# Service difficulty reports: N908AX, cancelled Mar 31, 2016

A list on [N908AX, cancelled Mar 31, 2016](https://openairdocs.org/deregistered/N908AX-2016-03-31.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 · 110 reports

- [SDR ABXA060072](https://openairdocs.org/sdr/ABXA060072.md): Intercostal · cracked · Jan 30, 2006 · N908AX · Doug DC931 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 996 LONGERON 12 RIGHT FOUND CRACKED. REPAIRED AREA IAW DC9 SRM 53-01.
- [SDR ABXA060071](https://openairdocs.org/sdr/ABXA060071.md): Fitting · cracked · Jan 19, 2006 · N908AX · Doug DC931 · Fuselage Main, Attach Fittings
  > AFT PRESSURE BULKHEAD DOOR JAMB HAD BOTH LEFT AND RIGHT UPPER ATTACH ANGLES CRACKED. REMOVED AND REPLACED UPPER ATTACH ANGLES IAW DC9 SRM 51-30-5 AND 51-30-2.
- [SDR ABXA060068](https://openairdocs.org/sdr/ABXA060068.md): Splice · corroded · Jan 18, 2006 · N908AX · Doug DC931 · Fuselage Main, Bulkhead
  > FOUND LONGERON 23 LEFT AT P DOME SPLICE HAD CORROSION ON OUTBOARD FLANGE. REMOVED AND REPLACED LONGERON SECTION IAW DC9 SRM 53-02.
- [SDR ABXA060069](https://openairdocs.org/sdr/ABXA060069.md): Skin · corroded · Jan 18, 2006 · N908AX · Doug DC931 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN INTERIOR SURFACE HAD SURFACE CORROSION FROM LONGERON 26 RIGHT TO 26 LEFT AT AFT PRESSURE BULKHEAD TEE CAP AREA. REPAIRED SKIN IAW DC9 SRM.
- [SDR ABXA060067](https://openairdocs.org/sdr/ABXA060067.md): Bulkhead · corroded · Jan 18, 2006 · N908AX · Doug DC931 · Fuselage Main, Bulkhead
  > AFT LOWER CARGO BULKHEAD WEB, STA 996 LEFT, CORRODED AT NUMEROUS AREAS. REMOVED AND REPLACED WEB IAW DC9 SRM 53-11-3.
- [SDR ABXA060070](https://openairdocs.org/sdr/ABXA060070.md): Bulkhead · corroded · Jan 18, 2006 · N908AX · Doug DC931 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD LOWER WEB HAD SURFACE CORROSION ON FORWARD AND AFT SIDE LONGERON 23 RIGHT TO 23 LEFT IN TEE CAP AREA. REPAIRED AFT PRESSURE BULKHEAD WEB IAW DC9 SRM 53-05.
- [SDR ABXA060066](https://openairdocs.org/sdr/ABXA060066.md): Bulkhead · cracked · Jan 17, 2006 · N908AX · Doug DC931 · Fuselage Main, Bulkhead
  > FORMER ON AFT PRESSURE BULKHEAD STA. Z74 RIGHT CRACKED. REMOVED AND REPLACED FORMER IAW DC9 SRM 51-30-2.
- [SDR ABXA060065](https://openairdocs.org/sdr/ABXA060065.md): Structure · gouged · Jan 13, 2006 · N908AX · Doug DC931 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD 'T' CAP WAS GOUGED ABOUT 3/8" BELOW SKIN JUST TO THE RIGHT OF CENTER AT BOTTOM. NR 4 TEE CAP REMOVED AND REPLACED ON JC EA 53120035-006.
- [SDR ABXA060063](https://openairdocs.org/sdr/ABXA060063.md): Repair · cracked · Jan 12, 2006 · N908AX · Doug DC931 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD LEFT UPPER CORNER 5910130-13 DOUBLER (ORIGINAL OEM) CRACKED FROM LEFT EOP. REPAIRED CORNER IAW REA D953-53106-MR.
- [SDR ABXA060061](https://openairdocs.org/sdr/ABXA060061.md): Repair · cracked · Jan 12, 2006 · N908AX · Doug DC931 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD LEFT DOOR JAMB CORNER REPAIR DOUBLER CRACKED. REMOVED AND REPLACED DOUBLER IAW DC9 SRM.
