JASC 1430

Service difficulty reports · 705

Reports filed under 1430 · Fasteners, 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 jasc_code = '1430'
  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 03FDEA02108Collar · crackedRT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE FOUND WITH 2 LOCKBOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 364MR. RT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL 2 AND REPLACED AS Dec 7, 2003 · N583FE · Doug MD11SDR 03FDEA02107Collar · crackedLT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE FOUND WITH 3 LOCKBOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 363AL. LT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE 3 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL 2 AND REPLACED AS Dec 7, 2003 · N583FE · Doug MD11SDR 03FDEA02106Collar · crackedLT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE FOUND WITH 1 LOCKBOLT COLLAR CRACKED. GAIN ACCESS FROM PANEL 363PL. LT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE 1 CRACKED LOCKBOLT COLLAR REMOVED AS PER SRM51-32-01 VOL 2 AND REPLACED AS PERDec 7, 2003 · N583FE · Doug MD11SDR 03FDEA02105Fitting · crackedLT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE FOUND WITH 1 LOCK BOLT COLLARS CRACKED. LT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE 1 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM51-32-01 VOL 2 AND REPLACED AS PER SRM 51-33-01 VOL 2.Dec 7, 2003 · N583FE · Doug MD11SDR 03FDEA02104Collar · crackedLT CENTER SECTION OF NR 3 BANJO FITTING FWD FACE FLANGE FOUND WITH 2 LOCKBOLT COLLARS CRACKED. LT CENTER SECTION OF NR 3 BANJO FITTING FWD FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM51-32-01 VOL 2 AND REPLACED AS PER SRM51-33-01 VOL 2Dec 7, 2003 · N583FE · Doug MD11SDR 03FDEA02102Collar · crackedLT CENTER SECTION OF NR 2 BANJO FITTING FWD FACE FLANGE FOUND WITH 2 LOCKBOLT COLLARS CRACKED. LT CENTER SECTION OF NR 2 BANJO FITTING FWD FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM51-32-01 VOL2 AND REPLACED AS PER SRM51-33-01VOL2Dec 7, 2003 · N583FE · Doug MD11SDR 03FDEA02093Collar · crackedLEFT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE FOUND WITH 02 EA LOCK BOLT COLLARS CRACKED. LT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01, VOL.II & INSTALLED AS PER SRM 51-33-01, VOLDec 7, 2003 · N583FE · Doug MD11SDR 03FDEA02092Collar · crackedBETWEEN UPPER SECTION OF BANJO FITTINGS NR 2 & 3 INTERCOSTAL STIFFENERS (AJC7581-11 & AJC7581-19) FOUND WITH 02 EA LOCKBOLT COLLARS CRACKED. LT BETWEEN UPPER SECTION OF BANJO FITTINGS NR 2 & 3 INTERCOSTAL STIFFENERS AJC7581-11 & AJC7581-19, 02 EA. CRACKED Dec 7, 2003 · N583FE · Doug MD11SDR 03FDEA02091Collar · crackedBETWEEN UPPER SECTION OF BANJO FITTINGS NR 2 & 3 ATTACHED HORIZONTAL WEB FOUND WITH 03 EA LOCKBOLT COLLARS CRACKED. LT BETWEEN UPPER SECTION OF BANJO FITTINGS NR 2 & 3 ATTACHED HORIZONTAL WEB 3 CRACKED LOCKBOLT COLLARS REMOVED AND REPLACED AS PER SRM 51-3Dec 7, 2003 · N583FE · Doug MD11SDR 03FDEA02090Collar · crackedBETWEEN UPPER SECTION OF BANJO FITTINGS NR 1 & 2 ATTACHED HORIZONTAL WEB FOUND WITH 02EA LOCKBOLT COLLARS CRACKED. LT BETWEEN UPP SECTION OF BANJO