N83SW
Registered owner: ROGERS GARY A, MI (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.
44 reports on file, 1996-03-18 – 2000-03-16.
Part: BEAM — CORRODED (BS 540 - 727)
DURING SCHEDULED D CHECK, FOUND CORROSION ON UPPER FLANGE OF LONGITUDINAL BEAM, BS 540-727, RBL 25. REMOVED AND REPLACED LONGITUDINAL BEAM UPPER FLANGE PER SRM.
Part: BEAM — CRACKED (BS 663 - 667)
DURING SCHEDULED D-CHECK, FOUND CENTER SECTION LONGITUDINAL BEAM CRACKED IN 2 PLACES, BS 663 AND BS 667, LBL 25. REPAIRED BEAM PER ACO523-57.
Part: SKIN — CRACKED (FUSELAGE)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED ON LOWER FWD CORNER OF AFT CARGO DOOR CUTOUT. REPAIRED SKIN PER ER 00-0244.
Part: STRINGER — CRACKED (BS 297)
DURING SCHEDULED D-CHECK, FOUND STRINGER 10L CRACKED BS 297. REPAIRED STRINGER PER SRM.
Part: STRINGER — CORRODED (BS 901 - 913)
DURING SCHEDULED D-CHECK, FOUND STRINGER 20R CORRODED, BS 901-913. REPAIRED STRINGER PER SRM.
Part: FRAME — CRACKED (BS 460 & 480)
DURING SCHEDULED D-CHECK, FOUND 2 FRAMES CRACKED, BS 480 AND BS 460 LBL 21. REPAIRED FRAMES PER SRM.
Part: FRAME — CRACKED (BS 727)
DURING SCHEDULED D-CHECK, FOUND BS 727, FRAME CRACKED IN 3 PLACES LBL 37-RBL 45. REPAIRED FRAME PER SRM.
Part: STRINGER — CRACKED (BS 663.75)
DURING SCHEDULED D-CHECK, FOUND BS 663.75, STRINGERS 3L AND 9R CRACKED. REPAIRED STRINGERS PER SRM.
Part: FLOORBEAM — CORRODED (BS 1016)
DURING SCHEDULED D CHECK, FOUND BS 1016 FLOORBEAM CORRODED, LBL 36-RBL 36. REPAIRED BEAM PER SRM.
Part: FLOORBEAM — CORRODED (BS 707)
DURING SCHEDULED D CHECK, FOUND BS 707 FLOORBEAM CORRODED, LBL 17. REPAIRED BEAM PER SRM.
Part: FRAME — CRACKED (BS 1156)
DURING SCHEDULED D CHECK, FOUND BS 1156 AFT BULKHEAD CHORD CRACKED AT 8 O'CLOCK POSITION. REPAIRED CHORD SECTION PER SRM.
Part: FRAME — CRACKED (BS 360)
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 360, RBL 62. REPAIRED FRAME PER SRM.
Part: FRAME — CORRODED (BS 227)
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED, BS 227, RBL 41. REPAIRED FRAME PER SRM.
Part: FRAME — CORRODED (BS 1016)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED, BS 1016, BETWEEN STRINGERS 26R-27R. REPAIRED FRAME PER SRM.
Part: STRINGER — CRACKED (BS 381)
DURING SCHEDULED D-CHECK, FOUND STRINGER 25L CRACKED, BS 381. REPAIRED STRINGER PER SRM.
Part: FRAME — CRACKED (BS 344)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED, BS 344, STRINGER 23L. REPAIRED FRAME PER SRM.
Part: FRAME — CRACKED (BS 1098)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED, BS 1098, STRINGER 5L. REPAIRED FRAME PER SRM.
Part: CLIP — CRACKED (BS 727)
DURING SCHEDULED D-CHECK, FOUND 2 STRINGER CLIPS CRACKED, BS 727, STRINGER 14R, AND BS 727B, STRINGER 6R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.
Earlier reports · 1996–1999 · 26 reports
1999
Part: CONNECTOR — FAILED (NR 1 ENGINE)
INFLIGHT ENGINE SHUT DOWN, AIR RETURN WITH THE NR 1 ENGINE SHUT DOWN DUE TO START VALVE OPEN LIGHT ILLUMINATED. REMOVED AND REPLACED START VALVE AND OPEN LIGHT REMAINED ON AFTER ENG START. FOUND START VALVE CANNON PLUG CONNECTOR BAD. REMOVED AND REPLACED CONNECTOR, OPS CKD GOOD PER MM.
