# Service difficulty reports: N816AX, cancelled Jun 19, 2008

A list on [N816AX, cancelled Jun 19, 2008](https://openairdocs.org/deregistered/N816AX-2008-06-19.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 4 · 165 reports

- [SDR ABXA070184](https://openairdocs.org/sdr/ABXA070184.md): Battery · discharged · Jun 12, 2007 · N816AX · Doug DC863F · Emergency Lighting
  > EMERGENCY EXIT LIGHT BATTERY PACK DEAD UNABLE TO CHANGE. REMOVED AND REPLACED EMERGENCY LIGHT PACK ASSEMBLY IAW DC8 AMM 33-50-01.
- [SDR ABXA070072](https://openairdocs.org/sdr/ABXA070072.md): Wire · damaged · Mar 15, 2007 · N816AX · Doug DC863F · Light System Wiring
  > DURING SERVICE CHECK FOUND ELECTRICAL ODOR COMING FROM OVERHEAD LIGHT. FOUND ONE FLUORESCENT LIGHT RECEPTACLE CORRODED AT TERMINAL ENDS AND SHORTING. CLEANED RECEPTACLE AND REPLACED BOTH TERMINAL ENDS ON WIRES COMING TO RECEPTACLE. REPLACED LAMP AND OPS CHE
- [SDR ABXA070069](https://openairdocs.org/sdr/ABXA070069.md): Wire · chafed · Mar 13, 2007 · N816AX · Doug DC863F · Navigation System Wiring
  > ACRID ODOR OF ELECTRICAL SMOKE BY ALL 3 CREW MEMBERS, SOURCE NOT IDENTIFIED. ODOR COMES AND GOES. FOUND LOAD CALCULATOR WIRES CHAFING ON PANEL. ROUTED PANEL AREA OUT AND REPAIRED WIRES IAW DC8 MM CHAPTER 20. NO OTHER DEFECTS NOTED AT THIS TIME.
- [SDR ABXA070051](https://openairdocs.org/sdr/ABXA070051.md): Drive Link · cracked · Feb 21, 2007 · N816AX · Doug DC863F · Trailing Edge Flap Actuator
  > LEFT INBOARD FLAP DRIVE LINK AT STA XW 98.00 FOUND CRACKED WHILE COMPLYING WITH JC 8020401 AND ASB 27-269, AD 088-10-7. REMOVED AND REPLACED LINK, DETAILS IN WORK PACK 600264601.
- [SDR ABXA060233](https://openairdocs.org/sdr/ABXA060233.md): Door · missing · Aug 22, 2006 · N816AX · Doug DC863F · Engine Cowling System
  > NR 4 ENGINE RIGHT COWL DOOR BLOWOUT PANEL MISSING. REPLACED NR 4 ENGINE RIGHT COWL BLOWOUT PANEL AND DOOR FORWARD DOOR LATCH IAW DC8 MM 71-10 AND DC8 MM CHAPTER 20. OPS CHECKED GOOD.
- [SDR ABXA060161](https://openairdocs.org/sdr/ABXA060161.md): Engine · fod · Apr 12, 2006 · N816AX · Doug DC863F · Fire Detection
  > IMMEDIATELY AFTER TAKEOFF FROM ILN, NR 3 FIRE WARNING LIGHT AND BELL CAME ON. AFTER APPROXIMATELY 5 SECONDS, THEN LIGHT WENT OUT. FIRE WARNING TESTED GOOD. SECURED NR 3 ENGINE AND LANDED. POSITIVE OIL PRESSURE INDICATED. FOUND CHARRED BIRD NEST NEXT TO AF
- [SDR ABXA060126](https://openairdocs.org/sdr/ABXA060126.md): Pin · corroded · Feb 18, 2006 · N816AX · Doug DC863F · Main Landing Gear
  > FORWARD TRUNNION MAIN LANDING GEAR PIN CORRODED BEYOND LIMITS (LEFT). LEFT MAIN GEAR FORWARD TRUNNION PIN REMOVED AND REPLACED IAW DC8 MM 32-11-01-4.
- [SDR ABXA060125](https://openairdocs.org/sdr/ABXA060125.md): Pin · sheared · Feb 17, 2006 · N816AX · Doug DC863F · Landing Gear Position and Warning
  > LEFT MAIN LANDING GEAR ACTUATOR LOWER ATTACH POINT PIN SHEARED DURING RETRACTION. REMOVED AND REPLACED LEFT MAIN LANDING GEAR ACTUATOR LOWER PIN AS PER AAR FORM 0909-02, REV 3. OPS CHECKED GOOD IAW DC8 AMM 32-32-0.
