N872SJ
Service difficulty reports · 54
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 = 'N872SJ' 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 = 'N872SJ' 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 U2RA449SPIM003Skin · corrodedRT HORIZ STAB BETWEEN XE 75.672 AND XE 147.906 T/E UPPER PANEL SKIN WITH CORROSION AROUND FASTENERS.SDR U2RA449SPIM004Drive Assy · crackedRUDDER TAB DRIVE SECTOR BROKEN.SDR U2RA449SPIM002Web · crackedFUSELAGE TAIL SECTION INTERIOR, FS 1817 TO FS 1823 UPPER WEB WITH 11" CRACK.SDR U2RA449SPIM001Skin · wornLT WING, T/E UPPER SURFACE, XRS 272 EXISTING REPAIR WITH WEAR.SDR 2009F00089Line · crackedDURING DESCENT HYD QUANITY AND PRESSURE LOST. UTILIZED EMERGENCY/ABNORMAL HYD CHECKLIST FOR APPROACH AND LANDING. FOUND LEAK AT NLG PIPE ASSY-CROSS TO GLAND STA 244 TO 240. REPLACED PIPE ASSY. ACFT RETURNED TO SERVICE.SDR U2RA2009F00088Line · crackedIN DESCENT HYDRAULIC QUANITY AND PRESSURE LOST. UTILIZED EMERGENCY/ABNORMAL HYDRAULIC CHECKLIST FOR APPROACH AND LANDING AT LBBG. FOUND LEAK AT NLG PIPE ASSY-CROSS TO GLAND STA 244 TO 240. REPLACED PIPE ASSY. AIRCRAFT RETURNED TO SERVICE.SDR U2RA872LP2993Cable · out of rigNR 1 ENGINE FLAMED OUT AT IDLE AT 30,000 FT. BEGAN PERFORMING ENGINE FLAMEOUT ABNORMAL CK LIST. ENGINE RELITE AND PERFORMED NORMALLY AFTER IGNITION TURNED ON. FINISHED ABNORMAL CK LIST. WEATHER VMC. PERFORMED PULL, TRAVEL AND RIGGING CHECKS OF VBV AND VSV SDR U2RA872CWO1839Strap · crackedDURING C-CHECK, FOUND RT WING XFS 6.225 CENTER LEADING EDGE INTERIOR LOWER STRAP HAS 5 INCH CRACK.SDR U2R2008F00010Strap · crackedDURING C-CHECK FOUND RT WING XFS 341.500 CENTER LEADING EDGE INTERIOR LOWER SURFACE STRAP HAS 12 INCHES CRACK. (K)SDR U2R2008F00012Fitting · corrodedDURING C-CHECK FOUND NR 1, 2, 3, 4 ENGINE THRUST REVERSER TRANSLATING COWL RAIL FITTINGS CORRODED. (K)SDR U2R2008F00011Strap · crackedDURING C-CHECK, FOUND RT WING XFS 430.000 CTR LEADING EDGE INTERIOR LOWER SURFACE STRAP HAS 18 INCH CRACK. (K)SDR U2R2008F00009Skin · corrodedDURING C-CHECK INSP, FOUND FUSELAGE EXTERIOR FS 8.000, L-21R SKIN WITH BULGING AND CHERRY MAX RIVETS. (K)SDR U2R2008F00008Structure · crackedDURING C-CHECK INSP, FOUND LWR CARGO COMPARTMENT, STA 560.000 RT CUSP EXTRUSION WITH 2 INCH CRACK. (K)SDR U2R2008F00007Strap · crackedDURING C-CHECK INSPECTION, FOUND AFT SERVICE DOOR (R2) AFT UPPER JAMB CORNER WITH CRACK OF 0.800 LENGTH ON BEAR STRAP (AFTER ACCOMPLISHED X-RAY INSPECTION). (K)SDR U2R2008F00006Frame · corrodedDURING C-CHECK INSP, FOUND FWD CARGO COMPARTMENT F3 8.00 BTW L-24R FRAME WITH CORROSION. (K)SDR U2R2008F00005Stringer · crackedDURING C-CHECK INSP, FOUND RT WING X RS 202 NR 4 MAIN FUEL TANK STRINGER 67 HAS 