# Service difficulty reports: N202ME, cancelled Apr 16, 2004

A list on [N202ME, cancelled Apr 16, 2004](https://openairdocs.org/deregistered/N202ME-2004-04-16.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 · 203 reports

- [SDR MWEA030474](https://openairdocs.org/sdr/MWEA030474.md): Slat Track · broken · Dec 5, 2003 · N202ME · Doug DC932 · Leading Edge Devices
  > SLATS WERE RETRACTED, THE AMBER SLAT DISAGREEMENT LIGHT STAYED ON. FOUND SLAT TRACK DOOR AT NUMBER TWO AND NUMBER THREE SLAT JUNCTION BENT AND BROKEN. REMOVED AND REPLACED SLAT TRACK DOOR.
- [SDR MWEA030401](https://openairdocs.org/sdr/MWEA030401.md): Switch · inoperative · Sep 30, 2003 · N202ME · Doug DC932 · Leading Edge Slat Position Indicating System
  > NO SLAT EXTEND LIGHT WITH SLATS OUT, SLAT DISAGREEMENT LIGHT INTERMITTENT. REMOVED AND REPLACED LEFT SLAT EXTEND SWITCH.
- [SDR MWEA030351](https://openairdocs.org/sdr/MWEA030351.md): Proximity Switch · faulty · Aug 28, 2003 · N202ME · Doug DC932 · Landing Gear Position and Warning
  > RED LEFT GEAR UNSAFE LIGHT CAME ON ALONG WITH HORN. REMOVED AND REPLACED PROXIMITY SWITCH CONTROL BOX.
- [SDR MWEA030288](https://openairdocs.org/sdr/MWEA030288.md): Fire Bottle · discharged · Jul 22, 2003 · N202ME · Doug DC932 · Fire Bottle, Fixed
  > EXTIGUISHING AGENT TWO LOW LIGHT ILLUMINATED, THERMAL BOTTLE DISCHARGED TO ZERO PSI. REMOVED AND REPLACED BOTTLE.
- [SDR MWEA020717](https://openairdocs.org/sdr/MWEA020717.md): Frame · damaged · Nov 20, 2002 · N202ME · Doug DC932 · Fuselage Main, Frame
  > FUSELAGE FRAME STATION 897 HAS 1 EACH OVERSIZED HOLE IN THE INBOARD CAP LOCATED BETWEEN LONGERON 28 RIGHT AND LONGERON 29 RIGHT HOLE MEASURES.403 INCH DIAMETER. FABRICATED AND INSTALLED BUSHING.
- [SDR MWEA020716](https://openairdocs.org/sdr/MWEA020716.md): Frame · damaged · Nov 20, 2002 · N202ME · Doug DC932 · Fuselage Main, Frame
  > THE INBOARD CAP OF FUSELAGE FRAME STATION 937 HAS ADDITIONAL HOLES LOCATED BETWEEN LONGERON 26 RIGHT AND LONGERON 26 RIGHT, WHICH MEASURES.098 INCH IN DIAMETER. PLUGGED ADDITIONAL HOLES WITH AD MATERIAL MWX-ORD-02-00349 H.
- [SDR MWEA020715](https://openairdocs.org/sdr/MWEA020715.md): Angle · dented · Nov 20, 2002 · N202ME · Doug DC932 · Fuselage Main, Frame
  > AFT BAGGAGE PIT FRAME HAS A DENT IN IT BETWEEN THE DOOR JAMB AND THE DOOR BEAM. -- FABRICATED AND INSTALLED REPAIR ANGLE.
- [SDR MWEA020714](https://openairdocs.org/sdr/MWEA020714.md): Track · corroded · Nov 20, 2002 · N202ME · DC932 · Fuselage Main, Structure
  > AFT PIT, AFT LEFT CARGO TIE-DOWN TRACK IS CORRODED OUT OF LIMITS. -- FABRICATED AND INSTALLED REPLACEMENT TRACK.
