# N69739: 1975 Boeing 727-224, registration cancelled 2011-09-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 22, 2011
- Status when cancelled: Registration pending
- Airframe: [Boeing 727-224](https://openairdocs.org/model/boeing-727-224) (registry code 1384076)
- 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: 20667
- Year built: 1975
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: October 2, 1975
- Last registry action: August 19, 2011
- Mode S code: A9479A
- Location: [Guthrie, OK](https://openairdocs.org/faa-place/OK/Guthrie)
- Owner type: Individual
- Owner's area on the map: 35.8679° N, 97.4344° W: Placed by OpenAirDocs at the center of ZIP code 73044, within about 9 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N69739
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=69739
- Page: https://openairdocs.org/deregistered/N69739-2011-09-22

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 727-224: https://openairdocs.org/model/boeing-727-224.md

## Service difficulty reports (59, newest 50)

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

- [SDR GAIA05007ST](https://openairdocs.org/sdr/GAIA05007ST), Feb 28, 2005: SKIN. DENTED. DURING WALK AROUND, A DENT WAS FOUND ON THE FUSELAGE SKIN AT FS 343 STRINGER 24R. INSTALLED DOUBLER REPAIR IAW BOEING LETTER 1-17DF4Y AND KITTY HAWK EA B7-53-12
- [SDR GAIA05001ST](https://openairdocs.org/sdr/GAIA05001ST), Jan 14, 2005: BRACKET. CRACKED. DURING B-CHECK A CRACK WAS FOUND ON THE NR 3 SPOILER ACTUATOR ATTACH BRACKET AT WING STATION 501. REMOVED AND REPLACED SPOILER ACTUATOR ATTACH BRACKET. OPS CHEC
- [SDR GAIA04074OP](https://openairdocs.org/sdr/GAIA04074OP), May 14, 2004: ACTUATOR. LEAKING. NOTED ELEVATOR LOW PRESSURE LIGHT CAME ON, HYDRAULIC SYSTEM (A) QUANTITY INDICATED ZERO, SYSTEM (A) ENGINE PUMP LOW PRESSURE LIGHTS BLINKING. FLIGHT DIVERTED MA
- [SDR GAIA04055OP](https://openairdocs.org/sdr/GAIA04055OP), Mar 18, 2004: ACCESSORY UNIT. MALFUNCTIONED. FLT 772 - DTW-FWA - NOSE GEAR RED LIGHT ON GEAR ANNUNCIATOR PANEL CAME ON AFTER GEAR RETRACTION. RERACKED LANDING GEAR ACCESSORY UNIT. CYCLED GEAR NUMEROUS TIME
- [SDR GAIA04030OP](https://openairdocs.org/sdr/GAIA04030OP), Feb 18, 2004: COUPLER. DAMAGED. DURING TAXI, THE UPPER YAW DAMPER WAS CAUSING THE RUDDER TO SWING SIDE TO SIDE CAUSING VIBRATION. REMOVED AND REPLACED THE UPPER YAW DAMPER COUPLER. OPERATIONAL
- [SDR GAIA04012OP](https://openairdocs.org/sdr/GAIA04012OP), Feb 4, 2004: PROXIMITY SENSOR. OUT OF ADJUST. AFTER TAKEOFF THE FLIGHT CREW NOTICED THAT THE NOSE GEAR RED AND GREEN LIGHTS STAYED ON AFTER GEAR RETRACTION. THE AIRCRAFT WAS REROUTED. A NORMAL LANDING WAS M
- [SDR GAIA04011OP](https://openairdocs.org/sdr/GAIA04011OP), Feb 3, 2004: PROXIMITY SENSOR. DIRTY. AFTER TAKEOFF THE FLIGHT CREW NOTICED THAT THE NOSE GEAR RED AND GREEN LIGHTS STAYED ON AFTER GEAR RETRACTION. A NORMAL LANDING WAS MADE. CLEANED NOSE GEAR PROX
- [SDR GAIA03162OP](https://openairdocs.org/sdr/GAIA03162OP), Nov 19, 2003: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OP
- [SDR GAIA03160OP](https://openairdocs.org/sdr/GAIA03160OP), Nov 7, 2003: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE MAIN ENTRY EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. C/A: REMOVED AND REPLACED THE EMERGENCY EXIT L
- [SDR GAIA02074OP](https://openairdocs.org/sdr/GAIA02074OP), Jul 23, 2002: LIGHT. WILL NOT TEST. DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE LEFT FORWARD ENTRY DOOR, EMEREGNCY EXIT LIGHT WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT A
