# Service difficulty reports: N815AX, cancelled Mar 20, 2007

A list on [N815AX, cancelled Mar 20, 2007](https://openairdocs.org/deregistered/N815AX-2007-03-20.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 · 80 reports

- [SDR ABXA040382](https://openairdocs.org/sdr/ABXA040382.md): Floorbeam · corroded · Nov 10, 2004 · N815AX · Doug DC863F · Fuselage Main, Floor Beam
  > FLOORBEAM AT STA 52, RIGHT BUTTLINE 51 HAD CORROSION ON BOTTOM CAP. REPAIRED AREA IAW REA D853-50309MR.
- [SDR ABXA040381](https://openairdocs.org/sdr/ABXA040381.md): Skin · corroded · Sep 23, 2004 · N815AX · Doug DC863 · Fuselage Main, Plate/Skin
  > CORROSION FUSELAGE SKIN STA 1040, LONGERON 36. DEFERRED TIL 9-6-04 IAW REA D853-50415, IAW ABX GMM CHAPTER 1 07-04. FABRICATED DOUBLER AND FILLER IAW REA D853-50292MR. ALODINED AND PRIMED DOUBLER FILLER AND SKIN IAW DC-8 SRM 51-1-8. INSTALLED DOUBLER AND F
- [SDR ABXA030365](https://openairdocs.org/sdr/ABXA030365.md): Fitting · cracked · Sep 8, 2003 · N815AX · Doug DC9* · Fuselage Miscellaneous Structure
  > FITTING IN RIGHT WHEEL WELL DAMAGED (CRACKED). FABRICATED NEW PART REF: ST-9300-01 AND PARTS FABRICATION RECORD WO 600179300 AND IAW SRM.
- [SDR ABXA030366](https://openairdocs.org/sdr/ABXA030366.md): Fitting · cracked · Sep 8, 2003 · N815AX · Doug DC9* · Fuselage Miscellaneous Structure
  > FITTING IN RT WHEEL WELL DAMAGED (CRACKED). FABRICATED NEW PART REF: ST-9300-01 AND PARTS FABRICATION RECORD WO 600179300 AND IAW SRM.
- [SDR ABXA030282](https://openairdocs.org/sdr/ABXA030282.md): Cable · broken · Jul 12, 2003 · N815AX · Doug DC863 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. GOT (MAIN GEAR SPOILERS INOP) LIGHT. PERFORMED ABNORMALS, GEAR RETRACTED. ALL OTHER INDICATIONS NORMAL. PRESSURIZATION OK. - REPLACED ANTI-RETRACTION CABLE IAW DC8 MM 32-31-00-2-0003. TESTED AND OPS CHECKED GOOD D
- [SDR ABXA030264](https://openairdocs.org/sdr/ABXA030264.md): Frame · damaged · Mar 22, 2003 · N815AX · Doug DC863F · Cargo/Baggage Doors
  > REMOVE AND REPLACE STUB FRAME IN MAIN CARGO DOOR AT STA 183.5. REMOVED STUB FRAME, LOCATED AND DRILLED, AND INSTALLED STUB FRAME IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-24.
- [SDR ABXA030255](https://openairdocs.org/sdr/ABXA030255.md): Door Frame · cracked · Mar 16, 2003 · N815AX · Doug DC863F · Doors
  > UPPER LATCH HOOK MOUNT HOLE AT STA 196.5 HAD CRACK INDICATION. REMOVED DAMAGED FRAME, LOCATED, DRILLED, AND DEBURRED NEW FRAME, INSTALLED IAW ABX REA D852-46041MR AND DC-8 SRM 51-1-21 AND 51-1-8.
- [SDR ABXA030254](https://openairdocs.org/sdr/ABXA030254.md): Structure · cracked · Mar 16, 2003 · N815AX · Doug DC863F · Doors
  > CENTER LATCH HOOK MOUNT HOLE AT STA 203.5 HAD CRACK INDICATION. REPAIRED AREA IAW ABX REA D852-46041MR.
