# Service difficulty reports: N826AX, cancelled Nov 21, 2007

A list on [N826AX, cancelled Nov 21, 2007](https://openairdocs.org/deregistered/N826AX-2007-11-21.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 5 · 217 reports

- [SDR ABXA070149](https://openairdocs.org/sdr/ABXA070149.md): Transmitter · defective · Apr 30, 2007 · N826AX · Doug DC863F · Engine Oil Pressure
  > DURING CRUISE NR 2 ENGINE OIL PRESSURE WENT TO OFF SCALE LOW MOMENTARILY AND RECOVERED. FIFTEEN MINUTES LATER, AGAIN OFF SCALE LOW AND STAYED. SECURED NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE PRESSURE TRANSMITTER IAW DC8 MM 70-32-01-2. RAN ENGINE, NO
- [SDR ABXA070107](https://openairdocs.org/sdr/ABXA070107.md): Transmitter · defective · Apr 17, 2007 · N826AX · Doug DC863F · Engine Oil Pressure
  > AT TOP OF CLIMB, NR 1 ENGINE OIL PRESSURE STARTED DROPPING OFF INTO CAUTIONARY RANGE. RAN ABNORMAL CHECK LIST, REDUCED POWER TO IDLE. OIL PRESSURE DROPPED BELOW RED LINE, SECURED ENGINE AND RETURNED FOR LANDING. REPLACED NR 1 ENGINE OIL PRESSURE TRANSMITTER
- [SDR ABXA070016](https://openairdocs.org/sdr/ABXA070016.md): Bolt · broken · Dec 23, 2006 · N826AX · Doug DC863F · Main Landing Gear Strut/Axle/Truck
  > LEFT MAIN LANDING GEAR STRUT LEAKED. FOUND TORSION LINK APEX BOLT DAMAGED/BROKE ON LEFT MAIN LANDING GEAR. REPLACED TORSION LINK APEX BOLT ON LEFT MAIN LANDING GEAR REPACK ON (AVBORNE) NR WX-314, IAW DC8 MM. REPLACED LEFT MAIN LANDING GEAR DOOR RETRACT ACTU
- [SDR ABXA060311](https://openairdocs.org/sdr/ABXA060311.md): Engine · leaking · Dec 4, 2006 · N826AX · Doug DC863F · Turbine Engine Oil System
  > NR 3 ENGINE SHUT DOWN IN FLIGHT (STA SDF) DUE TO LOSS OF OIL. FERRIED AIRCRAFT BACK TO ILN. REMOVED AND REPLACED NR 3 ENGINE PER JOB CARD 8090507 IN WORK PACK 600261630.
- [SDR ABXA060201](https://openairdocs.org/sdr/ABXA060201.md): Ctc · defective · Jul 12, 2006 · N826AX · Doug DC863F · Cabin Compressor System
  > NR 2 CTC SMOKED AND MADE LOUD NOISE, STA. MIA. REMOVED AND REPLACED NR 2 CTC IAW DC8 MM 21-10-01-4. OPS CHECKED GOOD.
- [SDR ABXA060159](https://openairdocs.org/sdr/ABXA060159.md): Pump · leaking · Apr 11, 2006 · N826AX · Doug DC863F · Hydraulic Pump, Auxiliary
  > LOSS OF HYDRAULIC QUANTITY NOTED DURING DESCENT. FOUND STANDBY RUDDER PUMP OVERBOARD DRAIN LEAKING. REMOVED AND REPLACED STANDBY RUDDER PUMP IAW D8C MM 27-24-02. ALSO, CHECKED BYPASS LINE CHECK VALVE OPERATION. OPERATED NORMALLY. REINSTALLED CHECK VALVE.
