# Service difficulty reports: N700ME, cancelled Oct 2, 2012

A list on [N700ME, cancelled Oct 2, 2012](https://openairdocs.org/deregistered/N700ME-2012-10-02.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 · 195 reports

- [SDR COOSDR040041](https://openairdocs.org/sdr/COOSDR040041.md): Fitting · cracked · Sep 24, 2004 · N700ME · Doug DC914 · Fuselage, Landing Gear Attach Fittings
  > FUSELAGE NOSE LANDING GEAR WHEEL WELL RT SIDE AT Y STA 69.55-X 24 INCH -Z16 INCH FITTING (PN 49568801) WITH CRACK. (K)
- [SDR MWEA030442](https://openairdocs.org/sdr/MWEA030442.md): Switch · intermittent · Nov 4, 2003 · N700ME · Doug DC914 · Emergency Equipment
  > INTERIOR TAIL CONE RELEASE HANDLE SWITCH IS INTERMITTENT. REMOVED AND REPLACED SWITCH.
- [SDR MWEA030318](https://openairdocs.org/sdr/MWEA030318.md): Fuel Control · malfunctioned · Aug 18, 2003 · N700ME · Doug DC914 · Fuel Control/Turbine Engines
  > CREW OBSERVED THE N2 SLOWLY DROP TO 40 PERCENT. REMOVED AND REPLACED ROD END AND PERFORMED ENGINE TRIM ALL PARAMETERS NORMAL. ALSO REPLACED FUEL CONTROL.
- [SDR MWEA030286](https://openairdocs.org/sdr/MWEA030286.md): Starter · failed · Jul 8, 2003 · N700ME · Doug DC914 · Engine Cranking
  > LEFT ENGINE WOULD NOT START. REMOVED AND REPLACED LEFT STARTER.
- [SDR MWEA030191](https://openairdocs.org/sdr/MWEA030191.md): Wire · arced · Apr 29, 2003 · N700ME · Doug DC914 · Light System Wiring
  > A BURNING ODOR WAS NOTICED IN THE COCKPIT AND SMOKE WAS OBSERVED COMING OUT OF THE FIRST OFFICERS MAP LIGHT AREA. FOUND GROUND WIRE TO RHEOSTAT BROKEN CAUSING WIRE TO ARC. REMOVED AND REPLACED FIRST OFFICER'S LIGHT ASSEMBLY.
- [SDR MWEA030143](https://openairdocs.org/sdr/MWEA030143.md): Packing · leaking · Mar 21, 2003 · N700ME · Doug DC914 · Fuel Controlling System
  > EPR DROPPED DOWN TO DOWN SLIGHTLY ADVANCED THROTTLE, POWER CAME ON BACK AFTER A FEW MORE MINUTES, POWER STARTER FALLING AGAIN. REMOVED AND REPLACED RIGHT PRESSURE AND DUMP VALVE LINE PACKING.
- [SDR MWEA020668](https://openairdocs.org/sdr/MWEA020668.md): Ring · broken · Oct 31, 2002 · N700ME · Doug DC914 · Landing Gear Retraction/Extension System
  > LANDING GEAR HANDLE WOULD NOT RETRACT. -- FOUND NOSE LANDING GEAR PISTON INNER RING BROKEN AND DAMAGED SEVERAL PARTS. REPLACED #74 RING, #75 SPACER, #77 VALVE, #80 RETAINER AND #82 STOP.
- [SDR MWEA020630](https://openairdocs.org/sdr/MWEA020630.md): Landing Gear · malfunctioned · Oct 24, 2002 · N700ME · Doug DC914 · Landing Gear Retraction/Extension System
  > CREW WAS UNABLE TO RAISE LANDING GEAR. -- FOUND TENSION ON CABLE RUN 116 A & B LOW. PERFORMED STEPS 1-5 OF ADJUSTMENT TEST, SERVICED NOSE STRUT AND REMOVED AND REPLACED LEFT AND RIGHT NOSE TIRE.
- [SDR MWEA020596](https://openairdocs.org/sdr/MWEA020596.md): Floorbeam · corroded · Sep 25, 2002 · N700ME · Doug DC914 · Fuselage Main, Floor Beam
  > RIGHT LAV FLOOR BEAM AT FRAME STATION 817 HAS CORROSION AROUND 3 NUTPLATES APPROXIMATELY 24" RIGHT OF CENTER LINE. -- REMOVED DAMAGED AREA, FABRICATED, LOCATED AND DRILLED REPAIR ANGLE, INSTALLED REPAIR ANGLE,FILLER AND NUTPLATES.
