N238NN

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 23,153 hrs · 15,514 cycles

AFT SERVICE DOOR R2 EXIT IDENTIFIER SIGN INOP/HALF LIT. R & R AFT SERVICE DOOR R2 EXIT IDENTIFIER SIGN IAW AMM 33-50-15. OPS CHK GOOD.

Part: LAMP — NO TEST (FLASHLIGHT) · airframe 23,135 hrs · 15,500 cycles

FO FLASHLIGHT INOP. RELAMPED FO FLASHLIGHT OPC GOOD EJ25-085

Part: LIGHT — NO TEST (ZONE 200) · airframe 22,669 hrs · 15,138 cycles

DURING EMER LT TEST FIRST THREE LIGHTS ON CEILING DO NOT LIGHT UP. DID AIRCRAFT RESET WITH NO LUCK PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM IAW AMM 33-50-00 OPC GOOD NO FURTHER DEFECT NOTED

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,352 hrs · 14,910 cycles

CENTER FUSELAGE III - LH AFT SEAT TRACK AFT END CORRODED AS MARKED. (MAJOR REPAIR) (LEVEL 2 CORROSION). BLENDED CORRISION ON LH AFT SEAT TRACK AFT END REF E175 SRM 51-10-03. CORROSION ON SEAT TRACK IS IN A NO DAMAGE ALOW AERA SEAT TRACK FOUND TO BE OUT OF LIMITS PER E175 SRM 53-23-10/AD01. REMOVED LH AFT SEAT TRACK PER EMB 175 SRM 51-40-08. LOCATED, DRILLED, AND TREATED HOLES ON NEW LH AFT SEAT TRACK PN: AE170-86081-005 PER EMB 175 SRM 51-40-02, AND EMB 175 SRM 51-23-04. RESTORED FINISH ON AFT L/H SEAT TRACK PER ETN-EJ-51-015, EMB 175 SRM 51-23-06, AND EMB 175 CPM 51-25-00-910-001-A. REMOVED AND REPLACED LH AFT SEAT TRACK PER EMB 175 SRM 51-40-08.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,352 hrs · 14,910 cycles

CNTR FUSELAGE III FLOOR STRUCTURE RH BEAM CORRODED AS MARKED AT FR88-89 Y +10" (MAJOR REPAIR) (LEVEL 2 CORROSION). BLENDED CORROSION ON CNTR FUSELAGE III FLOOR STRUCTURE RH BEAM AT FR88-89 Y+10" IAW E-175 SRM 51-10-03 ORIGINAL MATERIAL .080. MATERIAL REMOVED .020 L=1.00 X W=.050 X H=.020 FOUND TO BE OUT OF LIMITS IAW E-175 SRM 51-75-16 PART REQUIRES REPLACING. LOCATED, DRILLED AND DEBURED NEW R/H BEAM Y + 10" FR 86 - FR 89 REF EMB 175 SRM 51-40-02. RESTORED FINISH AT FLOOR BEAM PART# 170-65669-004 COMMON TO FR86-FR89 REF ENVOY ERJ-175 SRM 51-23-06, ENVOY ERJ-175 ETN-EJ-51-015 AND ETN-EJ-51-025. APPLIED CIC ON CNTR FUSELAGE III FLOOR STRUCTURE RH BEAM FR 88-89 Y+10 IAW E-175 CPM 51-25-00. REMOVED AND REPLACED FLOOR BEAM FROM FR 86 - FR 89 Y + 10" REF EMB 175 SRM 51-40-08.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 14,863 hrs · 9,620 cycles

(LEVEL 2 CORROSION) (MAJOR REPAIR) SSI 53-10-027 FWD GALLEY RH FLOOR BEAM BETWEEN FR 13-14 HAS CORROSION-C/A-ACCOMPLISHED PERMANENT REPAIR ON FWD GALLEY RH FLOOR BEAM BETWEEN FR 13-14 IAW ERS-EJ-53MR-4613

Part: BEAM — CORRODED (FR 87) · corrosion level 2 · airframe 14,863 hrs · 9,620 cycles

(LEVEL 2 CORROSION) (MAJOR REPAIR) SSI 53-23-005 LH FLOOR BEAM IS CORRODED AT FR 87-C/A- ACCOMPLISHED PERMANENT REPAIR ON LH FLOOR BEAM AT FR 87 IAW ERS-EJ-53MR-4611

Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 14,863 hrs · 9,620 cycles

SSI 53-23-005 LH SHEAR PANEL BETWEEN FR 87-88 IS CORRODED. (LEVEL 2 CORROSION)-C/A-RAR LH SHEAR PANEL BETWEEN FR 87-88 IAW EMB 175 SRM 51-40-08

Part: SHEAR PANEL — CORRODED (RIGHT) · corrosion level 2 · airframe 14,863 hrs · 9,620 cycles

SSI 53-23-005 RH SHEAR PANEL BETWEEN FR 87-88 CORRODED. (LEVEL 2 CORROSION)-C/A-RAR RH SHEAR PANEL BETWEEN FR 87-88 IAW EMB 175 SRM 51-40-08

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 14,863 hrs · 9,620 cycles

(LEVEL 2 CORROSION) (MAJOR REPAIR) SSI 53-10-027 FWD GALLEY RH FLOOR BEAM BETWEEN FR 12-14 HAS CORROSION-C/A-SSI 53-10-027 FWD GALLEY RH FLOOR BEAM BETWEEN FR 12-14 HAS CORROSION ACCOMPLISHED PERMANENT REPAIR ON FWD GALLEY RH FLOOR BEAM BETWEEN FR 12-14 IAW ERS-EJ-53MR-4609

Part: SHEAR PANEL — CORRODED (CENTER) · corrosion level 2 · airframe 14,863 hrs · 9,620 cycles

SSI 53-23-005 CENTER SHEAR PANEL BETWEEN FR 87-88 CORRODED. (LEVLL 2 CORROSION)-C/A-RAR CENTER SHEAR PANEL BETWEEN FR 87-88 IAW EMB 175 SRM 51-40-08

Part: FRAME SPLICE — CORRODED (ZONE 200) · corrosion level 2 · airframe 14,863 hrs · 9,620 cycles

SSI 53-23-005 CENTER SPLICE ON FR 90 CORRODED. (LEVEL 2 CORROSION)-C/A-RAR CENTER SPLICE ON FR 90 IAW EMB 175 SRM 51-40-08

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 14,863 hrs · 9,620 cycles

SSI 53-23-005 RH FLOOR PANEL SUPPORT AFT GALLEY BETWEEN FR88-90 CORRODED. (LEVEL 2 CORROSION)-C/A-RAR RH FLOOR PANEL SUPPORT AFT GALLEY BETWEEN FR 88-90 IAW EMB 175 SRM 51-40-08

Part: SPLICE — CORRODED (FR 89) · corrosion level 2 · airframe 14,863 hrs · 9,620 cycles

SSI 53-23-005 RH SPLICE ON FR 89 CORRODED-C/A-RAR RH SPLICE AT FR 89 IAW EMB 175 SRM 51-40-08

Part: FLOOR SUPPORT — CORRODED (AFT GALLEY FLOOR) · corrosion level 2 · airframe 14,863 hrs · 9,620 cycles

SSI 53-23-005 LH FLOOR PANEL SUPPORT AFT GALLEY BETWEEN FR 88-90 CORRODED. (LEVEL 2 CORROSION)-C/A-RAR LH FLOOR PANEL SUPPORT AFT GALLEY BETWEEN FR 88-90 IAW EMB 175 SRM 51-40-08

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 14,863 hrs · 9,620 cycles

SSI 53-10-027 FWD GALLEY RH SILL BETWEEN FR 12-14 CORRODED. (LEVEL 2 CORROSION)-C/A-REMOVED AND REPLACED FWD GALLEY RH SILL BETWEEN FR 12-14 IAW EMB 175 SRM 51-40-08

Part: NONE — GOUGED (RH LOWER CENTER) · airframe 14,863 hrs · 9,620 cycles

SSI 53-23-005 CABIN RH LOWER CENTER SEAT TRACK GOUGED BETWEEN FR 78-79. (MAJOR REPAIR)-C/A-REMOVED AND REPLACED RH LOWER CENTER SEAT TRACK AFT SECTION FR 79-85 IAW EMB 175 SRM 53-00-10, SRM 51-43-03 AND SRM 51-43-04.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 14,863 hrs · 9,620 cycles

