# Service difficulty reports: N500ME, cancelled May 25, 2004 A list on [N500ME, cancelled May 25, 2004](https://openairdocs.org/deregistered/N500ME-2004-05-25.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 · 219 reports - [SDR MWEA030134](https://openairdocs.org/sdr/MWEA030134.md): Control Valve · inoperative · Mar 9, 2003 · N500ME · Doug DC914 · Master Cylinder/Brake Valve > LEFT BRAKE DOES NOT WORK WITH RIGHT HYDRAULIC SYSTEM SELECTED. REMOVED AND REPLACED RIGHT WHEEL WELL BRAKE CONTROL VALVE. - [SDR MWEA020687](https://openairdocs.org/sdr/MWEA020687.md): Gear · defective · Nov 8, 2002 · N500ME · Doug DC914 · Landing Gear Doors > CREW REPORTED GEAR DOOR OPEN LIGHT STAYED ON WITH GEAR HANDLE UP. -- REMOVED AND REPLACED STIFFENER. - [SDR MWEA020447](https://openairdocs.org/sdr/MWEA020447.md): Oil System · Jul 13, 2002 · N500ME · Doug DC914 · Engine Oil Quantity > ON DEPARTURE OUT OF MILWUAKEE RIGHT ENGINE OIL QTY INDICATION DECREASED TO ZERO. -- DEFERRED RIGHT ENGINE OIL QTY PER MEL 79-3 - [SDR MWEA020321](https://openairdocs.org/sdr/MWEA020321.md): Oven · shorted · May 5, 2002 · N500ME · Doug DC914 · Equipment/Furnishings Wiring > F/A REPORTED SEEING AN ORANGE FLASH ABOVE AND BEHIND GALLEY OVEN. -- NWA MTC INSPECTED LEFT AND RIGHT OVENS. FOUND OVEN GROUND WIRE SHORTED. PULLED AND COLLARD LEFT AND RIGHT OVEN CIRCUIT BREAKERS. DEFERRED OVENS PER MEL 25-12. REMOVED AND REPLACED OVENS DMI - [SDR MWEA020207](https://openairdocs.org/sdr/MWEA020207.md): Stiffener · elongated · Apr 2, 2002 · N500ME · Doug DC914 · Fuselage Main, Structure > VERTICAL STIFFENER IN FORWARD ELECTONIC POWER CENTER HAS ELONGATED HOLES. -- REPAIRED VERTICAL STIFFENER IAW SRM 53-01 FIGURE SHEET 4. - [SDR MWEA020045](https://openairdocs.org/sdr/MWEA020045.md): Spar · cracked · Jan 8, 2002 · N500ME · Doug DC914 · Elevator Control System > RIGHT HAND ELEVATOR FORWARD SPAR HAS A CRACK INDICATION VIEWED ON RADIOGRAPH "RG" AT APPROXIMATELY STATION XE 105 UPPER CAP LOWER SURFACE -- FABRICATED AND HEAT TREAT PARTS. INSTALLED REPAIR SPAR. REBALANCED RIGHT HAND ELEVATOR. - [SDR MWEA020044](https://openairdocs.org/sdr/MWEA020044.md): Spar · cracked · Jan 8, 2002 · N500ME · Doug DC914 · Elevator Control System > LEFT HAND ELEVATOR FORWARD SPAR HAS A CRACK INDICATION VIEWED ON RADIOGRAPH "LM" AT APPROXIMATELY STATION XE 203 -- LOCATED ENDS OF CRACK. FABRICATED AND INSTALLED REPAIR SPAR. REBALANCED LEFT HAND ELEVATOR. - [SDR MWEA020043](https://openairdocs.org/sdr/MWEA020043.md): Spar · cracked · Jan 8, 2002 · N500ME · Doug DC914 · Elevator Control System > LEFT HAND ELEVATOR FORWARD SPAR HAS CRACK INDICATION VIEWED ON RADIOGRAPH "LK" AT APPROXIMATELY STATION XE 169 -- LOCATED AND MARKED ENDS OF CRACK. INSTALLED REPAIR SPAR. REBALANCED LEFT HAND ELEVATOR. - [SDR MWEA011085](https://openairdocs.org/sdr/MWEA011085.md): Computer · malfunctioned · Jul 28, 2001 · N500ME · Doug DC914 · Doppler System > WINDSHEAR LIGHT CAME