- [SDR ABXA030270](https://openairdocs.org/sdr/ABXA030270.md): Door Frame · damaged · Mar 15, 2003 · N815AX · Doug DC863F · Cargo/Baggage Doors
  > CUT AND SPLICE MAIN CARGO DOOR FRAME AT STA 233.5. CUT AND REMOVED DOOR FRAME, AND SPLICED IN NEW SECTION IAW ABX REA D852-46041MR AND DC-8 SRM 51-1-20D.
- [SDR ABXA030260](https://openairdocs.org/sdr/ABXA030260.md): Door Frame · cracked · Mar 12, 2003 · N815AX · Doug DC863F · Doors
  > UPPER LATCH HOOK MOUNT HOLE AT STA 153.0 HAD CRACK INDICATION. REPAIRED AREA IAW ABX REA D852-46041MR.
- [SDR ABXA030257](https://openairdocs.org/sdr/ABXA030257.md): Door Frame · cracked · Mar 12, 2003 · N815AX · Doug DC863F · Doors
  > UPPER LATCH HOOK MOUNT HOLE AT STA 176.5 HAD CRACK INDICATION. REPLACED STUB FRAME IAW ABX REA D852-46043MR.
- [SDR ABXA030259](https://openairdocs.org/sdr/ABXA030259.md): Door Frame · cracked · Mar 12, 2003 · N815AX · Doug DC863F · Doors
  > UPPER LATCH HOOK MOUNT HOLE AT STA 163.5 HAD CRACK INDICATION. REPAIRED AREA IAW ABX REA D852-46041MR.
- [SDR ABXA030258](https://openairdocs.org/sdr/ABXA030258.md): Door Frame · cracked · Mar 12, 2003 · N815AX · Doug DC863F · Doors
  > CENTER LATCH HOOK MOUNT HOLE AT STA 167.0 HAD CRACK INDICATION. REPAIRED AREA IAW ABX REA D852-46043MR.
- [SDR ABXA030250](https://openairdocs.org/sdr/ABXA030250.md): Skin · cracked · Mar 5, 2003 · N815AX · Doug DC863F · Wing, Plate/Skin
  > HOLE NR 2 ON RIGHT WING AT XFS 515, SHOWED CRACK INDICATION IN SKIN DURING INSPECTION. REPAIRED AREA IAW ABX REA D857-46040MR.
- [SDR ABXA030276](https://openairdocs.org/sdr/ABXA030276.md): Spar · damaged · Feb 24, 2003 · N815AX · Doug DC863F · Wing Spar
  > RIGHT FORWARD LOWER SPAR HAD EXISTING CUTOUT THAT EXCEEDED THE LIMITS OF THE SERVICE REWORK DRAWING SR-8570012. FABRICATED FILLER IAW ABX REA D857-46655MR. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED IAW DC-8 SRM 51-1-21.
- [SDR ABXA030263](https://openairdocs.org/sdr/ABXA030263.md): Door Frame · damaged · Feb 23, 2003 · N815AX · Doug DC863F · Cargo/Baggage Doors
  > CUT AND SPLICE MAIN CARGO DOOR FRAME AT STA 147. CUT AND REMOVED DOOR FRAME SECTION, FABRICATED AND INSTALLED FRAME SECTION AND SPLICES IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-20D.
- [SDR ABXA030262](https://openairdocs.org/sdr/ABXA030262.md): Door Frame · damaged · Feb 23, 2003 · N815AX · Doug DC863F · Cargo/Baggage Doors
  > REMOVE AND REPLACE STUB FRAME AT MAIN CARGO DOOR STA 143.5. REMOVED STUB FRAME IAW DC-9 SRM 51-1-21. RECEIVED SERVICEABLE FRAME, LOCATED AND DRILLED FASTENER HOLES IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-24. INSTALLED SERVICEABLE FRAME IAW ABX REA D852-4
- [SDR ABXA030266](https://openairdocs.org/sdr/ABXA030266.md): Door Frame · damaged · Feb 22, 2003 · N815AX · Doug DC863F · Cargo/Baggage Doors
  > CUT AND SPLICE MAIN CARGO DOOR AT FRAME STA 213.5. CUT AND NEW SECTION SPLICED IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-8, 51-1-20D, AND 51-3-0.
