# Service difficulty reports: N806ME, cancelled May 17, 2006

A list on [N806ME, cancelled May 17, 2006](https://openairdocs.org/deregistered/N806ME-2006-05-17.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 · 118 reports

- [SDR MWEA050034](https://openairdocs.org/sdr/MWEA050034.md): Doubler · dented · Apr 25, 2005 · N806ME · Doug DC981 · Fuselage Main, Plate/Skin
  > DENT REQUIRES REPAIR AT FRAME STATION 245 BETWEEN 1181 AND 1171. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040047](https://openairdocs.org/sdr/MWEA040047.md): Bracket · corroded · Mar 31, 2004 · N806ME · Doug DC981 · Rudder Miscellaneous Structure
  > FOUR AREAS OF CORROSION ON LOWER RUDDER BRACKET. REMOVED AND REPLACED LOWER BRACKETS.
- [SDR MWEA040046](https://openairdocs.org/sdr/MWEA040046.md): Angle · cracked · Mar 29, 2004 · N806ME · Doug DC981 · Cargo/Baggage Doors
  > CRACK ON DOOR PAN AFT SIDE OF PAN NEAR TORQUE TUBE END CAM FORWARD CARGO DOOR. FABRICATED AND INSTALLED REPAIR ANGLE.
- [SDR MWEA040042](https://openairdocs.org/sdr/MWEA040042.md): Longeron · cracked · Mar 29, 2004 · N806ME · Doug DC981 · Fuselage Main, Longeron/Stringer
  > LONGERON 4 LEFT IS CRACKED AT FRAME STATION 541. FABRICATED AND INSTALLED LONGERON AND SPLICES.
- [SDR MWEA040045](https://openairdocs.org/sdr/MWEA040045.md): Skin · dented · Mar 29, 2004 · N806ME · Doug DC981 · Rudder, Plate/Skin
  > RUDDER SKIN ON LEFT SIDE IS DENTED BETWEEN RIB NR 14 AND 15 FROM TOP AT CENTER OF PANEL. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040044](https://openairdocs.org/sdr/MWEA040044.md): Door Frame · chafed · Mar 29, 2004 · N806ME · Doug DC981 · Fuselage Main, Structure
  > MID CARGO PIT DOOR JAMB FORWARD HINGE, FORWARD SUPPORT IS CHAFED AT THE HINGE BOLT. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040043](https://openairdocs.org/sdr/MWEA040043.md): Bulkhead · punctured · Mar 29, 2004 · N806ME · Doug DC981 · Fuselage Main, Bulkhead
  > STATION 218 AT LONGERON 27 RIGHT THE 218 BULKHEAD HAS A PUNCTURE APPROXIMATELY 6 INCHES ABOVE LONGERON 27 RIGHT. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040041](https://openairdocs.org/sdr/MWEA040041.md): Intercostal · corroded · Mar 29, 2004 · N806ME · Doug DC981 · Fuselage Miscellaneous Structure
  > STATION 636 INTERCOSTAL BETWEEN LONGERON 30 AND 26 RIGHT HAS CORROSION. FABRICATED AND INSTALLED INTERCOSTAL.
- [SDR MWEA040040](https://openairdocs.org/sdr/MWEA040040.md): Skin · dented · Mar 29, 2004 · N806ME · Doug DC981 · Rudder, Plate/Skin
  > RUDDER SKIN LEFT SIDE IS DENTED BETWEEN RIBS 12 AND 13 FROM TOP AT CENTER OF PANEL. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040039](https://openairdocs.org/sdr/MWEA040039.md): Frame · cracked · Mar 29, 2004 · N806ME · Doug DC981 · Vertical Stabilizer, Attach Fittings
  > AFT ACCESSORY CANTED FRAME WEB HAS A CRACK LOCATED JUST RIGHT OF FORWARD VERTICAL STABILIZER FRONT ATTACH TANG. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040038](https://openairdocs.org/sdr/MWEA040038.md): Fastener · corroded · Mar 26, 2004 · N806ME · Doug DC981 · Fasteners
  > RIGHT WING EXTERIOR BOTTOM AFT SKIN HAS 3 EACH SPOTS OF CORROSION BETWEEN STATION XRS69 AND XRS91, ALL CORROSION SPOTS ARE WITHIN 14 INCHES OF AFT SPAR T. REMOVED CORROSION AND REMOVED AND REPLACED FASTENERS.
