# Service difficulty reports: N950DL, cancelled Aug 13, 2019 A list on [N950DL, cancelled Aug 13, 2019](https://openairdocs.org/deregistered/N950DL-2019-08-13.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 3 · 136 reports - [SDR DALA2018110606456](https://openairdocs.org/sdr/DALA2018110606456.md): Battery Pack · inoperative · Nov 5, 2018 · N950DL · Doug MD88 · Emergency Lighting > FOUND EMERGENCY CEILING LIGHTS INOP FROM ROW 24-28 AND ROW 4-1. REPLACED BATTERIES IN BOTH BATTERY PACKS IN OVERHEAD BINS 4 AND 28 PER MD88 AMM 33-53. LIGHTS WORK GOOD. (LP5255009) - [SDR DALA2018080304837](https://openairdocs.org/sdr/DALA2018080304837.md): Smoke Detector · false activation · Aug 2, 2018 · N950DL · Doug MD88 · Smoke Detection > RT AFT LAV SMOKE DETECTOR KEEPS GOING OFF. REPLACED BATTERY- NO HELP. REMOVED BATTERY AND FWD SMOKE DETECTOR TO MEL 26-00-07. - [SDR DALA2018072404637](https://openairdocs.org/sdr/DALA2018072404637.md): Battery · discharged · Jul 24, 2018 · N950DL · Doug MD88 · Emergency Lighting > TAIL EMERGENCY CEILING LIGHT INOP. REMOVED AND REPLACED BATTERIES IN RIGHT AFT LAV. OPERATIONAL CHECK OK IAW AMM 33-50. P/N:AD4002P. - [SDR DALA2018071904559](https://openairdocs.org/sdr/DALA2018071904559.md): Battery · discharged · Jul 19, 2018 · N950DL · Doug MD88 · Emergency Lighting > THE COCKPIT & FWD GALLEY CEILING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE EMERGENCY BATTERY PACK B5-23 PER AMM 33-53. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. - [SDR DALA2018061804118](https://openairdocs.org/sdr/DALA2018061804118.md): Battery · discharged · Jun 18, 2018 · N950DL · Doug MD88 · Emergency Lighting > EMERGENCY CEILING LIGHTS INOP ROWS 15-20. REMOVED AND REPLACED BATTERIES AT B5-102 PER AMM 33-53. LIGHTS CK NML. - [SDR DALA2018052003454](https://openairdocs.org/sdr/DALA2018052003454.md): Frame · cracked · May 19, 2018 · N950DL · Doug MD88 · Aerodynamic Fairings > TAILCONE AREA, FOUND FRAME CRACKED AT 9:00 POSITION. REMOVED CRACKED FRAME FROM 9-6:00 O'CLOCK POSITION BEGAN DRILLING REPLACEMENT FRAME. COMPLETED DRILLING FRAME AND INSTALLED PER DWG 5966769-1. - [SDR DALA2018052003453](https://openairdocs.org/sdr/DALA2018052003453.md): Cable · damaged · May 19, 2018 · N950DL · Doug MD88 · Aerodynamic Fairings > KEVLAR CABLE DAMAGED AND BULGED-OUTER COVERING NOT COMPLETE IN ONE AREA. REPLACED KEVLAR CABLE PER AMM 53-53. - [SDR DALA2018010400066](https://openairdocs.org/sdr/DALA2018010400066.md): Compressor · stalled · Jan 3, 2018 · N950DL · Doug MD88 · Turbine Engine Compressor Section > ON APPROACH TO DTW AT APPROXIMATELY 2000'AGL, RIGHT ENGINE EXPERIENCED COMPRESSOR STALL. STALL STOPPED WHEN THROTTLE WAS RETARDED. EMERGENCY DECLARED. RT ENGINE REPLACED. - [SDR DALA2017121808713](https://openairdocs.org/sdr/DALA2017121808713.md): Battery Pack · inoperative · Dec 16, 2017 · N950DL · Doug MD88 · Emergency Lighting > OVERHEAD CABIN EMERGENCY LIGHTS INOPERATIVE ROWS 22-25. REPLACED THE BATTERIES. - [SDR DALA2017070705268](https://openairdocs.org/sdr/DALA2017070705268.md): Wire Harness · damaged · Jul 6, 2017 · N950DL · Doug MD88 · Light System Wiring > EMERGENCY LIGHT AT 35D INOPERATIVE. FOUND HARNESS DAMAGED. REPLACED HARNESS IAW AMM 33-53. OPS NORMAL. - [SDR DALA2017012900735](https://openairdocs.org/sdr/DALA2017012900735.md): Cable · misrouted · Jan 28, 2017 · N950DL · Doug MD88 · Aerodynamic Fairings > TAILCONE CABLE MISROUTED. NOT THROUGH TAILCONE FAIRLEAD. TAILCONE INSTALLED IAW AMD S5350-4642. CABLE ROUTED CORRECTLY. - [SDR DALA2016122910131](https://openairdocs.org/sdr/DALA2016122910131.md): Acm · leaking · Dec 28, 2016 · N950DL · Doug MD88 · Cabin Cooling System > ON SHORT FINAL, SMELLED A SMOKE TYPE ODOR. FA STATED BOTH LAVATORY SMOKE DETECTORS ON CAPTAIN SIDE (FRONT & BACK) WENT OFF. A HAZE WAS OBSERVED IN THE CABIN. FOUND RIGHT ACM LEAKING OIL. REPLACED THE ACM. COMPLETED DUCT BURN-OUT. - [SDR DALA2016122910129](https://openairdocs.org/sdr/DALA2016122910129.md): Door Frame · corroded · Dec 28, 2016 · N950DL · Doug MD88 · Fuselage Main, Structure > MID CARGO LOWER DOOR FRAME HAS CORROSION BETWEEN BS 636 - 693. REPAIRED THE LOWER DOOR FRAME IAW PRI/ERA 553436-14. - [SDR DALA2016122810103](https://openairdocs.org/sdr/DALA2016122810103.md): Angle · damaged · Dec 28, 2016 · N950DL · Doug MD88 · Fuselage Main, Frame > DENT AND CRACKED ANGLE AT AIRSTAIR CUTOUT 1 FT FWD OF AFT RT CORNER. REPAIRED IAW ER/A 553772-14. - [SDR DALA2016122810102](https://openairdocs.org/sdr/DALA2016122810102.md): Frame · damaged · Dec 28, 2016 · N950DL · Doug MD88 · Fuselage Main, Frame > REPAIR ANGLE CRACKED AT LOWER END OF BS 1485 FRAME RT SIDE NEAR STAIR ACTUATING CYLINDER. REPAIRED IAW ER/A 553772-14. - [SDR DALA2016122710090](https://openairdocs.org/sdr/DALA2016122710090.md): Fitting · cracked · Dec 26, 2016 · N950DL · Doug MD88 · Wing, Attach Fittings > RT WING TE GROUND SPOILER ACTUATOR FWD FITTING CRACKED. REPLACED THE FITTING IAW DWG SR09570010 REV. H. - [SDR DALA2016122210026](https://openairdocs.org/sdr/DALA2016122210026.md): Beam · corroded · Dec 21, 2016 · N950DL · Doug MD88 · Fuselage Main, Structure > MID CARGO DOOR THRESHOLD BEAM SEVERAL AREAS OF CORROSION FROM BS 636 TO 693. REMOVED AND REPLACED THE BEAM IAW DWG 5936038. - [SDR DALA2016121909974](https://openairdocs.org/sdr/DALA2016121909974.md): Clamp · out of adjust · Dec 19, 2016 · N950DL · Doug MD88 · Aerodynamic Fairings > TAILCONE RELEASE SYSTEM, LOCKING CABLE CLAMP DOES NOT CLEAR LOWER END OF CONDUITS BY 1/2" REF AMDS CARD5350-01077-0101 STEP 7, D, 5. REPAIR REF AMM 53-53-00. OPS WILL BE PERFORMED ON AMDS 5350-01077-0101. - [SDR