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 AUS20021331Fastener · loose(AUS) STRUT INBOARD MIDSPAR FITTING HORIZONTAL AND VERTICAL TANGS HAD SEVERAL LOOSE FASTENERS.Nov 8, 2002 · Boeing 747400SDR QXEA0201875Snap Ring · defectiveSEA - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKE OFF THE AIRCRAFT DEPRESSURIZED AT 7000 FEET. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE SNAP RING ON THE VENT DOOR SHAFT OF THE FORWARD CARGO DOOR. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WNov 7, 2002 · N405QX · Bombdr DHC8401SDR QXEA0201918Collar · wornPDX - LEFT HAND WING, NR 4 FLAP TRACK HAS SEVEN LOCKBOLT COLLARS WORN OFF ON UPPER SIDES. REPAIRED IAW DHC-8 RD 8-51-102.Nov 6, 2002 · N369PH · Dhav DHC8202SDR QXEA0201851Rivet · loosePDX - CENTER ROW OF RIVETS ON EXTERIOR OF CARGO DOOR SMOKING AT FORWARD AND AFT ENDS. REPAIRED IAW DHC-8 SRM 51-40-11, PAGES 1-4.Nov 6, 2002 · N369PH · Dhav DHC8202SDR QXEA0201849Fastener · corrodedPDX - BAGGAGE COMPARTMENT DOOR THRESHOLD SCREWS AND SCREW NUTPLATES HAVE CORROSION ON THEM AT APPROXIMATELY STATIONS X550.000 AND X564.500. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26.Nov 6, 2002 · N369PH · Dhav DHC8202SDR QXEA0201848Rivet · damagedPDX - CARGO DOOR MID BEAM TO SKIN RIVET BUCKTAIL DAMAGED. REPAIRED IAW DHC-8 SRM 51-40-11, SRM 51-20-36 AND SRM 51-20-41.Nov 5, 2002 · N369PH · Dhav DHC8202SDR QXEA0201843Rivet · loosePDX - RIVET APPEARS TO BE SMOKING IN RIGHT HAND AFT TAIL CONE AREA AT APPROXIMATELY FRAME 7, Z176.50. REPAIRED IAW DHC-8 SRM 51-40-11, SRM 51-20-36 AND SRM 51-20-41.Nov 5, 2002 · N369PH · Dhav DHC8202SDR VY1L110899Bolt · wornBOLTS, WORN. (SN 27148, 27269, 27486, 27143, 27423, 27619)Nov 2, 2002 · N211FN · Snias AS350B1SDR UC22002F00004Cotter Pin · failedDURING TRAINING FLIGHT, THE PILOTS RIGHT RUDDER PEDAL WAS REPORTED TO BE UNRESPONSIVE DURING FLIGHT. THE PILOT LANDED THE AIRPLANE WITHOUT AN INCIDENT. UPON INSPECTION OF THE PILOTS RIGHT RUDDER PEDAL AND THE TOE BRAKE ASSEMBLY THE CLEVIS ASSY WAS FOUND DISCOct 28, 2002 · N4144K · Piper PA28181SDR QXEA0201820Nut Plate · failedPDX- INBOARD NUTPLATE FOR FUEL TANK ACCESS PANEL 522AT SPIN WHEN TRYING TO TIGHTEN OR LOOSEN THE BOLT. REPAIRED IAW Q400 SRM 51-42-05.Oct 26, 2002 · N412QX · Bombdr DHC8401SDR DL764021243Bolt · shearedON LANDING ROLL-OUT, L/E SLAT ASYM MSG ILLUMINATED ON EICAS. FOUND PROX TARGET BOLT BROKEN NR 9 SLAT O/B. REPLACED SAME, CHECKS OK.Oct 26, 2002 · N832MH · Boeing 767432ERSDR 2004FA0000618Bolt · 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, 2002 · N487NM · Piper PA24180SDR 2004FA0000610Bolt · 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, 2002 · N6613P · Piper PA24SDR MWEA020633Nut Plate · corrodedRIGHT FLAP LEADING EDGE ATTACH NUT PLATE IS BROKEN AT XFLS 265. FORMED RIB ANGLE, DRILLED UP RIB ANGLE AND DRILLED 2 HOLES THROUGH LEADING EDGE. INSTALLED NUT