N870RW

Part: PUMP — FAULTED (ZONE 100) · airframe 37,163 hrs · 27,429 cycles

HYDRAULIC SYSTEM 2 LOW PRESSURE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R NUMBER 2 HYDRAULIC ACMP.

Part: BRACKET — CRACKED (WINDSHIELD) · airframe 32,282 hrs · 23,869 cycles

FWD WINDSHIELD CUT OUT STRUCTURE, CRACK FOUND ON T SHAPE BRACKET R/H SIDE. FWD WINDSHIELD CUT-OUT STRUCTURE ON T-SHAPE BRACKET R/H SIDE REMOVED AND REPLACED IAW SRM 53-10-2 FIG 68. FASTENERS REPLACED IAW SRM 51-41-01

Part: SUPPORT — CRACKED (ZONE 100) · airframe 32,282 hrs · 23,869 cycles

CFI, LOWER SKIN, CRACK FOUND ON SUPPORT EMER VENT ASSY BTWEEN FR 33-34 AND BETWEEN STR 23-24 LH. CFI, LOWER SKIN SUPPORT EMER VENT ASSY BETWEEN FR 33-34 AND BETWEEN STR 23-24 L/H, REMOVED AND REPLACED IAW EMBRAER SRM 51-41-01.

Part: SEAT TRACK — CORRODED (FRMS 75-85) · corrosion level 2 · airframe 32,282 hrs · 23,869 cycles

CFIII, FLOOR STRUCTURE, CORROSION FOUND ON RH INBD SEAT TRACK BETWEE FR 83-84. REPLACED CFIII R/H INBD SEAT TRACK FROM FR 75-78 WITH NEW P/N 170-86082-005 IAW SRM 51-43-03 AND 51-43-04.

Part: SHEAR PANEL — CORRODED (FRMS 87-88) · corrosion level 2 · airframe 32,282 hrs · 23,869 cycles

CF III, FLOOR STRUCTURE, CORROSION FOUND ON MID SHEAR PANEL BETWEEN FR 87-88. CFIII, FLOOR STRUCTURE, REPLACED MID SHEAR PANEL BETWEEN FR 87-88 WITH NEW P/N 170-65928-001 IAW SRM 51-42-01.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 32,282 hrs · 23,869 cycles

RH HORIZONTAL STAB, CRACK FOUND AT RIB 11. R/H HORIZONTAL STAB, CRACK AT RIB 11, REPAIR CARRIED OUT UNDER THE TASK CARD 170EO-55-10-0004.

Part: BRACKET — CORRODED (FWD LAVATORY) · corrosion level 2 · airframe 23,869 hrs

FWD LAV AFT O/B HOLD DOWN BRACKET AND HARDWARE CORRODED. FWD LAV AFT O/B HOLD DOWN BRACKET AND HARDWARE REMOVEDC AND REPLACED IAW AMM 20-10-01 AND 51-40-08

Part: LIGHT — UNSERVICEABLE (CABIN) · airframe 32,282 hrs · 23,869 cycles

PAX DOOR ENTRANCE EMERGENCY LIGHT UNSERVICEABLE. PAX DOOR ENTRANCE EMERGENCY LIGHT REPLACED IAW : AMM 33-26-01-400-802-A. OPERATIONAL TEST TRANSFERRED TO AVIONICS FINAL FUNCTION NRC# 4500886-7000-0001, AWS-4

Part: SUPPORT — CRACKED (ZONE 100) · airframe 32,282 hrs · 23,869 cycles

LOWER FUSELAGE, CRACK FOUND ON SUPPORT ASSY - EMER VENT AT FR 34 LH SIDE. LOWER FUSELAGE, SUPPORT ASSY - EMER VENT AT FR 34 L/H SIDE REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-41-01

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,623 hrs · 23,312 cycles

AFT OUTBOARD EMERGENCY LIGHT BATTERY FAULTED. R & R AFT OUTBOARD EMERGENCY LIGHT BATTERY.

Part: DOOR — LACK OF LUBE (FWD) · airframe 31,428 hrs · 23,140 cycles

FORWARD ENTRANCE DOOR DIFFICULT TO OPEN, STICKS UPPER FWD FUSELAGE. CLEANED AND LUBED DOOR AS REQUIRED IAW AMM 52-11-20.

Part: TRACK — LACK OF LUBE (PAX DOOR) · airframe 30,713 hrs · 22,601 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. CLEANED AND LUBED DOOR TRACKS IAW AMM 52-10-03.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 30,261 hrs · 22,219 cycles

LH FWD EMERGENCY LIGHTS POWER UNIT FAILED FUNCTION CHECK. R&R LH FWD EMERGENCY LIGHTS POWER UNIT IAW AMM 35-50-01/400.

Part: REGULATOR VALVE — INOPERATIVE (NR 2 BLEED SYS) · airframe 29,770 hrs · 21,818 cycles

BLEED 2 OVERPRESSURE EICAS IN FLIGHT, WOULD NOT EXTINGUISH. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. R & R E2 BLEED PRESSURE REGULATING VALVE.

