# N6827: 1969 Boeing 727-223, registration cancelled 2011-09-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 26, 2011 - 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-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: 20180 - Year built: 1969 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 14, 1969 - Certificate issued: July 25, 2002 - Last registry action: April 21, 2009 - Mode S code: A90DF2 - Owner when cancelled: [Kitty Hawk Collateral Liquidating Trust](https://openairdocs.org/faa-owner/KITTY%20HAWK%20COLLATERAL%20LIQUIDATING%20TRUST) - Location: [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco) - Owner type: Corporation - Owner's area on the map: 37.7984° N, 122.3992° W: Placed by OpenAirDocs at the center of ZIP code 94111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N6827 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=6827 - Page: https://openairdocs.org/deregistered/N6827-2011-09-26 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 (61, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR GAIA05036OP](https://openairdocs.org/sdr/GAIA05036OP), Dec 16, 2005: LIGHT. INOPERATIVE. DURING MAINTENANCE THE CREW ENTRY DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK GOOD. AC WAS RETURNED TO - [SDR GAIA05023](https://openairdocs.org/sdr/GAIA05023), Sep 8, 2005: ENGINE. FAILED. DURING CRUISE, NR 2 ENGINE LOW OIL PRESSURE LIGHT CAME ON BRIGHT, NOTICED NR 2 OIL PRESSURE DROPPED RAPIDLY TO ZERO. OIL TEMPS AND QUANTITY REMAINED NORMAL. ENG - [SDR GAIA04075OP](https://openairdocs.org/sdr/GAIA04075OP), May 6, 2004: LIGHT. INOPERATIVE. L-1 EMERGENCY EXIT LIGHT DIM, COCKPIT EMERGENCY EXIT LIGHT DIM. REMOVED AND REPLACED (L-1 AND COCKPIT) EMERGENCY LIGHTS. OPS CHECKS GOOD. AIRCRAFT RETURNED TO S - [SDR GAIA04048OP](https://openairdocs.org/sdr/GAIA04048OP), Mar 10, 2004: SMOKE DETECTOR. INOPERATIVE. LOWER CARGO FIRE WARNING ILLUMINATED SHORTLY AFTER TAKEOFF, RETURNED TO FWA. LIGHT WENT OUT BEFORE LANDING. BITE TEST CARRIED OUT. FOUND THREE SMOKE DETECTORS W - [SDR GAIA01305OP](https://openairdocs.org/sdr/GAIA01305OP), Aug 31, 2001: ACTUATOR. FAILED. FLT - 1843 - PHL-FWA - ON APPROACH TO FWA, THE FLIGHT CREW NOTICED THAT THE NR 8 SLAT DID NOT INDICATE EXTENDED WHEN THE FLAP HANDLE WAS MOVED FROM 2 DEGREES TO - [SDR GAIA01291OP](https://openairdocs.org/sdr/GAIA01291OP), Aug 7, 2001: COALESCER BAG. DIRTY. FLT 2031 - RNO-DEN - AFTER TAKEOFF, THERE WAS A STRONG ODOR OF JET FUEL IN THE COCKPIT. THIS AIRCRAFT MADE AN UNEVENTFUL RETURN TO RNO. REMOVED AND REPLACED BOT - [SDR GAIA01257ST](https://openairdocs.org/sdr/GAIA01257ST), Jul 6, 2001: FRAME. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 380 FRAME HAS SEVERAL HOLES IN THE INBOARD RADIUS BETWEEN STRINGER 4-7L. ACCOMPLISHED BS 380 FRAME R - [SDR GAIA01256ST](https://openairdocs.org/sdr/GAIA01256ST), Jul 6, 2001: SKIN. CRACKED. DURING A LTC INSPECTION, IT WAS DISCOVERED RIGHT WING UPPER SURFACE LEADING EDGE SKIN CRACKED IN 2 PLACES AT AFT END OF NR 6 SLAT OUTBOARD HOOK SEAL CUTOUT. (M) - [SDR GAIA01255ST](https://openairdocs.org/sdr/GAIA01255ST), Jul 6, 2001: SKIN. CORRODED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BULGING SKIN, POPPED FASTENER HEADS, CORROSION ALONG STRINGER 24L, BS 294-310. ACCOMPLISHED FUSELAGE SK - [SDR GAIA01253ST](https://openairdocs.org/sdr/GAIA01253ST), Jul 6, 2001: WEB. CRACKED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 178 BULKHEAD CRACKED AT RBL 2, WL 198, ALSO STIFFENERS (HORIZONTAL) ABOVE WL 200 AND BELOW WL 196 AR - [SDR GAIA01252ST](https://openairdocs.org/sdr/GAIA01252ST), Jul 6, 2001: WEB. CRACKED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED RIGHT TORQUE BOX LIGHTNING HOLE AT STATION 1225 HAS A CRACK 1 INCH LONG. ACCOMPLISHED RIGHT TORQUE BOX - [SDR GAIA01251ST](https://openairdocs.org/sdr/GAIA01251ST), Jul 6, 2001: FRAME. CRACKED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED C-3 CARGO DOOR CUT OUT FORWARD OUTBOARD CHORD IS CRACKED 1.5 INCH BS 1090, STRINGER 24R. ACCOMPLISHED B - [SDR GAIA01250ST](https://openairdocs.org/sdr/GAIA01250ST), Jul 6, 2001: WEB. CRACKED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 178 BULKHEAD WEB IS CRACKED AT APPROXIMATELY WL 218, LBL 12 (POSITION 1L PER W/C 2210). ACCOMPLISHED - [SDR GAIA01249ST](https://openairdocs.org/sdr/GAIA01249ST), Jul 6, 2001: ANGLE. CRACKED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED C-2 DOOR CUT OUT FORWARD FRAME LOWER STANCHION ADAPTER ATTACH ANGLE BROKEN AT BS 950E, STRINGER 26R. AC - [SDR GAIA01248ST](https://openairdocs.org/sdr/GAIA01248ST), Jul 6, 2001: SKIN. CORRODED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BULGING SKIN AND DISHED FASTENER HEADS AT BS 215, STRINGER 24R. ACCOMPLISHED FUSELAGE SKIN LONGITUDINAL - [SDR GAIA01247ST](https://openairdocs.org/sdr/GAIA01247ST), Jul 6, 2001: SKIN. CRACKED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED L1 DOOR AFT UPPER CORNER FRAME IS CRACKED 1.5 INCH BS 344, STRINGER 5L-6L. ACCOMPLISHED FORWARD ENTRY D - [SDR GAIA01246ST](https://openairdocs.org/sdr/GAIA01246ST), Jul 6, 2001: SEAT TRACK. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED SEAT TRACK AT BS 520-540, LBL 45.5 HAS ELONGATED HOLES. ACCOMPLISHED SEAT TRACK REPLACEMENT AT BS 480-5 - [SDR GAIA01237ST](https://openairdocs.org/sdr/GAIA01237ST), Jul 6, 2001: WEB. CORRODED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED WEB AT BS 328 LBL 45 CORRODED, FLIGHTSTAR AIRCRAFT SERVICES, INC. ACCOMPLISHED FLOORWEB REPLACEMENT BS - [SDR GAIA01236ST](https://openairdocs.org/sdr/GAIA01236ST), Jul 6, 2001: WEB. CRACKED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 620 FRAME FORWARD WEB CRACKED THROUGH SEAL RETAINER FASTENER HOLES ABOVE