# N967AX: Mcdonnell Douglas DC-9-41, registration cancelled 2017-05-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 24, 2017 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Mcdonnell Douglas DC-9-41](https://openairdocs.org/model/mcdonnell-douglas-dc-9-41) (registry code 302207P) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 47509 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: August 25, 1992 - Certificate issued: June 29, 2010 - Last registry action: June 29, 2010 - Mode S code: AD763D - Owner when cancelled: [Dhl Network Operations (USA) Inc](https://openairdocs.org/faa-owner/DHL%20NETWORK%20OPERATIONS%20(USA)%20INC) - Location: [Plantation, FL](https://openairdocs.org/faa-place/FL/Plantation) - Owner type: Corporation - Owner's area on the map: 26.1125° N, 80.2749° W: Placed by OpenAirDocs at the center of ZIP code 33324, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N967AX - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=967AX - Page: https://openairdocs.org/deregistered/N967AX-2017-05-24 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 Mcdonnell Douglas DC-9-41: https://openairdocs.org/model/mcdonnell-douglas-dc-9-41.md ## Service difficulty reports (92, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ABXA200811120263](https://openairdocs.org/sdr/ABXA200811120263), Nov 6, 2008: BATTERY PACK. DISCHARGED. COCKPIT EMERGENCY LIGHTS DIM. DEFERRED: 62445 REMOVED AND REPLACED 1.2 VDC BATTERIES IAW 33-53-02-4. OPS CHECK GOOD. BATTERY PACK NEED REPLACED WITHIN 3 FLT DAY - [SDR ABX2008F00001](https://openairdocs.org/sdr/ABX2008F00001), Jul 19, 2008: ROD. DETACHED. F/O WINDOW WOULD NOT OPEN. FOUND LOWER AFT LINKAGE ROD NOT ATTACHED AT THE AFT LOCK BAR. SECURED ROD (ATTACHED) TO AFT LOCK BAR IAW AMM CHAPTER 56. (K) - [SDR ABXA070325](https://openairdocs.org/sdr/ABXA070325), Sep 22, 2007: ANGLE. CRACKED. NR 1 PYLON STRUCTURE CRACKED FORWARD OF CONNECTOR. REPAIRED NR 1 PYLON STRUCTURE FORWARD OF CONNECTOR IAW DC9 SSRM DWG K05159. - [SDR ABXA070046](https://openairdocs.org/sdr/ABXA070046), Feb 7, 2007: SEAL. LEAKING. LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. COMPLIED WITH ABNORMALS. FOUND NLG STRUT SERVICING 50 PSI LOW. STRUT DID NOT EXTEND SMOOTHLY. REPLACED NLG STRUT S - [SDR ABXA060060](https://openairdocs.org/sdr/ABXA060060), Jan 27, 2006: SWITCH. OUT OF POSITION. AIRCRAFT DEPRESSURIZED WHILE AT 6000 FEET, OUTFLOW VALVE WAS FULL CLOSED. THE AIR CONDITIONING SUPPLY SWITCHES WERE ON AND PRESSURIZATION WAS SET FOR LANDING. P - [SDR ABXA050254](https://openairdocs.org/sdr/ABXA050254), Oct 7, 2005: FRAME. CRACKED. ADDITIONAL CRACK FOUND IN LEFT AFT MAIN FRAME FORWARD FLANGE. FRAME IS OUT OF REPAIR LIMITS IAW ES00916 DUE TO CRACKS IN BOTH FLANGES. REPLACED MAIN FRAME ON EA - [SDR ABXA050253](https://openairdocs.org/sdr/ABXA050253), Oct 6, 2005: SUPPORT FITTING. CRACKED. LEFT SUPPORT FITTING CRACKED CANTED BULKHEAD 1219, LT OF RUDDER TORQUE TUBE MECHANISM. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-2. - [SDR ABXA050252](https://openairdocs.org/sdr/ABXA050252), Oct 6, 2005: SEAT TRACK. CRACKED. SEAT TRACK WAS CRACKED 2 PLACES BETWEEN FS 160 AND 200 AT LEFT BUTT LINE 41.5. REPAIRED DAMAGED AREAS (2 EA) IAW DC-9 SSRM DWG K05159. - [SDR ABXA050251](https://openairdocs.org/sdr/ABXA050251), Oct 6, 2005: FITTING. CRACKED. LEFT INBOARD SPOILER HAD AN APPROXIMATE .1562 INCH CRACK IN THE CENTER DOUBLER ABOVE THE CENTER DRIVE FITTING. BLENDED CRACK IAW REA D957-52510. - [SDR ABXA050250](https://openairdocs.org/sdr/ABXA050250), Oct 4, 2005: SKIN. CORRODED. AREA OF BULGING AND DISHED RIVETS - FS 626 AT LONGERON 26 LEFT. EXFOLIATED DOUBLER ON THE INSIDE, ABOVE HAT CHANNEL. REPAIRED AREA IAW REA D953-52507. - [SDR ABXA040076](https://openairdocs.org/sdr/ABXA040076), Feb 10, 2004: LONGERON. CRACKED. STA. 1040 LONGERON 17 LT CRACKED. SPLICED IN NEW SECTION OF LONGERON IAW DC-9 SRM 53-02. - [SDR ABXA040075](https://openairdocs.org/sdr/ABXA040075), Feb 9, 2004: BULKHEAD. CRACKED. LT FORWARD PYLON BULKHEAD WAS CRACKED AT BOTTOM AT LT BUTT LINE 44.0. REPAIRED LT FORWARD PYLON BULKHEAD IAW DC-9 SRM 53-03. - [SDR ABXA040074](https://openairdocs.org/sdr/ABXA040074), Feb 6, 2004: FRAME. CRACKED. STA 775 AFT OVERWHEEL WELL FRAME WAS CRACKED BETWEEN POINTS E AND E IN AFT OB POCKET AND CRACKED BETWEEN POINTS H AND I IN AFT IB POCKET AND CRACKED IN FORWARD - [SDR ABXA040072](https://openairdocs.org/sdr/ABXA040072), Feb 6, 2004: FRAME. CRACKED. EDDY CURRENT INDICATED LT MAIN FRAME AT FS 737 CRACKED AT AFT SIDE AT POINT J TO POINT G. REPAIRED IAW J.C. EA 53400110-001-2. - [SDR ABXA040070](https://openairdocs.org/sdr/ABXA040070), Feb 6, 2004: FITTING. CORRODED. LONGERON 23 RT END CAP EXFOLIATED AT FS 1065. REPLACED LONGERON 23 RT END CAP USING P/N 3914590-1N IAW DC-9 SRM 51-30-2 AND 51-30-5. - [SDR ABXA040071](https://openairdocs.org/sdr/ABXA040071), Feb 6, 2004: WEB. CRACKED. CUSP WEB CRACKED FROM F.S. 1025-1039 APPROXIMATELY LT BUTT LINE 56. REPAIRED CUSP WEB IAW DC-9 SRM 53-01. - [SDR ABXA040066](https://openairdocs.org/sdr/ABXA040066), Feb 5, 2004: RIB. CRACKED. RT WING LE HAD CRACKED RIB AT LOWER NUTPLATES FOR NR 2 IB SLAT TRACK RIB. FOUND 4 CRACKS, REPAIRED IAW REA D957-49005 AND INSTALLED NUTPLATES IAW DC-9 SRM 51-30 - [SDR ABXA040073](https://openairdocs.org/sdr/ABXA040073), Feb 5, 2004: SUPPORT. CRACKED. VERTICAL SUPPORT NR 7 CRACKED FORWARD SIDE OF FORWARD AUX TANK. REPLACED VERTICAL SUPPORT NR 7 IAW DC-9 SRM 51-30-1. - [SDR ABXA040069](https://openairdocs.org/sdr/ABXA040069), Feb 5, 2004: NOSE COWL. CRACKED. NOSE COWL CRACKED 3 PLACES 6:00 POSITION AT NOSE COWL ANTI-ICE DUCT. INSTALLED ANTI-ICE DUCT IAW DC-9 MM 71-10-01-2-0001, REPLACED DOUBLER IAW DOUGLAS DWG 59591 - [SDR ABXA040068](https://openairdocs.org/sdr/ABXA040068), Feb 5, 2004: SKIN. DAMAGED. FORWARD LOWER CARGO DOOR'S EXTERIOR SKIN WAS DAMAGED AT LOWER EDGE 3 PLACES. REPAIRED AREA IAW REA D952-49012. - [SDR ABXA040067](https://openairdocs.org/sdr/ABXA040067), Feb 5, 2004: INTERCOSTAL. CRACKED. FORWARD LOWER CARGO DOOR HAD CRACKED INTERCOSTAL AT AFT HINGE. