N859RW

Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,686 hrs · 27,615 cycles

SHEAR CLIP AT FR81, STR 29R - 28R FOUND CORRODED. R&R IAW SRM 51-41-01 AND 51-41-02.

Part: SHEAR PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,686 hrs · 27,615 cycles

AFT CARGO R/H SHEAR CLIP AT FR 87, STR 27R - 27R FOUND CORRODED. R&R IAW SRM 51-41-01 AND 51-41-02.

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,686 hrs · 27,615 cycles

AFT CARGO INTERCOSTAL AND CLIP AT FR 87+2, STE 27R - 28R FOUND CORRODED. R&R IAW SRM 51-41-01.

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,686 hrs · 27,615 cycles

R/H SILL DOUBLER BTWN FR 12-14 FOUND CORRODED. R&R IAW SRM 51-41-02.

Part: UPPER SHEET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,686 hrs · 27,615 cycles

R/H PNL SUPPORT FR 84 RBL 39 FOUND CORRODED. R&R IAW SRM 51-41-02 AND 51-43-02.

Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,686 hrs · 27,615 cycles

MID SHEAR PNL BTWN FR 87-88 FOUND CORRODED. R&R IAW SRM 51-42-01.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,686 hrs · 27,615 cycles

GUSSET PLATE AT FR 90 RBL 11 FOUND CORRODED. R&R IAW SRM 51-41-02.

Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,686 hrs · 27,615 cycles

L2 DOOR LOWER BEAM FR 86-87 FOUND CORRODED. R&R IAW SRM 51-43-03 AND 51-43-04.

Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,686 hrs · 27,615 cycles

R/H SHEAR PNL BTWN FR 87-88 FOUND CORRODED. R&R IAW SRM 51-42-01 AND 51-42-02.

Part: UPPER SHEET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,686 hrs · 27,615 cycles

R&R R/H UPPER SHEET BTWN FR 85-86 FOUND CORROSION. R&R IAW SRM 51-41-01 AND 51-43-03.

Part: ACM — SMOKE (ZONE 100) · airframe 45,429 hrs · 27,415 cycles

SMOKE IN CABIN. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED FIM TASK 21-20-00-810-801. R&R PACK 1 AIR CYCLE MACHINE.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 45,321 hrs · 27,341 cycles

WASTE SERVICE BOX DOUBLER CORRODED. REPLACED DOUBLER IAW EMB 170/175 SRM 51-41-02 AND51-43-04. REF VP-015745-2022 NR 10,11,12,13,14,15.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,895 hrs · 26,389 cycles

SECOND REAR CEILING EMERGENCY LIGHT IS OUT. R&R EMERGENCY LIGHT POWER UNIT #3 IAW AMM 33-50-01.

Part: DISK — PUNCTURED (R2 DOOR) · airframe 41,687 hrs · 24,919 cycles

AFT R2 SERVICE DOOR NO PRESSURE, BURST DISK PUNCTURED. R&R AFT R2 DOOR DIAPHRAGM, SERVICED DOOR REF AMM 52-42-53.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,687 hrs · 24,919 cycles

MULTIPLE FWD EMERGENCY LIGHTS INOP. R&R #1 FWD EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01.

Part: CLOSEOUT PANEL — CORRODED (FRAMES 24-27) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY MAINTENANCE - FWD CARGO CLOSEOUT PANEL HAS CORROSION IN SEVERAL PLACES. REPLACED FWD CARGO DOOR CLOSE OUT PANEL. REF: E170 AMM 20-10-01.

Part: SEAT TRACK — CORRODED (FRAMES 74-84) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK - RIGHT HAND INBOARD SEAT TRACK FR 74 -FR 84 HAS MULTIPLE AREAS OF CORROSION / GOUGES AS MARKED

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND SHEAR CLIP CORRODED FR17 BETWEEN STRG 28L AND 28R. REMOVED AND REPLACED NEW SHEAR CLIP AT FR 17 STR 28L-28R REF SRM 51-40-08. RESTORED SURFACE PROTECTION TO THE NEW SHEAR CLIP AT FR 17 STR 28L-28R. REF SRM 51-23-06. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND FR17 SHEAR CLIP CORRODED AT STRG 27L-28L. REMOVED AND REPLACED SHEAR CLIP FR17 ST 28-27L REF EMB SRM 51-40-08, 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: SEAT TRACK — CORRODED (FRAME 17) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND RH SEAT TRACK BEAM IS CORRODED AT FR 17. REPAIRED RH SEAT TRACK BEAM AT FR 17 BY WAY FOR CUTTING OUT DAMAGE, FRABRICATING AND INSTALLING AND FILLER AND DOUBLER REF EMB SRM 53-10-10/ REPAIR01P. A/C REMAINS IN CHECK.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

