# Service difficulty reports: N526FE, cancelled Sep 4, 2012

A list on [N526FE, cancelled Sep 4, 2012](https://openairdocs.org/deregistered/N526FE-2012-09-04.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 2 · 84 reports

- [SDR 07FDEA04675](https://openairdocs.org/sdr/07FDEA04675.md): Frame · dented · Oct 24, 2007 · N526FE · Doug MD11F · Fuselage Main, Frame
  > MAIN DECK CARGO COMPARTMENT, LEFT STA 1761 FRAME AT ABOUT STRINGER 12R AREA FOUND CRACKED. 11-07-07 MAIN DECK CARGO COMPARTMENT - LEFT HAND STA 1761 FRAME AT STRINGER 12L CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 3 VOLUME I. DUE TO CATEGORY B REPAI
- [SDR 07FDEA04674](https://openairdocs.org/sdr/07FDEA04674.md): Frame · dented · Oct 24, 2007 · N526FE · Doug MD11F · Fuselage Main, Frame
  > MAIN DECK CARGO COMPARTMENT, RIGHT STA 1681 FRAME AT ABOUT STRINGER 12R AREA FOUND DENT. 11-05-07 CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECT
- [SDR 07FDEA04673](https://openairdocs.org/sdr/07FDEA04673.md): Frame · dented · Oct 24, 2007 · N526FE · Doug MD11F · Fuselage Main, Frame
  > MAIN DECK CARGO COMPARTMENT, RIGHT STA 1701 FRAME AT ABOUT STRINGER 12R AREA FOUND DENT. 11-05-07 CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION IS REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSP
- [SDR 07FDEA04672](https://openairdocs.org/sdr/07FDEA04672.md): Frame · dented · Oct 24, 2007 · N526FE · Doug MD11F · Fuselage Main, Frame
  > MAIN DECK CARGO COMPARTMENT, RIGHT STA 1721 FRAME AT ABOUT STRINGER 12R AREA FOUND DENT. 11-05-07 CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIO
- [SDR 06FDEA2637](https://openairdocs.org/sdr/06FDEA2637.md): Structure · corroded · Jul 20, 2006 · N526FE · Doug MD11 · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STABILIZER - INSPECT/REPAIR HORIZONTAL STABILIZER BARREL NUT HOLES. WORK ACCOMPLISHED AS PER EA 1-5510-94622 AIR WORTHINESS DIRECTIVE AD 2003-22-08- STABILIZERS - HORIZONTAL STABILIZER - EMBODIMENT OF HORIZONTAL STABILIZER S/B MD11-55-023 BARREL NU
- [SDR 06FDEA2491](https://openairdocs.org/sdr/06FDEA2491.md): Skin · damaged · Jul 10, 2006 · N526FE · Doug MD11 · Leading Edge Devices
  > FOUND RT WING NR 3 SLAT LE SURFACE FOUND DAMAGED. REPAIR CARRIED OUT ON RT WING NR 3 SLAT L/E SURFACE AS PER SRM 57-10-00 FIG.33 VOL.I.REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
- [SDR 06FDEA2459](https://openairdocs.org/sdr/06FDEA2459.md): Skin · cracked · Jul 4, 2006 · N526FE · Doug MD11 · Leading Edge Devices
  > FOUND CRACKED FASTENER HOLE AT UPPER SURFACE OF RT WING DROOP LE SLAT. WORK CARRIED OUT AS PER E.A.1-5740-99695 REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
- [SDR 06FDEA2415](https://openairdocs.org/sdr/06FDEA2415.md): Skin · cracked · Jun 27, 2006 · N526FE · Doug MD11 · Leading Edge Devices
  > SNRM N02174: RT WING NR 7 SLAT INTERIOR SURFACE MID SECTION SUSPECT SKIN CRACK. REPAIRED AS PER SRM 57-10-00 FIG.10 VOL.I. REPAIR CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.
- [SDR 06FDEA2045](https://openairdocs.org/sdr/06FDEA2045.md): Skin Panel · unknown · May 28, 2006 · N526FE · Doug MD11 · Fuselage Main, Plate/Skin
  > FOUND EXISTING FLUSH REPAIR FOUND AT RT FWD CORNER OF FUSELAGE CAC ACCESS DOOR CUTOUT (REF EO1-5100-7-5001). SKIN REPAIRED AS PER EA 1-5330-94701.
