# Service difficulty reports: N813AX, cancelled May 15, 2007

A list on [N813AX, cancelled May 15, 2007](https://openairdocs.org/deregistered/N813AX-2007-05-15.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 · 54 reports

- [SDR ABXA060151](https://openairdocs.org/sdr/ABXA060151.md): Skin · corroded · Mar 23, 2006 · N813AX · Doug DC863 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE EXTERIOR FASTENER SHEARED AT LONGERON 39 LEFT AND SKIN BULGED AT FS -32.00. REPAIRED FUSELAGE EXTERIOR SKIN AT FS 32.00, LONGERON 30 LEFT IAW DC8 SRM 53-2-1, 51-1-8, AND DWG K04888.
- [SDR ABXA060149](https://openairdocs.org/sdr/ABXA060149.md): Strut · corroded · Mar 15, 2006 · N813AX · Doug DC863 · Main Landing Gear Strut/Axle/Truck
  > RIGHT MAIN LANDING GEAR STRUT CYLINDER SHOWED PITTING ALONG THE INNER SURFACE AT LOWER FLANGE AT CHROME AREA. DAMAGED GLAND THREADS. RIGHT MAIN LANDING GEAR STRUT ASSEMBLY REMOVED AND REPLACED WITH SERVICABLE UNIT IAW MM 32-40-1-02, 32-42-01-4 AND 32-43-02-2
- [SDR ABXA060150](https://openairdocs.org/sdr/ABXA060150.md): Support · cracked · Mar 14, 2006 · N813AX · Doug DC863 · Ailerons
  > RIGHT INBOARD AILERON MANUAL REVERSION MECHANISM CRACKED AT UPPER MOUNT HOLE. REMOVED AND REPLACED SUPPORT ASSEMBLY ON AILERON MANUAL REVERSION MECHANISM IAW DC8 OHM 27-6-2.
- [SDR ABXA060148](https://openairdocs.org/sdr/ABXA060148.md): Fitting · cracked · Mar 13, 2006 · N813AX · Doug DC863 · Wing, Attach Fittings
  > FOUND RIGHT WING FUEL, NR 6 STRINGER TIE INSIDE PANEL 505C CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.
- [SDR ABXA060147](https://openairdocs.org/sdr/ABXA060147.md): Fitting · corroded · Mar 13, 2006 · N813AX · Doug DC863 · Fuselage Main, Attach Fittings
  > RIGHT WHEEL WELL LONGERON 24 RIGHT, BATHTUB FITTING STA 879 CORRODED. DAMAGE OUT OF LIMITS AND CRACKED. REMOVED CORRODED BATHTUB FITTING. DRILLED UP NEW ONE AND INSTALLED IAW DC8 SRM 53-2-0.
- [SDR ABXA050189](https://openairdocs.org/sdr/ABXA050189.md): Engine · failed · Aug 17, 2005 · N813AX · Doug DC863 · Engine (Turbine/Turboprop)
  > LOW OIL PRESSURE LIGHT NR 2 ENGINE OIL PRESSURE DROPPED TO 30 PSI. SHUT DOWN NR 2 ENGINE DOWN AT 0350Z. ZERO OIL PRESSURE AFTER ENGINE SHUT DOWN. REMOVED AND REPLACED NR 2 ENGINE IAW JOB CARD 8090507 AND WORK PACK 600230688.
- [SDR ABXA040137](https://openairdocs.org/sdr/ABXA040137.md): Floorbeam · corroded · Apr 5, 2004 · N813AX · Doug DC863 · Fuselage Main, Floor Beam
  > MAIN CABIN STA 920 FLOORBEAM LOWER FLANGE FORWARD SIDE WAS CORRODED APPROXIMATELY 5 INCHES INBOARD OF CUSP LEFT SIDE. REPAIRED AREA IAW REA D853-49122MR.
