# N314NE: 1968 Boeing 727-223, registration cancelled 2004-02-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 26, 2004 - Status when cancelled: Valid registration - 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: 19495 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: November 26, 1968 - Certificate issued: June 10, 2003 - Last registry action: June 10, 2003 - Mode S code: A356DE - Owner when cancelled: [Avsets Com Inc](https://openairdocs.org/faa-owner/AVSETS%20COM%20INC) - Location: [Chandler, AZ](https://openairdocs.org/faa-place/AZ/Chandler) - Owner type: Corporation - Owner's area on the map: 33.2749° N, 111.9249° W: Placed by OpenAirDocs at the center of ZIP code 85226, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N314NE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=314NE - Page: https://openairdocs.org/deregistered/N314NE-2004-02-26 From the FAA registry file of November 5, 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 (82, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR EISA20010109](https://openairdocs.org/sdr/EISA20010109), Jul 26, 2001: ENGINE. INOPERATIVE. JUST AFTER ROTATION, SEVERAL COMPRESSOR STALLS WERE HEARD. GAUGES FOR #1 ENGINE SHOWED SOME FLUCTUATION; ENG. FAIL LIGHT FLASHED. ACCOMPANIED BY AUTO PACK TRIP. - [SDR EISA20010104](https://openairdocs.org/sdr/EISA20010104), Jul 6, 2001: LIGHT. INOPERATIVE. DURING APPROACH NOSE GEAR DOWN AND LOCKED LIGHT INOP. WOULD NOT PRESS TO TEST. RELAMPED BULB. - [SDR EISA20010021](https://openairdocs.org/sdr/EISA20010021), Feb 2, 2001: SEAT TRACK. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON SEAT TRACK AT RBL 45.50 BS 700. REMOVED CORRODED SECTION, FABRICATED SEAT TRACK LOCATED HOLES, ALODINED, PR - [SDR EISA20010020](https://openairdocs.org/sdr/EISA20010020), Feb 2, 2001: ANGLE. CRACKED. DURING ROUTINE C-CHECK INSPECTION FOUND ANGLE CRACKED IN LEFT WING LEADING EDGE OF NR 3 KRUEGER FLAP. REMOVED ANGLE, FABRICATED AND INSTALLED REPAIR ANGLE, ALOD - [SDR EISA20010019](https://openairdocs.org/sdr/EISA20010019), Feb 2, 2001: SEAT TRACK. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON SCREW HEADS ON SEAT TRACK RBL 24.50 FROM BS 480 TO BS 680. REMOVED SEAT TRACK, FABRICATED, TRIMMED, DRILLED - [SDR EISA20010018](https://openairdocs.org/sdr/EISA20010018), Feb 2, 2001: SEAT TRACK. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AROUND SCREW HEADS ON SEAT TRACK LBL 24.50 FROM BS 640 TO BS 720. REMOVED CORRODED SEAT TRACK FABRICATED, TRIM - [SDR EISA20010017](https://openairdocs.org/sdr/EISA20010017), Feb 2, 2001: SEAT TRACK. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AROUND FASTENER HEADS ON SEAT TRACK FROM BS 480 TO BS 580. REMOVED CORRODED SEAT TRACK SECTION, FABRICATED SEA - [SDR EISA20010016](https://openairdocs.org/sdr/EISA20010016), Feb 2, 2001: SKIN. CRACKED. DURING ROUTINE C-CHECK FOUND SEVERAL CRACK INDICATIONS ON EXTERNAL SKIN AND DOUBLER AT MAIN CARGO DOOR. STEP REAMED HOLES, FABRICATED FREEZE PLUG BUSHINGS, AND - [SDR EISA20010015](https://openairdocs.org/sdr/EISA20010015), Feb 2, 2001: MOUNT BRACKET. DAMAGED. DURING ROUTINE C-CHECK INSPECTION FOUND NR 3 ENGINE AFT MOUNT LOWER FLANGE HAS ELONGATED HOLES. FABRICATED FREEZE PLUGS, STAP, ALODINED, PRIMED, AND INSTALLED R - [SDR EISA20010014](https://openairdocs.org/sdr/EISA20010014), Feb 2, 2001: FRAME. PUNCTURED. DURING ROUTINE C-CHECK INSPECTION FOUND AFT UPPER CORNER AFT CARGO DOOR HAS HOLE IN FRAME. REMOVED AND REPLACED CORNER BRACE IAW SRM 51-20-4, 51-30-2. - [SDR EISA20010013](https://openairdocs.org/sdr/EISA20010013), Feb 2, 2001: SEAT TRACK. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON SEAT TRACK FROM BS 580 TO BS 620 LBL 45.50. REMOVED CORRODED SEAT TRACK, FABRICATED TRACK SPLICE, DRILLED D - [SDR EISA20010012](https://openairdocs.org/sdr/EISA20010012), Feb 2, 2001: SKIN. CRACKED. DURING ROUTINE C-CHECK INSPECTION FOUND SKIN CRACKED ON LEFT WING ABOVE NR 4 SLAT. ROUTED OUT CRACK, FABRICATED REPAIR DOUBLER, PRIMED, ALODINED, AND INSTALLED - [SDR EISA20010011](https://openairdocs.org/sdr/EISA20010011), Feb 2, 2001: ATTACH FITTING. CRACKED. DURING ROUTINE C-CHECK INSPECTION FOUND CRACKS AT TOP OF LEFT WING AT NR 2, 3, AND 4 SPOILER ATTACH POINTS. STOP DRILLED CRACKS, FABRICATED, INSTALLED, ALODINED - [SDR EISA20010010](https://openairdocs.org/sdr/EISA20010010), Feb 2, 2001: SKIN. DAMAGED. DURING ROUTINE C-CHECK INSPECTION FOUND HOLE IN LT ELEVATOR TAB UPPER SURFACE. CLEANED PREPPED AND POTTED .250 DIAMETER AREA, ALODINED, PRIMED, AND PAINTED. WEI - [SDR EISA20010009](https://openairdocs.org/sdr/EISA20010009), Feb 2, 2001: SKIN. DELAMINATED. DURING ROUTINE C-CHECK INSPECTION FOUND NR 4 AFT FLAP TRAILING EDGE DELAMINATED. REMOVED DELAMINATED AREAS OF FLAP TRAILING EDGE, CLEANED, PREPPED, ALODINED, PR - [SDR EISA20010008](https://openairdocs.org/sdr/EISA20010008), Feb 2, 2001: FRAME. CRACKED. DURING ROUTINE C-CHECK INSPECTION FOUND BS 620 FRAME WEB HAS CRACK STARTING AT LOWER TOOLING HOLE AND EXTENDING DOWN THROUGH FASTENER HOLE. CORRECTIVE ACTION: F - [SDR EISA20010007](https://openairdocs.org/sdr/EISA20010007), Feb 2, 2001: FRAME. DAMAGED. DURING ROUTINE C-CHECK INSPECTION FOUND ELONGATED HOLE AT BS 870. REAMED HOLE PER SB 53-0194 TO 402. - [SDR EISA20010006](https://openairdocs.org/sdr/EISA20010006), Feb 2, 2001: SUPPORT FITTING. DAMAGED. DURING ROUTINE C-CHECK INSPECTION FOUND OUTBOARD TRACK SUPPORT HAS ELONGATED HOLE. REAMED FITTING IAW SB 57-0134, ALODINED AND PRIMED IAW SRM 51-10-2. - [SDR EISA20010005](https://openairdocs.org/sdr/EISA20010005), Feb 2, 2001: FORMER. CRACKED. DURING ROUTINE C-CHECK INSPECTION FOUND CRACK AT NR 4 SLAT ACTUATOR INBOARD FORMER. STOP DRILLED CRACK, FABRICATED, REPAIR DOUBLER, ALODINED, PRIMED, AND INSTAL - [SDR EISA20010004](https://openairdocs.org/sdr/EISA20010004), Feb 2, 2001: STIFFENER. CRACKED. DURING ROUTINE C-CHECK INSPECTION, FOUND CRACK AT NR 2 SLAT ACTUATOR STIFFENER. REMOVED CRACKED STIFFENER, FABRICATED STIFFENER, DOUBLER AND FILLER, ALODINED, P - [SDR EISA200120025](https://openairdocs.org/sdr/EISA200120025), Feb 2, 2001: FRAME. CRACKED. DURING ROUTINE C-CHECK, INSPECTION FOUND CRACK AT BS 298 RBL 14. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED, AND INSTALLED REPAIR IAW SRM 51-10-1 PARA 9, 51-40 - [SDR EISA20010024](https://openairdocs.org/sdr/EISA20010024), Feb 2, 2001: ANGLE. CRACKED. DURING ROUTINE C-CHECK INSPECTION FOUND CRACKED ANGLE UNDER FLOOR PANEL AT BS 300 RBL 10. REMOVED ANGLE, FABRICATED, ALODINED, PRIMED, AND INSTALLED REPAIR ANGL - [SDR EISA20010023](https://openairdocs.org/sdr/EISA20010023), Feb 2, 2001: FRAME. DAMAGED. DURING ROUTINE C-CHECK INSPECTION FOUND HOLE IN FRAME AT STRINGER 17L. FABRICATED REPAIR