- [SDR ABXA060064](https://openairdocs.org/sdr/ABXA060064.md): Frame · cracked · Jan 12, 2006 · N908AX · Doug DC931 · Fuselage Main, Frame
  > LEFT FORWARD MAIN FRAME FS 699, FORWARD FLANGE CRACKED AT PT J AND AFT FLANGE CRACKED PTS H-I. REMOVED AND REPLACED MAIN FRAME AT FS 699 LEFT IAW JC EA 53400321-001-2.
- [SDR ABXA060062](https://openairdocs.org/sdr/ABXA060062.md): Longeron · cracked · Jan 12, 2006 · N908AX · Doug DC931 · Fuselage Main, Longeron/Stringer
  > FOUND LONGERON 4 FEET AT STA 200 CRACKED. REMOVED AND REPLACED LONGERON 4 LEFT, STA 160.230 IAW DC9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA050151](https://openairdocs.org/sdr/ABXA050151.md): Wire · broken · Jun 10, 2005 · N908AX · Doug DC931 · Landing Gear System Wiring
  > RT MAIN GEAR DOWN INDICATION "GREEN LIGHT" INTERMITTENT. CHECKED WITH ALT MAIN GEAR INDICATION. SHOWED GEAR DOWN. DID A MISSED APPROACH AND DECLARED AN EMERGENCY. VERIFIED NO RIGHT GEAR INDICATION, ALT SYS GOOD, FOUND CORROSION ON SWITCH S1-184 AND CONNECT
- [SDR ABXA040142](https://openairdocs.org/sdr/ABXA040142.md): Latch · jammed · Apr 21, 2004 · N908AX · Doug DC931 · Fixed Inner Doors
  > COCKPIT DOOR LATCH JAMMED. DISASSEMBLED COCKPIT DOOR LATCH ASSEMBLY, FOUND HANDLE JAMMED. FREED JAM AND REASSEMBLED. OPS CHECKED GOOD IAW DC-9 MM.
- [SDR ABXA040084](https://openairdocs.org/sdr/ABXA040084.md): Structure · cracked · Feb 18, 2004 · N908AX · Doug DC931 · Fuselage Main, Structure
  > RIVET ROW FOUND CRACKED AT STA 76.550 UNDER CO-PILOT'S WINDSHIELD WIPER BETWEEN APPROXIMATELY LONGERON 3 AND 4 RIGHT. REPAIRED AREA IAW EA 53100075-003-2.
- [SDR ABXA040082](https://openairdocs.org/sdr/ABXA040082.md): Fitting · cracked · Feb 17, 2004 · N908AX · Doug DC931 · Fuselage Miscellaneous Structure
  > SLANT PANEL INBOARD ANGLE FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2, 51-10-4, AND 51-30-1.
- [SDR ABXA040080](https://openairdocs.org/sdr/ABXA040080.md): Angle · cracked · Feb 17, 2004 · N908AX · Doug DC931 · Nacelle/Pylon Miscellaneous Structure
  > LEFT PYLON UPPER ATTACH ANGLE WAS CRACKED AT STA 1019. REPAIRED AREA IAW DC-9 SRM 54-04.
- [SDR ABXA040083](https://openairdocs.org/sdr/ABXA040083.md): Actuator · cracked · Feb 17, 2004 · N908AX · Doug DC931 · Landing Gear Door Actuator
  > FITTING FORWARD OF DOOR ACTUATOR CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.
- [SDR ABXA040081](https://openairdocs.org/sdr/ABXA040081.md): Longeron · cracked · Feb 17, 2004 · N908AX · Doug DC931 · Fuselage Main, Longeron/Stringer
  > LONGERON 17 RIGHT HAD 2 CRACKS AT EACH LOCATION, FS 389, FS 408 AND FS 427. REPAIRED LONGERON 17 RIGHT FROM STA 388 TO 446 IAW DC-9 SRM 53-02.