Part: LIGHT — INOP (CABIN)
DURING PREFLIGHT CHECK, FOUND CAPT OVERWING EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER BOEING M/M.
Part: LIGHT — INOP (CABIN)
DURING PREFLIGHT, FOUND CAPT SIDE OVERWING LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY.
1997
Part: SKIN — CRACKED (BS 947)
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED FWD OF BS 947, S24R. REPAIRED PER BOEING SRM.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED TERMINAL CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.
Part: BRACKET — BROKEN (NLG DOOR)
AFTER TAKEOFF, NOTED LOUD NOISE FROM NOSE GEAR DURING RETRACTION. LOWERED GEAR AND RETURNED TO TPA AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND GEAR DOOR BRACKET BROKEN. REMOVED RIGHT NOSE GEAR DOOR, PINNNED GEAR DOWN AND FERRIED AIRCRAFT TO HOU. REPLACED BROKEN HARDWARE AND REPLACED NLG A-FRAME DRAG BRACE PER BOEING M/M.
1996
Part: SLIDE — PRESS LOW (FWD ENTRY DOOR)
DURING WALKAROUND CHECK, FOUND FWD ENTRY DOOR SLIDE PRESSURE BELOW MINIMUM LIMITS. REPLACED SLIDE PER BOEING M/M.
Part: SKIN — CRACKED (BS 781-800)
DURING SCHEDULED SV CHECK, FOUND 2 CRACKS ALONG S24L AND BETWEEN BS 781-800. REPAIRED PER BOEING SRM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE AFT ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK PER BOEING M/M.
Part: FRAME — CRACKED (BS 349)
DURING SCHEDULED D-CHECK, FOUND LEFT FRAME CRACKED AT BS 349 WL 225. REPLACED FRAME CHORD PER BOEING SRM.
Part: ANGLE — CRACKED (BS 294)
DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 294 RBL 55 WL 208. REPLACED PER BOEING SRM.
Part: ANGLE — CRACKED (BS 289)
DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED FWD OF SERVICE DOOR AT BS 289 WL 248. REPLACED PER BOEING SRM.
Part: ANGLE — CRACKED (BS 302)
DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 302 AT S10L. REPLACED PER BOEING SRM.
Part: WEB — CRACKED (BS 530)
DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 530, RBL 43 WL 161. REPAIRED PER BOEING SRM.
Part: BULKHEAD WEB — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND 2 INCH CRACK AT BS 178 BULKHEAD PRESSURE WEB, RBL 9.7 WL 219. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (BS 663)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 663 RBL 24 AND LBL 24 WL 201. REPAIRED PER BOEING SRM AND BOEING DRAWING 691A0032.
Part: BULKHEAD WEB — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND 1.8 INCH CRACK AT BS 178 BULKHEAD PRESSURE WEB, LBL 11.3 WL 219. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACK INDICATION AROUND FASTENER HEAD AT BS 178 WL 234 RBL 10. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (BS 663)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 663, RBL 24 AND LBL 24. REPAIRED PER BOEING SRM.
Part: SPLICE — CORRODED (BS 907)
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT AFT BAY AT BS 907, S25L, LBL 21, WL 168. REPLACED SECTION PER BOEING SRM.
Part: BLKHD WEB — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND BULKHEAD 178 PRESSURE WEB CRACKED AT RBL 9.7, WL 219. ALSO, AT LBL 11.3, WL 219. REPAIRED PER BOEING SRM.
Part: FLOOR BEAM — CORRODED (BS 294/238)
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294, RBL 36 AND RBL 46, WL 208. ALSO, AT BS 328, RBL 15 AND 25, WL 208. REPAIRED PER BOEING SRM.
Part: WEB — CRACKED (BS 726)
DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 726, STRINGER 18A, RBL 61, WL 188.25. ALSO, AT BS 530, RBL 43, WL 161. REPAIRED PER BOEING SRM.
Part: BEAM — CRACKED (BS 616)
DURING SCHEDULED D-CHECK, FOUND INBOARD CREASE BEAM CRACKED AT BS 616, RBL 65, WL 208. REPAIRED PER BOEING SRM.
Part: FRAME — CRACKED (BS 328)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, RBL 55, BETWEEN S20R AND 21R. REPAIRED PER BOEING SRM.
Part: SUPPORT — CRACKED (BS 540)
DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540, BL 0 TO LBL 25, WL 208. REPLACED PER BOEING SRM.