# Service difficulty reports: N401EA, cancelled Dec 6, 2018

A list on [N401EA, cancelled Dec 6, 2018](https://openairdocs.org/deregistered/N401EA-2018-12-06.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 2 · 71 reports

- [SDR DALA12012650885](https://openairdocs.org/sdr/DALA12012650885.md): Floor Panel · damaged · Nov 10, 2012 · N401EA · Doug DC951 · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL DAMAGED. REMOVED FLOOR PANEL REF AMM 25-52. INSTALLED REPLACEMENT FLOOR PANEL IAW AMM 25-52.
- [SDR DALA12012630885](https://openairdocs.org/sdr/DALA12012630885.md): Power Supply · inoperative · Nov 10, 2012 · N401EA · Doug DC951 · Emergency Lighting
  > EMERGENCY PATH LIGHTS FROM SEAT ROW 9-13 INOPERATIVE. R & R POWER SUPPLY IAW AMM 33-53. CHECKED GOOD.
- [SDR DALA12012640885](https://openairdocs.org/sdr/DALA12012640885.md): Floor Panel · damaged · Oct 25, 2012 · N401EA · Doug DC951 · Fuselage Floor Panel
  > FOUND DAMAGE IN FORWARD CARGO FLOOR PANEL IN FRONT OF DOOR AFT SIDE. REMOVED FLOOR PANEL REF AMM 25-52. INSTALLED REPLACEMENT FLOOR PANEL IAW AMM 25-52.
- [SDR DALA12003570885](https://openairdocs.org/sdr/DALA12003570885.md): Slide · low pressure · Jul 15, 2012 · N401EA · Doug DC951 · Escape Slide
  > DURING LINE CHECK, MAINTENANCE FOUND THE 1R DOOR SLIDE TO BE WITHOUT PRESSURE. MAINTENANCE REPLACED THE 1R DOOR SLIDE AND RETURNED THE AIRCRAFT TO SERVICE.
- [SDR DALA12002850885](https://openairdocs.org/sdr/DALA12002850885.md): Slide · low pressure · Jul 4, 2012 · N401EA · Doug DC951 · Escape Slide
  > DURING LINE CHECK, MAINTENANCE FOUND THE TAILCONE SLIDE PRESSURE TO BE ZERO. MAINTENANCE REPLACED THE TAILCONE SLIDE ASSEMBLY AND RETURNED THE AIRCRAFT TO SERVICE.
- [SDR DALA1240009885](https://openairdocs.org/sdr/DALA1240009885.md): Battery Pack · inoperative · Jul 1, 2012 · N401EA · Doug DC951 · Emergency Lighting
  > DURING EMERGENCY LIGHT CHECK, G1 DOOR EMERGENCY EXIT AND F/C SEAT PATH LIGHTS WERE INOPERATIVE. REPLACED BATTERIES AND TESTS OK.
- [SDR DALA1223479885](https://openairdocs.org/sdr/DALA1223479885.md): Light · inoperative · Apr 14, 2012 · N401EA · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROW 12 OF THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND FUNCTIONALLY CHECKED IT.
- [SDR DALA1201979885](https://openairdocs.org/sdr/DALA1201979885.md): Skin · cracked · Jan 16, 2012 · N401EA · Doug DC951 · Fuselage Main, Plate/Skin
  > CRACK IN SKIN AT CANTED FRAME, STATION 1292, JUST BELOW STRINGER L14. CRACK APPROXIMATELY 2 INCHES LONG, WITH SMALLER CRACK AT STATION 1294, STRINGER L14 APPROXIMATELY 1/4 INCH LONG. CUT OUT DAMAGED SKIN, FABRICATED FILLER AND EXTERNAL DOUBLER, INSTALLED AND
- [SDR DALA1153979885](https://openairdocs.org/sdr/DALA1153979885.md): Power Supply · inoperative · Sep 13, 2011 · N401EA · Doug DC951 · Emergency Lighting
  > MAINTENANCE FOUND THE CATWALK EMERGENCY LIGHTS IN TAIL CONE INOPERATIVE. MAINTENANCE FOUND AFT LEFT POWER SUPPLY BAD AND REPLACED IT. OPERATIONAL CHECK WAS GOOD. AIRCRAFT OK FOR SERVICE.
