# Service difficulty reports: N501ME, cancelled Jun 3, 2004

A list on [N501ME, cancelled Jun 3, 2004](https://openairdocs.org/deregistered/N501ME-2004-06-03.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 6 · 266 reports

- [SDR MWEA040024](https://openairdocs.org/sdr/MWEA040024.md): Engine · vibration · Mar 12, 2004 · N501ME · Doug DC932 · Engine (Turbine/Turboprop)
  > LEFT ENGINE VIBRATION. COMPLIED WITH VIBRATON TEST, INLET HAS A VIBRATION OF 1.0 MILS, TEST 1 VIBRATION CHECKED OK FOR SERVICE.
- [SDR MWEA040018](https://openairdocs.org/sdr/MWEA040018.md): Smoke Detector · false indication · Feb 19, 2004 · N501ME · Doug DC932 · Smoke Detection
  > LEFT LAVATORY SMOKE DETECTOR WENT OFF. INSPECTED LAVATORY COMPARTMENT, LIGHTING SOCKETS, LAVATORY TIMER, WATER HEATER, TRASH COMPARTMENT AND CYCLED LAVATORY MOTOR. REMOVED AND REPLACED SMOKE DETECTOR.
- [SDR MWEA030500](https://openairdocs.org/sdr/MWEA030500.md): Bulkhead · cracked · Dec 31, 2003 · N501ME · Doug DC932 · Fuselage Main, Bulkhead
  > LOWER LT VENTRAL DOOR CORNER WEB IS CRACKED. INSTALLED DOUBLERS TO BOTH LOWER DOOR CORNERS OF THE AFT PRESSURE BULKHEAD.
- [SDR MWEA030305](https://openairdocs.org/sdr/MWEA030305.md): Transceiver · inoperative · Aug 7, 2003 · N501ME · Doug DC932 · VHF Communications System
  > UNABLE TO TRANSMIT ON NUMBER ONE COMMUNICATION. REMOVED AND REPLACED NUMBER ONE COMMUNICATION TRANCEIVER.
- [SDR MWEA030198](https://openairdocs.org/sdr/MWEA030198.md): Heater · inoperative · Apr 30, 2003 · N501ME · Doug DC932 · Pitot/Static Anti-Ice System
  > AUX PITOT HEAT SHOWS NO AMPS AND PITOT STALL HEATER ANNUNCIATOR LIGHT CAME ON. REMOVED AND REPLACED AUX PITOT TUBE.
- [SDR MWEA030174](https://openairdocs.org/sdr/MWEA030174.md): Smoke Detector · defective · Apr 11, 2003 · N501ME · Doug DC932 · Smoke Detection
  > RIGHT LAVATORY SMOKE ALARM WENT OFF DURING PUSHBACK. INSPECTED AFT ACCESSARY AND APU COMPARTMENT FOR EVIDENCE OF LEAKAGE, NONE FOUND. REMOVED AND REPLACED RIGHT SMOKE DETECTOR.
- [SDR MWEA030137](https://openairdocs.org/sdr/MWEA030137.md): Stall Warning · failed · Mar 21, 2003 · N501ME · Doug DC932 · Stall Warning System
  > STALL INDICATING FAILURE LIGHT CAME ON. -- REMOVED AND REPLACED #2 STALL WARNING COMPUTER.
- [SDR MWEA020719](https://openairdocs.org/sdr/MWEA020719.md): Switch · defective · Nov 22, 2002 · N501ME · Doug DC932 · Airfoil Anti/De-ice System
  > AFTER LEFT ENGINE START LEFT AIRFOIL ICE PROTECTION TEMPERATURE LIGHT CAME ON. -- REMOVED AND REPLACED ELECTRONIC THERMAL SWITCH CONTROL.
