# Service difficulty reports: N980AX, cancelled Jan 4, 2010

A list on [N980AX, cancelled Jan 4, 2010](https://openairdocs.org/deregistered/N980AX-2010-01-04.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 3 · 119 reports

- [SDR ABXA060189](https://openairdocs.org/sdr/ABXA060189.md): Battery · discharged · Jul 6, 2006 · N980AX · Doug DC932 · Emergency Lighting
  > ON SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW 33-53-02-4-0001.
- [SDR ABXA050128](https://openairdocs.org/sdr/ABXA050128.md): Shear Tie · cracked · May 21, 2005 · N980AX · Doug DC932 · Fuselage Internal Mounting Structure
  > SHEAR TIE CRACKED AT STA 1090, 8 INCHES OUTBOARD OF RT CENTER LINE. REMOVED AND REPLACED SHEAR TIE AT STA 1090 IAW DC-9 SRM 51-30-5 AND 53-30-2.
- [SDR ABXA050129](https://openairdocs.org/sdr/ABXA050129.md): Skin · cracked · May 20, 2005 · N980AX · Doug DC932 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED FS 1090, APPROXIMATELY 2 INCHES TO THE RIGHT SIDE OF VERTICAL STAB, SKIN CRACKED OUT OF HI-LOK APPROXIMATELY.25 INCH LONG. REPAIRED FUSELAGE SKIN AT FS 1090, RIGHT SIDE OF VERTICAL STAB IAW DC-9 SRM 53-01.
- [SDR ABXA050127](https://openairdocs.org/sdr/ABXA050127.md): Skin · cracked · May 20, 2005 · N980AX · Doug DC932 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED FS 1090, ONE O'CLOCK POSITION FACING AFT. CRACK APPROXIMATELY 2.5 INCHES LONG, LEFT SIDE OF VERTICAL STABILIZER. MANUFACTURED REPAIR DOUBLER FROM 2014T6.063 PO 408448187. REPAIRED AREA IAW DC-9 SRM 53-01.
- [SDR ABXA050130](https://openairdocs.org/sdr/ABXA050130.md): Skin · cracked · May 20, 2005 · N980AX · Doug DC932 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED FS 1090, APPROXIMATELY 4 INCHES TO THE LEFT OF VERTICAL STAB. MANUFACTURED REPAIR DOUBLER FROM 2014-T6.063 PO 408448187. REPAIRED AREA IAW DC-9 SRM 53-01.
- [SDR ABXA040379](https://openairdocs.org/sdr/ABXA040379.md): Angle · corroded · Nov 2, 2004 · N980AX · Doug DC932 · Fuselage Main, Bulkhead
  > LEFT WHEEL WELL AFT BULKHEAD UPPER ANGLE CORRODED AT BUTTLINE 0. REPAIRED ANGLE IAW REA D953-51024-MR.
- [SDR ABXA040378](https://openairdocs.org/sdr/ABXA040378.md): Longeron · cracked · Nov 1, 2004 · N980AX · Doug DC932 · Fuselage Main, Longeron/Stringer
  > LONGERON 23 LEFT CRACKED AT STA 200. REPAIRED LONGERON IAW DC-9 SRM 53-02.
- [SDR ABXA040174](https://openairdocs.org/sdr/ABXA040174.md): Battery · discharged · May 10, 2004 · N980AX · Doug DC932 · Emergency Lighting
  > EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW AMM 33-00-00.
- [SDR ABXA030171](https://openairdocs.org/sdr/ABXA030171.md): Connector · damaged · May 28, 2003 · N980AX · Doug DC932 · Overheat Detection
  > AFTER TAKEOFF, TAIL COMPARTMENT TEMP HIGH ILLUMINATED. ACCOMPLISHED EMERGENCY PROCEDURE CHECKLIST AND ANNUNCIATOR REMAINED ILLUMINATED. LANDED WITHOUT INCIDENT. REPLACED CONNECTOR P1-387, AFTER FINDING WIRES SHORTED AND TOUCHING EACH OTHER. TAIL COMPARTMENT
- [SDR ABXA030173](https://openairdocs.org/sdr/ABXA030173.md): Fitting · cracked · May 1, 2003 · N980AX · Doug DC932 · Wing Spar
  > RIGHT INBOARD FIXED VANE NR 2 SUPPORT CRACKED. REPLACED BROKEN FITTING IAW DC-9 SRM 51-30-2.
