# Service difficulty reports: N108AX, cancelled Aug 3, 2011

A list on [N108AX, cancelled Aug 3, 2011](https://openairdocs.org/deregistered/N108AX-2011-08-03.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR CNMA20100003](https://openairdocs.org/sdr/CNMA20100003.md): Access Door · leaking · Jan 28, 2010 · N108AX · Doug DC1030 · Electrical/Electronic Compartment Doors
  > AT 370 FL COULD NOT CONTROL CABIN CLIMB IN AUTO, STANBY, OR MANUAL CLIMBING AT 1000 FT IAW MIN HAD TO DESCENT TO MAINTAIN 9500 FT CABIN AT FL 290. FOUND FWD AVIONICS DOOR LEAKING, RESET DOOR & PRESSURIZED ACFT TO 5 PSID & INSPECTED ALL DOORS ACFT OK FOR CONTI
- [SDR CNMA20090015](https://openairdocs.org/sdr/CNMA20090015.md): Fuel Tank · leaking · Jul 13, 2009 · N108AX · Doug DC1030 · Fuel Storage
  > RT WING LEAKING FUEL IN FLIGHT.
- [SDR CNMA20090055](https://openairdocs.org/sdr/CNMA20090055.md): Seat Track · corroded · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > LIGHT CORROSION ON SEAT TRACK (N6) LT UNDER THRESHOLD PAX DOOR 4 LT REMOVE THRESHOLD PLATE AND DRAIN VALVES ON DOOR NR 4 LT OK DONE AS AMM 53-10-01, REV 81. REMOVE CORROSION IAW SRM 51-21-01, VOL II, REV 93 PERFORMED AS REQUIRED MAX DEPTH 2.5 MM OUT OF SRM LI
- [SDR CNMA20090054](https://openairdocs.org/sdr/CNMA20090054.md): Skin · dented · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN STA 729 - LONGERON 43. PERFORM REPAIR IAW SRM 53-20-00 FIG SH3, REV 45, VOL I, OK PERFORM REPAIR AS REQUIRED.
- [SDR CNMA20090053](https://openairdocs.org/sdr/CNMA20090053.md): Floorbeam · corroded · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR SUPPORT AT STA 815 X19. FABRICATED AND INSTALLED NEW PN ADA7326-1 IAW DWG ADA7326 AND 7548 AND SRM 51-35-01, STEP 1, VOL II, REV 94.
- [SDR CNMA20090052](https://openairdocs.org/sdr/CNMA20090052.md): Floorbeam · corroded · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Floor Beam
  > LIGHT CORROSION ON FLOORBEAM AT STA 859 X-72. REMOVED CORROSION IAW SRM 51-21-01, ERV 94, VOL II OUT OF LIMITS. REPLACED PN ADD 7160-2 IAW SRM 51-35-01, VOL II, REV 94, STEP 1 (REF DWG ADD 7163).
- [SDR CNMA20090051](https://openairdocs.org/sdr/CNMA20090051.md): Floorbeam · corroded · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR SUPPORT TEE AT AFTER PRESSURE BULKHEAD, STA 2007. X-40 - X-60, AND X 20. PERFORMED REPAIR IAW SRM 53-40-00, FIG 16, REF 94, VOL I.
- [SDR CNMA20090050](https://openairdocs.org/sdr/CNMA20090050.md): Support · cracked · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Miscellaneous Structure
  > GALLEY SUPPORT CORRODED AT STA 459 XX24. REPLACED PN ACA7366-501 IAW DWG ACA7365 AND SRM51-35-01, VOL II, REV 94.
- [SDR CNMA20090049](https://openairdocs.org/sdr/CNMA20090049.md): Fitting · corroded · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Attach Fittings
  > CORROSION ON FITTING GALLEY AT STA 879, X44. REMOVED CORROSION IAW SRM 51-21-24 VOL II, REV 94 WITHOUT LIMITS DEPTH MATERIAL REMOVED 3.5 MM. FABRICATED PN AWD7743-503, REF DWG AWD 7743 AND INSTALL NEW PN IAW SRM 51-31-03, VOL II, REV 94, PAGES 1 THRU 66 AS
- [SDR CNMA20090048](https://openairdocs.org/sdr/CNMA20090048.md): Floorbeam · corroded · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Floor Beam
  > LIGHT CORROSION ON FLOOR SUPPORT AT STA 815 X-18. FABRICATED AND INSTALLED NEW PN ADA7326-1 IAW DWG 7696 AND ADA7548 AND SRM 51-35-01 STEP 1, VOL II REV 94.