- [SDR ABXA060031](https://openairdocs.org/sdr/ABXA060031.md): Fitting · cracked · Dec 30, 2005 · N826AX · Doug DC863F · Fuselage Main, Attach Fittings
  > INTERCOSTAL CORNER FITTING CRACKED FUSELAGE STA 50, RIGHT BUTT LINE 50, FORWARD OF FLOORBEAM. REMOVED CRACKED CORNER FITTING IAW DC8 SRM 51-1-20D. FABRICATED NEW CORNER FITTING IAW REA D853-52924 AND INSTALLED AT STA 50, RIGHT BUTT LINE 50, FORWARD OF FLOORB
- [SDR ABXA060033](https://openairdocs.org/sdr/ABXA060033.md): Doubler · corroded · Dec 29, 2005 · N826AX · Doug DC863F · Fuselage Main, Plate/Skin
  > CORROSION ON BELLY SKIN DOUBLER IN 4 AREAS BETWEEN STA 781 AND STA 798, LEFT BUTT LINE 4 TO LEFT BUTT LINE 10. REMOVED CORROSION ON BELLY SKIN DOUBLER IAW DC8 SRM 51-1-8. THREE AREAS WITHIN LIMITS IAW DC8 SRM 53-02. REMAINING AREA OUT OF LIMITS. ACCOMPLISH
- [SDR ABXA060030](https://openairdocs.org/sdr/ABXA060030.md): Frame · corroded · Dec 22, 2005 · N826AX · Doug DC863F · Fuselage Main, Frame
  > MAIN CARGO STA 1734 BUTT LINE 0, LONGERON 35 LEFT - 35 RIGHT, SURFACE CORROSION ON FRAME. REMOVED CORROSION FROM FRAME. DAMAGE WAS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 53-2-0 FIG 2, SHT 2.
- [SDR ABXA060029](https://openairdocs.org/sdr/ABXA060029.md): Support Bracket · corroded · Dec 15, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT, TORQUE BOX FORWARD SIDE AT STA 1160, BETWEEN LONGERON 31 RIGHT & 32 RIGHT, ANGLE AND WEB HAD CORROSION. REMOVED CORROSION, TREATED AND PRIMED. FABRICATED NEW SUPPORT BRACKET, FOUND TO BE OUT OF LIMITS. WORK ACCOMPLISHED IAW REA D853-5
- [SDR ABXA060032](https://openairdocs.org/sdr/ABXA060032.md): Floorbeam · corroded · Dec 14, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor Beam
  > UPPER HORIZONTAL CAP OF FLOORBEAM CORRODED AT STA 920, LEFT BUTT LINE 10. REMOVED CORROSION. DAMAGE OUT OF LIMITS. FLOORBEAM REPAIRED IAW REA D853-52567.
- [SDR ABXA060037](https://openairdocs.org/sdr/ABXA060037.md): Intercostal · corroded · Dec 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > UPPER CARGO, STA 30, LEFT BUTT LINE 48, INTERCOSTAL HAD CORROSION JUST AFT OF MAIN CARGO DOOR CONTROL BOX. REMOVED CORROSION ON INTERCOSTAL BEAM AT STA 30, LEFT BUTT LINE 48, AND DETERMINED AREA WAS OUT OF LIMITS. FABRICATED DOUBLER, TREATED, PRIMED AND INST
- [SDR ABXA060021](https://openairdocs.org/sdr/ABXA060021.md): Frame · corroded · Dec 2, 2005 · N826AX · Doug DC863F · Fuselage Main, Frame
  > STA. 1100, LONGERON 18 RT, FRAME CORRODED. REPAIRED FRAME AT STA. 1100, LONGERON 18 RT IAW SRM 53-2-0, FIGURE 2.
- [SDR ABXA060035](https://openairdocs.org/sdr/ABXA060035.md): Floorbeam · corroded · Nov 29, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor Beam
  > MAIN CABIN, STA 880, RIGHT BUTT LINE 63, FLOORBEAM LOWER CHORD, FORWARD SIDE CORRODED. REPAIRED FLOORBEAM STA 880, RIGHT BUTT LINE 63 IAW REA D853-52566MR.
- [SDR ABXA050354](https://openairdocs.org/sdr/ABXA050354.md): Stiffener · corroded · Nov 27, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING REMOVAL OF LEFT LONGERON, STIFFENER AT STA 940, LONGERON 24 LEFT, LEFT WHEEL WELL, WAS FOUND CRACKED ON BOTTOM OF BASE. FABRICATED NEW STIFFENER FOR STA 940, LONGERON 24 LEFT IAW REA D853-52556, PO NR 1123110.
- [SDR ABXA050367](https://openairdocs.org/sdr/ABXA050367.md): Access Panel · leaking · Nov 16, 2005 · N826AX · Doug DC863F · Wing, Plate/Skin
  > 12 BLIND RIVETS LEAKING UPON PRESSURE CHECKS. RIGHT WING, STRINGER NR 7 NEAR ACCESS PANEL 505F. REMOVED 12 BLIND FASTENERS ON STRINGER NR 7 NEAR ACCESS PANEL 505F OF THE RIGHT WING AND WET INSTALLED NEW FASTENERS IAW DC8 SRM 51-1-21 USING 1422 B1/2 SEALANT.
