# N6819: 1979 Boeing 727-223, registration cancelled 2003-07-11 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 11, 2003 - Exported to: Sri Lanka - Status when cancelled: Triennial form not returned - Airframe: [Boeing 727-223](https://openairdocs.org/model/boeing-727-223) (registry code 1384074) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs) - Serial number: 19494 - Year built: 1979 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: February 18, 2000 - Certificate issued: December 3, 1997 - Last registry action: December 19, 2000 - Mode S code: A90A81 - Owner when cancelled: [Prewitt Leasing Inc](https://openairdocs.org/faa-owner/PREWITT%20LEASING%20INC) - Location: [Bedford, TX](https://openairdocs.org/faa-place/TX/Bedford) - Owner type: Corporation - Owner's area on the map: 32.8530° N, 97.1304° W: Placed by OpenAirDocs at the center of ZIP code 76021, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N6819 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=6819 - Page: https://openairdocs.org/deregistered/N6819-2003-07-11 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 727-223: https://openairdocs.org/model/boeing-727-223.md ## Service difficulty reports (39) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR EISA20010127](https://openairdocs.org/sdr/EISA20010127), Oct 16, 2001: THROTTLE CABLE. DISCONNECTED. EN ROUTE NR 3 ENGINE WENT TO MAX POWER. RETARDING THROTTLE HAD NO EFFECT. SHUT DOWN ENGINE. AFTER 20 MINUTES, MOVED START LEVER TO IDLE FOR 3 MINUTES TO PURGE F - [SDR EISA20010092](https://openairdocs.org/sdr/EISA20010092), May 30, 2001: PITOT TUBE. CLOGGED. ABORTED TAKEOFF DUE TO FIRST OFFICERS AIRSPEED IND INOP. USED NORMAL BRAKING DUE TO LOW SPEED ABORT. CORRECTIVE ACTION: FOUND F/O'S PITOT TUBE BLOCKED. CLEANED - [SDR EISA20010081](https://openairdocs.org/sdr/EISA20010081), Apr 27, 2001: SKIN. DAMAGED. WHILE AIRCRAFT WAS PARKED, AIRBOURNE EXPRESS VAN STRUCK AIRCRAFT RIGHT WING TIP FROM BEHIND. RIGHT WING TIP TOP AND BOTTOM SKIN DAMAGED.CORRECTIVE ACTION: CUT O - [SDR EISA20010080](https://openairdocs.org/sdr/EISA20010080), Apr 27, 2001: CHANNEL. DAMAGED. WHILE AIRCRAFT WAS PARKED, AIRBOURNE EXPRESS VAN STRUCK, AIRCRAFT FROM BEHIND ON RIGHT WING, RIGHT WING TIP CHANNEL IS DAMAGED. CORRECTIVE ACTION: REMOVED AND R - [SDR EISA20010079](https://openairdocs.org/sdr/EISA20010079), Apr 27, 2001: RIB. DAMAGED. WHILE AIRCRAFT WAS PARKED, AIRBOURNE EXPRESS VAN STRUCK AIRCRAFT FROM BEHIND ON RIGHT WING. RIGHT WING TIP OUTBOARD RIB DAMAGED. CORRECTIVE ACTION: REMOVED DAMA - [SDR EISA20010078](https://openairdocs.org/sdr/EISA20010078), Apr 27, 2001: RIB. DAMAGED. WHILE AICRAFT WAS PARKED, AIRBOURNE EXPRESS VAN STRUCK WING FROM BEHIND.DAMAGED #2 RIB FROM OUTBOARD RIGHT WING TIP. CORRECTIVE ACTION: REMOVED AND REPLACED RIG - [SDR EISA20010068](https://openairdocs.org/sdr/EISA20010068), Mar 15, 2001: SWITCH. FAULTY. DURING CRUISE AT FL 310, NR 2 ENGINE OIL FILTER BYPASS LIGHT ON F/E PANEL ILLUMINATED. PERFORMED APPROPRIATE CHECKLIST NR 2 ENGINE SHUT DOWN. REMOVED AND REPLAC - [SDR EISA20010030](https://openairdocs.org/sdr/EISA20010030), Feb 