N806MD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,998 hrs · 30,836 cycles

DIVR SDF ACCT FUEL LEAK ON ENG2 EMERGENCY DECLARED. TRANSFERRED FROM AML PAGE 5044722 FUEL LEAK OUT OF RIGHT TANK OR ENGINE #2 1000LBS DIFERANCE ON FMS.-C/A-RAR FUEL CONDITIONING UNIT IAW E170 AMM 28-41-03. OPS CHECK GOOD.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 38,926 hrs · 29,356 cycles

WHILE IN HEAVY CHECK - CORROSION CENTER FUSELAGE III FR87 STGRS 28R TO 27R SHEAR CLIP. REPLACED CENTER FUSELAGE III FR87 STGRS 28R TO 27R SHEAR CLIP REF EMB SRM 51-40-08

Part: FINGER DOUBLER — CORRODED (ZONE 100) · airframe 38,926 hrs · 29,356 cycles

WHILE IN HEAVY CHECK - AFT CARGO AFT FINGER DOUBLER HAS CORROSION AS MARKED. REPLACED AFT CARGO AFT FINGER DOUBLER. REF EMB SRM 51-40-08, 51-40-02, 51-40-04

Part: CROSSBEAM — CORRODED (ZONE 200) · airframe 38,926 hrs · 29,356 cycles

WHILE IN HEAVY CHECK - CORROSION ON CROSSBEAM FRAME 84 BETWEEN RH FUSELAGE AND CENTER TRACK. REPAIRED CROSSBEAM IAW ETD2022-170-030568.

Part: FINGER DOUBLER — CORRODED (ZONE 100) · airframe 38,926 hrs · 29,356 cycles

WHILE IN HEAVY CHECK - AFT CARGO FWD FINGER DOUBLER HAS CORROSION AS MARKED. REPLACED AFT CARGO FINGER DOULBER PN: 170-85070-001 REF EMB SRM 51-40-02. RESTORE FINISH REF EMB SRM 51-23-04,51-23-05 AND 51-23-06

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,926 hrs · 29,356 cycles

L1 DOOR SILL FWD GIRT BAR FITTING WELL CORRODED AROUND 3 EA RIVETS IN BOTTOM OF WELL. REMOVED AND REPLACED L1 DOOR SILL BEAM REF EMB SRM 51-40-08 SEE WIP'S AND TASKS FOR WORK ACCOMPLISHED

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,926 hrs · 29,356 cycles

CORROSION ON CO-PILOT COCKPIT FLOOR DOUBLER IN MULTIPLE LOCATION BETWEEN FR 07-12 AS MARKED.: REMOVED AND REPLACED CO-PILOT COCKPIT FLOOR DOUBLER REF EMB170 SRM 51-40-08 SEE WIPS AND TASKS FOR WORK ACCOMPLISHED

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,926 hrs · 29,356 cycles

CORROSION ON PILOT COCKPIT FLOOR DOUBLER IN MULTIPLE LOCATION BETWEEN FR 07-12 AS MARKED. : PERFORMED PERMANENT REPAIR ON PILOT COCKPIT FLOOR DOUBLER BY SPLICING IN NEW SECTION BETWEEN FR 07-12. REF EMB ETD2022-170-030432 REV. A. SEE WIPS AND TASKS FOR WORK ACCOMPLISHED.

Part: WING — CRACKED (ZONE 600) · airframe 38,926 hrs · 29,356 cycles

CRACK LOWER SKIN ON RH WING RIB 4 AS MARKED. REPAIRED CRACK ON LOWER SKIN ON RH WING RIB 4 AS MARKED. REF ETD2022-170-029954. SEE WIPS AND TASKS FOR WORK PERFORMED.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 36,206 hrs · 27,419 cycles

E2 HIGH NOISE/VIBRATIONS. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. DISCOVERED TO BE DAMAGE FROM A BIRD STRIKE. R&R FAN BLADES 1, 14, 2, AND 15. OPS CHECK GOOD.