- [SDR MWEA020713](https://openairdocs.org/sdr/MWEA020713.md): Splice · corroded · Nov 19, 2002 · N202ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO BAY AFT SIDE AND BOTTOM SIDE OF FRAME HEAVILY CORRODED STATION 503 LONGERON 28 RIGHT TO 28 LEFT. -- CUT AND REMOVED CORRODED SECTION OF FRAME AND INSTALLED Z FRAME REPAIR SPLICE.
- [SDR MWEA020712](https://openairdocs.org/sdr/MWEA020712.md): Pan · corroded · Nov 19, 2002 · N202ME · Doug DC932 · Fuselage Main, Frame
  > AFT PIT DOOR JAMB PAN HAS AREAS OF CORROSION. -- REMOVED AND REPLACED PAN AND SPLICE PLATE.
- [SDR MWEA020708](https://openairdocs.org/sdr/MWEA020708.md): Door Frame · damaged · Nov 19, 2002 · N202ME · Doug DC932 · Fuselage Main, Structure
  > AFT CARGO DOOR LOWER JAMB HAS NR 40 SIZE HOLES AROUND MULTIPLE BLIND NUTS FASTENER HOLES. REMOVED AND INSTALLED NEW JAMB.
- [SDR MWEA020698](https://openairdocs.org/sdr/MWEA020698.md): Web · corroded · Nov 18, 2002 · N202ME · Doug DC932 · Fuselage Main, Frame
  > AFT DOOR JAMB PAM WEB HAS AREAS OF CORROSION. -- REMOVED AND INSTALLED NEW WEB.
- [SDR MWEA020693](https://openairdocs.org/sdr/MWEA020693.md): Doubler · cracked · Nov 14, 2002 · N202ME · Doug DC932 · Fuselage Main, Structure
  > FORWARD CARGO BAY SUBFLOOR CRACKED NEXT TO CARGO DOOR FORWARD HINGE ATTACH POINT. -- FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA020692](https://openairdocs.org/sdr/MWEA020692.md): Intercostal · corroded · Nov 14, 2002 · N202ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL IN FORWARD BAG PIT HAS CORROSION ON FLANGE AT STATION 484-503 LONGERON 27-28 LEFT. -- FORMED AND INSTALLED NEW INTERCOSTAL.
- [SDR MWEA020691](https://openairdocs.org/sdr/MWEA020691.md): Longeron · corroded · Nov 14, 2002 · N202ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO BAY CORRODED AROUND FASTENERS IN LONGERON 30 STATION 520-524. -- REMOVED AND REPLACED LONGERON SECTION AND INSTALLED FORWARD AND AFT LONGERON SPLICE.
- [SDR MWEA020669](https://openairdocs.org/sdr/MWEA020669.md): Longeron · tool damage · Nov 6, 2002 · N202ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > STATION 598 T ANGLE AT LONGERON 17 LEFT HAS TWO DRILL STARTS JX6. -- REMOVED T ANGLE, BLENDED OUT TOOLING DAMAGE, FABRICATED AND INSTALLED NEW T ANGLE.
- [SDR MWWA020519](https://openairdocs.org/sdr/MWWA020519.md): Door · corroded · Aug 29, 2002 · N202ME · Doug DC932 · Galley Doors
  > GALLEY DOOR SILL DRAIN SKIN DOUBLER CORRODED BEYOND LIMITS. -- LOCATED AND DRILLED NEW 23 DOUBLER.
- [SDR MWEA020262](https://openairdocs.org/sdr/MWEA020262.md): Microphone · dirty · Apr 17, 2002 · N202ME · Doug DC932 · Audio Integrating System
  > COMMUNICATIONS INTERMITTENT. -- FOUND CAPTAIN'S AND FIRST OFFICER'S MICROPHONE JACKS DIRTY. REMOVED AND REPLACED BOTH MICROPHONE JACKS IAW MM 20-50-01.