- [SDR ABXA030272](https://openairdocs.org/sdr/ABXA030272.md): Door Frame · damaged · Feb 22, 2003 · N815AX · Doug DC863F · Cargo/Baggage Doors
  > CUT AND SPLICE MAIN CARGO DOOR FRAME AT STA 247. REMOVED DAMAGED FRAME SECTION, FABRICATED NEW SECTION AND SPLICES, AND INSTALLED IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-8.
- [SDR ABXA030275](https://openairdocs.org/sdr/ABXA030275.md): Door Frame · damaged · Feb 22, 2003 · N815AX · Doug DC863F · Cargo/Baggage Doors
  > REMOVE AND REPLACE MAIN CARGO DOOR STUB FRAME STA 237. REMOVED AND REPLACED MAIN CARGO DOOR STUB FRAME IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-8, 51-1-24, AND 51-3-0.
- [SDR ABXA030274](https://openairdocs.org/sdr/ABXA030274.md): Door Frame · damaged · Feb 22, 2003 · N815AX · Doug DC863F · Cargo/Baggage Doors
  > REMOVE AND REPLACE MAIN CARGO DOOR STUB FRAME STA 173.8. REMOVED AND REPLACED MAIN CARGO DOOR STUB FRAME IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-21.
- [SDR ABXA030273](https://openairdocs.org/sdr/ABXA030273.md): Door Frame · damaged · Feb 22, 2003 · N815AX · Doug DC863F · Cargo/Baggage Doors
  > REMOVE AND REPLACE MAIN CARGO DOOR STUB FRAME AT STA 157. REMOVED AND REPLACED MAIN CARGO DOOR STUB FRAME IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-24 AND 51-1-21.
- [SDR ABXA030269](https://openairdocs.org/sdr/ABXA030269.md): Door Frame · damaged · Feb 22, 2003 · N815AX · Doug DC863F · Cargo/Baggage Doors
  > CUT AND SPLICE MAIN CARGO DOOR FRAME AT STA 227. CUT AND REMOVED DOOR FRAME, INSTALLED SPLICED SECTION IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-20.
- [SDR ABXA030268](https://openairdocs.org/sdr/ABXA030268.md): Door Frame · damaged · Feb 22, 2003 · N815AX · Doug DC863F · Cargo/Baggage Doors
  > REMOVE AND REPLACE STUB FRAME IN MAIN CARGO DOOR STA 223.5. REMOVED STUB FRAME, FABRICATED AND INSTALLED FRAME IAW ABX REA D852-46043MR AND DC-8 SRM 51-3-0 AND 51-1-20D.
- [SDR ABXA030267](https://openairdocs.org/sdr/ABXA030267.md): Door Frame · damaged · Feb 22, 2003 · N815AX · Doug DC863F · Cargo/Baggage Doors
  > REMOVE AND REPLACE STUB FRAME IN MAIN CARGO DOOR STA 217. REMOVED, FABRICATED AND INSTALLED NEW FRAME IAW ABX REA D852-46043MR AND DC-8 SRM 51-3-0.
- [SDR ABXA030265](https://openairdocs.org/sdr/ABXA030265.md): Door Frame · damaged · Feb 22, 2003 · N815AX · Doug DC863F · Cargo/Baggage Doors
  > CUT AND SPLICE MAIN CARGO DOOR FRAME AT STA 187. CUT AND NEW SECTION SPLICED IN IAW ABX REA D852-46043MR.
