N806US, cancelled Jul 29, 2013
Service difficulty reports · 38
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 = 'N806US' AND deregistration_id = 'N806US-2013-07-29' 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 = 'N806US' AND deregistration_id = 'N806US-2013-07-29' 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 USAAD01077Light · failedIND - THE MAIN ENTRY DOOR WALK-AROUND AND THE LOW LEVEL EMERGENCY LIGHTS AT THE FORWARD SERVICE DOOR AND SEAT ROW 11 WERE INOPERATIVE. THE AFT LOW LEVEL EMERGENCY LIGHT RECEIVER WAS INOPERATIVE. MAINTENANCE REPLACED THE MAIN ENTRY DOOR WALK-AROUND LIGHT ASSESDR USAAD01037Battery · dischargedIND - THE CEILING EMERGENCY LIGHTS BETWEEN THE AFT LAVATORIES WERE INOPERATIVE. REPLACED BATTERIES AT B5-27 IN THE RIGHT LAVATORY CEILING. (M)SDR USAAD00154Relay · stuckPIT-FLL - FLT 1221 - OUT OF 10,000 FEET, THE AUTOPILOT WAS ENGAGED AND OPERATION WAS NORMAL FOR 2-3 MINUTES BEFORE THE AIRCRAFT NOSED DOWN. THE AUTOPILOT WAS DISENGAGED AND THE AIRCRAFT WAS RE-TRIMMED TO NORMAL FLIGHT. AT 26,000 FT, THE AUTOPILOT WAS AGAIN ESDR USAAD00034Power Supply · failedTPA - THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHT POWER SUPPLIES. (M)SDR USAAD99107Battery · dischargedPHL - THE TAIL AREA EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY FOR THE TAIL AREA EMERGENCY LIGHTS. (M)SDR USAA990794Skin · crackedPIT - DURING Q5/C2 CHECK, FOUND 2.375 INCH CRACK AT LOWER LEFT WING FIXED LEADING EDGE XFS 343. INSTALLED DOUBLERS PER EA 52330. (M)SDR USAA990741Doubler · crackedPIT - DURING Q5/C2 CHECK FOUND 2 INCH CRACK AT LEFT WING PRODUCTIONS SPLICE DOUBLER STATION XFS 196.236. REPLACED DOUBLER (SPLICE) AND ADDED STRAPS PER SRM 57-06B (FIGURE 9). (M)SDR USAAD98189O-Ring · failedCLT-TPA - FLT 1816 - DURING CRUISE THE LEFT HYDRAULIC QUANTITY LOW LIGHT ILLUMINATED. THE AIRCRAFT DIVERTED TO SAV AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED AN O-RING ON THE LEFT THRUST REVERSER CONTROL VALVE. (M)SDR USAAD98129Sensor · out of adjustPIT - FLT 2032 - AFTER TAKEOFF, THE FORWARD CARGO DOOR CAUTION LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FORWARD CARGO DOOR WARNING SENSOR TARGET SLIGHTLY OUT OF POSITION. THE TARGET WAS STRAIGHSDR USAAD98072Filter · failedMCO - FLT 1445 - EN ROUTE CLT/ MIA, CREW RECEIVED THE RIGHT ENGINE OIL CLOG LIGHT. CREW REDUCED POWER TO IDLE AND THE LIGHT REMAINED ILLUMINATED. FLIGHT DIVERTED TO MCO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE OIL FILTER PAPERS WERE SEPARASDR USAAD97163Engine · failedMCO - FL 1484 - CLIMBING THROUGH 3000 FT, CREW RECEIVED THE NR 1 ENGINE OIL STRAINER CLOG LIGHT. CREW REDUCED POWER ON THE NR 1 ENGINE. FLIGHT RETURNED TO MCO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 ENGIEN 'MAKING METAL' AND REPLACEDSDR USAAD97122Batteries · dischargedROC - FOUND FORWARD SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY. (M)SDR USAAD97024Battery Pack · dischargedRSW - GALLEY