N929VA

ATA 5610

Part: SLIDING WINDOW — SCRATCHED (FIRST OFFICER'S) · airframe 14,203 hrs · 3,513 cycles

AIRCRAFT IN BASE MAINTENANCE: FIRST OFFICER SLIDING WINDOW HAS SCRATCHES. REPLACED FIRST OFFICER SLIDING WINDOW.

ATA 2565

Part: SLIDE — NO TEST (R4 DOOR) · airframe 5,805 hrs · 1,491 cycles

WHILE PERFORMING WEEKLY T/C, STEP (9) (G) CABIN EMERGENCY LIGHTING, REF AMM 33-51-00-710-001-A. (1) OPERATIONAL TEST OF THE EMERGENCY LIGHTS, TEST RESULTS: ESCAPE SLIDE LT / EPSU (13WL) AFT L.. GROUNDED - YES. PERFORMED TSM 25-62-00-810-819-A (4) (B), AFTER OPS TEST OF THE EMERGENCY LIGHTING SYS REF AMM 33-51-00-710-001, (ESCAPE SLIDE LT / EPSU (13WL) AFT L) ON THE RESULTS. PER TSM 25-62-00-810-819-A. NEXT STEP (4) (B)(1) REQUEST REPLACE SLIDE / REFT, DOOR 4, LH ESCAPE SLIDE AFT L (7502MM). F.C. 98566.CONTINUED WITH TSM 25-62-00-810-819-A. REMOVED AND REPLACED SLIDE / REAFT, DOOR 4, LH ESCAPE SLIDE AFT L (7502MM) PER AMM 25-62-44, OPS CHECKED GOOD. PERFORMED OPS CHECK OF THE EMERGENCY POWER SUPPLY UNIT BITE CHECK, TESTED OK PER AMM 33-51-00-710-001-A.

ATA 7497

Part: CONNECTOR — OUT OF POSITION (NR 1 ENGINE) · airframe 2,204 hrs · 515 cycles

ENGINE 1 IGN A FAULT DURING START GROUNDED - YES. CW IGN TEST IAW AMM 74-00-00-710-803-A, BOTH CHAN A/B TEST OK #1 ENG .VERIFIED IGN EXCITER CONN IN CORRECT POSITION. REF TSM74-21-00-810-809-A AND TECH OPS BRIEF (LEAP 1A DELAYED LIGHT OFF) NO MAINT ACTION IS NEEDED.

ATA 7400

Part: IGNITION SYS — WARNING MESSAGE (NR 1 ENGINE) · airframe 2,171 hrs · 507 cycles

ENGINE 1 IGN A FAULT GROUNDED - YES. PER TSM 74-21-00-810-809-A, PERFORMED OPS TEST OF ENG 1 IGN SYS PER AMM 74-00-00-710-803 SYS TEST OK PER TBN 7400-00 A/C OK FOR SVC.SWAPPED ENG 1 A & B IGN HARDWARE, PULLED AND COLLARED CB P41 ENG 1 IGN B SYS, PLACED ON MEL 74-31-01-01-C, MEL LOG UPDATED, PLACARD INSTALLED,DEFERRED

ATA 7700

Part: FAULT MESSAGE — ILLUMINATED (NR 1 ENGINE) · airframe 2,026 hrs · 471 cycles

NR 1 ENGINE START FAILED WITH ENG 1 IGN B FAULTING, 1 OUTER DROT FAULT, GROUNDED - YES. LAST LEG REPORT FOR NR 1 ENG BOTH CHANNELS SHOWS TCM CUTBACK TEST FAILED, TSM'S 73-21-01-810-928-A FOR CHANNELS A AND 73-21-01-810-929-A FOR CHANNEL B. AFTER ENG IDLE TEST BOTH CHANNELS, NO FAULTS RECORDED BOTH CHANNELS. NO CONFIRMATION OF THE FAULT

