N89SW
Registered owner: RAW DOG AVIATION AND MEDIA LLC, FL (owner ≠ operator)
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.
28 reports on file, 1996-07-07 – 2000-03-16.
Part: ACTUATOR — FAILED (LT WING)
AIR TURNBACK, NR 3 L/E SLAT TRANSIT LIGHT REMAINED ILLUMINATED AFTER FLAP RETRACTION. REMOVED AND REPLACED NR 3 L/E SLAT ACTUATOR PER MM.
Earlier reports · 1996–1999 · 27 reports
1999
Part: LIGHT — INOPERATIVE (LT EMER EXIT)
DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP, BATTERY PACK, (P/N 61-0478-1) PER MM.
Part: BALLAST — FAILED (LAVATORY)
SMOKE IN COCKPIT, ENTERED IN STEADY HEAVY STREAM IN AREA OF BRACE IN C/B PANEL BY CAPT LEFT SHOULDER. LAVATORY MIRROR C/B FOUND TRIPPED. CHECKED P-18 PNL FOR BURN WIRE AND CIRCUIT BREAKER, ALL CHECK NORMAL. FOUND FWD LAV MIRROR LT BALLAST BAD. PULLED AND COLLARED LAV MIRROR LT C/B. CONTINUED PER MEL 33-2. DURING OVERNIGHT CHECK, REMOVED AND REPLACED LIGHT BALLAST PER BOEING MM.
1997
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.
Part: SKIN — CRACKED (BS 945)
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945, AT S24L. REPAIRED PER BOEING SRM.
Part: SLAT — DELAMINATED (NR 5 LE SLAT)
FOUND NR 5 L/E SLAT DELAMINATED. REPLACED NR 5 L/E SLAT PER BOEING M/M.
Part: SKIN — CRACKED (FUSELAGE)
DURING WALKAROUND CHECK, FOUND A 2 FUSELAGE SKIN CRACK RIGHT SIDE, AFT OF ICE LIGHT. REPAIRED PER BOEING SRM.
Part: BRAKE VALVE — CRACKED (MLG WW)
CREW EXPERIENCED B-SYSTEM HYDRAULIC QUANTITY LOSS. AIRCRAFT RETURNED TO HOU AND LANDED WITHOUT INCIDENT. INSPECTED AND FOUND AUTO-BRAKE VALVE CASE CRACKED. REPLACED AND LEAKED CHECKED PER BOEING M/M.
1996
Part: SKIN — CRACKED (FWD ENTRY)
DURING SCHEDULED B2 CHECK, FOUND FUSELAGE SKIN CRACKED AT UPPER HINGE CUTOUT OF FWD ENTRY DOOR. REPAIRED PER BOEING SRM.
Part: LIGHT — BROKEN (CABIN)
DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT LIGHT OVER FWD SERVICE DOOR UNSECURED. REPLACED LIGHT ASSEMBLY PER BOEING M/M.
Part: WEB — CRACKED (BS 178)
DURING SCHEDULED 1/2 D CHECK, FOUND CRACK INDICATION UNDER VERTICAL STRAP AT BS 178, LBL 5, WL 196. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (LT WING)
DURING SCHEDULED 1/2 D CHECK, FOUND LT WING NR 3 OUTBOARD AUXILIARY TRACK CUTOUT CRACKED APPROXIMATELY .25 INCH. REPAIRED PER SWA RA 1-257-167.
Part: STRINGER — CRACKED (BS 500)
DURING SCHEDULED 1/2 D CHECK, FOUND STRINGER 16R CRACKED BETWEEN 500A AND 500B. REPAIRED PER BOEING SRM.
Part: FLOOR BEAM — CORRODED (BS 1016)
DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORROSION ON FORWARD EDGE OF BEAM, BS 1016, RBL 4.5. REPAIRED PER SWA RA 1-253-1476.
Part: WEB — CRACKED (BS 468)
DURING SCHEDULED 1/2 D CHECK, FOUND WEB IN FORWARD CARGO BIN CRACKED APPROX 1.75 INCH AT BS 468, RBL 23. REPAIRED PER BOEING SRM.
Part: STRINGER — CORRODED (BS 1006)
DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 26R CORRODED AT BS 1006. REPLACED STRINGER SECTION PER BOEING SRM.
Part: WEB — CORRODED (BS 1000)
DURING SCHEDULED 1/2 D-CHECK, FOUND WEB UNDER AFT GALLEY CORRODED AROUND NUTPLATE AT BS 1000, RBL 44. REPLACED WEB PER BOEING SRM.
Part: FLOOR BEAM — CORRODED (BS 986)
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 986, RBL 5. REPAIRED PER BOEING SRM.
Part: ANGLE — CRACKED (FWD SERV)
DURING SCHEDULED 1/2 D-CHECK, ANGLE BELOW S13R FORWARD OF FORWARD SERVICE DOOR CRACKED AT AFT END. REPLACED ANGLE PER BOEING SRM.
Part: CHORD — CRACKED (BS 178)
DURING SCHEDULED 1/2 D-CHECK, FOUND CHORD CRACKED AT BS 178 BULKHEAD AT LBL 5.7. REPAIRED PER BOEING SRM AND T1-253-031.
Part: FLOOR BEAM — CORRODED (BS 312)
DURING SCHEDULED 1/2 D-CHECK, FOUND UPPER AND LOWER SURFACES OF FLOOR BEAM UPPER T-CHORD AFT FLANGE CORRODED, BS 312, LBL 1. REPAIRED PER BOEING SRM.
Part: FLOOR BEAM — CORRODED (BS 986.5)
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORROSION IN AND AROUND FWD FLANGE AT RBL 15 AND 45, BS 986.5. REPAIRED PER BOEING SRM.
Part: FLOOR BEAM — CORRODED (BS 294)
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORROSION AT UPPER FLANGE, BS 294, LBL 1, 8 AND 11. REPAIRED PER BOEING SRM.
Part: STRINGER — DAMAGED (BS 967)
DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 25L DAMAGED AT BS 967. REPAIRED PER BOEING SRM.
Part: ANGLE — CORRODED (BS 294.5)
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR SUPPORT ANGLE AT FWD GALLEY CORRODED AT BS 294.5. REPLACED PER BOEING SRM.
Part: STRAP — CRACKED (BS 178)
DURING SCHEDULED 1/2 D-CHECK, FOUND CRACK UNDER VERTICAL STRAP AT RBL 5, WL 192, BS 178. REPAIRED PER BOEING SRM.
Part: FLOOR BEAM — CORRODED (BS 294.5)
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM AT FWD GALLEY CORRODED AT BS 294.5, LBL 11 AND LBL 19. REPLACED T-CAP PER BOEING SRM.
Part: FLOOR BEAM — CORRODED (BS 344/294)
DURING SCHEDULED 1/2 D-CHECK, FOUND FWD GALLEY FLOOR BEAM UPPER SURFACE CORRODED AT BS 344, RBL 3 TO 10. ALSO, BS 294, 294.5. REPLACED T-CAP PER BOEING SRM.