N864RW

Part: UNKNOWN — UNKNOWN · airframe 27,693 hrs · 45,289 cycles

EMERGENCY DECLARED. NO FURTHER INCIDENT. LG WOW SYSTEM FAILS ON TAKEOFF. ADJUSTED THE NLG WOW SENSOR CLEARANCE IAW AMM 32-62-01. PERFORMED LANDING GEAR SWINGS IAW AMM 32-33-00. THE OPS CHECK IS GOOD.

Part: SHEAR TIE — CORRODED (FRM 17 S21-22R) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

FWD FUSELAGE SHEAR CLIP FR 17 BTWN STR 21R AND 22R CORRODED. R&R IAW SRM 51-41-01 AND 51-41-02.

Part: SHEAR TIE — CORRODED (FRM 17 S20-21R) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

FWD FUSELAGE SHEAR CLIP FR 17 BTWN STR 20R AND 21R CORRODED. R&R IAW SRM 51-41-01 AND 51-41-02.

Part: SHEAR TIE — CORRODED (FRM 17 S23-24L) · airframe 45,238 hrs · 27,650 cycles

FWD FUSELAGE SHEAR CLIP FR 17 BTWN STR 23L AND 24L CORRODED. R&R IAW SRM 51-41-01 AND 51-41-02.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

CORROSION FOUND ON FWD FUSELAGE STRINGER 23R, BETWEEN FR 16 & 17. FWD FUSELAGE STR 23 REPLACED WITH NEW. STRINGER INSTALLED IAW WRM 51-41-01, SRM 51-41-02, AND SRM 51-43-01.

Part: SEAT TRACK — CORRODED (FRMS 84) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

CF III RH I/B SEAT TRACK AT FR 84 CORRODED. REPAIRED IAW SRM 53-23-10 REPAIR 64.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

FWD FLOOR CROSSBEAM UPPER FLANGE AT FR 17 AND RH I/B SEAT TRACK CORRODED. REPAIRED IAW SRM 53-00-10 REPAIR 03.

Part: SUPPORT ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

CF III RH O/B FLOOR BOARD SUPPORT ANGLE BTWN FR 88 AND 90 CORRODED. R&R IAW SRM 51-42-01.

Part: FLOOR SUPPORT — CORRODED (FRMS 12-14) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

FWD FUSELAGE FLOOR PAN BTWN FR12 AND 14, RH FWD R1 DOOR CUTOUT CORRODED. R&R IAW SRM 51-41-02 AND 51-43-04.

Part: SEAT TRACK — CORRODED (FRM 17) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

FWD FUSELAGE RH I/B SEAT TRACK AT FR 17. REPAIRED SEAT TRACK IAW SRM 53-10-10 REPAIR 01.

Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

CF III FLOOR STRUCTURE CENTER SHEAR PANEL FR 87 AND 88 CORRODED. R&R IAW SRM 51-42-01.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

CF 1 R/H I/B SEAT TRACK HAS CORROSION AT FR 22 + 3 INCHES. PERFORMED PERMANENT REPAIR ON CF1 RH I/B SEAT TRACK AT FR 22 IAW SRM 53-00-10, REPAIR 02.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

CORROSION ON CFIII LH INBD CABIN SEAT TRACK BETWEEN FR 83, AND FR84 FOUND TO BE OUT OF LIMITS. PERFROMED PERMANENT REPAIR ON CFIII LH INBD CABIN SEAT TRACK BETWEN FR 83 AND FR 84 IAW SRM 53-00-10 REPAIR 02.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

AFT LH I/B FUSELAGE FLOOR STRUCTURE GUSSET PLATE AT FR 90 CORRODED. R&R IAW SRM 51-41-02.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

AFT RH O/B FUSELAGE FLOOR STRUCTURE GUSSET PLATE AT FR 90 CORRODED. R&R IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FRM 17) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

FWD FUSELAGE RH I/B SEAT TRACK AT FR 17. REPAIRED SEAT TRACK IAW SRM 53-10-10 REPAIR 01.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

BL 0, CF III FLOOR STRUCTURE GUSSET PLATE AT FR 90 CORRODED. R&R IAW SRM 51-41-03.

Part: SHEAR PANEL — CORRODED (FRMS 87-88) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

CF III FLOOR RH SHEAR PNL BTWN FR 87 AND FR88 CORRODED. R&R IAW SRM 51-42-01, 51-42-02 AND 51-43-04.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

CORROSION ON CFIII RH INBD CABIN SEAT TRACK BETWEEN FR 83 AND FR 84 FOUND TO BE OUT OF LIMITS. PERFORMED PERMANENT REPAIR ON CRIII RH INBD CABIN SEAT TRACK BETWEEN FR 83 AND FR 84 IAW SRM 53-00-10 REPAIR 02.

Part: STRINGER CLIP — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

CORROSION FOUND ON CFIII STRINGER CLIP AT FR 87, STGR 19L. REPLACED CFIII STRINGER CLIP AT FR 87, STGR 19L, WITH NEW IAW SRM 51-41-01.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

CF 1 R/H I/B SEAT TRACK HAS CORROSION AT FR 22 + 3 INCHES. PERFORMED PERMANENT REPAIR ON CF1 RH I/B SEAT TRACK AT FR 22 IAW SRM 53-00-10, REPAIR 02.

Part: DOOR — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

CORROSION FOUND ON CFIII WASTE ACCESS DOOR OUTER SKIN. WASTE ACCESS DOOR REPLACED IAW AMM 20-10-01

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

CF III FLOOR UPPER SHEET BTWN FR 86 AND 87 AFT RH I/B SEAT TRACK CORRODED. R&R IAW SRM 51-41-01 AND 51-43-03.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

AFT OF RH I/B CABIN SEAT TRACK CF III FLOOR SUPPORT BEAM FR 88 AND 90 CORRODED. R&R IAW SRM 51-41-01 AND 51-43-03.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

AFT RH I/B FUSELAGE FLOOR STRUCTURE GUSSET PLATE AT FR 90 CORRODED. R&R IAW SRM 51-41-02.

