# Service difficulty reports: N982AX, cancelled Mar 8, 2018

A list on [N982AX, cancelled Mar 8, 2018](https://openairdocs.org/deregistered/N982AX-2018-03-08.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 · 131 reports

- [SDR ABXA070076](https://openairdocs.org/sdr/ABXA070076.md): Unknown · odor · Mar 20, 2007 · N982AX · Doug DC932 · Air Distribution System
  > AIRCRAFT HAS STRONG ODOR OF FUEL OR SOLVENT IN COCKPIT AND CARGO AREA. NO FUEL LEAK OR ODOR NOTED IAW DC9 MM 28-00-00.
- [SDR ABXA050164](https://openairdocs.org/sdr/ABXA050164.md): Door Frame · cracked · Jun 17, 2005 · N982AX · Doug DC932 · Fuselage Main, Structure
  > LEFT AFT UPPER DOOR JAMB CRACKED, EMERGENCY EXIT, IN 2 PLACES. REPAIRED LEFT AFT UPPER DOOR JAMB IAW DC-9 SRM 53-05.
- [SDR ABXA050163](https://openairdocs.org/sdr/ABXA050163.md): Threshold · corroded · Jun 16, 2005 · N982AX · Doug DC932 · Fuselage Miscellaneous Structure
  > SERVICE DOOR THRESHOLD SKIN BULGING AT STA 176, RIGHT BUTT LINE 58. REPAIRED AREA IAW DC-9 SRM 51-10-2.
- [SDR ABXA050162](https://openairdocs.org/sdr/ABXA050162.md): Frame · cracked · Jun 15, 2005 · N982AX · Doug DC932 · Fuselage Main, Frame
  > SHEAR TIE CRACKED IN RADIUS FRAME STA 813 BETWEEN LONGERON 29 LEFT AND 30. REPAIRED SHEAR TIE IAW DC-9 SRM 53-03 AND DWG SR09530212.
- [SDR ABXA050161](https://openairdocs.org/sdr/ABXA050161.md): Floorbeam · corroded · Jun 14, 2005 · N982AX · Doug DC932 · Fuselage Main, Floor Beam
  > LOWER LEG OF FLOORBEAM WAS CORRODED ON UPPER AND LOWER SURFACE AT STA 313, BUTTLINE 38 RIGHT. REPAIRED FLOORBEAM IAW DC-9 SRM 53.
- [SDR ABXA050159](https://openairdocs.org/sdr/ABXA050159.md): Retainer · cracked · Jun 14, 2005 · N982AX · Doug DC932 · Fuselage Main, Structure
  > STA 756, LONGERON 15 RIGHT, HAD CRACK AT WINDOW RETAINER. REMOVED AND REPLACED DAMAGED CLIP. FABRICATED AND INSTALLED NEW CLIP IAW DACO DWG 3914137 AND DC-9 SRM 51-30-5.
- [SDR ABXA050160](https://openairdocs.org/sdr/ABXA050160.md): Retainer · cracked · Jun 14, 2005 · N982AX · Doug DC932 · Fuselage Main, Structure
  > STA 598, LONGERON 10 RT, HAD CRACK AT WINDOW RETAINER. REPAIRED WINDOW RETAINER AT FS 598, LONGERON 10 RIGHT IAW DC-9 SSRM DWG K07226.
- [SDR ABXA040385](https://openairdocs.org/sdr/ABXA040385.md): Warning Light · illuminated · Nov 26, 2004 · N982AX · Doug DC932 · Landing Gear Position and Warning
  > NOSE LANDING GEAR LIGHT WAS NOT ILLUMINATED ON GEAR EXTENSION. RECYCLED GEAR, LIGHT CAME ON. INSPECTED NOSE LANDING GEAR WIRING FOR CONTINUITY & PIN ENGAGEMENT AT SWITCH CONNECTORS. INSPECTED SWITCHES FOR SECURITY AND OPERATION. CYCLED NOSE LANDING GEAR 10
- [SDR ABXA030446](https://openairdocs.org/sdr/ABXA030446.md): Wire · burned · Nov 21, 2003 · N982AX · Doug DC932 · Electrical Power System Wiring
  > WIRE BURNED ON PHASE C, GROUND SERVICE BUS POWER PANEL, WIRE HV X22810C. REMOVED BURNED AREA OF WIRE AND REPLACED WIRE END CONNECTOR. INSTALLED WIRE TO GROUND SERVICE BUS PHASE C IAW DC9 MM 20-50-01-2-0001. OPS CHECK GOOD.
