# N927AX: 1966 Douglas DC9-15, registration cancelled 2007-04-25 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 25, 2007 - Status when cancelled: Triennial form not returned - Airframe: [Douglas DC9-15](https://openairdocs.org/model/douglas-dc9-15) (registry code 3022036) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 45717 - Year built: 1966 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: September 17, 1990 - Certificate issued: August 10, 1983 - Last registry action: January 16, 2007 - Mode S code: ACD841 - Owner when cancelled: [Abx Air Inc](https://openairdocs.org/faa-owner/ABX%20AIR%20INC) - Location: [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.4607° N, 83.8443° W: Placed by OpenAirDocs at the center of ZIP code 45177, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N927AX - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=927AX - Page: https://openairdocs.org/deregistered/N927AX-2007-04-25 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 Douglas DC9-15: https://openairdocs.org/model/douglas-dc9-15.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 ABXA040242](https://openairdocs.org/sdr/ABXA040242), Jul 1, 2004: CONDUIT. BROKEN. AFTER GEAR RETRACTION ON CLIMBOUT, (LT GEAR UNSAFE) LIGHT ILLUMINATED, CYCLED GEAR, NORMAL INDICATION THEREAFTER. THE LT MAIN LANDING GEAR DOWNLOCK FLEX CONDUIT - [SDR ABXA040204](https://openairdocs.org/sdr/ABXA040204), Jun 9, 2004: POWER SUPPLY. INOPERATIVE. ON POWER SHUT DOWN, EMERGENCY LIGHTS STAYED ON. REPLACED EMERGENCY LIGHT POWER SUPPLY WITH A SERVICEABLE UNIT IAW DC-9 MM 33-53-02-4-0001. OPS CHECKED GOOD. - [SDR ABXA040180](https://openairdocs.org/sdr/ABXA040180), May 20, 2004: BATTERY. DEFECTIVE. EMERGENCY LIGHTS STAYED ON AFTER POWER SHUT DOWN. REPLACED BATTERY POWER SUPPLY WITH A SERVICEABLE UNIT IAW DC-9 MM 33-53-02-4-0001. OPS CHECKED GOOD. - [SDR ABXA040051](https://openairdocs.org/sdr/ABXA040051), Jan 20, 2004: CONTROL CABLE. LACK OF LUBE. FLIGHT SPOILERS WERE BINDING IN FLIGHT. UNABLE TO DEPLOY. INSPECTED CABLES AND LINKAGE IN PEDESTAL. INSPECTED AND LUBRICATED CABLES AND MIXERS IN WHEEL WELLS AN - [SDR ABXA030277](https://openairdocs.org/sdr/ABXA030277), Jun 10, 2003: FRAME. CRACKED. FRAME FS 523 WAS CRACKED. REMOVED AND REPLACED FRAME FS 523 LEFT IAW DC-9 SRM. - [SDR ABXA030056](https://openairdocs.org/sdr/ABXA030056), Jan 29, 2003: WARNING HORN. ACTIVATED. AFTER TAKE-OFF OUT OF ILN, AIRCRAFT FAILED TO PRESSURIZE AND CONFIGURATION WARNING HORN SOUNDED. CHECKED LT OLEO SWITCH, EXERCISED SWITCH SEVERAL TIMES. CLEANED - [SDR ABXA010880](https://openairdocs.org/sdr/ABXA010880), May 16, 2002: STOP FITTING. SHEARED. HORIZONTAL STABILIZER JACKSCREW, UPPER MECHANICAL STOP SHEARED OFF. REMOVED AND REPLACED THE JACKSCREW ASSEMBLY IAW DC-9 MM. - [SDR ABXA010579](https://openairdocs.org/sdr/ABXA010579), Oct 30, 2001: SPAR CAP. CRACKED. CRACK ON REAR SPAR LOWER T-CAP AT APPROXIMATELY XCW 3. REPAIRED AREA IAW DC-9 SRM 57-09. - [SDR ABXA010578](https://openairdocs.org/sdr/ABXA010578), Oct 23, 2001: FRAME. CRACKED. FRAME AT F.S. 930 WAS CRACKED AT LONGERON 3 RIGHT. REPAIRED FRAME IAW DC-9 SSRM K05159. - [SDR ABXA010577](https://openairdocs.org/sdr/ABXA010577), Oct 