N635RW

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,487 hrs · 30,732 cycles

PITCH CONTROL/AUTO PILOT FAIL DISCONECT EMERGENCY DECLARED. -C/A-PERFORMED PITCH CONTROL OPERATIONAL CHK IAW AMM 27-40-00-710-801A. OPC GOOD NO DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,253 hrs · 30,542 cycles

FWD SERVICE DOOR LOWER EMERGENCY LIGHT INOP-C/A-RAR FWD RH EMERGENCY LIGHT POWER UNIT IAW ERJ AMM 33-50-01-000-801-A AND 33-50-01-400-801-A. OPS CHECK GOOD

Part: PRESSURE SWITCH — DAMAGED (LH) · airframe 48,207 hrs · 30,506 cycles

BLEED 1 OVERPRESSURE AT 27,000 FT FOLLOWED QRH PROCEDURE EICAS MSG REMAINED ON TILL 10,000 FT. LANDED UNDER MLW.-C/A-CMC FAULT CODE 36146225AM1 RAR LH BLEED OVERPRESSURE SWITCH IAWEMB 175 AMM 36-14-01 CHECK GOOD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,208 hrs · 30,507 cycles

THIS IS A SUPPLEMENTAL AC785(N635RW) HAD A REPEAT ISSUE FIRST EVENT WAS ON SEP 24 FLT 3887 - 2ND EVENT SEP 25 FLT 4073 CLIMBING THRU FL 280 BLEED OVERPRESS , RAN QRH REMAINED ANNUCIATED AFTER DESCENDING TO 16000 MSL.DECLARED EMERGENCY-C/A-PERFORMED WIRING TEST IAW WM 36-11-50 SHEET 1 AND SWPM 20-64-00 FOUND INTERMITTENT GROUND CONNECTION AT RELAY K0507 PIN C2 TO GS0947 INSPECTION FOUND GROUND STUD LOOSE CLEANED AND SECURED GROUND POINT GS0947 IAW AMM 20-13-21 AND PERFORMED WIRING TEST FOUND ALL CONECTION GOOD. INSTALLED NEW RELAY K0507 IAW SWPM 20-32-01.

Part: SKIN — MISREPAIRED (FR 9-10) · airframe 48,204 hrs · 30,502 cycles

RE EVALUATE EXISTING SKIN REPAIR BETWEEN FR9-10 AND STR 20L-21L (MAJOR REPAIR) -C/A-PERFORMED ONE TIME REPAIR OF EXISTING SKIN REPAIR BETWEEN FR9-10 AND STR 20L-21L IAW ERS-EJ-53DF-4853 OPS PT B PERMANENT REPAIR

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 48,204 hrs · 30,502 cycles

"EMERGENCY LIGHTT BATTERY FAULT" ON EICAS-C/A-REMOVED AND REPLACED #4 ELPU IAW EMB 170 AMM 33-50-01 AND REINSTALLED RECESSED PIN 65 ON ELECTRICAL PLUG J1162 IAW EMB 170 SWPM 20-41-10 AN 20-50-10. ELPU OPC GOOD AND EMERGENCY LIGHTS OPC GOOD.

Part: SHEAR TIE — CORRODED (AFT CARGO SHEAR) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-23-003 AFT CARGO COMPARTMENT SHEAR CLIP AT FR 82 BETWEEN STGR 27R-28R CORRODED (LEVEL 2 CORROSION)-C/A-REMOVED AND REPLACED SHEAR CLIP AT FR 82 BTW STGR 27R-28R IAW EMB 170 SRM 51-40-08.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-23-003 SHEAR CLIP AT FR 86 BETWEEN STGR 29R-29L CORRODED (LEVEL 2 CORROSION)-C/A- RAR SHEAR CLIP AT FR 86 BTW STGR 29R-29L IAW EMB 170 SRM 51-40-08.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-23-003 AFT CARGO UNDER FLOOR STGR 29L CORRODED BETWEEN FR 82-83 (LEVEL 2 CORROSION) (MAJOR REPAIR) -C/A-REMOVED AFT CARGO UNDER FLOOR STGR 29L BTW FR 80-90A AND INSTALLED AFT CARGO UNDER FLOOR STGR 29L PN:170-66555-001 BTW FR 80-90A IAW ERS-EJ-5300-4840 AND EMB 170 SRM 51-40-08.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-23-003 ? AFT CARGO UNDER FLOOR STGR 29R CORRODED BTW FR 82-83. (LEVEL 2 CORROSION) (MAJOR REPAIR) -C/A-REMOVED AFT CARGO UNDERFLOOR STRINGER BTW FR 81-90A AND INSTALLED STGR 29R PN: 170-91888-003 BTW FR 81-90A IAW ERS-EJ-5300-4840 AND EMB 170 SRM 51-40-08.

Part: UNKNOWN — CORRODED (AFT CARGO) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-23-003 AFT CARGO COMPARTMENT SHEAR CLIP AT FR 83 BETWEEN STGR 27R-28R CORRODED (LEVEL 2 CORROSION)-C/A-RAR SHEAR CLIP AT FR 83 BTW STGR 27R-28R IAW EMB 170 SRM 51-40-08

Part: SHEAR TIE — CORRODED (AFT CARGO) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-23-003 AFT CARGO COMPARTMENT SHEAR CLIP AT FR 83 BETWEEN STGR 28R-29R CORRODED (LEVEL 2 CORROSION)-C/A-REMOVED AND REPLACED SHEAR CLIP AT FR 83 BTW STGR 28R-29R IAW EMB 170 SRM 51-40-08.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-21-005 - LH LOWER OUTBD SEAT TRACK CORRODED BTW FR 26-27. (LEVEL 2 CORROSION) (MAJOR REPIAR)-C/A-BLENDED LH LOWER OUTBD SEAT TRACK CORRODED BTW FR 26-27 AND FOUND THE CROWN TEETH AREA TO BE OUT OF LIMITS AND CROWN BOTTOM AREA TO BE WITHIN LIMITS IAW EMB 170 SRM 51-10-03 AND SRM 53-21-10-AD01. PERFORMED SPLICE DEVICE REPAIR IAW EMB 170 SRM 53-00-10-REPAIR 02P.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-21-005 ? LH LOWER INBD SEAT TRACK CORRODED BTW FR 32-33. (LEVEL 2 CORROSION) (MAJOR REPAIR)-C/A-BLENDED LH LOWER INBD SEAT TRACK BETWEEN FR 32-33 AND FOUND TO BE OUT OF LIMITS IAW EMB 170 SRM 51-10-03 AND 53-21-10-AD01. REMOVED DAMAGED TEETH FROM LH LOWER INBD SEAT TRACK BETWEEN FR 32-33 IAW EMB-170 SRM 53-00-10 REPAIR 02P. NO SEAT MOUNTING POINT AT THIS LOCATION, NO SPLICE DEVICE FITTINGS REQUIRED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-21-005 - RH LOWER SEAT TRACK BETWEEN FR 32-33. (LEVEL 2 CORROSION)-C/A-BLENDED RH LOWER SEAT TRACK BETWEEN FR 32-33 AND FOUND SEAT TRACK TO BE OUT OF LIMITS IAW EMB 170 SRM 51-10-03 AND SRM 53-21-10-AD01. REMOVED DAMAGED TEETH FROM RH LOWER SEAT TRACK BETWEEN FR 32-33 IAW EMB 170 SRM 53-00-10 REPAIR 02P. SEAT IS NOT MOUNTED AT THIS LOCATION; INSTALLATION OF SPLICE DEVICE FITTINGS IS NOT REQUIRED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-21-005 ? RH LOWER SEAT TRACK CORRODED BTW FR25-26 (LEVEL 2 CORROSION)-C/A-BLENDED RH LOWER SEAT TRACK BETWEEN FR 25-26 AND FOUND TO BE OUT OF LIMITS IAW EMB 170 SRM 51-10-03 AND 53-21-10-AD01. REMOVED DAMAGED TEETH FROM RH LOWER SEAT TRACK BETWEEN FR 25-26 IAW EMB-170 SRM 53-00-10 REPAIR 02P. NO SEAT MOUNT AT THIS LOCATION, INSTALLATION OF SPLICE DEVICE FITTINGS NOT REQUIRED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