RH SILL AFT SIDE OF FWD SERVICE DOOR AT FR15 HAS CORROSION AS MARKED. REMOVED CORRODED RH SILL , AFT SIDE , LOCATED ,DRILLED NEW RH SILL AFT SIDE REF EMB SRM 51-40-02 ALODINED NEW PART REF EMB SRM 51-23-04 PO# 207882 FULLY INSTALLED RH SILL BETWEEN FR 17-19, REF. EMB SRM 51-40-08 RESTORED SURFACE PROTECTION BY APPLYING TOPCOAT (PO#251151) REF SRM 51-23-06. SEE EAMS W/O H6959 SN 883 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

LH FUSELAGE FR19 5 HOLE DOUBLER HAS 3 EA AREAS OF CORROSION AS MARKED. REMOVED LH FUSELAGE FR19 5 HOLE DOUBLER REF EMB SRM 51-40-08 INSTALLED NEW LH FUSELAGE 5 HOLE DOUBLER AT FR 19 REF EMB SRM 51-40-02 AND SRM 51-40-08 RESTORED SURFACE PROTECTION BY APPLYING TOPCOAT (PO#251151) REF SRM 51-23-06. SEE EAMS W/O H6959 SN 882 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: BEAM — CORRODED (FRAMES 24-27) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND FORWARD CARGO DOOR CUTOUT LOWER BEAM IS CORRODED AT LATCH 1 AND LATCH 4 MOUNTING AREAS. REMOVED AND REPLACED NEW FWD CARGO LOWER BEAM REF EMB SRM 51-40-08. RESTORED SURFACE PROTECTION ON FWD CARGO LOWER BEAM REF SRM 51-23-06. A/C REMAINS IN CHECK

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

RH OUTBOARD GALLEY SUPPORT IS CORRODED AT FR 88. REMOVED AND REPLACED RH OUTBOARD GALLEY SUPPORT AT FR 88 REF SRM 51-40-08 APPLIED SURFACE PROTECTION. REF: SRM 51-23-05, 51-23-06. SEE EAMS W/O H6959 SN 843 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

CORROSION THREE AREAS CENTER OF FRAME 11 CROSSBEAM. REMOVED AND REPLACED FR 11 UPPER CONNECTOR SUPPORT DOUBLER REF SRM 51-40-08. APPLIED SURFACE PROTECTION. REF: SRM 51-23-06. SEE EAMS W/O H6959 SN 792 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP FR 16 ST 27-28L. REMOVED AND REPLACED SHEAR CLIP @ FR16 STGR27L-28L REF EMB SRM 51-40-08, 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP FR 17 ST 26-27L. REMOVED AND REPLACED SHEAR CLIP FR17 ST 26-27L REF EMB SRM 51-40-08, 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 86) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND SHEAR CLIP CORRODED AT FR86 ST29L-ST29R. REMOVED AND REPLACED SHEAR CLIP AT FR86 ST29L-ST29R. REF: EMB ETD 2019-170-133517, SRM 51-21-01, SRM 51-40-08. RESTORED SURFACE PROTECTION TO SHEAR CLIPS BETWEEN FR86 STGR29L AND 29R AND AFT DRAIN FAIRING SUPPORT REF EMB SRM 51-23-06. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 86) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND AFT CARGO AT FR86 SHEAR CLIP CORRODED BETWEEN STRG. 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP AT FR86 BETWEEN STRG. 27R AND 28R REF SRM 51-40-08, 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR 17 ST 28L-28R. REMOVED AND REPLACED SHEAR CLIP AT FR 17 ST 28L-28R REF EMB SRM 51-40-08, 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 75) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND AFT CARGO AT FR75 SHEAR CLIP CORRODED BETWEEN STRG. 28R AND 27R. REMOVED AND REPLACED AFT CARGO AT FR75 SHEAR CLIP BETWEEN STRG 28R AND 27R PER REF SRM 51-40-08, 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR 17 ST 25R-26R. REMOVED AND REPLACED SHEAR CLIP AT FR17 ST 25R-26R REF SRM 51-40-08, 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 87) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND AFT CARGO AT FR87 SHEAR CLIP CORRODED BETWEEN STRG. 28R AND 29R. REMOVED AND REPLACED SHEAR CLIP AT FR87 BETWEEN STRG 28R-29R (AFT CARGO). REF EMB SRM 51-40-08, 51-23-06,CPM 51-25-00. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 87) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND AFT CARGO AT FR87 SHEAR CLIP CORRODED BETWEEN STRG. 29L AND 29R. REMOVED AND REPLACED 2EA SHEAR CLIPS AT FR87 STRG. 29L-29R (AFT CARGO). REF EMB SRM 51-40-08, 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

