# Service difficulty reports: N216ME, cancelled Jan 24, 2005

A list on [N216ME, cancelled Jan 24, 2005](https://openairdocs.org/deregistered/N216ME-2005-01-24.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 · 268 reports

- [SDR MWEA030367](https://openairdocs.org/sdr/MWEA030367.md): Skin · canning · Sep 9, 2003 · N216ME · Doug DC932 · Fuselage Main, Plate/Skin
  > STATION 959 LONGERON 18 RIGHT & LONGERON 16 RIGHT EVIDENCE OF OIL CANNING UNDER RIGHT PYLON. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA030366](https://openairdocs.org/sdr/MWEA030366.md): Skin · canning · Sep 9, 2003 · N216ME · Doug DC932 · Fuselage Main, Plate/Skin
  > EVIDENCE OF OIL CANNING ON RIGHT SIDE OF FUSELAGE UNDER PYLON STATION 988 LONGERON 17,18 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA030365](https://openairdocs.org/sdr/MWEA030365.md): Skin · canning · Sep 9, 2003 · N216ME · Doug DC932 · Fuselage Main, Plate/Skin
  > EVIDENCE OF OIL CANNING RIGHT SIDE OF FUSELAGE UNDER PYLON STATION 1006 LONGERON 8 RIGHT AND LONGERON 17 RIGHT. FABRICATED AND INSTALLED REPAIR SPLICE AND DOUBLER.
- [SDR MWEA030402](https://openairdocs.org/sdr/MWEA030402.md): Skin · canning · Mar 10, 2003 · N216ME · Doug DC932 · Fuselage Main, Frame
  > EVIDENCE OF OIL CANNING ON LEFT SIDE OF FUSELAGE STATION 1025. INSTALLED DOUBLER.
- [SDR MWEA030129](https://openairdocs.org/sdr/MWEA030129.md): Engine · failed · Mar 5, 2003 · N216ME · Doug DC932 · Engine Emergency Shutdown System
  > AT 32,500 FEET AIRCRAFT SUFFERED SEVERE ENGINE VIBRATION, RIGHT ENGINE OIL PRESSURE WENT TO ZERO AND RIGHT HYDRAULIC FLUIDS QUANTITY WAS AT ZERO. REMOVED AND REPLACED ENGINE.
- [SDR MWEA030120](https://openairdocs.org/sdr/MWEA030120.md): Warning Light · illuminated · Feb 28, 2003 · N216ME · Doug DC932 · Engine Cranking
  > RT START ENGINE VALVE ANNUNCIATOR STAYED ON. VERIFIED VALVE CLOSED, LIGHT IN COCKPIT OUT, COULD NOT DULPICATE AT THIS TIME.
- [SDR MWEA030009](https://openairdocs.org/sdr/MWEA030009.md): Filter · defective · Jan 7, 2003 · N216ME · Doug DC932 · Hydraulic Filter, Auxiliary
  > RIGHT HYDRAULIC SYSTEM FLUID QUANTITY DEPLETED AND LOST PRESSURE. REMOVED AND REPLACED AUXILIARY LINE FILTER HOUSING AND FILTERS.
- [SDR MWEA020741](https://openairdocs.org/sdr/MWEA020741.md): Bearing · not seated · Dec 17, 2002 · N216ME · Doug DC932 · Landing Gear Retraction/Extension System
  > WHEN GEAR RETRACTED ALL LIGHTS OUT, EXCEPT THE LEFT GEAR UNSAFE LIGHT. MAINTENANCE RESEATED LEFT UPLATCH HOOK CENTER BEARINGS.
- [SDR MWEA020452](https://openairdocs.org/sdr/MWEA020452.md): Switch · faulty · Jul 18, 2002 · N216ME · Doug DC932 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS, NO SMOKING LIGHTS AND FASTEN SEATBELT LIGHTS FLASHING ON AND OFF RAPIDLY. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT SWITCH AND B5-23 BATTERY PACK FOR PRECAUTION.
- [SDR MWEA020449](https://openairdocs.org/sdr/MWEA020449.md): Stringer · corroded · Jul 17, 2002 · N216ME · Doug DC932 · Wing, Longeron/Stringer
  > RIGHT WING STRINGER 21 HAS LIGHT CORROSION ON UPPER AND LOWER AFT LEG BETWEEN XRS 91&111. BLENDED CORROSION OUT OF STRINGER.