ATA 7400

Part: WARNING MESSAGE — FALSE ACTIVATION (IGNITION SYSTEM) · airframe 1,960 hrs · 457 cycles

ENGINE 1 IGN B FAULT GROUNDED - YES. PERFORMED TSM 74-21-00-810-809-A. NO FAULT FOUND. NO FAULT FOUND FOR LAST THREE FLIGHT LEGS ALT REF TO TBN-7400-00 FOR SPECIFICATIONS AT MAINT PROCEDURES REVERSED MEL 75512 IS CLEARED PLACARD REMOVED LIST UPDATED MCC LESTER IN O

ATA 7420

Part: FAULT MESSAGE — FALSE ACTIVATION (NR 1 ENGINE) · airframe 1,955 hrs · 452 cycles

ENGINE 1 IGN A FAULT. GROUNDED - YES. PERFORMED TSM 74-21-00-810-809-A FOR ENG NR 1 A&B CHANNEL , NO FAULT , OPS TESTED OK

ATA 7200

Part: WARNING MESSAGE — ILLUMINATED (NR 1 ENGINE) · airframe 1,948 hrs · 447 cycles

GATE RETURN DUE TO THE NR 1 ENGINE START FAULT & NR 1 ENG IGNITER A FAULT. GROUNDED - YES. REFER EA PWRL-74EA -00284 FOR WORK ACCOMPLISHED. REVERSED MAINT PROCEDURE PLACARD REMOVED. REF TSM 74-21-00-810-809A. PASSED TEST ENGINE CONTINUES TO FAIL ON START 3 TIMES R.F.15312 1/22/2020. ACCOMPLISHED EA PWRL-74EA-00284. OK FOR CONTINUED SERVICE.

ATA 7497

Part: WIRE HARNESS — FAULTED (NR 1 IGNITION) · airframe 1,474 hrs · 340 cycles

ENGINE #1 IGN A FAULT DURING START UP. AFTER THIRD START ATTEMPT ITS STARTED BUT DISPLAYED ENG 1 START FAULT AND ENG 1 IGN FAIL. GROUNDED - YES. DEFERRED. VERIFIED ENG 1 IGN A FAULT, ITEM RELEASED PER MEL 74-31-01-01-C, MX PROCEDURE C/W SWAPPED OF IGN SYS HARNESS, UPDATED MEL LIST, INSTALLED PLACARD, AUTHORIZED BY SEAMC ARNIE.

ATA 7421

Part: IGNITER — FAILED (NR 1 ENGINE) · airframe 1,420 hrs · 327 cycles

AFTER 2 FADEC START ATTEMPTS OF # 1 ENGINE RECEIVED "ENG 1 IGN A" INOP STATUS MSSG. (BOTH ENGINES AUTOMATICALLY STARTED SUCCESSFULLY ON IGN B). MEL 74-31-01-01-C. GROUNDED - YES. R & R ENG #1 IGNITER SYS A IAW AMM 74-21-10 PB 401 OPS CHK GOOD , A/C RELEASED FROM MEL 74-31-01-01 -C MAINT PROCEDURES REVERSED, MDDR 73540 REMOVED, LOG UPDATED, PLACARD REMOVED MCC JACK NOTIFIED

ATA 7320

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 794 hrs · 187 cycles

ENGINE 1 FADEC MAINTENANCE MESSAGE ON SHUTDOWN. GROUNDED - YES. ACCOMPLISHED FADEC TEST PER AMM 73-29-00, OPS CHECK GOOD. MESSAGE CLEARED. OK FOR SERVICE.

ATA 7320

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 698 hrs · 167 cycles

ENGINE 1 OVER-THROTTLE PROTECTION FAULT. GROUNDED - YES. PERFORMED ENG 1 IDLE TEST ON CHANNEL A AND B, NO FAULTS NOTED PER TSM 73-21-01-810-922-A. NO MAINTENANCE ACTION REQUIRED.