Part: SEAL — MISSING (E/E BAY DOOR) · airframe 35,901 hrs · 27,217 cycles

AFT EBAY SMOKE SEAL CENTER TO SECTION MISSING WHILE COMPLYING WITH JC 170EI-25-34-0016-1 AFT EBAY DOOR OPEN. INSTALLED AFT EBAY TOP CENTER SMOKE SEAL AND SECURED ACCESS DOOR 252A2 IAW AMM 28-84-01.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 35,807 hrs · 27,130 cycles

MAJOR REPAIR, WHILE AIRCRAFT WAS IN FOR HEAVY CHECK FOUND LT STAB FRONT SPAR CRACK AT FLANGE ON FASTENER ATTACHMENT TO RIB 12. CORRECTIVE ACTION: REPAIR PERFORMED BY AAR NRC 4500812-3000-0046, PER ETD 2020-170-034311. AIRCRFT HAS BEEN RETURNED TO SERVICE.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK A CRACK WAS FOUND ON VERTICAL STAB TRAILING EDGE AT RIB 11. REPAIR WAS COMPLETED BY AAR ON NRC 4500812-3000-0040, PER SRM 55-30-07 AND DWG 170-63630-001. THIS ARICRAFT HAS BEEN RETURNED TO SERVICE.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK A CRACK WAS FOUND ON THE VERTICAL STAB TRAILING EDGE RIB 8. AAR REPLACED RIB 8 ON NRC 4500812-3000-0041, PER SRM 51-41-01/02 AND ETD2020-170-034323. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECKCRACK FOUND ON VERTICAL STAB TRAILING EDGE RIB 9/10. REPLACED ON AAR NRC 4500812-3000-0039, PER SRM 51-41-01/02. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK, THE AFT SERVICE DOOR CUT-OUT CORROSION FOUND AT SUPPORT SEAL REST. THIS PART WAS REPLACED BY AAR ON NRC 4500812-2000-0106.

Part: DOUBLER — CORRODED (AFT CARGO) · corrosion level 2 · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK, CORROSION WAS FOUND AT AFT CARGO, POTABLE WATER PAN, FORWARD RETAINER. AAR REPLACED THE DOUBLER ON NRC 4500812-1000-0085, PER SRM 51-43-04. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FRAMES 24-25) · corrosion level 2 · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK, CORROSION WAS FOUND ON FWD CARGO CUT-OUT, NUTPLATE SUPPORT AT LOWER SILL BETWEEN FR 24 & 25. THE SUPPORT WAS REPLACED BY AAR ON NRC 4500812-1000-0077, PER THE SRM 51-41-01. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: INTERCOSTAL — CORRODED (FRAMES 86-87) · corrosion level 2 · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK, CORROSION WAS FOUND ON AN INTERCOSTAL BETWEEN FRAME 86 & 87 AND STRINGER 27 & 28. INTERCOSTAL WAS REPLACED BY AAR ON NRC 4500812-1000-0087, PER THE SRM 51-41-02 AND SRM 51-43-03. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK, A CRACK WAS FOUND IN THE H STAB L/E AT RIB 5. AAR REPAIRED PER SRM 55-15-01 ON NRC 4500812-3000-0018. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,807 hrs · 27,130 cycles

