# N6806: 1968 Boeing 727-223, registration cancelled 2007-05-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 10, 2007
- 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: 19481
- Year built: 1968
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: August 15, 1995
- Certificate issued: November 19, 1997
- Last registry action: August 17, 2004
- Mode S code: A90661
- Owner when cancelled: [Kitty Hawk Aircargo Inc](https://openairdocs.org/faa-owner/KITTY%20HAWK%20AIRCARGO%20INC)
- Location: [Dfw Airport, TX](https://openairdocs.org/faa-place/TX/Dfw%20Airport)
- Owner type: Corporation
- Owner's area on the map: 32.9032° N, 97.0531° W: Placed by OpenAirDocs at the center of ZIP code 75261, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N6806
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=6806
- Page: https://openairdocs.org/deregistered/N6806-2007-05-10

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 (80, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR GAIA04089OP](https://openairdocs.org/sdr/GAIA04089OP), Jul 22, 2004: LIGHT. INOPERATIVE. ON PREFLIGHT, FOUND EXIT LIGHT IN COCKPIT INOPERATIVE. REMOVED EXIT LIGHT FOR CHARGING AND INSTALLED SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED
- [SDR GAIA04072](https://openairdocs.org/sdr/GAIA04072), May 6, 2004: ROD. UNSERVICEABLE. AT DEPARTURE, LT MAIN GEAR FAILED TO RETRACT. THIS WAS VERIFIED BY THE TOWER. CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT WHERE A LANDING WAS MADE WITHOUT INCID
- [SDR GAIA04007OP](https://openairdocs.org/sdr/GAIA04007OP), Jan 23, 2004: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE COCKPIT DOOR EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGH
- [SDR GAIA03105](https://openairdocs.org/sdr/GAIA03105), Sep 10, 2003: FRAME. DENTED. DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 1010 HAS A DENT ABOVE STRINGER 25R. REF FASI N/R 53289 CUT OUT DAMAGE, 7 INCHES BY 3.5 INCHES DOUBLER REPAIR PER B72
- [SDR GAIA03094](https://openairdocs.org/sdr/GAIA03094), Sep 10, 2003: FLOORBEAM. CORRODED. DURNG B-2 CHECK, FOUND MAIN CABIN FLOORBEAM ANGLE CORRODED LBL 60 BS 848. REF FASI N/R 53138 ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 51-40-3 AND 53-10-1 FIG 1.
- [SDR GAIA03093](https://openairdocs.org/sdr/GAIA03093), Sep 10, 2003: FLOORBEAM. CORRODED. DURING B-2 CHECK, FOUND MAIN CABIN FLOORBEAM UPPER 'T' CAP CORRODED RBL 45.5 BS 765 TO 848. REF FASI N/R 53136 REPLACED DAMAGED 'T' CAP P/N 65-16279-10 PER B-72
- [SDR GAIA03092](https://openairdocs.org/sdr/GAIA03092), Sep 10, 2003: STRINGER. CRACKED. DURING B-2 CHECK, FOUND MAIN CABIN STRINGER 15 RT CRACKED AT AFT SIDE OF BS 720B. REF FASI N/R 53135, ACCOMPLISHED STRINGER REPAIR PER B727 SRM 53-10-3 TABLE ON
- [SDR GAIA03106](https://openairdocs.org/sdr/GAIA03106), Sep 10, 2003: FRAME. DENTED. DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 950E HAS A DENT BY STRINGER 25L. REF FASI N/R 53292. FABRICATED DOUBLER REPAIR FROM 7075-T6, .080, DIMENSIONS 17.75 
- [SDR GAIA03086](https://openairdocs.org/sdr/GAIA03086), Sep 10, 2003: FRAME. DENTED. DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 380 HAS A DENT IN THE RADIUS BELOW STRINGER 6LT. REF FASI N/R 53129, CUT OUT DAMAGE 4.75 BY 1.25, DOUBLER REPAIR PER
- [SDR GAIA03091](https://openairdocs.org/sdr/GAIA03091), Sep 10, 2003: STRINGER. CRACKED. DURING B-2 CHECK FUOND MAIN CABIN STRINGER 15 LT CRACKED FORWARD OF BS 720C. REF FASI N/R 53134 ACCOMPLISHED STRINGER REPAIR PER B727 SRM 53-10-3 TABLE ONE. (M)
- [SDR GAIA03090](https://openairdocs.org/sdr/GAIA03090), Sep 10, 2003: FRAME. DENTED. DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 600 DENTED IN RADIUS BELOW STRINGER 16RT. REF FASI N/R 53133, ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 51-40-3 FIG 1
- [SDR GAIA03089](https://openairdocs.org/sdr/GAIA03089), Sep 10, 2003: FRAME. DENTED. DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 580 DENTED IN RADIUS BELOW STRINGER 16RT. REF FASI N/R 53132 ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 51-40-3 FIG 1.
