N655RW

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 48,541 hrs · 30,804 cycles

.CRACK FOUND ON LH BEAM W CLIPNUT HOLE AT FR47 & 49. REPAIRED IAW ETD2024-170-02035

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,451 hrs · 30,804 cycles

FWD CARGO INTERNAL PLATE AT FR23 TO FR24 BETWEEN STR20R AND 21R HAS CORROSION. REPLACED PLATE IAW SRM 51-43-03

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,451 hrs · 30,804 cycles

INBD RH SEAT TRACK FR17 DOUBLER OF REPAIR HAS CORROSION. REPLACED DOUBLER IAW SRM 51-41-02, 51-43-04 AND 53-10-10

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 48,451 hrs · 30,804 cycles

LH OUTBOARD SEAT TRACK AT FR84 HAS CRACKED GUSSET. GUSSET REPLACED IAW SRM 51-43-03

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,541 hrs · 30,804 cycles

FWD CABIN WET AREA INBD LH SEAT TRACK FR19 REPAIR DOUBLER HAS CORROSION. REPLACED DOUBLER IAW SRM 51-41-02, 51-43-04 AND 53-10-10

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,541 hrs · 30,804 cycles

CORROSION FOUND ON AFT CARGO FLOOR SUPPORT SHEAR CLIPAT FR77 S29R. REPLACED SHEAR CLIP IAW SRM 51-41-01 AND 51-41-02

Part: SHEAR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,541 hrs · 30,804 cycles

CORROSION FOUND AT AFT WET AREA SHEAR WEB FLOOR FR87-88 AND LBL11-45. REPLACED SHEAR CLIP IAW SRM 51-42-01 AND 51-42-02

Part: ANCHOR FITTING — CORRODED (L2 GIRT BAR) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

CORROSION AT ANCHOR NUT SUPP PLATE L2 DOOR, FWD GIRT BAR, AFT SUPP PLATE. R&R IAW SRM 51-41-01 & 51-41-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

L/H AFT SEAT TRACK BTWN FR 74 - 84 CORRODED OUT OF LIMITS. R&R IAW SRM 51-41-01, 51-43-01 & 51-43-02.

Part: ANCHOR FITTING — CORRODED (L2 GIRT BAR) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

CORROSION AT ANCHOR NUT SUPP PLATE L2 DOOR, AFT GIRT BAR, AFT SUPP PLATE. R&R IAW SRM 51-41-01 & 51-41-02.

Part: THRESHOLD — CORRODED (L2 DOOR AREA) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

L2 LOWER THRESHOLD FOUND FURTHER CORRODED TO PREVIOUS BLENDS. CORRODED L2 LOWER THRESHOLD REMOVED AND REPLACED IAW EMB SRM 51-41-01, 51-41-02, 51-43-01 AND 51-43-02.

Part: INTERCOSTAL — CORRODED (FRMS 90-91) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

AFT WET AREA , LONG INTERCOSTAL BETWEEN FR 90-91 ADJACENT TO BATTERY / AVIONICS RACK AND SUPPORT BRACKET FOUND CORRODED. INTERCOSTAL BETWEEN FR 90-91 REPLACED IAW SRM 51-41-01, 51-41-02 AND 51-43-04.

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

AFT WET AREA, LONG INTERCOSTAL BTWN FR 90-91 ADJANCENT TO BATT/AVI RACK SUPP BRKT.CORRODED. R&R IAW SRM 51-41-02, 51-43-04.

Part: ANCHOR FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

FWD CARGO DOOR SORROUND ANCHOR NUT BRKT BOTTOM SILL BTWN FR 24 - 25 STR 25R CORRODED. R&R IAW SRM 51-45-00.

Part: SUPPORT FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

FWD CARGO SUPP FRAME CORRODED. R&R IAW SRM 51-41-01.

Part: SHEAR TIE — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

SHEAR TIE AT FR 16 BTWN STRN 27L - 26L CORRODED. R&R IAW SRM 51-41-02 & 51-43-03.

Part: SHEAR TIE — CORRODED (FRM 17 S26-27L) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

SHEAR TIE CORRODED AT FR 17, BTWN STRN 26L & 27L. R&R IAW SRM 51-41-01 & 51-41-02.

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

INTERCOSTAL AT FR 17 STR 23R CORRODED. R7R IAW SRM 51-41-01 & 51-41-02.

Part: BEAM — CORRODED (FRMS 86-89) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

L/H BEAM BTWN FR 86 - 89 CORRODED. R&R IAE SRM 51-41-01 & 51-43-01.

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

L/H UPPER SHEET BTWN FR 85 - 86 CORRODED. R&R IAW SRM 51-41-01 & 51-43-01.

