# N602TW: 1982 Boeing 767-231, registration cancelled 2003-04-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 2, 2003 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 767-231](https://openairdocs.org/model/boeing-767-231) (registry code 1385131) - Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999) - Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM) (OpenAirDocs) - Serial number: 22565 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: December 3, 1982 - Certificate issued: February 9, 1983 - Last registry action: October 17, 2000 - Mode S code: A7D06B - Owner when cancelled: [Trans World Airlines Inc](https://openairdocs.org/faa-owner/TRANS%20WORLD%20AIRLINES%20INC) - Location: [Kansas City, MO](https://openairdocs.org/faa-place/MO/Kansas%20City) - Owner type: Corporation - Owner's area on the map: 39.2746° N, 94.7266° W: Placed by OpenAirDocs at the center of ZIP code 64153, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N602TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=602TW - Page: https://openairdocs.org/deregistered/N602TW-2003-04-02 From the FAA registry file of November 3, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 767-231: https://openairdocs.org/model/boeing-767-231.md ## Service difficulty reports (72, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR TWAA0103101](https://openairdocs.org/sdr/TWAA0103101), Feb 16, 2001: POWER SUPPLY. DISCHARGED. THE EGRESS LIGHTS ON RT SIDE OF CABIN ROWS 11 THRU 16 ILLUMINATED INTERMITTENTLY. REPLACED THE POWER SUPPLY. CHECK-C 11-29-00 LAX. - [SDR TWAA0018902](https://openairdocs.org/sdr/TWAA0018902), Dec 5, 2000: FLAP. PUNCTURED. DURING CHECK-C MAINT ON RT WING FOUND 2 PUNCTURES INSIDE FLAP UNDER PANEL 666NT. FILLED HOLES WITH 934 ADHESIVE. ACCOMPLISHED HOT BOND METAL TO METAL REPAIR PER - [SDR TWAA0018906](https://openairdocs.org/sdr/TWAA0018906), Dec 4, 2000: SKIN. DELAMINATED. DURING CHECK-C MAINT THE RT WING INBD FLAP HAD DELAMINATION ON COMPOSITE MATERIAL AT APPROX. 45 INCHES, 55 INCHES, AND 60 INCHES FROM INBD SIDE. REMOVED SKIN AN - [SDR TWAA0018903](https://openairdocs.org/sdr/TWAA0018903), Dec 4, 2000: SKIN. DELAMINATED. DURING CHECK-C MAINT FOUND NUMBER 8 L/E SLAT INBD EDGE WAS DELAMINATED ON PREVIOUS REPAIR IN TWO PLACES, ONE EA INSIDE (BACK) AND OUTER SKIN. INSTALLED A 11 IN - [SDR TWAA0018905](https://openairdocs.org/sdr/TWAA0018905), Dec 3, 2000: DOUBLER. DELAMINATED. DURING CHECK-C MAINT THE LT WING NUMBER 3 L.E. SLAT REPAIR, INBD EDGE WAS NOT ADHEARING TO SKIN. REMOVED OLD REPAIR AND INSTALLED NEW 6 IN BY 6 IN METAL TO META - [SDR TWAA0018904](https://openairdocs.org/sdr/TWAA0018904), Nov 30, 2000: DOUBLER. DELAMINATED. DURING CHECK-C MAINT THE NUMBER 7 L/E SLAT HAD 4 BY 5 PREVIOUS REPAIR THAT HAD DELAMINATION IN CENTER OF REPAIR. INSTALLED A 4 1/2 BY 7 IN METAL BOND REPAIR PER - [SDR TWAA0018503](https://openairdocs.org/sdr/TWAA0018503), Nov 27, 2000: POWER SUPPLY. WORN. THE EGRESS LIGHTS ON THE LEFT SIDE OF THE FIRST