- [SDR MWEA020603](https://openairdocs.org/sdr/MWEA020603.md): Latch · broken · Sep 25, 2002 · N501ME · Doug DC932 · Passenger/Crew Doors
  > LAV SERVICE DOOR TOP AFT LATCH SURFACE BROKEN (AIRCRAFT SIDE). -- TRIMMED OUT DAMAGE TO DOUBLER, FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA020411](https://openairdocs.org/sdr/MWEA020411.md): Longeron · cracked · Jun 17, 2002 · N501ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > AFT ACCESSORY COMPARTMENT LONGERON 2 RIGHT HAS A CRACK AT STATION 1076. FABRICATED AND INSTALLED LONGERON SPLICE REPAIR.
- [SDR MWEA020410](https://openairdocs.org/sdr/MWEA020410.md): Attach Angle · cracked · Jun 17, 2002 · N501ME · Doug DC932 · Fuselage, Stabilizer Attach Fittings
  > A.5 INCH CRACK IN RIGHT SIDE VERTICAL TO FUSELAGE ATTACH ANGLE AT STATION 1130, APPROXIMATELY 1 FOOT FORWARD OF RUDDER TORQUE TUBE. FABRICATED AND INSTALLED SPLICE, STRAP AND FILTER.
- [SDR MWEA020409](https://openairdocs.org/sdr/MWEA020409.md): Frame · corroded · Jun 17, 2002 · N501ME · Doug DC932 · Fuselage Main, Frame
  > FORWARD PIT MODERATE CORROSION AT LONGERON 30 ON LOWER FLANGE OF FRAME 446. FABRICATED, INSTALLED NEW FRAME SECTION AND SPLICES.
- [SDR MWEA020406](https://openairdocs.org/sdr/MWEA020406.md): Shear Tie · cracked · Jun 17, 2002 · N501ME · Doug DC932 · Fuselage Main, Bulkhead
  > AFT ACCESSORY COMPARTMENT BULKHEAD FRAME STATION 1038 SHEAR TIE IS CRACKED JUST ABOVE LONGERON 18 LEFT. -- REMOVED SHEAR TIE SEGMENT. FABRICATED AND INSTALLED SHEAR TIE SEGMENT AND CLIPS.
- [SDR MWEA020405](https://openairdocs.org/sdr/MWEA020405.md): Frame · Jun 17, 2002 · N501ME · Doug DC932 · Fuselage Main, Frame
  > CANTED FRAME STATION 1132 FRAME IS CRACKED AND CORRODED APPROXAMITLY 8 INCHES RIGHT OF UPPER FUSELAGE CENTERLINE. -- REMOVED DAMAGE FRAME SECTION. FABRICATED FILLERS AND STACKED ANGLES.
- [SDR MWEA020413](https://openairdocs.org/sdr/MWEA020413.md): Shear Tie · damaged · Jun 17, 2002 · N501ME · Doug DC932 · Fuselage Main, Structure
  > FORWARD CARGO COMPARTMENT FRAME STATION 446 SHEAR TIE HAS NUMEROUS ELONGATED FASTENER HOLES LOCATED BETWEEN LONGERON 28 LEFT AND 26 RIGHT. FABRICATED AND INSTALLED FORMERS.
- [SDR MWEA020412](https://openairdocs.org/sdr/MWEA020412.md): Shear Tie · cracked · Jun 17, 2002 · N501ME · Doug DC932 · Fuselage Main, Structure
  > AFT ACCESSORY COMPARTMENT FRAME STATION 1019. DOUBLER HAS A CRACK LOCATED BELOW LONGERON 14 LEFT. FABRICATED AND INSTALLED FORMER.
- [SDR MWEA020408](https://openairdocs.org/sdr/MWEA020408.md): Longeron · cracked · Jun 17, 2002 · N501ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > AFT ACCESSORY COMPARTMENT LONGERON 2 LEFT AND HAS A CRACK AT STATION 1076. REMOVED DAMAGED SECTION 2 LEFT, FABRICATED, INSTALLED LONGERON. INSTALLED REPAIR SPLICE.
