# Service difficulty reports: N800ME, cancelled Oct 29, 2002

A list on [N800ME, cancelled Oct 29, 2002](https://openairdocs.org/deregistered/N800ME-2002-10-29.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 8 · 365 reports

- [SDR MWEA020513](https://openairdocs.org/sdr/MWEA020513.md): Stiffener · cracked · Aug 14, 2002 · N800ME · Doug DC914 · Engine Cowling System
  > RADIAL STIFFENER AT 5 O'CLOCK POSITION IS CRACKED AT ATTACH FASTNER LEFT ENGINE. -- REMOVED AND REPLACED STIFFENER.
- [SDR MWEA020511](https://openairdocs.org/sdr/MWEA020511.md): Stiffener · cracked · Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Main, Bulkhead
  > RECEPTACLE UNDER RADIAL STIFFENER AT 10 O'CLOCK POSITION #6 LEFT FOUND TO BE CRACKED IN 2 PLACES. -- DRILLED UP AND INSTALLED RECEPTACLE.
- [SDR MWEA020501](https://openairdocs.org/sdr/MWEA020501.md): Stiffener · cracked · Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD RADIAL STIFFENER ON AFT SIDE AT 10 O'CLOCK POSSITION HAS A SMALL CRACK AT THE RIGHT SIDE. -- FABRICATED AND INSTALLED STIFFENER.
- [SDR MWEA020495](https://openairdocs.org/sdr/MWEA020495.md): Stringer · corroded · Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach Fittings
  > LEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 18&19 ALSO EXTENDING UNDER STRINGER 18 FORWARD AND AFT. -- FABRICATED AND INSTALLED SHIM.
- [SDR MWEA020483](https://openairdocs.org/sdr/MWEA020483.md): Stringer · damaged · Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach Fittings
  > REPAIR CLIPS REQUIRED BETWEEN STRINGERS 15&14 ON THE INBOARD AND OUTBOARD SIDES OF XWC 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS.
- [SDR MWEA020484](https://openairdocs.org/sdr/MWEA020484.md): Stringer · damaged · Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach Fittings
  > REPAIR CLIPS REQUIRED INSTALL BETWEEN STRINGERS 14&13 ON THE INBOARD AND OUTBOARD SIDE OF XCW 58 WING.
- [SDR MWEA020485](https://openairdocs.org/sdr/MWEA020485.md): Stringer · damaged · Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach Fittings
  > REPAIR CLIP REQUIRED INSTALL BETWEEN STRINGERS 13&12 ON THE INBOARD AND OUTBOARD SIDES OF XCW 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS.
- [SDR MWEA02505](https://openairdocs.org/sdr/MWEA02505.md): Stringer · damaged · Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach Fittings
  > REQUESTING BOEING AGREEMENT OF FASTENER PLACEMENT IN UPPER PORTION OF REPAIR CLIPS BETWEEN STRINGER 14,15&16 THERE ARE TWO CLIPS AND TWO FASTENERS PER CLIP. -- BOEING APPROVES OF THE PLACEMENT OF THE FASTENERS.
- [SDR MWEA02504](https://openairdocs.org/sdr/MWEA02504.md): Stiffener · damaged · Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Main, Structure
  > 1 EACH DOUBLE DRILLED HOLES ON AFT PRESSURE BULKHEAD BETWEEN RADIAL STIFFENER 18&20 LEFT. -- REAMED HOLES AND INSTALLED BUSHING.
- [SDR MWEA020503](https://openairdocs.org/sdr/MWEA020503.md): Stiffener · damaged · Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Main, Structure
  > 2 EACH DOUBLE DRILLED HOLES ON AFT PRESSURE BULKHEAD RADIAL STIFFNERS 2&6 LEFT. -- REAMED HOLE UP AND INSTALLED 2 EACH BUSHINGS.
- [SDR MWEA020500](https://openairdocs.org/sdr/MWEA020500.md): Angle · cracked · Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD RIGHT HAND RADIAL #2 LOWER ANGLE THAT ATTACHES TO JAMB GUSSET HAS A CRACKED ATTACH HOLE. -- FABRICATED AND INSTALLED ANGLE.