Part: SENSOR — OUT OF ADJUST (L1 DOOR) · airframe 29,528 hrs · 21,624 cycles

L1 DOOR INDICATION IN FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED FORWARD DOOR WARNING SENSOR ADJUSTMENT IAW AMM 52-72-20. OPS CHECK GOOD. L1 DOOR INDICATOR ON MFD CORRESPONDS WITH POSITION OF ARMING LEVER.

Part: HANDLE — OBSTRUCTED (CABIN DOOR) · airframe 29,301 hrs · 21,456 cycles

MAIN CABIN DOOR ARMING HANDLE IS HARD TO MOVE. REMOVED DEBRIS IN SURROUNDING AREA OF ARMING HANDLE IAW AMM 52-11-00. OPS CHECK GOOD.

Part: DOOR — LACK OF LUBE (L1) · airframe 29,302 hrs · 21,457 cycles

MCD VERY DIFFICULT TO OPEN. CLEAN AND LUBED L1 DOOR AS REQUIRED IAW CMM 52-11-22.

Part: DOOR — CORRODED (WASTE SERVICE) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND WASTE SERVICE DOOR IS CORRODED. REMOVED AND REPLACED WASTE SERVICE DOOR. REF EMB AMM 53-03-60. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 88) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND SHEAR CLIP, FRAME, AND SKIN WITH CORROSION AT FR88, STR27R/28R. REMOVED AND REPLACED SHEAR CLIP AT FR- 88 STGR 27R-28R REF. EMB SRM51-40-08. BLENDED OUT CORROSION ON FRAME 88 AT STR27R/28R REF SRM 51-10-03, MATERIAL LOST 4"X2"X.003".THIS IS WITHIN ALLOWABLE LIMITS REF SRM 53-23-04/AD01. FOUND NO CORROSION ON THE SKIN ONLY ON THE FASTENERS. REMOVED AND REPLACED FASTENERS REF. EMB SRM 51-- 40-08. A/C REMAINS IN CHECK.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND AFT WET AREA RH SHEAR PANEL BETWEEN FR87-88 IS CORRODED AROUND GALLEY MOUNT HOLE. REMOVED AND REPLACED RH SHEAR PANEL BETWEEN FR87-88 REF. EMB SRM 51-40-08. A/C REMAINS IN CHECK.

Part: DOUBLER — CORRODED (FRAME 16) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LH INBOARD DOUBLER IS CORRODED AT FR 16. REMOVED DAMAGED LH INBOARD FLOOR DOUBLER FROM FRAME 13-16. LOCATED, DRILLED AND INSTALLED LH INBOARD FLOOR DOUBLER AT FRAME 13-16 REF:EMB SRM 51-40-08. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 87) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION - SHEAR CLIP FR87, STR27R/28R. REMOVED AND REPLACED SHEAR CLIP AT FR87, STR27R/28R AND RESTORED SURFACE PROTECTION. REF: SRM 51-40-08, 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: BEAM — CORRODED (L1 DOOR AREA) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND L1 DOOR LOWER BEAM REWORK FOUND LVL 2 CORROSION AROUND THE AFT GIRT BAR FITTING. REMOVED AND REPLACED FWD PAX DOOR LOWER BEAM. REF: SRM 51-40-08. A/C REMAINS IN CHECK.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LVL 2 CORRODED SHEAR CLIP IN THE AFT CARGO ON FR 84 BETWEEN STR 26-27R. REMOVED AND REPLACED NEW SHEAR CLIP FR84, STR27R/26R, REF SRM 51-40-08. A/C REMAINS IN CHECK.

Part: FLOORBEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LH OUTBOARD FLOOR SUPPORT IS CORRODED AT FR 16. REMOVED AND REPLACED L-H O/B FLOOR SUPPORT AT FR 16. REF EMB SRM 51-40-08. A/C REMAINS IN CHECK.

Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LVL 2 CORROSION LT UPPER SHEET FR86. REMOVED AND REPLACED LT UPPER SHEET FR86 REF SRM 51-40-08. A/C REMAINS IN CHECK.

Part: BEAM — CORRODED (FWD CARGO DOOR) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LVL 2 CORROSION AT FWD CARGO DOOR NUT SUPPORT AT THE LOWER BEAM AS MARKED WITH RED GREASE PENCIL. REMOVED AND REPLACED FWD CARGO DOOR NUT SUPPORT AT THE LOWER BEAM AND RESTORED SURFACE PROTECTION REF:SRM 51-40-08, 51-23-06 A/C REMAINS IN CHECK.

Part: SEAT TRACK — CORRODED (FRAME 16) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LH SEAT TRACK BEAM IS CORRODED AT FR 16. REMOVED AND REPLACED L-H SEAT TRACK FR 12-21. REF EMB SRM 51-40-08. A/C REMAINS IN CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND RT SEAT TRACK BEAM IS CORRODED BETWEEN FR 14 AND FR 15. PERFORMED REPAIR ON RT SEAT TRACK BEAM BETWEEN FR 14-15 UPPER CAP REF SRM 53-10-10/REPAIR 03P. A/C REMAINS IN CHECK.

