# N934AX: Douglas DC-9-33F, registration cancelled 2011-04-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 18, 2011 - Exported to: Mexico - Status when cancelled: Valid registration - Airframe: [Douglas DC-9-33F](https://openairdocs.org/model/douglas-dc-9-33f) (registry code 302207A) - Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 47462 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: February 19, 1987 - Certificate issued: January 6, 2011 - Last registry action: January 6, 2011 - Mode S code: ACF49B - Owner when cancelled: [Frontera Flight Holdings Inc](https://openairdocs.org/faa-owner/FRONTERA%20FLIGHT%20HOLDINGS%20INC) - Location: [Dover, DE](https://openairdocs.org/faa-place/DE/Dover) - Owner type: Corporation - Owner's area on the map: 39.1815° N, 75.4736° W: Placed by OpenAirDocs at the center of ZIP code 19901, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N934AX - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=934AX - Page: https://openairdocs.org/deregistered/N934AX-2011-04-18 From the FAA registry file of October 28, 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 DC-9-33F: https://openairdocs.org/model/douglas-dc-9-33f.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 ABXR201009250052](https://openairdocs.org/sdr/ABXR201009250052), Sep 25, 2010: CONTROL CABLE. CORRODED. DURING FERRY FLIGHT PREP FOUND CABLE 51C CORRODED FWD OF APB. R & R CABLE 51C IAW AMM. - [SDR ABXR201009250051](https://openairdocs.org/sdr/ABXR201009250051), Sep 25, 2010: CONTROL CABLE. BROKEN. DURING FERRY FLIGHT PREP FOUND NR 1 ENGINE FWD TELESCOPING BRAIDED CABLE RUSTED, WORN, AND BROKEN STRANDS. R & R NR1 ENGINE FWD TELESCOPING GRAIDED CABLE IAW AM - [SDR ABXR201009250050](https://openairdocs.org/sdr/ABXR201009250050), Sep 25, 2010: CONTROL CABLE. BROKEN. DURING FERRY FLIGHT PREP FOUND CABLE RUN 52C FOR RT THRUST REVERSER CORRODED AND BROKEN STRANDS. R & R CABLE 52C IAW AMM. - [SDR ABXR201009250049](https://openairdocs.org/sdr/ABXR201009250049), Sep 25, 2010: CONTROL CABLE. BROKEN. DURING FERRY FLIGHT PREP FOUND THRUST REVERSER CONTROL CABLE 48C BROKEN. R & R CABLE 48C IAW AMM. - [SDR ABXR201009250048](https://openairdocs.org/sdr/ABXR201009250048), Sep 25, 2010: CONTROL CABLE. BROKEN. DURING FERRY FLIGHT PREP FOUND NR 1 T/R SECTOR ON AFT 'P' DOME DOESN'T MOVE WITH T/R HANDLE MOVEMENT. REPLACED CABLE 47C IAW AMM. - [SDR ABXR201009250047](https://openairdocs.org/sdr/ABXR201009250047), Sep 25, 2010: PUSH-PULL CABLE. DAMAGED. DURING FERRY FLIGHT PREP FOUND NR 2 ENGINE THROTTLE DOES NOT MOVE FROM THROTTLE LEVER. R & R NR 2 ENGINE THROTTLE PUSH PULL