# N312NE: 1969 Boeing 727-223, registration cancelled 2004-01-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 28, 2004
- Status when cancelled: Valid registration
- Airframe: [Boeing 727-223](https://openairdocs.org/model/boeing-727-223) (registry code 1384074)
- Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 20193
- Year built: 1969
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: September 24, 1969
- Last registry action: January 28, 2004
- Mode S code: A34F70
- Owner when cancelled: [Avsets.Com Inc](https://openairdocs.org/faa-owner/AVSETS.COM%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/N312NE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=312NE
- Page: https://openairdocs.org/deregistered/N312NE-2004-01-28

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 (81, newest 50)

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

- [SDR EISA20010117](https://openairdocs.org/sdr/EISA20010117), Aug 28, 2001: HYDRAULIC SYSTEM. LOW. AFTER TAKEOFF WITH GEAR UP AND FLAPS AT 2 DEGREES HYD SYS A QTY DROPPED TO 1.6 GALLONS. SERVICED A-SYSTEM HYDRAULICS, RAN ALL FLT CONTROLS, SYS OPS OK AND A-SYS
- [SDR EISA20010060](https://openairdocs.org/sdr/EISA20010060), Feb 14, 2001: SKIN. DELAMINATED. DURING ROUTINE C-CHECK INSPECTION FOUND DELAMINATION ON PANEL SKIN AT RT WING L/E AFT OF NR 5 KRUEGER FLAP. CLEANED PREPPED AREA BONDED FIBERGLASS OVERLAY, PRIM
- [SDR EISA20010058](https://openairdocs.org/sdr/EISA20010058), Feb 14, 2001: STRAP. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON FLOOR STRAP AT BS 1130 AND LBL 24.75 UNDERSIDE. FABRICATED AND INSTALLED FLOOR STRAP, ALODINED AND PRIMED I
- [SDR EISA20010057](https://openairdocs.org/sdr/EISA20010057), Feb 14, 2001: FLOORBEAM. GOUGED. DURING ROUTINE C-CHECK INSPECTION FOUND GOUGE AT MAIN CABIN FLOORBEAM BS 950 AT RBL 7. FABRICATED AND INSTALLED ANGLES, FILLER AND FLOORBEAM T-CAP AT BS 950 RBL
- [SDR EISA20010056](https://openairdocs.org/sdr/EISA20010056), Feb 14, 2001: SKIN. CRACKED. DURING ROUTINE C-CHECK INSPECTION FOUND MAIN CABIN SKIN CRACKED AT BS 1096 STRINGER 1. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AT BS 1096 STR 1, ALOD
- [SDR EISA20010055](https://openairdocs.org/sdr/EISA20010055), Feb 14, 2001: WEB. CRACKED. DURING ROUTINE C-CHECK INSPECTION FOUND LEFT WING NR 1 SLAT II/B WEB FOR ACTUATOR ATTACH POINT CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER, ALODINED, AND P
- [SDR EISA20010054](https://openairdocs.org/sdr/EISA20010054), Feb 14, 2001: FLOORBEAM. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION UNDER NUT PLATE ON FLOOR ANGLE AT BS 1148 12 FT LEFT OF BL 0 UNDER FLOOR SIDE. FABRICATED AND INSTALLED REPAIR
- [SDR EISA20010053](https://openairdocs.org/sdr/EISA20010053), Feb 14, 2001: STRINGER. GOUGED. DURING ROUTINE C-CHECK INSPECTION FOUND GOUGE AT STRINGER 25L BS 400. FABRICATED AND INSTALLED REPAIR DOUBLERS AT BS 400 STR 25L, ALODINED AND PRIMED IAW SRM 53
- [SDR EISA20010052](https://openairdocs.org/sdr/EISA20010052), Feb 14, 2001: FRAME. GOUGED. DURING ROUTINE C-CHECK INSPECTION FOUND GOUGE AT MAIN CABIN FRAME BS 1166 WL 210 LBL 63. FABRICATED AND INSTALLED REPAIR WEB AND FLOOR SUPPORT DOUBLER AND FILLE
