# Service difficulty reports: N802AX, cancelled Mar 12, 2004

A list on [N802AX, cancelled Mar 12, 2004](https://openairdocs.org/deregistered/N802AX-2004-03-12.md).

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

- [SDR ABXA9900285](https://openairdocs.org/sdr/ABXA9900285.md): Skin · corroded · Mar 9, 1999 · N802AX · Doug DC862 · Wing, Plate/Skin
  > DURING C-CHECK, FOUND LEVEL-2 CORROSION AROUND LEADING EDGE SCREW HOLE FORWARD OF INBOARD END OF OUTBOARD SLOT PANEL, RIGHT WING. REPAIRED IAW ABX REA D827-26073MR.
- [SDR ABXA9900290](https://openairdocs.org/sdr/ABXA9900290.md): Web · corroded · Mar 4, 1999 · N802AX · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND UPPER CARGO COMPARTMENT RIGHT CUSP WEB AT STATION 477 CORRODED. REPAIRED CUSP WEB IAW ABX REA D853-26780MR.
- [SDR ABXA9900291](https://openairdocs.org/sdr/ABXA9900291.md): Pan · cracked · Feb 24, 1999 · N802AX · Doug DC862 · Service Doors
  > DURING C-CHECK, FOUND CRACK IN FORWARD SERVICE DOOR PAN AT SECOND DOOR STOP FROM BOTTOM, FORWARD SIDE OF DOOR. REPAIRED IAW ABX REA D853-27050MR.
- [SDR ABXA9900284](https://openairdocs.org/sdr/ABXA9900284.md): Skin · cracked · Feb 24, 1999 · N802AX · Doug DC862 · Wing, Plate/Skin
  > DURING C-CHECK, FOUND LOWER SURFACE OF RIGHT OUTBOARD LEADING EDGE CRACKED AT SCREW HOLES AT STATIONS FS 743, 746, 762, 765, 768, 771 AND 780. REPAIRED IAW DC8 SRM 57-2-1.
- [SDR ABXA9900283](https://openairdocs.org/sdr/ABXA9900283.md): Skin · cracked · Feb 24, 1999 · N802AX · Doug DC862 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND CRACK IN FUSELAGE SKIN AT UPPER AFT CORNER OF LEFT AIRCRAFT PASSENGER DOOR CUTOUT. REPAIRED IAW DC8 SRM 53-2-0.
- [SDR ABXA9900282](https://openairdocs.org/sdr/ABXA9900282.md): Skin · cracked · Feb 24, 1999 · N802AX · Doug DC862 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND SKIN CRACKED AT RIGHT AFT CORNER OF RIGHT FORWARD SERVICE DOOR CUTOUT. REPAIRED IAW DC8 SRM 53-2-0.
- [SDR ABXA9900274](https://openairdocs.org/sdr/ABXA9900274.md): Angle · cracked · Feb 24, 1999 · N802AX · Doug DC862 · Nacelle/Pylon Structure
  > DURING C-CHECK, FOUND NR 2 PYLON INBOARD VERTICAL ATTACH ANGLE CRACKED AFT OF FOOTSTOOL FITTING. REPAIRED IAW DC8 SRM 54-22.
- [SDR ABXA9900277](https://openairdocs.org/sdr/ABXA9900277.md): Longeron · corroded · Feb 23, 1999 · N802AX · Doug DC862 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND LEVEL 2 CORROSION ON LONGERON 33 RIGHT AT STATION 1500. REPLACED LONGERON 33 RIGHT IAW DC8 SRM 51-1-21 AND 51-1-20D.
- [SDR ABXA9900296](https://openairdocs.org/sdr/ABXA9900296.md): Fitting · corroded · Feb 18, 1999 · N802AX · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND LEVEL 2 CORROSION ON FRAME TO CUSP ATTACH FITTING AT STATION 1458 RIGHT. REPLACED FITTING IAW DC8 SRM 51-3-0 AND 51-1-21.
- [SDR ABXA9900295](https://openairdocs.org/sdr/ABXA9900295.md): Frame · cracked · Feb 18, 1999 · N802AX · Doug DC862 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND FRAME CRACKED AT STATION 1180 RIGHT, AT FLOOR LEVEL. REPAIRED FRAME IAW DC8 SRM 53-2-0.
- [SDR ABXA9900294](https://openairdocs.org/sdr/ABXA9900294.md): Fitting · corroded · Feb 18, 1999 · N802AX · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND LEVEL 2 CORROSION ON FITING AT 1180, RIGHT SIDE OF CUSP. REPLACED FITTING IAW DC8 SRM 51-3-0 AND 51-1-21.