- [SDR ABXA010896](https://openairdocs.org/sdr/ABXA010896.md): Fitting · cracked · May 16, 2002 · N813AX · Doug DC863 · Fuselage Structure (General)
  > EMPENNAGE INTERIOR LONGERON 17 LEFT, END FITTING WAS CRACKED AT F.S. 1769. REPLACED END FITTING IAW DC-8 SRM 51-1-21, 51-3-2 AND 51-1-20D.
- [SDR ABXA010895](https://openairdocs.org/sdr/ABXA010895.md): Spar · cracked · May 13, 2002 · N813AX · Doug DC863 · Wing, Plate/Skin
  > LEFT WING AT STATION 515 - 526, HOLES 4 AND 5 FROM THE INBOARD SIDE, SHOWED CRACK INDICATION. REPAIRED AREA IAW REA D857-43866MR.
- [SDR ABXA010894](https://openairdocs.org/sdr/ABXA010894.md): Fitting · cracked · May 13, 2002 · N813AX · Doug DC863 · Fuselage Structure (General)
  > EMPENNAGE INTERIOR LONGERON 17 RIGHT, WAS CRACKED AT F.S. 1769. REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-8 AND 51-1-20D.
- [SDR ABXA010893](https://openairdocs.org/sdr/ABXA010893.md): Fitting · cracked · May 13, 2002 · N813AX · Doug DC863 · Fuselage Miscellaneous Structure
  > EMPENNAGE INTERIOR LONGERON 17 RIGHT, END FITTING WAS CRACKED AT FS 1769. REPLACED END FITTING IAW DC-8 SRM 51-3-2 AND 51-1-20D.
- [SDR ABXA010891](https://openairdocs.org/sdr/ABXA010891.md): Skin · cracked · May 13, 2002 · N813AX · Doug DC863 · Fuselage Main, Plate/Skin
  > L-1 DOOR, LOWER FORWARD CORNER, HAD A CRACK INDICATION AT EDGE OF MIDDLE LAYER SKIN. FABRICATED DOUBLER AND TRIPLER, AND REPAIRED AREA IAW DC-8 SRM 51-1-21, 53-20, 53-2-0, 51-1-8, AND DOUGLAS NDT SPM 06-10-01-001.
- [SDR ABXA010892](https://openairdocs.org/sdr/ABXA010892.md): Strap · broken · May 8, 2002 · N813AX · Doug DC863 · Wing, Attach Fittings
  > LOWER FRONT SPAR CAP, OUTBOARD OF #3 PYLON, #4 MAIN STRAP WAS BROKEN. REPLACED STRAP AND COMPLIED WITH REA #D857-43875.
- [SDR ABXA010001](https://openairdocs.org/sdr/ABXA010001.md): Handle · malfunctioned · Jan 8, 2001 · N813AX · Doug DC863 · Landing Gear Retraction/Extension System
  > LANDING GEAR HANDLE WOULD NOT COME UP AFTER TAKEOFF. PRESSURIZATION WAS NORMAL AND THERE WAS NO WARNING HORN. CREW PUSHED IN THE ANTI-RETRACT LATCH AND LANDING GEAR CAME UP NORMALLY. ON DESCENT INTO ILN, CREW RE-CYCLED LANDING GEAR. THE LANDING GEAR OPERATED N
- [SDR ABXA000518](https://openairdocs.org/sdr/ABXA000518.md): Bleed Valve · malfunctioned · Dec 1, 2000 · N813AX · Doug DC863 · Compressor Bleed Valve
  > AT CRUISE, FL 330 ENGINE A/I ON NR 3 ENGINE STARTED TO COMPRESSURE STALL. TURNED IGNITION ON, ENGINE STOPPED STALLING. AFTER FIVE MINUTES, CREW TURNED IGNITION OFF. THE ENGINE STARTED STALLING AGAIN. THE CREW SECURED THE NUMBER THREE ENGINE. CREW REPORTED THAT
- [SDR ABXA000102](https://openairdocs.org/sdr/ABXA000102.md): Skin · cracked · Feb 7, 2000 · N813AX · Doug DC863 · Wing, Plate/Skin
  > RIGHT FLAP WEDGE MIDDLE WEDGE HAS SEPERATING SKIN AND INNER ATTACH ANGLE CRACKED. REPAIRED RIGHT OUTBOARD FLAP REMOVEABLE SEGMENT, IAW ABX REA D857-34763-MR.
