N8825Q
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2024-05-25 – 2024-05-25 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2024-05-25 – 2024-05-25 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
TWO FLASHLIGHTS IN AFT GALLEY WILL NOT TEST. SECURED BOTH LT AFT FLASHLIGHTS IN CHARGER SYSTEMS. OPS CHKD GOOD IAW AMM 25-64-00.
TWO FLASHLIGHTS IN AFT GALLEY WILL NOT TEST. SECURED BOTH LT AFT FLASHLIGHTS IN CHARGER SYSTEMS, OPS CHKD GOOD IAW AMM 25-64-00.
TWO FLASHLIGHTS IN AFT GALLEY WILL NOT TEST. RESECURED BOTH LH AFT FLASHLIGHTS IN CHARGER SYSTEM OPS CHECKS GOOD IAW AMM 25-64-00. THIS CLEARS MEL 25-64-02A
TWO RIGHT AFT GALLEY FLASHLIGHTS DID NOT TEST. REMOVED AND REPLACED BOTH RIGHT AFT EMERGENCY FLASHLIGHTS IAW AMM 25-64-00. OP?S CHECK GOOD.
AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT HOLDER INOPERATIVE. OK TO CONT IAW MEL 25-64-02A SP1B. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-64-00, NO FAULTS NOTED.
FA REPORTS FLASHLIGHT IS INOPERATIVE IN AFT GALLEY. REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-64-00.
PHOTO ILLUMINESCENT STRIP AT 12DEF PEELING UP. SECURED THE PHOTOLUMINESCENT STRIP AT 12DEF REF AMM 33-51-15.
RIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED ALONG FWD TRACK EDGE APPROX 4.5 INCH IN LENGTH. R & R RT HORIZONTAL STAB FWD UPPER SLIDING SEAL. IAW AMM 53-31-31.
LEFT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED ALONG FWD TRACK EDGE APPROX 2 INCH IN LENGTH. REMOVED AND REPLACED CRACKED LEFT FWD UPPER HORIZONTAL STABILIZER SLIDING SEAL IAW AMM 53-31-31.
PART FLOOR SEPARATION AFT CARGO HOLD APPROX ONE THIRD FORWARD OF CARGO DOOR LEFT SIDE<[01] REMOVED AND REPLACED AFTER CARGO PANELS 141DW AND 142DW PER AMM 50-10-02.
COCKPIT FLASHLIGHT BEHIND CAPT SEAT DOES NOT TEST CORRECTLY<[01] ITEM OK TO CONTINUE PER MEL 25-64-02A SP1B
COCKPIT FLASHLIGHT BEHIND CAPT SEAT DOES NOT TEST CORRECTLY<[01] ITEM OK TO CONTINUE PER MEL 25-64-02A SP1B;[02] FOUND COCKPIT FLASHLIGHT WAS MISSING; INSTALLED A NEW FLASHLIGHT AND BATTERY BEHIND CAPT SEAT IAW AMM 25-64-00; OPS CHECK GOOD.
WHILE PERFORMING RIG CHECK ON RUDDER CONTROL ROD. DISCOVERED CRACK IN L/H L/H BRACKET PN 251A3426-2 REF. IPC 27-21-00 FIG ITEM 70 REF LOGPAGE 2520929 FOR ORIG. DISCREPANCY. YAW DAMP DUTCH ROLL PROBLEM. WHILE PERFORMING RIG CHECK ON RUDDER CONTROL ROD. DISCOVERED CRACK IN L/H L/H BRACKET PN 251A3426-2 REF. IPC 27-21-00 FIG ITEM 70. PERFORMED EA 24-155-01449. PERFORMED EA 24-155-01449. PERFORMED EA 24-155-01449.
WHILE PERFORMING RIG CHECK ON RUDDER CONTROL ROD. DISCOVERED CRACK IN UPPER RUDDER TRAILING EDGE HINGE PN175A1210-5 REF IPC 55-40-51 FIG ITEM 1 REF LOGPAGE 2520929 FOR ORIG. DISCREPANCY. YAW DAMP DUTCH ROLL PROBLEM. WHILE PERFORMING RIG CHECK ON RUDDER CONTROL ROD. DISCOVERED CRACK IN UPPER RUDDER TRAILING EDGE HINGE PN175A1210-5 REF IPC 55-40-51 FIG ITEM 1<[01] PERFORMED EA 24-155-01449;[02] VERIFIED PERFORMED EA 24-155-01449.
WHILE PERFORMING RIG CHECK ON RUDDER CONTROL ROD. DISCOVERED CRACK IN LOWER RUDDER TRAILING EDGE HINGE PN175A1207-4 REF IPC 55-40-51 FIG ITEM 1 REF LOGPAGE 2520929 FOR ORIG. DISCREPANCY. YAW DAMP DUTCH ROLL PROBLEM. WHILE PERFORMING RIG CHECK ON RUDDER CONTROL ROD. DISCOVERED CRACK IN LOWER RUDDER TRAILING EDGE HINGE PN175A1207-4 REF IPC 55-40-51 FIG ITEM 1<[01] PERFORMED EA 24-155-01449;[02] VERIFIED PERFORMED EA 24-155-01449.
CRACK/PUNCTURE ON ENGINE #2 INLET<[01] REPAIRED PER EA 23-171-01656