- [SDR MWEA040037](https://openairdocs.org/sdr/MWEA040037.md): Doubler · corroded · Mar 26, 2004 · N806ME · Doug DC981 · Wing, Plate/Skin
  > RIGHT WIND EXTERIOR BOTTOM AFT SKIN HAS A CORROSION SPOT AT STATION XRS234 STRINGER 17. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040036](https://openairdocs.org/sdr/MWEA040036.md): Skin · corroded · Mar 26, 2004 · N806ME · Doug DC981 · Aileron Tabs
  > LEFT AILERON UPPER SURFACE FORWARD INBOARD EDGE, STAINLESS STEEL CHAFE PLATE IS LIFTING UP ON THE AFT END, ALSO CORROSION IS EVIDENT ALONG THE INBOARD AND OUTBOARD EDGES AND SEEMS TO GO UNDER CHAFE PLATE. FABRICATED AND INSTALLED FILLER AND REPAIR STRIP.
- [SDR MWEA040035](https://openairdocs.org/sdr/MWEA040035.md): Doubler · corroded · Mar 25, 2004 · N806ME · Doug DC981 · Leading Edge Devices
  > LEFT WING LEADING EDGE HAS CORROSION 12 FT OUTBOARD OF NR 1 SLAT INBOARD IDLER ARM. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA04034](https://openairdocs.org/sdr/MWEA04034.md): Frame · corroded · Mar 25, 2004 · N806ME · Doug DC981 · Fuselage Main, Frame
  > FRAME STATION 1307 BETWEEN LONGERON 29 LEFT AND 29 RIGHT HAS CORROSION. CUT OUT DAMADED SECTION OF FRAME, FABRICATED 13 PLATES AND INSTALLED 16 FASTENERS, REINSTALLED FRAME TO INTERCOSTAL.
- [SDR MWEA040033](https://openairdocs.org/sdr/MWEA040033.md): Longeron · cracked · Mar 25, 2004 · N806ME · Doug DC981 · Fuselage Main, Floor Beam
  > WINDOW BELT CRACK VISUALLY DETECTED, STATION 408 LONGERON 15 LEFT. FABRICATED AND INSTALLED REPAIR PARTS FABRICATED AND INSTALLED EACH LONGERON SPLICE, INSTALLED TITANIUM DOUBLER AND INSTALLED INTERCOSTAL.
- [SDR MWEA040027](https://openairdocs.org/sdr/MWEA040027.md): Skin · corroded · Mar 19, 2004 · N806ME · Doug DC981 · Wing, Plate/Skin
  > RIGHT WING EXTERIOR BOTTOM AFT SKIN HAS A SPOT OF CORROSION AT STATION XRS410 AFT SPAR TEE AREA. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA040025](https://openairdocs.org/sdr/MWEA040025.md): Angle · corroded · Mar 18, 2004 · N806ME · Doug DC981 · Wing Miscellaneous Structure
  > CORROSION ON ANGLE SUPPORT BRACKET ON RIGHT FLAP TRAILING EDGE AT RIGHT WING STATION XCW 104.5. FABRICATED AND INSTALLED REPAIR ANGLE.
- [SDR MWEA040020](https://openairdocs.org/sdr/MWEA040020.md): Bottle · low · Feb 22, 2004 · N806ME · Doug DC981 · Escape Slide
  > AFT ACCESS EVACUATION SLIDE PRESSURE BELOW 2000 PSI. REMOVED AND REPLACED AFT EVACUATION SLIDE.
- [SDR MWEA040014](https://openairdocs.org/sdr/MWEA040014.md): O-Ring · leaking · Jan 30, 2004 · N806ME · Doug DC981 · Hydraulic System, Main
  > RT HYDRAULIC QUANTITY GAUGE INDICATED IN RED ARC FOLLOWED BY RT HYDRAULIC PRESSURE LOW AND RUDDER CONTROL MANUAL LIGHTS ILLUMINATING. ACCOMPLISHED QRH PROCEDURES. -- REMOVED AND REPLACED O-RING AT TOP REDUCER.