Part: SHEAR TIE — CORRODED (FRM 82 S27-28R) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

CF III SHEAR TIE CLIP FR 82, BTWN STR 27R AND 28R CORRODED. R&R IAW SRM 51-41-02 AND 51-41-03.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

CF II RH I/B SEAT TRACK BTWN FR 43 AND 59 CORRODED.R&R IAW SRM 51-43-03 AND 51-43-04.

Part: ACCESS DOOR — CORRODED (FRM 88 S27-28R) · corrosion level 2 · airframe 45,238 hrs · 27,650 cycles

CF III EXTERNAL WASTE ACCESS DOOR CUTOUT INNER DOUBLER FR88, BTWN STR 27R AND 28R. R&R IAW SRM 51-41-02.

Part: BELLCRANK — DIRTY (L1 ARMING LEVER) · airframe 42,357 hrs · 25,632 cycles

L1 DOOR ARMING LEVER STICKING. CLEANED BELL CRANKS ON L1 DOOR, OPS CHECK GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 41,948 hrs · 25,363 cycles

EXIT SIGN ON FORWARD GALLEY NOT WORKING. RESECURED CONNECTOR. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-50-19.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 41,142 hrs · 24,868 cycles

DAMAGE TO AFT LOWER FUSALAGE BETWEEN FR 87 AND 88 AND BETWEEN STR 29L AND 26L, REF VP-040437-2020/NR2 C1-4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CORROSION FOUND AT L/H CENTRAL SEAT TRACK CROWN BTW FR 43-59 RBL 12. REPAIRED SEAT TRACK IAW SRM 53-00-10 REPAIR 02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** FWD CARGO, CORROSION FOUND ON SHEAR CLIP AT FR 17 BTW STR 26-27R. REPLACED SHEAR CLIP IAW SRM 51-41-01 AND 51-43-03. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** FWD CARGO, CORROSION FOUND ON SHEAR CLIP AT FR 17 BTW STR 22-23R. REPLACED SHEAR CLIP IAW SRM 51-41-02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CORROSION FOUND AT R/H CENTRAL SEAT TRACK CROWN BTW FR 43-59 RBL 12. REPAIRED SEAT TRACK IAW SRM 53-00-10 REPAIR 02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CORROSION FOUND ON SHEAR CLIP AT FR 81 BTW STR 24-25L. REPLACED SHEAR CLIP IAW SRM 51-41-01 AND 51-41-02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CF III, CORROSION FOUND ON MIDDLE SHEAR PANEL BTW FR 87-88 ANDS BTW RBL 12 AND LBL 12. REPLACED SHEAR PANEL IAW SRM 51-42-01 & 51-43-03. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CABIN FLOOR STRUCTURE, CORROSION FOUND AT R/H SHEAR PANEL BTW FR 87-88 ND BTW RBL 12-36. REPLACED SHEAR PANEL IAW SRM 51-42-01/02 & 51-43-03. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** AFT CARGO, CORROSION FOUND ON SHEAR CLIP AT FR 77M BTW STR 24-25L. REPLACED SHEAR CLIP IAW SRM 51-41-01 AND 51-41-02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CF III, CORROSION FOUND AT PANEL SUPPORT BTW FR 88-90, LBL 36. REPLACED PANEWL SUPPORT IAW SRM 51-41-01, 51-42-01 AND 51-43-03. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** AFT CARGO, CORROSION FOUND ON SHEAR CLIP AT FR 82 BTW STR 27-28L. REPLACED SHEAR CLIP IAW SRM 51-41-01 AND 51-41-02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: UPPER SHEET — CORRODED (FUSELAGE) · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CF III, CORROSION FOUND AT UPPER SHEET BTW FR 85-86 RBL 12. REPLACED UPPER SHEET IAW SRM 51-43-03 AND 51-41-01.***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** AFT CARGO, CORROSION FOUND ON SHEAR CLIP AT FR 83 BTW STR 27-28R. REPLACED SHEAR CLIP IAW SRM 51-41-01 AND 51-41-02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CF III, CORROSION FOUND ON SHEAR CLIP AT FR 85 BTW STR 27-28L. REPLACED SHEAR CLIP IAW SRM 51-43-03 AND 51-41-02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CF III, CORROSION FOUND ON SHEAR CLIP AT F 88 BTW STR 27-28R. REPLACED SHEAR CLIP IAW SRM 51-41-02 AND 51-43-03 ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CF III, CORROSION FOUND ON SHEAR CLIP AT FR 87 BTW STR 27-28R. REPLACED SHEAR CLIP IAW SRM 51-41-02 AND 51-43-03. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CF III, CORROSION FOUND ON SHEAR CLIP AT FR 90 BTW STR 23-25L. REPLACED SHEAR CLIP IAW SRM 51-41-01 AND 51-41-02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CORROSION FOUND ON SHEAR CLIP AT FR 83 BTW STR 19-20R./ REPLACED SHEAR CLIP IAW SRM 51-41-02 AND 51-43-03. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CF III, CORROSION FOUND ON SHEAR CLIP AT FR 86 BTW STR 27-28L. REPLACED SHEAR CLIP IAW SRM 51-41-02 AND 51-43-03. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CF III, CORROSION FOUND ON STRINGER 23L BTW FR 89-90. REPAIRED STRINGER IAW SRM 53-23-03 REP 6 AND ETD2020-170-011427. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** 2 CRACKED ANGLES ON FLOOR CROSSBEAM FR 12 FWD FACE AT BL 0 AND LBL 37. REPLACED ANGLES IAW SRM 51-41-01. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: RIB — CRACKED (HORIZ STAB) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CRACKS AT L/H AND R/H HORIZ. STAB RIBS 11 AND 12. REPLACED RIBS IAW 170EO-55-10-0004_1. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CF I, CORROSION FOUND ON SEAT TRACK BEAM BTW FR 20-43 AT RBL 11. REPLACED SEAT TRACK IAW SRM 51-43-03 AND 51-43-04. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CORROSION FOUND ON SEAT TRACK BEAM BTW FR 17-20 AND LBL 11. REPLACED SEAT TRACK IAW SRM 51-41-01, 51-41-02 AND 51-43-03. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CORROSION FOUND ON CABIN FLOOR STRUCTURE DOUBLER AT FR 16 AND LBL 14. REPLACED DOUBLER IAW SRM 51-41-02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** FWD CARGO, CORROSION FOUND ON SHEAR CLIP AT FR 17 BTW STR 25-26R. REPLACED SHEAR CLIP IAW SRM 51-41-02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CORROSION FOUND ON SEAT TRACK BEAM BTW FR 17-20, RBL 11. REPLACED SEAT TRACK IAW SRM 51-41-01,51-41-02, 51-43-03, AND 51-43-04. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,437 hrs · 24,377 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CORROSION FOUND ON SEAT TRACK CROWN BTWFR 29-43 AT LBL 11. REPAIRED SEAT TRACK IAW SRM 53-00-10 REP 01 AND ETD2020-170-011299. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,300 hrs · 23,086 cycles