- [SDR ABXA040029](https://openairdocs.org/sdr/ABXA040029.md): Amplifier · failed · Jan 15, 2004 · N908AX · Doug DC931 · Smoke Detection
  > CARGO SMOKE LIGHT ON IN FLT. COULD NOT DUPLICATE. INSPECTED WIRING, TAPPED ON DETECTORS & AMPLIFIER, LIGHT REMAINED OUT. FOR PRECAUTION, R & R BOTH SMOKE DETECTORS & SMOKE DETECTOR AMP. PERFORMED CHECK USING LIQUID SMOKE. SYSTEM OPS CHECKED GOOD IAW DC-9
- [SDR ABXA030371](https://openairdocs.org/sdr/ABXA030371.md): Uplock · out of adjust · Sep 30, 2003 · N908AX · Doug DC931 · Landing Gear Position and Warning
  > CYCLED MAIN LANDING GEAR AT 210 KNOTS, 3000 FT, CLEAN UPON RETRACT. RIGHT MAIN LANDING GEAR UNSAFE LIGHT STAYED ON. ADJUSTED RIGHT MAIN LANDING GEAR DOOR UPLATCH IAW DC-9 MM AND WORK ACCOMPLISHED ON W.O. NR 2003908. OPS CHECKED GOOD.
- [SDR ABXA030055](https://openairdocs.org/sdr/ABXA030055.md): Control Panel · defective · Jan 30, 2003 · N908AX · Doug DC931 · Autopilot System
  > AIRCRAFT SHOOK VIOLENTLY WHEN AUTO PILOT TURNED ON. TURNED OFF AND TRIED AGAIN. SAME RESULTS. TURNED OFF AUTO PILOT, NOTICED NO YOKE MOVEMENT. REMOVED AND REPLACED AUTO PILOT CONTROLLER. SYSTEM OPS CHECKED GOOD IAW DC-9 MM 22-10-00-5.
- [SDR ABXA020342](https://openairdocs.org/sdr/ABXA020342.md): Elevator · jammed · Nov 26, 2002 · N908AX · Doug DC931 · Elevator Control System
  > ELEVATOR JAMMED, WOULD NOT PULL BACK WHILE PERFORMING CONTROL CHECK. INSPECTED ELEVATOR TABS, CONTROL VALVES, FOLLOW UP MECHANISMS, LOAD FEEL AND CENTERING SPRING, VISIBLE PORTIONS OF CABLE RUNS IN TAIL COMPARTMENT AND E/E COMPARTMENT. NO DEFECTS FOUND. CONTRO
- [SDR ABXA020169](https://openairdocs.org/sdr/ABXA020169.md): Skin · corroded · Sep 4, 2002 · N908AX · Doug DC931 · Fuselage Structure (General)
  > DURING ROUTINE LINE OPERATIONS AT ILN, MAINTENANCE DISCOVERED CORROSION ON THE FUSELAGE SKIN, LOCATED AT THE LOWER CARGO DOOR JAMB, FORWARD LOWER CORNER. THE DAMAGE TO THE SKIN WAS TRIMMED OUT AND A NEW SECTION OF SKIN WAS SPLICED IN, IAW DC-9 SRM 53-04, FIG.
- [SDR ABXA020168](https://openairdocs.org/sdr/ABXA020168.md): Doubler · corroded · Sep 4, 2002 · N908AX · Doug DC931 · Fuselage Structure (General)
  > DURING ROUTINE LINE OPERATIONS AT ILN, MAINTENANCE DISCOVERED CORROSION ON THE FUSELAGE SKIN RESULTING IN THE DISCOVERY OF CORROSION ON THE INTERNAL DOUBLER P/N 5910158-24. THE DAMAGE TO THE INTERNAL DOUBLER WAS TRIMMED OUT AND A NEW SECTION SPLICED IN IAW DC-
- [SDR ABXA020152](https://openairdocs.org/sdr/ABXA020152.md): Latch · out of adjust · Aug 30, 2002 · N908AX · Doug DC931 · Landing Gear Position and Warning
  > RIGHT GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. UPLATCH CHECK FAILED (GEAR DOOR OPEN LIGHT CAME ON AND GEAR EXTENDED). WHEN THE GEAR HANDLE WAS PLACED IN UP POSITION, RIGHT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT WENT OUT. RIGHT GEAR RETRACTED
- [SDR ABXA020146](https://openairdocs.org/sdr/ABXA020146.md): Bracket · out of adjust · Aug 28, 2002 · N908AX · Doug DC931 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF WITH GEAR HANDLE UP, THE RIGHT GEAR RED UNSAFE LIGHT ILLUMINATED. RECYCLED THE GEAR WITH NO CHANGE. THE GEAR UPLATCH CHECK ALSO FAILED. ADJUSTED THE TENSION ON THE RIGHT MAIN GEAR DOOR ROLLER BRACKET AND SPRING ASSEMBLY IAW DC-9 MM 32-31-04-2-
- [SDR ABXA020155](https://openairdocs.org/sdr/ABXA020155.md): Doubler · cracked · Jul 8, 2002 · N908AX · Doug DC931 · Fuselage Structure (General)
  > CRACK IN FUSELAGE SKIN AT STATION 994, LONGERON 12 RIGHT, BETWEEN 2 RIVETS AND EXTENDING 1/4" PAST BOTH RIVETS. REPAIRED CRACK IAW DC-9 DWG SR09530151 AND E.A. 5311005-034.