- [SDR MWEA040002](https://openairdocs.org/sdr/MWEA040002.md): Engine · malfunctioned · Jan 4, 2004 · N806ME · Doug DC981 · Engine (Turbine/Turboprop)
  > LEFT ENGINE WOULD NOT GO ABOVE 1.8 ENGINE PRESSURE RATIO. COMPLIED WITH POWER ASSSURANCE CHECK. ALL SYSTEMS NORMAL.
- [SDR MWEA030432](https://openairdocs.org/sdr/MWEA030432.md): Starter · inoperative · Oct 23, 2003 · N806ME · Doug DC981 · Engine Starter
  > NO HIGH-PRESSURE COMPRESSOR SHAFT SPEED ROTATION WHEN STARTING RT ENGINE, START VALVE OPEN LIGHT DID NOT COME ON. REMOVED AND REPLACED ENGINE STARTER.
- [SDR MWEA030307](https://openairdocs.org/sdr/MWEA030307.md): Catcher · plugged · Aug 13, 2003 · N806ME · Doug DC981 · Engine Pressure Ratio (EPR)
  > ADDING POWER FOR TAKE-OFF THE ENGINE PRESSURE RATIO WAS AT 1.80. UNPLUGGED TRAP ASSY- CONDENSATION LEAK CHECK GOOD.
- [SDR MWEA030266](https://openairdocs.org/sdr/MWEA030266.md): Pan · cracked · Jun 28, 2003 · N806ME · Doug DC981 · Service Doors
  > FORWARD GALLEY SERVICE DOOR HOOK PAN ASSEMBLY IS CRACKED. REMOVED AND REPLACED CRACKED PAN ASSEMBLY.
- [SDR MWEA030166](https://openairdocs.org/sdr/MWEA030166.md): Bushing · damaged · Apr 14, 2003 · N806ME · Doug DC981 · Wing, Attach Fittings
  > FOUR HI-LOKS REQUIRED REMOVAL IN THE LEFT WING FUEL TANK APPROXIMATELY XCW 67 AND XCW 69 DUE TO FUEL LEAKS. FABRICATED AND INSTALLED BUSHINGS.
- [SDR MWEA030161](https://openairdocs.org/sdr/MWEA030161.md): Filler · cracked · Apr 7, 2003 · N806ME · Doug DC981 · Leading Edge Devices
  > RIGHT WING LEADING EDGE INTERNAL, CRACK IN MILLED AREA OF INTERNAL LEADING EDGE AT WING STATION XFS112. FABRICATED AND INSTALLED FILLER, INSTALLED FASTENERS.
- [SDR MWEA030160](https://openairdocs.org/sdr/MWEA030160.md): Skin · cracked · Apr 7, 2003 · N806ME · Doug DC981 · Leading Edge Devices
  > RIGHT WING LEADING EDGE INTERNAL CRACK, LOWER AND FORWARD SURFACE. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER AND FILLERS.
- [SDR MWEA030158](https://openairdocs.org/sdr/MWEA030158.md): Bushing · corroded · Apr 4, 2003 · N806ME · Doug DC981 · Horizontal Stabilizer, Attach Fittings
  > LEFT OUTBOARD LOBE FOR HORIZONTAL STABILIZER PIVOT BEARING CORRODED. FABRICATED AND INSTALLED BUSHING.
- [SDR MWEA030157](https://openairdocs.org/sdr/MWEA030157.md): Rib · corroded · Apr 2, 2003 · N806ME · Doug DC981 · Leading Edge Devices
  > LEFT NR 0 SLAT TRACK ATTACH RIB STATION XIS40.014 HAS CORROSION IN THE HOLES FOR THE AFT ECCENTRIC'S. REMOVED CORROSION, INSTALLED BUSHING ON LEFT NR 0 SLAT DRIVE TRACK ATTACH RIB.
- [SDR MWEA030156](https://openairdocs.org/sdr/MWEA030156.md): Skin · damaged · Apr 2, 2003 · N806ME · Doug DC981 · Fuselage Main, Plate/Skin
  > RIGHT FUSELAGE SKIN AT A NUT PLATE HOLE STATION 1095 BELOW LONGERON 19 RIGHT HAS DAMAGE. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA030154](https://openairdocs.org/sdr/MWEA030154.md): Plate · damaged · Apr 1, 2003 · N806ME · Doug DC981 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER CONSTANT UPPER FORWARD PLATE IS DAMAGED 2.5 INCH AFT OF FWD EDGE 1 INCH FROM INBOARD EDGE. FABRICATED AND INSTALLED DOUBLER, FILLER AND SHIMS.