Part: SHEAR WEB — CORRODED (FRMS 87-88) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

R/H SHEAR WEB BTWN FR 87 - 88 CORRODED. R&R IAW SRM 51-42-01.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

L1 DOOR FLOOR BOARD SUPP FWD OF FR 12 - 16 CORRODED AT FR 16. R&R IAW SRM 51-41-02 & 51-43-02.

Part: GUSSET — CORRODED (FRM 90) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

R/H O/B GUSSET FOUND CORRODED AT FR 90. R&R IAW SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

L1 DOOR FLOOR SUPPORT FWD OF FR 12 - 16 CORRODED AT FR 16. R&R IAW SRM 51-41-02 & 51-43-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

FWD R/H SEAT TRACK DOUBLER AT FR 14 CORRODED. R&R IAW SRM 53-10-10 / REPAIR.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

SHEAR WEB AFT OF L1 DOOR CORRODED. R&R IAW SRM 51-41-02 & 51-43-02.

Part: SHEAR WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

FWD R1 DOOR SHEAR WEB BTWN FR 12 - 14 CORRODED. R&R IAW SRM 51-41-02 & 51-43-01.

Part: GUSSET — CORRODED (FRM 90) · corrosion level 2 · airframe 45,783 hrs · 28,596 cycles

R/H I/B GUSSET FR 90 CORRODED. R&R IAW SRM 51-41-02.

Part: SENSOR — OUT OF ADJUST (R1 DOOR) · airframe 41,228 hrs · 25,509 cycles

SUPPLEMENTAL INFORMATION: R1 DOOR INDICATION INTERMITTENT IN FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. ADJUSTED R1 DOOR SENSOR PER AMM 52-72-00. OPS CHECK GOOD.

Part: SUPPORT ANGLE — CORRODED (FRAME 80) · corrosion level 2 · airframe 39,828 hrs · 24,674 cycles

AFT CARGO DOOR CUTOUT STRUCTURE FRAME 80 STRINGERS 25-26R, ANGLE SUPPORT FOUND CORRODED. REPLACED THE SUPPORT ANGLE IAW SRM 51-41-02 & 51-43-03.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,828 hrs · 24,674 cycles

***WHILE A/C WAS OUT OF SERVICE FOR HEAVY CHECK*** FWD FUSELAGE LOWER STRUCTURE FR17 STGR27-28R, SHEAR CLIP FOUND CORRODED. REMOVED AND REPLACED SHEAR CLIP AT FR17 STGR27-28R IAW SRM 51-41-01 & 51-41-02. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 39,828 hrs · 24,674 cycles

FWD FUSELAGE LOWER FRAME 16, STRINGERS 27-28R SHEAR TIE FOUND CORRODED. REPLACED THE SHEAR TIE IAW SRM 51-41-02 & 51-43-03.

Part: CABLE — WORN (FRAME 9-56) · airframe 39,828 hrs · 24,674 cycles

MLG EMERGENCY EXTENSION SYSTEM CLOSED LOOP CONTROL CABLES (MAIN & RETURN) WORN. REPLACED MAIN (PN 170-71348-401) AND RETURN (PN 170-71349-401) MLG EMERGENCY SYST CLOSED LOOP CABLES IAW AMM TASK 32-44-09-400-801-A, ADJUSTMENT CARRIED OUT IAW AMM TASK 32-34-09-820-801-A/500. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SEAT TRACK — CORRODED (FRAMES 18-20) · corrosion level 2 · airframe 39,828 hrs · 24,674 cycles

FWD FUSELAGE FLOOR STRUCTURE FR19 LBL11" LH SEAT TRACK UPPER FLANGE FOUND CORRODED. FWD FUSELAGE FLOOR SWTRUCTURE FR19 LBL11" SEAT TRACK UPPER FLANGE REPAIRED IAW SRM 53-10-10 REPAIR 1.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,828 hrs · 24,674 cycles

MAINTENANCE FOUND CORROSION AT FWD FUSELAGE LOWER STRUCTURE SHEAR TIE AT FRAME 17, STRINGERS 27-28R. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-41-01, AND 51-41-02.

Part: ANGLE — CRACKED (FRAME 12) · airframe 39,828 hrs · 24,674 cycles

COCKPIT FLOOR STRUCTURE FR12 LBL36" ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE AT FR12 LBL36" IAW SRM 51-41-01.

Part: FLOORBEAM — CRACKED (FRAMES 12) · airframe 39,828 hrs · 24,674 cycles

COCKPIT FLOOR STRUCTURE FR12 CROSSBEAM BL0, ANGLE FOUND CRACKED. REMOVED AND REPLACED ANGLE IAW ON COCKPIT FLOOR STRUCTURE AT FR12 BL0 IAW SRM 51-41-01.