LH LOWER INBD SEAT TRACK CORRODED BTW FR 31-32 (LEVEL 2 CORROSION) (MAJOR REPAIR)-C/A-BLENDED LH LOWER INBD SEAT TRACK BETWEEN FR 31-32 AND FOUND TO BE OUT OF LIMITS IAW EMB 170 SRM 51-10-03 AND 53-21-10-AD01. REMOVED DAMAGED TEETH FROM LH LOWER INBD SEAT TRACK BETWEEN FR 31-32 IAW EMB-170 SRM 53-00-10 REPAIR 02P. NO SEAT MOUNTING POINT AT THIS LOCATION, NO SPLICE DEVICE FITTINGS REQUIRED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,202 hrs · 30,500 cycles

LH LOWER INBD SEAT TRACK GOUGED BTW FR 30-31. (MAJOR REPAIR)-C/A-BLENDED LH LOWER INBD SEAT TRACK BETWEEN FR 30-31 AND FOUND TO BE OUT OF LIMITS IAW EMB 170 SRM 51-10-03 AND 53-21-10-AD01. REMOVED DAMAGED TEETH FROM LH LOWER INBD SEAT TRACK BETWEEN FR 30-31 IAW EMB-170 SRM 53-00-10 REPAIR 02P. NO SEAT MOUNT AT THIS LOCATION, INSTALLATION OF SPLICE DEVICE FITTINGS NOT REQUIRED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-21-005 - RH LOWER SEAT TRACK CORRODED AT FR 28. (LEVEL 2 CORROSION)-C/A-BLENDED RH LOWER SEAT TRACK AT FR 28 AND FOUND TO BE OUT OF LIMITS IAW EMB 170 SRM 51-10-03 AND 53-21-10-AD10. REMOVED DAMAGED TEETH FROM RH LOWER SEAT TRACK AT FR 28 IAW EMB-170 SRM 53-00-10 REPAIR 02P. NO SEAT MOUNT AT THIS LOCATION, INSTALLATION OF SPLICE DEVICE FITTINGS NOT REQUIRED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-21-005 - LH LOWER OUTBD SEAT TRACK CORRODED JUST FWD OF FR 23. (LEVEL 2 CORROSION) (MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-21-005 ? RH LOWER SEAT TRACK CORRODED BTW FR 33-34 (LEVEL 2 CORROSION) (MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-21-005 - LH LOWER INBD SEAT TRACK CORRODED BTW FR 29-30. (LEVEL 2 CORROSION) (MAJOR REPAIR)-C/A-BLENDED CROWN TEETH AREA ON LH LOWER INBD SEAT TRACK BETWEEN FR 29-30 AND FOUND TO BE OUT OF LIMITS IAW EMB 170 SRM 51-10-03 AND 53-21-10-AD01. REMOVED DAMAGED TEETH FROM LH LOWER INBD SEAT TRACK BETWEEN FR 29-30 IAW EMB-170 SRM 53-00-10 REPAIR 02P. NO SEAT AT THIS LOCATION, SPLICE DEVICE FITTINGS NOT REQUIRED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-21-005 - RH LOWER SEAT TRACK CORRODED BTW FR 30-31. (MAJOR REPAIR) (LEVEL 2 CORROSION)-C/A-BLENDED RH LOWER SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW EMB 170 SRM 51-10-03 AND 53-21-10-AD01. REMOVED DAMAGED TEETH FROM RH LOWER SEAT TRACK BETWEEN FR 30-31 IAW EMB-170 SRM 53-00-10 REPAIR 02P. NO SEAT MOUNT AT THIS LOCATION, INSTALLATION OF SPLICE DEVICE FITTINGS NOT REQUIRED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-21-005 - RH LOWER SEAT TRACK CORRODED BTW FR 26-27 (LEVEL 2 CORROSION)-C/A-ACCOMPLISHED PERMANENT REPAIR ON RH LOWER SEAT TRACK CORRODED BETWEEN FR 26-27 IAW ERS-EJ-5300-4852

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,202 hrs · 30,500 cycles

RH LOWER SEAT TRACK GOUGED FR 75-76. (MAJOR REPAIR)-C/A-BLENDED RH LOWER SEAT TRACK BETWEEN FR 75-76 AND FOUND TO BE OUT OF LIMITS IAW EMB 170 SRM 51-10-03, AND 53-23-01-AD01. REMOVED DAMAGED TEETH FROM RH LOWER SEAT TRACK BETWEEN FR 75-76 IAW EMB-170 SRM 53-00-10 REPAIR 02P. NO SEAT MOUNT AT THIS LOCATION, INSTALLATION OF SPLICE DEVICE FITTINGS NOT REQUIRED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,202 hrs · 30,500 cycles

RH LOWER SEAT TRACK GOUGED BETWEEN FR 81-82 (MAJOR REPAIR)-C/A-BLENDED GOUGE ON RH LOWER SEAT TRACK BETWEEN FR 81-82 AND FOUND TO BE OUT OF LIMITS IAW EMB 170 SRM 51-10-03 AND 53-23-10-AD01. REMOVED DAMAGED TEETH FROM RH LOWER SEAT TRACK BETWEEN FR 81-82 IAW EMB-170 SRM 53-00-10 REPAIR 02P. NO SEAT MOUNT AT THIS LOCATION, INSTALLATION OF SPLICE DEVICE FITTINGS NOT REQUIRED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,202 hrs · 30,500 cycles