- [SDR MWEA030147](https://openairdocs.org/sdr/MWEA030147.md): Access Panel · damaged · Mar 28, 2003 · N806ME · Doug DC981 · Elevator Miscellaneous Structure
  > RIGHT ELEVATOR UPPER ACCESS PANEL 3632 DOUBLER DAMAGED AT INBOARD SCREW HOLE. FABRICATED AND INSTALLED DOUBLER AND FILLER AND BALANCED ELEVATOR.
- [SDR MWEA030146](https://openairdocs.org/sdr/MWEA030146.md): Shear Tie · cracked · Mar 26, 2003 · N806ME · Doug DC981 · Fuselage Main, Structure
  > SHEAR CLIP IS CRACKED AT FRAME STATION 1309 ABOVE LONGERON 16 LEFT. LOCATED, DRILLED AND INSTALLED SHEAR CLIP.
- [SDR MWEA030145](https://openairdocs.org/sdr/MWEA030145.md): Seat Track · corroded · Mar 26, 2003 · N806ME · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > NR 1 SEAT TRACK CORRODED INBOARD OF AFT SERVICE DOOR BY NUT PLATES. LOCATED, DRILLED AND INSTALLED TRACK SECTION.
- [SDR MWEA030144](https://openairdocs.org/sdr/MWEA030144.md): Shear Tie · cracked · Mar 26, 2003 · N806ME · Doug DC981 · Fuselage Miscellaneous Structure
  > SHEAR TIE IS CRACKED AT FRAME STATION 1309 ABOVE LONGERON 16 RIGHT. FABRICATED AND INSTALLED TWO SHIMS AND NEW SHEAR TIE.
- [SDR MWEA030141](https://openairdocs.org/sdr/MWEA030141.md): Seat Track · corroded · Mar 24, 2003 · N806ME · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > # 1&2 SEAT TRACK HAS CORROSION AT FRAME STATION 1265. -- BLENDED SEAT TRACK, LOCATED,DRILLED AND INSTALLED REPAIR.
- [SDR MWEA030140](https://openairdocs.org/sdr/MWEA030140.md): Doubler · gouged · Mar 24, 2003 · N806ME · Doug DC981 · Fuselage Main, Longeron/Stringer
  > STATION 237 FRAME ABOVE LONGERON 15 RIGHT IS GOUGED. -- FABRICATED,LOCATED,DRILLED AND INSTALLED DOUBLER.
- [SDR MWEA030139](https://openairdocs.org/sdr/MWEA030139.md): Doubler · corroded · Mar 24, 2003 · N806ME · Doug DC981 · Fuselage Floor Panel
  > SUBFLOOR HAS A SPOT OF LIGHT CORROSION AT STATION 207 APPROBIMATELY 6" RIGHT OF CENTER. -- FABRICATED AND INSTALLED NEW REPAIR DOUBLER.
- [SDR MWEA030138](https://openairdocs.org/sdr/MWEA030138.md): Intercostal · cracked · Mar 21, 2003 · N806ME · Doug DC981 · Fuselage Floor Panel
  > SUBFLOOR INTERCOSTAL CRACKED IN SEVERAL PLACES BETWEEN FRAME STATION 788 AND 769 CENTERLINE. --FABRICATED AND INSTALLED REPAIR.
- [SDR MWEA030001](https://openairdocs.org/sdr/MWEA030001.md): Valve · defective · Jan 6, 2003 · N806ME · Doug DC981 · Cabin Pressure Control System
  > NOTICED RIGHT AIRPACK CYCLING ON AND OFF. -- REMOVED AND REPLACED PRESSURE REGULATOR VALVE, TURBINE INLET SWITCH AND COMPRESSOR DISCHARGE SWITCH.
- [SDR MWEA020639](https://openairdocs.org/sdr/MWEA020639.md): Doubler · damaged · Oct 25, 2002 · N806ME · Doug DC981 · Landing Gear Doors
  > CHAFED ON REPAIR DOUBLER AROUND LEFT GEAR DOOR SENSOR. REMOVED AND INSTALLED NEW DOUBLER.