- [SDR MWEA020595](https://openairdocs.org/sdr/MWEA020595.md): Frame · cracked · Sep 25, 2002 · N700ME · Doug DC914 · Fuselage Main, Frame
  > CRACK ON FRAME AROUND FASTENER HOLE AT FRAME STATION 25 RIGHT SIDE OF NOSE WHEEL WELL AREA ABOUT 1" DOWN FROM CEILING. -- REMOVED FASTENERS, FABRICATED AND LOCATED REPAIR DOUBLER AND INSTALLED DOUBLER.
- [SDR MWEA020577](https://openairdocs.org/sdr/MWEA020577.md): Attach Angle · cracked · Sep 20, 2002 · N700ME · Doug DC914 · Fuselage Main, Structure
  > RIGHT SIDE OF VERTICAL TO FUSELAGE ATTACH ANGLE HAS A CRACK AT STATION 951. -- STOP DRILLED CRACK, DRILLED HOLES IN REPAIR ANGLE, INSTALLED REPAIR ANGLE, REMOVED HIGH AND LOW FASTENERS AND INSTALLED OVERSIZED FASTENERS. REINSTALLED HEAD KNOCKER COVER PANEL.
- [SDR MWEA020578](https://openairdocs.org/sdr/MWEA020578.md): Slide · defective · Sep 20, 2002 · N700ME · Doug DC914 · Escape Slide
  > TAILCONE EMERGENCY SLIDE WILL NOT DEPLOY WHEN TAILCONE IS DROPPED USING TAILCONE SLIDE. -- REMOVED TAILCONE PANEL, ADJUSTED FORWARD HOLD DOWN STRAP ON SLIDE COVER AND REINSTALLED TAILCONE.
- [SDR MWEA020541](https://openairdocs.org/sdr/MWEA020541.md): Window Frame · tool damage · Sep 11, 2002 · N700ME · Doug DC914 · Fuselage Main, Plate/Skin
  > WINDOW FRAME RETAINER FOR THE MOST FORWARD RIGHT PLUG WINDOW LOWER FORWARD CORNER HAS TOOL MARKS STATION 218 RIGHT -- BLENDED TOOL MARKS FABRICATED AND INSTALLED ANGLE.
- [SDR MWEA020540](https://openairdocs.org/sdr/MWEA020540.md): Floorboard · corroded · Sep 6, 2002 · N700ME · Doug DC914 · Fuselage Main, Attach Fittings
  > FLOOR BOARD ATTACH FASTENER HOLES AND FORWARD EDGE LIGHTLY CORRODED ON SEAT TRACK #3 BETWEEN STATIONS 200 AND 218. -- REMOVED CORROSION, LOCATED AND DRILLED NEW SEAT TRACK, INSTALLED NUTPLATES.
- [SDR MWEA020538](https://openairdocs.org/sdr/MWEA020538.md): Floorboard · corroded · Sep 5, 2002 · N700ME · Doug DC914 · Fuselage Floor Panel
  > FLOORBOARD ATTACH FASTENERS HOLES ARE LIGHTLY CORRODED ON J-CHANNEL BETWEEN STATIONS 160 AND 200 FORWARD OF SEAT TRACK 4. REMOVED CORROSION AND INSTALLED FLOOR SUPPORT.
- [SDR MWEA020537](https://openairdocs.org/sdr/MWEA020537.md): Elevator · cracked · Sep 5, 2002 · N700ME · Doug DC914 · Elevator Control System
  > LEFT ELEVATOR LOWER FORWARD SPAR FLANGE IS CRACKED APPROXIMATELY 2" AT STATION XE200. -- FABRICATED AND INSTALLED REPAIRED PART.
- [SDR MWEA020290](https://openairdocs.org/sdr/MWEA020290.md): Arm · failed · Apr 25, 2002 · N700ME · Doug DC914 · Passenger/Crew Doors
  > PASSENGER DOOR HAS STRUCTURAL DAMAGE (CRACK) TO INTERCOSTAL LOCATED WHERE CRANK ARM PASSES THROUGH. DAMAGED CAUSED BY CRANK ARM FAILURE. REMOVED AND REPLACED INTERCOSTAL.
- [SDR MWEA020292](https://openairdocs.org/sdr/MWEA020292.md): Beam · elongated · Apr 25, 2002 · N700ME · Doug DC914 · Passenger/Crew Doors
  > REMOVED DAMAGED INTERCOSTAL AND SUPPORT AND FOUND PAX DOOR BEAM #5 TO HAVE AN ELONGATED HOLE. -- FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA020291](https://openairdocs.org/sdr/MWEA020291.md): Support · elongated · Apr 25, 2002 · N700ME · Doug DC914 · Passenger/Crew Doors
  > INTERCOSTAL SUPPORT WAS REMOVED TO FACILITATE OTHER MAINTENANCE AND WAS FOUND TO HAVE ELONGATED HOLES AFTER REMOVAL. -- REPLACED WITH NEW SUPPORT.