23, 2001: WEB. CRACKED. LEFT PYLON 45 DEGREE WEB JUST FORWARD OF AFT ENGINE MOUNT CRACKED AT LOWER ATTACH ANGLE. REPAIRED WEB IAW DC-9 SSRM K05159. - [SDR ABXA010576](https://openairdocs.org/sdr/ABXA010576), Oct 23, 2001: RIB. CRACKED. LEFT HORIZONTAL STABILIZER RIB WAS CRACKED AT XFS 77. REPAIRED RIB EDGE IAW DC-9 SRM 55-01. PROTECTED AREA AGAINST CORROSION IAW DC-9 SRM 51-10-3. - [SDR ABXA010575](https://openairdocs.org/sdr/ABXA010575), Oct 23, 2001: RIB. CRACKED. LEFT HORIZONTAL STABILIZER LEADING EDGE RIB WAS CRACKED AT XFS 95. REPAIRED RIB IAW DC-9 SSRM K0-5159. PROTECTED AREA AGAINST CORROSION IAW DC-9 SRM 51-10-3. - [SDR ABXA010574](https://openairdocs.org/sdr/ABXA010574), Oct 22, 2001: LONGERON. CRACKED. LONGERON 3 LEFT WAS CRACKED AT F.S. 160. REPLACED CRACKED LONGERON IAW DC-9 SRM 53-02. - [SDR ABXA000420](https://openairdocs.org/sdr/ABXA000420), Sep 14, 2000: SMOKE DETECTOR. MALFUNCTIONED. AMBER CARGO SMOKE ANNUNCIATOR ILLUMINATED DURING FLIGHT. THE LIGHT EXTINGUISHED AFTER 10 SECONDS. REPLACED FORWARD CARGO SMOKE DETECTOR. - [SDR ABXA000197](https://openairdocs.org/sdr/ABXA000197), Apr 16, 2000: ACTUATOR. FAILED. GEAR DOOR OPEN LIGHT WOULD NOT EXTINGUISH. PERFORMED EMERGENCY GEAR EXTENSION. LANDING WAS UNEVENTFUL. REPLACED LEFT MAIN LANDING GEAR DOOR ACTUATOR. - [SDR ABXA000139](https://openairdocs.org/sdr/ABXA000139), Feb 28, 2000: SPAR. CORRODED. DURING C CHECK, FOUND CORROSION ON THE LEFT REAR SPAR XA 461. CORROSION REMOVED IAW DC9 SRM 57-09. REPAIRED IAW REA D957-35569MR. - [SDR ABXA000138](https://openairdocs.org/sdr/ABXA000138), Feb 23, 2000: SPOILER. DELAMINATED. DURING C CHECK, FOUND LEFT FIXED GROUND SPOILER DELAMINATED. REPLACED FIXED GROUND SPOILER IAW DC9 MM 27-62-01. - [SDR ABXA9800645](https://openairdocs.org/sdr/ABXA9800645), Jul 22, 1998: FRAME. CRACKED. WHILE COMPLYING WITH C INSPECTION, FOUND FUSELAGE FRAME 544 RIGHT CRACKED AT TRANSVERSE FLOORBEAM. REPLACED FUSELAGE FRAME IAW DC-9 SRM CHAPTERS 51-30-2 AND 51- - [SDR ABXA9800643](https://openairdocs.org/sdr/ABXA9800643), Jul 20, 1998: FLOORBEAM. CORRODED. WHILE COMPLYING WITH C INSPECTION, FOUND A FLOORBEAM CORRODED ALONG LOWER FLANGE AT FS801 AND LBL44. REPAIRED FLOORBEAM IAW ABX REA D953-24225MR. - [SDR ABXA9800642](https://openairdocs.org/sdr/ABXA9800642), Jul 20, 1998: BULKHEAD BRACKET. CRACKED. WHILE COMPLYING WITH 'C' INSPECTION, FOUND THE AFT FACE OF THE AFT PRESSURE BULKHEAD HAD A CRACKED BRACKET AT LOWER LEFT CORNER OF DOOR JAMB. REPLACED BRACKET I - [SDR ABXA9800649](https://openairdocs.org/sdr/ABXA9800649), Jul 17, 1998: WEB. CRACKED. WHILE COMPLYING WITH C INSPECTION, FOUND A WEB CRACKED BETWEEN LONGERON 8L AND 9L AT FS206. REPAIRED WEB IAW ABX REA D953-24104. - [SDR ABXA9800650](https://openairdocs.org/sdr/ABXA9800650), Jul 15, 1998: SPAR. CRACKED. WHILE COMPLYING WITH C INSPECTION, FOUND A CRACK IN THE RIGHT UPPER SPAR TEE CAP AT XCW 58. REPAIRED CRACK IAW ABX REA D957-24102MR. - [SDR ABXA9800648](https://openairdocs.org/sdr/ABXA9800648), Jul 15, 1998: SPAR. CRACKED. WHILE COMPLYING WITH C INSPECTION, FOUND THE LEFT WING UPPER FRONT SPAR CRACKED BETWEEN TWO SCREW HOLES 10 OUTBOARD OF XCW 58. REPAIRED CRACK IAW ABX REA D957-2 - [SDR