- [SDR GAIA03088](https://openairdocs.org/sdr/GAIA03088), Sep 10, 2003: FRAME. CRACKED. DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 560 CRACKED BELOW STRINGER 16RT. REF FASI N/R 53131 CUTOUT DAMAGE, ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 51-40-3 
- [SDR GAIA03085](https://openairdocs.org/sdr/GAIA03085), Sep 10, 2003: FLAP TRACK. CRACKED. DURING B-2 CHECK, FOUND NR 5 FLAP TRACK SPACER BLOCK CRACKED AT WBL 124. REF FASI N/R 50408, INSTALLED OVERSIZE FASTENERS IAW S/B 727-57-136 REV 1, FIGURE 2. (M
- [SDR GAIA03084](https://openairdocs.org/sdr/GAIA03084), Sep 10, 2003: FRAME. CRACKED. DURING B-2 CHECK, FOUND FUSELAGE FRAME AT BS 950D CRACKED, ABOVE STRINGER 22R. REF FASI N/R 50407, FABRICATED REPAIR DOUBLER FROM 7075-T6, .080, DIMENSIONS 9 IN
- [SDR GAIA03083](https://openairdocs.org/sdr/GAIA03083), Sep 10, 2003: SEAT TRACK. CORRODED. DURING B-2 CHECK, FOUND MAIN CABIN SEAT TRACK CORRODED AT BS 344 TO BS 360, RBL 45.5. REF FASI N/R 50403. FABRICATED REPAIR FROM BAC 1520-792 MATERIAL. LENGTH 1
- [SDR GAIA03096](https://openairdocs.org/sdr/GAIA03096), Sep 10, 2003: FLOORBEAM. CORRODED. DURING B-2 CHECK, FOUND FORWARD LAVATORY FLOORBEAM UPPER 'T' CORRODED BS 344 RBL 25 TO RBL 50 ALSO AT LBL 25. REF FASI N/R 53195, REPLACED FLOORBEAM UPPER 'T' C
- [SDR GAIA03099](https://openairdocs.org/sdr/GAIA03099), Sep 10, 2003: BEAM. CRACKED. DURING B-2 CHECK, FOUND BS 1183 VERTICAL BEAM CRACKED LBL 36 INCHES WL 250. REF FASI N/R 53249, INSTALLED REPAIR PER S/B 727-53-0192 REV 2. (M)
- [SDR GAIA03098](https://openairdocs.org/sdr/GAIA03098), Sep 10, 2003: RIB. CRACKED. DURING B-2 CHECK, FOUND RIGHT ELEVATOR SUPPORT RIB STATION 17.2 CRACKED. REF FASI N/R 53208, REPLACED ELEVATOR SUPPORT RIB PER S/B 727-55A0091. (M)
- [SDR GAIA03097](https://openairdocs.org/sdr/GAIA03097), Sep 10, 2003: STIFFENER. CRACKED. DURING B-2 CHECK, FOUND LEFT WING REAR SPAR VERTICAL STIFFENER CRACKED AT WS 556. REF FASI N/R 53206, REPLACED STIFFENER PER B727 SRM 51-30-2. (M)
- [SDR GAIA03095](https://openairdocs.org/sdr/GAIA03095), Sep 10, 2003: FLOORBEAM. CORRODED. DURING B-2 CHECK, FOUND MAIN CABIN FLOORBEAM BS 480 CORRODED AT LBL 30 AND CRACKED AT LBL 59. REF FASI N/R 53187, CUT OUT DAMAGED AREA, INSTALLED REPAIR PER B72
- [SDR GAIA03087](https://openairdocs.org/sdr/GAIA03087), Sep 10, 2003: FRAME. DENTED. DURING B-2 CHECK, FOUND MAIN CARGO CABIN FRAME BS 540 HAS A DENT IN THE RADIUS BELOW STRINGER 16RT. REF FASI N/R 53130 ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 
- [SDR GAIA03104](https://openairdocs.org/sdr/GAIA03104), Sep 10, 2003: FRAME. DENTED. DURING B-2 CHECK, FOUND AFT CARGO FRAME DENTED BS 1070 AT STRINGER 25 RT. REF FASI N/R 53281, DOUBLER REPAIR IAW B727 SRM 53-10-2 FIG 5. (M)
