N858RW

Part: UNKNOWN — CRACKED (ZONE 300) · airframe 46,285 hrs · 27,976 cycles

MAJOR****CRACK FOUND ON HSTAB RIB 10A REPAIRED IAW 170EO-55-10-0004_1***MAJOR

Part: BOLT — CRACKED (ZONE 500) · airframe 46,285 hrs · 27,976 cycles

CRACK FOUND ON LH WINGSTUB SPAR 1 BOLT. REPLACED UPSIZED BOLT IAW ETD2023-170-005530 REVA.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,285 hrs · 27,976 cycles

LEVEL 2 CORROSION WAS FOUND ON LH INBD CABIN SEAT TRACK BETWEEN FR 23 AND FR 34. TRACK WAS REPLACED IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,285 hrs · 27,976 cycles

CENTER FUSELAGE III, CORROSIONS FOUND ON R/H I/B SEAT TRACK BETWEEN FR 74 - 84. CENTER FUSELAGE III, R/H I/B SEAT TRACK BETWEEN FR 74 - FR 84 REPLACED WITH NEW AND INSTALLED IAW SRM 51-41-01, SRM 51-43-03, AND SRM 51-43-04.

Part: RIB — CRACKED (ZONE 300) · airframe 46,285 hrs · 27,976 cycles

L/H HORIZONTAL STABILIZER , SUSPECTED CRACK FOUND ON RIB 10 UPPER FLANGE. MAJOR. CRACK CONFIRMED ON LH H-STAB RIB 10 UPPER FLANGE. SEE AWS AND NDT REPORT TW038274-9 FOR DETAILS. REPLACED RIB 10 ON TASK CARD 170EO-55-10-0004_1. NO FURTHER ACTION REQUIRED

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,285 hrs · 27,976 cycles

CF3 CORROSION FOUND ON LH IB SEAT TRACK BTWN FR 74-84. RERPLACED SEAT TRACK IAW SRM 51-43-03, 51-43-04

Part: SKIN — DENTED (ZONE 100) · airframe 46,285 hrs · 27,976 cycles

FWD FUSE LOWER SKIN PNL DENT FOUND BTWN FR 16-17 STR 22L-23L. ALLOWED DAMAGE IAW ETD 2023-170-006285

Part: SKIN — DENTED (ZONE 100) · airframe 46,285 hrs · 27,976 cycles

FWD FUSE LOWER SKIN PNL DENT FOUND BTWN FR16-17, STR 23L-24L. ALLOWED DAMAGE IAW ETD2023-170-006285

Part: PANEL — CORRODED (ZONE 100) · airframe 46,285 hrs · 27,976 cycles

CORROSION FOUND ON CF3 WATER ACCESS DOOR. REPLACED IAW SRM 53-03-02/400

Part: SKIN — DENTED (ZONE 100) · corrosion level 2 · airframe 46,285 hrs · 27,976 cycles

FORWARD FUSE LOWER SKIN PNL 4 PROTRUDING DENTS BTWN FR-2-3 STR 28R-26R. ALLOWED DAMAGE IAW ETD 2023-170-006146.

Part: SKIN — DENTED (ZONE 100) · airframe 44,372 hrs · 26,553 cycles

DENT ON L/H FWD FUSE BETWEEN FR11 & FR12, STR 13L & 15L. REPAIRED IAW ETD2022-170-004230

Part: SHEAR TIE — CORRODED (FRM 16 S27-28L) · corrosion level 2 · airframe 42,956 hrs · 25,591 cycles

CORROSION FOUND ON FWD FUSELAGE SHEAR CLIP AT FR 16 AND BETWEEN STR 28-27L. ON FWD FUSELAGE CORRODED SHEAR CLIP AT FR 16 AND BETWEEN STR 28-27L REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-41-02, AND 51-43-01.

Part: DOUBLER — CRACKED (LT WING) · corrosion level 2 · airframe 42,956 hrs · 25,591 cycles

WHILE AC WAS IN FOR HVY CK FOUND LH WING FOUND 1 CRACK .710" LONG ON DOUBLER OF SKIN CUT OUT, SLAT TRACK 6. AAR REPLACED SKIN DOUBLER PN 170-31085-001 IAW SRM 51-41-02, 51-73-04. SEE AAR NRC#4500913-5000-0060 FOR WORK PERFORMED. AC RTS.

Part: SEAT TRACK — CORRODED (FRMS 19-20) · corrosion level 2 · airframe 42,956 hrs · 25,591 cycles

WHILE AC WAS IN FOR HVY CK FOUND CF1, FLOOR STRUCTURE, CORROSION FOUND ON INBD LH SEAT TRACK BTWN FR19-20. REPLACED SEAT TRACK PN 170-03264-001 IAW SRM 51-41-01, 51-41-02, 51-43-04, 51-43-03, 51-21-01. SEE AAR NRC# 4500913-2000-0207 FOR WORK PERFORMED. AC WAS RTS'ED.

Part: DOUBLER — CORRODED (FRMS 19-20) · corrosion level 2 · airframe 42,956 hrs · 25,591 cycles

CFI, FLOOR STRUCTURE, CORROSION FOUND ON DOUBLER LH SIDE BETWEEN FR 19-20. CFI, FLOOR STRUCTURE DOUBLER ON L/H SIDE BETWEEN FR 19-20 REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-41-02 AND 51-43-04.