- [SDR GAIA01319OP](https://openairdocs.org/sdr/GAIA01319OP), Dec 18, 2001: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE L-1 EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT. OPERAT
- [SDR GAIA01106OP](https://openairdocs.org/sdr/GAIA01106OP), Mar 7, 2001: LIGHT. LOOSE. FLT 2031 - RNO-IND - DURING CRUISE, THE EMERGENCY EXIT LIGHT ILLUMINATED. THE AIRCRAFT LANDED WITHOUT ANY FURTHER DIFFICULITIES. FOUND THE EMERGENCY EXIT LIGHT 
- [SDR GAIA01045BOP](https://openairdocs.org/sdr/GAIA01045BOP), Feb 14, 2001: SHUTOFF VALVE. SHORTED. FLT 2724 - ROC-BOS - NR 2 ENGINE FAILED ON CLIMB-OUT. ATTEMPTED RESTART FAILED. DID HAVE OIL PRESSURE AND ROTATION. AIRCAFT MADE AN UNEVENTFUL RETURN TO ROC. FO
- [SDR GAIA01042](https://openairdocs.org/sdr/GAIA01042), Feb 1, 2001: LIGHT. INOPERATIVE. FLT 739 - OSC - AFTER COMPLETION OF C-CHECK MAINTENANCE, EMERGENCY EXIT LIGHTS UNABLE TO SWITCH OFF. RE-SEATED COCKPIT ENTRY ''EMERGENCY EXIT'' LIGHT. OPS CHECK
- [SDR GAIA01036](https://openairdocs.org/sdr/GAIA01036), Jan 29, 2001: DOOR FRAME. CRACKED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. THRESHOLD FRAME BOTTOM FLANGE AT THE C-1 DOOR, BS 593, RBL 20, FORWARD PIT
- [SDR GAIA01035](https://openairdocs.org/sdr/GAIA01035), Jan 29, 2001: FLOORBEAM. CRACKED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. FLOORBEAM UPPER SURFACE OF UPPER CHORD AT BS 420, RBL 45 IS CORRODED. REPA
- [SDR GAIA01034](https://openairdocs.org/sdr/GAIA01034), Jan 29, 2001: KEELBEAM. CRACKED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. KEELBEAM LOWER CHORD AT BS 873, CRACKED THROUGH FASTENER. REMOVED FASTENER
- [SDR GAIA01033](https://openairdocs.org/sdr/GAIA01033), Jan 29, 2001: SHEAR TIE. CORRODED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. CORROSION FOUND ON BELLY FRAME TO SKIN ATTACH ANGLE AT BS 600, LBL 3 TO RB
- [SDR GAIA01032](https://openairdocs.org/sdr/GAIA01032), Jan 29, 2001: FLOORBEAM. MISDRILLED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. FLOORBEAM UPPER CAP AT BS 360, RBL 63 HAS DOUBLER DRILLED HOLES. REMOVED D
- [SDR GAIA01031](https://openairdocs.org/sdr/GAIA01031), Jan 29, 2001: FRAME. DENTED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE ACILITY. CABIN FRAME DENTED AT BS 600, STRINGER 9R. FABRICATED REPAIR DOUBLER IAW B7
- [SDR GAIA01030](https://openairdocs.org/sdr/GAIA01030), Jan 29, 2001: SEAT TRACK. CORRODED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. SEAT TRACK AND FASTENERS AT BS 760 TO 870 RBL 25 CORRODED. REMOVED AND REP
- [SDR GAIA01029](https://openairdocs.org/sdr/GAIA01029), Jan 29, 2001: SPLICE. CORRODED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. SEAT TRACK SPLICE FOUND CORRODED AT BS 690 RBL 24. REMOVED SEAT TRACK SPLI
- [SDR GAIA01028](https://openairdocs.org/sdr/GAIA01028), Jan 29, 2001: FLOORBEAM. MISDRILLED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. FLOORBEAM UPPER CAP AT BS 344 HAS SEVERAL HOLES WITH NO EDGE DISTANCE. REM
- [SDR GAIA01027](https://openairdocs.org/sdr/GAIA01027), Jan 29, 2001: SEAT TRACK. CORRODED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY, COROSION FOUND ON SEAT TRACK AT BS 760 TO 870 RBL 45. REMOVED CORROSION IA
- [SDR GAIA01026](https://openairdocs.org/sdr/GAIA01026), Jan 29, 2001: SKIN. CORRODED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. CORROSION FOUND ON BILGE SKIN FROM BS 720D TO 720E, STRINGER 29L TO 29R. C
