# Service difficulty reports: N209ME, cancelled Jul 28, 2006

A list on [N209ME, cancelled Jul 28, 2006](https://openairdocs.org/deregistered/N209ME-2006-07-28.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 7 · 335 reports

- [SDR MWEA040015](https://openairdocs.org/sdr/MWEA040015.md): Indicator · inoperative · Feb 3, 2004 · N209ME · Doug DC932 · Escape Slide
  > FORWARD ENTRANCE DOOR SLIDE PRESSURE GAUGE IS INOPERATIVE. REMOVED AND REPLACED FORWARD EVACUATION SLIDE.
- [SDR MWEA030437](https://openairdocs.org/sdr/MWEA030437.md): Light · loose · Oct 31, 2003 · N209ME · Doug DC932 · Emergency Lighting
  > EMERGENCY EXIT LIGHT FOR SERVICE DOOR AFT SIDE HAS COME LOOSE FROM TOP SIDE. REMOVED AND REPLACED EEPLS EXIT LIGHT FOR SERVICE DOOR.
- [SDR MWEA030421](https://openairdocs.org/sdr/MWEA030421.md): Control Panel · inoperative · Oct 13, 2003 · N209ME · Doug DC932 · AC Generation System
  > ON START OF RT ENGINE, AC CROSS-TIE LOCK OUT CAME ON, UNABLE TO RESET. REMOVED AND REPLACED AC BUSS CONTROL PANEL.
- [SDR MWEA030400](https://openairdocs.org/sdr/MWEA030400.md): Thrust Reverser · corroded · Oct 1, 2003 · N209ME · Doug DC932 · Engine Thrust Reverser
  > LIGHT CORROSION ON OUTER FACE OF LEFT DRIVE ARM, TOP BUCKET IN FLANGE RADIUS. REMOVED AND REPLACED THRUST REVERSER.
- [SDR MWEA030395](https://openairdocs.org/sdr/MWEA030395.md): Skin · dented · Sep 25, 2003 · N209ME · Doug DC932 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT AT STATION 967, 2 INCHES ABOVE LONGERON 27 LEFT. FABRICATED AND INSTALLED DOUBLER AND FILLERS.
- [SDR MWEA030393](https://openairdocs.org/sdr/MWEA030393.md): Longeron · cracked · Sep 25, 2003 · N209ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > WHILE REPLACING DOME NUTS FOR FUSELAGE FILET PANEL, FOUND SUSPECT CRACK ON AFT END OF LONGERON 26 RT FRAME STATION 604. FABRICATED AND INSTALLED FITTING.
- [SDR MWEA030392](https://openairdocs.org/sdr/MWEA030392.md): Skin · dented · Sep 25, 2003 · N209ME · Doug DC932 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT AT STATION 388 AT LONGERON 5 RIGHT. FABRICATED AND INSTALLED FILLER AND DOUBLER.
- [SDR MWEA030391](https://openairdocs.org/sdr/MWEA030391.md): Skin · gouged · Sep 25, 2003 · N209ME · Doug DC932 · Vertical Stabilizer, Plate/Skin
  > LEFT SIDE OF VERTICAL STABILIZER SKIN UNDER VERTICAL TO HORIZONTAL STABILIZER, FAIRING HAS A GOUGE FROM TOP SKIN RADIUS EXTENDING DOWN AT 1.5 INCHES. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA030272](https://openairdocs.org/sdr/MWEA030272.md): Connector · faulty · Jul 8, 2003 · N209ME · Doug DC932 · Fire Detection
  > LEFT ENGINE LOOP A FIRE INDICATION CAME ON. REMOVED AND REPLACED BOTH FIRE EXTINGUISHER BOTTLE,1 EACH SQUIBS,LEFT ENGINE B AND REPLACED FAULTY CONNECTORS,
- [SDR MWEA030179](https://openairdocs.org/sdr/MWEA030179.md): Switch · dirty · Apr 21, 2003 · N209ME · Doug DC932 · Stabilizer Position Indicating
  > AFTER THROTTLE ADVANCEMENT, TAKEOFF WARNING HORN SOUNDED. ALL INDICATIONS NORMAL. HORIZONTAL STABILIZER SWITCH FOUND STICKING. CLEANED SWITCH.
