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. (SWAA) | Operator | on 2024-05-25 | Operator named in NTSB report |
Accident & incident history
Operated by SOUTHWEST AIRLINES CO (per NTSB report)
Not yet finalized — may be revised.Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
18 reports on file, 2023-05-23 – 2026-07-17.
Part: LIGHT — LOOSE (ZONE 200) · airframe 11,627 hrs · 6,282 cycles
CENTER AISLE PHOTOLUMINESCENT STRIP LOOSE AT 12D. SECURED CENTER AISLE PHOTOLUMINESCENT STRIP AT 12D IAW SIP.
Part: SHUTOFF VALVE — FAULTY (NR 2 ENGINE) · airframe 11,568 hrs · 6,250 cycles
ENG ANTI-ICE AND COWL-VALVE LIGHTS ON ENG 2 ILLUMINATED IN FLIGHT IN. ICEING CONDITIONS. RAN QRH AND RETUREND TO BWI. OVERWEIGHT LANDING. SMOOTH LANDING. FOUND FAULT (BLEED P1 SENSOR R). R & R NR 2 ENG. PRSOV IAW FIM 36-10-00-810-856 & AMM 36-11-04. OPS CHKD GOOD.
Part: FLASHLIGHT — FAILED (ZONE 200) · airframe 11,217 hrs · 6,070 cycles
TWO FLASHLIGHTS IN AFT GALLEY WILL NOT TEST. SECURED BOTH LT AFT FLASHLIGHTS IN CHARGER SYSTEMS. OPS CHKD GOOD IAW AMM 25-64-00.
Part: FLASHLIGHT — FAILED (ZONE 200) · airframe 11,217 hrs · 6,070 cycles
TWO FLASHLIGHTS IN AFT GALLEY WILL NOT TEST. SECURED BOTH LT AFT FLASHLIGHTS IN CHARGER SYSTEMS, OPS CHKD GOOD IAW AMM 25-64-00.
Part: FLASHLIGHT — UNSECURE (ZONE 200) · airframe 11,217 hrs · 6,070 cycles
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
Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 11,088 hrs · 6,007 cycles
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.
Part: CRADLE — INOPERATIVE (ZONE 200) · airframe 10,778 hrs · 5,852 cycles
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.
Earlier reports · 2023–2025 · 11 reports
2025
Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 9,588 hrs · 5,245 cycles
FA REPORTS FLASHLIGHT IS INOPERATIVE IN AFT GALLEY. REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-64-00.
Part: SEAL — CRACKED (ZONE 300) · airframe 9,330 hrs · 5,119 cycles
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: GLOWSTRIP — PEELING (ZONE 200) · airframe 9,330 hrs · 5,119 cycles
PHOTO ILLUMINESCENT STRIP AT 12DEF PEELING UP. SECURED THE PHOTOLUMINESCENT STRIP AT 12DEF REF AMM 33-51-15.
Part: SEAL — CRACKED (ZONE 300) · airframe 9,330 hrs · 5,119 cycles
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.
Part: FLOOR PANEL — SEPARATED (ZONE 100) · airframe 8,350 hrs · 4,632 cycles
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.
2024
Part: BATTERY — NO TEST (ZONE 200) · airframe 5,765 hrs · 3,255 cycles
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.
Part: FLASHLIGHT — NO TEST (ZONE 200) · airframe 5,765 hrs · 3,255 cycles
COCKPIT FLASHLIGHT BEHIND CAPT SEAT DOES NOT TEST CORRECTLY<[01] ITEM OK TO CONTINUE PER MEL 25-64-02A SP1B
Part: BRACKET — CRACKED (ZONE 300) · airframe 4,750 hrs · 2,693 cycles
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.
Part: HINGE — CRACKED (VERTICAL STAB) · airframe 4,750 hrs · 2,693 cycles
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.
Part: HINGE — CRACKED (VERTICAL STAB) · airframe 4,750 hrs · 2,693 cycles
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.
2023
Part: INLET — CRACKED (ZN 400 NACELLE/P) · airframe 1,329 hrs · 771 cycles
CRACK/PUNCTURE ON ENGINE #2 INLET<[01] REPAIRED PER EA 23-171-01656