMM 32-53-09. OPS CHECKED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 29,254 hrs · 17,389 cycles

EMERGENCY LIGHT AT ROW 15 DOES NOT COME ON DURING TEST. MADE REPAIR TO WIRE W202-03212-2 IAW SWPM 20-41-20 AND ALSO R & R EMERGENCY BATTERY NR 4 IAW AMM 33-50-01. OPS CHECK GOOD.

Part: FITTING — CORRODED (LAVATORY MOUNT) · airframe 29,010 hrs · 17,227 cycles

FWD LAV AFT SECTION HAS 1 FLOOR FITTING CORRODED. REMOVED 1 FLOOR FITTING ON FWD LAV AFT SECTION. EVALUATED CORROSION AND REPLACED/INSTALLED NEW FLOOR FITTING REF CMM 25-42-03 AND SRM 51-40-00.

Part: FITTING — CORRODED (LAVATORY MOUNT) · airframe 29,010 hrs · 17,227 cycles

FWD LAV FWD SECTION HAS 1 FLOOR FITTING HAS SURFACE CORROSION. R & R FWD LAV FWD SECTION FLOOR FITTING REF SRM 51-40-00.

Part: FITTING — CORRODED (LAVATORY MOUNT) · corrosion level 2 · airframe 29,010 hrs · 17,227 cycles

AFT LAV OTBD HALF 3 FLOOR FITTINGS ARE CORRODED. REMOVED 3 FLOOR FITTINGS FWD, MID, AND AFT FROM AFT LAV OTBD HALF. EVALUATED CORROSION AND REPLACED/INSTALLED NEW FLOOR FITTINGS, 3 REF CMM 25-42-03 AND SRM 51-40-00.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 28,736 hrs · 17,045 cycles

EMERGENCY EXIT SIGN IN AFT GALLEY B DETACHED. SECURED AFT EMERGENCY EXIT SIGN COVER IAW AMM 33-50-00. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 27,756 hrs · 16,373 cycles

EMERGENCY LIGHT BATTERY FAULT. RESET ACFT POWER, OPS CHECKED GOOD.

Part: SENSOR — DAMAGED (L1 DOOR) · airframe 27,687 hrs · 16,324 cycles

L1 DOOR OPEN ON MFD. R & R L1 DOOR WARNING SENSOR LATCH ROLL PIN REF AMM 53-10-2. DOOR OPS CHECKS GOOD.

Part: WIRE HARNESS — DAMAGED (L1 DOOR) · airframe 27,661 hrs · 16,305 cycles

L1 DOOR INDICATION SHOWING OPEN IN FLIGHT. R & R L1 DOOR HARNESS.

Part: SENSOR — FAILED (SLAT SYSTEM) · airframe 26,894 hrs · 15,795 cycles

SLAT FAIL EICAS MESSAGE IN FLIGHT WHEN FLAPS 1 WAS SELECTED. FLAPS O/O INDICATION. COMPLIED WITH QRH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R 2/3 SLAT SKEW SENSOR ON RT WING IAW AMM 27-83-01. PERFORMED SLAT CONTROL SYSTEM RIGGING IAW AMM 27-80-00. PERFORMED OPS TEST IAW AMM 27-80-00. OPS CHECK GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 25,108 hrs · 14,715 cycles

CABIN HAS AN ODOR AFTER TAKEOFF, AND THROUGH OUT FLIGHT. FOLLOWED FIM TASK 21-20-00 FOR ABNORMAL ODOR IN COCKPIT, COULD NOT REPRODUCE.

Part: UNKNOWN — UNKNOWN (EMERGENCY LIGHTS) · airframe 24,853 hrs · 14,574 cycles

EMERGENCY LIGHTS CAME ON WHEN SHUTTING DOWN ENGINES AND WITH APU ON. COULD NOT GET THEM OFF. EMERGENCY LIGHT FAULT CAME ON, THEN OFF ON EICAS. EMERGENCY LIGHTS FINALLY SHUT OFF. IAW AMM, OPS CHECKED EMERGENCY LIGHT SYSTEM. EMERGENCY LIGHTS OPS CHECKED GOOD IAW AMM 33-50-00.

Part: COMPRESSOR — DAMAGED (NR 1 ENGINE) · airframe 21,099 hrs · 12,365 cycles

AT FL180 E1 SURGED REPEATEDLY. ENGINE 1 CONTROL FAULT CAME ON EICAS. FOLLOWED QRH AND THRUST WAS UNSTABLE. PERFORMED INFLIGHT SHUTDOWN OF ENGINE 1 AND RETURNED TO DTW. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. MTX PERFORMED BOROSCOPE OF ENG 1 IAW GE MM 72-00-00-220-802, FOUND EXTENSIVE DAMAGE TO COMPRESSOR SECTION. 865RW REMOVED AND REPLACED E1 ENGINE IAW JOB CARD.

