N304FE
Service difficulty reports · 283
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 = 'N304FE' 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 = 'N304FE' 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 FDEA201008303200Frame · damagedFUSELAGE INTERNAL FRAME HAS DAMAGE AT STA 1099 BETWEEN LONGERON 14R AND 15R. REPAIRED IAW E.A. 8-5310-136696,SDR FDEA201008273166Floor Panel · damagedMCC FLOOR PANEL NR 357 GC IS BROKEN. FABRICATED NEW FLOORBOARD IAW DWG SRZ 25-005, REV "H".SDR FDEA201008253131Floor Panel · crackedMCC FLOOR PANEL FROM STA 1259-1299, RBL 70-107 IS CRACKED AND DELAMINATED. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV "H".SDR FDEA201008233108Seat Track · wornMAIN CABIN SEAT TRACK SCALLOPS ARE WORN AT BS 1623; LBL 48. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED NEW SECTION IAW SRM 53-70-00, FIG 1, SHEET 2, VOL I. ALODINED AND PRIMED NEW SECTION IAW SRM 51-21-01, VOL II. FABBED AND INSTALLED SPLICE SECTIONSDR FDEA201008193050Skin · damagedFOUND A REPAIR DOUBLER ON THE R/W TIP UPPER SURFACE ON THE INBD END OF THE SPLICE STRAP THAT REQUIRES A MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED WING TIP IAW SRM 51-31-01, VOL II. REMOVED AND REPLACED TESDR FDEA201008193049Skin · damagedFOUND AN EXTERNAL DOUBLER ON THE RT WING NR 4 SLAT INNER SKIN BETWEEN STA XOS 613 AND XOS 618 THAT REQUIRES A MAJOR / MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED REPAIR AND FOUND TO BE WITHIN LIMITS IAW EO 8-510SDR FDEA201008183041Support · gougedRIGHT WING SLAT TRACK NR 6 OUTBD L/E BEARING SUPPORT FITTING IS GOUGED. REPAIRED RIB SUPPORT FITTING IAW EA 8-5720-136701.SDR FDEA201008183039Rib · corrodedNUMBER 3 RT WING SLAT CENTER SLAT TRACK RIB AFT HOLE IS PITTED. REMOVED PITTING IN HOLE IAW SRM 57-10-00, FIG 27, SHEET 3, VOL I. FINAL HOLE SIZE 0.7479, WITHIN LIMITS IAW SRM 57-10-00, FIG 27, SHEET 3, VOL I. FABRICATED BUSHING IAW SRM 57-10-00, FIG 27, SDR FDEA201008183034Rib · crackedRT WING NR 3 SLAT, INBD RIB CLOSE OUT IS CRACKED. REPAIRED IAW SRM 57-00-01, FIG 4, VOL I.SDR FDEA201008183038Motor · failedL-1 DOOR DOES NOT OPEN WHEN PNEUMATIC EMERGENCY OPS CHECK IS PERFORMED. REMOVED AND REPLACED L-1 DOOR AIR MOTOR IAW AMM 52-11-02-2. PERFORMED AIR MOTOR FUNCTIONAL CHECK IAW AMM 52-10-01/201.SDR FDEA201008173026Floorboard · damagedMAIN CABIN FLOORBOARD IS DAMAGED IN 2 AREAS FROM 755 TO FS 795; LBL 6. FABRICATED NEW FLOORBOARD AT LBL 6; FS 755 - FS 795 IAW DWG SRZ 25-005, REV "H". REMOVED TO F.O.M. AND REPLACED IAW AMM 53-21-00.SDR FDEA201008173025Floor Panel · damagedMAIN CABIN FLOOR PANEL IS DAMAGED AT THE AFT CORNER FROM BS 879 TO BS 979; RBL 8 TO LBL 8. FABRICATED NEW FLOOR PANEL FROM BS 879 - 979; RBL 8 TO LBL 8 IAW DWG SRZ 25- 005, REV "H".SDR FDEA201008173024Floor