# N7455U: 1979 Boeing 727-222, registration cancelled 2012-10-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 19, 2012 - Status when cancelled: Sale reported, pending cancellation - Airframe: [Boeing 727-222](https://openairdocs.org/model/boeing-727-222) (registry code 1384073) - Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs) - Serial number: 21909 - Year built: 1979 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: December 18, 1979 - Last registry action: January 18, 2006 - Mode S code: AA0837 - Location: [Sacramento, CA](https://openairdocs.org/faa-place/CA/Sacramento) - Owner type: Individual - Owner's area on the map: 38.5438° N, 121.3783° W: Placed by OpenAirDocs at the center of ZIP code 95826, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N7455U - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=7455U - Page: https://openairdocs.org/deregistered/N7455U-2012-10-19 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 727-222: https://openairdocs.org/model/boeing-727-222.md ## Service difficulty reports (22) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2002UALA01143](https://openairdocs.org/sdr/2002UALA01143), Jul 8, 2002: SKIN. DAMAGED. FORWARD LOWER FUSELAGE SKIN, BODY STATION 312-328, DRAIN HOLE AFT OF NOSE LANDING GEAR WHEEL WELL IS PUNCTURED AND BROKEN OUT. MAJOR REPAIR ACCOMPLISHED. DOUBLE - [SDR 2002UALA01118](https://openairdocs.org/sdr/2002UALA01118), Jul 2, 2002: STRINGER. CORRODED. FORWARD PIT STRINGER 27R CORRODED BEYOND LIMITS BODY STATION 630. MAJOR REPAIR ACCOMPLISHED. HAT SECTION REPAIR. - [SDR 2002UALA01117](https://openairdocs.org/sdr/2002UALA01117), Jul 2, 2002: STRINGER. CORRODED. FORWARD CARGO PIT AT BODY STATION 480, STRINGER 27L IS CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. STRINGER SPLICE REPAIR. - [SDR 2002UALA01101](https://openairdocs.org/sdr/2002UALA01101), Jun 28, 2002: SHEAR TIE. CORRODED. FORWARD CARGO PIT AT BODY STATION 480-500, STRINGER 28R, INTERCOSTAL LOWER FLANGE IS CORRODED AND SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED INTERC - [SDR 2002UALA01100](https://openairdocs.org/sdr/2002UALA01100), Jun 28, 2002: SKIN. CORRODED. FORWARD PIT INTERNAL SKIN STATION 500 AT STRINGER 28R IS BLENDED BEYOND LIMITS DUE TO CORROSION REMOVAL. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL DOUBLER R - [SDR 2002UALA01099](https://openairdocs.org/sdr/2002UALA01099), Jun 28, 2002: STRINGER. CORRODED. FORWARD PIT STRINGER 28R CORRODED ON LOWER SIDE AT BODY STATION 494. MAJOR REPAIR ACCOMPLISHED. SPLICE REPAIR. - [SDR 2002UALA01083](https://openairdocs.org/sdr/2002UALA01083), Jun 27, 2002: FRAME. CORRODED. AFT PIT FRAME AT BODY STATION 950F BETWEEN STRINGER 27L AND 28L, FRAME AND SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED SHEAR TIE. - [SDR 2002UALA01082](https://openairdocs.org/sdr/2002UALA01082), Jun 27, 2002: DOUBLER. DAMAGED. SLIGHT EDGE DAMAGE TO REPAIR DOUBLER FOUND UNDER AFT PIT BELOW LOADING THRESHOLD. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND QUADRUPLER. - [SDR 2001UALA00323](https://openairdocs.org/sdr/2001UALA00323), Mar 23, 2001: REGULATOR. FAILED. AT DEPARTURE TIME CREW LOST ALL OXYGEN PRESSURE TO ALL MASKS IN THE FLIGHT DECK. SUPPLEMENTAL DATA UPDATE FOUND THAT PRESSURE REDUCING REGULATOR WAS NOT LETTING - [SDR 2000UALA00222](https://openairdocs.org/sdr/2000UALA00222), Apr 29, 2000: VALVE. STUCK. NR 1 ENGINE OIL TEMPERATURE AT 135 TO 140 DEGREES FOR 13 MINUTES. WENT TO 150 DEGREES AT SHUT DOWN. WINDMILLED ENGINE FOR 25 MINUTES. RE-STARTED ENGINE ON FINAL - [SDR 98UAL900556](https://openairdocs.org/sdr/98UAL900556), Nov 22, 1998: COFFEEMAKER. DEFECTIVE. MINOR SMOKE IN AFT GALLEY. SUBMITTER STATES, SUSPECTED CAUSE WAS EITHER A LIGHT BULB OR A COFFEE MAKER. SUBSEQUENT INSPECTION SHOWED THAT THE COFFEE MAKER WAS D - [SDR 98UAL900502](https://openairdocs.org/sdr/98UAL900502), Oct 14, 1998: CONTROL MECH. MALFUNCTIONED. WHEN THE SPEED BRAKE IS DEPLOYED, AIRCRAFT BANKS TO THE LEFT EXCESSIVELY. AILERON TRIM SET AT 0. WHEN THE B-SYSTEM IS OFF, THE AIRCRAFT DOES NOT ROLL. - [SDR 98UAL900467](https://openairdocs.org/sdr/98UAL900467), Sep 22, 1998: DRIVE MOTOR. LEAKING. AFTER DEPARTURE LOST HYDRAULIC SYSTEM A PRESSURE. CONTINUED TO ORD AND WAS TOWED TO THE GATE. *S/D* REPLACED HYD FLAP DRIVE MOTOR AND NR 1 AND NR 2 ENGINE DRIVE - [SDR 97UAL900832](https://openairdocs.org/sdr/97UAL900832), Nov 17, 1997: PROX SENSOR. FAILED. AFTER TAKEOFF, INTERMITTENT AURAL WARNING HORN SOUNDED. TCAS FAILED AND BOTH TRANSPONDERS STOPPED WORKING. CABIN PRESSURE CONTROLLER WAS NOT CONTROLLING PRESSUR - [SDR 97UAL900532](https://openairdocs.org/sdr/97UAL900532), Jul 11, 1997: CONNECTOR. LEAKING. HAD A RIGHT STRUT OVERHEAT LIGHT ON CLIMBOUT. REDUCED POWER AND LIGHT WENT OUT. SLOWLY INCREASED BACK TO CLIMB POWER AND LIGHT REMAINED OUT. *S/D* FOUND SMALL I - [SDR 97UAL900424](https://openairdocs.org/sdr/97UAL900424), Jun 4, 1997: ACTUATOR. FAILED. STABILIZER MAIN ELECTRIC TRIM SLOW. CRUISE TRIM OK. FORWARD TRIM STALLS OUT, AFT TRIM OK. BRAKE ASSEMBLY SEEMS TO BE INOPERATIVE. COULD NOT MANUALLY CRANK STABI - [SDR 97UAL900302](https://openairdocs.org/sdr/97UAL900302), Apr 15, 1997: SEAL. WORN. SMOKE IN CABIN AT DISPATCH TIME APU LOAD CONTROL VALVE WOULD NOT OPEN AFTERWARDS. SUPPLEMENTAL DATA UPDATE, SEALS ON THE OIL BREATHER FITTING HAD WORN AND OIL W - [SDR 97UAL900293](https://openairdocs.org/sdr/97UAL900293), Apr 11, 1997: OIL SEAL. LEAKING. DISPATCH MECHANIC NOTED SMOKE COMING FROM APU IN THE RT WHEEL WELL AREA AROUND EXHAUST DUCT. SUPPLEMENTAL DATA UPDATE, THE CAUSE OF THE SMOKE WAS BELIEVED TO BE - [SDR 96UAL900923](https://openairdocs.org/sdr/96UAL900923), Dec 6, 1996: INFLATION TUBE. LEAKING. SLIDE REMOVED PER AIR CRUISERS SERVICE INFORMATION LETTER 25-98. DURING SHOP OVERHAUL A SEAM LEAK DEVELOPED ON THE INFLATION TUBE. SCRAPPED SLIDE. - [SDR 96UAL900325](https://openairdocs.org/sdr/96UAL900325), May 7, 1996: INPUT ROD. OUT OF ADJUST. EN ROUTE, STABILIZER STUCK IN NOSEDOWN POSITION. LANDED DEN UNDER AMBER ALERT. *S/D* STABILIZER BRAKE UNDER COCKPIT FLOOR WAS NOT COMPLETELY DISENGAGING. ADJUST - [SDR 95UAL900319](https://openairdocs.org/sdr/95UAL900319), Dec 15, 1995: RETRACT MECH. MALFUNCTIONED. NR 5 L.E. FLAP WOULD NOT RETRACT WHEN FLAPS RETRACTED FROM 2 DEGREES TO ZERO DEGREES. RETURNED TO ORD. - [SDR 95UAL900106](https://openairdocs.org/sdr/95UAL900106), Aug 23, 1995: LIGHT. INOP. EMERGENCY EXIT LIGHT INOP AT AIRSTAIRS DOOR. REPLACED LIGHT AND POWER CABLE ASSEMBLY, CHECKS OK. ## FAA accident and incident reports (1) 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 19801227089349I](https://openairdocs.org/incident/19801227089349I), Dec 27, 1980: Boeing 727222 (N7455U), Las Vegas, NV, Minor damage. Crew advised to hold after landing on arrival pad. While taxiing into position elevator of craft struck light pole. --- 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.