Part: FLOOR SUPPORT — CORRODED (FRM 84) · corrosion level 2 · airframe 42,956 hrs · 25,591 cycles

CFIII, FLOOR STRUCTURE, FORROSION FOUND ON LH PANEL SUPPORT AT FR 84. REPLACED L/H O/B FLOOR PANEL SUPPORT AT FR 84 WITH NEW. P/N 170-92907-001 IAW SRM 51-41-01 AND SRM 51-41-02

Part: SEAT TRACK — CORRODED (FRM 84) · corrosion level 2 · airframe 42,956 hrs · 25,591 cycles

CFIII, FLOOR STRUCTURE, CORROSION FOUND ON RH INBD SEAT TRACK AT FR 84. FLOOR STRUCTURE R/H I/B SEAT TRACK @ FR 84 REPAIR CARRIED OUT IAW EMBRAER SRM 53-23-40 FIG 201

Part: SUPPORT — CORRODED (FRMS 88-90) · corrosion level 2 · airframe 42,956 hrs · 25,591 cycles

WHILE AC WAS IN FOR HVY CK FOUND CF3 FLOOR STRUCTURE CORROSION FOUND ON RH PANEL SUPPORT BTWN FR88-90. REPLACED RH PANEL SUPPORT PN 170-86181-005 IAW SRM 51-41-01, 51-43-03. SEE AAR NRC#4500913.2000-0125 FOR WORK PERFORMED. AC WAS RTS'ED.

Part: FLOORBEAM — CORRODED (FRM 84) · corrosion level 2 · airframe 42,956 hrs · 25,591 cycles

CFIII, FLOOR STRUCTURE, CORROSION FOUND ON RH PANEL SUPPORT AT FR 84. CFIII, FLOOR STRUCTURE, CORRODED RH PANEL AT FR 84, REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-41-02, 51-41-01, AND 51-43-02

Part: GUSSET — CORRODED (FRM 90) · corrosion level 2 · airframe 42,956 hrs · 25,591 cycles

WHILE AC WAS IN FOR HVY CK FOUND CF3 FLOOR STRUCTURE CORROSION FOUND ON RH GUSSET PLATE AT FR 90. REPLACED GUSSET PLATE PN 170-60259-001 IAW SRM 51-41-02. SEE AAR NRC# 4500913-2000-0124 FOR WORK PERFORMED. AC WAS RTS'ED.

Part: DOUBLER — CORRODED (FRMS 85-86) · corrosion level 2 · airframe 42,956 hrs · 25,591 cycles

WHILE AC WAS IN FOR HVY CK FOUND CF3 FLOOR STRUCTURE CORROSION FOUND ON UPPER SHEET DOUBLER LH AFT INBD SEAT TRACK BTWN FR 85-86. REPLACED DOUBLER PN 170-86101-001 IAW SRM 51-41-01, 51-43-03.

Part: FITTING — DAMAGED (HORIZONTAL STAB) · airframe 39,203 hrs · 23,178 cycles

DUE TO HORIZONTAL STABILIZER BACKLASH FAILURE, SCORING DAMAGE FOUND ON LH FITTING HINGE LINE (PIVOT) ASSY IB FACE LUG REAR SPAR AREA PN: 170-62480-403. MUST BE INSTRUCTIONS REPAIR REQUIRED. AT LH HINGE FITTING PIVOT ASSY, IB FACE OF LUG FITTING REWORKED AS A TEMPORARY REPAIR IAW ETD2019-170-071866. THIS REPAIR IS CONSIDERED TEMPORARY AS IT WILL REQUIRE A DETAIL STRUCTURE ANALYSIS. CONSIDERED A MAJOR REPAIR.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 39,203 hrs · 23,178 cycles

LH WING FIXED LE SLAT #2 OB TRACK CUT OUT CRACK TO BE INVESTIGATED. LH WING FIXED LE SLAT #2 OB CUT OUT REPAIRED IAW ETD2019-170-072282. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 39,203 hrs · 23,178 cycles

DURING HEAVY CHECK, LEFT HORIZ. STAB. RIB 12A FOUND CRACKED. REMOVED AND REPLACED RIB IAW SRM 51-41-01.

Part: FLOORBEAM — CRACKED (FRAME 12) · airframe 39,203 hrs · 23,178 cycles

COCKPIT FLOOR STRUCTURE AT FR 12 BL 0, ANGLE FOUND CRACKED. COCKPIT FLOOR STRUCTURE AT FR 12 BL 0 ANGLE REPLACED IAW SRM 51-41-01. A/C REMAINS OUT OF SERVICE.

Part: FLOORBEAM — CRACKED (FRAME 12) · airframe 39,203 hrs · 23,178 cycles

COCKPIT FLOOR STRUCTURE AT FR 12 LBL 36, ANGLE FOUND CRACKED. COCKPIT FLOOR STRUCTURE AT FR 12 LBL 36 ANGLE REPLACED IAW SRM 51-41-01. PSE 53-10-26. A/C REMAINS OUT OF SERVICE .