- [SDR ABXA9900293](https://openairdocs.org/sdr/ABXA9900293.md): Fitting · cracked · Feb 18, 1999 · N802AX · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND FUSELAGE FRAME FITTING CRACKED AFT SIDE AT BOTTOM OF LONGERON 11 RIGHT, STATION 682. REPLACED FRAME FITTING IAW DC8 SRM 51-3-0 AND 51-1-21.
- [SDR ABXA9900292](https://openairdocs.org/sdr/ABXA9900292.md): Fitting · cracked · Feb 18, 1999 · N802AX · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND FITTING CRACKED AT LONGERON 11 LEFT, STATION 680. REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51-3-0.
- [SDR ABXA9900289](https://openairdocs.org/sdr/ABXA9900289.md): Fitting · corroded · Feb 18, 1999 · N802AX · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND CORROSION ON CUSP FITTING AT STATION 1200 LT SIDE. REPLACED FITTING IAW DC8 SRM 51-30-0 AND 51-1-20D.
- [SDR ABXA9900288](https://openairdocs.org/sdr/ABXA9900288.md): Fitting · corroded · Feb 18, 1999 · N802AX · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND CORROSION ON STATION 1530 PRODUCTION SPLICE FITTING AT LONGERON 34 RIGHT. REPLACED FITTING IAW DC8 SRM 51-30-0 AND 51-1-20D.
- [SDR ABXA9900287](https://openairdocs.org/sdr/ABXA9900287.md): Fitting · corroded · Feb 18, 1999 · N802AX · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND CORROSION ON LONGERON FITTING, STATION 1540, LONGERON 32 RIGHT AT AFT PRESSURE BULKHEAD. REPLACED FITTING IAW DC8 SRM 51-3-0 AND 51-1-21.
- [SDR ABXA9900279](https://openairdocs.org/sdr/ABXA9900279.md): Fitting · cracked · Feb 18, 1999 · N802AX · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND PRODUCTION SPLICE FITTING CRACKED AT STATION 1530, LONGERON 34 LEFT. REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51-3-0.
- [SDR ABXA9900278](https://openairdocs.org/sdr/ABXA9900278.md): Fitting · cracked · Feb 18, 1999 · N802AX · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND 3 FITTINGS CRACKED AT BOTTOM OF KEEL BEAM BETWEEN MAIN LANDING GEAR DOORS, STATION 940 TO 960. REPLACED KEEL BEAM FITTINGS IAW DC8 SRM 51-3-0.
- [SDR ABXA9900276](https://openairdocs.org/sdr/ABXA9900276.md): Fitting · cracked · Feb 18, 1999 · N802AX · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND PRODUCTION SPLICE FITTING AT STATION 1530 LONGERON 34 RIGHT CRACKED AND CORRODED. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-21 AND 51-3-0.
- [SDR ABXA9900275](https://openairdocs.org/sdr/ABXA9900275.md): Link · cracked · Feb 18, 1999 · N802AX · Doug DC862 · Nacelle/Pylon Structure
  > DURING C-CHECK, FOUND NR 2 PYLON OUTBOARD THRUST LINK CRACKED. REPLACED PYLON THRUST LINK IAW DC8 MM 71-20-1.
- [SDR ABXA9800914](https://openairdocs.org/sdr/ABXA9800914.md): Clamp · loose · Oct 14, 1998 · N802AX · Doug DC862 · Air Distribution System
  > AT FL 220, A LOUD BANG OCCURRED AND CABIN PRESSURE BEGAN TO INCREASE 500 FT PER MIN. INITIATED EMERGENCY DESCENT INTO BFI. FOUND RIGHT HEAT EXCHANGER DUCT CLAMP NOT SECURED. RESECURED CLAMP, OPS CHECKED GOOD.
- [SDR ABXA9800601](https://openairdocs.org/sdr/ABXA9800601.md): Switch · inoperative · Jul 3, 1998 · N802AX · Doug DC862 · Landing Gear Position and Warning
  > ON GEAR EXTENSION RT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE. RECYCLED GEAR, LIGHT ILLUMINATED. REPLACED RIGHT MAIN LANDING GEAR INDICATION SWITCH IAW DC8 MM 32-60-00.