DOUBLER, ALODINED, REPAIRED, AND INSTALLED REPAIR IAW SRM 51-30-2, 51-1 - [SDR EISA20010022](https://openairdocs.org/sdr/EISA20010022), Feb 2, 2001: ANGLE. CRACKED. DURING ROUTINE C-CHECK INSPECTION FOUND ANGLE CRACKED AT STATION 92L WING ROOT. FABRICATED REPAIR ANGLE, ALODINED, PRIMED, AND INSTALLED REPAIR ANGLE IAW SRM 51 - [SDR EISA2000054](https://openairdocs.org/sdr/EISA2000054), Jun 9, 2000: BRAKE. DAMAGED. FLT 746 - SAT - DURING TAXI OUT, BRAKES LOCKED AND AIRCRAFT CAME TO A STOP. NO ACTION WOULD RELEASE BRAKES. SERVICED DE-BOOST CYL AND CHANGED NR 1 BRAKE ASSY AN - [SDR EISA2000016](https://openairdocs.org/sdr/EISA2000016), Feb 15, 2000: ENGINE. LEAKING. NR 2 ENGINE OIL LOSS IN FLIGHT. PRECAUTIONARY SHUTDOWN OF ENGINE. (M) - [SDR EISA2000030](https://openairdocs.org/sdr/EISA2000030), Feb 11, 2000: O-RING. WORN. NR 2 ENGINE LOSING 1 QUART OF OIL EVERY 5-7 MINUTES. IN FLIGHT SHUT DOWN NR 2 ENGINE. REMOVED AND REPLACED O-RING ON OIL LINE FROM ENGINE OIL BYPASS SWITCH TO O - [SDR EISA99081](https://openairdocs.org/sdr/EISA99081), Mar 27, 1999: SKIN. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND 5 INCH CRACK ON RIGHT WING LEADING EDGE AT WS 456 ABOVE FUELING BAY. TRIMMED OUT DAMAGED AREA PER SRM - [SDR EISA99080](https://openairdocs.org/sdr/EISA99080), Mar 27, 1999: SEAT TRACK. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND LEFT OUTBOARD SEAT TRACK CRACKED AT BS 620-720. REMOVED DAMAGED SEAT TRACK FROM BS 620-720. FABRICATED - [SDR EISA99079](https://openairdocs.org/sdr/EISA99079), Mar 27, 1999: SEAT TRACK. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND RIGHT OUTBOARD SEAT TRACK CRACKED AT BS 520. REMOVED DAMAGED SEAT TRACK FROM BS 480-580. FABRICATED NE - [SDR EISA99078](https://openairdocs.org/sdr/EISA99078), Mar 27, 1999: RIB. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND INBOARD RIB AND RIB ATTACH ANGLE AT NR 1 SLAT ACTUATOR ATTACH POINT CRACKED. REMOVED AND REPLACED SLAT - [SDR EISA99077](https://openairdocs.org/sdr/EISA99077), Mar 27, 1999: RIB. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND NR 4 SLAT OUTBOARD SUPPORT RIB CRACKED. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED AND INSTALLED D - [SDR EISA99076](https://openairdocs.org/sdr/EISA99076), Mar 27, 1999: TIE CLIP. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND STRINGER TIE CRACKED AT BS 675, 527L. REMOVED DAMAGED PART, FABRICATED AND INSTALLED NEW STRINGER TIE - [SDR EISA99075](https://openairdocs.org/sdr/EISA99075), Mar 27, 1999: ANGLE. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND SUPPORT ANGLE CRACKED AT FS 720B, 525L. REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED NEW ANGLE PER S - [SDR EISA99074](https://openairdocs.org/sdr/EISA99074), Mar 27, 1999: STIFFENER. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND CRACKED STIFFENER ON FORWARD SIDE OF NR 2 ENGINE FIREWALL AT BS 1342.4, PREVIOUS REPAIR. REMOVED OLD R - [SDR EISA99073](https://openairdocs.org/sdr/EISA99073), Mar 27, 1999: FRAME. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND FRAME CRACKED AND DEFORMED AT BS 440, WL 210. TRIMMED DAMAGED SECTION PER SRM 51-40-3. FABRICATED AND - [SDR EISA99072](https://openairdocs.org/sdr/EISA99072), Mar 27, 1999: EXIT CASE. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND NR 3 ENGINE FAN EXIT CASE CRACKED RIGHT SIDE AT 2 O'CLOCK POSITION. REMOVED AND REPLACED FAN EXIT CASE - [SDR EISA99071](https://openairdocs.org/sdr/EISA99071), Mar 27, 1999: EXIT CASE. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND NR 3 ENGINE FAN EXIT CASE CRACKED AROUND STATOR ON LEFT SIDE AT 9 O'CLOCK POSITION JUST ABOVE CASE LIN - [SDR EISA99070](https://openairdocs.org/sdr/EISA99070), Mar 27, 1999: SUPPORT. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND CRACK AT NR 13 SPOILER ACTUATOR INBOARD SUPPORT ANGLE ON REAR SPAR. REMOVED CRACKED SUPPORT AND FABRIC - [SDR EISA99068](https://openairdocs.org/sdr/EISA99068), Mar 27, 1999: SKIN. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND A 2.5 INCH CRACK IN SKIN ON LEFT ELEVATOR LOWER SURFACE, 20 INCH AFT OF PANEL NR 9308. STOP DRILLED CR - [SDR EISA99067](https://openairdocs.org/sdr/EISA99067), Mar 27, 1999: SKIN. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND SKIN CRACKED ON NR 1 SLAT TRAINING EDGE AREA OUTBOARD SIDE AT OUTBOARD TRACK. REMOVED DAMAGED AREA. FAB - [SDR EISA99066](https://openairdocs.org/sdr/EISA99066), Mar 27, 1999: RIB. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND INBOARD RIB AND RIB ATTACH ANGLE CRACKED AT NR 1 SLAT ACTUATOR. REMOVED AND REPLACED SLAT WITH A SERVIC - [SDR EISA99065](https://openairdocs.org/sdr/EISA99065), Mar 27, 1999: RIB. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND NR 4 SLAT OUTBOARD SUPPORT CRACKED. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED AND INSTALLED DOUBLE - [SDR EISA99064](https://openairdocs.org/sdr/EISA99064), Mar 27, 1999: CASE. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND NR 3 ENGINE FAN EXIT CASE CRACKED AROUND STATOR ON LEFT SIDE AT 9 O'CLOCK POSITION AND RIGHT SIDE AT 2 - [SDR EISA98182](https://openairdocs.org/sdr/EISA98182), Jul 23, 1998: FIRE LOOP. FAILED. ON PRE-FLIGHT, FOUND NR 1 ENGINE FIRE LIGHT WOULD NOT ILLUMINATE WHEN TESTED. FIRE BELL WORKED OK. GENERATED FROM PILOT REPORT. CORRECTIVE ACTION: REMOVED AND R - [SDR EISA98167](https://openairdocs.org/sdr/EISA98167), Jul 7, 1998: STRUT. OVERHEAT. AT 1,000 FEET, AGL ON REDUCED POWER TAKEOFF OUT OF DFW, AIRCRAFT INDICATED NR 1 STRUT OVERHEAT. LIGHT EXTINGUISHED 2 MINUTES AFTER THROTTLE RETARDED. GENERATED - [SDR EISA97280](https://openairdocs.org/sdr/EISA97280), Dec 13, 1997: SWITCH. MALFUNCTIONED. TAKEOFF, AURAL WARNING SOUNDS AT ALL TIMES. REMOVED AND REPLACED UPPER STABILIZER TRIM SWITCH. (X) - [SDR EISA97167](https://openairdocs.org/sdr/EISA97167), Jul 26, 1997: CONNECTOR. LOOSE. ON CLIMB-OUT LAX, NR 2 ENGINE OIL TEMP EXCEEDED THE RED LINE. ACCOMPLISHED ABNORMAL HIGH ENGINE OIL TEMP CHECKLIST, PERFORMED ENGINE FAILURE/FIRE/DAMAGE CHECKLI - [SDR EISA96283](https://openairdocs.org/sdr/EISA96283), Dec 13, 1996: ADC. INOPERATIVE. F/O'S AIRSPEED AND ALTIMETER INTERMITTENTLY INOP. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER. OPS CHECK NORMAL. (M) - [SDR EISA96284](https://openairdocs.org/sdr/EISA96284), Nov 1, 1996: CLIP. CRACKED. DURING A SCHEDULED D-CHECK, FOUND STRINGER TIE CLIPS AT VARIOUS STATIONS CRACKED FROM BS 560 TO 1050. REPLACED CLIPS PER SRM 51-10-1 AND 51-30-2. (M) All 82: https://openairdocs.org/deregistered/N314NE-2004-02-26/reports.md ## Other aircraft with N314NE - [Registered now](https://openairdocs.org/aircraft/N314NE): Piper PA-28-161, S/N 287716112 --- 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.