N210JQ

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 32,110 hrs · 23,148 cycles

MULTIPLE DENTS ON FWD FUSELAGE AT FRA 10 TO 11 AND STR 17L TO 18L. REPAIRED IAW ETD2023-170-010467 ALSO REF VP-017657-2023 N/R #1 FOR MATERIALS,DEMENTIONS,NDT AND FINAL INSPECTION.

Part: SLIDE — PARTIAL DEPLOY (ZONE 800) · airframe 32,026 hrs · 23,079 cycles

L1 DOOR SLIDE PARTIAL DEPLOYMENT. PILOTS DISARMED DOOR, PUT VENT FLAP DOWN, SLIDE PARTIALLY DEPLOYED WHEN AGENT OPENED DOOR. R&R L1 DOOR SLIDE.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,129 hrs · 20,841 cycles

** WHILE AIRCRAFT WAS IN HEAVY CHECK ** COCKPIT FLOOR STRUCTURE CORROSION FOUND ON FLOOR STRUCTURE AT FR 12 LH SIDE BEHIND PILOT SEAT. MX REPAIRED FLOOR WEB PN 170-03237-005 IAW ETD2021-170-037719.

Part: SHEAR ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,129 hrs · 20,841 cycles

** WHILE AIRCRAFT WAS IN HEAVY CHECK ** CENTER FUSELAGE 3 SHEAR CLIP FOUND CORRODED AT FR 87 BTWN STR 28R-27R. MX REPLACED SHEAR CLIP PN 170-66041-002 IAW SRM 51-41-02,51-43-03

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,129 hrs · 20,841 cycles

WHILE AC WAS IN FOR HVY CK FOUND AFT WING TO BODY FAIRING FWD SPLICE ASSY CORRODED. MX REPLACED SPLICE PN 170-02460-401 IAW SRM 20-10-01 SEE AAR NRC# 4500985-1000-0100 FOR WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.

Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,129 hrs · 20,841 cycles

LEVEL 2 CORROSION WAS FOUND AT FWD WET AREA CROSSBEAM FR16 LH. CROSSBEAM WAS REPAIRED IAW ETD 2021-170-037104.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,129 hrs · 20,841 cycles

** WHILE AIRCRAFT WAS IN HEAVY CHECK ** CENTER FUSELAGE 3 WASTE BOX INNER DOUBLER FOUND CORRODED. MX REPAIRED DOUBLER PN 2024T3.125 IAW SRM 53-23-60 REPAIR 7.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,129 hrs · 20,841 cycles

WHILE AC WAS IN FOR HVY CK FOUND FWD WET AREA FLOOR BOARD SUPPORT ANGLE AT FR 19 LH BEHIND L1 DOOR FOUND CORRODED. MX REPLACED SUPPORT ANGLE PN 170-12320-403 IAW SRM 51-43-01 SEE AAR NRC# 4500985-1000-0079 FOR WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.

Part: RIB — CRACKED (ZONE 300) · airframe 29,129 hrs · 20,841 cycles

LH H-STAB RIB 11A AND R/H H-STAB RIB 12A FOUND CRACKED. REPLACED RIBS L/H 11A & R/H 12A IAW REPUBLIC 170EO-55-10-0004_1 AND AAR TASK CARD 4500984-3000-0074. "MAJOR" P/N'S 170-62783-001 & 170-62642-002

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 29,129 hrs · 20,841 cycles

LEVEL 2 CORROSION WAS FOUND AT CENTER FUSELAGE RH IB SEAT TRACK FR78 TO FR85. SEAT TRACK WAS REPLACED IAW SRM 51-43-03 AND 51-42-04

Part: UPPER SHEET — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,129 hrs · 20,841 cycles

** WHILE AIRCRAFT WAS IN HEAVY CHECK** FUSELAGE 3 FLOOR STRUCTURE RH UPPER SHEET FOUND CORRODED BTWN FR-85-86. MX REPLACED UPPER SHEET PN 170-86101-001 IAW SRM 51-41-01,51-43-03

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,129 hrs · 20,841 cycles

** WHILE AIRCRAFT WAS IN HEAVY CHECK** FWD LH IB SEAT TRACK BTWN FR 12-20 FOUND CORRODED. MX REPLACED SEAT TRACK PN 170-03264-001 IAW SRM 51-41-01, 51-41-02, 51-43-03, 51-43-04