- [SDR 06FDEA1932](https://openairdocs.org/sdr/06FDEA1932.md): Longeron · cracked · May 15, 2006 · N526FE · Doug MD11 · Fuselage Main, Longeron/Stringer
  > FOUND CRACKED LONGERON 7L ON INTERCOSTAL AT BS 518 RT. INTERCOSTAL REPLACED AS PER SRM 51-35-01 VOL2 AND DRAWING AFA3086.
- [SDR 06FDEA1704](https://openairdocs.org/sdr/06FDEA1704.md): Repair · unknown · May 4, 2006 · N526FE · Doug MD11 · Standard Practices/Structures
  > REPAIR REQUIRED AT UNUSED MOUNTING BASE HOLES OF ANTENNA (P/N S65- 5366-890L QTY 04 EACH) AFTER ITS REMOVAL AS PER EA1-2310-94626 STEP 18 REQUIREMENT, SNRM N01696: SKIN REPAIR AT BS 839-879 LONGERON 51L-51R AND INNER DOUBLER AT BS 859-879 LONGERON 51R-52. IN
- [SDR 06FDEA1678](https://openairdocs.org/sdr/06FDEA1678.md): Bracket · cracked · May 2, 2006 · N526FE · Doug MD11 · Horizontal Stabilizer Structure
  > CRACK SUPPORT BRACKET FOR TAIL FUEL TRANSFER PIPE IN EMPERAGE.
- [SDR 06FDEA1677](https://openairdocs.org/sdr/06FDEA1677.md): Attach Fitting · corroded · May 2, 2006 · N526FE · Doug MD11 · Wing, Attach Fittings
  > CORROSION OUTBOARD HINGE (WING SIDE) SIDE LINK ATTACHMENT SPOT FACE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94688.
- [SDR 06FDEA1676](https://openairdocs.org/sdr/06FDEA1676.md): Attach Fitting · corroded · May 2, 2006 · N526FE · Doug MD11 · Wing, Attach Fittings
  > CORROSION OUTBOARD HINGE (WING SIDE) SIDE LINK ATTACHMENT BARREL NUT BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94688.
- [SDR 06FDEA1675](https://openairdocs.org/sdr/06FDEA1675.md): Attach Fitting · corroded · May 2, 2006 · N526FE · Doug MD11 · Wing, Attach Fittings
  > CORROSION OUTBOARD HINGE (WING SIDE) ACTUATOR ATTACHMENT OUTBOARD BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94688.
- [SDR 06FDEA1674](https://openairdocs.org/sdr/06FDEA1674.md): Attach Fitting · corroded · May 2, 2006 · N526FE · Doug MD11 · Wing, Attach Fittings
  > CORROSION OUTBOARD HINGE (WING SIDE) ACTUATOR ATTACHMENT INBOARD BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94688.
- [SDR 06FDEA1673](https://openairdocs.org/sdr/06FDEA1673.md): Attach Fitting · corroded · May 2, 2006 · N526FE · Doug MD11 · Wing, Attach Fittings
  > CORROSION INBOARD HINGE (WING SIDE) SIDE LINK ATTACHMENT SPOT FACE OF OUTBOARD FLAP IN RIGHT WING. CORROSION REMOVED AS PER CMM 57-44-08 PAGE 612-615 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0502 AND REPAIRED AS PER CMM 57-44-08.
- [SDR 06FDEA1672](https://openairdocs.org/sdr/06FDEA1672.md): Attach Fitting · corroded · May 2, 2006 · N526FE · Doug MD11 · Wing, Attach Fittings
  > CORROSION INBOARD HINGE (WING SIDE) LOWER ATTACHMENT SPOT FACE OF OUTBOARD FLAP IN RIGHT WING. CORROSION REMOVED AS PER CMM 57-44-08 PAGE 602-605 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0502 AND REPAIRED AS PER CMM 57-44-08.
- [SDR 06FDEA1671](https://openairdocs.org/sdr/06FDEA1671.md): Attach Fitting · corroded · May 2, 2006 · N526FE · Doug MD11 · Wing, Attach Fittings
  > CORROSION INBOARD HINGE (WING SIDE) ACTUATOR ATTACHMENT OUTBOARD BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-08 PAGE 602-607 AND EA 1-5750-94697.
- [SDR 06FDEA1670](https://openairdocs.org/sdr/06FDEA1670.md): Attach Fitting · corroded · May 2, 2006 · N526FE · Doug MD11 · Wing, Attach Fittings
  > CORROSION INBOARD HINGE (WING SIDE) ACTUATOR ATTACHMENT INBOARD BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-08 PAGE 602-607 AND EA 1-5750-94697.