23, 2001: ACTUATOR. MALFUNCTIONED. ON DEPARTURE WHEN RETRACTING FLAPS FROM 5 TO 2 DEGREES NR 8 SLAT WAS STUCK, IN THE EXTEND POSITION. AMBER L/E FLAP LIGHT ILLUMINATED AND NR 8 SLAT ILLUMINATED. - [SDR EISA2000040](https://openairdocs.org/sdr/EISA2000040), Mar 27, 2000: DRIVE GEAR. LEAKING. FOUND LOSS OF A SYSTEM HYDRAULIC POWER. EMERGENCY DECLARED LANDING OK. TAXI OK. TOWED TO BLOCKS. FOUND OUTBOARD FLAP HYDRAULIC DRIVE MOTOR LEAKING. REMOVED AND - [SDR EISA2000018](https://openairdocs.org/sdr/EISA2000018), Feb 18, 2000: WARNING LIGHT. ILLUMINATED. ON TAKEOFF, NR 1 LEADING EDGE FLAP UNSAFE LIGHT ILLUMINATED. AIR TURN BACK TO (OVL). (M) - [SDR EISA99210](https://openairdocs.org/sdr/EISA99210), Oct 28, 1999: AILERON. DAMAGED. AIRCRAFT HAS VIBRATION IN FLIGHT. REMOVED AND REPLACED LEFT OUTBOARD AILERON IAW MM REF 27-10, FUNCTIONAL CHECK GOOD. (M) - [SDR EISA99169](https://openairdocs.org/sdr/EISA99169), Sep 10, 1999: BATTERY. OVERHEATED. FOUR MINUTES AFTER APU CONNECTED, SMOKE IN COCKPIT. CREW SHUTDOWN ALL POWER AND FIRE DEPARTMENT REMOVED SMOKING BATTERY. REMOVED AND REPLACED BATTERY IAW MM 24- - [SDR EISA99165](https://openairdocs.org/sdr/EISA99165), Sep 10, 1999: BATTERY. OVERHEATED. FOUR MINUTES AFTER APU CONNECTED, SMOKE IN COCKPIT. CREW SHUT DOWN ALL POWER. FIRE DEPARTMENT REMOVED SMOKING BATTERY. REMOVED AND REPLACED BATTERY. (M) - [SDR EISA99133](https://openairdocs.org/sdr/EISA99133), Jul 13, 1999: BOLT. MISSING. NR 1 T/R LIGHT ON IN FLIGHT AIR ABORT, RETURN TO BRU. TROUBLE SHOT, FOUND BOLT ON SWITCH MISSING. INSTALLED BOLT. OPS CHECK GOOD. (M) - [SDR EISA99144](https://openairdocs.org/sdr/EISA99144), May 16, 1999: DUCT. FAILED. DURING PREFLIGHT, SMOKE IN COCKPIT COOLING DUCT COLLAPSED CAUSING NR 1 TRANSFORMER TO OVERHEAT. REPLACED NR 1 T/R. (M) - [SDR EISA99120](https://openairdocs.org/sdr/EISA99120), May 14, 1999: CIRCUIT BREAKER. FAILED. ON APPROACH, SMELLED SMOKE NOTICED NR 1 AFT AND NR 2 RT FORWARD CIRCUIT BREAKERS TRIPPED. VISUAL SMOKE NOTICED ON TAXI IN. INSPECTED ELECTRICAL SYSTEM FOR HEAT - [SDR EISA99057](https://openairdocs.org/sdr/EISA99057), Mar 14, 1999: SWITCH. OUT OF ADJUST. NR 1 REVERSER LIGHT CAME ON WHEN THROTTLES ADVANCED. ADJUSTED SWITCH FOR NR 1 THRUST REVERSER OPERATING LIGHT PER MM 79-30. RAN NR 1 ENGINE AND FUNCTION CHECKED - [SDR EISA98253](https://openairdocs.org/sdr/EISA98253), Nov 18, 1998: WIRE. BROKEN. MAIN CARGO DOOR LIGHT ILLUMINATED DURING FLIGHT, WITH A POSSIBLE PRESSURE LOSS, RESULTING IN AN AIR TURN BACK TO EDI. FOUND BROKEN WIRE REPAIRED IAW MM CHAPTER - [SDR EISA98054](https://openairdocs.org/sdr/EISA98054), Feb 18, 1998: HINGE. BROKEN. DURING D-CHECK INSPECTION, REMOVED RIGHT OUTBOARD OUTBOARD AILERON TAB TO FOM AND FOUND NR 3 HINGE BROKEN. REMOVED AND REPLACED NR 3 HINGE. REINSTALLED AILERON - [SDR EISA98053](https://openairdocs.org/sdr/EISA98053), Feb 18, 1998: FRAME. CRACKED. FOUND DURING CARGO MOD, DURING D-CHECK INSPECTION, FOUND CRACK IN FRAME AT FS 700, AT STRINGER 20L-21L. FABRICATED AND INSTALLED DOUBLER PER SRM 53-10-04. (M) - [SDR EISA98051](https://openairdocs.org/sdr/EISA98051), Feb 18, 1998: FLOOR PAN. CORRODED. FOUND DURING CARGO COMPT MOD, DURING D-CHECK INSPECTION, FOUND CORROSION ON FLOOR PAN AT FS 1178 LT SIDE. CUT OUT DAMAGE. FABRICATED AND INSTALLED DOUBLER PER S - [SDR EISA98050](https://openairdocs.org/sdr/EISA98050), Feb 18, 1998: INTERCOSTAL. CRACKED. DURING D-CHECK INSPECTION, FOUND INTERCOSTAL CRACKED AT FS 720F-740 AFT END, LEFT SIDE. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER SRM 57-40-03. ( - [SDR EISA98049](https://openairdocs.org/sdr/EISA98049), Feb 18, 1998: RIB. CRACKED. DURING D-CHECK INSPECTION, FOUND 3 CRACKS IN WING RIB AT RT WING STATION 171, TOP SIDE OF RIB. REMOVED STIFFENER, FABRICATED ANGLES OF 7075-0 AND HEAT TREATED T - [SDR EISA98048](https://openairdocs.org/sdr/EISA98048), Feb 18, 1998: STRINGER. CRACKED. DURING D-CHECK INSPECTION, FOUND .25 INCH CRACK ON STRINGER 6L AT FS 303.9. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER PER SRM 53-30-01. (M) - [SDR EISA98047](https://openairdocs.org/sdr/EISA98047), Feb 18, 1998: RIB. CRACKED. DURING D-CHECK INSPECTION, FOUND LEFT WING RIB CRACKED AT TOP OF RIB, WS 171 AS MARKED. REMOVED STIFFENER, FABRICATED ANGLES OF 7075-0 AND HEAT TREATED TO 7075- - [SDR EISA98046](https://openairdocs.org/sdr/EISA98046), Feb 18, 1998: ANGLE. CRACKED. DURING D-CHECK INSPECTION, FOUND ANGLE CRACKED IN E/E BAY, FS 303, LBL 10. REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE PER SRM 51-40-03 AND INSTALLED PER SRM 51 - [SDR EISA98045](https://openairdocs.org/sdr/EISA98045), Feb 18, 1998: STIFFENER. CRACKED. DURING D-CHECK INSPECTION, FOUND STIFFENER CRACKED IN E/E BAY, FS 312, LBL 32, WL 208. REMOVED STIFFENER AND FABRICATED NEW PART PER SRM 51-40-03, INSTALLED SRM - [SDR EISA98044](https://openairdocs.org/sdr/EISA98044), Feb 18, 1998: INTERCOSTAL. CRACKED. DURING D-CHECK INSPECTION, FOUND INTERCOSTAL CRACKED IN 5 PLACES AT FS 720-720A. REMOVED ANGLE, FABRICATED NEW ANGLE PER SRM 51-40-03 AND INSTALLED PER SRM 53-1 - [SDR EISA98043](https://openairdocs.org/sdr/EISA98043), Feb 18, 1998: WEB. CRACKED. DURING D-CHECK INSPECTION, FOUND 2.5 INCH CRACK IN FORWARD CARGO DOOR WEB AT FS 575, BOTTOM AFT, LOWER SIDE OF DOOR. STOPPED DRILLED CRACK, FABRICATED AND INSTA - [SDR EISA98042](https://openairdocs.org/sdr/EISA98042), Feb 18, 1998: ANGLE. CRACKED. DURING D-CHECK INSPECTION, X-RAY OF LEFT ELEVATOR REVEALED ANGLE MATERIAL MISSING AND 1.5 INCH CRACK AS SHOWN IN SHOTS NR 1 AND NR 2. PULLED BACK SKIN TO ACCESS - [SDR EISA98041](https://openairdocs.org/sdr/EISA98041), Feb 16, 1998: TAB. MOISTURE. DURING D-CHECK, X-RAY INSPECTION OF RUDDER MOISTURE IN HONEYCOMB AS SHOWN IN SHOTS NR 5C, 9C AND 9D. CUT OUT PORTION OF RUDDER TAB TO REMOVE WATER. REMOVED WATE - [SDR AALA970845](https://openairdocs.org/sdr/AALA970845), May 3, 1997: RETRACT MECH. MALFUNCTIONED. DFW - FLT 1125 - AFTER TAKEOFF PHL AFTER LANDING GEAR RETRACTED, RED DOOR LGIHT AND AMBER RIGHT MAIN LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED WITH GEAR LEVE - [SDR AALA970358](https://openairdocs.org/sdr/AALA970358), Feb 18, 1997: FRAME. CRACKED. TUL - FOUND CRACK IN FRAME AT STATION 