Part: SKIN — GOUGED (RT WING SLAT) · airframe 39,828 hrs · 24,674 cycles

RH WING LEADING EDGE GOUGED NEAR SLAT TRACK #8, L/E RIBS 32-34. GOUGE FOUND TO BE OUT OF LIMITS IAW SRM 57-49-01 AD01, REPAIRED AREA IAW SRM 57-49-01.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,828 hrs · 24,674 cycles

***WHILE A/C WAS OUT OF SERVICE FOR HEAVY CHECK*** CF III LOWER STRUCTURE FR88 STGR27-28R, SHEAR CLIP FOUND CORRODED. CF III LOWER STRUCTURE FR88 STGR27-28R, SHEAR CLIP REPLACED IAW SRM 51-41-01 & 51-41-02. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: RIVET — ABNORMAL (FRAMES 96-97) · airframe 39,828 hrs · 24,674 cycles

MAINTENANCE FOUND A PROTRUDING RIVET AT REAR FUSELAGE LOWER EXTERNAL SKIN BETWEEN FRAMES 96-97, STRINGERS 21R TO 23R. THE RIVET WAS REMOVED AND REPLACED IAW SRM 53-30-01, ALLOWABLE DAMAGE 03, PARA 6 (A).

Part: SKIN — CORRODED (FRAMES 97-98) · corrosion level 2 · airframe 39,828 hrs · 24,674 cycles

MAJOR - REAR FUSELAGE LOWER EXTERNAL SKIN FR97-98 STR29L-28R, DATA PLATE AREA CORROSION FOUND. ACCOMPLISHED PERMANENT REPAIR ON REAR FUSELAGE SKIN FR97-98 STGR29L-28R IAW ETD2019-170-130281. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 39,828 hrs · 24,674 cycles

RH HORIZONTAL STAB CRACK FOUND ON RIB 10 UPPER SECTION, BTWN FRONT SPAR AND MID SPAR. REMOVED AND REPLACED IAW 170EO-55-10-0004 REV 1.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 39,828 hrs · 24,674 cycles

RH HORIZONTAL STAB CRACK FOUND ON RIB 12 UPPER SECTION, BTWN FRONT SPAR AND MID SPAR. REMOVED AND REPLACED IAW 170EO-55-10-0004 REV 1.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 39,828 hrs · 24,674 cycles

RH HORIZONTAL STAB CRACK FOUND ON RIB 11 UPPER SECTION, BTWN FRONT SPAR AND MID SPAR. REMOVED AND REPLACED IAW 170EO-55-10-0004 REV 1.

Part: POWER UNIT — FAILED (CABIN) · airframe 39,828 hrs · 24,674 cycles

EMERGENCY LIGHT POWER UNIT (ELPU)#2 FAILED 15 FUNCTIONAL TEST. REMOVED AND REPLACED ELPU #2 IAW 33-50-01-400-801-A. OPS CHECKED GOOD. SEE 40000653-7000-0003 AWS FOR TESTING INFO.

Part: ROD — OUT OF ADJUST (R2 DOOR VENT) · airframe 35,349 hrs · 21,939 cycles

R2 DOOR VENT FLAP ARMING LEVER HARD TO MOVE. PERFORMED ADJUSTMENT OF R2 DOOR VENT FLAP ROD IAW AMM 52-42-25.

Part: BELLCRANK — DAMAGED (R2 DOOR) · airframe 34,721 hrs · 21,569 cycles

R2 DOOR HARD TO ARM. FOUND FORWARD BELL CRANK TO HAVE A SMALL BURR CAUSING INTERFERENCE DURING ACTUATION. REMOVED BURR, CLEANED FORWARD BELL CRANK AND ADJUSTED AS REQUIRED. R2 DOOR OPS CHECK GOOD REF AMM 52-42-00.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 34,541 hrs · 21,455 cycles

FOUND THE AFT WET AREA, RT SHEAR PANEL CORRODED AT FRAMES 87 TO 88. MX REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 53-23-10, 5142-01, AND 51-43-03.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 34,532 hrs · 21,448 cycles

MAINTENANCE FOUND LEVEL 2 CORROSION ON THE FLOOR SUPPORT. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01, AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 34,541 hrs · 21,455 cycles

DURING A CHECK, FOUND THE RT FLOOR SUPPORT FRAME 84 JUST FWD OF R2 DOOR CUTOUT SHOWS EVIDENCE OF CORROSION. MX REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01, 51-41-02, AND 51-43-02.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 34,541 hrs · 21,455 cycles

DURING A CHECK, FOUND THE AFT WET AREA CENTER SHEAR PANEL CORRODED, FRAMES 87 - 88. MX REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 51-10-03, 53-23-10, 51-42-01, AND 51-40-02.