- [SDR MWEA020197](https://openairdocs.org/sdr/MWEA020197.md): Tip Cap · damaged · Mar 27, 2002 · N806ME · Doug DC981 · Elevator, Plate/Skin
  > RIGHT ELEVATOR TIP END HAS SEVERAL ELONGATED HOLES. FABRICATED AND INSTALLED TIP END.
- [SDR MWEA020204](https://openairdocs.org/sdr/MWEA020204.md): Longeron · chafed · Mar 27, 2002 · N806ME · Doug DC981 · Fuselage Main, Structure
  > LONGERON 17 LEFT CHAFED AFT OF SHOVEL CLIP AT STATION 1338. -- REMOVED DAMAGED SECTION. FORMED REPAIR SPLICE AND FILLER SECTION. INSTALLED LONGERON REPAIR SPLICE.
- [SDR MWEA020203](https://openairdocs.org/sdr/MWEA020203.md): Intercostal · damaged · Mar 27, 2002 · N806ME · Doug DC981 · Fuselage Miscellaneous Structure
  > STATION 180 INTERCOSTAL HAS TWO DAMAGED FASTENER HOLES AT A GUSSET 40 INCHES RIGHT OF THE AIRCRAFT CENTERLINE. FABRICATED AND INSTALLED STACKED ANGLE REPAIR.
- [SDR MWEA020202](https://openairdocs.org/sdr/MWEA020202.md): Pan · gouged · Mar 27, 2002 · N806ME · Doug DC981 · Galley Doors
  > FORWARD GALLEY SERVICE DOOR PAN HAS TWO GOUGE MARKS LOCATED ON BOTTOM CENTER BY TWO RIVNUTS, WHICH APPEAR TO HAVE STRIPED THREADS. DRILLED AND PLUGGED HOLES PER TELEX-MWX-ORD-02-00130H.
- [SDR MWEA020201](https://openairdocs.org/sdr/MWEA020201.md): Clip · cracked · Mar 27, 2002 · N806ME · Doug DC981 · Galley Doors
  > FORWARD GALLEY SERVICE DOOR BEAM #1 ATTACH CLIP TO DOOR PAN IS CRACKED, LOCATED ON BOTTOM AFT END. -- INSTALLED NEW CLIP. REPLACED 2 SHORT FASTENERS.
- [SDR MWEA020200](https://openairdocs.org/sdr/MWEA020200.md): Vane · delaminated · Mar 27, 2002 · N806ME · Doug DC981 · Trailing Edge Flaps
  > TWO SPOTS OF DELAMINATION ON THE RIGHT WING, FIXED FLAP VANE (NR 2 FROM FUSELAGE) ON TOP AFT SIDE. APPLIED COLD BOND REPAIR.
- [SDR MWEA020199](https://openairdocs.org/sdr/MWEA020199.md): Skin · cracked · Mar 27, 2002 · N806ME · Doug DC981 · Trailing Edge Flaps
  > RIGHT FLAP HAS A CRACK FROM A SCREW HOLE, 3RD FLAP TRAILING EDGE REMOVABLE SECTION OUT FROM THE FUSELAGE. THE CRACK IS ON THE TOP BACK SIDE. FABRICATED AND INSTALLED PLUG AND DOUBLER.
- [SDR MWEA020198](https://openairdocs.org/sdr/MWEA020198.md): Vane · delaminated · Mar 27, 2002 · N806ME · Doug DC981 · Trailing Edge Flaps
  > LEFT WING OUTBOARD FLAP, INBOARD FIXED VANE HAS A 2 INCH BY 2 INCH AREA OF DELAMINATION 12 INCH INBOARD OF OUTBOARD LOWER EDGE. FABRICATED AND INSTALLED FILLER AND DOUBLER.
- [SDR MWEA020196](https://openairdocs.org/sdr/MWEA020196.md): Vane · delaminated · Mar 27, 2002 · N806ME · Doug DC981 · Trailing Edge Flaps
  > LEFT WING OUTBOARD FLAP, INBOARD FIXED VANE HAS A 2 INCH BY 2 INCH AREA OF DELAMINATION 4 INCHES INBOARD OF OUTBOARD UPPER EDGE. REMOVED AND REPLACED CORE. FABRICATED AND INSTALLED REPAIR DOUBLER.

Next page: https://openairdocs.org/deregistered/N806ME-2006-05-17/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 = 'N806ME' AND deregistration_id = 'N806ME-2006-05-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N806ME-2006-05-17/reports

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