804, OUTBOARD OF RIGHT OUTBOARD SEAT TRACK AND INBOARD OF CONDUIT CRACK FROM CONDUIT PASS THROUGH AT 10 O'CLOCK POSITION A - [SDR AALA961246](https://openairdocs.org/sdr/AALA961246), Aug 22, 1996: LIGHT. INOPERATIVE. DFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT FLOOR PATH LIGHT AT ROWS 3 INOPERATIVE. REPAIRED LIGHT STRIP AT ROW 3. SYSTEM GROUND CHECKED NORMAL OPE - [SDR AALA961245](https://openairdocs.org/sdr/AALA961245), Aug 22, 1996: CONNECTOR. INOPERATIVE. DFW - DURING OVERNIGHT MAINTENANCE, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS AT ROWS 27 AND 28 INOPERATIVE. REPAIRED CONNECTOR AT ROW 27. SYSTEM GROUND CHECKE - [SDR AALA960423](https://openairdocs.org/sdr/AALA960423), Mar 20, 1996: CONNECTOR. LOOSE. DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS AT ROWS 26 AND 27 INOPERATIVE. RECONNECTED LOOSE CONNECTOR AT EMERGENCY EXIT FLOOR PATH - [SDR AALA960097](https://openairdocs.org/sdr/AALA960097), Jan 22, 1996: RIB. CRACKED. TULE - FOUND CRACK IN RADIUS OF LOWER RIB CHORD WING STATION 738.5 RIGHT WING (FWD CHORD) IN FUEL TANK. STOP DRILLED BOTH ENDS OF CRACK, NDT CHECKED BOTH STOP D - [SDR AALA960096](https://openairdocs.org/sdr/AALA960096), Jan 22, 1996: RIB. CRACKED. TULE - FOUND LOWER RIB CHORD CRACKED AT STRINGER 5 AT STATION 601.5 INSIDE RIGHT WING FUEL TANK. REMOVED RIB AND INSTALLED NEW BUILT UP RIB PER SB 727-57-0127 F - [SDR AALA960095](https://openairdocs.org/sdr/AALA960095), Jan 22, 1996: STRINGER. CRACKED. TULE - FOUND NR 2 STRINGER AFT RIB ATTACH ANGLE (STRINGER NR 13) STATION WS 629 CRACKED. REPAIRED STRINGER PER SB 727-57A159. (M) ## NTSB investigations (1) 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 MIA87IA068](https://openairdocs.org/ntsb/MIA87IA068), Jan 6, 1987: Boeing 727-223 (N6819), Tampa, FL, incident, minor damage ## 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 19950926034329I](https://openairdocs.org/incident/19950926034329I), Sep 26, 1995: Boeing 727223 (N6819), Memphis, TN. En route fuel quanity rapid decrease. Diverted to mem. Fuel quanity indicator defective. - [Incident 19870106005649I](https://openairdocs.org/incident/19870106005649I), Jan 6, 1987: Boeing 727223 (N6819), Tampa, FL. The airliner landed safely on one engine. One engine had a broken oil line, another, a clogged oil filter. - [Incident 19850613035559I](https://openairdocs.org/incident/19850613035559I), Jun 13, 1985: Boeing 727 (N6819), Boston, MA. Priority landing due to ill passenger. Aircraft also had a mechanical problem with pressurization system. - [Incident 19801013074109I](https://openairdocs.org/incident/19801013074109I), Oct 13, 1980: Boeing 727223 (N6819), Chicago, IL. Before takeoff pilot requested permission to clear runway due to a hydraulic problem. Crew fixed it and departed. ## Other aircraft with N6819 - [Cancelled 1932-11-01](https://openairdocs.org/deregistered/N6819-1932-11-01): Waco GXE, S/N 1663. Owner: [Dunbar Henry S](https://openairdocs.org/faa-owner/DUNBAR%20HENRY%20S), [Oshkosh, WI](https://openairdocs.org/faa-place/WI/Oshkosh) --- 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.