N134HQ

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,947 hrs · 28,918 cycles

RH WING UPPER SURFACE CRACKED O/B OF RIB 10 DOUBLER AND I/B OF # 3 SPOILER I/B HINGE AFT OF REAR SPAR FASTNER LINE. REPAIRED CRACK IAW ETD2023-170-027242 REV A. ALSO REF VP-042017-2023 N/R 6 C1 THRU C3 FOR WORK PERFORMED.

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 34,885 hrs · 26,770 cycles

WHILE ACFT IN HEAVY CHECK, MAINTENANCE FOUND CORROSION ON THE SHEAR CLIPS ON FR 83, 84, 85 AND 86 AT STR 27R-28R. REMOVED AND REPLACED SHEAR CLIPS ON FR 83,84,85 AND 86 AT STR 27R-28R. IAW EMB SRM 51-40-08. ACFT REMAINS IN HEAVY CHECK.

Part: PYLON — CRACKED (ZONE 400) · airframe 34,618 hrs · 26,557 cycles

ENG #2 AFT INBD PYLON LUG CRACKED. REPAIRED #2 PYLON IAW ETD2022-170-008394 REV A ALSO REF VP-009415-2022 N/R #10 AND #13 FOR WORKED PERFORMED. PYLON WILL BE INSTALLED AT SDF.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 31,834 hrs · 24,543 cycles

DURING HEAVY CHECK, SHEAR CLIP AT FR 88 STGR 27R-28R FOUND TO BE CORRODED. REPLACED PER SRM 51-40-08.

Part: SIGN — DEFECTIVE (CABIN) · airframe 31,253 hrs · 24,096 cycles

L2 DOOR EXIT IDENTIFIER SIGN ONLY HALF WORKS. R&R L2 DOOR EXIT IDENTIFIER SIGN PER AMM 33-50-15.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,253 hrs · 24,096 cycles

SUPPLEMENTAL INFORMATION: EMERGENCY LIGHT BATTERY FAULT. R&R AFT LT AND RT EMERGENCY BATTERIES IAW AMM 33-50-01.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,496 hrs · 23,589 cycles

ELPU 2 FAILED FUNCTIONAL TEST. R&R ELPU 2 IAW AMM 33-50-01.

Part: WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 29,574 hrs · 22,958 cycles

L1 EXIT SIGN LIGHT INOP. RESECURED L1 DOOR EXIT SIGN WIRES IAW AMM 33-50-15.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,175 hrs · 22,673 cycles

COCKPIT EMERGENCY LIGHT INOP. R&R LIGHT IAW AMM 33-50-03.

Part: SKIN — CRACKED (RT WING) · airframe 29,159 hrs · 22,661 cycles

DURING HEAVY CHECK MAINTENANCE FOUND THE RH WING CRACKED AT RIB 4-5 NEAR DOUBLER. INSTALLED FILLER, DOUBLER AND EXTERNAL DOUBLER IAW EMB ETD2019-170-084215 REV C. A/C REMAINS IN CHECK.

Part: CABLE — BINDING (R1 DOOR) · airframe 27,741 hrs · 21,687 cycles

R1 DOOR HARD TO OPEN. REPLACED R1 DOOR SLIDE CABLE WITH UPGRADED CABLE, OPS CHECK GOOD, REF JOB CARD R170EO-52-41-0002.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 27,741 hrs · 21,687 cycles

WINDSHIELD 1 CRACKED, RETURNED TO FIELD. A/C FERRIED TO CMH, R&R CAPT WINDSHIELD IAW AMM 56-11-00.

Part: CABLE — BROKEN (R2 DOOR) · airframe 25,957 hrs · 20,372 cycles

R2 DOOR ARMING HANDLE STIFF TO MOVE. COMPLIED WITH PART IV OF SB 170-52-0058 R&R R2 ESCAPE SLIDE FLEXBALL CABLE IAW AMM 52-42-40. OPS CHECK GOOD.

Part: SKIN — DENTED (FRAME 89) · airframe 25,825 hrs · 20,263 cycles

SKIN DENTED BY LAVATORY WASTE RECEPTACLE PANEL NEAR FRAME 89, STRINGER 29R. REPAIRED IAW ETD2018-170-029774.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,825 hrs · 20,263 cycles

WHILE THE ACFT WAS OUT OF SERVICE FOR HEAVY MAINT CHECK, CORROSION WAS FOUND AT CENTER FUSELAGE III AFT WET AREA FR 90 AT LT SPLICE. REMOVED SPLICE MADE NEW LOCATED, DRILLED AND ALODINED NEW FR 90 LT SPLICE AND INSTALLED REF SRM 51-41-02 APPLIED TOP COAT REF SRM 51-23-06, CPM 51-25-00.