- [SDR DALA1151739885](https://openairdocs.org/sdr/DALA1151739885.md): Skin · dented · Sep 6, 2011 · N401EA · Doug DC951 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN BETWEEN STA 110 - STA 115 AND ABOVE CUSP LINE, THE DENT WAS FOUND OUT OF LIMITS PER DC-9 SRM. ER/A 495311-14 SECTION I-ACCOMPLISHED DURING LCK AT SAT, SEP11. ER/A SECTION II- TO BE ACCOMPLISHED AT EVERY 3000FC AFTER SECT I ER/A SECTION
- [SDR DALA1151699885](https://openairdocs.org/sdr/DALA1151699885.md): Sill · cracked · Sep 6, 2011 · N401EA · Doug DC951 · Fuselage Miscellaneous Structure
  > LT NR 1 MAIN ENTRY DOOR UPPER SILL WEB CRACK. BS 460. S-17L. L=0.8" PER B747-400 SRM 53-10-15 R1 PERFORMED THE REPAIR. REPEAT DVI OF THE MAIN ENTRY DOOR 1 UPPER MAIN SILL OUTER CHORD, WEB, AND FRAME ATTACH ANGLES FOR CRACK(S) PER PART 2. (WHICHEVER OCCURS LAS
- [SDR DALA1151629885](https://openairdocs.org/sdr/DALA1151629885.md): Doubler · gouged · Sep 5, 2011 · N401EA · Doug DC951 · Spoilers
  > LT WING I/B SPOILER LOWER DOUBLER REPAIR IS GOUGED. REMOVED AND REPLACED LT I/B SPOILER CLEARENCES /OP'S CHECKED GOOD IAW AMM DC-9-A-27-61-01-401-926A-A PG 1-9. COMPLETED, RII INSPECTION COMPLETED. SPOILER, FLIGHT OFF 09-2760-9-0021 00854 ON 09-2760-9-0021
- [SDR DALA1151669885](https://openairdocs.org/sdr/DALA1151669885.md): Skin · dented · Aug 30, 2011 · N401EA · Doug DC951 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN AT STA 222, 3" BELOW CUSP LINE L18L. COMPLIED WITH ER/A 495312-14 REV ORIG SECTION 1 ACCOMPLISH CLOSE VISUAL INSP OF REPAIR AREA FOR LOOSE MISSING FASTENERS, REF SECTION 2 ER/A 495312-14 REV ORIGINAL ACCOMPLISH SECTION 2 PRIOR TO 3000 FL
- [SDR DALA1149959885](https://openairdocs.org/sdr/DALA1149959885.md): Skin · cracked · Aug 25, 2011 · N401EA · Doug DC951 · Passenger/Crew Doors
  > L1 DOOR EXTERIOR SURFACE HAS A CRACK (APPX 2 1/2"). MAINTENANCE REMOVED AND REPLACED L1 DOOR IAW DC9 AMM 52-11-00, PG 401 AND T/C 0500-0534M.
- [SDR DALA1137489885](https://openairdocs.org/sdr/DALA1137489885.md): Battery Pack · discharged · Jun 1, 2011 · N401EA · Doug DC951 · Emergency Lighting
  > ON OVERNIGHT CHECK, MAINTENANCE FOUND THE LAST 4 EACH SEAT EMERGENCY AISLE LIGHTS AND AFT LAVATORY AREA EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE PERFORMED TROUBLESHOOTING OF EMERGENCY LIGHT SYSTEM AND FOUND BAD BATTERIES. MAINTENANCE REPLACED BATTERY PACK.