CLASS CABIN WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 8-1-00 LAX. - [SDR TWAA0018101](https://openairdocs.org/sdr/TWAA0018101), Nov 17, 2000: POWER SUPPLY. INOPERATIVE. THE FIRST CLASS SECTION EGRESS LIGHTS WERE INOPERATIVE ON LT SIDE OF CABIN. REPLACED THE BATTERY PACK. CHECK-C 8-1-00 LAX. - [SDR TWAA0016701](https://openairdocs.org/sdr/TWAA0016701), Oct 26, 2000: BATTERY PACK. DISCHARGED. THE EGRESS LIGHT ON LT SIDE OF FIRST CLASS, AND THE FWD GALLEY CROSS WALK EGRESS LIGHTS, WERE INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS MALFUNCTION, AN - [SDR TWAA0006434](https://openairdocs.org/sdr/TWAA0006434), Apr 24, 2000: SKIN. DEBONDED. DURING CHECK-C MAINT, THE LT WING NUMBER 6 LEADING EDGE SLAT TOP SIDE AT MID SPAN HAD THE HOT BOND LIFTED AND HAD BEEN SEALED WITH SPEED TAPE PER SRM 57-43-02. - [SDR TWAA0006433](https://openairdocs.org/sdr/TWAA0006433), Apr 24, 2000: SKIN. DENTED. DURING CHECK-C MAINT, THE RT WING LEADING EDGE OF I/B TRAILING EDGE FLAP HAD A 1 INCH DENT, 2 FT I/B FROM THE O/B END. APPLIED FILLER ADHESIVE ON TRAILING EDGE - [SDR TWAA0006302](https://openairdocs.org/sdr/TWAA0006302), Apr 19, 2000: SKIN. DELAMINATED. DURING CHECK-C MAINT, THE LT WING NUMBER 2 L/E SLAT O/B END, THE T/E WEDGE HAD A BULGE THAT WAS DELAMINATING. APPLIED HOT BOND REPAIR ON NR 2 SLAT APPROX 4 IN B - [SDR TWAA0006301](https://openairdocs.org/sdr/TWAA0006301), Apr 19, 2000: STRUCTURE. DAMAGED. DURING CHECK-C MAINT, THE LT WING NUMBER 4 L/E SLAT ASSY HAD A HOLE IN THE INSIDE SURFACE. FILLED DAMAGED AREA AND APPLIED 2 IN BY 2 IN METAL TO METAL HOT BOND. - [SDR TWAA0006206](https://openairdocs.org/sdr/TWAA0006206), Apr 19, 2000: SKIN. DELAMINATED. DURING CHECK-C MAINT THE RH WING NUMBER 10 L/E SLAT HAD 5 INCH SQUARE DOUBLER THAT WAS DELAMINATING, ON TOP SURFACE, 5 FT I/B FROM THE O/B END. REMOVED DELAMINA - [SDR TWAA0006205](https://openairdocs.org/sdr/TWAA0006205), Apr 19, 2000: SKIN. DELAMINATED. DURING CHECK-C MAINT, FOUND RT WING NUMBER 7 L/E SLAT REPAIR HAD A 6 INCH BY 4 INCH DELAMINATION, 4 INCHES FROM THE I/B END, ON TOP. APPLIED HOT BOND REPAIR ON - [SDR TWAA0002001](https://openairdocs.org/sdr/TWAA0002001), Feb 3, 2000: SKIN. DELAMINATED. DURING CHECK-C MAINTENANCE, THE NUMBER 1 LE SLAT TOP SIDE, AN EXISTING 6 IN BY 6 IN PATCH WAS LOOSE AND DELAMINATING AT THE INBD TE WEDGE. REMOVED OLD REPAIR. I - [SDR TWAA9914601](https://openairdocs.org/sdr/TWAA9914601), Oct 29, 1999: BATTERY. DISCHARGED. DURING PREFLIGHT, FOUND EGRESS LIGHTS INOP FROM SEAT 33 LT TO ROW 35 LT. REPLACED BATTERY. CC 10-24-99 LAX. - [SDR TWAA9913904](https://openairdocs.org/sdr/TWAA9913904), Oct 10, 1999: SWITCH. FAILED. IN AN ETOPS FLIGHT SEGMENT THE LEFT ENGINE FILTER BYPASS LIGHT BLINKED THEN CAME ON STEADY. THE ENGINE WAS SHUT DOWN AND THE FLIGHT DIVERTED TO TER. THE MAIN OI - [SDR TWAA9913302](https://openairdocs.org/sdr/TWAA9913302), Sep 28, 1999: LIGHT. DAMAGED. FOUND CABIN EGRESS LIGHTS INOPERATIVE AT THE NUMBER 2 CROSSOVER POINT. REPLACED THE