- [SDR ABXA030271](https://openairdocs.org/sdr/ABXA030271.md): Door Frame · damaged · Feb 22, 2003 · N815AX · Doug DC863F · Cargo/Baggage Doors
  > REMOVE AND REPLACE MAIN CARGO DOOR STUB FRAME AT STA 243.5. REMOVED AND REPLACED MAIN CARGO DOOR STUB FRAME IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-21, 51-3-0, AND 51-1-20D.
- [SDR ABXA030261](https://openairdocs.org/sdr/ABXA030261.md): Mount · damaged · Feb 14, 2003 · N815AX · Doug DC863F · Cargo/Baggage Doors
  > MAIN CARGO DOOR FRAMES LATCH MOUNT HOLES OVERSIZED. REPAIRED AREA IAW ABX REA D852-46043MR.
- [SDR ABXA030251](https://openairdocs.org/sdr/ABXA030251.md): Mount · cracked · Feb 11, 2003 · N815AX · Doug DC863F · Doors
  > LOWER LATCH HOOK MOUNT HOLE AT STA 256.5 HAD CRACK INDICATION. REPAIRED AREA IAW ABX REA D852-46041MR.
- [SDR ABXA030256](https://openairdocs.org/sdr/ABXA030256.md): Mount · cracked · Feb 11, 2003 · N815AX · Doug DC863F · Doors
  > UPPER LATCH HOOK MOUNT HOLE AT STA 193 HAD CRACK INDICATION. REPAIRED AREA IAW ABX REA D852-46041MR.
- [SDR ABXA030253](https://openairdocs.org/sdr/ABXA030253.md): Door Frame · cracked · Feb 11, 2003 · N815AX · Doug DC863F · Doors
  > CENTER LATCH HOOK MOUNT HOLE STA 207.0 HAD CRACK INDICATION. REMOVED DOOR FRAME, FABRICATED NEW FRAME SECTION AND SPLICES, AND INSTALLED IAW ABX REA D852-46041MR, DC-8 SRM 51-1-8 AND 51-1-20D.
- [SDR ABXA030252](https://openairdocs.org/sdr/ABXA030252.md): Door Frame · cracked · Feb 11, 2003 · N815AX · Doug DC863F · Doors
  > UPPER LATCH HOOK MOUNT HOLE AT STA 253.0 HAD CRACK INDICATION. CUT AND REMOVED DOOR FRAME, FABRICATED SPLICES FOR FRAME REPAIR, LOCATED & DRILLED NEW FRAME SECTION AND SPLICES, INSTALLED IAW ABX REA D852-46041MR, DC-8 SRM 51-3-2, 51-1-20D, AND 51-1-21.
- [SDR ABXA030040](https://openairdocs.org/sdr/ABXA030040.md): Uplock · malfunctioned · Jan 17, 2003 · N815AX · Doug DC863F · Landing Gear Retraction/Extension System
  > CREW REPORTED DURING GEAR UPLATCH CHECK, NOSE GEAR SHOWED NOT UP AND LOCKED. GEAR HANDLE WOULD NOT SEAT INTO UPLATCH POSITION. RECYCLED GEAR DOWN AND UP AS PER ABNORMAL PROCEDURES. RED UNSAFE LIGHT REMAINED ON. AFTER SECOND RECYCLE ATTEMPT, UNSAFE LIGHT AN
- [SDR ABXA020327](https://openairdocs.org/sdr/ABXA020327.md): Battery Pack · discharged · Dec 2, 2002 · N815AX · Doug DC863F · Emergency Lighting
  > EMERGENCY LIGHTS BATTERY PACK WOULD NOT CHARGE. REPLACED EMERGENCY LIGHT BATTERY AND RELAY PACK IAW DC-8 MM 33-50-01. OPS CHECKED GOOD.
- [SDR ABXA020326](https://openairdocs.org/sdr/ABXA020326.md): Skin · corroded · Nov 30, 2002 · N815AX · Doug DC863F · Fuselage Structure (General)
  > LOWER BELLY SKIN AFT OF ANTENNA F.S. 216 BETWEEN LONGERON 33 RIGHT AND 34 RIGHT WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51-1-8.