- [SDR MWEA020158](https://openairdocs.org/sdr/MWEA020158.md): Stiffener · cracked · Mar 2, 2002 · N700ME · Doug DC914 · Nacelle/Pylon, Attach Fittings
  > LEFT ENGINE PYLON AFT VERITCAL STIFFENER IS CRACKED LOCATED BETWEEN UPPER AND LOWER AFT PYLON SPARS. -- FABRICATED AND INSTALLED STIFFENER.
- [SDR MWEA011057](https://openairdocs.org/sdr/MWEA011057.md): Wire · broken · Jul 17, 2001 · N700ME · Doug DC914 · Trailing Flap Position Indicating System
  > STICK SHAKER CAME ON AFTER ROTATION. -- REPAIRED BROKEN WIRE ON RIGHT FLAP POSITION TRANSMITTER.
- [SDR MWEA011054](https://openairdocs.org/sdr/MWEA011054.md): Skin · cracked · Jul 17, 2001 · N700ME · Doug DC914 · Wing, Attach Fittings
  > NUMEROUS CRACKS ON LEFT WING UPPER AND LOWER INNER SKIN OF #2 LEADING EDGE, BETWEEN STATIONS XFS 202.400 - 299.939. -- REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS.
- [SDR MWEA011053](https://openairdocs.org/sdr/MWEA011053.md): Cap · cracked · Jul 17, 2001 · N700ME · Doug DC914 · Horizontal Stabilizer Structure
  > CRACK INDICATION ON LEFT HORIZONTAL STABILIZER REAR SPAR LOWER CAP, EXTENDING BETWEEN TWO RIVETS, CONFIRMED BY HFEC STATION XHS 146 APPROXIMATELY. -- REMOVED CORROSION, FABRICATED FILLER, DRILLED AND INSTALLED REPAIR ANGLE AND FILLER.
- [SDR MWEA011052](https://openairdocs.org/sdr/MWEA011052.md): Skin · dented · Jul 17, 2001 · N700ME · Doug DC914 · Wing, Plate/Skin
  > LEFT WING LEADING EDGE HAS EIGHT DENTS BETWEEN XRS 214-267. REMOVED DAMAGED AREAS, FABRICATED AND LOCATED EXTERNAL DOUBLER, FABRICATED INTERNAL FILLER AND DOUBLER, LOCATED AND DRILLED INTERNAL FILLERS AND DOUBLER, INSTALLED EXTERNAL DOUBLER.
- [SDR MWEA011048](https://openairdocs.org/sdr/MWEA011048.md): Cap · cracked · Jul 16, 2001 · N700ME · Doug DC914 · Wing Main, Frame Structure
  > 3 1/2" CRACK FOUND ON LEFT UPPER FORWARD SPAR CAP 2 1/2" OUTBOARD OF XCW 58.5 AS VIEWED THROUGH ACCESS PANEL. -- TRIMMED OUT CRACK, TRIMMED AND LOCATED FILLERS, NESTED ANGLE, STIFFNER, INSTALLED FILLER AND ANGLE.
- [SDR MWEA011047](https://openairdocs.org/sdr/MWEA011047.md): Frame · corroded · Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > FORWARD CARGO BAY HAS CORROSION ON FRAME 427 AFT SIDE AND BOTTOM, FROM LONGERON 28 LEFT TO 28 RIGHT. -- REMOVED CORROSION, FLOOR SUPPORTS, DAMAGED SECTION OF FRAME, LOCATED NEW FRAME, INSTALLED FRAME SECTION AND DOUBLERS.
- [SDR MWEA011046](https://openairdocs.org/sdr/MWEA011046.md): Intercostal · damaged · Jul 16, 2001 · N700ME · Doug DC914 · Cargo/Baggage Doors
  > LOWER AFT CARGO DOOR JAMB HINGE INTERCOSTAL HAS AN ELONGATED HOLE. -- FABRICATED 2 EACH BUSHING PLATES, INSTALLED PLATES.
- [SDR MWEA011045](https://openairdocs.org/sdr/MWEA011045.md): Longeron · corroded · Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > FORWARD CARGO BAY HAS CORROSION ON LONGERON 29 RIGHT AT STATION 446 TO 465 AROUND RIVETS. -- REMOVED CORROSION, REMOVED DAMAGED SECTION OF LONGERON, LOCATED NEW LONGERON SECTION, LOCATED AND DRILLED NEW SPLICE, INSTALLED NEW LONGERON SECTION AND SPLICE.