DALA2016121909964](https://openairdocs.org/sdr/DALA2016121909964.md): Bushing · worn · Dec 19, 2016 · N950DL · Doug MD88 · Aerodynamic Fairings > TAILCONE RELEASE SYSTEM, T-PIN & BUSHING WORN FOR PULL CABLE. SEE NR FOR ADDITIONAL INFORMATION 031-0001:5350-01077-0101/002 00005 REPAIRED REF AMM 53-53-00. - [SDR DALA2016121909940](https://openairdocs.org/sdr/DALA2016121909940.md): Support Angle · corroded · Dec 17, 2016 · N950DL · Doug MD88 · Fuselage Miscellaneous Structure > AFT CARGO DOOR THRESHOLD BEAM AND STRAP SEVERAL AREAS OF CORROSION FROM STA 1154 TO STA 1211 ALSO BETWEEN SKIN LAYERS NEAR AFT DOOR STOP. AFT CARGO THRESHOLD, BLENDED AFT BEAM LOWER SUPPORT FOUND WITHIN LIMITS PER SRM 53-01. REPLACED FWD BEAM LOWER SUPPORT AN - [SDR DALA2016121809933](https://openairdocs.org/sdr/DALA2016121809933.md): Skin · corroded · Dec 17, 2016 · N950DL · Doug MD88 · Fuselage Main, Plate/Skin > ERA 553436-14 SECTION 1 ISSUED FOR CORROSION DAMAGE TO C2 DOOR FRAME DOUBLER AND SKIN. ACCOMPLISH SECTION II INSPECTION EVERY 8000 CYCLES FOLLOWING SECTION I ER/A 88-553436. - [SDR DALA2016121309796](https://openairdocs.org/sdr/DALA2016121309796.md): Cable · frayed · Dec 12, 2016 · N950DL · Doug MD88 · Aerodynamic Fairings > TAIL CONE KEVLAR CABLE FRAYING. A NEW KEVLAR CABLE WAS INSTALLED IAW AMM 53-53-00. - [SDR DALA2016120609642](https://openairdocs.org/sdr/DALA2016120609642.md): Cable · loose · Dec 5, 2016 · N950DL · Doug MD88 · Aerodynamic Fairings > TAILCONE RELEASE SYSTEM, TEE PIN PULL CABLE HAS EXCESSIVE SLACK. REPAIRED IAW AMM 53-53-00. RIGGED THE CABLE IAW AMDS 5350-01077-0101. - [SDR DALA2016071505331](https://openairdocs.org/sdr/DALA2016071505331.md): Engine · making metal · Jul 14, 2016 · N950DL · Doug MD88 · Engine (Turbine/Turboprop) > RETURNED TO DEPARTURE, DUE TO AN OIL STRAINER CLOGGED MESSAGE. MAINTENANCE FOUND METAL ON THE MCD AND IN THE OIL FILTER. ENGINE CHANGE REQUIRED. - [SDR DALA2016051703968](https://openairdocs.org/sdr/DALA2016051703968.md): Door · lack of lube · May 9, 2016 · N950DL · Doug MD88 · Aerodynamic Fairings > DURING TAILCONE RELEASE FUCTIONAL CHECK FOUND ARMING HANDLE HARD TO ROTATE. LUBED DOOR IAW AMM 12-21. CONFIRMED RIGGING AND RELEASE FORCE IAW AMM 52-12. OPS CHECK GOOD. - [SDR DALA2016022901490](https://openairdocs.org/sdr/DALA2016022901490.md): Line · broken · Feb 22, 2016 · N950DL · Doug MD88 · Hydraulic System, Main > WHILE ENROUTE, THE FLIGHT DIVERTED TO MEM FOLLOWING THE "RT HYDRAULIC LOW" MESSAGE ILLUMINATING ALONG WITH THE RT HYDRAULIC QUANTITY RAPID DECREASING TO 2 QUARTS. COMPLETED CHECKLIST. NOTE: F/A REPORTED LOUD NOISE DURING CLIMBOUT BUT NO INDICATIONS OF ANY PRO - [SDR DALA2015102706520](https://openairdocs.org/sdr/DALA2015102706520.md): Battery Pack · discharged · Oct 26, 2015 · N950DL · Doug MD88 · Emergency Lighting > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 