- [SDR 06FDEA1615](https://openairdocs.org/sdr/06FDEA1615.md): Spar · corroded · Apr 26, 2006 · N526FE · Doug MD11 · Wing Spar
  > CORROSION RT WING REAR SPAR UPPER SURFACE BETWEEN BS 799-827. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG16 VOL1.
- [SDR 06FDEA1614](https://openairdocs.org/sdr/06FDEA1614.md): Spar · corroded · Apr 26, 2006 · N526FE · Doug MD11 · Wing Spar
  > CORROSION RT WING REAR SPAR UPPER SURFACE BETWEEN BS 786-799. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG16 VOL1.
- [SDR 06FDEA1613](https://openairdocs.org/sdr/06FDEA1613.md): Spar · corroded · Apr 26, 2006 · N526FE · Doug MD11 · Wing Spar
  > CORROSION LT WING REAR SPAR UPPER SURFACE BETWEEN BS 738-773. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG16 VOL1.
- [SDR 06FDEA1606](https://openairdocs.org/sdr/06FDEA1606.md): Web · damaged · Apr 26, 2006 · N526FE · Doug MD11 · Fuselage Miscellaneous Structure
  > FLIGHT DECK OBSERVER SEAT DOUBLE FLANGE LIGHTENING HOLE LOCATED UNDERNEATH THE SEAT IN THE COCKPIT SUBFLOOR STRUCTURE FOUND DAMAGED.
- [SDR 06FDEA1605](https://openairdocs.org/sdr/06FDEA1605.md): Fitting · damaged · Apr 26, 2006 · N526FE · Doug MD11 · Trailing Edge Flaps
  > LEFT INBOARD FLAP AFT UPPER ROLLER SUPPORT STRUCTURE CENTER BOLT HOLE FOUND DAMAGED.
- [SDR 06FDEA1604](https://openairdocs.org/sdr/06FDEA1604.md): Wedge · severed · Apr 26, 2006 · N526FE · Doug MD11 · Trailing Edge Flaps
  > LT INBOARD FLAP TRAILING EDGE WEDGE ATTACH CHANNEL OUTBOARD REMOVABLE SEGMENT FOUND SEVERED AT THE OUTBOARD MOST 12 INCH (MATERIAL CLAD 2024-T42 SHEET 0.04 INCH).
- [SDR 06FDEA1603](https://openairdocs.org/sdr/06FDEA1603.md): Skin · dented · Apr 26, 2006 · N526FE · Doug MD11 · Fuselage Main, Plate/Skin
  > DENT FUSELAGE SKIN BETWEEN BS 1997-2015 AND S46L-47L. REPAIRED AS PER EA 1-5330-99714.
- [SDR 06FDEA1602](https://openairdocs.org/sdr/06FDEA1602.md): Attach Fitting · damaged · Apr 26, 2006 · N526FE · Doug MD11 · Horizontal Stabilizer, Attach Fittings
  > LT INBOARD AILERON ATTACH LUG FOUND DAMAGED AT 2 LOCATION ON THE INBOARD SURFACE OF THE LUG AT UPPER AND LOWER CORNER.
- [SDR 06FDEA1601](https://openairdocs.org/sdr/06FDEA1601.md): Structure · damaged · Apr 26, 2006 · N526FE · Doug MD11 · Horizontal Stabilizer Structure
  > LT INBOARD AILERON INBOARD TRAILING EDGE FOUND AN IMPACT DAMAGED.
- [SDR 06FDEA1600](https://openairdocs.org/sdr/06FDEA1600.md): Skin · damaged · Apr 26, 2006 · N526FE · Doug MD11 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STAB LEADING EDGE SECTION FOUND DAMAGED AT STA XFS91.2.
- [SDR 06FDEA1599](https://openairdocs.org/sdr/06FDEA1599.md): Rib · damaged · Apr 26, 2006 · N526FE · Doug MD11 · Elevator, Spar/Rib
  > RIGHT HORIZONTAL STAB INBOARD ELEVATOR ASSY OUTER RIB FOUND DAMAGED.
- [SDR 06FDEA1595](https://openairdocs.org/sdr/06FDEA1595.md): Bracket · dented · Apr 25, 2006 · N526FE · Doug MD11 · Passenger/Crew Doors
  > DENT AFT BRACKET AT DOOR 2R LOWER SIDE. REPLACED BRACKET AS PER DRAWING ADA3760 AND SRM 51-35-01 VOL2 (MAJOR REPAIR).
