N812FD, cancelled Feb 6, 2024
Service difficulty reports · 85
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 = 'N812FD' AND deregistration_id = 'N812FD-2024-02-06' 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 = 'N812FD' AND deregistration_id = 'N812FD-2024-02-06' 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 FDEA201403120491Check Valve · leakingLOST GREEN HYD AIR AT FLT LEVEL 390 IAW QRH QTY WAS MONITORED AFTER 1 MIN GREEN HYD QTY FLUCTUATED & PEGGED AT MAX. IAW QRH GREEN HYD PUMPS 1 & 2 WERE SECURED, IAW QRH LANDED. REPLACED DEPRESSURIZATION RELEIF VALVE IAW AMM 29-11-27-04. ALSO REPLACED GREENSDR FDEA201312102953Controller · failedON DESCENT TO KMDT RECEIVED CAD REG 2 FAULT, RESET NO HELP. ON LANDING, ACFT SHOWED 3300 CAB ALT, WENT TO MANUAL, TURNED OFF BLEEDS & PACKS. CABIN OUTFLOW VLVS FWD & AFT STAYED CLOSED. OVERBOARD VENT PARTIALLY OPENED, ACFT STILL PRESSURIZED. SAFETY VLV STASDR FDEA201308021750Jackscrew · contaminatedNR 1 & 2 SLAT SYSTEMS FAULTED ON APPROACH. COMPLIED WITH PHASE 1, NO HELP. COMPLIED WITH ECAM AND QRH. ON CONFIGURING FOR LANDING IAW QRH SLAT EXTENDED NORMALLY. SFCC 1 & 2 FAULT INDICATES SLAT 01111 SLAT BINDING IAW TSM 27-80-02, FIG 101. FOUND LT L/E TOSDR FDEA201301170121Connector · failedCAPTAIN'S RA DOES NOT PROPERLY AGREE WITH FO'S RA. DURING TROUBLESHOOTING NR 1 R/A WOULD FLUCTUATE BETWEEN 150FT AND 450FT, THEN GO ABOVE 2500FT. DISCONNECTED BOTH TRANSMIT AND RECEIVING ANTENNAS AND METERED BOTH COAX CABLES FROM NR 1 R/A RACK CONNECTOR (1SDR FDEA201212244367Skin · delaminatedRIGHT WING INBD LOWER FLAP T/E MID SECTION FOUND DELAMINATED. REMOVED DELAMINATED DOUBLER & DAMAGED HONEYCOMB CORE IAW SRM 57-52-12/201. MADE NEW SKIN DOUBLER IAW SRM 57-52-12/201. MADE HONEYCOMB CORE PLUG SRM 57-52-12/201. INSTALLED HONEYCOMB CORE PLUG ANSDR FDEA201212244368Skin · delaminatedLEFT WING OTBD FLAP T/E LOWER SURFACE FOUND DELAMINATED, FROM INBD TO OTBD 2000 MM, DIM:16" X 7". REMOVED DELAMINATED LOWER SKIN IAW SRM 57-53-12/201. MADE NEW SKIN DOUBLER IAW SRM 57-53-12/201. FILLED THE HONEYCOMB CORE WITH COMPOUND IAW SRM 57-53-12/201. SDR FDEA201212154307Fitting · corrodedLEFT WING-MLG FITTING-INSPECTION OF RIB 5 FORWARD LUG CORROSION EXCEED LIMITS. REMOVED CORROSION IAW REPAIR DWG R57249389, ISSUE B, STEP 1B. IAW EA6-5710-163164. PENETRANT INSPECT THE LUG BORE IAW NTM 51-90-00 TO CONFIRM ALL DAMAGED COMPLETELY REMOVED. IAW SDR FDEA201212144299Spar · crackedCENTER