MAJOR REPAIR: DAMAGE ON SKIN AND FASTENER AT FRAME 19 BETWEEN STRINGERS 22L AND 23L. REPAIRED DAMAGE IAW ETD2019-170-087516/A.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 37,071 hrs · 22,335 cycles

PHOTOLUMINESCENT STRIP IN FRONT OF FORWARD WARDROBE NOT GLOWING. R&R PHOTOLUMINESCENT STRIP IN FRONT OF FWD WARDROBE PER AMM 33-50-21.

Part: GIRT BAR — DISCONNECTED (R1 DOOR) · airframe 36,493 hrs · 21,981 cycles

R1 DOOR IS EXTREMELY HARD TO ARM AND DISARM. FERRIED TO IND. TROUBLESHOT AND FOUND GIRT BAR DISCONNECTED FROM AFT FRAME BELL CRANK ASSY CLIP. INSTALLED GIRT BAR INTO FRAME BELL CRANK ASSY CLIP OPERATION OF THE R1 DOOR ARM/DISARM GOOD REF AMM 25-65-01.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 34,643 hrs · 20,838 cycles

WHILE AC WAS OUT OF SERVICE FOR HEAVY CHECK, MAINTENANCE FOUND A CRACKED RIB ON THE RT STAB TIP PANEL 345AR. REMOVED AND REPLACED RIB IAW SRM 51-43-00 AND 51-40-03. AC REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: RIB — CORRODED (RT ELEVATOR) · airframe 34,634 hrs · 20,838 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, RT ELEVATOR OB MOST RIB IS CRACKED. RIB WAS REMOVED, REPLACED AND FABRICATED RIB IAW ETD 2018-170-020702 AND SRM 51-43-04 AND 51-42-01 . AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,634 hrs · 20,838 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND AT L2 AFT PASSENGER FLOORBEAM. BEAM WAS REMOVED AND A NEW BEAM WAS INSTALLED IAW SRM 51-42-03 AND 51-43-04. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: FUSE — FAILED (ZONE 100) · airframe 34,634 hrs · 20,838 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, EMERGENCY / PARKING BRAKE HYDRAULIC FUSE FOR NR 2 HYDRAULIC SYSTEM FAILED OPERATIONAL TEST. REMOVED AND REPLACED EMERGENCY FUSE IAW AMM 32-44-07. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: ACCESS PANEL — DENTED (ZONE 100) · airframe 34,643 hrs · 20,838 cycles

WHILE AC WAS OUT OF SERVICE FOR HEAVY CHECK, APU ACCESS PANEL 351GL WAS FOUND DENTED AT LEADING EDGE. PANEL WAS REPAIRED PER ETD 2018-170-018401. NO OTHER ACTION REQUIRED. AC REMAINS OUT OF SERVICE HEAVY CHECK COMPLETION.

Part: SPLICE PLATE — CORRODED (FRAMES 88-89) · corrosion level 2 · airframe 34,643 hrs · 20,838 cycles

CORROSION WAS FOUND ON THE SHEAR PANEL SPLICE PLATE BETWEEN FRAMES 88 - 89, RBL 35. THE SPLICE PLATE WAS REMOVED AND REPLACED IAW SRM 51-42-01.

Part: SPLICE PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 34,643 hrs · 20,838 cycles

CORROSION WAS FOUND ON THE SHEAR PANEL SPLICE PLATE BETWEEN FRAMES 87 - 88, LBL 40. THE SPLICE PLATE WAS REMOVED AND REPLACED IAW SRM 51-42-02, AND 51-40-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,634 hrs · 20,838 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND AT FRAME 87 BETWEEN STRINGERS 27R AND 28R. SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-41-02. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: FLOOR SUPPORT — CORRODED (FRAME 14) · corrosion level 2 · airframe 34,643 hrs · 20,838 cycles

CORROSION WAS FOUND ON THE FLOOR SUPPORT AT FRAME 14, RBL48. FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-75-16, AND 51-40-08.

Part: SPLICE PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 34,643 hrs · 20,838 cycles

CORROSION WAS FOUND ON THE SHEAR PANEL SPLICE PLATE BETWEEN FRAMES 87 - 88, RBL 40. THE SPLICE PLATE WAS REMOVED AND REPLACED IAW SRM 51-42-03 AND 51-40-02.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,643 hrs · 20,838 cycles

WHILE AC WAS OUT OF SERVICE FOR HEAVY CHECK, A SMALL DENT WAS DISCOVERED OB AND AFT OF WASTE SERVICE PANEL. DENT WAS REPAIRED PER EMB ETD 2018-170-018426. NO OTHER ACTION REQUIRED.AC REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: BOLT — MISSING (VGV ACTUATOR) · airframe 31,480 hrs · 18,822 cycles

DURING FLIGHT, CREW RECEIVED AN NR 1 ENGINE CONTROL FAULT MESSAGE. CREW NOTED THE NR 1 ENGINE WAS STUCK IN IDLE POWER SETTING. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE VG ACTUATOR BOLT MISSING, INSTALLED A NEW ONE IAW AMM AND OPS CHECKED GOOD.

