N865F
Service difficulty reports · 93
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 = 'N865F' 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 = 'N865F' 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 U2RA464AML5501Bulb · burned outEMERGENCY EXIT DISARM LIGHT INOP.SDR U2RA464M85463Access Panel · crackedNR 4 PYLON UPPER L/E CAP FAIRING HINGE IS CRACKED 2 PLACES ON OTBD SIDE.SDR U2RA464OSC18858Skin · crackedFUSELAGE SKIN CRACKED AT FS 8.000 AIR CONDITIONING CONDENSER EXHAUST DOOR CUTOUT UPPER AFT CORNER CRACK LENGTH APPROX 2".SDR U2RA464OSC18837Longeron · crackedLONGERON 35RIS CRACKED FROM STA 1343-1348 (5").SDR U2RA464OSC18449Attach Fitting · crackedFUSELAGE FRAME TO CUSP FITTING CRACKED APPROX 5" AT STA 717.75.SDR U2RA464OSC18836Longeron · crackedLONGERON 34R IS CRACKED FROM STA 1343-1349.SDR U2RA865FLP3376Skin · crackedFOUND 2 EACH CRACKS IN FUSELAGE SKIN APPROX AT STA 1760 LT SIDE MID POINT VERTICALLY. ONE CRACK APPROX 2 INCHES LONG BETWEEN L13L AND L14L AND ONE CRACK APPROX 1 INCH LONG BETWEEN L14L AND L15L. CRACKS WILL BE REPAIRED IAW DWG 53-09405-1.SDR U2RA865FLP3371Skin · damagedFUSELAGE DAMAGED BY FORKLIFT BETWEEN LONGERON 26 AND 27 AT STA 370. REPAIRED IAW DWG 53-09382-1.SDR 865FLP2936Compressor · stalledNR 1 ENGINE COMPRESSOR STALLED AT 1000 FT AND WAS SECURED. ENGINE WAS RELIT PRIOR TO LANDING. ENGINE POWER ASSURANCE RUN ON GROUND DETECTED NO DISCREPANCIES.SDR N865F1480010Panel · corrodedCOCKPIT SUBFLOOR PRESSURE PANEL EXISTING REPAIR WITH CORROSION STA -17.00 LBL 50".SDR N865F1479009Stringer · corrodedCOCKPIT SUB FLOOR STRINGER DOUBLER WITH CORROSION AT STA -117.00 CPCP 455R 0552.SDR N865F1134011Unknown · corrodedFOUND COCKPIT SUBFLOOR WITH CORROSION AT STA.-67.00 L21L CPCP455L 0552.SDR N865R1125006Unknown · corrodedCOCKPIT SUBFLOOR INNER AREA WITH CORROSION AT STA 67 L-21R CPCP 455R 0552.SDR N865R1124005Angle · corrodedCOCKPIT SUBFLOOR ANGLE WITH CORROSION AT STA 32.000 L-21R CPCP455R 0552.SDR N865R1076007Access Door · corrodedLT WING XFS 836 OUTBD L/E INNER LOWER SECTION ACCESS DOOR NR 517B JAMB WITH CORROSION CPCP 107L 0552.SDR N865F753008Skin · corrodedRUDDER ZR 168.656 LT EXTERNAL SKIN WITH CORROSION CPCP 6820 0551.SDR N865R623002Bulkhead · crackedAFT FLAT PRESSURE BULKHEAD WEB STA 1766 L11L CRACK CPCP 5730 0551.SDR N865F624003Bulkhead · crackedAFT FLAT PRESSURE BULKHEAD WEB STA 1766 L-11R-12R CRACK CPCP 5730 0551.SDR U2RA09900Downlock Switch · corrodedON LANDING AT KYIP, RT MAIN GEAR DOWN AND SAFE GREEN LIGHT WOULD NOT ILLUMINATE. FLEW BY TOWER TO SEE IF LANDING GEAR WAS DOWN. EMERGENCY VEHICLES STANDING BYE ON LANDING. AFTER ENGINE SHUTDOWN LIGHT CAME ON. COMPLIED WITH MURRAY ABNORMAL CHECK LIST. REMOSDR U2RA0990Downlock Switch · corrodedON LANDING AT KYIP-RT MAIN GEAR DOWN AND SAFE GREEN LIGHT WOULD NOT ILLUMINATE. FLEW BY TOWER TO SEE IF LANDING GEAR WAS DOWN. EMERGENCY VEHICLES STANDING BYE ON LANDING. AFTER ENGINE SHUTDOWN LIGHT CAME ON, COMPLIED