Panel · corrodedMAIN DECK FLOOR PANEL IS DELAMINATED AND CORRODED AT BS 1853; RBL 75. FABRICATED NEW FLOOR PANEL AT BS 1853; RBL 75 IAW DWG SRZ 25-005, REV "H". REMOVED PANEL TO F.O.M. AND REPLACED IAW AMM 53-21-01.SDR FDEA201008173023Floor Panel · gougedMAIN DECK FLOOR PANEL IS GOUGED WITH DAMAGED CORE AT BS 1831; RBL 72. FABRICATED NEW FLOOR PANEL AT BS 1831; RBL 72 IAW DWG SRZ 25-005, REV "H". REMOVED PANEL TO F.O.M. AND REPLACED IAW AMM 53-21-01.SDR FDEA201008173022Floor Panel · separatedMAIN CABIN FLOOR PANEL AT BS 1853; LBL 20 IS SEPARATED. FABRICATED NEW FLOOR PANEL AT BS 1853; LBL 20 IAW DWG SRZ 25-005, REV "H".SDR FDEA201008173021Floorboard · delaminatedMAIN CABIN FLOORBOARD IS DELAMINATED FROM BS 1996 TO BS 2007; LBL 53. FABRICATED NEW FLOORBOARD AT BS 1996; LBL 53 IAW DWG SRZ 25-005, REV "H".SDR FDEA201008173020Floor Panel · delaminatedMAIN CABIN FLOOR BOARD IS DELAMINATED FROM BS 1761 TO BS 1821; RBL 18. FABRICATED NEW FLOOR PANEL AT BS 1821; RBL 18 IAW DWG SRZ 25-005, REV "H". REMOVED PANEL AND REPLACED IAW AMM 53-21-00.SDR FDEA201008173019Floorboard · delaminatedMAIN CABIN FLOORBOARD IS DELAMINATED FROM BS 979 TO BS 1099; BL 0. FABRICATED NEW FLOORBOARD AT BS 1099 - BS 979; BL 0 IAW DWG SRZ 25-005, REV "H". REMOVED AND REPLACED IAW AMM 53-21-00.SDR FDEA201008173018Floor Panel · delaminatedMAIN CABIN FLOOR PANEL IS DELAMINATED AT BS 735; LBL 80. FABRICATED NEW FLOOR PANEL AT BS 735; LBL 80 IAW DWG SRZ 25-005, REV "H". REMOVED PANEL TO F.O.M AND REPLACED IAW AMM 53-21-01.SDR FDEA201008173017Floor Panel · delaminatedTAIL CONE LT UPPER WORK PLATFORM ACCESS DOOR FLOOR PANEL IS DELAMINATED. CRACKED AND MISSING EDGE MATERIAL. FABRICATED NEW TAIL CONE ACCESS FLOOR PANEL IAW DWG SRZ 25-005, REV "H". REMOVED AND INSTALLED ACCESS FLOOR PANEL IAW SRM 51-31-01, VOL II.SDR FDEA201008132991Hinge · wornCENTER CARGO DOOR FORWARD HINGE ON AIRFRAME SIDE FIRST 2 LOBES ARE WORN BEYOND MAX 0.343 LIMIT. REPAIRED CENTER PIT DOOR FWD HINGE ON THE AIRFRAME AIDE IAW MD/DC10 SRM 52-10-00, FIG 8, SHEET 1, VOL I.SDR FDEA201008122961Seat Track · wornMAIN CABIN SEAT TRACK SCALLOPS ARE WORN AT BS 1059; LBL 48. CHECKED SEAT TRACK AT BS 1059, LBL 48 AND FOUND OUT OF LIMITS IAW SRM 35-70-00, FIG 5 GENERAL NOTE 7. REPAIRED AREA IAW SRM 53-70-00, FIG 1, VOL I.SDR FDEA201008122964Angle · corrodedLOWER CTR CARGO PIT CLOSEOUT ANGLE HAS CORROSION AT STA 1781; RBL 36-56. REMOVED CORROSION. ORIGINAL THICKNESS 0.063. REMAINING THICKNESS 0.033. 