Part: SHEAR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,129 hrs · 20,841 cycles

** WHILE AIRCRAFT WAS IN HEAVY CHECK** FUSELAGE 3 FLOOR STRUCTURE RH SHEAR PANEL BTWN FR 87-88 FOUND CORRODED. MX REPLACED SHEAR PANEL PN 170-91919-001 IAW SRM 51-43-01

Part: TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,129 hrs · 20,841 cycles

** WHILE AIRCRAFT WAS IN HEAVY CHECK ** FWD RH IB SEAT TRACK BTWN FR 12-29 FOUND WITH CORROSION. MX REPLACED SEAT TRACK PN 170-03263-001 IAW SRM 51-41-01, 51-41-02, 51-43-01

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,129 hrs · 20,841 cycles

WHILE AC WAS IN FOR HVY CK FOUND FUSELAGE 3 FLOOR STRUCTURE RH PANEL SUPPORT FOUND CORRODED AT FR 89. MX REPLACED PANEL SUPPORT PN 170-86181-005 IAW SRM 51-43-03. SEE AAR NRC# 4500985-1000-0062 FOR WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.

Part: SHEAR WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,129 hrs · 20,841 cycles

** WHILE AIRCRAFT WAS IN HEAVY CHECK** FWD WET AREA FWD RH SHEAR WEB FROM FR 12-15 CORRODED. MX REPLACED SHEAR WEB PN 170-05663-003 IAW SRM 51-41-02, 51-43-02

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,285 hrs · 18,489 cycles

R2 EMERGENCY EXIT SIGN INOP. R&R R2 DOOR EMERGENCY EXIT SIGN BATTERY.

Part: SLIDE — PARTIAL DEPLOY (R2 DOOR) · airframe 25,315 hrs · 17,797 cycles

R2 SLIDE PARTIALLY DEPLOYED. FERRIED TO IND. R&R R2 DOOR SLIDE AND FLEXBALL CABLE.

Part: DOUBLER — CORRODED (THRESHOLD) · corrosion level 2 · airframe 24,858 hrs · 17,472 cycles

WHILE AC WAS IN FOR HVY CK FOUND CHAFFING DAMAGE ON FWD CARGO DOOR SURROUND LOWER THRESHOLD DOUBLER. AAR MX REMOVED AND REPLACED PN 170-67115-001 FWD CARGO DOOR SURROUND LOWER THRESHOLD DOUBLER IAW SRM 51-43-02. FOR WORK PERFORMED SEE AAR WC# 45000430-1000-0061. AC REMAINS IN YQG FOR COMPLETION.

Part: FLOORBEAM — CORRODED (FRAME 90) · corrosion level 2 · airframe 24,858 hrs · 17,472 cycles

WHILE AC WAS IN FOR HVY CK FOUND REAR FUSELAGE FLOOR STRUCTURE AT FR 90 GUSSETS AT RBL 14 AND RBL 32 HAVE CORROSION. MX REMOVED AND REPLACED REAR FUSELAGE FLOOR STRUCTURE AT FR 90 GUSSETS PN 170-60257-001 AT RBL 14 AND RBL 32 IAW SRM 51-41-02. SEE AAR WC# 4500430-2000-0021 FOR WORK PERFORMED. AC REMAINS IN YQR FOR COMPLETION.

Part: SUPPORT FITTING — CRACKED (LT ELEVATOR) · airframe 24,858 hrs · 17,472 cycles

WHILE AC WAS IN FOR HVY CK FOUND SUSPECTED CRACK ON LH OTBD ELEVATOR ACTUATOR SUPPORT FITTING. MX REMOVED CRACK BY DRILLING OUT DAMAGED AREA OF SUPPORT FITTING PN 170-62175-405 IAW ETD 2019-170-110817. SEE AAR WC# 4500430-3000-0009 FOR WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.