- [SDR MWEA020499](https://openairdocs.org/sdr/MWEA020499.md): Doubler · cracked · Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD PLUG DOOR STOP RECEPTACLE AT UPPER RIGHT CORNER HAS A CRACK EMANATING FROM CUTOUT HOLE TO THE DOOR JAMB EDGE DOT 30. -- FABRICATED AND INSTALLED DOUBLER, FABRICATED AND INSTALLED 8 FASTENERS.
- [SDR MWEA020492](https://openairdocs.org/sdr/MWEA020492.md): Doubler · cracked · Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD PLUG DOOR STOP RECEPTACLE AT LOWER LEFT CORNER HAS A CRACK EMANATING FROM CUT OUT HOLE TO DOOR JAMB EGDE DOT 31. -- FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA020491](https://openairdocs.org/sdr/MWEA020491.md): Stringer · corroded · Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach Fittings
  > LEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 14&15 ALSO EXTENDING UNDER STRINGER 14&15 AND ONE SPOT ON VERTICAL LEG. -- FABRICATED AND INSTALLED SHIM
- [SDR MWEA020482](https://openairdocs.org/sdr/MWEA020482.md): Clip · cracked · Aug 14, 2002 · N800ME · Doug DC914 · Wing Miscellaneous Structure
  > REMOVED LEFT FUEL TANK SHEAR CLIP AT 69 BULKHEAD BETWEEN STRINGER 12 & 13. DRILLED UP CLIP AND INSTALLED FASTENERS.
- [SDR MWEA020510](https://openairdocs.org/sdr/MWEA020510.md): Seal · cracked · Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Main, Structure
  > LEFT AND RIGHT AFT PRESSURE BULKHEAD SEAL RETAINERS ARE CRACKED. -- DRILLED UP AND INSTALLED SEAL RETAINERS.
- [SDR MWEA020509](https://openairdocs.org/sdr/MWEA020509.md): Stringer · damaged · Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach Fittings
  > REPAIR CLIPS REQUIRED INSTALL BETWEEN STRINGER 17&16 ON THE INBOARD AND OUTBOARD SIDES OF XWC 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS.
- [SDR MWEA020508](https://openairdocs.org/sdr/MWEA020508.md): Stringer · damaged · Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach Fittings
  > REPAIRED CLIPS REQUIRED INSTALL BETWEEN STRINGER 15&16 ON THE INBOARD AND OUTBOARD SIDES OF XWC 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS.
- [SDR MWEA020507](https://openairdocs.org/sdr/MWEA020507.md): Stringer · damaged · Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach Fittings
  > TEMPORARY STRINGER CLIP INSTALLED AT XRS 111 BETWEEN STRINGER 11 AND AFT SPAR RIGHT WING. -- DRILLED UP CLIP AND INSTALLED NEW CLIP.
- [SDR MWEA020494](https://openairdocs.org/sdr/MWEA020494.md): Stringer Clip · damaged · Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach Fittings
  > TEMPORARY STRINGER CLIP INSTALLED AT XRS 111 BETWEEN STRINGER 21&22 RIGHT WING. -- DRILLED UP CLIP AND INSTALLED NEW CLIP.
- [SDR MWEA020493](https://openairdocs.org/sdr/MWEA020493.md): Stiffener · cracked · Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Miscellaneous Structure
  > STIFFENER AFT SIDE OF AFT PRESSURE BULKHEAD AT RADIAL 20 LEFT IS CRACKED AND DENTED. FABRICATED AND INSTALLED STIFFENER.
- [SDR MWEA020488](https://openairdocs.org/sdr/MWEA020488.md): Fitting · cracked · Aug 13, 2002 · N800ME · Doug DC914 · Wing Miscellaneous Structure
  > LEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 13 AND 14, ALSO EXTENDING UNDER STRINGER 14 AND 13. ALSO FOUND CRACK ON OUTBOARD LEG. BLENDED OUT CRACK AND REMOVED CORROSION AROUND AND UNDER STRINGER.