Part: SHAFT — DAMAGED (L2 DOOR) · airframe 31,478 hrs · 18,820 cycles

MAINTENANCE REPORTED THAT THE L2 DOOR LATCH INDICATOR WAS NOT SHOWING GREEN WHEN DOOR WAS CLOSED. MAINTENANCE REMOVED AND REPLACED ROLLER DETECTOR SHAFT IAW AMM AND OPS CHECKED GOOD.

Part: STOP FITTING — DAMAGED (L1 DOOR) · airframe 30,868 hrs · 18,450 cycles

DURING FLIGHT, CREW REPORTED THAT THE L1 DOOR WAS NOISY. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE STOP FITTING IAW AMM AND OPS CHECKED GOOD.

Part: INDICATOR — DIRTY (L2 DOOR LATCH) · airframe 29,415 hrs · 17,524 cycles

L2 DOOR LATCH INDICATOR IS NOT GREEN WHEN DOOR IS CLOSED. REMOVED DEBRIS FROM L2 LATCH INDICATOR, OPS CHECK GOOD IAW AMM 52-12-25.

Part: DOUBLER — DENTED (ZONE 100) · airframe 29,307 hrs · 17,445 cycles

DOUBLER LISTED AS NR 2 IN DAMAGE LOG IS DENTED IN LOWER AFT CORNER. REMOVED, FABRICATED, AND INSTALLED NEW DOUBLER IAW ETD2016-170-013710 AND RECONTOURED DENT UNDER DOUBLER.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 29,307 hrs · 17,445 cycles

FOUND CORROSION ON FWD CARGO DOOR CUTOUT LOWER BEAM. R & R FWD CARGO CUTOUT LOWER BEAM IAW SRM 51-40-02, 51-41-00, AND 51-43-01 AND 02.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,307 hrs · 17,445 cycles

RIGHT HORIZONTAL STABILIZER, RIB 10 CRACKED TOP SIDE 6TH FASTENER FROM FRONT. REMOVED UPPER FWD CRACKED FLANGE AND FABRICATED AND INSTALLED SHEAR CLIP IAW ETD2016-170-012541.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,307 hrs · 17,445 cycles

RIGHT HORIZONTAL STABILIZER, RIB 11 CRACKED TOP SIDE 5TH FASTENER FROM FRONT. REMOVED UPPER FWD CRACKED FLANGE AND FABRICATED AND INSTALLED SHEAR CLIP IAW ETD2016-170-012541.

Part: SLIDE — ABNORMAL (L1 DOOR SLIDE) · airframe 29,280 hrs · 17,429 cycles

UNABLE TO DISARM L1 DOOR FULLY. R & R PARTIALLY DEPLOYED L1 DOOR SLIDE IAW S25-65-01-920-801A.

Part: WIRE HARNESS — DAMAGED (PAX DOOR) · airframe 28,641 hrs · 16,985 cycles

MAIN CABIN DOOR MFD INDICATION, UNCERTAIN WHEN DOOR OPEN. R & R FWD PAX DOOR WARNING SENSORS HARNESS IAW AMM 52-72-20. OPS CHECK OK.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 27,240 hrs · 15,987 cycles

DOOR L1 WILL NOT ARM. ADJUSTED L1 GIRT BAR, AMM 52-11-41.

Part: GIRT BAR — UNSECURE (L1 DOOR) · airframe 27,169 hrs · 15,943 cycles

L1 DOOR WILL NOT ARM FROM INSIDE. REATTACHED L1 SLIDE GIRT BAR IAW AMM 52-11-41. OPS CHECK GOOD.

Part: GIRT BAR — DISLODGED (L1 DOOR SLIDE) · airframe 27,112 hrs · 15,914 cycles

L1 DOOR WILL NOT ARM. LOOKS LIKE THE BAR ATTACHING THE DOOR AT THE BOTTOM OF THE DOOR HAS BECOME DISLODGED. RESECURED FORWARD PASSENGER DOOR GIRT BAR IAW AMM 52-11-41. OPS CHECK GOOD.

Part: GIRT BAR — UNSECURE (L1 DOOR) · airframe 26,975 hrs · 15,824 cycles

L1 DOOR WILL NOT ARM. RESECURED L1 GIRT BAR IAW AMM 52-11-41. OPS CHECK SATISFACTORY.

Part: LIGHT — DAMAGED (CABIN) · airframe 26,731 hrs · 15,680 cycles

FIRST TWO RT EMERGENCY LIGHT STRIPS DAMAGED. R & R THE EMERGENCY LIGHT IAW AMM 33-50-21.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 26,183 hrs · 15,365 cycles

L1 DOOR WILL NOT ARM. FOUND GIRT BAR OUT OF POSITION. REPOSITIONED GIRT BAR AND L1 DOOR OPS CHECKED GOOD IAW MM 52-70-00 AND 25-65-00.

Part: GIRT BAR — OUT OF ADJUST (PAX DOOR) · airframe 26,099 hrs · 15,317 cycles

MAIN CABIN DOOR WILL NOT ARM AFTER CLOSING. ADJUSTED GIRT BAR ON MAIN CABIN DOOR IAW AMM 52-11-41. OPS CHECKED GOOD.

Part: GIRT BAR — INOPERATIVE (L1 DOOR) · airframe 26,090 hrs · 15,309 cycles

L1 DOOR NOT ABLE TO ARM. R & R GIRT BAR IAW AMM 52-11-41. OPS CHECK NORMAL.