Part: SKIN — NICKED (FWD CARGO DOOR) · airframe 24,858 hrs · 17,472 cycles

MAINTENANCE REPORTED A NICK ON THE FORWARD CARGO INTERNAL SKIN AT AFT SIGHT GLASS. MAINTENANCE REPAIRED THE NICK ON THE FORWARD CARGO INTERNAL SKIN AT AFT SIGHT GLASS IAW EMB ETD2019-170-107755. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SKIN — NICKED (FWD CARGO DOOR) · airframe 24,858 hrs · 17,472 cycles

MAINTENANCE REPORTED A NICK ON THE FORWARD CARGO INTERNAL SKIN AT SIGHT GLASS SECOND FROM FWD. MAINTENANCE REPAIRED THE NICK ON THE FORWARD CARGO INTERNAL SKIN AT SIGHT GLASS SECOND FROM FWD. IAW EMB ETD2019-170-107755. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SKIN — NICKED (FWD CARGO DOOR) · airframe 24,858 hrs · 17,472 cycles

MAINTENANCE REPORTED A NICK ON THE FORWARD CARGO INTERNAL SKIN AT SIGHT GLASS THIRD FROM FWD. MAINTENANCE REPAIRED THE NICK ON THE FORWARD CARGO INTERNAL SKIN AT SIGHT GLASS THIRD FROM FWD IAW EMB ETD2019-170-107755. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SKIN — NICKED (FWD CARGO DOOR) · airframe 24,858 hrs · 17,472 cycles

MAINTENANCE REPORTED A NICK ON THE FORWARD CARGO INTERNAL SKIN AT THE FWD SIGHT GLASS. MAINTENANCE REPAIRED THE NICK ON THE FORWARD CARGO INTERNAL SKIN AT THE FWD SIGHT GLASS IAW EMB ETD2019-170-107755. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: RIB — CRACKED (ZONE 300) · airframe 24,944 hrs · 19,624 cycles

CRACK ON THE RT HORIZONTAL STAB RIB 12 AT UPPER SKIN ATTACHMENT, AFT OF SPAR 1. REMOVED AND REPLACED THE RIB.

Part: CROSSBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

FWD CENTER AND RT CROSSBEAM CORRODED FRAME 17. BLENDED AND CUT OUT DAMAGE AREA, INSTALLED A REPAIR ANGLE ON CROSSBEAM IAW SRM 53-00-10, REPAIR 03.

Part: DOUBLER — CORRODED (FRAMES 19-20) · corrosion level 2 · airframe 24,944 hrs · 196,924 cycles

LEFT FLOOR DOUBLER CORRODED FRAME 19-20. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-41-02, 51-43-04, AND 51-45-00.

Part: SEAL REST — CORRODED (FWD CARGO DOOR) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

CORROSION ON FWD CARGO DOOR SEAL RESTS. REMOVED AND REPLACED THE SEAL RESTS IAW SRM 51-23-06.

Part: ATTACH FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

LT OTBD MONUMENT ATTACH FITTING CORRODED FRAME 19. REMOVED AND REPLACED THE ATTACH FITTING IAW SRM 51-43-03.

Part: DOUBLER — CORRODED (FRAMES 46-48) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

CORROSION ON INTERNAL DOUBLER OF PANEL 192BL. REMOVED AND REPLACED INTERNAL DOUBLER IAW SRM 51-41-02 AND TOP COATED FASTENER IAW SRM 51-23-06

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

WHILE IN HEAVY CHECK, AFT SERVICE DOOR BEAM HAS CORROSION AROUND FWD AND AFT GIRT BAR FITTINGS AS MARKED. REMOVED AND REPLACED AFT SERVICE DOOR THRESHOLD BEAM AND RESTORED SURFACE PROTECTION REF SRM 51-41-01, 51-41-02, 51-43-04, 51-42-01, 51-43-03, 51-23-04, 51-23-06, 53-23-00 AND AMM 53-23-25, 51-41-01.

Part: BEAM — CORRODED (FRAMES 85-87) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

AFT PAX DOOR BEAM HAS CORROSION AROUND FWD AND AFT GIRT BAR FITTINGS. REPLACED THE AFT PAX DOOR THRESHOLD BEAM AND CENTER SEAL REST IAW SRM 51-41-01, 51-43-03, AND 51-43-04.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

LEFT OTBD SHEAR PANEL SPLICE CORRODED FRAMES 87-88. REMOVED AND REPLACED THE SHEAR PANEL SPLICE IAW SRM 51-42-02, 51-40-03, 51-23-04, AND 51-40-04.

Part: DOUBLER — CORRODED (FRAMES 46-48) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

CORROSION INTERNAL DOUBLER OF PANEL 192CR. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-41-02 AND TOP COATED FASTENERS IAW SRM 51-23-06.

Part: SEAT TRACK — CORRODED (FRAMES 83-84) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

AFT WET AREA AFT END OF LT CENTER SEAT TRACK IS CORRODED. PERFORMED A SPLICE REPAIR IAW ENGINEERING ETD2017-170-065008.

