# Service difficulty reports: N206ME, cancelled Jan 21, 2005

A list on [N206ME, cancelled Jan 21, 2005](https://openairdocs.org/deregistered/N206ME-2005-01-21.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 4 · 187 reports

- [SDR MWEA030254](https://openairdocs.org/sdr/MWEA030254.md): Rudder · inoperative · Jun 24, 2003 · N206ME · Doug DC932 · Rudder Control System
  > RUDDER FULL RIGHT APPLIED WITH NO APPARENT EFFECT. ADJUSTED CABLE RUN AND SENSING SECTOR, PERFORMED ADJUSTMENT TEST. NO DEFECTS NOTED. (AIRCRAFT PARKED SINCE 6-23-03, CURRENTLY ON OPERATION CERTIFICATE, PLANNED RETIREMENT DATE UNDECIDED)
- [SDR MWEA030233](https://openairdocs.org/sdr/MWEA030233.md): Switch · dirty · May 25, 2003 · N206ME · Doug DC9 · Central Warning
  > RECEIVED TAKEOFF WARNING HORN WHILE ADVANCING THROTTLES. -- CLEANED STICKY SWITCH.
- [SDR MWEA020618](https://openairdocs.org/sdr/MWEA020618.md): Line · disconnected · Oct 17, 2002 · N206ME · Doug DC932 · Engine Pressure Ratio (EPR)
  > RIGHT ENGINE PRESSURE RATIO GAUGE REMAINED AT 10. FOUND PT7 LINE DISCONNECTED AT LOWER AFT ATTACH FITTING. RECONNECTED PT7 LINE.
- [SDR MWEA020319](https://openairdocs.org/sdr/MWEA020319.md): Valve · clogged · May 6, 2002 · N206ME · Doug DC932 · Aileron Tab Control System
  > AILERON SERVO INDICATOR SHOWED FULL DEFLECTION. DISCONNECTED AUTO PILOT AND THE AIRCRAFT STARTED TO TURN TO THE LEFT. FOUND WATER DRAINING IN LEFT GEAR AREA AND ICE ON CABLES AT THE LEFT TRAPEZOID PANEL. FOUND DEBRIS IN DRAIN HOSE THAT CAUSED THE CHECK VALVE T
- [SDR MWEA020296](https://openairdocs.org/sdr/MWEA020296.md): Support Bracket · corroded · Apr 11, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous Structure
  > FORWARD PIT LEFT AUX TANK STRUT UPPER SUPPORT BRACKET HAS EXFOLIATION AROUND A FASTENER STATION 545 LONGERON 24 LEFT. REMOVED AND REPLACED FITTING.
- [SDR MWEA020295](https://openairdocs.org/sdr/MWEA020295.md): Skin · damaged · Apr 11, 2002 · N206ME · Doug DC932 · Fuselage Main, Plate/Skin
  > REPLACE AFT CARGO PIT BELLY SKIN SECTION LONGERON 28 LEFT TO 28 RIGHT STATION 803 THROUGH 996 TO COMPLY WITH CARRY OVER NR 2201. REMOVED AND REPLACED SKIN.
- [SDR MWEA020294](https://openairdocs.org/sdr/MWEA020294.md): Longeron · cracked · Apr 11, 2002 · N206ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FORWARD PIT LONGERON 29 RIGHT IS CRACKED AT STATION 570-578. -- REMOVED, MATCH DRILLED LONGERON AS REQUIRED PER DWG # 5910068, AND INSTALLED.
- [SDR MWEA020222](https://openairdocs.org/sdr/MWEA020222.md): Angle · cracked · Apr 8, 2002 · N206ME · Doug DC932 · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL STABILIZER LEADING EDGE TAIL TO FUSELAGE DORSAL INTERNAL ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE BRACKET.
- [SDR MWEA020223](https://openairdocs.org/sdr/MWEA020223.md): Web · out of tolerance · Apr 8, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous Structure
  > REMOVAL AFT CARGO DOOR JAMB LOWER INNER WEB TO FACILITATE OTHER MAINTENANCE. -- OLD WEB FOUND OUT OF LIMITS. INSTALLED NEW WEB.
