# Service difficulty reports: N207ME, cancelled Apr 18, 2005

A list on [N207ME, cancelled Apr 18, 2005](https://openairdocs.org/deregistered/N207ME-2005-04-18.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 · 199 reports

- [SDR MWEA030422](https://openairdocs.org/sdr/MWEA030422.md): Smoke Detector · inoperative · Oct 12, 2003 · N207ME · Doug DC932 · Smoke Detection
  > DURING FLIGHT THE MASTER WARNING CAME ON WITH NO OTHER ANNUNCIATIONS FOUND, NO POWER TO CARGO DETECTION PANEL. REMOVED AND REPLACED CARGO SMOKE DETECTORS, OHMED AND MEGGED ALL WIRING TO CARGO SMOKE DETECTOR.
- [SDR MWEA030420](https://openairdocs.org/sdr/MWEA030420.md): Control Panel · inoperative · Oct 10, 2003 · N207ME · Doug DC932 · Smoke Detection
  > MASTER WARNING CAME ON WITH NO OTHER ANNUNCIATIONS. SMOKE DETECTOR PANEL CIRCUIT BREAKER POPPED. INSPECTED OVERHEAD PANEL WIRING AND CARGO FIRE SUPPRESSION CONTROL PANEL. NO VISIBLE DEFECTS NOTED, ALSO INSPECTED CARGO PIT SMOKE DETECTOR. NO VISIBLE DEFECTS
- [SDR MWEA030316](https://openairdocs.org/sdr/MWEA030316.md): Relay · failed · Aug 18, 2003 · N207ME · Doug DC932 · Stall Warning System
  > AFTER ROTATION STICK SHAKERS AND STALL INDICATION LIGHT CAME ON. REMOVED AND REPLACED RIGHT RELAY.
- [SDR MWEA030311](https://openairdocs.org/sdr/MWEA030311.md): Relay · failed · Aug 17, 2003 · N207ME · Doug DC932 · Leading Edge Slat Control System
  > SLAT EXTEND LIGHT INOPERATIVE. REMOVED AND REPLACED RELAY.
- [SDR MWEA030310](https://openairdocs.org/sdr/MWEA030310.md): Connector · defective · Aug 15, 2003 · N207ME · Doug DC932 · Stall Warning System
  > STALL INDICATION FAILURE LIGHT CAME ON. REMOVED AND REPLACED FIRST OFFICER'S STICK SHAKER CONNECTOR.
- [SDR MWEA030309](https://openairdocs.org/sdr/MWEA030309.md): Transmitter · faulty · Aug 14, 2003 · N207ME · Doug DC932 · Trailing Flap Position Indicating System
  > STALL INDICATION FAILURE LIGHT CAME. REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER. PERFORMED ADJUSTMENT TEST OF STALL SYSTEM CHECKED GOOD.
- [SDR MWEA030303](https://openairdocs.org/sdr/MWEA030303.md): Computer · malfunctioned · Aug 1, 2003 · N207ME · Doug DC932 · Stall Warning System
  > STALL INDICATION FAILURE ANNUCIATOR COMES OFF AND ON. REMOVED AND REPLACED STALL WARNING COMPUTER.
- [SDR MWEA030273](https://openairdocs.org/sdr/MWEA030273.md): Flex Line · cracked · Jul 10, 2003 · N207ME · Doug DC932 · Pneumatic Distribution System
  > AT 35,000 FEET RED MASTER WARNING LIGHT ILLUMINATED ALONG WITH THE RED CABIN ANNUCIATOR, MASK DROPPED -- REPLACED COALESER BAG AND CLEANED BOTH WATER OUTLET SCEENS, ALSO PERFORMED A CABIN PRESSURIZATION CONTROL ADJUST, REMOVED AND REPLACED WATER SEPERATOR TE
- [SDR MWEA030133](https://openairdocs.org/sdr/MWEA030133.md): Windshield · failed · Mar 17, 2003 · N207ME · Doug DC932 · Flight Compartment Windows
  > FIRST OFFICER'S WINDSHIELD SHATTERED AT ALTITUDE (OUTER PANE). REMOVED AND REPLACED FIRST OFFICER'S WINDSHIELD.
- [SDR MWEA030122](https://openairdocs.org/sdr/MWEA030122.md): Computer · malfunctioned · Feb 27, 2003 · N207ME · Doug DC932 · Stall Warning System
  > DURING TAXI, STALL INDICATION FAILURE LIGHT CAME ON. SWAPPED AOA SYSTEM, CHECKS GOOD. MARKED FAULTLY TRANSDUCER ON NR 1 SIDE, NOW IN NR 1 POSITION, RESET NR 2 COMPUTER VANE PIN.
