# N6826: 1969 Boeing 727-223, registration cancelled 2009-08-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 3, 2009 - Status when cancelled: Valid registration - Airframe: [Boeing 727-223](https://openairdocs.org/model/boeing-727-223) (registry code 1384074) - Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 19704 - Year built: 1969 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: February 12, 1969 - Certificate issued: May 21, 2004 - Last registry action: November 6, 2007 - Mode S code: A90DCF - Owner when cancelled: [Aircorp Inc](https://openairdocs.org/faa-owner/AIRCORP%20INC) - Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas) - Owner type: Corporation - Owner's area on the map: 32.8483° N, 96.8255° W: Placed by OpenAirDocs at the center of ZIP code 75209, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N6826 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=6826 - Page: https://openairdocs.org/deregistered/N6826-2009-08-03 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 (35) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR EISA20000201](https://openairdocs.org/sdr/EISA20000201), Nov 7, 2000: MODULE. FAILED. ON ASCENT FLAPS AT 2 DEGREES, FORWARD LEADING EDGE AMBER LIGHT ILLUMINATED, F/E PANEL GREEN LIGHTS. EXTENDED AND RETRACTED FLAPS SEVERAL TIMES, ALL INDICATIONS - [SDR EISA99140](https://openairdocs.org/sdr/EISA99140), Jun 25, 1999: CONNECTOR. DIRTY. UPON GEAR EXTENSION THE RIGHT MAIN GEAR (RED) WARNING LIGHT ILLUMINATED. PERFORMED ABNORMALS SECTION 3 PAGE 50 PROCEDURE UNEVENTFUL LANDING. CLEANED AND REPOSIT - [SDR EISA98136](https://openairdocs.org/sdr/EISA98136), Jun 18, 1998: ACTUATOR. FAILED. ON TAKEOFF FROM BRUSSELS (BRU), A-SYSTEM HYDRAULIC QUANTITY WENT TO 2.0 GALLONS AND LOW LEVEL LIGHT ILLUMINATED. RETURNED FOR LANDING TO (BRU). GENERATED FROM P - [SDR EISA98135](https://openairdocs.org/sdr/EISA98135), Jun 12, 1998: MOISTURE TRAP. CONTAMINATED. AIRBORNE RETURN TO SOUTHEND, ENGLAND (SNN), DUE TO FLUCTUATIONS ON ENGINE VALUES, NR 1 EPR, NR 1 N1, AND NR 1 N2, NR 1 FUEL FLOW. PILOT REPORT. CARRIED OUT T/S - [SDR EISA98105](https://openairdocs.org/sdr/EISA98105), May 13, 1998: FITTING BOSS. STRIPPED. IN-FLIGHT, NR 1 LOW OIL PRESSURE LIGHT ILLUMINATED, NR 1 OIL PRESSURE GAUGE READ JUST ABOVE LOWER RED RADIAL. OIL QUANTITY READ ZERO. PRECAUTIONARY SHUT DOWN OF - [SDR EISA98038](https://openairdocs.org/sdr/EISA98038), Feb 9, 1998: GUIDE. CHIPPED. DURING C-CHECK, FOUND NR 2 SLAT GUIDE CHIPPED AT WS 620 LT TOP OF FLAT TRAILING EDGE. INSTALLED SLAT TRAILING EDGE DOUBLER PER SRM 57-50-03. (M) - [SDR EISA98037](https://openairdocs.org/sdr/EISA98037), Feb 