- [SDR ABXA030175](https://openairdocs.org/sdr/ABXA030175.md): Fitting · cracked · Apr 30, 2003 · N980AX · Doug DC932 · Nacelle/Pylon, Bulkhead/Firewall
  > AFT LOWER INBOARD FITTING CRACKED FS 965 PYLON BULKHEAD RIGHT SIDE. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.
- [SDR ABXA030174](https://openairdocs.org/sdr/ABXA030174.md): Frame · cracked · Apr 30, 2003 · N980AX · Doug DC932 · Fuselage Main, Frame
  > LT FORWARD MAIN FRAME FS 699 CRACKED ON FORWARD FLANGE FROM BOLT IN RADIUS. REPLACED FRAME ON JOB CARD EA 53400321-001.
- [SDR ABXA030176](https://openairdocs.org/sdr/ABXA030176.md): Attach Angle · cracked · Apr 29, 2003 · N980AX · Doug DC932 · Vertical Stabilizer, Attach Fittings
  > RIGHT AFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE WAS CRACKED. REPAIRED ANGLE IAW DC-9 SRM 53-05.
- [SDR ABXA020355](https://openairdocs.org/sdr/ABXA020355.md): Control Cable · contaminated · Dec 11, 2002 · N980AX · Doug DC932 · Power Lever
  > THROTTLES EXTREMELY DIFFICULT TO MOVE DURING FLIGHT. EXPECTED ICE CONTAMINATION. CLEANED AND LUBRICATED CABLES AND FAIRLEADS ABOVE FORWARD BAG BIN. ICE REMNENTS NOTED ON GILL LINER ABOVE BAG BIN. THROTTLE MOVEMENT NORMAL. REMOVED ICE. MOPPED CARGO COMPARTME
- [SDR ABXA020256](https://openairdocs.org/sdr/ABXA020256.md): Flange · cracked · Oct 21, 2002 · N980AX · Doug DC932 · Flight Control System
  > RIGHT FLAP INBOARD FIXED VANE GOUGED ON UPPER SURFACE DUE TO CRACKED ATTACH ANGLE. REPLACED FIXED VANE AND CRACKED VANE ATTACH ANGLE IAW DC-9 SRM 51-30-05 AND DC-9 MM 27-51-03-2-0002.
- [SDR ABXA020034](https://openairdocs.org/sdr/ABXA020034.md): Cushion · defective · Jul 8, 2002 · N980AX · Doug DC932 · Flight Compartment Equipment
  > FIRST OFFICER'S SEAT CUSHION DID NOT FIT OR ATTACH TO SEAT FRAME PROPERLY. SOMETIMES RESTRICTED AFT MOVEMENT OF CONTROL COLUMN. REPLACED FIRST OFFICER'S SEAT CUSHION AS REQUIRED IAW DC-9 MM.
- [SDR ABXA010496](https://openairdocs.org/sdr/ABXA010496.md): Switch · defective · Sep 19, 2001 · N980AX · Doug DC932 · Landing Gear Position and Warning
  > DURING DEPARTURE WHEN LANDING GEAR WAS RETRACTED, A RED NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE LANDING GEAR WAS RECYCLED AND THE GEAR RETRACTED NORMALLY. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK AND DOWN LOCK SWITCHES. OPERATIONAL CHECKS WERE C
- [SDR ABXA010494](https://openairdocs.org/sdr/ABXA010494.md): Skin · cracked · Sep 4, 2001 · N980AX · Doug DC932 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT THE AFT LOWER CORNER OF SERVICE DOOR CUT OUT. MAINTEANCE REPAIRED THE AREA IAW ABX EA 53100123-001.
- [SDR ABXA010493](https://openairdocs.org/sdr/ABXA010493.md): Splice · cracked · Sep 4, 2001 · N980AX · Doug DC932 · Fuselage Miscellaneous Structure
  > SPLICE FITTING AT FUSELAGE STATION 229, L18R WAS FOUND TO BE CRACKED. MAINTENANCE REPLACED THE FITTING IAW DC-9 SRM 51-30-1.
- [SDR ABXA010492](https://openairdocs.org/sdr/ABXA010492.md): Rib · corroded · Sep 4, 2001 · N980AX · Doug DC932 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON RIB LOCATED IN THE RIGHT NOSE WHEEL TUNNEL STATION 100, BELOW PRESSURE WEB. MAINTENANCE INSTALLED A DOUBLER IAW DC-9 SRM 51-30-2.