- [SDR ABXA020057](https://openairdocs.org/sdr/ABXA020057.md): Fire Detector · false indication · Jul 10, 2002 · N815AX · Doug DC863F · Smoke Detection
  > ON ONE MILE FINAL, THE LOWER CARGO FIRE LIGHT ILLUMINATED. MX DISPLAY SHOWED "FWD A FIRE". EMERGENCY DECLARED INTO KILN BY CREW. LANDED AND CLEARED RUNWAY, TOWER AND CRASH CREW OBSERVED NO EVIDENCE OF FIRE. APPROXIMATELY 5 MINUTES AFTER, CARGO FIRE INDICATED L
- [SDR ABXA010781](https://openairdocs.org/sdr/ABXA010781.md): Bushing · defective · Mar 18, 2002 · N815AX · Doug DC863F · Landing Gear Retraction/Extension System
  > UNABLE TO RETRACT GEAR ON FIRST ATTEMPT. GROUND COOLING AND BLOWAWAY JET RETRACTED NORMALLY. REMOVED THE RIGHT MAIN LANDING GEAR, REPLACED GEAR BUSHING IAW DC-8 MM. REINSTALLED RIGHT MAIN LANDING GEAR. SWING AND OPS CHECKED GOOD. REPLACED BLOW AWAY JET SW
- [SDR ABXA010649](https://openairdocs.org/sdr/ABXA010649.md): Door · missing · Dec 20, 2001 · N815AX · Doug DC863F · Landing Gear Doors
  > DURING MAINTENANCE POST FLIGHT WALKAROUND, THE RIGHT MAIN LANDING GEAR CENTER DOOR WAS MISSING. INSTALLED THE MAIN GEAR CENTER DOOR IAW DC-8 MM 32-12-01.
- [SDR ABXA010535](https://openairdocs.org/sdr/ABXA010535.md): Probe · damaged · Oct 14, 2001 · N815AX · Doug DC863F · Engine EGT/TIT Indicating System
  > NR 1 ENGINE EGT AT V1 WENT TO 575 DEGREES AND INCREASED, REDUCE POWER BY 1 KNOB. DURING INITIAL TAKEOFF ROLL ALL PARAMETERS WERE NORMAL. NR 4 ENGINE, SAME AS NR 1 ENGINE. FOUND THE NR 1 ENGINE EGT PROBES NR 2 AND NR 6 DAMAGED, FOUND THE NR 4 ENGINE EGT WIRE
- [SDR ABXA010504](https://openairdocs.org/sdr/ABXA010504.md): Rib · cracked · Sep 25, 2001 · N815AX · Doug DC863 · Fuselage Main, Structure
  > FUSELAGE RIB AT FS 880 LEFT WAS CRACKED. MAINTENANCE REPLACED THE RIB AT FS 880 LEFT, IAW DC-8 SRM 51-1-21.
- [SDR ABXA010503](https://openairdocs.org/sdr/ABXA010503.md): Angle · cracked · Sep 25, 2001 · N815AX · Doug DC863 · Passenger/Crew Doors
  > MAIN CARGO DOOR BOTTOM Z- ANGLE CRACKED AT FASTENER BS 140 AND BS 160. MAINTENANCE REPLACED THE Z-ANGLE AT BS 140 AND 160 IAW DC-8 SRM 53-01-0 AND 51-01-20.
- [SDR ABXA010505](https://openairdocs.org/sdr/ABXA010505.md): Longeron · cracked · Sep 25, 2001 · N815AX · Doug DC863 · Fuselage Main, Structure
  > L24L FOUND CRACKED AT FORWARD MAIN ATTACH BOLT HOLE. MAINTENANCE REPLACED L24L IAW REA D853-41938MR.