PLATES AND NOSE RIB GEAR.Oct 25, 2002 · N805ME · Doug DC981SDR QXEA0201783Rivet · inadequatePDX - ONE RIVET BUCKED TAIL DOES NOT FILL HOLE COMPLETELY, AFT RIVET NR 1 SEAT TRACK X333.30, OUTBOARD FLANGE. REPAIRED IAW DHC-8 SRM 51-40-00.Oct 17, 2002 · N364PH · Dhav DHC8202SDR CA021018001Rivet · corroded(CAN) DURING UNSCHEDULED MAINTENANCE, RIVET HEADS WERE FOUND SITTING ON THE FRAME BELOW THE WINDOW, AFTER FURTHER INVESTIGATION FOUND THAT THE RIVET HEADS CAME FROM THE SPLICE IN THE CHANNEL AT STA 193.00. RIVET HEADS WERE CORRODED AND SEPARATED WITH HALF OFOct 15, 2002 · Beech 200BEECHSDR 2004FA0000620Bolt · 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 10, 2002 · N9073P · Piper PA24260SDR USAABB02171Bolt · fracturedSJU - FLT 1677 - ON GEAR EXTENSION FOR LANDING AT SJU, AIRCRAFT LOST THE RIGHT MAIN LANDING GEAR SHOCK STRUT DOOR. MAINTENANCE EXAMINED THE AIRCRAFT FOR FURTHER DAMAGE AND NONE WAS FOUND. AIRCRAFT WAS FLOWN ON CDL. THE MOST LIKELY CAUSE OF THE STRUT DOOR SEOct 6, 2002 · N655US · Boeing 7672B7SDR QXEA0201657Rivet · fracturedPDX - NEW RIVET IN NR 9 SEAT TRACK HAS FRACTURED BUCKTAIL AT APPROXIMATELY X598.0. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 1.Oct 5, 2002 · N368PH · Dhav DHC8202SDR QXEA0201599Rivet · loosePDX- ON THE LT SIDE VERTICAL STABILIZER ATTACH ANGLE THE MOST AFT RIVET ON THE LOWER FLANGE OF THE ATTACH ANGLE IS LOOSE. REPAIRED IAW FOKKER SRM 51-31-01.Oct 5, 2002 · N493US · Fokker F28MK4000SDR QXEA0201712Rivet · misinstalledCKB - LT NACELLE AT FIREWALL BOTTOM SEVEN RIVETS WITH INSUFFIEIENT GRIP LENGTH. REPAIRED IAW Q400 SRM 51-42-02.Oct 3, 2002 · N407QX · Bombdr DHC8401SDR 2003FA0000015Bolt · looseINSPECTION IAW AD AND FOUND LOOSE BOLT HOLES FOR VERTICAL STABILIZER ATTACH. INSTALLED OVERSIZE BOLTS AND DYE CHECK, NO CRACKS FOUND, RETORQUED BOLTS DYE PENETRANT INSPECTION ITEMS.Sep 30, 2002 · N4994F · Cessna U206BSDR CA020930005Rivet · broken(CAN) INLET COWLING HAD APPROXIMATELY 1/4 OF THE RIVET HEADS MISSING ON THREE CONSECUTIVE RIVETS, PLUS 1 RIVET HEAD LIFTING. LOCATION WAS THE 3RD ROW OF RIVETS FROM THE FRONT OF THE INLET, AT THE 2 O'CLOCK POSITION.Sep 30, 2002 · Cessna 550SDR 2002FA0001251Bolt · looseFOUND BOTH MAIN GEAR FORWARD TRUNNION BOLTS LOOSE IN SPAR. THIS WAS FOUND ON AN 100 HOUR INSPECTION.Sep 27, 2002 · N4546F · Cessna A185ESDR 2002FA0001194Bolt · crackedLEFT AFT UPPER WINGBOLT CRACK FOUND WHERE SHAFT CONNECTS TO BOLT HEAD. WINGBOLT INSPECTION CARRIED OUT IAW AD. BOLT WAS INSPECTED 1 YEAR/ 324 HOURS, PRIOR. BOLT, TT 2716.5 HOURS, 2544 A/C CYCLES. INSTALLED APRIL 1991.Sep 20, 2002 · Beech B100SDR 2004FA0000615Bolt · 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 Sep 19, 2002 · N7672Y · Piper PA30SDR KPVA200227Bolt · looseHNL - A BOLT ON FORWARD SIDE OF AIRSTAIR SUPPORT FOR IS LOOSE AND INHIBITS DOOR FROM OPENING. INSTALLED THREADED BUSHING ON UPPER STAY STRUT