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5. - [SDR ABXA020045](https://openairdocs.org/sdr/ABXA020045), Jun 19, 2002: BULKHEAD. CRACKED. CRACK IN LEFT BULKHEAD WEB, FS 1041 AT LONGERON 17L, INBOARD END. REPAIRED BULKHEAD IAW DC-9 SRM 53-01. - [SDR ABXA020044](https://openairdocs.org/sdr/ABXA020044), Jun 19, 2002: FLOORBEAM. CRACKED. FLOORBEAM SUPPORT CRACKED AT LOWER END, FS 617 AND LONGERON 23L. REPAIRED FLOOR BEAM SUPPORT IAW DC-9 SRM 51-30-2 AND 51-30-5. - [SDR ABXA020043](https://openairdocs.org/sdr/ABXA020043), Jun 18, 2002: LONGERON. CRACKED. LONGERON 17, STATION 408, WAS CRACKED APPROXIMATELY .5-.75 INCH. REPAIRED LONGERON 17 IAW DC-9 SRM 53-02. - [SDR ABXA020042](https://openairdocs.org/sdr/ABXA020042), Jun 18, 2002: LONGERON. CRACKED. LONGERON 17, STATION 389, WAS CRACKED APPROXIMATELY 3/4 INCH. REPAIRED LONGERON 17 IAW DC-9 SRM 53-02. - [SDR ABXA020041](https://openairdocs.org/sdr/ABXA020041), Jun 18, 2002: PAN. CRACKED. AFT LOWER CARGO DOOR INNER PAN, WAS CRACKED IN RADIUS BELOW AFT LATCH. REPAIRED AREA IAW DC-9 SRM 52-05. - [SDR ABXA010720](https://openairdocs.org/sdr/ABXA010720), Feb 13, 2002: CLIP. DEFECTIVE. SMOKE FROM FIRST OFFICER'S YOKE CLIPBOARD LIGHT. TRIPPED MAP AND BRIEFCASE LIGHT CIRCUIT BREAKER. REMOVED METAL CLIP FROM FIRST OFFICER'S CLIPBOARD IAW DC-9 MM - [SDR ABXA010719](https://openairdocs.org/sdr/ABXA010719), Feb 12, 2002: RHEOSTAT. MALFUNCTIONED. BURNING SMELL FROM FIRST OFFICER'S YOKE FOLLOWED BY MAP AND BRIEFCASE CIRCUIT BREAKER TRIPPING. REPLACED FIRST OFFICER'S BRIEFCASE RHEOSTAT IAW DC-9 AMM 33-10-0 - [SDR ABXA010220](https://openairdocs.org/sdr/ABXA010220), May 8, 2001: STRUCTURE. VIBRATION. ON FINAL APPROACH WITH FLAPS EXTENDED TO 25 DEGREES, THE AIRCRAFT EXPERIENCED VIBRATIONS AND UNUSUAL NOISE. THE AIRCRAFT CONTINUED THE APPROACH AND LANDED WITH - [SDR ABXA010212](https://openairdocs.org/sdr/ABXA010212), Apr 30, 2001: ENGINE. FAILED. THE RIGHT ENGINE (NR 2) EXPERIENCED AN UNCOMMANDED SHUT DOWN DURING THE LANDING FLARE. MAINTENANCE COMPLETED VISUAL INSPECTIONS OF THE INTAKE AND EXHAUST. NO DE - [SDR ABXA0100005](https://openairdocs.org/sdr/ABXA0100005), Jan 15, 2001: UNKNOWN. ODOR. FLIGHT CREW REPORTED AN ELECTRICAL ODOR WAS NOTED IN THE AIRCRAFT DURING CLIMB. THE RIGHT CSD TEMPERATURE WAS NOTED TO BE IN THE UPPER YELLOW SCALE. ABNORMAL CS - [SDR ABXA0000001](https://openairdocs.org/sdr/ABXA0000001), Dec 30, 1999: BULB. FAILED. ON LANDING, WHEN GEAR WAS LOWERED, THE GEAR DOOR OPEN LIGHT WOULD NOT ILLUMINATE. PRESS TO TEST WAS OK. REPLACED GEAR DOOR OPEN LIGHT BULB. - [SDR ABXA9900360](https://openairdocs.org/sdr/ABXA9900360), May 10, 1999: BULKHEAD JAMB. CRACKED. DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB, RIGHT UPPER CORNER CRACKED. REPAIRED IAW DC9 SRM 53-03. - [SDR ABXA9900359](https://openairdocs.org/sdr/ABXA9900359), May 10, 1999: BULKHEAD JAMB. CRACKED. DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB UPPER CORNER CRACKED. REPAIRED CRACK IAW DC9 SRM 53-03. - [SDR ABXA9900358](https://openairdocs.org/sdr/ABXA9900358), May 10, 1999: SPAR CAP. CRACKED. DURING C-CHECK, FOUND LEFT WING REAR SPAR CAP CRACKED AT NUMEROUS HOLES. REPAIRED IAW ABX REA D957-28455MR. - [SDR ABXA9800589](https://openairdocs.org/sdr/ABXA9800589), Jun 30, 1998: LATCH. LOOSE. COCKPIT DOOR LATCH LOOSE ON THE INSIDE, SOMETIMES WOULD BIND. REPLACED LATCH ASSY. - [SDR ABXA9800588](https://openairdocs.org/sdr/ABXA9800588), Jun 29, 