N901FD
Service difficulty reports · 172
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 = 'N901FD' 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 = 'N901FD' 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 FDEA200711074750Stringer · damagedS26L HAS MINOR DAMAGE ON FREE FLANGE BETWEEN STA 510 AND 560. REMOVED DAMAGED SECTION OF STR IAW SRM 53-00-03, REPAIR NR 2. FABRICATED 2 STRINGER SPLICES. FABRICATED 3 SHIMS IAW SRM 53-00-03. TREATED AND PRIMED STRINGER SPLICES, SHIMS AND STRINGER CLIP IAWSDR 07FDEA04751Stringer · corrodedBULK CARGO AREA STA 1510 - S29R - AREA ON STRINGER EXFOLIATED. BLENDED AREA IAW SRM 53-60-03 FIG NR 101 DETAIL 1 STA 1510 S29R. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-03, L 3.0" BY W 2.0" BY D .039". REMOVED DAMAGED STR STA 1510 IAW SRM 53-00-03. REMOVSDR 07FDEA04750Stringer · damagedS26L HAS MINOR DAMAGE ON FREE FLANGE BETWEEN STA 510 AND 560 REMOVED DAMAGED SECTION OF STRINGER IAW SRM 53-00-03 REPAIR NR 2. FABRICATED 2 STRINGER SPLICES FROM BAC 1498-294 BATCH 3332A6. FABRICATED 3 SHIMS FROM 7075 T6 .025 BATCH 1256022 IAW SRM 53-00-03. SDR 07FDEA04710Fitting · damagedRT WING I/B LOAD FITTING HAS 3 FASTENER HOLES DAMAGED COMMON TO THE SIDE LOAD FITTING. REF S/B 757-54-0035 FIG 7, PANEL 3, STEPS 2 AND 3 IAW EA NR F-5450-108908, REAMED EACH HOLE TO REMOVE DAMAGE. ACCOMPLISHED BHEC OF THE REWORKED HOLES PER 757 NDT MANUAL D6SDR 07FDEA04705Frame · corrodedUPPER LOBE STATION 700 FRAME, BELOW STRINGER 1L IS CORRODED. REMOVED CORR ON BS 700 FRAME IAW SRM 53-00-07. ORIGINAL MATERIAL THICKNESS WAS .063". MATERIAL REMOVED WAS .018". MATERIAL REMAINING WAS .046", OUT OF LIMITS PER SRM 53-00-07. FABRICATED REPAIRSDR 07FDEA04561Seat Track · misalignedFS 377-440, LBL 45.5, SEAT TRACK ASSY REPLACE PER CUSTOMER REQUEST. REMOVED SEAT TRACK ASSY FROM FS 377-440, LBL 45.5, PER SRM 51-40-02. FABRICATED SEAT TRACK ASSY ON MAE FAB SHOP TRAVELER NR T7/704367, PART NUMBER FX-51-10-02-N567. LOCATED AND DRILLED SESDR 07FDEA04560Seat Track · misalignedFS 377-440, LBL 24.75, SEAT TRACK REPLACED PER CUSTOMER REQUEST. REMOVED SEAT TRACK ASSY AT FS 377-440, LBL 24.75 IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK ASSY ON MAE FAB SHOP TRAVELER NR T7/704366 AND SRM 51-10-02. PART NUMBER OF FABRICATED SEAT TRACK ASDR 07FDEA03950Skin · misrepairedFLUSH REPAIR ON L/E OF NR 5 SLAT DOES NOT COMPLY WITH SRM. REMOVED AND REPLACED REPAIR ON NR 5 L/E SLAT IAW SRM 57-43-01, FIG 201. FABRICATED REPAIR FILLER, HEAT TREATED TO T6 ON MAE TRAVELER T7/696092. FABRICATED DOUBLER AND SPLICES, HEAT TREATED ON MAE SDR 07FDEA03793Fitting · wornLEFT WING DIAGONAL BRACE ATTACH FITTING (WING SIDE) HAS MIGRATING BUSHINGS. REMOVED, FABRICATED AND REPLACED MIGRATED BUSHINGS IN ACCORDANCE WITH FEDEX EA NR F-5720-110765, DATED 7/30/2007 AND MAE TRAVELER NR T7/695654. CLASSIFIED AS A "MAJOR REPAIR" WITH NSDR 07FDEA03792Fitting · wornRIGHT WING DIAGONAL BRACE ATTACH FITTING (WING SIDE) HAS MIGRATING BUSHING. REMOVED, FABRICATED AND REPLACED MIGRATED BUSHINGS IN ACCORDANCE WITH FEDEX EA NR F-5720-110765, DATED 7/30/2007 AND MAE TRAVELER NR T7/695654. CLASSIFIED AS A "MAJOR REPAIR" WITH NSDR 07FDEA03232Skin · corrodedNR 2 STRUT, RIGHT SIDE SKIN AT APPROXIMATE PP STA 182 HAS CORROSION ON SKIN AND UNDER LOWER FRAME. CORROSION WAS REMOVED FROM SKIN, AND FOUND OUT OF LIMITS