# N6822: 1968 Boeing 727-223, registration cancelled 2013-08-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 23, 2013 - Status when cancelled: Sale reported, canceled - 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: 19700 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: December 27, 1968 - Last registry action: February 14, 2000 - Mode S code: A90D43 - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Individual - Owner's area on the map: 25.8050° N, 80.3151° W: Placed by OpenAirDocs at the center of ZIP code 33122, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N6822 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=6822 - Page: https://openairdocs.org/deregistered/N6822-2013-08-23 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 (33) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AALA990103](https://openairdocs.org/sdr/AALA990103), Jan 25, 1999: LIGHT. DEFECTIVE. DFW - DURING OVERNIGHT MAINTENANCE AFT AIR STAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIR STAIRS EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED - [SDR AALA990015](https://openairdocs.org/sdr/AALA990015), Jan 4, 1999: CONTROL. MALFUNCTIONED. DFW - FLT 535 - DURING CRUISE AT FL22 AIRCRAFT LOST PRESSURIZATION. CREW INITIATED EMERGENCY DESCENT AND LANDED DFW WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKE - [SDR AALA990052](https://openairdocs.org/sdr/AALA990052), Jan 1, 1999: STRINGER. DAMAGED. TUL - FOUND FASTENER HOLES DAMAGED 16 AFT OF STATION 940 IN STRINGER 18A, LEFT SIDE. OVERSIZED 16 FASTENER HOLES TO STD .3125 INCH AFT OF STATION 940 IN STRINGE - [SDR AALA990033](https://openairdocs.org/sdr/AALA990033), Dec 21, 1998: SKIN. DAMAGED. TUL - AFT SIDE OF 1183 BULKHEAD ABOVE VAULT DOOR SKIN HAS SEVERAL DEEP TOOL MARKS LBL 20 TO RBL 20, 6 ABOVE CABIN FLOOR. INSTALLED DOUBLER PER ESO 11697, DATED - [SDR AALA990032](https://openairdocs.org/sdr/AALA990032), Dec 18, 1998: ANGLE. MISDRILLED. TUL - RIGHT LOWER TORQUE BOX LOWER CHORD ANGLE HAS 14 MISDRILLED HOLES WITH VISUAL INDICATION OF CRACK STATION 1323-1333. ALSO, 9 MISDRILLED HOLES WITH VISUAL I - [SDR AALA99036](https://openairdocs.org/sdr/AALA99036), Dec 16, 1998: WEB. WORN. TUL - LEFT TORQUE BOX WEB HAD HOLE WORN ALMOST THROUGH AT APROX STATION 1343 (VERT WEB). INSTALLED DOUBLER PER MM 51-40-2. (M) - [SDR AALA990035](https://openairdocs.org/sdr/AALA990035), Dec 16, 1998: UNKNOWN. TUL - RIGHT TORQUE BOX HAD HOLE WORN ALMOST THROUGH AT APPROX STATION 1343, VERT WEB. INSTALLED DOUBLER PER MM 51-40-2. (M) - [SDR AALA990034](https://openairdocs.org/sdr/AALA990034), Dec 16, 1998: SHEAR TIE. CRACKED. TUL - SHEAR TIE CRACKED STATION 52 BETWEEN STRINGER 27L-28L. REPAIRED PER SRM 53-10-4 FIG 15. (M) - [SDR AALA990031](https://openairdocs.org/sdr/AALA990031), Dec 16, 1998: FRAME. CRACKED. TUL - STATION 620 WEB CRACKED BEHIND PRESSURE SEAL RETAINER 10 INCH FROM LOWER END OF AFT CUT OUT. CUTOUT CRACK AND INSTALLED FILLER AND DOUBLER PER SRM 51-40-2 - [SDR AALA990030](https://openairdocs.org/sdr/AALA990030), Dec 16, 1998: FRAME. CRACKED. TUL - CARGO DOOR AFT CUTOUT WEB CRACKED 13 INCHES FROM LOWER END OF CUTOUT BEHIND SEAL RETAINER STATION 620. CUTOUT CRACK AND INSTALLED FILLER AND DOUBLER PER