N670FE
Service difficulty reports · 205
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 = 'N670FE' AND registry_match = 'registration' 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 = 'N670FE' AND registry_match = 'registration' 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 FDEA201907251698Floor Panel · damagedMAIN CABIN HAS A DAMAGED FLOOR BOARD PANEL 242AJ. RECEIVED FABRICATED FLOOR BOARD 242AJ ON T19/1430522 IAW DWG SRZ-25-005. MAJOR REPAIR.SDR FDEA201907251697Floor Panel · damagedMAIN CABIN HAS A DAMAGED FLOOR BOARD PANEL 251TH. FABRICATED FLOOR PANEL ON T19/1431278 IAW SRZ-25-005 MAJOR REPAIR.SDR FDEA201907251696Floor Panel · damagedMAIN CABIN HAS A DAMAGED FLOOR BOARD PANEL 251BF. RECEIVED FABRICATED FLOOR BOARD 251BF ON T19/1430531 IAW DWG SRZ-25- 005. MAJOR REPAIRSDR FDEA201907251693Floor Panel · damagedFWD CARGO FLOOR PANEL 132MG SKIN TORN. FABRICATED FLOOR PANEL ON T19/1430155 IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201907251692Floor Panel · brokenFWD CARGO FLOOR PANEL 132SG BROKEN. FABRICATED FLOOR PANEL ON T19/1430072 IAW SRZ-25-005 MAJOR REPAIR.SDR FDEA201907251691Floor Panel · brokenFWD CARGO FLOOR PANEL 132QG BROKEN. FABRICATED FLOOR PANEL ON T19/1430042 IAW SRZ-25-005 MAJOR REPAIR.SDR FDEA201907251690Floor Panel · brokenFWD CARGO FLOOR PANEL 132KG BROKEN. FABRICATED FLOOR PANEL ON T19/1430148 IAW SRZ 25-005 MAJOR REPAIR.SDR FDEA201907241680Floor Panel · damagedFWD CARGO FLOOR PANEL 131PG BROKEN. FABRICATED FLOOR PANEL ON T19/1430053 IAW SRZ 25-00-05 MAJOR REPAIR.SDR FDEA201907241683Floor Panel · damagedFWD CARGO FLOOR PANEL 131NG BROKEN. FABRICATED FLOOR PANEL ON T19/1430055 IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201907241682Floor Panel · damagedFWD CARGO FLOOR PANEL 131SG CORNER CRUSHED. FABRICATED FLOOR PANEL ON T19/1430060 IAW SRZ 25-005. MAJOR REPAIR.SDR FDEA201907241681Floor Panel · damagedFWD CARGO FLOOR PANEL 131QG CORNER CRUSHED. FABRICATED FLOOR PANEL ON T19/1430050. IAW SRZ 25-005. MAJOR REPAIR.SDR FDEA201907241679Floor Panel · damagedFWD CARGO FLOOR PANEL 131RG CORNER BROKEN. FABRICATED FLOOR PANEL ON T19/1430077 IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA2019072501644Floor Panel · delaminatedFLOOR PANEL 221PF DELAMINATED FABRICATED COURIER FLOOR PANEL 221PF ON VT MAE TRAVELER # T19/1430367 IAW DWG SRZ 25-005 CLASS "A" MAJOR REPAIRSDR FDEA2018100252710Switch · failedPDIS 670 78-30 9159 25SEP18 MEM FACT U LOGPAGES:2122353 ENG 1 REV. PRESSURIZED ECAM MSG. IN FLIGHT. ALL ENGINE INDICATIONS NORMAL. FACT 25SEP18 17:12 MEM R&R'D NR 1 ENG LT AND RT T/R CDU SWITCH ASSEMBLIES IAW AMM 78-31-04-04. OPS CHECKS GOOD. RAN ENGINE ASDR FDEA2018091852547Wire Harness · failedON DEPARTURE, PASSING ABOUT 1000' ECAM WARNING NR 1 ENG REVERSER PRESSURIZED. FOLLOWED ECAM/QRH, DECLARED EMERGENCY AND RTB. REMOVED AND REPLACED NR 1 ENG LT T/R HARNESS CHANNEL B GOING TO LT RVDT AND PILOT VALVE PRESS SWITCH IAW MM 70-71-01-00 