Part: FLOOR SUPPORT — CORRODED (FRAME 86) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION - PANEL SUPPORT RH SIDE FR86. REMOVED AND REPLACED PANEL SUPPORT ON R-H SIDE FR 86 PER REF SRM 51-40-08. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 86) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION - SHEAR CLIP FR86, STR27R/28R. REMOVED AND REPLACED NEW SHEAR CLIP FR86, STR27R/28R REF SRM 51-40-08. A/C REMAINS IN CHECK.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LVL 2 CORROSION RT BEAM FR87. REMOVED AND REPLACED RT BEAM AT FR-87 REF SRM 51-40-08. A/C REMAINS IN CHECK.

Part: FLOOR SUPPORT — CORRODED (FRAME 85-86) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION - RH UPPER SHEET FR85/86. REMOVED AND REPLACED R/H UPPER SHEET FR85/86 AND RESTORED SURFACE PROTECTION. REF: SRM 51-40-08, 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND RT FLOOR PANEL SUPPORT IS CORRODED AT FR 16. REMOVED AND REPLACED RT FLOOR PANEL SUPPORT AT FR16 REF SRM 51-40-02/ SRM 51-40-08. A/C REMAINS IN CHECK.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LVL 2 CORROSION ON 3 EA LOWER ANGLES ON PANEL 1441FR. REMOVED AND REPLACED 3EA LOWER ANGLES ON PANEL 1441FR REF. EMB SRM 51-40-08. A/C REMAINS IN CHECK.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,049 hrs · 21,264 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LVL 2 CORROSION ON 3EA LOWER ANGLES ON PANEL 1431DL. REMOVED AND REPLACED 3 EA LOWER ANGLES ON PANEL 1431DL REF. EMB SRM 51-40-08. A/C REMAINS IN CHECK.

Part: GUIDE — OUT OF ADJUST (PAX DOOR) · airframe 28,697 hrs · 21,001 cycles

GATE AGENT HAVING TROUBLE OPENING LEFT PAX DOOR. READJUSTED THE L1 DOOR UPPER GUIDE RAMPS IAW AMM 52-11-00.

Part: SKIN — CANNING (FRAMES 1-2) · airframe 28,111 hrs · 20,574 cycles

DAMAGE FOUND TO BE OIL CANNING BETWEEN FRAMES 1 AND 2, STRINGERS 8R AND 10R. CUTOUT THE DAMAGE AND INSTALLED A DOUBLER IAW ETD2018-170-090830. MAJOR REPAIR.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,675 hrs · 20,251 cycles

COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE. R & R THE NR 1 EMERGENCY LIGHT BATTERY IAW AMM 33-50-01.

Part: STRUT — ABNORMAL (NLG) · airframe 26,696 hrs · 19,628 cycles

LANDING GEAR WOW SYSTEM FAIL MESSAGE APPEARED ON EICAS AFTER TAKEOFF. LANDING GEAR HANDLE WAS UNABLE TO BE MOVED TO THE UP POSITION. FOLLOWED QRH, DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. R&R NLG SHOCK STRUT IAW AMM 32-21-01.

Part: SENSOR — OUT OF ADJUST (WOW) · airframe 26,696 hrs · 19,627 cycles

LANDING GEAR WOULD NOT GO UP. EICAS MESSAGE LG WOW SYS FAIL DISPLAYED. RAN QRH, AND MESSAGE DISAPPEARED. FOUND NLG WOW SENSORS OUT OF ADJUSTMENT. ADJUSTED IAW AMM 32-62-01. FOUND MLG WOW SENSORS 1, 2, AND 3 OUT OF ADJUSTMENT. ADJUSTED IAW AMM 32-62-03.

Part: TRACK — DIRTY (R1 DOOR SLIDE) · airframe 26,647 hrs · 19,593 cycles

R1 DOOR, FA HAS HARD TIME DISARMING DOORS. FEELS LIKE ITS GETTING STUCK. CLEANED FLOOR TRACKS FOR SLIDE AND LUBRICATED. PERFORMED OPS CHECK IAW AMM 52-41-22, OPS CHECK GOOD.

Part: LEVER — LACK OF LUBE (R1 DOOR) · airframe 16,634 hrs · 19,586 cycles

R1 DOOR VERY DIFFICULT TO DISARM. LUBRICATED THE R1 DOOR DISARM LEVER IAW CMM 52-41-22. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,598 hrs · 18,843 cycles

OVERHEAD COCKPIT EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY IAW AMM 33-50-01-4. OPS CHECKED GOOD.

Part: PIN — OUT OF ADJUST (DOOR GATE) · airframe 23,689 hrs · 17,623 cycles

MAIN ENTRY DOOR UPPER LINER FLAP NOT WORKING PROPERLY. ADJUSTED ROLLER PIN, OPS CHECK GOOD AT THIS TIME IAW AMM 25-23-04.