CORRODED 3 EA LOWER CONTROL ANGLE AND 2 EA CRACK RECEPTACLE ON PANEL 1441FR. REMOVED AND REPLACED 3EA LOWER CONTROL ANGLE AND 2EA CRACKED RECEPTACLE ON PANEL 1441FR REF EMB SRM 51-40-02 AND 51-45-00. SEE EAMS W/O H6959 SN 592 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SEAL REST — CORRODED (FRAMES 25-26) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION- FORWARD CARGO DOOR CUTOUT LOWER CENTER SEAL REST. REMOVED AND REPLACED FORWARD CARGO DOOR CUTOUT LOWER CENTER SEAL REST REF EMB SRM 51-40-08. RESTORED SURFACE PROTECTION ON FORWARD CARGO DOOR CUTOUT LOWER CENTER SEAL REST, REF SRM 51-23-06. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR 16 ST 27R-28R. REMOVED AND REPLACED FWD CARGO SHEAR CLIP @ FR 16 ST 27R-28R REF SRM 51-40-08, SRM 51-23-06 AND CIC CPM 51-25-00. ACFT REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR 17 ST 24R-25R. REMOVED AND REPLACED SHEAR CLIP FR17 STR24-25R REF EMB SRM 51-40-08, 51-23-06, CPM 51-25-00-910-01-A. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR 17 ST 27R-28R. REMOVED AND REPLACED SHEAR CLIP @ FR17 ST 27R-28R REF SRM 51-40-08, 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR 16 ST 25R-26R. REMOVED AND REPLACED SHEAR CLIP @ FR16 ST 25R-26R REF SRM 51-40-08, 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: ANGLE — CORRODED (FRAMES 55-56) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED 3 EA LOWER CONTROL ANGLE ON PANEL 1431DL. REMOVED AND REPLACED 3EA LOWER CONTROL ANGLE ON PANEL 1431DL, REF. EMB SRM 51-40-08. REF. AMM 20-10-01. APPLIED SURFACE PROTECTION AS REQUIRED. REF EMB SRM 51-23-04,51-23-05. A/C REMAINS IN CHECK.

Part: SUPPORT — CORRODED (FRAMES 26-27) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION- FORWARD CARGO DOOR CUTOUT AFT FRAME LOWER NUT SUPPORT. REMOVED AND REPLACED FORWARD CARGO DOOR CUTOUT AFT FRAME LOWER NUT SUPPORT, REF SRM 51-40-08, RESTORED SURFACE PROTECTION ON FORWARD CARGO DOOR CUTOUT AFT FRAME LOWER NUT SUPPORT REF SRM 51-23-06. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 83) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK MAINTENANCE FOUND AFT CARGO AT FR83 SHEAR CLIP CORRODED BETWEEN STRG. 28R AND 29R. REMOVED AND REPLACE SHEAR CLIP AT FR83 STRG 29R-28R REF SRM 51-40-02 , 51-40-08. A/C REMAINS IN CHECK.

Part: BEAM — CORRODED (FRAMES 85-87) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND AFT SERVICE DOOR LOWER BEAM IS CORRODED AT FORWARD AND AFT GIRT BAR FLOOR FITTINGS, AND AT CENTER OF BEAM, FRAMES 85-87. REMOVED AND REPLACED AFT SERVICE DOOR LOWER BEAM PER SRM 51-40-08, 51-23-05, 51-23-06.

Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

LH SEAT TRACK BEAM UPPER SHEET CORRODED, FR85-86. REMOVED AND REPLACED LH SEAT TRACK BEAM UPPER SHEET FR85-86 REF SRM 51-40-08 APPLIED SURFACE PROTECTION. REF: SRM 51-23-06. SEE EAMS W/O H6959 SN 460 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

RH INBOARD PANEL SUPPORT IS CORRODED, FR 88. REMOVED AND REPLACED RH INBOARD PANEL SUPPORT AT FR 88 REF. EMB SRM 51-40-08. APPLIED SURFACE PROTECTION. REF: SRM 51-23-05, 51-23-06. SEE EAMS W/O H6959 SN 490 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

L/H INBOARD SEAT TRACK FR 74 - FR 84 HAS MULTIPLE ARES OF CORROSION / GOUGES. REMOVED AND REPLACED LH INBOARD SEAT TRACK REF SRM 51-40-08 APPLIED SURFACE PROTECTION. REF: SRM 51-23-05, 51-23-06. SEE EAMS W/O H6959 SN 475 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 40,381 hrs · 24,123 cycles

CENTER SPLICE IS CORRODED, FR 90. REMOVED AND REPLACED SPLICE REF SRM 51-40-08 APPLIED SURFACE PROTECTION. REF: SRM 51-23-06. SEE EAMS W/O H6959 SN 482 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

LH SEAT TRACK BEAM UPPER SHEET CORRODED, FR85-86. REMOVED AND REPLACED LH SEAT TRACK BEAM UPPER SHEET FR85-86 REF SRM 51-40-08 APPLIED SURFACE PROTECTION. REF: SRM 51-23-06. SEE EAMS W/O H6959 SN 460 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