LH LOWER SEAT TRACK GOUGED BETWEEN FR 81-82 (MAJOR REPAIR)-C/A-BLENDED LH LOWER SEAT TRACK BETWEEN FR 81-82 AND FOUND TO BE OUT OF LIMITS IAW EMB 170 SRM 51-10-03 AND 53-23-10-AD01. REMOVED DAMAGED TEETH FROM LH LOWER SEAT TRACK BETWEEN FR 81-82 IAW EMB-170 SRM 53-00-10 REPAIR 02P. NO SEAT MOUNT AT THIS LOCATION, INSTALLATION OF SPLICE DEVICE FITTINGS NOT REQUIRED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,202 hrs · 30,500 cycles

RH LOWER SEAT TRACK GOUGED BETWEEN FR 82-83 (MAJOR REPAIR)-C/A- BLENDED GOUGE ON RH LOWER SEAT TRACK BETWEEN FR 82-83 AND FOUND TO BE OUT OF LIMITS IAW EMB 170 SRM 51-10-03 AND 53-25-10-AD01. REMOVED DAMAGED TEETH FROM RH LOWER SEAT TRACK BETWEEN FR 82-83 IAW EMB-170 SRM 53-00-10 REPAIR 02P. NO SEAT MOUNT AT THIS LOCATION, INSTALLATION OF SPLICE DEVICE FITTINGS NOT REQUIRED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-23-003 CARGO UNDERFLOOR FR 75 SHEAR CLIP CORRODED AT STGR 25L (LEVEL 2 CORROSION)-C/A-RAR CARGO UNDERFLOOR SHEAR CLIP AT FR 75 STGR 24L-25L IAW EMB 170 SRM 51-40-08.

Part: SHEAR PANEL — CORRODED (UNKNOWN) · corrosion level 2 · airframe 48,202 hrs · 30,500 cycles

SSI 53-23-005 RH SHEAR PANEL CORRODED BETWEEN FR 87-88 (LEVEL 2 CORROSION)-C/A-RAR R/H SHEAR PANEL BETWEEN FR87/88 IAW EMB 170 SRM 51-40-08

Part: SHEAR PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,894 hrs · 29,525 cycles

FWD CARGO SHEAR CLIP AT FR 17 RH BTWN STR RH 25 & 26 CORRODED. R&R IAW SRM 51-41-01 7 51-41-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,894 hrs · 29,525 cycles

CF III LH SET TRACK AT FR 84, LBL 9 CORRODED. R&R IAW SRM 53-23-10 REPAIR 04.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,894 hrs · 29,525 cycles

FWD FSLG FLOOR RH I/B SEAT TRACK BTWN FR 12 & 20 CORRODED. R&R IAW SRM 51-41-02, 51-43-02 & 51-43-04.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,894 hrs · 29,525 cycles

FWD FSLG FLOOR LH I/B SEAT TRACK BTWN FR 12-20 CORRODED. R&R IAW SRM 51-41-01, 51-41-02, 51-43-03 & 51-43-04.

Part: DOUBLER — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,894 hrs · 29,525 cycles

FWD FSLG FLOOR LH DOUBLER BTWN FR 19 & 20 CORRODED. R&R IAW SRM 51-41-02 & 451-43-04.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,894 hrs · 29,525 cycles

CF III PAX CABIN FR 84 RH PNL SUPPORT AT RBL 38 CORRODED. R&R IAW SRM 51-41-02 AND 51-41-01

Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,894 hrs · 29,525 cycles

CF III FLOOR RH O/B SHEAR PNL AT FR 87 & 88 CORRODED. R&R IAW SRM 51-42-01 & 51-42-02.

Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,894 hrs · 29,525 cycles

CF III PAX CABIN AT FR 84 FROM RBL 12 TO RBL 33 CORRODED. R&R CROSSBEAM IAW SRM 51-43-03, 51-41-01.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,894 hrs · 29,525 cycles

CF III FLOOR GUSSET PLATE AT RH FR 90, RBL 9. R&R IAW SRM 51-41-02.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,894 hrs · 29,525 cycles

CF III FLOOR GUSSET PLATE AT RH FR 90, RBL 9. R&R IAW SRM 51-41-02.

Part: UPPER SHEET — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,894 hrs · 29,525 cycles

CF III FLOOR SUPPORT LH UPPER SHEET AT FR 85 & 86, LBL 9 CORRODED. R&R IAW SRM 51-41-01 & 51-43-03.

Part: UPPER SHEET — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,894 hrs · 29,525 cycles

CF IIICABIN FLOOR UPPER SHEET AT FR 85 RH TO 86 RH, RBL 9 CORRODED. R&R IAW SRM 51-41-01 & 51-43-01.

Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,894 hrs · 29,525 cycles

CF III FLOOR LH O/B SHEAR PNL AT FR 87 & 88 CORRODED. R&R IAW SRM 51-42-01, 51-41-02 & 51-43-01.

Part: SUPPORT BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,894 hrs · 29,525 cycles

CF III FLOOR RH BEAM AT FR 86 TO 89, RBL 9 CORRODED. R&R IAW SRM 51-43-01 & 51-41-01.

Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,894 hrs · 29,525 cycles

CF III FLOOR CENTER SHEAR PNL AT FR 87 & 88 CORRODED. R&R IAW SRM 51-42-61.

Part: I/O MODULE — FAULT MESSAGE (ZONE 100) · airframe 45,461 hrs · 28,541 cycles

SUPPLEMENTAL INFORMATION.

Part: I/O MODULE — FAULT MESSAGE (ZONE 100) · airframe 45,461 hrs · 28,541 cycles

TAT 1 FAIL, SPDBRK FAIL, ADS 1 FAIL, SPOILER FAULT, AND AVNX MAU 3A FAULT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R CUSTOM I/O MODULE 2 AND GENERIC I/O MODULE 1.

Part: WIRE HARNESS — INTERMITTENT (MLG) · airframe 45,024 hrs · 28,239 cycles

RETURN TO FIELD FOR LANDING GEAR WON'T RETRACT, LEVER STUCK IN DOWN POSITION AFTER TAKE-OFF. R/R STEERING FEEDBACK AND WOW SENSOR 2 HARNESS, OPS CHECK GOOD.

Part: HYDRAULIC LINE — DEFECTIVE (LT MLG) · airframe 42,817 hrs · 26,733 cycles

WHILE ON APPROACH, THE FLIGHT CREW REPORTED A HYDRAULIC SYSTEM 2 LOW PRESSURE MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. UPON LANDING SAFELY, THE AIRCRAFT REQUIRED A TOW TO THE GATE. REPLACED THE LEFT-HAND MAIN LANDING GEAR DOWN LOCK RELEASE ACTUATOR HYDRAULIC LINE IAW AMM 29-10-13.