- [SDR ABXA050368](https://openairdocs.org/sdr/ABXA050368.md): Access Panel · leaking · Nov 16, 2005 · N826AX · Doug DC863F · Wing, Plate/Skin
  > 16 BLIND RIVETS LEAKING UPON PRESSURE CHECKS. RIGHT WING, STRINGER NR 5 NEAR ACCESS PANEL 505F. REMOVED 16 BLIND FASTENERS ON STRINGER NR 5 NEAR ACCESS PANEL 505F OF THE RIGHT WING AND WET INSTALLED NEW FASTENERS IAW DC8 SRM 51-1-21 USING 1422 B1/2 SEALANT.
- [SDR ABXA050308](https://openairdocs.org/sdr/ABXA050308.md): Floorbeam · corroded · Nov 11, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor Beam
  > MAIN CABIN, STA 798, BUTT LINE 0 - RT BUTT LINE 48, FLOORBEAM CORRODED. REMOVED NUT PLATES, CLEANED CORROSION ON FLOORBEAM AT STA 798, BUTT LINE 0 - RT BUTT LINE 48, BLENDED AREA, OUT OF LIMITS AT.088 INCH MATERIAL REMAINING FROM ORIGINAL THICKNESS OF.186 I
- [SDR ABXA060036](https://openairdocs.org/sdr/ABXA060036.md): Floor Support · cracked · Nov 9, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT HAT CHANNEL AT APPROXIMATELY LEFT BUTT LINE 34 BETWEEN STA 25 AND STA 35 WAS CRACKED AND HOLES DAMAGED. REMOVED DAMAGED HAT CHANNEL AND SHIM FROM STA 25 - 35, LEFT BUTT LINE 34. DAMAGE BEYOND REPAIRABLE LIMITS. FABRICATED NEW HAT CHANNEL AND S
- [SDR ABXA050307](https://openairdocs.org/sdr/ABXA050307.md): Web · corroded · Nov 9, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > CENTERLINE WEB AT STA 800 - 857, BUTT LINE O CORRODED. FABRICATED WEB AT STA 800 - 857, BUTT LINE 0 IAW REA D853-52543. MATERIAL USED.080 7075-T6, P/O NR 1113384.
- [SDR ABXA050309](https://openairdocs.org/sdr/ABXA050309.md): Tripler · corroded · Nov 8, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > EXISTING TRIPLER CORRODED AT STA 857, RT BUTT LINE 50. FABRICATED TRIPLER AT STA 857, RT BUTT LINE 50 IAW REA D853-52539. MATERIAL USED.190 7075-T6, P/O NR 1073367.
- [SDR ABXA050306](https://openairdocs.org/sdr/ABXA050306.md): Angle · corroded · Nov 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > LOWER CHORD AT STA 857, RT BUTT LINE 23 CORRODED. FABRICATED CHORD AT STA 857, RT BUTT LINE 23 IAW REA D853-52537. MATERIAL USED P/N: AND-10134-1407, P/O NR1122772.
- [SDR ABXA050301](https://openairdocs.org/sdr/ABXA050301.md): Web · corroded · Nov 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > WEB CORRODED AT STA 857, LT BUTT LINE 46. FABRICATED WEB AT STA 857, LT BUTT LINE 46 USING.063 7075-T6, PO NR 1118787 IAW REA D853-52535.
- [SDR ABXA050304](https://openairdocs.org/sdr/ABXA050304.md): Attach Angle · corroded · Nov 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > RT PRESSURE PANEL AT STA 857, RT BUTT LINE 40 ATTACH ANGLE CORRODED. FABRICATED ATTACH ANGLE RT PRESSURE PANEL AT STA 857, P/N: 5644678 IAW REA D853-52534.
- [SDR ABXA050303](https://openairdocs.org/sdr/ABXA050303.md): Web · corroded · Nov 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > WEB CORRODED AT STA 857, RT BUTT LINE 46. FABRICATED WEB AT STA 857, RT BUTT LINE 46 USING.071 7075-T6, P/O NR 1084025 IAW REA D853-52538.
- [SDR ABXA050302](https://openairdocs.org/sdr/ABXA050302.md): Splice · corroded · Nov 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > SHIM SPLICE CORRODED AT STA 857, LEFT BUTT LINE 20. FABRICATED SHIM AT STA 857, LEFT BUTT LINE 20 IAW DC8 REA D853-52536. MATERIAL USED.090 P/O NR 1112038.