- [SDR MWEA020448](https://openairdocs.org/sdr/MWEA020448.md): Gyro · failed · Jul 16, 2002 · N216ME · Doug DC932 · Attitude Gyro and Indicating System
  > CAPTAIN'S ATTITUDE INDICATOR FAILED. REMOVED AND REPLACED NR 1 VERTICAL GYRO. OPS CHECK OK REF MM 34-27-0.
- [SDR MWEA020445](https://openairdocs.org/sdr/MWEA020445.md): Stiffener · corroded · Jul 12, 2002 · N216ME · Doug DC932 · Wing Miscellaneous Structure
  > RIGHT WING LIGHT CORROSION ON UPPER SURFACE OF HORIZONTAL STIFFENER ON INBOARD SIDE OF XRS 91 RIB ABOVE STRINGERS 17 TO 19. REMOVED AND INSTALLED STIFFENER AND FLAPPER VALVE.
- [SDR MWEA020433](https://openairdocs.org/sdr/MWEA020433.md): Skin · dented · Jun 28, 2002 · N216ME · Doug DC932 · Fuselage Main, Plate/Skin
  > FUSELAGE DENT AT STATION 353 1.5 INCH BELOW LONGERON 29 LEFT. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA020432](https://openairdocs.org/sdr/MWEA020432.md): Gusset · corroded · Jun 28, 2002 · N216ME · Doug DC932 · Fuselage Miscellaneous Structure
  > AFT PIT STRAP ON DOOR THRESHOLD CORRODED BETWEEN STATION 904 AND STATION 885 LONGERON 29 LEFT. REMOVED AND INSTALLED GUSSET.
- [SDR MWEA020431](https://openairdocs.org/sdr/MWEA020431.md): Splice · cracked · Jun 28, 2002 · N216ME · Doug DC932 · Fuselage Miscellaneous Structure
  > LONGERON SPLICE CRACKED AT FS415 AND 29 LEFT. FABRICATED AND INSTALLED SPLICE AND SHIMS.
- [SDR MWEA020430](https://openairdocs.org/sdr/MWEA020430.md): Fitting · cracked · Jun 28, 2002 · N216ME · Doug DC932 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY HAS A CRACKED FITTING ON FRAME 503 AT LONGERON 28 RIGHT. REMOVED AND INSTALLED FITTING.
- [SDR MWEA020429](https://openairdocs.org/sdr/MWEA020429.md): Stop Fitting · stripped · Jun 28, 2002 · N216ME · Doug DC932 · Fuselage Main, Structure
  > PAX JAMB DOOR STOP FITTING (THIRD FROM BOTTOM AFT JAMB) HAS STRIPPED OUT THREADS. REMOVED AND INSTALLED FITTING.
- [SDR MWEA020444](https://openairdocs.org/sdr/MWEA020444.md): Frame · corroded · Jun 25, 2002 · N216ME · Doug DC932 · Fuselage Main, Frame
  > FORWARD CARGO BAY FRAME AT STATION 446 LONGERON 30 IS EXFOLIATED. INSTALLED FRAME SECTION AND SPLICE.
- [SDR MWEA020266](https://openairdocs.org/sdr/MWEA020266.md): Odor · detected · Apr 22, 2002 · N216ME · Doug DC932 · Buffet/Galleys
  > CREW REPORTED STRONG CHEMICAL SMELL IN FORWARD GALLEY AREA OF AIRCRAFT. CLEANED CARPETING, REMOVED AND REPLACED WATER SOCKS, VERIFIED APU SERVICING. OPERATED BOTH ENGINES AND APU. PRESSURIZED AIR CONDITIONING SYSTEM AND PRESSURIZATION SYSTEM. NO SMELLS NOT
- [SDR MWEA020260](https://openairdocs.org/sdr/MWEA020260.md): Switch · faulty · Apr 14, 2002 · N216ME · Doug DC932 · High Speed Warning
  > AT 90 KNOTS, THE OVERSPEED WARNING WENT OFF. REMOVED AND REPLACED CAPTAIN'S OVERSPEED WARNING SWITCH.
- [SDR MWEA020259](https://openairdocs.org/sdr/MWEA020259.md): Sensor · faulty · Apr 12, 2002 · N216ME · Doug DC932 · High Speed Warning
  > THE OVERSPEED WARNING WENT OFF. REJECTED TAKEOFF. REMOVED AND REPLACED OVERSPEED SENSOR, OPS CHECK OK.