- [SDR ABXA030414](https://openairdocs.org/sdr/ABXA030414.md): Frame · cracked · Oct 15, 2003 · N982AX · Doug DC932 · Fuselage Main, Frame
  > FRAME CRACKED AT FS 1076 AND LONGERON 19 LEFT. REPAIRED FRAME AT FS 1076 IAW DC-9 SRM 53-03.
- [SDR ABXA030413](https://openairdocs.org/sdr/ABXA030413.md): Angle · cracked · Oct 15, 2003 · N982AX · Doug DC932 · Fuselage Miscellaneous Structure
  > CRACK IN FRAME ATTACH ANGLE AT STA 1038 ABOVE LONGERON 18 LT. REPAIRED ANGLE IAW DC-9 SSRM DWG K05159.
- [SDR ABXA030408](https://openairdocs.org/sdr/ABXA030408.md): Rib · cracked · Oct 14, 2003 · N982AX · Doug DC932 · Vertical Stabilizer, Spar/Rib
  > LEFT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON A RIB TOWARD THE TOP END OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159.
- [SDR ABXA030409](https://openairdocs.org/sdr/ABXA030409.md): Rib · cracked · Oct 14, 2003 · N982AX · Doug DC932 · Vertical Stabilizer, Spar/Rib
  > LEFT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON A RIB IN THE MIDDLE OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159.
- [SDR ABXA030412](https://openairdocs.org/sdr/ABXA030412.md): Rib · cracked · Oct 14, 2003 · N982AX · Doug DC932 · Wing, Rib/Bulkhead
  > END OF LEADING EDGE RIB RIGHT WING CRACKED AT STA 353. REPAIRED DAMAGED RIB IAW DC-9 SRM 57-06.
- [SDR ABXA030411](https://openairdocs.org/sdr/ABXA030411.md): Rib · cracked · Oct 14, 2003 · N982AX · Doug DC932 · Vertical Stabilizer, Spar/Rib
  > RIGHT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON RIB IN THE MIDDLE OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159.
- [SDR ABXA030410](https://openairdocs.org/sdr/ABXA030410.md): Rib · cracked · Oct 14, 2003 · N982AX · Doug DC932 · Vertical Stabilizer, Spar/Rib
  > RIGHT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON A RIB AT THE BOTTOM OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159.
- [SDR ABXA030151](https://openairdocs.org/sdr/ABXA030151.md): Panel · cracked · May 20, 2003 · N982AX · Doug DC932 · Wing, Plate/Skin
  > WHILE PERFORMING ROUTINE LINE MAINTENANCE, A FUEL LEAK WAS DISCOVERED AT THE LT WING FUEL PANEL 1307. FURTHER INSPECTION REVEALED A CRACK ON THE FUEL PANEL FLANGE. REPAIRED CRACK IAW DC-9 SRM 57-03, FIG 23.
- [SDR ABXA020076](https://openairdocs.org/sdr/ABXA020076.md): Duct · disconnected · Aug 12, 2002 · N982AX · Doug DC932 · Air Distribution System
  > AT FL 350, CABIN ALTITUDE INCREASED TO 9,500 ALONG WITH THE RIGHT GENERATOR TRIPPING OFF LINE. RESET GENERATOR. PERFORMED DESCENT TO 14,000 CABIN ALTITUDE WAS REGAINED AT APPROXIMATELY 17,000 TO 18,000. PACK PRESSURE NORMAL AS WELL AS ELECTRICAL PARAMETERS
- [SDR ABXA010782](https://openairdocs.org/sdr/ABXA010782.md): Wire · broken · Mar 20, 2002 · N982AX · Doug DC932 · Landing Gear System Wiring
  > ON LANDING AT BDL, NO GREEN GEAR LIGHT. RECYCLED LANDING GEAR, THE GREEN LIGHT ILLUMINATED. REPAIRED BROKEN WIRES TO THE NOSE GEAR UP LIMIT SWITCH CONNECTOR (P1-134) AND REPLACED THE UP LIMIT SWITCH AS A PRECAUTION. OPS CHECKED GOOD IAW DC9 MM 32-60-01-02.