- [SDR MWEA030052](https://openairdocs.org/sdr/MWEA030052.md): Bulkhead · cracked · Feb 3, 2003 · N207ME · Doug DC932 · Fuselage Main, Bulkhead
  > STATION 965 RIGHT, FORWARD PYLON, BULKHEAD WEB HAS TWO SMALL CRACKS EMANATING FROM SNAPS AT OUTBOARD SIDE NEXT TO LONGERON 11 AND LONGERON 10. CUT OUT DAMAGE, FABRICATED DOUBLER, INSTALLED TWO EACH OF DOUBLERS AND PARTITION GUIDE.
- [SDR MWEA030054](https://openairdocs.org/sdr/MWEA030054.md): Bulkhead · cracked · Feb 3, 2003 · N207ME · Doug DC932 · Fuselage Main, Bulkhead
  > AT APPROXIMATELY STATION 965 RIGHT FORWARD BULKHEAD WALL HAS A CRACK APPROXIMATELY SIX INCHES INBOARD OF OUTSIDE BULKHEAD ATTACH ANGLE, CRACK IS EMITTING FROM BOLT HOLE FOR THE LOWER SPAR. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED WEB.
- [SDR MWEA030053](https://openairdocs.org/sdr/MWEA030053.md): Bulkhead · cracked · Feb 3, 2003 · N207ME · Doug DC932 · Fuselage Miscellaneous Structure
  > STATION 965 RIGHT FORWARD PYLON BULKHEAD HAS A CRACK GOING INBOARD OF LIGHTENING HOLE AT Z = 50.0. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA030051](https://openairdocs.org/sdr/MWEA030051.md): Rib · cracked · Feb 3, 2003 · N207ME · Doug DC932 · Leading Edge Devices
  > LEFT NR 5 SLAT OUTBOARD RIB IS CRACKED AT LOWER AFT CORNER. REMOVED CRACKED RIB AND INSTALLED NEW RIB.
- [SDR MWEA030050](https://openairdocs.org/sdr/MWEA030050.md): Skin · cracked · Feb 3, 2003 · N207ME · Doug DC932 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT FRAME STATION 180 SHEAR TIE BETWEEN LONGERON 1&2 RIGHT. FABRICATED REPAIR DOUBLER AND FILLER, INSTALLED DOUBLER.
- [SDR MWEA020609](https://openairdocs.org/sdr/MWEA020609.md): Indicator · out of adjust · Oct 8, 2002 · N207ME · Doug DC932 · Visual Omnirange (VOR) System
  > BOTH CAPTAINS AND FIRST OFFICERS HORIZONTAL DIRECTION GYRO INDICATORS 30 DEGREES OFF CORRECT HEADING. RESLAVED BOTH RADIO MAGNETIC INDICATORS IAW MM 34-21-00. OPERATIONS CHECK GOOD.
- [SDR MWEA020418](https://openairdocs.org/sdr/MWEA020418.md): Transceiver · malfunctioned · Jun 4, 2002 · N207ME · Doug DC932 · Weather Radar System
  > JUST AFTER DEPARTURE FROM MILWAUKEE RADAR INDICATOR BLANKED OUT. RECYCLED UNIT OFF AND ON DISPLAY CAME YELLOW ONLY AND FLICKERED DISPLAY WAS SAME ALL THE WAY TO GATE. RETURNED TO MILWAUKEE. REPAIRED AND REPLACED WEATHER RADAR TRANSCEIVER SYSTEM OPS CHECK OK
- [SDR MWEA020331](https://openairdocs.org/sdr/MWEA020331.md): Skin · misdrilled · May 12, 2002 · N207ME · Doug DC932 · Fuselage Miscellaneous Structure
  > STATION 794 THROUGH 813, 16 HOLES WERE MISDRILLED IN BOTTOM 2 ROWS OF REPAIR ABOVE LONGERON 15 LEFT. -- FABRICATED AND INSTALLED REPAIR BUSHINGS AND PLUGS.
- [SDR MWEA020330](https://openairdocs.org/sdr/MWEA020330.md): Skin · misdrilled · May 12, 2002 · N207ME · Doug DC932 · Fuselage Miscellaneous Structure
  > STATION 756 LEFT SIDE 9 HOLES ARE TOO CLOSE TO WINDOW BELT SPLICE. -- FABRICATED AND INSTALLED REPAIR BUSHINGS.