Part: SLIDE — UNWANTED DEPLOY (L2 DOOR) · airframe 23,689 hrs · 17,623 cycles

L2 SLIDE DEPLOYED. DOOR ASSIST BOTTLE DID NOT ACTIVATE. GIRT BAR WAS ENGAGED IN FLOOR FITTING WHILE INDICATIONS SHOWED IT WAS DISARMED. R & R L2 DOOR SLIDE IAW AMM 25-65-01 AND R & R L2 DOOR FLEXBALL CABLE IAW S170EO-52-10-0001.

Part: WIRE HARNESS — DAMAGED (L2 DOOR) · airframe 23,636 hrs · 17,587 cycles

WHEN OPEN, L2 DOOR RED INDICATIONS GO TO YELLOW WITH X. R & R SENSOR HARNESS, OPS TESTED GOOD IAW AMM 52-72-21.

Part: CONNECTOR — LOOSE (L2 DOOR) · airframe 23,599 hrs · 17,550 cycles

L2 SERVICE DOOR CYCLES BETWEEN GREEN CLOSED INDICATION TO A YELLOW CIRCLE WITH BLACK X AND THEN TO RED OPEN INDICATION WITH ASSOCIATED EICAS MESSAGE. FOUND CONNECTOR PLUG LOOSE. RESECURED IT IAW AMM 52-12-00. OPS CHECK GOOD. ALSO CLEANED CONNECTOR IAW SWPM 20-61-20.

Part: CONNECTOR — UNSECURE (ZONE 800) · airframe 23,448 hrs · 17,455 cycles

L2 DOOR YELLOW X ON MFD. UPON FURTHER INSPECTION, FOUND ELECTRICAL CONNECTOR UNSECURE. REMOVED, CLEANED, AND RESECURED ELECTRICAL CONNECTOR IAW AMM 52-72-21. OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (DOOR SENSOR) · airframe 23,406 hrs · 17,428 cycles

AFT PAX DOOR OPEN EICAS MESSAGE IN FLIGHT WITH YELLOW X ON MFD INDICATION. FOUND DOOR WARNING SENSOR HARNESS LOOSE ON ACFT SIDE. SECURED THE CONNECTOR, OPS CHECKED GOOD IAW AMM 52-72-21.

Part: RIB — DAMAGED (ZONE 100) · airframe 23,382 hrs · 17,404 cycles

RIGHT MOUNT FLANGE FOR THE VERTICAL TIP CAP HAS A DRILL START AND 2 EACH DRILLED OUT SCREW SHANKS. R & R VERTICAL RIB 14 ASSY. MAJOR REPAIR.

Part: DOUBLER — CORRODED (FRAME 8) · corrosion level 2 · airframe 23,382 hrs · 17,404 cycles

CORROSION AT FRAME 8 AND CO-PILOT OUTBOARD FLOORBEAM. REPLACED CO-PILOT FLOOR DOUBLER IAW ETD2016-170-064688.

Part: STRINGER — CORRODED (FRAMES 88-90) · corrosion level 2 · airframe 23,382 hrs · 17,404 cycles

CORROSION ON STRINGER 19R, FRAMES 88 - 90. R & R THE STRINGER SEGMENT. MAJOR REPAIR

Part: SKIN — GOUGED (SERVICE DOOR) · airframe 23,382 hrs · 17,404 cycles

GOUGE ON FWD SERVICE DOOR INTERIOR SKIN STRUCTURE AREA COVERED BY SLIDE. R & R THE GUSSET IAW SRM 51-42-02, 51-41-01, 51-23-06. MAJOR REPAIR.

Part: SKIN — DENTED (FRAMES 19-20) · airframe 23,382 hrs · 17,404 cycles

FOUND TWO PROTRUDING DENTS BETWEEN FRAMES 19 - 20, STRINGERS 25 - 26L. REPAIRED IAW SRM 53-10-01/AD 03, SRM 51-23-05, AND 51-53-06.

Part: SEAT TRACK — DAMAGED (FRAMES 17-20) · corrosion level 2 · airframe 23,382 hrs · 17,404 cycles

RT SEAT TRACK HAS AREAS OF IMPACT DAMAGE, GOUGES, AND CORROSION FROM FRAMES 17-20. R & R THE SEAT TRACK.

Part: SEAT TRACK — DAMAGED (FRAMES 23-34) · corrosion level 2 · airframe 23,382 hrs · 17,404 cycles

LEFT SIDE CABIN SEAT TRACKS FRAMES 23-34 HAS AREAS OF IMPACT DAMAGE, NICKS, BARE METAL, AND CORROSION IN 5 AREAS. REMOVED THE DAMAGE.

Part: FINGER DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,382 hrs · 17,404 cycles

FWD CARGO DOOR BEAM FWD FINGER DOUBLER CORRODED. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-43-02, AND SRM 51-40-02. MAJOR REPAIR.

