# Service difficulty reports: N801US, cancelled Apr 13, 2017 A list on [N801US, cancelled Apr 13, 2017](https://openairdocs.org/deregistered/N801US-2017-04-13.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 · 60 reports - [SDR USAAD01180](https://openairdocs.org/sdr/USAAD01180.md): Light · inoperative · Nov 9, 2001 · N801US · Doug DC981 · Emergency Lighting > EWR - THE EMERGENCY LIGHT NOT ARMED BULB INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHTS ARM AND CHARGE CIRCUIT BREAKER. REPLACED THE FORWARD CONTROL MODULE PRECAUTIONARY. (M) - [SDR USAAD01133](https://openairdocs.org/sdr/USAAD01133.md): Controller · failed · Jul 8, 2001 · N801US · Doug DC981 · Cabin Pressure Controller > TPA-PIT - FLT 302 - THE CABIN ALTITUDE WARNING LIGHT ILLUMINATED AT 28,000 FEET. THE CREW STARTED AN EMERGENCY DESCENT BUT THE OXYGEN MASKS DEPLOYED. THE OXYGEN MASKS ABOVE SEATS 1A AND C DID NOT DEPLOY. THE AIRCRAFT LANDED AT ITS DESTINATION WITHOUT INCIDE - [SDR 2001F00174](https://openairdocs.org/sdr/2001F00174.md): Light · inoperative · Jul 6, 2001 · N801US · Doug DC981 · Emergency Lighting > IND - THE LOW LEVEL EMERGENCY LIGHTS AND THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE REMOTE RECEIVER. THE OVERWING EMERGENCY EXIT LIGHT WAS REPLACED. THE GREEN CUEING - [SDR 2001F00173](https://openairdocs.org/sdr/2001F00173.md): Receiver · failed · Jul 6, 2001 · N801US · Doug DC981 · Emergency Lighting > IND - THE LOW LEVEL EMERGENCY LIGHTS AND THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE REMOTE RECEIVER. THE OVERWING EMERGENCY EXIT LIGHT WAS REPLACED. THE GREEN CUEING - [SDR USAAD01131](https://openairdocs.org/sdr/USAAD01131.md): Battery · discharged · Jul 6, 2001 · N801US · Doug DC981 · Emergency Lighting > IND - THE LOW LEVEL EMERGENCY LIGHTS AND THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE REMOTE RECEIVER. THE OVERWING EMERGENCY EXIT LIGHT WAS REPLACED. THE GREEN CUEING - [SDR USAAD01121](https://openairdocs.org/sdr/USAAD01121.md): Battery · inoperative · Jun 5, 2001 · N801US · Doug DC981 · Emergency Lighting > IND - THE WALK AROUND FLASHLIGHT BY THE MAIN ENTRY DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) - [SDR USAAD01107](https://openairdocs.org/sdr/USAAD01107.md): Battery · discharged · May 16, 2001 · N801US · Doug DC981 · Emergency Lighting > IND - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 30 WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAAD01046](https://openairdocs.org/sdr/USAAD01046.md): Battery · discharged · Mar 12, 2001 · N801US · Doug DC981 · Emergency Lighting > IND - THE LOW LEVEL EMERGENCY LIGHTS FAILED THE LIGHT TEST. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (M) - [SDR USAA002230](https://openairdocs.org/sdr/USAA002230.md): Trunnion · corroded · Dec 21, 2000 · N801US · Doug DC981 · Nose/Tail Landing Gear Attach Section > PIT - FOUND NOSE GEAR CORRODED 2.417 INCH DIAMETER.148 INCH DEEP, NOSE GEAR RT SIDE TRUNNION FITTING. SPOT FACED OUTBOARD LUG, FABRICATED AND INSTALLED SLEEVE BUSHING PER EA 57052. (M) - [SDR USAA002229](https://openairdocs.org/sdr/USAA002229.md): Longeron · cracked · Dec 5, 2000 · N801US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - FOUND LONGERON CRACKED 2 INCHES, LONGERON 20 RT STATION 995. INSTALLED DOUBLER PER TYP 53-10-28. (M) - [SDR