- [SDR GAIA03103](https://openairdocs.org/sdr/GAIA03103), Sep 10, 2003: SEAT TRACK. CORRODED. DURING B-2, FOUND MAIN CABIN SEAT TRACK CORRODED BS 360 BL0. ERF FASI N/R 53268, REPLACED SEAT TRACK BS 344-480 BL 0 PER B727 SRM 53-10-5 FIG 7. (M)
- [SDR GAIA03102](https://openairdocs.org/sdr/GAIA03102), Sep 10, 2003: SEAT TRACK. CORRODED. DURING B-2 CHECK, FOUND MAIN CARGO SEAT TRACK CORRODED BS 360, LBL 25.5. REF FASI N/R 53267, REPLACED SEAT TRACK LBL 25.5 BS 344 TO 480 PER B727 SRM 53-10-2 FIG
- [SDR GAIA03101](https://openairdocs.org/sdr/GAIA03101), Sep 10, 2003: SEAT TRACK. CORRODED. DURING B-2 CHECK, FOUND MAIN CARGO SEAT TRACK CORRODED AT BS 760, RBL 45.5. REF FASI N/R 53265, REPLACED SEAT TRACK RBL 45.5, BS 760 TO 840 PER B727 SRM 51-30-2
- [SDR GAIA03100](https://openairdocs.org/sdr/GAIA03100), Sep 10, 2003: FLOOR SUPPORT. CORRODED. DURING B-2 CHECK, FOUND MAIN CABIN FLOOR SUPPORT ANGLE LBL 61 BS 1090 UPPER CHORD CORRODED. REF FASI N/R 53253, REPLACED UPPER CHORD PER B727 SRM 53-10-2 FIG 5 
- [SDR GAIA03082](https://openairdocs.org/sdr/GAIA03082), Sep 10, 2003: SEAT TRACK. CORRODED. DURING B-2 CHECK, FOUND MAIN CABIN SEAT TRACK CORRODED AT BS 360 TO BS 344, RBL 25.5. REF FASI N/R 50402, FABRICATED REPAIR FROM BAC 1520-792 MATERIAL. LENGTH 1
- [SDR GAIA03008OP](https://openairdocs.org/sdr/GAIA03008OP), Feb 14, 2003: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE AT IAH, IT WAS DISCOVERED THAT THE L-1 EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATION
- [SDR GAIA02166OP](https://openairdocs.org/sdr/GAIA02166OP), Dec 20, 2002: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONALL
- [SDR GAIA02025OP](https://openairdocs.org/sdr/GAIA02025OP), Mar 14, 2002: DUCT. WARPED. FLT 873 - FWA-LAX - DURING CLIMB-OUT, THE NR 1 STRUT OVERHEAT LIGHT CAME ON FIVE MINUTES AFTER TAKEOFF. THE AIRCRAFT RETURNED TO FWA AND THE LANDING WAS UNEVENT
- [SDR GAIA02024OP](https://openairdocs.org/sdr/GAIA02024OP), Mar 12, 2002: CLAMP. LOOSE. FLT 733 - DFW-FWA - DURING CLIMB-OUT, THE NR 1 STRUT OVERHEAT LIGHT CAME ON. THE AIRCRAFT RETURNED TO DFW AND THE LANDING WAS UNEVENTFUL. FOUND THE CLAMP FOR TH
- [SDR GAI2001F00000](https://openairdocs.org/sdr/GAI2001F00000), Oct 11, 2001: WIRE. DIRTY. AFTER TAKE OFF, THE FLIGHT CREW DISCOVERED THAT THE OUTBOARD FLAPS WERE STUCK AT THE 2 DEGREE POSITION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO A
- [SDR GAIA01245OP](https://openairdocs.org/sdr/GAIA01245OP), Jun 26, 2001: WIRE. FAULTY. KHA - FLT 202 - TYS TO DFW, ON CLIMB-OUT FROM TYS, THE NR 2 SLAT DID NOT RETRACT WHEN THE FLAP HANDLE WAS MOVED TO THE UP POSITION. EMERGENCY WAS DECLARED AND T