STRINGER 25 RT. ACCOMPLISHE - [SDR GAIA01235ST](https://openairdocs.org/sdr/GAIA01235ST), Jul 6, 2001: ANGLE. CRACKED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN THE AFT AIRSTAIR, THE LOWER TORQUE BOX TO BS 1342 LOWER SPANWISE CHORD STIFFENER ATTACH ANGLE IS CRA - [SDR GAIA01234ST](https://openairdocs.org/sdr/GAIA01234ST), Jul 6, 2001: STRINGER. CRACKED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15L CRACKED AT FORWARD END OF LEFT WING SCANNING LIGHT BS 720B PLUS 5. ACCOMPLISHED STRINGER 1 - [SDR GAIA01233ST](https://openairdocs.org/sdr/GAIA01233ST), Jul 6, 2001: STRINGER. CRACKED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15L CRAKED AT AFT END OF LEFT WING SCANNING LIGHT BS 720B PLUS 15. ACCOMPLISHED STRINGER 15L R - [SDR GAIA01232ST](https://openairdocs.org/sdr/GAIA01232ST), Jul 6, 2001: FRAME. DENTED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 720 FRAME DENTED IN RADIUS BETWEEN STRINER 16-17 LEFT. ACCOMPLISHED BS 720 FRAME REPAIR AT STRINER 1 - [SDR GAIA01231ST](https://openairdocs.org/sdr/GAIA01231ST), Jul 6, 2001: STRINGER. CRACKED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15R CRACKED AT FORWARD END OF WING SCANNING LIGHT CUT OUT BS 720B PLUS 5. ACCOMPLISHED STRINGE - [SDR GAIA01230ST](https://openairdocs.org/sdr/GAIA01230ST), Jul 6, 2001: FRAME. DENTED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN AFT CARGO FRAME BS 1110 HAS A DENT AT STRINGER 26L. ACCOMPLISHED BS 1110 FRAME REPAIR AT STRINGER 26 - [SDR GAIA01229ST](https://openairdocs.org/sdr/GAIA01229ST), Jul 6, 2001: FRAME. DENTED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN FORWARD CARGO FRAME BS 720 HAD A DENT BELOW STRINGER 25R. ACCOMPLISHED BS 720 FRAME REPAIR AT STRING - [SDR GAIA01228ST](https://openairdocs.org/sdr/GAIA01228ST), Jul 6, 2001: FRAME. DENTED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN FORWARD CARGO FRAME BS 720 HAS 2 DENTS AT STRINGER 25L. ACCOMPLISHED BS 720 FRAME REPAIR AT STRINGER - [SDR GAIA01227ST](https://openairdocs.org/sdr/GAIA01227ST), Jul 6, 2001: FRAME. DENTED. DURING A LTC INSPECTION, IT WAS DISCOVERED IN FORWARD CARGO FRAME BS 700 HAS 2 DENTS AT STRINGER 25L AND 24L. ACCOMPLISHED BS 700 FRAME REPAIR AT STRINGER 25L A - [SDR GAIA01226ST](https://openairdocs.org/sdr/GAIA01226ST), Jul 6, 2001: FLOORBEAM. CORRODED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN DOG HOUSE AREA, FLOORBEAM T-CAP IS CORRODED AT BS 312 LBL 3. ACCOMPLISHED BS 312 FLOORBEAM UPPER CHO - [SDR GAIA01225ST](https://openairdocs.org/sdr/GAIA01225ST), Jul 6, 2001: BULKHEAD. CRACKED. DURING A LTC INSPECTION , IT WAS DISCOVERED IN 2 CRACKS AT FASTENER LOCATIONS BS 178, RBL 10, WL 235. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR AT RBL 10, WL 235 - [SDR GAIA01224ST](https://openairdocs.org/sdr/GAIA01224ST), Jul 6, 2001: SKIN. CRACKED. DURING A LTC INSPECTION, IT WAS DISCOVERED RIGHT WING LEADING EDGE CAVITY LOWER SKIN CRACKED. ACCOMPLISHED RIGHT WING LEADING EDGE LOWER SKIN REPAIR AT WS 474 I - [SDR GAIA01223ST](https://openairdocs.org/sdr/GAIA01223ST), Jul 6, 2001: ANGLE. CRACKED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED RIGHT WING LEADING EDGE CAVITY UPPER ATTACH ANGLE CRACKED AT SLAT STATION .260, WL 343. ACCOMPLISHED RI - [SDR GAIA01222ST](https://openairdocs.org/sdr/GAIA01222ST), Jul 6, 2001: SKIN. CRACKED. DURING A LTC INSPECTION ,IT WAS DISCOVERED LEFT WING INBOARD INTERNAL LEADING EDGE SKIN, ACCESS THROUGH PANEL 6301, L/E STATION 130.5 IS CRACKED AROUND SEVERAL - [SDR GAIA01221ST](https://openairdocs.org/sdr/GAIA01221ST), Jul 6, 2001: PRESSURE PANEL. CRACKED. DURING A LTC INSPECTION, IT WAS DISCOVERED LEFT MAIN WHEEL WELL PRESSURE WEB IS CRACKED AT BS 948, LBL 65, WL 200. ACCOMPLISHED LEFT MAIN WHEEL WELL PRESSURE DE - [SDR GAIA01220ST](https://openairdocs.org/sdr/GAIA01220ST), Jul 6, 2001: PRESSURE PANEL. CRACKED. DURING A LTC INSPECTION, IT WAS DISCOVERED RIGHT MAIN WHEEL WELL PRESSURE WEB IS CRACKED AT BS 948, RBL 65, WL 200. ACCOMPLISHED RIGHT MAIN WHEEL WELL PRESSURE - [SDR GAIA01219ST](https://openairdocs.org/sdr/GAIA01219ST), Jul 6, 2001: PRESSURE PANEL. CRACKED. DURING A LTC INSPECTION ,DISCOVERED 2 CRACKS IN NWW CEILING RECESSED WEB AT BS 285, RBL 4-8 AND BS 290, BL 0. ACCOMPLISHED NOSE WHEEL WELL RECESSED CEILING WEB - [SDR GAIA01218ST](https://openairdocs.org/sdr/GAIA01218ST), Jul 6, 2001: PRESSURE PANEL. CRACKED. DURING A LTC INSPECTION , IT WAS DISCOVERED THAT THE NLG WW LEFT WEB IS CRACKED HORIZONTALLY AT BS 240-250, WL 180. ACCOMPLISHED LEFT NOSE WHEEL WELL WEB CRACK - [SDR GAIA01217ST](https://openairdocs.org/sdr/GAIA01217ST), Jul 6, 2001: SKIN. CRACKED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED C-3 DOOR SKIN CRACKED AT OUTER HANDLE COVER PLATE BS 1125 BETWEEN STRINGER 23-24 RIGHT, FILGHT STAR AIR - [SDR GAIA01254ST](https://openairdocs.org/sdr/GAIA01254ST), Jul 1, 2001: WEB. CRACKED. DURING A LTC INSPECTION AT FLIGHTSTAR, IT WS DISCOVERED VERTICAL CRACK NOSE WHEEL WELL LEFT WEB BS 260, WL 160. ACCOMPLISHED WEB REPAIR BS 260, WL 160 IN LEFT N - [SDR GAIA01239ST](https://openairdocs.org/sdr/GAIA01239ST), May 21, 2001: FLOORBEAM. CORRODED. DURING A ROUTINE MAINTENANCE INSPECTION, IT WAS DISCOVERED THAT THE FLOORBEAM AT BS 1030, RBL 34.5 WAS CORRODED OUT OF LIMITS. REPAIRED FLOORBEAM AT BS 1030, RB - [SDR GAIA01110OP](https://openairdocs.org/sdr/GAIA01110OP), Mar 9, 2001: GCU. FAULTY. FLT 2019 - ABQ-PHX, NO CLIMB-OUT, SHORTLY AFTER FLAP RETRACTION, EXPERIENCED DIFFERENTIAL FAULT IN NR 2 SYSTEM IN COMBINATION WITH ESSENTIAL POWER LOSS AND OVER - [SDR GAIA01108OP](https://openairdocs.org/sdr/GAIA01108OP), Mar 6, 2001: GENERATOR. MALFUNCTIONED. FLT 2071 - GEG-PHX - AFTER TAKEOFF, LOSS OF ALL GENERATORS OCCURRED. AIRCRAFT MADE