RH INBOARD SPLICE IS CORRODED, FR 89. REMOVED AND REPLACED RH INBOARD SPLICE AT FR 89 REF. EMB SRM 51-40-08 APPLIED SURFACE PROTECTION. REF: SRM 51-23-05, 51-23-06. SEE EAMS W/O H6959 SN 483 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

R/H OUTBOARD SEAT TRACK FR 74 - FR 84 HAS MULTIPLE AREAS OF GOUGES / CORROSION. REMOVED AND REPLACED RH OUTBOARD AFT SEAT TRACK REF EMB SRM 51-40-08. RESTORED PROTECTIVE AND APPLIED CIC REF EMB SRM 51-23-06 AND CPM 51-25-00. SEE EAMS W/O H6959 SN 496 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

RH OUTBOARD PANEL SUPPORT IS CORRODED, FR 89-90. REMOVED AND REPLACED R/H O/B PANEL SUPPORT. REF: SRM 51-40-08. APPLIED SURFACE PROTECTION. REF: SRM 51-23-05, 51-23-06. SEE EAMS W/O H6959 SN 489 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

LH OUTBOARD PANEL SUPPORT IS CORRODED, FR 89-90. REMOVED AND REPLACED L/H O/B PANEL SUPPORT AT FR 89-90. REF: SRM 51-40-08. APPLIED SURFACE PROTECTION. REF: SRM 51-23-06. SEE EAMS W/O H6959 SN 476 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

RH SEAT TRACK BEAM UPPER SHEET IS CORRODED, FR 85-86. REMOVED AND REPLACED UPPER SHEET REF SRM 51-40-08 APPLIED SURFACE PROTECTION. REF: SRM 51-23-06. SEE EAMS W/O H6959 SN 467 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

SPLICE OUTBOARD OF LH SHEAR PANEL IS CORRODED, FR 87-88. REMOVED AND REPLACED SPLICE OUTBOARD OF LH SHEAR PANEL FR 87-88.REF: SRM 51-40-08. APPLIED SURFACE PROTECTION. REF: SRM 51-23-06. SEE EAMS W/O H6959 SN 477 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

R/H INBOARD SEAT TRACK FR 23 - FR 34 HAS MULTIPLE AREAS OF CORROSION/GOUGES AS MARKED. CUT AND REMOVED R/H INBOARD SEAT TRACK FR 23 - FR 34 BETWEEN FR29 AND FR30 FOR SEAT TRACK REPAIR REF EMB SRM 53-00-10 REPAIR01 DRILLED, TREATED AND PRIMED SEAT TRACK AND 3EA SPLICES REF EMB SRM 53-00-10 R/01 INSTALLED NEW SEAT TRACK REPAIR SECTION AND SPLICES REF EMB SRM 51-40-08. SEE EAMS W/O H6959 SN 481 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

L/H INBOARD SEAT TRACK FR 74 - FR 84 HAS MULTIPLE ARES OF CORROSION / GOUGES REMOVED AND REPLACED LH INBOARD SEAT TRACK REF SRM 51-40-08 APPLIED SURFACE PROTECTION. REF: SRM 51-23-05, 51-23-06. SEE EAMS W/O H6959 SN 475 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,381 hrs · 24,123 cycles

RH SEAT TRACK BEAM (SUPPORT ANGLE) IS CORRODED APPROXIMATELY 3" AFT OF FR 90. REMOVED AND REPLACED RH SUPPORT ANGLE REF. EMB SRM 51-40-08. APPLIED SURFACE PROTECTION. REF: SRM 51-23-05, 51-23-06. SEE EAMS W/O H6959 SN 491 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: GATE — LACK OF LUBE (L2 DOOR) · airframe 36,521 hrs · 21,750 cycles

L2 VENT FLAP WILL NOT MOVE PROPERLY. STUCK WHEN ARRIVING AT GATE, IN THE CLOSED POSITION. CLEANED AND LUBED. OPS CHECKED IAW AMM 52-11-25.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,983 hrs · 20,816 cycles

CABIN EMERGENCY LIGHT WILL NOT ILLUMINATE. R & R THE POWER SUPPLY NR 2.

Part: PANEL — CORRODED (FRAME 28-30) · corrosion level 2 · airframe 34,714 hrs · 20,638 cycles

MAINTENANCE FOUND CORROSION ON PANEL 192CR. MAINTENANCE REPAIRED PANEL IAW SRM 51-23-04 AND 51-23-05.

Part: SHEAR PANEL — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 34,714 hrs · 20,638 cycles

MAINTENANCE FOUND CORROSION AT FRAMES 12 - 14 ON THE SHEAR PANEL. MAINTENANCE REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 51-40-02.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 34,714 hrs · 20,638 cycles

MAINTENANCE FOUND CORROSION AT FRAMES 87 - 88 ON THE SHEAR PANEL. MAINTENANCE REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 51-42-01, AND 51-42-02.