USAA002228](https://openairdocs.org/sdr/USAA002228.md): Longeron · corroded · Dec 5, 2000 · N801US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - FOUND LONGERON CORRODED 2 INCHES BY 1 INCH, LONGERON 25 LT AT STATION 1256-1271. INSTALLED SPLICE PER SRM 53-02 FIG 18 SHT 2. (M) - [SDR USAA002227](https://openairdocs.org/sdr/USAA002227.md): Angle · cracked · Dec 4, 2000 · N801US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - FOUND ANGLE CRACKED 2 INCHES, LT STATION 1347 ATTACH ANGLE. DOUBLER INSTALLED PER 53-05 FIG 23B. (M) - [SDR USAA002226](https://openairdocs.org/sdr/USAA002226.md): Longeron · corroded · Dec 3, 2000 · N801US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - FOUND LONGERON CORRODED 6 INCHES, 26 RT BETWEEN 1219-1233, CORROSION LEVEL 1 TASK NR C57-53300. SPLICED IN LONGERON PER SRM 53-02 FIG 1B. (M) - [SDR USAA010159](https://openairdocs.org/sdr/USAA010159.md): Skin · corroded · Dec 1, 2000 · N801US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - FOUND SKIN CORRODED 12 INCHES BY 3 INCHES, UNDER VHF NR 3 ANTENNA STATION 1155 TO 1174. EXT AND INTERIOR DOUBLER INSTALLED PE SRO DWG 9530005. (M) - [SDR USAA002225](https://openairdocs.org/sdr/USAA002225.md): Skin · corroded · Dec 1, 2000 · N801US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - FOUND SKIN CORRODED, 1 INCH DIAMETER.040, LEVEL 1 TASK NR C57-53300, STATION 823-29 RT SKIN. INSTALLED DOUBLER PER SRM 53-04 PAGE 53. (M) - [SDR USAA002224](https://openairdocs.org/sdr/USAA002224.md): Skin · corroded · Dec 1, 2000 · N801US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - FOUND SKIN CORRODED 12 INCHES BY 3 INCHES WIDE, CORROSION LEVEL 1, UNDER VHF NR 3 ANTENNA, STATION 1155-1174. EXT DOUBLER AND INTERIOR SKIN DOUBLER INSTALLED PER SRO DWG 9530005. (M) - [SDR USAA002222](https://openairdocs.org/sdr/USAA002222.md): Longeron · cracked · Nov 26, 2000 · N801US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - FOUND LONGERON CRACKED.5 INCH, AROUND OUTBOARD FASTENER, STATION 160, LONGERON 4L. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 18. (M) - [SDR USAA002221](https://openairdocs.org/sdr/USAA002221.md): Skin · cracked · Nov 15, 2000 · N801US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - FOUND SKIN CRACKED.25 INCH LONG, STATION 83.5, 10 INCHES LEFT OF C/L FORWARD OF CENTER WINDSHIELD. INSTALLED FILLER AND DOUBLER PER SRM 53-04 FIG 38 SHT 23. (M) - [SDR USAAD00147](https://openairdocs.org/sdr/USAAD00147.md): Valve · leaking · Sep 20, 2000 · N801US · Doug DC981 · Windshield/Door Rain/Ice Removal > PVD - AFTER LANDING IN PVD, THE CAPTAIN REPORTED A STRANGE SMELL IN THE COCKPIT, A BAD TASTE IN THE MOUTH, AND BURNING LUNGS AND EYES, ALONG WITH BEING A LITTLE LIGHT HEADED. MAINTENANCE REPLACED THE LEFT RAIN REPELLANT SOLENOID VALVE AND SPRAY NOZZLE. (M) - [SDR USAAD00119](https://openairdocs.org/sdr/USAAD00119.md): Annunciator · malfunctioned · Jul 27, 2000 · N801US · Doug DC981 · Fuel Pressure Indicating > PHL/DTW - FLT 1164 - DURING CLIMB AFTER TAKEOFF, THE LEFT FUEL FILTER PRESSURE DROP LIGHT CAME ON, BUT THE ENGINE PARAMETERS WERE NORMAL. ABOUT 1 MINUTE LATER, LEFT FUEL FILTER PRESSURE LIGHT EXTINGUISHED AND RIGHT FUEL PRESSURE DROP LIGHT ILLUMINATED. ACFT - [SDR USAAD00089](https://openairdocs.org/sdr/USAAD00089.md): Pump · leaking · Jun 1, 2000 · N801US · Doug DC981 · Hydraulic Pump (Electric/Engine), Main > PIT-ORD - FLT 909 - AFTER SELECTING HYDRAULIC PUMPS ON HIGH, RIGHT PRESSURE GAUGE STARTED TO OSCILLATE AND THEN WETN TO ZERO. QRH PROCEDURES WERE IMPLEMENTED AND FLIGTH LANDED WITHOUT INCIDENT. AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE REPLACED THE ELECTR - [SDR USAAD00032](https://openairdocs.org/sdr/USAAD00032.md): Packing · damaged · Feb 25, 2000 · N801US · Doug DC981 · Hydraulic System, Main > DFW-CLT - FLT 1152 - DURING APPROACH, THE RIGHT HYDRAULIC SYSTEM LOW LIGHT ILLUMINATED WITH A LOSS OF HYDRAULIC FLUID. THE LANDING GEAR WAS MANUALLY EXTENDED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE O-RING AT THE GEAR UP FITTING ON - [SDR USAAD00026](https://openairdocs.org/sdr/USAAD00026.md): Slide · discharged · Feb 7, 2000 · N801US · Doug DC981 · Escape Slide > PIT - THE PASSENGER ENTRY DOOR EVACUATION SLIDE PRESSURE WAS BELOW LIMITS. MAINTENANCE REPLACED THE PASSENGER ENTRY DOOR EVACUATION SLIDE. (M) - [SDR USAA000159](https://openairdocs.org/sdr/USAA000159.md): Skin · cracked · Jan 27, 2000 · N801US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - FOUND SKIN CRACKED AT STATION 1380 LONGERON 13R AND 14R, CRACKS WERE.375 INCH.125 INCH AND.0625 INCH. CUT OUT DAMAGE AREA, INSTALLED FILLER AND DOUBLER PER SRM 53-04, FIG 18. (M) - [SDR USAA991179](https://openairdocs.org/sdr/USAA991179.md): Skin · cracked · Oct 25, 1999 · N801US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING RON, FOUND 1 INCH LONG CRACK IN FUSELAGE SKIN AT FORWARD AIRSTAIR DOOR CUT OUT LOWER AFT CORNER AT STATION 200. INSTALLED EXTERNAL DOUBLERS PER SRM 53-05 FIG 57A. (M) - [SDR USAAD99148](https://openairdocs.org/sdr/USAAD99148.md): Battery · discharged · Oct 19, 1999 · N801US · Doug DC981 · Emergency Lighting > IND - THE LOW LEVEL LIGHTING DID NOT TEST. MAINTENANCE REPLACED THE AFT CONTROL MODULE BATTERY. (M) - [SDR USAAD99132](https://openairdocs.org/sdr/USAAD99132.md): Lanyard · loose · Sep 14, 1999 · N801US · Doug DC981 · Emergency Equipment > ROC - THE 2L DOOR ESCAPE SLIDE AUTO FIRING LANYARD WAS NOT ATTACHED TO THE GIRT BAR. MAINTENANCE ATTACHED THE LANYARD. (M) - [SDR USAA990145](https://openairdocs.org/sdr/USAA990145.md): Angle · cracked · Feb 27, 1999 · N801US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING C-2 CHECK, FOUND ONE.5 INCH CRACK AT UPPER PYLON ATTACH ANGLE AT STATION 1463 CANTED. STOP DRILLED AND FILLED PER TYPICAL REPAIR 54-10-06A. (M) - [SDR USAA990144](https://openairdocs.org/sdr/USAA990144.md): Frame · cracked · Feb 27, 1999 · N801US · Doug DC981 · Fuselage Main, Frame > PIT - DURING C-2 CHECK, FOUND CANTED FRAME CRACK 3 INCH LONG AT STATION 1474, LONGERON 18 LT. STOP DRILLED CRACKED AND DOUBLER. INSTALLED PER SRM 53-01, FIG 2 SH 4. (M) - [SDR USAAD98199](https://openairdocs.org/sdr/USAAD98199.md): Battery · discharged · Oct 31, 1998 · N801US · Doug DC981 · Emergency Lighting > PHL - THE EMERGENCY OVERHEAD, EXIT WINDOWS, AND LOW LEVEL LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD98194](https://openairdocs.org/sdr/USAAD98194.md): Battery · discharged · Oct 31, 1998 · N801US · Doug DC981 · Emergency Lighting > PHL - THE FOLLOWING EMERGENCY LIGHTS WERE INOPERATIVE, PASSENGER CABIN LOW LEVEL LIGHTS, OVERWING