WITH MURRAY ABNORMAL CHECK LIST. REMOVESDR U2RA1013Frame · corrodedDURING COCKPIT AREA CORROSION INSPECTION PER AD92-22-07 (CPCP 5), LEVEL 2 CORROSION WAS FOUND ON RT FRAME AT FS -67, L23R AND ADJACENT AREA. AFFECTED AREA IS IN PROCESS OF BEING REPAIRED.SDR U2RA1013865Frame · corrodedDURING COCKPIT AREA CORROSION INSPECTION PER AD92-22-07 (CPCP 5), LEVEL 2 CORROSION WAS FOUND ON RT FRAME AT FS -67, L23R AND ADJACENT AREA. AFFECTED AREA IS IN PROCESS OF BEING REPAIRED.SDR U2RA0809Transformer · brokenPILOTS OVERHEAD PANEL LIGHTS INOP, GLOW FUSE ON FOLLOWED BY SMOKE.SDR 0657Connector · dirtyLEFT MAIN GEAR DOWN AND LOCK SAFE LIGHTS DID NOT COME ON. PERFORMED ABNORMAL CHECKLIST. AFTER LANDING LIGHT CAME ON.SDR 0656Uplock · out of rigAFTER MAIN LANDING GEAR RETRACTION GEAR HANDLE IN THE UP POSITION, DOOR NOT LATCH LIGHT REMAINS ON. POSITION GEAR HANDLE IN THE UP-LATCH CHECK POSITION, DOOR NOT LATCHED LIGHT, GEAR NOT LATCHED LIGHT AND ALTERNATE RIGHT HAND DOOR NOT LATCHED LIGHT REMAINS ON,SDR 0378Frame · crackedDURING CPCP TASK NR 5570-0551 FORWARD LOWER CARGO COMPARTMENT FORWARD FRAME FITTING CRACKED AT FS299 BETWEEN LONGERON 32R AND 33R.SDR 0377Doubler · crackedDURING CPCP TASK 5570-0551 FORWARD LOWER CARGO COMPARTMENT INTERIOR SKIN DOUBLER CORRODED AND CRACKED AT FS270 LONGERON 31L AND IDENTIFIED AS LEVEL 2 CORROSION.SDR 0375Frame · corrodedDURING CPCP TASK 5570-0551 FORWARD LOWER CARGO COMPARTMENT CIRCUMFERENTIAL FRAME LOWER LEG CORRODED AT FS 80 BETWEEN LONGERON 36R AND 35R AND IDENTIFIED AS LEVEL 2 CORROSION.SDR 0370Fitting · crackedDURING CPCP TASK 5590-0551 AFT CARGO FS 1160 LONGERON 35R AND 34R FITTING CRACKED AND IDENTIFIED AS LEVEL 2 CORROSION.SDR 0369Clip · crackedDURING CPCP TASK 5690-0551 AFT CARGO FS 1210 LONGERON 33R CORRODED AND CRACKED 2 EACH FITTING CLIPS AND INDENTIFED AS LEVEL 2 CORROSIONSDR 0355Skin · corrodedDURING CPCP TASK 5600-0551 FOUND AFT ACCESSORY COMPARTMENT FS 1640 BETWEEN LONGERON 32R AND 33R. FASTENERS PULLING THROUGH FUSELAGE SKIN AND IDENTIFIED AS LEVEL 2 CORROSION.SDR 0354Duct · delaminatedNR 2 ENGINE LT ENGINE COWL TRANSITION DUCT DELAMINATED ON INBOARD SIDE.SDR 0479Fitting · crackedDURING FUEL TANK MAINTENANCE DETECTED LT WING NR 2 MAIN FUEL TANK CRACKED STRINGER END FITTING AT STA.XRS 78,S61.SDR 0390Hinge Fitting · crackedVISUALLY DETECTED LT OB AILERON CENTER HINGE FITTING CRACKED.SDR 0380Skin · crackedVISUALLY DETECTED CRACK IN PREVIOUS DOUBLER LEFT WING LEADING EDGE AT NR 2 ENGINE PYLON CUTOUT.SDR 0324Fitting · corrodedEXTERNAL FUSELAGE SKIN HAS A BULGE AT FS 324 LONGERON 33R FOUND DURING C-CHECK. FOUND FORWARD LOWER BELLY CARGO (A-PIT) DOOR STRUCTURE FITTING CORRODED.SDR 020104Fitting · corrodedEXTERNAL FUSELAGE SKIN HAS A BULGE AT FS 315 LONGERON 33R FOUND DURING C-CHECK. FOUND FORWARD LOWER BELLY CARGO (A PIT) DOOR STRUCTURE FITTING CORRODED-TASK CARD #0323.SDR 0471Longeron · corrodedDURING CPCP TASK NR 5570-0551 FORWARD LOWER CARGO COMPARTMENT