N535DA, cancelled Dec 18, 2012
Service difficulty reports · 41
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 = 'N535DA' AND deregistration_id = 'N535DA-2012-12-18' 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 = 'N535DA' AND deregistration_id = 'N535DA-2012-12-18' 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 DL72S010180Switch · shortedAIR TURNBACK ACCOUNT LEADING EDGE AMBER LIGHT ON F/OS PANEL AT FLAPS 2 WITH S/OS PANEL LIGHTS INDICATING NORMAL. FLAPS NOT RETRACTED PAST 2 DEGREES INFLIGHT. FOUND NR 5 L/E FLAP SW S206 SHORTED. REPLACED SAME.SDR DL72S010047Skin · crackedA CRACK WAS FOUND IN THE RT SIDE SKIN OF THE VERTICAL STABILIZER EMANATING FROM UNDER THE FUSELAGE TO STABILIZER CREASE CHORD AT STA 1209. THE CRACK IS REPAIRED WITH AN EXTERNAL DOUBLER INSTALLED PER SRM 55-30-3, FIG 7 AND PER THE REQUIREMENTS OF ER/A 379749-SDR DL72S002460Warning System · activatedNR 3 ENG FIRE INDICATION ON CLIMB THROUGH 10500. INDICATION CLEARED UPON RETARDING THROTTLE TO IDLE. CA- FND FUEL HEAT MANIFOLD BAD, REPLACED SAME. RAN ENG., ALL CHECKS GOOD.SDR DL72S001990Isolation Valve · chafedWHILE TROUBLESHOOTING WING ANTI-ICE PROBLEM FOUND RIGHT BLEED AIR ISOLATION VALVE WIRING CHAFING ON PNUEMATIC DUCT BETWEEN THE VALVE AND THE AFT PACK VALVE. WHILE INSTALLING PNUEMATIC DUCT FOUND WIRE BUNDLE FOR LEFT BLEED ISOLATION VALVE CHAFED. REPAIRED WIRSDR DL72S001688Light · failedON APPROACH INTO SDF, F/O UNDER GLARESHIELD FLOOR LIGHT GOT BRIGHTER THEN ALL THREE FLOUR LIGHTS INOP WITH ELECTRIC SMELL. TURNED OFF FLOUR LIGHTS AND SMELL WENT AWAY. REPLACED LIGHT ASSY.SDR DL72S001683Battery Pack · dischargedCENTER CABIN OVERHEAD EMERGENCY LIGHT BETWEEN OVERWING EXITS INOP. REPLACED BATTERY PACK, OPS NORMAL.SDR DL72S001560Actuator · failedSYSTEM A HYD LOSS IN FLIGHT WENT TO ZERO. FOUND NUMBER 6 LEADING EDGE KRUEGER FLAP ACTUATOR FAILED. REPLACED ACTUATOR.SDR DL72S001153Angle · crackedFOUND AT F-1 LETTER CHECK, NR 8 SLAT ACT I/B AND O/B SUPPORT DOUBLERS CRACKED. REPAIRED PER MM 57-20-21.SDR DL72S001152Stiffener · crackedFOUND AT F-1 LETTER CHECK, NR 7 O/B SLAT TRACK I/B SPAR STIFFENER CRACKED. REPAIRED PER MM 57-20-21.SDR DL72S000991Wire · brokenNUMBER 3 OIL TEMP WAS FLUCTUATING UP TO THE UPPER PEG. OIL QTY WAS SLOWLY DECREASING TO 1.4, OIL PRESS WAS NORMAL AT 50 PSI. ENG WAS SHUTDOWN IN FLT. ALL OTHER PARAMETERS WERE NORMAL. FOUND BROKEN WIRE AT CANNON PLUG TO OIL TEMP TRANSMITTER. REPAIRED BRSDR DL72S000764Harness · damagedFOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA OF NR 3 ENG. REPLACED CABLES FROM SPLICES IN RT 48 SECTION TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727SDR DL72S000603Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 480 & 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL MFEC INSPECTION CONFIRMED 4 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP WAS TRIMMED OFF ALONG THE PANEL LENGTH ANDSDR DL72S992490Skin · cracked4 INCH CRACK IN FUSELAGE SKIN AT FS 384 2 .5 INCH ABOVE STR 25R AND .25 INCH CRACK IN FUSE SKIN 2 INCH AFT OF ABOVE CRACK. REPAIR PER SRM 53-30-3 TIME LIMITED.SDR DL72S992446Mechanism · failedLOUD BANG DURING INITIAL GEAR RETRACTION ON T/O FROM SJC. FOLLOWED BY EXCESSIVE VIBS. RED GEAR DOOR LIGHT ILLUMINATED. ON FRONT PNL AS WELL AS AMBER NOSE GEAR LIGHT ON S/O PNL. GEAR EXTENDED NORMALLY. PER EMERGENCY CK-OUT. UPON ARR INTO SFO, MAINTENANCE SDR DL72S992133Compressor · stalledAS POWER WAS INCREASING TO TAKEOFF SETTING NR 2 ENGINE HAD A HARD COMPRESSOR STALL. A HEAVY VIBRATION AND RUMBLING NOISE WAS HEARD/FELT FROM NR 2 ENGINE. MAXIMUM CROSSWIND WAS LESS THAN 3 KTS. REPLACED NR 2 ENGINE.SDR DL72S991402Valve · failedENG RUNNING ESS PWR SEL ON ENG 1, BOTH PACKS ON. APU GEN/FIELD BREAKER OPENED WITH ASSOCIATED AMBER LIGHTS, 1-3 BTBS OPEN WITH LIGHTS. PACKS TRIPPED, SMOKE, HOT PACK SMELL AND LOSS ELECT. RETURNED TO GATE. ELECT FAULT PANEL UNDEREXCITED SYS 1-3. LIGHTS ILSDR DL72S991382Sill · corrodedFUSELAGE C2 DOOR SURROUND LOWER SILL OUTBD CHORD, CORROSION REPAIR. THE OUTBOARD CHORD OF THE C2 DOOR OPENING LOWER SILL WAS FOUND CORRODED ON THE OUTBD FLANGE BETWEEN FS 950F+11 AND FS 960. THE CORROSION WAS BLENDED AWAY WITH A MAXIMUM DEPTH OF .075. THE DSDR DL72S991340Frame · damagedFOUND DURING MV2 CORROSION VISIT NRC 213, CUT AND REMOVE FLOOR SUPPORT RAIL ABOVE STRINGER 29 LT STA 980 FOR ACCESS TO FRAME REPAIR (STA 990) REF NRC 128. REPAIRED PER SRM 53-10-5, WORKED WITH NRC 128, 93, 94.SDR DL72S991288Skin · dentedBULGE AT LT HORIZONTAL STABILIZER UPPER SKIN 6 IN FWD OF ELEVATOR 2ND FROM O/B HINGE(MARKED). INSTALLED DOUBLER PER SRM 55-20-3.SDR DL72S991341Stringer · damagedFOUND DURING MV2 CORROSION VISIT NRC 128, CUT FRAME STA 990 TO ACCESS REPAIR OF STR 29 LT REF NRC 89. REPAIRED PER M/M 53-12-0 FIG 805. WORKED WITH NRC 93, 94, 213.SDR DL72S991289Doubler · crackedA 1 INCH CRACK IN DOUBLER NR 3 SLAT RIB O/B OF ACT. REPLACED DOUBLER PER MM 57-54-0 FIG 804.SDR DL72S991342Stringer · crackedFOUND DURING MV2 CORROSION VISIT NRC 89, 1 IN CRACK STR 29 LT AT STA 1000. REPLACED STR 29 LT STA 980 TO STA 1007 PER SRM 53-10-11 FIG 3. WORKED WITH NRC 93, 94, 128, 213.SDR DL72S990860Frame · crackedTHE AFT FRAME OF THE C1 CARGO DOOR OPENING WAS FOUND WITH A 1 INCH CRACK IN THE FRAME WEB BELOW THE LOWER DOOR STOP FITTING. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED WITH A DOUBLER PER ER/A 367202-14.SDR DL72S990802Skin · crackedFUSELAGE SKIN FS 360-480 STRINGER 4R SKIN LAP SPLICE: CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 13 TOTAL CRACKS. TSDR DL72S990810Skin · crackedFUSELAGE SKIN FS 481-681 STRINGER 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 4 CRACKS IN SDR DL72S981813Panel · delaminatedFOUND AREA OF DELAMINATION ON NR 2 SPOILER UPPER SURFACE. REPAIRED PER SRM 57-50-6.SDR DL72S981812Web · crackedFOUND ON D2 LETTER CK, RT VERTICAL TORQUE BOX WEB CRACKED .1562 INCH AT LIGHTENING HOLE STA 1243 RT. ROUTED OUT DAMAGED AREA PER MM 53-11-0.SDR DL72S981811Web · crackedFOUND ON D2 LETTER CK, 2 EA .5 INCH CRACKS STA 1303 VERT WEB ABOVE S-DUCT RT SIDE. REPAIRED PER SRM 53-10-4.SDR DL72S981810Angle · crackedFOUND ON B2 LETTER CK, HORIZONTAL TORQUE BOX ANGLE CRACKED RT STA 1273. REPLACED ANGLE PER SRM 53-10-10.SDR DL72S981340Battery · dischargedR-2 DOOR EMER EXIT SIGN INOP. REPLACED BATT OPS CK OK.SDR DL72S980451Battery Pack · dischargedDURING S/C, FOUND AFT EMERG EXIT SIGN INOP WHEN TESTING EMERG LIGHTS. REPLACED BATTERY PACK.SDR DL72S972680Tube · brokenON TAXI OUT, -A- SYS HYD FAILED. REPLACED NR 2 L/E SLAT LINE.SDR DL72S971870Bulb · failedON FAA RAMP INSPECTION ONE EMER TRACK LIGHTING BULB INOP. REPLACED LAMP AND OK.SDR DL72S970258Floorbeam · corrosionCORROSION ON TOP SIDE OF FLOORBEAM STA 344 FROM BL 0 TO LBL 39. REMOVED DAMAGED SECTION OF BEAM, FABRICATED AND INSTALLED A REPLACEMENT CHORD SECTION PER SRM 53-10-8, FIG 11.SDR DL72S961632Window · failedON CLIMBOUT, AT 27,000 PASSENGER CABIN WINDOW AT ROW 2A CRACKED AND CABIN PRESSURE WAS MAINTAINED AT 7.6 PSI. FLT WAS CONTINUED AT FL200 AND CABIN PRESS AT 6.0 PSI. ON ARRIVAL PBI FOUND OUTER WINDOW PANE BROKEN, INNER PANE INTACT. REPLACED 2A WINDOW, INSPECSDR DL72S961004Angle · crackedFOUND ON B2 LETTER CHECK, NR 6 SLAT COVE SKIN SUPPORT ANGLE CRACKED INBOARD END. REPAIRED PER MM 57-54-0.SDR DL72S961003Torque Box Web · crackedFOUND ON B2 LETTER CHECK, .1875 INCH CRACK UPPER END OF TORQUE BOX WEB STA 1213 ABOVE STAIRWAY CLOSEOUT PANEL. REPAIRED PER MM 53-11-0.SDR DL72S954644Passenger Door · bentAC LOG ITEM Z60966002 RT CORNER OF FORWARD ENTRY DOOR IS BENT UP. REPAIRED PER MM 52-11-01 FIG 804.SDR DL72S953836Web · crackedDURING B-1 LTR CHECK, FOUND 48 SEC TORQUE BOX WEB IS CRACKED AT LIGHTENING HOLE, STA 1323 LT. REPAIRED PER MM 53-11-0.SDR DL72S961617Transverse Beam · crackedTHERE IS DAMAGE TO THE LOWER TORQUE BOX STATION 1263 TRANSVERSE BEAM FWD SIDE. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AD 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS REPLACEMENT DOES NOT TERMINATE THE REPETITIVE INSPECTION REQUIREMENTSSDR DL72S951246Web · crackedFOUND DURING A-2 LETTER CHECK, CRACK IN LT TORQUE BOX SKIN .5 INCH LONG AT UPPER RIVET ROW ABOVE FWD LIGHTENING HOLE. ALSO,A .125 INCH CRACK AT UPPER FWD LIGHTENING HOLE LT SIDE VERT STAIRWAY. REPAIRED PER B727 MM 53-11-0 PG 832.
Back to N535DA, cancelled Dec 18, 2012