- [SDR DALA1107969885](https://openairdocs.org/sdr/DALA1107969885.md): Fire Detector · false activation · Jan 31, 2011 · N401EA · Doug DC951 · Fire Detection
  > ACFT HAD A "FIRE" WARNING INDICATION FOR THE NR 2 ENG ON APPROACH INTO MSP. FLIGHT CREW COMPLIED WITH QRH AND ULTIMATELY ACTIVATED THE FIRE BOTTLE AND SHUTDOWN THE NR 2 ENGINE. CREW COMPLETED A SINGLE ENG APPROACH TO AN UNEVENTFUL LANDING. MX DID NOT FIND AN
- [SDR DALA1102049885](https://openairdocs.org/sdr/DALA1102049885.md): Light · melted · Jan 9, 2011 · N401EA · Doug DC951 · Passenger Compartment Lighting
  > FLIGHT DECLARED AN EMERGENCY AFTER A BURNING RUBBER ODOR WAS REPORTED IN THE FWD CABIN. NO VISIBLE SMOKE WAS IDENTIFIED. MX FOUND THE READING LIGHT INSULATOR AT ROW 2 A&B OVERHEATED, DISCOLORED, AND MELTED. THE READING LIGHT ASSY WAS REPLACED AND THE ACFT R
- [SDR DALA1050469885](https://openairdocs.org/sdr/DALA1050469885.md): Wire · damaged · Dec 4, 2010 · N401EA · Doug DC951 · Light System Wiring
  > DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 9 OF THE CABIN WAS INOPERATIVE. MX REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYS.
- [SDR DALA1020669885](https://openairdocs.org/sdr/DALA1020669885.md): Engine · failed · Aug 29, 2010 · N401EA · Doug DC951 · Engine (Turbine/Turboprop)
  > DURING CLIMB AT 4400 FEET ENGINE NR1 EXPERIENCED A COMPRESSOR STALL. THE ENGINE RECOVERED ON IT'S OWN, BUT SMOKE WAS EVIDENT IN THE CABIN AND THE COCKPIT AFTER THE EVENT. FLIGHT CREW COMPLETED THEIR SMOKE CLEARING PROCEDURES AND RETURNED ACFT TO DEPARTURE AIPO
- [SDR DALA100129885](https://openairdocs.org/sdr/DALA100129885.md): Support Channel · cracked · Jan 5, 2010 · N401EA · Doug DC951 · Fuselage Main, Bulkhead
  > DURING "M" CHECK FOUND BULKHEAD SUPPORT CHANNEL CRACKED AT STA 69, AND LBL 18. REPAIRED IAW SRM 51-72-01.
- [SDR DALA100089885](https://openairdocs.org/sdr/DALA100089885.md): Skin · bulged · Jan 4, 2010 · N401EA · Doug DC951 · Fuselage Main, Plate/Skin
  > DURING "M" CHECK FOUND BULGE IN FUSELAGE SKIN AT BS 674 L30. REPAIRED IAW DWG 5925992.
- [SDR DALA100029885](https://openairdocs.org/sdr/DALA100029885.md): Frame · damaged · Jan 2, 2010 · N401EA · Doug DC951 · Fuselage Main, Frame
  > DURING "M" CHECK FOUND DRILL STRIKES IN FWD CARGO FRAME BETWEEN BS 598 L24R-L27R. REPAIRED IAW EA 98-153382.
- [SDR DALA100019885](https://openairdocs.org/sdr/DALA100019885.md): Frame · damaged · Jan 2, 2010 · N401EA · Doug DC951 · Fuselage Main, Frame
  > DURING "M" CHECK FOUND DRILL STRIKES IN FWD CARGO FRAME AT BS 598 L24L-L27L. REPAIRED IAW SRM 51-10-3,51-30-05 AND EA 98-153382.
- [SDR NWAA094549885](https://openairdocs.org/sdr/NWAA094549885.md): Support · cracked · Dec 17, 2009 · N401EA · Doug DC951 · Fuselage Floor Panel
  > DURING "M" CHECK FOUND FLOOR PANEL NR 18 HAD 8 CRACKED SUPPORT RIBS. REPAIRED PER EA 98-216813.
- [SDR NWAA094529885](https://openairdocs.org/sdr/NWAA094529885.md): Support · cracked · Dec 17, 2009 · N401EA · Doug DC951 · Fuselage Floor Panel
  > DURING "M" CHECK FOUND FLOOR PANEL 60C HAD 1 CRACKED SUPPORT RIB. REPAIRED PER EA 98-216815.