WING RT REAR SPAR NR 61 HOLE FOUND CRACKED. REAMED HOLE AT 0.4MM THROUGH ALL LAYERS PER EA6-5710-163167. INSPECTED PER NTM51-10-01,NO CRACK FOUND. REAMED UP THE HOLE ON ALL LAYERS TO 15.836-15.875MM IN TRANSITION FIT PER EA6-5710-163167. WET INSTALLSDR FDEA201212144297Plate · crackedFOUND A CRACK ABOUT 5MM IN LENGTH, 1MM IN DEPTH INITIATED FROM THE NR 2 FASTENER HOLE OF THE RT WING UPPER CORNER ANGLE AT FR40. REAMED NR 2 HOLE AT 0.4MM THROUGH ALL LAYERS PER EA6-5710-163166. INSPECTED PER NTM51-10-01,NO CRACK FOUND. REAMED HOLE ON ALL LSDR FDEA201109294213Solenoid Valve · leakingGREEN HYD SYS LO RSVR INDICATION INFLIGHT FOLLOWED QRH, AFTER LANDING GREEN SYS REVR INDICATION RETURNED TO NORMAL. RESTORED FREE FALL EXTENSION SYSTEM TO NORMAL CONDITION AS PER AMM 32-33-00-2. PRESSURED GREEN HYD SYS AS PER AMM29-00-00-06, FOUND KRUEGER SSDR FDEA201011164400Skin · corrodedFUSELAGE SKIN EXTERIOR SURFACE FOUND CORROSION UNDER BULK CARGO DOOR SCUFF PLATE (FWD LWR CORNER). REMOVE THE CORROSION IAW SRM 51-74-10. APPLY ALODINE IAW SRM 51-21-10. MEASURE REMAIN THICKNESS OF THE REWORKED AREA IAW NTM51-10-04 (REMAINING THICKNESS WASDR FDEA201009263716Computer · malfunctionedON TAKEOFF ROLL, MASTER WARNING REPETITIVE CHIME, AT APPROX 130 KTS RTO. ECAM SHOWED PITCH TRIM 2 YD 2 OFF. PITCH TRIM 2 YD 2 BOTH RESET OK. BRAKE 3 670 DEGREES. WHILE WAITING FOR HOT BRAKES TO COOL, FUEL WENT BELOW RQR FOR FOR TO. SO RETURN TO GATE, OSDR FDEA201003301032B-Nut · leakingHYD GREEN SYS SERVICED WITHIN LIMITS, 10 MINUTES AFTER DEPARTURE, QTY IN AMBER BAN D. TURNED OFF NR 1 ENG HYD PUMP PRIOR TO TO RED DOT IN AMBER BAND AT FLT LEVEL 20. 15 MINUTES LATER RESERVOIR EMPTY. COMPLIED WITH QRH. SAFE LANDING. FOUND FLUID LEAKING OSDR FDEA201003070672Jackscrew · failedRECEIVED SLAT SYS 1 AND SYS 2 FAULT. SLAT STUCK AT APPROX 2 DEG, LANDED SLATS 2 DEG AND FLAPS 40 DEG, REPEAT WRITE UP. CYCLED ON THE GROUND PRIOR TO DEPARTURE AND THEY WORKED OK. CYCLED AIRBORN AND THEY STUCK. APPEAR TO BE AIRLOAD RELATED, CYCLED AT 210 KTSDR FDEA200911204098Brake Sys · malfunctionedDURING TRO WITH MAX BRAKES SELECTED, ONLY WHEEL BRAKES ON NR1,2,5,6 (LT SIDE) OPERATED NORMALLY. ACFT STARTED ABRUPT PULL TO LT DESELECTED AUTO BRAKES AND STOPPED USING MANUAL BRAKES. MEL 20NOV09 14:24 GRR RELEASED FOR SERVICE IAW MEL: 32-42-05 CATEGORY:SDR FDEA200911204097Anti-Ice System · faultedDURING T/O POWER APPLICATION, WHEN TOGA PWR WAS SELECTED THE GREEN A/THR LIGHT