2 INCH CRACK BY ACCESSORY PANEL NR 5050. (K)SDR U2R2008F00004Stringer · crackedDURING C-CHECK INSP, FOUND RT WING X RS NR 4 MAIN FUEL TANK STRINGER 58 HAS 2 INCH TRANSVERSAL CRACK BY ACCESSORY PANEL NR 5050. (K)SDR U2R2008F00003Support Angle · crackedDURING C-CHECK INSP, FOUND LT WING X RS 71, 5-52 NR 2 MAIN FUEL TANK INTERIOR LOWER SUPPORT ANGLE CRACKED. (K)SDR U2R2008F00002Bracket · crackedDURING C-CHECK INSP, FOUND LT WING NR 1 ALTERNATE FUEL TANK INTERIOR BOOST PUMP BRACKET FITTING (2) CRACKS. (K)SDR U2R2008F00001Skin · dentedDURING C-CHECK INSP, FOUND RT ELEVATOR XE117-594 LOWER SURFACE DENTED. (K)SDR U2RA872LP2804Engine · flamed outNR 1 ENGINE FLAMED OUT TOP OF DESCENT AT IDLE. RELIGHT PERFORMED IAW INFLIGHT ENGINE START PROCEDURES, OBSERVED NORMAL START AND INDICATION.SDR U2RA872LP2801Skin · corrodedDURING INSPECTION, FOUND CORROSION AT AFT CARGO COMPARTMENT AREA STATION 1440 LONGERON 36 RT EXTERNAL LOWER SKIN.SDR U2RA1576872Skin · crackedDURING INSPECTION FOUND CRACK AT AFT CARGO COMPARTMENT STATION 1380 STRINGER 36 RT ON EXTERNAL LOWER SKIN. COMPLETED FUSELAGE SKIN TEMPORARY EXTERNAL REPAIR AT FUSELAGE STATION 1380/LONG 36R PER FLIGHT VEHICLES CONSULTING, INC DRAWING NR 53-07027-1 AND FAA FOSDR U2RA1535872Skin · corrodedDURING INSPECTION FOUND CORROSION AT AFT CARGO COMPARTMENT AREA STATION 1418 STRINGER 36 RT ON EXTERNAL LOWER SKIN. FOUND 1" CRACK FWD OF FLIGHT STATION 1418 STRINGER 36 RT EXTERNAL SKIN. COMPLETED FUSELAGE SKIN TEMPORARY EXTERNAL REPAIR AT FS 1418/LONG 36 RSDR U2RAM83088Fitting · corrodedLONGERON END FITTING LOCATED AT FRAME 80 AFT, L27R FOUND CORRODED BEYOND LIMITS. CLASSIFIED AS LEVEL 2 CORROSION.SDR U2RA3056Bellcrank · disconnectedDURING INSPECTION, RT ELEVATOR GEARED TAB OUTBOARD CRANK P/N 4710542-3 FOUND DISCONNECTED FROM LINK P/N 271442-501. NOTE: AIRCRAFT IS CURRENTLY CLASSIFIED PART 91.SDR 872SJ009Floor Support · corrodedLT W/W UPPER LT SIDE FWD AND AFT OF SIXTH FLOOR SUPPORT HAS CORROSION. GBAMC NR 4178 CLEANED, CHECKED FOUND TO BE OUT OF LIMITS IAW DC-8 SRM 53-2-0. REMOVED LT W/W, L/H SIDE AFT FLOOR SUPPORT AT STA 960.00 AND REPLACED FLOOR SUPPORT FITTING AT STA 960.00 IAWSDR 872SJ008Gusset · crackedRT UPPER GUSSET CRACKED AT STA XW5.000 GBAMC NR#04187. STOP DRILLED, FAB`D DOUBLER IAW DC-8 SRM. INSTALLED TOP AND BOTTOM DOUBLER IAW DC-8 SRM 51-1-21 AT STA XW5.000SDR 872SJ006Finger Doubler · corrodedLT OB TOP SIDE OF WHEEL WELL PRESSURE DOGHOUSE BETWEEN STA 960 AND 980, FINGER DOUBLER HAS CORROSION ON FWD UNDERSIDE. GBAMC NR304186 -OPEN-SDR 872SJ005Finger Doubler · corrodedCARGO AREA RT SIDE STA 960 HAS CORROSION UNDER FINGER DOUBLER UNDER FLOORBOARD. GBAMC NR04182 -OPEN-SDR 872SJ007Structure · corrodedLT