EXIT LIGHTS, AFT FUSELAGE EMERGENCY LIGHTS, OVERWING EXIT IDENTIFIER LIGHTS. MAINTENANCE REPLACED THE BATTERIES FOR ALL THE INOPERATIVE EMERGENCY LIGHTS. (M) - [SDR 98ZZZM912](https://openairdocs.org/sdr/98ZZZM912.md): Battery · discharged · Oct 31, 1998 · N801US · Doug DC981 · Emergency Lighting > PHL - THE FOLLOWING EMERGENCY LIGHTS WERE INOPERATIVE, PASSENGER CABIN LOW LEVEL LIGHTS, OVERWING EXIT LIGHTS, AFT FUSELAGE EMERGENCY LIGHTS, OVERWING EXIT IDENTIFIER LIGHTS. MAINTENANCE REPLACED THE BATTERIES FOR ALL THE INOPERATIVE EMERGENCY LIGHTS. (M) - [SDR 98ZZZM911](https://openairdocs.org/sdr/98ZZZM911.md): Battery · discharged · Oct 31, 1998 · N801US · Doug DC981 · Emergency Lighting > PHL - THE FOLLOWING EMERGENCY LIGHTS WERE INOPERATIVE, PASSENGER CABIN LOW LEVEL LIGHTS, OVERWING EXIT LIGHTS, AFT FUSELAGE EMERGENCY LIGHTS, OVERWING EXIT IDENTIFIER LIGHTS. MAINTENANCE REPLACED THE BATTERIES FOR ALL THE INOPERATIVE EMERGENCY LIGHTS. (M) - [SDR 98ZZZM910](https://openairdocs.org/sdr/98ZZZM910.md): Battery · discharged · Oct 31, 1998 · N801US · Doug DC981 · Emergency Lighting > PHL - THE EMERGENCY OVERHEAD, EXIT WINDOWS, AND LOW LEVEL LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR 98ZZZM909](https://openairdocs.org/sdr/98ZZZM909.md): Battery · discharged · Oct 31, 1998 · N801US · Doug DC981 · Emergency Lighting > PHL - THE EMERGENCY OVERHEAD, EXIT WINDOWS, AND LOW LEVEL LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD98155](https://openairdocs.org/sdr/USAAD98155.md): Battery · discharged · Sep 6, 1998 · N801US · Doug DC981 · Emergency Lighting > PHL - THE LOW LEVEL EMERGENCY LIGHT AT ROW 25D STAYED ON WITH THE COCKPIT SWITCH IN THE ARM POSITION. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERY. (M) - [SDR USAAD98119](https://openairdocs.org/sdr/USAAD98119.md): Sensor · damaged · Jul 8, 1998 · N801US · Doug DC981 · Door Warning System > CLT - FLT 514 - AFTER TAKEOFF THE MID CARGO DOOR WARNING LIGHT ILLUMINATED AND THE CABIN WOULD NOT PRESSURIZE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. LANDING WEIGHT WAS 129,300 LB. MAINTENANCE INSPECTED THE MID CARGO DOOR FOR DAMAGE - [SDR USAAD98108](https://openairdocs.org/sdr/USAAD98108.md): Battery · discharged · Jun 8, 1998 · N801US · Doug DC981 · Emergency Lighting > DCA - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD97187](https://openairdocs.org/sdr/USAAD97187.md): Transmitter · malfunctioned · Oct 28, 1997 · N801US · Doug DC981 · Hydraulic Indicating System > PIT - FL 335 - ON FINAL APPROACH THE LANDING GEAR HANDLE REQUIRED MORE THAN NORMAL PRESSURE TO MOVE IT TO THE DOWN POSITION. THE CREW THEN EXTENDED THE SLATS AND FLAPS. THE SLATS EXTENDED BUT THE FLAPS DID NOT MOVE. AFTER PERFORMING A GO-AROUND AND TURNING - [SDR USAA970310](https://openairdocs.org/sdr/USAA970310.md): Longeron · cracked · Oct 17, 1997 · N801US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING UNSCHEDULED MAINTENANCE, FOUND 1 INCH CRACK BETWEEN STATION 237 AND STATION 258 AT LONGERON NR 30. INSTALLED SPLICE REPAIR PER TYPICAL REPAIR 53-10-17. (M) - [SDR USAA970309](https://openairdocs.org/sdr/USAA970309.md): Skin · corrosion · Oct 17, 1997 · N801US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING RON, FOUND CORRODED AREA 4 INCH BY 5 INCH AT TCAS ANTENNA, FUSELAGE