S - [SDR AALA990029](https://openairdocs.org/sdr/AALA990029), Dec 14, 1998: FRAME. CRACKED. TUL - NR 2 CARGO DOOR FRAME (FORWARD FRAME) IN FUSE CUTOUT HAS CRCK EXTENDING FROM LOWER STOP CASTING, LOWER SIDE. NDT FOUND CRACK AT LOWER STOP FITTING LOCATIO - [SDR AALA990028](https://openairdocs.org/sdr/AALA990028), Dec 14, 1998: SKIN. CRACKED. TUL - FOUND CRACK IN FUSELAGE SKIN AT SCREW IN AFT UPPER CORNER OF CO-PILOTS NR 3 WINDOW. STOP DRILLED CRACK. INSTALLED DOUBLER PER SRM 53-30-3 FIG 8, REPAIR NR - [SDR AALA981454](https://openairdocs.org/sdr/AALA981454), Aug 2, 1998: LIGHT. INOPERATIVE. DFW - DURING OVERNIGHT CHECK, RIGHT AFT EXTERIOR CARGO DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT AFT EXTERIOR CARGO DOOR EMERGENCY EXIT LIGHT. SYSTE - [SDR AALA980122](https://openairdocs.org/sdr/AALA980122), Jan 12, 1998: ELEMENT. DEFECTIVE. MIA - FLT 1746 - AFTER TAKEOFF MIA DURING CLIMB-OUT, NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. AIRCRAFT AIR INTERRUPTED MIA AND LANDED WITHOUT INCIDENT. REPLACED N - [SDR 98ZZZX326](https://openairdocs.org/sdr/98ZZZX326), Jan 12, 1998: DETECTOR. MALFUNCTIONED. MIA - ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT. (APPROXIMATELY 1,000 AFL). CONDUCTED AND COMPLETED STRUT OVERHEAT LIGHT EMERGENCY CHECKLIST. RETAR - [SDR AALA980012](https://openairdocs.org/sdr/AALA980012), Jan 4, 1998: ELEMENT. OUT OF POSITION. MCO - FLT 1941 - AFTER TAKEOFF MCO, NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. DUMPED FUEL AND LANDED WITHOUT INCIDENT. NR 1 ENGINE OVERHEAT DETECTOR ELEMENT WAS F - [SDR AALA971923](https://openairdocs.org/sdr/AALA971923), Oct 9, 1997: LIGHT ASSY. DEFECTIVE. DFW - DURING OVERNIGHT CHECK, AFT AIRSTAIR EMERGENCY EXIT LIGHT FOUND INOPERATIVE. REPLACED AFT AIRSTAIR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED, NORMAL OPE - [SDR AALA970575](https://openairdocs.org/sdr/AALA970575), Mar 19, 1997: ANGLE. CORRODED. TUL - CORROSION ON SUPPORT ANGLE TO NOSE GEAR DRAG SHELF FORWARD ANGLE ENTIRE WIDTH OF COMPARTMENT. REMOVED CORROSION PER 51-10-06 AND INSTALLED REPAIR PER ESO - [SDR AALA970574](https://openairdocs.org/sdr/AALA970574), Mar 19, 1997: CASTING. CORRODED. TUL - CORROSION ON 740 CASTING AT SKIN ATTACHMENT BETWEEN STR 27R AND STR 28R. INSTALLED NEW CASTING PER 51-10-01. TST: 76,923 HOURS. CYCLES: 52,656. (X) - [SDR AALA970573](https://openairdocs.org/sdr/AALA970573), Mar 19, 1997: BULKHEAD. CORRODED. TUL - FORWARD SIDE OF BULKHEAD STA 351 HAS CORROSION ON AREAS WHERE DRAG BRACE WAS ATTACHED, RBL 6 INCHES TO LBL 6 INCHES LOCATED AT 6 INCHES TO 12 INCHES ABOVE - [SDR AALA970572](https://openairdocs.org/sdr/AALA970572), Mar 19, 1997: SKIN. CORRODED. TUL - CORROSION ON AFT CARGO SKIN. INSTALLED DOUBLERS PER SRM 53-30-3 FIG 3 AND ESO 11697 DATED 2-20-97. TST: 76,923 HOURS. CYCLES: 52,656. (X) - [SDR AALA970571](https://openairdocs.org/sdr/AALA970571), Mar 19, 1997: SKIN. CORRODED. TUL - CORROSION ON SKIN INBETWEEN STR 26L TO STR 26R STA 720F + 15 INCHES TO STA 740. REMOVED CORROSION AND REMOVED ORIGINAL TRIPLER, TREATED AND PRIMED AREAS A - [SDR AALA970570](https://openairdocs.org/sdr/AALA970570), Mar 19, 1997: FLOOR BEAM. CRACKED. TUL - TOP FLANGE OF CABIN FLOOR BEAM CRACKED AT