Part: MECHANISM — OUT OF ADJUST (EVAC SLIDE) · airframe 19,293 hrs · 11,288 cycles

R2 SERVICE DOOR GIRT BAR INDICATOR SHOWING HALF RED WHEN ARMED. ADJUSTED EMERGENCY EVACUATION SLIDE MECHANISM WITHIN LIMITS IAW AMM 52-42-40. R2 ARM INDICATOR IN VIEW.

Part: MECHANISM — LACK OF LUBE (R2 DOOR) · airframe 18,428 hrs · 10,764 cycles

R2 DOOR DIFFICULT TO DISARM. LUBED ARM/DISARM VENT FLAP HANDLE MECHANISM IAW EMB 170 MM 52-70-00, OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (R2 DOOR) · airframe 18,293 hrs · 10,676 cycles

R2 DOOR VENT FLAP HANDLE STICKS. PERFORMED OPS CHECK OF R2 DOOR VENT FLAP, ALL OPS CHECK GOOD. COULD NOT DUPLICATE IAW CMM 52-42-2.

Part: FLAP — MALFUNCTIONED (R2 DOOR) · airframe 18,200 hrs · 10,619 cycles

R2 VENT FLAP HANDLE HANGING DURING DISARMING. TROUBLESHOT R2 VENT FLAP IAW EMB 170 MM 52-12-25. OPS CHECK GOOD.

Part: FLAP — LACK OF LUBE (R2 DOOR) · airframe 18,162 hrs · 10,592 cycles

R2 DOOR VENT FLAP IS DIFFICULT TO ARM AND DISARM. LUBED AND OPS CHECK R2 DOOR VENT FLAP IAW EMB 170 MM 52-12-22. OPS CHECK GOOD.

Part: HANDLE — LACK OF LUBE (R2 DOOR) · airframe 18,145 hrs · 10,580 cycles

R2 DISARM HANDLE GETS STUCK HALF WAY UP WHEN DISARMING AND NEEDS EXTRA PUSH TO GET IT DISARMED. LUBED AND PERFORMED OPS CHECK IAW EMB 170 MM 52-42-00. OPS CHECK GOOD.

Part: HANDLE — CONTAMINATED (R2 DOOR) · airframe 18,034 hrs · 10,514 cycles

R2 DOOR VENT FLAP HANDLE STICKING AND HARD TO MOVE. INSPECTED AND FOUND NO DEBRIS OR DAMAGE, VENT FLAP OPERATES NORMAL, NO DEFECTS NOTED.

Part: HANDLE — BINDING (R2 DOOR VENT) · airframe 17,994 hrs · 10,487 cycles

R2 SERVICE DOOR VENT FLAP HANDLE STICKING WHEN DISARMING. LUBRICATED R2 DOOR VENT FLAP HANDLE, OPS CHECKED GOOD.

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 17,658 hrs · 10,284 cycles

R2 SERVICE DOOR VENT FLAP HANDLE IS HARD TO OPEN/DISARM. LUBED AND ADJUSTED AFT SERVICE DOOR, FOUND TO BE WORKING PROPERLY IAW AMM 52-42-0.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,289 hrs · 10,051 cycles

LEVEL 2 CORROSION WATER SERVICE BOX AFT DOUBLER. REMOVED AND REPLACED WATER SERVICE BOX AFT INTERNAL DOUBLER IAW EMB 170 SRM 51-40-02 AND 51-43-02.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,289 hrs · 10,051 cycles

LEVEL 2 CORROSION WASTE BOX FWD DOUBLER. REMOVED AND REPLACED DOUBLER IAW EMB 170 SRM 51-43-02.

Part: CROSS TIE — BENT (FUSELAGE) · airframe 17,289 hrs · 10,051 cycles

MAJOR REPAIR - CROSS TIE ON RT SIDE OF FRAME 86 IS BENT. CUT OUT DAMAGED SECTION, PERFORMED HFEC INSPECTION ON AREA IAW EMB 170 NDT MANUAL, NO CRACK LIKE INDICATIONS FOUND, BENT REINFORCED ANGLE AND FABRICATED FILLER, PERFORMED HFEC INSPECTION AT BEND AT REINFORCEMENT ANGLE IAW EMB 170 NDT MANUAL, NO CRACK LIKE INDICATIONS FOUND, TRIMMED AND MATCH DRILLED ANGLE AND FILLER TO CROSS BEAM, AND INSTALLED IAW ETD 2012-170-000032 REV A.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,289 hrs · 10,051 cycles

LEVEL 2 CORROSION SHEAR WEB ON FWD POSITION OF R1 DOOR (FLOOR AREA). REMOVED AND REPLACED SHEAR WEB IAW EMB 170 SRM 51-41-02 AND 51-43-02.