Part: FINGER DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,382 hrs · 17,404 cycles

AFT CARGO DOOR BEAM AFT FINGER DOUBLER CORRODED. R & R AFT CARGO DOOR BEAM AFT FINGER DOUBLER. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,382 hrs · 17,404 cycles

FLOOR SUPPORT JUST FWD OF L2 DOOR, HAD TWO FASTENER HOLES SHOWING SIGNS OF CORROSION. R & R THE FLOOR SUPPORT IAW SRM 51-75-16, 51-43-01, 51-40-02, 51-23-04, AND 51-23-06.

Part: FINGER DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,382 hrs · 17,404 cycles

AFT CARGO BEAM FWD FINGER DOUBLER CORRODED. R & R THE FLINGER DOUBLER. MAJOR REPAIR.

Part: FINGER DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,382 hrs · 17,404 cycles

FWD CARGO DOOR BEAM AFT FINGER DOUBLER CORRODED. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-43-02, AND 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (FRAME 29) · corrosion level 2 · airframe 23,382 hrs · 17,404 cycles

SEAT TRACK AT FRAME 29 ON THE RT SIDE HAS IMPACT DAMAGE, NICKS, AND CORROSION. REMOVED DAMAGED SECTION OF SEAT TRACK AND SPLICE IN A NEW SECTION.

Part: MOUNT — CRACKED (E/E RACK) · airframe 23,382 hrs · 17,404 cycles

CRACK ON FWD AVIONICS RACK STRUCTURE, TCAS MODULE MOUNT PLATFORM HAS CRACKED SUPPORT BEAM OF RACK STRUCTURE. REMOVED CRACKED SUPPORT BEAM OF RACK STRUCTURE ON TCAS MODULE MOUNT PLATFORM REF SRM 51-41-01. FABRICATED, LOCATED, DRILLED, ALODINED, AND PRIMED NEW SUPPORT BEAM OF RACK STRUCTURE ON TCAS MODULE MOUNT PLATFORM IAW SRM 51-40-02, 51-23-04, 51-23-05, AND ETF2016-170-062460. MAJOR REPAIR

Part: SPAR — CRACKED (RT WING) · airframe 23,382 hrs · 17,404 cycles

RIGHT STUB WING SPAR 3 FORWARD FACE SHOWS CRACK INDICATIONS AT THE FASTENER REPLACEMENT HOLE, AT THE 3:00 AND 9:00 POSITIONS. PERFORMED PERMENANT REPAIR IAW ETD2016-170-062751. MAJOR REPAIR.

Part: SPAR — CRACKED (LT WING) · airframe 23,382 hrs · 17,404 cycles

LEFT STUB WING SPAR 3 FORWARD FACE SHOWS CRACK INDICATIONS AT THE FASTENER REPLACEMENT HOLE, EXTENDING .125" FROM THE EDGE OF THE HOLE AT THE 3:00 AND 9:00 POSITIONS. REPAIRED IAW ETD2016-170-062751. MAJOR REPAIR.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 23,214 hrs · 17,307 cycles

R & R EMERGENCY EXIT DOOR COVER CRACKED. R & R EMERGENCY EXIT COVER LENS IAW 33-50-17.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 23,214 hrs · 17,307 cycles

R1 EMERGENCY EXIT DOOR COVER CRACKED. R & R EMERGENCY EXIT COVER LENS IAW 33-50-17.

Part: LIGHT — DETACHED (ZONE 100) · airframe 22,697 hrs · 16,984 cycles

EMERGENCY LIGHT STRIP ROW 1 PEELED UP. SECURED THE LIGHT STRIP IAW AMM 33-50-21.

Part: SKIN — DAMAGED (FRAMES 91-92) · airframe 22,537 hrs · 16,843 cycles

DAMAGE TO FUSELAGE SKIN BETWEEN FRAMES 91 AND 92 STRINGERS 28L. REPAIRED IAW ETD2016-170-003505.

Part: LATCH — MISINSTALLED (L1 DOOR SLIDE) · airframe 22,150 hrs · 16,574 cycles

L1 DOOR SLIDE BUSTLE WILL NOT LATCH ONTO SLIDE, FWD TOP LOCK IS BACKWARDS. R & R BUSTLE WITH CORRECT LATCH IAW AMM 25-23-04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,393 hrs · 16,041 cycles

EMERGENCY LIGHT IS BAD. R & R IAW 33-50-500-0001.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 20,030 hrs · 15,205 cycles

EMERGENCY LIGHT STRIP AT SEAT 3 RT IS SHORT. ADJUSTED THE LIGHT IAW AMM 33-50-21.

Part: ROLLER — LACK OF LUBE (L1 DOOR) · airframe 19,437 hrs · 14,792 cycles

L1 DOOR IS HARD TO PULL OPEN. LUBED DOOR ROLLERS, PERFORMED OPS CHECK OF L1 DOOR IAW AMM 52-10-00. OPS CHECKED GOOD.

Part: ROD — BENT (L1 DOOR) · airframe 19,438 hrs · 14,793 cycles

DIFFICULTY OPENING THE L1 DOOR ON ARRIVAL. TROUBLESHOT L1 DOOR. R & R BENT L1 DOOR HOIST ROD IAW AMM 52-11-20, OPS CHECK GOOD.