- [SDR ABXA010491](https://openairdocs.org/sdr/ABXA010491.md): Door Frame · cracked · Sep 4, 2001 · N980AX · Doug DC932 · Emergency Exits
  > THE LEFT AFT EMERGENCY EXIT DOOR INNER JAMB WAS CRACKED ON UPPER INTERIOR AFT CORNER ADJACENT TO HANDLE. MAINTENANCE REPAIRED THE AREA IAW DC-9 SRM 52-05.
- [SDR ABXA010490](https://openairdocs.org/sdr/ABXA010490.md): Shear Tie · cracked · Aug 31, 2001 · N980AX · Doug DC932 · Fuselage Miscellaneous Structure
  > SHEAR TIE REPAIR WAS FOUND TO BE CRACKED AT FUSELAGE STATION 980, L16R. MAINTENANCE REPLACED THE SHEAR TIE IAW DC-9 SRM AND ABX DRAWING N07080.
- [SDR ABXA010489](https://openairdocs.org/sdr/ABXA010489.md): Shear Tie · cracked · Aug 31, 2001 · N980AX · Doug DC932 · Fuselage Miscellaneous Structure
  > SHEAR TIE REPAIR WAS FOUND TO BE CRACKED AT FUSELAGE STATION 945 L14R. MAINTENANCE REPLACED THE SHEAR TIE IAW DC-0 SRM 51-30-2.
- [SDR ABXA010488](https://openairdocs.org/sdr/ABXA010488.md): Frame · cracked · Aug 31, 2001 · N980AX · Doug DC932 · Fuselage Main, Frame
  > FRAME WAS FOUND CRACKED AT FUSELAGE STATION 980,L16L. MAINTENANCE REPAIRED THE FRAME IAW DC-9 SRM.
- [SDR ABXA010487](https://openairdocs.org/sdr/ABXA010487.md): Frame · cracked · Aug 31, 2001 · N980AX · Doug DC932 · Fuselage Main, Structure
  > MAIN FRAME AT STATION 737R WAS CRACKED BETWEEN "Z" ANGLE FASTENERS. MAINTENANCE REPAIRED THE FRAME IAW ABX EA 53400320-001-1.
- [SDR ABXA010485](https://openairdocs.org/sdr/ABXA010485.md): Shear Tie · cracked · Aug 31, 2001 · N980AX · Doug DC932 · Fuselage Miscellaneous Structure
  > SHEAR TIE WAS FOUND CRACKED AT FUSELAGE STATION 1059 L17L. MAINTENANCE REPLACED THE SHEAR TIE SECTION IAW DC-9 SRM.
- [SDR ABXA010484](https://openairdocs.org/sdr/ABXA010484.md): Fitting · cracked · Aug 30, 2001 · N980AX · Doug DC932 · Fuselage Miscellaneous Structure
  > THE CABIN FLOOR LH VERTICAL SUPPORT UPPER FITTING WAS FOUND TO BE CRACKED AT STA 965. MAINTENANCE REPLACED THE CABIN FLOOR LH VERTICAL SUPPORT UPPER FITTING IAW DC-9 SRM 51-30-5.
- [SDR ABXA010483](https://openairdocs.org/sdr/ABXA010483.md): Angle · cracked · Aug 30, 2001 · N980AX · Doug DC932 · Nacelle/Pylon Structure
  > THE UPPER PYLON ATTACH ANGLE WAS FOUND TO BE CRACKED AT THE FORWARD END. MAINTENANCE REPAIRED THE ANGLE IAW DC-9 SRM 54-04 FIG. 10.
- [SDR ABXA010486](https://openairdocs.org/sdr/ABXA010486.md): Frame · cracked · Aug 20, 2001 · N980AX · Doug DC932 · Fuselage Main, Structure
  > MAIN FRAME AT STATION 718L WAS CRACKED BETWEEN "Z" ANGLE FASTENERS. MAINTENANCE REPAIRED THE FRAME IAW ABX EA 53400210-001-1.
- [SDR ABXA000090](https://openairdocs.org/sdr/ABXA000090.md): Doubler · corroded · Jan 26, 2000 · N980AX · Doug DC932 · Fuselage Main, Plate/Skin
  > WHILE COMPLYING WITH A C CHECK INSPECTION, FOUND LEFT SIDE STATIC PORT INTERNAL DOUBLER CORRODED. REPLACED INTERNAL DOUBLER IAW DC9 SRM 51-30-2.