Part: SPLICE PLATE — CORRODED (FRAME 90) · corrosion level 2 · airframe 34,714 hrs · 20,638 cycles

MAINTENANCE FOUND CORROSION AT FRAME 90 ON A FLOOR SPLICE PLATE. MAINTENANCE REMOVED AND REPLACED SPLICE PLATE IAW SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 89-90) · corrosion level 2 · airframe 34,714 hrs · 20,638 cycles

MAINTENANCE FOUND CORROSION AT FRAME 89, ON THE FLOOR SUPPORT. MAINTENANCE REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-10-03, AND 51-75-16.

Part: ROLLER — LACK OF LUBE (L2 DOOR) · airframe 33,130 hrs · 19,610 cycles

CREW REPORTED THAT THE L2 DOOR LEVER WAS HARD TO ARM. MAINTENANCE LUBED THE L2 DOOR ROLLERS PER EMB AMM AND OPS CHECKED GOOD.

Part: UNKNOWN — NOISE (R1 DOOR) · airframe 32,769 hrs · 19,362 cycles

CREW REPORTED A LOUD VIBRATION SOUND ON THE R1 DOOR. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED R1 DOOR SEAL AND PERFORMED PRESSURIZATION CHECK IAW AMM AND OPS CHECKED GOOD.

Part: DEFLECTOR — MALFUNCTIONED (R1 DOOR) · airframe 32,773 hrs · 19,366 cycles

CREW REPORTED A HUM COMING FROM THE R1 DOOR. MAINTENANCE DEACTIVATED R1 DOOR DEFLECTOR IAW AMM AND LATER REMOVED AND REPLACED R1 DOOR DEFLECTOR IAW AMM AND OPS CHECKED GOOD.

Part: TORQUE LINK — OUT OF POSITION (LANDING GEAR) · airframe 32,398 hrs · 19,122 cycles

FLYING DTW - EWR, CREW REPORTED THAT THE GEAR WOULD NOT COME UP. CREW DECLARED AN EMERGENCY AND WITH VEHICLES ROLLING, LANDED IN DTW WITHOUT INCIDENT. AIRCRAFT WAS FLOWN VIA MAINTENANCE FERRY TO PIT WHERE MAINTENANCE FOUND WOW TARGET ON THE TORQUE LINKS ROTATED AROUND. MAINTENANCE ROTATED TORQUE LINK AND REMOVED AND REPLACED UPPER TORQUE LINK PER AMM AND OPS CHECKED GOOD.

Part: HANDLE — STICKING (L2 DOOR VENT) · airframe 32,086 hrs · 18,935 cycles

CREW REPORTED THAT THE L2 DOOR VENT FLAP HANDLE WAS GETTING STUCK AND HARD TO OPEN. MAINTENANCE LUBRICATED THE L2 DOOR VENT FLAP PER EMB AMM AND OPS CHECKED GOOD.

Part: VENT — OUT OF ADJUST (L2 DOOR) · airframe 32,009 hrs · 18,887 cycles

CREW REPORTED THAT THE L2 DOOR WOULD NOT DISARM. MAINTENANCE ADJUSTED L2 DOOR VENT FLAP PER EMB AMM AND OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 31,633 hrs · 18,658 cycles

CREW REPORTED THAT THE CAPTAINS FLASHLIGHT WAS NOT CHARGING. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.

Part: SKIN — DENTED (FRAMES 10-11) · airframe 31,581 hrs · 18,623 cycles

LT FORWARD FUSELAGE SKIN, DENTED AND SCRATCHED BETWEEN FRAMES 10-11 AND STRINGERS 15-16L. REPAIRED IAW ETD2016-170-065491 AND SRM 53-10-01 REPAIR 12P. MAJOR REPAIR.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 29,552 hrs · 17,301 cycles

HYDRAULIC 2 EDP FAIL EICAS MESSAGE AND HYDRAULIC SYSTEM 2 FLUID LEVEL DECREASING. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. R & R NR 2 EDP IAW AMM 29-11-01. OPS CHECK GOOD.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,125 hrs · 16,998 cycles

RT HORIZONTAL STABILIZER L/E HAS TWO CRACKED RIBS. CUTOUT DAMAGE, FABRICATED REPAIR DOUBLERS AND FILLERS, AND INSTALLED IAW ETD2015-170-063782.

Part: SHEAR TIE — DAMAGED (FRAME 11) · airframe 29,125 hrs · 16,998 cycles

SHEAR TIE FOUND DAMAGED AT FRAME 11 BETWEEN STRINGERS 17 - 18L. R & R THE SHEAR TIE IAW SRM 51-41-02 AND 51-41-01.