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 39,203 hrs · 23,178 cycles

RIGHT HORIZONTAL STABILIZER RIB 11A FOUND CRACKED. RIGHT HORIZONTAL STABILIZER RIB 11A REPLACED IAW SRM 51-41-01. A/C REMAINS OUT OF SERVICE.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 39,203 hrs · 23,178 cycles

MAINTENANCE REPORTED A CRACK ON THE LH HORIZONTAL STABILIZER RIB 11A. MAINTENANCE REMOVED AND REPLACED THE LH HORIZONTAL STABILIZER RIB 11A IAW EMBRAER SRM 51-41-01. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: CABLE — WORN (MLG) · airframe 39,203 hrs · 23,178 cycles

BOTH EMERGENCY EXTENSION MAIN CABLE AND RETURN CABLES WORN. BOTH EMERGENCY EXTENSION MAIN CABLE AND RETURN CABLE REPLACED IAW AMM 32-34-09.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 39,203 hrs · 23,178 cycles

LOCATED AT FR 17 BETWEEN STGRS 26-27L, SHEAR CLIP FOUND CORRODED. SHEAR CLIP REPLACE IAW SRM 51-42-02. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 39,203 hrs · 23,178 cycles

LOCATED AT FR 17 BTWN STGR27-28L, SHEAR CLIP FOUND CORRODED. SHEAR CLIP REPLACE IAW SRM 51-42-02. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: LIGHT — NOT REPORTED (CABIN) · airframe 38,522 hrs · 22,762 cycles

PHOTOLUMINESCENT STRIP ROW 2 RH SIDE. R&R RH PHOTOLUMINESCENT STRIP LIGHT FROM CLOSET TO ROW 2 IAW AMM 33-50-21.

Part: A/C PACK — CONTAMINATED (NR 1) · airframe 35,196 hrs · 20,742 cycles

LAV SMOKE ON EICAS AFTER TAKEOFF. SMOKE ODOR FILLED THE FLIGHT DECK AND CABIN. DECLARED AN EMERGENCY AND RETURNED TO FIELD, LANDED WITHOUT INCIDENT. TROUBLESHOT IAW FIM 21-20-00-810-801-A. ISOLATED TO DE-ICE FLUID IN THE NR 1 A/C PACK. RAN ENGINES SEVERAL TIMES AND THE ODOR DISSIPATED.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 34,345 hrs · 20,193 cycles

MAINTENANCE REPORTED CORROSION ON THE GUSSET PLATE AT FRAME 90. MAINTENANCE REMOVED AND REPLACED THE GUSSET IAW SRM 51-10-03, 51-75-16, 51-40-02, & 51-42-02.

Part: SPLICE PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 34,345 hrs · 20,193 cycles

MAINTENANCE REPORTED CORROSION ON THE RT SHEAR PANEL SPLICE PLATE AT FRAME 87. MAINTENANCE REMOVED, FABRICATED, AND INSTALLED THE SHEAR PANEL SPLICE PLATE IAW SRM 51-10-03, 51-75-16, 51-42-02, 53-23-10, 51-31-00, 51-40-03, 51-23-04, 51-23-05, & 51-23-06.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 34,345 hrs · 20,193 cycles

MAINTENANCE REPORTED CORROSION ON THE RT SHEAR PANEL AT FRAME 87. REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 53-23-10, 51-10-03, 51-42-01, 51-42-02, & 51-40-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,151 hrs · 19,418 cycles

DOOR EMERGENCY LIGHT INOPERATIVE. R & R L1 DOOR EMERGENCY LIGHT BATTERY IAW AMM 33-50-01. OPS CHECKED GOOD.

Part: LANDING GEAR — LACK OF LUBE (NOSE) · airframe 32,955 hrs · 19,295 cycles

CREW RECEIVED A 'LG WOW SYS FAIL' MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED NOSE STRUT SERVICE, ADJUSTED #2 WOW TARGET ON NOSE GEAR, INSPECTED CONNECTOR PLUGS, PERFORMED LUBE OF NOSE GEAR AND DID SEVERAL GEAR SWINGS PER EMB AMM AND OPS CHECKED GOOD.

Part: ROD — DIRTY (R2 DOOR) · airframe 32,618 hrs · 19,097 cycles

CREW REPORTED THAT THE R2 DOOR VENT WAS HARD TO CLOSE. MAINTENANCE CLEANED AND LUBED SLIDE LOCKING ROD IAW AMM AND OPS CHECKED GOOD.

Part: BRACKET — OUT OF ALIGNMENT (R1 DOOR) · airframe 32,469 hrs · 19,011 cycles

CREW REPORTED THAT THE R1 DOOR DISARMED INDICATION WINDOW WAS OUT OF ALIGNMENT. MAINTENANCE ADJUSTED BRACKET FOR DISARMED INDICATION PER EMB AMM AND OPS CHECKED GOOD.

Part: PRESSURE SWITCH — MALFUNCTIONED (BLEED SYSTEM) · airframe 32,219 hrs · 18,847 cycles

DURING FLIGHT, CREW RECEIVED A BLEED 1 OVER PRESSURE MESSAGE,RAN QRH. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED HPSOV HIGH PRESSURE SWITCH IAW AMM AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 32,185 hrs · 18,827 cycles

CREW REPORTED THAT THE FIRST OFFICERS FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IAW AMM AND OPS CHECKED GOOD.

Part: DOOR — UNKNOWN (L1) · airframe 32,093 hrs · 18,765 cycles

CREW REPORED THAT THE L1 DOOR WOULD NOT CLOSE. MAINTENANCE PERFORMED OPS CHECK OF THE L1 DOOR IAW AMM AND OPS CHECKED GOOD.