ILLUMINATED HOWEVER THE THROTTLES WOULD NOT MOVE. ACCOMPLISHED RTO AT 25 KTS. VERIFIED AT BLOCK IN NR1 ENGINE ANTI ICE WAS FAULTING IN ECAM. RELEASED FOR SERVICE IAW MEL: 22-30-01SDR FDEA200911204095Anti-Ice Valve · faultedDURING TAKEOFF ROLL AT 85KTS ECAM WARNING "ENG NAC ANTI ICE VALVE". ACCOMPLISHED RTO (ENG NR1) ENG ANTI ICE WAS ON DURING TAKE OFF. VERIFIED AT BLOCK IN NR 1 ENG ANTI ICE WAS FAULTING IN ECAM. VERIFIED AT BLOCK IN NR 1 ENG ANTI ICE WAS FAULTING IN ECAM. "MESDR FDEA200911204093Anti-Ice Valve · warning messageDURING TAKEOFF ROLL WITH ANTI-ICE ON, RECEIVED ECAM MESSAGE "ENG NR1 ANTI-ICE NAC VALVE". ACCOMPLISHED RTO AT 70 KTS. (RTO 1 OF 2) SEE WRI 30-20/3659 FOR DEFERRAL OF NR1 ENG NAC A/I VALVE. FAULT CLEARED WHEN REDUCING POWER, NO FURTHER FAULTS. CREW TAXIED SDR FDEA200811184905Control Unit · bindingSECOND REJECTED T/O DUE TO BLUE RUDDER SERVO CONTROL JAM, ECAM WARNING CAME ON AT 40-50 PERCENT N1. NO FAULT FOUND ON 1ST RTO. RAN ENGINE & CHECKED ALL FLT CONTROL OPERATIONS (WRI 27-20/2731). REPLACED JAMMING DETECTION CONTROL UNIT IAW AMM 27-14-17-4 PRECSDR 08FDEA04905Control Unit · inoperative2ND REJECTED TAKEOFF DUE TO BLUE RUDDER SERVO CTL JAM, ECAM WARNING CAME ON AT 40-50 PERCENT N1. NO FAULT FOUND ON 1ST RTO, RAN ENG AND CHECKED ALL FLT CONTROL OPERATION (WRI 27-20/2731). REPLACED JAMMING DETECTION CONTROL UNIT PER AMM 27-14-17-4 PRE CAUTIONSDR 08FDEA03353Skin · damagedUPON INSPECTION OF RUDDER BY THERMOGRAPHY IAW EO 6-5530-7-5004 PT 2 PARA 8 STEP C AND D THE FOLLOWING DEFECTS WERE NOTED IN ADDITION TO ORIGINAL FINDINGS REF EA 6-5740-118399 THE UPPER RT PORTION OF THE RUDDER HAS 1 ADDITIONAL AREA OF MOISTURE MEASURING .960 WSDR 08FDEA03264Skin · dentedEXTERNAL LT FUSELAGE SKIN HAS 2 DENTS. NR 1 AT FRAME 60 BETWEEN STRINGER 43 AND 44L 4 INCHES ABOVE BOTTOM SKIN LAP MEASURES 6 INCHES LONG BY .800 INCHES WIDE BY .037 INCHES DEEP. NR 2 DENT AT FRAME 61 BETWEEN STRINGER 43 AND 44L 3 INCHES ABOVE SKIN LAP MEASUSDR 08FDEA03263Skin · dentedDENT IN RT NR 1 LEADING EDGE SLAT, DENT MEASURES 4 INCH LONG BETWEEN RIBS 7 AND 8, 35 INCHES FROM INBD EDGE, 5 1/2 INCHES BELOW PAINTED SURFACE, AND 5/32 INCH DEEP. REMOVED DAMAGE AND REPAIRED DENT ON RT NR 1 LEADING EDGE SLAT BETWEEN RIBS 7 AND 8, 35 INCH FRSDR 07FDEA03644Angle · mismanufacturedLESS EDGE MARGIN (5-6 MM) AT ANGLES STRG 26 RT AT FRAME 69 AND STRG 26 LT FRAME 63 AND 65. IT'S IMPOSSIBLE TO INSTALL DAN5-6X OR DAN5-8 FASTENER DURING