Part: SLIDE — CRACKED (PAX DOOR) · airframe 25,825 hrs · 20,263 cycles

WHILE ACFT WAS OUT OF SERVICE FOR HEAVY MAINT, MAINT FOUND AFT PAX DOOR SLIDE BACK BOARD CRACKED. REMOVED AND REPLACED AFT PAX DOOR SLIDE IAW AMM 25-65-01. ACFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SUPPORT ANGLE — CORRODED (FRAMES 86-87) · corrosion level 2 · airframe 25,825 hrs · 20,263 cycles

CORROSION ON THE INTERNAL SUPPORT ANGLE BRACKETS, FWD AND AFT. DRAIN MAST SUPPORT FRAMES 86 - 87, STRINGER 26R - 28R. REMOVED AND REPLACED THE SUPPORT ANGLE BRACKETS IAW EAMS W/O H6153.

Part: RIB — GOUGED (RT WING) · airframe 25,825 hrs · 20,263 cycles

RIGHT WING RIB GROUP 4 FASTENER HOLES SHOW DAMAGE INDICATIONS ALONG ENTIRE LENGTH. REPAIRED IAW ETD2018-170-030302, REV B.

Part: RIB — DAMAGED (LT WING) · airframe 25,825 hrs · 20,263 cycles

LEFT WING RIB 4A GROUP 1 FASTENER HOLES SHOW DAMAGE INDICATIONS ALONG THE ENTIRE LENGTH OF HOLE BORES. REPAIRED THE RIB IAW ETD2018-170-030302, REV B.

Part: BEARING — EXCESS PLAY (HORIZONTAL STAB) · airframe 25,825 hrs · 20,263 cycles

RIGHT HORIZONTAL STAB BEARING ON HINGE FITTING HAS EXCESS PLAY. REPAIRED IAW ETD2018-170-031803.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,285 hrs · 20,263 cycles

DURING HEAVY CHECK, CORROSION AT FR 19 APPROX 35" L OBL. REMOVED AND REPLACED SUPPORT AT FR 19 REF SRM 51-40-08. RESTORED SURFACE FINISH REF SRM 51-23-05, 51-23-06. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: GUSSET — CORRODED (FRAME 15) · corrosion level 2 · airframe 25,825 hrs · 20,263 cycles

DURING HEAVY CHECK, CORROSION ON THE GUSSET AT FRAME 15 + 8", LBL 10. BLENDED THE CORROSION. LOCATED , DRILLED,AND INSTALLED A NEW GUSSET IAW SRM 51-41-02.

Part: SEAT TRACK — DAMAGED (FRAMES 43-59) · corrosion level 2 · airframe 25,825 hrs · 20,263 cycles

PASSENGER CABIN RT INBD SEAT TRACK, FRAMES 43 TO 59 CORRODED AND GOUGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08, SRM 51-42-01, AND 51-43-04.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,825 hrs · 20,263 cycles

DURING HEAVY CHECK, CORROSION AT FR 13+6" RT SILL. REMOVED AND REPLACED FR 13+6" RT SILL REF SRM 51-40-08. RESTORED SURFACE FINISH REF SRM 51-23-05, 51-23-06. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SEAT TRACK — CORRODED (FRAMES 30-34) · corrosion level 2 · airframe 25,825 hrs · 20,263 cycles

PASSENGER CABIN LT INBD SEAT TRACK AT FRAMES 30 TO 34 CORRODED. BLENDED AND FOUND OUT OF LIMITS IAW SRM 53-21-10. FABRICATED, LOCATED, DRILLED, AND INSTALLED THE LT INBD SEAT TRACK IAW SRM 51-23-04, 51-23-05, AND 51-23-06.