- [SDR GAIA00687](https://openairdocs.org/sdr/GAIA00687), Nov 1, 2000: INDICATOR. INOPERATIVE. DURING PREFLIGHT FOUND, EMERGENCY EXIT LIGHT ARMED INDICATOR LIGHT INOPERATIVE. REMOVED AND REPLACED INDICATOR LIGHT BASE ASSEMBLY, OPS CHECK OK. AIRCRAFT WAS R
- [SDR 00683](https://openairdocs.org/sdr/00683), Oct 19, 2000: FITTING. CRACKED. DISCREPANCY: DURING HEAVY CHECK FOUND: FUSELAGE FITTING AT FS 870 STR 18 HAS A CRACK INDICATION ON LOWER AFT BOLT HOLE CORRECTIVE ACTION: REPAIRED FITTING IAW T
- [SDR 00684](https://openairdocs.org/sdr/00684), Oct 16, 2000: ELEVATOR. CORRODED. DISCREPANCY: DURING HEAVY CHECK FOUND: ELEVATOR TRAILING EDGE CORRODED AT STA 179CORRECTIVE ACTION: REPAIRED ELEVATOR IAW B727 SRM 55-20-2
- [SDR 00685](https://openairdocs.org/sdr/00685), Oct 13, 2000: SEAT TRACK. CORRODED. DISCREPANCY: DURING HEAVY CHECK FOUND: CORROSION ON THE SEAT TRACK FLANGE AT LBL 45 BS 854 TO 870CORRECTIVE ACTION: REPLACED SEAT TRACK
- [SDR 00686](https://openairdocs.org/sdr/00686), Oct 13, 2000: SKIN. CORRODED. DISCREPANCY: DURING HEAVY CHECK FOUND:CORROSION ON TEH SKIN DOUBLER AT FS 1163 STR 19RCORRECTIVE ACTION: REPAIRED SKIN AND DOUBLER IAW TIMCO REO S00343 BY CUTTI
- [SDR GAIA00681](https://openairdocs.org/sdr/GAIA00681), Oct 12, 2000: LAP JOINT. DAMAGED. DISCREPANCY: DURING HEAVY CHECK FOUND: SKIN PULLING FASTENER HEADS, STA 460 STR 19R LAP SEAM. CORRECTIVE ACTION: REPAIRED TAP SEAM IAW B727 SRM53-30-3 FIG 5 STA
- [SDR GAIA00680](https://openairdocs.org/sdr/GAIA00680), Oct 12, 2000: ATTACH ANGLE. CRACKED. DISCREPANCY: DURING HEAVY CHECK FOUND: LBL 70.5 WL208, BS873-878, SKIN TO FLOOR WEB ATTACH "T" ANGLE CRACKED ON INNER FLANGE. CORRECTIVE ACTION: HAD EDDY CURREN
- [SDR GAIA00679](https://openairdocs.org/sdr/GAIA00679), Oct 12, 2000: ATTACH ANGLE. CRACKED. DURING HEAVY CHECK FOUND BS 1343 AFT SPLICE LBL 20 WL 280 SKIN ATTACH ANGLE CRACKED. REMOVED ANGLE IAW B727 SRM 51-30-2 FAB. NEW ANGLE PER B727 51-40-3. INSTALL
- [SDR 00682](https://openairdocs.org/sdr/00682), Oct 12, 2000: FRAMES. DENTED. DISCREPANCY: DURING HEAVY CHECK FOUND: FUSELAGE FRAME AT FS 1166 ABOVE STR 17 WL 210 HAS A DENTED FLANGE CORRECTIVE ACTION: REPAIRED FRAME IAW TIMCO REO S00340 
- [SDR GAIA00667](https://openairdocs.org/sdr/GAIA00667), Oct 11, 2000: KEELBEAM. CRACKED. DISCREPANCY: DURING HEAVY CHECK FOUND: LEFT LOWER KEELBEAM CHORD ATTACH FLANGE CRACKED AT STA 875, LBL6 WL137.8. CORRECTIVE ACTION: REPAIRED KEELBEAM ATTACH FLA