Part: SPLICE PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 34,541 hrs · 21,455 cycles

DURING CHECK, FOUND THE FLOOR SPLICE PLATE CORRODED FRAMES 87 - 88 JUST AFT OF THE R2 DOOR. MX REMOVED AND REPLACED THE SPLICE PLATE IAW SRM 51-10-03, 51-75-16, 51-42-02, 51-40-02, AND 51-40-04.

Part: SILENCER — CRACKED (APU INLET) · airframe 34,532 hrs · 21,448 cycles

THE APU INLET SILENCER WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED INLET SILENCER IAW AMM 49-16-01.

Part: FITTING — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 34,541 hrs · 21,455 cycles

FOUND THE AFT CARGO DOOR AFT UPPER CORNER FRAME, AFT SIDE HAS CORROSION AROUND ONE NUTPLATE HOLE. BLENDED THE AREA IAW ETD 2017-170-091962. FOUND TO BE WITHIN ALLOWABLE LIMITS.

Part: SKIN — DENTED (FRAME 11) · airframe 34,532 hrs · 21,448 cycles

MAINTENANCE FOUND DENTS ON EXISTING REPAIR DOUBLER FWD EDGE AND FUSELAGE SKIN FWD OF FRAME 11, STRINGERS 16L - 17L. MAINTENANCE REPAIRED THE DAMAGED AREA IAW ETD 2017-170-090443.

Part: CONNECTOR — LOOSE (FLASHLIGHT) · airframe 31,375 hrs · 19,445 cycles

CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT WAS INOPERATIVE. MAINTENANCE FOUND CONNECTOR FOR FOWARD F/A FLASHLIGHT CHARGER LOOSE. MAINTENANCE RECONNECTED IAW AMM AND OPS CHECKED GOOD.

Part: GIRT BAR — OBSTRUCTED (R2 DOOR) · airframe 30,393 hrs · 18,795 cycles

F/A REPORTS R2 DOOR WILL NOT ARM FULLY. INTERNAL HANDLE DOES NOT FULLY MOVE DOWN. FOUND R2 DOOR GIRT BAR INDICATOR LENS/COVER BLOCKING GIRT BAR. REMOVED LENS PIECE.

Part: WARNING MESSAGE — FALSE ACTIVATION (PARKING BRAKE) · airframe 30,369 hrs · 18,773 cycles

PARKING BRAKE NOT RELEASED, MESSAGE IN FLIGHT. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. SERVICED EMERGENCY PARKING BRAKE SYSTEM 1 ACCUMULATOR, INSPECTED BOTH EMERGENCY PARKING BRAKE PRESSURE SWITCHES, NO DEFECTS FOUND. CLEANED AND RESECURED BOTH PARKING BRAKE PRESSURE SWITCH ELECTRICAL CONNECTORS. OPS CHECK GOOD.

Part: PROXIMITY SENSOR — MALFUNCTIONED (R1 DOOR) · airframe 30,131 hrs · 18,612 cycles

R1 DOOR INDICATION SHOWS OPEN IN FLIGHT. EICAS MESSAGE, DOOR SERV FWD OPEN, ON EICAS. ALL INDICATIONS ON DOOR ARE GREEN, PRESSURIZATION NORMAL. R & R R1 DOOR LOCKED PROXIMITY SENSOR IAW AMM 52-74-20.

Part: CONNECTOR — LOOSE (R1 DOOR) · airframe 30,097 hrs · 18,595 cycles

R1 DOOR EICAS OPEN INDICATION IN FLIGHT. INSPECTED WIRE HARNESS, FOUND CONNECTOR PLUG J19000, LOOSE. CLEANED OHMMETER AND REINSTALLED OHMMETER, OPS CHECK GOOD IAW WM 52-74-50.

Part: SENSOR — OUT OF ADJUST (R1 DOOR) · airframe 30,089 hrs · 18,589 cycles

SERVICE DOOR FWD OPEN IN FLIGHT, VISUAL INDICATION NORMAL. ADJUSTED FWD SERVICE (R1) DOOR WARNING SENSOR IAW AMM 52-74-20. OPS CHECK GOOD.

Part: BULKHEAD — CRACKED (ZONE 500) · airframe 29,447 hrs · 18,167 cycles

AFTER REAMING OF FASTENER HOLE ON LT SPAR III/CFII BULKHEAD, FOUND CRACKS IN BORE. FABRICATED AND INSTALLED BUSHINGS FCBS: 57-01-00-004 IAW ETD2015-170-106642, REV A.

