# Service difficulty reports: N80ME, cancelled Jan 3, 2003

A list on [N80ME, cancelled Jan 3, 2003](https://openairdocs.org/deregistered/N80ME-2003-01-03.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 4 · 170 reports

- [SDR MWEA010034](https://openairdocs.org/sdr/MWEA010034.md): Relay · failed · Jan 4, 2001 · N80ME · Doug DC914 · Airfoil Anti/De-ice System
  > WHILE USING AIRFOIL ANTI-ICE LEFT HAND ICE PROTECTION TEMPERATURE HI ANNUNCIATOR ILLUMINATED. AFTER SECURING SYSTEM, RH ICE PROTECTION TEMP. HI ILLUMINATED. SECURED THE SYSTEM. -- PERFORMED SYSTEM TESTS ON RIGHT HAND AND LEFT HAND SIDES. ALL TESTS WERE WI
- [SDR MWEA001140](https://openairdocs.org/sdr/MWEA001140.md): Pan · gouged · Nov 7, 2000 · N80ME · Doug DC914 · Cargo/Baggage Doors
  > FORWARD BAG PIT DOOR JAMB AREA AFT BOTTOM CORNER HAS A DEEP GOUGE. REMOVED AND REPLACED PAN AND SPLICE PLATES.
- [SDR MWEA001139](https://openairdocs.org/sdr/MWEA001139.md): Floor Support · corroded · Nov 7, 2000 · N80ME · Doug DC914 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STATION 200 BETWEEN NR 2 TRACK AND CENTER SUPPORT HAS CORROSION AROUND/UNDER FOUR FASTENER HOLES. FABRICATED AND INSTALLED FLOOR SUPPORT.
- [SDR MWEA001138](https://openairdocs.org/sdr/MWEA001138.md): Beam · cracked · Nov 7, 2000 · N80ME · Doug DC914 · Cargo/Baggage Doors
  > AFT CARGO DOOR NR 2 BEAM END FITTING IS CRACKED AT AFT END OF DOOR. REMOVED AND REPLACED BEAM END FITTING.
- [SDR MWEA001137](https://openairdocs.org/sdr/MWEA001137.md): Intercostal · cracked · Nov 7, 2000 · N80ME · Doug DC914 · Cargo/Baggage Doors
  > AFT CARGO DOOR CENTER UPPER INTERCOSTAL END FITTING IS CRACKED ON THE AFT SIDE. FABRICATED AND INSTALLED INTERCOSTAL END FITTING.
- [SDR MWEA001136](https://openairdocs.org/sdr/MWEA001136.md): Fitting · cracked · Nov 7, 2000 · N80ME · Doug DC914 · Cargo/Baggage Doors
  > AFT CARGO DOOR NR 5 BEAM END FITTING IS CRACKED AT FORWARD OF DOOR. REMOVED AND REPLACED END FITTING.
- [SDR MWEA001135](https://openairdocs.org/sdr/MWEA001135.md): Doubler · cracked · Nov 7, 2000 · N80ME · Doug DC914 · Cargo/Baggage Doors
  > FOUND REPAIR AT AFT CARGO DOOR LOWER AFT CORNER STARTING AT CUTOUT GOING AFT 5 INCHES PAST STATION 766. REPAIR IS ATTACHED TO LONGERON 26 AND 25 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLERS AND SHIMS.
- [SDR MWEA001134](https://openairdocs.org/sdr/MWEA001134.md): Skin · cracked · Nov 7, 2000 · N80ME · Doug DC914 · Cargo/Baggage Doors
  > CRACK INDICATION USING LOW FREQUENCY EDDY CURRENT ON UPPER AFT CORNER OF AFT CARGO DOOR JAMB. FABRICATED AND INSTALLED DOOR JAMB REPAIR.
- [SDR MWEA001133](https://openairdocs.org/sdr/MWEA001133.md): Door Frame · misdrilled · Nov 7, 2000 · N80ME · Doug DC914 · Fuselage Main, Structure
  > RIGHT OVERWING DOOR JAMB HAS 2 FASTENER HOLES ON AFT SIDE OF JAMB THAT ARE SHORT ON EDGE DISTANCE. FABRICATED AND INSTALLED DOOR JAMB REPAIR AND PARTS.