WHLE IN HEAVY CHECK, FORWARD FUSELAGE FLOOR STRUCTURE, CORROSION FOUND ON FLOOR SUPPORT AT CROSSBEAM 16 LT SIDE. REPLACED SUPPORT ON AAR NRC 4500812-2000-071, PER SRM 51-53-03. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: RIB — CRACKED (HORIZONTAL STAB) · corrosion level 2 · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK, RT HORIZ STAB LEADING EDGE CRACK FOUND AT RIB 4. REPAIRED BY AAR ON NRC 4500812-3000-0017, PER SRM 55-15-07. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK CORROSION WAS FOUND ON CF 3 PANEL SUPPORT AT FR 84 AND STR 17 RT. REPLACED PANEL ON AAR NRC 4500812-10000-0046, PER SRM 51-41-02. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK, FLOORBOARD SUPPORT FOUND CRACKED CENTER FUSELAGE III FR 86 AT LBL 28. REPLACED SUPPORT ON AAR NRC 4500812-1000-0045, PER SRM 51-41-01. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: SHEAR PANEL — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK CORROSION WAS FOUND AT THE FORWARD FUSELAGE, FLOOR STRUCTURE SHEAR PANEL LT SIDE BETWEEN FRAME 12-14. AAR REPLACED THE PANEL ON NRC 4500812-1000-0035, PER SRM 51-43-03. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: STRINGER — CRACKED (RT NACELLE) · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK, RT ENGINE AFT PYLON STRINGER 5 OUTBOARD SIDE CRACKED. REPAIRED ON AAR NRC 4500812-4000-0039 AND SRM 54-50-23 ITEM 140. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: SPLICE — CORRODED (FRAMES 87-89) · corrosion level 2 · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK CORROSION WAS FOUND ON LT FLOOR SPLICE BETWEEN FRAME 87 AND 89. AAR REPLACED THE SPLICE ON NRC 4500812-1000-0054, PER SRM 51-42-02. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 35,807 hrs · 27,130 cycles

MAJOR REPAIR, WHILE AIRCRAFT WAS IN FOR HEAVY CHECK FOUND HORIZ STAB CRACKS ON LT SIDE RIB 11A AND 12A BETWEEN MID AND FRONT SPAR. THE CORRECTIVE ACTION AAR REPAIRED CRACKS, PER 170EO-55-10-0004. FOR DETAILS OF WORK PERFORMED SEE AAR NRC 4500812-3000-0012. AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: SCOOP — CORRODED (RT NACELLE) · corrosion level 2 · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK, CORROSION FOUND ON RT PYLON STRUCTURE INBOARD AIR SCOOP. REPLACED ON AAR NRC 4500812-4000-0013, PER ARM 51-41-02. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: SUPPORT — CRACKED (SEAT PAN) · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK AFT F/A SEAT PAN SIDE SUPPORT CRACKED. REPLACED ON AAR NRC 4500812-2000-0030, PER CMM 25-22-30. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK LT HORIZ STAB LEADING EDGE CRACK FOUND IN RIB 9. REPLACED ON AAR NRC 4500812-3000-005, PER ARM 51-41-02. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: HINGE — CORRODED (WASTE DOOR) · corrosion level 2 · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK CORROSION WAS FOUND AT WASTE DOOR HINGE AT FRAME 88. AAR REPLACED THE HINGE ON NRC 4500812-1000-002, PER SRM 51-41-02. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: SEAL DEPRESSOR — CRACKED (PAX DOOR) · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK, FWD PASS DOOR CUT-OUT UPPER CORNER SEAL DEPRESSOR HAS A CRACK. REPAIRED ON AAR NRC 4500812-2000-0029, PER SRM 51-41-01. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: STIFFENER — CORRODED (WASTE DOOR) · corrosion level 2 · airframe 35,807 hrs · 27,130 cycles

CORROSION FOUND ON WASTE ACCESS DOOR STIFFENER. AAR REPALCED THE STIFFENER ON NRC 4500812-1000-003, PER ARM 51-41-02. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: SUPPORT BRACKET — CRACKED (VENT) · airframe 35,807 hrs · 27,130 cycles

WHILE IN HEAVY CHECK CF 1 LT EMERGENCY VENT SUPPORT BRACKET AT FR 31 FOUND CRACKED. REPLACED ON AAR NRC 4500812-1000-007, PER SRM 51-41-01. THIS AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (O2 BOX) · airframe 35,349 hrs · 26,801 cycles

