# Service difficulty reports: N934AX, cancelled Apr 18, 2011

A list on [N934AX, cancelled Apr 18, 2011](https://openairdocs.org/deregistered/N934AX-2011-04-18.md).

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

Page 1 of 2 · 82 reports

- [SDR ABXR201009250052](https://openairdocs.org/sdr/ABXR201009250052.md): Control Cable · corroded · Sep 25, 2010 · N934AX · Doug DC933F · Engine Thrust Reverser
  > DURING FERRY FLIGHT PREP FOUND CABLE 51C CORRODED FWD OF APB. R & R CABLE 51C IAW AMM.
- [SDR ABXR201009250051](https://openairdocs.org/sdr/ABXR201009250051.md): Control Cable · broken · Sep 25, 2010 · N934AX · Doug DC933F · Power Lever
  > 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 AMM.
- [SDR ABXR201009250050](https://openairdocs.org/sdr/ABXR201009250050.md): Control Cable · broken · Sep 25, 2010 · N934AX · Doug DC933F · Engine Thrust Reverser
  > 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.md): Control Cable · broken · Sep 25, 2010 · N934AX · Doug DC933F · Engine Thrust Reverser
  > DURING FERRY FLIGHT PREP FOUND THRUST REVERSER CONTROL CABLE 48C BROKEN. R & R CABLE 48C IAW AMM.
- [SDR ABXR201009250048](https://openairdocs.org/sdr/ABXR201009250048.md): Control Cable · broken · Sep 25, 2010 · N934AX · Doug DC933F · Engine Thrust Reverser
  > 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.md): Push-Pull Cable · damaged · Sep 25, 2010 · N934AX · Doug DC933F · Power Lever
  > 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.md): Yoke · corroded · Sep 25, 2010 · N934AX · Doug DC933F · Nacelle/Pylon, Main Frame
  > 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.md): Fitting · corroded · Sep 25, 2010 · N934AX · Doug DC933F · Nacelle/Pylon Miscellaneous Structure
  > 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.md): Fitting · corroded · Sep 25, 2010 · N934AX · Doug DC933F · Nacelle/Pylon Miscellaneous Structure
  > 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.md): Mount · corroded · Sep 25, 2010 · N934AX · Doug DC933F · Engine Mount Section
  > 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.md): Isolator · corroded · Sep 25, 2010 · N934AX · Doug DC933F · Engine Mount Section
  > 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.md): Isolator · corroded · Sep 25, 2010 · N934AX · Doug DC933F · Engine Mount Section
  > 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.md): Mount · corroded · Sep 25, 2010 · N934AX · Doug DC933F · Engine Mount Section
  > 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.md): Link · corroded · Sep 24, 2010 · N934AX · Doug DC933F · Engine Mount Section
  > 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.md): Battery · discharged · Nov 5, 2007 · N934AX · Doug DC933F · Emergency Lighting
  > 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.md): Window · out of adjust · Sep 20, 2007 · N934AX · Doug DC933F · Flight Compartment Windows
  > 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.md): Linkage · lack of lube · Nov 10, 2006 · N934AX · Doug DC933F · Flight Compartment Windows
  > 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.md): Frame · cracked · Oct 13, 2006 · N934AX · Doug DC933F · Fuselage Main, Frame
  > 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.md): Angle · cracked · Oct 13, 2006 · N934AX · Doug DC933F · Fuselage Miscellaneous Structure
  > 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.md): Rod End · broken · Jan 25, 2006 · N934AX · Doug DC933F · Leading Edge Slat Actuator