- [SDR MWEA020487](https://openairdocs.org/sdr/MWEA020487.md): Stringer · corroded · Aug 13, 2002 · N800ME · Doug DC914 · Wing, Attach Fittings
  > LEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 12 AND 13 ALSO EXTENDING UNDER STRINGER 12 AND 13. -- FABRICATED SHIMS FOR STRINGER AND REMOVED CORROSION.
- [SDR MWEA020478](https://openairdocs.org/sdr/MWEA020478.md): Angle · cracked · Aug 13, 2002 · N800ME · Doug DC914 · Fuselage Main, Longeron/Stringer
  > ANGLE AT RADIAL 6 LEFT IS CRACKED. -- DRILLED UP ANGLE AND INSTALLED ANGLE.
- [SDR MWEA020486](https://openairdocs.org/sdr/MWEA020486.md): Stringer · corroded · Aug 13, 2002 · N800ME · Doug DC914 · Wing, Attach Fittings
  > LEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 11 AND 12 ALSO EXTENDING UNDER STRINGER 11. -- REMOVED CORRORION.
- [SDR MWEA020480](https://openairdocs.org/sdr/MWEA020480.md): Stringer · corroded · Aug 13, 2002 · N800ME · Doug DC914 · Wing, Attach Fittings
  > LEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGERS 16 AND 17 ALSO EXTENDING UNDER STRINGERS 16 AND 17.
- [SDR MWEA020476](https://openairdocs.org/sdr/MWEA020476.md): Bracket · damaged · Aug 13, 2002 · N800ME · Doug DC914 · Fuselage Main, Longeron/Stringer
  > SUPPORT BRACKET 5910163-191 LOCATED ON LEFT SIDE OF APB AT RADIAL 6 INBOARD END DAMAGED. -- LOCATED AND DRILLED INBOARD AND OUTBOARD END OF NEW 191 AND REMOVED AND INSTALLED BRACKET.
- [SDR MWEA020468](https://openairdocs.org/sdr/MWEA020468.md): Fastener · cracked · Jul 30, 2002 · N800ME · Doug DC914 · Fuselage Main, Longeron/Stringer
  > SKIN CRACK INDICATION NOTED STATION 180 JUST RIGHT OF LONGERON ONE. -- REMOVED AND INSTALLED FASTENERS INTO FORMERS.
- [SDR MWEA020465](https://openairdocs.org/sdr/MWEA020465.md): Fitting · oversized · Jul 30, 2002 · N800ME · Doug DC914 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR FITTINGS HAS OVERSIZED HOLES. -- REMOVED AND INSTALLED FITTINGS.
- [SDR MWEA020464](https://openairdocs.org/sdr/MWEA020464.md): Angle · oversized · Jul 30, 2002 · N800ME · Doug DC914 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR ANGLE HAS OVERSIZED HOLES. -- REMOVED AND REPLACED ANGLE.
- [SDR MWEA020470](https://openairdocs.org/sdr/MWEA020470.md): Doubler · cracked · Jul 30, 2002 · N800ME · Doug DC914 · Fuselage Main, Frame
  > PER PCI 9274 FOUND SMALL SKIN CRACK INTO DOOR STOP ADJUST HOLE ON AFT SIDE OF DOOR 3RD HOLE FROM THE TOP (MARKED). -- FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA020469](https://openairdocs.org/sdr/MWEA020469.md): Finger Doubler · cracked · Jul 30, 2002 · N800ME · Doug DC914 · Fuselage Main, Longeron/Stringer
  > SKIN CRACKED INDICATION NOTED STATION 525 JUST RIGHT OF LONGERON ONE (MARKED). -- FABRICATED AND INSTALLED SKIN PLUG AND FINGER DOUBLER.
- [SDR MWEA020467](https://openairdocs.org/sdr/MWEA020467.md): Angle · oversized · Jul 30, 2002 · N800ME · Doug DC914 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR ANGLE HAS OVERSIZED HOLES. -- REMOVED AND INSTALLED ANGLE.