SKIN BETWEEN STATION 237 AND STATION 258 LONGERON 29RT TO 29 LT. INSTALLED EXTERNAL DOUBLER AND REPLACED TCAS DOUBLER PER SRM 53-04 FIG 51 CLASS 2 REPAIR. (M) - [SDR USAAD97117](https://openairdocs.org/sdr/USAAD97117.md): Batteries · discharged · Jul 9, 1997 · N801US · Doug DC981 · Emergency Lighting > PIT - FOUND LOW LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROW 29. REPLACED BATTERIES. (M) - [SDR USAAD97031](https://openairdocs.org/sdr/USAAD97031.md): Batteries · discharged · Feb 2, 1997 · N801US · Doug DC981 · Emergency Lighting > IND - CEILING EMERGENCY LIGHTS INOPERATIVE IN ALL BUT 2 SECTIONS OF AIRCRAFT. REPLACED BATTERIES IN POWER SUPPLIES. CHECKS GOOD. (M) - [SDR USAAD97032](https://openairdocs.org/sdr/USAAD97032.md): Clamp · failed · Feb 1, 1997 · N801US · Doug DC981 · Pneumatic Distribution System > FLT 1020 - RSW-CLT - IN FLIGHT AT FL 240, THE NR 2 FIRE WARNING LIGHT ILLUMINATED. SELECTED B LOOP. RIGHT ENGINE FIRE HANDLE ILLUMINATED. FIRED NR 1 FIRE BOTTLE, SHUT DOWN RIGHT ENGINE. SINGLE ENGINE TIME WAS 15 MINUTES. REPLACED CLAMP ON 13TH STAGE DUCT - [SDR USAAD97018](https://openairdocs.org/sdr/USAAD97018.md): Power Supply · inoperative · Jan 21, 1997 · N801US · Doug DC981 · Emergency Lighting > IND - WING EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY. (M) - [SDR USAAD96130](https://openairdocs.org/sdr/USAAD96130.md): Retract Mech · malfunctioned · Sep 18, 1996 · N801US · Doug DC981 · Landing Gear Door Retract Section > FLT 368 - RSW-CLT - ON TAKEOFF, CREW HEARD SOUND FROM NOSE AREA, RETURNED TO FIELD. FOUND NOSEGEAR DOORS OPEN. CLOSED DOORS, INSPECTED NOSE AREA AND GLIDESLOPE ANTENNA. NO DEFECTS NOTED, RETURNED AIRCRAFT TO SERVICE. (M) - [SDR USAA960433](https://openairdocs.org/sdr/USAA960433.md): Skin · cracked · May 14, 1996 · N801US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND TWO CRACKS.25 INCH EACH, STATION 1437 BETWEEN LONGERON 2R AND 4R IN FUSELAGE SKIN. INSTALLED EXTERNAL DOUBLER PER SRM 53-04 FIG 27. (M) - [SDR USAA960432](https://openairdocs.org/sdr/USAA960432.md): Skin · cracked · May 14, 1996 · N801US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND TWO CRACKS.5 INCH LONG EACH, STATION 1437 BETWEEN LONGERON 2L AND 4L, IN AIRCRAFT FUSELAGE SKIN. REPAIRED WITH EXTERNAL DOUBLER PER SRM 53-04 FIG 27 USAIR EA NR 32644 AND EA NR 32647. (M) - [SDR USAA960426](https://openairdocs.org/sdr/USAA960426.md): Longeron · cracked · May 13, 1996 · N801US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND 1 INCH CRACK IN LOWER FLANGE IN LONGERON 17R, 4 PLACES AT STATION 256, 408, 370 AND 389. REMOVED DAMAGED SECTION OF LONGERON AND ACCOMPLISHED SPLICE REPAIR PER SRM 53-02 PAGE 2A. (M) - [SDR USAA960425](https://openairdocs.org/sdr/USAA960425.md): Longeron · cracked · May 13, 1996 · N801US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND TWO 1 INCH CRACKS IN LONGERON 17R LOWER FLANGE STATION 228 AND 237. REMOVED DAMAGED SECTION AND SPLICED IN NEW SECTION PER SRM 53-02 FIG 2 PG 2A. (M) Next page: https://openairdocs.org/deregistered/N801US-2017-04-13/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 = 'N801US' AND deregistration_id = 'N801US-2017-04-13' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N801US-2017-04-13/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.