WW UPPER LT SIDE FWD AND AFT OF NR 6 FLOOR SUPPORT HAS CORROSION. GBAMC NR04178 -OPEN-SDR 872SJ004Floor Support · corrodedLT W/W LT SIDE UPPER, SECOND FLOOR SUPPORT HAS CORROSION ON LOWER SIDE. GBAMC NR04176 -OPEN-SDR 872SJ003Door · corrodedD-PIT, AFT BULKHEAD DOOR 645 CORRODED GBAMC NR#04172 CUT OUT DAMAGED MATERIAL ON D PIT DOOR AFT BULKHEAD DOOR 645 IAW DC-8 SRM 52-2-0 FIG 4 SHEET 2. FABRICATED DOUBLER PATCH OUT OF 7075T6 .032 AND INSTALLED DOUBLER PATCH ON D-PIT BULKHEAD DOOR IAW DC-8 SRM 52SDR 872SJ001Skin · corrodedLAV ACCESS SERVICE PANEL HAS CORROSION UNDER PAINT GBAMC NR 04161 AND NR 04185 UPON INVESTIGSTION FOUND SKIN TO BE OUT OF LIMITS BELOW LIP ON ACCESS DOOR, REMOVED DAMAGED SKIN AREA OF 1.75X9.00 FABED FILLER,FABED FINGER DOUBLER FOR BACK, FAB DOUBLER FOR EXTERNSDR 872SJ002Skin · corrodedA/C COMP AREA INTERIOR A/C OUTFLOW DUCT HAS CORROSION GBAMC NR 04160 CLEANED CORRISON ON INTERIOR A/C OUTFLOW DUCT PANEL IAW DC-8 SRM 51-1-8,CORRISON FOUND TO BE OUT OF LIMITS IAW DC-8 SRM 53-2-0. MATERIAL THICKNESS.130,MATERIAL LOSS .104 FABED DOUBLER IAW COTSDR FWT2001F00001Altimeter · erraticON CLIMB OUT MIA AT 17,000 CAPT. ALTIMETER BECAME ERRACTIC AND STICKING AND GIVING ERRONEOUS READINGS, LOG BOOK, PAGE 201510. REMOVED AND REPLACED CAPT. ALTIMETER, ACCOMPLISHED PITOT STATIC SYSTEM LEAK CHECK AND OPS CHECK- FOUND NORMAL IAW MM. PITOT STATIC TSDR FWT2001F00000Engine · failedENGINE NR 4 SHUTDOWN DURING FLT. DUE TO LOSS OF OIL QUANITY AND PRESSURE. AFTER LANDING, MAINT FOUND TRANSFER GEARBOX MOTORING PAD COVER AND SPLINE-SHAFT IN COWLING, ALL CHIP DETECTORS INSPECTED AND FOUND TRANSFER GEARBOX SCAVENGE IN AND SUPPLY OIL FILTER ANSDR FWT2001F00003Actuator · inoperativeWING SLOT LIGHT ON AFTER TO, FLAPS UP, AND BUFFET. UNABLE TO COMPLETE WING SLOT LIGHT ON ABNORMAL PROCEDURE CONDITION NR 1. NOTE: FLAP INDICATOR REMAINS AT 0 FLAP HANDLE IS PLACED TO 0 DEGREE OR 25 DEGREE FLAP POSITION. CHANGED WING FLAP CONTROL VALVE IAW SDR FWT2001F00002Actuator · inoperativeWING SLOT LIGHT ON AFTER TO, FLAPS UP, AND BUFFET. UNABLE TO COMPLETE WING SLOT LIGHT ON ABNORMAL PROCEDURE CONDITION NR 1. NOTE: FLAP INDICATOR REMAINS AT 0 FLAP, WHEN FLAP HANDLE IS PLACED TO 0 DEGREE OR 25 DEGREE FLAP POSITION. CHANGED WING FLAP CONTROLSDR FWT2001F00004Indicator · faultyON CLIMB OUT, NR 3 EGT STARTED TO RISE AND REACHED TEMP LIMIT. WITH POWER LEVER BACK EGT STAYED WITHIN LIMITS. WITH PMC OFF TEMP STARTED TO RISE. DUMPED FUEL IAW AIRCRAFT ABNORMAL PROCEDURES CHECK LIST. BORESCOPE NR 3 ENGINE HPC AND HPT IAW MM. PERFORMED SDR SRAA971211Actuator · failedON ARRIVAL AT BRU FLIGHT NR 081, DURING ENGINE SHUTDOWN, HYDRAULIC QTY INDICATOR DROPPED TO 6 GAL. INSPECTED AIRCRAFT