- [SDR MWEA011044](https://openairdocs.org/sdr/MWEA011044.md): Frame · corroded · Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > FORWARD CARGO BAY HAS CORROSION ON FRAME 389 AFT SIDE AT LONGERONS 28 LEFT TO 28 RIGHT. -- BLENDED CORROSION, FABRICATED AND LOCATED DOUBLERS, LOCATED NEW FRAME SECTION, INSTALLED FRAME REPAIR SPLICE.
- [SDR MWEA011043](https://openairdocs.org/sdr/MWEA011043.md): Frame · bent · Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > FORWARD CARGO BAY DOOR JAMB FRAME IS BENT AT STATION 378 LONGERON 29 LEFT TO 29 RIGHT. -- RE-CONTOURED BEND, FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA011042](https://openairdocs.org/sdr/MWEA011042.md): Pan · cracked · Jul 16, 2001 · N700ME · Doug DC914 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR FORWARD UPPER CORNERS ON THE INNER PAN IS CRACKED AROUND A SEAL FASTENER HOLE. -- LOCATED, DRILLED AND INSTALLED NEW PAN.
- [SDR MWEA011041](https://openairdocs.org/sdr/MWEA011041.md): Longeron · cracked · Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > LONGERON 2 LEFT IS CRACKED WHERE IT ATTACHES TO FRAME AT STATION 897. -- REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, LOCATED, DRILLED NEW SECTION OF LONGERON, INSTALLED REPAIR PARTS.
- [SDR MWEA011040](https://openairdocs.org/sdr/MWEA011040.md): Longeron · cracked · Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > LONGERON 2 RIGHT IS CRACKED WHERE IT ATTACHES TO FRAME AT STATION 897. -- REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, LOCATED AND DRILLED NEW SECTION OF LONGERON, INSTALLED REPAIR PARTS.
- [SDR MWEA011039](https://openairdocs.org/sdr/MWEA011039.md): Angle · cracked · Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > STATION 897 AT LONGERON 2 RIGHT SUPPORT ANGLE IS CRACKED. -- REMOVED, FABRICATED AND INSTALLED SUPPORT ANGLE.
- [SDR MWEA011038](https://openairdocs.org/sdr/MWEA011038.md): Angle · cracked · Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > STATION 897 CRACKED AT LONGERON 2 LEFT, ALSO SUPPORT ANGLE AT THAT STATION IS CRACKED. -- FABRICATED GUSSET, LOCATED SUPPORT ANGLE, INSTALLED SUPPORT ANGLE.
- [SDR MWEA011037](https://openairdocs.org/sdr/MWEA011037.md): Longeron · damaged · Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > TWO MISDRILLED HOLES IN LONGERON 17 RIGHT AT STATION 897. -- FABRICATED AND LOCATED NEW LONGERON SECTION AND SPLICE, INSTALLED NEW LONGERON AND SPLICE.
- [SDR MWEA011036](https://openairdocs.org/sdr/MWEA011036.md): Longeron · cracked · Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > STATION 897 AT LONGERON 2 RIGHT IS CRACKED. -- REMOVED DAMAGE, TRIMMED AND LOCATED SPLICES AND FRAME, INSTALLED REPAIR PARTS.
- [SDR MWEA011035](https://openairdocs.org/sdr/MWEA011035.md): Seat Track · worn · Jul 12, 2001 · N700ME · Doug DC914 · Fuselage, Seat/Cargo Attach Fittings
  > CAPTAINS AFT OUTBOARD SEAT TRACK IS WORN AROUND LOCK PIN HOLES. -- REMOVED DAMAGE FROM SEAT TRACK UPPER CAP SURFACE, FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA011034](https://openairdocs.org/sdr/MWEA011034.md): Web · dented · Jul 12, 2001 · N700ME · Doug DC914 · Cargo/Baggage Doors
  > FORWARD CARGO BAY DOOR JAMB WEB HAS A SHARP DENT AT STATION 351 LONGERON 29 RIGHT. -- REMOVED DOOR JAMB WEB, LOCATED, DRILLED AND INSTALLED NEW WEB.
- [SDR MWEA011033](https://openairdocs.org/sdr/MWEA011033.md): Seat Track · worn · Jul 12, 2001 · N700ME · Doug DC914 · Fuselage, Seat/Cargo Attach Fittings
  > FIRST OFFICERS OUTBOARD SEAT TRACK IS WORN AROUND LOCK PIN HOLES. -- FABRICATED, LOCATED, DRILLED AND INSTALLED NEW SEAT TRACK.