- [SDR NWAA094519885](https://openairdocs.org/sdr/NWAA094519885.md): Support · cracked · Dec 17, 2009 · N401EA · Doug DC951 · Fuselage Floor Panel
  > DURING "M" CHECK FOUND FLOOR PANEL 60B HAD 3 CRACKED SUPPORT RIBS. REPAIRED PER EA 98-216814.
- [SDR NWAA094539885](https://openairdocs.org/sdr/NWAA094539885.md): Support · cracked · Dec 16, 2009 · N401EA · Doug DC951 · Fuselage Floor Panel
  > DURING "M" CHECK FOUND FLOOR PANEL NR 17 HAD 1 CRACKED SUPPORT RIB. REPAIRED PER EA 98-216819.
- [SDR NWAA094559885](https://openairdocs.org/sdr/NWAA094559885.md): Floor Panel · damaged · Dec 14, 2009 · N401EA · Doug DC951 · Fuselage Floor Panel
  > DURING "M" CHECK FOUND DAMAGE TO FLOOR PANEL NR 25. REPAIRED PER EA 98-216817.
- [SDR NWAA092499885](https://openairdocs.org/sdr/NWAA092499885.md): Wire · damaged · Jul 13, 2009 · N401EA · Doug DC951 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPAIRED THE WIRING AND FUNCTIONALLY CHECKED THE SYSTEM.
- [SDR NWAA 091709885](https://openairdocs.org/sdr/NWAA%20091709885.md): Battery Pack · inoperative · May 17, 2009 · N401EA · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTS FOR THE CATWALK IN THE TAIL COMPARTMENT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA1151039885](https://openairdocs.org/sdr/DALA1151039885.md): Skin · dented · Sep 10, 2008 · N401EA · Doug DC951 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR STA 237 BETWEEN L17L AND L18L SKIN APPROX HAS L-2 INCHES W-1 INCH AND DENT=.060 IN A PREVIOUS REPAIR. REMOVED EXISTING REPAIR 4 SQ, FABBED & INSTALLED FILLER &DOUBLER IAW DC-9 SRM 53-04 FIG 12B. COMPLETED INITIAL. REPETITIVE: TERMINATED: 2
- [SDR DALA1151709885](https://openairdocs.org/sdr/DALA1151709885.md): Skin · damaged · Sep 8, 2008 · N401EA · Doug DC951 · Fuselage Main, Plate/Skin
  > FUSELAGE EXT STA 120 BETWEEN 17L AND 18L SKIN PROTRUDING CAN'T MEET REQ OF TRM 53-30-8 INTERNAL INSP REQ BY 4500 FH. HFEC INSP REQ AT "L" CHECK INTERVALS. ACCOMPL CLOSE VISUAL INSP OF REPAIR AREA PRIOR TO 3000 FLT CYCLES AFTER SECT 1 AND REPEAT INSP EVERY 3
- [SDR DALA1151029885](https://openairdocs.org/sdr/DALA1151029885.md): Skin · dented · Sep 8, 2008 · N401EA · Doug DC951 · Fuselage Main, Plate/Skin
  > FWD FUSELAGE JUST FWD OF STA 239 AT LONGERON 17L SKIN HAS DENT. MEASURED DENT 1" X.026" D/X= 38. MEETS REQUIREMENTS OF DC-9 SRM 53-04 FIG 38. LESS THAN 1 INCN TO STRUCTURE CLASS III EXTERNAL DOUBLER REPAIR INSTALLED AT THIS LOCATION REF LOG PAGE 2935101 DA
- [SDR NWAA081969885](https://openairdocs.org/sdr/NWAA081969885.md): Battery Pack · inoperative · May 5, 2008 · N401EA · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 9 AND 13 OF THE CABIN GO DIM AFTER ABOUT 3 SECONDS. MAINTENANCE REPLACED THE BATTERY PACK AT THE OVERWING FWD LEFT EXIT LIGHT ASSEMBLY. LIGHTS RETURNED TO NORMAL FUNCTION AND OP
- [SDR NWAA081979885](https://openairdocs.org/sdr/NWAA081979885.md): Battery Pack · inoperative · May 5, 2008 · N401EA · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 12 AND 19 OF THE CABIN GO DIM AFTER ABOUT 3 SECONDS. MAINTENANCE REPLACED THE BATTERY PACK AT THE OVERWING AFT LEFT EXIT LIGHT ASSEMBLY. LIGHTS RETURNED TO NORMAL FUNCTION AND O