Part: BEAM — CORRODED (FRAME 85) · corrosion level 2 · airframe 25,825 hrs · 20,263 cycles

DURING HEAVY CHECK, FOUND THE AFT WET AREA HAS CORROSION ON THE UPPER SHEET , RIGHT BEAM, FRAME 85. BLENDED THE DAMAGE AND FOUND OUT OF LIMITS IAW SRM 51-75-16. REMOVED AND REPLACED THE UPPER SHEET RT BEAM IAW SRM 51-41-01, AND 51-43-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,825 hrs · 20,263 cycles

DURING HEAVY CHECK. PASSENGER CABIN LT HAND O/B SEAT TRACK FR 43 TO 59. BLENDED FOUND OUT OF LIMITS, REMOVED AND REPLACED SEAT TRACK AND APPLIED TOPCOAT REF SRM 51-40-08, 51-23-06 PO 231630. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SEAT TRACK — CORRODED (FRAMES 21-34) · corrosion level 2 · airframe 25,825 hrs · 20,263 cycles

PASSENGER CABIN RT INBD SEAT TRACK, FRAMES 21 TO 34 CORRODED. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-10. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-43-01, 51-43-02, AND 51-41-01.

Part: STRUCTURE — CORRODED (FRAME 89) · corrosion level 2 · airframe 25,825 hrs · 20,263 cycles

DURING HEAVY CHECK, AFT WET AREA AT FRAME 89 STRUCTURE HAS CORROSION RIGHT SIDE NEAR DRAIN RECEPTACLE. REMOVED AND REPLACED THE STRUCTURE IAW SRM 51-41-01, AND 51-43-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,825 hrs · 20,263 cycles

DURING HEAVY CHECK, AFT CENTER FUSELAGE III FRAME 86-88 RIGHT SIDE FLOORBEAM HAS CORROSION AS MARKED EFFECTING THE CROSSBEAM. BLENDED OUT DAMAGE FOUND OUT OF LIMITS, REMOVED AND REPLACED RT SHEAR PANEL AT FR 86-88 REF SRM 51-40-02, SRM 53-23-10. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SPLICE — CORRODED (FRAME 90) · corrosion level 2 · airframe 25,825 hrs · 20,263 cycles

DURING HEAVY CHECK, AFT WET AREA AT FRAME 90 HAS CORROSION ON SPLICE CAP. BLENDED OUT THE DAMAGE AND FOUND OUT OF LIMITS IAW SRM 51-75-16. FABRICATED A REPLACEMENT IAW SRM 51-41-02, AND 51-23-04. INSTALLED THE SPLICE CAP IAW SRM 51-41-02.

Part: SPLICE — CORRODED (FRAME 90) · corrosion level 2 · airframe 25,825 hrs · 20,263 cycles

DURING HEAVY CHECK, AFT WET AREA FRAME 90 HAS CORROSION AT THE CENTER SPLICE AFT. BLENDED THE DAMAGE AND FOUND OUT OF LIMITS IAW SRM 51-75-16. REMOVED THE SPLICE IAW SRM 51-43-03, FABRICATED A NEW SPLICE IAW SRM 51-43-03, AND 51-23-04. INSTALLED IAW SRM 51-43-03 .

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,825 hrs · 20,263 cycles

DURING HEAVY CHECK, AFT WET AREA CENTER FUSELAGE III CROSSBEAM (SHEAR PANEL) HAS CORROSION AS MARKED FRAME 87-88. REMOVED AND REPLACED CENTER SHEAR PANEL FR 87-88 REF SRM 51-42-01. RESTORED SURFACE FINISH REF E175 SRM 51-23-05, 51-23-06. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR SLIDE) · airframe 25,078 hrs · 19,710 cycles

R1 CABIN DOOR IS DIFFICULT TO ARM AND DISARM. ADJUSTED R1 DOOR GIRT BAR PLATES, OPS CHECK GOOD REF AMM 52-41-41.

Part: FLASHLIGHT — MALFUNCTIONED (COCKPIT) · airframe 22,322 hrs · 17,607 cycles

CREW REPORTED THAT THE CAPTAIN`S FLASHLIGHT WAS VERY DIM. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAMES 10-11) · corrosion level 2 · airframe 21,255 hrs · 16,771 cycles

DURING HEAVY CHECK, FLOOR SUPPORT AT FRAME 10-11 NEAR AFT END OF RT INBD FLIGHT DECK SEAT IS CORRODED. MAINTENANCE R & R FLOOR SUPPORT AT FRAME 10-11 NEAR AFT END OF RT INBD FLIGHT DECK SEAT IAW SRM 51-41-02, 51-45-00.