AND COCKPIT EMERGENCY LIGHTS WOULD NOT SHUT OFF. REPLACED BATTERY PACK. (M)SDR USAAD96178Engine · failedFLT 532 - CLT-BDL - AFTER TAKEOFF, CREW HEARD A LOUD BANG, AND NR 2 ENGINE EPR WAS DROPPING. RETURNED TO CLT. A/C WAS FERRIED TO PIT, WHERE NR 2 ENGINE WAS CHANGED. (M)SDR USAAD96040Duct · looseRSW - FL 1028 - AFTER TAKEOFF, CREW RECEIVED MASTER WARNING LIGHT DUE TO THE TAIL HIGH TEMPERATURE SIGNAL. FLIGHT RETURNED TO RSW AND LANDED WITH NO FURTHER INCIDENT. MX FOUND THE DUCTING AT THE WATER SEPARATOR ON THE RIGHT PACK LEAKING. DUCTING WAS SECUREDSDR USAAD96035Duct · separatedCAE - FL 256 - EN ROUTE SRQ-CLT, IN THE VICINITY OF CAE, CREW NOTED LOSS OF CABIN PRESSURIZATION. CREW PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET. FLIGHT CONTINUED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND AND REPAIRED A SEPARATED DUCSDR USAA950180Skin · crackedPIT - DURING Q-4 CHECK, INSPECTION FOUND CRACK .5 INCH AT STA 1408 AND 1429 LT SIDE LONGERON 2 LT DORSAL FIN SKIN. CUT OUT DAMAGE SKIN AND INSTALLED SKIN SPLICE REPAIR PER DACO PER SKETCH 3413J AND EA 29421 AND EO 5388X223. (W)SDR USAA950160Beltframe · crackedPIT - DURING Q-4 CHECK INSPECTION, FOUND TWO EACH CRACKS BOTH .5 INCH, STA 1418 LONGERON 2 LT BELTFRAME. CUT OUT DAMAGE AREA AND INSTALLED FILLER, DOUBLERS PER SRM 53-03 FIG 32 SHT 4 PG 135. (W)SDR USAA950159Tie Dn Track · corrosionPIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION BETWEEN STA 541 AND 634, LT SIDE TIE DOWN TRACK. INSTALLED REPAIR ANGLES PER TYPICAL REPAIR 53-20-09A. (W)SDR USAA950168Skin · crackedPIT - DURING Q-4 CHECK, INSPECTION FOUND CRACKS 2 EACH .25 INCH BY .1250 INCH RT WING FUEL PANELS ACCESS DOOR AREA, LEADING EDGE SKIN. STOP DRILLED CRACKS, MFG DOUBLERS AND INSTALLED REPAIR PER SRM 57-06B PAGE 9 FIG 3. (W)SDR USAA950167Longeron · crackedPIT - DURING Q-4 CHECK, INSPECTION FOUND CRACK .5 INCH STA 1418 LONGERON 2RT. SPLICED IN NEW SECTION OF LONGERON, PER SRM 53-02 FIG 5. (W)SDR USAA950166Skin · crackedPIT - DURING Q-4 CHECK, INSPECTION FOUND .52 INCH CRACK STA 1437 BETWEEN LONGERON 2 AND 3 LT, IN SKIN. CUT OUT DAMAGE AND INSTALLED PLUG REPAIR DOUBLER PER SRM 53-04 FIG 38. (W)SDR USAA950179Beltframe · crackedPIT - DURING Q-4 CHECK, INSPECTION FOUND CRACK .25 INCH STA 446 LONGERON 30 BELTFRAME. INSTALLED REPAIR 'J' ANGLE PLATES PER SRM 53-03 FIG 2A. (W)SDR USAA950177Floorbeam · corrosionPIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I AREA PREVIOUSLY REWORKED STA 1322 RT SIDE LAV AREA FLOORBEAM. CORROSION TASK NR C58-53300. CUT OUT DAMAGED AREA, INSTALLED FILLER, REPAIR ANGLES AND DOUBLER. PE SRM 53-05 TYPICAL REPAIR 53-10-19 EA SDR USAA950176Floorbeam · corrosionPIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I AREA PREVIOUSLY REWORKED STA 1338 RT LAV AREA FLOORBEAM. CORROSION TASK NR C58-53300. REPLACED TOP ANGLE AND INSTALLED DOUBLER REPAIRS, WEB AND FITTING TYPICAL REPAIR 53-10-14 AND SRM 53-05 FIG 72. SDR USAA950178Attach Angle · corrosionPIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I AREA PREVIOUSLY REWORKED AFT PAC DOOR LOWER THRESHOLD ATTACH ANGLE STA 1338 AT FLOOR PANEL NR 101 ATTACH ANGLE. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-05 FIG 34 EA 29474. (W)SDR USAA950175Seat Track · wornPIT - DURING Q-4 CHECK, INSPECTION FOUND COCKPIT AND CO-PILOTS AFT SEAT TRACKS WEAR BEYOND LIMITS. REMOVED AND INSTALLED REPAIR KIT PER TYPICAL REPAIR 53-20-06. (W)SDR USAA950173Seat Track · corrosionPIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION BETWEEN STA 332 AND 389 RT I/B SEAT TRACK. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4. (W)SDR USAA950172Seat Track · corrosionPIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION STA 693 LT SIDE TIE DOWN TRACK. REMOVED CORROSION AND INSTALLED REPAIR STRAPS PER USAIR TYPICAL REPAIR 53-20-09A. (W)SDR USAA950171Seat Track · corrosionPIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION STA 541 RT SIDE TIE DOWN TRACK. REMOVED CORROSION, CLEANED, ALODINE, PRIMED, INSTALLED 'L' ANGLES, PER USAIR TYPICAL REPAIR 53-20-09A. (W)SDR USAA950170Skin · lightning strikePIT - DURING Q-4 CHECK, INSPECTION FOUND LIGHTNING STRIKE .375 INCH BY .035 INCH DEEP STA 1172 LONGERON 30 IN SKIN. INSTALLED EXTERNAL DOUBLER, DAMAGE WAS BLENDED. PER SRM 53-04 FIG 38 VIEW G USAIR EA 29390. (W)SDR USAA950169Longeron · crackedPIT - DURING Q-4 CHECK, INSPECTION FOUND .75 INCH CRACK STA 1309 LONGERON 12 FEET. INSTALLED LONGERON AND SPLICE PER SRM USAIR TYPICAL REPAIR 53-10-17. (W)SDR USAA950165Stiffener · crackedPIT - DURING Q-4 CHECK, INSPECTION FOUND 1 INCH CRACK STA 1338 CENTER TOP OF AFT PASS DOCK IN STIFFENER. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE DOUBLERS PER SRM 53-01 FIG 2 SHEET 4. (W)SDR USAA950164Skin · corrosionPIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I STA 800 BETWEEN LONGERONS 28 RT AND 29 RT SKIN. CORROSION TASK NR C22-57301. INSTALLED DOUBLER PER SRM 53-04 FIG 53. (W)SDR USAA950163Skin · corrosionPIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I STA 823 LONGERON 29 RT, IN SKIN. CORROSION TASK NR C22-57301. INSTALLED DOUBLER PER SRM 53-04 FIG 53. (W)SDR USAA950161Skin · dentPIT - DURING Q-4 CHECK, INSPECTION FOUND DENT BEYOND LIMITS .065 INCH DEEP FUSELAGE STA 345 LONGERON 20 RT. CUT OUT DAMAGED SKIN AND INSTALLED PLUG FILLER AND INTERNAL DOUBLER PER SRM 53-04 FIG 38 AND EA 26628 REV B. (W)SDR USAA950174Skin · gougedPIT - DURING Q-4 CHECK, INSPECTION FOUND GOUGE .022 INCH IN FUSELAGE LT SIDE STA 229 BETWEEN LONGERON 18L AND 19L SKIN. BLENDED DAMAGED SKIN AND INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38. (W)SDR USAA950162Skin · dentDURING Q-4 CHECK, INSPECTION FOUND DENTS BOTH .063 INCH DEEP STA 229, LONGERONS 22 TO 26 LT, IN SKIN. CUT OUT DAMAGE SKIN AND INSTALLED FLUSH REPAIR WITH INTERNAL FINGER DOUBLER. PER SRM 53-04 FIG 26. (W)
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