- [SDR MWEA011368](https://openairdocs.org/sdr/MWEA011368.md): Skin · inoperative · Sep 30, 2001 · N202ME · Doug DC932 · Nose/Tail Landing Gear
  > WHEN GEAR RETRACTED, FORWARD RIGHT NOSE GEAR DOOR WOULD NOT CLOSE. 4 FOOT CABLE PULLED OUT OF SWAGGED END FOR DOOR. -- REMOVED AND REPLACED UPPER STRANDED WIRE DOOR STOP CABLE ASSY. MAINTENANCE FOUND GOUGE LOCATED ON RIGHT FORWARD NOSE LANDING GEAR DOOR INNE
- [SDR MWEA011129](https://openairdocs.org/sdr/MWEA011129.md): Shear Tie · cracked · Aug 16, 2001 · N202ME · Doug DC932 · Fuselage Main, Structure
  > SHEAR TIE AT STATION 945 LEFT SIDE BETWEEN LONGERON 16 AND 14 CRACKED IN RADIUS 2 PLACES. -- FABRICATED AND INSTALLED SHEAR TIE.
- [SDR MWEA011128](https://openairdocs.org/sdr/MWEA011128.md): Frame · misdrilled · Aug 16, 2001 · N202ME · Doug DC932 · Fuselage Main, Structure
  > TWO MISDRILLED HOLES AT STATION 945 LONGERON 14 LEFT ON FRAME. -- FABRICATED AND INSTALLED REPAIR ANGLES.
- [SDR MWEA011127](https://openairdocs.org/sdr/MWEA011127.md): Stop · cracked · Aug 16, 2001 · N202ME · Doug DC932 · Fuselage Main, Structure
  > REMOVE FORWARD CARGO JAMB, LOWER TWO CARGO DOOR STOPS TO FOM. -- MAINTENANCE FOUND FORWARD STOP TO BE CRACKED. REMOVED AND REPLACED NEW STOP.
- [SDR MWEA011117](https://openairdocs.org/sdr/MWEA011117.md): Pan · gouged · Aug 9, 2001 · N202ME · Doug DC932 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR JAMB PAN IS GOUGED APPROXIMATELY 10" AFT OF THE LOWER AFT DOOR STOP. -- BLENDED GOUGE, LOCATED AND INSTALLED NEW LOWER PAN.
- [SDR MWEA011116](https://openairdocs.org/sdr/MWEA011116.md): Door Frame · cracked · Aug 9, 2001 · N202ME · Doug DC932 · Fuselage Miscellaneous Structure
  > CRACK APPROXIMATELY 3/4 INCH LONG FOUND ON FORWARD CARGO DOOR JAMB JUST AFT OF AFT BOTTOM STOP SCREW HOLE. REMOVED, LOCATED AND INSTALLED NEW JAMB.
- [SDR MWEA011094](https://openairdocs.org/sdr/MWEA011094.md): Support Bracket · cracked · Aug 2, 2001 · N202ME · Doug DC932 · Spoilers
  > RIGHT WING OUTBOARD SPOILER TORSION BAR SUPPORT BRACKET IS CRACKED. -- REMOVED SUPPORT BRACKET, INSTALLED NEW SUPPORT BRACKET.
- [SDR MWEA011093](https://openairdocs.org/sdr/MWEA011093.md): Pan · torn · Aug 2, 2001 · N202ME · Doug DC932 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR INNER PAN IS TORN BY A BN FASTENER AT THE AFT END AT BEAM #3. -- REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR. DOUBLER.
- [SDR MWEA011092](https://openairdocs.org/sdr/MWEA011092.md): Longeron · cracked · Aug 2, 2001 · N202ME · Doug DC932 · Fuselage Main, Structure
  > LONGERON 17 CRACKED AT STATION 965 LEFT SIDE VIEWABLE WITH MIRROR ON BOTTOM SIDE. -- REMOVED DAMAGED LONGERON SECTION, FABRICATED NEW SECTION AND LONGERON SPLICE, INSTALLED LONGERON ASSOCIATED ITEMS AND LONGERON SPLICE.