- [SDR ABXA050305](https://openairdocs.org/sdr/ABXA050305.md): Web · corroded · Nov 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > PSI WEB FROM STA 847, LEFT BUTT LINE 40 - 60 CORRODED. FABRICATED PSI WEB FROM STA 847, LEFT BUTT LINE 40 - 60 IAW DC8 REA D853-52534. MATERIAL USED.063 2024-T3, P/O NR 1118786.
- [SDR ABXA050300](https://openairdocs.org/sdr/ABXA050300.md): Doubler · corroded · Nov 4, 2005 · N826AX · Doug DC863F · Fuselage Main, Longeron/Stringer
  > CORROSION ON TOP OF LONGERON REINFORCEMENT DOUBLER IN AFT CARGO BILGE AT STA 1180, LONGERON 36 TO 34 RIGHT. REMOVED DOUBLER AT STA 1200 LONGERON 34 RIGHT TO 36. REMOVED CORROSION FROM DOUBLER. FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, PRIMED AND INST
- [SDR ABXA050346](https://openairdocs.org/sdr/ABXA050346.md): Floorbeam · corroded · Nov 2, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor Beam
  > FOUND MAIN CABIN FLOORBEAM AT STA 120, RIGHT BUTT LINE 51, FORWARD SIDE OF T CAP, CORRODED. REMOVED DAMAGED AREA AND REPLACED WITH ANGLE DOUBLER REPAIR ON FLOORBEAM STA 120, RIGHT BUTT LINE 51 IAW DC8 SRM 51-1-8, 53-2-0, 51-3-0, 53-7-3, 53-0, 51-2-0, 51-1-8,
- [SDR ABXA050294](https://openairdocs.org/sdr/ABXA050294.md): Finger Doubler · damaged · Nov 2, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > INSIDE CENTER TANK, STA 857, LT BUTT LINE 20, AFT FINGER TAB OF DOUBLER BROKEN OFF. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW REA D853-52530.
- [SDR ABXA060028](https://openairdocs.org/sdr/ABXA060028.md): Floorbeam · corroded · Nov 1, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor Beam
  > MAIN CARGO, STA 55, LEFT BUTT LINE 20, CORROSION ON UPPER FLANGE FLOORBEAM. REMOVED 3.5 X.75 INCH SECTION OF UPPER FLANGE FLOORBEAM. ACCOMPLISHED FLOORBEAM REPAIR IAW SSRM DWG K04881.
- [SDR ABXA060019](https://openairdocs.org/sdr/ABXA060019.md): Floorbeam · corroded · Nov 1, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor Beam
  > MAIN CARGO, STA. 55, LBL 20, CORROSION ON UNDERSIDE OF FLOORBEAM CORNER. REMOVED A 3.5 INCH X.7500 INCH SECTION OF UPPER FLANGE FLOORBEAM AT STA. 55, LBL 20 IAW SRM DWG K04881. FABRICATED REPAIR ANGLE, SHIM AND FILLER IAW SRM DWG K04881.
- [SDR ABXA050313](https://openairdocs.org/sdr/ABXA050313.md): Doubler · corroded · Nov 1, 2005 · N826AX · Doug DC863F · Fuselage Main, Plate/Skin
  > DOUBLER CORRODED TOP OF WING CENTER SECTION PRESSURE DECK, STA 683, LONGERON 22 LEFT, LEFT BUTT LINE 10. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-8 AND REA D853-52529.
- [SDR ABXA050299](https://openairdocs.org/sdr/ABXA050299.md): Doubler · corroded · Nov 1, 2005 · N826AX · Doug DC863F · Wing, Center Box
  > DOUBLER CORRODED TOP OF WING CENTER SECTION PRESSURE DECK, STA. 683, RT BUTT LINE 10. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-8 AND REA D853-52529.
- [SDR ABXA050342](https://openairdocs.org/sdr/ABXA050342.md): Skin · misdrilled · Oct 31, 2005 · N826AX · Doug DC863F · Fuselage Main, Plate/Skin
  > FOUND UPPER CARGO STA 857, LEFT BUTT LINE 60 - RIGHT BUTT LINE 60, 5 FASTENERS MIS-DRILLED IN TOP OF CENTER TANK TO SPAR SKIN. REAMED HOLES TO REMOVE DAMAGE, FABRICATED REPAIR BUSHINGS FOR 11 HOLES. INSTALLED REPAIR BUSHINGS WITH WET SEALANT IN HOLES. CONTO
- [SDR ABXA050343](https://openairdocs.org/sdr/ABXA050343.md): Skin · misdrilled · Oct 31, 2005 · N826AX · Doug DC863F · Fuselage Main, Plate/Skin
  > FOUND UPPER CARGO STA 834, BUTT LINE 0, 4 FASTENERS MIS-DRILLED IN TOP OF CENTER WING SKIN ON TANK. MIS-DRILLED HOLES CLEANED UP, HOLES OPENED UP TO 0.312" AND 0.308", FASTENERS INSTALLED IAW DC8 SRM 51-1-20 ON SPLICE DOUBLER INSTALLATION.