CORROSION ON LONGERON 30L AT FS 270 AND IDENTIFIED AS LEVEL 2 CORROSION.SDR KO0R0323Fitting · corrodedEXTERNAL FUSELAGE SKIN HAS A BULGE AT FS315, LONGERON NR 33R. FOUND DOOR STRUCTURE FITTING CORRODED (FS 315, LONGERON 33R). REMOVED AND REPLACED FITTING IAW DC8, SRM 53-2-0, FIG 2D. CORROSION REMOVED IAW DC SRM 51-1-8.SDR U2RB010103Skin · crackedDURING COMPLIANCE WITH A/D 2000-20-08 AND REMOVAL OF TEMPORARY EXTERNAL REPAIR AT LEFT FRONT PAX ENTRANCE DOOR UPPER FORWARD CORNER, VISUALLY DETECTED ONE ADDITIONAL FUSELAGE SKIN CRACK TERMINATING AT RIVET FASTENER 3 FASTENERS UP FROM PREVIOUS CRACK REPAIRED SDR U2RB100102Skin · crackedDURING B-4 CHECK, FOUND RIVET POPPED AT FUSELAGE STATION -12, LEFT LONGERON NR 30. INVESTGATION REVEALED STRESS CRACK IN FUSELAGE SKIN AT RIVET HEAD. REMOVED DAMAGE SKIN, CLEANED AND TREATED IAW DC8 SRM 51-1-8 AND REPAIRED IAW DC8 SRM 53-2-0 /51-1-21 AND REFSDR U2RB070302Fitting · corrodedDURING COMPLIANCE OF BOEING S/B 53-61 R4 DURING DISASSEMBLY FOR REPLACEMENT OF CRACKED RT MLG SUPPORT FITTING DURING DISASSEMBLY FOUND RT LONGERON NR 24 FUSELAGE FRAME FITTING CORRODED.SDR U2RB070202Support Fitting · crackedDURING COMPLIANCE WITH BOEING S/B DC8-53-61 R4, VISUALLY DETECTED LEFT HAND WHEEL WELL TRAPEZOID FITTING CRACKED AND EXTENDING FROM BOLT HOLE APPROXIMATELY 2.25 INCHES.SDR U2RB070102Support Fitting · crackedDURING COMPLIANCE BOEING S/B DC8-53-061R4 VISUALLY DETECTED RT MLG SUPPORT FITTING CRACKED IN TWO PLACES. UPPER AREA .875 INCH AND AFT UPPER AREA CRACK EXTENDING UP AND OUT INTO SUPPORT FITTING FLANGE.SDR U2RB040202Floorbeam · corrodedDURING CPCP 18 MONTH INSPECTION, AFT ACCESSORY COMPARTMENT INTERIOR. DETECTED LEVEL 2 CORROSION OF UPPER TEE OF FORWARD FLANGE OF FLOORBEAM 11.5 INCHES INBOARD OF RIGHT FUSELAGE CUSP LINE 1.75 INCHES LONG.SDR U2RB050101Fitting · crackedON POST FLIGHT INSPECTION WITH NR 4 ENGINE THRUST REVERSER (T/R) TRANSLATING RING EXTENDED FOUND LOWER AFT T/R TRACK SUPPORT FITTING MOUNTED ON BOTTOM CENTER LINE OF ENGINE EXHAUST NOZZLE OUTBOARD FLANGE CRACKED THROUGHOUT BOLT HOLE.SDR U2RB030101Spar Cap · crackedDURING COMPLIANCE OF MCDONNELL DOUGLAS DC-8 S/B 57-90 R5 (NPRM 99-NM-60-AD) DETECTED CRACK ATLOWER FORWARD SPAR AT ATTACH FASTENERS STA XFS 524. CRACK BEYOND S/B 57-90 R5 REPAIR LIMITS.SDR RRXA98177Cowling · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO NR 1 ENGINE RIGHT SIDE FAN COWLING, ZEE CLOSE-OUT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-0448SDR RRXA98166Cowling · corrosionDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO NR 4 ENGINE, RIGHT SIDE AFT FAN COWLING, ZEE CLOSE-OUT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REOSDR RRXA98153Cowl · wornDURING A MAINTENANCE VISIT, FOUND NR 1 ENGINE FAN COWLING, ZEE CLOSE-OUT WORN. FABRICATED AND INSTALLED NEW ZEE CLOSE-OUT, (P/N 575716-503), IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04413.
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