- [SDR MWEA020221](https://openairdocs.org/sdr/MWEA020221.md): Former · cracked · Apr 8, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous Structure
  > FORMER AT STATION 237 LONGERON 18 LEFT TO 17 LEFT IS CRACKED. -- FABRICATED AND INSTALLED SHIM TO ACHIEVE EDGE DISTANCE.
- [SDR MWEA020219](https://openairdocs.org/sdr/MWEA020219.md): Web · misdrilled · Apr 8, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous Structure
  > FORWARD CARGO DOOR JAMB WEB AND FRAME AT 427 HAS A DOUBLE DRILLED HOLE BETWEEN LONGERON 29 RIGHT AND LONGERON 28 RIGHT. -- FABRICATED AND INSTALLED REPAIR STRAP AND WEB REPAIR DOUBLER.
- [SDR MWEA020217](https://openairdocs.org/sdr/MWEA020217.md): Angle · broken · Apr 8, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER LEG FORWARD SIDE OF ELECTRONIC POWER CENTER PANEL SUPPORT FROM COCKPIT DOOR JAMB TO BANANA PANEL. FOUND ANGLE CRACKED OFF. REMOVED AND REPLACED ANGLE.
- [SDR MWEA020216](https://openairdocs.org/sdr/MWEA020216.md): Skin · damaged · Apr 8, 2002 · N206ME · Doug DC932 · Fuselage Main, Plate/Skin
  > FUSELAGE CLASS III DOUBLER NEEDS UPGRADE AT STATION 218 LONGERON 25 LEFT. REMOVED DOUBLER, VERIFIED AS NO CRACKS IN SKIN. INSTALLED DOUBLER. REPAIR PLACED ON WATCH ITEM 6712 FOR REINSPECTION PER SRM 53-04 FIGURE 12B.
- [SDR MWEA020215](https://openairdocs.org/sdr/MWEA020215.md): Skin · corroded · Apr 8, 2002 · N206ME · Doug DC932 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AROUND SOME OF THE WRAP AROUND SCREWS (CENTER SECTION INBOARD AREA). THERE WAS PREVIOUS BLEND-OUT ALREADY IN THIS AREA. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA020214](https://openairdocs.org/sdr/MWEA020214.md): Skin · corroded · Apr 8, 2002 · N206ME · Doug DC932 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AROUND SOME OF THE WRAP AROUND SCREWS (CENTER SECTION INBOARD AREA). THERE WAS PREVIOUS BLEND OUT ALREADY IN THIS AREA. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA020213](https://openairdocs.org/sdr/MWEA020213.md): Intercostal · cracked · Apr 8, 2002 · N206ME · Doug DC932 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR, INTERCOSTAL CRACKED, LOWER AFT AREA OF DOOR. -- REMOVED AND REPLACED INTERCOSTAL.
- [SDR MWEA020212](https://openairdocs.org/sdr/MWEA020212.md): Doubler · blown · Apr 8, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT DOUBLER AROUND THE SUGAR SCOOP IS BLOWN OUT ON THE BOTTOM AFT AREA AT STATION 965 ABOVE LONGERON 22 LEFT. -- REMOVED DOUBLER. DRILLED UP AND TRIMMED DOUBLER TO FIT IAW SRM 51-10-4 DAC DRAWING 5914558. INSTALLED DOUBLER.
- [SDR MWEA020211](https://openairdocs.org/sdr/MWEA020211.md): Longeron · blown · Apr 8, 2002 · N206ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT HAS A LONGERON BLOWN OUT IN THE CENTER OF LONGERON 23 LEFT AT STATION 945. -- FABRICATED AND INSTALLED STRAP.
- [SDR MWEA020210](https://openairdocs.org/sdr/MWEA020210.md): Panel · damaged · Apr 8, 2002 · N206ME · Doug DC932 · Fuselage Floor Panel
  > REMOVED CABIN FLOOR PANEL B-5 TO FACILITATE OTHER MAINTENANCE. -- FORWARD END OF PANEL IS DAMAGED. FABRICATED NEW SKIN AND REINSTALLED CABIN FLOOR PANEL.