Part: CROSSBEAM — CRACKED (FRAME 12) · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK***FR 12 CROSSBEAM FWD SIDE, LBL 36, ANGLE FOUND CRACKED. REPLACED ANGLE IAW SRM 51-41-01.***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: CROSSBEAM — CRACKED (FRAME 12) · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK***FR 12 CROSSBEAM FWD SIDE, BL 0, ANGLE FOUND CRACKED. REPLACED ANGLE IAW SRM 51-41-01.***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** SHEAR CLIP CORRODED AT FRT 16 BTW STR 27-28L. REPLACED SHEAR CLIP IAW SRM 51-41-01/02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** SHEAR CLIP CORRODED AT FRT 16 BTW STR 26-27L. REPLACED SHEAR CLIP IAW SRM 51-43-03. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK***L/H HORIZ STAB RIB 10A FOUND CRACKED. REPLACEMENT COVERED BY EMBODIMENT OF 170EO-55-10-0004_1. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK***R/H HORIZ STAB RIB 12A FOUND CRACKED. REPLACEMENT COVERED BY EMBODIMENT OF 170EO-55-10-0004_1. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK***R/H HORIZ STAB RIB 14 FOUND CRACKED. REPLACED RIB IAW SRM 51-41-01/02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: FLOOR SUPPORT — CRACKED (FRAME 86) · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK***FLOOR PANEL SUPPORT FOUND CRACKED AT FR 86, LBL 24. REPLACED SUPPORT BRACKET IAW SRM 51-41-00.***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: CROSSBEAM — CORRODED (FRAME 84) · corrosion level 2 · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CORROSION AND SCRIBE MARKS FOUND AT CROSSBEAM, FR 84 BTW RBL 5 AND RBL 36. REPAIRED CROSSBEAM IAW ETD2020-170-001102. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SUPPORT — CORRODED (FRAMES 88-89) · corrosion level 2 · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CORROSION FOUND ON PANEL SUPPORT BTW FR 88-89 LBL 36. REPLACED PANEL SUPPORT IAW SRM 51-43-03 AND 51-41-01. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CORROSION FOUND ON FLOOR STRUCTURE GUSSET PLATE AT FR 90, RBL 24. REPLACED GUSSET PLATE IAW SRM 51-41-02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SEAT TRACK — CORRODED (FRAMES 12-18) · corrosion level 2 · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** R/H SEAT TRACK CORRODED ON TOP BTW FR 12-18. REPLACED SEAT TRACK IAW SRM 51-41-01 AND 51-43-04. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CORROSION FOUND ON PANEL SUPPORT, FR 84 RBL 36. REPLACED SUPPORT IAW SRM 51-41-02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SUPPORT — CORRODED (FRAMES 88-89) · corrosion level 2 · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CORROSION FOUND ON PANEL SUPPORT BTW FR 88-89 RBL 36. REPLACED PANEL SUPPORT IAW SRM 51-43-03. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FRAME 75) · corrosion level 2 · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** SHEAR CLIP CORRODED AT FRT 75 BTW STR 28-29R. REPLACED SHEAR CLIP IAW SRM 51-41-01/02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FRAME 81) · corrosion level 2 · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** AFT CARGO,SHEAR CLIP CORRODED AT FR 81 BTW STR 29R-29L.REPLACED SHEAR CLIP IAW SRM 51-41-01/02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SUPPORT BRACKET — CORRODED (FRAME 84) · corrosion level 2 · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** AFT CARGO, R/H SUPPORT BRACKET CORRODED AT FR 84 BTW 29R-29L. REPLACED SUPPORT BRACKET IAW SRM 51-41-01/02 AND 51-43-03. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FRME 84) · corrosion level 2 · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** AFT CARGO, SHEAR CLIP CORRODED AT FR 84 BTW STR 28-29R. REPLACED SHEAR CLIP IAW SRM 51-41-01/02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SKIN — CORRODED (FRAMES 76-80) · corrosion level 2 · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CORROSION ON SKIN PANEL (INTERNAL) AROUND RIVETS BTW FR 76 BTW STR 29L-29R. REPAIRED SKIN PANEL IAW ETD2020-170-001065. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SUPPORT BRACKET — CORRODED (FRAME 76) · corrosion level 2 · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** AFT CARGO, R/H AND L/H SUPPORT BRACKETS CORRODED AT FR 76 BTW STR 29R-29L.REPLACED BRACKETS IAW SRM 51-41-01/02. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FRAME 84) · corrosion level 2 · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** SHEAR CLIP CORRODED AT FRT 84 BTW STR 27-28R. REPLACED SHEAR CLIP IAW SRM 51-41-01. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** EMERGENCY LIGHT POWER UNIT #2 FAILED FUNCTIONAL TEST. REPLACED ELPU IAW AMM 33-50-01/400. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,295 hrs · 26,418 cycles

***AIRCRAFT IS IN HEAVY CHECK*** AFT ENTRANCE EMERGENCY EXIT LOCATOR SIGN FOUND INOP. REPLACED EMERGENCY EXIT MARKING SIGN IAW AMM 33-50-17-400-801-A. ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: DOOR SEAL — DEFECTIVE (L1 DOOR) · airframe 39,567 hrs · 24,763 cycles

DOOR L1 HISSING WHILE CABIN PRESSURIZED. NO ABNORMAL INDICATIONS. FERRIED TO IND. R&R L1 DOOR SEAL.

Part: WARNING LIGHT — FALSE ACTIVATION (FUEL LOW) · airframe 39,200 hrs · 24,540 cycles

FUEL 1 LOW LEVEL, 5,000 LBS SHOWING ON LH SIDE. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. PERFORMED WIRE CHECKS PER FIM 28-44-00-810-803A, OPS CHECK GOOD. FOUND TO BE TRANSITORY.

Part: LIGHT — DETACHED (CABIN) · airframe 36,577 hrs · 22,919 cycles

EMERGENCY LIGHT STRIP NEAR SEAT 1D WAS DISCOVERED MISSING. FOUND AND SECURED.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,512 hrs · 22,877 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. MAINTENANCE FOUND LEVEL 2 CORROSION ON SEAR CLIP. THEY REMOVED AND REPLACED CLIP IAW SRM 51-41-01. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,512 hrs · 22,877 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. MAINTENANCE FOUND LEVEL 2 CORROSION ON SHEAR TIE AND STABILIZER. THEY REMOVED AND REPLACED SHEAR TIE AND STABILIZER IAW SRM 51-41-01, 51-43-03. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,512 hrs · 22,877 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. MAINTENANCE FOUND LEVEL 2 CORROSION ON GUSSET AT FR 90 RBL 24. THEY REMOVED AND REPLACED GUSSET IAW SRM 51-10-03 AND 51-41-02. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,512 hrs · 22,877 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. MAINTENANCE FOUND LEVEL 2 CORROSION AFT WET AREA CENTER SHEAR PANEL FR 87 TO FR 88. THEY REMOVED AND REPLACED PANEL IAW SRM 51-42-01 AND 51-40-02. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,512 hrs · 22,877 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. MAINTENANCE FOUND LEVEL 2 CORROSION AFT WET AREA RT SHEAR PANEL FR 87 TO FR 88. THEY REMOVED AND REPLACED PANEL IAW SRM 51-42-01, 51-43-03 AND 51-40-02. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: STRINGER — CORRODED (FRAMES 86-90) · corrosion level 2 · airframe 36,512 hrs · 22,877 cycles

MAINTENANCE FOUND CORROSION ON STRINGER 28R, BETWEEN FRAMES 86 TO 90. REPAIRED IAW ETD 2018-170-000038.