- [SDR ABXA060127](https://openairdocs.org/sdr/ABXA060127.md): Pin · corroded · Feb 10, 2006 · N816AX · Doug DC863F · Main Landing Gear
  > AFT TRUNNION MAIN LANDING GEAR PIN HAD PITTING THROUGH OUT PIN. LEFT MAIN GEAR AFT TRUNNION PIN REMOVED AND REPLACED IAW DC8 MM 32-11-01-4.
- [SDR ABXA060124](https://openairdocs.org/sdr/ABXA060124.md): Splice · cracked · Jan 22, 2006 · N816AX · Doug DC863F · Fuselage Miscellaneous Structure
  > RIGHT SIDE CABIN STA. 680, LONGERON 11 RIGHT, AFT UPPER SPLICE FITTING HAD A CRACK. REMOVED AND REPLACED SPLICE FITTING AT RIGHT SIDE MAIN CABIN, STA 680, LONGERON 11 RIGHT AFT IAW DC8 SRM 51-1-20 AND 51-3-0.
- [SDR ABXA060123](https://openairdocs.org/sdr/ABXA060123.md): Fitting · cracked · Jan 22, 2006 · N816AX · Doug DC863F · Fuselage Main, Attach Fittings
  > LEFT CENTER WING FLOOR AREA AT FS 759, LEFT BUTT LINE 48, SUPPORT FITTING HAD CORROSION AT BASE ATTACH NUTS. CLEANED AREA IAW DC8 MM 12-06-00, FITTING FOUND CRACKED. REMOVED AND REPLACED WITH NEW FITTING IAW DC8 SRM 51-1-20D.
- [SDR ABXA060121](https://openairdocs.org/sdr/ABXA060121.md): Fitting · corroded · Jan 21, 2006 · N816AX · Doug DC863F · Fuselage Main, Attach Fittings
  > AFT CARGO COMPARTMENT AREA BELOW C-3 DOOR HAD CORROSION ON FITTING APPROXIMATELY FS 1195, RIGHT BUTT LINE 19. REMOVED AND REPLACED FITTING AT C-3 DOOR AREA FS 1195, RIGHT BUTT LINE 19 IAW DC8 SRM 51-1-20D AND 53-2-0.
- [SDR ABXA060122](https://openairdocs.org/sdr/ABXA060122.md): Fitting · corroded · Jan 21, 2006 · N816AX · Doug DC863F · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT AREA BELOW C-3 DOOR HAD FITTINGS (2 EACH) CORRODED IN BOX SECTION FS 1176, RIGHT BUTT LINE 20. REMOVED AND REPLACED FITTINGS AT AFT CARGO COMPARTMENT BELOW C-3 DOOR IAW DC8 SRM 51-1-20 AND 53-2-00.
- [SDR ABXA060120](https://openairdocs.org/sdr/ABXA060120.md): Fitting · cracked · Jan 20, 2006 · N816AX · Doug DC863F · Fuselage Main, Attach Fittings
  > AFT LOWER CARGO COMPARTMENT FITTINGS (3 EACH) CRACKED, BETWEEN FS 1200 - 1220, RIGHT BUTT LINE 20, LOWER DOOR CUT OUT BOX SECTION. REMOVED AND REPLACED FITTINGS AT AFT CARGO COMPARTMENT BELOW C-3 DOOR IAW DC8 SRM 51-1-20D.
- [SDR ABXA050379](https://openairdocs.org/sdr/ABXA050379.md): Transmitter · defective · Dec 21, 2005 · N816AX · Doug DC863F · Engine Oil Indicating System
  > NR 3 ENGINE OIL PRESSURE WAS 37 TO 39 PSI IN CRUISE. RETARDED THROTTLE TO IDLE TO COMPLY WITH ABNORMAL PROCEDURES, OIL PRESSURE WAS 35 PSI. OIL PRESSURE DROPPED TO 34 PSI, SECURED NR 3 ENGINE AT 0850 HRS - 10 PSI WINDMILLING OIL PRESSURE. 0855 HRS OIL PRESSURE
- [SDR ABXA050126](https://openairdocs.org/sdr/ABXA050126.md): Fitting · cracked · May 18, 2005 · N816AX · Doug DC863F · Wing, Center Box
  > DURING LINE MAINTENANCE, FOUND THE CENTER WING TANK FRONT SPAR LT SUPPORT FITTING CRACKED AT STA XCW 67. REPLACED FITTING IAW DC-8 SRM 51-3-0.