Part: SEAL REST — CORRODED (AFT CARGO) · airframe 29,125 hrs · 16,998 cycles

AFT CARGO, AFT SEAL REST HAS CORROSION. REMOVED AND REPLACED THE SEAL REST IAW AMM 20-10-01, 53-23-29, AND SRM 51-40-02, 51-21-01.

Part: SEAL REST — CORRODED (AFT CARGO DOOR) · airframe 29,125 hrs · 16,998 cycles

AFT CARGO FWD SEAL REST CORRODED. R & R THE SEAL REST IAW AMM 20-10-01 AND SRM 51-21-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,054 hrs · 15,701 cycles

EMERGENCY LIGHT INOPERATIVE. R & R THE LIGHT IAW AMM 33-50-21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,491 hrs · 14,796 cycles

MOST FORWARD RT EMERGENCY LIGHT NOT WORKING PROPERLY. R & R IAW AMM 33-2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,253 hrs · 14,660 cycles

EMERGENCY LIGHT NOT ILLUMINATING ADJACENT TO ROWS 1 AND 2. PERFORMED OPS CHECK OF LIGHT IAW AMM 33-50-21.

Part: COVER — BROKEN (L1 DOOR HANDLE) · airframe 24,848 hrs · 14,449 cycles

L1 DOOR HANDLE COVER IS BROKEN. R & R, OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 24,772 hrs · 14,403 cycles

FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOLLOWED FIM TASK 27-53-00-810-813A, CLEARED INHIBITS, MESSAGE CLEARED. FLAPS OPERATIONAL AT THIS TIME. INSPECTED FLAP ACTUATORS, NO DEFECTS NOTED AT THIS TIME.

Part: SPLICE — CORRODED (ZONE 100) · airframe 23,641 hrs · 13,716 cycles

CORROSION FOUND ON AFT CENTER SPLICE AT FR 90. R & R AFT CENTER SPLICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,641 hrs · 13,716 cycles

CORROSION FOUND ON RT SEAT TRACK EXTENSION UPPER PLATE AT FR 86. R & R RT SEAT TRACK.

Part: SKIN — CRACKED (LT WING) · airframe 23,641 hrs · 13,716 cycles

LEFT WING UPPER SKIN SURFACE ABOVE RIB 10 CRACKED. CUT OUT DAMAGE, FABRICATED FILLER AND INSTALLED.

Part: SKIN — CRACKED (RIGHT WING) · airframe 23,641 hrs · 13,716 cycles

RIGHT WING UPPER SKIN SURFACE ABOVE RIB 10 CRACKED. CUT OUT DAMAGE, FABRICATED FILLER AND INSTALLED.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 23,641 hrs · 13,716 cycles

SHEAR TIE HAS CORROSION FWD OF WASTE BOX ON FR88. R & R SHEAR TIE. MAJOR REPAIR

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 23,641 hrs · 13,716 cycles

CORROSION FOUND ON SHEAR TIE IN AFT CARGO ON FR 82 BETWEEN S27 AND 28R. R & R SHEAR TIE. MAJOR REPAIR.

Part: STRUCTURE — CORRODED (WASTE BOX) · corrosion level 2 · airframe 23,641 hrs · 13,716 cycles

CORROSION FOUND ON WASTE BOX. R & R WASTE BOX.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,641 hrs · 13,716 cycles

CORROSION FOUND ON FLOOR PLATE AFT OF R2 DOOR. R & R RT AFT SHEAR PLATE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,641 hrs · 13,716 cycles

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

Part: RIB — CRACKED (RT WING) · airframe 23,641 hrs · 13,716 cycles

RIGHT WING RIB 10 EXTENSION CRACKED ON UPPER FLANGE AT 3 RT LOCK FASTENER. R & R RT RIB EXTENSION.

Part: DOOR — CORRODED (WASTE SERVICE) · corrosion level 2 · airframe 23,641 hrs · 13,716 cycles

CORROSION WAS FOUND ON WASTE SERVICE PANEL DOOR. R & R WASTER SERVICE PANEL.

Part: SIGN — DAMAGED (CABIN) · airframe 22,952 hrs · 13,278 cycles

EXIT SIGN AT KNEE LEVEL BELOW FLASHLIGHT AT L1 DOOR IS DAMAGED FROM PASSENGER BAG WHILE EXITING. REMOVED AND REPLACED L1 DOOR EXIT IDENTIFIER SIGN IAW AMM 33-50-15. OPS CHECK GOOD.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 21,820 hrs · 12,616 cycles

FLOOR LEVEL EMERGENCY LIGHTING STRIPS MISSING REAR ORANGE EXIT INDICATOR SQUARES. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP IN LEFT AFT CABIN IAW AMM 33-50-21.