- [SDR 06FDEA1594](https://openairdocs.org/sdr/06FDEA1594.md): Bracket · cracked · Apr 25, 2006 · N526FE · Doug MD11 · Passenger/Crew Doors
  > CRACK FWD BRACKET AT DOOR 4R LOWER SIDE. REPLACED BRACKET AS PER DRAWING ADA3760 AND SRM 51-35-01 VOL2 (MAJOR REPAIR).
- [SDR 06FDEA1593](https://openairdocs.org/sdr/06FDEA1593.md): Skin · damaged · Apr 24, 2006 · N526FE · Doug MD11 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN FOUND DAMAGED BETWEEN BS 1951-1961 LONGERON 38R-39R. REMOVED AS PER SRM 51-21-01 VOL.II. ORIGINAL MATERIAL THK.0.068" REMOVED 0.006"X L=3"X W=3" REMAIN 0.062" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG.1A VOL.I. CLASSIFIED MINOR REP
- [SDR 06FDEA1592](https://openairdocs.org/sdr/06FDEA1592.md): Structure · cracked · Apr 24, 2006 · N526FE · Doug MD11 · Cargo/Baggage Doors
  > CRACK LOWER FWD CORNER OF AFT CARGO DOOR. REPAIRED AS PER SRM 52-10-00 FIG. 17 VOL.I. CLASSIFIED MINOR REPAIR PER GMM 6-2-100.
- [SDR 06FDEA1591](https://openairdocs.org/sdr/06FDEA1591.md): Skin · dented · Apr 24, 2006 · N526FE · Doug MD11 · Wing, Plate/Skin
  > MULTIPLE DENTS FOUND AT RT WING INBOARD FLAP ASSY LOWER SURFACE OUTBOARD SEGMENT. DENT REPAIRED AS PER SRM 57-10-00 FIG2 VOL1.
- [SDR 06FDEA1590](https://openairdocs.org/sdr/06FDEA1590.md): Skin · dented · Apr 24, 2006 · N526FE · Doug MD11 · Wing, Plate/Skin
  > MULTIPLE DENTS FOUND AT RT WING INBOARD FLAP ASSY LOWER SURFACE INBOARD SEGMENT. DENT REPAIRED AS PER SRM 57-10-00 FIG2 VOL1.
- [SDR 06FDEA1589](https://openairdocs.org/sdr/06FDEA1589.md): Hinge · corroded · Apr 24, 2006 · N526FE · Doug MD11 · Trailing Edge Flaps
  > CORROSION PIVOT BORE AT RT WING INBOARD FLAP OUTBOARD HINGE ON THE WING SIDE. REPAIRED AS PER CMM 57-44-07 PAGE 403-404 AND EA 1-5750- 94700.
- [SDR 06FDEA1588](https://openairdocs.org/sdr/06FDEA1588.md): Skin · dented · Apr 24, 2006 · N526FE · Doug MD11 · Wing, Plate/Skin
  > EXISTING DENT FOUND AT LT WING INBOARD FLAP LOWER SURFACE LOCATED 69 INCHES FROM OUTBOARD AND 6 INCHES FROM AFT. DENT REPAIRED AS PER SRM 57-10-00 FIG2 VOL1 (MAJOR REPAIR).
- [SDR 06FDEA1587](https://openairdocs.org/sdr/06FDEA1587.md): None · none · Apr 24, 2006 · N526FE · Doug MD11 · Standard Practices/Structures
  > EXISTING REPAIR FOUND AT LT WING INBOARD FLAP LOWER SURFACE LOCATED ABOUT 76 INCHES FROM OUTBOARD AND 6 INCHES FROM AFT. REPAIRED AS PER SRM 57-10-00 FIG2 VOL1 (MAJOR REPAIR).
- [SDR 06FDEA1586](https://openairdocs.org/sdr/06FDEA1586.md): Hinge · corroded · Apr 24, 2006 · N526FE · Doug MD11 · Trailing Edge Flaps
  > FOUND CORROSION, SIDE LINK ATTACHMENT SPOT FACE AT LT WING OUTBD FLAP OUTBD HINGE ON THE WING SIDE. CORROSION REMOVED AS PER CMM 57-44-09 PAGE 402-407 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0503 AND REPAIRED AS PER CMM 57-44-09.
- [SDR 06FDEA1585](https://openairdocs.org/sdr/06FDEA1585.md): Hinge · corroded · Apr 24, 2006 · N526FE · Doug MD11 · Trailing Edge Flaps
  > FOUND CORROSION, LOWER ATTACHMENT INBD BORE AT LT WING OUTBD FLAP OUTBD HINGE ON THE WING SIDE. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94681.