ABXA9800647](https://openairdocs.org/sdr/ABXA9800647), Jul 14, 1998: SPAR. CORRODED. WHILE COMPLYING WITH C INSPECTION, FOUND THE LEFT HORIZONTAL STABILIZER UPPER REAR SPAR CORRODED AT XE 147. REPLACED SPAR SECTION IAW DC-9 SRM CHAPTER 55-02. - [SDR ABXA9800641](https://openairdocs.org/sdr/ABXA9800641), Jul 14, 1998: BULKHEAD WEB. CORRODED. WHILE COMPLYING WITH C INSPECTION, FOUND THE AFT PRESSURE BULKHEAD WEB CORRODED BETWEEN LONGERON 26L TO 30L. REPAIRED IAW ABX REA D953-24142MR. - [SDR ABXA9800620](https://openairdocs.org/sdr/ABXA9800620), Jul 14, 1998: PANEL. CORRODED. WHILE COMPLYING WITH C-CHECK, FOUND LEFT SLANT PANEL CORRODED. REPAIRED IAW DACO DWG 5956065, ABX DWG NR 4255 AND DC9 SRM 51-30-2. - [SDR ABXA9800619](https://openairdocs.org/sdr/ABXA9800619), Jul 14, 1998: SHIELD. CRACKED. WHILE COMPLYING WITH C-CHECK FOUND A CRACKED HEAT SHIELD IN THE RIGHT WING NR 1 LEADING EDGE SECTION. REPAIRED IAW ABX REA NR D957-24148. - [SDR ABXA9800618](https://openairdocs.org/sdr/ABXA9800618), Jul 14, 1998: DOUBLER. CORRODED. WHILE COMPLYING WITH C-CHECK, FOUND STATION 817 FLOORBEAM WEB DOUBLER CORRODED. INSTALLED WEB DOUBLER IAW DACO DWG NR 9915561. - [SDR ABXA9800617](https://openairdocs.org/sdr/ABXA9800617), Jul 14, 1998: FLOORBEAM. CORRODED. WHILE COMPLYING WITH C-CHECK FOUND STATION 817 FLOORBEAM WEB CORRODED. REPLACED WEB IAW DC9 SRM 51-10-2 AND 51-10-5. - [SDR ABXA9800646](https://openairdocs.org/sdr/ABXA9800646), Jul 9, 1998: BULKHEAD JAMB. CRACKED. WHILE COMPLYING WITH C INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB UPPER RIGHT CORNER CRACKED. REPAIRED IAW ABX REA D953-24119. - [SDR ABXA9800644](https://openairdocs.org/sdr/ABXA9800644), Jul 9, 1998: SPAR. CORRODED. WHILE COMPLYING WITH C INSPECTION, FOUND THE RIGHT WING FORWARD UPPER SPAR CAP CORRODED FROM XFS 410 TO 406. REPAIRED RIGHT WING FRONT SPAR CAP IAW ABX REA D957 - [SDR ABXA9800613](https://openairdocs.org/sdr/ABXA9800613), Jul 8, 1998: HOUSING. CRACKED. WHILE COMPLYING WITH C-CHECK, FOUND MAIN ENTRY DOOR EXTERIOR HANDLE HOUSING CRACKED. REPLACED HOUSING IAW DC9 SRM 51-30-2. - [SDR ABXA9800612](https://openairdocs.org/sdr/ABXA9800612), Jul 7, 1998: SPAR CAP. CORRODED. WHILE COMPLYING WITH C-CHECK, FOUND CORROSION ON LEFT WING FRONT SPAR UPPER CAP AT STATION XRS 459. REPAIRED UPPER CAP IAW REA D957-24092. - [SDR ABXA9800611](https://openairdocs.org/sdr/ABXA9800611), Jul 7, 1998: LONGERON. CRACKED. WHILE COMPLYING WITH C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT FUSELAGE STATION 786. REPLACED LONGERON 17 RIGHT SECTION AT STATION 786 IAW DC9 SRM. - [SDR ABXA9800610](https://openairdocs.org/sdr/ABXA9800610), Jul 7, 1998: STRUCTURE. CRACKED. WHILE COMPLYING WITH C-CHECK FOUND FORWARD SUB FLOOR CRACKED AT STATION 170 LBL 40. REPAIRED CRACKED SUB FLOOR IAW DC9 SRM 53-01. - [SDR ABXA9700535](https://openairdocs.org/sdr/ABXA9700535), Mar 8, 1997: DOOR. CRACKED. DURING COMPLIANCE OF AD 91-22-07, FOUND RIGHT HAND GEAR STRUT DOOR UPPER SEAL SECTION CRACKED AND END BROKEN OFF. REPLACED SEAL IAW DC9 SRM 51-30-2. - [SDR ABXA9700534](https://openairdocs.org/sdr/ABXA9700534), Mar 8, 1997: DOOR. CRACKED. DURING COMPLIANCE OF AD 91-22-07, FOUND LEFT HAND GEAR STRUT DOOR UPPER SEAL SECTION