N52SW
Registered owner: WEINSTOCK STEVEN R, IL (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.
50 reports on file, 1995-01-31 – 1997-11-14.
Part: LINE — RUPTURED (NR 1 ENGINE)
EN ROUTE LOST A AND B HYDRAULIC SYSTEMS. DIVERTED TO AGS. MANUAL REVERSION LANDING PERFORMED. REPLACED HYDRAULIC LINE AT NUMBER 1 ENGINE AND ALL MAIN GEAR WHEEL/TIRES AND BRAKES PER BOEING M/M.
Part: SKIN — CRACKED (FUSELAGE)
DURING SCHEDULED D CHECK, COMPLIED WITH SKIN LAP MOD JOINT REMOVAL AND MODIFICATION PER ACO 6752-53.
Part: CLIP — CRACKED (BS 380)
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE TOP HOLE CRACKED AT BS 380, S14L. REPAIRED PER BOEING SRM.
Part: SHEAR TIE — CRACKED (BS 360)
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360 AND 460, BETWEEN S14R AND 15R. REPAIRED PER BOEING SRM.
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT LT CHORD WL 193. REPAIRED PER BOEING SRM.
Part: STRINGER — CORRODED (BS 296)
DURING SCHEDULED D-CHECK, FOUND STRINGER 25L CORRODED AT BS 296. REPAIRED PER BOEING SRM.
Part: SILL — CORRODED (BS 947-986)
DURING SCHEDULED D-CHECK, FOUND MOPSILL CORRODED AT BS 947 TO 986. REPLACED SECTION PER BOEING SRM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING RON CHECK, FOUND AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOP. REPLACED BATTERY PACK PER BOEING M/M.
Part: BULKHEAD SKIN — CRACKED (BS 178)
DURING SCHEDULED SERVICE CHECK, FOUND BULKHEAD BS 178 SKIN CRACKED AT WL 220, BL 13. REPAIRED PER BOEING SRM.
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED C-CHECK, FOUND A 7 INCH CRACK AT BS 178 BULKHEAD. REPAIRED PER BOEING SRM.
Part: OVERHEAT LIGHT — ILLUMINATED (NR 1 ENGINE)
NUMBER 1 ENGINE OVERHEAT LIGHT ILLUMINATED, WITH OVERHEAT DETECTION SYSTEM ALREADY ON MEL. AIRCRAFT RETURNED TO OKC AND MADE AN UNEVENTFUL LANDING. INSPECTED, UNABLE TO DUPLICATE PROBLEM, CONTINUED SERVICE WITH SYSTEM PER MEL.
Part: COFFEEMAKER — FAILED (AFT GALLEY)
NOTED ELECTRICAL ODOR SMELL AT AFT GALLEY. INSPECTED AND FOUND ODOR EMITTING FROM AFT GALLEY UPPER COFFEEMAKER. DEACTIVATED COFFEEMAKER AND CONTINUED.
Earlier reports · 1995–1996 · 38 reports
1996
Part: BATTERY — DISCHARGED (FWD GALLEY)
DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY EMERGENCY FLASHLIGHTS NOT CHARGING. REPLACED BATTERIES PER BOEING M/M.
Part: SKIN — CRACKED (FWD ENTRY DOOR)
DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE CUTOUT CRACKED IN RADIUS OF OUTER SKIN. REPAIRED PER BOEING SRM.
Part: LIGHT — INOPERATIVE (CABIN)
FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER BOEING M/M.
Part: LIGHT — INOP (COCKPIT)
FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M.
Part: LIGHT — INOP (CABIN)
FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M.
Part: FLASHLIGHT — INOPERATIVE (FWD GALLEY)
AT GATE, FOUND EMERGENCY FLASHLIGHT IN FWD GALLEY INOP. REPLACED PER BOEING M/M.