- [SDR MWEA020258](https://openairdocs.org/sdr/MWEA020258.md): Warning System · out of adjust · Apr 11, 2002 · N216ME · Doug DC932 · High Speed Warning
  > OVERSPEED WARNING SOUNDED. REJECTED TAKEOFF AT LESS THAN 20 KTS. DEFERRED OVERSPEED WARNING. PERFORMED ADJUSTMENT/TEST OF OVERSPEED WARNING SYSTEM. REF MM 34-10-5. NO DEFECTS NOTED.
- [SDR MWEA020166](https://openairdocs.org/sdr/MWEA020166.md): Engine · leaking · Mar 13, 2002 · N216ME · Doug DC932 · Engine (Turbine/Turboprop)
  > LEFT ENGINE OIL PRESSURE DECREASING, LEFT TEMPERATURE RISING INTO YELLOW ARCH 120 DEGREES CELSIUS. REDUCED POWER TO IDLE, OIL QUANTITY WENT TO ZERO, OIL PRESSURE LOW LIGHT CAME ON, OIL PRESSURE INDICATED 30 PSI. PERFORMED ENGINE SHUT DOWN PER QRH. MAINTENAN
- [SDR MWEA011459](https://openairdocs.org/sdr/MWEA011459.md): Battery Pack · failed · Nov 25, 2001 · N216ME · Doug DC932 · Emergency Lighting
  > COCKPIT LIGHTS CABIN SIDEWALL LIGHTS AND THE EMERGENCY EXIT LIGHTS ABOVE THE FORWARD PAX AND GALLEY DOOR ARE ALL PULSING. -- REPLACED EMERGENCY BATTERY PACK.
- [SDR MWEA010995](https://openairdocs.org/sdr/MWEA010995.md): Skin · damaged · Jun 18, 2001 · N216ME · Doug DC932 · Elevator Control System
  > LEFT ELEVATOR UPGRADE REPAIR INSTALLED AT STATION XHS 70 TO SRM 55-03 FIGURE 14. -- REMOVED SKIN, FABRICATED NEW SKIN AND FINGER DOUBLER, INSTALLED SKIN.
- [SDR MWEA010994](https://openairdocs.org/sdr/MWEA010994.md): Skin · cracked · Jun 18, 2001 · N216ME · Doug DC932 · Passenger/Crew Doors
  > FORWARD PAX DOOR SKIN HAS A SMALL CRACK AT THE LOWER SIDE OF THE HOLD OPEN HOOK CUT OUT. -- REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA010993](https://openairdocs.org/sdr/MWEA010993.md): Frame · damaged · Jun 18, 2001 · N216ME · Doug DC932 · Fuselage Main, Structure
  > EXTERIOR FUSELAGE HAS LIGHTENING STRIKES AT WINDOW 9L. -- BLENDED OUT DAMAGED AREAS, LOCATED AND DRILLED DOUBLER, INSTALLED REPAIR AT WINDOW.
- [SDR MWEA010992](https://openairdocs.org/sdr/MWEA010992.md): Seat Track · corroded · Jun 18, 2001 · N216ME · Doug DC932 · Fuselage Main, Structure
  > #3 SEAT TRACK CORRODED AT FORWARD END APPROXIMATELY STATION 200. -- REMOVED CORROSION, REMOVED DAMAGED SECTION OF SEAT TRACK, LOCATED AND DRILLED AND INSTALLED NEW SEAT TRACK.
- [SDR MWEA010991](https://openairdocs.org/sdr/MWEA010991.md): Frame · gouged · Jun 18, 2001 · N216ME · Doug DC932 · Fuselage Main, Structure
  > WINDOW 9L INNER WINDOW FRAME HAS SEVERAL MODERATE GOUGES/TOOL MARKS IN RADIUS OF FRAME BOTH FORWARD AND AFT SIDES. -- BLENDED TOOL MARKS, LOCATED AND DRILLED NEW INNER WINDOW FRAME, INSTALLED WINDOW RETAINER.
- [SDR MWEA010990](https://openairdocs.org/sdr/MWEA010990.md): Bracket · elongated · Jun 18, 2001 · N216ME · Doug DC932 · Fuselage Main, Structure
  > ATTACH BRACKET HOLES ELONGATED FORWARD AND AFT, FORWARD CARGO DOOR HINGES ATTACH TO FUSELAGE. -- FABRICATED AND INSTALLED DOUBLERS.
