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 P5CA2016083000248Module · malfunctionedSTABILIZER TRIM UNSCHEDULED STATUS. SRM R & R, TESTED OK IAW AMM 27-41-01, LP691776M8. STABILIZER COMPARTMENT RELATED PARTS INSPECTED NORMAL. FCC L, C, R AND SRM L AND R RERACKED, STABILIZER TRIM GROUND TEST CUTOUT PASSED IAW AMM 22-11-00.SDR P5CA2016080100179Warning System · activatedABORTED TAKEOFF LOW SPEED 70 KNOTS DUE TO EICAS MESSAGE ELECTRIC DRIVE 3. TRANSFER TO MDDR 68827 IAW MEL 24-11-01A, CAT B.SDR P5CA2016072700174Fire Detector · warning messageNR 1 ENGINE FIRE LOOP B STATUS MESSAGE. REMOVE AND REPLACED THE UPPER AFT DETECTOR ASSY IAW AMM 26-11-02. OPS CHECKED GOOD, NO FAULTS.SDR P5CA2016070200160Detector · faultyEICAS EQUIPMENT COOLING MSG DISPLAYED. FOLLOWED FIM TASK 21-58-02-102-035. REMOVED, CLEANED AND REINSTALLED FLIGHT DECK FLOW DETECTOR IAW MM 21-58-02. GROUND OPS CHECK NORMAL. REF LP 78029, REPLACED FLIGHT DECK LOW FLOW DETECTOR AND OPERATES NORMAL.SDR P5CA2016060600128Warning Message · activatedLOW SPEED REJECT DUE TO ENGINE 2 REVERSER EICAS APPPLIED MEL 78-31-01A. CAT "C". MAINTENANCE PROCEDURE COMPLETED.SDR P5CA2016052800119Power Supply · faultedUPPER DECK EMERGENCY LIGHT INOPERATIVE, REAR LIGHT ASSY. T/S FOUND EMERGENCY LIGHT POWER SUPPLY AT FAULT BS 590, RT EQUIPMENT M5169 IAW WDM 33-51-71, PAGE 1. REPLACED WITH SERVICEABLE POWER SUPPLY ASSY. OP'S CHECKED NORMAL IAW AMM 33-51-04.SDR P5CA2016051000106Panel · damagedNR 2 PYLON V/V PANEL 462ER FASTENER HOLE ELONGATED. NR 2 PYLON V/V PANEL 462ER IS REPAIRED IAW HX R1 R1-54-00-11339, REV A.SDR P5CA2016051000105Floorbeam · crackedAFT CARGO COMPT RT BS 1840, RBL 1 FLOOR SUPPORT BEAM FOUND CRACK. AFT CARGO COMPARTMENT BS 1840, RBL 0 TO RBL 4 FLOORBEAM UPPER CAP IS REPAIRED IAW HX R1, NO R1-53-25-11337, REV A REPEAT INSPECTION IS REQUIRED IAW RT R1 NR R1-53-25-11337, REV A REPEAT INSPECTSDR P5CA2016051000104Floorbeam · crackedAFT CARGO BS 1900, LBL 41, FLOOR STRUCTURE FOUND CRACK. AFT CARGO COMPARTMENT BS 1900, LBL 39 TO LT OTBD FLOORBEAM UPPER CAP IS REPAIRED IAW SRM 53-60-07-2R, REPAIR 6 FIG 201, DETAIL I. ADJACENT INTERCOSTAL IS REPAIRED IAW SRM 51-70-12-06-0.SDR P5CA2016051000103Channel · crackedM/D BS 720 RT SIDE TENSION TIE END OF OTBD CHANNEL CORNER FOUND CRACK. M/DECK, BS 720 RT SIDE TENSION TIE CHANNEL ARE REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1. SUP: INSPECTION IS REQUIRED IAW SRM 53-20-30-2R-1, REPAIR 1 TABLE NR 3.SDR P5CA2016051000102Channel · crackedM/DECK BS 720 LT SIDE TENSION, THE END OF OTBD CHANNEL CORNER FOUND CRACK. M/DECK BS 720 LT SIDE TENSION THE CHANNELS ARE REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1. SUP: INSPECTION IS REQUIRED IAW SRM 53-20-30-2R-1, REPAIR 1, TABLE 203.SDR P5CA2016051000107Access Panel · damagedNR 1 PYLON 452EL ACCESS PANEL, PYLON V/V, LOWER AFT CORNER FASTENER HOLE ELONGATED. NR 1 PYLON 452EL ACCESS PANEL, PYLON V/V, LOWER AFT CORNER HOLE IS REPAIRED IAW HX R1 NR R1-54-00-11338, REV A.SDR P5CA2016051000109Support · crackedLEFT HORIZAONTAL STABILIZER OTBD FAIRING AFT PANEL SUPPORT CRACK. LT HORIZONTAL STABILIZER OTBD TIP FAIRING AFT T/E CHANNEL IS REPAIRED IAW HX RE NR R1-55-10-11322, REV A.SDR P5CA2016051000110Manifold · chafedNR 4 ENGINE, RT CORE COWL AIR COOLING MANIFOLD DEEP CHAFING. NR 4 ENGINE RT CORE COWL AIR COOLING MANIFOLD, PRE-COOLER EXIT DUCT FLANGE REPAIRED IAW ROHR SB TBC 80C2-NAC-71-032.SDR P5CA2016051000111Duct · chafedNR 1 ENGINE RT CORE COWL AIR COOLING DUCT INTERNAL EDGE AREA FOUND DEEP CHAFING. NR 1 ENGINE, RT CORE COWL AIR COOLING DUCT INTERNAL EDGE, PRE-COOLER EXIT DUCT. REPAIRED IAW ROHR SB TBC 80C2-NAC-71-032.SDR P5CA2016051000112Skin · damagedLEFT BLG INBD STRUT DOOR EXTERIOR SKIN HAS A SCRATCH MARK. LT BLG INBD STRUT DOOR SKIN IS REPAIRED AT BS 1416.5 AREA IAW SRM 52-80-01-2R-1, REPAIR 1, FIG 201.SDR P5CA2016051000113Fitting · crackedFS 1480 TO 1540, STR L32 TO L33 CRACK WAS FOUND AT LT LONGERON EXTENSION FITTING CRACK LENGTH .3750" APPROXIMATELY AT RADIUS AREA. FS 1480 TO 1540, STR L32 TO L33 LT LONGERON EXTENSION FITTING IS REPAIRED IAW EO NR 4453A818, PART 3, REV 12, POST MODIFICATION SDR P5CA2016051000114Fitting · crackedFS 1480 TO 1540, STR R32 TO R33 CRACK WAS FOUND AT RT LONGERON EXTENSION FITTING CRACK LENGTH .5" APPROXIMATELY AT RADIUS AREA. FS 1480 TO 1540, STR R32 TO R33, RT LONGERON EXTENSION FITTING IS REPAIRED IAW EO NR 4453A818, PART 3, REV 12, POST MODIFICATION INSDR P5CA2016051000116Battery Pack · no testU/D MERGENCY LIGHT BATTERY PACK CAPACITY CHECK FAILED, LESS THAN 15 MINUTES,POWER PACK REPLACED IAW AMM33-51-04.SDR P5CA2016051000115Battery Pack · no testM/D EMERGENCY LIGHT BATTERY PACK CAPACITY CHECK FAILED, LESS THAN 15 MINUTES, POWER PACK REPLACED IAW AMM 33-51-04.SDR P5CA2016051000108Skin · corrodedLT WING OTBD T/E MID FLAP T/E TOP PANEL FOUND CORROSION. LT WING OTBD MID FLAP T/E THE TOP PANEL SUPT AT OTBD AREA CORROSION IS REMOVED. PROTECTED IAW SRM 51-10-02 & 51-20-01 WITHIN SRM 57-53-02-1A-1 ALLOWABLE DAMAGE 1, FIG 101, LIMITATION. BLEND OUT AREA 2SDR P5CA2016051000101Attach Fitting · crackedUPPER LOBE DOUBLER AT THE FUSELAGE AND VERTICAL STABILIZER ATTACH FITTING RT RADIUS UPPER LOBE DOUBLER FOUND CRACK APPROXIMATELY 80MM LONGERON STABILIZER 2403-2524. RT UPPER LOBE DOUBLER AT THE FUSELAGE AND VERTICAL STABILIZER ATTACH FITTING AREA IS REPAIRED SDR P5CA2016020400024Fitting · crackedLONGERON EXTENSION FITTING ONE CRACK WAS FOUND ON RT BS 1480, LONGERON EXTENSION FITTING APPROXIMATELY .3125" LENGTH. REPAIRED IAW EO: 4453A818 PART 1 AND PART 3.SDR