- [SDR CNMA20090047](https://openairdocs.org/sdr/CNMA20090047.md): Floor Support · corroded · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT AT STA 859 - 893 X73. REPLACED PN ADA7160-1 IAW DWG ADA7160 AND DWG 7163 AND MM 20-50-02 REV 81.
- [SDR CNMA20090046](https://openairdocs.org/sdr/CNMA20090046.md): Floor Support · corroded · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Miscellaneous Structure
  > LIGHT CORROSION ON FLOORBEAM SUPPORT BETWEEN STA 1820-1887 X36. REMOVED BEAM IAW SRM 51-31-01 VOL II REV 94. FABRICATED PN AGA7085-1 ED INSTALLED IAW DWG ASA 7127 AND MM 20-50-02 REV 81.
- [SDR CNMA20090045](https://openairdocs.org/sdr/CNMA20090045.md): Track · corroded · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Structure (General)
  > FOUND CORROSION ON DOWN TRACK AT STA 1871-2007 AND X=107.25. REMOVED CORROSION IAW SRM 51-21-01 V II REV 94 DIMENSIONS OUT OF LIMITS (120 X 50 X 2,3 MM). REPLACED PN NRA6222-9 IAW DWG NFA6222. INSTALLED PN AFA7789-535 IAW SRM 51-35-01 AND 51-33-01 V II INSTE
- [SDR CNMA20090044](https://openairdocs.org/sdr/CNMA20090044.md): Track · corroded · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Structure (General)
  > FOUND CORROSION ON DOWN TRACK AT STA 1902 - 2007 AND X=75.25. CORROSION REMOVED IAW SRM 51-21-01 V G REV 94 DIMENTIONS ARE OUT OF LIMITS (240 X 8T X 2,4 MM) FABRICATED AND INSTALLED TRACK PN AGA7086-506 IAW DWG AGA7086 AND DWG ASA 7127 AND MM 205002 REV 81.
- [SDR CNMA20090043](https://openairdocs.org/sdr/CNMA20090043.md): Track · corroded · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Structure (General)
  > FOUND CORROSION ON DOWN TRACK AT STA 1887-2007 AND X=27.50. REMOVED BEAM IAW SRM 51-31-01, VOL II, REV 94 AND MM 20-50-02 REV 81. FABRICATED PN ASA7087-1 IAW DWG ASA7087 AND INSTALLED IAW DWG AGA7127 AND MM 20-50-02 REV 81.
- [SDR CNMA20090041](https://openairdocs.org/sdr/CNMA20090041.md): Skin · cracked · Aug 8, 2008 · N108AX · Doug DC1030 · Horizontal Stabilizer, Plate/Skin
  > HFEC INSP ON HS IAW J/C 10AD-904 SB 455-18. FOUND ONE CRACK INDICATION 37MM LENGTH ON OUTER SECTION UPPER AFTER SKIN PANEL RT SIDE. PERFORMED STOP DRILL AS REQUIED IAW SB A55-18 STEP 11C PAG 7 REV 6. FOR REPLACEMENT SEE ODL PGO-067.
- [SDR CNMA20090042](https://openairdocs.org/sdr/CNMA20090042.md): Cargo Track · corroded · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON DOWN TRACK AT STA 1931.500 -2007 AND X=8.50. REMOVED BEAM IAW SRM 51-31-01 VOL I REV 94 AND MM 20-50-02 REV 81. FABRICATED PN AGA7088-1 IAW DWG ASA7088 AND INSTALLED IAW DWG ASA7127 AND SRM 51-35-01 VOL II REV 94 AND MM 20-50-02 REV 81.
- [SDR CNMA20090041A](https://openairdocs.org/sdr/CNMA20090041A.md): Door Frame · cracked · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Structure
  > FWD CARGO NEAR DOOR JAMB PANEL NR 127AR CRACKED. REMOVED PANEL 127AR AMM 20-50-02 REV 81. WELD PER DPS 10225 INSTALLED PANEL 127AR IAW MM 20-50-02 REV 81.
- [SDR CNMA20090040](https://openairdocs.org/sdr/CNMA20090040.md): Stiffener · corroded · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Bulkhead
  > CTR WHEEL WELL AFT CLOSING BULKHEADS WITH A STIFFENER CORRODED. REPLACED PN AYB7080-9, REF DWG BOE AYB 7080 IAW SRM 51-35-01, REV 94, VOL I, STEP 9.