- [SDR MWEA020466](https://openairdocs.org/sdr/MWEA020466.md): Doubler · cracked · Jul 30, 2002 · N800ME · Doug DC914 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR #2 OUTBOARD UPPER ATTACH HOLE IS CRACKED. -- FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA020456](https://openairdocs.org/sdr/MWEA020456.md): Intercostal · cracked · Jul 23, 2002 · N800ME · Doug DC914 · Cargo/Baggage Doors
  > INTERCOSTAL IS CRACKED AROUND FASTENER HOLES FORWARD CARGO DOOR BELOW #1 BEAM FORWARD END OF DOOR (DOT JH 23). -- REMOVED AND INSTALLED INTERCOSTAL.
- [SDR MWEA020455](https://openairdocs.org/sdr/MWEA020455.md): Clip · gouged · Jul 23, 2002 · N800ME · Doug DC914 · Fuselage Main, Bulkhead
  > SHOVEL CLIP JUST AFT OF APB LEFT 17 LONGERON IS GOUGED. -- REPAIRED GOUGE AND INSTALLED SHOVEL CLIP.
- [SDR MWEA020454](https://openairdocs.org/sdr/MWEA020454.md): Clip · cracked · Jul 23, 2002 · N800ME · Doug DC914 · Fuselage Miscellaneous Structure
  > APB RADIAL NR 16 LEFT END CLIP HAS A CRACK AROUND END FASTENER HOLE. FABRICATED AND INSTALLED CLIP.
- [SDR MWEA020451](https://openairdocs.org/sdr/MWEA020451.md): Splice Plate · cracked · Jul 18, 2002 · N800ME · Doug DC914 · Fuselage Miscellaneous Structure
  > AFT PRESSURE BULKHEAD PLUG DOOR JAMB HAS A CRACK AT APPROXIMATELY THE 6 O'CLOCK POSITION IN THE SPLICE PLATE CONNECTION. REMOVED AND INSTALLED SPLICE PLATE.
- [SDR MWEA011491](https://openairdocs.org/sdr/MWEA011491.md): Switch · faulty · Dec 22, 2001 · N800ME · Doug DC914 · Cabin Pressure Control System
  > AIRCRAFT DEPRESSURIZED DURING CLIMB. REPLACED RIGHT HAND SECOND SEGMENT CLIMB SWITCH.
- [SDR MWEA011060](https://openairdocs.org/sdr/MWEA011060.md): Servo · inoperative · Jul 19, 2001 · N800ME · Doug DC914 · Autopilot Main Servo
  > WITH AUTOPILOT AND ELEVATOR SERVO OFF TRIM MOVES UNCOMMANDED NOSE UP AND NOSE DOWN. -- REPLACED ELEVATOR SERVO, OPERATIONAL CHECK GOOD.
- [SDR MWEA010246](https://openairdocs.org/sdr/MWEA010246.md): Spar · corroded · Apr 5, 2001 · N800ME · Doug DC914 · Wing Spar
  > REMOVE RIGHT LOWER WING TEE P/N 9911603-4 DUE TO NUMEROUS CORROSION DISCREPANCIES. REMOVED AND REPLACED RIGHT LOWER WING SPAR TEE.
- [SDR MWEA010247](https://openairdocs.org/sdr/MWEA010247.md): Splice · nicked · Apr 5, 2001 · N800ME · Doug DC914 · Wing Main, Frame Structure
  > REMOVED STRINGER 14 FORWARD SPLICE P/N 3913324-1 TO FACILITATE OTHER MAINTENANCE. FOUND NICKS, DINGS, AND SCRATCHES. LOCATED, DRILLED, FABRICATED AND INSTALLED CENTER FORWARD 14 SPLICE.
- [SDR MWEA010227](https://openairdocs.org/sdr/MWEA010227.md): Pan · gouged · Apr 5, 2001 · N800ME · Doug DC914 · Passenger Compartment Windows
  > REMOVE WINDOW PAN AT WINDOW NR 19 LEFT STATION 604- STATION 623, HAS DEEP NICKS AND GOUGES. REMOVED WINDOW PAN AND 4EA CLIP, LOCATED AND DRILLED NEW PAN, FABRICATED CLIPS, INSTALLED CLIP AND NEW PAN.