***WHILE AIRCRAFT WAS IN FOR BRIDGING*** MAINTENANCE FOUND FWD LAV O2 MASK FAIL TO OPEN DURING OPERATIONAL CHECK. PERFORMED TROUBLESHOOTING OF FWD LAVATORY O2 BOX NOT DEPLOYING DURING OPERATIONAL CHECK. MANUALLY OPENED THE BOX AND REMOVED BOX FROM THE CEILING OF THE LAVATORY. FOUND CONNECTOR THAT DEPLOYS THE SWITCH NOT CONNECTED. RECONNECTED SPLICES AND PERFORMED OPERATIONAL CHECK OF PASSENGER OXYGEN DEPLOY-OPERATIONAL CHECK GOOD IAW AMM 35-21-00.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 35,349 hrs · 26,801 cycles

***WHILE AIRCRAFT WAS IN FOR BRIDGING*** MAINTENANCE FOUND DURING FASTENER REMOVAL, DAMAGES ON LOWER FR 17, STR 27L TO 27R, IN THE RADIUS AND BY THE LOWEST FASTENER. REMOVED AND REPLACED DAMAGED LOWER FR 17, STR 27L-27R IAW SRM 51-40-08. SEE APPROVED ETD2019-170-054592 FOR SUBSTANTIATION TO USE P/N 170-03871-401.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,349 hrs · 26,801 cycles

***WHILE AIRCRAFT WAS IN FOR BRIDGING*** MAINTENANCE FOUND ADDITIONAL CORROSION AND CHAFE DAMAGE DURING REMOVAL OF SHEAR CLIPS, AT FR17 BETWEEN STR 24R AND 24L. REMOVED AND REPLACED BEAM AT FR 17, BETWEEN STR 24R AND 24L IAW SRM 51-40-08.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 35,349 hrs · 26,801 cycles

***WHILE AIRCRAFT WAS IN FOR BRIDGING**** MAINTENANCE FOUND LT HORIZONTAL AT RIB 14 HAS CRACK ON UPPER TRAILING EDGE. REMOVED AND REPLACED RIB 14 ON HORIZONTAL STAB IAW SRM 51-40-08.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 35,349 hrs · 26,801 cycles

***WHILE AIRCRAFT WAS IN FOR BRIDGING*** MAINTENANCE FOUND LT HORIZONTAL STABILIZER RIB 12 HAS 2EA. SUSPECTED CRACKS IN BETWEEN FRONT AND MID SPAR. PERFORMED HFEC AND CONFIRMED FWD MOST CRACK IAW NTM PT6, 51-06-00-250-801-A MAINTENANCE REMOVED AND REPLACED CRACKED RIB IAW SRM 51-40-08.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 35,349 hrs · 26,801 cycles

MAINTENANCE FOUND CORRODED SHEAR CLIP AT FR 17 BETWEEN STRG. 28R AND 27R FWD CARGO COMPARTMENT UNDER VENTILATION DUCT BRACKET. REMOVED AND REPLACED SHEAR CLIP IAW EMB 170/175 SRM 51-40-08.

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 35,349 hrs · 26,801 cycles

MAINTENANCE FOUND CORRODED SHEAR CLIP AT FR 16 BETWEEN STRG. 28L AND 27L FWD CARGO COMPARTMENT. REMOVED AND REPLACED CORRODED SHEAR CLIP IAW EMB 170/175 SRM 51-40-08.

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 35,349 hrs · 26,801 cycles

***WHILE AIRCRAFT WAS IN FOR BRIDGING*** MAINTENANCE FOUND CORRODED SHEAR CLIP AT FR16 BETWEEN STRG.28R AND 27R FWD CARGO COMPARTMENT. REMOVED AND REPLACED SHEAR CLIP IAW EMB170/175 SRM 51-40-08.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 35,349 hrs · 26,801 cycles

MAINTENANCE FOUND A CORRODED SHEAR TIE AT FR 17 BETWEEN STRG. 28L AND 28R UNDER VENTILATION DUCT BRACKET AND CABLES SUPPORT BRACKET. REMOVED AND REPLACED SHEAR CLIPS IAW EMB 170/175 SRM 51-40-08.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 35,349 hrs · 26,801 cycles