Part: BEAM — CORRODED (FRAME 87) · airframe 21,255 hrs · 16,771 cycles

DURING HEAVY CHECK, RT LONGITUDINAL BEAM +10.748, FRAME 87 IS CORRODED. MX REPAIRED CORROSION DAMAGE TO RT LONGITUDINAL BEAM +10.748 FRAME 87 BY BLENDING AND INSTALLING DOUBLER IAW SRM 53-23-10, 51-31-00, 51-42-02.

Part: FINGER DOUBLER — CORRODED (ZONE 100) · airframe 21,255 hrs · 16,771 cycles

DURING HEAVY CHECK, FWD CARGO AFT FINGER DOUBLER IS CORRODED. MAINTENANCE REPAIRED CORROSION BY BLENDING FWD CARGO AFT FINGER DOUBLER IAW ETD 2016-170-036934.

Part: SPLICE PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 21,255 hrs · 16,771 cycles

DURING HEAVY CHECK, WAS REPORTED THAT LT OTBD SPLICE PLATE AT FRAMES 88-87 IS CORRODED. MAINTENANCE R & R LT OTBD SPLICE PLATE AT FRAMES 88-87 IAW SRM 51-42-02. PN 170-65644-001, SPLICE PLATE.

Part: BEAM — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,255 hrs · 16,771 cycles

DURING HEAVY CHECK, LT LONGITUDINAL BEAM -10.784 AT FRAME 87 IS CORRODED. MX REPAIRED CORROSION BY BLENDING OUT AND INSTALLING A DOUBLER IAW SRM 53-23-10, 51-41-02, 51-23-04.

Part: UPPER SHEET — CORRODED (FRAMES 84-86) · corrosion level 2 · airframe 21,255 hrs · 16,771 cycles

DURING HEAVY CHECK, RT UPPER SHEET BETWEEN FRAMES 86-84 IS CORRODED. MAINTENANCE R & R RT UPPER SHEET BETWEEN FRAMES 86-84 IAW SRM 51-41-01, 51-43-01, PN 170-86101-001, UPPER SHEET.

Part: STRINGER — CORRODED (FRAMES 83-86) · airframe 21,255 hrs · 16,771 cycles

DURING HEAVY CHECK, STRINGER 20L BETWEEN FRAMES 86-5 AND 84-83 IS CORRODED. MAINTENANCE COMPLIED WITH ETD 2016-170-033333.

Part: STRINGER — CORRODED (FRAMES 82-84) · corrosion level 2 · airframe 21,255 hrs · 16,771 cycles

DURING HEAVY CHECK, STR 19 LT BETWEEN FRAMES 84-82 IS CORRODED. MAINTENANCE R & R STRINGER 19 LT BETWEEN FRAMES 84-82 IAW ETD2016-170-033333.

Part: SEAT TRACK — CORRODED (FRAME 19) · corrosion level 2 · airframe 21,255 hrs · 16,771 cycles

DURING HEAVY CHECK, LT SEAT TRACK AT FRAME 19 IS CORRODED. MAINTENANCE R & R LT SEAT TRACK AT FRAME 19 IAW SRM 51-41-01, 51-41-02, 51-43-03, 51-43-04, PN 170-03264-001 SEAT TRACK.

Part: BARREL NUT — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,255 hrs · 16,771 cycles

DURING HEAVY CHECK, BARREL NUT FITTING AT FRAME 84 CROSSBEAM AND RT SEAT TRACK BEAM IS CORRODED. MAINTENANCE R & R BARREL NUT FITTING AT FRAME 84 CROSSBEAM AND RT SEAT TRACK BEAM IAW SRM 51-23-04, 51-41-01, 51-23-06. PN 170-92859-001, BARREL NUT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,780 hrs · 16,436 cycles

CREW REPORTED THAT THE FORWARD CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE R & R EMERGENCY LIGHTS IAW AMM AND OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,733 hrs · 16,405 cycles

CREW REPORTED THAT THE 2 FWD MOST EMERGENCY LIGHT STRIPS WERE NOT GLOWING. MAINTENANCE R & R FORWARD EMERGENCY LIGHT STRIPS IAW AMM AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 20,045 hrs · 15,892 cycles

CREW REPORTED THAT THE F/O FLASHLIGHT WAS INOPERATIVE. MAINTENANCE R & R F/O FLASHLIGHT BATTERY IAW AMM AND OPS CHECKED GOOD.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 19,554 hrs · 15,491 cycles

FWD E-BAY BACK UP BATTERY, FWD SUPPORT BRACKET IS CRACKED. MAINTENANCE R & R FWD E-BAY BACK UP BATTERY FWD SUPPORT BRACKET IAW SRM 51-41-01, PN 170-27348-403, BRACKET.