- [SDR MWEA020325](https://openairdocs.org/sdr/MWEA020325.md): Longeron · tool damage · May 12, 2002 · N207ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DRILL START ON BOTTOM OF LONGERON 30 STATION 269. -- FABRICATED AND INSTALLED LONGERON SPLICE.
- [SDR MWEA020061](https://openairdocs.org/sdr/MWEA020061.md): Skin · damaged · Jan 24, 2002 · N207ME · Doug DC932 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGED AT APPROXIMATLEY STATION 237 LONGERON 30. -- REMOVED DAMAGE INSTALL FLUSH INTERNAL REPAIR PER SRM 53-04 FIGURE 38 SHEET 31 TELEX MWX.MKE-02-00001H.
- [SDR MWEA011432](https://openairdocs.org/sdr/MWEA011432.md): Web · corroded · Nov 15, 2001 · N207ME · Doug DC931 · Fuselage Miscellaneous Structure
  > CORROSION OF AFT PIT DOOR WEB AT STATION 937 JUST FORWARD OF LONGERONS 24 RIGHT TO 26 RIGHT AFT PIT. REMOVED CORROSION, FABRICATED AND INSTALLED WEB.
- [SDR MWEA011431](https://openairdocs.org/sdr/MWEA011431.md): Angle · cracked · Nov 14, 2001 · N207ME · Doug DC932 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED AT FUSELAGE STATION 83.5 AT INBOARD END, 1.0625 INCHES IN LENGTH. STOPPED DRILL, FABRICATED AND INSTALLED REPAIR ANGLE.
- [SDR MWEA011430](https://openairdocs.org/sdr/MWEA011430.md): Angle · cracked · Nov 14, 2001 · N207ME · Doug DC932 · Fuselage Miscellaneous Structure
  > ANGLE AT FUSELAGE STATION 83.5 HAS A 1 INCH CRACK AT INBOARD END. FABRICATED, DRILLED AND INSTALLED REPAIR ANGLE.
- [SDR MWEA011429](https://openairdocs.org/sdr/MWEA011429.md): Frame · cracked · Nov 14, 2001 · N207ME · Doug DC932 · Fuselage Main, Frame
  > FRAME IS CRACKED AT FUSELAGE STATION 83.5 AT 10 RIGHT 1 INCH IN LENGTH. REMOVED, STOPPED DRILL, FABRICATED AND INSTALLED REPAIR ANGLE.
- [SDR MWEA011428](https://openairdocs.org/sdr/MWEA011428.md): Frame · cracked · Nov 14, 2001 · N207ME · Doug DC932 · Fuselage Main, Frame
  > FRAME AT FUSELAGE STATION 83.5 BY 10 LEFT IS CRACKED. LENGTH OF CRACK IS 1.00 INCH. STOPPED DRILL, FABRICATED AND INSTALLED REPAIR ANGLE.
- [SDR MWEA011427](https://openairdocs.org/sdr/MWEA011427.md): Angle · corroded · Nov 14, 2001 · N207ME · Doug DC932 · Fuselage Miscellaneous Structure
  > GOUGES AND CORROSION ON INNER SKIN AND ANGLE BRACKETS OF LOWER BACK SIDE OF DOOR JAMB AFT PIT STATION 945-889. BLENDED CORROSION AND GOUGES. FABRICATED AND INSTALLED LOWER JAMB/INTERCOSTAL BRACKET. INSTALLED WEB STRAPS AT LONGERON 28 RIGHT AND 29 RIGHT.
- [SDR MWEA011426](https://openairdocs.org/sdr/MWEA011426.md): Frame · corroded · Nov 14, 2001 · N207ME · Doug DC932 · Fuselage Main, Frame
  > CORROSION ON J-CHANNEL FUSELAGE STATION 503 BETWEEN LONGERON 29 LEFT AND RIGHT. REMOVED CORROSION, CUT OUT DAMAGE IN FRAME. INSTALLED REPAIR SPLICE.
- [SDR MWEA011420](https://openairdocs.org/sdr/MWEA011420.md): Skin · dented · Nov 6, 2001 · N207ME · Doug DC932 · Elevator, Tab Structure
  > LEFT HAND ELEVATOR CONTROL TAB UPPER SURFACE HAS A DENT BETWEEN THE NR 3 AND NR 4 HINGE POINTS,.75 BY.5 INCH. FABRICATED CORE, FILLER AND DOUBLER. HOT BONDED REPAIR AND REPAINTED TRIM TAB. PERFORMED WEIGHT AND BALANCE.