Part: CONTROL UNIT — INOPERATIVE (TE FLAP) · airframe 31,943 hrs · 18,664 cycles

CREW RECEIVED A FLAP FAIL MESSAGE. CREW RAN QRH AND DECLARED AN EMERGENCY WITH EMERGENCY VEHICLES ROLLING, CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R SFACE 1 IAW AMM AND OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 31,942 hrs · 18,663 cycles

CREW RECEIVED A FLAP FAIL MESSAGE. CREW RAN QRH AND DECLARED AN EMERGENCY, WITH EMERGENCY VEHICLES ROLLING, CREW LANDED WITHOUT INCIDENT. MAINTENANCE C/W FIM 27-51-00, CLEARED INHIBITS ON SF 1 AND 2 CHANNELS AND PERFORMED OPS CHECK OF THE FLAPS IAW AMM. OPS CHECKED GOOD.

Part: INDICATOR — OUT OF ADJUST (R2 DOOR) · airframe 30,552 hrs · 17,762 cycles

R2 DOOR ARMED, DISARMED INDICATOR IN VIEW WINDOW MISALIGNED. R & R R2 SLIDE INDICATION ADJUSTING SCREW IAW AMM 52-41-22. OPS CHECK GOOD.

Part: SIGHT GAUGE — OUT OF ADJUST (L2 GIRT BAR) · airframe 29,518 hrs · 17,099 cycles

F/A REPORTS DOOR L2 GIRT BAR DOES NOT SHOW ARMED IN WINDOW. ADJUSTED L2 GIRT BAR SIGHT WINDOW IAW AMM 52-12-00.

Part: MOUNT — CRACKED (NR 1 ENGINE) · airframe 29,471 hrs · 17,067 cycles

LT WING NR 1 ENGINE INBD MOUNT CRACKED. CUTOUT SECTION OF CRACKED CHORD ASSY, SPLICED IN NEW PIECE AND REWORKED A TOOLING HOLE IAW ETD2015-170-082729, REV D.

Part: LINK — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 29,471 hrs · 17,067 cycles

NR 1 ENGINE PYLON OTBD LOWER LINK INBOARD SURFACE HAS CORROSION FOUND UNDER FAIL SAFE ANGLE WHILE PERFORMING CRACKED LOWER LINK REPAIR. PERFORMED ROTO PEAN AND FINAL REPAIR IAW ETD2015-170-085250.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,471 hrs · 17,067 cycles

RT HORIZONTAL STABILIZER L/E 341AR HAS A CRACK IN RIB 4 AS MARKED. CUT OUT DAMAGE, INSTALLED DOUBLER AND FILLER IAW ETD2015-170-082627. MAJOR REPAIR.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,471 hrs · 17,067 cycles

RIGHT HORIZONTAL STABILIZER, RIB 10 CRACKED, 2 PLACES, LOWER FLANGE, FWD END. REMOVED CRACKED FLANGES AND FABRICATED AND INSTALLED SHEAR CLIPS IAW ETD2015-170-083748.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,471 hrs · 17,067 cycles

RIGHT HORIZONTAL STABILIZER RIB 12 CRACKED, 1 PLACE. REMOVED CRACKED FLANGE AND FABRICATED AND INSTALLED SHEAR CLIP IAW ETD2015-170-083748.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,471 hrs · 17,067 cycles

RIGHT HORIZONTAL STABILIZER RIB 11 CRACKED, 3 PLACES, 1 UPPER FLANGE, 2 LOWER FLANGE, FWD END. REMOVED CRACKED FLANGES AND FABRICATED AND INSTALLED SHEAR CLIPS IAW ETD2015-170-083748.

Part: SPAR — CRACKED (LT WING) · airframe 29,471 hrs · 17,067 cycles

LEFT FASTENER HOLE IN SPAR 3 WING STUB HAS MULTIPLE CRACK INDICATIONS. REAMED SPAR 3 TO REMOVE DAMAGE, FABRICATED AND INSTALLED PLUGS FCBS 57-01-00-004 IAW ETD2015-170-086572, REV A.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 29,471 hrs · 17,067 cycles

SHEAR TIE CORRODED AT FRAME 17, STGR 27-28R. R & R SHEAR TIE IAW SRM 51-41-02.

Part: SPAR — CRACKED (RT WING) · airframe 29,471 hrs · 17,067 cycles

RT FASTENER HOLE IN SPAR 3 WING STUB HAS MULTIPLE CRACK INDICATIONS. REAMED SPAR 3 TO REMOVE DAMAGE, FABRICATED AND INSTALLED PLUGS FCBS 57-01-00-004 IAW ETD2015-170-086572, REV A.

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 29,471 hrs · 17,067 cycles

SHEAR TIE ON FRAME 16, STR 27R-28R, SHOWS EVIDENCE OF CORROSION. R & R SHEAR TIE IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 29,471 hrs · 17,067 cycles

SHEAR CLIP, FRAME 17, STRINGERS 26-27R. R & R SHEAR TIE IAW SRM 51-41-01, 51-41-02.

Part: SHEAR TIE — DAMAGED (FRAMES 12) · airframe 29,471 hrs · 17,067 cycles

FRAME 12, SHEAR TIE BETWEEN STRINGERS 18-19L . SKIN DENTED ON BOTH SIDES OF SHEAR TIE. R & R SHEAR TIE IAW SRM 51-41-02.

Part: DOUBLER — NOT REPORTED (FRAMES 17-21) · airframe 29,471 hrs · 17,067 cycles

INTERNAL DOUBLER BETWEEN FRAMES 17 AND 21 AT STR 22L-23L REQUIRES REPLACEMENT OF EXTERNAL MS20470AD RIVETS IAW ETD2010-170-00952B. THE LT SECTION OF THE FWD FUSELAGE SKIN AT FRAMES 17L TO 21L AND BETWEEN STR 22L TO 23L WAS REPAIRED IAW ETD2010-170-00952, REV B. MAJOR REPAIR.