Part: GIRT BAR — UNSECURE (L1 DOOR SLIDE) · airframe 26,045 hrs · 15,282 cycles

L1 DOOR ARMING LEVER JAMMED IN DEARMED POSITION. INSPECTED, FOUND GIRT BAR UNSECURED. RESECURED GIRT BAR IAW AMM 52-11-41. OPS CHECKED GOOD.

Part: ROLLER — MISSING (L1 DOOR) · airframe 25,974 hrs · 15,238 cycles

ROLLER ON L1 DOOR LOCKING ACTUATOR MISSING. R & R ROLLER IAW AMM 52-11-52. OPS CHECKED GOOD.

Part: GIRT BAR — UNSECURE (L1 DOOR AREA) · airframe 25,045 hrs · 14,700 cycles

L1 DOOR WILL NOT ARM. FOUND GIRT BAR ON L1 DOOR TO BE UNSECURE. SECURED GIRT BAR IAW AMM 52-11-41. OPS CHECKED GOOD IAW AMM 52-11-20.

Part: VALVE — FAILED (NR 2 BLEED) · airframe 25,047 hrs · 14,702 cycles

NR 2 BLEED FAILED IN FLIGHT WHILE NR 1 BLEED, MOMENTARY DEPRESSURIZATION. DIVERTED. R & R NR 2 FAV IAW AMM 36-11-09, OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 24,935 hrs · 14,638 cycles

VERY STRONG MUSTY/BURNING OIL ODOR DURING TAKEOFF AND DESCENT. ODOR WAS NAUSEATING AND NOTICED IN CABIN AND COCKPIT. PERFORMED ENGINE RUNS REF AMM 71-00-01. COULD NOT DUPLICATE ODOR IN COCKPIT OR CABIN.

Part: O-RING — FAILED (HYD SYSTEM) · airframe 24,436 hrs · 14,356 cycles

DURING DESCENT, RECEIVED HYD 2 LOW QTY MESSAGE FOLLOWED BY HYD 2 LOW PRESSURE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R HYD SYS 2 MANIFOLD PRESSURE O-RING, HYD SYS 2 EDP, AND HYD 2 PRESSURE RETURN EDP CASE DRAIN FILTERS.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 23,853 hrs · 14,032 cycles

MAIN CABIN DOOR DIFFICULT TO CLOSE. LUBRICATED THE MAIN DOOR MECHANISM IAW AMM 52-11-00. OPS CHECK GOOD.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,447 hrs · 13,800 cycles

CORROSION ON RT PANEL SUPPORT AT FRAMES 83-84. R & R RT PANEL SUPPORT.

Part: INSERT — CORRODED (GIRT BAR) · corrosion level 2 · airframe 23,447 hrs · 13,800 cycles

CORROSION ON PAX FLOORBOARD 226BRF AFT GIRT BAR COVER PLATE INSERTS. R & R FLOORBOARD 226BRF.

Part: SPAR — CRACKED (RT WING) · airframe 23,447 hrs · 13,800 cycles

RT WING HAS A CRACK INDICATIONS IN SPAR 2. PERFORMED MAJOR REPAIR AT SPAR 2 AND RIB 10 IAW ETD 2013-170-065600, REV B AND AMEX A.

Part: JOINT — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,447 hrs · 13,800 cycles

CORROSION ON AFT GALLEY SPLIT JOINTS. REMOVED AND REPLACED SPLIT JOINT.

Part: FRAME — CORRODED (ZONE 100) · airframe 23,447 hrs · 13,800 cycles

CORROSION, PEELING BLISTER, SIZE OF 4-5 INCHES, ON FRAMES 87-88 AT SURFACE EDGE OF FRAME 87 ON LT SIDE OF BEAM, L2 DOOR SIDE. ALSO, FRAME 86 ON SUPPORT FLOORBOARD TAB ON LT SIDE IN L2 DOOR ARE SURFACE CORROSION. R & R LT SHEAR PLATE AT FRAMES 88-87 AND FLOOR SUPPORT ASSY AT FRAME 86.

Part: SEAT TRACK — CORRODED (FRAMES 13-15) · corrosion level 2 · airframe 23,447 hrs · 13,800 cycles

CORROSION ON RT FWD SEAT TRACK FRAMES 13-15. REMOVED FILLER AND DOUBLER.

Part: AXLE — CORRODED (NLG) · corrosion level 2 · airframe 23,447 hrs · 13,800 cycles

CORROSION, NLG WHEEL AXLE AT INTERFACE WITH SLIDING TUBE. R & R NLG SLIDING TUBE.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 23,447 hrs · 13,800 cycles

CORROSION ON RT SIDE OF SHEAR PANEL FRAMES 87-88 AROUND VARIOUS SCREW HOLES AND RIVETS IN R2 DOOR AREA. R & R SHEAR PANEL.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,447 hrs · 13,800 cycles

CORROSION ON RT SEAT TRACK AT ROW 23CD. R & R SEAT TRACK.

Part: ACCESS PANEL — CORRODED (ZONE 100) · airframe 23,447 hrs · 13,800 cycles

CORROSION ON WASTE DISPOSAL ACCESS PANEL. R & R WASTE PANEL.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 21,784 hrs · 12,774 cycles

WHEN FLAPS 1 CALLED FOR VISUAL APPROACH, FLAP FAIL EICAS MESSAGE APPEARED. FOLLOWED QRH, EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. MAINTENANCE RETRACTED FLAPS TO 0 AND PERFORMED ELECTRICAL RIG ON FLAPS IAW AMM 27-50-00. OPS CHECKED FLAPS MULTIPLE TIMES ON GROUND, NO DEFECTS NOTED IAW AMM 27-50-00.

