# N315NE: 1969 Boeing 727-223, registration cancelled 2008-02-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 29, 2008 - Exported to: Côte d’Ivoire - 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: 20190 - Year built: 1969 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: July 11, 1969 - Certificate issued: September 5, 2007 - Last registry action: September 5, 2007 - Mode S code: A35A95 - Owner when cancelled: [Airsmith Inc](https://openairdocs.org/faa-owner/AIRSMITH%20INC) - Location: [Opa Locka, FL](https://openairdocs.org/faa-place/FL/Opa%20Locka) - Owner type: Corporation - Owner's area on the map: 25.9080° N, 80.2575° W: Placed by OpenAirDocs at the center of ZIP code 33054, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N315NE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=315NE - Page: https://openairdocs.org/deregistered/N315NE-2008-02-29 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 (102, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR EISA20010101](https://openairdocs.org/sdr/EISA20010101), Jun 17, 2001: CREASE BEAM. CRACKED. LT FUSELAGE CREASE BEAM WEB IS CRACKED AT BS 1090 FLOOR LEVEL. CUT OUT CRACKED AREA. FABRICATED AND INSTALLED WEB AND FILLER ANGLE. REPAIRS IAW B727 SRM 51-30-2 - [SDR EISA20010100](https://openairdocs.org/sdr/EISA20010100), Jun 17, 2001: FLOORBEAM. CORRODED. AFT PIT-CABIN FLOORBEAM BS 1110 RBL 22 AFT SIDE EXFOLIATED AT NUT CLIP. CUT OUT CORRODED SECTION OF THE UPPER FLANGE OF FLOORBEAM, FABRICATED AND INSTALLED FILL - [SDR EISA20010099](https://openairdocs.org/sdr/EISA20010099), Jun 16, 2001: FLOORBEAM. CRACKED. FLOORBEAM IS CRACKED IN THE RT MID CABIN AT BS 848, UNDER THE O/B, RT SEAT TRACK APPROX 10 INCHES LONG IN LENGTH. REMOVED CRACKED SECTION. FABRICATED AND INSTAL - [SDR EISA20010070](https://openairdocs.org/sdr/EISA20010070), Mar 12, 2001: FLAP. DELAMINATED. DURING ROUTINE B-CHECK INSPECTION, FOUND RT INBOARD LOWER FLAP HAS DELAMINATED AREA. BONDED FIBERGLASS OVERLAYS TO REPAIR DOUBLER AND FILLER, ALODINED, SEALED A - [SDR EISA20010031](https://openairdocs.org/sdr/EISA20010031), Feb 24, 2001: CONNECTOR. LOOSE. NR 8 LEADING EDGE SLAT HAD BOTH AMBER LIGHTS ON IN AGREEMENT, PILOT STATED THAT HE COULD FEEL VIBRATION. THE AIRCRAFT OVERFLEW DFW TO IND. INSPECTED NR 8 ACTUAT - [SDR EISA20000195](https://openairdocs.org/sdr/EISA20000195), Oct 29, 2000: CYLINDER. INTERMITTENT. PERFORMED MANUAL NOSE GEAR EXTENSION INTO (JFK). REMOVED AND REPLACED NOSE GEAR TRANSFER CYLINDER AND REDUCER VALVE. - [SDR EISA20000147](https://openairdocs.org/sdr/EISA20000147), Sep 12, 2000: COUPLER. INOPERATIVE. ON TAKEOFF UPPER YAW DAMPER INOP. AIR TURNBACK TO (IND). REMOVED AND REPLACED YAW DAMPER COUPLER. OPS CHECK NORMAL. - [SDR EISA20000131](https://openairdocs.org/sdr/EISA20000131), Aug 27, 2000: FLOW VALVE. INOPERATIVE. UNABLE TO MAINTAIN CABIN PRESSURE. LEFT PACK APPEARS TO BE INOP, RETURNED TO IND. REMOVED AND REPLACED NEW FLOW CONTROL VALVE, OPS CHECK NORMAL, PER M/M 36-10. - [SDR EISA2000029](https://openairdocs.org/sdr/EISA2000029), Mar 7, 2000: RIVET. SHEARED. TAILSKID LIGHT REMAINED ON AFTER GEAR UP. REPLACED SHEARED RIVETS IN ENERGY ABSORBER IAW 32-71-71. ADJUSTED SWITCH IAW 3271-91. (M) - [SDR EISA99179](https://openairdocs.org/sdr/EISA99179), Oct 7, 1999: SKIN. CORRODED. DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND CORROSION ON RIGHT WING LOWER SURFACE OF AT WS 491.5 TO 505 BETWEEN STRINGER 5 AND 6. REMOVED CORR - [SDR EISA99178](https://openairdocs.org/sdr/EISA99178), Oct 7, 1999: SKIN. CORRODED. DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND CORROSION ON LOWER SURFACE OF RIGHT WING AT WS 460 BETWEEN STRINGER 8 AND 9. REMOVED CORROSION PER - [SDR EISA99204](https://openairdocs.org/sdr/EISA99204), Oct 5, 1999: FITTING. MISDRILLED. DURING REPLACEMENT OF VERTICAL FIN FRONT SPAR UPPER RIGHT TERMINAL FITTING AND SUBSEQUENT REMOVAL OF PREVIOUS REPAIR FOUND MIS-DRILLED HOLES IN LEFT HAND TERMIN - [SDR EISA99203](https://openairdocs.org/sdr/EISA99203), Oct 5, 1999: SKIN. CORRODED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CORROSION ON RIGHT WING LOWER SURFACE FROM WS 460 TO 650 AROUND FASTENERS. REMOVED CORROSION AND MATERI - [SDR EISA99205](https://openairdocs.org/sdr/EISA99205), Sep 14, 1999: FITTING. CRACKED. DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND 1 INCH CRACK IN VERTICAL FIN SPAR TERMINAL FITTING RIGHT SIDE. REMOVED DAMAGED FITTING REPLACED WITH - [SDR EISA99202](https://openairdocs.org/sdr/EISA99202), Sep 14, 1999: TIE CLIP. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 348, STRINGER 25R. FABRICATED NEW TIE CLIP PER SAMPLE, TREATED AND PRIMED PER SR - [SDR EISA99201](https://openairdocs.org/sdr/EISA99201), Sep 14, 1999: TIE CLIP. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 277, STRINGER 25R. FABRICATED NEW TIE CLIP PER SAMPLE, TREATED AND PRIMED PER SR - [SDR EISA99200](https://openairdocs.org/sdr/EISA99200), Sep 14, 1999: TIE CLIP. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 400 STRINGER 26L. FABRICATED NEW TIE CLIP PER SAMPLE, TREATED AND PRIMED PER SRM - [SDR EISA99199](https://openairdocs.org/sdr/EISA99199), Sep 14, 1999: SKIN. DELAMINATED. DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND DELAMINATION AT TRAILING EDGE OF RIGHT INBOARD AFT FLAP. REMOVED DAMAGED AREA. INSTALLED NEW HONEYCOM - [SDR EISA99198](https://openairdocs.org/sdr/EISA99198), Sep 14, 1999: SKIN. DELAMINATED. DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND RIGHT INBOARD MID FLAP DELAMINATED AT TRAILING EDGE AT WBL 200. REMOVED DAMAGED SKIN PER SRM 51-40-6. - [SDR EISA99197](https://openairdocs.org/sdr/EISA99197), Sep 14, 1999: SKIN. CRACKED. DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND CRACK AT INBOARD OF RIGHT INBOARD FOREFLAP. REMOVED DAMAGED AREA, REPAIRED INBOARD TIP WITH POTTING C - [SDR EISA99196](https://openairdocs.org/sdr/EISA99196), Sep 14, 1999: SKIN. CORRODED. DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND CORROSION ON NR 2 FUEL TANK LOWER SURFACE AT FS 800 RBL 18. REMOVED CORROSION, MATERIAL LOSS OUT OF L - [SDR EISA99195](https://openairdocs.org/sdr/EISA99195), Sep 14, 1999: SUPPORT. CORRODED. DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND CORROSION AT FS 805 WING CENTER FUEL TANK ABOVE AFT END OF RIGHT HEAT EXCHANGER ON STRUCTURE SUPPORT - [SDR EISA99194](https://openairdocs.org/sdr/EISA99194), Sep 14, 1999: SKIN. CORRODED. DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND CORROSION ON NR 2 FUEL TANK LOWER SURFACE AT FS 805, LBL 18. REMOVED CORROSION, MATERIAL LOSS OUT OF - [SDR EISA99193](https://openairdocs.org/sdr/EISA99193), Sep 14, 1999: TIE CLIP. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 480 STRINGER 23L. FABRICATED NEW TIE CLIP PER SAMPLE, TREATED AND PRIMED PER SRM - [SDR EISA99192](https://openairdocs.org/sdr/EISA99192), Sep 14, 1999: TIE CLIP. CRACKED. DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 480 STRINGER 22L. FABRICATED NEW TIE CLIP PER SAMPLE, TREATED AND PRIMED PER S - [SDR EISA99191](https://openairdocs.org/sdr/EISA99191), Sep 14, 1999: TIE CLIP. CRACKED. DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 480 STRINGER 20L. FABRICATED NEW CLIP PER SAMPLE, TREATED AND PRIMED PER SRM 5 - [SDR EISA99190](https://openairdocs.org/sdr/EISA99190), Sep 14, 1999: TIE CLIP. CRACKED. DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND TIE CLIP CRACKED AT FS 480 STRINGER 19L. FABRICATED NEW CLIP PER SAMPLE, TREATED AND PRIMED PER SRM - [SDR EISA99189](https://openairdocs.org/sdr/EISA99189), Sep 14, 1999: TIE CLIP. CRACKED. DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND TIE CLIP CRACKED AT FS 500 STRINGER 19R. FABRICATED NEW CLIP PER SAMPLE, TREATED AND PRIMED PER SRM - [SDR EISA99188](https://openairdocs.org/sdr/EISA99188), Sep 14, 1999: TIE CLIP. CRACKED. DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND CLIP CRACKED AT FS 700 STRINGER 20L. FABRICATED NEW CLIP PER SAMPLE, TREATED AND PRIMED PER SRM 51-1 - [SDR EISA99187](https://openairdocs.org/sdr/EISA99187), Sep 14, 1999: SEAT TRACK. GOUGED. DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND NR 5 SEAT TRACK GOUGED FROM FS 720D TO 720E. DAMAGE OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK F - [SDR EISA99186](https://openairdocs.org/sdr/EISA99186), Sep 14, 1999: SEAT TRACK. CORRODED. DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARAD FOUND NR 4 SEAT TRACK CORRODED AT FS 640. MATERIAL OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK FROM B - [SDR EISA99185](https://openairdocs.org/sdr/EISA99185), Sep 14, 1999: SEAT TRACK. CORRODED. DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND NR 1 SEAT TRACK CORRODED AT FS 1110. MATERIAL OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK FROM - [SDR EISA99184](https://openairdocs.org/sdr/EISA99184), Sep 14, 1999: SEAT TRACK. CORRODED. DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND NR 2 SEAT TRACK CORRODED AT FS 1070. MATERIAL OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK FROM BA - [SDR EISA99183](https://openairdocs.org/sdr/EISA99183), Sep 14, 1999: SEAT TRACK. CORRODED. DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND NR 2 SEAT TRACK CORRODED AT FS 870. REMOVED CORROSION, MATERIAL OUT OF LIMITS. FABRICATED NEW SECT - [SDR EISA99182](https://openairdocs.org/sdr/EISA99182), Sep 14, 1999: SEAT TRACK. CORRODED. DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND NR 2 SEAT TRACK, LBL 24, CORRODED FROM FS 760 TO 850. MATERIAL LOSS OUT OF LIMITS. FABRICATED NEW - [SDR EISA99181](https://openairdocs.org/sdr/EISA99181), Sep 14, 1999: SEAT TRACK. CORRODED. DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND NR 2 SEAT TRACK CORRODED AT FS 720C. CORROSION OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK PER SR - [SDR EISA99180](https://openairdocs.org/sdr/EISA99180), Sep 14, 1999: SEAT TRACK. CORRODED. DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND NR 1 SEAT TRACK CORRODED FROM FS 460 TO 690 LBL 42. CORROSION OUT OF LIMITS. FABRICATED NEW