Part: GUSSET — CORRODED (FRAME 84) · corrosion level 2 · airframe 19,384 hrs · 14,747 cycles

CORROSION FOUND ON GUSSET FRAME 84. R & R GUSSET.

Part: DOUBLER — CORRODED (THRESHOLD) · airframe 19,384 hrs · 14,747 cycles

CORROSION FOUND AROUND SCUFF PLATE DOME NUTPLATES IN LIP OF FWD CARGO DOOR THRESHOLD. R & R NUTPLATE DOUBLER ASSY.

Part: SEAT TRACK — CORRODED (FRAMES 82-84) · airframe 19,384 hrs · 14,747 cycles

CORROSION FOUND ON RT SEAT TRACK AT FRAMES 82-84. R & R RT SEAT TRACK.

Part: THRESHOLD — CORRODED (L2 DOORWAY) · corrosion level 2 · airframe 19,384 hrs · 14,747 cycles

CORROSION FOUND ON L2 DOOR THRESHOLD BEAM AFT FLOOR FITTING AREA. PERFORMED SPOTFACE TO REMOVED DAMAGE IAW ETD2014-170-052382. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FRAMES 83-84) · corrosion level 2 · airframe 19,384 hrs · 14,747 cycles

CORROSION FOUND ON LT SEAT TRACK Y-10.748, BETWEEN FRAMES 83-84. REPAIRED SEAT TRACK.

Part: CROSSBEAM — CORRODED (FRAME 84) · corrosion level 2 · airframe 19,384 hrs · 14,747 cycles

CORROSION FOUND ON CROSSBEAM FRAME 84 RT. REPAIRED CROSSBEAM. MAJOR REPAIR.

Part: CROSSBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 19,384 hrs · 14,747 cycles

CORROSION FOUND ON CROSSBEAM, FRAME 17 BETWEEN SEAT TRACKS. CUT OUT DAMAGED AREA AND INSTALLED A ANGLE DOUBLER IAW ETD2014-170-053184. MAJOR REPAIR.

Part: CROSSBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 19,384 hrs · 14,747 cycles

CORROSION FOUND ON CROSSBEAM FRAME 17 Y+10.748. CUT OUT DAMAGED AREA OF CROSSBEAM AND INSTALLED AN ANGLE DOUBLER IAW ETD2014-170-053184. MAJOR REPAIR.

Part: CROSSBEAM — CORRODED (FRAME 84) · corrosion level 2 · airframe 19,384 hrs · 14,747 cycles

CORROSION FOUND ON CROSSBEAM FRAME 84 LT. REPAIRED CROSSBEAM. MAJOR REPAIR.

Part: CROSSBEAM — CORRODED (FRAME 84) · corrosion level 2 · airframe 19,384 hrs · 14,747 cycles

CORROSION FOUND ON CROSSBEAM BETWEEN SEAT TRACKS FRAME 84. REPAIRED CROSSBEAM. MAJOR REPAIR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 18,958 hrs · 14,471 cycles

BIRDSTRIKE DAMAGE TO LT FWD FUSELAGE SKIN AT FRAMES 1-4, BETWEEN STGR 22L-25L. INSTALLED SERVICEABLE FWD FUSELAGE SKIN FCBS 53-10-00-004.

Part: SHEAR TIE — CORRODED (FRAME 3) · airframe 18,959 hrs · 14,472 cycles

CORROSION FOUND ON SHEAR TIE AT FRAME 3 BETWEEN S24 - 25L. R & R DAMAGED SHEAR TIE.

Part: LIGHT — DAMAGED (CABIN) · airframe 18,258 hrs · 13,988 cycles

EMERGENCY LIGHT 15 DAMAGED ON RT SIDE OF AISLE NEXT TO SEAT 18DF, DAMAGE MEASURED 11 INCHES. REPLACED EMERGENCY LIGHT IAW AMM 33-50-21.

Part: GLOWSTRIP — UNSECURE (ZONE 100) · airframe 17,685 hrs · 23,468 cycles

PHOTOLUMINESCENT STRIP IN FRONT OF CLOSET IS COMING OFF. SECURED PHOTOLUMINESCENT STRIP IAW AMM 33-50-21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,534 hrs · 13,441 cycles

ROW 1, 2, 3 CD SIDE EXIT LIGHTS NOT ILLUMINATING. REMOVED LIGHTS AND INSTALLED NEW LIGHT IAW SE252043.

Part: LIGHT — UNSECURE (CABIN) · airframe 17,480 hrs · 13,396 cycles

EMERGENCY LIGHT UNSECURE. SECURED EMERGENCY LIGHT IAW AMM 33-50-21.

Part: HANDLE — LACK OF LUBE (R1 DOOR) · airframe 15,642 hrs · 12,019 cycles

R1 DOOR WILL NOT ARM. CLEANED AND LUBED HANDLE AND LATCH IAW AMM 52-41-22.