- [SDR EISA20010051](https://openairdocs.org/sdr/EISA20010051), Feb 14, 2001: FLOORBEAM. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT BS 620 WL 208 RBL 65 TO RBL 70 FLOORBEAM UPPER CHORD LOWER SECTION. FABRICATED AND INSTALLED REPAIR ANGLE A
- [SDR EISA20010059](https://openairdocs.org/sdr/EISA20010059), Feb 14, 2001: FLOORBEAM. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND FLOORBEAM AT BS 1130 CORRODED AT NUT PLATES FROM RBL 62.5 TO LBL 62.5. FABRICATED AND INSTALLED REPAIR ANGLE AND RADIUS 
- [SDR EISA20010066](https://openairdocs.org/sdr/EISA20010066), Feb 14, 2001: STRINGER. CRACKED. DURING ROUTINE C-CHECK INSPECTION FOUND CRACK AT FORWARD CARGO COMPARTMENT, LOWER LOBE, STRINGER 26L EITHER SIDE OF BS 540 FRAME. STOP DRILLED, FABRICATED AND I
- [SDR EISA20010065](https://openairdocs.org/sdr/EISA20010065), Feb 14, 2001: SKIN. PUNCTURED. DURING ROUTINE C-CHECK INSPECTION FOUND RIGHT TRAILING EDGE FLAP HAS PUNCTURE HOLE. FABRICATED REPAIR DOUBLE, SEPTUM AND CONE FILLER, BONDED REPAIRS, ALODINED, 
- [SDR EISA20010064](https://openairdocs.org/sdr/EISA20010064), Feb 14, 2001: STRINGER. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND FORWARD CARGO COMPARTMENT, LOWER LOBE AREA STRINGER 27R BS 560 CORRODED. FABRICATED AND INSTALLED STRINGER SPLICE, ALODI
- [SDR EISA20010063](https://openairdocs.org/sdr/EISA20010063), Feb 14, 2001: STRINGER. CRACKED. DURING ROUTINE C-CHECK INSPECTION FOUND FORWARD CARGO COMPARTMENT, LOWER LOBE AREA STRINGER 25L CRACKED/CORRODED AT ATTACH POINT AT BS 580. FABRICATED AND INSTA
- [SDR EISA20010062](https://openairdocs.org/sdr/EISA20010062), Feb 14, 2001: SKIN. GOUGED. DURING ROUTINE C-CHECK INSPECTION FOUND LEFT WING INBOARD FOREFLAP INBOARD END UPPER AND LOWER SURFACES GOUGED. FABRICATED DOUBLER AND FILLER, BONDED REPAIR FIL
- [SDR EISA20010061](https://openairdocs.org/sdr/EISA20010061), Feb 14, 2001: FRAME. MISDRILLED. DURING ROUTINE C-CHECK INSPECTION FOUND DOUBLE DRILLED HOLES AT BS 950A STRINGER 8R TO 9R. FABRICATED AND INSTALLED ANGLE REPAIR, ALODINED AND PRIMED ANGLE REPA
- [SDR EISA20010050](https://openairdocs.org/sdr/EISA20010050), Feb 14, 2001: SPAR. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT RIGHT WING CENTER SECTION, REAR SPAR LOWER CHORD AND WEB. FABRICATED AND INSTALLED WEB REPAIR AND SPACERS A
- [SDR EISA20010049](https://openairdocs.org/sdr/EISA20010049), Feb 14, 2001: HINGE. ELONGATED. DURING ROUTINE C-CHECK INSPECTION FOUND MAIN CARGO DOOR HINGE AREA HAS ELONGATED HOLES. REAMED HOLES FABRICATED AND INSTALLED FREEZE PLUG BUSHINGS AND RADIUS FI
- [SDR EISA20010048](https://openairdocs.org/sdr/EISA20010048), Feb 14, 2001: ANGLE. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND Z-ANGLE CORRODED AT BS 570 TO BS 600, RBL 20. FABRICATED AND INSTALLED Z-ANGLE AND WEB REPAIR, ALODINED AND PRIMED IAW S
- [SDR EISA20010047](https://openairdocs.org/sdr/EISA20010047), Feb 14, 2001: FLOORBEAM. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND FLOORBEAM AT BS 1060 LOWER LEG CORRODED. FABRICATED AND INSTALLED 2 REPAIR ANGLES, ALODINED AND PRIMED ANGLE REPAIRS IAW
- [SDR EISA20010046](https://openairdocs.org/sdr/EISA20010046), Feb 14, 2001: SEAT TRACK. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CARGO COMPARTMENT RIGHT O/B SEAT TRACK SECTION FROM BS 580 TO BS 620. FABRICATED AND INSTALLED SEAT TR