  > UPON SLAT EXTENSION, AIRCRAFT ROLLED TO THE RIGHT AND SLAT DISAGREEMENT LIGHT ILLUMINATED AND THE SLAT EXTEND LIGHT DID NOT ILLUMINATE AFTER RECYCLING SLATS, NORMAL INDICATIONS WERE OBTAINED. FOUND BROKEN ROD END ON LEFT WING INBOARD SLAT ACTUATOR. REMOVED A
- [SDR ABXA050039](https://openairdocs.org/sdr/ABXA050039.md): Contact · worn · Mar 2, 2005 · N934AX · Doug DC933F · Landing Gear Position and Warning
  > 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 (APPROXIMATELY 30 SECONDS). FOUND BULB CONTACTS TO BE WORN. RELAMPED, OPS CHECKED GOOD.
- [SDR ABXA040387](https://openairdocs.org/sdr/ABXA040387.md): Window · stuck · Dec 1, 2004 · N934AX · Doug DC933F · Flight Compartment Windows
  > 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.md): Bearing · cracked · Nov 16, 2004 · N934AX · Doug DC933F · Horizontal Stabilizer Structure
  > 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.md): Frame · cracked · Nov 12, 2004 · N934AX · Doug DC933F · Fuselage Main, Frame
  > 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.md): Skin · cracked · Nov 11, 2004 · N934AX · Doug DC933F · Fuselage Main, Plate/Skin
  > 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.md): Skin · cracked · Nov 11, 2004 · N934AX · Doug DC933F · Fuselage Main, Plate/Skin
  > 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 SR09530252-7001 AND DC-9 SRM 53-05.
- [SDR ABXA040397](https://openairdocs.org/sdr/ABXA040397.md): Frame · cracked · Nov 11, 2004 · N934AX · Doug DC933F · Fuselage Main, Frame
  > 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.md): Skin Panel · cracked · Nov 11, 2004 · N934AX · Doug DC933F · Fuselage Main, Plate/Skin
  > 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.md): Frame · cracked · Nov 10, 2004 · N934AX · Doug DC933F · Fuselage Main, Frame
  > 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.md): Longeron · cracked · Nov 10, 2004 · N934AX · Doug DC933F · Fuselage Main, Longeron/Stringer
  > 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.md): Switch · malfunctioned · Mar 23, 2004 · N934AX · Doug DC933F · Landing Gear Position and Warning
  > 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 ILLUMINATED AT 500 FT AGL ON FINAL. FOUND WIRING HARNESS KINKED BEHIND DOWNLOCK SWITCH CANNON PLUG. RE-
- [SDR ABXA030162](https://openairdocs.org/sdr/ABXA030162.md): Skin · delaminated · Apr 21, 2003 · N934AX · Doug DC933F · Spoilers
  > 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.md): Outflow Valve · lack of lube · Jan 17, 2003 · N934AX · Doug DC933F · Pressure Regulator/Outflow Valve
  > AIRCRAFT WOULD NOT AUTO PRESSURIZE ON CLIMBOUT. MANUAL PRESSURIZATION ATTEMPTED, BUT OUTFLOW CONTROL WHEEL WOULD NOT MOVE. INSPECTED AND CLEANED OUTFLOW VALVE AS REQUIRED. NO DEFECTS NOTED. REMOVED CIRCUIT BREAKER COLLARS FROM CABIN PRESS CONTROL. OPS CHE
- [SDR ABXA020276](https://openairdocs.org/sdr/ABXA020276.md): Actuator · failed · Oct 29, 2002 · N934AX · Doug DC933F · Rudder Tab Control System
  > 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 OFF YAW DAMPER AND GOING TO MANUAL RUDDER DID NOT STOP YAW/DUTCH ROLL. AIRCRAFT SLOWED AND DESCEND
- [SDR ABXA020188](https://openairdocs.org/sdr/ABXA020188.md): Control Cable · broken · Sep 11, 2002 · N934AX · Doug DC933F · Landing Gear Door Retract Section
  > 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 OPEN, AND DOOR STOP CABLE BROKEN. REPLACED LEFT AND RIGHT NOSE GEAR DOOR STOP CABLES IAW DC-9 MM 32