- [SDR MWEA011421](https://openairdocs.org/sdr/MWEA011421.md): Skin · corroded · Nov 6, 2001 · N207ME · Doug DC932 · Fuselage Main, Plate/Skin
  > CORROSION ON INNER FUSELAGE SKIN ST STATION 889 AND 897 ON RIGHT HAND SIDE OF INTERCOSTAL AFT PIT. REMOVED, FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA011416](https://openairdocs.org/sdr/MWEA011416.md): Strap · corroded · Nov 1, 2001 · N207ME · Doug DC932 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP IN LONGERON 23 LEFT AT STATION 945 AFT PIT. BLENDED, FABRICATED AND INSTALLED LONGERON.
- [SDR MWEA011415](https://openairdocs.org/sdr/MWEA011415.md): Longeron · corroded · Nov 1, 2001 · N207ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 21 LEFT AT STATION 990 AFT PIT. BLENDED, DRILLED, LOCATED AND INSTALLED NEW LONGERON.
- [SDR MWEA011414](https://openairdocs.org/sdr/MWEA011414.md): Longeron · cracked · Oct 30, 2001 · N207ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > STATION 1087 LONGERON 7 RIGHT IS CRACKED. FABRICATED AND INSTALLED NEW LONGERON AND LONGERON SPLICE.
- [SDR MWEA011413](https://openairdocs.org/sdr/MWEA011413.md): Longeron · cracked · Oct 30, 2001 · N207ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > STATION 1087 LONGERON 7 LEFT IS CRACKED. REMOVED, FABRICATED AND INSTALLED LONGERON.
- [SDR MWEA011411](https://openairdocs.org/sdr/MWEA011411.md): Doubler · cracked · Oct 30, 2001 · N207ME · Doug DC932 · Fuselage Main, Plate/Skin
  > TWO AREAS OF CRACKS AROUND FASTENERS ON WINDOW INNER DOUBLER AT STATION 654 LOWER RIGHT CORNER AND AT STATION 643 UPPER LEFT CORNER OF DOUBLER. FABRICATED AND INSTALLED DOUBLERS.
- [SDR MWEA011130](https://openairdocs.org/sdr/MWEA011130.md): Gyro · failed · Aug 19, 2001 · N207ME · Doug DC932 · Attitude Gyro and Indicating System
  > ON CLIMB OUT WX RADAR ATT FAILURE DISPLAYED INTERMITTENTLY (MOSTLY ON) IN ALL RANGES. VERIFIED BAD NR 1 VG REMOVED AND REPLACED SAME, RETURNED ANTENNA CONNECTOR BACK TO J1 SYSTEM. OPERATION CHECK OK. REF DC9 MM 34-27-0 AND 34-41-0.
- [SDR MWEA011090](https://openairdocs.org/sdr/MWEA011090.md): Rib · gouged · Jul 18, 2001 · N207ME · Doug DC932 · Wing, Rib/Bulkhead
  > GOUGE ON INBOARD SLAT SUPPORT TRACK STATION 480.871. REMOVED AND REPLACED RIB.
- [SDR MWEA011089](https://openairdocs.org/sdr/MWEA011089.md): Skin · cracked · Jul 18, 2001 · N207ME · Doug DC932 · Leading Edge Devices
  > RIGHT WING SLAT DOOR CUT OUT BETWEEN NR 4 AND NR 5 SLAT SKIN IS CRACKED. TRIMMED OUT CRACK, INSTALLED FILLER AND DOUBLER.
- [SDR MWEA011087](https://openairdocs.org/sdr/MWEA011087.md): Longeron · damaged · Jul 18, 2001 · N207ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > LONGERON 6 RIGHT DAMAGED BETWEEN STATION 503 AND 522. BLENDED DAMAGED AND ATTACHED SPLICE PLATE OVER DAMAGE.
- [SDR MWEA010482](https://openairdocs.org/sdr/MWEA010482.md): Plate · out of adj · Mar 28, 2001 · N207ME · Doug DC932 · Door Warning System
  > ON TAKE OFF ROLL, FORWARD STAIRWAY DOOR ANNUNCIATOR CAME ON. -- ADJUSTED SWITCH STRIKER PLATE, PRESSURIZED AIRCRAFT TO 7 PSI, LIGHT REMAINED OFF.
