N813FD, cancelled Feb 3, 2024
Service difficulty reports · 130
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 = 'N813FD' AND deregistration_id = 'N813FD-2024-02-03' 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.
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 = 'N813FD' AND deregistration_id = 'N813FD-2024-02-03' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201310252617Controller · malfunctionedCABIN NR 2 PRESSURE REGULATOR INITIALLY ROUGH DURING TAKEOFF AND CLIMBOUT, EVENTUALLY SMOOTHED OUT. FAULTED AT FL 310. HAD TO TURN BOTH NR 1 & NR 2 OFF & USE MANUAL PRESSURIZATION CONTROL TO RECOVER, EMERGENCY DECLARED, CONTINUED TO DESTINATION. TESTED NSDR FDEA201308131865Windscreen · crackedDURING CRUISE AT FL340, CAPT'S WINDSCREEN CRACKED. ARCING NOTED TOP RT CORNER AFTER CRACKING. COMPLIED WITH QRH, PROCEED TO DESTINATION IAW GOC GUIDANCE. ENTERED IN ERROR, PREVIOUSLY REPORTED ON 13-1864. THIS DUPLICATE OCCURED AFTER A DOUBLE CLICK OF MOUSE OSDR FDEA201308131864Windscreen · crackedDURING CRUISE AT FL340, CAPTAIN'S WINDSCREEN CRACKED. ARCING NOTED TOP RT CORNER AFTER CRACKING. COMPLIED WITH QRH, PROCEED TO DESTINATION IAW GOC GUIDANCE. TEXT REMAINS OPEN FOR WINDOW COMPONENT(S) R & R IAW AMM 30-42-11-04. LEFT WINDOW HEAT PROTECTION UNSDR FDEA201307041476Drain · obstructedSTANDBY AIRSPEED INDICATORS INOPERATIVE. AT 250 KTS ON BOTH PFD'S BOTH STANDBY AIRSPEED INDICATORS SHOWED 180 KTS, THIS WAS AT 10,000 FT, BOTH STANDBY AIRSPEED INDICATORS SLOWLY DECREASED DURING THE CLIMB TO FL 380, AT FL 380 BOTH PFD'S SHOWED 255 KTS, BOTH SSDR FDEA201110094389Skin · puncturedLT WING INBD FLAP LWR SKIN JUST AFT OF THE CARRIAGE FOUND PUNCTURED. CUT OUT THE DAMAGED LOWER SKIN PER SRM 57-52-12/201 FIG205.SDR FDEA201109284176Skin · chafedFLUSH DOUBLER REPAIR ON L/E OF D-NOSE SKIN CHAFED AT TRACK NR 1. REPAIRED IAW EA6-5741-103419SDR FDEA201109274146Fitting · corrodedNR 1 ENG PYLON SPIGOT RECEPTACLE UPPER AND LOWER FITTING CORRODED. REMOVED THE SPIGOT FITTINGS PER SRM51-40-21 MACHINE THE MATING SURFACE OF THE NEW SPIGOT LOWER FITTING PER DWG A54611053. HORNED THE BORES C/T THE LOWER AND UPPER SPIGOT FITTINGS PER DWG A54SDR FDEA201109244113Angle · crackedCENTER WING FUEL TANK REAR SPAR INNER ANGLE FOUND CRACKED. REPAIRED IAW SRM 51-40-44, EO 6-5710-7-3322 &SRM 51-40-21. NO CRACK FOUND IAW NTM51-10-18.SDR FDEA201109193958Angle · crackedCENTER WING FUEL TANK REAR SPAR INTERNAL ANGLE FOUND CRACKED. COMPLIED WITH EA 6-5710-153425. REAMED HOLE IAW EA:6-5710-7-3322, B1, PART 1.SDR FDEA201109163902Slat Track · damagedLEFT WING SLAT NR 3, NR 9 TRACK BLEND OUT AREA EXCEEDED THE LIMITS (WIDTH=56.21MM). COMPLIED WITH EA 6-5741-103381, PART 3. REPLACED SLAT TRACK IAW AMM27-80-14-04. PERFORMED TEST OF SLAT IAW AMM27-80-14-04. TESTED OK.SDR FDEA201102010448Fluid · odorON TAKEOFF AT 4000FT. ECAM ALERT OF MAIN DECK CARGO SMOKE. FOLLOWED QRH AND RETURNED TO DEPARTURE. WE HAD EXTENSIVE ICE ON ACFT WHICH REQUIRED 1 