Boeing 747-46NF
Service difficulty reports · 1,079
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '74746NF' 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 aircraft_model_key = '74746NF' 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 P5CA2012082800035Pdu · failedPDU 19L1 HOT AND SMOKING. REMOVED PDU. PDU REPLACED IAW AMM 25-57-01. SYSTEM OPS CHECKED GOOD.SDR P5CA2012082400034Structure · damagedDAMAGE FOUND TO MDSCD AREA - BS 1780 SIDEWALL TRIM GUTTER DEFORMED AND MOUNT FASTENERS MISSING, DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 OF EO 4425A315 AND FAA 8110-3 DATED 24AUG12 WORK INSTRUCTIONS. REPETITIVE DVIS REQUIRESDR P5CA2012080600033Skin · damagedSKIN DAMAGED AT AFT CARGO DOOR FWD LOWER EDGE BS 1810 BETWEEN S38-40R. DAMAGE AREA REPAIRED AS PER RS-NO R-53-60-37384.453PA.SDR P5CA2012072900030Oil System · lowSHUTDOWN NR 1 ENGINE AS A PRECAUTION DUE TO LOW OIL QUANTITY. TWO QUARTS REMAINED. SHUTDOWN TIME 16:40Z. FIRE SWITCH NOT PULLED. REMOVED AND REPLACED ENGINE 1 IDG BLANKING PLATE AND PLUG. SERVICED ENGINE IAW AMM 12-13-03. POST WINDMILL INSPECTION IAW 72-SDR P5CA2012080600032Channel · crackedBS 760 RT TENSION TIE AREA FOUND HOLE CRACK AT AFT CHANNEL RUNNING 10 O/C APPROX 0.020 INCH LENGTH. AFT CHANNEL REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 FIG 201 AND EO NR 4453A746.SDR P5CA2012080600031Channel · crackedBS 760 RT TENSION TIE AREA, FOUND 1 CRACK AT FWD CHANNEL RUNNING 6 O/C APPROX 0.020 INCH, FWD CHANNEL REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 FIG 201 AND EO NR 4453A745.SDR P5CA2012071600029Bulb · inoperativeCREW REST COMPARTMENT EMERGENCY LIGHT INOPERATIVE, DEFECTIVE LIGHT BULB. REPLACED AND OPERATIONAL TESTED NORMAL.SDR P5CA2012070500028Skin · damagedDURING WALKAROUND INSPECTION, DAMAGE FOUND TO BS 1780 SIDEWALL TRIM/GUTTER DEFORMED AND MOUNT FASTENERS MISSING. PERFORMED A TIME LIMITED REPAIR.SDR P5CA2012052700027Support · crackedMAIN DECK SIDE CARGO DOOR AREA AT BS 1920, SIDEWALL SUPPORT CRACKED AND RIVET SHEARED. TIME LIMITED REPAIR ACCOMPLISHED. REPEAT DETAILED VISUAL INSPECTION REQUIRED PRIOR TO EVERY FLIGHT WITH THE PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO 1000 FLIGHT HOURS.SDR P5CA2012052300026Oven · dislodgedTHE UPPER DECK GALLEY OVEN FELL OUT DURING LANDING THEN THERE WAS A BURNING ODOR FOR SEVERAL MINUTES DURING TAXI IN. REMOVED OVEN UNIT AND CHECKED AREA. FOUND ELECTRIC RECEPTACLE DIRTY. CLEANED CONNECTOR PER SWPM 20-10-04. OVEN INSTALLED AND OPS WAS NORMALSDR P5CA2012050700025Lens · brokenFOUND LT OUTBD LANDING LIGHT LENS WAS BROKEN. (ACCOMPLISHED TIME LIMITED REPAIR PER EO 4433A034 AS DESCRIBED IN PART 1 WORK INSTRUCTIONS. PART 2 INSPECTION REQUIRED EVERY FLIGHT. PERMANENT REPAIR BY REPLACING THE DAMAGED LENS COVER ASSY PRIOR TO THE ACCUMULSDR P5CA2012040900024Pump · overheatedNR 1 HYDRAULIC SYSTEM OVERHEAT USING EDP, ADP TURNED ON, ALL FLUID EVENTUALLY LOST FROM NR 1. FOUND EDP TO BE OVERHEATED, INOPERATIVE AND LEAKING. REPLACED EDP AND CORRELATED FILTERS.SDR P5CA2012040100023Relief Valve · faultyNRT TOWER OBSERVED FLUID STREAMING FROM UNDER THE RIGHT WING. NO NOTICEABLE REDUCTION IN FUEL, HYDRAULIC OR OIL QUANTITIES. (DURING MAINTENANCE WALK AROUND THE RIGHT INBOARD FUEL PRESSURE RELIEF VALVE WAS FOUND TO BE OPEN SLIGHTLY. REMOVED AND REPLACED THESDR P5CA2012030500022Seat Track · chafedFORWARD MAIN DECK SEAT TRACK WORN AND CHAFING DAMAGE AT SEVERAL LOCATIONS STA 1680 - 1800 RBL 11.33. (PERFORMED PERMANENT REPAIR TO SEAT TRACK PER SRM 53-00-52 REPAIR 12 AND INSTRUCTION CONTAINED IN EO 4453A702 AND BOEING REPAIR AND DEVIATION RECORD (RDR) ASDR P5CA2012030500021Skate Angle · crackedCRACK ON SKATE ANGLE OF NR 3 PYLON INBOARD