Part: BEAM — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 29,471 hrs · 17,067 cycles

FWD CARGO DOOR CUTOUT LOWER BEAM CORRODED. R & R LOWER BEAM IAW SRM 51-43-01, 51-40-02, 51-41-01, 51-43-02.

Part: LINK — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 29,471 hrs · 17,067 cycles

NR 1 ENGINE PYLON OTBD LOWER LINK INBD SURFACE HAS CORROSION FOUND UNDER FAIL SAFE ANGLE WHILE PERFORMING CRACKED LOWER LINK REPAIR. REMOVED CORROSION IAW SRM 51-10-03 AND 51-10-02.

Part: DOUBLER — DAMAGED (ZONE 100) · airframe 29,471 hrs · 17,067 cycles

FWD CARGO CUTOUT LOWER BEAM AFT DOUBLER DAMAGED. R & R AFT DOUBLER IN FWD CARGO DOOR CUTOUT IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FRAME 19) · corrosion level 2 · airframe 29,471 hrs · 17,067 cycles

REPAIR DOUBLER ON LT SEAT TRACK BEAM AT FR 19 IS CORRODED. REMOVED CORRODED DOUBLER AND INSTALLED NEW DOUBLER IAW SRM 51-10-10.

Part: GIRT BAR — DISPLACED (L2 DOOR) · airframe 29,427 hrs · 17,033 cycles

GIRT BAR INDICATOR L2 DOOR IS DISPLACED. ADJUSTED L2 GIRT BAR INDICATOR. OPS CHECK GOOD IAW MM 52-12-22.

Part: SKIN — DENTED (FRAMES 1 - 2) · airframe 28,111 hrs · 16,137 cycles

FOUND DENT IN FWD LT FUSELAGE BETWEEN FR 1-2 ON STR 26L. LENGTH OF 6", WIDTH 3", DEPTH .03125. REMOVED FASTENER, SKIN RETURNED TO ORIGINAL CONTOUR WITHOUT REWORK AND LT A .080" GAP BETWEEN SKIN AND INTERCOSTAL. R & R INTERCOSTAL IAW ETD2015-170-011303, REV B.

Part: GIRT BAR — CONTAMINATED (L2 DOOR) · airframe 27,871 hrs · 15,978 cycles

L2 DOOR ARMING HANDLE JAMMED, CANNOT DISARM DOOR. REMOVED DEBRIS FROM UNDER GIRT BAR, DOOR OPERATES NORMALLY IAW AMM 52-42-00.

Part: LINKAGE — OUT OF ADJUST (L2 DOOR) · airframe 27,190 hrs · 15,581 cycles

L2 ARM/DISARM DOES NOT LINE UP. ADJUSTED L2 ARM/DISARM INDICATION LINKAGE IAW AMM 32-12-22.

Part: INDICATOR — OUT OF LIMITS (L2 DOOR) · airframe 26,506 hrs · 15,173 cycles

L2 DOOR NOT ARMING. THE DOOR INDICATIONS DO NOT SHOW ARMED. ADJUSTED WINDOW FOR L2 DOOR IAW AMM 20-10-02, OPS CHECKED GOOD.

Part: DEFLECTOR — DAMAGED (L2 DOOR) · airframe 26,080 hrs · 14,928 cycles

AFTER CLIMBING THROUGH 10,000 FEET, F/A CALLED AND REPORTED AND ABNORMAL VIBRATION AND A "RUSHING, ROARING" NOISE FROM THE REAR CABIN. RETURNED TO FIELD, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH FIM TASK 05-50-00-810-801A FOR ABNORMAL NOISE. DURING INSPECTION, FOUND L2 DOOR DEFLECTOR DAMAGED, AND WORN. R & R L2 DOOR DEFLECTOR IAW AMM 52-12-28.

Part: CAM — OUT OF ADJUST (L1 DOOR) · airframe 26,042 hrs · 14,907 cycles

L1 DOOR IS NOT CLOSING. RESET CAM ON MAIN ENTRY DOOR HOISTING AND LIFTING MECHANISM IAW MM 52-11-00-820-803A. PERFORMED OPS CHECK OF DOOR ACTUATION AND CLOSING, NO DEFECTS NOTED.

Part: DOOR — OBSTRUCTED (L1) · airframe 25,017 hrs · 14,311 cycles

MAIN PAX DOOR HARD TO OPEN/CLOSE, SEEMS TO BE HANGING UP ON SOME BROKEN SHEET METAL. RESECURED L1 DOOR TRIM REF AMM 25-23-04. DOOR OPERATION OK.

Part: FITTING — DAMAGED (PAX DOOR) · airframe 24,857 hrs · 14,217 cycles

MAIN CABIN DOOR WILL NOT OPEN NORMALLY FROM THE EXTERIOR. DOOR OPENS NORMALLY FROM THE INTERIOR. ACFT FERRIED. R & R MAIN PASSENGER DOOR SUPPORT ARM FITTINGS LOWER IAW AMM 52-11-30. OPS CHECK GOOD.