LIGHT STRIP. CHECK-C 8-25-99 LAX. - [SDR TWAA9908006](https://openairdocs.org/sdr/TWAA9908006), Jun 2, 1999: TEE. WORN. DURING CHECK-C MAINT MO 72F01 CALLED FOR REPLACING THE RT ELEVATOR SLAVE LINKAGE LOST MOTION DEVICE TEE. REPLACED TEE PER SERVICE BULLETIN 27A0136, REV 1. - [SDR TWAA9907202](https://openairdocs.org/sdr/TWAA9907202), May 14, 1999: BULB. FAILED. FOUND EXTERNAL EMERGENCY LIGHT INOPERATIVE AT THE NUMBER 4 DOOR ON LT SIDE OF FUSELAGE. REPLACED THE BULB. CHECK-C 2-26-99 LAX. - [SDR TWAA9907201](https://openairdocs.org/sdr/TWAA9907201), May 14, 1999: BULB. FAILED. THE AFT GALLEY CEILING EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BULB. CHECK-C 2-26-99 LAX. - [SDR TWAA9906103](https://openairdocs.org/sdr/TWAA9906103), Apr 25, 1999: SKIN. DELAMINATED. THE NR 7 LEADING EDGE SLAT TRAILING EDGE WEDGE HAD DELAMINATION APPROX 8.5 FT FROM I/B EDGE. AREAS APPROX 2.5 INCHES IN DIAMETER AND 1.5 INCH APART ON LOWER SUR - [SDR TWAA9901701](https://openairdocs.org/sdr/TWAA9901701), Jan 19, 1999: POWER SUPPLY. INOP. FOUND FLOOR EGRESS LIGHTS OUT ON LT SIDE OF CABIN FROM ROW 24 TO ROW 33. REPLACED POWER SUPPLY. CHECK-C 11-17-98 MCI. - [SDR TWAA9818311](https://openairdocs.org/sdr/TWAA9818311), Nov 6, 1998: STRINGER. CORRODED. DURING OP 15 MAINT CHECK, FOUND FUSELAGE STRINGER 39R CORRODED BETWEEN STA 610 AND 632. REMOVED S39R AT STA 600 TO 622 AND INSTALLED NEW FABRICATED PART PER SRM - [SDR TWAA9901008](https://openairdocs.org/sdr/TWAA9901008), Oct 30, 1998: SKIN. CORRODED. DURING OP 15 MAINT CHECK, FOUND STA 1269, STRINGER 39R WITH CORROSION BETWEEN INBD SIDE OF STRINGER AND FUSELAGE SKIN, AND STRINGER 39L CORRODED BETWEEN STRINGE - [SDR TWAA9818206](https://openairdocs.org/sdr/TWAA9818206), Oct 30, 1998: STRINGER. CORRODED. DURING OP 15 MAINT CHECK, FOUND CORROSION ON LOWER SIDE OF STRINGER 38R, STA 565. CUT OUT CORROSION PER SRM 51-10-03 PAGE 16. INSTALLED SECTION OF STRINGER AT 3 - [SDR TWAA9818205](https://openairdocs.org/sdr/TWAA9818205), Oct 30, 1998: STRINGER. CORRODED. DURING OP 15 MAINT CHECK, FOUND CORROSION ON STRINGER 39L BETWEEN STA 616 TO 632. REMOVED SECTION OF CORRODED STRINGER AND CLEANED STA 606 TO 632 PER SRM 51-10- - [SDR TWAA9818204](https://openairdocs.org/sdr/TWAA9818204), Oct 30, 1998: STRINGER. CORRODED. DURING OP 15 MAINT CHECK, FOUND CORRODED STRINGER 38R BETWEEN STA 610 TO 632. CUT OUT SECTION OF STRINGER FROM STA 600 TO 627. REMOVED CORROSION PER SRM 51-10-0 - [SDR TWAA9818203](https://openairdocs.org/sdr/TWAA9818203), Oct 30, 1998: STRINGER. CORRODED. DURING OP 15 MAINT CHECK, FOUND STRINGER 39L CORRODED AT STA 610 TO 632. REMOVED SECTION OF CORRODED STRINGER AND CLEANED STA 606 TO 632. INSTALLED SPLICE BETWE - [SDR TWAA9818202](https://openairdocs.org/sdr/TWAA9818202), Oct 29, 1998: STRINGER. CORRODED. DURING OP 15 MAINT CHECK, FOUND CORROSION AT STA 580 STRINGER 39L ON THE STRINGER. SPLICED STRINGER AT STA 577 TO 600 PER SRM 53-00-03 PAGE 215, DETAIL III, FIG - [SDR