PTOF. REPAIR PERFORMED BY INSTALLING REPAIR ANGLES FABRICATED IN EFW-DRS (RE0074-201/RE0074-200) IAW SRM 5SDR 07FDEA03642Fitting · crackedCRACKED ATTACHMENT HOLES IN CORNER PROFILE AT FRAME 25A BETWEEN STRG. 28-34 RT. REPLACEMENT OF CORNER PROFILE IAW SRM 51-72-10 AND PTOF DRW, R255B0061.SDR 07FDEA03641Fitting · crackedCRACKED ATTACHMENT HOLES IN CORNER PROFILE AT FRAME 25A BETWEEN STRG 28-34 RT. REPLACEMENT OF CORNER PROFILE IAW SRM 51-72-10 AND PTOF DRW, R255B0061.SDR 07FDEA03634Bracket · crackedCRACKED BRACKET AT FRAME 19, STRG 50 LT. REPLACEMENT OF BRACKET IAW SRM 51-72-10.SDR 07FDEA03633Bracket · crackedCRACKED BRACKET AT FRAME 19, STRG 49 LT . REPLACEMENT OF BRACKET IAW SRM 51-72-10.SDR 07FDEA03632Bracket · crackedCRACKED BRACKET AT FRAME 19, STRG 46 LT. REPLACEMENT OF BRACKET IAW SRM 51-72-10.SDR 07FDEA03663Fitting · damagedFOUND MISDRILLED HOLE IN CORNER FITTING ADJACENT AND LESS MARGIN TO ROLLER TRACK HOLE, FRAME 60, CARGO FLOOR STRUCTURE, Y1460 LT. REPAIR PERFORMED BY CREATING AN OBLONG HOLE AND INSTALLING FASTENER WITH STRENGTHENING PLATE IAW 6-5317-95859 AND RAS/DAHAM/40202SDR 07FDEA03662Door Frame · damagedTOOLING IMPACTS FOUND ON DOOR FRAME 14 UNDER DOOR STOP 8 LH, PAX DOOR 1. REPAIR PERFORMED BY SMOOTH BLEND OUT, DVI INSPECTING OF FASTENER HOLES AND HFEC INSPECTION OF BLENDED AREAS FOR CRACK FREE CONDITION IAW EA 6-5312-95486 AND RAS 041687/013/2005 ISSUE A.SDR 07FDEA03659Frame · dentedTOOL IMPACT CAUSES DENT IN FRAME 71, STRG 15 RHS. SPLICE REPAIR PERFORMED IAW SRM 53-10-13 / PG 210, 213 / FIG 203.SDR 07FDEA03658Frame · dentedTOOL IMPACT CAUSES DENT IN FRAME 70, STRG 15 RHS. SPLICE REPAIR PERFORMED IAW SRM 53-10-13 / PG 210, 213/FIG 203.SDR 07FDEA03656Frame · corrodedHEAVY CORROSION FOUND ON THE T-SECTION AT FRAME 92, BETWEEN STRG 19-23 LT (TAILCONE). REPAIR PERFORMED BY CUT OUT THE T-SECTION AND INSTALLING NEW PORTION AND REPAIR ANGLES IAW EA 6-5319-92229 AND RAS/DAHAM/4020157/2005 ISSUE B.SDR 07FDEA03653Floor Support · corrodedHEAVY CORROSION ON FLOOR SUPPORT BETWEEN FRAME 14-17, STRINGER 26, Y-1959 RT. REPAIR PERFORMED BY REINFORCING WITH ANGLE IAW SRM 53-12-15/FIG 207.SDR 07FDEA03651Fitting · damagedMISDRILLED HOLE IN CORNER FITTING FRAME 54.1 RT DUE TO FAILED INSTALLED ROLLERTRACK ON CARGO FLOOR STRUCTURE. REPLACEMENT OF CORNERFITTING IAW SRM 51-72-10.SDR 07FDEA03650Angle · failedLESS MARGIN AT ONE HOLE AT FRAME 59, STRG 26 LT. NEW SUPPORT CAN'T BE INSTALLED BETWEEN FRAME 59 