N783SA
Service difficulty reports not matched to an aircraft · 24
They name N783SA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N783SA' AND registry_match IS NULL 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 = 'N783SA' AND registry_match IS NULL 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 Q2SA20120930197Battery Pack · dischargedEMERGENCY FLOOR LIGHTING IN UPPER DECK INOP. REMOVED AND REPLACED BATTERY PACK CARTRIDGE IAW 3-51-04. SYS OPS CHECK NORMAL.SDR Q2SA201209301Battery Pack · defectiveEMERGENCY LIGHT IN THE COCKPIT INTERMITTENT. REMOVED AND REPLACED BATTERY PACK AND CHARGER ASSY IAW 33-51-07. SYSTEM OPS CHECK NORMAL.SDR Q2SA2012091178305Generator · failedWHILE EN ROUTE FROM MIA TO ANC EXPERIENCED A NR 1 AND NR 3 GENERATOR FAILURE. THEREAFTER DISPATCH WAS NOTIFIED BY THE CREW, THE AIRCRAFT HAD LOST A THIRD GENERATOR. SHORTLY AFTER THAT THEY LOST THE FOURTH AND FINAL AIRCRAFT GENERATOR JUST BEFORE LANDING. THSDR TX9Y20111121010Access Panel · damagedMAIN DECK MEC BAY ACCESS PANEL ASSY (P/N:65B11970-35) LOWER SURFACE WAS FOUND DENTS AND PUNCTURE HOLE, AND AT THE ACCESS PANEL (P/N:65B16167-14) CORNERS WAS FOUND CHIPPED OFF. THE REPAIR WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0097 AND SRM 51-40-20SDR TX9Y20111116009Tension Tie · crackedUPPER DECK TENSION TIE STA 860 RT FAIL SAFE CHORD WAS FOUND CRACK. UPPER DECK TENSION TIE STA 860 RT FAIL SAFE CHORD WAS REPAIRED PER SRM 51-40-03 FIG 2 REV 120. THE REPAIR IS APPROVED FOR 24 MONTHS.SDR TX9Y20111115008Tension Tie · crackedUPPER DECK STA 800 LT & RT FWD CHANNEL OF TENSION TIE WAS FOUND CRACK. UPPER DECK STA 840 LT FWD CHANNEL OF TENSION TIE WAS FOUND CRACK. UPPER DECK STA 860 RT TENSION TIE WAS FOUND CRACK. UPPER DECK TENSION TIES (STA 800 LT & RT, STA 840 LT AND STA 860 RT) SDR TX9Y20111114007Structure · damagedONE ELONGATED HOLE WAS FOUND COMMON TO RT INBOARD FIXED TRAILING EDGE BEAM UPPER CHORD (P/N:65B11614) AT APPROX WBL 235.20. THE REPAIR WAS CARRIED OUT PER BOEING MESSAGE NUMBER TEC-SOF-11-0077 AND SRM 51-10-02. DETAILS OF THE REPAIR ARE RECORDED IN EN EA-57-SDR TX9Y20111111006Doubler · corrodedWATER SERVICE PORT EXTERIOR DOUBLER WAS FOUND CORROSION (BS 980-BS 1000, STR 44R-STR 46R). THE CORROSION WAS REMOVED AS PER SRM 51-10-01 REV 120. THE CORROSION WAS BLENDED OUT, NOT WITHIN SRM 53-30-01 REV 120 LIMITS. THE NEW WATER SERVICE PORT EXTERIOR DOUBLESDR TX9Y20111111005Shear Tie · crackedWING CENTER SECTION FRONT SPAR LOCATION RBBL 33.89 SHEAR TIE (P/N:69B14267-9) WAS FOUND CRACK. A NEW SHEAR TIE WAS FABRICATED AS PER DRAWING 69B14267-9. THE REWORK OF TWO TAPER HOLES WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0096 AND SRM 51-30-05. DESDR TX9Y20111111004Panel · damagedONE ELONGATED HOLE WAS FOUND COMMON TO DOOR PANEL (P/N:65B90719-86) OF NR 1 PYLON INBOARD TRAILING EDGE FAIRING DOOR ASSY (P/N:65B90717) AT APPROX STA 297.5. THE REPAIR WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0078 AND SRM 51-10-01. DETAILS OF THE SDR TX9Y20111108003Flap Track · corrodedFLAP TRACK NR 4 FORWARD END CLEVIS INBOARD LUG SURFACE FOUND CORROSION INDICATION ON INBOARD LUG INBOARD SURFACE. THE REPAIR WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0092 AND SB 747-57-2307 REVISION 2. THE DEVIATION WAS APPROVED UNDER ODA-300064-NMSDR TX9Y20111104002Structure · crackedCRACK INDICATIONS FOUND ON NR 2 PYLON STRUT STRUCTURE. REPAIRED PER MN TEC-SOF-11-0088, SRM 51-10-01 AND SRM 51-40-02.SDR TX9Y20111104001Splice Plate · crackedA FASTENER HOLE WAS FOUND CRACKED AT HORIZONTAL STABILIZER CENTER SECTION LT SIDE LOWER SPLICE PLATE. REPLACED PER MN TEC-SOF-11-0082 AND SRM 51-30-05.SDR Q2SA783004Duct · crackedNR 3 ENG FIRE WARNING LIGHT ILLUM WHILE ADVANCING POWER TO 88% RPM. BOTH NR 3 ENG NACELLE IND WERE AT 10 UNITS. EGT WAS RISING THRU 800 DEG CELCIUS WHILE OTHER ENG WERE AT APPROX 700 DEG CELSIUS. AIRSPEED WAS 200 KTS, 3500 FT MSL, LEVEL, FLAPS 5 CONFIG. ENSDR VGQY2010041300005Skin · damagedCOMPLIED WITH EN 1040-10, PERMANENT REPAIR FOR SKIN DAMAGE AT STA 520 T0 STA 700 BETWEEN S-39R TO S-42R.SDR VGQY2010041400006Skin · damagedREQUEST PERMANENT REPAIR ON BELLY SKIN AT STA 520 - 540 STR 38R - 42R IAW SRM 783-007. COMPLIED WITH EN 1040-10, PERMANENT REPAIR FOR SKIN DAMAGE AT STA 520 T0 STA 700 BETWEEN S-39R TO S-42R.SDR VGQY2010041400005Skin · damagedREQUEST PERMANENT REPAIR ON BELLY SKIN AT STA 670-700 S37-42R IAW REP 783-024 PAGE 1 OF 4. REF: RAP 783-007. COMPLIED WITH EN 1040-10, PERMANENT REPAIR FOR SKIN DAMAGE AT STA 520 T0 STA 700 BETWEEN S-39R TO S-42R.SDR VGQY2010041400004Mount · corrodedNR 4 ENG PYLON, LOWER AFT MOUNT FOUND WITH SURFACE CORROSION. REMOVED AND REPLACED NR 4 ENGINE AFT LOWER ENGINE MOUNT AS PER AMM 71-21-04 REV 84.SDR VGQY2010041400003Mount · corrodedNR 4 ENG PYLON, UPPER AFT MOUNT FOUND WITH SURFACE CORROSION. REMOVED AND REPLACED NR 4 ENGINE AFT UPPER ENGINE MOUNT AS PER AMM 71-21-04 REV 84.SDR VGQY2010041300002Structure · corrodedSTA 1920 FRAME BULB TEE 65B04333-89 VERTICAL FLANGE IS FOUND CRACKED AND CHIPPED OFF AT RBL 6.30. COMPLIED WITH EN 1044-10, REPAIR FOR CRACKED 65B0433-89 BULB TEE VERTICAL FLANGE AT STA 1920 FRAME RBL 6.30.SDR VGQY2010041300001Stiffener · corrodedRIGHT HORIZONTAL STABILIZER REAR SPAR AT ELEVATOR STATION 206.8 STIFFENER LOWER END FOUND CORRODED. COMPLIED WITH EN 1048-10, ALTERNATIVE FABRICATION FOR HORIZONTAL STAB REAR SPAR ATTACHED ANGLE 65B03779-12.SDR Q2SA783003Hydraulic Line · rupturedAFTER TAKING OFF FROM KDOV, NR 1 HYDRAULIC SYSTEM QUANTITY DECREASED RAPIDLY, CREW RAN ABNORMAL CHECKLIST IN ACCORDANCE WITH B-747-200/300 QUICK REFERENCE HANDBOOK. CONTINUED FLIGHT AND LANDED SAFELY AT KJFK. AFTER LANDING MAINTENANCE CREW FOUND A RUPTURED HSDR Q2SA783002Pitot Line · brokenON DEPARTURE FROM KJFK, CAPTAIN'S POSITION LOST ALL PRIMARY INSTRUMENTS (AIRSPEED, ALTITUDE, IVSI INDICATORS). AIR TURN BACK TO KFJK, NO FUEL DUMP PERFORMED. CADC REPLACED AND BROKEN PITOT LINE FOUND BEHIND CAPTAIN'S ALTIMETER.SDR Q2SA783001Slide · unwanted deployDURING MAINTENANCE ACTIVITY IN SBKP, ACFT DOOR OPENED WITH FLOOR MOUNTED ESCAPE SLIDE HANDLE IN "AUTO", WHICH INADVERTENTLY ACTIVATED RT SIDE UPPER DECK SLIDE. NO DAMAGE CAUSED TO ACFT. SLIDE REMOVED IAW AMM 25-68-00/PG 201. TRANSFERRED TO DI 16944 IAW DDPG
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