N721SW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
9 reports on file, 1998-03-23 – 1998-10-09.
Part: WIRE — LOOSE (ROW 8)
DURING SCHEDULED RON CHECK, FOUND LOOSE WIRES IN THE EMERGENCY EXIT LIGHTS AT ROW 8 F/O SIDE ONE WHITE LIGHT WON'T ILLUMINATE. REPAIRED WIRING AT ROW 8 F/O SIDE PER BOEING MM.
Part: ENGINE — MALFUNCTIONED (NR 1)
AIR RETURN DUE TO NR 1 ENGINE EGT WAS AT REDLINE FOR T/O AND REQUIRED REDUCING THROTTLE SIGNIFICANTLY TO MAINTAIN IN LIMITS. A/C MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED NR 1 ENGINE ASSY AS PER SAM FORMS 104, 111, 117, 636. INSTALLED STAGE II MOTOR. PERFORMED TRIM RUN AND ALL PARAMETER WERE WITHIN BOEING MM LIMITS.
Part: LIGHT — LOOSE (CABIN)
DURING SCHEDULED CI CHECK, FOUND EMERGENCY EXIT LIGHT OVER AFT SERVICE DOOR FELL OUT OF MOUNTING. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (BS 727)
DURING SCHEDULED CI CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B+7 AT STR 17R CONFIRMED BY EDDY CURRENT. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (BS 784)
DURING SCHEDULED CI CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 784, STR 17L CONFIRMED BY EDDY CURRENT. REPAIRED PER BOEING SRM.
Part: ACTUATOR — FAILED (NR 5 LE SLAT)
AFTER DEPARTURE CREW GOT INDICATIONS OF NR 5 SLAT ACTUATOR REMAINS EXTENDED, VISUALLY CONFIRMED. AIR TURNBACK TO NASHVILLE. AIRCRAFT MADE AN UNEVENTFUL LANDING. REPLACED SLAT ACTUATOR PER BOEING MM.
Part: LIGHTS — LOOSE (CABIN)
DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT EGRESS FLOOR LIGHTING LOOSE AT ROW 14. SECURED AND STOWED FLOOR EGRESS LIGHTING, OPS CK GOOD PER BOEING MM.
Part: LIGHT — INOPERATIVE (CABIN)
DURING SCHEDULED C4 CHECK, FOUND EMERGENCY LIGHT ON FLOOR INOP AT 14D. REPLACED LAMP AT 14D, OPS CK LAMPS PER BOEING MM.
Part: SKIN — CRACKED (BS 742)
DURING SCHEDULED RON CHECK, FOUND CRACK IN FUSELAGE SKIN AT BS 742 AT S16L APPROX 1.25 INCH LENGHT. REPAIRED PER BOEING SRM.