- [SDR MWEA001132](https://openairdocs.org/sdr/MWEA001132.md): Frame · tool damage · Nov 7, 2000 · N80ME · Doug DC914 · Fuselage Main, Frame
  > TOOL MARKS INBOARD SECTION OF FRAME AT STATION 544 LONGERON 16 RIGHT AND 15 RIGHT. FABRICATED AND INSTALLED FRAME REPAIR AND PARTS.
- [SDR MWEA001131](https://openairdocs.org/sdr/MWEA001131.md): Frame · misdrilled · Nov 7, 2000 · N80ME · Doug DC914 · Fuselage Main, Frame
  > SEVERAL PLUG HOLES ON FRAME STATION 503 BETWEEN LONGERONS 13 RIGHT AND 15 RIGHT WITH IMPROPER SPACING. FABRICATED AND INSTALLED FRAME REPAIR AND PARTS.
- [SDR MWEA001130](https://openairdocs.org/sdr/MWEA001130.md): Beam · corroded · Nov 7, 2000 · N80ME · Doug DC914 · Fuselage Miscellaneous Structure
  > E&E HORIZONTAL T BEAM FOR FORWARD BULKHEAD HAS AREA OF CORROSION, STATION 110, ABOVE BELLY SKIN. FABRICATED AND INSTALLED T BEAM REPAIR.
- [SDR MWEA001129](https://openairdocs.org/sdr/MWEA001129.md): Doubler · cracked · Nov 7, 2000 · N80ME · Doug DC914 · Fuselage Main, Plate/Skin
  > STATION 76 UPPER SURFACE 3 INCHES FORWARD OF REPAIR DOUBLER HAS A.25 INCH SKIN CRACK BETWEEN RIVETS. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA001128](https://openairdocs.org/sdr/MWEA001128.md): Floorbeam · cracked · Nov 7, 2000 · N80ME · Doug DC914 · Fuselage Main, Floor Beam
  > FLOORBEAM HAS A CRACK ORIGINATING FROM FASTENER HOLE ON AFT SIDE OF RIGHT FUSELAGE FRAME STATION 544. FABRICATED AND INSTALLED NEW FLOORBEAM.
- [SDR MWEA001127](https://openairdocs.org/sdr/MWEA001127.md): Longeron · tool damage · Nov 7, 2000 · N80ME · Doug DC914 · Fuselage Main, Longeron/Stringer
  > TOOL MARKS ON LONGERON 11 RIGHT, STATION 492. FABRICATED AND INSTALLED LONGERON REPAIR.
- [SDR MWEA001126](https://openairdocs.org/sdr/MWEA001126.md): Seat Track · corroded · Nov 7, 2000 · N80ME · Doug DC914 · Fuselage, Seat/Cargo Attach Fittings
  > NR 3 SEAT TRACK HAS HEAVY CORROSION IN CHANNEL STATION 200 - 229. REMOVED AND REPLACED SEAT TRACK SECTION.
- [SDR MWEA001125](https://openairdocs.org/sdr/MWEA001125.md): Seat Track · corroded · Nov 7, 2000 · N80ME · Doug DC914 · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD INBOARD EDGE OF NR 4 SEAT TRACK CORRODED (STATION 200). FABRICATED AND INSTALLED SEAT TRACK REPAIR.
- [SDR MWEA001124](https://openairdocs.org/sdr/MWEA001124.md): Floorbeam · corroded · Nov 7, 2000 · N80ME · Doug DC914 · Fuselage Main, Floor Beam
  > RIGHT LAV AREA HAS CORROSION ON FLOORBEAM STATION 801. FABRICATED AND INSTALLED REPAIR ANGLE.