- [SDR MWEA010245](https://openairdocs.org/sdr/MWEA010245.md): Splice · gouged · Apr 5, 2001 · N800ME · Doug DC914 · Wing Miscellaneous Structure
  > CENTER TANK STRINGER NR 11 FORWARD SPLICE HAS 2 EA. HOLES WITH DEEP GOUGES. FABRICATED AND INSTALLED SPLICE.
- [SDR MWEA010511](https://openairdocs.org/sdr/MWEA010511.md): Intercostal · cracked · Apr 2, 2001 · N800ME · Doug DC914 · Nacelle/Pylon, Main Frame
  > RIGHT PYLON INTERCOSTAL AFT OF AFT SPAR HAS A CRACK ON UPPER END. REMOVED PYLON SKIN, FABRICATED TWO EACH REPAIR DOUBLERS, INSTALLED DOUBLERS AND SKIN.
- [SDR MWEA010510](https://openairdocs.org/sdr/MWEA010510.md): Web · misdrilled · Apr 2, 2001 · N800ME · Doug DC914 · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT WEBBING SECTION HAS BN NUT INSTALLED WITH NO PITCH DISTANCE INCLUDING TWO IN THE EDGE OF FRAME STATION 377 FLANGE, LOCATED BETWEEN LONGERON 25 RIGHT AND 26 RIGHT. - REMOVED DAMAGED WEB, FABRICATED NEW WEB AND SPLICE REPAIR, LOCATED,
- [SDR MWEA010509](https://openairdocs.org/sdr/MWEA010509.md): Frame · tool damage · Apr 2, 2001 · N800ME · Doug DC914 · Fuselage Main, Frame
  > MODERATE TOOL DAMAGE AROUND SIX FASTENERS, JUST AFT OF FRAME STATION 817, LONGERON 11 RIGHT. REMOVED FASTENERS AND DAMAGED SECTION, FABRICATED REPAIR FILLER, DOUBELRS AND FINGER DOUBLERS, INSTALLED REPAIR PARTS.
- [SDR MWEA010508](https://openairdocs.org/sdr/MWEA010508.md): Skin · dented · Apr 2, 2001 · N800ME · Doug DC914 · Rudder, Plate/Skin
  > DENT IN RUDDER SKIN AT STATION ZR 117 ON LEFT SIDE JUST AFT OF LEADING EDGE PANEL. FABRICATED SKIN PANEL AND SKIN, INSTALLED SKIN, FABRICATED AND INSTALLED NEW BALANCE TAG.
- [SDR MWEA010507](https://openairdocs.org/sdr/MWEA010507.md): Door Frame · corroded · Apr 2, 2001 · N800ME · Doug DC914 · Fuselage Main, Structure
  > FORWARD CARGO COMPARTMENT DOOR JAMB WEBBING BETWEEN STATION 305 AND 377 HAS AREAS OF LIGHT CORROISON ON TOP SIDE FORM LONGERON 26 RIGHT TO 29 RIGHT. REMOVED AND BLENDED CORROSION AND FORWARD CARGO DOOR JAMB WEB, LOCATED, DRILLED AND INSTALLED NEW DOOR JAMB
- [SDR MWEA010506](https://openairdocs.org/sdr/MWEA010506.md): Frame · corroded · Apr 2, 2001 · N800ME · Doug DC914 · Fuselage Main, Frame
  > FORWARD CARGO COMPARTMENT FRAME STATION 218 AFT SIDE HAS AREAS OF LIGHT CORROSION FROM LONGERON 28 RIGHT TO 29 LEFT. FABRICATED SPLICE DOUBLERS, FRAME FILLER, AND REPAIR PARTS, INSTALLED REPAIR PARTS.

Next page: https://openairdocs.org/deregistered/N800ME-2002-10-29/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 = 'N800ME' AND deregistration_id = 'N800ME-2002-10-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N800ME-2002-10-29/reports

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