# Service difficulty reports: N301ME, cancelled Mar 25, 2004 A list on [N301ME, cancelled Mar 25, 2004](https://openairdocs.org/deregistered/N301ME-2004-03-25.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 5 · 226 reports - [SDR MWEA030494](https://openairdocs.org/sdr/MWEA030494.md): Downlock Switch · inoperative · Dec 15, 2003 · N301ME · Doug DC932 · Landing Gear Position and Warning > RT MLG GREEN LIGHT STAYED ON. REPLACED RT MLG DOWNLOCK SWITCH. - [SDR MWEA030431](https://openairdocs.org/sdr/MWEA030431.md): Skin · damaged · Oct 23, 2003 · N301ME · Doug DC932 · Elevator, Plate/Skin > RIGHT ELEVATOR HAS DAMAGE AT INBOARD TRAILING EDGE 1INCH X.5000 HOLE IN TOP SKIN. EXTERNAL SKIN REPAIR. - [SDR MWEA030430](https://openairdocs.org/sdr/MWEA030430.md): Skin · lightning strike · Oct 23, 2003 · N301ME · Doug DC932 · Fuselage Main, Plate/Skin > EXTERNAL FUSELAGE SKIN HAS SEVERAL LIGHTING STRIKES AT FRAME STATION 256 LONGERON 29 LEFT. CUT OUT DAMAGE AND INSTALLED FLUSH REPAIR. - [SDR MWEA030429](https://openairdocs.org/sdr/MWEA030429.md): Skin · damaged · Oct 23, 2003 · N301ME · Doug DC932 · Elevator, Plate/Skin > RIGHT ELEVATOR HAS DAMAGE TO OUTBOARD TRAILING EDGE 1INCH X.5 INCH. INSTALLED EXTERNAL DOUBLER. - [SDR MWEA030428](https://openairdocs.org/sdr/MWEA030428.md): Frame · cracked · Oct 23, 2003 · N301ME · Doug DC932 · Fuselage Main, Frame > CRACK AT FUSELAGE FRAME STATION 718 LEFT OUTBOARD FORWARD FLANGE HAS GROWN FROM 6 INCHES TO 7.6250. -- INSTALLED DOUBLER. - [SDR MWEA030377](https://openairdocs.org/sdr/MWEA030377.md): Start Valve · inoperative · Sep 17, 2003 · N301ME · Doug DC932 · Engine Start Valves/Controls > RIGHT ENGINE HIGH-PRESSURE COMPRESSOR SHAFT SPEED WOULD NOT RISE ABOVE 13 PERCENT, HIGH-PRESSURE COMPRESSOR SHAFT SPEED ABORTED START. REMOVED AND REPLACED RIGHT ENGINE START VALVE. - [SDR MWEA030364](https://openairdocs.org/sdr/MWEA030364.md): Doubler · corroded · Sep 7, 2003 · N301ME · Doug DC932 · Fuselage Main, Plate/Skin > CORROSION FOUND ON COVER PLATE AND ON FUSELAGE. REMOVED AND REPLACED REPAIR DOUBLER. - [SDR MWEA030317](https://openairdocs.org/sdr/MWEA030317.md): Wire · open · Aug 18, 2003 · N301ME · Doug DC932 · Landing Gear System Wiring > UNABLE TO GET A GREEN DOWN LIGHT. FOUND OPEN WIRES IN RIGHT GEAR DOWN CONNECTOR, ALL ASSOCIATED WIRES WERE REPLACED. - [SDR MWEA030136](https://openairdocs.org/sdr/MWEA030136.md): Fuel Control · out of adjust · Mar 20, 2003 · N301ME · Doug DC932 · Fuel Controlling System > LEFT ENGINE HUNG AT ABOUT 45 PERCENT AND ROLLED BACK TO ABOUT 40 PERCENT. ADJUSTED IDLE AND DRAINED MOISTURE TRAP. - [SDR MWEA030135](https://openairdocs.org/sdr/MWEA030135.md): Seat Track · defective · Mar 18, 2003 · N301ME · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings > FIRST OFFICER SEAT HITS THE HI-LOCS ON SEAT TRACK OUTBOARD OF EXSISTING REPAIR. -- INSTALLED STAINLESS STEEL STRAP ON SEAT TRACK OUTBOARD AND REMOVED AND REPLACED SEAT TRACK. - [SDR MWEA030111](https://openairdocs.org/sdr/MWEA030111.md): Flange · elongated · Feb 22, 2003 · N301ME · Doug DC932 · Flight Compartment Equipment > FIRST OFFICER AFT INBOARD SEAT TRACK FOUND ENLONGATED HOLES. -- REMOVED AND REPLACED UPPER FLANGE OF FIRST OFFICER'S INBOARD SEAT TRACK. - [SDR MWEA020722](https://openairdocs.org/sdr/MWEA020722.md): Skin · damaged · Nov 26, 2002 · N301ME · Doug DC932 · Fuselage Main, Plate/Skin > SKIN AT STATION 1121 LONGERON LEFT 18 HAS A APPROXIMATE 1.5" HOLE. -- REMOVED AND REPLACED SKIN. - [SDR MWEA020475](https://openairdocs.org/sdr/MWEA020475.md): Spoiler · chafed · Aug 13, 2002 · N301ME · Doug DC932 · Spoilers > INBOARD FLIGHT SPOILER OUTBOARD HINGE SUPPORT IS CHAFED. TAG #1 RIGHT WING. -- SUPPORT IS CHAFED TO LIMITS. LOCATED AND DRILLED NEW FITTINGS. - [SDR MWEA020474](https://openairdocs.org/sdr/MWEA020474.md): Wing · delaminated · Aug 13, 2002 · N301ME · Doug DC932 · Trailing Edge Flaps > LEFT WING AFT SIDE OF WING FLAP TRAILING EDGE PANEL IS DELAMINATED AT FORWARD OUTBOARD CORNER DOT.18. -- FABRICATED AND INSTALLED SKIN. - [SDR MWEA020420](https://openairdocs.org/sdr/MWEA020420.md): Controller · malfunctioned · Jun 8, 2002 · N301ME · Doug DC932 · Cabin Pressure Controller > PRESSURIZATION INOP DURING CLIMB, SWITCHED TO MANUALLY CONTROLLED PRESSURIZATION AT CRUISE ABOUT 10 MINUTES. CABIN WENT TO FULL CLIMB BUT COULD NOT BE CONTROLLED MANUALLY. INITIATED EMERGENCY DESCENT, HAD NORMAL PACK PRESSURE. DEFERRED PER MEL 21-25 T FUNCT - [SDR MWEA020308](https://openairdocs.org/sdr/MWEA020308.md): Shear Tie · damaged · Apr 29, 2002 · N301ME · Doug DC932 · Fuselage Miscellaneous Structure > DAMAGED LOWER SECTION OF SHEAR TIE AT STATION 965 LEFT HAND DURING THE REMOVAL OF SHEAR TIE TO FACILITATE OTHER MAINTENANCE. -- INSTALLED WITH NEW LOWER SECTION OF SHEAR TIE AT STATION 965 LEFT HAND IAW SRM 51-30-5. - [SDR MWEA020307](https://openairdocs.org/sdr/MWEA020307.md): Longeron · corroded · Apr 29, 2002 · N301ME · Doug DC932 · Fuselage Main, Longeron/Stringer > CORROSION PRESENT ON LONGERON 23 LEFT AT STATION 946. REMOVED DAMAGED SECTION OF LONGERON AND INSTALLED REPAIR SECTION AND SPLICES. - [SDR MWEA020305](https://openairdocs.org/sdr/MWEA020305.md): Doubler · corroded · Apr 29, 2002 · N301ME · Doug DC932 · Fuselage Miscellaneous Structure > SUGAR SCOOP ATTACH RING DOUBLER CORRODED ON AFT END AT 2 SPOTS. -- REMOVED ATTACH RING DOUBLER. LOCATED AND INSTALLED NEW DOUBLER IAW SRM 51-30. - [SDR MWEA020304](https://openairdocs.org/sdr/MWEA020304.md): Longeron · damaged · Apr 29, 2002 · N301ME · Doug DC932 · Fuselage Main, Longeron/Stringer > LONGERON 19 LEFT CUT AT STATION 956 AND AFT SECTION MOVED TO FACILITATE OTHER MAINTENANCE. INSTALLED SPLICE PER SRM 51-30-5. INSTALLED LONGERON 19 IAW SRM 51-50-5. - [SDR MWEA020303](https://openairdocs.org/sdr/MWEA020303.md): Longeron · unserviceable · Apr 29, 2002 · N301ME · Doug DC932 · Fuselage Main, Longeron/Stringer > LONGERON 22 LEFT CUT AT STATION 956 AND AFT SECTION REMOVED TO FACILITATE OTHER MAINTENANCE. -- SPLICED SEGMENT OF LONGERON 22 LEFT AT STATION 