- [SDR ABXA050358](https://openairdocs.org/sdr/ABXA050358.md): Pressure Panel · corroded · Oct 30, 2005 · N826AX · Doug DC863F · Fuselage Main, Bulkhead
  > CORROSION FOUND UNDER THREE FASTENERS ON PRESSURE WEB IN RT WHEEL WELL, STA. 857, RT BUTT LINE 27. CORROSION FOUND TO BE OUT OF LIMITS ON PRESSURE WEB IN RT WHEEL WELL, STA. 857, RT BUTT LINE 27 IAW SRM 51-1-8 AND 53-2-0. FABRICATED AND INSTALLED REPAIR IAW R
- [SDR ABXA060020](https://openairdocs.org/sdr/ABXA060020.md): Floorbeam · corroded · Oct 26, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor Beam
  > MAIN CABIN, STA. 857, LBL 12, FLOORBEAM UPPER CAP CORRODED. REMOVED CORROSION ON FLOORBEAM STA. 857, LBL 12. MATERIAL LOSS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM DWG K04881.
- [SDR ABXA050345](https://openairdocs.org/sdr/ABXA050345.md): Doubler · corroded · Oct 26, 2005 · N826AX · Doug DC863F · Fuselage Main, Structure
  > CORROSION ON TOP OF LONGERON REINFORCEMENT DOUBLER IN AFT CARGO BILGE AT STA 1180, LONGERON 35 RIGHT. REMOVED CORROSION AT STA 1180, LONGERON 35 RIGHT. FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, PRIMED AND INSTALLED NEW DOUBLER FROM 7075-T6, 0.125", PO
- [SDR ABXA050310](https://openairdocs.org/sdr/ABXA050310.md): Longeron · corroded · Oct 26, 2005 · N826AX · Doug DC863F · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STR 31 L (LONGERON) FROM STA. 610 - 730 IN MID ACCESSORY COMPARTMENT. REMOVED AND REPLACED LONGERON 31 LT FROM STA. 610-730 REF SRM 51-1-20 AND DPS 3.67-22.
- [SDR ABXA050355](https://openairdocs.org/sdr/ABXA050355.md): Shear Tie · cracked · Oct 25, 2005 · N826AX · Doug DC863F · Fuselage Internal Mounting Structure
  > FOUND SHEAR TIE CRACKED AT STA 440, LONGERON 31 RIGHT (REF. NRC HY-275). REMOVED AREA STRUCTURE FOR ACCESS, REMOVED DAMAGED AREA OF FORMER SECTION/SHEAR TIE, LONGERON 30 RIGHT AND LONGERON 31 RIGHT, STA 440. FABRICATED REPAIR PARTS: 1 FORMER SECTION FROM 0.07
- [SDR ABXA050353](https://openairdocs.org/sdr/ABXA050353.md): Bulkhead · corroded · Oct 25, 2005 · N826AX · Doug DC863F · Fuselage Main, Bulkhead
  > FOUND CORROSION ON RIGHT WHEEL WELL, STA 980, LONGERON 24 RIGHT, AFT BULKHEAD UNDER LOWER SIDE OF DIAGONAL FRAME. REMOVED BRACKET AT STA 980 IAW DC8 SRM 51-3-0, 51-1-S0D. REMOVED CORROSION IAW DC8 SRM 53-2-0. ORIGINAL MATERIAL MEASURED.047" AND.046", OUT
- [SDR ABXA050344](https://openairdocs.org/sdr/ABXA050344.md): Attach Fitting · cracked · Oct 25, 2005 · N826AX · Doug DC863F · Fuselage Main, Attach Fittings
  > FOUND CORNER FITTING OF CENTER WING BOX UPPER SURFACE AT STA 680, RIGHT BUTT LINE 62 WAS CRACKED. REMOVED CRACKED FITTING AT CENTER WING BOX UPPER SURFACE STA 680, RIGHT BUTT LINE 62 IAW DC8 SRM 51-1-20D AND SRM 51-3-1, DRILLED, REAMED AND COUNTERSUNK CORNER
- [SDR ABXA050295](https://openairdocs.org/sdr/ABXA050295.md): Keelbeam · corroded · Oct 25, 2005 · N826AX · Doug DC863F · Fuselage Main, Keel
  > KEEL BEAM CORRODED AT AFT BULKHEAD OF MID ACCESSORY COMPARTMENT, STA 680, BUTT LINE 0, CORROSION APPEARED TO EXTEND UNDER WING CENTER SECTION. REMOVED CORROSION AT KEEL BEAM STA 620 FWD OF BULKHEAD AND UNDER BULKHEAD AS REQUIRED REF SRM 51-1-8, REF REA D853-
- [SDR ABXA050311](https://openairdocs.org/sdr/ABXA050311.md): Finger Doubler · corroded · Oct 24, 2005 · N826AX · Doug DC863F · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON FINGER DOUBLER AT STA 1540, LONGERON 31 RIGHT, RIGHT BUTT LINE 25. REPAIRS ACCOMPLISHED AT STA 1540 - 1560, LONGERON 31 RIGHT IAW REA D853-52525.