Part: RIB — CRACKED (ZONE 100) · airframe 36,512 hrs · 22,877 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. MAINTENANCE FOUND CRACK AT FRAME 52 LT WTF DOUBLER CRACK. THEY REMOVED AND REPLACED LT FRAME 52 RIB IAW SRM 51-40-02 AND 01. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: DOOR — CORRODED (LAV SERVICE) · corrosion level 2 · airframe 36,512 hrs · 22,877 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY MAINTENANCE CHECK. MAINTENANCE FOUND LEVEL 2 CORROSION AT AFT FUSELAGE WASTE SERVICE DOOR EXTERNAL SIDE. THEY REMOVED AND REPLACED SERVICE DOOR IAW AMM 53-03-60. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: GIRT BAR — OUT OF ADJUST (R2 DOOR) · airframe 31,867 hrs · 19,786 cycles

R2 DOOR HARD TO DISARM. ADJUSTED R2 FWD FLOOR GIRT BAR FITTING, OPS CHECK GOOD REF AMM 53-01-39, 52-42-20.

Part: SHEAR PLATE — CORRODED (CARGO DOOR) · airframe 31,846 hrs · 19,777 cycles

CORROSION AROUND SCREW HOLE IN AFT CARGO PIT ON DOOR SHEAR PLATE AT FRAME 80 AT STR 26R. R & R SHEAR PLATE, FINGER PLATE, IN AFT CARGO DOOR CUTOUT AFT FINGER PLATE.

Part: SEAL REST — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 31,846 hrs · 19,777 cycles

AFT CARGO DOOR CUTOUT AFT CORNER SEAL REST CORRODED. R & R AFT CARGO DOOR CUTOUT AFT CORNER SEAL REST.

Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 31,846 hrs · 19,777 cycles

LT SHEAR PLATE AT FRAME 87 IS CORRODED. R & R SHEAR PANEL IAW SRM 51-42-01 AND 51-43-01.

Part: SEAL REST — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 31,846 hrs · 19,777 cycles

AFT CARGO DOOR CUTOUT MIDDLE SEAL REST CORRODED. R & R SEAL REST AFT CARGO DOOR CUTOUT LOWER CENTER IAW SRM 51-40-02 AND 51-41-01.

Part: BEAM — CORRODED (CARGO DOOR FRAME) · airframe 31,846 hrs · 19,777 cycles

FWD CARGO DOOR CUTOUT LOWER BEAM HAS CORROSION. R & R FWD CARGO DOOR CUTOUT LOWER BEAM IAW SRM 51-40-02, 51-41-02, AND 51-43-02.

Part: SEAL REST — CORRODED (CARGO DOORWAY) · airframe 31,846 hrs · 19,777 cycles

POSSIBLE CORROSION ON FWD CARGO DOOR MIDDLE SEAL REST, RT ABOVE CARGO DOOR LATCH FITTINGS. R & R FWD CARGO DOOR CUTOUT MIDDLE SEAL REST IAW SRM 51-40-02 AND 51-41-01.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,846 hrs · 19,777 cycles

FWD CARGO DOOR CUTOUT LOWER AFT DOUBLER CORRODED. R & R FWD CARGO DOOR CUTOUT LOWER AFT DOUBLER IAW SRM 51-40-02, 51-41-02, 51-43-02.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 31,846 hrs · 19,777 cycles

FWD CARGO DOOR CUTOUT LWR FWD DOUBLER CORRODED. REMOVED DOUBLER, MATCH DRILLED AND INSTALLED NEW FWD CARGO DOOR CUTOUT LWR FWD DOUBLER IAW SRM 51-40-02 AND 51-43-02.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 31,861 hrs · 19,783 cycles

FWD CARGO DOOR CUTOUT LOWER FWD DOUBLER CORRODED. REMOVED DOUBLE. MATCH DRILLED AND INSTALLED NEW FWD CARGO DOOR CUTOUT LOWER FWD DOUBLER IAW SRM 51-40-02 AND 51-43-02.

Part: SHEAR PLATE — CORRODED (FRAME 16) · corrosion level 2 · airframe 31,846 hrs · 19,777 cycles

CORROSION ON SHEAR PLATE AT FRAME 16, OTBD OF LT FLOORBEAM. R & R CORRODED FASTENER, RESTORED TOP COAT IAW SRM 51-40-02, 51-41-02, AND 51-23-06.

Part: SUPPORT FRAME — CRACKED (FAIRING) · airframe 31,846 hrs · 19,777 cycles

RT AFT FIXED PYLON FAIRING FRAME 3 CRACKED AT OTBD BOLT HOLE. REMOVED CRACKED FRAME 3, MATCH DRILLED, AND INSTALLED NEW FRAME 3 IAW SRM 51-43-03 AND 51-43-04.

Part: COVER — CRACKED (EMERGENCY LIGHTS) · airframe 30,854 hrs · 19,144 cycles

FWD EMERGENCY EXIT COVER CRACKED. R & R FWD EMERGENCY EXIT COVER IAW AMM 33-50-17.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 29,868 hrs · 18,464 cycles

LEFT FWD MLG WHEEL WELL OTBD CENTER BELLY FAIRING SUPPORT BULKHEAD UPPER SECTION CRACKED. CUTOUT CRACK ON LT FWD MLG WHEEL WELL OTBD CENTER BELLY FAIRING SUPPORT BULKHEAD UPPER SECTION IAW SRM 53-22-04.

Part: ROD END — LOOSE (L1 DOOR) · airframe 26,226 hrs · 16,253 cycles

L1 DOOR HANDLE WILL NOT ARM. TIGHTENED LOOSE VISUAL INDICATION ROD END AND ADJUSTED DOOR IAW AMM 52-11-00, OPS CHECK GOOD.

Part: SHEAR TIE — UNKNOWN (ZONE 100) · airframe 26,225 hrs · 16,252 cycles

SHEAR TIE JUST FWD INBD OF WASTE BOX. R & R SHEAR TIE. MAJOR REPAIR.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,225 hrs · 16,252 cycles

CORROSION FOUND ON WASTE BOX SKIN DOUBLER. R & R WASTE BOX SKIN DOUBLER.

Part: NUT PLATE — CORRODED (ZONE 100) · airframe 26,225 hrs · 16,252 cycles

CORROSION FOUND ON NUT PLATE BRACKET ON FWD CARGO SILL. R & R SUPPORT, PN 170-67176-403.

Part: RIB — CRACKED (LT WING) · airframe 26,225 hrs · 16,252 cycles

CRACK FOUND ON LT WING L/E RIB NR 28, AFT OF SLAT 3. R & R L/E RIB 28 ON LT WING .