Part: SHEAR PLATE — CORRODED (FRAMES 86-87) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

WHILE IN HEAVY CHECK, CORROSION WAS FOUND ON THE RT SHEAR PLATE. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-21-00, 51-42-02, AND 51-42-02.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

WHILE IN HEAVY CHECK, CORROSION FOUND ON THE RT CENTER GUSSET, FRAME 90. REMOVED AND REPLACED THE GUSSET IAW SRM 51-23-05

Part: FLOOR SUPPORT — CORRODED (FRAME 14) · airframe 24,944 hrs · 19,624 cycles

FWD RT FLOOR SUPPORT CORRODED FRAME 14. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-43-04, AND 51-41-02.

Part: SEAT TRACK — CORRODED (FRAMES 14-19) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

LEFT CENTER SEAT TRACK CORRODED, FRAMES 14 - 19. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-01 , 51-41-02, AND 51-43-04.

Part: FITTING — CORRODED (FRAME 16) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

FWD LT LAVATORY FLOOR FITTING CORRODED AT FRAME 16. REMOVED AND REPLACED THE FITTING IAW SRM 51-43-03.

Part: DOUBLER — CORRODED (FRAME 16) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

FWD LT FLOOR DOUBLER CORRODED FRAME 16. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-41-02, 51-40-02, 51-23-04, AND 51-23-06.

Part: DOUBLER — CORRODED (FRAME 90) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

DURING HEAVY CHECK, CORROSION WAS FOUND ON THE AFT WET AREA FLOORBEAM AT FRAME 90 ON RT SIDE DOUBLER. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FRAMES 14-17) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

FWD RT CENTER SEAT TRACK CORRODED FRAMES 14 - 17. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-43-03, 51-43-04, 51-23-04, 51-23-05, 51-23-06, 51-41-01, 51-41-02, AND CPM 51-25-00.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

FWD RT FLOOR SUPPORT CORRODED FRAME 16. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01, 51-23-06.

Part: FLOORBEAM — CORRODED (FRAME 89) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

WHILE IN HEAVY CHECK, CORROSION WAS FOUND ON THE FLOORBEAM AT FRAME 89. REMOVED AND REPLACED IAW SRM 51-21-00, & 51-42-01.

Part: INTERCOSTAL — CORRODED (FRAMES 90-91) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

AFT WET AREA RT AFT INTERCOSTAL CORRODED AT FRAMES 90 - 91. REPAIRED IAW ETD2017-170-065844.

Part: FLOOR SUPPORT — CORRODED (FRAMES 84-85) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

CORROSION ON THE RT OTBD FLOOR SUPPORT AT FRAMES 84 - 85. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01, 51-41-02, AND 51-43-04.

Part: UPPER SHEET — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

LEFT INBD UPPER SHEET CORRODED, FRAMES 85-86. REMOVED AND REPLACED THE UPPER SHEET IAW SRM'S 51-41-01, AND 51-43-03.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

CENTER GUSSET AT FRAME 90 CORRODED. REMOVED AND REPLACED THE GUSSET IAW SRM 51-43-03, AND 51-23-06.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

RIGHT OTBD SHEAR PANEL SPLICE CORRODED, FRAMES 87 - 88. REMOVED AND REPLACED THE SHEAR PANEL SPLICE IAW SRM 51-42-02, 51-40-03, 51-23-04, 51-40-02, 51-23-06, AND 51-40-04.

Part: BEAM — CORRODED (FRAMES 86-89) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

CORROSION ON BEAM IN AFT WET AREA FRAMES 86-89. REMOVED AND REPLACED THE BEAM.

Part: SHEAR ANGLE — CORRODED (FRAMES 84-85) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

AFT WET AREA SHEAR TIE AFT OF RT CENTER SEAT TRACK CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, AND 51-43-03.

Part: ATTACH FITTING — CORRODED (WNG-BDY FAIRING) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

FWD WING-TO-FUSELAGE FAIRING AFT LOWER ATTACH FLANGE. REMOVED AND REPLACED THE ATTACH FLANGE IAW SRM 51-40-02, 51-23-04, 51-41-02, 51-42-02, SRM 51-23-06, AND 51-25-00-910-001.