AN UNEVENTFUL LANDING IN GEG. RAN ENGINES AND GENERATORS. LOADED GENERATORS U - [SDR GAIA01075OP](https://openairdocs.org/sdr/GAIA01075OP), Feb 23, 2001: CLAMP. LEAKING. FLT 2507 - GEG-IND - AT 1000 FEET AGL, ENGINE AND WING HEAT OPENED. ONE MINUTE LATER NR 1 STRUT OVER HEAT LIGHT ILLUMINATED AS A/C CLIMBED THROUGH CLOUDS INTO C - [SDR GAIA01014](https://openairdocs.org/sdr/GAIA01014), Jan 24, 2001: LIGHT. INTERMITTENT. FLT 1777 - BOS-FWA - LOWER AFT BODY HEAT LIGHT INTERMITTENT TEST. PTT WORKS GOOD. AIRCRAFT MADE AN UNEVENTFUL LANDING IN FWA. REPLACED AFT BODY OVERHEAT LAMP. O - [SDR GAIA00793](https://openairdocs.org/sdr/GAIA00793), Dec 22, 2000: LIGHT. INOPERATIVE. MAINTENANCE ONLY, MHR, EMERGENCY EXIT LIGHT IN COCKPIT DOES NOT ILLUMINATE.REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT. SYSTEM OPERATIONALLY CKS GOOD. AIR - [SDR GAIA00721](https://openairdocs.org/sdr/GAIA00721), Nov 27, 2000: HANDLE. STUCK. FLT 8106 - SEA-ANC - ON APPROACH, FLAP HANDLE WOULDN'T MOVE. AIRCRAFT MADE AN UNEVENTFUL ZERO FLAP LANDING IN ANC. CANNOT DUPLICATE PROBLEM ON GROUND. FLAP SYST - [SDR GAIA9931](https://openairdocs.org/sdr/GAIA9931), Mar 3, 1999: BULB. FAILED. EN ROUTE FROM YIP TO HUF, THE CARGO SMOKE LIGHT ILLUMINATED. THE FLIGHT CREW FOLLOWED EMERGENCY CHECKLIST PROCEDURES. THERE WAS NO SMOKE OR SMELL INTHE COCKPIT - [SDR GAIA9857A](https://openairdocs.org/sdr/GAIA9857A), May 27, 1998: SEAL. WORN. DFW - AFTER DEPARTING, NR 2 ENGINE OIL PRESSURE LOW, (LOSS OF PRESSURE). ENGINE SHUT DOWN. AIRCRAFT MADE AN UNEVENTFUL RETURN TO DFW. INSPECTED ENGINE WITH NO D - [SDR GAIA9838](https://openairdocs.org/sdr/GAIA9838), Apr 8, 1998: LIGHT. INOPERATIVE. DURING MAINTENANCE AT OKC, FOUND EMERGENCY LIGHT ABOVE L-1 DOOR FAILED TO ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. SYSTEM OPERATIONALLY CHECKS - [SDR GAIA9809](https://openairdocs.org/sdr/GAIA9809), Feb 6, 1998: LIGHT. INOPERATIVE. UPON ARRIVAL TOL, CREW REPORTS EMERGENCY EXIT LIGHT OVER L-1 DOOR INOP. REMOVED AND REPLACED EXIT LIGHT IAW MM ATA 33-50. SYSTEM CHECK NORMAL ON GROUND. AIRCRAF All 61: https://openairdocs.org/deregistered/N6827-2011-09-26/reports.md ## 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 19951013038269I](https://openairdocs.org/incident/19951013038269I), Oct 13, 1995: Boeing 727200 (N6827), Roanoke, VA, Minor damage. Narrative: the number four main wheel assembly was found missing by ground crew after the aircraft parked on the ramp. The wheel assembly was later found on… ## Other aircraft with N6827 - [Cancelled 1930-08-01](https://openairdocs.org/deregistered/N6827-1930-08-01): Stinson SM1-B, S/N M-252. Owner: [Thompson Aeronautical Corp](https://openairdocs.org/faa-owner/THOMPSON%20AERONAUTICAL%20CORP), [Cleveland, OH](https://openairdocs.org/faa-place/OH/Cleveland) --- 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.