AND SEAT TRACK AS PER DRW, R539H0112. REPAIR PERFORMED BY INSTALLING REINFORCING PLATE WHICH IS FIXED WITH HI-LOK'S DAN5-5 IAW, SRM 51-72-10 AND EFW DD-0467024SDR 07FDEA03648Skin · corrodedHEAVY CORROSION UNDER ANTI-CHAFING PLATE ON SKIN PANEL BETWEEN FRAME 92-94, STRG 9-13 LT AND RT, OUT OF LIMIT. REPLACEMENT OF BOTH SKIN-PANELS (FABRICATED BY EFW-DRS) IAW SRM 51-72-10.SDR 07FDEA03647Stringer · damagedSEVERAL MISDRILLED HOLES ON STRINGER 33 RT BETWEEN FRAME 69-70. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201 / SEC "C-C".SDR 07FDEA03645Skin · dentedDENT IN BOTTOM SKIN OF LT ELEVATOR TRAILING EDGE (30X30X1,5). REPAIR PERFORMED IAW SRM 55-21-11/CONFIG 1/PARA 5D/FIG 204.SDR 07FDEA03637Plate · crackedCRACKED SHEAR PLATES BETWEEN FRAME 79-80/82, STRG 26 LT AND RT. REPLACEMENT OF BOTH SHEAR PLATES IAW SRM 51-72-10.SDR 07FDEA03631Skin Panel · chafedCHAFING MARKS FOUND AROUND MANHOLE 9 APERTURE ON THE UPPER SURFACE OF THE BOTTOM WING SKIN PANEL NR 2 BETWEEN RIB 14-15, BOTH WINGS. REPAIR PERFORMED BY SMOOTH BLEND OUT, NDT INSPECTION FOR CRACK FREE AND FILLING BLEND LEVEL RESIN IAW EA 6-5720-92205 AND RAS/SDR 07FDEA03616Skin · corrodedFOUND SKIN BULGE (CORROSION) ON LEADING EDGE OF RT WING INBOARD FLAP, NEAR TO TRACK 1. REPLACEMENT OF L/E SKIN AT FLAP IAW SRM 51-72-10.SDR 07FDEA03615Tube · crackedDAMAGED (CRACKED) TUBE ASSY BETWEEN FRAME 24-25, STRG 52 RT. REPLACEMENT OF TUBE ASSY IAW SRM 51-72-10.SDR 07FDEA03628Stringer · corrodedCORROSION ON STRINGER 53, 54 AND 55 LHS BETWEEN FRAME 70-71. STRINGER SPLICE REPAIRS PERFORMED IAW SRM 53-10-14/FIG 201.SDR 07FDEA03627Web · damagedFOUND DAMAGED WEB PLATE BETWEEN FRAME 86-87, STRG 36 LT. REPLACEMENT OF WEB PLATE IAW SRM 51-72-10 AND SRM 53-19-18/PG 76/ ITEM 40.SDR 07FDEA03626Web · damagedFOUND DAMAGED WEB PLATE BETWEEN FRAME 86-87, STRG 39 RT. REPLACEMENT OF WEB PLATE IAW SRM 51-72-10 AND SRM 53-19-18 / PG 76 / ITEM 10.SDR 07FDEA03625Web · damagedFOUND DAMAGED WEB PLATES BETWEEN FRAME 86-87, STRG 33 LT AND RT. REPLACEMENT OF WEB PLATES IAW SRM 51-72-10 AND SRM 53-19-18/PG 53.SDR 07FDEA03624Fitting · corrodedCORROSION ON FITTING AT FRAME 63, STR 41-45 LT, OUT OF LIMIT. REPLACEMENT OF FITTING IAW SRM 51-72-10.SDR 07FDEA03623Longeron · misrepairedFOUND SPLICE REPAIR ON EXTRUSION BETWEEN FRAME 12A-14, Y-953 RT, MATERIAL NOT CONFORM TO SRM 53-12-15/FIG 207. SPLICE REPAIR ON EXTRUSION RENEWED IAW SRM 53-12-15/FIG 207.
Back to N812FD, cancelled Feb 6, 2024