# N610TW: 1983 Boeing 767-231, registration cancelled 2009-01-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 13, 2009 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 767-231](https://openairdocs.org/model/boeing-767-231) (registry code 1385131) - Engine: [Pratt & Whitney JT9D series](https://openairdocs.org/engine/pratt-whitney-jt9d-series) (registry code 52054) - Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM) (OpenAirDocs) - Serial number: 22573 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 15, 1983 - Certificate issued: December 5, 2002 - Last registry action: December 16, 2008 - Mode S code: A7F07C - Owner when cancelled: [Phoenix Aircraft Leasing Inc](https://openairdocs.org/faa-owner/PHOENIX%20AIRCRAFT%20LEASING%20INC) - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Corporation - Owner's area on the map: 25.8166° N, 80.3105° W: Placed by OpenAirDocs at the center of ZIP code 33166, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N610TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=610TW - Page: https://openairdocs.org/deregistered/N610TW-2009-01-13 From the FAA registry file of November 5, 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 (32) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR TWAA0103402](https://openairdocs.org/sdr/TWAA0103402), Feb 21, 2001: LIGHT. INOPERATIVE. THE EGRESS LIGHTING WAS INOPERATIVE IN MID GALLEY AND RT SIDE OF CABIN ROWS 18 TO 23. REPLACED FLEX CABLE 5854-3 AT MID GALLEY AND FLEX CABLE 5854-5 FOR ROWS 18 - [SDR TWAA0014802](https://openairdocs.org/sdr/TWAA0014802), Sep 24, 2000: BATTERY PACK. DISCHARGED. THE EGRESS LIGHTS STAYED ON ALL THE TIME AT ROWS 18 TO 22 ON RT SIDE OF CABIN. CLEANED AND SECURED CONNECTOR D9024 ON BATTERY PACK AND D1126 ON POWER SUPPLY. CH - [SDR TWAA0014801](https://openairdocs.org/sdr/TWAA0014801), Sep 24, 2000: BATTERY PACK. DISCHARGED. THE EGRESS LIGHTS AT ROWS 22 TO 28 ON RT SIDE INTERMITTANTLY TURNED ON AND OFF WITH THE SWITCH IN OFF OR ARMED POSITION. REPLACED BATTERY PACK. CHECK-C 8-22-00 - [SDR TWAA0014005](https://openairdocs.org/sdr/TWAA0014005), Sep 10, 2000: BATTERY PACK. DISCHARGED. THE EXIT SIGNS AT THE LEFT SIDE NUMBER 2 DOOR, AND THE RT SIDE NUMBER 2 DOOR, WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 5-15-00. - [SDR TWAA0013601](https://openairdocs.org/sdr/TWAA0013601), Aug 31, 2000: LIGHT. INOPERATIVE. THE EGRESS LIGHTS WERE INOPERATIVE ON RT SIDE OF AIRCRAFT AT THE AFT GALLEY. DEFERRED CORRECTIONS PER MEL. CHECK-C 5-15-00. MAINTENANCE LATER FOUND THAT SYSTEM - [SDR TWAA0013318](https://openairdocs.org/sdr/TWAA0013318), Aug 25, 2000: SKIN. DELAMINATED. DURING CHECK-C MAINT, ON RT WING L/E SLAT NUMBER 11, O/B END LOWER SURFACE OF THE WEDGE HAD DELAMINATION. INSTALLED REPLACEMENT HONEYCOMB CORE AND 3 INCH BY 9 I - [SDR TWAA0013406](https://openairdocs.org/sdr/TWAA0013406), Aug 24, 2000: SKIN. DELAMINATED. DURING CHECK-C, MAINT ON LT WING, FOUND NUMBER 5 L/E SLAT TRAILING EDGE WEDGE I/B AFT CORNER, TOP SURFACE DELAMINATED. INSTALLED 6 INCH BY 8 INCH HOT BOND EXTER - [SDR TWAA0013320](https://openairdocs.org/sdr/TWAA0013320), Aug 24, 2000: SKIN. DELAMINATED. DURING CHECK-C MAINT, ON RT WING THE L/E SLAT NUMBER 11, I/B END LOWER SURFACE T/E WEDGE HAD DELAMINATION. INSTALLED HOT BOND REPAIR PER SRM 51-70-10. REPLACED - [SDR TWAA0013319](https://openairdocs.org/sdr/TWAA0013319), Aug 24, 2000: SKIN. DELAMINATED. DURING CHECK-C MAINT ON RT WING, THE L/E SLAT NUMBER 12 I/B END LOWER SURFACE OF THE T/E WEDGE HAD DELAMINATION. INSTALLED REPLACEMENT HONEYCOMB CORE AND 12 INC - [SDR TWAA0000111](https://openairdocs.org/sdr/TWAA0000111), Nov 29, 1999: PATCH. LOOSE. DURING CHECK-C MAINT, THE PATCH ON THE LEFT WING NUMBER 6 LE SLAT, TOWARD THE OTBD END, WAS COMING LOOSE AT THE EDGES. INSTALLED A 4 1/2 IN DIAMETER METAL HOT B - [SDR TWAA9904008](https://openairdocs.org/sdr/TWAA9904008), Mar 7, 1999: SKIN. DAMAGED. DURING CHECK-C MAINT, FOUND ON LT WING, THE O/B TRAILING EDGE FLAP WITH A .25 IN HOLE AT I/B END OF LOWER SURFACE. INSTALLED A 2 IN BY 2 IN WET LAY-UP PER SRM 5 - [SDR TWAA9904007](https://openairdocs.org/sdr/TWAA9904007), Mar 7, 1999: SKIN. DELAMINATED. DURING CHECK-C MAINT, FOUND LT WING LOWER SURFACE ONE FOOT FROM I/B EDGE, WITH A 6 BY 4 IN DELAMINATION, 6 IN FROM THE TRAILING EDGE. REMOVED DELAMINATED AREA A - [SDR TWAA9904006](https://openairdocs.org/sdr/TWAA9904006), Mar 7, 1999: SKIN. DAMAGED. DURING CHECK-C MAINT, FOUND LT WING TRAILING EDGE AFT FLAP OF THE I/B FLAP WITH A HOLE 28 IN I/B OF O/B EDGE, 9 IN AFT OF LEADING EDGE. INSTALLED HOT BOND REPAI - [SDR TWAA9904005](https://openairdocs.org/sdr/TWAA9904005), Mar 7, 1999: WEDGE. DELAMINATED. DURING CHECK-C MAINT, FOUND THE NR 11 LEADING EDGE SLAT TRAILING EDGE WEDGE WITH DELAMINATION 4.5 INCHES IN DIAMETER, LOCATED 78 IN O/B OF I/B END. INSTALLED ME - [SDR TWAA9901101](https://openairdocs.org/sdr/TWAA9901101), Jan 18, 1999: LIGHT. INOP. FLOOR EGRESS LIGHTING WAS INOPERATIVE FROM CABIN ROW 18 TO 22. REMOVED MOISTURE FROM TRACK AT SERVICE CENTER CROSSOVER. CHECK-C 12-2-98 LAX. - [SDR TWAA9818102](https://openairdocs.org/sdr/TWAA9818102), Nov 10, 1998: SWITCH. WORN. THE EXTERIOR EMERGENCY LIGHT TEST SWITCH WAS FOUND INOPERATIVE. REPLACED SWITCH. CHECK-C 9-16-98 LAX. - [SDR TWAA9815002](https://openairdocs.org/sdr/TWAA9815002), Sep 16, 1998: SKIN. DELAMINATED. DURING CHECK-C MAINT, FOUND RT WING NR 11 LE SLAT REPAIR LOOSE IN CENTER AREA, 1.5 IN BY 2.5 IN. REMOVED OLD REPAIR. REMOVED 1 IN BY 3 IN DELAMINATION ON O/B EN - [SDR TWAA9814701](https://openairdocs.org/sdr/TWAA9814701), Sep 10, 1998: BATTERY PACK. DISCHARGED. EGRESS LIGHTS WERE REPORTED AS FLASHING WITH SWITCH IN ARMED POSITION. REPLACED BATTERY PACK. CHECK-C 6-14-98 LAX. - [SDR TWAA9814304](https://openairdocs.org/sdr/TWAA9814304), Sep 6, 1998: CONNECTOR. LOOSE. FOUND EGRESS LIGHT STRIP INOPERATIVE IN AFT GALLEY AREA DURING MAINTENANCE TEST. FOUND LOOSE CONNECTION. RESEATED FLEX JUMPER TO POWER FLEX CABLE AND SECURED. C - [SDR TWAA9814303](https://openairdocs.org/sdr/TWAA9814303), Sep 6, 1998: POWER SUPPLY. INOPERATIVE. EGRESS LIGHT ON RT SIDE OF FWD CABIN ILLUMINATE INTERMITTENTLY. REPLACED EGRESS POWER SUPPLY. CHECK-C 6-14-98 LAX. - [SDR TWAA9807403](https://openairdocs.org/sdr/TWAA9807403), May 10, 1998: OVEN. WORN. JFK - FLT 842 - CREW REPORTED AN ELECTRICAL SMELL AND SMOKE FROM THE A3 GALLEY OVEN. CREW TURNED OFF THE OVEN. REPLACED OVEN. CHECK-C 3-18-98 LAX. (M) - [SDR TWAA9804203](https://openairdocs.org/sdr/TWAA9804203), Mar 18, 1998: STRINGER. CORRODED. LAX - DURING CHECK-C MAINTENANCE, FOUND CORROSION AT STRINGER 34L, FS 1275 IN AFT CARGO COMPARTMENT. REPAIRED STRINGER 34L PER SRM 53-30-03. (M) - [SDR TWAA9803706](https://openairdocs.org/sdr/TWAA9803706), Mar 13, 1998: SKIN. BULGED. LAX - DURING C-CHECK, FOUND FUSELAGE STRINGER 35L WITH A BULGE IN THE SKIN BETWEEN RIVETS, FUSELAGE STATION 1285. REMOVED FOREIGN OBJECT FROM BENEATH SKIN AND S - [SDR TWAA9804404](https://openairdocs.org/sdr/TWAA9804404), Mar 12, 1998: SKIN. DELAMINATED. LAX - DURING C-CHECK MAINTENANCE, ON TOP OF LEFT WING, TOP SURFACE OF LE BULL NOSE PANEL AFT OF NR 5 SLAT, OUTER SURFACE OF COMPOSIT MATERIAL WAS CRACKED IN TEN - [SDR TWAA9804014](https://openairdocs.org/sdr/TWAA9804014), Dec 9, 1997: SKIN. DELAMINATED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LEFT WING NR 5 LE SLAT DELAMINATED TOP SURFACE INBOARD END AT TE. REPAIRED PER SRM 57-43-02 FIG 201 DETAIL III ITEM - [SDR TWAA9711901](https://openairdocs.org/sdr/TWAA9711901), Sep 30, 1997: IDG. OVERSERVICED. STL - FLT 818 - DURING CLIMB, THE GENERATOR DRIVE WARNING LIGHT FLICKERED. IGD WAS NOT DISCONNECTED. REMOVED AND REPLACED THE IDG, MFG P/N 736664B LEAK CHECKED - [SDR 97ZZZX3593](https://openairdocs.org/sdr/97ZZZX3593), Jul 24, 1997: COMPRESSOR. STALLED. LAX - FLT 15 - DURING CLIMB, NR 1 ENGINE, S/N 4602, EXPERIENCED TWO COMPRESSOR STALLS. CHANGED NR 1 ENGINE. ENGINE TOTAL TIME: 46,477 HOURS; 11,789 CYCLES. CHEC - [SDR TWAA9771001](https://openairdocs.org/sdr/TWAA9771001), Jun 20, 1997: ENGINE. SURGED. DTW - FLT 720 - DURING CRUISE, RIGHT ENGINE SURGED WHILE IN TURBULENCE. INSPECTED INLET AND EXHAUST AND 3.5 BLEED VALVE. ALSO, CHECKED 5TH, 6TH, AND 7TH IVG UNI - [SDR 96ZZZM1356](https://openairdocs.org/sdr/96ZZZM1356), Aug 12, 1996: FAN. FAILED. BOS - DURING CLIMB, FORWARD EXHAUST COOLING FAN, MFG P/N 732591E, OVERHEATED AND EMITTED SMOKE ELECTRICAL ODOR TO FLIGHT DECK. TURNED OFF COOLING FAN. FOUND COO - [SDR 96ZZZX1201](https://openairdocs.org/sdr/96ZZZX1201), Feb 23, 1996: IND LIGHT SOCKET. BROKEN. MXP - FLT 843 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RT MLG DID NOT INDICATE DOWN AND LOCKED. CYCLED LANDING GEAR. FOUND RT MLG GREEN INDICATOR LIGHT - [SDR 95ZZZX877](https://openairdocs.org/sdr/95ZZZX877), Feb 9, 1995: A5 CARD. FAILED. LAX - FLT 721 - ON DESCENT WHEN LANDING GEAR WAS EXTENDED, RT MLG GREEN LIGHT DID NOT ILLUMINATE. CYCLED LANDING GEAR AND ALTERNATE LANDING GEAR EXTENSION. FOUN - [SDR 95ZZZX1396](https://openairdocs.org/sdr/95ZZZX1396), Feb 9, 1995: GEAR LIGHT. MALFUNCTIONED. LAX - FLT 721 - ON DESCENT WHEN LANDING GEAR WAS EXTENDED, RT MLG GREEN LIGHT DID NOT ILLUMINATE. CYCLED LANDING GEAR AND ALTERNATE LANDING GEAR EXTENSION. FOUN ## Other aircraft with N610TW - [Registered now](https://openairdocs.org/aircraft/N610TW): Douglas S Taylor RV-8, S/N 83466, built 2017 --- 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.