- [SDR ABXA9800448](https://openairdocs.org/sdr/ABXA9800448.md): Light · loose · May 12, 1998 · N802AX · Doug DC862 · Emergency Lighting
  > DURING CRUISE EMERGENCY LIGHT ON CAPTAIN'S SIDE WAS ARCING BETWEEN LIGHT ASSEMBLY BRACKET AND BULB. LIGHT ASSEMBLY WAS LOOSE IN MOUNT. TIGHTENED MOUNT NUT. OPS CHECKED GOOD IAW DC8 MM 33-00.
- [SDR ABXA9701996](https://openairdocs.org/sdr/ABXA9701996.md): Battery · discharged · Dec 19, 1997 · N802AX · Doug DC862 · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY PACK.
- [SDR ABXA9701289](https://openairdocs.org/sdr/ABXA9701289.md): Pressure Web · corroded · Jul 25, 1997 · N802AX · Doug DC862 · Fuselage Miscellaneous Structure
  > NUMEROUS SHEARED FASTENERS AT PRESSURE PANEL, RT NLG TUNNEL AREA STA 160. REPAIRED IAW SRM 51-1-8 AND ABX REA D853-19564-MR.
- [SDR ABXA9701284](https://openairdocs.org/sdr/ABXA9701284.md): Longeron · cracked · Jul 21, 1997 · N802AX · Doug DC862 · Fuselage Main, Longeron/Stringer
  > FORWARD WEB AT FS 960 TO 980, LONGERON 24 IS CRACKED. REPAIRED IAW DC-8 SRM 53-2-0.
- [SDR ABXA9701283](https://openairdocs.org/sdr/ABXA9701283.md): Frame · cracked · Jul 21, 1997 · N802AX · Doug DC862 · Fuselage Miscellaneous Structure
  > CONTROL PEDESTAL FRAME CASTING CRACKED, LT AT BASE (FLOOR ATTACH POINT). REPAIRED IAW DC8 SRM 51-1-21 AND ABX REA D853-19823MR.
- [SDR ABXA9701282](https://openairdocs.org/sdr/ABXA9701282.md): Pressure Panel · corroded · Jul 21, 1997 · N802AX · Doug DC862 · Fuselage Miscellaneous Structure
  > FOUND CORROSION DAMAGE ON RT PRESSURE PANEL, UNDER PRODUCTION FINGER DOUBLERS WEB AT FS 159.5 TO FS 228. *S/D* REPAIRED IAW DC8 SRM 51-1-8 AND ABX REA D853-19564MR.
- [SDR ABXA9701281](https://openairdocs.org/sdr/ABXA9701281.md): Skin · cracked · Jul 21, 1997 · N802AX · Doug DC862 · Fuselage Main, Plate/Skin
  > LOOSE RIVETS FOUND ON A DOUBLER AT FS 178 LT. WHEN REMOVED FOUND A 54 INCH CRACK AND AN 8 X 3.25 INCH CUTOUT IN THE FUSELAGE SKIN. INSTALLED DOUBLER AND FINGER DOUBLER IAW ABX REA D853-19550-MR.
- [SDR ABXA9701254](https://openairdocs.org/sdr/ABXA9701254.md): Skin · wrinkled · Jul 15, 1997 · N802AX · Doug DC862 · Rudder, Plate/Skin
  > DURING C-CHECK, FOUND TOP LEFT SIDE OF RUDDER TO HAVE DENTS AND WRINKLED SKIN. REPLACED DAMAGED SKIN IAW DC8 SRM 51-1-21 AND DAC DWG 5655077-3.
- [SDR ABXA9701225](https://openairdocs.org/sdr/ABXA9701225.md): Panel · cracked · Jul 9, 1997 · N802AX · Doug DC862 · Wing, Plate/Skin
  > RT WING PANEL 505F HAS CRACKS AT HOLES. REPAIRED IAW DC8 SRM 51-1-21 AND ABX REA D857-19555MR.
- [SDR ABXA9701224](https://openairdocs.org/sdr/ABXA9701224.md): Panel · cracked · Jul 9, 1997 · N802AX · Doug DC862 · Wing, Plate/Skin
  > LT WING PANEL 505F HAS CRACKS AT HOLES. *S/D* REPAIRED PANEL IAW DC8 SRM 51-1-21 AND ABX REA D857-19566MR.