Part: BULB — BURNED OUT (SMOKE DETECTOR) · airframe 19,554 hrs · 15,491 cycles

AFT LAV SMOKE DETECTOR LIGHT DOES NOT COME ON. MAINTENANCE R & R LIGHT BULB IAW AMM 33-28-00, PN 8GA002987-28, LAMP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 18,548 hrs · 14,674 cycles

CREW REPORTED THAT THE F/O FLASHLIGHT WAS INOPERATIVE MAINTENANCE R & R F/O FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 17,205 hrs · 13,630 cycles

CREW REPORTED THAT THE F/O FLASHLIGHT WAS DIM. MAINTENANCE R & R F/O FLASHLIGHT BATTERY IAW AMM AND OPS CHECKED GOOD.

Part: CONTROL MODULE — FAILED (BRAKE SYS) · airframe 16,671 hrs · 13,230 cycles

CREW RECEIVED "BRAKE RT FAULT" AND "BRAKE LT FAULT" MESSAGES. CREW RAN QRH AND CONTINUED TO DESTINATION. DECLARED AN EMERGENCY. LANDED AND TAXIIED TO GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND R & R THE BRAKE CONTROL MODULE IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.

Part: FILTER — CLOGGED (LT A/C PACK) · airframe 16,593 hrs · 13,163 cycles

CREW RECEIVED A NR 1 PACK FAIL MESSAGE AT FL 280. TRIED TO RESET WITH NO SUCCESS AND CABIN WOULD NOT HOLD PRESSURE. DECLARED AN EMERGENCY AND ELECTED TO RETURN TO DEPARTURE. LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE LT PACK FILTER CLOGGED. MAINTENANCE CLEANED FILTER IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,574 hrs · 12,348 cycles

CREW REPORTED THAT THE EMERGENCY LIGHT IN FRONT OF SEAT 1D DOES NOT ILLUMINATE. MAINTENANCE R & R LIGHT IAW AMM AND OPS CHECKED GOOD.

Part: STRIKER — DAMAGED (L1 DOOR SENSOR) · airframe 14,625 hrs · 11,616 cycles

CREW RECEIVED A L1 DOOR OPEN MESSAGE. AN EMERGENCY WAS NOT DECLARED AND LANDED WITHOUT INCIDENT. MX R & R THE L1 DOOR FRAME TARGET AND STRIKER IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (L1 DOOR) · airframe 14,596 hrs · 11,592 cycles

CREW RECEIVED A L1 DOOR OPEN INDICATION AT FL 320. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. R & R THE L1 DOOR PROXIMITY SWITCH AND ADJUSTED HARNESS IAW AMM AND OPS CHECKED GOOD.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 14,221 hrs · 11,286 cycles

CREW REPORTED THAT THE PHOTO LUMINESCENT STRIP AT THE FRONT OF THE ACFT IS NOT LONGER PHOTO LUMINESCENT. MX INSPECTED AND FOUND IT TO BE IN SERVICEABLE CONDITION IAW AMM. ACFT IS GOOD FOR SERVICE.

Part: SKIN — BUCKLED (FUSELAGE) · airframe 13,521 hrs · 10,735 cycles

WHILE PERFORMING MAINTENANCE IN HEAVY CHECK MAINTENANCE DAMAGED SKIN AFT LOWER FUSELAGE JACK PAD AREA. MAINTENANCE REPAIRED SKIN IAW EMB ETD 2013-170-006071 AND TI170-13-033. THIS WAS A MAJOR REPAIR. ITEMS REMOVED AND REPLACED WITH THE SKIN REPAIR ARE NON-FCS STRUCTURE, VERTICAL SUPPORT P/N 170-60205-001,VERTICAL SUPPORT P/N 170-60206-001, JACK FITTING P/N 170-60353-401, INTERCOSTAL P/N 170-61349-003, AND INTERCOSTAL P/N 170-61349-004. THE AIRCRAFT IS BEING RETURNED TO SERVICE CMH AT 18:00 4-25-2013.