- [SDR MWEA001123](https://openairdocs.org/sdr/MWEA001123.md): Stiffener · cracked · Nov 7, 2000 · N80ME · Doug DC914 · Fuselage Miscellaneous Structure
  > AFT PRESSURE BULKHEAD DOOR STIFFENER IS CRACKED ON RIGHT SIDE. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA001115](https://openairdocs.org/sdr/MWEA001115.md): Stiffener · tool damage · Nov 7, 2000 · N80ME · Doug DC914 · Fuselage Miscellaneous Structure
  > STIFFENER AT 2 O CLOCK POSITION LOOKING FORWARD ON AFT SIDE OF AFT PRESSURE BULKHEAD HAS TOOL MARKS. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA00439](https://openairdocs.org/sdr/MWEA00439.md): Battery Pack · inoperative · May 11, 2000 · N80ME · Doug DC914 · Emergency Lighting
  > LEFT NACELLE EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK.
- [SDR MWEA00048](https://openairdocs.org/sdr/MWEA00048.md): Longeron · cracked · Feb 10, 2000 · N80ME · Doug DC914 · Fuselage Main, Longeron/Stringer
  > LONGERON 13 RIGHT IS CRACKED AT ATTACH POINT TO FRAME STATION 897. MAINTENANCE FABRICATED AND INSTALLED LONGERON REPAIR.
- [SDR MWEA00047](https://openairdocs.org/sdr/MWEA00047.md): Frame · cracked · Feb 10, 2000 · N80ME · Doug DC914 · Fuselage Main, Frame
  > FRAME AT STATION 897 AND LONGERON 14 AND 15 RIGHT HAS 3 CRACKS. MAINTENANCE FABRICATED AND INSTALLED FRAME REPAIR.
- [SDR MWEA00046](https://openairdocs.org/sdr/MWEA00046.md): Shear Tie · damaged · Feb 10, 2000 · N80ME · Doug DC914 · Fuselage Miscellaneous Structure
  > SHEAR TIE TO FRAME STATION 880 AT LONGERON 9 RIGHT TO 13 RIGHT HAS HEAT DAMAGE. MAINTENANCE REMOVED AND REPLACED SHEAR TIE.
- [SDR MWEA00045](https://openairdocs.org/sdr/MWEA00045.md): Longeron · damaged · Feb 10, 2000 · N80ME · Doug DC914 · Fuselage Main, Longeron/Stringer
  > LONGERON 13 RIGHT FROM STATION 880 TO 885 HAS HEAT DAMAGE. MAINTENANCE FABRICATED AND INSTALLED LONGERON REPAIR.
- [SDR MWEA00044](https://openairdocs.org/sdr/MWEA00044.md): Longeron · damaged · Feb 10, 2000 · N80ME · Doug DC914 · Fuselage Main, Longeron/Stringer
  > LONGERON 11 RIGHT FROM STATION 880 TO 885 HAS HEAT DAMAGE. MAINTENANCE FABRICATED AND INSTALLED LONGERON REPAIR.
- [SDR MWEA00043](https://openairdocs.org/sdr/MWEA00043.md): Longeron · damaged · Feb 10, 2000 · N80ME · Doug DC914 · Fuselage Main, Longeron/Stringer
  > LONGERON 12 RIGHT FROM STATION 880 TO 906 HAS HEAT DAMAGE. MAINTENANCE FABRICATED AND INSTALLED LONGERON REPAIR.
- [SDR MWEA00042](https://openairdocs.org/sdr/MWEA00042.md): Pan · chafed · Feb 10, 2000 · N80ME · Doug DC914 · Service Doors
  > GALLEY SERVICE DOOR PAN HAS CHAFE JUST UNDER GUIDE VAIL ASSEMBLY. MAINTENANCE FABRICATED AND INSTALLED PAN REPAIR.
- [SDR MWEA00041](https://openairdocs.org/sdr/MWEA00041.md): Frame · damaged · Feb 10, 2000 · N80ME · Doug DC914 · Fuselage Main, Frame
  > FOUND FRAME AT FUSELAGE STATION 880 AT LONGERON 12 RIGHT TO HAVE HEAT DAMAGE. MAINTENANCE FABRICATED AND INSTALLED FRAME REPAIR.