HOLE, STA 1110 LBL 7 INCHES. CORROSION THE CAUSE OF CRACK. REPAIRED FLOOR BEAM PER SRM 53-10-8 FIG 8 PG 47. TST: - [SDR AALA970569](https://openairdocs.org/sdr/AALA970569), Mar 19, 1997: FLOOR BEAM. CORRODED. TUL - UPPER FLOOR BEAM CAP HAS BULGES AT RBL 18 TO RBL 19 STA 380, CORROSION AT RBL 16 TO RBL 12, AND CRACK AT RBL 18 TO RBL 19 STA 380. REPAIRED FLOOR BEAM CAP - [SDR AALA970568](https://openairdocs.org/sdr/AALA970568), Mar 19, 1997: STRINGER. CORRODED. TUL - CORROSION AT STR 27R FROM STA 720E + 10 INCHES TO STA 740. INSTALL NEW STRINGER FROM BS 720E + 10 INCHES TO BS 740 ON STR 27R PER SRM 53-10-03 PAGES 1-11. - [SDR AALA970567](https://openairdocs.org/sdr/AALA970567), Mar 19, 1997: PRESSURE DECK. CRACKED. TUL - RIGHT WHEELWELL PRESSURE DECK HAS 1.50 INCH CRACK, FS 930, FORWARD SIDE OF SECOND RIB, FORWARD OF VIEWING WINDOW. STOP DRILLED CRACK, REMOVED OLD DOUBLER - [SDR AALA970566](https://openairdocs.org/sdr/AALA970566), Mar 19, 1997: STRINGER. CRACKED. TUL - 2 INCH CRACK IN UPPER FLANGE INTO LOWER RADIUS IN STR 16R AT FS 500. CUT OUT CRACKED SECTION OF STR 16R AND INSTALLED STRINGER REPAIR PER SRM 53-10-3 FIG - [SDR AALA970565](https://openairdocs.org/sdr/AALA970565), Mar 19, 1997: STRINGER. CRACKED. TUL - STR 15R CRACKED AT STA 720B + 4 INCHES FORWARD OF WING ICE LIGHT HOUSING. REMOVED CRACKED SECTION OF STR 15R AND INSTALLED REPAIR PER SRM 53-10-3 FIGURE 1 - [SDR AALA970564](https://openairdocs.org/sdr/AALA970564), Mar 19, 1997: BELL FRAME. CRACKED. TUL - BS 540, BELL FRAME CRACKED .50 INCH AT FASTENER HOLE BETWEEN STR 8 AND STR 9R. ROUTED OUT CRACK AND INSTALLED DOUBLER PER SRM 53-10-4 PAGE 4 FIGURE 1. TST - [SDR AALA970563](https://openairdocs.org/sdr/AALA970563), Mar 19, 1997: HINGE BOX. CRACKED. TUL - FORWARD GALLEY DOOR UPPER HINGE BOX CRACKED AND HAS DEEP GOUGE. REMOVED AND REPLACED FORWARD GALLEY DOOR UPPER HINGE BOX PER SRM 51-10-1 PAGE 4. TST: 76,9 - [SDR AALA970562](https://openairdocs.org/sdr/AALA970562), Mar 19, 1997: STRINGER. CORRODED. TUL - CORROSION ON STR 21R AT STA 1031. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-10-3. TST: 61,615 HOURS. CYCLES: 20,785. (X) - [SDR AALA960725](https://openairdocs.org/sdr/AALA960725), May 5, 1996: RELAY. DEFECTIVE. FLT 1920 - ORD-BDL - DURING CRUISE, EMERGENCY FLOOR LIGHT SYSTEM UNCOMMANDED ILLUMINATION. AIRCRAFT PROCEEDED BDL AND LANDED WITHOUT INCIDENT. REPLACED EMERGENC - [SDR AALA950780](https://openairdocs.org/sdr/AALA950780), Apr 27, 1995: LIGHT SWITCH. DEFECTIVE. DFW - FLT NR 1902 - DURING DESCENT INTO DFW, ELECTRICAL BURNING SMELL NOTED IN COCKPIT. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. ## 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 19810107005109I](https://openairdocs.org/incident/19810107005109I), Jan 7, 1981: Boeing 727223 (N6822), Chicago, IL. Number three engine failed in climb. Found metal filings in tailpipe. Engine replaced. ## Other aircraft with N6822 - [Cancelled 1937-03-06](https://openairdocs.org/deregistered/N6822-1937-03-06): Waco GXE, S/N 1720. Owner: [Alderman Halsey C](https://openairdocs.org/faa-owner/ALDERMAN%20HALSEY%20C), [Endicott, NY](https://openairdocs.org/faa-place/NY/Endicott) --- 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.