- [SDR MWEA020194](https://openairdocs.org/sdr/MWEA020194.md): Panel · damaged · Mar 27, 2002 · N206ME · Doug DC932 · Rudder, Plate/Skin
  > DENT DAMAGE ON RUDDER LEADING EDGE STRUCTURE AT STATION ZR70 RIGHT SIDE. MEASURES APPROX 4 INCHES IN LENGTH. FABRICATED AND INSTALLED REPAIR.
- [SDR MWEA020195](https://openairdocs.org/sdr/MWEA020195.md): Gusset · corroded · Mar 27, 2002 · N206ME · Doug DC932 · Fuselage Main, Structure
  > GUSSET AT STATION 580 IS CORRODED ON INTERCOSTAL. -- FABRICATED AND INSTALLED GUSSET.
- [SDR MWEA020193](https://openairdocs.org/sdr/MWEA020193.md): Fitting · misdrilled · Mar 27, 2002 · N206ME · Doug DC932 · Fuselage Main, Structure
  > FITTINGS MISDRILLED AT STATION 207 (INTERCOSTAL ATTACH CLIP). -- FABRICATED AND INSTALLED NEW FITTING. LOCATED AND PRIMED AND INSTALLED PARTS.
- [SDR MWEA020192](https://openairdocs.org/sdr/MWEA020192.md): Fitting · damaged · Mar 27, 2002 · N206ME · Doug DC932 · Fuselage Main, Structure
  > REMOVED FLOOR BEAM END FITTING AT CUSP, STATION 218 LEFT SIDE TO FACILITATE OTHER MAINTENANCE. -- FITTING DAMAGED UPON REMOVAL. INSTALLED NEW FITTING.
- [SDR MWEA020191](https://openairdocs.org/sdr/MWEA020191.md): Angle · corroded · Mar 27, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous Structure
  > CORROSION ON CELING IN E&E BAY FROM STATION 200 TO 218 JUST BELOW THE CUSP LINE NEAR LONGERON 18 LEFT. REMOVED DAMAGED SECTION OF UPPER CUSP ANGLE. FABRICATED AND FORMED -3 REPAIR SPLICE. INSTALLED CUSP ANGLE AND SPLICE.
- [SDR MWEA020190](https://openairdocs.org/sdr/MWEA020190.md): Intercostal · improper · Mar 27, 2002 · N206ME · Doug DC932 · Fuselage Main, Structure
  > FORWARD PIT INTERCOASTAL LOCATED BETWEEN LONGERON 28 RIGHT AND 27 RIGHT AND FRAMES 560-579 HAS SEVERAL DIVETS IMPROPERLY BACKED. -- FABRICATED AND INSTALLED AFT FLANGE. FOUND CRACKS ON INTERCOSTAL LOWER ATTACH HOLES. FABRICATED AND INSTALLED INTERCOSTAL.
- [SDR MWEA020188](https://openairdocs.org/sdr/MWEA020188.md): Bracket · corroded · Mar 27, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE BRACKET FOR FLOOR SUPPORT AT STATION 367 RIGHT SIDE. REMOVED AND REPLACED BRACKET.
- [SDR MWEA020187](https://openairdocs.org/sdr/MWEA020187.md): Splice · cracked · Mar 22, 2002 · N206ME · Doug DC932 · Fuselage Main, Structure
  > LONGERON 28 LEFT SPLICE AT STATION 560 IS CRACKED OUT AFT HOLE. -- REMOVED LONGERON SPLICE FITTING. MATCH DRILLED FITTING. FABRICATED AND INSTALLED SHIMS TO SPLICE AND INSTALLED SPLICE TO LONGERONS.
- [SDR MWEA020186](https://openairdocs.org/sdr/MWEA020186.md): Panel · corroded · Mar 22, 2002 · N206ME · Doug DC932 · Trailing Edge Flaps
  > LEFT FLAP TRAILING EDGE PANEL NR 3 HAS MODERATE TO HEAVY CORROSION AROUND FINGER DOUBLERS IN SEVERAL BAYS. FINGER DOUBLERS LOOSE IN SEVERAL AREAS. FABRICATED AND INSTALLED LOWER AND UPPER PANELS.