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 26,225 hrs · 16,252 cycles

THREE CRACKS IN RT HORZONTAL STAB RIB II ANGLES, 1ST AND 2ND LOWER ANGLES AFT OF SPAR 1 AND 1ST UPPER ANGLE AFT OF SPAR 1. REPAIRED LWR FWD FLANGE CRACK, UPPER FWD FLANGE CRACK AND AFT LWR FLANGE CRACK ON RIB IIA IAW ETD2014-170-004836, REV A. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 26,225 hrs · 16,252 cycles

CORROSION FOUND ON RT INBD SEAT TRACK AT FRAME 17. R & R RT SEAT TRACK.

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,225 hrs · 16,252 cycles

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

Part: SILL — CORRODED (R2 DOORWAY) · corrosion level 2 · airframe 26,225 hrs · 16,252 cycles

CORROSION ON RT R2 DOOR SILL. PERFORMED TEMP REPAIR IAW ETD2014-170-003896.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,225 hrs · 16,252 cycles

CORROSION FOUND ON FRAME 84 FLOOR SUPPORT. R & R FLOOR SUPPORT.

Part: VAPOR BARRIER — CRACKED (WING) · airframe 26,225 hrs · 16,252 cycles

CRACKS FOUND ON WING STUB REAR VAPOR BARRIER ASSY AROUND BOLT HEADS. REMOVED, FABRICATED, REPLACED NEW WING STUB REAR VAPOR BARRIER. PN 170-30726-003, 170-30636-003.

Part: FLOORBEAM — DAMAGED (FRAME 14) · airframe 26,225 hrs · 16,252 cycles

FWD WET AREA AT FR14, RT SIDE IN ONE SPOT. REPAIR FLOORBEAM AT FR14 WITH A L-DOUBLER AND FILLER IAW ETD2014-170-003654. MAJOR REPAIR

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 26,225 hrs · 16,252 cycles

CRACK ON VERTICAL STAB REAR SPAR FILLET CRACKED IN 2 PLACES RT SIDE ABOVE UPPER STRUT RIB 9/10. TRIMMES AFFECTED RIB FLANGES, FABRICATED SHEAR CLIP, FABRICATED FILLER, MATCH DRILLED AND INSTALLED.

Part: DRAIN — CORRODED (LAVATORY) · airframe 26,225 hrs · 16,252 cycles

CORROSION FOUND ON LAV DRAIN BOX ON INTERNAL SIDE OF ACFT. R & R LAV DRAIN BOX.

Part: FITTING — CORRODED (GIRT BAR) · airframe 26,225 hrs · 16,252 cycles

GIRT BAR FLOOR FITTINGS HAVE CORROSION INSIDE THEM, L1. R & R L1 LOWER FLOORBEAM IAW SRM 51-41-01, 51-43-01, 51-43-02, 51-41-01, MAJOR REPAIR

Part: ENGINE — VIBRATION (RIGHT) · airframe 25,488 hrs · 15,791 cycles

DURING CLIMB, NOTICED VIBRATION FROM RT ENGINE, VIBRATION REDUCED WITH POWER REDUCED. RECEIVED ENG 2 T2 HEAT FAIL MESSAGE, RAN QRH. ATC REPORTED AFTER TAKE OFF, TIRE RUBBER ON RUNWAY. DIVERTED, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. MX R & R ENGINE AND TIRES.

Part: MECHANISM — DIRTY (L1 DOOR) · airframe 23,878 hrs · 14,824 cycles

GATE AGENT REPORTS L1 DOOR HARD TO OPEN FROM OUTSIDE. CLEANED AND LUBED L1 DOOR ACTUATING AND LOCKING MECHANISM IAW AMM 52-11-20.

Part: SEAL — LOOSE (WINDOW) · airframe 23,362 hrs · 14,505 cycles

AT FL280 WINDOW SEAL ON CAPTAINS SIDE WINDOW CAME LOOSE AND WAS HITTING THE WINDOW. DIVERTED TO DTW. APPLIED SPEED TAPE TO DAMAGED HUMP SEAL AND PLACED ON DMI.

Part: SENSOR — OUT OF ADJUST (L2 DOOR) · airframe 22,406 hrs · 13,915 cycles

DURING APPRAOCH "DOOR PAX AFT OPEN" WARNING. MFD STATUS PAGE SHOWED L2 DOOR RED AND PRESSURIZATION APPEARED NORMAL. VERIFIED DOOR CLOSED AND ALL INDICATIONS NORMAL ON GROUND WITH DOOR UNARMED. ADJUSTED L2 DOOR LATCH SENSOR IAW AMM 52-72-21. OPS CHECK GOOD.

Part: INDICATOR — OUT OF ADJUST (L1 DOOR) · airframe 21,011 hrs · 13,081 cycles

L1 DISARM INDICATOR NOT FULL IN WINDOW. ADJUSTED ARM/DISARM INDICATOR, OPS CHECK GOOD IAW EMB 170 MM 52-11-00.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 20,993 hrs · 13,067 cycles

LEVEL 2 CORROSION, FRAME 11 COCKPIT FLOORBEAM AND CENTER SPLICE. FABRICATED AND INSTALLED REPAIR DOUBLERS ON FRAME 11 IAW ETD 2012-170-004722 AND SRM 51-41-02 AND 51-43-01.

Part: CROSSBEAM — DAMAGED (L2 DOOR) · airframe 20,993 hrs · 13,067 cycles

MAJOR REPAIR - DAMAGE ON L2 DOOR HORIZONTAL BEAM. REPAIRED CROSSBEAM 86 AROUND L2 DOOR IAW ETD 2012-170/004319 REV A.

Part: SPAR — CRACKED (ZONE 500) · airframe 20,993 hrs · 13,067 cycles

LEFT WING SPAR 2 RIB 10 EXTENSION CRACKED AT 3RD HI-LOK FROM BACK. REMOVED AND REPLACED LT WING SPAR 2 RIB 10 IAW EMB 170 SRM 51-43-03 AND 51-43-04. MAJOR REPAIR

Part: RIB — CRACKED (RT WING) · airframe 20,993 hrs · 13,067 cycles

RT WING SPAR 2 RIB 10 EXTENSION CRACKED. REMOVED AND INSTALLED NEW RIB 10 AND ATTACH FASTENERS IAW EMB 170 SRM 51-43-01, 51-43-02, AND 51-40-02.

Part: INDICATOR — OUT OF ADJUST (L2 DOOR) · airframe 20,936 hrs · 13,032 cycles

L2 DOOR GIRT BAR INDICATION WINDOW CLEAR WHEN DOOR IS ARMED. ADJUSTED L2 DOOR GIRT INDICATOR IAW EMB 170 MM 52-70-01. OPS CHECK GOOD.

Part: HINGE — DIRTY (MAIN DOOR) · airframe 20,928 hrs · 13,025 cycles

MAIN DOOR HARD TO OPEN FROM THE OUTSIDE. CLEANED AND LUBRICATED DOOR HINGE POINTS, OPS CHECK GOOD IAW EMB 170 MM 52-11-00.