CABLE IAW MM. - [SDR ABXR201009250046](https://openairdocs.org/sdr/ABXR201009250046), Sep 25, 2010: YOKE. CORRODED. DURING FERRY FLIGHT PREP FOUND NR 2 ENGING FWD. YOKE CORRODED. R & R NR 2 ENG FWD YOKE IAW AMM. - [SDR ABXR201009250045](https://openairdocs.org/sdr/ABXR201009250045), Sep 25, 2010: FITTING. CORRODED. DURING FERRY FLIGHT PREP FOUND NR 2 PYLON FWD. UPPER SPLICE FITTING CORRODED. R & R NR2 PYLON FWD UPPER SPLICE FITTING IAW AMM. - [SDR ABXR201009250044](https://openairdocs.org/sdr/ABXR201009250044), Sep 25, 2010: FITTING. CORRODED. DURING FERRY FLIGHT PREP FOUND NR 2 PYLON FWD LOWER SPLICE FITTING CORRODED. R & R SPLICE FITTING IAW SRM. - [SDR ABXR201009250043](https://openairdocs.org/sdr/ABXR201009250043), Sep 25, 2010: MOUNT. CORRODED. DURING FERRY FLIGHT PREP FOUND NR2 PYLON AFT ENGINE MOUNT CORRODED. R AND R AFT MOUNT ASSY IAW MM. - [SDR ABXR201009250042](https://openairdocs.org/sdr/ABXR201009250042), Sep 25, 2010: ISOLATOR. CORRODED. DURING FERRY FLIGHT PREP FOUND NR1 PYLON UPPER VIBRATION ISOLATOR RUSTED AND PITTED. R & R NR1 PYLON UPPER VIBRATION ISOLATOR IAW MM. - [SDR ABXR201009250041](https://openairdocs.org/sdr/ABXR201009250041), Sep 25, 2010: ISOLATOR. CORRODED. DURING FERRY FLIGHT PREP FOUND NR 1 PYLON YOKE LOWER ISOLATION ABSORBER RUSTED AND PITTED. R & R LOWER ISOLATION ABSORBER IAW MM. - [SDR ABXR201009250040](https://openairdocs.org/sdr/ABXR201009250040), Sep 25, 2010: MOUNT. CORRODED. DURING FERRY FLIGHT FLIGHT, PREP FOUND NR1 PYLON AFT MOUNT RECEIVER RUSTED AND PITTED. R & R NR1 PYLON AFT MOUNT IAW MM. - [SDR ABXR2010092400039](https://openairdocs.org/sdr/ABXR2010092400039), Sep 24, 2010: LINK. CORRODED. DURING FERRY FLIGHT, PREP FOUND NR1 PYLON AFT MOUNT UPPER INBD "H" DOG BONE AND OTBD BOLT RUSTY. R & R BOLT AND MOUNT LINK IAW MM. - [SDR ABXA070365](https://openairdocs.org/sdr/ABXA070365), Nov 5, 2007: BATTERY. DISCHARGED. EMERGENCY LIGHTS WILL ARM BUT WOULD NOT ILLUMINATE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY IAW DC9 MM 33-53-00-8. - [SDR ABXA070322](https://openairdocs.org/sdr/ABXA070322), Sep 20, 2007: WINDOW. OUT OF ADJUST. CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED CAPTAIN'S CLEARVIEW WINDOW IAW DC9 MM 56-10-03-5. - [SDR ABXA060287](https://openairdocs.org/sdr/ABXA060287), Nov 10, 2006: LINKAGE. LACK OF LUBE. CAPTAIN'S SLIDING WINDOW (EMERGENCY EXIT) WOULD NOT OPEN. LUBED CAPTAIN'S SLIDING WINDOW LINKAGE AS REQUIRED. OPERATIONAL CHECK GOOD IAW MM 56-10-03-5-0002. - [SDR ABXA060293](https://openairdocs.org/sdr/ABXA060293), Oct 13, 2006: FRAME. CRACKED. LEFT WHEEL WELL, LEFT AFT CORNER ANGLE WAS