- [SDR ABXA020160](https://openairdocs.org/sdr/ABXA020160.md): Cap · cracked · Jul 6, 2002 · N908AX · Doug DC931 · Fuselage Miscellaneous Structure
  > LONGERON END CAP CRACKED NR 11 RIGHT. INSTALLED NEW END CAP NR 11 RIGHT IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA020159](https://openairdocs.org/sdr/ABXA020159.md): Bulkhead · damaged · Jun 25, 2002 · N908AX · Doug DC931 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD SIDE SKIN SPLICED AT Z 14.00. SPLICE NOT IAW DOUGLAS AFT PRESSURE BULKHEAD RE-WORK. SPLICED NEW SECTION (LOWER) OF RIGHT AFT PRESSURE BULKHEAD WEB IAW REA D953-44534-MR AND DOUGLAS DWG J060088.
- [SDR ABXA020158](https://openairdocs.org/sdr/ABXA020158.md): Doubler · cracked · Jun 24, 2002 · N908AX · Doug DC931 · Wing Structure
  > ANGLED DOUBLER COMMON TO #7 SLAT TRACK RIB INBOARD AND FRONT SPAR CRACKED. REPAIRED AREA IAW DC-9 SRM 57-09.
- [SDR ABXA020157](https://openairdocs.org/sdr/ABXA020157.md): Rib · cracked · Jun 24, 2002 · N908AX · Doug DC931 · Wing, Rib/Bulkhead
  > NR 8 SLAT TRACK INBOARD LEADING EDGE RIB ANGLE COMMON TO ROLLERS CRACKED AT AFT LOWER VERTICAL LEG. REPLACED RIB IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA020156](https://openairdocs.org/sdr/ABXA020156.md): Doubler · cracked · Jun 21, 2002 · N908AX · Doug DC931 · Fuselage Structure (General)
  > 5" CRACK TOP OF FUSELAGE AT #1 LONGERON IN AFT PRESSURE BULKHEAD AREA. REPAIRED CRACK IAW DC-9 DWG SR0953151 AND E.A. 5311005-034.
- [SDR ABXA010783](https://openairdocs.org/sdr/ABXA010783.md): Power Supply · discharged · Mar 25, 2002 · N908AX · Doug DC931 · Emergency Lighting
  > DURING PREFLIGHT CHECK, FOUND THE EMERGENCY CABIN LIGHTS INOPERATIVE. REPLACED THE BATTERY POWER SUPPLY IAW DC-9 MM. OPS CHECKED GOOD.
- [SDR ABXA010566](https://openairdocs.org/sdr/ABXA010566.md): Battery · discharged · Oct 29, 2001 · N908AX · Doug DC931 · Emergency Lighting
  > AFT COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC-9 AMM 33-53-02-4-0001. OPS CHECKED GOOD.
- [SDR ABXA000495](https://openairdocs.org/sdr/ABXA000495.md): Beam · cracked · Nov 15, 2000 · N908AX · Doug DC931 · Passenger/Crew Doors
  > AFT VENTRAL DOOR BEAM WAS FOUND TO BE CRACKED. MAINTENANCE REPLACED VENTRAL DOOR BEAM IAW DC-9 MM.
- [SDR ABXA000510](https://openairdocs.org/sdr/ABXA000510.md): Gusset · cracked · Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Miscellaneous Structure
  > INTERCOSTAL GUSSET CRACKED AT FS 465. MAINTENANCE REPLACED THE GUSSET IAW DC-9 SRM.