MAINTENANCE FOUND CORRODED SHEAR CLIP AT FR 17 BETWEEN STRG. 27R AND 26R FWD CARGO COMPARTMENT. REMOVED AND REPLACED SHEAR CLIP IAW EMB170/175 SRM 51-40-08.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 35,349 hrs · 26,801 cycles

MAINTENANCE FOUND CORRODED SHEAR CLIP AT FR 17 BETWEEN STRG. 28L AND 27L. REMOVED AND REPLACED SHEAR CLIP IAW SRM 51-40-08.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 19,034 hrs · 13,344 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK, MAINTENANCE FOUND THE LEFT WHEEL WELL FORWARD BULKHEAD ATTACH ANGLE SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE LEFT WHEEL WELL FORWARD BULKHEAD ATTACH ANGLE SUPPORT IAW SRM 51-41-01,51-42-01, 51-43-03, AND 51-21-05. THE AIRCRAFT IS OUT OF SERVICE.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 19,034 hrs · 13,344 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK, MAINTENANCE FOUND THE LEFT BAND CLAMP SUPPORT BROKEN FOR THE LEFT PACK RAM AIR SHUTOFF VALVE. MAINTENANCE REMOVED AND REPLACED SUPPORT FOR LEFT PACK RAM AIR SHUTOFF VALVE IAW EMB 170 AMM 20-10-01. THE AIRCRAFT IS OUT OF SERVICE.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 19,034 hrs · 13,344 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK, MAINTENANCE FOUND PROFILE SUPPORT CRACKED ON LEFT PACK RAM AIR SHUTOFF VALVE. MAINTENACE REMOVED AND REPLACED CRACKED PROFILE SUPPORT ON LEFT PACK RAM AIR SHUTOFF VALVE IAW SRM 51-41-02. THE AIRCRAFT IS OUT OF SERVICE.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 19,034 hrs · 13,344 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK, MAINTENANCE FOUND SUPPORT CRACKED FOR LEFT PACK RAM AIR SHUTOFF VALVE. MAINTENANCE REMOVED AND REPLACED THE SUPPORT ON THE LEFT PACK RAM AIR SHUTOFF VALVE IAW SRM 51-41-02. THE AIRCRAFT IS OUT OF SERVICE.

Part: BRACKET — CRACKED (ZONE 100) · airframe 19,034 hrs · 13,344 cycles

ACFT IN FOR HEAVY CHECK, FOUND FWD CARGO DOOR SURROUND LOWER PANEL MOUNT BRACKETS ARE CRACKED AND BROKEN AT MIDDLE 4 BRACKET'S OF SIX. MX REMOVED AND REPLACED FOUR BRACKETS IAW SRM 51-41-01.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 19,034 hrs · 13,344 cycles

WHILE ACFT WAS IN FOR HEAVY CHECK FOUND BROKEN BRACKET ON PANEL 195FL. MX REMOVED AND REPLACED BROKEN BRACKET AT PNL 195FL IAW SRM 51-41-01, 51-40-02. ACFT REMAINS IN HEAVY CHECK.

Part: MECHANISM — LACK OF LUBE (L2 DOOR) · airframe 18,406 hrs · 12,934 cycles

CREW REPORTED L-2 DOOR WASN'T ARMING PROPERLY. MAINTENANCE LUBED L-2 DOOR ARMING MECHANISM PER EMB AMM, OPS CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,077 hrs · 12,690 cycles