- [SDR MWEA030132](https://openairdocs.org/sdr/MWEA030132.md): Control Box · inoperative · Mar 13, 2003 · N209ME · Doug DC932 · Brake Anti-Skid Section
  > WHILE ARMING ANTI-SKID RIGHT OUTBOARD AND INBOARD LIGHTS REMAINED ON. REMOVED AND REPLACED ANTI-SKID CONTROL BOX.
- [SDR MWEA030105](https://openairdocs.org/sdr/MWEA030105.md): Receiver · inoperative · Feb 15, 2003 · N209ME · Doug DC932 · Localizer/VOR System
  > FIRST OFFICER NR 2 NAV FAILED, VOR, GS, AND LOC FLAGS SHOWING. REMOVED AND REPLACED VOR/ILS RECEIVER.
- [SDR MWEA030072](https://openairdocs.org/sdr/MWEA030072.md): Drive Shaft · sheared · Feb 12, 2003 · N209ME · Doug DC932 · Engine Starter
  > WHEN ATTEMPTING TO START #2 ENGINE THE N2 WENT TO 10% THEN DROPPED OFF TO ZERO. -- REMOVED AND REPLACED STARTER DRIVE SHAFT.
- [SDR MWEA020727](https://openairdocs.org/sdr/MWEA020727.md): Starter · inoperative · Dec 6, 2002 · N209ME · Doug DC932 · Engine Cranking
  > LEFT ENGINE STARTER INOPERATIVE -- REMOVED AND REPLACED ENGINE STARTER.
- [SDR MWEA020576](https://openairdocs.org/sdr/MWEA020576.md): Altimeter · fluctuates · Sep 18, 2002 · N209ME · Doug DC932 · Altimeter, Barometric/Encoder
  > CAPTAIN'S STANDBY ALTIMETER FLUCTUATING. -- REMOVED AND REPLACED CAPTAIN'S STATIC SELECTOR VALVE.
- [SDR MWEA020521](https://openairdocs.org/sdr/MWEA020521.md): Wing · damaged · Aug 29, 2002 · N209ME · Doug DC932 · Trailing Edge Flaps
  > LEFT OUTBOARD FLAP TRAILING EDGE DAMAGED AND AFT TRAILING EDGE CHANNEL. -- REMOVED AND REPLACED TRAILING EDGE.
- [SDR MWEA020459](https://openairdocs.org/sdr/MWEA020459.md): Bracket · cracked · Jul 25, 2002 · N209ME · Doug DC932 · Galley Doors
  > CRACKED ANGLE BRACKET FORWARD END UNDER #1 BEAM OF GALLEY DOOR (DOT JH 36). -- FABRICATED AND INSTALLED BRACKET.
- [SDR MWEA020070](https://openairdocs.org/sdr/MWEA020070.md): Angle · oversized · Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Main Frame
  > PYLON WEB ANGLE HAS AN OVERSIZED HOLE. -- FABRICATED AND INSTALLED ANGLE.
- [SDR MWEA020069](https://openairdocs.org/sdr/MWEA020069.md): Doubler · damaged · Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Frame/Spar/Rib
  > RIGHT PYLON AFT SPAR WEB DOUBLER HAS OVERSIZED FASTENER HOLES. FABRICATED AND INSTALLED NEW DOUBLER.
- [SDR MWEA020068](https://openairdocs.org/sdr/MWEA020068.md): Angle · oversized · Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Main Frame
  > REMOVED RIGHT PYLON AFT SPAR WEB ANGLE TO FACILITATE OTHER MAINTENANCE. (UPPER FASTENER HOLE OVERSIZED.) -- FABRICATED AND INSTALLED "L" ANGLE ON NEW WEB.
- [SDR MWEA020124](https://openairdocs.org/sdr/MWEA020124.md): Web · oversized · Feb 6, 2002 · N209ME · Doug DC932 · Fuselage Main, Structure
  > WEB AT 15 RIGHT BETWEEN STATION 1038 AND 1059 HAS OVERSIZED HOLES. -- FABRICATED AND INSTALLED SPLICE ANGLE.