FITTINGS NR 1 & 2 ATTACHED HORIZONTAL WEBS 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL2 & REPLACEDec 7, 2003 · N583FE · Doug MD11SDR 03FDEA02080Collar · crackedRIGHT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE FOUND WITH 04 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE 4 CRACKED LOCKBOLT COLLARS REMOVED & REPLACED AS PER SRM 51-32-01, VOL. II & SRM 51- 33-01, VOL II Dec 7, 2003 · N583FE · Doug MD11SDR 03FDEA02079Collar · crackedRIGHT CENTER SECTION OF NR 2 BANJO FITTING (AJC7052-501) FWD FACE FLANGE FOUND WITH 01 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 2 BANJO FITTING FWD FACE FLANGE 1 CRACKED LOCKBOLT COLLAR REMOVED & REPLACED AS PER SRM 51-32-01, VOL. II & SRM 51- 3Dec 7, 2003 · N583FE · Doug MD11SDR 03FDEA02078Collar · crackedRIGHT CENTER SECTION OF NR 2 BANJO FITTING (AJC7052-501) AFT FACE FLANGE FOUND WITH 05 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 2 BANJO FITTING AJC7052-501 AFT FACE FLANGE 05EA CRACK LOCK BOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL. II AND REPDec 7, 2003 · N583FE · Doug MD11SDR 03FDEA02077Collar · crackedRIGHT CENTER SECTION OF NR 2 BANJO FITTING FWD FACE FLANGE FOUND WITH 04 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 2 BANJO FITTING FWD FACE FLANGE 4 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01, VOL. II AND REPLACED AS PER SRM 51-33-01, VODec 7, 2003 · N583FE · Doug MD11SDR 03FDEA02076Collar · crackedRIGHT CENTER SECTION OF NR 2 BANJO FITTING (AJC7052-501) AFT FACE FLANGE FOUND WITH 05 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 2 BANJO FITTING AJC7052-501AFT FACE FLANGE 5 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACEDDec 7, 2003 · N583FE · Doug MD11SDR QXEA200301540Rivet · damagedCHERRY RIVET AT INBOARD EDGE OF NR 5 FLAP TRACK FITTING SIDE ANGLE THROUGH LOWER SKIN DOES NOT HAVE SHOP HEAD. REMOVED AND REPLACED RIVET IAW Q400 SRM 51-42-45.Dec 6, 2003 · N406QX · Bombdr DHC8401SDR AMWA88Rivet · looseLEFT WHEEL WELL GRAVEL FENDER INBOARD UPPER ATTACH POINT AT KEEL HAS LOOSE RIVETS CAUSING WEAR ON KEEL BEAM. REPAIRED BY INSTALLING DOUBLER ON KEEL BEAM USING ADHESIVE AND HUCK BOLT FASTENERS IN ACCORDANCE WITH ENGINEERING REPORT 4849-3.Dec 5, 2003 · N161YV · Beech 1900DSDR ABXA030462Fastener · looseCAPTAIN'S EMERGENCY LIGHT UNDER GLARESHIELD WAS LOOSE AND INTERMITTENTLY INOPERATIVE. TIGHTENED LOOSE MOUNTING HARDWARE FOR CAPTAIN'S EMERGENCY LIGHT UNDER GLARESHIELD REF DC-8 MM 20-00.Dec 5, 2003 · N843AX · Doug DC861SDR GLBA20030513Fastener · crackedSEVERAL CHERRY MAX RIVET HEADS CRACKED AROUND EMERGENCY EXIT DOOR INNER FRAME SKIN, REMOVED AND REPLACED CRACKED RIVETS STATION R4C 273.75, 288.00, 327.63, 348.25 USED RIVETS PN CR3243-5 AND -3.Dec 3, 2003 · N192GL · Beech 1900DSDR AUS20031225Bolt · mismanufactured(AUS) MAIN ROTOR SWASHPLATE LOWER BOLT DAMAGED. INVESTIGATION FOUND A FLAT SPOT ON THE BLADE SHANK. SUSPECT MANUFACTURING ERROR AS FLAT SPOT HAD BEEN CADMIUM PLATED. FOUND DURING INSPECTION IAW AD/R44/20.Dec 2, 2003 · Robsin R44SDR CA031203009Bolt · failed(CAN) ON DOING A SIRM WING BOLT INSP THE FWD UPPER RT WING BOLT SHOWED REJECTIONABLE INDICATIONS. BOLT WAS CHANGED AND RETURNED