- [SDR GAIA01025](https://openairdocs.org/sdr/GAIA01025), Jan 29, 2001: SEAT TRACK. CORRODED. THIS ITEM WAS FOUND DURING ROUTINE NAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. CORROSION FOUND ON SEAT TRACK INBOARD FLANGE AT BS 634, OUTBOARD FLANGE AT
- [SDR GAIA01024](https://openairdocs.org/sdr/GAIA01024), Jan 29, 2001: SHEAR TIE. CORRODED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. CORROSION FOUND ON SHEAR TIE, FORWARD SIDE AT BS 700 BETWEEN STRINGER 27L 
- [SDR GAIA01023](https://openairdocs.org/sdr/GAIA01023), Jan 29, 2001: FLOORBEAM. CORRODED. THIS ITME WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. CABIN FLOORBEAM FOUND CORRODED ON UPPER SURFACE OF UPPER CHORD AT BS 400, 
- [SDR GAIA01022](https://openairdocs.org/sdr/GAIA01022), Jan 29, 2001: SEAT TRACK. CORRODED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. CORROSION FOUND AROUND FASTENERS IN SEAT TRACK AT LBL 45 FROM STATION 760 
- [SDR GAIA01021](https://openairdocs.org/sdr/GAIA01021), Jan 29, 2001: FRAME. CORRODED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. STATION 720E FORWARD SIDE OF CIRCUMFERENTIAL FRAME HAS CORROSION BETWEEN S
- [SDR GAIA01020](https://openairdocs.org/sdr/GAIA01020), Jan 29, 2001: FLOORBEAM. CORRODED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY, BS 1090 CABIN FLOORBEAM IS CORRODED AT THE LOWER CHORD AS SEEN FROM THE AF
- [SDR GAIA01019](https://openairdocs.org/sdr/GAIA01019), Jan 29, 2001: SEAT TRACK. CORRODED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. CORROSION AROUND FASTENERS IN SEAT TRACK AT LBL 25, STATION 760 TO 870. RE
- [SDR GAIA01018](https://openairdocs.org/sdr/GAIA01018), Jan 29, 2001: SEAT TRACK. CORRODED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. SEAT TRACK HAS CORROSION ON INBOARD FLANGE AT BS 686 AND BS 700. REMOVED D
- [SDR GAIA01017](https://openairdocs.org/sdr/GAIA01017), Jan 29, 2001: SEAT TRACK. DAMAGED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY, CENTER SEAT TRACK IS REQUIRED TO BE SPLICED AT BS 450 AND BS 550. REMOVED 
- [SDR GAIA01015](https://openairdocs.org/sdr/GAIA01015), Jan 29, 2001: FRAME. DENTED. THIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. DENT IN FRAME BETWEEN STRINGER 4R AND 5R AT FS 380. REMOVED DAMAGED AT STA
- [SDR GAIA00794](https://openairdocs.org/sdr/GAIA00794), Dec 22, 2000: WIRE. LACK OF LUBE. AFTER TAKE OFF, THE OUTBOARD FLAPS WOULD NOT RETRACT FROM 2 DEGREES TO ZERO DEGREES AND THE 2,3,6&7 LEADING EDGE FLAPS WOULD NOT RETRACT. PERFORMED OUTBOARD FLA
- [SDR GAIA00797](https://openairdocs.org/sdr/GAIA00797), Dec 6, 2000: MOTOR. WEAK. FLIGHT 739 FROM DFW TO BYH, AFTER TAKE OFF, THE OUTBOARD FLAPS REMAINED AT 15 DEGREES. EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT ANY F
- [SDR GAIA0040](https://openairdocs.org/sdr/GAIA0040), Jan 27, 2000: HANDLE. INOPERATIVE. FLT 1724 - TOL-BOS - AFTER TAKEOFF, THE CREW TRIED TO RETRACT THE GEAR AND FOUND THAT THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE FULL UP POSITION. ALL THREE 
- [SDR GAIA9950](https://openairdocs.org/sdr/GAIA9950), Apr 19, 1999: BATTERIES. DISCHARGED. DURING ROUTINE 'B' CHECK MAINTENANCE, FOUND TWO, EACH FORWARD EMERGENCY EXIT LIGHTS WITH DEAD BATTERIES. REMOVED AND REPLACED TWO FORWARD ENTRY AREA "EMERGENCY 
- [SDR GAIA9948](https://openairdocs.org/sdr/GAIA9948), Apr 9, 1999: ACCESSORY BOX. MALFUNCTION. ON FINAL APPROACH TO TOL, PUT GEAR DOWN AND 3 RED LIGHTS, AND 3 GREEN LIGHTS AND TAIL SKID LIGHT. RECYCLED GEAR AND GOT 3 GREEN LIGHTS, NORMAL INDICATIONS. AIRC
- [SDR GAIA9912](https://openairdocs.org/sdr/GAIA9912), Feb 4, 1999: SWITCH. DIRTY. AFTER DEPARTING TOL, CARGO DOOR ANNUNCIATOR FLICKERED. AIRCRAFT RETURNED TO TOL AND MADE AN UNEVENTFUL LANDING. CLEANED DIRT AND DEBRIS FROM (FORWARD BELLY) CAR