- [SDR ABXA000509](https://openairdocs.org/sdr/ABXA000509.md): Splice · cracked · Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Miscellaneous Structure
  > AFT PRESSURE BULKHEAD TEE CAP SPLICE CRACKED. MAINTENANCE REPLACED THE SPLICE IAW DC-9 SRM 51-30-5.
- [SDR ABXA000508](https://openairdocs.org/sdr/ABXA000508.md): Frame · cracked · Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Main, Frame
  > FUSELAGE FRAME CRACKED AT FS 680. MAINTENANCE REPLACED FRAME IAW ABX REA 953-38971-MR.
- [SDR ABXA000507](https://openairdocs.org/sdr/ABXA000507.md): Web · cracked · Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Miscellaneous Structure
  > CUSP WEB CRACKED AT FS 218. MAINTENANCE REPLACED THE CUSP WEB IAW DC-9 SRM 51-30-1.
- [SDR ABXA000506](https://openairdocs.org/sdr/ABXA000506.md): Floorbeam · cracked · Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Main, Floor Beam
  > FLOORBEAM SUPPORT CRACKED AT FS 560. MAINTENANCE REPAIRED THE SUPPORT IAW DC-9 SRM DRAWING K05159.
- [SDR ABXA000505](https://openairdocs.org/sdr/ABXA000505.md): Floorbeam · cracked · Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Main, Floor Beam
  > FLOORBEAM SUPPORT CRACKED AT LOWER INBOARD FASTENER. MAINTENANCE REPAIRED IAW DC-9 SRM DRAWING K05159.
- [SDR ABXA000504](https://openairdocs.org/sdr/ABXA000504.md): Fitting · cracked · Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO DOOR BEAM NR 2 END FITTING CRACKED. MAINTENANCE REPLACED THE END FITTING IAW SRM 51-30-5.
- [SDR ABXA000503](https://openairdocs.org/sdr/ABXA000503.md): Fitting · cracked · Nov 15, 2000 · N908AX · Doug DC931 · Cargo/Baggage Doors
  > AFT LOWER CARGO DOOR NR 1 BEAM FITTING CRACKED. MAINTENANCE REPLACED THE NR 1 BEAM END FITTING IAW DC-9 SRM.
- [SDR ABXA000502](https://openairdocs.org/sdr/ABXA000502.md): Intercostal · corroded · Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT FS 579 - 598 HAD LEVEL ONE CORROSION. MAINTENANCE REPLACED THE INTERCOSTAL IAW DC-9 SRM 51-30-2.
- [SDR ABXA000501](https://openairdocs.org/sdr/ABXA000501.md): Doubler · cracked · Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Miscellaneous Structure
  > AFT PRESSURE BULKHEAD DOOR FRAME HAS A CRACKED DOUBLER. REPAIRED DOUBLER IAW ABX REA D953-38986.
- [SDR ABXA000500](https://openairdocs.org/sdr/ABXA000500.md): Stiffener · cracked · Nov 15, 2000 · N908AX · Doug DC931 · Cargo/Baggage Doors
  > AFT LOWER CARGO DOOR FORWARD STIFFENER CRACKED. MAINTENANCE REPLACED THE STIFFENER IAW DRAWING 5913304-11.
- [SDR ABXA000499](https://openairdocs.org/sdr/ABXA000499.md): Intercostal · cracked · Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Miscellaneous Structure
  > UPPER CARGO FLOOR INTERCOSTAL CRACKED. MAINTENANCE REPLACED THE INTERCOSTAL END CLIPS IAW DC-9 MM.
- [SDR ABXA000498](https://openairdocs.org/sdr/ABXA000498.md): Tee Chord · cracked · Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD NR 2 TEE CRACKED. MAINTENANCE REPLACED THE TEE IAW ABX EA 53120033-006.
- [SDR ABXA000497](https://openairdocs.org/sdr/ABXA000497.md): Panel · delaminated · Nov 15, 2000 · N908AX · Doug DC931 · Wing, Plate/Skin
  > LEFT WING TRAILING EDGE PANEL DELAMINATED. MAINTENANCE REPLACED PANEL IAW DC-9 MM.

Next page: https://openairdocs.org/deregistered/N908AX-2016-03-31/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 = 'N908AX' AND deregistration_id = 'N908AX-2016-03-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N908AX-2016-03-31/reports

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