- [SDR 06FDEA1584](https://openairdocs.org/sdr/06FDEA1584.md): Hinge · corroded · Apr 24, 2006 · N526FE · Doug MD11 · Trailing Edge Flaps
  > FOUND CORROSION, ACTUATOR ATTACHMENT OUTBD BORE AT LT WING OUTBD FLAP OUTBD HINGE ON THE WING SIDE. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94681.
- [SDR 06FDEA1583](https://openairdocs.org/sdr/06FDEA1583.md): Hinge · corroded · Apr 24, 2006 · N526FE · Doug MD11 · Trailing Edge Flaps
  > FOUND CORROSION, ACTUATOR ATTACHMENT INBD BORE AT LT WING OUTBD FLAP OUTBD HINGE ON THE WING SIDE. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94681.
- [SDR 06FDEA1582](https://openairdocs.org/sdr/06FDEA1582.md): Hinge · corroded · Apr 24, 2006 · N526FE · Doug MD11 · Trailing Edge Flaps
  > FOUND CORROSION, SIDE LINK ATTACHMENT SPOT FACE AT LT WING OUTBD FLAP INBD HINGE ON THE WING SIDE. CORROSION REMOVED AS PER CMM 57-44-08 PAGE 612-615 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0502 AND REPAIRED AS PER CMM 57-44-08.
- [SDR 06FDEA1581](https://openairdocs.org/sdr/06FDEA1581.md): Hinge · corroded · Apr 24, 2006 · N526FE · Doug MD11 · Trailing Edge Flaps
  > FOUND CORROSION, LOWER ATTACHMENT SPOT FACE AT LT WING OUTBD FLAP INBD HINGE ON THE WING SIDE. CORROSION REMOVED AS PER CMM 57-44-08 PAGE 602-607 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0502 AND REPAIRED AS PER CMM 57-44-08.
- [SDR 06FDEA1580](https://openairdocs.org/sdr/06FDEA1580.md): Skin · dented · Apr 24, 2006 · N526FE · Doug MD11 · Trailing Edge Flaps
  > EXISTING DENT FOUND AT LT WING INBD FLAP ASSY UPP SURFACE LOCATED 37 INCH FROM INBD AND 30 INCH FROM AFT. FOUND EXCEED LIMIT AND REPAIRED AS PER SRM 57-10-00 FIG. 34 VOL.I. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.
- [SDR 06FDEA1556](https://openairdocs.org/sdr/06FDEA1556.md): Repair · unknown · Apr 20, 2006 · N526FE · Doug MD11 · Fuselage Main, Plate/Skin
  > EXISTING FLUSH REPAIR FOUND AT FUSELAGE ADJACENT TO BS435 BILGE BETWEEN LONGERON 51L TO 51R (REF EO 1-5100-7-5001). SKIN REPAIRED AS PER SRM 53-20-00 FIG6 SHEET8 VOL1 CATB REPAIR-INITIAL INSPECTION AT 7500 CYCLES AND REPETITIVE INSPECTION AT 4750 CYCLES
- [SDR 06FDEA1555](https://openairdocs.org/sdr/06FDEA1555.md): Doubler · cracked · Apr 20, 2006 · N526FE · Doug MD11 · Fuselage Main, Plate/Skin
  > FOUND CRACK-MACHINED DOUBLER LOCATED BETWEEN RT WALL (ADJACENT TO RT SPOILER MIXER OUTPUT ROD) AND RT WHEEL WELL CUTOUT OF CENTER LANDING GEAR WHEEL WELL. CRACKED DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MINOR AS PER GMM
- [SDR 06FDEA1554](https://openairdocs.org/sdr/06FDEA1554.md): Doubler · cracked · Apr 20, 2006 · N526FE · Doug MD11 · Fuselage Main, Plate/Skin
  > FOUND CRACK-MACHINED DOUBLER LOCATED BETWEEN LT WALL (ADJACENT TO LT SPOILER MIXER OUTPUT ROD) AND LT WHEEL WELL CUTOUT OF CENTER LANDING GEAR WHEEL WELL. CRACKED DOUBLER REMOVED AND REPLACED AS PER 51-31-01 VOL.II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2

Next page: https://openairdocs.org/deregistered/N526FE-2012-09-04/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 = 'N526FE' AND deregistration_id = 'N526FE-2012-09-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N526FE-2012-09-04/reports

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