- [SDR MWEA010391](https://openairdocs.org/sdr/MWEA010391.md): Pump · inoperative · Mar 25, 2001 · N207ME · Doug DC932 · Hydraulic Pump (Electric/Engine), Main
  > LEFT HYDRAULIC QUANTITY DROPPED TO 1 1/2 QUARTS IN FLIGHT, LEFT ENGINE DRIVER HYDRAULIC PUMP LEAKING. REPLACE LEFT ENGINE DRIVEN HYDRAULIC PUMP.
- [SDR MWEA010364](https://openairdocs.org/sdr/MWEA010364.md): Receiver · inoperative · Mar 21, 2001 · N207ME · Doug DC932 · Dependent Position Determining System
  > NR 2 NAV CIRCUIT BREAKER TRIPPED WHEN NR 2 ENGINE STARTED AND APU POWER SWITCHED TO ENGINE ELECTRICAL. REPLACED NR 2 NAV RECEIVER.
- [SDR MWEA010143](https://openairdocs.org/sdr/MWEA010143.md): Fuel Control · inoperative · Jan 31, 2001 · N207ME · Doug DC932 · Fuel Control/Turbine Engines
  > LEFT ENGINE WS SLOW TO SPOOL UP. REPLACED FUEL CONTROL UNIT ON LEFT ENGINE.
- [SDR MWEA010126](https://openairdocs.org/sdr/MWEA010126.md): Stringer · damaged · Jan 29, 2001 · N207ME · Doug DC932 · Wing, Longeron/Stringer
  > STRINGER 22 RIGHT DAMAGED IN RADIUS BEYOND LIMITS/BETWEEN XCW 20 RIGHT AND XCW 42 RIGHT. REMOVED AND REPLACED STRINGER REPAIR ANGLE.
- [SDR MWEA010130](https://openairdocs.org/sdr/MWEA010130.md): Rib · corroded · Jan 29, 2001 · N207ME · Doug DC932 · Wing, Rib/Bulkhead
  > RIGHT WING RIB STATION 69 WEB AND LOWER T-EXTRUSION HAS AREAS OF MODERATE CORROSION FROM AFT SPAR TO STRINGER 17. REMOVED AND REPLACED T-CORD.
- [SDR MWEA010129](https://openairdocs.org/sdr/MWEA010129.md): Bulkhead · cracked · Jan 29, 2001 · N207ME · Doug DC932 · Fuselage Main, Bulkhead
  > LEFT FORWARD WEB ON BULKHEAD AT STATION 965 CRACKED NEAR SUBFLOOR, OUTBOARD OF NR 1 SEAT TRACK. FABRICATED AND INSTALLED WEB.
- [SDR MWEA010128](https://openairdocs.org/sdr/MWEA010128.md): Floorboard · damaged · Jan 29, 2001 · N207ME · Doug DC932 · Fuselage Floor Panel
  > HOLE IN SUBFLOOR, RIGHT SIDE JUST AFT OF STATION 945, OUTBOARD OF NR 4 SEAT TRACK. FABRICATED AND INSTALLED DOUBLERS.
- [SDR MWEA010127](https://openairdocs.org/sdr/MWEA010127.md): Longeron · cracked · Jan 29, 2001 · N207ME · Doug DC932 · Fuselage Main, Longeron/Stringer
  > LONGERON 17 LEFT IS CRACKED AT STATION 965. FABRICATED AND INSTALLED LONGERON AND SPLICES.
- [SDR MWEA010125](https://openairdocs.org/sdr/MWEA010125.md): Panel · corroded · Jan 29, 2001 · N207ME · Doug DC932 · Fuselage Main, Plate/Skin
  > WINDOW NR 19 LEFT BELT PANEL HAS CORROSION IN ZONE 1 (INTERNAL) ON RIGHT SIDE. REMOVED AND REPLACED WINDOW BELT.
- [SDR MWEA010124](https://openairdocs.org/sdr/MWEA010124.md): Skin · corroded · Jan 29, 2001 · N207ME · Doug DC932 · Ailerons
  > RIGHT AILERON UPPER OUTBOARD SKIN JUST FORWARD OF STATIC WICK HAS A SPOT OF CORROSION. FABRICATED AND INSTALLED DOUBLER.

Next page: https://openairdocs.org/deregistered/N207ME-2005-04-18/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 = 'N207ME' AND deregistration_id = 'N207ME-2005-04-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N207ME-2005-04-18/reports

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