- [SDR MWEA010989](https://openairdocs.org/sdr/MWEA010989.md): Skin · cracked · Jun 18, 2001 · N216ME · Doug DC932 · Fuselage Main, Structure
  > EXTERIOR SKIN ABOVE FORWARD PAX DOOR HOLD OPEN HOOK CUT OUT HAS TWO SMALL CRACKS. -- TRIMMED, LOCATED AND DRILLED PLATE AND DOUBLERS, INTSTALLED DOUBLERS, PAN, PIN.
- [SDR MWEA010988](https://openairdocs.org/sdr/MWEA010988.md): Tab · delaminated · Jun 18, 2001 · N216ME · Doug DC932 · Elevator Control System
  > RIGHT ELEVATOR GEARED TAB HAS TWO AREAS OF DELAMINATION ON PREVIOUS REPAIR. 1.5" BY 6.0" AREA ON TOP AND 4.0" BY 2.5" AREA ON BOTTOM. -- REMOVED DELAMINATED REPAIR, BONDED ON NEW REPAIR.
- [SDR MWEA010941](https://openairdocs.org/sdr/MWEA010941.md): Angle · cracked · Jun 12, 2001 · N216ME · Doug DC932 · Nacelle/Pylon, Main Frame
  > STATION 980 ANGLE ON THE TOP OF RIGHT PYLON IS CRACKED. REMOVED DAMAGED ANGLE, FABRICATED NEW ANGLE AND REPAIR STRAPS, INSTALLED REPAIR PARTS.
- [SDR MWEA010940](https://openairdocs.org/sdr/MWEA010940.md): Fitting · cracked · Jun 12, 2001 · N216ME · Doug DC932 · Cargo/Baggage Doors
  > AFT CARGO DOOR FORWARD NR 5 BEAM END FITTING CRACKED. REMOVED CRACK AND FITTING, POSITIONED AND DRILLED NEW FITTING, INSTALLED NEW FITTING.
- [SDR MWEA010939](https://openairdocs.org/sdr/MWEA010939.md): Intercostal · cracked · Jun 12, 2001 · N216ME · Doug DC932 · Fuselage Miscellaneous Structure
  > INTERCOSTAL JUST ABOVE AND INBOARD OF YAW DAMPENER ACTUATOR IS CRACKED. REMOVED CRACKED INTERCOSTAL, FABRICATED AND INSTALLED NEW INTERCOSTAL.
- [SDR MWEA010938](https://openairdocs.org/sdr/MWEA010938.md): Shear Tie · cracked · Jun 12, 2001 · N216ME · Doug DC932 · Fuselage Main, Structure
  > RIGHT LAVATORY SHEAR TIE CRACKED ON FRAME 980 JUST BELOW LONGERON 14 RIGHT. LOCATED, DRILLED AND INSTALLED NEW SHEAR TIE.
- [SDR MWEA010937](https://openairdocs.org/sdr/MWEA010937.md): Frame · cracked · Jun 12, 2001 · N216ME · Doug DC932 · Fuselage Main, Frame
  > FRAME STATION 699 LEFT HAS AN APPROXIMATELY 3.5 INCH CRACK IN LOWER POCKET AFT HORIZONTAL AND VERTICAL FLANGE AREA. REMOVED TWO MOUNT BRACKETS FROM FRAME, FABRICATED SHIM, LOCATED AND DRILLED HOLES IN DOUBLER, LOCATED AND INSTALLED COVER, INSTALLED DOUBLER AND
- [SDR MWEA010936](https://openairdocs.org/sdr/MWEA010936.md): Window Frame · cracked · Jun 12, 2001 · N216ME · Doug DC932 · Passenger Compartment Windows
  > RIGHT CABIN WINDOW FRAME BETWEEN STATION 639-658 INNER DOUBLER CRACKED AT LOWER AFT CORNER. FABRICATED REPAIR, INSTALLED STACKED ANGLE REPAIR.
- [SDR MWEA010935](https://openairdocs.org/sdr/MWEA010935.md): Web · cracked · Jun 12, 2001 · N216ME · Doug DC932 · Nacelle/Pylon, Main Frame
  > RIGHT PYLON WEB IS CRACKED APPROXIMATELY 6 INCHES BELOW FIRE EXTINGUISHER DISCHARGE TUBE. FABRICATED AND INSTALLED REPAIR DOUBLERS.
- [SDR MWEA010932](https://openairdocs.org/sdr/MWEA010932.md): Floorboard · corroded · Jun 12, 2001 · N216ME · Doug DC932 · Fuselage Floor Panel
  > FLOORBOARD SKIN CORRODED BETWEEN FIRST OFFICERS AFT SEAT TRACK, FORWARD OF STATION 160. BLENDED CORRODED AREA, MADE NEW SKIN.