0.030 REMOVED - OUT OF LIMITS PER SRM 53-00-01, FIG 1-B, VOL I. LOCATED, DRILLED, DEBURRED AND COUNTERSUNKSDR FDEA201008112935Web · crackedNR 3 PYLON INSIDE COMPARTMENT 487 DL, WEB CRACKED UNDER THE FUEL LINES. REMOVED WEB 487 DL IAW SRM 51-35-01, VOL II. REMOVED DAMAGED AREA AND FABRICATED DOUBLER AND FILLER IAW SRM 54-00-01, FIG 2-B, SHEET 2, VOL I. ALODINED AND PRIMED IAW 51-21-01, VOL II. SDR FDEA201008112940Hinge · corrodedCTR CARGO DOOR HINGE INNER SURFACE HAS RUST. FOUND 4 HINGE SEGMENTS OUT OF LIMITS ON DOOR IAW SRM 52-10-00, FIG 8, VOL I. R & R HINGE SEGMENTS IAW SRM 51-33-01, VOL II AND DWG ACA0012, REV "M". BLENDED CORROSION IAW SRM 51-21-01, VOL II. R & R CTR CARGO DOSDR FDEA201008112929Skin · scratchedFUSELAGE EXTERNAL SKIN HAS A SERIES OF SCRATCHES FROM FS 465-FS 535; LONGERON 26L - LONGERON 27L. COMPLIED WITH EA 8-5330-123553.SDR FDEA201008102906Former · chafedNR 1 PYLON, PANEL 437EL, AFT SUPPORT HAS FRETTED AREAS. REMOVED DAMAGED STIFFENER AND DOUBLER IAW SRM 51-31-01, VOL II. RECEIVED NEW STIFFENER, PO 689690.1 AND FABRICATED NEW DOUBLER IAW DWG AUB7070, REV "F". ALODINED AND PRIMED IAW SRM 51- 21-01, VOL II. SDR FDEA201008092876Skin · chafedRIGHT WING INBOARD FLAP LOWER SURFACE IS CHAFED AT THE OUTBD HINGE . REPLACED RUB STRIPS IAW SRM 51-35-01, VOL II. REMOVED AND REINSTALLED PANEL ARC 3007-414 TO HAVE ACCESS IAW SRM 51-31-01, VOL II. DAMAGE ON CHAFED FLAP FOUND TO BE OUT OF LIMITS IAW SRM 57-SDR FDEA201008092878Skin · delaminatedRT WING, OTBD AILERON, LOWER SKIN, FWD L/E IS DELAMINATED. TRIMMED OUT DELAMINATED EDGE IAW SRM 57-00-01, FIG 1A, VOL I. CHECKED EDGE BLENDOUT AND MAINTAINED 2D FROM ALL ATTACH FASTENERS IAW SRM 57-00-01, FIG 1A, SHEET 1, VOL I. ALODINED AND PRIMED IAW SRSDR FDEA201008092883Beam · crackedLT OVERWING DOOR HAS A CRACKED UPPER BEAM PN ADA 0006-1. LT OVERWING DOOR IS BEING REPLACED ON N/R N01074. NO FURTHER MX REQUIRED ON THIS N/R.SDR FDEA201008092877Support Bracket · gougedLT WING, NR 2 SPOILER, INBD SUPPORT BRACKET IS GOUGED BY THE FLAP. REPAIRED GOUGED SUPPORT BRACKET IAW EA 8-5740-136702,SDR FDEA201008062864Fastener · looseNR 1 PYLON INTERIOR UPPER SPAR FASTENERS ARE LOOSE BELOW THE AFT PYLON SUPPORT LUG. (18 PLACES) R & R FASTENERS AT ACCESSIBLE LOCATION IAW DAC DWG AUB 7025, REV "AZ". R & R NUTS AT 2 EA TRAPPED FASTENERS IAW EA 8-5450-136697.SDR FDEA201008062863Spar · damagedNR 3 PYLON UPPER SPAR AT THE AFT BULKHEAD HAS (4 EA) BOLTS SPINNING (NR 5,6,7 & 9) GOING INBD TO OTBD. R & R 1 EA FASTENER AT ACCESSIBLE LOCATION IAW DWG AUB 7025, REV "AZ". R & R NUTS AT 3 EA TRAPPED FASTENERS IAW EA 8-5450-136697.SDR FDEA201008062852Case · chafedNR 3 ENGINE OTBD SIDE, A CONNECTOR BACK SHELL IS CHAFING THE STRUCTURE AT 1:00 O'CLOCK POSITION. REPAIRED CHAFED AREA IAW EM 72-23-01, REPAIR 001. RESTORED AREA IAW EM 72-23-01, REPAIR 001.SDR FDEA201008052840Floor Panel · damagedCENTER CARGO COMPARTMENT FLOOR PANEL 183 RF HAS A MISSING INSERT AND HOLE IS ELONGATED. FABBED NEW FLOOR PANEL 183 RF IAW DWG SRZ 25-005, REV "H".SDR FDEA201008052839Floor Panel · crackedCENTER CARGO COMPARTMENT