- [SDR NWAA081959885](https://openairdocs.org/sdr/NWAA081959885.md): Battery Pack · inoperative · May 5, 2008 · N401EA · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 5 AND 8 OF THE CABIN GO DIM AFTER ABOUT 3 SECONDS. MAINTENANCE REPLACED THE BATTERY PACK AT THE OVERWING FWD RIGHT EXIT LIGHT ASSEMBLY. LIGHTS RETURNED TO NORMAL FUNCTION AND OP
- [SDR NWAA081899885](https://openairdocs.org/sdr/NWAA081899885.md): Power Supply · discharged · May 1, 2008 · N401EA · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK THE EMERGENCY OVERWING EXIT SIGNS AT ROW 19, 20, 21 AND 22 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE ASSOCIATED FUSE AND BATTERY, NEITHER CORRECTED THE PROBLEM. THE POWER SUPPLY WAS CHANGED AND THE SYSTEM CHECKS NORMAL.
- [SDR NWAA070689885](https://openairdocs.org/sdr/NWAA070689885.md): Stringer · cracked · Jan 29, 2007 · N401EA · Doug DC951 · Trailing Edge Flaps
  > DURING "H" CHECK, FOUND CRACK IN LT WING TRAILING EDGE FLAP FORWARD SPAR UPPER STRINGER. REPAIRED PER EA 99-208451.
- [SDR 0602819885](https://openairdocs.org/sdr/0602819885.md): Coupling · leaking · Dec 26, 2006 · N401EA · Doug DC951 · Hydraulic System, Main
  > DURING THE CLIMB JUST AFTER TAKEOFF, THE COCKPIT CREW HEARD A POP SOUND AND NOTICED A CHANGE IN AIR-CONDITIONING AIRFLOW. SOON THERE AFTER THE CABIN CREW REPORTED A BURNING RUBBER SMELL PERMEATING THE CABIN AREA. COM PROCEDURES WERE COMPLIED WITH AND AFTER CO
- [SDR 0500269885](https://openairdocs.org/sdr/0500269885.md): Wheel · failed · Mar 2, 2005 · N401EA · Doug DC951 · Wheel/Ski/Float
  > ON LANDING ROLL-OUT WITH MODERATE BRAKING AND LITTLE ANTI-SKID CYCLING, THE LEFT MAIN GEAR OUTBOARD WHEEL FAILED ALLOWING TIRE DEFLATION. CREW SAFELY STOPPED THE AIRCRAFT ON THE TAXIWAY FOR INSPECTION AND THE PASSENGERS WERE TRANSPORTED TO THE TERMINAL. RUNW
- [SDR 0500019885](https://openairdocs.org/sdr/0500019885.md): Line · failed · Jan 5, 2005 · N401EA · Doug DC951 · Hydraulic System, Main
  > THE AIRCRAFT EXPERIENCED A COMPLETE LOSS OF HYDRAULIC FLUID FROM THE RT SYS AFTER THE LANDING GEAR WAS EXTENDED FOR LANDING. LANDING WAS UNEVENTFUL AT MCI BUT CFR WAS ON STANDBY. MAINTENANCE FOUND A FAILED HYDRAULIC LINE IN THE WHEEL WELL. THE LINE, RIGHT E
- [SDR 0202089885](https://openairdocs.org/sdr/0202089885.md): Duct · cracked · Jun 21, 2002 · N401EA · Doug DC951 · Engine Anti-Icing System
  > DURING CLIMB, THE LEFT ENGINE EXPERIENCED A FIRE WARNING INDICATION. CREW RETARDED THE LEFT ENGINE THRUST TO IDLE. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE LEFT ENGINE FUEL HEAT DUCT. ENGINE OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE
- [SDR 9903169885](https://openairdocs.org/sdr/9903169885.md): Prox Contl Box · malfunctioned · Aug 12, 1999 · N401EA · Doug DC951 · Landing Gear Position and Warning
  > DURING APPROACH INTO DTW, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. FLIGHT CREW DECLARED AN EMERGENCY AND ALTERNATE GEAR EXTENSION PROCEDURES WERE UTILIZED FOR LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED G
- [SDR 9902109885](https://openairdocs.org/sdr/9902109885.md): Battery · discharged · Jun 16, 1999 · N401EA · Doug DC951 · Emergency Lighting
  > FLIGHT CREW REPORTED EMERGENCY LIGHTING INOPERATIVE OR DIM IN TAIL CONE AREA. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.