- [SDR ABXA000089](https://openairdocs.org/sdr/ABXA000089.md): Column · cracked · Jan 26, 2000 · N980AX · Doug DC932 · Control Column Section
  > WHILE COMPLYING WITH A C CHECK INSPECTION, FOUND FIRST OFFICER'S CONTROL COLUMN CRACKED. REPLACED FIRST OFFICER'S CONTROL COLUMN REF DOUGLAS SERVICE BULLETIN.
- [SDR ABXA000088](https://openairdocs.org/sdr/ABXA000088.md): Fairing · corroded · Jan 26, 2000 · N980AX · Doug DC932 · Vertical Stabilizer
  > WHILE COMPLYING WITH A C-CHECK INSPECTION, FOUND LOWER RIGHT SIDE HORSE COLLAR CORRODED. REPLACED LOWER RIGHT SIDE HORSE COLLAR IAW DC9 MM 55-10-0 AND DC9 SRM 51-30-1.
- [SDR ABXA000084](https://openairdocs.org/sdr/ABXA000084.md): Panel · cracked · Jan 14, 2000 · N980AX · Doug DC932 · Fuselage Miscellaneous Structure
  > UPPER OUTBOARD FLANGE OF LEFT TRAP PANEL CRACKED IN AREA OF HYDRAULIC LINES. VERIFIED WITH EDDY CURRENT INSPECTION. REPLACED LEFT TRAP PANEL IAW REA NR D953-35095-MR AND DC9 SERVICE BULLETIN 53-182.
- [SDR ABXA000083](https://openairdocs.org/sdr/ABXA000083.md): Intercostal · cracked · Jan 14, 2000 · N980AX · Doug DC932 · Fuselage Miscellaneous Structure
  > WHILE COMPLYING WITH A C CHECK INSPECTION, FOUND FORWARD LOWER CARGO DOOR INTERCOSTAL WEB CRACKED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-1.
- [SDR ABXA000082](https://openairdocs.org/sdr/ABXA000082.md): Fitting · cracked · Jan 14, 2000 · N980AX · Doug DC932 · Fuselage Miscellaneous Structure
  > WHILE COMPLYING WITH A C CHECK INSPECTION, FOUND RIGHT WHEEL WELL KEEL TO FLOORBEAM ATTACH FITTING CRACKED AT STA 718. REPLACED FITTING IAW DC9 SRM 51-30-5.
- [SDR ABXA000081](https://openairdocs.org/sdr/ABXA000081.md): Fitting · cracked · Jan 14, 2000 · N980AX · Doug DC932 · Fuselage Miscellaneous Structure
  > WHILE COMPLYING WITH A C CHECK INSPECTION, FOUND RIGHT WHEEL WELL KEEL TO FLOORBEAM ATACH FITTING CRACKED AT STA 737. REPLACED FITTING IAW DC9 SRM 51-30-5.
- [SDR ABXA9900376](https://openairdocs.org/sdr/ABXA9900376.md): Relay · failed · May 19, 1999 · N980AX · Doug DC932 · DC Power Distribution System
  > EMERGENCY DC BUS OFF LIGHT ILLUMINATED ON GENERATOR INOP CROSS-TIE CHECK. FOUND CONTACTS BETWEEN TERMINALS B1 AND B2 OPEN ON RELAY R2-19. REPLACED RELAY IAW DC9 MM, OPS CHECKED GOOD.
- [SDR ABXA9800876](https://openairdocs.org/sdr/ABXA9800876.md): Light · malfunctioned · Oct 6, 1998 · N980AX · Doug DC932 · Landing Gear Position and Warning
  > DURING LANDING GEAR RETRACTION, THE RIGHT GEAR UNSAFE (RED) LIGHT REMAINED ILLUMINATED. RECYCLED GEAR. NO CHANGE. GREEN LIGHT REMAINED OUT. WITH GEAR DOWN, LIGHTS WERE NORMAL. REPAIRED SHORTED WIRE AT TERMINAL STRIP S3-66.
- [SDR ABXA9800477](https://openairdocs.org/sdr/ABXA9800477.md): Valve · failed · May 29, 1998 · N980AX · Doug DC932 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, GEAR HANDLE SELECTED UP, THE NOSE LANDING GEAR AND MAIN LANDING GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. GEAR WAS RECYCLED THREE TIMES WITH THE SAME RESULT. REPLACED LANDING GEAR CONTROL VALVE IAW DC9 MM 32-32-0.