IAW DHC 8MM 52-10-00 PATE 219 PARAGRAPH C. NO DEFECTS NOTED. (M)Sep 18, 2002 · N806WP · Dhav DHC8103SDR GTIA020974Dome Nut · brokenRIGHT TANK FUEL QUANTITY WENT DOWN FASTER THAN LEFT WHILE IN FLIGHT. LANDED WITH 5600 IN LEFT AND 4300 IN RIGHT. CONFIRMED QUANTITY WITH DRIP STICKS. FOUND MISSING BOLT ON FORWARD PANEL ON RIGHT WING. FOUND 2 DOME NUTS FOR RIGHT WING FQ PROBE NR 2 ACCESS PSep 16, 2002 · N131NK · Doug DC941SDR 2002UALA01444Screw · backed outNO OIL PRESSURE IN LEFT ENGINE, ENGINE SHUTDOWN. FLIGHT LANDED WITHOUT INCIDENT. OIL PUMP DRIVE GEAR FAILURE. REF IPC 72-61-00-019: OIL PUMP DRIVE BEARING AND GEAR ASSY WERE FOUND LOOSE AND COCKED IN THE GEARBOX BEARING BORE. BEARING RETAINING SCREWS WERE BSep 11, 2002 · N652UA · Boeing 767322SDR QXEA0201572Rivet · looseCKB- RIVETS LOOSE ON LEFT HAND CENTER WING BOTTOM SKIN, AFT EDGE NEAR JACKING POINT. REPAIRED IAW Q400 SRM 51-42-00.Sep 11, 2002 · N406QX · Bombdr DHC8401SDR DHL2002742006Cotter Pin · looseMAIN CARGO DOOR LIGHT ILLUMINATED IN FLIGHT. COMPLETED EMERGENCY CHECKLIST. FOUND AFT DOOR LOCK PIN MICRO SWITCH STRIKER COTTER PIN LOOSE. REPLACED PIN INSURING STRIKER SECURITY IAW 727 WIRING DIAGRAM SUPPLEMENT 52-73-11 PG 1, OPS CHECK NORMAL. OK FOR CONTSep 10, 2002 · N742DH · Boeing 727225SDR SWIA200211179Screw · looseF/O'S WINDSHIELD HEAT IS SPARKING IN THE TERMINAL BOX. TIGHTENED UPPER TERMINAL SCREW. OPS CHECK OK.Aug 25, 2002 · N417SW · Cndair CL6002B19SDR QXEA0201290Rivet · missingPDX - RIVET MISSING FROM OIL COOLER BOX STRUCTURE, OUTBOARD OF OIL COOLER. REPLACED RIVET IAW DHC-8-200 SRM 51-40-11.Aug 22, 2002 · N363PH · Dhav DHC8202SDR QXEA0201289Rivet · loosePDX - TWO LOOSE RIVETS AT RIGHT HAND WING ROOT FAIRING SCUPPER DRAIN OUTLET AT STATION X424. REPAIRED IAW DHC-8-200 SRM 51-40-11.Aug 22, 2002 · N363PH · Dhav DHC8202SDR QXEA0201288Rivet · loosePDX - TWO SMOKING RIVETS IN SKIN ABOVE RIGHT HAND EMERGENCY EXIT. REPAIRED IAW DHC-8 SRM 51-40-11.Aug 21, 2002 · N363PH · Dhav DHC8202SDR 2002FA0001175Rivet · missingELEVATOR TRIM TABS ON AIRCRAFT WERE INSPECTED FOR RIVETS. FOUND LT ELEVATOR TRIM TAB THAT WAS INSTALLED 10 HOURS PRIOR, TO BE MISSING ALL RIVETS. THE SKINS WERE BONDED BUT RIVETS WERE NEVER INSTALLED. THE TRIM TAB HAD BEEN SITTING ON OUR SHELF FOR 2 YEARS BAug 20, 2002 · N1554 · Beech A200SDR MALA020500Fastener · corrodedDURING 4K INSPECTION IN CWA, LT AND RT CENTER AISLE SEAT TRACK CLIPS ARE CORRODED. MAINTENANCE REMOVED AND REPLACED CORROSION IAW SRM 51-70-40.Aug 19, 2002 · N452XJ · Saab 340BSDR MALA020499Rivet · corrodedDURING 4K INSPECTION IN CWA, WEB AT STA 294 HAS CORRODED FASTENERS. MAINTENANCE REMOVED AND REPLACED RIVETS.Aug 19, 2002 · N452XJ · Saab 340BSDR QXEA0201249Fastener · loosePDX - FASTENER LIFTING BELOW RIGHT HAND AFT LOWER CORNER OF VERTICAL STABILIZER LEADING EDGE PANEL 321GT. REPAIRED IAW DHC-8 SRM 51-40-1.Aug 18, 2002 · N363PH · Dhav DHC8202SDR QXEA0201248Fastener · loosePDX - FASTENER LIFTING BELOW RIGHT HAND AFT CORNER OF VERTICAL STABILIZER LEADING EDGE PANEL 321GT. REPAIRED IAW DHC-82 SRM 51-40-11.Aug 18, 2002 · N363PH · Dhav DHC8202SDR CTU2003F00000Bolt · bentAFTER FAILURE OF BOLT PRIOR TO FLIGHT MAINTENANCE FACILITY PERFORMED INSPECTION OF BOLT WHICH THE ELEVATOR BELLCRANK ROTATION. BOLT MUST BE REMOVED FOR PROPER INSPECTION. BOLTS HAVE BOTH STRESSED AND BENT. MANUFACTURER SHOULD HAVE BOLT OF LARGER SIZE INSTALAug 16, 2002 · N98560 · Cessna 340ASDR MALA020485Rivet · corrodedDURING 4K/2Y/4Y INSPECTION IN CWA, RIVETS ON FRAME ANGLE AT STA 236 HAVE CORROSION. MAINTENANCE REMOVED CORROSION AND REPLACED RIVETS AS REQUIRED IAW SRM 51-70-40 AND 51-40-21.Aug 16, 2002 · N448XJ · Saab 340BSDR QXEA0201231Fastener · loosePDX- CLASS THREE FUEL SEEP FROM LEFT HAND NR 5 LIFT DUMPER BELLCRANK FITTING, LOWER SIDE UPPER OUTBOARD HI-LOK. REPAIRED IAW F-28 SRM 28-11-0-5 AND 27-50-5.Aug 9, 2002 · N497US · Fokker F28MK4000SDR QXEA0201169Nut Plate · corrodedPDX-NUT PLATE CORRODED AT BAG BAY STEP BULKHEAD JUST OUTBOARD OF PULLEYS ON LEFT HAND SIDE. REPAIRED IAW DHC8 SRM 51-20-16, PAGE 4 AND SRM 51-40-00.Aug 7, 2002 · N362PH · Dhav DHC8202SDR DLM90020907Screw · looseAIR TURNBACK, 2L DOOR HAD A LARGE AIRLEAK AUTO CONTROLLER DID NOT HAVE OUTFLOW VALVE FULL CLOSED. GOT CABIN ALT WARN LIGHT CABIN WAS AT 10000 FT/BIT AUTO CONTROLLER 1 FAULTED GROUND SWITCH. PRESSURIZED A/C PER M/M, NO DOOR LEAKS NOTED. FOUND LOOSE SCREW HADAug 5, 2002 · N904DA · Doug MD9030SDR SWIA200211225Rivet · corrodedANCHOR NUTS FOR RT OVERWING EMERGENCY EXIT BOTTOM HINGE FITTINGS HAVE CORRODED RIVETS. DISCOVERED DURING C-CHECK. FITTINGS REMOVED FOR ACCESS. RIVETS INSTALLED IAW CRJ SRM 51-42-16. INSTALLED FITTINGS IAW MM 20-21-00.Aug 4, 2002 · N412SW · Cndair CL6002B19SDR PNSA020706Fastener · looseON CLIMBOUT FROM ANC AN UNUSUAL VIBRATION WAS FELT IN CONTROL YOKE AND RUDDER PEDALS. AIRCRAFT RETURNED TO ANC. MAINTENANCE FOUND TAIL CONE ACCESS PANEL 317AB FORWARD TWO CAM LOCK FASTENERS LOOSE AND HANDLE FOR PANEL WAS STOWED WHICH MADE PANEL APPEARED INSTJul 28, 2002 · N675PA · Saab 340BSDR 02FDEA00522Bolt · shearedRIGHT MAIN GEAR W/W SHEARED AT VERTICAL FITTING TO TRAPEZOIDAL PANEL AT OM SIDE OF W/W BS 1381. INSTALLED NEW BOLT PER AOL 10-20088.Jul 25, 2002 · N301FE · Doug DC1030SDR 02FDEA00516Bolt · corrodedRIGHT TRUNNION MOUNTING BOLTS FOUND EMITTING RUST. REMOVED AND REPLACED BOLTS PER MM.Jul 24, 2002 · N616FE · Doug MD11SDR DL764020862Bolt · failedEICAS MSG L/E SLAT ASSYM ILLUMINATED WHILE EXTENDING FLAPS TO 15 DEGS. T/E FLAPS INDICATE 15 DEG L/E SLATS YELLOW. PSEU TEST SHOWS SENSOR TARGET 285. FOUND TARGET MISSING AND BOLT SHEARED. REPLACED BOLT AND TARGET TO INBOARD AUX TRACK NR 4 SLAT PER AMM NO Jul 23, 2002 · N833MH · Boeing 767432ER
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