Part: DOOR — OUT OF POSITION (L2) · airframe 20,893 hrs · 13,003 cycles

CLEANERS REPORTED L2 DOOR WON'T CLOSE. SET L2 DOOR BACK ON TRACK AS REQUIRED, OPERATED DOOR IAW AMM 52-12-00.

Part: ACM — INOPERATIVE (AC BAY) · airframe 20,035 hrs · 12,472 cycles

HEARD NOISE AND POP SOUND FOLLOWED BY SMOKE SMELL AND HAZE IN COCKPIT AND REPORTED IN CABIN, ON TAKEOFF. DECLARED EMERGENCY AND RETURNED TO DEN. OVERWEIGHT LANDING DUE TO EMERGENCY, LANDING WEIGHT APPROX 76,000 APPROACH DESCENT RATE 700 FPM LANDING DECENT RATE LESS THAN 100 FPM. PERFORMED GVI OF GEAR/TIRES AND BRAKES, NO DEFECTS NOTED, LANDING PARAMETERS WITHIN LIMITS IAW EMB 170 MM 05-50-27. PERFORMED GROUND RUNS IAW EMB 170 AMM 71-00-01, DETERMINED SMELL COMING FROM PACK NR 1, DEFERRED. REPLACED PACK 1 ACM IAW EMB 170 AMM 21-51-05, OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (GALLEY DOOR) · airframe 19,289 hrs · 12,016 cycles

AFT GALLEY DOOR 2L ARMING LEVER DOES NOT LINE UP WITH VENT FLAP. PERFORMED OPS CHECK OF L2 DOOR VENT FLAP IAW EMB MM 52-12-25. NO DEFECTS NOTED.

Part: GIRT BAR — DETACHED (L2 DOOR) · airframe 19,108 hrs · 11,907 cycles

L2 DOOR DOESN'T ARM. RE-ATTACHED GIRT BAR TO DOOR CLIP AS REQUIRED. OPS CHECK OF L2 DOOR GOOD IAW EMB 170 MM 52-12-00.

Part: GIRT BAR — OBSTRUCTED (L2 DOOR) · airframe 18,063 hrs · 11,291 cycles

L2 DOOR WILL NOT ARM. INSPECTED AND FOUND DEBRIS AROUND GIRT BAR RETAINER. CLEANED AREA AROUND GIRT BAR AND DOOR THRESHOLD. OPS CHECK GOOD.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,898 hrs · 11,236 cycles

LEVEL 2 CORROSION AND GOUGE LT CF3 FLOOR TRACK. REMOVED AND REPLACED LT CF3 IAW EMB 170 SRM 51-41-01.

Part: GLOWSTRIP — OUT OF POSITION (CABIN) · airframe 17,337 hrs · 10,860 cycles

ESCAPE PATH LIGHT STRIP OUT OF PLACE AT ROWS RT SIDE 15-18. RE-ADJUSTED ESCAPE PATH PHOTO LUMINESCENT STRIP AND INSTALLED IAW EMB 170 MM 33-50-21. OK FOR SERVICE.

Part: SLIDE — UNWANTED DEPLOY (L2 DOOR) · airframe 15,589 hrs · 9,788 cycles

CATERING OPENED L2 DOOR CAUSING SLIDE DEPLOYMENT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EVACUATION SLIDE.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,310 hrs · 10,724 cycles

LEVEL 2 CORROSION BETWEEN RT AND LT OMEGA BEAMS, FR 87-88. REMOVED AND REPLACED SHEAR PLATE IAW EMB 170 SRM 51-42-00.

Part: MECHANISM — OUT OF ADJUST (L2 DOOR) · airframe 15,589 hrs · 9,788 cycles

L2 DOOR ARMING HANDLE NOT SEATING PROPERLY. ADJUSTED EMERGENCY ARM MECHANISM IAW 52-12-40-700-801A. OPS CHECK GOOD.

Part: MECHANISM — OUT OF ADJUST (L2 DOOR) · airframe 15,589 hrs · 9,788 cycles

L2 DOOR ARMING HANDLE NOT SEATING PROPERLY. ADJUSTED EMERGENCY ARM MECHANISM IAW EMB MM 52-12-40-700-801-A. OPS CHECK GOOD.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,589 hrs · 9,788 cycles

LEVEL 2 CORROSION AT RT SHEAR PLATE BETWEEN FR 87-88. REMOVED AND REPLACED RT SHEAR PLATE IAW EMB 170 SRM 51-42-01 AND 51-43-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,589 hrs · 9,788 cycles

MAJOR REPAIR - LT CENTER FLOORBEAM CORRODED AT FRS 17-19. REMOVED DAMAGED AREAS, FABRICATED FILLER AND DOUBLER, NDT CUTOUT AND INSTALLED IAW ETD 2010-170/07407.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,589 hrs · 9,788 cycles

MAJOR REPAIR - LEVEL 2 CORROSION AT RT SEAT TRACK BEAM BETWEEN FR 85 AND FR 86. REMOVED AND REPLACED RT SEAT TRACK BEAM AT FR 85-FR 86 IAW EMB 170 SRM 51-41-01 AND 51-43-01.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,589 hrs · 9,788 cycles

LEVEL 2 CORROSION LT SHEAR PLATE IN FWD GALLEY, IN TWO AREAS ON EDGE AT FR16. REMOVED AND REPLACED LT SHEAR PLATE IAW EMB 170 SRM 51-41-02.

Part: SILL — CORRODED (PAX DOOR) · airframe 15,589 hrs · 9,788 cycles

LEVEL 2 CORROSION AFT PASSENGER DOOR LOWER SILL. REMOVED AND REPLACED AFT PASSENGER DOOR LOWER SILL IAW EMB 170 SRM 51-43-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,589 hrs · 9,788 cycles

LEVEL 2 CORROSION RT CENTER FLOORBEAM AT FR 14, 16, 17. REMOVED AND REPLACED RT CENTER SEAT TRACK BEAM IAW EMB 170 SRM 51-40-02, 51-41-01, 51-43-01, 51-41-02, 51-43-03 AND 51-43-04.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,589 hrs · 9,788 cycles

LEVEL 2 CORROSION RT SEAT TRACK BEAM GUSSET AT FR90. REMOVED AND REPLACED GUSSET IAW EMB 170 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,589 hrs · 9,788 cycles

LEVEL 2 CORROSION AT RT SEAT TRACK BEAM BETWEEN FR 87-88. REMOVED AND REPLACED SEAT TRACK BEAM IAW EMB 170 SRM 51-41-01 AND 51-43-01.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,589 hrs · 9,788 cycles

LEVEL 2 CORROSION WASTE TANK HOLD DOWN GUSSET AT FR90. REMOVED AND REPLACED GUSSET IAW EMB 170 SRM 51-41-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,589 hrs · 9,788 cycles