1998: LATCH. INOPERATIVE. COCKPIT DOOR INSIDE LATCH INOPERATIVE. CREW WAS UNABLE TO OPEN DOOR FROM COCKPIT. REPAIRED AS REQUIRED. - [SDR ABXA9800446](https://openairdocs.org/sdr/ABXA9800446), May 11, 1998: DRIVE LINK. CRACKED. DURING COMPLIANCE WITH AD 96-10-11 AND AD 75-14-06, FOUND NR 2 ENGINE THRUST REVERSER, UPPER, LEFT, DRIVE LINK CRACKED. REPLACED DRIVE LINK IAW DC9 MM 78-31-5. - [SDR ABXA9800036](https://openairdocs.org/sdr/ABXA9800036), Jan 22, 1998: LATCH. OUT OF ADJUST. COCKPIT DOOR WOULD NOT OPEN. LUBRICATED AND ADJUSTED DOOR LATCH ASSEMBLY. - [SDR ABXA9701681](https://openairdocs.org/sdr/ABXA9701681), Oct 17, 1997: LATCH ASSY. DEFECTIVE. DURING MAINTENANCE CHECK, FOUND COCKPIT DOOR WOULD NOT OPEN FROM INSIDE OR OUTSIDE. REINSTALLED TUMBLER MECHANISM INSIDE DOOR HANDLE. - [SDR ABXA9701624](https://openairdocs.org/sdr/ABXA9701624), Oct 14, 1997: LATCH. WORN. COCKPIT DOOR WOULD NOT OPEN FROM THE INSIDE. REPAIRED THE LATCH ASSEMBLY. OPS CHECKED GOOD. - [SDR ABXA9701517](https://openairdocs.org/sdr/ABXA9701517), Sep 24, 1997: FITTING. CORRODED. DURING C-CHECK, FOUND THE SUPPORT FITTING ON TOP OF THE CENTER WING FUEL TANK AT STA 645 BELOW THE LT CUSP WEB EXFOLIATED. REPLACED FITTING IAW DC9 SRM 51-30-5 - [SDR ABXA9701516](https://openairdocs.org/sdr/ABXA9701516), Sep 24, 1997: WEB. CRACKED. DURING C-CHECK, FOUND THE RIGHT HORIZONTAL STABILIZER LEADING EDGE WEB CRACKED BETWEEN STA XRS.83.624 AND 145.000. REPAIRED WEB IAW ABX REA D955-20896. - [SDR ABXA9701515](https://openairdocs.org/sdr/ABXA9701515), Sep 24, 1997: ANGLE. CRACKED. DURING C-CHECK, FOUND A CRACKED ANGLE AT STA 1041 AND LONGERON 18 LEFT, UNDER CUSP WEB. REPAIRED ANGLE IAW ABX REA D953-20903-MR. - [SDR ABXA9701511](https://openairdocs.org/sdr/ABXA9701511), Sep 22, 1997: CUSP WEB. CRACKED. DURING C-CHECK, FOUND LT CUSP WEB AT STA 1040 CRACKED. REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-2. - [SDR ABXA9701510](https://openairdocs.org/sdr/ABXA9701510), Sep 22, 1997: FRAME. CRACKED. DURING C-CHECK, FOUND THE MAINFRAME AT STA 655 LEFT CRACKED AT BASE OF FRAME JUST BELOW LONGERON 18L. REPAIRED FRAME IAW ABX REA D953-2092-MR AND DC9 SRM 53-03. - [SDR ABXA9701512](https://openairdocs.org/sdr/ABXA9701512), Sep 19, 1997: BLKHD FITTING. CRACKED. DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB FITTING AT THE LOWER RT STOP PAD ATTACH FASTENER HOLE CRACKED. REPLACED THE FITTING IAW DC9 SRM 51-30- - [SDR ABXA9701504](https://openairdocs.org/sdr/ABXA9701504), Sep 19, 1997: CUSP WEB. CRACKED. DURING C-CHECK, FOUND RT CUSP WEB AT STA 665 TO 677 CRACKED. REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-2. - [SDR ABXA9701503](https://openairdocs.org/sdr/ABXA9701503), Sep 19, 1997: FRAME. CRACKED. DURING C-CHECK, FOUND THE LT MAINFRAME AT STA 775 CENTER POCKET AFT LOWER FLANGE CRACKED. REPAIRED FRAME IAW ABX REA D953-20786-MR. - [SDR ABXA9701502](https://openairdocs.org/sdr/ABXA9701502), Sep 19, 1997: FIXED VANE. DELAMINATED. DURING C-CHECK, FOUND THE CENTER FIXED VANE TOP SIDE DELAMINATED. REPLACED VANE IAW DC9 MM 27-51-3. All 92: https://openairdocs.org/deregistered/N967AX-2017-05-24/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.