P5CA2016020400026Fitting · crackedLONGERON EXTENSION FITTING HAD ONE CRACK FOUND ON RT BS 1480, LONGERON EXTERSION FITTING APPROXIMATELY .3125" IN LENGTH. REPAIRED IAW EO:4453A818, PART 2 AND PART 4.SDR P5CA2016020400022Frame · chafedNR 1 LEFT CORE COWL NR 2 FRAME FOUND CHAFING NR 1 LT CORE COWL NR 2 FRAME CHAFING MARK AREA REPAIRED IAW NR; RE 71-13-11226, REV A, EO 44TSA.61 REV 0.SDR P5CA2016020400025Seat Track · corrodedCABIN BS 1900-1920, RBL 11.33" SEAT TRACK FOUND CORROSION. CABIN-BS 1870 TO 1946.45, RBL 11.33" SEAT TRACK REPAIRED IAW RI: RI-53-65-11220, REV A AND EO: 4453B 176, REV O.SDR P5CA2016020400027Skin · crackedL5 DOOR CUTOUT, BS 2231, STR 21L TO STR 22L REVEAL SKIN FOUND CRACKED. L5 ENTER DOOR BS 2231, STR 22L REVEAL DOUBLER CRACK AREA REPAIRED IAW SRM 53-60-15-2R-3, REPAIR 3 AND ATLAS EO4453B178.SDR P5CA2016020400028Panel · crackedFWD CARGO BS 600-660 CTR BALL MATERIAL PANEL UPPER SURFACE FOUND CRACK. FWD CARGO BS 600-660 CTR BALL MATERIAL PANEL UPPER SURFACE CRACKED AREA REPAIRED IAW EO: 4425A467, REV O.SDR P5CA2016020400023Floor Panel · damagedFLOOR PANEL BS 1740-1860, RBL 35-70 FOUND DAMAGED. FLOOR PANEL FABRICATED AND REPLACED IAW R1-53-65-11224, EO4453B180.SDR P5CA2016020400020Floor Panel · damagedBS 1740-1840, LBL 35-70, FLOOR PANEL FOUND DAMAGED. FLOOR PANEL FABRICATED AND REPLACED IAW R1-53-65-11224, EO 4453B180.SDR P5CA2016020400019Floor Panel · damagedBS 1840-1940, LBL 35-70, FLOOR PANEL FOUND DAMAGED. FLOOR PANEL FABRICATED AND REPLACED IAW R1-53-65-11224, EO 4453B180.SDR P5CA2016013100016Sensor · shortedHEATER RT TAT, FIM TASK 30-31, TASK 810. T/S FOUND RT TAT SENSOR HEATER INTERNALLY SHORTED TO GROUND. THE SENSOR WAS REPLACED IAW AMM 30-31-00 AND TEST PASSED AND MESSAGE CLEARED.SDR P5CA2016012500015Rvdt · out of rigLOW SPEED RTO DUE TO NR 2 ENGINE FAILED TO SPOOL BEYOND 74 PERCENT N1. FOUND RVDT OUT OF RIG. RIGGED RVDT AS REQUIRED IAW AMM 78-34-10. OPS CHECK GOOD.SDR P5CA2015121200198Escape Reel · damagedCOCKPIT DESCENT DEVICE NR 4 HAS CABLE EXTENDED. R & R NR 4 COCKPIT DESCENT DEVICE IAW AMM 25-61-01.SDR P5CA2015121200199Escape Reel · damagedCOCKPIT DESCENT DEVICE NR 6 HAS CABLE EXTENDED. R & R COCKPIT DESCENT DEVICE IAW AMM 25-61-01.SDR P5CA2015121200200Escape Reel · damagedCOCKPIT DESCENT DEVICE NR 5 HAS CABLE EXTENDED. R & R DESCENT DEVICE IAW AMM 25-61-01.SDR P5CA2015121200201Escape Reel · damagedCOCKPIT DESCENT DEVICE NR 7 HAS CABLE EXTENDED. R & R NR 7 DESCENT DEVICE IAW 25-61-01.SDR P5CA2015121200202Escape Reel · damagedCOCKPIT DESCENT DEVICE NR 8 HAS CABLE EXTENDED. R & R COCKPIT DESCENT DEVICE IAW AMM 25-61-01.SDR P5CA2015110900173Oil System · lowLOW OIL QUANTITY IN CRUISE. GOT DOWN TO 2 QTS INDICATED. INSPECTED NR 1 ENGINE IAW AMM 72-00-00 AND FOUND LEAKAGE FROM B-SUMP SCAVANGE DRAIN TUBE. R & R NR 1 ENGINE IAW BOOTSTRAP METHOD IAW W/C E2023.SDR P5CA2015100100162Unknown · odorODOR FROM INSIDE COCKPIT, LIKE VINYL BURNED. INSPECTED INSIDE, E1, E2 RACK BOTH SIDE TUNNEL, SUPPLY FAN, EXHAUST FAN, INSIDE COCKPIT, INSIDE LT PFD AND RT PFD, UPPER AND LOWER EICAS ALL CDU OK IAW MM 05-51-56-200-801, ENGINE RUN CHECKED IAW MM 71-00-00-862-00SDR P5CA2015092700159Brake Assy · fireBRAKE/GREASE FIRE MOMENTARILY AFTER BLOCK IN. HOT BRAKE INSPECTION ACCOMPLISHED ON NR 9, NR 10, NR 11 BRAKES IAW MM 5-51-26. NO DEFECTS NOTED. AS PRECAUTION, REPLACED NR 9, NR 10, AND NR 11 TIRES AND NR 9 AND NR 10 BRAKES.SDR P5CA2015091200136Tire · damagedAFTER TAKEOFF, UNABLE TO RAISE GEAR. BODY GEAR ADVISORY MESSAGE ALONG WITH GEAR TILT ADVISORY MESSAGE. IN WORK DURING THE CURRENT AOG EVENT NR 11 TIRE REPLACED IAW MM 32-45-01 AND FOUND CONDUIT DAMAGED. REPLACED CONDUIT IAW MM 32-13-00. PERFORMED GEAR RESDR P5CA2015082400093Lamp · inoperativeON CHECK, FOUND CREW EMERGENCY LANDING LIGHT L1382 DIM, CREW EMERGENCY LIGHT L1382. REPLACED THE LAMP AND CHECKED OK IAW AMM 33-51-00.SDR P5CA2015081100083Frame · damagedNR 2 ENGINE LT CORE COWL FRAME HOLD OPEN ROD BRACKET MOUNT HOLE 3 EA ELONGATED. NR 2 ENGINE LT CORE COWL FRAME HOLD OPEN ROD BRACKET, MOUNT HOLE ELONGATED AREAS. REPAIRED IAW SRM 51-70-11: EO 4471A153, REV 0.SDR P5CA2015081100082Panel · damagedNR 3 PYLON, RT EXHAUST NOZZLE UPPER SKIRT PANEL 1 EA HOLE FOUND ELONGATED, NR 3 PYLON RT SKIRT FAIRING SKIN ELONGATED FASTENER HOLE REPAIRED IAW R1-54-50-11007.SDR P5CA2015081100081Skin · dentedRIGHT MLG INBD AFT STRUT DOOR EXTERNAL OUTER SKIN FOUND DENT, RT BLG INBD AFT STRUT DOOR EXTERNAL OUTER SKIN DENT AREAS AND DAMAGED RIB REPAIRED IAW R1-52-80-11002, REV B.SDR P5CA2015081100080Support Fitting · crackedLEFT WING - NR 6 SPOILER ACTUATOR SUPPORT FITTING FOUND CRACKED AT OTBD LOWER FLANGE, LT WING - NR 6 SPOILER ACTUATOR SUPPORT FITTING OTBD LOWER FLANGE CRACK AREA REPAIRED IAW SRM 57-51-13-2R-1, REPAIR 1.SDR P5CA2015081100078Shear Tie · crackedFWD CARGO -BS 980, STR 37R -STR 38R FWD FRAME SHEAR TIE FOUND CRACKED AT RADIUS, FWD CARGO COMPARTMENT BS 980 RIGHT BETWEEN STR 37R TO STR 38R FRAME SHEAR TIE IS REPAIRED IAW R1: R1-53-22-11018.SDR P5CA2015081100077Skin · crackedRT SIDE BS 980 DRAG SPLICE LOWER FITTING AT STR 38R CRACK FOUND ON SKIN LAYER UNDER FITTING, CRACK RUNNING DOWNWARD AT 6 O'CLOCK POSITION THROUGH THICKNESS, FUSELAGE SKIN IS REPAIRED IAW SRM 53-20-01-2R-2. REPAIR 2 AT BS 939.5 TO 991.5 BETWEEN STR 37R-39R ARESDR P5CA2015081100076Hinge Fitting · crackedRT WING REAR SPAR NR 7 SPOILER MID HINGE FITTING OTBD LOWER 3EA RIVET HEAD CRACKED. RT WING REAR SPAR NR 7 SPOILER ACTUATOR SUPPORT FITTING CRACKED AREA REPAIRED IAW R1-57-51-11009.
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