- [SDR MWEA020416](https://openairdocs.org/sdr/MWEA020416.md): Longeron · dented · Jun 17, 2002 · N501ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > AT STATION 484 LONGERON 19 RIGHT HAS A DENT BEYOND LIMITS PER SRM 53-04. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA020415](https://openairdocs.org/sdr/MWEA020415.md): Doubler · corroded · Jun 17, 2002 · N501ME · Doug DC932 · Fuselage Main, Plate/Skin
  > FUSELAGE INTERNAL SKIN DOUBLER SHOWS SIGNS OF EXFOLIATION CORROSION AT STATION 996 - 1019. REMOVED INTERNAL DOUBLER AND SKIN. FABRICATED AND INSTALLED INTERNAL DOUBLER AND INSTALLED NEW SKIN.
- [SDR MWEA020414](https://openairdocs.org/sdr/MWEA020414.md): Panel · corroded · Jun 17, 2002 · N501ME · Doug DC932 · Fuselage Main, Plate/Skin
  > CORROSION ON LEFT LOWER DIAMOND PANEL FORWARD OF MAIN LANDING GEAR. FABRICATED AND INSTALLED FILLER.
- [SDR MWEA020391](https://openairdocs.org/sdr/MWEA020391.md): Stringer Clip · corroded · Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Miscellaneous Structure
  > AFT ACCESSORY COMPARTMENT LONGERON 22 CLIP RIGHT HAS LIGHT CORROSION, LOCATED JUST FORWARD OF CANTED FRAME STATION 1121. REMOVED AND REPLACED END FITTING.
- [SDR MWEA020403](https://openairdocs.org/sdr/MWEA020403.md): Frame · corroded · Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT FRAME STATION 870 HAS LIGHT CORROSION AROUND LONGERON 30 ATTACH BOLTS. CUT OUT DAMAGED AREA OF FRAME AND INSTALLED REPAIR PARTS.
- [SDR MWEA020402](https://openairdocs.org/sdr/MWEA020402.md): Frame · corroded · Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Frame
  > LIGHT CORROSION ON AFT FACE OF FORWARD FRAME 237 FROM LONGERON 29 LEFT TO 26 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLERS.
- [SDR MWEA020401](https://openairdocs.org/sdr/MWEA020401.md): Frame · corroded · Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Frame
  > MODERATE CORROSION ON AFT FACE OF FORWARD FRAME 332 AT LONGERON 30, 29, & 28 RIGHT. REMOVED AND REPLACED FRAME SECTION REPAIR.
- [SDR MWEA020400](https://openairdocs.org/sdr/MWEA020400.md): Skin · corroded · Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Plate/Skin
  > AFT ACCESSORY COMPARTMENT SKIN HAS HEAVY CORROSION ON SKIN AT STATION 1009 BETWEEN LONGERON 18 AND 19 RIGHT. FABRICATED AND INSTALLED DOUBLER, FAIRING PLATE, AND SHIMS.
- [SDR MWEA020399](https://openairdocs.org/sdr/MWEA020399.md): Web · torn · Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Miscellaneous Structure
  > WEB BELOW LEFT AFT OVERWING EMERGENCY EXIT DOOR HAS A LARGE HOLE/TEAR IN IT. -- REMOVED AND REPLACED WEB.
- [SDR MWEA020398](https://openairdocs.org/sdr/MWEA020398.md): Shear Tie · cracked · Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Miscellaneous Structure
  > AFT ACCESSORY COMPARTMENT FRAME STATION 1059 SHEAR TIE IS CRACKED BELOW LONGERON 15 RIGHT. -- FABRICATED AND INSTALLED SHEAR TIE.
- [SDR MWEA020397](https://openairdocs.org/sdr/MWEA020397.md): Longeron · dented · Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > A SERIES OF SMALL DENTS BETWEEN STATION 851-889, LONGERONS 24 & 25 RIGHT. (REFERENCE CO #6277) -- FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA020396](https://openairdocs.org/sdr/MWEA020396.md): Door Frame · chafed · Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Structure
  > AFT RIGHT EMERGENCY EXIT DOOR JAMB IS CHAFED AT UPPER LATCH ASSY. LOCATED, DRILLED AND INSTALLED DOUBLER.