- [SDR MWEA020123](https://openairdocs.org/sdr/MWEA020123.md): Web · oversized · Feb 6, 2002 · N209ME · Doug DC932 · Fuselage Main, Structure
  > REMOVED SECTION OF WEB AT STATION 1038 BETWEEN LONGERON 14 RIGHT AND 17 RIGHT. SPAR STRAP HOLES OVERSIZED. -- FABRICATED AND INSTALLED WEB SECTION AND WEB SPLICES.
- [SDR MWEA020121](https://openairdocs.org/sdr/MWEA020121.md): Frame · damaged · Feb 6, 2002 · N209ME · Doug DC932 · Fuselage Main, Frame
  > AT STATION 1038, LONGERON 15 RIGHT INNER, OUTER FRAME CAP AND SHEAR TIE HAS 5 OVERSIZED HOLES. FABRICATED AND INSTALLED REPAIR BUSHINGS AND BUSHING RETAINING STRAPS.
- [SDR MWEA020120](https://openairdocs.org/sdr/MWEA020120.md): Angle · oversized · Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Main Frame
  > RIGHT PYLON AFT SPAR ANGLE HAS OVERSIZED FASTENER H0LE. -- FABRICATED AND INSTALLED ANGLE.
- [SDR MWEA020119](https://openairdocs.org/sdr/MWEA020119.md): Fitting · oversized · Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Main Frame
  > RIGHT PYLON FITTING HAS OVERSIZE HOLE. -- FABRICATED AND INSTALLED FITTING AND RADIUS BLOCKS.
- [SDR MWEA020118](https://openairdocs.org/sdr/MWEA020118.md): Angle · oversized · Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Main Frame
  > RIGHT SPAR AFT UPPER ANGLE HAS OVERSIZED HOLES. -- FABRICATED AND INSTALLED ANGLE.
- [SDR MWEA020117](https://openairdocs.org/sdr/MWEA020117.md): Fitting · oversized · Feb 6, 2002 · N209ME · Doug DC932 · Fuselage Main, Structure
  > REMOVED FITTING THAT ATTACHES TO UPPER WEB AT FUSELAGE STATION 1038 LONGERON 15 RIGHT DUE TO OVERSIZED HOLES. -- FABRICATED AND INSTALLED FITTING.
- [SDR MWEA020116](https://openairdocs.org/sdr/MWEA020116.md): Spar · damaged · Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Frame/Spar/Rib
  > RIGHT PYLON AFT SPAR WEB UPPER HOLES OVERSIZED. FABRICATED AND INSTALLED SPAR WEB.
- [SDR MWEA020115](https://openairdocs.org/sdr/MWEA020115.md): Angle · oversized · Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Main Frame
  > RIGHT PYLON AFT SPAR UPPER ANGLE HAS OVERSIZE HOLES. -- FABRICATED AND INSTALLED ANGLE.
- [SDR MWEA020114](https://openairdocs.org/sdr/MWEA020114.md): Angle · oversized · Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Main Frame
  > RIGHT PYLON AFT SPAR ANGLE HAS OVERSIZE HOLE. -- FABRICATED AND INSTALLED ANGLE.
- [SDR MWEA011251](https://openairdocs.org/sdr/MWEA011251.md): Skin · cracked · Sep 8, 2001 · N209ME · Doug DC932 · Fuselage Main, Structure
  > FUSELAGE SKIN WAS CRACKED AT STATION 718 BELOW LONGERON 10 RIGHT. -- REMOVED DAMAGE, INSTALLED DOUBLERS.
- [SDR MWEA011144](https://openairdocs.org/sdr/MWEA011144.md): Engine · overtemp · Aug 22, 2001 · N209ME · Doug DC932 · Engine (Turbine/Turboprop)
  > ON TAKE OFF LEFT ENGINE REACHED 605-610 DEGREES CELSIUS AFTER V1, ABOUT 40 SECONDS AFTER TAKE OFF POWER WAS REDUCED TO BRING TEMP BACK TO 590 DEGREES CELSIUS AT A NORMAL CLIMB, POWER SETTING ENGINE TEMP WAS 545 DEGREES CELSIUS MCI TEMP 37 DEGREES CELSIUS EPR 1
- [SDR MWEA010982](https://openairdocs.org/sdr/MWEA010982.md): Solenoid Valve · inoperative · Jun 13, 2001 · N209ME · Doug DC932 · Hydraulic System, Auxiliary
  > RIGHT HYDRAULIC TEMP HI ANNUNCIATOR CAME ON DURING TAXI OUT. -- REFERENCE DMI #6-50 "ALTERNATE PUMP WILL NOT OPERATE WHEN SWITCH IS TURNED ON," REMOVED AND REPLACED ALTERNATE PUMP SOLENOID VALVE, OPERATIONAL CHECK GOOD.