- [SDR ABXA9700996](https://openairdocs.org/sdr/ABXA9700996.md): Hose · leaking · May 12, 1997 · N802AX · Doug DC862 · Hydraulic System, Main
  > DURING CLIMBOUT, RIGHT AFTER GEAR RETRACTION, HYDRAULIC QUANTITY DROPPED TO NEAR STANDPIPE LEVEL FOLLOWED BY A LOSS OF HYDRAULIC PRESSURE. REPLACED FLEX LINE AT LEFT MAIN GEAR BUNGEE CYLINDER AND THE LEFT AND RIGHT ENGINE DRIVEN PUMPS. SERVICED SYSTEM IAW DC
- [SDR ABXA9700041](https://openairdocs.org/sdr/ABXA9700041.md): Fire Bell · sounded · Feb 21, 1997 · N802AX · Doug DC862 · Fire Detection
  > DURING CLIMB, FIRE BELL SOUNDED FOR APPROXIMATELY ONE SECOND WITH NO ASSOCIATED FIRE LIGHT IN HANDLE OR MASTER FIRE LIGHT. FIRE WARNING TEST WAS PERFORMED FOR ALL ENGINES AND ALL TESTED NORMALLY. COULD NOT DUPLICATE. CHECKED PNEUMATIC SYSTEM, FOUND NO LEAKS
- [SDR ABXA9700482](https://openairdocs.org/sdr/ABXA9700482.md): Override Mech · failed · Nov 1, 1996 · N802AX · Doug DC862 · Aileron Control System
  > OVERRIDE MECHANISM SHAFT AND BEARING FAILED DAMAGING LOWER SKIN, GUSSETT AND HINGE WEB FITTING. REPAIRED PER DC8 MM.
- [SDR ABXA9600498](https://openairdocs.org/sdr/ABXA9600498.md): Seat · unlocked · May 29, 1996 · N802AX · Doug DC862 · Flight Compartment Equipment
  > DURING CRUISE, FLIGHT ENGINEER'S SEAT DROPPED FROM THE MID VERTICAL RANGE TO THE LOWEST POSITION. INSPECTED AND LUBED THE VERTICAL ADJUSTMENT MECHANISM OF THE FLIGHT ENGINEER'S SEAT, OPS CHECK GOOD.
- [SDR ABXA9500750](https://openairdocs.org/sdr/ABXA9500750.md): O-Rings · leaking · Sep 29, 1995 · N802AX · Doug DC862 · Hydraulic System, Main
  > GENERAL HYDRAULIC SYSTEM FLUID QUANTITY BEGAN DECREASING IN FLIGHT. ACCOMPLISHED HYDRAULIC PRESSURE OR FLUID LOSS CHECKLIST. DURING APPROACH WITH AUX PUMP ON, QUANTITY STOPPED DECREASING HALFWAY BETWEEN FULL AND STANDPIPE. NO FURTHER FLUID LOSS WAS NOTED.
- [SDR ABXA9500675](https://openairdocs.org/sdr/ABXA9500675.md): Eel Battery Pack · discharged · Aug 18, 1995 · N802AX · Doug DC862 · Emergency Lighting
  > COCKPIT EMERGENCY LIGHTS FAILED DURING A-1 CHECK. REPLACED EMERGENCY LIGHTING BATTERY PACK. SYSTEM OPS CHECKED GOOD IAW DC 8 MM.
- [SDR ABXA9500062](https://openairdocs.org/sdr/ABXA9500062.md): Link Assy · defective · Jan 30, 1995 · N802AX · Doug DC862 · Landing Gear Door Retract Section
  > LOUD 'BANG' EXPERIENCED AFTER GEAR RETRACTION. ONCE GEAR WAS SAFELY UP, NOISE AND VIBRATION WAS NOTICED. AIRCRAFT RETURNED TO SAN. INSPECTED AND FERRIED AIRCRAFT TO ONT. JACKED AIRCRAFT, FOUND RT NOSE GEAR DOOR FORWARD LINK UNLATCHING. REMOVED AND REPLACE
- [SDR ABXA9500060](https://openairdocs.org/sdr/ABXA9500060.md): Link Assy · malfunctioned · Jan 26, 1995 · N802AX · Doug DC862 · Landing Gear Door Retract Section
  > AFTER TAKEOFF AND GEAR RETRACTION, CREW HEARD A LOUD 'BANG' ACCOMPANIED BY AN EXTREME VIBRATION IN THE NOSE GEAR AREA. AIRCRAFT RETURNED TO DFW. RAN ALL FOUR TURBO COMPRESSORS, AND CHECKED DUCTING IN NOSE GEAR AREA. NO DISCREPANCIES WERE NOTED. JACKED NOSE

## 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 = 'N802AX' AND deregistration_id = 'N802AX-2004-03-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N802AX-2004-03-12/reports

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