Part: PIN — CORRODED (RT MLG) · corrosion level 2 · airframe 13,521 hrs · 10,735 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT MLG LOWER SIDESTAY PIN CORRODED. MAINTENANCE REMOVED AND REPLACED THE PIN IAW JOB CARD R170EO-32-11-0001. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 13,285 hrs · 10,553 cycles

CREW REPORTED THAT THE CAPTAINS FLASHLIGHT IS DIM. MAINTENANCE PLACED FLASHLIGHT ON MEL PER EMB AMM.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 12,132 hrs · 9,682 cycles

CREW REPORTED THAT ON CLIMB THE LANDING GEAR LEVER WOULD NOT COME UP. TOWER CONFIRMED ALL 3 GEARS WERE STILL DOWN. A/C RETURNED TO THE FIELD. MAINTENANCE RESET C/B FOR THE LEVER AND PERFORMED GEAR SWINGS AND ALL CHECKS WERE NORMAL. MAINTENANCE REPLACED THE LG CONTROL LEVER MODULE ASSY JUST TO BE ON THE SAFE SIDE.

Part: UNKNOWN — ODOR (BLEED AIR SYS) · airframe 11,761 hrs · 9,377 cycles

DURING TAKEOFF ROLL, WITH TO-1 THRUST SET, STRONG ODOR/FUMES NOTICED UNTIL 1000 FEET. WHEN BLEED 1 WAS PUSHED OUT ODOR/FUMES DISSIPATED. THE ODOR/FUME WAS HAZARDOUS BUT STOPPED WHEN BLEED 1 WAS OFF. PERFORMED HIGH POWER ENGINE RUNS WITH VALVE OPEN, UNABLE TO DUPLICATE ODOR OR FUMES. OPS CHECK NORMAL WITH NO UNUSUAL ODOR, OK FOR SERVICE. REF AMM 36-11-00/GEMM 72-00-0.

Part: MODULE — INOPERATIVE (CABIN) · airframe 11,394 hrs · 9,077 cycles

CREW REPORTED CABIN INTERPHONE, EMERGENCY LIGHTS, AND LIGHTS ON RAINBOW STRIP INOP IN NORMAL MODE. MTX TROUBLESHOT, REMOVED AND REPLACED NIM 2 PER EMB AMM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 11,047 hrs · 8,805 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE FLOOR SUPPORT BRACKET AT FRAME 86 BROKEN. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT BRACKET AT FRAME 86 IAW EMB 175 SRM 51-41-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: BRACKET — CRACKED (NLG) · airframe 11,047 hrs · 8,805 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT NOSE WHEEL BRAKE BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED THE LEFT NOSE WHEEL BRAKE BRACKET IAW EMB 175 SRM 51-43-03, 51-21-02, 51-23-06 AND AMM 32-49-13. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,047 hrs · 8,805 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT OUTBOARD GUSSET CORRODED AT FRAME 90. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD GUSSET IAW EMB 175 SRM 51-41-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,047 hrs · 8,805 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT INBOARD GUSSET AT FRAME 89 CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD GUSSET AT FRAME 89 IAW EMB 175 SRM 51-41-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,047 hrs · 8,805 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND LT SEAT TRACK BEAM EXTENSION CORRODED BETWEEN FR 85-87. MX REMOVED AND REPLACED LT SEAT TRACK BEAM EXTENSION IAW EMB 170/175 SRM 51-43-01. PN 170-65669-003. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 11,047 hrs · 8,805 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT PACK RAM AIR VALVE DUCT BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK RAM AIR DUCT BRACKET IAW EMB 175 SRM 51-40-02 AND 51-41-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,047 hrs · 8,805 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND RT SILL CORRODED BETWEEN FR 88-90. MX REMOVED AND REPLACED PANEL SUPPORT IAW EMB 175 SRM 51-42-01, 51-43-03. PN 170-86139-005. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,047 hrs · 8,805 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENACE FOUND THE RIGHT INBOARD GUSSET CORRODED AT FRAME 90. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD GUSSET IAW EMB 175 SRM 51-41-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,047 hrs · 8,805 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND LT SHEAR PLATE CORRODED BETWEEN FR 87-88. MX REMOVED AND REPLACED LT SHEAR PLATE BETWEEN FR 87-88 IAW EMB SRM 51-40-02, 51-21-01, 51-42-01, 51-43-01. PN 170-65927-007. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.