Part: FLOOR SUPPORT — CORRODED (FRAMES 13-16) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

FWD LEFT OTBD FLOOR SUPPORT CORRODED FRAMES 13-16. REMOVED AND REPLACED THE LT OTBD FWD FLOOR SUPPORT IAW EAMS SRM 51-43-04,51-41-02.

Part: SHEAR TIE — CORRODED (FRAME 88) · corrosion level 2 · airframe 24,944 hrs · 19,624 cycles

CORROSION SHEAR TIE AT FRAME 88, STRINGER 26R - 27R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, AND 51-41-02.

Part: WIRE HARNESS — DEFECTIVE (ENTRY DOOR) · airframe 19,161 hrs · 13,626 cycles

RADIO COM MAIN ENTRY DOOR SHOWING NOT CLOSED. COMPLIED WITH MAINT PROCEDURE AND DEFERRED IAW MEL52-70-00-1 CAT C TICKET NUMBER 149164. REMOVED AND REPLACED HARNESS IAW AMM 52-72-20 OPS CHK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 17,339 hrs · 12,493 cycles

L2 DOOR SLIDE BUSTLE LENS MISSING. R & R LENS FOR L2 DOOR SLIDE BUSTLE IAW SRM 51-21-03 AND AMM 25-00-23.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,022 hrs · 12,294 cycles

FLOOR EMERGENCY LIGHT IN FRONT OF WARDROBE CLOSET ARE BURNED OUT . R & R THE EMERGENCY LIGHT IAW AMM 33-50-21.

Part: PROXIMITY SENSOR — MALFUNCTIONED (L2 DOOR) · airframe 16,248 hrs · 11,796 cycles

PAX DOOR OPEN L2 INDICATION. ADJUSTED L2 DOOR CLOSED PROXIMITY SENSOR IAW AMM 52-72-21. OPS CHECK GOOD.

Part: SHROUD — CRACKED (EMERGENCY LIGHT) · airframe 15,736 hrs · 11,469 cycles

PHOTOLUMINESCENT STRIP SHROUD CRACKED AT SEAT 6B. R & R PHOTOLUMINESCENT STRIP SHROUD NEAR SEAT 6B REF AMM 33-50-21.

Part: SIGN — CRACKED (EMERGENCY LIGHTS) · airframe 15,443 hrs · 11,282 cycles

AFT RT SIDE EMERGENCY EXIT SIGN IS CRACKED. R & R EMERGENCY EXIT SIGN IAW AMM 33-50-17.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 13,632 hrs · 10,262 cycles

NR 2 EMERGENCY LIGHTS ONLY LAST 14 MINUTES WHEN DOING JC S33-50-01-720-801A. R & R THE NR 2 EMERGENCY BATTERY PACK IAW AMM 33-50-01.

Part: INDICATOR — OUT OF ADJUST (R1 DOOR LATCH) · airframe 13,584 hrs · 10,231 cycles

R1 DOOR LATCH INDICATOR NOT SHOWING "GREEN" WHEN DOOR IS ARMED. CLEANED AND ADJUSTED DOOR LATCH INDICATOR REF AMM 52-41-00. OPS CHECK GOOD.

Part: WIRE HARNESS — DAMAGED (L2 DOOR) · airframe 13,401 hrs · 10,094 cycles

L2 DOOR, SERVICE DOOR, NOT INDICATING CLOSED OR OPEN. R & R L2 DOOR ELECTRICAL WIRE HARNESS IAW AMM 52-72-21. OPS CHECKED GOOD.

Part: SENSOR — OUT OF ADJUST (SERVICE DOOR) · airframe 13,386 hrs · 10,087 cycles

FORWARD RT SERVICE DOOR HAD AN OPEN INDICATION STARTING AT FL280, THEN WENT BACK TO GREEN INDICATION, CLOSED. ADJUSTED FWD SERVICE DOOR CLOSED SENSOR, OPS CHECKED GOOD IAW MM 52-41-20.

Part: PIN — BACKED OUT (L1 DOOR) · airframe 11,554 hrs · 8,861 cycles

DOOR PASSENGER FWD OPEN FOR L1 DOOR, ANNUNCIATED DURING FLIGHT. R & R PIN THAT WAS BACKED OUT ON L1 DOOR CLOSED SENSOR IAW AMM 52-72-20, OPS CHECKED GOOD.

Part: INTERCOSTAL — CORRODED (FRAMES 90-91) · corrosion level 2 · airframe 11,022 hrs · 8,692 cycles

CORROSION ON LT INTERCOSTAL FRAMES 90-91. R & R INTERCOSTAL.