956 AND AFT SECTION IAW SRM 53-02 FIG 18. - [SDR MWEA020302](https://openairdocs.org/sdr/MWEA020302.md): Frame · corroded · Apr 29, 2002 · N301ME · Doug DC932 · Fuselage Main, Frame > FRAME AT 965 IS CORRODED BETWEEN LONGERON 22 AND 23 LEFT. -- REMOVED AND REPLACED FRAME SECTION. - [SDR MWEA020301](https://openairdocs.org/sdr/MWEA020301.md): Shear Tie · elongated · Apr 29, 2002 · N301ME · Doug DC932 · Fuselage Miscellaneous Structure > SHEAR TIE AT STATION 965 BETWEEN LONGERON 20 LEFT AND LONGERON 128 LEFT HAS OBLONG HOLE COMMON TO SKIN. -- REMOVED AND REPLACED UPPER SECTION OF SHEAR TIE. - [SDR MWEA020299](https://openairdocs.org/sdr/MWEA020299.md): Doubler · worn · Apr 29, 2002 · N301ME · Doug DC932 · Fuselage Miscellaneous Structure > LAVATORY SERVICE PANEL 2 UPPER LATCHES WORN THRU DOUBLERS. -- REPAIRED BY INSTALLING DOUBLER PER IAW TELEX MWX-ORD-02-002-00249H DATED APRIL 18 2002. - [SDR MWEA020300](https://openairdocs.org/sdr/MWEA020300.md): Gusset · corroded · Apr 19, 2002 · N301ME · Doug DC932 · Fuselage Miscellaneous Structure > FRAME TO STRUT GUSSET, LEFT SIDE AT STATION 965 CORRODED. -- REMOVED AND REPLACED GUSSET. - [SDR MWEA020136](https://openairdocs.org/sdr/MWEA020136.md): Frame · cracked · Feb 23, 2002 · N301ME · Doug DC932 · Fuselage Main, Structure > RIGHT FUSELAGE FRAME AT STATION 718 IS CRACKED (REF WI 3673). -- INSTALLED 7075-T651.375 DOUBLER ON STATION 718 FRAME. REQUIRES DOUBLER INSTALLATION PER SERVICE BULLETIN 53-100. - [SDR MWEA011011](https://openairdocs.org/sdr/MWEA011011.md): Harness · defective · Jul 2, 2001 · N301ME · Doug DC932 · Landing Gear Position and Warning > NO NOSE LANDING GEAR SAFE (GREEN EXTENDED) OR OTHER LIGHT OR VISUAL INDICATION. REMOVED AND REPLACED UP LIMIT SWITCH WIRING HARNESS, CLEANED NOSE GEAR VIEWING COMPONENTS. - [SDR MWEA011006](https://openairdocs.org/sdr/MWEA011006.md): Fitting · cracked · Jun 28, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > FRAME ATTACH FITTING FORWARD SPAR CENTER TANK STATION XCW 40 LEFT IS CRACKED. -- LOCATED AND INSTALLED NEW FITTING. - [SDR MWEA011005](https://openairdocs.org/sdr/MWEA011005.md): Angle · cracked · Jun 28, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > RIGHT WING TO FUSELAGE FITTING AT STATION 604 LONGERON 22 RIGHT IS CRACKED. -- REMOVED FITTING, LOCATED AND INSTALLED NEW FITTING. - [SDR MWEA010985](https://openairdocs.org/sdr/MWEA010985.md): Skin · gouged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > GOUGE AT STATION 813 BETWEEN LONGERONS 25 AND 26 RIGHT. -- BLENDED GOUGE, CUT OUT SKIN, REMOVED LOWER FLANGE OF SHEAR TIES, FABRICATED REPAIR, INSTALLED REPAIR DOUBLER AND SKIN REPAIR, FABRICATED SHEAR TIE REPAIR ANGLES, INSTALLED SHEAR TIES. - [SDR MWEA010984](https://openairdocs.org/sdr/MWEA010984.md): Floorboard · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > REMOVED CABIN FLOORBOARD B10 TO FACILITATE OTHER MAINTENANCE. -- FABRICATED NEW SKIN AND HAT SECTIONS, INSTALLED INSULATION AND SHIM MATERIAL. - [SDR MWEA010983](https://openairdocs.org/sdr/MWEA010983.