- [SDR MWEA020395](https://openairdocs.org/sdr/MWEA020395.md): Door Frame · chafed · Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Structure
  > RIGHT FORWARD EMERGENCY EXIT DOOR JAMB IS CHAFED AT THE TOP LATCH. LOCATED, DRILLED, AND INSTALLED DOUBLER.
- [SDR MWEA020394](https://openairdocs.org/sdr/MWEA020394.md): Longeron · corroded · Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > AFT ACCESSORY COMPARTMENT LONGERON 19 LEFT HAS AREAS OF LIGHT CORROSION UNDER FLANGES ON TOP AND BOTTOM SIDE FROM STATION 1080 TO CANTED FRAME 1121. MANUFACTURED AND INSTALLED LONGERON.
- [SDR MWEA020393](https://openairdocs.org/sdr/MWEA020393.md): Longeron · corroded · Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > AFT ACCESSORY COMPARTMENT LONGERON 21 LEFT HAS LIGHT CORROSION UNDER BOTTOM FLANGE AT STATION 1080. REMOVED AND REPLACED LONGERON SECTION.
- [SDR MWEA020392](https://openairdocs.org/sdr/MWEA020392.md): Skin · corroded · Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Plate/Skin
  > AFT ACCESSORY COMPARTMENT, SKIN BELOW LONGERON 18 LEFT STATION 1086 TO CANTED FRAME 1121 HAS CORROSION ON INNER SURFACE. FABRICATED AND INSTALLED SKIN.
- [SDR MWEA020390](https://openairdocs.org/sdr/MWEA020390.md): Fitting · worn · Jun 4, 2002 · N501ME · Doug DC932 · Leading Edge Devices
  > #5 SLAT INBOARD SADDLE FITTING BUSHINGS WORN. -- REMOVED AND REPLACED RIB.
- [SDR MWEA020389](https://openairdocs.org/sdr/MWEA020389.md): Web · punctured · Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Miscellaneous Structure
  > COCKPIT SUBFLOOR AT STATION 134 APPROXIMATELY 24 INCHES RIGHT OF THE AIRCRAFT CENTERLINE IS PUNCTURED. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA020388](https://openairdocs.org/sdr/MWEA020388.md): Doubler · chafed · Jun 4, 2002 · N501ME · Doug DC932 · Passenger/Crew Doors
  > FORWARD PASSENGER DOOR HANDLE CHAFING ON DOUBLER AROUND HANDLE CUTOUT. REMOVED AND REPLACED DOUBLER.
- [SDR MWEA020387](https://openairdocs.org/sdr/MWEA020387.md): Longeron · corroded · Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > AFT ACCESSORY COMPARTMENT LONGERON 15 LEFT HAS LIGHT CORROSION UNDER TOP FLANGE AT STATION 1076. REMOVED AND REPLACED LONGERON SECTION AND SPLICE.
- [SDR MWEA020383](https://openairdocs.org/sdr/MWEA020383.md): Retainer · cracked · May 24, 2002 · N501ME · Doug DC932 · Flight Compartment Windows
  > RIGHT WINDOW RETAINER HAS A CRACK INDICATION IN THE TITANIUM DOUBLER. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA020382](https://openairdocs.org/sdr/MWEA020382.md): Attach Fitting · cracked · May 24, 2002 · N501ME · Doug DC932 · Trailing Edge Flaps
  > RIGHT FLAP #3 TRAILING EDGE PANEL UPPER INBOARD ATTACH FITTING CRACKED. -- REMOVED AND REPLACED FITTING.
