N192SY

ATA 2130

Part: CABIN PRESS SYS — WARNING MESSAGE · airframe 24,960 hrs · 16,895 cycles

AFTER CLIMBING THROUGH 10,000 RECEIVED TRIPLE CHIME AND CABIN ALTITUDE HI MESSAGE. PERFORMED QRH AND RETURNED TO DEPARTURE AIRPORT. (FLIGHT 3495) WHEN ARRIVING TO THE AIRCRAFT, THE PRESSURIZATION PANEL THE MODE WAS SET TO MANUAL, RATHER THAN BEING IN AUTO FOR NORMAL OPERATION. ASKED THE PILOTS IF THEY MOVED THE SELECTOR FROM AUTO INTO MANUAL, THEY COULD NOT REMEMBER. ASKED THE CAPTAIN WHAT REFERENCE HE USED FOR QRH PROCEDURES. THE ABNORMAL AND EMERGENCY PROCEDURES MANUAL USED DOES NOT HAVE THE FLIGHT CREW CHANGE THE POSITION OF THE MODE SELECTOR. THE ONLY INSTRUCTION FOR THE PRESSURIZATION CONTROL PANEL WAS FOR THE PILOTS TO PRESS THE DUMP BUTTON, WHICH THE CAPTAIN DID CONFIRM WAS DONE. REFERENCE AML 1973357 FOR SPEED TAPE REMOVAL AND REAPPLICATION. REFERENCE AML 1973367 FOR TROUBLESHOOTING. REFERENCE AML 1973390 FOR TROUBLESHOOTING. DURING TROUBLESHOOTING PER FIM TASK: 21-31-00-810-818-A NO DEFECTS WERE FOUND DURING REQUIRED VISUAL INSPECTIONS AND THE CABIN LEAKAGE TEST DURING PRESSURIZATION WAS WITHIN NORMAL LIMITS. FOLLOWING TROUBLESHOOTING AND WITH NOT FINDING ANY DEFECTS, OTHER THAN THE FINDING OF THE MODE S

ATA 5730

Part: SKIN — GOUGED (ZONE 500) · airframe 20,303 hrs · 13,199 cycles

GOUGE ON TOP OF LH WING SKIN OUTBD OF RIB 25 - AREA MARKED (C-CHECK RO 9/29/2024) (FILED OPEN)REPAIRED L/E WING L/E SKIN AT WING RIB 25 REF EMB ETD2024-170-025180 REV:A.

ATA 5610

Part: WINDSHIELD — DAMAGED (COCKPIT RIGHT) · airframe 16,366 hrs · 10,049 cycles

REMOVE AND REPLACE RH WINDSHIELD. REMOVED AND REPLACED RH WINDSHIELD UP TO AMM 56-11-00 SUBTAKS 420-003-A EXCLUDING SUBTASK 420-001-A STEPS 5-8. SEE CP 26094450-1 FOR INSTALLATION OF RH WINDOW SUBTASK 420-001-A STEPS 5-8 AND 420-003-A TO CLOSEOUT. ORIG SUBMISSION DATE: 1/19/2023

ATA 5610

Part: WINDSHIELD — LEAKING (LEFT) · airframe 16,373 hrs · 10,053 cycles

FOUND LH WINDSHIELD TO BE LEAKING BETWEEN TRANSPARENCY AND WINDSHIELD FRAME ON INBOARD SIDE OF WINDSHIELD.

ATA 5552

Part: NONE — CORRODED · airframe 13,255 hrs · 7,802 cycles

POST REMOVAL INSPECTION- R/H ELEVATOR #3 ATTACH POINT BOLT CORRODED. (C-CHECK RO 10/27/2021) REMOVED AND REPLACED R/H ELEVATOR #3 ATTACH POINT BOLT ON RACK. SEE CAMP # 23657716 FOR FINAL INSTALLATION.

ATA 5552

Part: NONE — CORRODED · airframe 13,255 hrs · 7,802 cycles

POST REMOVAL INSPECTION- L/H ELEVATOR #1 ATTACH POINT BOLT CORRODED AND HARD TO SLIDE IN AND OUT OF FLOATING BUSHING. (C-CHECK RO 10/27/2021) REMOVED AND REPLACED L/H ELEVATOR #1 ATTACH POINT BOLT AND FLOATING BUSHING REF AMM 27-31-05-400-801-A ON RACK;SEE WO# H8270 TASK 3013 FOR FINAL INSTALL

ATA 5330

Part: SKIN — DENTED (FRM 22 S16-17L) · airframe 11,817 hrs · 6,853 cycles

FOUND DENT ON LT EXTERIOR SURFACE APPRX AT STRINGER 16 AND 17 FWD FRAME 22. COMPLIED WITH TEMPORARY REPAIR PER TO ETD2021-170-008950. PERMANENT REPAIR DUE WITHIN 200 FLT CYCLES BY TAC 6855, PART NUMBER: - , SERIAL NUMBER: 17000638, POSITION: PER GMM 3-26 PERMANENT REPAIR DETERMINED TO BE A MAJOR REPAIR FORM M-337 REQUIREDPERFORMED PERMENANT REPAIR IN REFERENCE TO ETD2021-170-008950, ALSO ERJ 175 SRM TOPIC 53-10-01/REPAIR 12P, ALSO ERJ SRM TOPIC 51-75-12. COMPLIED WITH TASK CARD 51-00-00-002-SKY-U AND COMPLETED M-337. SEE CP # 22707169 FOR PRESSURIZATION CHECK

ATA 3240

Part: PRESSURE SWITCH — FAILED (NR 1) · airframe 3,934 hrs · 2,057 cycles

INTERMITTENT PARKING BRAKE NOT RELEASED CAUTION MESSAGE IN THE AIR. DIVERTED. DURING TAXI, RECEIVED A EMERGENCY BRAKE FAULT ADVISORY MESSAGE. REMOVED AND REPLACED THE NR 1 EMERGENCY PARKING BRAKE PRESSURE SWITCH IAW AMM. OPS CHECKED GOOD.