MAJOR REPAIR - LEVEL 2 CORROSION LT CENTER FLOORBEAM AT FR 17-19. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER, NDT CUTOUT, AND INSTALLED IAW EMB ETD 2010-170/07407.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,995 hrs · 7,680 cycles

FLOOR GUSSET AT JCT OF FR90 AND LT FLOORBEAM LEVEL 2 CORROSION. REMOVED AND REPLACED IAW SRM 51-41-02.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,995 hrs · 7,680 cycles

LEVEL 2 CORROSION ON AFT INNER DOUBLER OF WATER SERVICE BOX. REMOVED AND REPLACED DOUBLER IAW SRM 51-43-04.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,995 hrs · 7,680 cycles

LEVEL 2 CORROSION ON AFT AND FWD INNER DOUBLER OF WASTE SERVICE BOX. REMOVED AND REPLACED WASTE SERVICE BOX AFT AND FWD INNER DOUBLER IAW SRM 51-43-04.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,995 hrs · 7,680 cycles

LT FLOORBEAM BETWEEN FR85-89 LEVEL 2 CORROSION. REMOVED AND REPLACED IAW SRM 51-41-01 AND 51-43-01.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,995 hrs · 7,680 cycles

FLOOR GUSSET AT JCT OF FR90 AND RT FLOORBEAM LEVEL 2 CORROSION. REMOVED AND REPLACED IAW SRM 51-41-02.

Part: SLIDE — MISMANUFACTURED (L1 DOOR) · airframe 7,637 hrs · 4,968 cycles

DURING A SCHEDULED OPS CHECK OF L1 DOOR AND SLIDE THE SLIDE EXTENDED INVERTED (COMPLETELY UPSIDE DOWN) WHICH CAUSED MINOR DAMAGE BENEATH L1 DOOR OPENING. THE FUSELAGE DAMAGE WAS ADDRESSED WITH AN IC2007-170/07425. THE SLIDE VENDOR HAS BEEN CONTACTED AND AN INVESTIGATION IS UNDERWAY TO DISCOVER THE ROOT CAUSE.

Part: ACCELEROMETER — DEFECTIVE (NR 2 ENGINE) · airframe 5,966 hrs · 3,917 cycles

FLIGHT 7542 IAD TO YUL - DURING CLIMBOUT AND DURING CRUISE CREW REPORTED AN NR 2 ENG LP SPOOL VIBE 4.1 DURING CLIMB AND WENT TO 4.0 AT CRUISE. PERFORMED QRH PROCEDURE AND RETURNED TO FIELD. OCM REMOVED AND REPLACED FWD ACCELEROMETER. PERFORMED ENGINE RUNS AT ALL POWER SETTINGS TO INCLUDE TOGA, NO ABNORMAL VIBES DETECTED. DISCREPANCY REPEATED 03/27/2007. FERRIED TO IND. MAINT ACCOMPLISHED BLADE LUBE AND INSTALLED NEW BLADE BUMPERS.

Part: POWER SUPPLY — DEFECTIVE (SPOILERS) · airframe 4,390 hrs · 2,882 cycles

FLIGHT 7537 ATL TO DEN CREW RECEIVED AN AMBER MESSAGE ON THE EICAS OF (ADS 1 FAIL) FOLLOWED BY AN AMBER (SPOILER FAULT). THERE WERE ALSO 2 CYAN MESSAGES STATING (TAT 1 FAIL) AND (FDR FWD FAIL). CREW NOTICED A SLIGHT ELECTRICAL BURNING SCENT. WITHIN 30 SECONDS THE SCENT WAS GONE AND THE B6 CIRCUIT BREAKER WAS POPPED. NO FURTHER SCENT, NO SMOKE, AND NO INDICATION OF FIRE. DECLARED AN EMERGENCY AND NOTIFIED THEM OF OUR CURRENT SITUATION. LANDED, AND TAXIED TO THE GATE UNEVENTFULLY. MAINTENANCE T/S AND REPLACED MAU 1 PWR SUPPLY 2, GPS MODULE AND CMC MODULE. ACCOMPLISHED FLT CONTROL RTS TASK.

Part: WIRE HARNESS — FAULTY (L/E SLAT) · airframe 3,478 hrs · 2,307 cycles

REPEAT DISCREPANCY. FLT 7707 HPN TO ORD DURING CLIMB RECEIVED A SLAT FAIL CAS MESS. CREW FOLLOWED SLAT FAIL CHECKLIST IN QRH AND LANDED WITHOUT INCIDENT. ORD MX CLEARED SLAT INHIBITS, OPS CHECK OK. FLT 7601 ORD TO MCI SLAT FAIL TO EXTEND ON APPROACH INTO MCI. RAN THE QRH AND MADE A NO SLAT/FLAP LANDING. DECLARED EMERGENCY DUE TO THE HIGH REF SPEED 190 KNOTS. MCI MAINTENANCE CLEARED S-FACE 1&2 INHIBITS CYCLED FLAPS AND SLATS 3 TIMES; NO DEFECTS NOTED. FLT 7615 MCI TO ORD EXPERIENCED SLAT FAILURE DURING CRUISE. RAN AND COMPLIED WITH THE SLAT/FLAP FAIL QRH PROCEDURE. LANDED SAFELY, AND TAXIED TO THE GATE AFTER CFR INSPECTION OF MAIN GEAR AND BRAKES. REPLACED LT O/B SLAT HARNESS, OPS CK GOOD.

Part: GEARBOX — BINDING (TE FLAPS) · airframe 600 hrs · 409 cycles

FLIGHT 7740 ORD-DFW - ON FINAL APPROACH INTO DFW, THE FLAPS FAILED AT THE SLAT 3/ FLAP 0 POSITION. FLAP FAIL MESSAGE APPEARED ON EICAS. THE APPROACH WAS ABORTED WHILE THE QRH WAS WORKED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED IN DFW UNEVENTFULLY. THE AIRCRAFT WAS FERRIED TO IND FOR MAINTENANCE. MAINTENANCE TROUBLESHOT THE FLAP SYSTEM AND FOUND THE RIGHTHAND INBOARD FLAP ANGLE GEARBOX TO BE BINDING. REMOVED AND REPLACED RIGHTHAND INBOARD FLAP ANGLE GEARBOX IAW EMB 170 AMM 27-50-00. OPS CHECK GOOD.

Part: ACTUATOR — UNSERVICEABLE (TE FLAPS) · airframe 579 hrs · 396 cycles

FLIGHT 7723 IAD-MSY - AFTER SELECTING FLAPS DOWN A FLAP FAIL MESSAGE APPEARED ON EICAS AND THE FLAPS WOULD NOT MOVE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED UNEVENTFULLY. THE AIRCRAFT WAS FERRIED TO IND FOR MAINTENANCE. MAINTENANCE TROUBLESHOT THE AIRCRAFT AND REMOVED AND REPLACED THE LEFT HAND OUTBOARD FLAP ACTUATOR. OPS CHECK GOOD.