# N601TW: Boeing 767-231, registration cancelled 2001-07-20 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 20, 2001 - Exported to: Cameroon - Status when cancelled: Triennial form not returned - Airframe: [Boeing 767-231](https://openairdocs.org/model/boeing-767-231) (registry code 1385131) - Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM) (OpenAirDocs) - Serial number: 22564 - Type of aircraft: Fixed wing multi engine - Certificate issued: January 20, 1983 - Last registry action: July 17, 2001 - Mode S code: A7CCB4 - 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: 39.0997° N, 94.5786° W: Placed by OpenAirDocs: center of Kansas City, MO, within about 10 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N601TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=601TW - Page: https://openairdocs.org/deregistered/N601TW-2001-07-20 From the FAA registry file of October 29, 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 (28) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR TWAA0100201](https://openairdocs.org/sdr/TWAA0100201), Dec 28, 2000: LIGHT. INOPERATIVE. THE EGRESS LAMP WAS INOPERATIVE IN LEFT AFT CABIN AT SEAT 35 AREA. REPLACED THE FLEX LAMP. CHECK-C 11-2-00 LAX. - [SDR TWAA0019801](https://openairdocs.org/sdr/TWAA0019801), Dec 21, 2000: OVEN. BURNED. SMOKE WAS COMING FROM BEHIND THE NUMBER 2 OVEN IN THE FORWARD GALLEY. CREW PULLED THE OVEN CIRCUIT BREAKERS. FOUND OVEN FAN MOTOR BURNED. REPLACED THE OVEN. CHE - [SDR TWAA0012801](https://openairdocs.org/sdr/TWAA0012801), Aug 17, 2000: POWER SUPPLY. DISCHARGED. THE EGRESS LIGHTS ON THE LEFT SIDE OF THE CABIN FLASHED WITH THE EMERGENCY LIGHT SWITCH IN THE ARMED POSITION. REPLACED THE POWER SUPPLY. CHECK-C 7-27-00 LAX. - [SDR TWAA0011402](https://openairdocs.org/sdr/TWAA0011402), Jul 21, 2000: POWER SUPPLY. INOPERATIVE. THE EGRESS LIGHTS WERE INOPERATIVE ON LEFT SIDE OF CABIN FROM ROW 11 TO 17. REPLACED THE POWER SUPPLY. CHECK-C 3-11-00 LAX. - [SDR TWAA0009702](https://openairdocs.org/sdr/TWAA0009702), Jun 13, 2000: ANGLE. CRACKED. DURING OP 15 MAINT CHECK, ON THE RT WING, NUMBER 8 L/E SLAT WAS CRACKED ON THE L/E. SPAR SUPPORT ANGLE, O/B END. REPLACED LOWER CORD ANGLE 114T07-71, PER BOEING - [SDR TWAA0009701](https://openairdocs.org/sdr/TWAA0009701), Jun 12, 2000: SKIN. GOUGED. DURING OP 15 MAINT CHECK ON THE LT WING A GOUGE WITH MISSING AND EXPOSED HONEYCOMB WAS FOUND ON NUMBER 5 SPOILER, UNDER PANEL APPROX 24 INCHES FROM I/B END. REP - [SDR TWAA0009616](https://openairdocs.org/sdr/TWAA0009616), Jun 12, 2000: SKIN. WORN. DURING OP 15 MAINT CHECK ON THE RT WING THE NUMBER 12 LEADING EDGE SLAT HAD WORN SPOT ON I/B TRAILING EDGE 43 INCHES FROM THE O/B END. REPAIRED PER SRM 51-70-10 - [SDR TWAA0009615](https://openairdocs.org/sdr/TWAA0009615), Jun 11, 2000: SKIN. DENTED. DURING OP 15 MAINT CHECK ON THE LT WING THE I/B TRAILING EDGE FLAP BOTTOM HAD DENT 10 INCHES FROM TRAILING EDGE AND 14 INCHES I/B OF O/B HINGE DRIVE APPROX 1.5 - [SDR