- [SDR ABXA000101](https://openairdocs.org/sdr/ABXA000101.md): Skin · cracked · Feb 7, 2000 · N813AX · Doug DC863 · Wing, Plate/Skin
  > RIGHT OUTBOARD FLAP WEDGE MIDDLE OUTBOARD WEDGE HAS GOUGED AND CRACKED CORNER. REPAIRED RIGHT OUTBOARD TRAILING EDGE FLAP REMOVEABLE SEGMENT, IAW ABX REA D857-34769-MR.
- [SDR ABXA9900813](https://openairdocs.org/sdr/ABXA9900813.md): Ballast · failed · Nov 30, 1999 · N813AX · Doug DC863 · Flight Compartment Lighting
  > COCKPIT INSTRUMENT LIGHTS FAILED AND BURNING ODOR WAS NOTICED. PULLED CIRCUIT BREAKER AND SMELL DISSIPATED. REPLACED LIGHTING BALLAST IAW DC8 MM, OPS CHECKED GOOD.
- [SDR ABXA9900806](https://openairdocs.org/sdr/ABXA9900806.md): Switch · corroded · Nov 26, 1999 · N813AX · Doug DC863 · Landing Gear Position and Warning
  > RIGHT MAIN LANDING GEAR DOWN LIGHT (GREEN) DID NOT ILLUMINATE AFTER GEAR EXTENSION. RED UNSAFE LIGHT DID NOT ILLUMINATE. RECYCLED LANDING GEAR, RIGHT GEAR LIGHT CAME ON. REPLACED MAIN GEAR DOWNLOCK SWITCH IAW DC8 MM, OPS CHECKED GOOD.
- [SDR ABXA9900716](https://openairdocs.org/sdr/ABXA9900716.md): Actuator · out of adjust · Sep 15, 1999 · N813AX · Doug DC863 · Landing Gear Retraction/Extension System
  > NOSE LANDING GEAR FAILED UPLATCH CHECK AND FELL OUT OF THE WHEEL WELL. RECYCLED GEAR, NO HELP. PERFORMED ALTERNATE UPLATCH CHECK AND GEAR REMAINED IN WHEEL WELL. CHECKED ALL NOSE LANDING GEAR COMPONENTS. NO DEFECTS NOTED. ADJUSTED NOSE LANDING GEAR RETRAC
- [SDR ABXA9900343](https://openairdocs.org/sdr/ABXA9900343.md): Frame · cracked · Apr 11, 1999 · N813AX · Doug DC863 · Fuselage Main, Frame
  > FRAME AT STATION 520 AT LONGERON 34 RIGHT CRACKED. REPAIRED IAW DC8 SRM 53-2-0.
- [SDR ABXA9900335](https://openairdocs.org/sdr/ABXA9900335.md): Fitting · cracked · Mar 26, 1999 · N813AX · Doug DC863 · Fuselage Miscellaneous Structure
  > LOWER FORWARD CARGO COMPARTMENT, STATION 440-460, LONGERON 31 LEFT SPLICE CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D.
- [SDR ABXA9900316](https://openairdocs.org/sdr/ABXA9900316.md): Angle · cracked · Mar 20, 1999 · N813AX · Doug DC863 · Fuselage Miscellaneous Structure
  > STATION 220, LONGERON 31 RIGHT, FLOOR PANEL SUPPORT ANGLE CRACKED. REPAIRED ANGLE IAW REA D853-24965 AND DC8 SRM 51-1-20.