Part: SIGN — INOPERATIVE (CABIN) · airframe 15,130 hrs · 11,683 cycles

EXIT SIGN ABOVE R2 DOOR IS CRACKED AND DOES NOT LIGHT UP WHEN EMERGENCY LIGHTS ARE ACTIVATED. REMOVED AND REPLACED EXIT SIGN LENS IAW EMB 170 MM 33-50-17 AND REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT IAW EMB 170 MM 33-50-0.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 15,130 hrs · 11,683 cycles

MAJOR REPAIR - FWD CARGO DOOR CUTOUT FWD LOWER SEAL REST CORRODED. REMOVED, MATCH DRILLED, AND INSTALLED NEW FWD LOWER SEAL REST IAW EMB 170 SRM 51-40-02.

Part: BEAM — CORRODED (FUSELAGE) · airframe 15,130 hrs · 11,683 cycles

MAJOR REPAIR - EVIDENCE OF CORROSION UNDER FWD CARGO DOOR, FWD MOST DOOR LATCH ROLLER. REMOVED AND REPLACED FWD CARGO DOOR BEAM BETWEEN FR24R TO 27R IAW EMB 170 SRM 51-40-02 AND 51-43-02.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,130 hrs · 11,683 cycles

LEVEL 2 CORROSION AND GOUGE DOWN LENGTH OF I-BEAM FROM FR 85-88. REMOVED AND REPLACED LEFT I-BEAM IAW EMB 170 SRM 51-40-02, 51-41-01, AND 51-43-03.

Part: SERVICE PANEL — CORRODED (FUSELAGE) · airframe 15,130 hrs · 11,683 cycles

MAJOR REPAIR - INTERNAL SIDE OF AFT WASTE SERVICE BOX FLANGE CORRODED. REMOVED AND INSTALLED WASTE SERVICE BOX DOUBLERS IAW EMB 170 SRM 51-40-02. ACCOMPLISHED SB 170-53-0056 IAW ETD2012-170-009600.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,130 hrs · 11,683 cycles

LEVEL 2 CORROSION RIGHT SEAT TRACK ON PAX CABIN FLOOR STRUCTURE BETWEEN FRAMES 13-16. REMOVED, MATCH DRILLED, AND INSTALLED RIGHT SEAT TRACK IAW EMB 170 SRM 51-40-02, 51-43-01, AND 51-43-02.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 14,304 hrs · 11,223 cycles

BY ROW 6 ON "A" SIDE, A PIECE OF PHOTO LUMINESCENT FLOOR ESCAPE PATH LIGHTING IS MISSING. REPOSITIONED PHOTO LUMINESCENT STRIPS REQUIRED IAW EMB 170 MM 33-50-21. NO FURTHER DEFECTS NOTED.

Part: LIGHT — MISSING (CABIN) · airframe 14,136 hrs · 11,127 cycles

EMERGENCY FLOOR LIGHT STRIP FOR LT SIDE AISLE ROW 5 MISSING. INSTALLED EMERGENCY FLOOR LIGHTING STRIP FOR LT SIDE AISLE ROW 5 IAW AMM 33-50-21.

Part: DOOR — OUT OF ADJUST (L1) · airframe 13,809 hrs · 10,956 cycles

MAIN CABIN DOOR WILL OPEN FROM INSIDE BUT NOT FROM OUTSIDE. ADJUSTED L1 DOOR TO OPERATE NORMALLY FROM BOTH INTERNAL AND EXTERNAL HANDLES IAW EMB 170 MM 52-11-00. OPS CHECK GOOD.

Part: HANDLE — OUT OF ADJUST (L1 DOOR) · airframe 13,763 hrs · 10,929 cycles

L1 DOOR VERY DIFFICULT TO OPEN FROM OUTSIDE, MUST BE PUSHED FROM INSIDE TO OPEN. ADJUSTED L1 DOOR HANDLE TO OPERATE NORMAL. OPS CHECK GOOD IAW AMM 52-11-00.

Part: ENGINE — FOD (NR 2) · airframe 13,675 hrs · 10,870 cycles

DURING CLIMB OUT BETWEEN 10,000 AND 13,000 FEET EXPERIENCED A LOUD BANG NOISE AND E2 SHUT DOWN IN FLIGHT. CREW DECLARED EMERGENCY AND DIVERTED TO JFK. MAINTENANCE INSPECTED ENGINE AND FOUND DEBRIS IN EXHAUST OF E2, APPEARING TO BE A BLADE. MAINTENANCE REMOVED AND REPLACED E2.

Part: GLOWSTRIP — OUT OF POSITION (CABIN) · airframe 13,408 hrs · 10,693 cycles

EMERGENCY LIGHT STRIP AT SEAT 6B HAS SLIPPED IN ITS CHANNEL. ADJUSTED PHOTOLUMINESCENT STRIP IAW EMB 170 MM 33-50-21.

Part: GLOWSTRIP — OUT OF POSITION (CABIN) · airframe 13,012 hrs · 10,466 cycles

PHOTOLUMINESCENT STRIP ON LEFT SIDE ROW 5 SLID OUT OF PLACE. REPOSITIONED EMERGENCY LIGHTING STRIP ON ROW 5 AISLE IAW EMB MM 33-50-21.

