# N6839: 1969 Boeing 727-223, registration cancelled 2006-06-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 22, 2006
- 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-5](https://openairdocs.org/engine/pratt-whitney-jt8d-5) (registry code 52046)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 20192
- Year built: 1969
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: September 5, 1969
- Certificate issued: January 10, 1995
- Last registry action: February 17, 2004
- Mode S code: A911EF
- 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: 32.7883° N, 96.7996° W: Placed by OpenAirDocs at the center of ZIP code 75201, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N6839
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=6839
- Page: https://openairdocs.org/deregistered/N6839-2006-06-22

From the FAA registry file of November 3, 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 (41)

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

- [SDR EISA20010129](https://openairdocs.org/sdr/EISA20010129), Oct 16, 2001: LIGHT. INOPERATIVE. FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FWD EMERGENCY EXIT LIGHT ASSY IAW B727 MM 33, OPS CHECK GOOD.
- [SDR EISA20010075](https://openairdocs.org/sdr/EISA20010075), Apr 15, 2001: GARLOCK SEAL. DAMAGED. NR 2 ENGINE OIL QUANTITY LOSS IN FLIGHT AT RATE OF 3 GALLONS PER HOUR. AIR TURNBACK TO (IND). FOUND GARLOCK SEAL DAMAGED BEHIND HYDRAULIC A-PUMP. REMOVED AND RE
- [SDR EISA20000228](https://openairdocs.org/sdr/EISA20000228), Dec 21, 2000: WARNING LIGHT. ILLUMINATED. NR 6 L/E FLAP LIGHT ON INFLIGHT. AIR TURNBACK TO LAX. COULD NOT DUPLICATE ON GROUND. OPS CHECK GOOD.
- [SDR EISA20000226](https://openairdocs.org/sdr/EISA20000226), Dec 21, 2000: CONNECTOR. DIRTY. AFTER TAKEOFF, DURING FLAP RETRACTION NR 6 LEADING EDGE FLAP FAILED TO RETRACT WHEN FLAPS UP WAS SELECTED. POSITION TRANSMITTER CANNON PLUG, CLEANED WITH CONTAC
- [SDR EISA20000208](https://openairdocs.org/sdr/EISA20000208), Nov 30, 2000: RELAY. INOPERATIVE. EMERGENCY EXIT LIGHTS INOP. STAY ON IN ARMED POSITION. CORRECTIVE ACTION: REMOVED AND REPLACED R70 RELAY. SYSTEM OPS CHECK GOOD PER M/M 33-50.
- [SDR EISA20000209](https://openairdocs.org/sdr/EISA20000209), Nov 30, 2000: LIGHT. INOPERATIVE. FORWARD ENTRY EMERGENCY EXIT LIGHT INOP. CORRECTIVE ACTION: REPLACED FORWARD ENTRY EMERGENCY LIGHT ASSEMBLY PER M/M 33-50.
- [SDR EISA2000043](https://openairdocs.org/sdr/EISA2000043), Feb 11, 2000: ACTUATOR. CRACKED. AFTER TAKEOFF, FLAPS UP APPROXIMATELY 225 INDICATED AIR SPEED AIRCRAFT WENT INTO LEFT BANK. HAD TO USE 30 DEGREES RIGHT AILERON TRIM TO BRING AIRCRAFT BACK TO L
- [SDR EISA2000015](https://openairdocs.org/sdr/EISA2000015), Feb 11, 2000: ACTUATOR. FAILED. AFTER TAKEOFF FLAPS UP APPROX 225 IAS AIRCRAFT WENT INTO LEFT BANK, HAD TO USE 30 DEGREES RIGHT AILERON TRIM TO BRING AIRCRAFT BACK TO LEVEL FLIGHT. AIR TURN BA
- [SDR EISA99085](https://openairdocs.org/sdr/EISA99085), Apr 22, 1999: RESERVOIR. REQ'D SERVICE. LEADING EDGE FLAPS LIGHT ON AFTER TAKEOFF, FLAPS SELECTED UP NR 2 SLAT DID NOT RETRACT. HYDRAULIC QUANTITY FLUCTUATES FROM 4 TO 2.4 GALLONS. AIR TURN BACK TO BR
- [SDR EISA98240](https://openairdocs.org/sdr/EISA98240), Sep 20, 1998: LINE. OUT OF POSITION. NR 3 STRUT OVERHEAT LIGHT ILLUMINATED AFTER APPLYING CLIMB POWER. AIR TURNBACK TO CPH. GENERATED BY PILOT REPORT. REPOSITIONED BLEED AIR SHUT-OFF LINE. OPS CHEC
- [SDR EISA98222](https://openairdocs.org/sdr/EISA98222), Sep 20, 1998: VALVE. OUT OF POSITION. NR 3 STRUT OVERHEAT LIGHT ILLUMINATED AFTER APPLYING CLIMB POWER. AIR TURN TACK TO CHP. GENERATED FROM PILOT REPORT. REPOSITIONED AND TIGHTENED MODULAR VALVE AN
- [SDR EISA98218](https://openairdocs.org/sdr/EISA98218), Sep 15, 1998: VALVE. MALFUNCTIONED. ON DEPARTURE FROM EMA, NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. PERFORMED CHECKLIST PER AFM VOLUME 1 LIGHT EXTINGUISHED. CONTINUED FLIGHT TO BRU. GENERATED
- [SDR EISA97209](https://openairdocs.org/sdr/EISA97209), Oct 21, 1997: VALVE. LEAKING. ON TAKEOFF FROM BRU, THE NR 2 FIRE WARNING SOUNDED SHORTLY AFTER TAKEOFF, RETURNED TO BRU (ATB). FOUND UPPER LEFT ANTI-ICE VALVE LEAKING, RESECURED VALVE, AND R
- [SDR EISA97075](https://openairdocs.org/sdr/EISA97075), Mar 18, 1997: ACTUATOR. FAILED. NR 3 SLAT FAILED TO RETREAT. REMOVED AND REPLACED SLAT ACTUATOR AND SWITCH. (M)
- [SDR 97ZZZM483](https://openairdocs.org/sdr/97ZZZM483), Mar 18, 1997: SWITCH. FAILED. NR 3 SLAT FAILED TO RETREAT. REMOVED AND REPLACED SLAT ACTUATOR AND SWITCH. REFERENCE EISA97075.