Part: RIB — CRACKED (RT WING) · airframe 17,289 hrs · 10,051 cycles

RIGHT WING SPAR 2, RIB 10 EXTENSION CRACKED AT THIRD AFT MOST FASTENER. REMOVED AND REPLACED RIB IAW SRM 51-41-01 AND 51-43-03. MAJOR REPAIR

Part: INDICATION SYS — FAULTY (L2 DOOR) · airframe 16,782 hrs · 9,739 cycles

L2 DOOR INDICATION FAULT. VERIFIED DOOR POSITION, NO DEFECTS.

Part: WIRE HARNESS — DEFECTIVE (L2 DOOR) · airframe 16,709 hrs · 9,683 cycles

L2 DOOR MFD INDICATION FAULT. REMOVED AND REPLACED L2 DOOR POSITION AND WARNING HARNESS IAW AMM 52-72-21. OPS CHECK GOOD.

Part: DOOR — LACK OF LUBE (L1) · airframe 16,024 hrs · 9,272 cycles

L1 DOOR DIFFICULT TO OPEN. LUBRICATED L1 DOOR, OPS CHECK GOOD IAW EMB 170 MM 52-11-22.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 15,486 hrs · 8,953 cycles

ROW 15 HAS 12 INCH PIECE OF PHOTO ILLUMINESCENT STRIP ON FLOOR MISSING. REPLACED ROW 12 PHOTO ILLUMINESCENT STRIP IAW EMB 170 MM 33-50-21.

Part: PROCESSOR — INOPERATIVE (COCKPIT) · airframe 12,658 hrs · 7,259 cycles

RECEIVED AVNX MAU 2B FAIL MESSAGE IN CRUISE FLIGHT. FOLLOWED QRH. CREW DECLARED EMERGENCY, LANDING WAS UNEVENTFUL. MAINTENANCE ACCOMPLISHED FIM TASK 31-42-00-810-811 AND PERFORMED NIC 4 AND AIOP RESET. OPS CHECK GOOD. MAINTENANCE LATER REPLACED NIC 4 IN MAU 2 PER EMB 170 MM 31-41-04.

Part: RIVET — DAMAGED (FUSELAGE) · airframe 11,908 hrs · 6,802 cycles

MAJOR REPAIR - THREE PROTRUDING HEAD RIVETS FAILED RII INSPECTION ON FR 10 IN RAT COMPARTMENT. RIVETS WERE DAMAGED ON INSTALL AND STRUCTURE AROUND RIVET HEAD. REMOVED AND REPLACED RIVETS IAW EMB 170 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,908 hrs · 6,802 cycles

LEVEL 2 CORROSION RT SEAT TRACK BEAM BETWEEN FR 13 AND FR 14. REMOVED AND REPLACED RT SEAT TRACK BEAM IAW EMB 170 SRM 51-41-02 AND 51-43-02.

Part: BEAM — CRACKED (NLG) · airframe 11,908 hrs · 6,802 cycles

NLG I SHAPED BEAM HAS A CRACK LIKE INDICATION ON FWD FLANGE. REMOVED BEAM, DRILLED, AND INSTALLED IAW EMB 170 SRM 51-40-01, 51-43-01, 51-40-02, AND 51-43-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,908 hrs · 6,802 cycles

LEVEL 2 CORROSION ON RT SEAT TRACK BEAM BETWEEN FR 15 AND 16. REMOVED AND REPLACED RT SEAT TRACK BEAT AT FR 17.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,908 hrs · 6,802 cycles

LEVEL 2 CORROSION ON RT SEAT TRACK BEAM AT FR 17. REMOVED AND REPLACED RT SEAT TRACK BEAM AT FR 17.

Part: SILL — CORRODED (FUSELAGE) · airframe 11,908 hrs · 6,802 cycles

LEVEL 2 CORROSION ON ALL FOUR SILL PLATES ALONG FR90. REMOVED AND REPLACED RT AND TWO CENTER SILL GUSSET PLATES AND REMOVED LT SILL PLATE PAINT LAYER AND LIGHTLY BRUSHED DAMAGE PRIMER THEN RE-APPLIED PRIMER AND TOP COAT TO ALL FOUR SILL GUSSET PLATES IAW EMB 170 SRM 51-40-02, 5-41-02, AND 51-23-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,908 hrs · 6,802 cycles

MAJOR REPAIR - LT SEAT TRACK BEAM HAS LEVEL 2 CORROSION AT FR 19. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER IAW EMB ETD 2010-170/02635.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,908 hrs · 6,802 cycles

MAJOR REPAIR - LT SEAT TRACK BEAM HAS LEVEL 2 CORROSION AT FR 17. REMOVED CORROSION, INSTALLED DOUBLER OVER TOP IAW EMB ETD 2010-170/02635.

