N588US, cancelled Feb 27, 2012

Service difficulty reports · 109

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 = 'N588US' AND deregistration_id = 'N588US-2012-02-27'
  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 USAA920080554Skin · crackedCLT - MAJOR REPAIR -RON - CRACKED FUSELAGE SKIN, BS 930 - BS 932, S25R. REPAIRED FUSELAGE SKIN, BS 930 - BS 932, S25R IAW B737 SRM 53-00-01 REPAIR 31.Mar 3, 2008 · N588US · Boeing 737301 · Fuselage Main, Plate/SkinSDR SB07037Coalescer Bag · dirtyBWI FLT 1853 - ON TAKEOFF FROM PHL, EN ROUTE TO BWI, CREW REPORTED A NAUSEATING SMELL IN THE COCKPIT FROM THE AIR CONDITIONING SYSTEM. SMELL REMAINED DURING FLIGHT AND LANDING. MAINTENANCE OPERATED EACH PACK FOR 30 MINUTES AND DETECTED A STALE ODOR FROM THE May 7, 2007 · N588US · Boeing 737301 · Humidity Control SystemSDR USAA070168Door Frame · crackedFWD FRAME OF FWD CARGO DOOR CUTOUT STA 440 RT NR 2 STOP HAS CRACK. CUT OUT DAMAGE, FAB'D DOUBLER & INSTALLED PER EA 98509, DEFECT SIZE: 1 INCH.Feb 28, 2007 · N588US · Boeing 7373B7 · Fuselage Main, StructureSDR USAA070169Door Frame · crackedAFT FRAME OF FWD CARGO DOOR CUTOUT STA 492.4, RT S-24R HAS CRACK. CUT OUT DAMAGE, FAB'D DOUBLER, INSTALLED REPAIR PER EA 98508, DEFECT SIZE: 0.125 INCH.Feb 28, 2007 · N588US · Boeing 7373B7 · Fuselage Main, StructureSDR SB06126Circuit Breaker · failedPBI FLT1286 ON CLIMBOUT FROM PBI, AT 1,300 FEET AGL, THE CAPTAIN REPORTED LOST ALL OF HIS PRIMARY FLIGHT INSTRUMENTS. CONTROL OF AIRCRAFT WAS GIVEN TO THE FIRST OFFICER, WHEREAS, HIS INSTRUMENTS FUNCTIONED PROPERLY. FLIGHT RETURNED TO FIELD AT PBI AND LANDEDDec 27, 2006 · N588US · Boeing 737301 · AC Power Distribution SystemSDR USAASB06106Transmission · failedPVD - FLT 1110 ON APPROACH TO PVD FROM DCA, CREW REPORTED THE TRAILING EDGE FLAPS WOULD NOT EXTEND FOR LANDING NORMALLY OR ALTERNATE. LEADING EDGE FLAPS DID EXTEND FULLY WITH ALTERNATE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACOct 24, 2006 · N588US · Boeing 737301 · Trailing Edge Flap Control SystemSDR USAA060881Skin · crackedBS 727E + 6 JUST ABOVE S-25R CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLERS IAW SRM 53-00-01 REPAIR 31, DEFECT SIZE: 3 INCHES.Jul 6, 2006 · N588US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA060874Skin · crackedBS 727E + 6 JUST ABOVE S-25R CRACKED. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-00-01 REPAIR 31, DEFECT SIZE: 3 INCHES.Jun 29, 2006 · N588US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR SB06031Battery Pack · dischargedMAINTENANCE REPORTED THE FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.Mar 24, 2006 · N588US · Boeing 737301 · Emergency LightingSDR SB05167Slide · reads lowPIT - THE FORWARD LEFT SLIDE ASSEMBLY PRESSURE VESSEL WAS FOUND TO BE BELOW LIMITS. MAINTENANCE REPLACED THE LEFT FORWARD SLIDE ASSEMBLY. OK FOR SERVICE.Dec 12, 2005 · N588US · Boeing 737301 · Escape SlideSDR USAA051063Skin · chafedLOCATION: BS 869- BS 887 ACTION: REMOVED DAMAGE, INSTALLED TRIPLER IAW EA 96764 DEFECT SIZE: APPX 18 INCH AREA OF CHAFING ON SKIN BELOW DORSAL FIN TIP CONTACT AREA, BOTH SIDESAug 30, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA051062Keelbeam · corrodedSTA 520 S-28/KEEL BEAM. REMOVED DAMAGED, INSTALL