Part: BULKHEAD — CRACKED (ZONE 600) · airframe 29,447 hrs · 18,167 cycles

AFTER REAMING OF FASTENER HOLE ON RT SPAR III/CFII BULKHEAD, FOUND CRACKS IN BORE. FABRICATED AND INSTALLED BUSHINGS FCBS: 57-01-00-004 IAW ETD2015-170-106642, REV A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,761 hrs · 16,426 cycles

AISLE PATH LIGHTING AT ROW 1-2 ON THE RT SIDE DOES NOT ILLUMINATE. R & R EMERGENCY LIGHT IAW AMM 33-50-21. OPS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (L2 DOOR) · airframe 26,114 hrs · 16,030 cycles

L2 DOOR INDICATION SHOWS AMBER AND X'D OUT, ALL DOOR VISUAL INDICATORS VERIFIED CORRECT AND DOOR IS LOCKED, LATCHED, AND CLOSED. R & R L2 DOOR HARNESS IAW AMM 52-72-21, OPS CHECK GOOD.

Part: ACTUATOR — TRIPPED (TE FLAPS) · airframe 25,345 hrs · 15,593 cycles

FLAP FAIL ON INITIAL FLAP RETRACTION. RETURNED TO FIELD, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. & R NR 3 RT OTBD FLAP ACTUATOR IAW AMM 27-51-01, PERFORMED ELECTRICAL RIG AND MECHANICAL IAW 27-51-00. OPS CHECK GOOD.

Part: FLAP SYSTEM — FAILED · airframe 24,299 hrs · 14,975 cycles

FLAP FAILED ON APPROACH, SLATS -3, FLAPS -0. UNABLE TO GET FLAPS/SLATS RESET WITH QRH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. INSPECTED FLAPS/SLATS ROLLERS, TRIP INDICATORS, SKEW SENSORS, LINKAGES. PERFORMED MULTIPLE OPS CHECKS, NO DEFECTS OR MESSAGES NOTED, COULD NOT DUPLICATE. OPS CHECK GOOD IAW AMM 27-51-00-810-802-A.

Part: VALVE — FAILED (ZONE 400) · airframe 23,938 hrs · 14,774 cycles

RETURN TO FIELD, AFT LAV SMOKE INDICATION. R & R SEAL PRESSURE REGULATING VALVE.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 23,679 hrs · 14,597 cycles

CORROSION FOUND ON LOWER DOOR SILL IN AFT CARGO. REMOVED DOOR SILL IAW SRM 51-40-02, INSTALLED NEW SILL IAW SRM 51-41-01. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 23,679 hrs · 14,597 cycles

CORROSION ON RT AFT SEAT TRACK AT FRAMES 86-89. R & R SEAT TRACK.

Part: BEAM — DAMAGED (CARGO DOOR) · airframe 23,718 hrs · 14,629 cycles

FWD CARGO DOOR BEAM, DAMAGED. R & R FORWARD CARGO DOOR BEAM BETWEEN FRAMES 24-27R.

Part: SILL — GOUGED (L2 DOORWAY) · airframe 23,718 hrs · 14,629 cycles

NUMEROUS GOUGES ALONG L2 DOOR SILL PLATE OTBD SIDE. PERFORMED REPAIR OF DOOR SILL PLATE AT OTBD SIDE OF L2 DOOR. R & R SEAL SUPPORT IAW ETD2013-170-049623. MAJOR REPAIR

Part: BUMPER — CORRODED (R1 DOOR) · corrosion level 2 · airframe 23,713 hrs · 14,627 cycles

CORROSION FOUND ON R1 DOOR BUMPER. R & R R1 DOOR DAMPER.

Part: STOP FITTING — CORRODED (L1 DOOR) · corrosion level 2 · airframe 23,713 hrs · 14,627 cycles

CORROSION FOUND ON L1 DOOR CUTOUT FRAME DOOR STOPS FWD 1-5 FROM TOP, AFT 1,6,6 FROM TOP MOUNTING BOLTS. R & R NEW BOLTS.

Part: SUPPORT — CORRODED (FLAP TRACK) · corrosion level 2 · airframe 23,713 hrs · 14,627 cycles

CORROSION FOUND ON LT FLAP TRACK SUPPORT 2 AND 3 AT FORWARD MOST THROUH BOLT NUT. R & R FWD MOST THROUGH BOLT NUT, WASHER AND ELASTIC WASHER ON INBD AND MIDDLE FLAP TRACK SUPPORTS ON LT WING.

Part: FLAP TRACK — CORRODED (RT WING TE FLAP) · airframe 23,713 hrs · 14,627 cycles

CORROSION FOUND ON RT FLAP TRACK SUPPORT 2,3, 4 AT FWD MOST THROUH BOLT NUTS. R & R FWD MOST THROUGH BOLT NUT, WASHER AND ELASTIC WASHER ON OTBD SIDE OF RT WING FLAP TRACK SUPPORTS.

Part: SUPPORT ANGLE — CRACKED (MLG WW BULKHEAD) · corrosion level 2 · airframe 23,713 hrs · 14,627 cycles

CORROSION FOUND ON LT MLG WELL FWD BULKHEAD SUPPORT ANGLE IS CRACKED. R & R LT MAIN GEAR FWD BULKHEAD SUPPORT BRACKET.