- [SDR ABXA040221](https://openairdocs.org/sdr/ABXA040221.md): Hinge · cracked · Jun 8, 2004 · N816AX · Doug DC863F · Cargo/Baggage Doors
  > MAIN CARGO DOOR AFT HINGE HAD AFT ATTACHMENT FASTENER HOLE SHOWING CRACK INDICATION. REPAIRED AREA IAW REA D852-49168MR.
- [SDR ABXA040220](https://openairdocs.org/sdr/ABXA040220.md): Mount · worn · Jun 8, 2004 · N816AX · Doug DC863F · Fuselage Main, Attach Fittings
  > MAIN CARGO DOOR LOWER LATCH MOUNT HOLES WORN. REPAIRED AREA IAW REA D852-49174MR.
- [SDR ABXA040224](https://openairdocs.org/sdr/ABXA040224.md): Skin · damaged · Jun 4, 2004 · N816AX · Doug DC863F · Fuselage Main, Plate/Skin
  > STA 1440, LONGERON 29 RIGHT REQUIRED PERMANENT REPAIR. PERMANENT REPAIR ACCOMPLISHED IAW REA D853-49148MR.
- [SDR ABXA040223](https://openairdocs.org/sdr/ABXA040223.md): Floorbeam · corroded · Jun 4, 2004 · N816AX · Doug DC863F · Fuselage Main, Floor Beam
  > FLOORBEAM WEB AT BS 180 WAS CORRODED AT 3 ATTACH FASTENERS FOR SPLICE PLATE LEFT BUTTLINE 57. REPAIRED AREA IAW REA D853-49182MR.
- [SDR ABXA040222](https://openairdocs.org/sdr/ABXA040222.md): Floorbeam · cracked · Jun 4, 2004 · N816AX · Doug DC863F · Fuselage Main, Floor Beam
  > FLOORBEAM WEB AT BS 240 HAD 4 CRACK INDICATIONS AT SPLICE PLATE ATTACH FASTENERS LEFT BUTTLINE 57. REPAIRED AREA IAW REA D853-49184MR.
- [SDR ABXA040219](https://openairdocs.org/sdr/ABXA040219.md): Finger Doubler · corroded · Jun 4, 2004 · N816AX · Doug DC863F · Fuselage Main, Plate/Skin
  > AFT CARGO STA 1480, LONGERON 31 LEFT, FINGER DOUBLER, CORRODED. REPAIRED FUSELAGE SKIN IAW DC-8 SRM 53-2-1 AND REPAIRED FRAME SECTION IAW DWG K04888 AND REA D853-49146, SRM 53-2-0, 51-1-21, 51-1-20D, AND 51-3-1.
- [SDR ABXA040036](https://openairdocs.org/sdr/ABXA040036.md): Wire · burned · Dec 29, 2003 · N816AX · Doug DC863F · Electrical Power System Wiring
  > NR 3 GENERATOR UNPARALLED LIGHT ILLUMINATED IN FLIGHT, NO VOLTS, NO FREQS. RESET, NO VOLTS, NO FREQS, DISCONNECTED. REPLACED NR 3 ENGINE GENERATOR IAW 24-20-01-4-0002. DURING OPS CHECK, NOTED SPARKS COMING FROM THE TOP OF ENGINE. FOUND T1, T2, AND T3 WIRES
- [SDR ABXA030473](https://openairdocs.org/sdr/ABXA030473.md): Cylinder · leaking · Dec 12, 2003 · N816AX · Doug DC863F · Landing Gear Steering System
  > HYDRAULIC QUANTITY GRADUALLY DECREASED DOWN TO 7 GALLONS. LOSS OF HYDRAULICS EMERGENCY PROCEDURE FOLLOWED. MAINTENANCE FOUND RT BOGIE TRIM CYLINDER LEAKING. REPLACED RT BOGIE TRIM CYLINDER IAW MM 32-33-01-2.