- [SDR ABXA9900342](https://openairdocs.org/sdr/ABXA9900342.md): Clip · cracked · Mar 18, 1999 · N813AX · Doug DC863 · Wing Miscellaneous Structure
  > RIGHT WING LEADING EDGE RIB CLIP CRACKED AT STATION XOLDI 6.225. REPLACED CLIP IAW DC8 SRM 57-3-0.
- [SDR ABXA9900317](https://openairdocs.org/sdr/ABXA9900317.md): Skin · cracked · Mar 18, 1999 · N813AX · Doug DC863 · Wing, Plate/Skin
  > RIGHT WING STATION 890.000, CRACK IS EMINATING FROM SCREW COUNTERSINK. REPAIRED IAW DC8 SRM 51-1-26.
- [SDR ABXA9900345](https://openairdocs.org/sdr/ABXA9900345.md): Rib · cracked · Mar 17, 1999 · N813AX · Doug DC863 · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE RIB CRACKED AT STATION XS 250.089. REPLACED ANGLE IAW DC8 SRM 51-1-20D.
- [SDR ABXA9900339](https://openairdocs.org/sdr/ABXA9900339.md): Fitting · cracked · Mar 17, 1999 · N813AX · Doug DC863 · Fuselage Miscellaneous Structure
  > STRINGER 31 LEFT SPLICE FITTING CRACKED BETWEEN STATIONS 600 AND 620. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D.
- [SDR ABXA9900338](https://openairdocs.org/sdr/ABXA9900338.md): Angle · cracked · Mar 17, 1999 · N813AX · Doug DC863 · Wing Miscellaneous Structure
  > RIGHT WING LEADING EDGE, INBOARD OF STATION XS 250.084 RIB AT THE AFT SIDE OF THE SLOT, VERTICAL ANGLE IS CRACKED. REPLACED VERTICAL ANGLE IAW DRAWING 5769859 AND DC8 SRM 57-3-3 AND 51-1-20D.
- [SDR ABXA9900334](https://openairdocs.org/sdr/ABXA9900334.md): Rib · cracked · Mar 17, 1999 · N813AX · Doug DC863 · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE RIB AT STATION XS 227.335 CRACKED AT AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0.
- [SDR ABXA9900347](https://openairdocs.org/sdr/ABXA9900347.md): Fitting · cracked · Mar 16, 1999 · N813AX · Doug DC863 · Fuselage Miscellaneous Structure
  > TAIL SKID UPPER HORIZONTAL ATTACH FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.
- [SDR ABXA9900344](https://openairdocs.org/sdr/ABXA9900344.md): Fitting · cracked · Mar 16, 1999 · N813AX · Doug DC863 · Fuselage Miscellaneous Structure
  > STATION 1220 BETWEEN LONGERONS 33 RIGHT AND 34 RIGHT, SHEAR TIE FITTING CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-20D.
- [SDR ABXA9900340](https://openairdocs.org/sdr/ABXA9900340.md): Fitting · cracked · Mar 16, 1999 · N813AX · Doug DC863 · Wing Miscellaneous Structure
  > NR 2 MAIN TANK, INBOARD OF XRS 74 BULKHEAD, FORWARD STRINGER 51, END FITTING CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-20D.
- [SDR ABXA9900333](https://openairdocs.org/sdr/ABXA9900333.md): Skin · corroded · Mar 16, 1999 · N813AX · Doug DC863 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STABILIZER LEADING EDGE AT STATION XFS 147.5 HAD INTERGRANULAR CORROSION. REPAIRED IAW DC8 SRM 55-2-1.
- [SDR ABXA9900341](https://openairdocs.org/sdr/ABXA9900341.md): Splice · cracked · Mar 15, 1999 · N813AX · Doug DC863 · Fuselage Miscellaneous Structure
  > SPLICE CRACKED BETWEEN STATION 1260 AND 1280, AT LONGERON 31 LEFT. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D.