(LEVEL 2 CORROSION) (MAJOR REPAIR) SSI 53-21-005 CABIN RH LOWER CENTER SEAT TRACK CORRODED BETWEEN FR 16-18-C/A-ACCOMPLISHED PERMANENT REPAIR ON CABIN LOWER CENTER SEAT TRACK BETWEEN FR 16-18 IAW ERS-RJ-53MR-4610

Part: NONE — CRACKED (LH) · airframe 14,863 hrs · 9,620 cycles

LH #6 EMERGENCY PHOTOLUMINRSCENT INDICATOR LIGHT STRIP IS CRACKED-C/A-COMPLETE:REMOVED AND REPLACED LH #6 EMERGENCY PHOTOLUMINRSCENT INDICATOR LIGHT STRIP IAW EMB 175 AMM 33-50-21.

Part: SKIN — CRACKED (LT WING TIP) · airframe 14,469 hrs · 9,354 cycles

LH WING TIP CRACKED ON FWD SPAR AT ATTACHMENT POINT.-C/A-CA PENDING

Part: SPAR — CRACKED (RT WING) · airframe 14,469 hrs · 9,354 cycles

RH WING FWD SPAR CRACKED AT WING TO WINGTIP ATTACHMENT POINT.-C/A-RAR'D RH WING TIP IAW AMM 57-30-00.-C/A-RAR'D RH WING TIP IAW AMM 57-30-00.

Part: NONE — INOPERATIVE (GALLEY) · airframe 14,306 hrs · 9,263 cycles

FOUND PHOTO LUMINESCENTSTRIP INOP NEAR FWD GALLEY-C/A-FOUND PHOTO ILLUMENECENT STRIP INOP NEAR FWD GALLEY RAR PHOTO LUMINESCENT IAW AMM 33-50-21 NO FURTHER DEFECTS NOTED

Part: STRINGER — BENT · airframe 13,910 hrs · 9,018 cycles

STRINGER 11L BENT BTW FR89 AND FR90.( MAJOR REPAIR)-C/A-RAR STRINGER 11L BETWEEN FR88-91 IAW EMB 175 SRM 51-40-08 AND 51-41-02. SEE TURNOVER FOR DETAILS

Part: NONE — NONE · airframe 13,492 hrs · 8,763 cycles

LG WOW SYS FAIL WARNING ON TAKEOFF DURING GEAR RETRACTION DECLARED EMERGENCY - RETURN TO ORD "TRANSFERRED TO NRWC 038-ORD-02484"-C/A-SEE NRWC 038-ORD-02484 FOR WORK ACCOMPLISHED. PERFORMED GEAR SWING IAW ERJ 175 AMM TASK 32-33-00. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 11,261 hrs · 7,322 cycles

FOUND AFT LH PASSAGE WAY EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED #3 EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01. OPERATIONAL CHECK IS GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 11,258 hrs · 7,321 cycles

TRANSFERRED FROM NRWC 038-ORD-01910 "FUSELAGE SKIN ABOVE GPU RECEPTACLE HAS SIGNIFICANT HEAT DAMAGE DUE TO FIRE. (REF AML PG 4675896 ITEM 2) UPGRADED TO A MAJOR REPAIR-C/A-RERPAIRED IAW ERS-EJ-53MR-4290

Part: SKIN — NOT REPORTED (FRAME 11) · airframe 11,258 hrs · 7,321 cycles

SKIN SECTION FROM FRAME 11 (FACTORY SPLICE) TO FRAME 18 (FACTORY SPLICE) AND FROM STRINGER 20L TO BETWEEN STRINGERS 24L-25L REQUIRES REMOVAL PER ETD2021-170-004959.-C/A-REPAIRED IAW ERS-EJ-53MR-4290.

Part: HOUSING — DAMAGED (GPU) · airframe 11,257 hrs · 7,320 cycles

GPU CONNECTION HOUSING STRUCTURE IS DAMAGED DUE TO FIRE (INSIDE OF PANEL 125AL)- GPU RECEPTACLE FIRE WHILE CONNECTED TO GPU (REF AML PG 4675896 ITEM 2). REPAIRED IAW ERS-EJ-53MR-4290.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,884 hrs · 6,453 cycles

EMERGENCY LIGHT STRIP NEXT TO THE WARDROB WORN. REMOVED AND REPLACED EMERGENCY LIGHT STRIP NEXT TO THE WARDROBE IAW AMM 35-50-21. OPS CHECKED GOOD.