PER SRM 54-50-01. CONTACTED ENGINEERING AND WAS PRESENTED EA NR F-5450-110764A FOR CORRECTIVE ACTIONSDR 07FDEA03056Skin Panel · damagedLT SIDE OF FUSELAGE HAS A DIVOT IN SKIN AT BS 726, APPROXIMATELY 5" ABOVE STRINGER 23L. MEASURED AND EVALUATED DAMAGE IAW SRM 53-00-01, FIGURE 101, DETAIL 2 AND SRM 53-00- 01, FIGURE 201, SECTION 1, PARA 2.C. L = 1.0", W = .700", D = .013". OUT OF LIMITS IAWSDR 07FDEA03054Skin Panel · damagedLT SIDE OF FUSELAGE HAS A DIVOT IN THE SKIN AND RUNNING INTO A RIVET AT STATION 700, APPROXIMATELY 5" ABOVE STRINGER 23L. MEASURED THE DAMAGED AREA PER SRM 53-00-01 AND SRM 53-00-01. OUT OF LIMITS IAW SRM 53-30- 01. ACCOMPLISHED REPAIR IAW EA F-5310-110755SDR 07FDEA02963Skin · corrodedNR 2 STRUT, RT SIDE, SIDE SKIN AT APPROXIMATELY NAC STA 144 INTERNAL, IS CORRODED ON SKIN AND UNDER LOWER FRAME/CHORD. REMOVED CORROSION FROM INTERNAL SKIN AS MARKED PER SRM 54-50-01. ORIGINAL SKIN THICKNESS (DOUBLER SIDE) .090", AFTER REWORK .075" AT LOWESDR 07FDEA02871Bushing · misalignedACCOMPLISHED DVI OF THE LT WING OUT BOARD DRAG FITTING AND FOUND THE INBOARD SIDE BUSHING MIGRATED .060 INCH. REMOVED BUSHINGS IAW SOPM 20-50-03. HFEC INSPECTED FITTING IAW NTM 51-00-16, PT.6. NO DEFECTS NOTED. HONED, CHAMFERED AND FLAP PENNED LUG BORES IASDR 07FDEA02869Bushing · misalignedRT WING OUTBOARD UPPER LINK FITTING HAS MIGRATING BUSHINGS. REMOVED BUSHINGS PER SOPM 20-50-03. INSPECTED FITTING PER NTM 51-00-00, PT.6, NO DEFECTS NOTED. HONED, CHAMFERED FLAP PEENED AND SWAGED PER F-5450-108892 FINAL DIA OF THE LUG BORE IS 1.7507. TRESDR 07FDEA02825Skin · corrodedNUMBER ONE STRUT/PYLON, LT SIDE SKIN, AT APPROXIMATE NAC STA 144, INTERNAL, IS CORRODED ON SKIN AND UNDER LOWER FRAME/CHORD. REMOVED CORROSION IAW SRM 54-50-01. ORIGINAL MATERIAL THICKNESS WAS .090", AFTER REWORK REMAINING MATERIAL THICKNESS WAS .079", OUT OSDR 07FDEA02518Stringer · damagedAFT PIT - BS 1640 S27L, DRILL MARKS IN STRINGER (4 EACH HOLES) BLENDED DRILL MARKS ON STRINGER 27L IAW SRM 53-00-03. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, FIG 101, SHEET 1. NO HOLES ALLOWED. REMOVED DAMAGE IAW SRM 53-00-03, FIG 201. FABRICATED REPAIRSDR 07FDEA02517Skin · corrodedBULK CARGO - BILGE AREA, BS 1580, BETWEEN S27R AND 28R, SHEAR TIE AND SKIN EXFOLIATED. REMOVED AND REPLACED SHEAR TIE AS IT HAD 100 PERCENT MATERIAL LOSS IAW SRM 51-40-02. SHEAR TIE WAS FABRICATED ON MAE TRAVELER T7/689492 IAW SRM 51-10-01. REMOVED CORROSIOSDR 07FDEA02509Stringer · damagedAFT PIT, STATION 1660 AT STRINGER 27R, HAS TOOLING MARKS ON STRINGER. BLENDED TOOL MARKS FROM STRINGER IAW SRM 53-00-03. FOUND TO BE OUT OF LIMITS PER SRM 53-00-03, FIG 101. REMOVED DAMAGED SECTION OF STRINGER IAW SRM 53-00-03, FIG 201. FABRICATED REPAIR STSDR 07FDEA02507Skin · dentedEXTERNAL FUSELAGE HAS A LARGE DENT AT STATION 1507 ON STRINGER 2R. FOUND TO BE OUT OF LIMITS PER SRM 53-00-01, FIG 101. CUT OUT DAMAGE ON SKIN PER SRM 53-00-01, FIG 201. FABRICATED REPAIR DOUBLER. TREATED AND PRIMED DOUBLER IAW SRM 51-20-01.SDR 07FDEA02508Stringer · damagedAFT PIT, BS 1660, S26R DAMAGED. BLENDED DAMAGE ON STRINGER IAW SRM 53-00-03. FOUND TO BE OUT OF LIMITS PER SRM 53-00-03, FIG 101. REMOVED DAMAGED SECTION OF STRINGER IAW SRM 53-00-03. FABRICATED REPAIR STRINGER. FABRICATED FILLER IAW SRM 53-00-03, FIG 201
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