- [SDR ABXA010506](https://openairdocs.org/sdr/ABXA010506.md): Door · cracked · Sep 25, 2001 · N815AX · Doug DC863 · Passenger/Crew Doors
  > MAIN CARGO DOOR LOWER FORWARD CORNER SKIN AND FRAME CRACKED. MAINTENANCE REPAIRED THE AREA IAW REA D852-41939MR AND REA 852-41940MR.
- [SDR ABXA010507](https://openairdocs.org/sdr/ABXA010507.md): Skin · cracked · Sep 25, 2001 · N815AX · Doug DC863 · Wing Main, Frame Structure
  > RIGHT WING AT STATION XW 253 OUTBD OF #3 PYLON AT LEADING EDGE, WAS CRACKED. MAINTENANCE REPAIRED THE AREA IAW DC-8 SRM 57-2-1 FIG 2H.
- [SDR ABXA010508](https://openairdocs.org/sdr/ABXA010508.md): Skin · cracked · Sep 25, 2001 · N815AX · Doug DC863 · Fuselage Main, Structure
  > FUSELAGE EXTERIOR SKIN AT LEFT MID SERVICE DOOR CUTOUT FS 1287, CRACKED AT DOOR STRUT ATTACH POINT. MAINTENANCE INSTALLED A DOUBLER REPAIR AT FUSELAGE IAW REA D853-41936MR.
- [SDR ABXA010509](https://openairdocs.org/sdr/ABXA010509.md): Fitting · cracked · Sep 25, 2001 · N815AX · Doug DC863 · Fuselage Miscellaneous Structure
  > L24L SUPPORT FITTING AT STATION 960 WAS CRACKED AT UPPER FORWARD SIDE. MAINTENANCE REPLACED THE STUB FITTING IAW REA D 853-41938MR.
- [SDR ABXA010510](https://openairdocs.org/sdr/ABXA010510.md): Fitting · cracked · Sep 25, 2001 · N815AX · Doug DC863 · Fuselage Miscellaneous Structure
  > FUSELAGE INTERIOR LONGERON SPLICE FITTING CRACKED AT FS 680.5, RIGHT LONGERON 10 AT UPPER NUT ANGLE. MAINTENANCE REPLACED THE SPLICE FITTING IAW SRM 51-1-20D.
- [SDR ABXA010511](https://openairdocs.org/sdr/ABXA010511.md): Doubler · corroded · Sep 25, 2001 · N815AX · Doug DC863 · Fuselage Main, Structure
  > CORROSION FOUND AT FUSELAGE STATION 960 LEFT AT FLOOR LINE FINGER DOUBLER. MAINTENANCE INSTALLED DOUBLER REPAIR IAW REA D853-41935MR.
- [SDR ABXA010512](https://openairdocs.org/sdr/ABXA010512.md): Fitting · cracked · Aug 15, 2001 · N815AX · Doug DC863 · Fuselage Main, Structure
  > LEFT WHEEL WELL LONGERON 24, FUSALAGE STATION 960, SUPPORT FITTING WAS CRACKED AND CORRODED AT UPPER FORWARD AND AFT HORIZONTAL FLANGES. MAINTENANCE REPLACED THE FITTING AT STATION 960 IAW REA D853-41938MR.
- [SDR ABXA000528](https://openairdocs.org/sdr/ABXA000528.md): Seal · cut · Dec 11, 2000 · N815AX · Doug DC863F · Turbine Engine Oil System
  > TWENTY MINUTES AFTER TAKEOFF FROM EWR, THE NR 3 ENGINE OIL PRESSURE FLUCTUATED AND OIL QUANTITY DROPPED TO APPROX. ZERO GALLONS. THE CREW SHUT THE ENGINE DOWN IN FLIGHT, IAW ABX PROCEDURES. MAINTENANCE INSPECTED AND FOUND THE NR 3 FRONT ACCESSORY HOUSING O-RIN

Next page: https://openairdocs.org/deregistered/N815AX-2007-03-20/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 = 'N815AX' AND deregistration_id = 'N815AX-2007-03-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N815AX-2007-03-20/reports

---
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