Part: SKIN — GOUGED (FUSELAGE) · airframe 9,882 hrs · 6,452 cycles

ONETIME REPAIR - ERS-EJ-53DF-3877 OPS PTC DUE - LH FWD FUSELAGE SKIN - DENT WITH GOUGE BTW FR. 10 & 11, STR. 15 & 16 - PERMANENT REPAIR. MAJOR REPAIR-C/A-ACCOMPLISH ERS-EJ-53DF-3877 PART C

Part: LIGHT — WORN (CABIN) · airframe 9,882 hrs · 6,452 cycles

EMERGENCY LIGHT STRIP NEXT TO THE WARDROB WORN-C/A-REMOVED AND REPLACED EMERGENCY LIGHT STRIP NEXT TO THE WARDROB IAW EMB 175 AMM 35-50-21. OPS CHECK GOOD.

Part: BRAKE — MALFUNCTIONED (LT MLG) · airframe 7,073 hrs · 4,674 cycles

BRAKE LH FAULT ADVISORY MSG POSTED AFTER LOWERING LNDG GEAR. LND GEAR NO DISPATCH MSG POSTED AFTER ARRIVING AT GATE.-C/A-PERFORMED FIM TASK 32412011BCM STEPS 1 & 7. FAULT IS TRANSITORY CONDITION MAIN BRAKE CONT MODULE 2.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 6,813 hrs · 4,512 cycles

SUPPLEMENTAL BLEED 1 FAIL CAUTION IN FLIGHT FL370 QRH PROCEDURES C/W. BLEED 1 FAIL REANNONCIATED AT 2000 ON APPROACH. CREW COMPLIED WITH QRH AND DIVERTED TO CMH. C/A-DEFERRED BLEED 1 PER MEL 36-13 AUTH#020282DM-C. M PROCEDURES C/W. REMOVED E1 NAPRSOV REF ERJ AMM 36-11-03-000-801. INSTALLED SERVICEABLE E1 NAPRSOV IAW AMM 36-11-03-400-801 UP TO AND INCLUDING STEP 3.J.[7] COMPLIED WITH COMPLETION OF AMM 36-11-03 FROM STEP 3.J.(8). LEAK CHECK OF LT NAPRSOV IAW AMM 36-11-03-790-802-A/500 GOOD. OPC OF ENGINE PNEUMATIC BLEED SYSTEM GOOD IAW AMM 36-11-00-710-801-A. NO OTHER DFEFECTS NOTED AT THIS TIME. MEL RESTORED. MTX PROCEDURES REVERSED.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 5,621 hrs · 3,741 cycles

2 STRIPS FLOOR ILLUMINATION INOP. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS IAW AMM 33-50-21.

Part: APU — ODOR (APU BAY) · airframe 5,620 hrs · 3,740 cycles

BURNING ODOR SENSED THROUGH GASPERS AFTER APU BLEED TAKE-OVER W/ ENGINES RUNNING. C/W FIM TASK 21-20-00, SMOKE AND/ OR ABNORMAL SMELL IN PAX CABIN AND/OR COCKPIT, SMOKE / SMELL IN THE CABIN CAUSED BY THE APU TASK 49-10-00-810-813A. COULD NOT DUPLICATE.

Part: PROXIMITY SENSOR — FAILED (NR 1 MAU) · airframe 4,710 hrs · 3,150 cycles

AFCS FAULT MULTIPLE ERRONEOUS MSGS ON SHORT FINAL, EMERGENCY DECLARED. REMOVED AND REPLACED THE NR 1 PSEM ON MAU 1 IAW AMM 32-61-01, LOADED SOFTWARE IAW AMM 45-45-00. OPS CHECKED GOOD IAW AMM 22-11-00.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 1,191 hrs · 786 cycles

MOMENTARY LAVATORY SMOKE INDICATION. FWD & AFT LAVATORY SMOKE TEST OPS CHECKED OK IAW AMM 26 14 00. OK FOR SERVICE