31-35 OF THE CABIN WERE INOPERATIVE. MAINTENANCE CHARGED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION. - [SDR DALA2015102706519](https://openairdocs.org/sdr/DALA2015102706519.md): Battery Pack · discharged · Oct 26, 2015 · N950DL · Doug MD88 · Emergency Lighting > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE VENTRAL STAIRWAY WERE INOPERATIVE. MAINTENANCE CHARGED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION. - [SDR DALA2015093005879](https://openairdocs.org/sdr/DALA2015093005879.md): Light · inoperative · Sep 14, 2015 · N950DL · Doug MD88 · Emergency Lighting > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 35 WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT. - [SDR DALA2015012900776](https://openairdocs.org/sdr/DALA2015012900776.md): Lanyard · damaged · Jan 28, 2015 · N950DL · Doug MD88 · Escape Slide > MAINTENANCE FOUND SLIDE LANYARD AT THE L1 DOOR FREYED AND DAMAGED. MAINTENANCE REPLACED SLIDE LANYARD ASSY AT L-1 DOOR. CKS OK. - [SDR DALA2014111706132](https://openairdocs.org/sdr/DALA2014111706132.md): Rib · cracked · Nov 13, 2014 · N950DL · Doug MD88 · Wing, Rib/Bulkhead > CRACK ON RIB XRS=164.000 L/E RT WING. RIB WAS REPAIRED IAW SRM 57-06-B, PAR-16. - [SDR DALA2014071104063](https://openairdocs.org/sdr/DALA2014071104063.md): Outflow Valve · leaking · Jul 10, 2014 · N950DL · Doug MD88 · Pressure Regulator/Outflow Valve > FLIGHT DIVERTED DUE TO THE LOSS OF CABIN PRESSURE CONTROL. AN EMERGENCY WAS DECLARED. MAINTENANCE DISCOVERED THAT THE OUTFLOW VALVE WAS LEAKING BEYOND ALLOWABLE LIMITS AND PLACED IT ON MEL 21-00-25. THE OUTFLOW VALVE WAS REPLACED AND 2 OTHER FUSELAGE LEAKS W - [SDR DALA14015810950](https://openairdocs.org/sdr/DALA14015810950.md): Power Supply · inoperative · Mar 8, 2014 · N950DL · Doug MD88 · Emergency Lighting > DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY EMERGENCY POWER SUPPLY IAW AMM 33-53-00. OPS CHECKED OK. ACFT OK FOR SERVICE. - [SDR DALA14010840950](https://openairdocs.org/sdr/DALA14010840950.md): Battery Pack · inoperative · Feb 18, 2014 · N950DL · Doug MD88 · Emergency Lighting > DURING LINE CHECK, NOTED AFT WING ENERGENCY DOOR UPPER LIGHTS WERE INOPERATIVE. REPLACED BATTERY PACKS IAW AMM 33-50 AND OPS CHECKED GOOD. - [SDR DALA13042580950](https://openairdocs.org/sdr/DALA13042580950.md): Battery Pack · inoperative · Sep 1, 2013 · N950DL · Doug MD88 · Emergency Lighting > DURING LINE CHECK, MX FOUND THAT BOTH OF THE OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION. - [SDR DALA13027160950](https://openairdocs.org/sdr/DALA13027160950.md): Heater Blanket · damaged · Jun 4, 2013 · N950DL · Doug MD88 · Airfoil Anti/De-ice System > CRACK AFT EDGE ON RT WING HEATER BLANKET. RT WING HEATER BLANKET PANEL WAS REPLACED DUE TO DIMENTIONS OF DAMAGE (0.656") IAW AMM 30-80-02, PAGE BLOCK 401 