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,713 hrs · 14,627 cycles

CORROSION FOUND ON RT SHEAR PLATE AROUND RIVETS. R & R RT SHEAR PLATE LOCATED IN AFT GALLEY AREA BETWEEN FRAMES 87 AND 88.

Part: ROD — DEFECTIVE (CABIN DOOR) · airframe 22,620 hrs · 13,960 cycles

MAIN CABIN DOOR HANDLE COMES DOWN DURING CLOSING PROCESS OF ENTIRE DOOR. FERRIED TO IND. REPLACED BOTH COUNTERBALANCE RODS IN L1 DOOR IAW 52-11-20, OPS CHECK GOOD.

Part: INDICATOR — OBSTRUCTED (R1 DOOR) · airframe 19,854 hrs · 12,283 cycles

R1 DOOR SLIDE INDICATOR INOP. FOUND DEBRIS OBSTRUCTION, REMOVED AND CLEANED SLIDE LENS VIEW INDICATION, OPS CHECK GOOD IAW EMB 170 AMM.

Part: INDICATOR — DEFECTIVE (SERVICE DOOR) · airframe 17,924 hrs · 11,069 cycles

FRONT SERVICE DOOR (R1) ARMED/DISARMED INDICATORS RECESSED FROM WINDOW ABOUT 2-3 INCHES. INSPETED AND OPS CHECK R1 DOOR DISARM/ARM MECH IAW MM 52-41-20. NO DEFECTS NOTED.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 17,908 hrs · 11,056 cycles

LOWER FWD CARGO DOOR FRAME CUTOUT HAS CORROSION ABOVE FED AND AFT DOOR LATCHES. BLENDOUT REQUIRES NDT, PERFORMED HFEC FOR CORROSION REMOVAL, NO INDICATIONS NOTED. BLENDED AREAS IAW EMB ETD 2011-170-107390 REV A. TREATED, PRIMED, AND PAINTED AREA IAW EMB ETD AND SRM 51-23-04, 51-23-05, AND 51-23-06.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,908 hrs · 11,056 cycles

LEVEL 2 CORROSION POTABLE WATER BOX FWD AND AFT RETAINER, DOUBLERS CORRODED FR85-86. REMOVED FWD AND AFT RETAINER DOUBLERS ON POTABLE WATER BOX, REPLACED IAW EMB 170 SRM 51-43-02.

Part: STRUCTURE — UNKNOWN (FUSELAGE) · airframe 17,908 hrs · 11,056 cycles

MAJOR REPAIR - REPAIR DOCUMENT DATED 12/10/08 "FRAME 30 AND STRINGER 26" NEEDS REINSPECT FOR RII VERIFICATION. FOUND REPAIR LOCATION MISIDENTIFIED. RE-IDENTIFIED REPAIR BETWEEN FR23 AND 24 CUTOUT ON STGR 16L 44MM X 88MM. REMOVED REPAIR IAW EMB 170 SRM 51-40-02. PERFORMED HFEC IAW NDT MANUAL, NO CRACKLINE INDICATION NOTED. FABRICATED INNER AND OUTER DOUBLER, AND INSTALLED REPAIR IAW EMB 170 SRM 51-41-01 AND 51-41-02.

Part: SILL — CORRODED (FUSELAGE) · airframe 17,908 hrs · 11,056 cycles

LEVEL 2 CORROSION ON FWD CARGO DOOR SILL. REMOVED UNSERVICEABLE SUPPORTING SQUARES AND MATCH DRILLED SERVICEABLE SUPPORTING SQUARES AND INSTALLED PRIMED AND PAINTED FASTENERS IAW EMB 170 SRM 51-41-01, 51-20-00, 51-23-05, AND 51-23-06.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,908 hrs · 11,056 cycles

LEVEL 2 CORROSION FWD CARGO DOOR LOWER SILL CORNERS. REMOVED AND REPLACED FWD AND AFT SEAL REST CORNERS IAW EMB 170 AMM 53-21-21.

Part: EXTENSION — CRACKED (LT WING) · airframe 17,908 hrs · 11,056 cycles

MAJOR REPAIR - LT WING AFT RIB 10 EXTENSION CRACKED AT UPPER FLANGE HI-LOK. REMOVED AND REPLACED RIB 10 ON LT WING AFT SIDE IAW EBM 170 SRM 51-40-02, 51-43-01, 51-43-02, AND 51-43-03.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,908 hrs · 11,056 cycles

LEVEL 2 CORROSION FWD CARGO DOOR, AFT FRAME SILL. REMOVED AND REPLACED IAW EMB 170 SRM 51-43-03 AND 51-42-02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,908 hrs · 11,056 cycles

LEVEL 2 CORROSION FWD CARGO DOOR, FWD FRAME SILL. REMOVED AND REPLACED FWD DOUBLER AND FWD SEAL REST IAW EMB 170 SRM 51-43-04.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,908 hrs · 11,056 cycles

MAJOR REPAIR - LEVEL 2 CORROSION ALONG RT CENTER I-BEAM UNDER GALLEY AREA AND UNDER GALLEY NEAR WATER FITTINGS. REMOVED CORRODED DOUBLERS. FABRICATED AND INSTALLED NEW DOUBLERS IAW ETD 2009-170/08886 AND 2011-170-10732.