- [SDR GAIA00666](https://openairdocs.org/sdr/GAIA00666), Oct 11, 2000: ANGLE. CORRODED. DISCREPANCY: DURING HEAVY CHECK FOUND:C-2 DOOR CUT-OUT AFT FRAME INNER ANGLE CORRODED ABOVE S25 & S26 RT 2 AREAS. CORRECTIVE ACTION: REMOVED CORROSION AND FOUND
- [SDR GAIA00665](https://openairdocs.org/sdr/GAIA00665), Oct 11, 2000: FRAME. CRACKED. DISCREPANCY: DURING HEAVY CHECK FOUND: FS360 FRAME CRACKED BELOW STRINGER 7L.CORRECTIVE ACTION: REMOVED DAMAGE FABRICATED NEW ANGLE & FILLERS, FASTENERS IAW REO
- [SDR GAIA00668](https://openairdocs.org/sdr/GAIA00668), Oct 9, 2000: FLOORBEAM. CORRODED. DISCREPANCY: DURING HEAVY CHECK FOUND: FLOORBEAM STA 727 CORRODED ON UPPER CHORD UPPER SURFACE LBL30, LBL10 & RBL15 EXTENDING UNDER FLOOR SKIN. CORRECTIVE ACTIO
- [SDR GAIA00656](https://openairdocs.org/sdr/GAIA00656), Oct 3, 2000: FRAME. DENTED. DISCREPANCY: DURING HEAVY CEHCK FOUND: FS460 FRAME DENTED BETWEEN STRINGERS 17R & 16RCORRECTIVE ACTION: FABRICATED BEW FRAME DOUBLER AT BS460 BETWEEN STR 16 & 1
- [SDR GAIA00655](https://openairdocs.org/sdr/GAIA00655), Oct 2, 2000: LAP JOINT. BULGED. DISCREPANCY: DURING HEAVY CEHCK FOUND: SKIN JOINT BS359-360, STR 11R-14R SKIN BULGING. CORRECTIVE ACTION: REMOVED FASTENERS, FOUND SKIN TO BE OUT OF LIMITS, FAB
- [SDR GAIA00654](https://openairdocs.org/sdr/GAIA00654), Oct 2, 2000: SKIN. CORRODED. DISCREPANCY: DURING HEAVY CHECK FOUND: SKIN, UNDER FORWARD LAV SERVICE DOOR, CORRODED & BULGING STA 304 STR 20R. CORRECTIVE ACTION: REPAIRED IAW B727 SRM 53-30-

All 80: https://openairdocs.org/deregistered/N6806-2007-05-10/reports.md

## 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 19890708038589I](https://openairdocs.org/incident/19890708038589I), Jul 8, 1989: Boeing 727223 (N6806), Nashville, TN, Minor damage. NR3 engine failed on takeoff. Declared emergency. Returned. Found compressor section had failed.
- [Incident 19850918049869I](https://openairdocs.org/incident/19850918049869I), Sep 18, 1985: Boeing 727223 (N6806), Mobile, AL. Passenger short of breath and mercy landing made. Portable oxygen canister came apart while being used on passenger
- [Incident 19830410020969I](https://openairdocs.org/incident/19830410020969I), Apr 10, 1983: Boeing 727223 (N6806), Memphis, TN. Fire occurred in a bag under seat. Attendant put out fire. Fire resulted from a cigarette ash. Bad fire extinguisher

## Other aircraft with N6806

- [Cancelled 1931-10-20](https://openairdocs.org/deregistered/N6806-1931-10-20): Waco GXE, S/N G-1594. Owner: [Ludington Flying Service Inc](https://openairdocs.org/faa-owner/LUDINGTON%20FLYING%20SERVICE%20INC), [Camden, NJ](https://openairdocs.org/faa-place/NJ/Camden)

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