- [SDR MWEA011079](https://openairdocs.org/sdr/MWEA011079.md): Shear Tie · cracked · Jul 30, 2001 · N202ME · Doug DC932 · Fuselage Main, Structure
  > SHEAR TIE CRACKED AT STATION 945 BETWEEN LONGERON 14 AND 15 RIGHT SIDE. -- REMOVED SHEAR TIE SECTION, FABRICATED NEW SECTION AND SHEAR TIE SPLICE, INSTALLED NEW SHEAR TIE SECTION AND SPLICE.
- [SDR MWEA011078](https://openairdocs.org/sdr/MWEA011078.md): Rib · cracked · Jul 30, 2001 · N202ME · Doug DC932 · Wing, Attach Fittings
  > LEFT WING #3 SLAT DRIVER OUTBOARD FITTING HAS A SMALL 1/8" CRACK ACROSS THE SIDE TO SIDE GUIDE ROLLER LOBE. -- REMOVED CRACKED RIB, LOCATED BOTH INBOARD AND OUTBOARD FITTING, INSTALLED RIB.
- [SDR MWEA001252](https://openairdocs.org/sdr/MWEA001252.md): Thermostat · inoperative · Dec 20, 2000 · N202ME · Doug DC932 · Pneumatic Indicating System
  > DURING CLIMBOUT WITH CLIMB POWER, FULL ANTI-ICE "ON" RIGHT ICE PROTECT TEMP HIGH ANNUNCIATOR ILLUMINATED. QRH PROCEDURE TURNED OFF LIGHT IN ABOUT 1 MINUTE. -- PERFORMED RESISTANCE CHECK ON ELECTRONIC THERMO SWITCH NO DEFECTS NOTED. FOUND RIGHT ICE PROTECTIO
- [SDR MWEA001245](https://openairdocs.org/sdr/MWEA001245.md): Fairing · cracked · Dec 13, 2000 · N202ME · Doug DC932 · Vertical Stabilizer
  > RH VERTICAL STAB SKIN UNDER AFT LOWER HORIZONTAL STAB FAIRING IS CRACKED. -- REPLACED SKIN.
- [SDR MWEA001193](https://openairdocs.org/sdr/MWEA001193.md): Harness · faulty · Nov 17, 2000 · N202ME · Doug DC932 · Hydraulic System, Auxiliary
  > ON TAXI OUT AUXILIARY HYDRAULIC PUMP CIRCUIT BREAKERS TRIPPED. REPLACED AUX PUMP WIRING HARNESS.
- [SDR MWEA001175](https://openairdocs.org/sdr/MWEA001175.md): Web · cracked · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Miscellaneous Structure
  > LEFT HAND SUB FLOOR WEB CRACKED AT STATION 605 OUTBOARD OF POWER FEEDER CABLES, INBOARD EDGE OF LIGHTING HOLE. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA001182](https://openairdocs.org/sdr/MWEA001182.md): Web · cracked · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Miscellaneous Structure
  > LEFT HAND SUBFLOOR WEB CRACKED AT STATION 605 OUTBOARD OF POWER FEEDER CABLES. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA001181](https://openairdocs.org/sdr/MWEA001181.md): Floorboard · corroded · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Floor Panel
  > FLOORBOARD BETWEEN NR 3 AND 4 SEAT TRACK HAS CORROSION AT FORWARD ENGINE STATION 237. FABRICATED AND INSTALLED NEW SKIN.
- [SDR MWEA001180](https://openairdocs.org/sdr/MWEA001180.md): Floorbeam · corroded · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Main, Floor Beam
  > FLOORBEAM AT STATION 980 HAS LIGHT CORROSION AROUND FASTENER HOLE LEFT HAND SIDE 15 INCHES INBOARD OF FRAME. FABRICATED AND INSTALLED ANGLE REPAIR.
- [SDR MWEA001179](https://openairdocs.org/sdr/MWEA001179.md): Intercostal · cracked · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED AT CANTED FRAME STATION 1168 AT APPROXIMATELY LONGERON 10 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA001178](https://openairdocs.org/sdr/MWEA001178.md): Frame · cracked · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Main, Frame
  > FRAME 942 IN BETWEEEN LONGERON 15 AND 16 RIGHT HAND SIDE SHEAR TIE FOR FRAME IS CRACKED. FABRICATED AND INSTALLED SHEAR TIE.