Part: SEAL DEPRESSOR — GOUGED (FUSELAGE) · airframe 17,908 hrs · 11,056 cycles

MAJOR REPAIR - DOOR L1 CUTOUT FWD SEAL DEPRESSOR GOUGED. REMOVED OLD SEAL RETAINER IAW EMB 170 SRM 51-40-02. LOCATED AND MATCH DRILLER NEW RETAINER IAW EMB 170 SRM 51-40-03. INSTALLED NEW RETAINER IAW EMB 170 SRM 51-41-01 AND 51-43-01.

Part: SEAL DEPRESSOR — GOUGED (FUSELAGE) · airframe 17,908 hrs · 11,056 cycles

MAJOR REPAIR - DOOR L1 CUTOUT FWD SEAL DEPRESSOR GOUGED. REMOVED DAMAGED L1 DOOR FWD SEAL RETAINER. MATCH DRILLED IAW EMB 170 SRM 51-40-03. INSTALLED SEAL RETAINER IAW EMB 170 SRM 51-41-01 AND 51-43-01.

Part: STRIP — MISSING (CABIN) · airframe 17,338 hrs · 10,662 cycles

LUMINESCENT STRIP ROW 18 A/C RIGHT MISSING. FOUND AND REINSTALLED LUMINESCENT STRIP IAW EMB 170 MM 33-50-21-04.

Part: INDICATOR — MALFUNCTIONED (R1 DOOR) · airframe 16,516 hrs · 10,177 cycles

ARM/DISARM WINDOW ON R1 DOOR ONLY MOVES HALF WAY. MAINTENANCE PERFORMED TEST ON R1 DOOR INDICATOR, OPS CHECK GOOD.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 16,412 hrs · 10,113 cycles

SLIDE FELL OUT OF PLACE ON L1 DOOR FROM GIRT BAR ENGAGED UPON OPENING. REMOVED AND REPLACED L1 DOOR SLIDE IAW AMM 25-65-01, OPS CHECK GOOD.

Part: ATTACH FITTING — DEFECTIVE (GIRT BAR) · airframe 15,679 hrs · 9,678 cycles

L2 SLIDE INDICATOR NOT SHOWING ARMED. L2 GIRT BAR INDICATOR INOP, DEFERRED. CLEARED MEL - SERVICED L2 DOOR GIRT BAR ATTACHMENT FITTINGS, OPS CHECK GOOD IAW EMB MM 52-12-41.

Part: GIRT BAR — JAMMED (R2 DOOR) · airframe 14,295 hrs · 8,831 cycles

DOOR R2 WILL NOT DISARM. FOUND GIRT BAR JAMMED WITH EMERGENCY SLIDE PIN. CLEARED JAM AND RE-SECURED PIN, OPS CHECK GOOD IAW EMB 170 MM 52-70-01.

Part: ENGINE — VIBRATES (NR 2) · airframe 14,143 hrs · 8,736 cycles

WHILE PASSING FL265 CLIMBING TO FL300 NOTICED LP VIBRATIONS ON ENGINE 2. IT WAS APPROXIMATELY 4.2-4.4 AND RISING. DISCONNECTED AUTO THROTTLE AND SLIGHTLY PULLED BACK POWER ON NR 2 ENGINE. VIBRATION CONTINUED TO SLOWLY RISE TO AROUND 4.8. ADVISED ATC THAT A LOWER ALTITUDE WAS NEEDED AND WAS APPROVED TO DESCEND TO FL260. VIBRATION CONTINUED AROUND 4.5. DECLARED AN EMERGENCY AND DIVERTED TO COS. DURING DESCENT, VIBRATION REMAINED AT 4.2-4.4. LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE.

Part: GIRT BAR — OUT OF ADJUST (R2 DOOR) · airframe 14,049 hrs · 8,684 cycles

CREW REPORTED R2 DOOR WILL NOT ARM, GIRT BAR LEVER IS JAMMED. MAINTENANCE ADJUSTED R2 DOOR GIRT BAR IAW EMB 170 MM 52-42-00. OPS CHECK GOOD.