- [SDR ABXA9800465](https://openairdocs.org/sdr/ABXA9800465.md): Shear Tie · cracked · May 25, 1998 · N980AX · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND FRAME SHEAR TIE AT STATION 1019 CRACKED BETWEEN LONGERON 14L AND 15L. REPLACED SHEAR TIE IAW DC9 SRM 51-30-5.
- [SDR ABXA9800463](https://openairdocs.org/sdr/ABXA9800463.md): Floorbeam · cracked · May 12, 1998 · N980AX · Doug DC932 · Fuselage Main, Floor Beam
  > DURING C-CHECK, FLOORBEAM AT STATION 351 BL6 LEFT WAS FOUND CRACKED. REPAIRED IAW ABX REA D953-23658-MR.
- [SDR ABXA9800460](https://openairdocs.org/sdr/ABXA9800460.md): Blkhd Fitting · cracked · May 12, 1998 · N980AX · Doug DC932 · Fuselage Main, Bulkhead
  > DURING C-CHECK, AFT PRESSURE BULKHEAD DOOR RIGHT VERTICAL SUPPORT FITTING WAS FOUND CRACKED. REPLACED FITTING IAW DC9 SRM 51-10-04.
- [SDR ABXA9800458](https://openairdocs.org/sdr/ABXA9800458.md): Fitting · corroded · May 12, 1998 · N980AX · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, LEVEL II CORROSION WAS FOUND ON LONGERON 28 RIGHT END CAP STATION 604. REPLACED IAW DC9 SRM 51-10-03.
- [SDR ABXA9800462](https://openairdocs.org/sdr/ABXA9800462.md): Splice · cracked · May 11, 1998 · N980AX · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, LONGERON SPLICE AT STATION 794-813, LONGERON 30 WAS FOUND CRACKED. REPLACED IAW DC9 SRM 53-02.
- [SDR ABXA9800461](https://openairdocs.org/sdr/ABXA9800461.md): Longeron · cracked · May 11, 1998 · N980AX · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, LONGERON 5 RIGHT WAS FOUND CRACKED AT STATION 756. REPAIRED IAW DC9 SRM 51-30-1.
- [SDR ABXA9800459](https://openairdocs.org/sdr/ABXA9800459.md): Fitting · corroded · May 11, 1998 · N980AX · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, LEVEL II CORROSION WAS FOUND ON LONGERON 27 RIGHT AND END CAP AT STATION 604. REPLACED FITTING IAW DC9 SRM 51-30-2.
- [SDR ABXA9800456](https://openairdocs.org/sdr/ABXA9800456.md): Angle · cracked · May 11, 1998 · N980AX · Doug DC932 · Nacelle/Pylon Structure
  > DURING C-CHECK, THE LEFT UPPER PYLON ATTACH ANGLE WAS FOUND CRACKED. REPAIRED IAW DC9 SRM 54-04.
- [SDR ABXA9800457](https://openairdocs.org/sdr/ABXA9800457.md): Hinge · cracked · May 6, 1998 · N980AX · Doug DC932 · Trailing Edge Flaps
  > DURING C-CHECK, THE LEFT FLAP CENTER HINGE WAS FOUND CRACKED. REPLACED IAW DC9 MM 27-50-1.
- [SDR ABXA9800311](https://openairdocs.org/sdr/ABXA9800311.md): Uplatch · worn · Apr 1, 1998 · N980AX · Doug DC932 · Landing Gear Position and Warning
  > AFTER GEAR RETRACTION ON TAKEOFF, THE RIGHT GEAR UNSAFE LIGHT REMAINED ON. RECYCLED GEAR AND PERFORMED UPLATCH CHECK WITH NORMAL INDICATION. REPLACED RIGHT MAIN LANDING GEAR DOOR UPLATCH ASSEMBLY IAW DC9 MM 32-31-4.
- [SDR ABXA9800290](https://openairdocs.org/sdr/ABXA9800290.md): Unsafe Light · illuminated · Mar 31, 1998 · N980AX · Doug DC932 · Landing Gear Position and Warning
  > AFTER GEAR RETRACTION, THE RIGHT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. IN THE GEAR UP-LATCH CHECK POSITION, THE GEAR DOOR UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR DOWN AND UP, NORMAL OPERATION. PERFORMED ADJUSTMENT/TEST IAW DC9 MM 32-31-4, FOUND NO DEFECTS

Next page: https://openairdocs.org/deregistered/N980AX-2010-01-04/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 = 'N980AX' AND deregistration_id = 'N980AX-2010-01-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N980AX-2010-01-04/reports

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