- [SDR MWEA010981](https://openairdocs.org/sdr/MWEA010981.md): Servo · inoperative · Jun 12, 2001 · N209ME · Doug DC932 · Autopilot System
  > WHEN AUTOPILOT WAS ENGAGED THE AIRCRAFT ROLLED VIOLENTLY TO THE LEFT. AP WAS IMMEDIATELY DISENGAGED AND WE NOTICED A WHINING/HUMMING SOUND WHICH CONTINUED FOR REMAINDER OF THE FLIGHT. -- DEFERRED AUTOPILOT CONTROLLER PER MEL 22-05 PULLED AND COLLERED C/B'S D
- [SDR MWEA010605](https://openairdocs.org/sdr/MWEA010605.md): Floorboard · corroded · Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Floor Panel
  > FLOORBOARD A-6 HAS SEVERAL AREAS OF CORROSION ON TOP SURFACE AND CORROSION AROUND SOME OF THE FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFES AND CORROSION. FABRICATED AND INSTALLED FLOORBOARD SKIN AND HAT CHANNELS.
- [SDR MWEA010604](https://openairdocs.org/sdr/MWEA010604.md): Floorboard · corroded · Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Floor Panel
  > FLOORBOARD A-4 HAS SEVERAL AREAS OF CORROSION ON TOP SURFACE AND CORROSION AROUND SOME OF THE FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFES AND CORROSION. REMOVED CORROSION AND CHAFING. REPAIRED FLOOR PANEL IAW DC9 SRM 51-30-2 AND DRW 9915597 & SR
- [SDR MWEA010603](https://openairdocs.org/sdr/MWEA010603.md): Intercostal · damaged · Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STATION 390 LONGERON 27 RIGHT - 29 RIGHT HAS ELONGATED HOLES AND IS BENT. FABRICATED AND INSTALLED INTERCOSTAL AND INBOARD AND OUTBOARD TEE CLIPS.
- [SDR MWEA010602](https://openairdocs.org/sdr/MWEA010602.md): Intercostal · corroded · Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STATION 1018 AND RBL 15 TO 25 CORRODED AND CRACKED. REMOVED AND REPLACED INTERCOSTAL.
- [SDR MWEA010601](https://openairdocs.org/sdr/MWEA010601.md): Spar · corroded · Apr 17, 2001 · N209ME · Doug DC932 · Wing Spar
  > RIGHT WING INTERNAL AFT LOWER SPAR TEE HAD HEAVY CORROSION. FABRICATED REPAIR FILLERS, INSTALLED IAW BOEING TELEX MWX-ORD-01-00272H, DATED 03 APRIL 2001. PLACED ON WATCH ITEM 5720 FOR FINAL DISPOSITION.
- [SDR MWEA010600](https://openairdocs.org/sdr/MWEA010600.md): Intercostal · cracked · Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BETWEEN STATION 945 - 965 AT CENTERLINE OF AIRCRAFT BELOW SUPPORT IS CRACKED. REMOVED INTERCOSTAL, FABRICATED, DRILLED, AND INSTALLED NEW PART.
- [SDR MWEA010599](https://openairdocs.org/sdr/MWEA010599.md): Longeron · corroded · Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > LONGERON 28 RIGHT IS CORRODED FROM STATION 323 - 360. REMOVED DAMAGED SECTION, FABRICATED SECTION, REPAIR SPLICE, DRILLED AND INSTALLED.