PARA 2A. RII COMPLETED BY INSPECTION STAMP INSPECTOR. - [SDR DALA13027150950](https://openairdocs.org/sdr/DALA13027150950.md): Skin · cracked · Jun 3, 2013 · N950DL · Doug MD88 · Fuselage Main, Plate/Skin > CRACK ON FUSELAGE SKIN AT STA Y=1418 BETWEEN LONGERON 2 AND 3LT WITH A LENGTH OF 0.593 INCH. CRACK REMOVED, REPAIR DOUBLERS & FILLERS WERE FABRICATED AND INSTALLED IAW ER/A 514799-14AD REV ORIGINAL. REPAIR WAS IDENTIFIED IAW PS 900-5-1, NR 4. - [SDR DALA13027080950](https://openairdocs.org/sdr/DALA13027080950.md): Floorbeam · corroded · Jun 3, 2013 · N950DL · Doug MD88 · Fuselage Main, Floor Beam > CORROSION ON FLOORBEAM ANGLE BS 1309 X=-20. CORROSION WAS REMOVED IAW SRM 51-10-3 OAR 26 MEASURED AND FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1. REPAIRED IAW ER/A 514805-14 REV ORIGINAL. - [SDR DALA13026960950](https://openairdocs.org/sdr/DALA13026960950.md): Floor Support · corroded · May 31, 2013 · N950DL · Doug MD88 · Fuselage Miscellaneous Structure > CORROSION ON FLOOR SUPPORT FROM BS 1212 TO 1136 ABOVE LONGERON 29R. CORROSION WAS REMOVED, FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1. FLOOR SUPPORT REPLACED IAW DWG 593660, REV BZ AND SRM 51-30-2 AND 51-30-5. - [SDR DALA13026950950](https://openairdocs.org/sdr/DALA13026950950.md): Cargo Track · corroded · May 31, 2013 · N950DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON TIE TRACK FROM BS 1212 - 1322 AT AFT CARGO COMPARTMENT. REMOVED CARGO TRACK AND INSTALLED NEW CARGO TRACK IAW SRM 51-30-1 AND 51-10-4, 51-10-3, PAR 18 AND 21. - [SDR DALA13026940950](https://openairdocs.org/sdr/DALA13026940950.md): Cargo Track · corroded · May 31, 2013 · N950DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON LT CARGO TRACK BETWEEN BS 1007-1222 ALSO ON SPLICE AT AFT CARGO COMPARTMENT. LT CARGO TRACK OUT OF LIMITS WAS REPLACED IAW SRM 51-30-2 AND 51-30-1. - [SDR DALA13026920950](https://openairdocs.org/sdr/DALA13026920950.md): Cargo Track · corroded · May 31, 2013 · N950DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON LT CARGO TRACK FROM BS 1022 TO 1322 AT AFT CARGO COMPARTMENT. LEFT CARGO TRACK OUT OF LIMITS AND WAS REPLACED IAW SRM 51-30-1 AND 51-30-2. - [SDR DALA13026880950](https://openairdocs.org/sdr/DALA13026880950.md): Skin · dented · May 31, 2013 · N950DL · Doug MD88 · Elevator, Plate/Skin > DENT ON LT ELEVATOR LOWER SKIN STA XE 219 6" LENGHT 2.437 WITH REF ONRC 702. DENT OUT OF LIMITS IAW SRM 51-50-2, PARA 5. DENT WAS REPAIRED IAW SRM 55-01, FIG 2 AND 51-60-0 PARA 5. REMOVE FROM MONITOR. DENT REPAIR IS PERMANENT. - [SDR DALA13026870950](https://openairdocs.org/sdr/DALA13026870950.md): Access Panel · corroded · May 31, 2013 · N950DL · Doug MD88 · Wing, Plate/Skin > CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL TANK ACCESS DOOR NR 1361C. CORROSION WAS REMOVED, COUNTERSINK WERE