Part: UPPER SHEET — CORRODED (FRAMES 85-86) · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND ON LEFT UPPER SHEET, FRAMES 85-86. R & R UPPER SHEET.

Part: DOUBLER — CORRODED (FRAMES 19-20) · corrosion level 2 · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND LT DOUBLER FRAMES 19-20. R & R DOUBLER.

Part: CLOSEOUT PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND ON CLOSE OUT PLATE. R & R CLOSE OUT PLATE.

Part: SEAT TRACK — CORRODED (FRAMES 14-17) · corrosion level 2 · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND RT SEAT TRACK FRAMES 14, 16, & 17. R & R SEAT TRACK.

Part: FINGER DOUBLER — CHAFED (ZONE 100) · airframe 11,429 hrs · 8,785 cycles

CHAFE ON FWD FINGER DOUBLER BY FWD LATCH FWD CARGO DOOR FRAME. R & R FWD FINGER DOUBLER FWD CARGO REF SRM 51-43-02. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-20) · corrosion level 2 · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND ON RT AFT FLOOR SUPPORT FRAMES 17-20. R & R FLOOR SUPPORT.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND ON RT SHEAR PLATE FRAMES 87-88. R & R SHEAR PLATE.

Part: SEAL DEPRESSOR — CORRODED (CARGO DOOR FRAME) · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND ON CENTER SEAL DEPRESSION BY NR 3 LATCH FWD CARGO DOOR FRAME. R & R CENTER SEAL REST. MAJOR REPAIR

Part: BEAM — CORRODED (FRAMES 86-89) · corrosion level 2 · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND ON RT BEAM AT FRAMES 86-89. R & R RT BEAM.

Part: FLOORBEAM — CORRODED (FRAME 84) · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND ON FLOORBEAM RT FRAME 84. REPAIRED FLOORBEAM IAW ETD 2013-170-062806. MAJOR REPAIR.

Part: UPPER SHEET — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND ON RT UPPER SHEET FRAMES 85-86. R & R RT UPPER SHEET .

Part: DOUBLER — CORRODED (FRAMES 13-16) · corrosion level 2 · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND ON FLOOR DOUBLER LT FRAMES 13-16. R & R LT FLOOR DOUBLER.

Part: BEAM — CORRODED (ZONE 100) · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND LT BEAM FRAMES 86-89. R & R BEAM.

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND ON RT CENTER SPLICE AT FRAME 89. R & R GUSSET.

Part: SEAT TRACK — CORRODED (FRAME 85) · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND ON SEAT TRACK FRAME 85. BLENDED AREA, REMOVED CORROSION, INSTALLED REPAIR DOUBLER IAW ETD 2013-170-062834A. MAJOR REPAIR.

Part: GUSSET — CORRODED (FRAME 90) · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND ON RT GUSSET PLATE AT FRAME 90. R & R GUSSET.

Part: CLOSEOUT PANEL — CORRODED (ZONE 100) · airframe 11,429 hrs · 8,785 cycles

CORROSION ON CLOSE OUT PLATE. R & R CLOSE OUT PANEL. MAJOR REPAIR

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND ON RT FWD FLOOR SUPPORT FRAMES 12-14. R & R FLOOR SUPPORT.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND ON GUSSET LT CENTER AT FRAME 90. R & R GUSSET.

Part: SEAT TRACK — CORRODED (FRAMES 14-16) · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND ON FWD LT SEAT TRACK FRAMES 14-16. R & R SEAT TRACK.

Part: INTERCOSTAL — CORRODED (FRAMES 88-89) · corrosion level 2 · airframe 11,429 hrs · 8,785 cycles

CORROSION FOUND ON AFT INTERCOSTAL BETWEEN FRAMES 88-89. R & R INTERCOSTAL.

Part: INDICATOR — FALSE INDICATION (L1 DOOR) · airframe 10,305 hrs · 7,963 cycles

L1 DOOR DOES NOT SHOW LOCKED ON MFD. TOP LT INDICATOR DOES NOT SHOW GREEN ON DOOR. OPS CHECK L1 DOOR IAW AMM 52-72-20. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE INDICATION (L1 DOOR) · airframe 10,290 hrs · 7,950 cycles

L1 DOOR SHOWING OPEN ON MFD WHEN VERIFIED CLOSED. PERFORMED SEVERAL OPS CHECKS OF DOOR INDICATION IAW AMM 52-12-52. ALL INDICATIONS NORMAL AT THIS TIME.

