# N7263U: 1978 Boeing 727-222, registration cancelled 2006-06-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 28, 2006 - Status when cancelled: Valid registration - Airframe: [Boeing 727-222](https://openairdocs.org/model/boeing-727-222) (registry code 1384073) - Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 21410 - Year built: 1978 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: May 15, 1978 - Certificate issued: February 14, 2005 - Last registry action: February 14, 2005 - Mode S code: A9BCAA - Owner when cancelled: [Ljh Aviation Management Services Corp](https://openairdocs.org/faa-owner/LJH%20AVIATION%20MANAGEMENT%20SERVICES%20CORP) - Location: [Hot Springs, AR](https://openairdocs.org/faa-place/AR/Hot%20Springs) - Owner type: Corporation - Owner's area on the map: 34.5267° N, 92.9735° W: Placed by OpenAirDocs at the center of ZIP code 71901, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N7263U - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=7263U - Page: https://openairdocs.org/deregistered/N7263U-2006-06-28 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 (21) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2001UALA01444](https://openairdocs.org/sdr/2001UALA01444), Jul 20, 2001: COWLING. CRACKED. NR 2 ENGINE LOWER FORWARD COWLING MATING FLANGE, FOUND 3 CRACKS, ONE 8 INCHES LONG, THE OTHERS 3.5 INCHES LONG. ALSO, THERE IS A HOLE WORN THRU COWL MATING FLAN - [SDR 2001UALA01306](https://openairdocs.org/sdr/2001UALA01306), Jun 27, 2001: BATTERY. MISSING. THE R1DOOR EMERGENCY EXIT EXTERIOR LIGHT IS INOPERABLE. BATTERY ASSY IS MISSING. INSTALLED MISSING BATTERY ASSY. OPERATIONS CHECK NORMAL. - [SDR 2001UALA00188](https://openairdocs.org/sdr/2001UALA00188), Mar 3, 2001: WIRE. BROKEN. EMERGENCY EXIT SIGN IS LOOSE AND EEL LIGHTING IS INOPERABLE. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED CABLE ASSEMBLY INTERIM REPAIR PER MM 33-50-32. OPERATIONS CHE - [SDR 2000UALA00549](https://openairdocs.org/sdr/2000UALA00549), Sep 13, 2000: LEAD. FAILED. EEL STRIP BLINKING AT SEAT 27. *S/D* REPLACED POWER LEAD CABLE DUE TO ARCING AT STRIP CONNECTION. - [SDR 2000UALA00057](https://openairdocs.org/sdr/2000UALA00057), Feb 5, 2000: SHUTOFF VALVE. STUCK. UNABLE TO CONTROL CABIN PRESSURE ON CLIMBOUT OF DEN. RETURNED TO DEN. CORRECTED THE AIRCRAFT FROM 7762 TO 7763. *S/D* ENG 3 BLEED SHUT OFF VALVE STICKING. REPLA - [SDR 2000UALA00012](https://openairdocs.org/sdr/2000UALA00012), Jan 4, 2000: ELBOW. CRACKED. WITH FUEL PANEL CONFIGURED TO BURN OUT OF NR 2 TANK ONLY, 900 POUNDS OF FUEL WERE USED FROM TANK NR 3. ALL X-FEEDS WERE OPEN AND FORWARD PUMPS WERE OFF IN TANKS - [SDR 99UAL900544](https://openairdocs.org/sdr/99UAL900544), Oct 21, 1999: WIRE. BROKEN. EEL LIGHTING INOPERATIVE FROM ROWS 19 TO 26. *S/D* REPAIRED BROKEN WIRE TO BATTERY PACK AT SEAT 20, OPERATIONALLY CHECKED NORMAL. - [SDR 99UAL900350](https://openairdocs.org/sdr/99UAL900350), Jun 30, 1999: CONTROLLER. MALFUNCTIONED. OVER BVL, AIRCRAFT LOST CABIN PRESSURE. CABIN ALTITUDE CLIMBED ABOUT I000 FEET PER MINUTE TO FL 140. DESCENDED TO FL 140. FLIGHT DIVERTED TO SLC. *S/D* REPLACED - [SDR 98UAL900492](https://openairdocs.org/sdr/98UAL900492), Oct 5, 1998: WIRE. BROKEN. FORWARD ENTRY DOOR LOWER EMERGENCY EXIT SIGN INOP. REPLACED EEL CABLE, OPS CHECKS OK. - [SDR 97UAL900606](https://openairdocs.org/sdr/97UAL900606), Aug 6, 1997: FILLER CAP. LOOSE. NR 3 ENGINE OIL QUANTITY STARTED AT 3 GALLONS, ON TAKEOFF IT WENT DOWN TO 2.5. APPROXIMATELY 1 HOUR INTO THE FLIGHT THE QUANTITY WAS DOWN TO I.75 GALLONS. DIVER - [SDR 97UAL900245](https://openairdocs.org/sdr/97UAL900245), Mar 28, 1997: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHTING INOPERABLE FROM ROW 20 AFT. REPLACED INOP EMERGENCY EXIT LIGHTING. OPERATION CHECKS NORMAL. - [SDR 96UAL900795](https://openairdocs.org/sdr/96UAL900795), Nov 1, 1996: FUEL CONTL UNIT. MALFUNCTIONED. NR 1 ENGINE NOISY AND VIBRATION ON TAKEOFF. *S/D* LOW FREQUENCY VIBRATION CAUSED THE NOISE AND VIBRATION. THE FUEL CONTROL UNIT WAS REPLACED AND THERE HAS BEEN - [SDR 96UAL900815](https://openairdocs.org/sdr/96UAL900815), Oct 15, 1996: INFLATE TUBE. SEPARATED. DURING TIME CONTROLLED OVERHAUL, SLIDE SUFFERED SEAM SEPARATION OF THE INFLATION TUBE. SCRAPPED UNIT. - [SDR 96UAL900730](https://openairdocs.org/sdr/96UAL900730), Sep 21, 1996: RETRACT MECH. MALFUNCTIONED. ON TAXI IN, INBOARD TRAILING EDGE FLAPS DO NOT OPERATE HYDRAULICALLY, STUCK AT 25 DEGREES. FLAPS RETRACTED FROM 30 TO 25 ON LANDING ROLLOUT. - [SDR 96UAL900485](https://openairdocs.org/sdr/96UAL900485), Jun 25, 1996: FUEL VENT TUBE. BROKEN. WHILE CROSS-FEEDING ALL ENGINES FROM NUMBER 2 TANK NUMBER 3 FUEL QUANTITY DECREASED 700 LBS. *S/D* FUEL VENT TUBE ELBOW CRACKED AT FLANGE. REPLACED TUBE ELBOW, - [SDR 96UAL900221](https://openairdocs.org/sdr/96UAL900221), Mar 26, 1996: SKIN. CRACKED. AT APPROXIMATELY BODY STATION 943, STRINGER 18AL, A CRACK WAS FOUND IN THE 65-72702 FUSELAGE SKIN PANEL. REPAIRED THE SKIN PANEL PER THE 65C29069-7 REPAIR DRAWI - [SDR 96UAL900208](https://openairdocs.org/sdr/96UAL900208), Mar 21, 1996: STRINGER. CRACKED. AT APPROXIMATELY BODY STATION 943, STRINGER 18AL A CRACK WAS FOUND IN THE VERTICAL FLANGE OF THE 65-58488-25 STRINGER. REPAIRED STRINGER PER SPLICE REPAIR DRAWI - [SDR 95UAL900368](https://openairdocs.org/sdr/95UAL900368), Jan 3, 1996: BATTERY PACK. DISCHARGED. RAMP PERSONNEL NOTICED EXTERIOR EMERG LIGHTS ON INITIALLY AND THEN WENT OUT. FOUND BOTH ENTRY DOORS AND SERVICE DOORS SLIDE LIGHTS INOPERATIVE. USAIR BATTERY PA - [SDR 95UAL900207](https://openairdocs.org/sdr/95UAL900207), Oct 16, 1995: BATTERY PACK. DISCHARGED. FWD GALLEY DOOR EVACUATION SLIDE EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. - [SDR 95UAL900090](https://openairdocs.org/sdr/95UAL900090), Aug 15, 1995: PACKING. FAILED. LANDED LGA UNDER AMBER ALERT DUE TO LOSS OF A-SYSTEM HYDRAULIC. REPLACED ELEVATOR FEEL COMPUTER UNIT FILTER PACKING P/N NAS161216. - [SDR 95UAL900008](https://openairdocs.org/sdr/95UAL900008), Jun 19, 1995: EEL. INOPERATIVE. DOOR 1 LT AND RT EMERGENCY SLIDE LIGHT IS ON WITH EMERGENCY EXIT LIGHT SWITCH IN THE OFF POSITION. REPLACED EMERGENCY SLIDE LIGHT BATTERY AND POWER SUPPLY. --- 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.