- [SDR ABXA9900326](https://openairdocs.org/sdr/ABXA9900326.md): Fitting · cracked · Mar 14, 1999 · N813AX · Doug DC863 · Ailerons
  > RIGHT WING INBOARD AILERON, INBOARD ATTACH FITTING IS BROKEN OFF ON AILERON SIDE. REPLACED FITTING IAW DC8 SRM 27-10-00.
- [SDR ABXA9900337](https://openairdocs.org/sdr/ABXA9900337.md): Rib · cracked · Mar 13, 1999 · N813AX · Doug DC863 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE LOWER RIB CRACKED AT FASTENER END, FORWARD OF PANEL 518B, AT STATION XFS 772.5. REPAIRED IAW DC8 SRM 57-2-0.
- [SDR ABXA9900336](https://openairdocs.org/sdr/ABXA9900336.md): Rib · cracked · Mar 13, 1999 · N813AX · Doug DC863 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE UPPER RIB CRACKED AT FASTENER EDGE AT STATION XFS 735. REPAIRED IAW DC8 SRM 57-2-0.
- [SDR ABXA9900329](https://openairdocs.org/sdr/ABXA9900329.md): Skin · corroded · Mar 13, 1999 · N813AX · Doug DC863 · Wing, Plate/Skin
  > LEFT WING UPPER SURFACE AT FRONT SPAR BETWEEN STATIONS XOLDI 6.225 AND XFS 379.000 HAD HEAVY INTERNAL CORROSION. REPAIRED IAW DC8 SRM 57-2-1.
- [SDR ABXA9900328](https://openairdocs.org/sdr/ABXA9900328.md): Rib · cracked · Mar 13, 1999 · N813AX · Doug DC863 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE RIB CRACKED JUST FORWARD OF ACCESS PANEL NR 519A. REPAIRED IAW DC8 SRM 57-2-0.
- [SDR ABXA9900327](https://openairdocs.org/sdr/ABXA9900327.md): Skin · cracked · Mar 13, 1999 · N813AX · Doug DC863 · Wing, Plate/Skin
  > LEFT WING AT LEADING EDGE XFS 285.250 CRACKED AT 3 SCREWS. REPAIRED IAW DC8 SRM 57-2-1.
- [SDR ABXA9800590](https://openairdocs.org/sdr/ABXA9800590.md): Transmitter · clogged · Jun 30, 1998 · N813AX · Doug DC863 · Engine Oil Pressure
  > DURING CRUISE, NR 3 ENGINE OIL PRESSURE WENT TO 100 PSI. SECURED NR 3 ENGINE. REPLACED NR 3 ENGINE OIL PRESSURE TRANSMITTER AND OIL FILTER IAW DC8 MM 79-30-00.
- [SDR ABXA9800064](https://openairdocs.org/sdr/ABXA9800064.md): Hook · out of adjust · Feb 5, 1998 · N813AX · Doug DC863 · Landing Gear Retraction/Extension System
  > NOSE GEAR FAILED UPLATCH CHECK. RECYCLED GEAR SEVERAL TIMES AND PERFORMED ALTERNATE UPLATCH CHECK WITH SAME RESULTS. ADJUSTED NOSE UPLATCH MECHANISM IAW DC8 MM 32-31-0. PERFORMED GEAR SWING AND UPLATCH CHECK. OPS CHECKED GOOD.
- [SDR ABXA9701288](https://openairdocs.org/sdr/ABXA9701288.md): Retract Mech · lack of lube · Jul 23, 1997 · N813AX · Doug DC863 · Landing Gear Retraction/Extension System
  > NOSE GEAR EXTENDED SEVERAL TIMES DURING GEAR UPLATCH CHECK. LUBRICATED NOSE GEAR UPLATCH MECHANISM. OPS CHECKED IAW DC8 MM 32-31-00.