Part: GIRT BAR — OUT OF ADJUST (L2 DOOR) · airframe 12,476 hrs · 7,767 cycles

L2 DOOR GIRT BAR INDICATION DOES NOT SHOW ARMED. MAINTENANCE ADJUSTED GIRT BAR.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,723 hrs · 7,322 cycles

CORROSION ON GUSSET ON RT FLOORBEAM BETWEEN FR 85 AND FR 86 LEVEL 2 CORROSION. REPAIRED IAW IC2009-170/00325. FABRICATED AND INSTALLED NEW GUSSET.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,723 hrs · 7,322 cycles

LEVEL 2 CORROSION ON GUSSET AT FR 90 OUTBOARD OF LT FLOORBEAM. REMOVED CORRODED GUSSET AND INSTALLED FABRICATED SERVICEABLE GUSSET IAW IC2009-170/00325.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,723 hrs · 7,322 cycles

LEVEL 2 CORROSION OF GUSSET AT FR 90 OUTBOARD OF THE RT FLOORBEAM. REMOVED CORRODED GUSSET AT FR 90, FABRICATED AND INSTALLED GUSSET IAW EMB IC2009-170/00325.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,723 hrs · 7,322 cycles

LEVEL 2 CORROSION AT FR 90 ON LT FLOORBEAM. REMOVED CORRODED GUSSET AT FR90, FABRICATED AND REPLACED IAW EMB IC2009-170/00325.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,723 hrs · 7,322 cycles

LEVEL 2 CORROSION AROUND NUT PLATE ON RT SILL AT FR 89. REMOVED AND REPLACED RT SILL PANEL SUPPORT IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,723 hrs · 7,322 cycles

LEVEL 2 CORROSION ON LT FLOORBEAM 2 INCHES AFT OF FR 86. FLOORBEAM REPLACED FROM STA 86 TO 88.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,723 hrs · 7,322 cycles

FWD CABIN FLOOR RT SEAT TRACK BEAM AT FR 17 HAS LEVEL 2 CORROSION ON TOP. REPAIRED FLOORBEAM AT FR 17 IAW ETD2009-170/08886.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,723 hrs · 7,322 cycles

LEVEL 2 CORROSION ON GUSSET AT FR 90 BETWEEN LT AND RT FLOORBEAMS. REMOVED CORRODED GUSSET AND MANUFACTURED REPLACEMENT GUSSET IAW EMB IC2009-170/00325. REMOVED AND INSTALLED GUSSET IAW EMB SRM 51-43-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,723 hrs · 7,322 cycles

FWD CABIN RT SEAT TRACK AT FR 14 HAS LEVEL 2 CORROSION. REPAIRED FWD CABIN RT SEAT TRACK AT FR 14-15 IAW ETD2009-170/08886.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,723 hrs · 7,322 cycles

LEVEL 2 CORROSION ON RT FLOORBEAM AT FR 87. REMOVED AND REPLACED RT FLOORBEAM AT FR 87 IAW EMB 170 SRM 51-40-01, 51-40-02, 51-43-01, AND 51-40-04.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,723 hrs · 7,322 cycles

LEVEL 2 CORROSION ON GUSSET AT FR 90 ON THE RT FLOORBEAM. REMOVED GUSSET AT FR 90, FABRICATED AND REPLACED IAW EMB IC2009-170/00325.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,723 hrs · 7,322 cycles

FWD CABIN FLOOR SEAT TRACK BEAM LT SIDE AT FR 16 HAS LEVEL 2 CORROSION ON TOP. REPAIRED LT SEAT TRACK BEAM IAW ETD2009-170/08886.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,723 hrs · 7,322 cycles

FWD CABIN FLOOR LT SEAT TRACK BEAM AT FR 19 HAS LEVEL 2 CORROSION ON TOP. CUT OUT DAMAGE AND REPAIRED IAW EMB ETD 2009-170/08886.

Part: RCCB — TRIPPED (CABIN) · airframe 10,797 hrs · 6,739 cycles

AFTER STARTING ENGINE NR 2 AND LINING UP FOR TAKEOFF "REMOTE C/B TRIP" MESSAGE APPEARED. MCDU INDICATED "EMER AFT BAT HTR" C/B WAS OUT. MAINTENANCE RESET C/B NR 39 OF RICC. PERFORMED EMERGENCY LIGHTING TEST IAW EMB 170 MM 33-50-00-5. OPS CHECK GOOD. NO WRITE UPS SINCE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 10,140 hrs · 6,338 cycles

EMERGENCY LIGHT AT ROW 9 INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY IAW EMB 170 MM 33-50-01-04.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS)

CREW RECEIVED A EMER LT BATT FAULT. MX PERFORMED EMERGENCY BATTERY CHARGING. DISCREPANCY HAS NOT REPEATED THIS DATE 09/23/08.