- [SDR MWEA99912](https://openairdocs.org/sdr/MWEA99912.md): Slide · discharged · Dec 25, 1999 · N80ME · Doug DC914 · Escape Slide
  > GALLEY DOOR EVACUATION SLIDE PRESSURE LOW. MAINTENANCE REPLACED GALLEY DOOR EVACUATION SLIDE.
- [SDR MWEA99880](https://openairdocs.org/sdr/MWEA99880.md): Wire · chafed · Dec 8, 1999 · N80ME · Doug DC914 · Engine Oil System Wiring
  > MASTER CAUTION LIGHT AND RIGHT OIL STRAINER CLOGGING LIGHT CAME ON. FOUND CHAFED WIRE IN WIRE BUNDLE IN DIFFERENTIAL PRESSURE SENSOR ON RIGHT ENGINE AND REPAIRED.
- [SDR MWEA99836](https://openairdocs.org/sdr/MWEA99836.md): Battery Pack · discharged · Nov 23, 1999 · N80ME · Doug DC914 · Emergency Lighting
  > LEFT OVERWING EMERGENCY EXIT IDENTIFIER SIGN BATTERY PACK IS DISCHARGED. MAINTENANCE REPLACED BATTERY PACK
- [SDR MWEA99784](https://openairdocs.org/sdr/MWEA99784.md): Battery Pack · discharged · Nov 7, 1999 · N80ME · Doug DC914 · Emergency Lighting
  > EMERGENCY LIGHTS DID NOT ILLUMINATE ABOVE LEFT OVERWING EMERGENCY EXIT OR AT ROWS 9 TO 11 CEILING EMERGENCY LIGHTS. MAINTENANCE REPLACED BATTERY PACK.
- [SDR MWEA99722](https://openairdocs.org/sdr/MWEA99722.md): Battery Pack · discharged · Oct 23, 1999 · N80ME · Doug DC914 · Emergency Lighting
  > TWO CEILING LIGHTS BETWEEN GALLEY AND COAT CLOSET DID NOT EXTINGUISH WITH EMERGENCY LIGHTS OF. MTC REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK.
- [SDR MWEA99671](https://openairdocs.org/sdr/MWEA99671.md): Channel · dented · Oct 5, 1999 · N80ME · Doug DC914 · Trailing Edge Flaps
  > RIGHT FLAP NR 3 WEDGE TRAILING EDGE V-CHANNEL HAD A DENT. MTC REMOVED AND REPLACED V-CHANNEL.
- [SDR MWEA99670](https://openairdocs.org/sdr/MWEA99670.md): Skin · dented · Oct 5, 1999 · N80ME · Doug DC914 · Trailing Edge Flaps
  > RIGHT FLAP NR 3 WEDGE HAD A DENT OUT OF LIMITS. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.
- [SDR MWEA99515](https://openairdocs.org/sdr/MWEA99515.md): Battery Pack · discharged · Aug 19, 1999 · N80ME · Doug DC914 · Emergency Lighting
  > WHEN AIRCRAFT BUSSES ARE DEPOWERED THE EMERGENCY FLOOR TRACK LIGHT ILLUMINATES. MTC REMOVED AND REPLACED FORWARD EMERGENCY FLOOR TRACK BATTERY PACK.
- [SDR MWEA99506](https://openairdocs.org/sdr/MWEA99506.md): Cover · detached · Aug 11, 1999 · N80ME · Doug DC914 · Emergency Equipment
  > GALLEY DOOR SLIDE COVER FELL OFF. REPLACED COVER.
- [SDR MWEA99503](https://openairdocs.org/sdr/MWEA99503.md): Fitting · cracked · Aug 6, 1999 · N80ME · Doug DC914 · Fuselage Miscellaneous Structure
  > RIGHT FITTING AT STATION 484 WAS CRACKED. MTC REMOVED AND REPLACED FITTING.
- [SDR MWEA99502](https://openairdocs.org/sdr/MWEA99502.md): Fitting · corroded · Aug 6, 1999 · N80ME · Doug DC914 · Fuselage Miscellaneous Structure
  > LONGERON 26R END FITTING AT STATION 484 IS CORRODED. MTC REMOVED AND REPLACED END FITTING.