- [SDR ABXA030323](https://openairdocs.org/sdr/ABXA030323.md): Engine · overheated · Aug 4, 2003 · N816AX · Doug DC863F · Engine (Turbine/Turboprop)
  > DURING TAKEOFF, NR 3 ENGINE EGT WENT TO 600 DEGREES. RETARDED THROTTLE AND EGT DECREASED INTO NORMAL RANGE. OTHER INSTRUMENTS DECREASED AS WELL. SECURED ENGINE PER ABNORMAL PROCEDURES. EGT AT 600 DEGREES FOR APPROXIMATELY 15 SECONDS. NR 3 ENGINE WAS SHUTD
- [SDR ABXA020246](https://openairdocs.org/sdr/ABXA020246.md): Ground Wire · loose · Oct 11, 2002 · N816AX · Doug DC863F · Light System Wiring
  > WHEN HOT CUP WAS TURNED ON, EMERGENCY EXIT LIGHTS IN COCKPIT INTERMITTENTLY FLICKERED ON AND OFF RANDOMLY. FOUND LOOSE WIRING AT GROUND STUD FOR EMERGENCY POWER SUPPLY. TIGHTENED LOOSE CONNECTION AT GROUND STUD. NO DEFECTS NOTED WITH HOT CUP. SYSTEM OPS CH
- [SDR ABXA020212](https://openairdocs.org/sdr/ABXA020212.md): Torque Link · disconnected · Sep 19, 2002 · N816AX · Doug DC863F · Nose/Tail Landing Gear Strut/Axle
  > GROUND SHIFT FAILED AFTER TAKEOFF, UNABLE TO RAISE GEAR HANDLE, AUTO PRESSURIZATION INOPERATIVE. TAKEOFF WARNING HORN SOUNDED. RAN ABNORMAL. PULLED GROUND CONTROL CIRCUIT BREAKERS. SYSTEMS RESTORED. AFTER LANDING, AND NOSE WHEEL TOUCH DOWN, A LOUD POP WAS
- [SDR ABXA030221](https://openairdocs.org/sdr/ABXA030221.md): Frame · corroded · Aug 12, 2002 · N816AX · Doug DC863F · Fuselage Main, Frame
  > FORWARD LOWER CARGO STA 280, LONGERON 36, UPPER FRAME FLANGE WAS CRACKED AND CORRODED. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED FILLER, DOUBLER, ALODINED, PRIMED, AND INSTALLED FASTENERS IAW REA D853-43982MR, DC-8 SRM 51-1-8, 51-1-20D, AND 51-1-20E.
- [SDR ABXA030217](https://openairdocs.org/sdr/ABXA030217.md): Skin · cracked · Aug 10, 2002 · N816AX · Doug DC863F · Fuselage Main, Plate/Skin
  > AFT PASSENGER DOOR UPPER AFT CORNER OUTER SKIN HAD 2 CRACKS. REMOVED DAMAGED, NO CRACKS NOTED AFT OF CUTOUTS. FABRICATED DOUBLER AND FILLERS, INSTALLED IAW DC-8 SRM 53-2-0, NDT SPM 06-10-001, DC-8 SRM 51-1-8, 51-1-20D AND SRM 51-1-21.
- [SDR ABXA030227](https://openairdocs.org/sdr/ABXA030227.md): Skin · cracked · Aug 7, 2002 · N816AX · Doug DC863F · Service Doors
  > FORWARD SERVICE DOOR LOWER AFT CORNER SKIN HAD A CRACK. CUT OUT DAMAGE IAW DC-8 SRM 53-2-0. FABRICATED DOUBLERS AND FILLERS IAW DC-8 SRM 53-2-0. INSTALLED DOUBLERS AND FILLERS IAW DC-8 SRM 53-2-0. REINSTALLED INNER TORQUE BOX WEB IAW DC-8 SRM 51-1-20E AND 51-3
- [SDR ABXA030220](https://openairdocs.org/sdr/ABXA030220.md): Door Frame · cracked · Aug 7, 2002 · N816AX · Doug DC863F · Fuselage Main, Structure
  > L1 DOOR JAMB LOWER AFT CORNER HAD STAINLESS STEEL REPAIR. REMOVED DOOR CLOSE OUT PANEL TO FOM. FABRICATED 3 DOUBLER, 5 DOUBLER AND FILLERS, INSTALLED ALL IAW DC-8 SRM 53-2-0, 51-1-21 AND 51-3-0.
- [SDR ABXA030222](https://openairdocs.org/sdr/ABXA030222.md): Structure · corroded · Aug 6, 2002 · N816AX · Doug DC863F · Leading Edge Devices
  > LT WING LEADING EDGE UPPER SECTION APPROXIMATELY, STA. XFS 126.250, CORROSION AROUND FASTENERS. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPAIRED IAW REA D857-43958MR.