- [SDR GAIA98123](https://openairdocs.org/sdr/GAIA98123), Nov 13, 1998: FRAME. CORRODED. LEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. CABIN FRAME HAS CORROSION AT BS 1160, STRINGER 25L. REMOVED CORROSION AND DAMAGE. FABRICATE
- [SDR GAIA98122](https://openairdocs.org/sdr/GAIA98122), Nov 13, 1998: ANGLE. CORRODED. LEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. OUTER SIDE OF FLOORBEAM WEB, AFT ATTACH ANGLE IS CORRODED, BS 870, RBL 45. REMOVED CORROSIO
- [SDR GAIA98121](https://openairdocs.org/sdr/GAIA98121), Nov 13, 1998: FLOORBEAM. CORRODED. LEVEL 2 CORROSIO NFOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. MAIN CABIN FLOORBEAM HAS SURFACE CORROSION, TOP FLANGE, AT BS 1070 RBL 48 AND 53. REMOVED C
- [SDR GAIA98120](https://openairdocs.org/sdr/GAIA98120), Nov 13, 1998: FLOORBEAM. CORRODED. LEVEL 2 CORROSION FOUND DURNIG A TRANSITION LIGHT 'C' PHASE IN PLAN. MAIN CABIN FLOORBEAM TOP SURFACE HAS CORROSION AT BS 1070, RBL 53. REMOVED CORROSION FROM U
- [SDR GAIA98119](https://openairdocs.org/sdr/GAIA98119), Nov 13, 1998: ANGLE. CORRODED. LEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. MAIN CABIN FLOOR CHORD ANGLE HAS SURFACE CORROSION AT BS 1177, RBL 54 TO RBL 66. REMOVED CO
- [SDR GAIA98118](https://openairdocs.org/sdr/GAIA98118), Nov 13, 1998: FRAME. CORRODED. LEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. MAIN CABIN FUSELAGE CIRCUMFERENTIAL FRAME HAS SURFACE CORROSION AT BS 1148, STRINGER 16R TO
- [SDR GAIA98117](https://openairdocs.org/sdr/GAIA98117), Nov 13, 1998: FLOORBEAM. CORRODED. LEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. MAIN CABIN FLOOR CHORD AND UPPER ANGLE HAS SURFACE CORROSION AT BS 1176.9, LBL 61 - LBL 66.
- [SDR GAIA98116](https://openairdocs.org/sdr/GAIA98116), Nov 13, 1998: FLOORBEAM. CORRODED. LEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN, MAIN CABIN FLOORBEAM HAS SURFACE CORROSION ON TOP FLANGE, BS 1110, RBL 43. REMOVED CORROSIO
- [SDR GAIA9862A](https://openairdocs.org/sdr/GAIA9862A), Jun 15, 1998: CLAMP. FAILED. MKE - AFTER DEPARTING JUST PRIOR TO FLAP RETRACTION, THE NR 1 FIRE WARNING CAME ON. FIREWARNING LIGHT WENT OUT AFTER NR 1 THROTTLE WAS RETARDED. AIRCRAFT RETURN

All 59: https://openairdocs.org/deregistered/N69739-2011-09-22/reports.md

## FAA accident and incident reports (4)

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 20010210002599I](https://openairdocs.org/incident/20010210002599I), Feb 10, 2001: Boeing 727224 (N69739), Rochester, NY. (-23) On Saturday February 10, 2001, at 12:37 pm local time, a Boeing 727 aircraft, bearing registration number N69739, operated under 14 CFR part 121 as kitty…
- [Incident 19890109009039I](https://openairdocs.org/incident/19890109009039I), Jan 9, 1989: Boeing 727224 (N69739), Agana, Guam. NR3 engine oil temperature rose on climb. Shutdown and returned. Engine fuel heater valve stuck in open position.
- [Incident 19821104065279I](https://openairdocs.org/incident/19821104065279I), Nov 4, 1982: Boeing 727 (N69739), Chicago, IL, Minor damage. #3 Engine shut down due to low oil pressure. #2 engine generator tripped. Would not reset. Internal oil leak.
- [Incident 19791016052049I](https://openairdocs.org/incident/19791016052049I), Oct 16, 1979: Boeing 727 (N69739), San Antonio, TX, Minor damage. Both nose tires blown out on landing due to failure of the hydraulic debooster.

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