FAIRING AT NACELLE STATION 457. (ACCOMPLISHED TIME LIMITED REPAIR PER EO 4454A142 AND BOEING SR 2112722461 AND REPAIR AND DEVIATION RECORD. PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO 24 MONTHS).SDR P5CA2012030500020Frame · crackedCRACK ON THE FUSELAGE FRAME OF MAIN DECK CARGO COMPARTMENT AT STA 1900, S-12R - S-13R. (PERFORMED REPAIR PER EO 4453A690 WHICH REFERS TO VENDOR ENGINEERING INSTRUCTIONS AND APPROVAL PER BOEING SR SR 1-2110434060 AND FAA 8100-9 FORM).SDR P5CA2012030500019Skin · wornTHREE EA FASTENER HOLES WORN ON LT WING LEADING EDGE SKIN AT ILES 653.39. (PERFORMED INTERNAL FLUSH PERMANENT REPAIR PER INSTRUCTIONS IN EO 4457A406 AND BOEING SR 1-2110443013 AND REPAIR AND DEVIATION RECORD RDR).SDR P5CA2012030500018Intercostal · crackedCRACK ON THE INTERCOSTAL OF FLOOR STRUCTURE AT STATION 990.5 RBL 99.08 AND WL 200. (PERFORMED PERMANENT REPAIR PER INSTRUCTIONS IN EO 4453A700 AND BOEING SR 1-2111730438 AND REPAIR DEVIATION RECORD).SDR P5CA2012030500017Rib · crackedCRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 145, LOWER SIDE. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).SDR P5CA2012030500016Rib · crackedCRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 131. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).SDR P5CA2012030500015Rib · crackedCRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 145 UPPER SIDE. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).SDR P5CA2012030500012Rib · crackedCRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 484. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).SDR P5CA2012030500014Rib · crackedCRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 151 UPPER SIDE. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM RDR).SDR P5CA2012030500013Rib · crackedCRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 159. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM RDR).SDR P5CA2012030200011Rib · crackedCRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 151. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).SDR P5CA2012030200010Rib · crackedCRACK ON RIB OF RT HORIZONTAL STABILIZER LEADING EDGE AT STA 518. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).SDR P5CA2012030100009Rib · crackedCRACK ON RIB OF RT HORIZONTAL STABILIZER LEADING EDGE AT STA 510. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).SDR P5CA2012030100007Skin · dentedREPAIR DENT ON LT FUSELAGE SKIN AT STA 710, S-29L & NBSP. DENT MEASURES 8.0" X 1.5" AND IS .210" DEEP. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4453A321 WITH APPROVAL PER 8100-9).SDR P5CA2012030100005Skin · nickedFOUND SKIN NICK/DAMAGE 1.8" X 2.1" AT STA 2592, S-38R TO S-42R NEAR AFT JACK POINT AREA. (REPAIRED PER EO 4453A699 APPROVED BY 8100-9).SDR P5CA2012030100008Rib · crackedCRACK ON RIB OF RT HORIZONTAL STABILIZER LEADING EDGE AT STA 501. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).SDR P5CA2012030100006Winglet · damagedEVIDENCE OF LIGHTNING STRIKE FOUND ON THE UPPER TIP T/E OF RT WINGLET. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4457A405).SDR P5CA2012022900004Skin · dentedFOUND SKIN DENT AT STA 732, S41L TO S42L &NBSP. (PERMANENT REPAIR ACCOMPLISHED PER EO 4453A706).SDR P5CA2012012300001Channel · crackedDURING INSPECTION AS REQUIRED BY EO 4453A301 REV C A CRACK WAS FOUND AT FASTENER HOLE AT BS 760 LT TENSION TIE, AFT CHANNEL. (THE DAMAGE WAS REPAIRED IAW STEP 6 OF PART 1 OF EO 4453A301 REV C. REPEAT INSPECTIONS ARE REQUIRED IAW PART 2 OF EO 4453A672 WITH ISDR P5CA2012012300002Channel · crackedDURING INSPECTION AS REQUIRED BY EO 4453A301 REV C CRACKS WERE FOUND AT 2 FASTENER HOLES AT BS 760 RT TENSION TIE, FORWARD CHANNEL (THE DAMAGE WAS