- [SDR CNMA20090039](https://openairdocs.org/sdr/CNMA20090039.md): Support · corroded · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Miscellaneous Structure
  > NR 2 GALLEY SUPPORT CORRODED AT STA 465 RT AND LT SIDE. REMOVED CORROSION IAW SRM 51-21-01, VOL II, REV 94 WITHOUT LIMITS DEPTH MATERIAL REMOVED 4 MM. FABRICATED PN AWD7743-503 REF DWG AWD7743 AND INSTALLED NEW PN IAW SRM 51-33-01 VOL II REV 94 (PAGES 1 - 66
- [SDR CNMA20090038](https://openairdocs.org/sdr/CNMA20090038.md): Support · corroded · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Miscellaneous Structure
  > NR 2 GALLEY SUPPORT CORRODED AT STA 435, RT AND LT SIDE. REMOVED CORROSION IAW SRM 51-21-01, VOL II, REV 94 WITHOUT LIMITS DEPTH MATERIAL REMOVED 3 MM. FABRICATED PN AWD7743-503 REF DWG AWD7743 AND INSTALLED NEW PN IAW SRM 51-33-01, VOL II, REV 94 (PAGE 1 T
- [SDR CNMA20090037](https://openairdocs.org/sdr/CNMA20090037.md): Floor Support · corroded · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT BETWEEN STA 440 / 453, XO. FABRICATED AND INSTALLED NEW PN ACA7374-1 IAW DWG ACA7374 AND 7365 AND SRM 51-35-01 V I REV 94 STEP 1.
- [SDR CNMA20090036](https://openairdocs.org/sdr/CNMA20090036.md): Support · cracked · Aug 8, 2008 · N108AX · Doug DC1030 · Cargo/Baggage Doors
  > CTR CARGO DOOR EXTERNAL FAIRING SUPPORT CRACKED (AFT POSITION). PERFORM REPAIR IAW SRM 53-00-01, FIG 8, SHEET 2, REV 94.
- [SDR CNMA20090035](https://openairdocs.org/sdr/CNMA20090035.md): Floorbeam · cracked · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Floor Beam
  > CTR CARGO COMPT, FLOOR STRUCTURE, AT STA 1523 (FWD BULKHEAD) NR 4 ANGULARS CRACKED. OPEN PANELS 183JE-183FE FWD BULKHEAD CTR CARGO COMPARTMENT IAW AMM 20-50-02 REV 81. PERFORM REPAIR IAW SRM 53-00-01, FIG 8, SHI REV 93 VOL I OK DONE. CLOSE PANELS 183JE, 189
- [SDR CNMA20090034](https://openairdocs.org/sdr/CNMA20090034.md): Floor Support · cracked · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT FLOOR SUPPORT STRUCTURE AT STA 1921 LT SIDE ANGULAR CRACKED. PERFORMED REPAIR IAW SRM 53-00-01, FIG 8, SHT 1, REV 94 (VOL I).
- [SDR CNMA20090033](https://openairdocs.org/sdr/CNMA20090033.md): Panel · damaged · Aug 8, 2008 · N108AX · Doug DC1030 · Nacelle/Pylon, Plate/Skin
  > PYLON NR 2 PANEL, 457BT DAMAGED. REPAIRED IAW SRM 54-00-01, FIG 1A SHEET 1 REV 94 VOL J.
- [SDR CNMA20090032](https://openairdocs.org/sdr/CNMA20090032.md): Beam · cracked · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Structure
  > CTR CARGO COMP STA 1781 NR 3 LT BEAM OF ZONE PLENUM CRACKED. REMOVED BEAM IAW MM 20-50-02 REV 81. PERFORMED DRILL NEW BEAM IAW DWG AF)7011-3. REPLACED BEAM IAW AMM 20-50-02 REV 81 AND INSTALLED ALL OMNI DIRECTIONAL ROLLERS.
- [SDR CNMA20090031](https://openairdocs.org/sdr/CNMA20090031.md): Floorbeam · cracked · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Floor Beam
  > CTR CARGO COMP FLOOR UNLOAD BEAM CRACKED AT STA 1690 (UPPER FLANGE) PERFORMED REPAIR IAW SRM 53-70-00 FIG 3 REV 93 VOL J. PERFORMED PAINTING IAW SRM 51-21-02 VOL II REV 94.