- [SDR MWEA020381](https://openairdocs.org/sdr/MWEA020381.md): Skin · damaged · May 24, 2002 · N501ME · Doug DC932 · Rudder, Plate/Skin
  > LEFT SIDE OF RUDDER 5 INCHES AFT OF FORWARD SPAR BETWEEN ZR 117 AND ZR 113 HAS CREASE 2.5 INCHES LONG. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA020380](https://openairdocs.org/sdr/MWEA020380.md): Pressure Panel · gouged · May 24, 2002 · N501ME · Doug DC932 · Fuselage Main, Bulkhead
  > CENTER WING FORWARD LOWER BULKHEAD WEB HAS 1 VERY DEEP GOUGE ON FORWARD SURFACE AT STATION 606 & LONGERON 25 LEFT. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA020370](https://openairdocs.org/sdr/MWEA020370.md): Pan · cracked · May 21, 2002 · N501ME · Doug DC932 · Cargo/Baggage Doors
  > AFT CARGO DOOR INNER PAN CRACKED AT AFT LOCKING CAM. -- FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA020375](https://openairdocs.org/sdr/MWEA020375.md): Fitting · cracked · May 21, 2002 · N501ME · Doug DC932 · Fuselage Miscellaneous Structure
  > CENTER WING FORWARD LOWER BULKHEAD FITTING CRACKED AT STATION 606 AND LONGERON 24 LEFT. REMOVED AND REPLACED FITTING.
- [SDR MWEA020369](https://openairdocs.org/sdr/MWEA020369.md): Longeron · cracked · May 21, 2002 · N501ME · Doug DC932 · Fuselage Main, Structure
  > LONGERON 17 RIGHT IS CRACKED UNDER FRAME 484. -- FABRICATED AND INSTALLED LONGERON SECTION AND REPAIR SPLICE.
- [SDR MWEA020368](https://openairdocs.org/sdr/MWEA020368.md): Pan · chafed · May 21, 2002 · N501ME · Doug DC932 · Cargo/Baggage Doors
  > AFT CARGO DOOR INNER PAN HAS A DEEP CHAFE NEXT TO AFT LOCK CAM. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA020367](https://openairdocs.org/sdr/MWEA020367.md): Fitting · cracked · May 21, 2002 · N501ME · Doug DC932 · Wing, Rib/Bulkhead
  > CENTER WING FORWARD LOWER BULKHEAD FITTING CRACKED AT STATION 606 AND LONGERON 24 RIGHT. -- REMOVED AND INSTALLED FITTING.
- [SDR MWEA020365](https://openairdocs.org/sdr/MWEA020365.md): Web · cracked · May 21, 2002 · N501ME · Doug DC932 · Fuselage Main, Bulkhead
  > AFT ACCESSORY COMPARTMENT BULKHEAD WEB AT FRAME STATION 1038 IS CRACKED AT LIGHTNING HOLE AT LONGERON 12 LEFT. -- FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA020224](https://openairdocs.org/sdr/MWEA020224.md): Skin · corroded · Apr 8, 2002 · N501ME · Doug DC932 · Trailing Edge Flaps
  > LEFT FLAP LOWER SKIN HAS A SMALL AREA OF CORROSION ABOUT 20 INCHES OUTBOARD OF INBOARD FLAP HINGE. FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLERS.
- [SDR MWEA011460](https://openairdocs.org/sdr/MWEA011460.md): Web · cracked · Nov 22, 2001 · N501ME · Doug DC932 · Fuselage Miscellaneous Structure
  > RIGHT HAND WEB IN AFT ACCESSORY COMPARTMENT HAS A CRACK EXTENDING FROM LIGHTENING HOLE JUST OF STRINGER 11 AT STATION 1038. INSTALLED DOUBLER IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 53-01 FIGURE 2, SHEET 3.
- [SDR MWEA011361](https://openairdocs.org/sdr/MWEA011361.md): Doubler · dented · Sep 27, 2001 · N501ME · Doug DC932 · Fuselage Main, Structure
  > SKIN DENTED AT STATION 330, LONGERON 26 APPROXIMATELY 1 1/4 INCH BY.046 DEEP RIGHT HAND SIDE. -- REMOVED DAMAGE, INSTALLED INTERNAL DOUBLER AND FLUSH PLUG.

Next page: https://openairdocs.org/deregistered/N501ME-2004-06-03/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 = 'N501ME' AND deregistration_id = 'N501ME-2004-06-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N501ME-2004-06-03/reports

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