9, 1998: S-DUCT. TORN. DURING C-CHECK, FOUND NR 2 ENGINE INTAKE 12 O'CLOCK POSITION HAS A TEAR IN SKIN AT OPENING NEXT TO ENGINE RING FLANGE. REMOVED DAMAGED AREA, FABRICATED REPAIR F - [SDR EISA98036](https://openairdocs.org/sdr/EISA98036), Feb 9, 1998: SKIN. DELAMINATED. DURING C-CHECK, FOUND TORN AND DELAMINATED LEFT INBOARD AFT FLAP TRAILING EDGE. REPAIR DELAMINATION ON LEFT INBOARD AFT FLAP BY INJECTION METHOD PR SRM 51-40-06 - [SDR EISA98035](https://openairdocs.org/sdr/EISA98035), Feb 9, 1998: ANGLE. CRACKED. DURING C-CHECK, FOUND 50 INCH CRACK IN SUPPORT ANGLE FOR LEFT MAIN GEAR DOOR UPSTOP, FS 850. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER SRM 51-30- - [SDR EISA98034](https://openairdocs.org/sdr/EISA98034), Feb 9, 1998: SKIN. DELAMINATED. DURING C-CHECK, FOUND RT INBOARD AFT FLAP DELAMINATED TRAILING EDGE. REPAIR DELAMINATION BY INJECTION METHOD PER SRM 51-40-06. (M) - [SDR EISA98033](https://openairdocs.org/sdr/EISA98033), Feb 9, 1998: SKIN. CRACKED. DURING C-CHECK, FOUND LEFT INBOARD AFT FLAP BOTTOM SKIN WITH CRACKS AND DENTS IN AREA 18 INCHES BY 24 INCHES. ACCOMPLISHED POTTING REPAIR PER SRM 51-40-06 AND I - [SDR EISA98032](https://openairdocs.org/sdr/EISA98032), Feb 9, 1998: SKIN. CRACKED. DURIGN C-CHECK, FOUND RT INBOARD AFT FLAP BOTTOM SKIN WITH CRACKS AND DENTS IN AREA 18 INCHES BY 24 INCHES. ACCOMPLISHED POTTING REPAIR PER SRM 51-40-06 AND INS - [SDR EISA98031](https://openairdocs.org/sdr/EISA98031), Feb 9, 1998: SKIN. HOLE. DURING C-CHECK, FOUND CRACK AND HOLE, RT INBOARD AFT FLAP. REPAIRED HOLE WITH POTTING REPAIR PER SRM 51-40-06 FIBERGLASS OVERLAY APPLIED PER SRM 51-40-08. (M) - [SDR EISA98030](https://openairdocs.org/sdr/EISA98030), Feb 9, 1998: SEAT TRACK. CORRODED. DURING C-CHECK, FOUND CORROSION ON SEAT TRACK, LEFT SIDE FROM FS 750 TO 950E ON MAIN CARGO DECK. REMOVED TRACK AND INSTALLED NEW SEAT TRACK IAW SRM 53-10-05. (M - [SDR EISA98029](https://openairdocs.org/sdr/EISA98029), Feb 9, 1998: ANGLE. CORROSION. DURING C-CHECK, FOUND FS 178 BULKHEAD, FIRST ANGLE FROM BOTTOM HAS CORROSION. REMOVED ANGLE, FABRICATED ANGLE FROM 7075-T6 AND INSTALLED PER SRM 51-10-1. (M) - [SDR EISA98028](https://openairdocs.org/sdr/EISA98028), Feb 9, 1998: SKIN. DELAMINATED. DURING C-CHECK, FOUND LEFT INBOARD AFT FLAP DELAMINATED AT TRAILING EDGE. REPAIRED DELAMINATION BY INJECTION METHOD PER SRM 51-40-06. (M) - [SDR EISA98027](https://openairdocs.org/sdr/EISA98027), Feb 9, 1998: SKIN. DAMAGED. DURING C-CHECK, FOUND LEFT INBOARD AFT FLAP HAS HOLE AND DENT ON BOTTOM SKIN. REPAIRED HOLE AND DENT IN BOTTOM SKIN WITH POTTING REPAIR PER SRM 51-40-06 AND MAD - [SDR EISA98026](https://openairdocs.org/sdr/EISA98026), Feb 9, 1998: SKIN. DELAMINATED. DURING C-CHECK, FOUND TRAILING EDGE DELAMINATION ON LEFT INBOARD AFT FLAP. REPAIRED DELAMINATION WITH FIBERGLASS OVERLAY PER SRM 51-40-08. (M) - [SDR EISA98025](https://openairdocs.org/sdr/EISA98025), Feb 9, 1998: SKIN. DELAMINATED. DURING C-CHECK, FOUND INBOARD FLAP, AFT FLAP TRAILING EDGE DELAMINATED. REPAIRED DELAMINATION ON TRAILING EDGE WITH FIBERGLASS OVERLAY PER SRM 51-40-08. (M) - [SDR EISA98024](https://openairdocs.org/sdr/EISA98024), Feb 9, 1998: SEAT TRACK. CORRODED. DURING C-CHECK, FOUND CORROSION ON FLOORBEAM AND SEAT TRACK AT FS 560-580. SURFACE CORROSION REMOVED ON FLOORBEAM. FOUND IN LIMITS PER SRM 53-10-1. INSTALLED NE - [SDR EISA98023](https://openairdocs.org/sdr/EISA98023), Feb 9, 1998: SEAT TRACK. CORRODED. DURING C-CHECK, FOUND FS 580 RT AND 620 CORROSION ON CENTER BEAM AND SIDE OF SEAT TRACK. REMOVED SURFACE CORROSION ON FLOORBEAM AND FOUND TO BE IN LIMITS. REMOV - [SDR EISA98022](https://openairdocs.org/sdr/EISA98022), Feb 9, 1998: DOUBLER. CORRODED. DURING C-CHECK, FOUND CORROSION ON COCKPIT SHEER DOUBLER JUST BELOW PILOTS WINDOW FS 253 LT. REMOVED CORROSION, FABRICATED DOUBLER AND INSTALLED DOUBLER PER SRM - [SDR EISA98021](https://openairdocs.org/sdr/EISA98021), Feb 9, 1998: VENT BOX. CRACKED. DURING C-CHECK, FOUND WING STATION 171.5 RT WING, FUEL VENT BOX HAS CRACKED FLANGE AT UPPER CHORD. FABRICATED REPAIR PARTS PER SRM 57-10-4 AND INSTALLED REPAIR - [SDR EISA98020](https://openairdocs.org/sdr/EISA98020), Feb 9, 1998: FUEL TANK. LEAK. DURING C-CHECK, FUOND FUEL LEAK NR 3 SLAT ACTUATOR CAN ON RT WING. REMOVED OLD SEALER AND RESEALED AT LEAK SOURCE PER 727 MM 28-11-0, PAGE 801. (M) - [SDR EISA98019](https://openairdocs.org/sdr/EISA98019), Feb 9, 1998: STRINGER. CRACKED. DURING C-CHECK, FOUND LEFT WING STATION 629, CRACK ON UPPER STRINGER ATTACHMENT TO RIB, 7TH FROM FWD SPAR. DRILLED REPAIR ANGLES AND RADIUS BLOCKS AND INSTALLED - [SDR EISA98018](https://openairdocs.org/sdr/EISA98018), Feb 9, 1998: STRINGER. CRACKED. DURING C-CHECK, FOUND LEFT WING STATION 519, 10TH STRINGER AFT OF FRONT SPAR HAS CRACK AT STRINGER TO RIB ATTACHMENT (UPPER STRINGER). DRILLED REPAIR ANGLES AND - [SDR EISA98017](https://openairdocs.org/sdr/EISA98017), Feb 9, 1998: SKIN. CRACKED. DURING C-CHECK, FOUND RIGHT ELEVATOR HAS CRACK AND HOLE IN BOTTOM SKIN, OUTBOARD END. FABRICATED DOUBLER PER SRM 55-20-03. (M) - [SDR EISA98016](https://openairdocs.org/sdr/EISA98016), Feb 9, 1998: ANGLE. CRACKED. DURING C-CHECK, FOUND X-RAY INSPECTION OF RT ELEVATOR SHOWS A CRACK INDICATION AS SHOWN IN SHOTS R7, R1 