Part: GLOWSTRIP — DEFECTIVE (CABIN) · airframe 21,755 hrs · 12,579 cycles

ROW 1FD EMERGENCY PHOTO STRIP OUT. REMOVED AND REPLACED PHOTO STRIP AT SEAT 1FD PER EMB 170 MM 33-50-21. OPS CHECK GOOD.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 20,028 hrs · 11,329 cycles

WHILE AT CRUISE ALT FL340 APPROX 1 HOUR INTO FLIGHT, EICAS MESSAGE HYD 3 QTY LOW APPEARED. PULLED UP HYD PAGE ON MFD AND QTY WAS AT 16 PERCENT. ATC DECLARED EMERGENCY AFTER BEING NOTIFIED. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ACMP 3A IAW EMB 170 MM 29-12-01. NO LEAKS FOUND, OPS CHECK GOOD.

Part: LINER — OUT OF ADJUST (R1 DOOR) · airframe 18,936 hrs · 10,826 cycles

R1 DOOR ARM DISARM INSCRIPTION NOT SHOWING. ADJUSTED R1 DOOR LINING IAW EMB 170 MM 25-23-06. OPS CHECK GOOD.

Part: GUST LOCK — BROKEN (CABIN DOOR) · airframe 18,876 hrs · 10,784 cycles

GUST LOCK ON MAIN CABIN DOOR IS BROKEN. CLEANED AND INSPECTED GUST LOCK, OPS CHECK GOOD IAW EMB 170 MM 52-11-00.

Part: DOOR SEAL — DEFECTIVE (R1 DOOR) · airframe 18,709 hrs · 10,683 cycles

DOOR R2 SQUEALING NOISE DURING CLIMB AND CRUISE. REMOVED AND REPLACED R2 DOOR SEAL IAW EMB 170 MM 52-42-21.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,511 hrs · 10,552 cycles

MAJOR REPAIR - BIRD STRIKE DENT RT NOSE BETWEEN FR4-5 AND BELOW STR 10R AND STR 9R 9.5"X5.25"X0.3125" WITH CREASE ON FCS WITH OIL CANNING. REPAIRED DAMAGE PER ETD 2011-170-108532 REV D, STRIPPED PAINT IAW EMB 170 SRM 51-23-02, CUTOUT DAMAGED AREA PER ETD, INSPECTED AND PERFORMED HFEC TO RT SIDE CUTOUT, NO CRACK LIKE INDICATIONS NOTED, FABRICATED REPAIR DOUBLER AND FILLER, BACK DRILLED EXISTING HOLES AND DEVELOPED FIELD RIVET PATTERN AND DRILLED ONTO DOUBLER/FILLER.

Part: LATCH — LACK OF LUBE (L1 DOOR) · airframe 17,870 hrs · 10,137 cycles

L1 DOOR IS NOT LATCHING IN THE OPEN POSITION. LUBED DOOR OPEN LATCH, OPS CHECK GOOD IAW EMB 170 MM 52-11-00.

Part: FITTING — CORRODED (FUSELAGE) · airframe 17,833 hrs · 10,114 cycles

LEVEL 2 CORROSION SHEAR CLIP AT FR86 AND BETWEEN STR 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP IAW EMB 170 SRM 51-41-02.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 17,833 hrs · 10,114 cycles

CORROSION AROUND INBOARD DRAIN HOLD AFT OF ANTENNA DOUBLER AFT OF FR84 AND STR 28-29R. REPLACED DAMAGE IAW ETD 2011-170-104673 REV A.

Part: FITTING — CORRODED (FUSELAGE) · airframe 17,833 hrs · 10,114 cycles

LEVEL 2 CORROSION SHEAR CLIP AT FR87 BETWEEN 26R-27R. REMOVED AND REPLACED IAW EMB 170 SRM 51-41-01 AND 51-42-02.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 17,833 hrs · 10,114 cycles

LEVEL 2 CORROSION ON DOUBLER AROUND WASTE SERVICE DOOR BOX. REMOVED AND REPLACED DOUBLER IAW EMB 170 SRM 51-41-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 17,833 hrs · 10,114 cycles

LEVEL 2 CORROSION FR 89 SHEAR CLIP BETWEEN STR 26R-27R. REMOVED AND REPLACED SHEAR CLIP AT FR 89 BETWEEN STRINGERS 26R AND 27R IAW EMB 170 SRM 51-41-01 AND 51-41-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 17,833 hrs · 10,114 cycles

LEVEL 2 CORROSION FRAME 88 SHEAR CLIP BETWEEN STRINGER 25R-26R. REMOVED AND REPLACED SHEAR CLIP IAW EMB 170 SRM 51-41-01 AND 51-41-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 17,833 hrs · 10,114 cycles

LEVEL 2 CORROSION FRAME 89 SHEAR CLIP BETWEEN STRINGER 25R-26R. REMOVED AND REPLACED SHEAR CLIP IAW EMB 170 SRM 51-41-01 AND 51-41-02.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 17,833 hrs · 10,114 cycles

LEVEL 2 CORROSION BETWEEN FR 86-60 STR 25L-25R. REMOVED AND REPLACED WASTE BOX DOUBLER.