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > UPPER FUSELAGE FRAME STATION 737 HAS THREE HOLES THAT DO NOT HAVE (2D) SPACING BETWEEN LONGERONS 5 AND 6 LEFT. -- PLUGGED HOLES, FABRICATED, LOCATED AND DRILLED REPAIR ANGLES, INSTALLED REPAIR. - [SDR MWEA010979](https://openairdocs.org/sdr/MWEA010979.md): Intercostal · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > FORWARD ENTRY INTERCOSTAL HAS FIVE OPEN FASTENER HOLES AND INNER LEG HAS MATERIAL TRIMMED OUT STATION 228 ABOVE LONGERON 11 LEFT. -- FABRICATED AND INSTALLED REPAIR ANGLES. - [SDR MWEA010978](https://openairdocs.org/sdr/MWEA010978.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > UPPER FUSELAGE FRAME STATION 889 HAS THREE HOLES THAT DO NOT HAVE (2D) SPACING BETWEEN LONGERON 5 AND 6 LEFT. -- FABRICATED, LOCATED AND DRILLED REPAIR ANGLE AND FILLER, INSTALLED REPAIR ANGLE DOUBLER. - [SDR MWEA010977](https://openairdocs.org/sdr/MWEA010977.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > UPPER FUSELAGE FRAME 870 HAS TWO HOLES THAT DO NOT HAVE (2D) SPACING BETWEEN LONGERON 5 AND 6 RIGHT. -- PLUGGED HOLES, FABRICATED A REPAIR ANGLE, INSTALLED REPAIR ANGLE. - [SDR MWEA010976](https://openairdocs.org/sdr/MWEA010976.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > UPPER FUSELAGE STATION 870 HAS TWO HOLES THAT DO NOT HAVE (2D) SPACING BETWEEN LONGERON 5 AND 6 LEFT. -- PLUGGED HOLES, FABRICATED A REPAIR ANGLE, INSTALLED REPAIR ANGLE. - [SDR MWEA010975](https://openairdocs.org/sdr/MWEA010975.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > UPPER FUSELAGE FRAME 813 HAS THREE HOLES THAT DO NOT HAVE (2D) SPACING BETWEEN LONGERON 5 AND 6 LEFT. -- PLUGGED HOLES IN FRAME, FABRICATED REPAIR PARTS, INSTALLED REPAIR. - [SDR MWEA010974](https://openairdocs.org/sdr/MWEA010974.md): Frame · misdrilled · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > FRAME STATION 503 IN BETWEEN LONGERON 5 AND 6 RIGHT SIDE HAS ONE MISDRILLED HOLE AND THREE OPEN DRILLED HOLES, CHECK EDGE DISTANCE. -- FABRICATED, LOCATED AND DRILLED NEW ANGLE, INSTALLED REPAIR. - [SDR MWEA010973](https://openairdocs.org/sdr/MWEA010973.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > UPPER FUSELAGE FRAME STATION 832 HAS TWO HOLES THAT DO NOT HAVE 2D SPACING BETWEEN LONGERON 5 AND 6 RIGHT. -- PLUGGED HOLES, FABRICATED A REPAIR ANGLE, INSTALLED REPAIR. - [SDR MWEA010972](https://openairdocs.org/sdr/MWEA010972.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > UPPER FUSELAGE FRAME STATION 794 HAS TWO HOLES THAT DO NOT HAVE (2 D) SPACING BETWEEN LONGERON 5 AND 6 LEFT. -- FABRICATED REPAIR DOUBLER AND SHIMS, INSTALLED REPAIR. - [SDR MWEA010971](https://openairdocs.org/sdr/MWEA010971.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > UPPER FUSELAGE FRAME STATION 756 HAS TWO HOLES THAT DO NOT HAVE (2 D) SPACING BETWEEN LONGERON 5 AND 6 RIGHT. -- FABRICATED, LOCATED AND DRILLED REPAIR, INSTALLED REPAIR ANGLE. - [SDR MWEA010970](https://openairdocs.org/sdr/MWEA010970.