FILLERS, SHIMS AND REPAIR ANGLE IAW EA 96839, DEFECT SIZE: 1 X 3.Aug 29, 2005 · N588US · Boeing 7373B7 · Fuselage Main, KeelSDR USAA051054Skin · crackedCLT - FOUND SKIN CRACKED 12 INCHES, IMMEDIATELY AFT OF SLAT ACTUATOR. REMOVED DAMAGE AND INSTALLED SPACER AND DOUBLER IAW SRM 57-43-01. (M)Aug 24, 2005 · N588US · Boeing 7373B7 · Wing, Plate/SkinSDR USAA051053Wedge · dentedCLT - FOUND WEDGE WITH DENT 4 INCH BY 5 INCH, BOTTOM OF THE WEDGE AT THE OUTBOARD TRAILING EDGE. REMOVED DAMAGE, INSTALLED A NEW CORE AND DOUBLER IAW EA 96745. (M)Aug 24, 2005 · N588US · Boeing 7373B7 · Trailing Edge FlapsSDR USAA051041Bushing · corrodedVERTICAL FIN AFT JUGS RT BUSINGS AFT FACES CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED BUSHINGS IAW BOEING DWG 69-72039, 65-55274, DEFECT SIZE: 1 X 2 INCH TYPICAL.Aug 23, 2005 · N588US · Boeing 737301 · Vertical StabilizerSDR USAA051046Threshold · crackedAFT CARGO DOOR MOST FWD THRESHOLD HAS CRACK. WELDED CRACK IAW BOEING PROCESS SPEC BAC 5975, DEFECT SIZE: .75 INCH.Aug 23, 2005 · N588US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA051045Strip · wornAFT CARGO CAP STRIP BETWEEN SCUFF PLATE AND ACF-3 DAMAGED. REMOVED DAMAGED STRIP, FABRICATED & INSTALLED NEW STRIP IAW BOEING DWG 65-49613 DEFECT SIZE: 3 X 2 INCH WORN AREA.Aug 23, 2005 · N588US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA051044Fitting · corrodedO/B ATTACH HOLE IN RT AFT DRAG BRACE ATTACH FITTING OFR VERTICAL FIN CORRODED. REMOVED CORROSION, FABRICATED BUSHING AND INSTALLED IAW EA 96816, DEFECT SIZE: 1 X 2 INCH TYPICAL.Aug 23, 2005 · N588US · Boeing 737301 · Vertical StabilizerSDR USAA051042Bushing · corrodedVERTICAL FIN, AFT MOUNT LUGS LT SIDE BUSHINGS, FWD FACE CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED BUSHINGS IAW BOEING DWGS 69-72039 & 65-52274 DEFECT SIZE: 1 X 2 INCH AREA.Aug 23, 2005 · N588US · Boeing 737301 · Vertical StabilizerSDR USAA051033Web · crackedSTA 699 INSIDE KEEL BEAM STRUT LOWER RT CORNER OF LIGHTENING HOLE IN BULKHEAD. REMOVED DAMAGE, INSTALLED DOUBLER IAW EA 69760 DEFECT SIZE: LOWER RT CORNER OF LIGHTENING HOLE CRACKED .500 INCH.Aug 23, 2005 · N588US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA051040Bushing · corrodedVERTICAL FIN AFT ATTACH LUGS RT SIDE FWD FACES. REMOVED CORROSION MACHINED & INSTALLED BUSHINGS IAW BOEING DWG 69-72039, 65-52274 DEFECT SIZE: 1 X 2 INCHES TYPICAL.Aug 23, 2005 · N588US · Boeing 737301 · Vertical StabilizerSDR USAA051039Angle · crackedLEFT PACK BAY, AFT RIGHT CORNER CRACKED. FABRICATED ATTACH ANGLE SRM 51-10-02 BOEING DWG 66-24798, DEFECT SIZE: 1 INCH.Aug 23, 2005 · N588US · Boeing 737301 · Fuselage Main, Attach FittingsSDR USAA051037Attach Fitting · corrodedRIGHT AFT O/B VERTICAL FIN ATTACH LUG ON FUSELAGE. MACHINED AFT CHAMFER AND BOR TO CLEAN UP CORROSION & INSTALL NEW BUSHING IAW EA 96788, DEFECT SIZE .080 INCH DEEP.Aug 23, 2005 · N588US · Boeing 737301 · Vertical StabilizerSDR USAA051036Seat Track · crackedBS 662-670, RBL 24 CRACKED. STOP DRILLED CRACKS, INSTALLED REPAIR DOUBLER/CHANNELS IAW EA 96799, DEFECT SIZE: .250 X 2 INCH.Aug 23, 2005 · N588US · Boeing 737301 · Fuselage, Seat/Cargo Attach FittingsSDR USAA051035Seat Track · crackedSEAT TRACK VERTICAL LEG HAS 0250 INCH CRACK AT