- [SDR ABXA010755](https://openairdocs.org/sdr/ABXA010755.md): Switch · defective · Mar 1, 2002 · N982AX · Doug DC932 · Landing Gear Position and Warning
  > ON INITIAL GEAR EXTENSION AT ILN, NOSE GEAR DID NOT INDICATE DOWN/LOCKED. SUBSEQUENT RETRACTION/EXTENSION CYCLE YIELDED NORMAL INDICATION. REPLACED THE NOSE GEAR DOWN LOCK SWITCH IAW DC-9 MM 32-60-02.
- [SDR ABXA010754](https://openairdocs.org/sdr/ABXA010754.md): Warning System · malfunctioned · Feb 28, 2002 · N982AX · Doug DC932 · Landing Gear Position and Warning
  > ON INITIAL GEAR EXTENSION AT ILN, NOSE LANDING GEAR DID NOT INDICATE DOWN/LOCKED. SUBSEQUENTIAL RETRACT/EXTENSION CYCLE YIELDED NORMAL INDICATION. PERFORMED FUNCTIONAL CHECK IAW DC-9 MM 32-60-00-2-0101, NORMAL INDICATION AT THIS TIME.
- [SDR ABXA010749](https://openairdocs.org/sdr/ABXA010749.md): Rib · cracked · Feb 19, 2002 · N982AX · Doug DC932 · Wing Structure
  > RIGHT WING LEADING EDGE RIB (JUST INBOARD OF #2 SLAT TRACK) CRACKED AT THE LOWER ATTACH FASTENER. REPAIRED RIB IAW DC-9 REA D957-43342.
- [SDR ABXA010748](https://openairdocs.org/sdr/ABXA010748.md): Web · cracked · Feb 13, 2002 · N982AX · Doug DC932 · Fuselage Miscellaneous Structure
  > CUSP WEB CRACKED (AFT WEB) AT FS 236, LONGERON 18 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01.
- [SDR ABXA010746](https://openairdocs.org/sdr/ABXA010746.md): Door Frame · cracked · Feb 13, 2002 · N982AX · Doug DC932 · Fuselage Main, Structure
  > CRACK IN FORWARD ACCESSORY COMPARTMENT DOOR JAMB, APPROXIMATELY 1.5 INCH LONG, LOCATED ALONG THE UPPER AFT SIDE OF JAMB. REPAIRED DOOR JAMB IAW DC-9 SRM 51-10-3 AND 51-20.
- [SDR ABXA010745](https://openairdocs.org/sdr/ABXA010745.md): Shear Tie · corroded · Feb 13, 2002 · N982AX · Doug DC932 · Fuselage Main, Structure
  > HEAVY CORROSION ON FRAME SPLICE ANGLE ON AFT SIDE OF FRAME AT STATION 943, ABOVE LONGERON 29 LEFT. REPLACED SPLICE ANGLE IAW DC-9 SRM 51-30-5.
- [SDR ABXA010744](https://openairdocs.org/sdr/ABXA010744.md): Frame · corroded · Feb 13, 2002 · N982AX · Doug DC932 · Fuselage Main, Structure
  > HEAVY CORROSION ON UPPER CARGO FLOOR FRAME AT STATION 929 ABOVE TWO FASTENERS THAT HOLD THE AFT LOWER CARGO DOOR HOLD OPEN HOOK. REMOVED CORROSION AND INSTALLED REPAIR IAW DC-9 SRM 53-05.
- [SDR ABXA010747](https://openairdocs.org/sdr/ABXA010747.md): Frame · corroded · Feb 13, 2002 · N982AX · Doug DC932 · Fuselage Main, Structure
  > FRAME WAS CORRODED AT STATION 332, FROM LONGERON 29 LEFT TO LONGERON 29 RIGHT. REPAIRED FRAME IAW DC-9 SRM.
- [SDR ABXA010743](https://openairdocs.org/sdr/ABXA010743.md): Web · cracked · Feb 13, 2002 · N982AX · Doug DC932 · Fuselage Miscellaneous Structure
  > CUSP WEB CRACKED BETWEEN FS 945 AND 965, LEFT SIDE. REPAIRED CRACKED AREA IAW DC-9 SRM 53-01.