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > FRAME STATION 598 IN BETWEEN LONGERON 5 AND 6 LEFT SIDE HAS SEVERAL OPEN DRILL HOLES ONE IS IN THE RADIUS. -- PLUGGED HOLES AND FABRICATED REPAIR DOUBLER, INSTALLED ANGLE REPAIR. - [SDR MWEA010969](https://openairdocs.org/sdr/MWEA010969.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > FRAME STATION 598 IN BETWEEN LONGERON 5 AND 6 RIGHT SIDE HAS SEVERAL OPEN DRILL HOLES ONE IS FIGURE EIGHT. -- PLUGGED HOLES, FABRICATED REPAIR DOUBLER, INSTALLED ANGLE REPAIR. - [SDR MWEA010968](https://openairdocs.org/sdr/MWEA010968.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > FRAME STATION 579 IN BETWEEN LONGERON 5 AND 6 RIGHT SIDE HAS SEVERAL OPEN DRILL HOLES. -- FABRICATED REPAIR DOUBLER, INSTALLED REPAIR. - [SDR MWEA010967](https://openairdocs.org/sdr/MWEA010967.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > FRAME STATION 579 IN BETWEEN LONGERON 4 AND 5 RIGHT SIDE TWO OPEN DRILL HOLES CHECK EDGE DISTANCE. -- FABRICATED REPAIR DOUBLER, INSTALLED REPAIR. - [SDR MWEA010966](https://openairdocs.org/sdr/MWEA010966.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > UPPER FUSELAGE FRAME STATION 718 HAS TWO FASTENER HOLES THAT DO NOT HAVE (2 D) SPACING INBOARD OF LONGERON 6 RIGHT. -- PLUGGED HOLES, FABRICATED AND INSTALLED REPAIR ANGLE. - [SDR MWEA010965](https://openairdocs.org/sdr/MWEA010965.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > UPPER FUSELAGE FRAME STATION 718 HAS TWO FASTENER HOLES THAT DO NOT HAVE (2 D) SPACING INBOARD OF LONGERON 5 AND 6 LEFT. -- PLUGGED HOLES, FABRICATED REPAIR ANGLE, INSTALLED REPAIR ANGLE. - [SDR MWEA010962](https://openairdocs.org/sdr/MWEA010962.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > UPPER FUSELAGE FRAME STATION 658 HAS HOLES THAT DO NOT HAVE (2 D) SPACING LONGERON 5 TO 6 RIGHT. -- PLUGGED HOLES, FABRICATED REPAIR ANGLE, INSTALLED REPAIR. - [SDR MWEA010961](https://openairdocs.org/sdr/MWEA010961.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > UPPER FUSELAGE FRAME STATION 658 HAS THREE HOLES THAT DO NOT HAVE (2 D) SPACING BETWEEN LONGERON 5 TO 6 LEFT. -- PLUGGED HOLES, FABRICATED, LOCATED AND DRILLED ANGLE DOUBLER, INSTALLED REPAIR. - [SDR MWEA010960](https://openairdocs.org/sdr/MWEA010960.md): Frame · damaged · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > FUSELAGE FRAME STATION 446 HAS MISDRILLED/OPEN FASTENER HOLES AT LONGERON 6 LEFT. -- FABRICATED REPAIR DOUBLER, PLUGGED HOLES, INSTALLED REPAIR. - [SDR MWEA010959](https://openairdocs.org/sdr/MWEA010959.md): Frame · misdrilled · Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure > FUSELAGE FRAME STATION 427 HAS MISDRILLED/OPEN FASTENER HOLES AT LONGERON 6 LEFT. -- FABRICATED REPAIR DOUBLER, INSTALLED REPAIR. Next page: https://openairdocs.org/deregistered/N301ME-2004-03-25/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 = 'N301ME' AND deregistration_id = 'N301ME-2004-03-25' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N301ME-2004-03-25/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.