Part: DEFLECTOR — OBSTRUCTED (L2 DOOR) · airframe 24,319 hrs · 13,906 cycles

L2 DOOR MAKING LOUD VIBRATION NOISE IN FLIGHT. INSPECTED L2 DOOR AREA AND FOUND DEBRIS UNDER DEFLECTOR, CLEANED DEBRIS, INSPECTED IAW AMM 52-12-28-06, OPS CHECK GOOD.

Part: STRUCTURE — DAMAGED (ZONE 100) · airframe 23,473 hrs · 13,392 cycles

RIGHT WING AFT SPUR DAMAGED AT HYD SYS NR 1 PRESSURE PASS THROUGH. REMOVED DAMAGE, FABRICATED BUSHING, INSTALLED. MAJOR REPAIR.

Part: RIB — CRACKED (ZONE 100) · airframe 23,479 hrs · 13,392 cycles

LEFT RIB 10 EXTENSION CRACKED. R & R RIB. MAJOR REPAIR.

Part: RIB — CRACKED (ZONE 100) · airframe 23,473 hrs · 13,392 cycles

RIGHT RIB 10 CRACKED. R & R RIB. MAJOR REPAIR.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 23,479 hrs · 13,392 cycles

CRACK FOUND ON FLOORBOARD SUPPORT BRACKET CRACKED AT FR 85 RT SIDE CROSSBEAM. R & R SUPPORT BRACKET.

Part: CROSSBEAM — CORRODED (ZONE 100) · airframe 23,423 hrs · 13,392 cycles

CROSSBEAM AT FRAME 14 CORRODED BETWEEN RT SEAT TRACK AND OTBD FLOOR SUPPORTS. REPAIRED FR 14 IAW ETD 2013-170-019325. MAJOR REPAIR.

Part: RETAINER — GOUGED (PAX DOOR SEAL) · airframe 23,473 hrs · 13,392 cycles

FWD PASSENGER DOOR AFT METAL SEAL HAS TWO GOUGES. R & R L1 DOOR SEAL RETAINER AFT. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,473 hrs · 13,392 cycles

CORROSION FOUND ON LT SEAT TRACK AT FR 19 CROSSBEAM. REMOVED DAMAGE AND FABRICATED FILLER AND DOUBLER AND INSTALLED REPAIR PARTS.

Part: LIGHT — WRONG PART (CABIN) · airframe 23,366 hrs · 13,327 cycles

EMERGENCY LIGHT JUST AFT OF WARDROBE WRONG COLOR. R & R EMERGENCY LIGHT IAW AMM 33-50-21.

Part: ENGINE — LEAKING (NR 1) · airframe 21,024 hrs · 11,937 cycles

STRONG BURNT SMELL ON TAKEOFF ROLL, NO SMELL NOTED WITH APU BLEED ON, SMELL RETURNED ON APPROACH. FERRIED A/C TO IND. REMOVED AND REPLACED E1.

Part: FILTER — DIRTY (CABIN) · airframe 20,931 hrs · 11,885 cycles

MOLDY SMELL FROM PACKS ON TAKEOFF TO FL180 AND BACK AGAIN THROUGH DESCENT. REMOVED AND REPLACED RECIRC FILTERS PER JOB CARD.

Part: PIN — OUT OF POSITION (CABIN DOOR) · airframe 20,587 hrs · 11,677 cycles

MAIN CABIN DOOR WILL NOT CLOSE. UPON FURTHER INSPECTION FOUND PIN OUT ON BOTTOM FORWARD POSITION ON INFLATABLE SLIDE. RE-SECURED IAW EMB 170 MM 52-11-40.

Part: ROD — BROKEN (R2 DOOR) · airframe 20,474 hrs · 11,614 cycles

THE 2R DOOR ARM/DISARM MESSAGE FOR SLIDE NOT INDICATING PROPERLY. REPLACED BROKEN ROD ON VISUAL DOOR INDICATOR PER AMM 52-42-22, OPS CHECK GOOD.

Part: PROXIMITY SWITCH — OUT OF ADJUST (SERVICE DOOR) · airframe 19,317 hrs · 10,896 cycles

DOOR SVC FWD OPEN MESSAGE IN FLIGHT, PRESSURIZATION NORMAL. ADJUSTED FWD SVC DOOR LATCH PROX SWITCH IAW EMB 170 MM 52-74-20. OPS CHECK GOOD.

Part: PIN — UNSECURE (L1 DOOR SLIDE) · airframe 19,118 hrs · 10,773 cycles

PIN HANGING FROM BOTTOM OF L1 DOOR, PREVENTING DOOR FROM OPERATING PROPERLY. SECURED BUSTLE PIN ON L1 DOOR IAW MM 52-11-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 19,039 hrs · 10,727 cycles

DOOR SERV FWD OPEN EICAS MESSAGE EN ROUTE, DOOR INDICATORS SHOW CLOSED AND ARMED, PRESSURE CHECKS NORMAL. PERFORMED OPS CHECK IAW FIM 52-74-00-810-801-A00. NO MESSAGE PRESENT ON EICAS AT THIS TIME, OPS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (SERVICE DOOR) · airframe 18,689 hrs · 10,491 cycles

SERVICE DOOR FWD OPEN MESSAGE. PERFORMED OPS CHECK ON FWD SERVICE DOOR IAW MM 12-13-01.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,322 hrs · 10,267 cycles

AFTER TAKEOFF FA'S REPORTED BURNING ODOR IN CABIN. RETURNED TO EWR. PERFORMED OPS CHECK OF APU, ALL CHECKS GOOD. PERFORMED OPS CHECK BY MEANS OF RUNNING ENG 1 AND 2, COULD NOT DUPLICATE ODOR. NO DEFECTS NOTED IAW AMM 49-10-00 AND GE 72-00-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 18,316 hrs · 10,263 cycles