- [SDR MWEA001177](https://openairdocs.org/sdr/MWEA001177.md): Web · cracked · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Miscellaneous Structure
  > RIGHT HAND SUBFLOOR WEB CRACKED AT STATION 610. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA001176](https://openairdocs.org/sdr/MWEA001176.md): Longeron · damaged · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FORWARD ENTRY LONGERON 8 RIGHT HAND AREA HAS AREAS OF MECHANICAL DAMAGE STATION 190 - 194. FABRICATED AND INSTALLED REPAIR SPLICES AND REPLACEMENT SECTION OF LONGERON.
- [SDR MWEA001174](https://openairdocs.org/sdr/MWEA001174.md): Floorboard · cracked · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Floor Panel
  > FLOORBOARD B6 HAS TWO CRACKED HAT CHANNELS. REMOVED AND REPLACED HAT CHANNEL.
- [SDR MWEA001173](https://openairdocs.org/sdr/MWEA001173.md): Frame · cracked · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Main, Frame
  > FUSELAGE FRAME AT STATION 980 IS CRACKED ON AFT SIDE ABOVE LONGERON 16 RIGHT AND BELOW LONGERON 14 RIGHT. FABRICATED AND INSTALLED NEW FORMER.
- [SDR MWEA001172](https://openairdocs.org/sdr/MWEA001172.md): Floorboard · gouged · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Floor Panel
  > FLOORBOARD B9 FORWARD END HAS 3 FASTENER HOLES GOUGED FROM WASHERS. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA001171](https://openairdocs.org/sdr/MWEA001171.md): Floorboard · damaged · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Floor Panel
  > FLOORBOARD B3 HAS A HOLE IN THE OUTBOARD AFT CORNER. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA001170](https://openairdocs.org/sdr/MWEA001170.md): Floorboard · chafed · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Floor Panel
  > FLOORBOARD F5 SKIN IS TORN AND NUMEROUS FASTENER HOLES ARE CHAFED. FABRICATED AND INSTALLED NEW FLOORBOARD.
- [SDR MWEA001169](https://openairdocs.org/sdr/MWEA001169.md): Floorboard · gouged · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Floor Panel
  > FLOORBOARD A5 HAS GOUGES AROUND 3 FASTENER HOLES. FABRICATED AND INSTALLED SKIN DOUBLER.
- [SDR MWEA001168](https://openairdocs.org/sdr/MWEA001168.md): Floorboard · damaged · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Floor Panel
  > FLOORBOARD B5 HAS ONE END WITH NUMEROUS FASTENER HOLES DAMAGED BY THE LARGE AREA BEAUTY WASHERS. FABRICATED AND INSTALLED FLOOR PANEL.
- [SDR MWEA001167](https://openairdocs.org/sdr/MWEA001167.md): Floorboard · cracked · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Floor Panel
  > FLOORBOARD E8 HAS TWO HAT CHANNELS WITH CRACKED ENDS. FABRICATED AND INSTALLED NEW HAT CHANNELS.
- [SDR MWEA001166](https://openairdocs.org/sdr/MWEA001166.md): Floorboard · mismanufactured · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Floor Panel
  > FLOORBOARD E9 HAS ONE END WITH TOO LITTLE OR NO EDGE DISTANCE FOR THE FASTENER HOLES. FABRICATED AND INSTALLED NEW PANELS.
- [SDR MWEA001162](https://openairdocs.org/sdr/MWEA001162.md): Shear Tie · cracked · Nov 16, 2000 · N202ME · Doug DC932 · Fuselage Main, Structure
  > SHEAR TIE CRACKED AT STATION 1019 BELOW LONGERON 14 LEFT. FABRICATED AND INSTALLED NEW SHEAR TIE SPLICE.

Next page: https://openairdocs.org/deregistered/N202ME-2004-04-16/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 = 'N202ME' AND deregistration_id = 'N202ME-2004-04-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N202ME-2004-04-16/reports

---
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