Part: SUPPORT ANGLE — CRACKED (LT MLG WW) · airframe 11,047 hrs · 8,805 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT WHEEL WELL FORWARD BULKHEAD UPPER SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD BULKHEAD UPPER SUPPORT BRACKET IAW EMB 175 SRM 51-40-02, 51-42-01, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,047 hrs · 8,805 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT UPPER SHEET CORRODED BETWEEN FRAME 85-86. MAINTENANCE REMOVED AND REPLACED THE RIGHT UPPER SHEET AT FRAME 85 TO 86 IAW EMB 175 SRM 51-41-01, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,047 hrs · 8,805 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE CENTER SHEAR PLATE CORRODED BETWEEN FRAME 87 AND 88. MAINTENANCE REMOVED AND REPLACED THE CENTER SHEAR PLATE BETWEEN FRAMES 87 AND 88 IAW EMB 175 SRM 51-43-01, 51-42-01, 51-42-02 AND 51-40-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,047 hrs · 8,805 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE WASTE BOX FORWARD DOUBLER CORRODED. MAINTENANCE REMOVED AND REPLACED THE FORWARD WASTE BOX DOUBLER IAW EMB 175 SRM 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,047 hrs · 8,805 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT OUTBOARD GUSSET CORRODED AT FRAME 90. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD GUSSET AT FRAME 90 IAW EMB 175 SRM 51-41-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: SCREW — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 11,047 hrs · 8,805 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTNENACE FOUND THE LAV SERVICE DOOR HINGE HAS CORROSION. MAINTENANCE FOUND NO EVIDENCE OF CORROSION ON HINGE, REPLACED HARDWARE IAW EMB 175 AMM 20-10-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: WIRE HARNESS — FAILED (LE SLAT) · airframe 10,396 hrs · 8,285 cycles

DURING PREPARATION FOR APPROACH, THE CREW RECEIVED A "SLAT FAIL" MESSAGE. THE CAPTAIN DECLARED AN EMERGENCY INTO PHL. THE FLIGHT LANDED NORMALLY AND TAXIED TO THE GATE. MAINTENANCE WAS NOTIFIED, TROUBLESHOT THE SLAT SYSTEM. MAINTENANCE THEN REMOVED AND REPLACED 3/4 SLAT HARNESS PER THE EMB 175 AMM. OPS CHECK WAS GOOD AND AC WAS RETURNED BACK INTO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 10,359 hrs · 8,254 cycles

CREW REPORTED SLAT FAIL MSG ON APPROACH INTO CLT, AND DECLARED AN EMERGENCY. THE A/C LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND PERFORMED OPS CHECKS OF SLAT SYSTEM PER EMB AMM, NO DEFECTS NOTED. A/C WAS THEN RETURNED TO SERVICE.

Part: SLIDE — UNLACED (R1 DOOR) · airframe 5,770 hrs · 4,661 cycles

***GENERATED FROM HEAVY CHECK*** MAINTENANCE REMOVED AND REPLACED R-1 EMERGENCY EVACUATION SLIDE PER EMB AMM, DUE TO LACING COMING LOOSE. A/C IS STILL CURRENTLY OUT OF SERVICE FOR IT'S HEAVY CHECK.

Part: STAND OFF — CORRODED (LAVATORY BOX) · corrosion level 2 · airframe 5,770 hrs · 4,661 cycles

WHILE AC WAS IN FOR HEAVY CHECK, LEVEL TWO CORROSION WAS FOUND ON AFT SIDE OF THE LAV DUMP BOX STANDOFF. MAINTENANCE REMOVED CORRODED STANDOFF, FABRICATED NEW STANDOFF AND REPLACED ON AC PER EMB SRM. AC STILL OUT OF SERVICE FOR REMAINDER OF HEAVY CHECK.

Part: LINKAGE — LACK OF LUBE (R2 DOOR) · airframe 4,812 hrs · 3,905 cycles

CREW REPORTED THE R-2 DOOR IS EXTREMELY HARD TO CLOSE. MAINTENANCE TROUBLESHOT AND LUBED THE R-2 DOOR INDICATION LINKAGE PER EMB AMM, OPS CHECK GOOD AFTER THAT.