N509DC

Service difficulty reports not matched to an aircraft · 53

They name N509DC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N509DC' AND registry_match IS NULL
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR AWXA200100525Transmitter · arcedON APPROACH T/E FLAPS LOCKED OUT AT 5 UNITS, APPROACH WAS ABORTED. CREW FOLLOWED QRH CHECKLIST. ON RETURN FLAP POS INDICATOR NEEDLES MARRIED UP, CREW SELECTED FLAPS 10 & DOWN TO 30, PERFORMED NORMAL LANDING. MX PERFORMED T/E FLAP ASYMMETRY CHECK & T/E FLAP Oct 8, 2001 · N509DC · Boeing 73733A · Trailing Flap Position Indicating SystemSDR AWXA200100452Flap · malfunctionedSFO - FLAP LOCKOUT - FLT 815 - C - ON APPROACH TO SFO FLAPS 5 WAS SELECTED AND THE FLAP POSITION INDICATOR NEEDLES SPLIT AT FLAPS 1 AND THE FLAPS STOPPED AT FLAPS 1. THE AIRCRAFT LANDED AT FLAPS 1 AND UPON TOUCHDOWN THE FLAPS MOVED TO FLAPS 5 AS WAS SELECTED.Sep 18, 2001 · N509DC · Boeing 73733A · Trailing Edge Flap Control SystemSDR AWXA0002077Cylinder · faultyPHX-EMERGENCY LANDING -FLT 229- ON LANDING GEAR EXTENSION THE CREW HEARD A LOUD NOISE AND THE ACFT YAWED TO THE LEFT. ALL INDICATIONS WERE NORMAL AND ALL PRESSURE OK. AS A PRECAUTION THE CREW CALLED OUT EMERGENCY EQUIPMENT AND MADE AN UNEVENTFUL LANDING. MXAug 5, 2001 · N509DC · Boeing 73733A · Landing Gear Retraction/Extension SystemSDR AWXA0001297Skin · crackedR-1 DOOR FRAME LOWER AFT CORNER SKIN IS CRACKED; EMINATING FROM FASTENER TRAVELING TOWARD RADIUS. STOP DRILLED CRACK; FABED REPAIR DOUBLERS; DRILLED, TREATED, PRIMED, AND INSTALLED IAW B737-300 SRM 53-10-01 PG 204.Feb 8, 2001 · N509DC · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA0001296Skin · chafedRT WING O/B MID FLAP HAS A CHAFED AREA AT I/B FLAP TRACK ON LOWER SKIN. REPAIRED IAW AWA ER 03-5754-01027.Feb 8, 2001 · N509DC · Boeing 73733A · Trailing Edge FlapsSDR AWXA0001295Skin · chafedLT WING O/B MID FLAP HAS A CHAFED AREA AT I/B FLAP TRACK ON LOWER SKIN. REPAIRED IAW AWA ER 03-5754-01027.Feb 8, 2001 · N509DC · Boeing 73733A · Trailing Edge FlapsSDR AWXA0001294Doubler · crackedCRACK IN RT WING INBOARD L/E SKIN JUST ABOVE INBOARD END OF L/E FLAP SEAL DOOR. CUT OUT CRACKED AREA; HFEC PERFORMED; FABED FILLER AND INTERNAL DOUBLER; INSTALLED IAW AWA ER 03-5741-01027-SS1 AND B737-300 SRM 57-41-01.Feb 8, 2001 · N509DC · Boeing 73733A · Wing, Plate/SkinSDR AWXA0001293Floor Support · damagedSUSPECT CRACK IN LEFT W/W AT STA 664.75 BL 33 UPPER PRESSURE PANEL. HFEC PERFORMED; CUTOUT DAMAGED AREA; FABED REPAIR DOUBLER, FILLER AND STIFFENER; INSTALLED IAW AWA ER 03-5710-01025-JS1 AND B737-300 SRM 51-00-00 FIG 23, 51-10-02, 51-20-01.Feb 8, 2001 · N509DC · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001292Skin · crackedL-2 DOOR UPPER HINGE CUTOUT SKIN IS CRACKED.CUTOUT DAMAGED FUSELAGE SKIN; FABED REPAIR DOUBLER AND FILLER; DRILLED ATTACHMENT LOCATIONS; TREATED AND PRIMED REPAIR