ON WITH AUTO WARNING. FIRST MAINTENANCE DEFERRED, THEN COLLARD CIRCUIT BREAKER, AND REPLACED THE WINDSHEAR COMPUTER. - [SDR MWEA010946](https://openairdocs.org/sdr/MWEA010946.md): Charger · defective · Jun 13, 2001 · N500ME · Doug DC914 · DC Generating System > ON CLIMB OUT THROUGH FL 200 BATTERY CHARGER C.B. POPPED. -- REMOVED AND REPLACED BATTERY CHARGER. REMOVED AND REPLACED LEFT AND RIGHT SHIP BATTERIES. - [SDR MWEA010829](https://openairdocs.org/sdr/MWEA010829.md): Vane · dented · May 29, 2001 · N500ME · Doug DC914 · Trailing Edge Flaps > DENT FOUND IN LEFT FLAP MOVEABLE VANE, DENT MEASURES.080 DEEP. REPAIRED IN ACCORDANCE WITH 51-70-2. - [SDR MWEA010807](https://openairdocs.org/sdr/MWEA010807.md): Panel · cracked · May 21, 2001 · N500ME · Doug DC914 · Wing, Plate/Skin > RIGHT WING D-DUCT LOCATED AT XRS 320 HAS A CRACK. INSTALLED DOUBLER IN ACCORDANCE WITH 57-06 FIG. 01. - [SDR MWEA010806](https://openairdocs.org/sdr/MWEA010806.md): Panel · dented · May 21, 2001 · N500ME · Doug DC914 · Wing, Plate/Skin > FOUR DENTS FOUND ON TOP LEFT WING INBOARD TRAILING EDGE PANEL FORWARD OF AILERON. REMOVED DAMAGE AND INSTALLED REPAIR IN ACCORDANCE WITH 51-70. - [SDR MWEA010804](https://openairdocs.org/sdr/MWEA010804.md): Panel · dented · May 21, 2001 · N500ME · Doug DC914 · Wing, Plate/Skin > DENT ON TOP SIDE OF LEFT WING TRAILING EDGE PANEL LOCATED ABOVE OUTBOARD AILERON. REMOVED DAMAGE AND INSTALLED REPAIR IN ACCORDANCE WITH 51-70. - [SDR MWEA010803](https://openairdocs.org/sdr/MWEA010803.md): Panel · delaminated · May 21, 2001 · N500ME · Doug DC914 · Wing, Plate/Skin > REPAIR XRS 437 IS DELAMINATED ON LEFT WING TRAILING EDGE PANEL. REMOVED DAMAGE AND INSTALLED REPAIR IN ACCORDANCE WITH 51-70. - [SDR MWEA010799](https://openairdocs.org/sdr/MWEA010799.md): Skin · dented · May 21, 2001 · N500ME · Doug DC914 · Wing, Plate/Skin > DENT LOCATED ON RIGHT WING LEADING EDGE AT STATION 477. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER. - [SDR MWEA010805](https://openairdocs.org/sdr/MWEA010805.md): Panel · dented · May 21, 2001 · N500ME · Doug DC914 · Wing, Plate/Skin > DENT FOUND IN LEFT WING TRAILING EDGE PANEL LOCATED 10 INCHES OUTBOARD OF AILERON AND 10 INCHES FORWARD OF TRAILING EDGE. REPAIRED DAMAGE IN ACCORDANCE WITH 57-01. - [SDR MWEA010812](https://openairdocs.org/sdr/MWEA010812.md): Vane · dented · May 21, 2001 · N500ME · Doug DC914 · Trailing Edge Flaps > RIGHT WING FLAP MOVEABLE VANE HAS A 1.5 INCH BY.875 INCH,.063 INCH DENT 15 INCHES FROM INBOARD EDGE. REMOVED DAMAGE AND INSTALLED REPAIR IN ACCORDANCE WITH 51-70-2. - [SDR MWEA010808](https://openairdocs.org/sdr/MWEA010808.md): Skin · dented · May 21, 2001 · N500ME · Doug DC914 · Elevator, Plate/Skin > UPPER RIGHT ELEVATOR SKIN HAS FIVE DENTS BETWEEN STATION XHS 100 AND XHS 119. INSTALLED DOUBLER IN ACCORDANCE WITH 55-03. - [SDR MWEA010809](https://openairdocs.org/sdr/MWEA010809.md): Rib · damaged · May 21, 2001 · N500ME · Doug DC914 · Elevator, Spar/Rib > RIGHT ELEVATOR XHS 116 RIB HAS DAMAGE AT THE FORWARD OUTBOARD EDGE. REPAIRED DAMAGE IN ACCORDANCE WITH 51-30. - [SDR MWEA010815](https://openairdocs.org/sdr/MWEA010815.md): Panel · dented · May 21, 2001 · N500ME · Doug DC914 · Wing, Plate/Skin > RIGHT WING TRAILING EDGE PANEL HAS A 3 INCH BY 1.375 INCH DENT,.060 INCH DEEP LOCATED AT XRS 487. REMOVED DAMAGE AND INSTALLED REPAIR IN ACCORDANCE WITH 57-04. - [SDR MWEA010814](https://openairdocs.org/sdr/MWEA010814.md): Panel · dented · May 21, 2001 · N500ME · Doug DC914 · Wing, Plate/Skin > RIGHT WING TRAILING EDGE PANEL HAS A 1.5 INCH BY 1.625 INCH DENT,.075 INCH DEEP LOCATED AT XRS 443. REMOVED DAMAGE AND INSTALLED REPAIR IN ACCORDANCE WITH 57-04. - [SDR MWEA010813](https://openairdocs.org/sdr/MWEA010813.md): Panel · dented · May 21, 2001 · N500ME · Doug DC914 · Wing, Plate/Skin > RIGHT WING TRAILING EDGE PANEL HAS A 1.25 INCH BY 1.5 INCH DENT,.063 DEEP LOCATED AT XRS 397. REMOVED DAMAGE AND INSTALLED REPAIR IN ACCORDANCE WITH 57-04. - [SDR MWEA010802](https://openairdocs.org/sdr/MWEA010802.md): Panel · dented · May 21, 2001 · N500ME · Doug DC914 · Wing, Plate/Skin > RIGHT WING TRAILING EDGE PANEL HAS 1 INCH BY 1 INCH DENT,.064 INCH DEEP LOCATED AT XRS 354. REMOVED DAMAGE AND INSTALLED REPAIR IN ACCORDANCE WITH 57-04. - [SDR MWEA010801](https://openairdocs.org/sdr/MWEA010801.md): Panel · dented · May 21, 2001 · N500ME · Doug DC914 · Wing, Plate/Skin > RIGHT WING TRAILING EDGE PANEL HAS A 2.25 INCH BY 2.125 INCH DENT,.099 INCH DEEP LOCATED AT XRS 467. REMOVED DAMAGE AND INSTALLED REPAIR IN ACCORDANCE WITH 57-04. - [SDR MWEA010800](https://openairdocs.org/sdr/MWEA010800.md): Panel · dented · May 21, 2001 · N500ME · Doug DC914 · Wing, Plate/Skin > RIGHT WING TRAILING EDGE PANEL HAS A 1.625 BY 1.0625 INCH DENT, 060 DEEP LOCATED AT XRS 474. REMOVED DAMAGE AND INSTALLED REPAIR IN ACCORDANCE WITH 57-04. - [SDR MWEA010811](https://openairdocs.org/sdr/MWEA010811.md): Skin · dented · May 21, 2001 · N500ME · Doug DC914 · Wing, Plate/Skin > RIGHT WING WALK AREA HAS A DENT.075 DEEP AND FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, REMOVED DAMAGED CORNER AND MADE NEW REPAIR PARTS. - [SDR MWEA010810](https://openairdocs.org/sdr/MWEA010810.md): Skin · cracked · May 21, 2001 · N500ME · Doug DC914 · Wing, Plate/Skin > RIGHT WING LEADING EDGE HAS ONE DENT AT APPROXIMATELY XRS 353 WITH CRACK INDICATIONS. REMOVED DAMAGE AND INSTALLED DOUBLER. - [SDR MWEA010452](https://openairdocs.org/sdr/MWEA010452.md): Duct · separated · Mar 28, 2001 · N500ME · Doug DC914 · Pneumatic Distribution System > RECEIVED RIGHT ENGINE FIRE WARNING, THEN WHEN SILENCE BELL BUTTON WAS PUSHED FIRE WARNING WENT AWAY. LOOP A TESTED NORMAL. LOOP B ALREADY DEFERRED. FOUND 13TH STAGE BLEED AIR DUCT TO FUEL HEAT VALVE MOUNTING FLANGE SEPERATED AT JOINT. REMOVED AND REPLACED AI - [SDR MWEA010298](https://openairdocs.org/sdr/MWEA010298.md): Intercostal · damaged · Mar 5, 2001 · N500ME · Doug DC914 · Fuselage Miscellaneous Structure > INTERCOSTAL AT STATION 305 HAS DAMAGED UPPER HORIZONTAL LEG. INSTALLED DOUBLERS. - [SDR MWEA010297](https://openairdocs.org/sdr/MWEA010297.md): Web · misdrilled · Mar 5, 2001 · N500ME · Doug DC914 · Fuselage Miscellaneous Structure > WEB AT STATION 305 HAS MISDRILLED HOLES. INSTALLED DOUBLER. - [SDR MWEA010296](https://openairdocs.org/sdr/MWEA010296.md): Former · misdrilled · Mar 5, 2001 · N500ME · Doug DC914 · Fuselage Main, Frame > FORMER AT STATION 305 HAS MISDRILLED HOLES. INSTALLED DOUBLERS. - [SDR MWEA010114](https://openairdocs.org/sdr/MWEA010114.md): Slide · will not test · Jan 23, 2001 · N500ME · Doug DC914 · Escape Slide > THE TAIL CONE SLIDE DEPLOYMENT CHECK FAILED WHEN TAIL CONE WAS RELEASED, THE EVACUATION SLIDE COVER DID NOT RELEASE. BLENDED CRACKED/TORN METAL FOUND AROUND GIRT BAR MOUNT HOLES AND FABRICATED AND INSTALLED REPAIR CATWALK DOUBLERS AND SHIMS. FABRICATED AND I - [SDR MWEA010113](https://openairdocs.org/sdr/MWEA010113.md): Frame · cracked · Jan 23, 2001 · N500ME · Doug DC914 · Fuselage Main, Frame > LEFT MAIN LANDING GEAR MAIN FRAME FORWARD OUTBOARD RADIUS CRACK NOW EXCEEDS 7 INCHES. LOCATED, DRILLED, AND INSTALLED REPAIR ANGLE DOUBLERS. - [SDR MWEA010112](https://openairdocs.org/sdr/MWEA010112.md): Fastener · missing · Jan 23, 2001 · N500ME · Doug DC914 · Fuselage Main, Floor Beam > CABIN FLOORBEAM UPPER ANGLE, STATION 160, AFT SIDE, HAS SIX UNFILLED FASTENER HOLES. FABRICATED AND INSTALLED SPLICE ANGLES. - [SDR MWEA010111](https://openairdocs.org/sdr/MWEA010111.md): Pan · gouged · Jan 23, 2001 · N500ME · Doug DC914 · Fuselage Miscellaneous Structure > OVERWING EXIT FRAME HAS SEVERAL DEEP GOUGES ON FORWARD AND AFT LOWER CORNERS. REMOVED AND REPLACED JAMB PAN. - [SDR MWEA010110](https://openairdocs.org/sdr/MWEA010110.md): Floorbeam · chafed · Jan 23, 2001 · N500ME · Doug DC914 · Fuselage Main, Floor Beam > CENTER FLOOR SUPPORT IS CHAFING INTO FLOORBEAM AT STATION 484. FABRICATED AND INSTALLED FILLERS AND REPAIR ANGLES. - [SDR MWEA010109](https://openairdocs.org/sdr/MWEA010109.md): Pan · misinstalled · Jan 23, 2001 · N500ME · Doug DC914 · Fuselage Miscellaneous Structure > GALLEY SERVICE DOOR JAMB REPAIR IMPROPERLY INSTALLED, STATION 200, NEXT TO BAYONET ROLLERS. FABRICATED AND INSTALLED DOUBLER REPAIR. - [SDR MWEA010108](https://openairdocs.org/sdr/MWEA010108.md): Door Frame · misrepaired · Jan 23, 2001 · N500ME · Doug DC914 · Fuselage Main, Structure > APB PLUG DOOR PAN REPAIR INTERFERES WITH DOOR OPERATION AND SEAL. REMOVED AND REPLACED DOOR FRAME. - [SDR MWEA010089](https://openairdocs.org/sdr/MWEA010089.md): Frame · cracked · Jan 18, 2001 · N500ME · Doug DC914 · Fuselage, Landing Gear Attach Fittings > LEFT HAND MLG MAINFRAME AFT INBOARD RADIUS CRACKED. FABRICATED AND INSTALLED ANGLE AND PLATE DOUBLERS. - [SDR MWEA010088](https://openairdocs.org/sdr/MWEA010088.md): Frame · cracked · Jan 18, 2001 · N500ME · Doug DC914 · Fuselage, Landing Gear Attach Fittings > LEFT HAND MAIN LANDING GEAR MAIN FRAME FORWARD INBOARD RADIUS CRACKED. FABRICATED AND INSTALLED ANGLE AND PLATE DOUBLERS. - [SDR MWEA010087](https://openairdocs.org/sdr/MWEA010087.md): Intercostal · cracked · Jan 18, 2001 · N500ME · Doug DC914 · Fuselage Miscellaneous Structure > INTERCOSTAL BETWEEN STATION 585 - 604 AT NR 4 SEAT TRACK IS CRACKED AT LIGHTENING HOLE. FABRICATED AND INSTALLED REPAIR DOUBLER. - [SDR MWEA010086](https://openairdocs.org/sdr/MWEA010086.md): Floorboard · corroded · Jan 18, 2001 · N500ME · Doug DC914 · Fuselage Floor Panel > SKIN CORROSION SEVERAL PLACES OUT OF LIMITS AND 4 HAT CHANNELS HAVE CORROSION OUT OF LIMITS ON FLOORBOARD E-1. FABRICATED AND INSTALLED FLOORBOARD SKIN AND 4 HAT CHANNELS. - [SDR MWEA010085](https://openairdocs.org/sdr/MWEA010085.md): Cargo Track · corroded · Jan 18, 2001 · N500ME · Doug DC914 · Fuselage, Seat/Cargo Attach Fittings > LUGGAGE TRACK STATION 738 - 817 HAS CORROSION. FABRICATED AND INSTALLED NEW LUGGAGE TRACK. - [SDR MWEA010084](https://openairdocs.org/sdr/MWEA010084.md): Floorboard · cracked · Jan 18, 2001 · N500ME · Doug DC914 · Fuselage Floor Panel > FLOORBOARD BETWEEN SEAT TRACKS UNDER F/O SEAT IS CRACKED IN SEVERAL LOCATIONS OF THE SKIN. FABRICATED NEW FLOORBOARD SKIN. - [SDR MWEA010083](https://openairdocs.org/sdr/MWEA010083.md): Web · damaged · Jan 18, 2001 · N500ME · Doug DC914 · Fuselage Miscellaneous Structure > SUBFLOOR/CUSP REMOVED FROM STATION 160 - 200. FABRICATED AND INSTALLED REPLACEMENT SUBFLOOR. - [SDR MWEA010082](https://openairdocs.org/sdr/MWEA010082.md): Floorbeam · misdrilled · Jan 18, 2001 · N500ME · Doug DC914 · Fuselage Main, Floor Beam > TWO HOLES WITH IMPROPER SPACING ON UPPER TEE OF STATION 200. FABRICATED AND INSTALLED T-ANGLE AND OUTBOARD LEFT HAND SPLICES. - [SDR MWEA010081](https://openairdocs.org/sdr/MWEA010081.md): Frame · gouged · Jan 18, 2001 · N500ME · Doug DC914 · Fuselage Main, Frame > FRAME GOUGED AT STATION 389 LONGERON 29 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE, PLATE, AND FILLER. - [SDR MWEA010080](https://openairdocs.org/sdr/MWEA010080.md): Floorbeam · gouged · Jan 18, 2001 · N500ME · Doug DC914 · Fuselage Main, Floor Beam > GOUGE IN FLOOR WEB AT STATION 159. FABRICATED AND INSTALLED REPAIR DOUBLER. - [SDR MWEA010079](https://openairdocs.org/sdr/MWEA010079.md): Bulkhead · damaged · Jan 18, 2001 · N500ME · Doug DC914 · Nacelle/Pylon, Bulkhead/Firewall > RIGHT HAND PYLON BULKHEAD LOWER WEB AT STATION 786 HAS SEVERAL ELONGATED HOLES. FABRICATED AND INSTALLED NEW WEB. Next page: https://openairdocs.org/deregistered/N500ME-2004-05-25/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 = 'N500ME' AND deregistration_id = 'N500ME-2004-05-25' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N500ME-2004-05-25/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.