Part: INDICATOR — INOPERATIVE (GIRT BAR) · airframe 21,597 hrs · 12,654 cycles

L1 DOOR GIRT BAR VISUAL INDICATION INOPERATIVE. SECURED L1 DOOR GIRT BAR INDICATOR IAW AMM 52-11-22, OPS CHECKED GOOD.

Part: HYDRAULIC LINE — FAILED (HYDRAULIC SYS) · airframe 20,294 hrs · 11,864 cycles

HYD 2 FAILURE, RETURNED TO FIELD, DECLARED EMERGENCY. REMOVED AND REPLACED HYDRAULIC LINE FROM E2 ENGINE TO PYLON, LEAK AND OPS CHECK GOOD IAW GE MM 72-00-0. ALSO REMOVED AND REPLACED NR 2 EDP AND CLAMP.

Part: FITTING — OUT OF POSITION (L1 DOOR) · airframe 20,197 hrs · 11,795 cycles

L1 DOOR ESCAPE SLIDE HANDLE IS STUCK, CANNOT ENGAGE SLIDE. RE-INSTALLED FORWARD GIRT BAR CLIP, OPS CHECK GOOD IAW AMM 52-11-20.

Part: PIN — OUT OF POSITION (EVAC SLIDE) · airframe 19,303 hrs · 11,272 cycles

AFTER CLOSING MAIN CABIN DOOR GROUND CREW REPORTED SOMETHING STICKING OUT OF BOTTOM OF DOOR. UPON INSPECTION FOUND A PIN ATTACHED TO A ROPE HANGING FROM ESCAPE SLIDE. FOUND L1 DOOR BUSTLE PIN UNSECURED, REINSTALLED BUSTLE PIN PER AMM 25-65-01 SUBTASK 420-002-A PARAGRAPH (5) TASK (A).

Part: PIN — UNSECURE (L1 DOOR) · airframe 19,207 hrs · 11,193 cycles

L1 DOOR DIFFICULT TO CLOSE, HANDLE BINDS AROUND 3/4 WAY DOWN. INSPECTED AND FOUND BUSTLE PIN HANGING IN DOORWAY OBSTRUCTING DOOR MOVEMENT. RESTOWED PIN, OPS CHECK GOOD IAW EMB 170 AMM.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 19,193 hrs · 11,185 cycles

L1 DOOR HARD TO CLOSE AND ARM. FOUND GIRT BAR OUT OF HOLES, RE-INSTALLED PER EMB 170 MM 52-13-41. ARM OPERATION NORMAL, OPS CHECK GOOD IAW EMB 170 MM 52-11-20.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,554 hrs · 10,158 cycles

MAJOR REPAIR - CTR SEAL REST LEVEL 2 CORROSION ON FWD CARGO DOOR LOWER BEAM. REMOVED CORRODED SEAL REST AND INSTALLED NEW SEAL REST IAW EMB 170 SRM 51-40-02, 51-41-01, AND 51-21-00.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,554 hrs · 10,158 cycles

LEVEL 2 CORROSION FR90 IN AFT WET AREA, OUTBOARD LT AND RT AREAS. REMOVED AND REPLACED RT GUSSET AT FR90 AND CLEANED AND RESTORED TOP COAT AT ALL OTHER AREAS ON FR90 IAW SRM 51-41-02 AND 51-23-06.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,554 hrs · 10,158 cycles

LEVEL 2 CORROSION AFT WET AREA RT BEAM, CORRODED 6 INCHES AFT OF FRAM 86. REMOVED AND REPLACED BEAM IAW EMB 170 SRM 51-43-01 AND 51-41-01.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,554 hrs · 10,158 cycles

LEVEL 2 CORROSION LT AFT WET AREA BETWEEN FR85 AND 86. REMOVED AND REPLACED UPPER SHEET IAW EMB 170 SRM 51-41-01 AND 51-43-02.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,554 hrs · 10,158 cycles

LEVEL 2 CORROSION AFT WET AREA WEBBINGS, LEFT, RIGHT, AND CENTER PORTIONS AND AROUND BOLT HOLES. REMOVED AND REPLACED RIGHT AND CENTER SHEAR PANELS, RESTORED TOP COAT ON LEFT SHEAR PANELS IAW EMB 170 SRM 51-41-01, 51-42-01, AND 51-43-03.

Part: SKIN — DENTED (FUSELAGE) · airframe 17,554 hrs · 10,158 cycles

MAJOR REPAIR - FOUR DENTS BETWEEN FR9-11 JUST ABOVE STR 17L. REMOVED PAINT FROM AREA IAW EMB 170 SRM 51-23-02, RECONTOURED SKIN AT FR10L, FOUND SKIN OIL CANNING. CUT AND REMOVED DAMAGED AREA IAW EMB 170 SRM 53-10-01 ABD 51-75-12. PERFORMED HFEC, NO CRACKLIKE INDICATIONS NOTED IAW EMB 170 NDT MANUAL. FABRICATED DOUBLER AND FILLER AND INSTALLED IAW EMB 170 SRM 51-41-02, EDGE SEALED AND PAINTED, AND PERFORMED HFEC AGAIN IAW EMB 170 NDT MANUAL, NO CRACKLIKE DAMAGE NOTED.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,554 hrs · 10,158 cycles

LEVEL 2 CORROSION AROUND SEVERAL AREAS OF LT SHEAR WEB. REMOVED AND REPLACED SHEAR WEB IAW EMB 170 SRM 51-43-04, 51-46-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,554 hrs · 10,158 cycles

LEVEL 2 CORROSION ON FLOORBEAM AT LT FR17. REMOVED AND REPLACED FLOORBEAM IAW EMB 170 SRM 51-41-01 AND 51-43-01.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,554 hrs · 10,158 cycles

LEVEL 2 CORROSION AROUND FASTENER HOLES ON FWD GALLEY RT SHEAR WEB (FWD OF R1 DOOR). REMOVED AND REPLACED SHEAR WEB FWD OF R1 DOOR IAW EMB 170 SRM 51-40-02, 51-41-02, 51-41-02, 51-42-02, 51-43-02, AND 51-43-04.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,554 hrs · 10,158 cycles

LEVEL 2 CORROSION AT RT FLOORBEAM BETWEEN FR12-13. REMOVED AND REPLACED FLOORBEAM IAW EMB 170 SRM 51-41-01, 51-41-02, 51-43-01, AND 51-43-02.