PARTS; INSTALLED REPAIR IAW B737 SRM 53-60-01 FIG 205.Feb 8, 2001 · N509DC · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA0001291Floor Support · damagedFLOOR SUPPORT END FITTING AT BS 328 HAS A HOLE DRILLED IN THE RADIUS. DRILLED HOLE TO .159 THROUGH INTERNAL DOUBLER AND EXTERNAL SKIN; COUNTERSUNK SKIN; INSTALLED RIVET IAW AWA ER 03-5310-01024-SS2.Feb 8, 2001 · N509DC · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001290Skin · dentedHORIZONTAL STABILIZER LEADING EDGE SKIN DENTED STA 258.28. REPAIRED DENT IN LEADING EDGE SKIN OF LEFT HORIZONTAL STABILIZER IAW B737-300 SRM 55-10-01 FIG 203 WITH -1 PLATE, -2 FILLER.Feb 8, 2001 · N509DC · Boeing 73733A · Horizontal Stabilizer, Plate/SkinSDR AWXA0001289Floorbeam · corrodedCORROSION ON UPPER SURFACE OF TRANSVERSE FLOORBEAM AT BS 312 RBL 3 - 9. REMOVED UPPER T-ANGLE OF TRANSVERSE FLOORBEAM; REMOVED LT SPLICE ANGLES; FABED SPLICE PLATES, FABED T-ANGLE; TREATED, PRIMED, AND INSTALLED REPAIR IAW B737-300 SRM 51-20-01, 53-10-51.Feb 8, 2001 · N509DC · Boeing 73733A · Fuselage Main, Floor BeamSDR AWXA0001288Bulkhead · crackedHFEC AND VISUAL (10X) CONFIRMS CRACK OF UNDETERMINED LENGTH UNDER STRAP AT BS 178 RBL 4 7/8 WL 199.5 TO 201.5. REMOVED STIFFENERS, RADOME ATTACH BRACKETS AND BACKUP STRIPS BS 178 WL 188 TO 218 RBL 10 TO LBL 4; LOCATED, DRILLED AND INSTALLED DOUBLER AND FILLERFeb 8, 2001 · N509DC · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001287Bulkhead · crackedULTRASONIC INSPECTION REVEALED CRACK INDICATION BS 178 BULKHEAD WEB AT RBL 1.3 TO UNDETERMINED POINT BENEATH STRAP AT WL 205.7; CONFIRMED HFEC. REMOVED LOWER L-ANGLE BS 178 WL 184 RBL 18 TO LBL 18; CUTOUT DAMAGED AREA WHERE HFEC CONFIRMED CRACK; LOCATED, DRILFeb 8, 2001 · N509DC · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001226Light · inoperativeSEAT EMERGENCY LIGHT AT SEAT 21C INOP. RESECURED LOOSE WIRE; LIGHT OPS CHECKS GOODJan 4, 2001 · N509DC · Boeing 73733A · Emergency LightingSDR AWXA9900352Apu · malfunctionedFAINT BURNING SMELL IN COCKPIT. T/S AIR CONDITIONING SYSTEM, DETERMINED TO BE APU BLEED. PLACED ON MEL 49-01, CNTL NR 121373.Oct 11, 1999 · N509DC · Boeing 73733A · APU Bleed Air SystemSDR AWXA9900026Egt Gauge · malfunctionedNR 1 ENG EGT GAUGE VERY ERRATIC. NEEDLE FOLLOWS DIGITAL INDICATION WHICH INTERMITTENTLY BLANKS. BEGAN WORKING NORMAL FOR ABOUT THE LAST 15 MIN OF APPROACH. INSPECTED WIRE HARNESS AND ENGINE, ALL OK. REMOVED AND REPLACED NR 1 ENGINE EGT GAUGE. RAN ENGINE, Jan 20, 1999 · N509DC · Boeing 73733A · Engine EGT/TIT Indicating SystemSDR AWXA9700610Frame · corrodedDURING SCHEDULED C-13 INSPECTION, FOUND CORROSION IN RT 685 FRAME UPLOCK SUPPORT SHAFT BORE UNDER BUSHINGS. LINE BORED 685 FITTING PER ER 3-32-33-05 STEP 1, 2.365 AND INSTALLED BUSHINGS AND SLEEVE PER ER 3-32-33-05. TCO-PAN-97-1977RR8110-3.Oct 1, 1997 · N509DC · Boeing 73733A · Fuselage Main, FrameSDR AWXA9700609Trunnion · corrodedDURING SCHEDULED C-13 INSPECTION, FOUND MINOR SURFACE CORROSION AT NLG RT TRUNNION BEARING BORE AT 2:30 POSITION. REMOVED ALL CORROSION FROM BORE AND BORE ID TO 3.52 AND INSTALLED SLEEVE AND BUSHINGS PER ER 3-53-12-20A. TCO-PAN-97-1972RR8110-3.Oct 1, 1997 · N509DC · Boeing 73733A · Nose/Tail Landing Gear Attach SectionSDR AWXA9700608Frame · corrodedDURING SCHEDULED C-13 INSPECTION, FOUND PITTING CORROSION AND MINOR GOUGES UPON REMOVAL OF BUSHINGS FROM LT 685 FRAME. REMOVED ALL CORROSION AND LINE BORED 685 FITTING PER ER 3-32-33-05 STEP 1 AND INSTALLED REPAIR SLEEVES AND BUSHING PER ER 3-32-33-05. TCO-PAOct 1, 1997 · N509DC · Boeing 73733A · Fuselage Main, FrameSDR AWXA9700403Actuator · leakingAIR TURNBACK APPROXIMATELY 20 MINUTES AFTER TAKEOFF, NOTICED B-SYSTEM HYDRAULIC SLOWLY MOVING DOWN PASSED HALF FULL. REMOVED AND REPLACED PLUG AND O-RING ON NR 3 SLAT ACTUATOR BODY. OPS AND LEAK CHECK GOOD.Jul 19, 1997 · N509DC · Boeing 73733A · Leading Edge Slat ActuatorSDR AWXA9600673Floor Beam · corrodedPAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM UPPER CHORD BS 312, LBL 15 - RBL 15, WL 208. FABRICATED AND REPAIRED FLOOR BEAM PER SRM 53-10-51. (M)Nov 18, 1996 · N509DC · Boeing 73733A · Fuselage Main, Floor BeamSDR AWXA9600686Galley Track · corrodedPAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON INBOARD GALLEY TRACK STATION 294.5, WL 208, RBL 16. INSTALLED FABRICATED SEAT TRACK AT BS 277-294.5, WL 208, RBL 26 PER 53-10-5. (M)Nov 14, 1996 · N509DC · Boeing 73733A · Fuselage, Seat/Cargo Attach FittingsSDR AWXA9600685Seat Track · corrodedPAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK FLANGE STATION 328, RBL 45, WL 208. INSTALLED FABRICATED SEAT TRACK AT BS 328-344, WL 208, RBL 45, PER 53-10-5. (M)Nov 14, 1996 · N509DC · Boeing 73733A · Fuselage, Seat/Cargo Attach FittingsSDR AWXA9600684Galley Track · corrodedPAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON OUTBOARD GALLEY TRACK STATION 328, RBL 55, WL 208. INSTALLED FABRICATED SEAT TRACK AT BS 328-360, RBL 55, WL 208 PER 53-10-5. (M)Nov 14, 1996 · N509DC · Boeing 73733A · Fuselage, Seat/Cargo Attach FittingsSDR AWXA9600677Skin · disbondedPAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND GRAVEL DAMAGE ON LOWER SURFACE INBOARD END, R/W INBOARD FOREFLAP. REPAIRED GRAVEL DAMAGE PER IAW SRM 51-70-10. (M)Oct 30, 1996 · N509DC · Boeing 73733A · Trailing Edge FlapsSDR AWXA9600676Skin · disbondedPAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND GRAVEL DAMAGE ON INBOARD END LOWER SURFACE OF L/W INBOARD FOREFLAP. REPAIRED GRAVEL DAMAGE PER IAW SRM 51-70-10. (M)Oct 30, 1996 · N509DC · Boeing 73733A · Trailing Edge FlapsSDR AWXA9600675Stringer · corrodedPAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND TWO AREAS OF CORROSION ON BOTH LOWER CORNERS OF THE APU INLET DOOR OPENING IN APU CAVITY. LOWER STRINGER OUT OF LIMITS. REMOVED AND REPLACED STRINGER PER IAW SRM 51-40-02 AND 52-80-14. (M)Oct 30, 1996 · N509DC · Boeing 73733A · Fuselage Main, Longeron/StringerSDR AWXA9600674Floor Beam · corrodedPAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM STATION 328, RBL 24-55, WL 208. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-51. (M)Oct 28, 1996 · N509DC · Boeing 73733A · Fuselage Main, Floor BeamSDR AWXA9600672Seat Track · corrodedPAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION IN SEAT TRACK WELL, STATION 498 TO 500 AND 500 A PLUS 10 INCH, LBL 45, WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 480-520, LBL 45, WL 208 PER SRM 53-00-52. (M)Oct 25, 1996 · N509DC · Boeing 73733A · Fuselage, Seat/Cargo Attach FittingsSDR AWXA9600671Floor Beam · corrodedPAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM STATION 294.5, LBL 12 TO RBL 12, WL 208. FABRICATED REPAIR AND INSTALLED PER IAW SRM 53-10-51. (M)Oct 25, 1996 · N509DC · Boeing 73733A · Fuselage Main, Floor BeamSDR AWXA960477Wire · brokenPHX - FLT 0543 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE AT ROW 16. REPAIRED BROKEN WIRE. OSP CHECK GOOD. (X)Jul 8, 1996 · N509DC · Boeing 73733A · Light System WiringSDR AWXA9500835Skin · dentedPHX/SNA - FLT 0661 - DENT FOUND IN LT HORIZONTAL STABILIZER 8 FEET INBOARD OF TIP. PERFORMED INTERIM REPAIR PER SRM 55-10-01. (X)Dec 30, 1995 · N509DC · Boeing 73733A · Horizontal Stabilizer, Plate/SkinSDR AWXA9500812Wire · brokenPHX - FLT NR 0202 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT OUT AT ROW 4. BROKEN WIRE, REPINNED, OPS CHECK GOOD. (M)Dec 13, 1995 · N509DC · Boeing 73733A · Light System WiringSDR AWXA9500785Fuse · failedPHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE, FROM ROW 3ABC THROUGH ROW 6ABC. REMOVED AND REPLACED FUSE IN BATTERY CHARGER ASSEMBLY, OPS CHECK GOOD. (M)Nov 22, 1995 · N509DC · Boeing 73733A · Emergency LightingSDR AWXA9500784Fuse · failedPHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE, FROM ROW 3 THROUGH ROW 6. REMOVED AND REPLACED FUSE AT FORWARD OVERHEAD BATTERY PACK, OPS CHECK GOOD. (M)Nov 20, 1995 · N509DC · Boeing 73733A · Emergency LightingSDR AWXA9500709Bracket · crackedPHX - DURING SCHEDULED C11 INSPECTION, FOUND SUPPORT BRACKET CRACKED UNDER NOSE GEAR VIEWING WINDOW PANEL. FABRICATED AND INSTALLED NEW ANGLE BRACKET AND DOUBLER PER SRM 51-10-25. (M)Oct 10, 1995 · N509DC · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA9500708Threshold · corrodedPHX - DURING SCHEDULED C11 INSPECTION, FOUND R2 DOOR THRESHOLD CHORD NUT PLATE HOLE CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 51-70-11. (M)Oct 10, 1995 · N509DC · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA9500707Threshold · corrodedPHX - DURING SCHEDULED C11 INSPECTION, FOUND L2 DOOR THRESHOLD CHORD NUT PLATE HOLE CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 51-70-11. (M)Oct 10, 1995 · N509DC · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA9500706Skin · crackedPHX - DURING SCHEDULED C11 INSPECTION, FOUND FORWARD GALLEY DOOR OUTER SKIN CUTOUT FOR UPPER HINGE CRACKED IN LOWER AFT RADIUS CORNER. FABRICATED AND INSTALLED DOUBLER REPAIR PER ER 3-52-48-04A. (M)Oct 10, 1995 · N509DC · Boeing 73733A · Cargo/Baggage DoorsSDR AWXA9500705Skin · crackedPHX - DUIRNG SCHEDULED C11 INSPECTION, FOUND FORWARD CARGO DOOR OUTER SKIN CRACKED AT DOOR HANDLE FLAPPER DOOR CUTOUT. REPAIRED PER ER 1-52-30-01B. (M)Oct 10, 1995 · N509DC · Boeing 73733A · Cargo/Baggage DoorsSDR AWXA9500704Floor Beam · corrodedPHX - DURING SCHEDULED C11 INSPECTION, FOUND FLOOR BEAM CORRODED AT NUT PLATE HOLES, STATION 986.5 RBL 23.5 TO RBL 40. (M)Oct 10, 1995 · N509DC · Boeing 73733A · Fuselage Main, Floor BeamSDR AWXA9500703Keel Beam · crackedPHX - DURING SCHEDULED C11 INSPECTION, FOUND TWO CRACKS IN KEEL BEAM SKIN BETWEEN WHEEL WELL. REPAIRED CRACKS PER SRM 53-60-12, FIGURE 202. (M)Oct 10, 1995 · N509DC · Boeing 73733A · Fuselage Main, KeelSDR AWXA9500524Eel Connector · loosePHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 18 THROUGH ROW 22. RESECURED LIGHT CONNECTOR AT ROW 18, OPS CHECK OK. (W)Aug 11, 1995 · N509DC · Boeing 73733A · Emergency LightingSDR AWXA9500515Engine · overtempCOS - DURING CLIMB, CREW REPORTED BOTH ENGINES EXCEEDED ALLOWABLE EGT LIMITS, E1 GOING TO 980 DEGREES AND E2 TO 960 DEGREES. CREW CONTINUED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED BOTH ENGINES. (M)Aug 8, 1995 · N509DC · Boeing 73733A · Engine (Turbine/Turboprop)SDR 95ZZZM366Engine · overtempCOS - DURING CLIMB, CREW REPORTED BOTH ENGINES EXCEEDED ALLOWABLE EGT LIMITS, E1 GOING TO 980 DEGREES AND E2 TO 960 DEGREES. CREW CONTINUED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED BOTH ENGINES. (M)Aug 8, 1995 · N509DC · Boeing 73733A · Engine (Turbine/Turboprop)SDR AWXA9500490Eel Connector · loosePHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATAIVE IN CABIN. RECONNECTED LOOSE CONNECTOR AT ROW 14, OPS CHECK GOOD. (M)Aug 1, 1995 · N509DC · Boeing 73733A · Emergency LightingSDR AWXA9500486Eel Wire · inoperativePHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE ROW 14 THROUGH ROW 18. REPAIRED WIRING, OPS CHECK GOOD. (M)Jul 31, 1995 · N509DC · Boeing 73733A · Emergency LightingSDR AWXA9500425Eel Lamp · inoperativePHX - DURING ROUTINE MAINTENANCE CHK, FOUND AFT, 4 EACH, FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BROKEN WIRE AND RELAMPED 2 ASSEMBLIES, OPS CHECK GOOD. (X)Jul 6, 1995 · N509DC · Boeing 73733A · Emergency LightingSDR AWXA9500259Eel Wire · brokenPHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY LIGHTS INOPERATIVE AT ROWS 18 THROUGH 20. CRIMPED NEW CONNECTOR ON BROKEN WIRE, OPS CHECK GOOD. (W)May 3, 1995 · N509DC · Boeing 73733A · Emergency Lighting
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