TO SERVICE. BOLT LIFE WAS 9YEARS.Nov 30, 2003 · Beech A100SDR CA031203008Bolt · failed(CAN) ON INSP OF A/C AT SIRM INSP FOUND REJECTIONABLE INDICATIONS ON THE FORWARD UPPER RT WING BOLT. REPLACED AND A/C RETURNED TO SERVICE. PART WAS 9 YEARS OLD.Nov 30, 2003 · Beech A100SDR CA031203007Bolt · failed(CAN) ON A SIRM INSP OF THE WING BOLTS THE RT FWD UPPER WING BOLT SHOWED REJECTIONABLE INDICATIONS. THE BOLT WAS REPLACED AND A/C RETURNED TO SERVICE.Nov 30, 2003 · Beech A100SDR SWAA032640Bolt · corrodedDURING SCHEDULED D CHECK, FOUND VERT FIN REAR SPAR ATTACH BOLTS (4 EA) CORRODED. REMOVED AND REPLACED BOLTS PER MM.Nov 30, 2003 · N376SW · Boeing 7373H4SDR 03FDEA01990Bolt · gougedUPON REMOVAL OF BOLT 36 LT FAILSAFE FOUND BOLT HOLE INNER SURFACE WITH 03 EA GOUGES. COMPLIED WITH FEDEX EA 1-5510-74261 STABILIZERS - HORIZONTAL STABILIZER 36L FAIL-SAFE BORE GAUGEDNov 26, 2003 · N583FE · Doug MD11SDR 03FDEA01985Collar · crackedAFT FUSELAGE COMPT: AFT BODY BULKHEAD FRONT FACE STA Y2014 CAN NOT BE FOUND WITH MANY LOCK BOLT COLLARS CRACKED AXIALLY AS MARKED. AFT FUSELAGE COMPT : AFT BODY BULKHEAD FRONT FACE STA Y2014 CRACK FASTENERS REMOVED & REPLACED AS PER SRM 51-33--01 VOL2.Nov 26, 2003 · N583FE · Doug MD11SDR SWAA032597Bolt · looseNOTABLE ACFT ROLL TO THE RIGHT AFTER T/E FLAPS ARE POSITIONED AT 15 UNITS. FOUND RT OUTBD T/E FLAP CARRIAGE BEARING SUPPORT BOLTS LOOSE. TORQUED BOLTS PER MM. OPS CK GOOD.Nov 25, 2003 · N722WN · Boeing 7372T4SDR LR7A03091Fastener · looseDURING SCHEDULED C4 INSPECTION, FOUND LOOSE FASTENERS FS 345E-245 FUSELAGE SKIN, LBL 30, WL 230-285. REPLACED 60 EA RIVETS IAW AC 43.13-1B AND SB 382-53-42. NR 2067.Nov 21, 2003 · N404LC · Lkheed 382GSDR 2004FA0000621Bolt · corrodedDURING ANNUAL INSPECTION THE STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30/39 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS AN175C33A THAT ATTACHES THE Nov 11, 2003 · N727DS · Piper PA24250SDR FFK2004F00000Bolt · failedUPON LANDING, NOTICED THAT THE RT SIDE IB GEAR DOOR WAS NOT IN THE STOWED POSITION. CAUSE OF FAILURE, THE ROD END THAT CONTROLS MOVEMENT OF THE IB GEAR DOOR HAD EXCESSIVE WEAR CAUSING THE BOLT TO SHEAR AND ALLOWING GEAR DOOR TO SWING FREELY.Nov 11, 2003 · N707RA · Beech 58SDR AUS20031177Bolt · broken(AUS) RT MAIN LANDING GEAR UPLOCK ROLLER ATTACHMENT BOLT BROKEN.Nov 10, 2003 · Swrngn SA227ACSDR DHL2003782013Stud · strippedAFTER ENGINE START NR 3 OIL PRESSURE LIGHT CAME ON, AND CONFIRMED BY LOW OIL PRESSURE GAUGE. ENGINE SHUT DOWN OIL QUANTITY DECREASED TO ZERO. FOUND STUD ON OIL FILTER COVER IN GEARBOX STRIPPED. REMOVED STUD AND INSTALLED HELICAL COIL INSERT PER P&W M/M 70-0Nov 6, 2003 · N769AT · Boeing 727227SDR QXEA200301450Nut Plate · corrodedPDX- FLOOR NUTPLATE HAS CORROSION AT STATION X223.00, LEFT OF YL29.00. REPAIRED IAW DHC-8 SRM 51-00-06, 51-40-11 AND RD 8-53-7637.Nov 5, 2003 · N349PH · Dhav DHC8202SDR QXEA200301453Rivet · brokenPDX- BROKEN RIVET ON LEFT HAND SIDE OF VERTICAL STABILIZER ALONG TOP EDGE, MID POINT OF STABILIZER. REPAIRED IAW DHC-8 SRM 51-40-00.Nov 4, 2003 · N349PH · Dhav DHC8202SDR QXEA200301452Rivet · loosePDX- FORE RUDDER LOWER CLOSING RIB HAS LOOSE RIVET AT FORWARD RIGHT