AND ASM 78-31-0SDR FDEA2018091062419Holder · out of positionON APPROACH TO KLCK, NOTICED SMOKING COMING FROM CAPTAINS YOKE LIGHT WITH LIGHT ON. TURNED LIGHT OFF SMOKE STOPPED. FOUND PLASTIC TIP OF RT SIDE CHART HOLDER EXTENSION CABLE HAD AT SOME POINT BEEN STUCK INTO CHART HOLDER LIGHT BULB MELTING ONTO THE BULB. REMOSDR FDEA2018073091848Processing Unit · faultedON TAKEOFF AFTER GEAR RETRACTION LOST PITCH TRIM 1, 2 ATS, PRESSURE REG 1 AND 2 AND SEVERAL PITOT STATIC PROBE LIGHTS. COMPLIED QRH, MANUAL PRESSURIZATION. COULD NOT RESET AT FIRST. APPROX 5 MIN LATER WE COULD RESET PITCH TRIM AND ATS, ATB. PERFORMED TROUBLESHSDR FDEA201710283090Warning System · false activationREPEAT WRITEUP, L1 ENTRY DOOR RED LIGHT FLASHING WITH WARNING HORN BLARING AND HIGH PITCH SQUEAL. COCKPIT INDICATIONS NORMAL. CABIN PSI 8.3. COULD NOT DUPLICATE WRITE UP. DOOR ARMS NORMALLY AND WARNING SYSTEM LIGHT AND HORN OPS NORMAL PER MM 52-73-00-00-02.SDR FDEA201704271282Line · chafedABOUT 20 MINUTES AFTER TAKEOFF YELLOW SYSTEM HYDRAULICS PRESSURE AND QUANTITY FAILED ON ECAM AND OVERHEAD. FOLLOWED ECAM AND QRH PROCEDURES AND RETURNED. R & R A CHAFED YELLOW SYSTEM RT WING SUPPLY FLEX LINE IAW MM 29-00-00-04. CHECKED NORMAL, .ACCOMPLISHEDSDR FDEA201704091121Skin · damagedWHILE PERFORMING THERMOGRAPHY INSP. OF RUDDER SIDE SHELLS IAW WORK CARDS E 6- 5540-E0319362P1 & 55400090-00-11, 1 EA AREA OF FLUID INGRESS DETECTED AT R/H SIDE FWD OF FASTENER #20 AS MARKED (FLUID INGRESS WAS VERIFIED WITH U.T. INSP. NTM PT. 4, 51- 10-24. SDR FDEA201704071112Floorboard · damagedMAIN CABIN FLOORBOARD 241HK HAS IMPACT DAMAGE AND DAMAGED INSERTS. FABRICATED A NEW MAIN CABIN FLOORBOARD IAW DWG SRZ 25-005. MAJOR REPAIR.SDR FDEA201703311024Skin · chafedLT WING O/B FLAP I/B BULLNOSE SKIN CHAFFED. REPAIRED LT WING O/B FLAP I/B BULLNOSE SKIN IAW SRM 57-50-00 FIG 208, MAJOR REPAIR.SDR FDEA201703291002Floor Panel · damagedBULK CARGO FLOOR PANEL 161GF IS MISSING ONE INSERT AND THE METAL SKIN IS DISBONDED AT THE SIDE CUTOUT. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005, AND SRZ-25-01. MAJOR REPAIR.SDR FDEA201606302242Control Unit · malfunctionedR1 DOOR ESCAPE SLIDE ARMED, INDICATION NOT SHOWING ON ECAM. RESET AND OPS CHECK OF THE AUTONOMOUS STANDBY POWER SUPPLY UNIT, ASPSU.SDR FDEA201410052971Splice · crackedONE EACH CRACK INDICATION WAS FOUND AT THE LT J HOLE OF THE FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGER 24 & 26 IAW AB6 NTM 51-10-01 PART 1. REWORKED THE HOLE & INSTALLED BUSHING IAW EA 6-5310-T0311900. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201410022907Mount Fitting · corrodedENG 1 PYLON TO ENG FWD MOUNT FITTING LT AFT HOLE SURROUND UPPER SURFACE GOT CORROSION, BOLT HEAD SURROUND AREA. IAW EA 6-5450-T0311918 REPAIRED. NACELLES PYLON STRUCTURES NR 1 PYLON FWD MOUNT AFT HOLE CORROSION IAW GMM 6-2-100 REPAIR CLASSIFIED MINOR.SDR FDEA201410022906Mount Fitting · corrodedNUMBER 1 PYLON TO ENG FWD MOUNT FITTING RT AFT HOLE SURROUND UPPER SURFACE GOT CORROSION, BOLT HEAD SURROUND AREA. IAW EA 6-5450-T0311918 REPAIRED. NACELLES PYLON STRUCTURES NR 1 PYLON FWD MOUNT AFT HOLE CORROSION IAW GMM 6-2-100 REPAIR CLASSIFIED MINOR.SDR FDEA201410022905Mount · corrodedENG 1 PYLON FWD MOUNT MATING FACE LT AFT HOLE EDGE GOT MINOR CORROSION. IAW EA 6-5450-T0311918 REPAIRED. NACELLES PYLON STRUCTURES NR 1 PYLON FWD MOUNT AFT HOLE CORROSION IAW GMM 6-2-100 REPAIR CLASSIFIED MINOR.SDR FDEA201408012030Rib · corrodedLEFT RIB 5 FWD LUG HAS CORROSION IN BORE, FWD & AFT FACES COMPLIED WITH EA 6-5710-T0310153 P 1 WINGS BASIC WING STRUCTURE LT & RT RIB 5 BORE CORROSION.SDR FDEA201408012029Rib · corrodedRIGHT RIB 5 FWD LUG HAS CORROSION IN BORE, FWD & AFT FACES COMPLIED WITH EA 6-5710-T0310153 P 2 WING BASIC WING STRUCTURE LT & RT RIB 5 BASIC CORROSION.SDR FDEA201403230548Transmitter · leakingHAD A TOTAL LOSS OF SYS GREEN HYDRALIC FLUID IN FLIGHT. MANUALLY EXTENDED GEAR. INSPECTED MAIN WHEEL AREA, FOUND PRESSURE TRANSMITTER LEAKING, HYD RESERVIOR NEVER WENT COMPLETELY EMPTY. REPLACED GREEN HYDRAULIC PRESSURE TRANSMITTER IAW AMM 29-32-13-04, OPSSDR FDEA201212134290Window · crackedON DEPARTURE, THE CAPTS WINDSHIELD BEGAN ARCING THEN CRACKED. FOLLOWED ECAM PROCEDURES. WHEN WINDOW HEAT TURNED OFF THE WINDOW CRACKED. R & R CAPTAINS WINDSHIELD IAW MM 56-11-11-04.SDR FDEA201204121379Fairing · crackedNR 1 ENGINE PYLON LOWER AFT FAIRING ASSY, LT AFT ATTACH LUG AT RIB 18 CRACKED. REPAIRED IAW DWG R54610384 ISSUE A COMPLIED WITH EA 6-5450-160114, PT1.SDR FDEA201204121378Skin · dentedLEFT WING NR 1 SLAT BOTTOM SKIN SURFACE HAS A DENT MEASURING 0.75"X 1.30"X 0.60" DEEP. DENT FOUND TO BE OUT OF LIMITS IAW FSRM 57-40-00, PG 103. REPAIRED DAMAGE IAW EA 6-5750-160116.SDR FDEA201204091330Crossbeam · corrodedON REMOVAL OF SEAT TRACK 3L AT FR 26 TO 35, FOUND CORROSION ON FR 32 CROSSBEAM, EXTENDING UNDER CLEVIS ADAPTER. AFTER REMOVAL OF LEVEL 1 CORROSION ON UPPER SURFACE OF CROSSBEAM AT FR 32, IAW SRM 51-74-10, IT WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15, FIGSDR FDEA201204081297Crossbeam · damagedMDCC AFTER REMOVAL OF SEAT TRACK 4R FR 40-44 FOUND CROSSBEAM AT FR 40 BETWEEN TRACKS 3R AND 4R DAMAGED. FABRICATED NEW CROSSBEAM IAW DWG 53812969. REMOVED AND REPLACED CROSSBEAM IAW FSRM 51-40-21, PARA 6.SDR FDEA201204061276Skin · crackedNR 1 ENGINE PYLON, AFT LOWER FAIRING, LOWER SKIN CRACKED 2 INCHES INCHES LONG, AROUND HYD RESERVOIR PRESSURIZATION LINE HOLE CUT OUT BETWEEN PYLON RIB 19 - 20. REMOVED CRACKED WEB ASSY AND INSTALLED NEW WEB ASSY ON NR 1 ENGINE LOWER AFT PYLON AREA BETWEEN RIB SDR FDEA201204031234Seat Track · corrodedMDCC SEAT TRACK 4R AT FR 42 6 IN. HAS 2 SQ. IN OF CORROSION INSIDE SCALLOP AREA. AFTER REMOVAL OF LEVEL 1 CORROSION INSIDE SCALLOP AREA ON SEAT TRACK 4R, FR 42 6IN IAW SRM 51-74-10, PG 205, FOUND AREA TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 102. R & R SEAT SDR FDEA201203311207Seat Track · corrodedSEAT TRACK 5L AT FR 43. HAS 4 X 2 SQUARE INCHES OF CORROSION INSIDE SCALLOP AREA. R & R SEAT TRACK, REPROTECTED AREA IAW SRM 51-23-20, PG 5.SDR FDEA201203311205Seat Track · corrodedSEAT TRACK 5R AT FR42, 4 X 3 SQUARE INCHES OF CORROSION IN SCALLOP AREA. REMOVED CORROSION IAW SRM 51-74-10, PARA 5. DAMAGE AREA MEASURED L=5.9" X W=1" MATERIAL LOSS .072 MAX ALLOWED .040 & FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 102. REMOVED DAMASDR FDEA201203311203Seat Track · corrodedMDCC SEAT TRACK 1 CENTER LINE AT FR. 43 1" OF CORROSION. REMOVED CORROSION IAW SRM 51-74-10 PAR.5, FOUND TO BE OUT OF LIMITS MAT LOSS .067 IAW SRM 53-16-10, FIG 102. REMOVED DAMAGE SEAT TRACK IAW SRM 51-40-21. LOCATED, DRILLED AND INSTALLED NEW SEAT TRACK ISDR FDEA201203301199Seat Track · crackedSEAT TRACK 3L AT FR. 43 HAS 9X2 SQUARE INCHES OF CORROSION ON INSIDE OF SCALLOP. REMOVED CORROSION ON SEAT TRACK 3L AT MDCC IAW SRM 51-74-10, FOUND A .5" CRACK IN SCALLOP, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 101. REMOVED TRACK 3L ON MDCC FROM FR SDR FDEA201203291192Skin · gougedAFT CARGO DOOR SURROUND SKIN AT LOWER FORWARD CORNER SKIN EDGE HAS 2 AREAS GOUGED (1) 1" X .5", (2) 2.5" X .6250".SDR FDEA201203291171Floor Support · corrodedMDCC FLOOR THRUST PLATE BETWEEN FR 30 TO 31 AND SEAT TRACKS 5R TO 6R UPPER SURFACE HAS 3 EA AREAS OF CORROSION. MEASURED 1 SQ", 2 SQ", AND 2 SQ". REMOVED CORROSION IAW SRM 51-74-10 AND FOUND TO BE OUT OF TOLERANCES IAW SRM51-73-11 AND DWG AIB STANDARD MASDR FDEA201203291196Floorboard · damagedFLOORBOARD 252PH, HAS AN AREA OF DAMAGED HONEYCOMB AND DELAMINATING SKIN APPROX 6' LONG BY 10" WIDE . CUT OUT "LEG" IS ALSO CRACKED FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201203291175Floor Support · corrodedCARGO BAY FR 67, FLOOR SUPPORT HAS 2 SQUARE INCHES OF CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15 FIG. 104 PG 113/114. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51- 72-10 AND 51-40-21 PARA'S 6 AND 7.SDR FDEA201203281169Stiffener · crackedFORWARD CARGO PIT OVERHEAD FRAME 35 LT SIDE BETWEEN SEAT TRACKS 4L AND 5L AT FWD FACE MILLED STIFFNER, HAS .2500 CRACK AT UPPER RADIUS. INSTALLED FABRICATED STIFFNER AT FORWARD CARGO PIT O/H FR 35 LT SIDE BETWEEN SEAT TRACKS 4L AND 5L AT FWD FACE IAW SRM 53-1SDR FDEA201203281168Floorboard · crackedFLOORBOARD 232CF HAS ONE, NINE INCH CRACK AND CRUSHED AREA. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005 REV JSDR FDEA201203271156Seat Track · corrodedBETWEEN FR 71 & FR 72 RT SIDE SEAT TRACK 3R HAS CORROSION INSIDE OF SCALLOP AND ON TOP. REMOVED CORRODED SEAT TRACK IAW SRM 51-40-21AND FABRICATED NEW SEAT TRACK IAW DWG A532-78433, INSTALLED NEW SEAT TRACK MDCC BETWEEN FR 71 & FR 72 3R IAW SRM 51-40-21.SDR FDEA201203271154Seat Track · corrodedSEAT TRACK 5R (Y-1959), FROM FRAME 45, 7 IN TO FRAME 54, 7EA PLACES WITH 1 SQ" OF CORROSION AT EACH LOCATION.
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