Part: DOOR — DIRTY (L2) · airframe 8,865 hrs · 6,907 cycles

L2 DOOR INDICATION NOT SHOWING CLOSED, YELLOW CIRCLE WITH BLACK X. CLEANED AND LUBED L2 DOOR AND PERFORMED SYSTEMS CHECK IAW AMM 52-72-21. OPS CHECK GOOD.

Part: WIRE HARNESS — DEFECTIVE (PAX DOOR) · airframe 8,863 hrs · 6,905 cycles

AFT PAX DOOR INDICATION INOP ON MFD STATUS PAGE. REMOVED AND REPLACED L2 DOOR SENSOR HARNESS IAW AMM 52-72-21, OPS CHECK GOOD.

Part: PROXIMITY SWITCH — MALFUNCTIONED (DOOR) · airframe 8,861 hrs · 6,901 cycles

MFD DOOR INDICATION AS WELL AS EICAS MESSAGE DOOR PAX AFT OPEN IN FLIGHT. PERFORMED FIM 52-72-00-810-802A. RESET PROX SWITCH, OPS CHECK GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 6,792 hrs · 5,334 cycles

MAJOR REPAIR - SKIN DENT ON RT FF FROM FR6 TO AFT OF FR8 AND STR 13R TO 11R. REMOVED AND REPLACED SKIN IAW EMB 170 SRM 51-41-02, 51-41-03, AND ETD 2011-170-108232 REV B. PAINTED IAW EMB 170 SRM 51-23-06. RVSM SURVEY REF AMM 34-15-00.

Part: CONTACT — LACK OF LUBE (PAX DOOR) · airframe 6,315 hrs · 4,989 cycles

WHILE IN FLIGHT AT FL290 DOOR PAX FWD OPEN EICAS MESSAGE CAME ON, MESSAGE WAS THEREAFTER INTERMITTENT. LUBRICATED L1 DOOR CONTACTS IAW EMB 170 MM 52-11-20-06. OPS CHECK GOOD IAW EMB 170 MM 52-11-20-06.

Part: INDICATOR — OUT OF ADJUST (CABIN DOOR) · airframe 6,219 hrs · 4,917 cycles

LATCH INDICATOR IS NOT INDICATING GREEN/CLOSED ON MAIN CABIN DOOR. MAINTENANCE DEFERRED. AUG 26 - CLEARED MEL, ADJUSTED LATCH INDICATOR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 5,884 hrs · 4,661 cycles

MAJOR REPAIR - FOUND CRACK ON LT FWD FUSELAGE, LOCATED BETWEEN FR11 AND FR12, STR 15L AND STR 17L. REPAIRED SKIN IAW ETD 2011-170*101422 REV A.

Part: SENSOR — MALFUNCTIONED (LE SLAT) · airframe 3,401 hrs · 2,839 cycles

ON DEPARTURE OUT OF DCA WHILE RETRACTING THE FLAPS FROM 2 TO 1, RECEIVED SLAT FAIL MESSAGE. SLATS INDICATED AMBER 3 AND FLAPS WERE INDICATED GREEN DASHES. COMPLIED WITH QRH, DIVERTED TO IAD. NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. MAINTENANCE CLEARED THE SF-ACE INHIBITS AND PERFORMED OPS CHECKS OF THE SLAT/FLAP SYSTEM IAW EMB 175 FIM 27-81-00-810-807. MAINTENANCE LATER REMOVED AND REPLACED BOTH RT OUTBOARD SLAT SKEW SENSORS AND THEN COMPLIED WITH SI 278065 TO REPLACE THE RT SLAT 3/4 HARNESS.

Part: SENSOR — UNSERVICEABLE (LE SLAT) · airframe 2,967 hrs · 2,493 cycles

WHILE BEGINNING APPROACH, CALLED FOR FLAPS 1 AND IMMEDIATELY RECEIVED EICAS MESSAGES: SLAT FAIL, SHAKER ANTICIPATED, AOA LIMIT FAIL, AND SPOILER FAULT. DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED THE RT 2/3 AND 3/4 SLAT SKEW SENSORS IAW EMB 175 MM 27-83-01.