FLOOR PANEL 183 MF HAS A MISSING INSERT AND PANEL IS CRACKED. FABBED NEW FLOOR PANEL 183 MF IAW IAW DWG SRZ 25-005, REV "H".SDR FDEA201008052838Floor Panel · damagedCTR CARGO COMPARTMENT FLOOR PANEL 183 JF HAS A MISSING INSERT. FABRICATED NEW FLOOR PANEL 183 JF IAW DWG SRZ 25-005, REV "H".SDR FDEA201008052837Floor Panel · damagedCENTER CARGO COMPARTMENT FLOOR PANEL 183CF HAS A MISSING INSERT. FABRICATED NEW FLOOR PANEL 183 CF IAW DWG SRZ 25-005, REV "H".SDR FDEA201008052836Floor Panel · damagedCENTER CARGO COMPARTMENT FLOOR PANEL 183 YF HAS BROKEN AND MISSING INSERTS. FABRICATED NEW FLOOR PANEL 183 YF IAW DWG SRZ 25-005, REV "H".SDR FDEA201008052835Floor Panel · damagedCENTER CARGO COMPARTMENT FLOOR PANEL 183FG NUTPLATE STRIPS ARE CORRODED ON THE LOWER SURFACE. FLOOR PANEL WAS FABRICATED ON N/R N00636.SDR FDEA201008052834Floor Panel · damagedCENTER CARGO COMPARTMENT FLOOR PANEL 183 FG HAS BROKEN INSERTS AND DRILLED. FABRICATED NEW FLOOR PANEL 183 FG IAW DWG SRZ 25-005, REV "H".SDR FDEA201008052833Floorboard · delaminatedMAIN CABIN FLOORBOARD IS DELAMINATED FROM BS 1561 TO BS 1661, LBL 90. FABRICATED NEW FLOOR PANEL IAW DWG SRZ 25-005, REV "H".SDR FDEA201008052832Floorboard · delaminatedMAIN CABIN FLOORBOARD IS DELAMINATED FROM BS 1741 TO BS 1821, LBL 90. FABRICATED NEW FLOOR PANEL BS 1741-1821, LBL 90 DWG IAW SRZ25-005, REV "H".SDR FDEA201008052831Floorboard · mismanufacturedAFT CARGO FLOORBOARD 187KF DOES NOT CONFORM TO DWG SRZ 25-011. FABRICATED NEW FLOOR PANEL 187 KF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".SDR FDEA201008052830Floorboard · mismanufacturedAFT CARGO FLOORBOARD 187JF DOES NOT CONFORM TO DWG SRZ 25-011. FABRICATED NEW FLOORBOARD 187 JF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".SDR FDEA201008052829Floorboard · mismanufacturedAFT CARGO FLOORBOARD 187HF DOES NOT CONFORM TO DWG SRZ 25-011. FABRICATED NEW FLOORBOARD 187 HF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".SDR FDEA201008052828Floorboard · mismanufacturedAFT CARGO FLOORBOARD 187GF DOES NOT CONFORM TO DWG SRZ 25-011. FABRICATED NEW FLOORBOARD 187 GF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".SDR FDEA201008052827Floorboard · mismanufacturedAFT CARGO FLOORBOARD 187FF DOES NOT CONFORM TO DWG SRZ 25-011. FABRICATED NEW FLOORBOARD 187 FF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".SDR FDEA201008052826Floorboard · mismanufacturedAFT CARGO FLOORBOARD 187EF DOES NOT CONFORM TO DWG SRZ 25-011. FABRICATED NEW FLOOR PANEL 187 EF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".SDR FDEA201008052842Floor Panel · damagedCENTER CARGO COMPARTMENT FLOOR PANEL 183AF HAS MISSING INSERTS. FABRICATED NEW FLOOR PANEL 183 AF IAW DWG SRZ 25-005, REV "H".
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