TWAA0009614](https://openairdocs.org/sdr/TWAA0009614), Jun 9, 2000: SKIN. DELAMINATED. DURING OP 15 MAINT CHECK ON THE LT WING, THE I/B AILERON HAD SEPARATION AND DELAMINATION AT THE L/E UPPER SURFACE, TWO PLACES. REPAIRED PER DWG 113T6002. - [SDR TWAA0001504](https://openairdocs.org/sdr/TWAA0001504), Jan 23, 2000: SKIN. DENTED. THE LT FUSELAGE WAS DENTED 5 INCH LONG BY 4 INCH WIDE AND 0.375 IN DEEP AT STA 1241, AT FORMER AND STRINGER 34L AND 35L. ACCOMPLISHED EXTERNAL REPAIR PER SRM 53 - [SDR TWAA9914901](https://openairdocs.org/sdr/TWAA9914901), Nov 3, 1999: LIGHT. INOP. FOUND CABIN EGRESS LIGHTS INOPERATIVE AT ROW 11 RT SIDE AND ON THE RT SIDE BY THE OVERWING EXIT. FOUND BOTH BULBS WERE LOOSE. SECURED LOOSE CONNECTIONS. CHECK-C - [SDR TWAA9908911](https://openairdocs.org/sdr/TWAA9908911), Jun 23, 1999: TEE. WORN. DURING CHECK-C MAINT MO-72F01A, REQUIRED THE RT ELEVATOR SLAVE LINKAGE LOST MOTION DEVICE HAVE THE TEE REPLACED PER FIG 2 OF SERVICE BULLETIN 767 27A0136. REMOV - [SDR TWAA9904924](https://openairdocs.org/sdr/TWAA9904924), Mar 31, 1999: STRUCTURE. DAMAGED. THE FUSELAGE SKIN WAS DAMAGED AT ST 478, STRINGER 35L, WITH STRINGER PUSHED IN .5 IN BY 7 IN BY 9 IN AREA. SKIN ON FORMER RING WAS BUCKLED .25 IN. SPLICED DOUBL - [SDR TWAA9813602](https://openairdocs.org/sdr/TWAA9813602), Aug 24, 1998: REGULATOR. LEAKING. CREW OXYGEN PRESSURE WENT TO ZERO, NOTICED AT TOP OF CLIMB. RETURNED TO JFK. FOUND CAPT OXY REGULATOR FAULTY. REPLACED REGULATOR AND OXY BOTTLE. CHECK-C 7-9-98 - [SDR TWAA9811301](https://openairdocs.org/sdr/TWAA9811301), Jun 25, 1998: SKIN. GOUGED. DURING CHECK-C, MAINTENANCE FOUND FUSELAGE SKIN GOUGE 3 FEET BELOW AFT EDGE OF THE R-1 CABIN DOOR. INSTALLED DOUBLER WITH HI-LOCKS (WEST) 8.50 INCHES BY 10 INCH - [SDR TWAA9805102](https://openairdocs.org/sdr/TWAA9805102), Apr 5, 1998: CART. WORN. JFK - FLT 841 - SERVING CART 343 POPPED NR 2 CIRCUIT BREAKER. THERE WAS SMELL OF BURNED ELECTRICAL WIRING IN OR NEAR CART. CREW DID NOT RESET CIRCUIT BREAKER. R - [SDR TWAA9771003](https://openairdocs.org/sdr/TWAA9771003), Jun 21, 1997: TAT PROBE. FAILED. JFK - FLT 722 - DURING CRUISE ALL AUTOPILOT FAILED TO ENGAGE FLT MANAGEMENT COMPUTER, NO UPDATE OR AUTO TUNE. ALSO, NO TOTAL AIR TEMPERATURE OR WIND DATA. REPLA - [SDR TWAA9728001](https://openairdocs.org/sdr/TWAA9728001), Feb 22, 1997: ENGINE. STALLED. STL - FLT 840 - DURING CLIMB, NR 1 ENGINE, S/N 4617, EXPERIENCED NUMEROUS STALLS. CHANGED ENGINE. (M) - [SDR TWAA9703005](https://openairdocs.org/sdr/TWAA9703005), Jan 4, 1997: O-RING. FAILED. JFK - FLT 740 - DURING CRUISE, LOST CENTER HYDRAULIC SYSTEM FLUID. REMOVED AND REPLACED WORN O-RING, MFG P/N NAS1611-014, AT THE DIFFERENTIAL PRESSURE SWITCH IN - [SDR TWAA9614602](https://openairdocs.org/sdr/TWAA9614602), Nov 26, 1996: CONTROLLER. FAILED. STL - FLT 104 - DURING CRUISE, AISLE WARMER CART EMITTED ELECTRICAL ODOR AND SMOKE. FOUND FAULTY POWER CONTROLLER, MFG PN 91658-3. REPLACED WARMER CART CONTROLL - [SDR 