- [SDR ABXA030219](https://openairdocs.org/sdr/ABXA030219.md): Doubler · cracked · Jul 22, 2002 · N816AX · Doug DC863F · Cargo/Baggage Doors
  > FORWARD LOWER CARGO C1 DOOR, FUSELAGE INNER DOUBLER WAS CRACKED AT FUSELAGE STA. 320, OUTER EDGE AND HAD AN IMPROPER REPAIR. CUT OUT DAMAGED SECTION OF DOUBLER, FABRICATED FILLER, REPAIR DOUBLER SPLICES, AND INSTALLED ALL REPAIRS PARTS IAW DC-8 SRM 51-1-20D, D
- [SDR ABXA030223](https://openairdocs.org/sdr/ABXA030223.md): Seat Track · corroded · Jul 22, 2002 · N816AX · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BUTT LINE 25 LEFT WAS CORRODED, FS 70 - 260. REMOVED WEB AND FLOORBOARDS FS 70 - 260, LEFT BUTT LINE 0 - 45 TO FOM. REMOVED SEAT TRACK SECTION. FABRICATED SECTION IAW ZANTOP DWG 86302. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED SEAT
- [SDR ABXA030231](https://openairdocs.org/sdr/ABXA030231.md): Pan · cracked · Jul 22, 2002 · N816AX · Doug DC863F · Fuselage Miscellaneous Structure
  > FORWARD PASSENGER DOOR LOWER AFT CORNER AT THE CUSP CHORD SHOWED CRACK INDICATION. STOP DRILLED CRACKED DOOR PAN, FABRICATED REPAIR AND SPLICE PARTS AND PLATES FOR DOOR PAN AND TORQUE BOX WEB IAW DAC 5597646, DC-8 SRM 53-2-0, 51-9-0, 51-1-21, 53-3-1, AND 51-1
- [SDR ABXA030229](https://openairdocs.org/sdr/ABXA030229.md): Longeron · corroded · Jul 20, 2002 · N816AX · Doug DC863F · Fuselage Main, Longeron/Stringer
  > REMOVE AND REPLACE LONGERON 32 LEFT INBOARD CHANNEL STA. 190 - 385. REMOVED CORRODED SECTION, FABRICATED LONGERON AND SPLICES. INSTALLED IAW DC-8 SRM 51-1-20D, 53-2-2, AND 51-1-8.
- [SDR ABXA030228](https://openairdocs.org/sdr/ABXA030228.md): Longeron · corroded · Jul 20, 2002 · N816AX · Doug DC863F · Fuselage Main, Longeron/Stringer
  > LONGERON 32 LEFT OB CHANNEL AT STA. 370 WAS CORRODED. REMOVED CORRODED SECTION OF LONGERON, FABRICATED LONGERON AND SPLICES. INSTALLED IAW SRM 51-1-20D, 51-1-24, AND 53-2-2.
- [SDR ABXA030230](https://openairdocs.org/sdr/ABXA030230.md): Longeron · corroded · Jul 20, 2002 · N816AX · Doug DC863F · Fuselage Main, Longeron/Stringer
  > LONGERON 35 RIGHT INBOARD CHANNEL WAS CORRODED AT STA 340. CUT AND REMOVED DAMAGED SECTION, FABRICATED NEW SECTION AND REPAIR SPLICES. INSTALLED IAW DC-8 SRM 53-2-2 AND 51-1-20D.
- [SDR ABXA030226](https://openairdocs.org/sdr/ABXA030226.md): Skin · corroded · Jul 19, 2002 · N816AX · Doug DC863F · Fuselage Main, Plate/Skin
  > REMOVE AND REPLACE FORWARD LOWER CARGO SKIN FROM F.S. 190 - 450 LONGERON 31 LEFT - 31 RIGHT. (COI NR 41207-001). REPLACED FORWARD LOWER CARGO SKIN IAW DC-8 SRM.
- [SDR ABXA030225](https://openairdocs.org/sdr/ABXA030225.md): Door Frame · corroded · Jul 17, 2002 · N816AX · Doug DC863F · Fuselage Main, Structure
  > AFT CARGO, BS 1220, FUSELAGE FRAME CORRODED JUST INBOARD OF SLIDING DOOR, LOWER AFT CUTOUT. REPLACED DOOR FRAME ZEE FITTING, FABRICATED REPAIR SPLICE ANGLES AND FILLERS. INSTALLED IAW DC-8 SRM 53-2-0, 51-1-8, AND 51-3-0.