Part: POWER UNIT — INOPERATIVE (CABIN) · airframe 16,635 hrs · 9,534 cycles

EMERGENCY LIGHT ABOVE ROW 9 INOP. FOUND EMERGENCY LIGHT POWER UNIT IN RT AFT FUSELAGE INOP. REMOVED AND REPLACED RT AFT EMERGENCY LIGHT POWER UNIT IAW EMB 170 MM 33-50-01. OPS CHECK NORMAL.

Part: SHAFT — OBSTRUCTED (R2 DOOR) · airframe 14,942 hrs · 8,515 cycles

R2 DOOR DIFFICULT TO ARM/DISARM. F/A STATES IT FEELS LIKE IT'S HANGING UP WHEN MOVING LEVERS. UPON INSPECTION OF LINKS AND RODS, REMOVED DEBRIS AND LUBRICATED CONNECTING ROD CABLE SHAFT ON ARM/DISARM LINK TO GIRT BAR AS REQUIRED. OPS CHECK GOOD.

Part: BUSHING — CRACKED (THRUST REVERSER)

PROBLEM FOUND ON AIRCELLE THRUST REVERSER REMOVED FROM ACFT, UPON PRELIMINARY INSPECTION AT APPLIED COMPOSITES ENGINEERING (ACE) IT WAS DISCOVERED THAT THE FWD HINGE BUSHING P/N 14G0311-203 WAS CRACKED ACROSS THE SHOULDER AND AROUND THE TRANSITION FROM THE RADIAL TO THE FLANGE ON THE OUTSIDE OF THE BUSHING.PHOTOGRAPHS OF THE BUSHING ARE ON FILE AT THE REPAIR STATION.

Part: TRIPLER — DAMAGED (FUSELAGE) · airframe 11,867 hrs · 6,699 cycles

MAJOR REPAIR - PREVIOUS REPAIR OF DENT BETWEEN FR24 AND FR25 AND STR 18L AND STR 19L HAS TOOLING MARKS ON TRIPLER AND RII NOT PERFORMED ON ORIGINAL REPAIR. REMOVED ORIGINAL REPAIR DOUBLERS IAW EMB 170 SRM 53-21-01 AND 51-41-02. HFEC OF DAMAGE CUT OUT IAW NDTM 51-00-00. REVEALED NO CRACK LIKE INDICATIONS OF DAMAGE REMOVED. INSTALLED ORIGINAL DOUBLER IAW EMB 170 SRM 51-41-03. MANUFACTURED NEW TRIPLER FROM 2024-T3 .050 IAW EMB 170 SRM 53-21-01. ALODINED AND PRIMED TRIPLER IAW EMB 170 SRM 51-23-04/05. INSTALLED TRIPLER IAW EMB 170 SRM 53-21-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 11,867 hrs · 6,699 cycles

DENT ON LT CTR FUSELAGE I APPROX 12 INCHES BELOW 'U' IN 'OPERATED BY SHUTTLE AMERICA' LOGO. DENT IS 1.75L X 1.5W X .085D. DENT IS BETWEEN FR24 AND FR25 AND BETWEEN STR 18L AND STR 19L. MANUFACTURED NEW TRIPLER FROM 2024-T3 .050 IAW EMB SRM 53-21-01. ALODINED AND PRIMED TRIPLER IAW EMB 170 SRM 51-23-04 AND 51-23-05. INSTALLED TRIPLER IAW EMB 170 SRM 53-21-01. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,867 hrs · 6,699 cycles

LEVEL 2 CORROSION LEFT FWD SEAT TRACK, 37 IN BACK, 54 IN, 64 IN BACK. PERFORMED REPAIR IAW EMB ETD 2010-170/01383. NDT PERFORMED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,867 hrs · 6,699 cycles

LEVEL 2 CORROSION RIGHT FWD SEAT TRACK BEAM, 23, 33, 41, 47, AND 54 INCHES AFT ON BEAM. REMOVED AND REPLACED RIGHT FWD SEAT TRACK IAW EMB SRM 51-41-02.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,867 hrs · 6,699 cycles

LEVEL 2 CORROSION ON RT SHEAR PLATE BETWEEN FR 87 AND FR 88. REMOVED AND REPLACED RT SHEAR PLATE IAW EMB SRM 51-42-01 AND 51-43-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,867 hrs · 6,699 cycles

LEVEL 2 CORROSION LT SEAT TRACK BEAM CORROSION AT FR 90 GUSSET. REMOVED AND REPLACED GUSSET IAW EMB 170 SRM 51-40-02 AND 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,867 hrs · 6,699 cycles

LEVEL 2 CORROSION RT SEAT TRACK BEAM, BETWEEN FR 84 AND 87. REMOVED AND REPLACED UPPER SHEET OF SEAT TRACK BEAM PER EMB 170 SRM 51-40-02 AND INSTALLED PER EMB 170 SRM 51-41-01.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,867 hrs · 6,699 cycles

LEVEL 2 CORROSION LT SIDE OF LT SHEAR PLATE CORRODED BETWEEN FR 87 AND FR 88. REMOVED AND REPLACED SPLICE IAW EMB 170 SRM 51-40-02 AND 51-42-01.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,867 hrs · 6,699 cycles

LEVEL 2 CORROSION LT SHEAR PLATE BETWEEN FR 87 AND FR 88 IN AFT LAV/GALLEY AREA. REMOVED AND REPLACED LT SHEAR PLATE IAW EMB 170 SRM 51-31-00, 51-40-02, 51-43-01 AND 51-42-01.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,867 hrs · 6,699 cycles

LEVEL 2 CORROSION WASTE TANK HOLD DOWN GUSSET AT FR 90. REMOVED AND FABRICATED NEW GUSSET PER EMB 170 SRM 51-31-00 AND EMB 170 SRM 51-41-01.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,867 hrs · 6,699 cycles

LEVEL 2 CORROSION RT FLOORBEAM GUSSET, FWD OF AFT AVIONICS RACKS AT FR 90. REMOVED AND REPLACED GUSSET PER EMB 170 SRM 51-41-01.