REPAIRED AS IAW STEP 6 OF PART 2 OF EO 4453A301 REV C. PART 2 OF EO 4453A674 REQUIRES AND INITIAL INSPECTION ATSDR P5CA2012012300003Channel · crackedDURING INSPECTION AS REQUIRED BY EO 4453A301 REV C A CRACK WAS FOUND AT 1 FASTENER HOLE ON BS 760 LT TENSION TIE, FORWARD CHANNEL. (THE DAMAGE WAS REPAIRED IAW STEP 6 OF PART 1 OF EO 4453A301 REV C. INITIAL INSPECTION REQUIRED AT 20,000 FLIGHT CYCLES AND REPSDR P5CA2011122900513Nozzle · crackedTHERE IS A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, BETWEEN THE 10 AND 12 O'CLOCK POSITION (LT SIDE) OF THE NR 3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROXIMATELY 15 INCHES LONG AND IS 13 INCHES FROM AFT SIDE OF EXHAUST SLEEVE JUST IN FRONT OF NAC STA 349.2SDR P5CA2011122100511Scoop · damagedTHE LEFT WING VENT SCOOP INLET AREA WAS FOUND TO BE DAMAGED. (PRELIMINARY INSPECTION REVEALED FATIGUE CRACKS ON VENT SCOOP ASSEMBLY WHICH ARE NOT REPAIRABLE. THE VENT SCOOP ASSEMBLY WILL BE REPLACED ONCE PARTS BECOME AVAILABLE. AIRCRAFT IS AOG. ).SDR P5CA2011121500510Rub Strip · damagedLIGHTNING STRIKE DAMAGE FOUND ON FUSELAGE SKIN RUB STRIP AT BS 1350-BS 1351 BETWEEN S26 & S27. (DAMAGE EXCEEDS THE LIMITS OF SRM 53-00-01, FIGURE 101, ALLOWABLE DAMAGE 1. A TIME LIMITED REPAIR WAS ACCOMPLISHED IAW EO 4453A663 FAA 8110-3 DATED 15 DEC 11 PART SDR P5CA2011120900508Pin · defectiveELECTRIC FLIGHT CONTROLS {PSM} LEFT 2 AC, DC CIRCUIT BREAKERS FOUND POPPED AND WILL NOT RESET. NON-FDE CMC MSG 27506A NOTED. (PRELIMINARY INSPECTION FOUND WIRE WRAP PINS 15A AND 15E OF WIU TO BE MAKING CONTACT. CONTACT CAUSED THE RECEPTACLE TO DISCOLOR. RSDR P5CA2011120600489Rib · crackedRIB AT STATION 433.210 OF LEADING EDGE OF LEFT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-1954 REV 1. NO FURTHER ACTION REQUIRED.SDR P5CA2011120600491Rib · crackedRIB AT STATION 458.841 OF THE LEADING EDGE OF THE LEFT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-1956 REV 1. NO FURTHER ACTION REQUIRED.SDR P5CA2011120600492Rib · crackedRIB AT STATION 458.841 OF THE LEADING EDGE OF THE RIGHT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-157 REV 1. NO FURTHER ACTION REQUIRED.SDR P5CA2011120600493Rib · crackedRIB AT STATION 467.384 OF THE LEADING EDGE OF THE RIGHT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011-158 REV 1. NO FURTHER ACTION REQUIRED.SDR P5CA2011120600494Rib · crackedRIB AT STATION 501.559 OF THE LEADING EDGE OF THE RIGHT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-159 REV 1. NO FURTHER ACTION REQUIRED.SDR P5CA2011120600495Rib · crackedTHE TOP SIDE OF THE RIB AT STATION 501.559 OF THE LEFT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-1960 REV 1. NO FURTHER ACTION REQUIRED.SDR P5CA2011120600496Rib · crackedBOTTOM OF RIB AT STATION 501.559 OF THE LEADING EDGE OF THE LEFT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-161 REV 1. NO FURTHER ACTION REQUIRED.SDR P5CA2011120600497Rib · crackedTOP SIDE OF RIB AT STATION 510.103 OF THE LEADING EDGE OF THE LEFT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-162 REV 1. NO FURTHER ACTION REQUIRED.SDR P5CA2011120600498Rib · crackedLOWER SIDE OF RIB AT STATION 510.103 OF THE LEADING EDGE OF THE LEFT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-1964 REV 1. NO FURTHER ACTION REQUIRED.SDR P5CA2011120600499Rib · crackedRIB AT STATION 510.103 OF THE LEADING EDGE OF THE RIGHT HORIZONTAL STABILIZER IS CRACKED. RIB REPAIRED IAW EI T2011A55B-1964 REV 1. NO FURTHER ACTION REQUIRED.SDR P5CA2011120600500Rib · crackedRIB AT STATION 518.646 OF THE LEADING EDGE OF THE RIGHT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-1965 REV 1. NO FURTHER ACTION REQUIRED.
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