- [SDR ABXA030218](https://openairdocs.org/sdr/ABXA030218.md): Structure · cracked · Jul 16, 2002 · N816AX · Doug DC863F · Fuselage Main, Attach Fittings
  > FORWARD SERVICE DOOR UPPER FORWARD CORNER HAD A CRACK IN OUTER SKIN. CUT OUT CRACKED AREA, FABRICATED DOUBLER, TRIPLER, FILLER, AND INSTALLED EACH IAW SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D, 51-3-0 AND 51-1-14.
- [SDR ABXA030216](https://openairdocs.org/sdr/ABXA030216.md): Frame · corroded · Jul 16, 2002 · N816AX · Doug DC863F · Fuselage Main, Frame
  > AFT CARGO BS 1010, BETWEEN LONGERON 35 LEFT AND 35 RT, FUSELAGE FRAME CORRODED ON UPPER CAP, UPPER AND LOWER SURFACES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED (1 EA) FRAME CAP, (6 EA) GUSSETS, CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE, FILLER
- [SDR ABXA030224](https://openairdocs.org/sdr/ABXA030224.md): Shear Tie · corroded · Jul 15, 2002 · N816AX · Doug DC863F · Fuselage Main, Structure
  > AFT LOWER CARGO, SHEARTIE CORRODED AT STA. 1200, LONGERON 28 - 29 LEFT. REMOVED CORROSION, OUT OF LIMITS. REMOVED FITTING AND FABRICATED SPLICE, INSTALLED NEW FITTING IAW DC-8 SRM 51-1-8, 53-2-0, AND 51-1-20D.
- [SDR ABXA020058](https://openairdocs.org/sdr/ABXA020058.md): Warning System · malfunctioned · Jul 13, 2002 · N816AX · Doug DC863F · Landing Gear Position and Warning
  > GEAR UNSAFE LIGHT REMAINED ILLUMINATED ON RETRACTION. LEFT GEAR DOWN INDICATED NOT LATCHED. RECYCLED ONCE, NO HELP. RUNNING ABNORMAL TO UPLATCH CHECK POSITION LIGHT EXTINGUISHED.
- [SDR ABXA020032](https://openairdocs.org/sdr/ABXA020032.md): Fitting · cracked · Jun 25, 2002 · N816AX · Doug DC863F · Fuselage Miscellaneous Structure
  > RIGHT WHEEL WELL AREA, STATION 920, FITTING WAS CRACKED AT CENTER KEEL. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-21 AND 51-1-20.
- [SDR ABXA020031](https://openairdocs.org/sdr/ABXA020031.md): Skin · corroded · Jun 25, 2002 · N816AX · Doug DC863F · Fuselage Main, Plate/Skin
  > SKIN CORROSION OUT OF LIMITS JUST AFT OF GYRO COMPARTMENT. INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-0.
- [SDR ABXA020030](https://openairdocs.org/sdr/ABXA020030.md): Skin · corroded · Jun 25, 2002 · N816AX · Doug DC863F · Fuselage Main, Plate/Skin
  > CORROSION OUT OF LIMITS ON FUSELAGE SKIN, STATION 280, LONGERON 35 LEFT AND STATION 335, LONGERON 35 RIGHT. INSTALLED REPAIR DOUBLER IAW REA D853-44492.
- [SDR ABXA010889](https://openairdocs.org/sdr/ABXA010889.md): Battery Pack · discharged · May 29, 2002 · N816AX · Doug DC863F · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, FOUND EMERGENCY EXIT LIGHTS DIM. REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK IAW DC-8 MM 33-50-01.
- [SDR ABXA010888](https://openairdocs.org/sdr/ABXA010888.md): Battery Pack · discharged · May 28, 2002 · N816AX · Doug DC863F · Emergency Lighting
  > EMERGENCY LIGHTS WERE COMING ON INTERMITTENTLY. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC-8 MM.
- [SDR ABXA010900](https://openairdocs.org/sdr/ABXA010900.md): Nut · missing · May 23, 2002 · N816AX · Doug DC863F · Fasteners
  > UPON FLAP EXTENSION FOR LANDING, SPLIT FLAPS WERE INDICATED. CONFIRMED BY ROLL TENDENCY. LEFT FLAP WAS APPROXIMATELY 6 DEGREES BEHIND RIGHT FLAP. RIGHT FLAP AT 35 DEGREES, LEFT FLAP AT 29 DEGREES. FOUND LEFT INBOARD FLAP ACTUATOR IDLER ARM TRACK MISSING NU

Next page: https://openairdocs.org/deregistered/N816AX-2008-06-19/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 = 'N816AX' AND deregistration_id = 'N816AX-2008-06-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N816AX-2008-06-19/reports

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