AT FL310 RECEIVED DOOR (SERVICE) FWD OPEN MESSAGE. WENT AWAY AT FL190. PERFORMED TROUBLESHOOTING CHECK OF SENSOR BY PULLING CBS AND FOUND NO PROBLEMS IAW EMB FIM TASK 52-74-00-810-A. NO MESSAGE PRESENT.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,685 hrs · 9,860 cycles

LEVEL 2 CORROSION FOUND ON GUSSET PLATE AT FR90 RT OUTBD. REMOVED AND REPLACED IAW EMB 170 SRM 51-41-02.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 17,685 hrs · 9,860 cycles

LEVEL 2 CORROSION FOUND ON GUSSET PLATE FR90 RT INBD. REMOVED AND REPLACED GUSSET PLATE IAW EMB 170 SRM 51-41-02.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,685 hrs · 9,860 cycles

LEVEL 2 CORROSION WASTE WATER SERVICE BOX DOUBLER AND FASTENERS. REMOVED AND REPLACED FWD DOUBLER AND CORRODED FASTENERS IAW EMB 170 SRM 51-43-01.

Part: DOOR — CORRODED (LAV SERVICE) · airframe 17,685 hrs · 9,860 cycles

LEVEL 2 CORROSION WASTE WATER SERVICE DOOR ON EXTERIOR AND INTERIOR AREAS AT HINGE. REMOVED AND REPLACED SERVICE PANEL AND HINGE ASSY IAW EMB 170 SRM.

Part: BELLCRANK — DAMAGED (L1 DOOR) · airframe 17,246 hrs · 9,590 cycles

L2 DOOR WON'T CLOSE. CYCLED DOOR, OPS CHECK GOOD IAW EMB MM 52-12-00. MOC REQUESTED TROUBLESHOOTING WHEN A/C RON. MAINTENANCE FOUND LOWER HOIST BELL CRANK ROLL PIN HOLE ELONGATED. REMOVED AND REPLACED L2 DOOR LOWER HOIST BELLCRANK IAW EMB 170 MM 52-12-20, OPS CHECK GOOD.

Part: GUIDE — DIRTY (L2 DOOR) · airframe 17,237 hrs · 9,585 cycles

L2 DOOR WILL NOT CLOSE AFTER CATERING SERVICED THE A/C. MAINTENANCE CLEANED AND LUBED DOOR GUIDES IAW EMB 170 MM 52-42-02. OPS CHECK GOOD.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 11,693 hrs · 6,227 cycles

AFT WASTE BOX METAL ON TOP OF BOX BETWEEN FIBERGLASS CORRODED. REMOVED AND REPLACED AFT WASTE BOX IAW EMB 170 SRM PART II 51-43-02.

Part: STRUCTURE — CORRODED (LT WING) · airframe 11,693 hrs · 6,227 cycles

OVERBRAID LOCATED AT LEFT WING ROOT LEADING EDGE HAS EVIDENCE OF CORROSION THROUGH INBOARD ACCESS PANEL. CLEANED CORROSION AND INSPECTED IAW SRM 51-12-00.

Part: WIRE HARNESS — CORRODED (LT ENGINE) · airframe 11,693 hrs · 6,227 cycles

EVIDENCE OF CORROSION ON OVERBRAID LOCATED AT REAR OF LEFT ENGINE PYLON AND EVIDENCE OF CHAFING. CLEANED CORROSION FROM BRAIDED LINE, INSPECTED IAW EMB SRM 51-12. FOUND CHAFING TO BE WITHIN LIMITS.

Part: WIRE HARNESS — CORRODED (RT ENGINE) · airframe 11,693 hrs · 6,227 cycles

EVIDENCE OF CORROSION ON OVERBRAID LOCATED AT REAR OF RIGHT ENGINE PYLON AND EVIDENCE OF CHAFING. REMOVED AND REPLACED RT ENGINE W604 HARNESS IAW EMB 170 WM 73-21-50, AMM 20-10-01 AND IPC 24-02-73.

Part: WIRE HARNESS — CORRODED (RT WING) · airframe 11,693 hrs · 6,227 cycles

RIGHT WING AFT SPAR, FORWARD OF OUTBOARD GROUND SPOILER ACTUATOR, OVERBRAID ON WIRE BUNDLE SHOWS EVIDENCE OF CORROSION. REMOVED AND REPLACED RT ENG W604 HARNESS IAW EMB 170 WM 73-21-50, AMM 20-10-01, IPC 24-02-73.

Part: PLATE — CORRODED (FUSELAGE) · airframe 11,693 hrs · 6,227 cycles

AFT LAV AREA TOP GUSSET PLATE AT FRAME 90 AND RT SEAT TRACK FLOORBEAM HAS CORROSION. REMOVED TOP GUSSET PLATE AT FRAME 90 AND MANUFACTURED SERVICEABLE GUSSET PLATE IAW IC2009-170/00325. INSTALLED SERVICEABLE GUSSET PLATE IAW EMB 170 SRM 51-41-02.

Part: PLATE — CORRODED (LAVATORY AREA) · airframe 11,693 hrs · 6,227 cycles

AFT LAV AREA TOP GUSSET PLATE AT FRAME 90 AND RT FLOORBEAM FWD OF AFT BATTERY RACK HAS CORROSION. REMOVED TOP GUSSET PLATE AT FRAME 90 AND MANUFACTURED SERVICEABLE GUSSET PLATE IAW IC2009-170/00325. INSTALLED SERVICEABLE GUSSET PLATE IAW EMB 170 SRM 51-41-02.