MEASURED AND WERE FOUND OUT OF LIMITS. CONDITION II MAXIMUM DIAMETER ALLOWABLE IS 0.554", 0.585", 0.554", 0.567", AND 0.0602". THEREFORE AC - [SDR DALA13026860950](https://openairdocs.org/sdr/DALA13026860950.md): Plate · corroded · May 31, 2013 · N950DL · Doug MD88 · Fuselage Miscellaneous Structure > CORROSION ON LONGERON PLATE 23LT BETWEEN STA Y=1238 TO 1260. UTILITARY TUNNEL AFT CARGO COMPARTMENT. STRIP WAS REMOVED AND A NEW STRIP WAS INTALLED IAW SRM 59300-2, REV EH. - [SDR DALA13026890950](https://openairdocs.org/sdr/DALA13026890950.md): Cargo Track · corroded · May 30, 2013 · N950DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings > CORROSION AND ELONGATED HOLES ON RT CARGO TRACK BETWEEN STA Y=1138-1155 AT AFT CARGO COMPARTMENT. REMOVE CARGO TRACK AND CORROSION, MEASURE, REPLACED CARGO TRACK, AND INSTALLED NEW CARGO TRACK IAW SRM 51-10-3, PAR 14, 21, 26, 38, 53,-05 FIG 4C, 51-30-2,51-30- - [SDR DALA13026800950](https://openairdocs.org/sdr/DALA13026800950.md): Longeron Splice · damaged · May 30, 2013 · N950DL · Doug MD88 · Fuselage Main, Longeron/Stringer > CRACK ON REPAIR SPLICE LONGERON 23LT BETWEEN STA Y=1155 TO Y=1174, UTILITARY TUNNEL AFT CARGO COMPARTMENT. REMOVE SPLICE, FABRICATE, AND INSTALL NEW SPLICE IAW SRM 51-10-3, PAR 21, 14 AND ER/A 269449-14, REV B. - [SDR DALA13026930950](https://openairdocs.org/sdr/DALA13026930950.md): Plate · corroded · May 29, 2013 · N950DL · Doug MD88 · Fuselage Main, Longeron/Stringer > CORROSION ON LONGERON PLATE 23L BETWEEN BS 1287 TO 1309 UTILITARY TUNNEL AT AFT CARGO COMPARTMENT. STRIP WAS REMOVED, NEW STRIP WAS REPLACED IAW SRM 51-30-2. - [SDR DALA13026810950](https://openairdocs.org/sdr/DALA13026810950.md): Doubler · corroded · May 29, 2013 · N950DL · Doug MD88 · Fuselage Main, Plate/Skin > CORROSION ON PRODUCTION DOUBLER BELOW VERTICAL WEB, STA 1338 BETWEEN LONG 28RT-28LT AT AFT CARGO COMPARTMENT. DUE TO EXCESIVE CORROSION ON PRODUCTION DOUBLER IT WAS REPLACED IAW DWG 9915561, REV CG AND SRM 51-30-2 AND 51-30-5. - [SDR DALA13026450950](https://openairdocs.org/sdr/DALA13026450950.md): Longeron · corroded · May 29, 2013 · N950DL · Doug MD88 · Fuselage Main, Longeron/Stringer > CORROSION ON LONGERON 22L BETWEEN BS 1287 TO 1309, ALSO RUSTED NUTS SAME AREA LT UTILITARY TUNNEL AFT CARGO COMPARTMENT. CORROSION ON LONGERON WAS REMOVED AND REMAINING THICKNESS WAS FOUND OUT OF LIMITS IAW SRM 53-01, FIG 61. SECTION OF LONGERON FROM BS 127 Next page: https://openairdocs.org/deregistered/N950DL-2019-08-13/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 = 'N950DL' AND deregistration_id = 'N950DL-2019-08-13' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N950DL-2019-08-13/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, except the copies of manufacturers’ service documents, which belong to their rights holders.