- [SDR MWEA020185](https://openairdocs.org/sdr/MWEA020185.md): Longeron · corroded · Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FORWARD PIT, CORROSION ON LONGERON AT STATION 570 LONGERON 30. REMOVED AND REPLACED LONGERON. FABRICATED AND INSTALLED RADIUS STRAP.
- [SDR MWEA020184](https://openairdocs.org/sdr/MWEA020184.md): Frame · corroded · Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, Frame
  > STATION 980 FRAME UPPER -J- CHANNEL HAS AREAS OF LIGHT CORROSION BETWEEN LONGERON 29 LEFT THROUGH LONGERON 28 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLES, SPLICES AND FRAME SECTION.
- [SDR MWEA020183](https://openairdocs.org/sdr/MWEA020183.md): Longeron · cracked · Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, Structure
  > FORWARD PIT LONGERON 28 LEFT IS CRACKED UNDER SPLICE AT STATION 552 THROUGH 560. -- REMOVED LONGERON, POSITIONED AND DRILLED, REINSTALLED LONGERON.
- [SDR MWEA020182](https://openairdocs.org/sdr/MWEA020182.md): Clip · corroded · Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT UNDERSIDE OF SHOVEL CLIP CORRODED AT STATION 945 LONGERON 26 RIGHT. -- REMOVED AND REPLACED SHOVEL CLIP.
- [SDR MWEA020181](https://openairdocs.org/sdr/MWEA020181.md): Frame · corroded · Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, Frame
  > STATION 832 FRAME AFT SIDE HAS CORROSION BETWEEN LONGERONS 29 RIGHT TO 28 RIGHT. FABRICATED AND INSTALLED FRAME REPAIR SECTIONS.
- [SDR MWEA020180](https://openairdocs.org/sdr/MWEA020180.md): Frame · corroded · Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, Frame
  > STATION 917 FRAME FORWARD SIDE HAS CORROSION FROM LONGERON 28 LEFT TO 29 RIGHT UNDER THE FLOOR SUPPORT. FABRICATED AND INSTALLED FRAME SECTION, REPAIR DOUBLERS, AND SUPPORT FITTING.
- [SDR MWEA020179](https://openairdocs.org/sdr/MWEA020179.md): Frame · corroded · Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, Frame
  > STATION 965 FRAME HAS LIGHT CORROSION FROM LONGERON 25 LEFT TO 27 RIGHT AFT SIDE. REMOVED AND REPLACED SPLICE.
- [SDR MWEA020177](https://openairdocs.org/sdr/MWEA020177.md): Frame · corroded · Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, Frame
  > FORMER AT STATION 980 HAS AREA OF LIGHT CORROSION BETWEEN LONGERON 25 THROUGH LONGERON 26 LEFT. FABRICATED AND INSTALLED FORMER AND SPLICES.
- [SDR MWEA020178](https://openairdocs.org/sdr/MWEA020178.md): Fitting · corroded · Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous Structure
  > CUSP SPLICE FITTING AT STATION 229 LEFT SIDE HAS CORROSION. REMOVED AND REPLACED FITTING.
- [SDR MWEA020176](https://openairdocs.org/sdr/MWEA020176.md): Support · cracked · Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous Structure
  > STATION 897 BETWEEN LONGERONS 27 LEFT AND 28 LEFT SUPPORT HAS CORROSION BY A FASTENER. WHILE REMOVING CORROSION, FOUND SUPPORT CRACK. REMOVED AND REPLACED SUPPORT.
- [SDR MWEA020175](https://openairdocs.org/sdr/MWEA020175.md): Fitting · corroded · Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, Structure
  > STATION 945 BETWEEN LONGERONS 28 LEFT AND 27 LEFT HAS A CORRODED SUPPORT FITTING. -- REMOVED AND REPLACED SUPPORT FITTING.