CREW REPORTED DURING A FAINT SMOKE SMELL DURING CRUISE NEAR ROW 12 AND CONTINUING AFT. NO EMERGENCY WAS DECLARED AND AIRCRAFT LANDED SAFELY AT DEN. MAINTENANCE PERFORMED OPS CHECK OF AIR CONDITIONING SYSTEM PER EMB AMM AND COULDN'T DUPLICATE ANY SMOKE SMELLS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,450 hrs · 12,219 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK FOUND LOWER LT SEAT TRACK BEAM AT CF1 FRS 23-34 CORROSION AND GOUGED. REMOVED AND REPLACED LT CF1 SEAT TRACK BEAM IAW EMB 170/175 SRM 51-40-02, SRM 51-41-02 AND SRM 51-43-01. AIRCRAFT STILL OUT OF SERVICE PENDING COMPLETION OF HEAVY CHECK. LEVEL 2 CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,450 hrs · 12,219 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE LOWER RT SEAT TRACK BEAM AT CF3, FR'S 74-85. MAINTENANCE REMOVED AND REPLACED THE RT SEAT TRACK BEAM AT CF3, FR'S 74-85 IAW EMB 170 SRM 51-41-01, 51-43-02, 51-43-01 & 51-40-02. A/C IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,450 hrs · 12,219 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE LOWER RT SEAT TRACK BEAM AT CF1, FR'S 23-34. MAINTENANCE REMOVED & REPLACED THE RT SEAT TRACK BEAM CF1, FR'S 23-34, IAW EMB 170 SRM 51-43-01, 51-43-02, 51-40-02, 51-43-00 & 51-41-01. A/C IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SIGN — INOPERATIVE (CABIN) · airframe 16,588 hrs · 11,599 cycles

CREW REPORTED THE AFT RAINBOW LIGHTS FOR THE AFT LAV SMOKE LIGHT WERE INOP. MX TROUBLESHOT AND REPORTED THE AFT AREA CALL SIGN WAS AT FAULT, R & R THE AFT F/A CALL, F/A PANEL IAW AMM, AND OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (LAVATORY) · airframe 16,407 hrs · 11,482 cycles

CREW REPORTED WHEN DOING AFT LAV FIRE TEST, THE RAINBOW LIGHTS WERE INOP. MAINTENANCE PLACED ON MEL 26-14-00-1.

Part: PRESSURE SENSOR — FAULTY (BRAKE SYSTEM) · airframe 15,901 hrs · 11,139 cycles

CREW REPORTED EMERG PARK BRAKE NOT RELEASED MSG IN FLIGHT, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT INTO DEN. MAINTENANCE REMOVED AND REPLACED NR 1 EMERG BRAKE PRESSURE SENSOR PER EMB AMM, OPS CHECK GOOD. A/C WAS THEN RETURNED TO SERVICE.

Part: HEAT EXCHANGER — FAILED (AC BAY) · airframe 15,863 hrs · 11,107 cycles

CREW RETURNED TO FIELD DUE TO SMOKE IN CABIN ALONG WITH PACK 2 FAIL, LANDED WITHOUT INCIDENT AT DEN. MAINTENANCE REMOVED AND REPLACED THE RT HEAT EXCHANGER PER AMM, OPS CHECK GOOD. CREW RETURNED TO FIELD DUE TO SMOKE IN CABIN ALONG WITH PACK 2 FAIL, LANDED WITHOUT INCIDENT AT DEN. MAINTENANCE PLACED PACK NR 2 ON MEL 21-51-00-1. A/C WAS THEN RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (COCKPIT) · airframe 15,794 hrs · 11,067 cycles

CREW REPORTED EMERGENCY EXIT LIGHT IN THE FLIGHT DECK FAILED TO ILLUMINATE DURING EMERGENCY EXIT LIGHT TEST. MAINTENANCE RESET A/C POWER PER EMB AMM, AND REPORTED NO DEFECTS AFTER THAT. A/C WAS THEN RETURNED TO SERVICE.

Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 15,186 hrs · 10,661 cycles

L-1 DOOR SLIDE DEPLOYED. MAINTENANCE REMOVED AND REPLACED L-1 EMERGENCY EVACUATION SLIDE PER EMB AMM.