- [SDR ABXA9701129](https://openairdocs.org/sdr/ABXA9701129.md): O-Ring · worn · Jun 9, 1997 · N813AX · Doug DC863 · Hydraulic Pump (Electric/Engine), Main
  > HYRAULIC QUANTITY DROPPED AFTER TAKEOFF, TO 0 IN NORMAL. CONTINUED TO DROP SLOWLY DURING FLIGHT. EMERGENCY CHECKLIST WAS FOLLOWED UP TO ABNORMAL PROCEDURES. HYDRAULIC QUANTITY REMAINED ABOVE STAND-PIPE. LANDING WAS UNEVENTFUL. FOUND NR 3 ENGINE DRIVEN HYD
- [SDR ABXA9701042](https://openairdocs.org/sdr/ABXA9701042.md): Aileron · cracked · May 23, 1997 · N813AX · Doug DC863 · Ailerons
  > DURING C/P3 CHECK,.5 INCH LONG CRACK WAS FOUND IN LEFT WING AILERON BETWEEN STA'S XW617 AND XW630. *S/D* REPAIRED IAW DC-8 SRM 57-51-00.
- [SDR ABXA9701041](https://openairdocs.org/sdr/ABXA9701041.md): Skin · cracked · May 23, 1997 · N813AX · Doug DC863 · Nacelle/Pylon, Plate/Skin
  > DURING C/P3 CHECK, FOUND LOOSE FASTENERS IN REMOVABLE PLANK ON NR 1 PYLON. REPAIRED IAW ABX EA SB 54-04020MR.
- [SDR ABXA9700550](https://openairdocs.org/sdr/ABXA9700550.md): Aileron · broken · Dec 5, 1996 · N813AX · Doug DC863 · Ailerons
  > DURING LEVEL FLIGHT, BALL CENTERED, BOTH CONTROL WHEELS WERE COCKED APPPROXIMATELY 30 DEGREES TO THE RIGHT AND THERE WAS 30 DEGREES OF AILERON TRIM NEEDED. AS AIRCRAFT WAS SLOWED DOWN MORE AILERON TRIM WAS NEEDED TO KEEP AIRCRAFT LEVEL. REPLACED LEFT INBOARD
- [SDR ABXA9600501](https://openairdocs.org/sdr/ABXA9600501.md): Switch · defective · Jun 3, 1996 · N813AX · Doug DC863 · Landing Gear Position and Warning
  > DURING DESCENT, RIGHT MAIN LANDING GEAR DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER THE LANDING GEAR WAS EXTENDED. RECYCLED THE LANDING GEAR AND RIGHT MAIN LANDING GEAR DOWNLOCK LIGHT ILLUMINATED AFTER APPROXIMATELY TWO MINUTES. REPLACED RIGHT MAIN LANDING GEAR
- [SDR ABXA9500922](https://openairdocs.org/sdr/ABXA9500922.md): Angle · cracked · Sep 11, 1995 · N813AX · Doug DC863 · Pneumatic Distribution System
  > DURING 813AX C-CHECK INSPECTION, FOUND AFT BAND CLAMP ON NR 3 ENGINE TRANSITION DUCT CRACKED. REPAIRED ATTACH ANGLE CHANNEL ON NR 3 ENGINE TRANSITION DUCT IAW ABX REA D878-12566MR.
- [SDR ABXA9500921](https://openairdocs.org/sdr/ABXA9500921.md): Spar · damaged · Sep 11, 1995 · N813AX · Doug DC863 · Wing Spar
  > DURING 813AX C-CHECK INSPECTION, FOUND LEFT HAND WING AT STATION XCW 69.5 HAS 3 EACH DAMAGED HOLES IN FORWARD LEG OF FORWARD LOWER SPAR CAP IN CENTER TANK. REPAIRED DAMAGED HOLES AT LEFT WING STATION XCW 69.5 IAW ABX REA D857-12575MR.

Next page: https://openairdocs.org/deregistered/N813AX-2007-05-15/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 = 'N813AX' AND deregistration_id = 'N813AX-2007-05-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N813AX-2007-05-15/reports

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