AND R4. REMOVED ANGLE, FABRICATED NEW ANGLE AND INSTALLE - [SDR EISA98015](https://openairdocs.org/sdr/EISA98015), Feb 9, 1998: GUSSET. CRACKED. DURING C-CHECK, FOUND FS 356, STRINGER 17L, GUSSET AND STRINGER CRACKED AT WIRE BUNDLE. FABRICATED PART PER SAMPLE AND INSTALLED PER SRM 51-40-2. (M) - [SDR EISA98014](https://openairdocs.org/sdr/EISA98014), Feb 9, 1998: FRAME. CRACKED. DURING C-CHECK, FOUND FS 360, STRINGER 17L FRAME CRACKED AND BROKEN. FABRICATED DOUBLER AND INSTALLED PER SRM 53-10-4. (M) - [SDR EISA97208](https://openairdocs.org/sdr/EISA97208), Oct 10, 1997: HYD PUMP. LEAKING. LOSS OF A-SYSTEM HYDRAULICS DURING CLIMB-OUT. REMOVED AND REPLACED NR 2 ENGINE PUMP. CHKS GOOD IAW MM. (X) - [SDR EISA97079](https://openairdocs.org/sdr/EISA97079), Apr 4, 1997: DOOR. DAMAGED. ON POST FLIGHT INSPECTION, FOUND DAMAGED RIGHT MAIN GEAR DOOR (WING DOOR). (M) - [SDR EISA97035](https://openairdocs.org/sdr/EISA97035), Mar 2, 1997: AOA VANE. INOP. STICK SHAKER ACTIVATED ON TAKEOFF FROM CPH (ATB). REPLACED AOA VANE. (M) - [SDR EISA97034](https://openairdocs.org/sdr/EISA97034), Mar 2, 1997: CONNECTORS. DIRTY. STICK SHAKER ACTIVATED ON TAKEOFF FROM CPH (ATB). PULLED LANDING GEAR ACCY BOX C/B'S. REMOVED L/G ACCY BOX CLEANED CONNECTORS. REINSTALLED L/B ACCY BOX, OPS CHE - [SDR EISA97033](https://openairdocs.org/sdr/EISA97033), Feb 28, 1997: LANDING ACCY BOX. FAILED. ON TAKEOFF ROTATION FROM BRU, STICK SHAKER ACTIVATED AND REMAINED ON UNTIL LANDING AT BRU (ATB). REPLACED LANDING GEAR ACCY UNIT, OPS CHECK OK PR MM 34 AND 32. ## FAA accident and incident reports (3) 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 19820713036899I](https://openairdocs.org/incident/19820713036899I), Jul 13, 1982: Boeing 727223 (N6826), Indianapolis, IN. Pilot returned to airport due to severe vibration and loss of epr on engine. All turbine blades damaged. - [Incident 19810921090209I](https://openairdocs.org/incident/19810921090209I), Sep 21, 1981: Boeing 727223 (N6826), Indianapolis, IN. En route lost a hydraulic system. Landed ok. Found firewall shutoff valve failed. Replaced. - [Incident 19780926028529I](https://openairdocs.org/incident/19780926028529I), Sep 26, 1978: Boeing 727223 (N6826), Boston, MA. Aircraft returned to airport with engine shutdown. Cracked seal in oil filter cap. ## Other aircraft with N6826 - [Cancelled 1929-07-25](https://openairdocs.org/deregistered/N6826-1929-07-25): Waco 10, S/N 1638. Owner: [Mosinee Airport Co](https://openairdocs.org/faa-owner/MOSINEE%20AIRPORT%20CO), [Mosinee, WI](https://openairdocs.org/faa-place/WI/Mosinee) --- 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.