Part: FITTING — CORRODED (FUSELAGE) · airframe 17,833 hrs · 10,114 cycles

LEVEL 3 CORROSION AFT SIDE FRAME 85 BETWEEN STR 26R-27R SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIP IAW EMB 170 SRM 51-41-01 AND 51-41-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,833 hrs · 10,114 cycles

LEVEL 2 CORROSION AFT SIDE OF FR 84 BETWEEN STR 27R-28R SHEAR CLIP. REMOVED AND REPLACED RIVET, CLEANED AREA, ALODINE PRIME AND PAINTED IAW SRM 51-41-00, 51-23-00, 51-40-02, 51-12-00.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,833 hrs · 10,114 cycles

LEVEL 2 CORROSION AFT SIDE FRAME 85 BETWEEN STR 26R-27R SHEAR CLIP. REMOVED AND REPLACED IAW EMB 170 SRM 51-41-01, 51-41-02, 53-23-04, 51-30-00, 51-23-04, 51-23-06, 51-23-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,833 hrs · 10,114 cycles

LEVEL 2 CORROSION ON COCKPIT FLOOR SUPPORT BEHIND F/O'S SEAT TRACKS BETWEEN FR12-13. BLENDED CORROSION AND FABRICATED AND INSTALLED DOUBLER IAW ETD 2011-170-104468.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,833 hrs · 10,114 cycles

LEVEL 2 CORROSION WASTE SERVICE PANEL AFT INTERNAL SUPPORT. REMOVED AND INSTALLED NEW DOUBLER ON AFT SIDE OF WASTE SERVICE PANEL IAW EMB SRM 51-40-02 AND 51-43-02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,833 hrs · 10,114 cycles

LEVEL 2 CORROSION FWD CARGO DOOR CUTOUT LOWER HORIZONTAL BEAM (FRONT) ON DOME NUTS. REPLACED SILL PLATE IAW EMB 170 SRM 51-41-01.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,833 hrs · 10,114 cycles

LEVEL 2 CORROSION WATER SERVICE PANEL FWD INTERNAL SUPPORT. REMOVED AND REPLACED WITH NEW DOUBLER IAW EMB 170 SRM 51-40-02 AND 51-43-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,368 hrs · 6,791 cycles

RIGHT GUSSET AT FR90 FWD OF ELECTRONICS RACK AT AFT GALLEY LEVEL 2 CORROSION. FABRICATED AND INSTALLED NEW GUSSET IAW EMB IC 2009-170/00325.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,368 hrs · 6,791 cycles

LEVEL 2 CORROSION ON RT FLOORBEAM AT FR 88R. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-41-01 AND 51-43-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 12,368 hrs · 6,791 cycles

FLOORBEAM AT FRAME 17 TOP SURFACE HAS LEVEL 2 CORROSION I/B OF LEFT I/B SEAT TRACK. REPAIRED FLOORBEAM AT FR 17 IAW EMB ETD 2009-170/09795.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,368 hrs · 6,791 cycles

RIGHT I/B SEAT TRACK HAS SEVERAL AREAS OF CORROSION AT TOP SURFACE, FRAMES 13 TO 17. REMOVED AND REPLACED SEAT TRACK SUPPORT BEAM FROM FR 12R TO FR 20R IAW EMB 170 SRM 51-41-01, 51-43-01, 51-43-02, AND 51-43-03.

Part: FADEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 1,659 hrs · 605 cycles

FLT NR 6491 ORD TO SLC, ON DESCENT AUTO THROTTLES STARTED TO CREATE A SPLIT IN PWR SETTING. CREW CYCLED AUTO THROTTLES, WHEN RE-ENGAGED AUTO THROTTLE SPLIT REOCCURRED. CREW DISENGAGED AUTO THROTTLES AGAIN AND REALIZED THAT N1, FUEL AND N2 WERE ALL SURGING. WENT TO FLT IDLE ON NR 2 ENG AND N1 WAS SURGING FROM 25%-95% AND PROGRESSIVELY GOT WORSE AND MORE FREQUENT. NO EICAS MESSAGES PRESENT WHILE THIS WAS OCCURRING. CREW COMPLIED WITH QRH ENG 2 CONT FAULT CHECKLIST REQUIRING PRECAUTIONARY SHUTDOWN OF ENG, ENG OUT LANDING CHECKLIST AND DRIFT DOWN CHECK. CREW DECLARED AN EMERG AND LANDED WITH NO OCCURRENCES. MX REMOVED AND REPLACED FMU AND FADEC, PERFORMED GROUND RUNS, ALL LEAK CHECK AND ENG RUNS CHECK GOOD.

Part: SLIDE — DEPLOYED (CABIN)

EVACUATION SLIDE DEPLOYED A THE GATE. AIRCRAFT WAS FERRIED, WHERE THE SLIDE WAS REPLACED.