N586US, cancelled Aug 13, 2007

Service difficulty reports · 98

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N586US' AND deregistration_id = 'N586US-2007-08-13'
  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 2007FA0000135Frame · crackedFRAME IS CRACKED AT BODY STATION 727, STRINGER 14L. (K)Sep 27, 2006 · N586US · Boeing 737301 · Fuselage Main, FrameSDR 2007FA0000128Skin · dentedBODY STATION 915 ABOVE STRINGER 25L LAP JOINT FUSELAGE SKIN HAS DENT. (K)Sep 27, 2006 · N586US · Boeing 737301 · Fuselage Main, Plate/SkinSDR 2007FA0000126Frame · crackedFRAME IS CRACKED AT BODY STAION 727, STRINGER 14L. (K)Sep 27, 2006 · N586US · Boeing 737301 · Fuselage Main, FrameSDR 2007FA0000125Frame · crackedUPPER FUSELAGE, BS 500A, BETWEEN STR 8R AND STR 9R, FRAME IS CRACKED AT PSU MOUNT. (K)Sep 26, 2006 · N586US · Boeing 737301 · Fuselage Main, FrameSDR 2007FA0000124Skin · gougedUPPER FUSELAGE, STA 860 THRU 885, LBL 8 THRU RBL 8, UNDER DORSAL FIN BLADE SEAL, SKIN IS GOUGED. (K)Sep 26, 2006 · N586US · Boeing 737301 · Fuselage Main, Plate/SkinSDR 2007FA0000136Fitting · corrodedDOOR 1R, BS 306-312, WL 248-249, LBL 57-63, SERPENTINE PLATE CASTING CORRODED AROUND FASTENER HOLES. (K)Sep 24, 2006 · N586US · Boeing 737301 · Fuselage Miscellaneous StructureSDR 2007FA0000134Pressure Panel · crackedMID CABIN BS 663, LBL 31, WHEEL WELL PRESSURE DECK WEB, CRACKED. (K)Sep 24, 2006 · N586US · Boeing 737301 · Fuselage Main, BulkheadSDR 2007FA0000133Frame · crackedCABIN, BS 787, FRAME AT STR 8R, CRACKED AT STOW BIN ATTACH BRACKET. (K)Sep 24, 2006 · N586US · Boeing 737301 · Fuselage Main, FrameSDR 2007FA0000129Floorbeam · gougedCABIN FLOORBEAM, STA 827, WL 203.6, RBL 10, LOWER T-CAP, AFT FLANGE, GOUGED. (K)Sep 24, 2006 · N586US · Boeing 737301 · Fuselage Main, Floor BeamSDR 2007FA0000140Support · crackedAT FWD CABIN STA 328+6, DOOR 2R AFT STOP FTG INTERCOSTAL TEE SUPPORT, CRACKED. (K)Sep 18, 2006 · N586US · Boeing 737300 · Passenger/Crew DoorsSDR 2007FA0000139Frame · crackedMID CABIN, STATION 500A FRAME, BETWEEN STRINGER 8 AND 9L, CRACKED AT PSU MOUNT RAIL ATTACH POINT. (K)Sep 18, 2006 · N586US · Boeing 737300 · Fuselage Main, FrameSDR 2007FA0000138Frame · crackedMID CABIN, STATION 480 FRAME, AT STRINGER 8L, CRACKED AT PSU MOUNT RAIL ATTACH POINT. (K)Sep 18, 2006 · N586US · Boeing 737300 · Fuselage Main, FrameSDR 2007FA0000137Stringer Clip · crackedPASSENGER CABIN, STATION 639 AT STRINGER 4L, STRINGER CLIP, CRACKED. (K)Sep 18, 2006 · N586US · Boeing 737300 · Fuselage Main, Attach FittingsSDR 2007FA0000131Crease Beam · corrodedAFT GALLEY DOOR CREASE BEAM INNER CHORD ANGLE, BS 947 TO 992, STRINGER 17R, WL 208, CORROSION OUT OF LIMITS. (K)Sep 18, 2006 · N586US · Boeing 737300 · Fuselage Main, StructureSDR 2007FA0000130Frame · crackedMID CABIN, STATION 400 FRAME AT STRINGER 8R, CRACKED AT PSU RAIL OUNT ATTACH POINT. (K)Sep 18, 2006 · N586US · Boeing 737300 · Fuselage Main, FrameSDR 2007FA0000127Frame · crackedMID CABIN, STA 500A FRAME, BETWEEN STRINGER 8 AND 9L, CRACKED AT PSU MOUNT RAIL ATTACH POINT. (K)Sep 18, 2006 · N586US · Boeing 737301 · Fuselage Main, FrameSDR 2007FA0000123Intercostal · crackedCABIN STA 303.9 JUST ABOVE STRINGER 10L. INTERCOSTAL OUTER CHORD ANGLE, CRACKED. (K)Sep 18, 2006 · N586US · Boeing 737300 · Fuselage Miscellaneous StructureSDR 2007FA0000132Floorbeam · corrodedCABIN BS 312, FROM LBL 55 TO RBL 55 WL 208, FLOORBEAM HAS LIGHT CORROSION. (K)Aug 17, 2006 · N586US · Boeing 737301 · Fuselage Main, Floor BeamSDR SB05061Wire · brokenMAINTENANCE REPORTED THE EMERGENCY LIGHT ON SEAT 5A INOPERATIVE. MAINTENANCE REPAIRED WIRE ON LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.May 