HAND SIDE. REPAIRED IAW DHC-8 SRM 51-40-11.Nov 4, 2003 · N349PH · Dhav DHC8202SDR AMWA79Rivet · chafedWHILE PERFORMING AN A-CHECK STRUCTURAL INSPECTION, RIVET HEAD CHAFED WAS FOUND TO THE LEFT PRESSURE PLATE, LBL 30.28.Nov 4, 2003 · N127YV · Beech 1900DSDR MWEA030441Setscrew · strippedLEFT TOP SET SCREW IS STRIPPED FOR NOSE WEIGHT ATTACHMENT POINT AT FRAME STATION 218. REMOVED AND REPLACED NEW SET SCREWS.Nov 3, 2003 · N812ME · Doug DC981SDR AMWA74Bolt · looseDURING A NR 6 DETAIL, IT WAS FOUND THAT THE FOUR BOLTS SECURING THE RUDDER TORQUE TUBE TO THE RUDDER AT THE LOWER ATTACH POINT FLANGE WERE LOOSE. CAUSING PLAY IN THE RUDDER CONTROL SYS AFTER REPLACING THE 4 BOLTS AND PERFORMING RUNNING TORQUE TESTS ON THE FASNov 2, 2003 · N3199Q · Beech 1900DSDR AMWA116Rivet · chafedWHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, THE LEFT WING ROOT PRESSURE PLATE WAS FOUND TO HAVE A RIVET HEAD CHAFED.Oct 30, 2003 · N23YV · Beech 1900DSDR AUS20031120Bolt · loose(AUS) AILERON CONTROL COLUMN IDLER SPROCKET BOLT LOW TORQUE. SUSPECT BOLTS LOOSENED DURING RIGGING AT MANUFACTURE AND NOT RETORQUED. PERSONNEL/MAINTENANCE ERROR.Oct 30, 2003 · Piper PA34220TSDR AUS20031119Bolt · loose(AUS) AILERON CONTROL COLUMN IDLER SPROCKET BOLT LOW TORQUE. SUSPECTBOLTS LOOSENED DURING RIGGING AT MANUFACTURE AND NOT RETORQUED.Oct 30, 2003 · Piper PA34220TSDR U2R2004F00001Fastener · mismanufacturedREPAIRED L2 DOOR AT LOWER FORWARD CORNER FS1620 IAW MM.Oct 29, 2003 · N921R · Doug DC863FSDR AUS20031118Bolt · loose(AUS) AILERON CONTROL COLUMN IDLER SPROCKET BOLT LOW TORQUE. SUSPECT BOLTS LOOSENED DURING RIGGING AT MANUFACTURE AND NOT RETORQUED.Oct 29, 2003 · Piper PA34220TSDR P5CA0300975Bolt · shearedBODY STATION 2360 - (AFT PRESSURE BULKHEAD) TWO SHEARED BOLTS AT STRINGERS 11R & 20R. REPLACED BROKEN BOLTS - DETAILED VISUAL INSPECTION AND TORQUE CHECK REMAINING BOLTS - FOUR BOLTS FOUND BOTTOMED OUT. ADDED WASHERS AND RETORQUED PER SB 747-53A2474.Oct 29, 2003 · N921FT · Boeing 747283BSDR Z1R2003F00008Screw · crackedMAIN ROTOR TIP CAP SCREWS/ MAIN ROTOR BLADE. HAD ONE (1) SCREW CRACKED, NR 1 UPPER POSITION LEADING EDGE. REPLACED AT 292.2 A/C HOURS. HAD ONE (1) SCREW CRACKED NR 1 BOTTION POSITION LEADING EDGE.Oct 28, 2003 · N760AF · Skrsky S76CSDR Z1R2003F00007Screw · crackedONE (1) SCREW CRACKED NR 1 BOTTOM POSITION FROM LEADING EDGES.Oct 28, 2003 · N760AF · Skrsky S76CSDR Z1R2003F00006Screw · crackedONE SCREW CRACKED NR 1 BOTTOM POSITION LEADING EDGES.Oct 28, 2003 · N760AF · Skrsky S76CSDR Z1R2003F00005Screw · crackedONE (1) SREW CRACKED NR 1 BOTTOM POSITION LENDING EDGE.Oct 28, 2003 · N761AF · Skrsky S76CSDR Z1R2003F00004Screw · corrodedHAD ONE SCREW BREAK ON REMOVAL. NR 1 BOTTOM POSITION LEADING EDGE. CORROSION AND EXCESSIVE BREAKING, TORQUE NOTED ON ALL MAIN ROTOR BLADES. ALL ATTACHMENT REPLACED AS PRE-CAUTION.(K)Oct 28, 2003 · N760AF · Skrsky S76CSDR 2004FA0000623Bolt · corrodedDURING ANNUAL INSPECTION THE STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30/39 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS AN175C33A THAT ATTACHES THE Oct 25, 2003 · N8843P · Piper PA24260
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