N94SW
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.
43 reports on file, 1995-02-14 – 2000-03-13.
Part: SKIN — CRACKED (BS 475 - 538)
DURING SCHEDULED SERVICE CHECK, FOUND 3 CRACKS ON FUSELAGE EXTERNAL SKIN, BS 475, BS 505 AND BS 538, ABOVE STRINGER 10R. REPAIRED SKIN PER SRM.
Part: STOP — OUT OF RIG (EMERGENCY EXIT)
DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT DOOR RELEASE HANDLE DIFFICULT TO OPERATE. ADJUSTED STOP PINS PER MM.
Part: COVER — BROKEN (CABIN)
DURING SCHEDULED C3 CHECK, FOUND EEPLS FWD END COVER BROKEN. REMOVED AND REPLACED FWD END COVER PER MM.
Earlier reports · 1995–1999 · 40 reports
1999
Part: INDICATOR — MOVED (ESCAPE SLIDE)
AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.
Part: BATTERY PACK — DISCHARGED (REAR CABIN)
DURING SCHEDULED OVERNIGHT CHECK, FOUND OVERHEAD EXIT LIGHTS FLICKERING AT REAR OF CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.
1997
Part: HOSE — RUPTURED (NR 3 BRAKE)
AFTER GEAR RETRACTION, NR 2 ENGINE LOW PRESS LIGHT ILLUMINATED FOR APPROX 5 SECONDS WITH LOW A SYSTEM HYD QUANTITY. APPROX 10 MINUTES LATER, A SYSTEM QUANTITY FAILED. INSPECTED AND FOUND NR 3 BRAKE PRESS HOSE RUPTURED. REPLACED PER BOEING M/M.
Part: SKIN — CRACKED (FUSELAGE)
DURING WALKAROUND CHECK, FOUND A FUSELAGE SKIN CRACKED 3 ABOVE #10 WINDOW RIGHT SIDE \N\NREPAIRED PER BOEING SRM
Part: EPR LINE — CHAFED (NR 1 ENGINE)
RETURNED TO BWI DUE TO #1 ENGINE LOW EPR INDICATION \N\NINSPECTED AND FOUND EPR LINE CHAFING IN A CLAMP IN KRUGER FLAP AREA. R&R LINE PER BOEING M/M
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED TERMINAL CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.
Part: SKIN — CRACKED (BS 460)
DURING SCHEDULED TERMINAL CHECK, FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT BS 460. REPAIRED PER BOEING SRM.
Part: SKIN — DAMAGED (GALLEY DOORWAY)
DURING SCHEDULED D CHECK, FOUND FWD GALLEY DOOR OUTER SKIN LOWER HINGE CUTOUT, DAMAGED. REPAIRED PER BOEING SRM.
Part: ANGLE — CORRODED (BS 344-360)
DURING SCHEDULED D CHECK, FOUND L ANGLE CORRODED UNDER MOPSILL AT BS 344 TO 360 , LBL 61, WL 207.5. REPLACED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 344)
DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 59 TO RBL 11, WL 208 AROUND NUTCLIP HOLES, AND AT BS 328, RBL 23-60, WL 208. REPAIRED PER BOEING SRM.
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED D CHECK, FOUND BULKHEAD BS 178 CRACKED AT WL 234, LBL 10 AND AT RBL 10. REPAIRED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 312)
DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 312, LBL 11-RBL 11, WL 208. REPAIRED PER BOEING SRM.
Part: SKIN — DAMAGED (BS 993)
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AND CREASED AT BS 993, WL 231. REPAIRED PER BOEING SRM.
Part: FRAME — CORRODED (BS 500)
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, RBL 25, WL 156. REPAIRED PER BOEING SRM.
Part: FRAME — CRACKED (BS 695)
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 695, LBL 65, WL 203.5. REPAIRED PER BOEING SRM.
Part: DOUBLER — CRACKED (GALLEY DOOR)
DURING SCHEDULED D CHECK, FOUND FWD GALLEY DOOR LOWER AFT FRAME INNER DOUBLER CRACKED. REPAIRED PER BOEING SRM.
Part: STRINGER — CORRODED (BS 322.5)
DURING SCHEDULED D CHECK, FOUND STRINGER END CORRODED AT BS 322.5, S28R. REPAIRED PER BOEING SRM.
Part: SUPPORT — CORRODED (BS 277-294.5)
DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 277-294.5, LBL 11, WL 208. REPAIRED PER BOEING SRM.
Part: WEB — CORRODED (BS 496)
DURING SCHEDULED D CHECK, FOUND CORROSION AT EXISTING WEB REPAIR AT BS 496, RBL 25, WL 156. REPAIRED PER BOEING SRM.