- [SDR CNMA20090030](https://openairdocs.org/sdr/CNMA20090030.md): Structure · cracked · Aug 8, 2008 · N108AX · Doug DC1030 · Trailing Edge Flaps
  > RT OTBD FLAP INBD RIB CLOSURE HAS AN ANGULAR CRACK. REMOVED RT OTBD FLAP, INBD T/E SECTION. REMOVED ALL SCREWS SIZED IAW SRM 51-31-01 VOL 2 REV 93. REMOVED RT OTBD FLAP INBD SECTION T/E IAS MM 20-50-02 REV 81. FABRICATED PN ARC1951-6 IAW DWG ARC1951 AND INS
- [SDR CNMA20090029](https://openairdocs.org/sdr/CNMA20090029.md): Panel · cracked · Aug 8, 2008 · N108AX · Doug DC1030 · Trailing Edge Flaps
  > LT OTBD FLAP, OTBD HINGE PANEL 526JL, CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 10.
- [SDR CNMA20090025](https://openairdocs.org/sdr/CNMA20090025.md): Panel · cracked · Aug 8, 2008 · N108AX · Doug DC1030 · Trailing Edge Flaps
  > LT WING OTBD FLAP INBD HINGE PANEL 535DL CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 4, SH1, VOL I, REV 94.
- [SDR CNMA20090028](https://openairdocs.org/sdr/CNMA20090028.md): Support · cracked · Aug 8, 2008 · N108AX · Doug DC1030 · Wing Miscellaneous Structure
  > LT OTBD FLAP, INBD HINGE STRUCTURE UNDER PANEL 535JL, SUPPORT CRACKED. REPLACED SUPPORTS CRACKED UNDER PANEL 535JL IAW SRM 51-35-01 VOL II REV 93.
- [SDR CNMA20090027](https://openairdocs.org/sdr/CNMA20090027.md): Panel · cracked · Aug 8, 2008 · N108AX · Doug DC1030 · Trailing Edge Flaps
  > LT OTBD FLAP, INBD HINGE PANEL 535JL CRACKED. REMOVED EXISTING REPAIR IAW SRM 51-31-01 VII PERFORMED WELD IAW DPS10225. REINSTALLED OLD REPAIR IAW SRM 51-35-02 VII 4REV 94.
- [SDR CNMA20090026](https://openairdocs.org/sdr/CNMA20090026.md): Panel · delaminated · Aug 8, 2008 · N108AX · Doug DC1030 · Trailing Edge Flaps
  > LT INBD FLAP, OTBD HINGE, PANEL 541JL UNGLUED. PERFORMED REPAIR IAW DWG ARC 2541.
- [SDR CNMA20090024](https://openairdocs.org/sdr/CNMA20090024.md): Panel · cracked · Aug 8, 2008 · N108AX · Doug DC1030 · Trailing Edge Flaps
  > LT WING OTBD FLAP INBD HINGE PANEL 535DL CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 4, SH1, VOL I, REV 94.
- [SDR CNMA20090023](https://openairdocs.org/sdr/CNMA20090023.md): Structure · dented · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Miscellaneous Structure
  > DENT AT STA 1853.93 LONG 47 REPAIR NEXT C CHK. PERFORMED SANDING AS REQUESTED AS DPS 9.316. PERFORMED REPAIR IAW SRM 53-20-00, FIG 6 (SHT 3) V.I. REV 93. PERFORMED PAINTING OF REPAIRED AREA IAW SRM 51-21-02 VOL 2 REV 94.
- [SDR CNMA20090022](https://openairdocs.org/sdr/CNMA20090022.md): Skin · dented · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Plate/Skin
  > DENT 30 INCH, FWD OF R1 DOOR SILL - DENT 6 INCH LONG WITHIN LIMITS IAW SRM VOL I-53-20-00 PERFORM PERMANENT REPAIR. REMOVED DUCT IAW 20-50-02 AND MANIFOLD AIR CONDITIONING IAW 21-10-00. PERFORM CUTOUT SKIN DAMAGE IAW SRM 53-20-00 FIG 6, REV 93, VOL I. MADE
- [SDR CNMA20090021](https://openairdocs.org/sdr/CNMA20090021.md): Skin · dented · Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Plate/Skin
  > UNDER RT PITOT TUBE HAS FUSELAGE DENT PERFORM PERMANENT REPAIR. REMOVED ELECTRICAL EQUIPMENT TO ACCESS ZONE. REMOVE BRACKET AS AMM 77-13-01 (TRANSDUCER NOT INSTALLED). REMOVED DUCT AS MM 21-26-00 REV 81. PERFORM STRIPPING AS REQUESTED IAW DPS 9.316. PERF

## 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 = 'N108AX' AND deregistration_id = 'N108AX-2011-08-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N108AX-2011-08-03/reports

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