- [SDR MWEA010598](https://openairdocs.org/sdr/MWEA010598.md): Floorboard · damaged · Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Floor Panel
  > FLOORBOARD A-1 HAD SEVERAL FASTENERS PULLED THRU AND CORROSION; CHAFES AROUND HAT CHANNELS. REMOVED FLOORBOARD, FABRICATED NEW FLOORBOARD, REMOVED CORROSION FROM HAT CHANNELS, FABRICATED ONE NEW HAT CHANNEL AND INSTALLED ALL.
- [SDR MWEA010597](https://openairdocs.org/sdr/MWEA010597.md): Floorboard · corroded · Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Floor Panel
  > FLOORBOARD E-9 HAD SEVERAL AREAS OF CORROSION AROUND FASTENER HOLES AND ON HAT CHANNELS. REMOVED FLOORBOARD, FABRICATED SKIN, REMOVED CORROSION FROM HAT CHANNELS, ASSEMBLED NEW SKIN AND CHANNELS.
- [SDR MWEA010596](https://openairdocs.org/sdr/MWEA010596.md): Floorboard · corroded · Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Floor Panel
  > FLOORBOARD A-5 HAD AREAS OF CORROSION AROUND HOLES AND ON HAT CHANNELS. REMOVED FLOORBOARD, FABRICATED PANEL, HAT CHANNELS, ASSEMBLED AND INSTALLED TOGETHER.
- [SDR MWEA010595](https://openairdocs.org/sdr/MWEA010595.md): Shear Tie · corroded · Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Main, Structure
  > FOUND CORROSION ON SKIN SPLICE DOUBLER AND FORWARD SIDE OF RIGHT LAV FLOORBEAM AT STATION 996. REMOVED SHEAR TIE, LOCATED, DRILLED, AND INSTALLED NEW SHEAR TIE.
- [SDR MWEA010594](https://openairdocs.org/sdr/MWEA010594.md): Spar · gouged · Apr 17, 2001 · N209ME · Doug DC932 · Wing Spar
  > REMOVED LEFT WING SPAR WEB AT TRUNNION AND FOUND GOUGES OUT OF LIMITS. FABRICATED, DRILLED AND INSTALLED NEW WEB SECTION.
- [SDR MWEA010592](https://openairdocs.org/sdr/MWEA010592.md): Fitting · gouged · Apr 17, 2001 · N209ME · Doug DC932 · Wing Miscellaneous Structure
  > FOUND DEEP GOUGES ON FITTING AT STATION XRS 353 BETWEEN STRINGER 11 AND AFT SPAR RIGHT WING. REMOVED FITTING, FABRICATED, DRILLED AND INSTALLED NEW FITTING.
- [SDR MWEA010591](https://openairdocs.org/sdr/MWEA010591.md): Clip · corroded · Apr 17, 2001 · N209ME · Doug DC932 · Wing Miscellaneous Structure
  > CORROSION FOUND ON OUTBOARD OF XCW 58 LOWER TEE CAP, HORIZONTAL LEG BETWEEN STRINGER 23. REMOVED 2 CLIPS FOR OUT OF LIMITS CORROSION. FABRICATED DRILLED AND INSTALLED NEW CLIPS.
- [SDR MWEA010590](https://openairdocs.org/sdr/MWEA010590.md): Structure · corroded · Apr 17, 2001 · N209ME · Doug DC932 · Wing Miscellaneous Structure
  > AT LEFT WING FOUND CORROSION ON LOWER TEE CAP HORIZONTAL LEG BETWEEN STRINGER 13 AND 14. REMOVED CORROSION, SUBMITTED BLENDOUTS TO BOEING AND ARE ACCEPTABLE PER TELEX MWX-ORD-01-00146H DATED 21, FEB, 2001. PLACED ON WATCH ITEM 5616 FOR REPETITIVE INSPECTION.
- [SDR MWEA010589](https://openairdocs.org/sdr/MWEA010589.md): Clip · damaged · Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous Structure
  > SEVERAL CLIPS (6) REQUIRED REPLACEMENT BETWEEN STATION 370 - 427. REMOVED CLIPS, FABRICATED AND INSTALLED NEW CLIPS.

Next page: https://openairdocs.org/deregistered/N209ME-2006-07-28/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 = 'N209ME' AND deregistration_id = 'N209ME-2006-07-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N209ME-2006-07-28/reports

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