SECTIO - [SDR EISA98173](https://openairdocs.org/sdr/EISA98173), Jul 8, 1998: LINE. FAILED. AFTER DEPARTURE FROM LAX, PASSING 4500 FT, NR 1 STRUT OVERHEAT LIGHT ILLUMINATED, PERFORMED CHECKLIST LIGHT EXTINGUISHED. FOUND LEAKING SENSE LINE AT 13TH STAGE - [SDR EISA98172](https://openairdocs.org/sdr/EISA98172), Jul 7, 1998: CLAMP. FAILED. ON CLIMB-OUT OF PDX AT APPROXIMATELY 4500 FT, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED, AOM ABNORMAL ACCOMPLISHED. OVERHEAT LIGHT EXTINGUISHED AS SOON AS TH - [SDR EISA98171](https://openairdocs.org/sdr/EISA98171), Jul 7, 1998: CLAMP. LOOSE. AFTER TAKEOFF FROM LAX WHILE CLIMBING THROUGH 5000 FEET, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED, AOM ABNORMAL ACCOMPLISHED. OVERHEAT LIGHT EXTINGUISHED AS - [SDR EISA98170](https://openairdocs.org/sdr/EISA98170), Jul 7, 1998: CLAMP. LOOSE. AFTER TAKEOFF FROM MCI WHILE CLIMBING THROUGH 3200 FT, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AOM ABNORMAL ACCOMPLISHED. OVERHEAT LIGHT EXTINGUISHED AS S - [SDR EISA98169](https://openairdocs.org/sdr/EISA98169), Jul 7, 1998: CLAMP. LOOSE. AFTER TAKEOFF FROM IND WHILE CLIMBING THROUGH APPROXIMATELY 5000 FT, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED, AOM ABNORMALS ACCOMPLISHED. OVERHEAT LIGHT EX - [SDR EISA98149](https://openairdocs.org/sdr/EISA98149), Jul 1, 1998: CLAMP. LOOSE. DFW - DURING CLIMB-OUT, NR 1 STRUT OVERHEAT LIGHT ILLUMINATED, REDUCED POWER, CLOSED NR 1 ENGINE BLEED PER ABNORMAL CHECKLIST, LIGHT EXTINGUISHED. TIGHTENED CLA - [SDR EISA98165](https://openairdocs.org/sdr/EISA98165), Jun 28, 1998: SKIN. DELAMINTATED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND LOWER RUDDER TAB DELAMINATED AT TRAILING EDGE LOWER CORNER. REPAIRED DELAMINATION PER SRM 51-40-6. (M) - [SDR EISA98164](https://openairdocs.org/sdr/EISA98164), Jun 28, 1998: FRAME. CRACKED. DURING ACCOMPLISHMENT OF CPCP CARD C53-224-05, FOUND CRACK IN FUSELAGE FRAME AT FS 500 WL 214. REMOVED DAMAGED AREA. FABRICATED REPAIR PER SRM 51-40-3 AND INSTA - [SDR EISA98162](https://openairdocs.org/sdr/EISA98162), Jun 28, 1998: SEAT TRACK. CORRODED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK AT FS 848-870. REMOVED CORRODED TRACK AND INSTALLED NEW TRACK F - [SDR EISA98161](https://openairdocs.org/sdr/EISA98161), Jun 28, 1998: FITTING. CRACKED. DURING REPLACEMENT OF LEFT MAIN LANDING GEAR, FOUND FORWARD TRUNNION BEARING ATTACH FITTING CRACKED AT LOWER INBOARD BUSHING HOLE. REMOVED DAMAGED FITTING. INST - [SDR EISA98160](https://openairdocs.org/sdr/EISA98160), Jun 28, 1998: STRINGER. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND STRINGER 24L CRACKED JUST FORWARD OF FS 950A. REMOVED DAMAGED AREA. FABRICATED REPAIR PER SRM 53-10-3 - [SDR EISA98159](https://openairdocs.org/sdr/EISA98159), Jun 28, 1998: BRACKET. CORRODED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND FORWARD CARGO DOOR LOWER AFT CORNER, ANGLE BRACKET EXFOLIATED. REMOVED BRACKET. FABRICATED AND INSTALL - [SDR EISA98158](https://openairdocs.org/sdr/EISA98158), Jun 28, 1998: WEB. CRACKED. DURING ACCOMPLISHMENT OF CPCP WORK CARD, C3-224-08, FOUND CRACK INSIDE FS 1183 WALL AT LBL 50 EXTENDING FROM LIGHTENING HOLE IN WEB. REMOVED DAMAGED AREA IN WEB All 102: https://openairdocs.org/deregistered/N315NE-2008-02-29/reports.md --- 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.