- [SDR MWEA011032](https://openairdocs.org/sdr/MWEA011032.md): Seat Track · worn · Jul 12, 2001 · N700ME · Doug DC914 · Fuselage, Seat/Cargo Attach Fittings
  > CAPTAINS AFT INBOARD SEAT TRACK IS WORN AROUND LOCK PIN HOLES. -- REMOVED DAMAGED FROM SEAT TRACK, FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA011031](https://openairdocs.org/sdr/MWEA011031.md): Seat Track · worn · Jul 12, 2001 · N700ME · Doug DC914 · Fuselage, Seat/Cargo Attach Fittings
  > FIRST OFFICERS AFT INBOARD SEAT TRACK IS WORN AROUND LOCK PIN HOLES. -- REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA011030](https://openairdocs.org/sdr/MWEA011030.md): Former · tool damage · Jul 12, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > TOOLING MARKS ON FORMER AFT SIDE BETWEEN LONGERON 28 RIGHT AND 27 RIGHT STATION 120. -- BLENDED TOOLING MARKS, REMOVED DAMAGED FORMER, FORMED NEW FORMER, LOCATED FASTENER HOLES, FABRICATED 2 REPAIR SPLICES, INSTALLED FORMER SECTION.
- [SDR MWEA011029](https://openairdocs.org/sdr/MWEA011029.md): Frame · corroded · Jul 12, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > AFT CARGO STATION 786 FRAME HAS LIGHT CORROSION ON AFT SIDE AND UNDER BOTTOM LIP BETWEEN LONGERONS 28 LEFT AND 29 RIGHT. -- REMOVED DAMAGED SECTION OF FRAME, LOCATED AND DRILLED NEW SECTION, FABRICATED NEW INTERCOSTAL SPLICE, INSTALLED FRAME SPLICE DOUBLER A
- [SDR MWEA011028](https://openairdocs.org/sdr/MWEA011028.md): Longeron · cracked · Jul 10, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > LEFT SIDE LONGERON 17 IS CRACKED AT STATION 801. -- REMOVED DAMAGED SECTION, DRILLED AND INSTALLED NEW SECTION OF LONGERON AND SPLICE.
- [SDR MWEA011027](https://openairdocs.org/sdr/MWEA011027.md): Clip · cracked · Jul 10, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > LEFT SIDE SHEAR CLIP ON LONGERON 17 AT STATION 786 IS CRACKED AT THE FASTENER HOLE. -- REMOVED SHEAR CLIP, FABRICATED AND INSTALLED SHEAR CLIP.
- [SDR MWEA011026](https://openairdocs.org/sdr/MWEA011026.md): Longeron · corroded · Jul 10, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > AFT CARGO LONGERON 26 LEFT HAS LIGHT CORROSION ALONG TOP VERTICAL LEG BETWEEN STATION 750-786. -- REMOVED LONGERON SECTION, LOCATED AND INSTALLED NEW LONGERON.
- [SDR MWEA011025](https://openairdocs.org/sdr/MWEA011025.md): Longeron · damaged · Jul 10, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > DUE TO SKIN REPAIR AT STATION 740 RIGHT SIDE AT LONGERON 17 RIGHT, FORMER BETWEEN LONGERON 16 RIGHT AND 17 RIGHT HAS TO BE CUT BETWEEN LONGERON 15 AND 16 RIGHT AND RE-MADE, THEN SPLICED INTO FORMER BETWEEN LONGERON 15 AND 16 RIGHT. -- REMOVED LONGERON ON FOR
- [SDR MWEA011024](https://openairdocs.org/sdr/MWEA011024.md): Splice · damaged · Jul 10, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > LONGERON 29 LEFT SPLICE HAS SEVERAL DRILL STARTS AT STATION 360. -- REMOVED SPLICE, LOCATED, DRILLED AND INSTALLED NEW LONGERON SPLICE.
- [SDR MWEA011023](https://openairdocs.org/sdr/MWEA011023.md): Longeron · damaged · Jul 10, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
  > IMPACT DAMAGE IN THE AFT ACCESSORY TO LONGERON 23 RIGHT AT STATION 897 AND DAMAGE TO THE FRAME AT SAME LOCATION. -- REMOVED DAMAGED SECTION OF FRAME, FABRICATED LONGERON SPLICE, INSTALLED LONGERON, FABRICATED NEW FRAME SECTION AND SHEAR CLIP, INSTALLED FRAME

Next page: https://openairdocs.org/deregistered/N700ME-2012-10-02/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 = 'N700ME' AND deregistration_id = 'N700ME-2012-10-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N700ME-2012-10-02/reports

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