TWAA9818302](https://openairdocs.org/sdr/TWAA9818302), Oct 26, 1998: STRINGER. CORRODED. DURING OP 15 MAINT CHECK, FOUND STRINGER 39R WITH EXFOLIATION CORROSION AT STA 561 TO 562, ON TOP INBD LIP APPROX 1 IN LONG. CORROSION REMOVED AND REPAIRED WITH - [SDR TWAA9818012](https://openairdocs.org/sdr/TWAA9818012), Oct 26, 1998: SKIN. CORRODED. DURING OP 15 MAINT CHECK, CENTER WING UPPER SKIN WAS CUT OUT FOR CORROSION TO SKIN STA 853 TO 855. RECTANGULAR SECT FRONT 71 RBL TO 84 RBL AND REAR 69 RBL TO 86 - [SDR TWAA9818011](https://openairdocs.org/sdr/TWAA9818011), Oct 26, 1998: SKIN. CORRODED. DURING OP 15 MAINT CHECK, FOUND BELOW UPPER CENTER WING SKIN SUPPORT BEAM WITH EXIFOLIATION CORROSION THRU BEAM. CORROSION VISIBLE FROM STA 855 TO 853 RBL 75 TO - [SDR TWAA9818010](https://openairdocs.org/sdr/TWAA9818010), Oct 26, 1998: SKIN. CORRODED. DURING OP 15 MAINT CHECK, FOUND INTERGRANULAR CORROSION ON CENTER UPPER WING SKIN AT STA 954.5 TO 858, RBL 75 TO RBL 88. ACCOMP HIGH FREQ EDDY CURRENT OF AREA A - [SDR TWAA9818009](https://openairdocs.org/sdr/TWAA9818009), Oct 26, 1998: SKIN. CORRODED. DURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION ON UPPER SURFACE OF WING CENTER SECTION AT STA 860 BELOW EMERGENCY EXIT ON RT SIDE. CUT OUT CORRODED AREA PER SR - [SDR TWAA9818008](https://openairdocs.org/sdr/TWAA9818008), Oct 26, 1998: SKIN. CORRODED. DURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION AT UPPER SKIN STA 830 TO 852, RBL 74 TO RBL 97. REMOVED CORROSION PER SRM 51-10-00. NDT HIGH FREQ EDY CURRENT PE - [SDR TWAA9818210](https://openairdocs.org/sdr/TWAA9818210), Oct 22, 1998: STRINGER. CRACKED. DURING OP 15 MAINT CHECK, FOUND STRINGER 33L CRACKED AT STA 434. REPAIRED STRINGER PER SRM 53-00-03 PAGE 209 FIG 202. - [SDR TWAA9818209](https://openairdocs.org/sdr/TWAA9818209), Oct 22, 1998: STRINGER. CRACKED. DURING OP 15 MAINT CHECK, FOUND FWD END OF STRINGER 33R CRACKED AT FORMER TIE FITTING, STA 1085. SPLICED IN NEW SECTION OF STRINGER PER 767-200 SRM 53-00-03 PAG - [SDR TWAA9818208](https://openairdocs.org/sdr/TWAA9818208), Oct 22, 1998: STRINGER. CRACKED. DURING OP 15 MAINT CHECK, FOUND STRINGER 33L CRACKED AT STA 434. REPAIRED STRINGER PER SRM 53-00-03 PG 209 FIG 202. - [SDR TWAA9818207](https://openairdocs.org/sdr/TWAA9818207), Oct 22, 1998: STRINGER. CORRODED. DURING OP 15 MAINT CHECK, FOUND FORWARD END OF STRINGER 33R CRACKED AT FORMER TIE FITTING, STA 1085. SPLICED IN NEW SECTION OF STRINGER PER 767-200 SRM 53-00-03 - [SDR TWAA9818312](https://openairdocs.org/sdr/TWAA9818312), Oct 21, 1998: SKIN. GOUGED. DURING OP 15 MAINT CHECK, FOUND LT ELEV HAD ONE INCH LONG GOUGE IN UPPER SURPACE, 29 IN OTBD FROM OTBD ACTUATOR, AND 15 IN AFT FROM THE LEADING EDGE. REMOVED DA - [SDR TWAA9818007](https://openairdocs.org/sdr/TWAA9818007), Oct 19, 1998: SKIN. CORRODED. DURING OP 15 MAINT CHECK, FOUND CORROSION AT UPPER SKIN CENTER WING AT STA 850 TO 852.5, RBL 83.5 TO RBL 88.5, INTERGRANULAR CORROSION. SANDED CORROSION PER SRM - [SDR TWAA9818006](https://openairdocs.org/sdr/TWAA9818006), Oct 19, 1998: SKIN. CORRODED. DURING OP 15 MAINT CHECK, FOUND CORROSION ON CENTER FUEL TANK UPPER SKIN AT STA 846, RBL 79 TO 83. SANDED CORROSION PER SRM 51-10-00, PAGE 16 PARA 6. NO CRACKS - [SDR TWAA9817806](https://openairdocs.org/sdr/TWAA9817806), Oct 16, 1998: SKIN. CORRODED. DURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION ON UPPER SKIN, STA 830 TO 852, LBL 74 IN TO LBL 97 IN. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6 AND - [SDR TWAA9817805](https://openairdocs.org/sdr/TWAA9817805), Oct 16, 1998: SKIN. CORRODED. DURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION ON UPPER SURFACE OF WING CENTER SECTION, STA 860 BELOW EMERGENCY EXIT ON LT SIDE. REMOVED CORROSION PER SRM 51-1 - [SDR TWAA9817804](https://openairdocs.org/sdr/TWAA9817804), Oct 16, 1998: SKIN. CORRODED. DURING OP 15 MAINT CHECK, FOUND CORROSION ON TOP WING AT FASTENERS STA 883 TO 911, LBL 74 IN TO 97 IN. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6, A - [SDR TWAA9817803](https://openairdocs.org/sdr/TWAA9817803), Oct 16, 1998: SKIN. CORRODED. DURING OP 15 MAINT CHECK, FOUND CORROSION AT TOP WING SKIN AT FASTENERS STA 911 TO 933, LBL 74 IN TO 97 IN. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART - [SDR TWAA9817802](https://openairdocs.org/sdr/TWAA9817802), Oct 16, 1998: SKIN. CORRODED. DURING OP 15 MAINT CHECK, FOUND CORROSION ON TOP WING SKIN AT FASTENERS STA 933 TO 965, LBL 74 IN TO 97 IN. REMOVED CORROSION PER SRM 51-10-00. NDT EDDY CURRENT - [SDR TWAA9817801](https://openairdocs.org/sdr/TWAA9817801), Oct 16, 1998: SKIN. CORRODED. DURING OP 15 MAINT CHECK, FOUND CORROSION ON TOP WING SKIN AT FASTENERS STA 859 TO 883, LBL 74 IN TO 97 IN. REMOVED CORROSION PER SRM 51-10-00. NDT HIGH FREQ ED All 72: https://openairdocs.org/deregistered/N602TW-2003-04-02/reports.md ## NTSB investigations (2) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB NYC92IA129](https://openairdocs.org/ntsb/NYC92IA129), Jun 28, 1992: Boeing 767-231ER (N602TW), Jamica, NY, incident, minor damage. Probable cause: THE FAILURE OF THE FIFTH STAGE LOW PRESSURE TURBINE VANES DUE TO FATIGUE. - [NTSB LAX83IA080](https://openairdocs.org/ntsb/LAX83IA080), Jan 24, 1983: Boeing 767-231 (N602TW), San Diego, CA, incident, minor damage ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19911211059749I](https://openairdocs.org/incident/19911211059749I), Dec 11, 1991: Boeing 767231 (N602TW), St Louis, MO. Right engine oil temperature increasing. Shut down. Returned. Found chaffed wire at oil temperature sensor. - [Incident 19830123006589I](https://openairdocs.org/incident/19830123006589I), Jan 23, 1983: Boeing 767231 (N602TW), San Diego, CA. On approach left over-wing escape slide fell from aircraft. Recovered by police. Found slide doors opened. ## Other aircraft with N602TW - [Registered now](https://openairdocs.org/aircraft/N602TW): Craig-Stearman John T VANS ACFT RV-4, S/N 1 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.