- [SDR ABXA010467](https://openairdocs.org/sdr/ABXA010467.md): Fitting · corroded · Aug 16, 2001 · N934AX · Doug DC933F · Fuselage Structure (General)
  > LEFT SLANT PANEL, OUTBOARD ATTACH FITTING WAS CORRODED. REPLACED FITTING IAW DC-9 SRM 51-30-5.
- [SDR ABXA010466](https://openairdocs.org/sdr/ABXA010466.md): Panel · corroded · Aug 14, 2001 · N934AX · Doug DC933F · Fuselage Structure (General)
  > 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.md): Panel · corroded · Aug 14, 2001 · N934AX · Doug DC933F · Fuselage Structure (General)
  > 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.md): Battery Pack · discharged · Jul 3, 2001 · N934AX · Doug DC933F · Emergency Lighting
  > COCKPIT EMERGENCY LIGHTING WAS FOUND TO BE INOPERATIVE AT RFD. MAINTENANCE INSPECTED AND RE-SEATED THE EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. IN ILN AS A PRECAUTION, MAINTENANCE INSPECTED AN
- [SDR ABXA010219](https://openairdocs.org/sdr/ABXA010219.md): Switch · intermittent · May 7, 2001 · N934AX · Doug DC933F · Emergency Lighting
  > THE EMERGENCY EVACUATION LIGHT SWITCH WAS REPORTED AS INTERMITTENT. MAINTENANCE INSPECTED AND REPLACED THE COCKPIT EMERGENCY LIGHT CONTROL SWITCH, AND RELAMPED THE EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVI
- [SDR ABXA000432](https://openairdocs.org/sdr/ABXA000432.md): Battery · discharged · Sep 25, 2000 · N934AX · Doug DC933F · Emergency Lighting
  > 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.md): Light · inoperative · Sep 14, 2000 · N934AX · Doug DC933F · Emergency Lighting
  > DURING PREFLIGHT INSPECTION, FOUND THE EMERGENCY LIGHTS INOPERATIVE. RESECURED WIRING TO OVERHEAD LIGHT SOCKET.
- [SDR ABXA000133](https://openairdocs.org/sdr/ABXA000133.md): Battery · discharged · Feb 23, 2000 · N934AX · Doug DC933F · Emergency Lighting
  > 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. OPS CHECKED GOOD.
- [SDR ABXA000050](https://openairdocs.org/sdr/ABXA000050.md): Web · corroded · Jan 6, 2000 · N934AX · Doug DC933F · Fuselage Main, Bulkhead
  > 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 SUPPORT. REPLACED WEB IAW DC9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA000049](https://openairdocs.org/sdr/ABXA000049.md): Panel · cracked · Jan 6, 2000 · N934AX · Doug DC933F · Spoilers
  > 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.md): Fitting · cracked · Jan 6, 2000 · N934AX · Doug DC933F · Fuselage Miscellaneous Structure
  > 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.md): Frame · cracked · Jan 3, 2000 · N934AX · Doug DC933F · Fuselage Main, Frame
  > 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.md): Web · corroded · Jan 3, 2000 · N934AX · Doug DC933F · Fuselage Miscellaneous Structure
  > 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.md): Spar · corroded · Jan 3, 2000 · N934AX · Doug DC933F · Wing Spar
  > 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 51-30-2.
- [SDR ABXA000054](https://openairdocs.org/sdr/ABXA000054.md): Floorbeam · corroded · Jan 3, 2000 · N934AX · Doug DC933F · Fuselage Main, Floor Beam
  > DURING C-CHECK, FOUND FLOORBEAM AT STATION 965 AND RBL 8 CORRODED. REPAIRED FLOORBEAM IAW ABX REA D95334885 MR.

Next page: https://openairdocs.org/deregistered/N934AX-2011-04-18/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N934AX' AND deregistration_id = 'N934AX-2011-04-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N934AX-2011-04-18/reports

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