CUTOUTS FOR FASTENERS. STOP DRILL CRACKS, INSTALL REPAIR ANGLES IAW EA 96799, DEFECT SIZE: 0250 INCH, CRACKED AT CUTOUTS FOR FASTENERS.Aug 23, 2005 · N588US · Boeing 737301 · Fuselage, Seat/Cargo Attach FittingsSDR USAA051034Keelbeam · wornKEEL BEAM LEFT OUTBOARD FLANGE STA 664 TO 727 DAMAGED. REMOVED DAMAGE, FAB & INSTALLED FILLER PLUGS, REPAIR STRAP AND APPROP SHIMS INCLUDED IAW EA 96777, DEFECT SIZE: 60 INCHES OF SURFACE WEAR AT FAIRING ATTACH HOLES AND STRAP.Aug 23, 2005 · N588US · Boeing 737301 · Fuselage Main, KeelSDR USAA051043Bushing · corrodedVERTICAL FIN LT MOUNT LUGS, AFT FACE CORRODED. REMOVED CORROSION, FABRICATED & INSTALLED BUSHINGS IAW BOEING DWGS 69-72039 & 65-52274 DEFECT SIZE: 1 X 2 INCH AREA.Aug 23, 2005 · N588US · Boeing 737301 · Vertical StabilizerSDR USAA051030Skin · damagedCLT - Q6 - PYLON SKIN, 1.3 INCH, GROOVE IB SIDE OF NR 2 ENGINE PYLON AT WING L/E JUNCTION. REPAIRED IAW TYPICAL REPAIR IAW TR. (K)Aug 19, 2005 · N588US · Boeing 7373B7 · Nacelle/Pylon, Plate/SkinSDR USAA051011Keelbeam · wornCLT - FOUND CHORD WITH 60 INCHES OF WEAR, KEEL BEAM LEFT OUTBOARD FLANGE STATION 664-727. REMOVED DAMAGED AREAS, FABRICATED AND INSTALLED FILLER PLUGS IAW EA 96777.Aug 17, 2005 · N588US · Boeing 7373B7 · Fuselage Main, KeelSDR USAA051010Support Beam · corrodedCLT - Q6 - LT MLG SUPPORT BEAM OB LUG FACE AND HEAVY WEAR/ MATERIAL LOSS ON IB LUG FACE 2 INCH X 2 INCH TYPICAL. LT MLG SUPPORT BEAM; STABILIZER BEAM FITTING ASSY. CLEANED AND TREATED CORROSION, INSTALLED BUSHINGS IAW SRM. (K)Aug 16, 2005 · N588US · Boeing 7373B7 · Fuselage, Landing Gear Attach FittingsSDR USAA051009Keelbeam · corrodedCLT - Q6 - ANGLE, ON KEELBEAM COMPOSITE SKIN ATTACH ANGLE HAS FRETTING WORN INTO IT, 5 INCHES X 1 INCH. CORROSION, STA 673, STA 678, LBL 8. REMOVED CORROSION, BLENDED, AND TREATED IAW SRM, DWG. (K)Aug 16, 2005 · N588US · Boeing 7373B7 · Fuselage Main, KeelSDR USAA051008Angle · corrodedCLT - Q6 - ANGLE, KEEL BEAM HAS FRETTING WEAR ON IT 17 IN X 1 INCH, CORRODED, STA 727-710, LBL 8. REMOVED SURF CORROSION, BLENDED AND TREATED IAW SRM, DWG. (K)Aug 16, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA051000Channel · corrodedCLT - FOUND HAT SECTION CHANNEL CORRODED 6 INCH AREA, STATION 500-500A, BL 0. REMOVED DAMAGED HAT SECTION, REMOVED LIGHT SURFACE CORROSION INSTALLED NEW HAT SECTION CHANNEL. (M)Aug 15, 2005 · N588US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051001Shear Tie · corrodedCLT - FOUND SHEAR TIE CORRODED .5 INCH BY 2 INCH, RBL 3, BETWEEN BS 727A AND 727B FRAMES AFT CARGO AREA. CORROSION LEVEL 1. DEFECTIVE PART REPLACED WITH IDENTICAL PART, IAW BOEING DWG 69-40710 AND SRM 51-10-02. (M)Aug 15, 2005 · N588US · Boeing 7373B7 · Fuselage Internal Mounting StructureSDR USAA051002Stringer · crackedCLT - FOUND STRINGER .5 INCH CRACK, FUSELAGE STATION 500A STRINGER 8L. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-00-03 FIG 203. (M)Aug 15, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA051006Skin · crackedCLT - Q6 - SKIN, 1.50 INCH CRACK. 1.25 INCH FWD OF REAR SPAR, SPAR STA 124 TO 55-123.6. HORIZONTAL STABILIZER. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER IAW EA. (K)Aug 15, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Plate/SkinSDR USAA051005Skin · crackedCLT - Q6 - LOWER SKIN, 1.7 INCH CRACK LOWER SKIN APPROX STAB STA 129 AT AFT SPAR, HORIZONTAL STAB. REPAIRED AND INSTALLED DOUBLER AND FILLER IAW EA. (K)Aug 15, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Plate/SkinSDR USAA050990Support · crackedCLT, Q6, PSU SUPPORT RAIL, 2 CRACKS, .1250 INCH, .1875 INCH, CRACK, BS 727D BETWEEN S8L AND 9L. DAMAGE REMOVED, INSTALLED REPAIR ANGLES IAW SRM. (K)Aug 8, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA050991Stringer Splice · crackedCLT, Q6, SPLICE CRACKED AT STA 907, S4R. REMOVED AND REPLACED STRINGER SPLICE IAW SRM. (K)Aug 8, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA050992Frame · crackedCLT, Q6 FRAME, 1.4 INCH CRACK, BS 616 RT BOTTOM OF FRAME INNER CHORD BS 616 RT. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER IAW TR 53-62-01. (K)Aug 8, 2005 · N588US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA050993Frame · crackedCLT, Q6, FRAME .125 INCH CRACK, STRINGER 9 LT STA 500A. REPAIRED IAW TR 53-10-20B. (K)Aug 8, 2005 · N588US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA050984Beam · crackedCLT - Q6 - BEAM, 3 INCH CRACK, STRINGER 8R, STA 500. ACCOMPLISHED SPLICE REPAIR. (K)Aug 5, 2005 · N588US · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050973Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, STRINGER 8R AT STATION 500. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 53-00-03. (M)Aug 4, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA050972Crease Beam · crackedCLT - FOUND CREASE BEAM CRACKED .75 INCH, BS 576, S17R. REPLACED WITH FACTORY NEW PART IAW SRM 51-10-02. (M)Aug 4, 2005 · N588US · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050968Clevis · corrodedCLT - FOUND ATTACH CLEVIS CORRODED 2 INCHES DIAMETER BY .015 TYPICAL, RIGHT HORIZ STAB FORWARD SPAR ATTACH CLEVIS AFT FACE. REMOVED CORROSION AND BUSHED IAW 55-10-10. (M)Aug 4, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050969Attach Fitting · corrodedCLT - FOUND STAB LUG CORRODED, R1 LUG AFT FACE RIGHT HORIZONTAL STABILIZER. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050967Attach Angle · wornCLT - FOUND ATTACH ANGLE CRACKED 1 INCH DIAMETER, WORN AREAS, RT WHEEL WELL STATION 727 RBL 14 BOTTOM OF BULKHEAD. REMOVED DAMAGED ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW BOEING DWG 65-48689 AND SRM 51-10-02 AND 51-40-02. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA050966Web · crackedCLT - FOUND WEB CRACKED 2 INCHES, AFT CARGO DOOR CUTOUT FRAME, LOWER WEB. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED NEW WEB IAW BOEING DWG 65-20723 AND SRM 51-10-02. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050965Angle · corrodedCLT - FOUND C-ANGLE CORRODED 2 INCHES, UPPER SURFACE OF FORWARD ENTRY DOOR THRESHOLD C-ANGLE. REMOVED DAMAGED ANGLE AND REINSTALLED NEW ANGLE IAW SRM 53-10-15. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050964Floorbeam · corrodedCLT - FOUND BEAM CORRODED 28 INCHES, T-CAP OF FLOORBEAM STATION 312, LBL 2, RBL 26. REMOVED PREVIOUS T-CAP AND REPLACED WITH NEW CAP EXTENDING SPLICES PER SRM IAW SRM 53-10-51. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Floor Beam
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