- [SDR ABXA050297](https://openairdocs.org/sdr/ABXA050297.md): Keelbeam · corroded · Oct 24, 2005 · N826AX · Doug DC863F · Fuselage Main, Keel
  > STA. 680 KEELBEAM INSIDE HEAVY CORROSION ON KEELBEAM TO PRESSURE WEB FOUND DURING ACCOMPLISHMENT OF NR HY-055. REMOVED CORROSION AT KEELBEAM STA. 680, BEHIND BULKHEAD AS REQUIRED REF. SRM 51-1-8 AND REA D853-52595-MR FOR REPAIR PROCEDURE TO REINFORCE KEELBEAM
- [SDR ABXA050298](https://openairdocs.org/sdr/ABXA050298.md): Finger Doubler · corroded · Oct 24, 2005 · N826AX · Doug DC863F · Fuselage Main, Plate/Skin
  > AFT LOWER CARGO HAD CORRODED FINGER DOUBLER ON INTERIOR SKIN LOCATED AT STA 1480, LEFT BUTT LINE 32, STRINGER 31 LEFT. REPAIRED FINGER DOUBLERS AT STA 1480 AND 1500, LONGERON 31 LEFT IAW REA D853-52524.
- [SDR ABXA060027](https://openairdocs.org/sdr/ABXA060027.md): Keelbeam · corroded · Oct 23, 2005 · N826AX · Doug DC863F · Fuselage Main, Keel
  > BS 700 - 740, LEFT BUTT LINE 10, LEFT SIDE OF KEELBEAM, CORROSION ON THE LOWER CENTER WING SPLICE DOUBLER. CLEANED CORROSION, TREATED, AND PRIMED IAW DC8 SRM 51-1-8, 53-2-0, LWR NR 200302015. FABRICATED AND INSTALLED REPAIR DOUBLER IAW REA D853-52564.
- [SDR ABXA060034](https://openairdocs.org/sdr/ABXA060034.md): Floorbeam · cracked · Oct 20, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor Beam
  > MAIN CABIN, STA 900, RIGHT BUTT LINE 54, FLOORBEAM CRACKED ON AFT SIDE UPPER CAP, FROM OUTBOARD END OF BEAM TOWARD INBOARD THROUGH TWO FASTENER HOLES. REPAIRED AREA IAW REA D853-52925 BY TRIMMING OUT CRACKED AREA AND INSTALLING A FILLER.
- [SDR ABXA060026](https://openairdocs.org/sdr/ABXA060026.md): Floorbeam · corroded · Oct 20, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor Beam
  > MAIN CABIN, BS 120, RIGHT BUTT LINE 50, FLOORBEAM HAD EXCESSIVE MATERIAL LOSS. REMOVED DAMAGED AREA AND REPLACED WITH ANGLE DOUBLER AND FILLER ON FLOORBEAM BS 120, RIGHT BUTT LINE 50 IAW DC8 SRM 51-1-8, 53-2-0, 51-3-0, 53-7-3, 53-0, 51-2-0, 51-1-8, 51-3-1, 51

Next page: https://openairdocs.org/deregistered/N826AX-2007-11-21/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 = 'N826AX' AND deregistration_id = 'N826AX-2007-11-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N826AX-2007-11-21/reports

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