- [SDR MWEA020174](https://openairdocs.org/sdr/MWEA020174.md): Support · cracked · Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, Structure
  > STATION 980 BY LONGERON 27 RIGHT HAS A CRACKED SUPPORT. -- REMOVED AND REPLACED FLOOR SUPPORT.
- [SDR MWEA020170](https://openairdocs.org/sdr/MWEA020170.md): Frame · corroded · Mar 15, 2002 · N206ME · Doug DC932 · Fuselage Main, Frame
  > STATION 897 FRAME AT LONGERON 29 RIGHT TO 30 HAS CORROSION ON THE LOWER SURFACE. FABRICATED AND INSTALLED CLIP, REPAIR DOUBLERS, AND SHIMS.
- [SDR MWEA020168](https://openairdocs.org/sdr/MWEA020168.md): Longeron · dented · Mar 15, 2002 · N206ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > LONGERON 20 LEFT STATION 214 HAS DENT AND HAS CARRY OVER 5735. FABRICATED AND INSTALLED LONGERON SECTION.
- [SDR MWEA020167](https://openairdocs.org/sdr/MWEA020167.md): Longeron · cracked · Mar 15, 2002 · N206ME · Doug DC932 · Fuselage Main, Structure
  > LONGERON 2 RIGHT AT FUSELAGE STATION 1076 CRACKED AT END. -- REMOVED AND REPLACED WITH REPAIR, NEW LONGERON SPLICE.
- [SDR MWEA020137](https://openairdocs.org/sdr/MWEA020137.md): Frame · cracked · Feb 22, 2002 · N206ME · Doug DC932 · Fuselage Main, Frame
  > LEFT HAND LOWER RADOME GUIDE PIN HAS A 1.5 INCH CRACK EMANATING FROM ITS HOLE OUTWARD TO A RIVET. REPAIRED PER SRM 53-01-00 FIGURE 2 SHEET 3, DOUBLER ON AFT SIDE OF FORMER.
- [SDR MWEA010773](https://openairdocs.org/sdr/MWEA010773.md): Fan · failed · May 17, 2001 · N206ME · Doug DC932 · Air Distribution Fan
  > IN ROUTE TO DSM WEATHER RADAR FAILED. AIRCRAFT DIVERTED TO OMA. REMOVED AND REPLACED WEATHER RADAR RT AND RT FAN.
- [SDR MWEA010669](https://openairdocs.org/sdr/MWEA010669.md): Skin · cracked · May 1, 2001 · N206ME · Doug DC932 · Fuselage Main, Plate/Skin
  > AT STATION 980 RIGHT, THERE IS A SMALL CRACK EXTENDING FROM A FASTENER BETWEEN LONGERON 14 RIGHT AND 16 RIGHT. REMOVED DAMAGED AREA, FABRICATED FILLERS, DOUBLER AND FINGER DOUBLER, INSTALLED REPAIR.
- [SDR MWEA010664](https://openairdocs.org/sdr/MWEA010664.md): Seat Track · damaged · Apr 27, 2001 · N206ME · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > F/O''S AFT OUTBOARD SEAT TRACK LOCKING HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR STRAP.
- [SDR MWEA010663](https://openairdocs.org/sdr/MWEA010663.md): Seat Track · damaged · Apr 27, 2001 · N206ME · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > CAPTAINS AFT SEAT TRACKS LOCKING HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR STRAP.
- [SDR MWEA010662](https://openairdocs.org/sdr/MWEA010662.md): Frame · cracked · Apr 27, 2001 · N206ME · Doug DC932 · Fuselage Main, Frame
  > STATION 980 RIGHT SIDE FRAME IS CRACKED ON LOWER LEG AT LONGERON 17 RIGHT. FABRICATED AND INSTALLED DOUBLERS.
- [SDR MWEA010660](https://openairdocs.org/sdr/MWEA010660.md): Seat Track · damaged · Apr 27, 2001 · N206ME · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > CAPTAINS AFT, INBOARD SEAT TRACK LOCKING HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR STRAP.

Next page: https://openairdocs.org/deregistered/N206ME-2005-01-21/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 = 'N206ME' AND deregistration_id = 'N206ME-2005-01-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N206ME-2005-01-21/reports

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