- [SDR ABXA010742](https://openairdocs.org/sdr/ABXA010742.md): Web · cracked · Feb 13, 2002 · N982AX · Doug DC932 · Fuselage Miscellaneous Structure
  > FRAME FOOT, WEB CRACKED AT FS 996, LONGERON 18 LEFT. REPLACED WEB IAW DC-9 SRM 53-11-3 AND 51-30-5.
- [SDR ABXA010750](https://openairdocs.org/sdr/ABXA010750.md): Fitting · cracked · Feb 12, 2002 · N982AX · Doug DC932 · Fuselage Main, Structure
  > LONGERON 29 RIGHT HAD CRACKED END FITTING AFT OF F.S. 604 "P" DOME. REPLACED END CAP IAW DC-9 SRM 51-30-5.
- [SDR ABXA010741](https://openairdocs.org/sdr/ABXA010741.md): Intercostal · cracked · Feb 12, 2002 · N982AX · Doug DC932 · Fuselage Main, Structure
  > CRACK IN INTERCOSTAL LONGERON 27 LEFT, STATION 761. REPAIRED AREA IAW DC-9 DOUGLAS DWG 9915574.
- [SDR ABXA010740](https://openairdocs.org/sdr/ABXA010740.md): Fitting · cracked · Feb 12, 2002 · N982AX · Doug DC932 · Fuselage Main, Structure
  > LONGERON 28 RIGHT HAD CRACKED END FITTING AFT OF F.S. 604 "P" DOME. REPLACED END CAP IAW DC-9 SRM 51-30-5.
- [SDR ABXA010536](https://openairdocs.org/sdr/ABXA010536.md): Engine · failed · Oct 15, 2001 · N982AX · Doug DC932 · Engine (Turbine/Turboprop)
  > CLIMBING THROUGH FL 190, CREW HEARD A LOUD POP AND NOTICED THE LEFT ENGINE HAD DECREASED TO 1.35 EPR AND THE EGT HAD INCREASED TO 550. OPERATED ENGINE AT REDUCED POWER AND RETURNED TO LAND. REPLACED THE NR 1 ENGINE IAW DC-9 JOB CARD 9090010 AND DC-9 8A & 8B.
- [SDR ABXA010456](https://openairdocs.org/sdr/ABXA010456.md): Light · inoperative · Aug 29, 2001 · N982AX · Doug DC932 · Landing Gear Position and Warning
  > CREW REPORTED ON APPROACH DOOR OPEN LIGHT WOULD NOT PRESS TO TEST. DID FLY BY, TOWER REPORTED DOORS CLOSED. RELAMPED GEAR DOOR OPEN LIGHT PRESS TO TEST INDICATOR. OPS CHECKED GOOD IAW DC-9 MM.
- [SDR ABXA0100013](https://openairdocs.org/sdr/ABXA0100013.md): Battery · discharged · Jan 16, 2001 · N982AX · Doug DC932 · Emergency Lighting
  > EMERGENCY LIGHTS WOULD NOT OPERATE WHEN SWITCH WAS SELECTED ON. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY IAW DC-9 MM 33-52-02.
- [SDR ABXA0100012](https://openairdocs.org/sdr/ABXA0100012.md): Contactor · dirty · Jan 16, 2001 · N982AX · Doug DC932 · Emergency Lighting
  > EMERGENCY LIGHTS WOULD NOT TEST DURING PRE-DEPARTURE CHECK. MAINTENANCE INSPECTED AND CLEANED THE EMERGENCY LIGHT BATTERY CONTACTS AND RESEATED BATTERIES IN THE CHARGER. OPS CHECKED GOOD IAW DC-9 MM.
- [SDR ABXA000328](https://openairdocs.org/sdr/ABXA000328.md): Angle · cracked · Jun 26, 2000 · N982AX · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND INTERCOSTAL TO FLOORBEAM ATTACH ANGLE CRACKED AT STATION 617, LEFT BL 44. REPLACED ANGLE IAW DC9 SRM 51-30-5.
- [SDR ABXA000327](https://openairdocs.org/sdr/ABXA000327.md): Panel · cracked · Jun 26, 2000 · N982AX · Doug DC932 · Wing, Plate/Skin
  > DURING C-CHECK, FOUND RIGHT TRAP PANEL CRACKED AT TOP OUTBOARD FLANGE. REPLACED RIGHT TRAP PANEL IAW DC9 SRM 51-30-5, AND DC9 S/B 53-182.