- [SDR MWEA010931](https://openairdocs.org/sdr/MWEA010931.md): Seat Track · corroded · Jun 12, 2001 · N216ME · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > NR 4 SEAT TRACK CORRODED FROM STATION 200-237. REMOVED CORROSION, FABRICATED NEW SEAT TRACK SECTION, INSTALLED SEAT TRACK AND SPLICES.
- [SDR MWEA010929](https://openairdocs.org/sdr/MWEA010929.md): Skin · cracked · Jun 12, 2001 · N216ME · Doug DC932 · Fuselage Main, Plate/Skin
  > RIGHT LAVATORY SKIN IS CRACKED AT STATION 990 APPROXIMATELY 2.5 INCH CRACK 2 INCHES BELOW LONGERON 14 RIGHT. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED DOUBLER, FILLER AND SHIM.
- [SDR MWEA010928](https://openairdocs.org/sdr/MWEA010928.md): Angle · cracked · Jun 12, 2001 · N216ME · Doug DC932 · Fuselage Miscellaneous Structure
  > RIGHT LAVATORY TOP STIFFENER FRAME ON AFT PRESSURE BULKHEAD THE INBOARD ANGLE THAT ATTACHES TO THE DOOR FRAME IS CRACKED. REMOVED DAMAGE, FABRICATED, LOCATED AND INSTALLED NEW ANGLE.
- [SDR MWEA010927](https://openairdocs.org/sdr/MWEA010927.md): Skin · cracked · Jun 12, 2001 · N216ME · Doug DC932 · Fuselage Main, Plate/Skin
  > LEFT LAV SKIN IS CRACKED JUST BELOW SHEAR TIE AND ABOVE LONGERON 16 LEFT STATION 980. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND FILLER, LOCATED AND DRILLED REPAIR PARTS, INSTALLED DOUBLER, FILLER AND SHIM.
- [SDR MWEA010926](https://openairdocs.org/sdr/MWEA010926.md): Skin · cracked · Jun 12, 2001 · N216ME · Doug DC932 · Fuselage Main, Plate/Skin
  > LEFT LAV SKIN IS CRACKED 2 INCH BELOW LONGERON 14 LEFT STATION 990. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER.
- [SDR MWEA010925](https://openairdocs.org/sdr/MWEA010925.md): Stiffener · cracked · Jun 12, 2001 · N216ME · Doug DC932 · Fuselage Miscellaneous Structure
  > RIGHT LAV BOTTOM AFT PRESSURE BULKHEAD 996 STIFFENER FRAME WEB PORTION IS CRACKED AT OUTBOARD END. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS.
- [SDR MWEA010924](https://openairdocs.org/sdr/MWEA010924.md): Floorboard · damaged · Jun 12, 2001 · N216ME · Doug DC932 · Fuselage Floor Panel
  > CABIN FLOOR PANEL B9 HAS A HOLE IN TOP SURFACE NEAR CENTER OF PANEL. REMOVED FLOORBOARD, REPAIRED AND INSTALLED.
- [SDR MWEA010923](https://openairdocs.org/sdr/MWEA010923.md): Web · damaged · Jun 12, 2001 · N216ME · Doug DC932 · Fuselage Miscellaneous Structure
  > SUBFLOORING FASTENER HOLES LOCATED UNDERNEATH SEAT TRACK NR 4 BETWEEN STATION 218 TO APPROXIMATELY 245 ARE ELONGATED. FABRICATED AND INSTALLED DOUBLER REPAIR.
- [SDR MWEA010922](https://openairdocs.org/sdr/MWEA010922.md): Floorboard · cracked · Jun 12, 2001 · N216ME · Doug DC932 · Fuselage Floor Panel
  > FLOOR PANEL A7 AT STATION 756 IS CRACKED. REMOVED DAMAGED END OF FLOOR PANEL, FABRICATED AND INSTALLED FILLER MATERIAL AND DOUBLER.
- [SDR MWEA010921](https://openairdocs.org/sdr/MWEA010921.md): Floorboard · cracked · Jun 12, 2001 · N216ME · Doug DC932 · Fuselage Floor Panel
  > FLOOR PANEL E6 AT STATION 579 IS CRACKED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER.

Next page: https://openairdocs.org/deregistered/N216ME-2005-01-24/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 = 'N216ME' AND deregistration_id = 'N216ME-2005-01-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N216ME-2005-01-24/reports

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