Part: BEAM — CRACKED (NLG) · airframe 11,867 hrs · 6,699 cycles

CRACK FOUND ON NLG I-BEAM, ON FWD SIDE OF I-BEAM, SHOWN IN FIG 2 OF SE531012. REMOVED DAMAGED I-BEAM ASSY PER EMB SRM 51-43-03. INSTALLED I-BEAM PER EMB SRM 51-43-03.

Part: BEAM — CRACKED (NLG) · airframe 11,867 hrs · 6,699 cycles

MAJOR REPAIR - CRACK FOUND ON NLG I-BEAM ON FWD SIDE OF I-BEAM. REMOVED DAMAGED I-BEAM AND INSTALLED SERVICEABLE UNIT PER EMB IC2008-170/08207 AND SB 170-53-0055.

Part: ACTUATOR — FAILED (TE FLAP) · airframe 10,766 hrs · 6,063 cycles

DURING APPROACH SELECTED FLAPS 1 AND RECEIVED `FLAP FAIL` EICAS MESSAGE. RAN QRH FOR NO FLAPS AND SLATS 3. DECLARED EMERGENCY. LANDED WITH 0 FLAPS. MAINTENANCE RELEASED ELECTRONIC BRAKE, CLEARED INHIBITS, AND OPS CHECKED GOOD. SI275042 WAS COMPLIED WITH 10/15/09 TO REPLACE THE 4R ACTUATOR.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 10,331 hrs · 5,773 cycles

AT CRUISE FL370, THE AUTO PILOT FAILED WITH THE ASSOCIATED A/P FAIL CAUTION EICAS MESSAGE. ABOUT 3-4 SECONDS LATER THE SHAKER ANTICIPATED EICAS CAUTION APPEARED AND THE SHAKER BEGAN TO ENGAGE. ATC WAS NOTIFIED OF THE FAILURE, DESCENDED TO FL280. RAN QRH PROCEDURE ON EAP 3-5 AND GRADUALLY SLOWED TO .50 MACH WHILE CONTINUING DESCENT TO FL250. THE STALL SHAKER CONTINUED TO ENGAGE ON AND OFF THROUGHOUT THE DESCENT BUT STOPPED AS ACFT DESCENDED BELOW 9000 FT. LANDED WITHOUT INCIDENT. ONCE ON THE GROUND, MULTIPLE AUTO FLIGHT RELATED EICAS MESSAGES APPEARED. NO EMERGENCY WAS DECLARED. MAINTENANCE RESET A/C POWER, PERFORMED TEST OF AIOP B1. ALL OPS CHECK GOOD IAW EMB 170 FIM 22-10-00-810-82.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 10,149 hrs · 5,667 cycles

AFTER FLIGHT ATTENDANT TESTED EMERGENCY LIGHTS, LIGHTS WOULD NOT TURN OFF. RECEIVED EMER LT BATT FAULT ON EICAS. UPON MAINTENANCE ARRIVAL TO AIRCRAFT, FOUND EMERGENCY LIGHTS IN CHARGING CYCLE. FAULTS CLEARED AND SYSTEM CHECKED NORMAL IAW EMB 170 MM 33-50-00.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 8,181 hrs · 4,402 cycles

FLIGHT 5952 ATL-HPN ON FINAL APPROACH WITH GEAR DOWN AND FLAPS AT NR 5 POS, NR 2 ENG SPOOLED UP TO 80% UN-COMMANDED. CREW SHOT MISSED APPROACH. ON SECOND APPROACH AND SAME THING HAPPENED. CREW SHUT DOWN ENGINE. CREW DID NOT RECEIVE ANY MESSAGES IN AIR OR ON GROUND. MAINTENANCE INSPECTED ENGINE, VG ACTUATORS AND SHAFTS, NO CHECKED HISTORY. RAN ENGINES, COULD NOT DUPLICATE.

Part: WARNING LIGHT — ILLUMINATED (BLEED SYS) · airframe 1,679 hrs · 644 cycles

FLIGHT 6453 LGA TO DFW ON CLIMB OUT CREW RECEIVED "BLEED 1 OVERPRESSURE" EICAS AMBER MESSAGE FOLLOWED BY "BLEED 1 LEAK" MESSAGE AND BLEED 1 BUTTON AMBER ILLUMINATION. CREW FOLLOWED QRH, AND DIVERT TO IAD. MTX VERIFIED NO ACTUAL LEAK THROUGH CMC. ONLY INDICATION FROM OVERPRESSURE. NR 1 BLEED OPS CHECKED GOOD. DISCREPANCY HAS NOT REPEATED.

Part: SENSOR — FAULTY (CARGO DOOR) · airframe 1,379 hrs · 501 cycles

FLIGHT 6445 AUS TO SLC CREW RECEIVED A MASTER WARNING OF AFT CARGO DOOR OPEN, ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED THE DOOR, DETERMINED DOOR SENSOR TO BE FAULTY. MEL THE DOOR INDICATION AND DEPARTED WITH NO FURTHER INCIDENT. NO PARTS HAVE BEEN CHANGED TO DATE. THE SENSOR HAS BEEN ADJUSTED AND CLEANED. ENGINEERING HAS GENERATED AN EI TO INSPECT THE WIRE HARNESS AND REPLACE THE DOOR PROX SENSOR.