- [SDR ABXA000331](https://openairdocs.org/sdr/ABXA000331.md): Intercostal · cracked · Jun 22, 2000 · N982AX · Doug DC932 · Cargo/Baggage Doors
  > DURING C-CHECK, FOUND THE FORWARD LOWER CARGO INTERCOSTAL WEB CRACKED. REPLACED FORWARD CARGO DOOR WEB IAW DC9 SRM 51-30-2.
- [SDR ABXA000309](https://openairdocs.org/sdr/ABXA000309.md): Splice · cracked · Jun 22, 2000 · N982AX · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING C-CHECK FOUND FLOOR SUPPORT TO INTERCOSTAL STRAP CRACKED AT STATION 737 OUTBOARD OF RIGHT BL 22. INSTALLED SPLICE IAW DC9 SRM 51-30-02.
- [SDR ABXA000330](https://openairdocs.org/sdr/ABXA000330.md): Pan · cracked · Jun 14, 2000 · N982AX · Doug DC932 · Cargo/Baggage Doors
  > DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR OUTER PAN CRACKED. REPAIRED IAW DC9 SRM 52-03.
- [SDR ABXA000329](https://openairdocs.org/sdr/ABXA000329.md): Intercostal · cracked · Jun 14, 2000 · N982AX · Doug DC932 · Cargo/Baggage Doors
  > DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2.
- [SDR ABXA000326](https://openairdocs.org/sdr/ABXA000326.md): Attach Fitting · cracked · Jun 14, 2000 · N982AX · Doug DC932 · Fuselage Main, Attach Fittings
  > DURING C-CHECK, FOUND CRACK AT UPPER ANTI-COLLISION LIGHT ATTACH PLATE. REPAIRED IAW ABX REA D953-37600MR.
- [SDR ABXA000073](https://openairdocs.org/sdr/ABXA000073.md): Battery · discharged · Jan 24, 2000 · N982AX · Doug DC932 · Emergency Lighting
  > EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES.
- [SDR ABXA9900794](https://openairdocs.org/sdr/ABXA9900794.md): Circuit Breaker · failed · Nov 16, 1999 · N982AX · Doug DC932 · Emergency Lighting
  > EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHTING 5 AMP CIRCUIT BREAKER IAW DC9 MM 33-53, OPS CHECKED GOOD.
- [SDR ABXA9801137](https://openairdocs.org/sdr/ABXA9801137.md): Web · corroded · Dec 1, 1998 · N982AX · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND PRESSURE DECK WEB CORRODED BEYOND LIMITS AT STATION 756 TO 752, RBL 15. REPAIRED PRESSURE DECK WEB IAW DC9 SRM 53-04.
- [SDR ABXA9801140](https://openairdocs.org/sdr/ABXA9801140.md): Bracket · corroded · Nov 30, 1998 · N982AX · Doug DC932 · Trailing Edge Flaps
  > DURING C-CHECK, FOUND LEFT FLAP INBOARD AFT HINGE BRACKET CORRODED AT PIVOT POINT. REPLACED AFT HINGE BRACKET IAW DC9 SRM.
- [SDR ABXA9801139](https://openairdocs.org/sdr/ABXA9801139.md): Frame · cracked · Nov 30, 1998 · N982AX · Doug DC932 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND FRAME 1076 CRACKED AT LONGERONS 2L AND 2R. REPAIRED FRAME IAW DC9 SRM 53-03.
- [SDR ABXA9801138](https://openairdocs.org/sdr/ABXA9801138.md): Blkhd Stiffener · cracked · Nov 30, 1998 · N982AX · Doug DC932 · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND STIFFENER CRACKED AT AFT SIDE OF BULKHEAD 1087, BL 0.0. REPLACED STIFFENER IAW DC9 SRM 51-30-5 AND 51-10-4.
- [SDR ABXA9801176](https://openairdocs.org/sdr/ABXA9801176.md): Frame · cracked · Nov 23, 1998 · N982AX · Doug DC932 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND FRAME AT STATION 980 CRACKED BETWEEN LONGERONS 14R AND 17R. REPAIRED FRAME IAW DC9 SRM 53-03.

Next page: https://openairdocs.org/deregistered/N982AX-2018-03-08/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 = 'N982AX' AND deregistration_id = 'N982AX-2018-03-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N982AX-2018-03-08/reports

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