Part: TEE CHORD — CRACKED (BS 178)
DURING SCHEDULED D CHECK, FOUND T CHORD CRACKED AT BS 178, LBL 4, WL 185. REPLACED DAMAGED SECTION PER BOEING SRM.
Part: TEARSTRAP — CORRODED (BS 787-847)
DURING SCHEDULED D CHECK, FOUND TEARSTRAP CORRODED AT BS 787-847, RBL 20, WL 156. REPAIRED PER BOEING SRM.
Part: SKIN — DAMAGED (FUSELAGE)
DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR FUSELAGE TORQUE TUBE CAVITY OUTER SKIN GOUGED AND DENTED ON INBOARD SIDE. REPAIRED PER BOEING SRM.
Part: ANGLE — CRACKED (BS 289)
DURING SCHEDULED D-CHECK, FOUND WEB ATTACH ANGLE CRACKED AT BS 289, WL 255, RIGHT SIDE. REPLACED ANGLE PER BOEING SRM.
Part: THRESHOLD — CORRODED (FWD SERV DOOR)
DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR THRESHOLD U-CHANNEL SUPPORT CORRODED. REPLACED CHANNEL PER BOEING SRM.
Part: STRAP — CORRODED (BS 400-500)
DURING SCHEDULED D-CHECK, FOUND TEAR STRAP CORRODED AT BS 440 TO 500, WL 156, RBL 22 AROUND FASTENER HOLES. REPLACED PER BOEING SRM.
Part: STRINGER — CRACKED (BS 500)
DURING SCHEDULED D-CHECK, FOUND STRINGER 16R CRACKED AT BS 500B. REPLACED DAMAGED SECTION PER BOEING SRM.
Part: ANGLE — CORRODED (BS 270)
DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR Z-ANGLE CORRODED AT BS 270, LBL 11-RBL 11, WL 208. REPAIRED PER BOEING SRM.
Part: BULKHEAD SUPPORT — CORRODED (BS 520)
DURING SCHEDULED D-CHECK, FOUND SIDEWALL TO BULKHEAD SUPPORT CORRODED AT BS 520, LBL 25, WL 157. REPLACED PER BOEING SRM.
Part: WEB — CRACKED (BS 986.5)
DURING SCHEDULED D-CHECK, FOUND SHEAR WEB CRACKED AT BS 986.5, RBL 42, WL 208. REPAIRED PER BOEING SRM.
Part: MOPSILL — CORRODED (FWD SERV DOOR)
DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR MOPSILL CORRODED. REPLACED PER BOEING SRM.
Part: ANGLE — CORRODED (BS 303)
DURING SCHEDULED D-CHECK, FOUND WEB ATTACH ANGLE COMMON TO SKIN CRACKED AT WL 240 RIGHT, BS 303. REPLACED PER BOEING SRM.
1996
Part: SKIN — CRACKED (AFT CARGO DOOR)
DURING SCHEDULED C2 CHECK, FOUND AFT RADIUS OF AFT CARGO DOOR HANDLE CUTOUT CRACKED. REPAIRED PER BOEING SRM.
Part: WEB — CRACKED (AFT CARGO DOOR)
DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR OUTER WEB CRACKED 1.5 INCH ON LOWER FWD SIDE. REPAIRED PER BOEING SRM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.
Part: ACTUATOR — LEAKING (ELEV)
NOTED A-SYSTEM FLUID LOSS EN ROUTE. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. INSPECTED TAIL AREA AND PERFORMED LEAK CHECK. REPLACED ELEVATOR FEEL ACTUATOR PER PER BOEING M/M. TEST FLOWN WITH NO DEFECTS NOTED.
1995
Part: ANGLE — CRACKED (AFT CARGO DOOR)
DURING SCHEDULED B2 CHECK, FOUND AFT CARGO DOOR WEB ANGLE CRACKED AT 4TH RIVET AT LOWER FWD STOP. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: WEB — CRACKED (LT FUSELAGE)
DURING SCHEDULED QUARTER D CHECK, FOUND WEB CRACKED 1 INCH AT I/B RADIUS ABOVE RAM AIR DUCT AT FWD END ATTACH POINT, LEFT AC BAY. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: BELTFRAME — CRACKED (BS 360)
DURING SCHEDULED QUARTER D CHECK, FOUND BELTFRAME CRACKED AT BS 360, STRINGER 26L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: BELTFRAME — CRACKED (BS 360)
DURING SCHEDULED 1/4 D-CHECK, FOUND BELTFRAME CRACKED AT BS 360, S26L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: ACCESS PANEL — CRACKED (NLG WW)
DURING SCHEDULED CHECK, FOUND NOSE WHEEL WELL CEILING LEFT PRESSURE ACCESS PANEL CRACKED AT AFT I/B RADIUS. REPAIRED PER SWA RA 1-253-1249.