- [SDR 9810669885](https://openairdocs.org/sdr/9810669885.md): Power Supply · inop · Sep 21, 1998 · N401EA · Doug DC951 · Emergency Lighting
  > THE FIRST CLASS SECTION ROW EMERGENCY LIGHTING ILLUMINATED WITHOUT MAIN CABIN LIGHTS. MAINTENANCE REPLACED POWER SUPPLY AND BATTERIES. OPERATIONAL CHECK NORMAL.
- [SDR 9810679885](https://openairdocs.org/sdr/9810679885.md): Power Supply · inop · Sep 18, 1998 · N401EA · Doug DC951 · Emergency Lighting
  > PRIOR TO DEPARTURE, THE FIRST CLASS SECTION ROW EMERGENCY LIGHTING ILLUMINATED. MAINTENANCE REPLACED POWER SUPPLY. OPERATIONAL CHECK NORMAL.
- [SDR 9810779985](https://openairdocs.org/sdr/9810779985.md): Power Supply · inoperative · Sep 16, 1998 · N401EA · Doug DC951 · Emergency Lighting
  > FLIGHT ATTENDANT REPORTED EMERGENCY PATH LIGHTING IN FIRST CLASS WOULD NOT SHUT OFF AFTER TAKEOFF. MAINTENANCE REPLACED POWER SUPPLY AT DOOR 1R. OPERATIONAL CHECK NORMAL.
- [SDR 9809889885](https://openairdocs.org/sdr/9809889885.md): Prox Switch · inoperative · Aug 9, 1998 · N401EA · Doug DC951 · Landing Gear Position and Warning
  > AFTER TAKEOFF, ALL THREE LANDING GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. THE FLIGHT CREW RECYCLED THE LANDING GEAR WITH UNSAFE LIGHTS REMAINING ILLUMINATED. LANDING GEAR UNSAFE LIGHTS EXTINGUISHED DURING FLIGHT DESCENT. AIRCRA
- [SDR 9809619885](https://openairdocs.org/sdr/9809619885.md): Controler · failed · Jun 28, 1998 · N401EA · Doug DC951 · Cabin Pressure Controller
  > AIRCRAFT LOST CABIN PRESSURIZATION AT FL350. FLIGHT CREW FOLLOWED COM PROCEDURES AND DESCENDED TO FL90. CABIN OXYGEN MASK DEPLOY SYSTEM ACTIVATED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED OXYGEN GENERATOR CANISTERS
- [SDR 9809589885](https://openairdocs.org/sdr/9809589885.md): Retract Mech · out of adjust · Jun 21, 1998 · N401EA · Doug DC951 · Landing Gear Door Retract Section
  > AFTER TAKEOFF, THE LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. THE FLIGHT CREW FOLLOWED COM PROCEDURES AND LANDED AT MEM WITH LANDING GEAR DOOR EXTENDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT AND RIGHT MAIN LANDI

Next page: https://openairdocs.org/deregistered/N401EA-2018-12-06/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 = 'N401EA' AND deregistration_id = 'N401EA-2018-12-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N401EA-2018-12-06/reports

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