Part: PRESSURE SWITCH — UNSERVICEABLE (BRAKE SYSTEM) · airframe 12,741 hrs · 10,292 cycles

PARK BRAKE NOT RELEASED EICAS MESSAGE. RETURNED TO FIELD, DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY BRAKE PRESS SWITCH IAW EMB 175 MM AND CUSTOM I/O 2 IN MAU 3 IAW EMB 175 MM 31-41-07.

Part: LIGHT — UNSECURE (CABIN) · airframe 12,574 hrs · 10,184 cycles

FLOOR EVACUATION STRIP BY ROW 7B IS NOT VISIBLE. FOUND EMERGENCY EVAC FLOOR STRIP PEELED UP BUT VISIBLE. RE-SECURED FLOOR STRIP IAW EMB 170 MM 33-50-02.

Part: RELIEF VALVE — LEAKING (NR 2 RESERVOIR) · airframe 11,988 hrs · 9,808 cycles

CREW REPORTED DURING CLIMB HYD 2 QTY DROPPED TO 10 PERCENT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT DEN, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 RELIEF VALVE PER EMB AMM, AND THE A/C WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 9,602 hrs · 8,069 cycles

CREW REPORTED EMERGENCY LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED ELPU NR 2 PER EMB AMM, OPS CHECK GOOD. THE A/C WAS THEN RETURNED TO SERVICE.

Part: HANDLE — MALFUNCTIONED (R1 DOOR) · airframe 9,399 hrs · 7,923 cycles

CREW REPORTED THAT THE R-1 DOOR ARMING HANDLE WAS VERY HARD TO MOVE. MAINTENANCE PERFORMED OPS CHECK OR ARMING HANDLE PER EMB AMM AND OPS CHECK GOOD.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 9,325 hrs · 7,855 cycles

WHILE AC WAS IN FOR HEAVY CHECK, A MAJOR REPAIR WAS ACCOMPLISHED DUE TO REPLACEMENT OF FRAME 80. MAINTENANCE REQUESTED EMB ENGINEERING SUPPORT AND RECEIVED ETD 2010-170/02228. MAINTENANCE REPLACED FRAME PER ETD AND SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,325 hrs · 7,855 cycles

ACFT WAS IN HEAVY CHECK, MTX REPORTED A MAJOR REPAIR DUE TO LT SEAT TRACK BEAM CORRODED BETWEEN FR 14 AND FR 19. MAINTENANCE INSTALLED DOUBLERS (2 EACH) AND FILLERS (3 EACH) IAW ETD 170/02064 AFTER REMOVING CORROSION AND FABRICATING FILLERS AND DOUBLERS IAW ETD 2010-170/02064.

Part: SENSOR — FAULTY (LE SLAT) · airframe 9,183 hrs · 7,758 cycles

CREW REPORTED, A SLAT FAIL DURING APPROACH INTO DCA. DECLARED AN EMERGENCY AND DIVERTED TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT TO TROUBLESHOOT. MAINTENANCE REMOVED AND REPLACED THE LT 2/3 O/B SLAT SKEW SENSOR AND PERFORMED OPS CHECKS PER EMB AMM. NO FURTHER FAULTS WERE FOUND AND THE A/C WAS RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,744 hrs · 7,484 cycles

CREW REPORTS L-1 DOOR EXIT SIGN IS BLANK. MAINTENANCE REMOVED AND REPLACED THE L-1 EXIT DOOR LENS/BULBS PER EMB AMM, OPS CHECK GOOD. A/C WAS THEN RETURNED INTO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 7,005 hrs · 4,158 cycles

L1 DOOR EMERGENCY LIGHT INOP. MX R&R L1 DOOR EMERGENCY BATTERY. OPS CHECKED GOOD IAW EMB 170 MM 33-50-01. PN OFF: 3400-22; SN OFF: 001383/PN ON: 3400-22; SN ON: 003944.

Part: SLIDE — MALFUNCTIONED (L1 DOOR) · airframe 4,382 hrs · 2,427 cycles

DURING A SCHEDULED EMERGENCY EVACUATION SLIDE SYSTEM OPERATIONAL CHECK OF THE L1 DOOR AND SLIDE THE OPERATIONAL CHECK FAILED. THE AIRCRAFT DOOR OPERATED NORMALLY BUT THE SLIDE PARTIALLY DEPLOYED IN A BALL SHAPE AND REMAINED IN THAT SHAPE.

Part: SENSOR — DEFECTIVE (LE SLATS) · airframe 739 hrs · 358 cycles

FLIGHT 6433, ON APPROACH THE CREW CONFIGURED THE AIRCRAFT TO FLAPS 1 AND RECEIVED A SLAT FAIL EICAS MESSAGE. THE CREW FOLLOWED THE QRH AND COULD NOT REMEDY THE PROBLEM THEN DECLARED AN EMERGENCY DUE TO THE HIGH APPROACH SPEEDS. THE LANDING WAS WITHOUT INCIDENT. MAINT REMOVED AND REPLACED 2/3 SLAT SENSOR.