1995
Part: FIRE LOOP — MALFUNCTIONED (APU)
APU FIRE DETECTION WARNING LIGHT ILLUMINATED. CREW EXPENDED FIRE BOTTLE. LANDED AT HOU WITHOUT INCIDENT. INSPECTED AREA AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. REPLACED FIRE BOTTLE AND CONTINUED PER MEL 26-7. DURING RON, REPLACED APU TAILPIPE FIRE LOOP PER BOEING M/M.
Part: LINE — RUPTURED (NR 2 ENGINE)
DURING CLIMBOUT, EXPERIENCED A-SYSTEM HYDRAULIC PRESSURE LOSS. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. INSPECTED AND REPLACED NUMBER 2 ENGINE REVERSER PRESSURE LINE AND HYDRAULIC CASE DRAIN FILTERS PER BOEING MAINTENANCE MANUAL.
Part: EEL BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND MAIN ENTRY AND SERVICE DOORS OUTSIDE EMERGENCY EXIT LIGHTS WEAK. REPLACED BATTERY PACK PER BOEING M/M.
Part: KEEL BEAM — CORRODED (BS 727)
DURING SCHEDULED D-CHECK, FOUND RIGHT KEEL BEAM INBOARD FLANGE CORRODED AT BS 727 PLUS 13.3, AND OUTBOARD FLANGE AT BS 727 PLUS 17.2, RBL 7.5. REPAIRED PER TRAMCO EWO 95-0260 AND BOEING STRUCTURAL REPAIR MANUAL.
Part: SKIN — DENTED (FUSELAGE)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 524, BETWEEN S15 AND 16L, AT BS 360 TO 420, BETWEEN S21 AND 22R, AT BS 998, BETWEEN S22 AND 23L, AT BS 931, BELOW S21R, AT BS 346, S24R, AT BS 345-360, BETWEEN S21 AND 22R, AT BS 877, S26R, AT BS 260 TO 280, BETWEEN S23 AND 24R, AT BS 967, AT S20L, AND AT BS 184, AT WL 182, RBL 22. REPAIRED ALL PER BOEING STRUCTURAL REPAIR MANUAL.
Part: FRAME — CRACKED (BS 277)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, S16L AND FRAME SHEAR TIE CRACKED AT BS 460, RBL 6. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: SPAR WEB — CRACKED (RT HORZ STAB)
DURING SCHEDULED D-CHECK, FOUND RIGHT HORIZONTAL STABILIZER FRONT SPAR WEB CRACKED AT L/E STA 128. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: DOUBLER — DAMAGED (FWD ENTRY DOOR)
DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR REPAIR DOUBLER NEEDING REWORK. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: STRINGER — DAMAGED (BS 727)
DURING SCHEDULED D-CHECK, FOUND TOOLING MARKS ON STRINGER AND SKIN DOUBLER AT BS 727B AND S7R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: SUPPORT — CORRODED (BS 312-344)
DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 312 TO 344, LBL 60, WL 208. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: CHORD — CRACKED (BS 947)
DURING SCHEDULED D-CHECK, FOUND FAILSAFE CHORD CRACKED AT BS 947, WL 175, LBL 4.5. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: FLOORBEAM — CORRODED (BS 987.5)
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 987.5, WL 208 AND WL 207, RBL 44.5 AND LBL 43.5. REPAIRED PER SWA RA 1-253-465.
Part: FRAME — CRACKED (BS 727)
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED BETWEEN S13 AND 14L, BS 727. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: STRINGER — CRACKED (BS 360)
DURING SCHEDULED D-CHECK, FOUND STRINGER CHANNEL CRACKED AT BS 360, S14L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: KEEL BEAM — CRACKED (BS 727)
DURING SCHEDULED D-CHECK, FOUND LEFT KEEL BEAM CRACKS AND HOLES AT BS 727 PLUS 18, LBL 6.5 AND 7.7, WL 149, I/B AND O/B FLANGES. REPAIRED PER TRAMCO EWO 95-0274 AND BOEING STRUCTURAL REPAIR MANUAL.