- [SDR MWEA99501](https://openairdocs.org/sdr/MWEA99501.md): Fitting · cracked · Aug 6, 1999 · N80ME · Doug DC914 · Fuselage Miscellaneous Structure
  > LONGERON 24R END FITTING AT STATION 484 WAS CRACKED. MTC REMOVED AND REPLACED END FITTING.
- [SDR MWEA99500](https://openairdocs.org/sdr/MWEA99500.md): Bulkhead Fitting · cracked · Aug 6, 1999 · N80ME · Doug DC914 · Fuselage Main, Bulkhead
  > RIGHT AND LEFT FITTINGS FOR PRESSURE BULKHEAD AT STATION 490 WAS CRACKED. MTC REMOVED AND REPLACED FITTINGS.
- [SDR MWEA99499](https://openairdocs.org/sdr/MWEA99499.md): Skin · corroded · Aug 6, 1999 · N80ME · Doug DC914 · Fuselage Main, Plate/Skin
  > UNDERWING PRESSURE DOME AT STATION 490 HAS CORROSION AND TOOLMARKS BEYOND LIMITS. MTC FABRICATED AND INSTALLED NEW SKIN.
- [SDR MWEA99498](https://openairdocs.org/sdr/MWEA99498.md): Bracket · cracked · Aug 6, 1999 · N80ME · Doug DC914 · Fuselage Miscellaneous Structure
  > LONGERON 30 LEFT END CAP BRACKET AT STATION 490-498 WAS CRACKED. MTC REMOVED AND REPLACED END CAP BRACKET.
- [SDR MWEA99497](https://openairdocs.org/sdr/MWEA99497.md): Fitting · corroded · Aug 6, 1999 · N80ME · Doug DC914 · Fuselage Miscellaneous Structure
  > RIGHT LONGERON 30 END CAP FITTING AT STATION 490-498 IS CORRODED. MTC REMOVED AND REPLACED END CAP FITTING.
- [SDR MWEA99496](https://openairdocs.org/sdr/MWEA99496.md): Tee · out of limits · Aug 6, 1999 · N80ME · Doug DC914 · Fuselage Miscellaneous Structure
  > THE TEE AT STATION 490 LONGERON 30 IS BLENDED OUT OF LIMITS. MTC REMOVED AND REPLACED TEE.
- [SDR MWEA99495](https://openairdocs.org/sdr/MWEA99495.md): Skin · corroded · Aug 6, 1999 · N80ME · Doug DC914 · Fuselage Main, Plate/Skin
  > LIGHT CORROSION ON INTERNAL SKIN AREA OF LONGERON 30 AT STATION 484. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.
- [SDR MWEA99494](https://openairdocs.org/sdr/MWEA99494.md): Fitting · cracked · Aug 6, 1999 · N80ME · Doug DC914 · Fuselage Miscellaneous Structure
  > FORWARD CARGO PIT LONGERON 30 END FITTING CRACKED BETWEEN STATION 470-484. MTC REMOVED AND REPLACED END FITTING.
- [SDR MWEA99493](https://openairdocs.org/sdr/MWEA99493.md): Intercostal · corroded · Aug 6, 1999 · N80ME · Doug DC914 · Cargo/Baggage Doors
  > AFT CARGO DOOR INTERCOSTAL AT STATION 730 HAS CORROSION UNDER NUT PLATE. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.
- [SDR MWEA99492](https://openairdocs.org/sdr/MWEA99492.md): Former · cracked · Aug 6, 1999 · N80ME · Doug DC914 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT AT STATION 801 FRAME FORMER CRACKED LEFT SIDE OF LONGERON 30. MTC FABRICATED AND INSTALLED REPAIR SPLICE.

Next page: https://openairdocs.org/deregistered/N80ME-2003-01-03/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 = 'N80ME' AND deregistration_id = 'N80ME-2003-01-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N80ME-2003-01-03/reports

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