Part: PLATE — CORRODED (FUSELAGE) · airframe 11,693 hrs · 6,227 cycles

AFT LAV AREA TOP GUSSET PLATE AT FRAME 90 AND LT SEAT TRACK FLOORBEAM HAS CORROSION. REMOVED TOP GUSSET PLATE AT FRAME 90 AND MANUFACTURED SERVIEABLE GUSSET PLATE IAW IC2009-170/00325. INSTALLED SERVICEABLE GUSSET PLATE IAW EMB 170 SRM 51-41-02.

Part: PLATE — CORRODED (LAVATORY AREA) · airframe 11,693 hrs · 6,227 cycles

AFT LAV AREA TOP GUSSET PLATE AT FRAME 90 AND FWD FLOOR MOUNT FOR WASTE TANK HAS CORROSION. REMOVED TOP GUSSET PLATE AT FRAME 90 AND MANUFACTURED SERVICEABLE GUSSET PLATE IAW EMB 170 IC2009-170/00325. INSTALLED SERVICEABLE GUSSET PLATE IAW SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 11,693 hrs · 6,227 cycles

AFT GALLEY AREA O/B RIGHT FLOOR SUPPORT AFT END OVER FRAME 90 HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT STRAP IAW SRM 51-40-02 AND SRM 51-41-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,693 hrs · 6,227 cycles

FLOORBEAM UNDER FWD GALLEY HAS LIGHT SURFACE CORROSION AROUND TWO RIVET FASTENERS. PERFORMED REPAIR AS CALLED OUT IN EMB 170 IC2009-170/06914.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,693 hrs · 6,227 cycles

FLOORBEAM AT RIGHT FWD SERVICE DOOR HAS LIGHT SURFACE CORROSION UNDER FLOOR PANEL. PERFORMED REPAIR AS CALLED OUT IN IC2009-170-06914.

Part: BATTERY — DISCHARGED (CABIN) · airframe 10,244 hrs · 5,363 cycles

EMER LT BATT FAULT EICAS MESSAGE WITH EMERGENCY LIGHTS ON. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY POWER (FORWARD LEFT) IAW EMB MM 33-50-01.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 9,666 hrs · 5,004 cycles

WHEN SELECTING SLAT/FLAP 5 THE CREW RECEIVED A MASTER CAUTION AND ASSOCIATED EICAS MESSAGE STATING SLAT/FLAP LEVER DISAGREE. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX REPOWERED THE ACFT AND TROUBLESHOT IAW FIM AND WAS UNABLE TO DUPLICATE THE FAULT.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 7,224 hrs · 3,463 cycles

MAJOR REPAIR: FORWARD CENTER FUSELAGE SUFFERED GROUND DAMAGE. SKIN HAS THROUGH DAMAGE AT STATION X=6232.5. DAMAGE RUNS FORWARD 7 FT 10 INCH AND 1 IN BELOW STRINGER 20L TO .750 INCH ABOVE STRINGER 22L. THE SKIN RUNNING AFT IS DENTED AND CREASED FROM FR23 TO FR27 WITH DEPTHS FROM 0.000 TO 0.800 INCH APPROX 2 IN FORWARD OF FRAME 27 BETWEEN STRINGERS 20L AND 21L. DAMAGE WAS REPAIRED IAW IC2007-170/09211D.

Part: UNKNOWN — UNKNOWN · airframe 3,358 hrs · 1,254 cycles

FLIGHT 6478 DTW TO SLC DURING CRUISE ENCOUNTERED AVIONICS MAU 1 FAIL. QRH FOLLOWED. DIVERTED TO DSM. NO FURTHER INCIDENT. OVERWEIGHT LANDING REPORTED. OCM RESET POWER AND MAU1 FAIL MSG CLEARED, ALSO HAD A FLT CONTROL FAULT ON POWER UP; PERFORMED RTS. SIGNED OFF OVERWEIGHT LANDING, NO INSP NEEDED, SINK RATE WAS REPORTED AT 200 FPM.

Part: SENSOR — FAULTY (T/E FLAP) · airframe 2,521 hrs · 888 cycles

FLIGHT 6436 AUS TO JFK AT 35,000 FEET IN NORMAL CRUISE, THE AMBER -FLAP FAIL- EICAS MESSAGE APPEARED. THE CREW RAN THE QRH BUT WAS UNABLE CYCLE THE FLAPS BECAUSE AIRCRAFT ABOVE MAX FLAP OPERATING ALTITUDE. ONCE THE AIRCRAFT DESCENDED BELOW 20,000 FT THE CREW ATTEMPTED TO CONFIGURE THE AIRCRAFT TO CYCLE THE FLAPS TO -FLAP ONE-, THE SLATS EXTENDED BUT THE FLAPS REMAINED AT ZERO. THE CREW MADE THREE ATTEMPTS WITH NO SUCCESS. THE CREW FINISHED THE QRH, DECLARED AN EMERGENCY AND PREPARED FOR A NO FLAPS LANDING. THE APPROACH AND LANDING WERE UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED BOTH LT FLAP SKEW SENSORS, THE NR 1 SF-ACE AND PERFORMED AN ELECTRICAL RIG OF THE SF-ACE.