96ZZZM912](https://openairdocs.org/sdr/96ZZZM912), Apr 18, 1996: SKIN. DAMAGED. MCI - DURING SPECIAL CHECK, FOUND FOD DAMAGE TO LEFT HORIZONTAL STABILIZER LOWER SKIN AND FRONT SPAR, FS 186 TO FS 255. REPAIRED PER ARA 9957 AND TWA AND STANDA - [SDR 96ZZZM910](https://openairdocs.org/sdr/96ZZZM910), Apr 18, 1996: SKIN. DAMAGED. MCI - DURING SPECIAL CHECK, FOUND FOD DAMAGE TO LEFT AFT FUSELAGE, FS 1605 TO FS 1629 AND FROM STRINGER 20L TO STRINGER 16L. REPLACED AND REPAIRED SKIN PANEL PE - [SDR 96ZZZM901](https://openairdocs.org/sdr/96ZZZM901), Apr 11, 1996: SKIN. DAMAGED. MCI - DURING SPECIAL CHECK, FOUND LEFT STABILIZER LOWER SKIN DAMAGED. REPAIRED PER ARA 9959. (M) - [SDR 96ZZZM899](https://openairdocs.org/sdr/96ZZZM899), Apr 11, 1996: FORMER. CRACKED. MCI - DURING SPECIAL CHECK, FOUND FUSELAGE FORMER, FS 1605, DENTED AND CRACKED, STRINGER 13L TO STRINGER 20L. REPLACED FORMER PER ARA 9958. (M) - [SDR 96ZZZM778](https://openairdocs.org/sdr/96ZZZM778), Mar 25, 1996: STRINGER. DAMAGED. DURING SPECIAL CHECK, FOUND LOWER HORIZONTAL STABILIZER DAMAGE AT STATION 304, STRINGER 7L. REPAIRED PER SRM 55-10-03, PAGE 101, DETAIL NR 1 AND TWA STANDARD PR - [SDR 96ZZZM777](https://openairdocs.org/sdr/96ZZZM777), Mar 25, 1996: STRINGER. CRACKED. DURING SPECIAL CHECK, FOUND FUSELAGE STRINGERS 16, 17L, 18L AND 19L, DENTED AND CRACKED, FS 1582 TO FS 1660. REPAIRED PER ARA 9958 AND SRM 53-00-03, PAGE 201, F - [SDR 96ZZZM776](https://openairdocs.org/sdr/96ZZZM776), Mar 25, 1996: STRINGER. CRACKED. DURING SPECIAL CHECK, FOUND CRACK IN LOWER HORIZONTAL STABILIZER STRINGER 6L, STATION 290. REPAIRED PER SRM 55-10-03, FIGURE 101, DETAIL NR 1 AND TWA STANDARD P - [SDR 96ZZZM769](https://openairdocs.org/sdr/96ZZZM769), Mar 25, 1996: STRINGER. DAMAGED. DURING SPECIAL CHECK, FOUND LOWER HORIZONTAL STABILIZER STRINGER 5L DAMAGED AT STATION 300. REPAIRED PER SRM 55-10-03, FIGURE 101, DETAIL NR 1 AND TWA STANDARD ## FAA accident and incident reports (4) 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 19880630031979I](https://openairdocs.org/incident/19880630031979I), Jun 30, 1988: Boeing 767 (N601TW), St Louis, MO. Landing gear failed to retract on climbout. Returned. Replaced c hydraulic pressure line. - [Incident 19861029065789I](https://openairdocs.org/incident/19861029065789I), Oct 29, 1986: Boeing 767231 (N601TW), Las Vegas, NV. Fire warning caused crew to shut down engine. Fire detection warning loop faulty. No actual fire occurred. - [Incident 19860707039709I](https://openairdocs.org/incident/19860707039709I), Jul 7, 1986: Boeing 767231 (N601TW), St Louis, MO. Discrepancy in altimeters noted after takeoff. Returned and found a leak in line to aux pitot tube. - [Incident 19821127066219I](https://openairdocs.org/incident/19821127066219I), Nov 27, 1982: Boeing 767231 (N601TW), Kansas City, KS, Minor damage. R/h offwing slide compartment door opened in flight. Slide assembly missing. Found 4 miles from runway. --- 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.