- [SDR EISA97022](https://openairdocs.org/sdr/EISA97022), Jan 24, 1997: FRAME. CRACKED. FOUND FRAME CRACKED, TOP OF GALLEY DOOR FRAME FS 380R. REPAIRED PER SRM 53-10-4 AND 51-30-2. (M)
- [SDR EISA97021](https://openairdocs.org/sdr/EISA97021), Jan 24, 1997: FRAME. CRACKED. FRAME CRACKED, 10 INCHES ABOVE GALLEY DOOR FS 400R. REPAIRED FRAME PER SRM 53-10-4 AND 51-30-2. (M)
- [SDR EISA97019](https://openairdocs.org/sdr/EISA97019), Jan 24, 1997: BULKHEAD. CRACKED. TWO CRACKS IN FS 178 BULKHEAD JUST TO THE LEFT AND SLIGHTLY ABOVE CENTER POINT. INSTALLED REPAIR PER SB 727-53-0123 USING KIT 65C 36289-2. (M)
- [SDR EISA97016](https://openairdocs.org/sdr/EISA97016), Jan 24, 1997: BULKHEAD FITTING. CRACKED. FOUND CRACKED FITTING AT 1183 BULKHEAD, LBL 22, WL LBL 22, WL 244.4. INSTALLED NEW FITTING PER SRM 51-10-2. (M)
- [SDR EISA97015](https://openairdocs.org/sdr/EISA97015), Jan 24, 1997: BULKHEAD FITTING. CRACKED. FOUND CRACKED FITTING AT 1183 BULKHEAD, LBL 22, WL LBL 22, WL 235.9. INSTALLED NEW FITTING PER SRM 51-10-2. (M)
- [SDR EISA97007](https://openairdocs.org/sdr/EISA97007), Jan 24, 1997: SKIN. DENTS. NUMEROUS DENTS ON LEFT ELEVATOR TAB SKIN. REPAIRED TAB PER SRM 51-40-1 PAINT AND REBALANCE PER SRM 51-80-9 AND 51-20-13. (M)
- [SDR EISA97031](https://openairdocs.org/sdr/EISA97031), Jan 22, 1997: CLIP. CRACKED. FOUND 13 STRINGER TIE CLIPS CRACKED FROM FS 950C THROUGH FS 1090 FROM STRINGER 4L TO 4R. REMOVED AND REPLACED TIE CLIPS PER SRM 51-10-1. (M)
- [SDR EISA97030](https://openairdocs.org/sdr/EISA97030), Jan 22, 1997: CLIP. CRACKED. FOUND 29 STRINGER TIE CLIPS CRACKED FROM FS 420 THROUGH FS 804 FROM STRINGER 9L TO 4R. REMOVED AND REPLACED TIE CLIPS PER SRM 51-10-1. (M)
- [SDR EISA97029](https://openairdocs.org/sdr/EISA97029), Jan 22, 1997: SKIN. HOLE. LEFT INBOARD FLAP, AFT FLAP INBOARD END HAS A SMALL HOLE. REPAIRED HOLE PER SRM 51-40-6. (M)
- [SDR EISA97028](https://openairdocs.org/sdr/EISA97028), Jan 22, 1997: ANGLE. CORRODED. FOUND CORROSION ON OUTBOARD FLOOR SUPPORT ANGLE FS 720-720A. FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 51-40-4. (M)
- [SDR EISA97027](https://openairdocs.org/sdr/EISA97027), Jan 22, 1997: SUPPORT. CRACKED. NR 3 FLAP CARRIAGE LINK SUPPORT FITTING CRACKED. REMOVED AND REPLACED SUPPORT PER MM 27-51-0. (M)
- [SDR EISA97026](https://openairdocs.org/sdr/EISA97026), Jan 22, 1997: STRINGER. CRACKED. RIGHT WING, WS 686.5, CRACKED FLANGE ON TOP STRINGER, 23 INCHES AFT OF LEADING EDGE. FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 57-10-4. (M)
- [SDR EISA97025](https://openairdocs.org/sdr/EISA97025), Jan 22, 1997: SUPPORT. CRACKED. LEFT INBOARD FLAP, INBOARD CARRIAGE, MIDFLAP BEAM LINK SUPPORT CRACKED. REMOVED AND REPLACED SUPPORT ASSEMBLY PER MM 27-51-0. (M)