14, 2005 · N586US · Boeing 737301 · Light System WiringSDR SB05034Switch · faultySYR - MAINTENANCE REPORTED THAT WHEN THE BATTERY IS SELECTED OFF, THE EMERGENCY EXIT LIGHTS ILLUMINATE AND WILL NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH. OPERATIONAL CHECK GOOD.Mar 2, 2005 · N586US · Boeing 737301 · Emergency LightingSDR USAA040685Skin · crackedCLT - FOUND SKIN CRACKED 1 NCH, STATION 943 STRINGER 24L. INSTALLED DOUBLER IAW EA 95872A. (M)Sep 29, 2004 · N586US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA040364Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH LONG, FS 727D AND STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)Jul 20, 2004 · N586US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB04081Battery Pack · inoperativePIT - FOUND DURING WEEKLY CHECK, MAINTENANCE FOUND THE INTERIOR EMERGENCY LIGHTS AT SEAT ROWS 12 THROUGH 16 AND THE EXTERIOR LIGHTS AT RIGHT OVERWING EXIT AND LEFT AFT FUSELAGE, EXTINGUISH AFTER 10 SECONDS OF OPERATION. MAINTENANCE REMOVED AND REPLACED THE BAJun 27, 2004 · N586US · Boeing 737301 · Emergency LightingSDR USAA030322Skin · crackedCLT - FOUND SKIN CRACKED 2.250 INCH, 4 INCHES FORWARD OF FS 727E .500 INCH ABOVE S-24R ON SKIN. INSTALLED DOUBLER 24 INCHES BY 30 INCHES PER SRM 53-00-01 FIG 229. (M)Dec 28, 2003 · N586US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB03120Control Valve · failedON SLOW DESCENT TO PHL, FROM FL370 TO FL350, THE NR 1 ENGINE BLEED TRIPPED FOLLOWED BY A PACK TRIP. FLIGHT DESCENDED TO 10,000 FEET AND CONTINUED TO PHL UNPRESSURIZED. BLEED RESET AFTER COOLING PERIOD PER QUICK REF HANDBOOK PROCEDURES. FLIGHT LANDED WITHOUTJul 23, 2003 · N586US · Boeing 737301 · Pneumatic Distribution SystemSDR USAA030092Structure · damagedPIT - BEARING BORE REPAIR, SINGLE LUGE MOUNT BEARING BORE OF CROSSBEAM. INSTALLED OVERSIZED BEARING. (M)Jun 6, 2003 · N586US · Boeing 737301 · Nacelle/Pylon Miscellaneous StructureSDR USAASB03022Actuator · malfunctionedPIT - FLT 865 - DURING APPROACH, CREW REPORTED THE NR 5 LEADING EDGE SLAT INTRANSIT LIGHT ILLUMINATED WHEN FLAPS/SLATS WERE SET TO 5 UNITS. CREW NOTED AIRCRAFT WANTED TO ROLL RT DURING FLAP/SLAT SET. NR 5 LEADING EDGE SLAT DID NOT RETRACT UNTIL APPROXIMATELY Feb 9, 2003 · N586US · Boeing 737301 · Leading Edge Slat ActuatorSDR USAASB02057Pump · failedCLT - FLT 9228 - DURING CLIMB-OUT FROM TPA, EN ROUTE TO CLT, CAPTAIN REPORTED THE HYDRAULIC MASTER CAUTION ILGHTS ILLUMINATING INTERMITTENTLY. CAPTAIN OBSERVED 'A' SYSTEM HYDRAULIC QUANTITY AT REFILL. A SHORT TIEM LATER, 'A' SYSTEM HYDRAULIC PRESSURE FLUCTUAMar 19, 2002 · N586US · Boeing 737301 · Hydraulic Pump (Electric/Engine), MainSDR USAASB01307Battery Pack · dischargedCLT - MAINTENANCE FOUND THREE SECTIONS OF CABIN EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THREE CABIN EMERGENCY LIGHT BATTERY PACKS. OPS CHECK OF EMERGENCY LIGHTS GOOD. (M)Nov 5, 2001 · N586US · Boeing 737301 · Emergency LightingSDR USAA010704Bellcrank · brokenPIT - FOUND BELLCRANK HAD .75 INCH SECTION BROKEN OUT, RT INBOARD AILERON HINGE ASSY. NOTCHED OUT TOP OF FITTING, REMOVED LOWER FLANGE, INSTALLED TWO MACHINED DOUBLERS PER EA 71077. (M)May 18, 2001 · N586US · Boeing 737301 · Aileron Control SystemSDR USAA010733Web · crackedPIT - FOUND ANGLE WEB CRACKED 1 INCH, UNDER AFT SERVICED DOOR SILL PLATE. MANUFACTURED AND INSTALLED NEW WEB PER BOEING DRAWING 65.45855. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA010734Skin · crackedPIT - FOUND PYLON SKIN CRACKED 1 INCH, UPPER RIGHT CORNER OF PANEL 5724L OPENING. STOP DRILLED CRACK, INSTALLED DOUBLER PER TYPICAL REPAIR 54-50-07. (M)May 17, 2001 · N586US · Boeing 737301 · Nacelle/Pylon, Plate/SkinSDR USAA010735Skin · crackedPIT - FOUND SKIN CRACKED .25 INCH, BS 947 AT STRINGER 11R. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-60-01. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010736Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, BS 663 AT S2L. CUT OUT DAMAGE, INSTALLED DOUBLER PER SRM 53-00-07 FIG 208, SRM 51-70-13, SRM 53-60-08, SRM 53-60-08. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010737Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, BS 747 AT S8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010738Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, BS 440 AT S8L. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010739Clip · crackedPIT - FOUND CLIP CRACKED .25 INCH, BS 360 AT S13L. FABRICATED, HEAT TREATED AND INSTALLED PER SRM 53-00-07 FIG 205. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010740Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, BS 440 AT STRINGER 8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010710Bulkhead · crackedPIT - FOUND BULKHEAD CRACKED .125 INCH, STATION 178 BETWEEN LBL 5.7 AND 17. REPAIRED DOUBLER, FILLER PER SRM 53-10-08 PAGES 265-269. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Main, StructureSDR USAA010728Skin · crackedPIT - FOUND SKIN CRACKED .095 INCH, LOWER HINGE CUTOUT. ROUTED OUT CRACK AND INSTALLED DOUBLER PER SRM 52-10-01 S/B 737-52-1096. (M)May 17, 2001 · N586US · Boeing 737301 · DoorsSDR USAA010708Web · crackedPIT - FOUND WEB CRACKED .75 INCH, STATION 178 BULKHEAD WL 184. REPAIRED FILLERS, DOUBLERS AND SHIMS PER SRM 53-10-08 FIG 211. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010711Web · crackedPIT - FOUND WEB CRACKED 5 INCHES, STATION 178 BULKHEAD RIGHT FLOOR WEB AT WL 207. REMOVED AND REPLACED FLOORWEB. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010712Angle · crackedPIT - FOUND ANGLE CRACKED .125 INCH, STATION 178 BULKHEAD RIGHT CHORD ANGLE AT WL 207. REPAIRED DOUBLER, CHORD, CLIPS, SPLICE ANGLE PER SRM 53-10-08. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010713Angle · crackedPIT - FOUND ANGLE CRACKED .125 INCH, STATION 178 BULKHEAD LEFT CHORD ANGLE AT WL 207. REPAIRED FILLER, DOUBLER AND SHIMS PER SRM 53-10-08 FIG 211. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010714Web · crackedPIT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD LBL 5.7 WL 200, LOWER ANTENNA MOUNT. REPAIRED FILLER, DOUBLER AND SHIMS PER SRM 53-10-08 FIG 211. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Main, StructureSDR USAA010715Web · crackedPIT - FOUND WEB CRACKED .25 INCHES IN LENGTH, STATION 178 BULKHEAD LBL 5.7 WL 210 UPPER ANTENNA MOUNT. REPAIRED FILLER, DOUBLER AND SHIMS PER SRM 53-10-08 FIG 211. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010716Clip · crackedPIT - FOUND CLIP CRACKED .25 INCH, BS 639 AT S11L. MANUFACTURED, HEAT TREATED, INSTALLED CLIP PER BOEING PRINT 66-2411241-1. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010718Frame · crackedPIT - FOUND FRAME CRACKED 1 INCH, BS 787 BETWEEN 58L AND 59L. INSTALLED DOUBLER PER T/R 53-10-14. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Main, StructureSDR USAA010723Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, BS 480 AT STRINGER 8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14 AND EA 70650. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010724Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, BS 500C AT STRINGER 8R. ROUTED OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14 AND EA 70647. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)
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