- [SDR EISA20010045](https://openairdocs.org/sdr/EISA20010045), Feb 14, 2001: SEAT TRACK. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN CARGO COMPARTMENT LEFT I/B SEAT TRACK SECTION FROM BS 741 TO BS 757. FABRICATED AND INSTALLED SE
- [SDR EISA20010044](https://openairdocs.org/sdr/EISA20010044), Feb 14, 2001: SEAT TRACK. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN LEFT I/B SEAT TRACK SECTION FROM BS 757 TO BS 852 LBL 25. FABRICATED AND INSTALLED SEAT TRACK SP
- [SDR EISA20010043](https://openairdocs.org/sdr/EISA20010043), Feb 14, 2001: SEAT TRACK. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN CARGO COMPARTMENT LEFT O/B SEAT TRACK SECTION FROM BS 440 TO BS 480 LBL 45. FABRICATED AND INSTA
- [SDR EISA20010042](https://openairdocs.org/sdr/EISA20010042), Feb 14, 2001: BULKHEAD. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT AFT CARGO BULKHEAD BS 1060, WL 208. FABRICATED AND INSTALLED REPAIR FRAME DOUBLER, FILLER, AND REPAIR ANGLE
- [SDR EISA20010041](https://openairdocs.org/sdr/EISA20010041), Feb 14, 2001: SEAT TRACK. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN CARGO COMPARTMENT LEFT O/B SEAT TRACK SECTION FROM BS 757 TO BS 852 LBL 45.5. FABRICATED AND INS
- [SDR EISA20010040](https://openairdocs.org/sdr/EISA20010040), Feb 14, 2001: SEAT TRACK. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN CARGO COMPARTMENT LEFT O/B SEAT TRACK SECTION BS 720C TO 720E LBL 45. FABRICATED AND INSTALLED S
- [SDR EISA20020039](https://openairdocs.org/sdr/EISA20020039), Feb 14, 2001: SEAT TRACK. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT MAIN CABIN SEAT TRACK SECTION BS 920 TO BS 960 AT 0 BL. FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 92
- [SDR EISA20010038](https://openairdocs.org/sdr/EISA20010038), Feb 14, 2001: SEAT TRACK. CORRODED. DURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT MAIN CABIN SEAT TRACK SECTION BS 910 TO BS 950 LBL 24.75. FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 
- [SDR EISA20010037](https://openairdocs.org/sdr/EISA20010037), Feb 14, 2001: WEB. CRACKED. DURING ROUTINE C-CHECK INSPECTION FOUND CRACK AT BS 1195 WL 290 FWD OF ACCESSORY COMPRT LEFT SIDE OF AFT ENTRY DOOR. FABRICATED INSTALLED WEB REPAIR DOUBLER AND
- [SDR EISA20010036](https://openairdocs.org/sdr/EISA20010036), Feb 14, 2001: SKIN. DELAMINATED. DURING ROUTINE C-CHECK INSP FOUND RIGHT WING NR 11 SPOILER UPPER SURFACE DELAMINATED. CLEANED AND PREPPED AREA, BONDED FIBERGLASS OVERLAYS, PRIMED AND PAINTED A
- [SDR EISA20010035](https://openairdocs.org/sdr/EISA20010035), Feb 14, 2001: TRIM TAB. DAMAGED. DURING ROUTINE C-CHECK INSPECTION FOUND RT ELEVATOR TRIM TAB HAS HOLE WHERE SCREW WAS LOCATED. FABRICATED INSTALLED BUSHING, ALODINED AND PRIMED IAW REO-W00026,
- [SDR EISA20000199](https://openairdocs.org/sdr/EISA20000199), Nov 4, 2000: FUEL LINE. LEAKING. DURING CLIMBOUT, LOST THRUST ON NR 1 ENGINE. AIR TURNBACK TO (IND). FOUND FUEL LINE LEAKING. REMOVED AND REPLACED FUEL LINE, OPS CHECK GOOD IAW M/M 73-00.
- [SDR EISA200000051](https://openairdocs.org/sdr/EISA200000051), Jun 3, 2000: SHUTTLE VALVE. INOPERATIVE. NR 2 SLAT FAILED TO RETRACT AFTER TAKEOFF. COMPLETED ABNORMAL CHECK.
- [SDR EISA200000050](https://openairdocs.org/sdr/EISA200000050), Jun 2, 2000: WARNING LIGHT. ILLUMINATED. AFTER TAKEOFF FROM PDX, NR 2 LEADING EDGE FLAP AMBER LIGHTS BOTH FWD AND AFT PANEL WOULD NOT EXTINGUISH.