Part: RING — DAMAGED (APU EXHAUST) · airframe 11,908 hrs · 6,802 cycles

MAJOR REPAIR - APU EXHAUST END CAP RING HAS LIGHTNING STRIKE. REMOVED AND REPLACED APU EXHAUST END CAP RING IAW SRM 51-41-01 AND 51-40-02.

Part: ISOLATOR — DAMAGED (CARGO DOOR) · airframe 11,908 hrs · 6,802 cycles

AFT CARGO DOOR HAS FOUR DAMAGED ISOLATORS THAT NEED REPLACED. REMOVED AND REPLACED ISOLATORS IAW EMB 170 SRM 51-41-01.

Part: HINGE — CORRODED (LAV SERVICE) · corrosion level 2 · airframe 11,908 hrs · 6,802 cycles

LEVEL 2 CORROSION ON AFT LAV SERVICE PANEL HINGE. REMOVED AND REPLACED WASTE SERVICE DOOR, APPLIED PRIMER AND TOPCOAT PER SRM 51-23-05 AND 51-23-06, AMM 53-03-60.

Part: NUT PLATE — DAMAGED (FUSELAGE) · airframe 11,908 hrs · 6,802 cycles

NUT PLATE NEEDS REPLACED ON FUSELAGE PANEL 419DT ON LT ENG. REMOVED AND REPLACED NUT PLATE IAW EMB 170 SRM 51-42-02.

Part: CONTROL LEVER — INOPERATIVE (COCKPIT) · airframe 9,089 hrs · 5,160 cycles

GEAR DID NOT RETRACT UPON CALLING GEAR UP. CREW REPORTED, TRIED 3 TIMES AND RETURNED TO FIELD. GEAR WAS DOWN AND LOCKED WITH 3 GREEN. NO EMERGENCY DECLARED. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER AND BOTH WOW PROX SWITCHES. PERFORMED 5 GEAR SWINGS WITH NO DEFECTS NOTED. THERE HAVE BEEN NO WRITE UPS SINCE.

Part: SLAT — MALFUNCTIONED (WING) · airframe 8,526 hrs · 4,806 cycles

SLAT FAIL ON APPROACH. CREW CYCLED PER QRH. DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT. MAINTENANCE CLEARED INHIBITS. NO SLAT ACTUATORS WERE FOUND TRIPPED.

Part: SLAT — MALFUNCTIONED (WING) · airframe 8,040 hrs · 4,456 cycles

FLIGHT 5941 MTY TO ATL ON DESCENT THE CREW RECEIVED A SLAT FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED THE AIRCRAFT WITHOUT INCIDENT. MAINTENANCE TROUBLE SHOT PER FIM, CLEARED INHIBITS AND CYCLED THE SLATS SEVERAL TIMES; OPS CHECKED GOOD. THIS DISCREPANCY HAS NOT REPEATED THIS DATE 12/08/2008.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 7,795 hrs · 4,289 cycles

FLIGHT 5986 ATL TO DCA ON APPROACH FLAPS WERE SELECTED TO "1" AND CREW RECEIVED A "SLAT FAIL" AND "SHAKER ANTICIPATED" EICAS MESSAGES. CREW FOLLOWING THE QRH; SLATS REMAINED AT 0 BUT FLAPS COULD BE EXTENDED TO 2. EMERGENCY WAS DECLARED AND LANDING UNEVENTFUL. MAINTENANCE CLEARED INHIBITS AND RESET SYSTEM; OPS CHECK GOOD. THIS DISCREPANCY HAS NOT REPEATED.

Part: UNKNOWN — MALFUNCTIONED (WING) · airframe 2,823 hrs · 1,266 cycles

FLIGHT 6471 SLC TO IAH WING FAIL ON TAKEOFF ROLL, RAN QRH. CLEARED THEN CAME ON AGAIN ONTAXI/SPEED 90KTS. OCM DID FIM TASK AND FAULT CLEARED AND WAS OPS CK NORMAL.

Part: UNKNOWN — MULTIPLE FAIL · airframe 1,151 hrs · 467 cycles

FLIGHT 643, AT CRUISE CREW REPORTED RECEIVING 5 DIFFERENT EICAS MESSAGES; SLAT LOW RATE, SHAKER ANTICIPATED, AUTOPILOT FAIL, AOA LIMIT FAIL, AND SPOILER FAULT. AT LANDING THE CREW DECLARED EMERGENCY AND HAD MOD FASTER THAN NORMAL LANDING FLAPS 2 WITH NO SLATS ON LANDING. OCM CLEARED SF-ACE INHIBITS, OPS CHECKED SLAT FLAP SYS OK. NO PRIOR HISTORY.