CRACKED. REMOVED AND REPLACED MAIN FRAME AT FS 756 LEFT IAW DACO DC9 DWG 9919649. - [SDR ABXA060284](https://openairdocs.org/sdr/ABXA060284), Oct 13, 2006: ANGLE. CRACKED. LEFT WHEEL WELL AFT CORNER ANGLE WAS CRACKED. REMOVED AND REPLACED MAIN FRAME AT FS 756 LEFT IAW DACO DC9 DWG 9919649. - [SDR ABXA060078](https://openairdocs.org/sdr/ABXA060078), Jan 25, 2006: ROD END. BROKEN. UPON SLAT EXTENSION, AIRCRAFT ROLLED TO THE RIGHT AND SLAT DISAGREEMENT LIGHT ILLUMINATED AND THE SLAT EXTEND LIGHT DID NOT ILLUMINATE AFTER RECYCLING SLATS, NO - [SDR ABXA050039](https://openairdocs.org/sdr/ABXA050039), Mar 2, 2005: CONTACT. WORN. UPON LOWERING THE LANDING GEAR, NO NOSE GEAR SAFE LIGHT. TESTED IN BRIGHT AND DIM. AFTER INITIATING A GO-AROUND, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED (APPROXI - [SDR ABXA040387](https://openairdocs.org/sdr/ABXA040387), Dec 1, 2004: WINDOW. STUCK. CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. OPENED WINDOW AND APPLIED LUBRICANT TO WINDOW MECHANISM, WINDOW OPERATES NORMAL. - [SDR ABXA040399](https://openairdocs.org/sdr/ABXA040399), Nov 16, 2004: BEARING. CRACKED. RIGHT HORIZONTAL STAB PIVOT BEARING FOUND CRACKED IN HALF. REPLACED BEARING ON NR 0131 IAW DC-9 SRM. - [SDR ABXA040398](https://openairdocs.org/sdr/ABXA040398), Nov 12, 2004: FRAME. CRACKED. RIGHT FORWARD MAIN FRAME FS 699 CRACKED AT FORWARD FLANGE POINTS F & E AND AFT FLANGE POINTS H & I. REMOVED AND REPLACED FRAME AT STA 699 IAW EA 53400322-001-3. - [SDR ABXA040393](https://openairdocs.org/sdr/ABXA040393), Nov 11, 2004: SKIN. CRACKED. LOWER AFT CORNER OF FORWARD LOWER CARGO DOOR CUTOUT HAD 2 EACH CRACKS. REPAIRED IAW DC-9 SRM 53-05 AND REA D953-51052MR. - [SDR ABXA040392](https://openairdocs.org/sdr/ABXA040392), Nov 11, 2004: SKIN. CRACKED. MAIN ENTRY DOOR UPPER AFT STOP HAD CRACKED SURFACE SKIN. REPAIRED MAIN ENTRY DOOR UPPER AFT CORNER IAW JOB CARD EA 53100126-001, SERVICE REPAIR DRAWING SR095302 - [SDR ABXA040397](https://openairdocs.org/sdr/ABXA040397), Nov 11, 2004: FRAME. CRACKED. AFT ASSY CANTED FRAME 1121 CRACKED BETWEEN LONGERON 16 LEFT AND LONGERON 17 LEFT. REPAIRED IAW DC-9 SSRM K05159. - [SDR ABXA040396](https://openairdocs.org/sdr/ABXA040396), Nov 11, 2004: SKIN PANEL. CRACKED. TWO CRACKS IN FUSELAGE SKIN FS 1143, APPROXIMATELY LONGERON 14 RIGHT. REPAIRED FUSELAGE SKIN IAW DC-9 SRM 53-01. - [SDR ABXA040395](https://openairdocs.org/sdr/ABXA040395), Nov 10, 2004: FRAME. CRACKED. FRAME CRACKED FS 357 AT LONGERON 30. REPAIRED FRAME STA 357 AT LONGERON 30 IAW DC-9 SRM 53-03. - [SDR ABXA040394](https://openairdocs.org/sdr/ABXA040394), Nov 10, 2004: LONGERON. CRACKED. LONGERON 30 CRACKED FORWARD AND AFT AT SPLICE FS 380. REMOVED AND REPLACED LONGERON 30 FROM STA 355 TO 415. - [SDR ABXA040112](https://openairdocs.org/sdr/ABXA040112), Mar 23, 2004: SWITCH. MALFUNCTIONED. AFTER GEAR HANDLE SELECTED DOWN, NOSE GEAR LIGHT DID NOT ILLUMINATE. RECYCLED GEAR WITH SAME RESULT. CHECKED GEAR DOWN VISUAL (PEEP HOLE) AND NOSE LIGHT ILLUMIN - [SDR ABXA030162](https://openairdocs.org/sdr/ABXA030162), Apr 21, 2003: SKIN. DELAMINATED. LARGE AREA OF DELAMINATION ON UPPER AND LOWER SURFACE OF THE RIGHT WING INBOARD SPOILER PANEL. REPLACED SPOILER IAW DC-9 MM 27-61-01-4-0001. - [SDR ABXA030041](https://openairdocs.org/sdr/ABXA030041), Jan 17, 2003: OUTFLOW VALVE. LACK OF LUBE. AIRCRAFT WOULD NOT AUTO PRESSURIZE ON CLIMBOUT. MANUAL PRESSURIZATION ATTEMPTED, BUT OUTFLOW CONTROL WHEEL WOULD NOT MOVE. INSPECTED AND CLEANED OUTFLOW VALVE A - [SDR ABXA020276](https://openairdocs.org/sdr/ABXA020276), Oct 29, 2002: ACTUATOR. FAILED. RUDDER PEDALS WERE STIFF DURING CONTROL CHECK, ON CLIMB OUT OF ICT. CLIMBING TO FL 350, AIRCRAFT STARTED TO YAW AND DUTCH ROLL. DISCONNECTED AUTO PILOT. TURNING - [SDR ABXA020188](https://openairdocs.org/sdr/ABXA020188), Sep 11, 2002: CONTROL CABLE. BROKEN. ON INITIAL CLIMB OUT, EXCESSIVE NOISE AND VIBRATION IN VICINITY OF NOSE GEAR. WHEN GEAR LOWERED, NOISE, VIBRATION STOPPED. FOUND RIGHT FORWARD NOSE GEAR DOOR OP - [SDR ABXA010467](https://openairdocs.org/sdr/ABXA010467), Aug 16, 2001: FITTING. CORRODED. LEFT SLANT PANEL, OUTBOARD ATTACH FITTING WAS CORRODED. REPLACED FITTING IAW DC-9 SRM 51-30-5. - [SDR ABXA010466](https://openairdocs.org/sdr/ABXA010466), Aug 14, 2001: PANEL. CORRODED. LEFT SLANT PANEL WAS CORRODED AROUND THE LOWER NUTPLATES. LEVEL II CORROSION. INSTALLED NEW SLANT PANEL IAW DC-9 SRM 51-30-1. - [SDR ABXA010465](https://openairdocs.org/sdr/ABXA010465), Aug 14, 2001: PANEL. CORRODED. RIGHT SLANT PANEL WAS CORRODED AROUND NUTPLATES ON THE LOWER EDGE OF PANEL. LEVEL II CORROSION. INSTALLED NEW SLANT PANEL IAW DC-9 SRM. - [SDR ABXA010362](https://openairdocs.org/sdr/ABXA010362), Jul 3, 2001: BATTERY PACK. DISCHARGED. COCKPIT EMERGENCY LIGHTING WAS FOUND TO BE INOPERATIVE AT RFD. MAINTENANCE INSPECTED AND RE-SEATED THE EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE COM - [SDR ABXA010219](https://openairdocs.org/sdr/ABXA010219), May 7, 2001: SWITCH. INTERMITTENT. THE EMERGENCY EVACUATION LIGHT SWITCH WAS REPORTED AS INTERMITTENT. MAINTENANCE INSPECTED AND REPLACED THE COCKPIT EMERGENCY LIGHT CONTROL SWITCH, AND RELAMPED - [SDR ABXA000432](https://openairdocs.org/sdr/ABXA000432), Sep 25, 2000: BATTERY. DISCHARGED. DURING PRE-DEPARTURE CHECK, NOTED COCKPIT EMERGENCY LIGHTS INOP. REPLACED COCKPIT EMERGENCY LIGHT BATTERIES IAW DC9 MM 33-51-0-2. OPS CHECKED GOOD. - [SDR ABXA000418](https://openairdocs.org/sdr/ABXA000418), Sep 14, 2000: LIGHT. INOPERATIVE. DURING PREFLIGHT INSPECTION, FOUND THE EMERGENCY LIGHTS INOPERATIVE. RESECURED WIRING TO OVERHEAD LIGHT SOCKET. - [SDR ABXA000133](https://openairdocs.org/sdr/ABXA000133), Feb 23, 2000: BATTERY. DISCHARGED. DURING COCKPIT CHECK, EMERGENCY EVAC LIGHT FOUND NOT WORKING WHEN SWITCH WAS IN THE ON POSITION. REPLACED EMERGENCY LIGHT BATTERY SUPPLY IAW DC9 SMM 33-53-00. O - [SDR ABXA000050](https://openairdocs.org/sdr/ABXA000050), Jan 6, 2000: WEB. CORRODED. DURING C-CHECK, FOUND THE AFT LOWER CARGO COMPARTMENT AFT BULKHEAD WEB EXFOLIATED AND RIVET HEADS POPPED JUST ABOVE LONGERON 30 ON BOTH SIDES OF BULKHEAD CENTER - [SDR ABXA000049](https://openairdocs.org/sdr/ABXA000049), Jan 6, 2000: PANEL. CRACKED. DURING C-CHECK, FOUND THE LEFT INBOARD SPOILER CRACKED AT THE UPPER SURFACE CUT-OUT. REPLACED SPOILER PANEL IAW DC9 SMM 27-61-01.. - [SDR ABXA000048](https://openairdocs.org/sdr/ABXA000048), Jan 6, 2000: FITTING. CRACKED. DURING C-CHECK, FOUND THE FLOORBEAM FITTING AT STATION 579 JUST BELOW CUSP WEB RIGHT SIDE CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5. - [SDR ABXA000065](https://openairdocs.org/sdr/ABXA000065), Jan 3, 2000: FRAME. CRACKED. DURING C-CHECK, FOUND THE FUSELAGE FRAME FOOT FITTING AT STATION 579 RIGHT CRACKED AT BOLT HOLE. REPLACED FITTING IAW DC9 SRM 51-30-5. - [SDR ABXA000064](https://openairdocs.org/sdr/ABXA000064), Jan 3, 2000: WEB. CORRODED. DURING C-CHECK, FOUND THE CUSP WEB CORRODED AND CRACKED AT STATION 579 ON RIGHT SIDE. REPLACED CUSP WEB IAW DC9 SRM 53-01. - [SDR ABXA000063](https://openairdocs.org/sdr/ABXA000063), Jan 3, 2000: SPAR. CORRODED. DURING C-CHECK, FOUND THE FORWARD SIDE OF THE LOWER T-CAP OF THE FRONT SPAR CORRODED AT LBL 5 TO RBL 12 (CENTER WING). REPLACED FINGER DOUBLER IAW DC9 SRM 51-30 - [SDR ABXA000054](https://openairdocs.org/sdr/ABXA000054), Jan 3, 2000: FLOORBEAM. CORRODED. DURING C-CHECK, FOUND FLOORBEAM AT STATION 965 AND RBL 8 CORRODED. REPAIRED FLOORBEAM IAW ABX REA D95334885 MR. All 82: https://openairdocs.org/deregistered/N934AX-2011-04-18/reports.md ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19891024058459I](https://openairdocs.org/incident/19891024058459I), Oct 24, 1989: Doug DC933F (N934AX), St Louis, MO. Aircraft had locked brake which required extra power to taxi. Jet blast damaged hangar. --- 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.