- [SDR 2000050](https://openairdocs.org/sdr/2000050), Jun 2, 2000: CONNECTOR. DIRTY. AFTER TAKEOFF FROM PDX, NR 2 LEADING EDGE FLAP AMBER LIGHTS BOTH FWD AND AFT PANEL WOULD NOT EXTINGUISH. CLEANED CONNECTOR, OPS CHECK GOOD IAW MM 27-81-00.
- [SDR EISA2000045](https://openairdocs.org/sdr/EISA2000045), Apr 19, 2000: SHUTOFF VALVE. FAILED. AIRCRAFT WILL NOT PRESSURIZE ON THE RIGHT PACK ONLY IN FLIGHT. REPAIRED WIRING TO LEFT PACK VALVE. OPS CHECK GOOD IAW MM 21-00. (M)
- [SDR EISA99217](https://openairdocs.org/sdr/EISA99217), Nov 16, 1999: DOOR. MISSING. B-SYSTEM SERVICE DOOR MISSING. PER MAINTENANCE THERE IS SHEET METAL DAMAGE, TO AIRFRAME, HINGE IS MISSING AND RIVETS PULLED. REPLACED DOOR ASSEMBLEY, DALFORT CO
- [SDR EISA99123](https://openairdocs.org/sdr/EISA99123), May 24, 1999: BULKHEAD WEB. GOUGED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND DRILL DAMAGE OF FS 1183 PRESSURE BULKHEAD AT WL 285 FROM LBL 18.2 TO RBL 18.2 (31 PLACES). REMOVED DAM
- [SDR 99ZZZM396](https://openairdocs.org/sdr/99ZZZM396), May 24, 1999: BULKHEAD WEB. GOUGED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND DRILL DAMAGE OF FS 1183 PRESSURE BULKHEAD AT WL 285 FROM LBL 18.2 TO RBL 18.2 (31 PLACES). REMOVED DAM
- [SDR EISA99119](https://openairdocs.org/sdr/EISA99119), May 17, 1999: SHEAR TIE. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND SHEAR TIE BROKEN AT FS 520 19R. REMOVED BROKEN SHEAR TIE, FABRICATED NEW PART PER SAMPLE AND INSTALLED 
- [SDR EISA99118](https://openairdocs.org/sdr/EISA99118), May 17, 1999: FRAME. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND FUSELAGE FRAME CRACKED AT FS 1166 LEFT AT WL 232.5. REMOVED DAMAGED AREA, FABRICATED REPAIR PER SRM 51-
- [SDR EISA99117](https://openairdocs.org/sdr/EISA99117), May 17, 1999: STRINGER. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND STRINGER 27L CRACKED AT FS 1050. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-40-2 
- [SDR EISA99116](https://openairdocs.org/sdr/EISA99116), May 17, 1999: BULKHEAD BEAM. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CRACK IN SUPPORT BEAM ON REAR BULKHEAD AT FS 1183 RBL 27, WL 262. REMOVED DAMAGED AREA PER SRM 51-40-4.
- [SDR EISA99115](https://openairdocs.org/sdr/EISA99115), May 17, 1999: FRAME. DEFORMED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND FORWARD LOWER CORNER OF FORWARD CARGO DOOR, GOUGED AND DEFORMED AT FS 620. REMOVED DAMAGED CORNER, POSI
- [SDR EISA99113](https://openairdocs.org/sdr/EISA99113), May 17, 1999: SEAT TRACK. CORRODED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CORROSION ON NR 1 SEAT TRACK AT FS 620. REMOVED SECTION TO TRACK FROM FS 620 TO 66O AND REPLACED WITH N
- [SDR EISA99112](https://openairdocs.org/sdr/EISA99112), May 17, 1999: SKIN. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CRACK IN LOWER SKIN ON LEFT ELEVATOR. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER SRM 55-2
- [SDR EISA99111](https://openairdocs.org/sdr/EISA99111), May 17, 1999: SKIN. CORRODED. DURING ACCOMPLISHMENT OF C-CHECK WORKCARD, FOUND CORROSION ON LOWER SKIN OF LEFT ELEVATOR, 42 INCH FROM OUTBOARD END. REMOVED CORROSION, FABRICATED AND INSTALLE
- [SDR EISA99110](https://openairdocs.org/sdr/EISA99110), May 17, 1999: SEAT TRACK. CORRODED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CORROSION OF SEAT TRACK AT FS 620 TO 720 LBL 24. REMOVED DAMAGE TRACK SECTION FROM FS 620 TO 720 AND RE

All 81: https://openairdocs.org/deregistered/N312NE-2004-01-28/reports.md

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