CRACKED. REPLACED SEAL IAW DC9 SRM 51-30-2. - [SDR ABXA9700533](https://openairdocs.org/sdr/ABXA9700533), Mar 8, 1997: LONGERON. CORRODED. DURING COMPLIANCE OF AD 96-07-51, ASB DC9-53A282, FOUND CORROSION ON LONGERON 2 LEFT HAND STATION 294 TO STATION 313. REPAIRED DAMAGED LONGERON PER DC9 SRM 53-0 - [SDR ABXA9700304](https://openairdocs.org/sdr/ABXA9700304), Nov 14, 1996: WEB. CUT OUT. DURING C-CHECK, FOUND A CUTOUT ON LEFT CUSP WEB BETWEEN STA 237-256. REPAIRED IAW ABX READ953-17208-MR. - [SDR ABXA9700303](https://openairdocs.org/sdr/ABXA9700303), Nov 14, 1996: CUSP. CRACKED. DURING C-CHECK, FOUND LEFT CUSP WEB, CRACKED AT STA 218 (AD 92-22-08). REPLACED CUSP WEB IAW DC 9 SRM 51-30-2, 51-30-5, ABX REA D953-17208-MR. - [SDR ABXA9700305](https://openairdocs.org/sdr/ABXA9700305), Nov 12, 1996: FRAME. MISDRILLED. DURING C-CHECK, FOUND FRAME STA 642 HAD A MISDRILLED HOLE. REPAIRED IAW REA D953-17177-MR. - [SDR ABXA9700680](https://openairdocs.org/sdr/ABXA9700680), Nov 11, 1996: VANE. DENTED. THE RIGHT WING FORWARD FLAP VANE HAD NUMEROUS DENTS ON LOWER SURFACE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. - [SDR ABXA9700894](https://openairdocs.org/sdr/ABXA9700894), Nov 7, 1996: TAB. DELAMINATED. THE RIGHT AILERON TAB INBOARD TRAILING EDGE CORNER WAS DELAMINATED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. - [SDR ABXA9700307](https://openairdocs.org/sdr/ABXA9700307), Nov 7, 1996: TAB. DELAMINATED. DURING C-CHECK, FOUND RIGHT AILERON TRIM TAB DELAMINATED AND DENTED (AD 92-22-08). REPLACED IAW DC-9 M/M 27-10-5. - [SDR ABXA9700678](https://openairdocs.org/sdr/ABXA9700678), Nov 6, 1996: VANE. DELAMINATED. THE LEFT WING INBOARD FIXED FLAP VANE HAD A AREA OF DELAMINATION BETWEEN MID RUBSTRIPS. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. - [SDR ABXA9700310](https://openairdocs.org/sdr/ABXA9700310), Nov 6, 1996: WEB. CUT. DURING C-CHECK, FOUND A CUTOUT ON LEFT CUSP WEB, BETWEEN STA 237-256. REPAIRED IAW ABX REA D953-17208-MR. - [SDR ABXA9700309](https://openairdocs.org/sdr/ABXA9700309), Nov 6, 1996: FRAME. MISDRILLED. DURING C-CHECK, FOUND FRAME STA 642 HAD A MISDRILLED HOLE. REPAIRED IAW REA D953-17177-MR. - [SDR ABXA9700308](https://openairdocs.org/sdr/ABXA9700308), Nov 6, 1996: VANE. DELAMINATED. DURING C-CHECK, FOUND RIGHT FLAP INBOARD FIXED VANE DELAMINATED (AD 92-22-08). REPLACED IAW DC-9 M/M 27-51-3. - [SDR ABXA9700306](https://openairdocs.org/sdr/ABXA9700306), Nov 6, 1996: SUBFLOOR. CRACKED. DURING C-CHECK, FOUND SUBFLOOR CRACKED AT STA 208 (AD 92-22-08). REPAIRED IAW DC-9 SRM 51-30-2. - [SDR ABXA9600606](https://openairdocs.org/sdr/ABXA9600606), Aug 5, 1996: BATTERIES. DISCHARGED. EMERGENCY LIGHTS DIM WHEN TESTED. REPLACED BATTERIES IN EMERGENCY LIGHT POWER PACK, OPS CHECK GOOD. All 59: https://openairdocs.org/deregistered/N927AX-2007-04-25/reports.md ## Other aircraft with N927AX - [Cancelled 2017-03-13](https://openairdocs.org/deregistered/N927AX-2017-03-13): Boeing 777-222, S/N 26943, built 1997. First renewal notice. Owner: [T7 Aviation Leasing LLC](https://openairdocs.org/faa-owner/T7%20AVIATION%20LEASING%20LLC), [Tulsa, OK](https://openairdocs.org/faa-place/OK/Tulsa) --- 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.