AND FOUND MID WING ACTUATOR ON LT FLAP SHEARED AND LEAKING AT CONNECTOR. REPLACED ACTUATOR, SYSTEM OPS CHECKED GOOD PER MM CH 27-00.SDR SRAA971011Wire · brokenDURING PREFLIGHT, NR 9 AND NR 10 SMOKE DETECTOR, WOULD NOT TEST. INSPECTED AND FOUND WIRE BROKEN DURING LOADING. NR 9 SMOKE DETECTOR REPAIRED, OPS CHECK GOOD IAW DC8 MM CH 26.SDR SRAA970610Fire Loops · malfunctionedON DESCENT, NR 1 ENGINE SHORT CIRCUIT LIGHT FLICKERED ON. REMOVED AND REPLACED ALL FIRE LOOPS ON NR 1 ENGINE. PERFORMED ENGINE RUN, OPS CHECKED GOOD IAW ATA CH 26.SDR SRAA970608Fire Control · inoperativeDURING FLIGHT, NR 1 ENGINE FIRE LOOP SHORT CIRCUIT LIGHT FLICKERS ON AND OFF. UPON TAXI IN FIRE WARNING ON NR 1 ENGINE CAME ON AND SHORT CIRCUIT LIGHT CAME ON STEADY. REMOVED AND REPLACED NR 1 FIRE WARNING CONTROL, SYSTEM OPS CHECKED GOOD PER MM CH 26-00.SDR SRAA970605Connector · dirtyDURING FLIGHT, NR 1 ENGINE FIRE WARNING SHORT CIRCUIT LIGHT FLICKERS ON AND OFF. VISUALLY OBSERVED NR 1 ENGINE, NO FIRE CONDITION EXISTS. AIRCRAFT CONTINUED TO DESTINATION WITHOUT INCIDENT. REMOVED AND CLEANED CANNON PLUG ON NR 1 FIRE CONTROL BOX, OPS CHECKSDR SRAA970402Fire Detector · failedDURING FLIGHT, NR 1 ENGINE FIRE SHORT CIRCUIT LIGHT, MASTER WARNING LIGHT AND FIRE HANDLE LIGHT ILLUMINATED INTERMITTENTLY, ALL OTHER INDICATIONS WERE NORMAL. OBSERVED NR 1 ENGINE AND FOUND NO ABNORMAL CONDITION EXISTS. AIRCRAFT LANDED WITHOUT INCIDENT. FOUSDR SRAA970309Actuator Seal · deterioratedAFTER TAKEOFF FOR FLIGHT 128 OUT OF EKCH, DURING GEAR RETRACTION, AIRCRAFT HYDRAULIC QUANTITY INDICATED A RAPID FLUID LOSS. FOLLOWED EMERGENCY PROCEDURE AND SELECTED HYDRAULIC SYSTEM TO STAND BY RUDDER PUMP, AIRCRAFT LANDED SAFELY USING AUXILARY PUMP, INSPECTSDR SRAA970303Fire Warn Light · illuminatedNR 1 ENGINE FIRE WARNING LIGHT CAME ON AFTER ENGINE SHUT-DOWN AT THE BLOCK, WITHIN 15 SECONDS FIRE LIGHT AND BELL WENT OFF, ENGINE SHORT CIRCUIT LIGHT ALSO CAME ON WITH FIRE WARNING WOULD NOT TEST WENT OFF. VISUALLY VERIFIED NR 1 ENGINE HAD NO FIRE, INSPECTEDSDR SRAA970302Switch · ice build-upDURING FLIGHT 577 TO KEF, LEFT MAIN GEAR GREEN DOWN LIGHT NOT ON AND GEAR UNSAFE LIGHT ILLUMINATED, RECYCLED GEAR WITH SAME RESULT. PERFORMED CHECK PER QRH AND DETERMINED GEARS WERE DOWN AND LOCKED, AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED LT GEAR DOWNLOCSDR SRAA961214Fire Loop · out of positionDURING DESCENT, FIRE BELL RANG ONCE AND NR 1 SHORT CIRCUIT TEST LIGHT FLICKERED ON BRIEFLY THEN STOPPED. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED NR 1 ENGINE, FOUND FIRE LOOP OUT OF POSITION, REPOSITIONED FIRE LOOP, PERFORMED FUNCTIONAL CHECK AND ENGINE R
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