Part: RIB — CRACKED (WS 453)
DURING SCHEDULED D-CHECK, FOUND RIB UPPER FLANGE CRACKED AT LEFT WING STA 453 AT FWD STRINGER ATTACH. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: INTERCOSTAL — CRACKED (BS 295-311)
DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CRACKED AT BS 295-311, S4L, AND AT BS 178 TO 188, LBL 26, WL 195. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: STRINGER — CORRODED (FUSELAGE)
DURING SCHEDULED D-CHECK, FOUND STRINGER GOUGED AT BS 864, S15L, AND AT BS 928 TO 935, S14R, STRINGER CRACKED AT BS 1140, 12L, AT BS 787, S10R, AT BS 1016, S7L, AT BS 907, AT S4R AND L, AT BS 467, AT S22L, STRINGER CORRODED AT BS 1138, S13L, AND AT BS 520 TO 528, WL 216, LBL 65, AT BS 897-907, S20R, AND STRINGER CHANNEL CRACKED AT BS 360, S11L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: MOPSILL — CORRODED (BS 312)
DURING SCHEDULED D-CHECK, FOUND FORWARD ENTRY VERTICAL FLANGE ON MOPSILL CORRODED AT BS 312, LBL 61, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: FRAME — CRACKED (BS 202)
DURING SCHEDULED D-CHECK, FOUND FRAME LOWER CHORD CRACKED AT BS 202, RBL 2 TO 6, WL 165. ALS, FRAME CRACKED AT BS 1104, 1 INCH ABOVE S5L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: DOUBLER — CRACKED (BS 1155)
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME DOUBLER STRAP CRACKED AT BS 1155, WL 303, RBL 24. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: MOPSILL — CORRODED (BS 312)
DURING SCHEDULED D-CHECK, FOUND FORWARD ENTRY MOPSILL CORRODED AT BS 312 TO 344, LBL 61, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: ANGLE — CORRODED (BS 270)
DURING SCHEDULED D-CHECK, FOUND Z-ANGLE CORRODED AT BS 270, WL 208, LBL 10 RBL 10. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: SHEAR TIE — CRACKED (BS 400)
DURING SCHEDULED D-CHECK, FOUND OUTBOARD FLANGE OF SHEAR TIE ABOVE S16R CRACKED AT LOWER FASTENER AND IN RADIUS. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: CLIPS — CRACKED (FUSELAGE)
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 380, S22L AND 21L, AT BS 787, S24R, AT BS 616, S5R AND L, AT BS 360, AT S4 AND 5L, AT BS 807, S15L, AT BS 787, S15L, AT BS 887, S15L, AT BS 520, S19L, AT BS 706, S11R, AT BS 500B, S19L, AND AT BS 807, S16L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: FLOORBEAM — CORRODED (BS 360)
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 360, RBL 45 TO 63, WL 208. REPAIRED PER TRAMCO EWO 95-0258.
Part: FLOORBEAM — CRACKED (BS 616)
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM INNER CHORD CRACKED AT BS 616, LBL 65, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: FRAME — CRACKED (BS 1138)
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 1138, S13L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: KEEL BEAM — CORRODED (BS 727 PLUS 7)
DURING SCHEDULED D-CHECK, FOUND LEFT KEEL BEAM CORRODED UNDER SKIN AT BS 727 PLUS 7, WL 149, RBL 7. REPAIRED PER TRAMCO EWO 95-0260 AND BOEING STRUCTURAL REPAIR MANUAL.
Part: FLOORBEAM — CORRODED (BS 1016)
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, RBL 5, RBL 14.5, RBL 20.5, RBL 26, RBL 31, WL 207 AND 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: FRAME — CRACKED (BS 663.5)
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT FASTENER HOLES AT S3L, 2L, 1L, 2R AND 3R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: EEL BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED A3 CHECK, FOUND FWD OVERHEAD EXIT SIGN INOP. REPLACED BATTERY PACK PER BOEING M/M.