- [SDR EISA97024](https://openairdocs.org/sdr/EISA97024), Jan 22, 1997: INTERCOSTAL. CORRODED. MAIN CABIN FS 1090, RBL 61, INTERCOSTAL CORRODED ON LOWER SIDE. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8. (M)
- [SDR EISA97023](https://openairdocs.org/sdr/EISA97023), Jan 22, 1997: INTERCOSTAL. CORRODED. MAIN CABIN FS 1110, LBL 59, CORROSION ON UNDERSIDE OF INTERCOSTAL. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-2. (M)
- [SDR EISA97020](https://openairdocs.org/sdr/EISA97020), Jan 21, 1997: STIFFENER. CRACKED. X-RAY INDICATES CRACK AND MISSING MATERIAL INTERNAL ON RT ELEVATOR, INBOARD END. FABRICATED AND INSTALLED REPAIR PARTS PER 51-10-1 AND 51-30-2. (M)
- [SDR EISA97018](https://openairdocs.org/sdr/EISA97018), Jan 21, 1997: FRAME. CORRODED. INTERGRANULAR CORROSION ON DOOR CUT OUT FRAME WEB AND OUTBOARD INTERCOSTAL, RT SIDE OF FORWARD AND E/E DOOR. FABRICATED NEW WEB AND ANGLE PER SRM 51-40-1 AND IN
- [SDR EISA97017](https://openairdocs.org/sdr/EISA97017), Jan 21, 1997: VENT BOX. CRACKED. RIGHT WING VENT BOX CRACKED AT WS 686. FABRICATED AND INSTALLED REPAIR PER SRM 57-10-4. (M)
- [SDR EISA97014](https://openairdocs.org/sdr/EISA97014), Jan 21, 1997: STIFFENER. CRACKED. FS 1183 BULKHEAD VERTICAL STIFFENER HAS CRACK IN FLANGE AT RBL 40. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-4. (M)
- [SDR EISA97013](https://openairdocs.org/sdr/EISA97013), Jan 21, 1997: SKIN. CRACKED. UPPER WING SKIN CRACKED AT NR 4 SPOILER OUTBOARD HINGE. FABRICATED AND INSTALLED REPAIR PER SRM 57-30-4. (M)
- [SDR EISA97012](https://openairdocs.org/sdr/EISA97012), Jan 21, 1997: PANEL. CRACKED. DENT WITH CRACK ON UPPER WING PANEL 34 INCHES FORWARD OF NR 6 SPOILER. REPAIRED PANEL PER SRM 51-40-6. (M)
- [SDR EISA97011](https://openairdocs.org/sdr/EISA97011), Jan 21, 1997: SKIN. DELAMINATED. NR 1 SPOILER SKIN DELAMINATED, LOWER INBOARD FORWARD CORNER. REPAIRED SPOILER PER SRM 51-40-6. (M)
- [SDR EISA97010](https://openairdocs.org/sdr/EISA97010), Jan 21, 1997: SKIN. DELAMINATION. RIGHT WING OUTBOARD AILERON TAB SKIN HAS AREA OF DELAMINATION. REPAIRED TAB PER SRM 57-50-5. (M)
- [SDR EISA97009](https://openairdocs.org/sdr/EISA97009), Jan 21, 1997: SUPPORT. CRACKED. FLOOR SUPPORT FRAME BETWEEN FS 1070 AND 1090 ABOVE STRINGER 27L IS CRACKED. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-2. (M)
- [SDR EISA97008](https://openairdocs.org/sdr/EISA97008), Jan 21, 1997: SKIN. CREASE. FS 188, 6 INCH CREASE IN SKIN AT STRINGER 23L. COLD WORKED AREA PER SRM 51-30-10. HFEC REVEALS NO CRACKS. INSTALLED FASTENERS PER SRM 51-30-2. (M)
- [SDR EISA96145](https://openairdocs.org/sdr/EISA96145), Aug 20, 1996: ENGINE. CASE CRACK. NR 1 ENGINE WOULD NOT MAKE TAKEOFF POWER. BOROSCOPED ENGINE FOUND INTERMEDIATE CASE AT 8TH STAGE BLEED BOSS CRACKED. REMOVED AND REPLACED ENGINE. (M)

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