Part: SLIDE — FAILED (R1 DOOR) · airframe 15,014 hrs · 10,493 cycles

MAINTENANCE PERFORMED A SCHEDULED JOB CARD FOR A DEPLOYMENT CHECK OF THE R1 DOOR SLIDE. UPON THE COMPLETION OF THE CARD THE SLIDE FAILED TO DEPLOY CORRECTLY. MAINTENANCE REMOVED AND REPLACED THE SLIDE ASSEMBLY, SERVICED THE DOOR ACTUATOR, ALL PER THE EMB AMM. AC RELEASED BACK TO SERVICE.

Part: FLANGE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,014 hrs · 10,493 cycles

WHILE AC WAS IN FOR MID C CHECK, LEVEL TWO CORROSION WAS FOUND ON WASTE SERVICE PANEL ON INTERNAL FLANGE. MAINTENANCE REMOVED AND REPLACED WASTE SERVICE PANEL BOX ASSEMBLY PER EMB SRM. AC STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,014 hrs · 10,493 cycles

WHILE AC WAS IN FOR MID C CHECK, LEVEL TWO CORROSION WAS FOUND ON FLOOR GUSSET AT FR 90 RIGHT OF CENTER. MAINTENANCE REMOVED AND REPLACED GUSSET PER EMB SRM. AC STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,014 hrs · 10,493 cycles

WHILE AC WAS IN FOR MID C CHECK, LEVEL TWO CORROSION WAS FOUND ON FLOOR GUSSET AT FR 90 LEFT OF CENTER. MAINTENANCE REMOVED AND REPLACED FLOOR GUSSET PER THE EMB SRM. AC STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: DAMPENER — CORRODED (R2 DOOR) · airframe 15,014 hrs · 10,493 cycles

WHILE AC WAS IN FOR MID C CHECK, LEVEL TWO CORROSION WAS FOUND ON R2 DOOR DAMPNER. MAINTENANCE REMOVED AND REPLACED THE DAMPNER PER EMB AMM. AC STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,014 hrs · 10,493 cycles

WHILE AC WAS IN FOR MID C CHECK, LEVEL TWO CORROSION WAS FOUND ON SHEAR PLATES IN THE AFT GALLEY, LEFT P/N 170-65927-007, RIGHT P/N 170-91919-001, AND CENTER P/N 170-65928-001. MAINTENANCE REMOVED AND REPLACED SHEAR PLATES PER THE EMB SRM. AC STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,014 hrs · 10,493 cycles

WHILE AC WAS IN FOR MID C CHECK, LEVEL TWO CORROSION WAS FOUND ON AFT GALLEY AFT MOUNT AT FR 90. MAINTENANCE REMOVED AND REPLACED MOUNT GUSSET PER EMB SRM. AC STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: FLANGE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,014 hrs · 10,493 cycles

WHILE AC WAS IN FOR MID C CHECK, LEVEL TWO CORROSION WAS FOUND ON WATER SERVICE PANEL INTERNAL FLANGE. MAINTENANCE REMOVED AND REPLACED INTERNAL FLANGE PER EMB SRM. AC STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,014 hrs · 10,493 cycles

WHILE AC WAS IN FOR MID C CHECK, LEVEL TWO CORROSION WAS FOUND ON FLOOR GUSSET AT FR 90 AT WASTE TANK FORWARD MOUNT. MAINTENANCE REMOVED AND REPLACED GUSSET PER THE EMB SRM. AC STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,014 hrs · 10,493 cycles

WHILE AC WAS IN FOR MID C CHECK, LEVEL TWO CORROSION WAS FOUND ON FWD GALLEY RT SEAT TRACK BEAM. MAINTENANCE REMOVED AND REPLACED RT SEAT TRACK BEAM PER THE EMB SRM. AC STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,014 hrs · 10,493 cycles

WHILE AC WAS IN FOR MID C CHECK, LEVEL TWO CORROSION WAS FOUND ON RT SEAT TRACK BEAM IN AFT GALLEY. MAINTENANCE REMOVED AND REPLACED SEAT TRACK BEAM PER EMB SRM. AC STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,997 hrs · 10,493 cycles

*** GENERATED WHILE IN HEAVY CHECK *** MTX REPORTED LT SEAT TRACK BEAM IN AFT GALLEY HAD AREAS OF CORROSION. MTX REMOVED AND REPLACED LT SEAT TRACK BEAM IAW EMB SRM 51-40-028 AND 51-43-01.