HR 45 MIN OF DEICING. EMERGENCY DECLARED. IAW CREW DEBRIEF, SMOKE INDICATIONS CEASED. VERY STRONG ODOR OF DEICSDR FDEA201006252142Uplock · failedON TAKEOFF WITH GEAR HANDLE SELECTED UP- HEARD LOUD NOISE FROM UNDER ACFT AND NOSE GEAR DOOR LIGHT ON BOTH MAIN INDICATOR AND OVERHEAD INDICATOR. DURING AFTER TAKEOFF CHECKLIST WITH GEAR HANDLE POSITION TO NEUTRAL- NOSE GEAR CAME DOWN AND LOCKED. PUT HANSDR FDEA200904081217Angle · crackedAFT LOWER CARGO, FRAME 63A, LOWER CLOSE OUT ANGLE IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-72-10.SDR FDEA200904061204Support Bracket · chafedNR 1 ENGINE OUTBD FAN COWL; FORWARD EDGE ALIGNMENT PIN SUPPORT BRACKET IS CHAFED AT THE BOTTOM SURFACE. REMOVED DAMAGE IAW EA 6-7110-127946. FOUND TO BE WITHIN LIMITS IAW EA 6-7110-127946; VIEW A-A. PRIMED IAW SRM 51-23-10.SDR FDEA200904061200Floor Support · corrodedFUSELAGE INTERNAL STRUCTURE BELOW THE CARGO COMPARTMENT FLOOR HAS CORROSION ON A SUPPORT ANGLE AT FRAME 35 LBL 55. REMOVED CORROSION & FOUND TO OUT OF LIMITS IAW SRM 51-31-20 & SRM 53-10-00. LOCATED, DRILLED & TRIMMED IAW SRM 51-72-10. INSTALLED NEW ANGLESDR FDEA200904061199Floor Support · corrodedFUSELAGE INTERNAL STRUCTURE & CARGO COMPARTMENT FLOOR FLANGE IS CORRODED UNDER & AROUND THE NUTPLATES AND NUTS FROM FRAMES 38-38.1 RBL 55. REMOVED CORROSION & FOUND TO OUT OF LIMITS IAW SRM 51-31-20 & SRM 53-10- 00. LOCATED, DRILLED, & TRIMMED IAW SRM 51-SDR FDEA200904061205Skin · delaminatedNR 1 PYLON PANEL 474 BR INNER SKIN IS DELAMINATED. REPAIRED NR 1 PYLON PANEL 474 BR BY REMOVING DAMAGE; CLEANING; PREPARING AREA AND APPLYING FIBERGLASS WET LAY-UP REPAIRED IAW 54-50-00 AND 51-77-10. INSTALLED SEAL IAW DWG A54515353 CURED REPAIR IAW SRM 51SDR FDEA200904021159Floor Support · corrodedBULK CARGO COMPARTMENT, FLOOR SUPPORT ANGLE BETWEEN FRAME 69 AND FRAME 70; AT STRINGER 42R THRU STRINGER 44R HAS CORROSION AROUND 2 FASTENER HOLES. ANGLE FOUND TO BE OUT OF LIMITS IAW SRM 51-10-00. NEW ANGLE MATERIAL ID A2557217220600, PO NR 650584.2. LOCATSDR FDEA200904011135Skin · dentedFUSELAGE SKIN FWD EDGE OF THE CARGO DOOR CUTOUT, 12 INCHES FROM THE LOWER FWD CORNER IS DENTED. REMOVED FASTENERS IAW SRM 51-40-21. REMOVED DAMAGE IAW SRM 53-13-12. FABRICATED THE DOUBLER & FILLER IAW SRM 53-13-12. ALODINED THE DOUBLER, FILLER & SKIN CUTOUSDR FDEA200903311114Beam · corrodedTHE BULK CARGO DOOR LOWER SUPPORT WEB IS CORRODED AROUND THE NUTPLATES AND SKIN BETWEEN FRAMES C-67 AND C-69. REMOVED AND INSTALLED NUTPLATES REF SRM 51-40-21. REMOVED CORROSION REF SRM SRM 51-74-10 AND CHECKED LIMITS REF SRM 53-17-18. FOUND TO BE OUT OF LSDR FDEA200903311113Panel · crackedNR 1 PYLON PANEL 413 BL IS CRACKED IN THE CORNER UNDER THE SEAL. REMOVED SEAL RETAINERS AND SEALS IAW SRM 51-40-21; PG 5. STOP DRILLED CRACKS IAW SRM 54-52-51; PG 225; STEP E. FABRICATED DOUBLER AND INSTALLED IAW SRM 54-52-51; PGS 229 / 230. REINSTALLED SDR FDEA200903301107Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE 341 AB CENTER RIB IS CRACKED. REMOVED FASTENERS IAW A310 ARM 51-40-21. STOP DRILED CRACK IAW SRM 55-12-19. FABRICATED REPAIR ANGLE IAW SRM 51-71-40 & SRM 51-71-40. INSTALLED REPAIR ANGLE IAW SRM 51-71-40.SDR FDEA200903261051Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL 131 QF HAS MULTIPLE PUNCTURES ON THE BACK. REPAIRED PANEL 131 QF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005, REV "H".SDR FDEA200903261075Floor Panel · damagedCABIN FLOOR PANEL 241 LK. REPAIRED PNL 241LK WITH FABRICATION OF NEW PANEL. USING OLD PNL AS TEMPLATE IAW SRZ 25-005 REV H.SDR FDEA200903261074Floor Panel · damagedCABIN FLOOR PANEL 242 LK IS BROKEN. REPAIRED PANEL 242 LK WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".SDR FDEA200903261073Floor Panel · crackedCABIN FLOOR BOARD 282 KF IS CRACKED. REPAIRED PANEL 282 KF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".SDR FDEA200903261058Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL 132 YF IS CRUSHED ALONG THE EDGE AND HAS A BROKEN INSERT. REPAIRED PANEL 132 YF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".SDR FDEA200903261056Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL 132 RF IS CRACKED AT THE PDU CUTOUT. REPAIRED PANEL 132 RF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".SDR FDEA200903261055Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL 132 ZF HAS MULTIPLE PUNCTURES ON THE BACK AND IS CRACKED AT THE CORNER OF THE PDU CUTOUT. REPAIRED PANEL 132 ZF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".SDR FDEA200903261054Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL 131 YF IS BROKEN ALONG THE EDGE OF THE PANEL. REPAIRED PANEL 131 YF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".SDR FDEA200903261053Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL 131 ZF IS CRUSHED AT THE CORNERS OF THE PDU CUTOUT. REPAIRED PANEL 131 ZF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".SDR FDEA200903261052Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL 131 RF IS BROKEN AT THE PDU CUTOUT. REPAIRED PANEL 131 RF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".SDR FDEA200903261070Sill · corrodedMAIN DECK, R-2 DOOR SILL AREA HAS A STRINGER ANGLE CORRODED AT FRAME 74, BS 3998 THRU 4005; STRINGER 26R. REMOVED CORROSION IN REF TO SRM 51-74-40. ORIGINAL MATERIAL THICKNESS 0.118 IAW DWG A539800712. MATERIAL REMOVED 0.026. MATERIAL REMANING 0.092 ANSDR FDEA200903261069Floor Panel · puncturedAFT CARGO COMPARTMENT FLOOR PANEL 152 AF HAS MULTIPLE PUNCTURES ON THE BACK. REPAIRED PANEL 152 AF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".SDR FDEA200903261068Floor Panel · delaminatedAFT CARGO COMPARTMENT FLOOR PANEL 152 FF HAS DELAMINATION AND EDGE DAMAGE. REPAIRED PANEL 152 FF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".SDR FDEA200903261067Floor Panel · puncturedAFT CARGO COMPARTMENT FLOOR PANEL 152 BF HAS MULTIPLE PUNCTURES ON THE BACK. REPAIRED PANEL 152 BF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".SDR FDEA200903261066Floor Panel · damagedAFT CARGO COMPARTMENT FLOOR PANEL 152 EF HAS A BROKEN CORNER AND IS MISSING AN INSERT. REPAIRED PANEL 152 EF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".SDR FDEA200903261065Floor Panel · damagedBULK CARGO COMPARTMENT FLOOR PANEL 162 HF IS CRACKED AND CORRODED ON THE BACK OF THE PANEL. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".SDR FDEA200903261064Floor Panel · puncturedBULK CARGO COMPARTMENT FLOOR PANEL 162 DF IS PUNCTURED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".SDR FDEA200903261063Floor Panel · damagedBULK PIT FLOOR PANEL 161 GF IS PUNCTURED AND DENTED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".SDR FDEA200903261062Floor Panel · puncturedBULK PIT FLOOR PANEL 161 HF IS PUNCTURED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".SDR FDEA200903261061Floor Panel · damagedBULK PIT FLOOR PANEL 161 GF IS PUNCTURED AND CORRODED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".SDR FDEA200903261060Floor Panel · damagedBULK PIT FLOOR PANEL 161 AF IS PUNCTURED AND CORRODED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".SDR FDEA200903261059Floor Panel · damagedBULK PIT FLOOR PANEL 161 BF IS PUNCTURED AND DENTED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".SDR FDEA200903261057Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL 132 QF IS BROKEN INTO MULTIPLE PIECES. REPAIRED FLOOR PANEL 132 QF WITH FABRICATION OF NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ 25-005, REV "H".SDR FDEA200903261050Floor Panel · puncturedAFT CARGO PIT SLANT PANEL 161 CW HAS SEVERAL PUNCTURES. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW DWG SRZ 25-005, REV "H" & DWG SRZ 25-011, REV "C".SDR FDEA200903251037Floorbeam · corrodedTHE MAIN DECK FLOORBEAMS ARE CORRODED AT FRAME C-14; RBL 36. REMOVED CORROSION IN REF TO SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-12-15. REMOVED FLOORBEAM IAW SRM 51-72-10 PG 2. DRILLED NEW SUPPORT IAW SRM 51-72-10 PG 2. INSTALLED NEW FLOORBEAMSDR FDEA200902260741Control Unit · smokeAT FL 330, ATS LEVER DROPPED OFF, NR 1 A/P DROPPED OFF ALONG WITH A PUFF OF SMOKE VISIBLE BE GLARESHIELD FLOOD LIGHTS. ATS RE-ENGAGED AS DID THE NR 1 A/P. NO FURTHER "PUFFS" OF SMOKE. NO FURTHER PROBLEMS. PERFORMED MTP AFS BITE AND FMC BITE, BOTH FAULTED FSDR FDEA200811154892Adc · failedON TAKEOFF ROLL, F/O HAD NO AIRSPEED INDICATION, PERFORMED REJECT (70KTS). PERFORMED ALL OTHER PARAMETERS THAT COME FROM ADC ARE NORMAL. THE ON ISSUE IS THE SEED. PER FLIGHT CREW THE SPEED STOP AND THERE WAS DIFFERENCE FROM THE CAPTAIN'S AND THE FO'S. DURISDR 08FDEA04892Adc · failedON TAKEOFF ROLL, F/O HAD NO AIRSPEED INDICATION, PERFORMED REJECT (70KTS). PERFORMED ALL OTHER PARAMETERS THAT COME FROM ADC ARE NORMAL. THE ON ISSUE IS THE SEED. PER FLIGHT CREW THE SPEED STOP AND THERE WAS DIFFERENCE FROM THE CAPTAIN'S AND THE F/O'S. DUR
Back to N813FD, cancelled Feb 3, 2024