Part: CONTROL ROD — OUT OF ADJUST (L1 DOOR) · airframe 14,983 hrs · 10,485 cycles

CREW REPORTED L-1 DOOR DISARMING HANDLE WASN'T RAISING COMPLETELY. MAINTENANCE ADJUSTED PNEUMATIC ASSIST CONTROL ROD PER EMB AMM.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 14,873 hrs · 10,414 cycles

DURING TAXI CREW REPORTED THAT THE GIRT BAR INDICATIONS WEREN'T SHOWING RED WHEN THE DOOR WAS ARMED AND THAT THE SLIDE BOTTLE PRESSURE INDICATOR WASN'T PRESENT IN THE WINDOW. MAINTENANCE TROUBLESHOT AND FOUND THE L-1 SLIDE TO BE AT FAULT AND REPLACED IT PER EMB AMM. A/C WAS THEN RETURNED TO SERVICE.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 14,864 hrs · 10,406 cycles

CREW REPORTED SPOILER FAULT AND FCND ON APPROACH, DECLARED AN EMERGENCY AND LANDED AT OMA WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT MID MFS PCU AND FCM NR 4 PER EMB AMM, ALL FAULTS CLEARED AND THE A/C WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,583 hrs · 10,247 cycles

MAINTENANCE REPORTED THE FWD CABIN EMERGENCY LIGHTS DID NOT STAY ON FOR THE 15 REQUIRED 15 MINUTE MINIMUM DURING IT'S FUNCTIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE NR 2 ELPU PER EMB AMM.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 14,078 hrs · 9,964 cycles

MAINTENANCE DISCOVERED THAT THE L-1 DOOR SLIDE WAS UNPACKED, WHILE THE A/C WAS PARKED AT THE GATE. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR SLIDE PER EMB AMM, A/C WAS THEN RETURNED TO SERVICE.

Part: SENSOR — FAULTY (RT WING) · airframe 14,026 hrs · 9,932 cycles

CREW REPORTED FLAP/SLAT FAIL MSG WHILE ON APPROACH INTO LGA. CREW DECLARED AN EMERGENCY AND LANDED AT LGA WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT TO TROUBLESHOOT. MAINTENANCE REMOVED AND REPLACED THE RT O/B SKEW SENSORS PER EMB AMM. A/C WAS THEN RELEASED BACK INTO SERVICE.

Part: BRAKE ASSY — DISINTEGRATED (ZONE 700) · airframe 12,982 hrs · 9,236 cycles

CREW REPORTED NR 4 BRAKE DISINTEGRATED ON LANDING. AIRCRAFT LANDED WITHOUT INCIDENT AND MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND REPLACED THE NR 4 RIGHT O/B BRAKE AND PERFORMED OPS CHECKS PER EMB AMM. A/C WAS THEN RELEASED BACK INTO SERVICE.

Part: SENSOR — DEFECTIVE (LE SLAT) · airframe 11,732 hrs · 8,327 cycles

CREW REPORTED SLAT FAIL/AOA LIMIT FAIL ON FINAL APPROACH, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT HAND OUTBOARD SKEW SENSOR AND COMPLETED OPERATIONAL CHECK SYSTEM OPERATIONAL CHECK GOOD AND A/C WAS RETURNED TO SERVICE.

Part: MODULE — MALFUNCTIONED (STEERING SYS) · airframe 8,720 hrs · 6,167 cycles

PILOT REPORTED AVIONICS MAU 2 FAIL, AND DCA TOWER DIVERTED AIRCRAFT TO IAD. MAINTENANCE REMOVED AND REPLACED STEERING CONTROL MODULE SYSTEM, OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.