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 P5CA0300963Valve · inactiveAT PUSHBACK, NR 3 ENGINE DID NOT START. NO FUEL FLOW. REF DMI 31578. REACTIVATED NR 3 ENG FUEL VALVE. EICAS MESSAGE GROUND. NR 3 ENG STARTS, GROUND STARTS NORMAL, IAWMM 71-00-00. DMI CLEARED, PLACARDS REMOVED.SDR P5CA0300909Indicator · inoperativeNR 4 ENG OIL PRESSURE INDICATION FAILED AFTER ENG START. RE-PINNED BRKN AND WIRE AT DT679 PIN A. ALSO REMOVED AND REPLACED INOP OIL TRANSMITTER.SDR P5CA0300901Start Valve · malfunctionedENG NR 2 WOULD NOT START EICAS MESSAGE -ENG NR 2 START VLV-. DEFERRED NR 2 ENG PER DDG START VLV REQUIRED MANUAL START.SDR P5CA0300893Aileron · malfunctionedAFTER ENG START CREW REPORTED AILERON INDICATION PROBLEMS DURING FLT CNTRL CHECK. CONFIRMED W/ VISUAL OPERATION THAT THE CONTROL SURFACES LOOKED NORMAL, DEFERRED IAW MEL 27-18-1SDR P5CA0300880Controller · malfunctionedZONE TEMP: CABIN FILLER WITH SMOKE - RESET - TEMP STARTED DOWN - TEMP TO 36 SMOKE AGAIN. T/S SYSTEM ORDERED ZONE TEMP CONTROLLER DEFERRED TRIM AIR SYSTEM MEL 21-61-9B CATC. INSPED TRIM AIR DUCTS AND VLVS. NO DEFECTS NOTED. FAULTY ZONE TEMP CONTROLLERSDR P5CA0300879Skin · gougedAFT FUSELAGE SKIN AT STA 2392 THRU 2394 DEEP GOUGE. CUT OUT DAMAGE, FABRICATED & INSTALLED REPAIR DOUBLER & FILLER AS PER SRM 53-00-01 FIF 201.SDR P5CA0300805Pedal · displacedWITH RUDDER SURFACES NEUTRAL RUDDER PEDALS WERE DISPLACED 1-8 UNITS (RIGHT). OPERATIONAL CHECKED PER AMM 27-21-00. OPS CHECK NORMAL. SUSPECT LARGE LATERAL IMBALANCE AS INDICATED ON W/B FORMS.SDR P5CA030078Connector · damagedNR 2 ENG OIL PRESSURE VARIED FROM 100-160 ON TAXI OUT. OPENED NR 2 ENG, CHECKED CONNECTION AT OIL PRESSURE TRANSMITTER AND FOUND PUSHED BACK PIN. RESEATED OPS CHECKED NORMAL ON ENG RUN.SDR P5CA0300783Access Panel · brokenGROUND DAMAGE TO RT WING TIP BETWEEN WS 155-25 & WBL 1243-75. TAIL JACK WAS DRAGGED UNDER WING TIP CAUSING DAMAGE TO HEADING EDGE, TRAILING EDGE A FUEL TANK EDGE A FUEL TANK ACCESS PANEL & UNDERSIDE OF WING. PERFORMED DYE PENETRANT CK, FOUND NO CRACKS MATERISDR P5CA0300774Display · inoperativeCENTER AUTO PILOT ON THE ILS DIDN'T CAPTURE LOCALIZER / GLIDE SLOPE. FOUND CMC MESSAGE VOR - RIGHT DISPLAYED. GROUND TEST CARRIED OUT PER 34-51-00. NO FAULTS NOTED.SDR P5CA0300767Bolt · strippedLOWER FWD CARGO DOOR ACTUATOR HAD TWO SUPPORT CARGO DOOR ACTUATORS WITH INSUFFICIENT BOLT THREAD SHOWING AND THE OTHER TWO BOLTS HAD EXCESSIVE THREAD ENGAGEMENT AND BOTTOMED OUT, INDICATING THE ENTIRE ACTUATOR LOAD WAS CARRIED OUT BY ONLY TWO BOLTS. REPOSITIOSDR P5CA0300765Controller · faultyAFTER TWO HOURS OF FLT SMOKE WAS OBSERVED COMING FROM RT SIDE COCKPIT. AOM PROCEDURE COMPLIED W/. SMOKE SOURCE TRACED TO LWR AREA OF NUMBER 1 RT WINDOW. WINDOW HEAT 1R SWITCHED OFF, SMOKE STOPPED. AREA OF GREASE WAS OBSERVED ALONG LWR PART OF WINDOW. REMOVED ASDR P5CA0300764A/C Pack · odorDURING CRUISE OILY ODOR WAS NOTICED ON FLT DECK FOLLOWED BY LITE SMOKE FROM F/O'S AC VENT. AOM PROCEDURE COMPLIED WITH, A/C DESCENDED TO FL29 AS A PRECAUTION WITH CREW ON 02. SMOKE CLEARED FOLLOWING COMPLETION OF PROCEDURE WITH INTERMITTANT INCREASED ODOR. SDR P5CA0300719Rudder · malfunctionedRUDDER TRAVEL NOT GOING TO LIMITS ON R/H INDICATOR DURING CONTROL CHECK. INSPECTED FWD & AFT RUDDER QUADRANT ASSYS, CABLE SYS., TRIM, CENTERING & FEEL MECHANISM PER MM 27-21-06, 27-21-08 & 27-21-11. ALL OK. PULLED A/C INTO HANGAR. AFTER 30 MIN. SYSTEM OPS CHECSDR P5CA0401022Warning Light · illuminatedBLEED OVERHEAT / PRU EICAS MESSAGE NNC 2.3. GROUND TESTED PER MM 36-11-00 TEST PASSED. NO MESSAGE FOUND ON EICAS WHEN RETURNED TO BLOCKS.SDR P5CA0200715Control Module · failedTRIM #2 & #3 FAILED AFTER T/O IN BOTH AUTO & MANUAL. A/C RETURNED TO MIA. REMOVED & REPLACED STAB. TRIM UNIT AS PER MM 27-41-06. OPS CHECK NORMAL.SDR P5CA0200669Skin · dentedLOWER AFT EDGE SKIN OF AFT LWR CARGO DOOR DENTED IN BY CONTACT WITH GROUND EQUIPMENT. TRANSFERRED TO COI #451-013 PER MX CTRL (JOHN). NO FURTHER DISCREPANCIES NOTED. OK FOR CONTINUED SERVICE. COMPLETED REPAIR AT NEXT STATION (MIA) ON AFT CARGO DOOR PER SRM 52-SDR P5CA0200659Smoke Detector · contaminatedCENTER FIRE SENSORS ON MAIN DECK INDICATED FIRE 9 HRS INTO FLT. VISUAL INSPECTION REVEALED NO FIRE. CB'S PULLED TO SILENCE ALARM FOR DURATION OF FLT & PERFORMED PERIODIC VISUAL FIRE INSPECTION. CLEANED & DRIED MAIN DECK SMOKE DETECTOR. (DETECTOR CONTAMINATED DSDR P5CA0200648Service Door · brokenAT SCL ARRIVAL FOUND LT WING LT FUELING PANEL DOOR BROKEN. TRANSFERRED TO CDL 28876 AS PER CDL 57-31-1. CAUSE IS UNDER INVESTIGATION. REMOVED DOOR AND COVERED WITH HIGH SPEED TAPE.SDR P5CA0200647Caster · crackedRT MAIN DECK BS 1725 CASTER TRAY EXTRUSION CRACKED/DAMAGED. REPAIRED PER SRM 51-70-11 FIG 1 & PER MM 25-57-04.SDR P5CA0200646Fairing · delaminatedNR 7 CANOE ASSY, OUTBOARD SIDE AT MID POINT 2 INCH DELAMINATION. REPAIRED PER SRM 51-40-00.SDR P5CA0200645Floorboard · puncturedMAIN DECK L/S FLOOR BOARD PUNCTURE BS 1720 LT SIDE. REPAIRED PER SRM 53-00-50.SDR P5CA0200644Caster · crackedMAIN DECK CASTER ASSY AT BS 1900 R/S CRACKED. REPAIRED PER SRM 51-40-00.SDR P5CA0200643Lock · damagedFWD CARGO COMPT AT STA 650 LOCK ASSY DAMAGED LEFT SIDE. REMOVED AND REPLACED PER MM 25-56-33.SDR P5CA0200642Guide · damagedAFT CARGO COMPT, STA 1820 SIDE GUIDE RAIL DAMAGED LT/SIDE. REPAIRED PER SRM 51-70-12 & MM 25-33-00.SDR P5CA0200641Floor Panel · puncturedMAIN DECK, STA 1920/2040 LEFT SIDE FLOOR PANEL DAMAGED (PUNCTURES). REMOVED AND REPLACED PER MM 53-00-50.SDR P5CA0200632Seat Track · crackedFORWARD CARGO COMPARTMENT BS 560 - RBL - 45, WL - 118 SEAT TRACK CRACKED. REPAIRED BY SPLICED IN SECTION OF SEAT TRACK IAW 400F SRM 53-00-52, PG 251SDR P5CA0200633Seat Track · crackedFORWARD CARGO COMPARTMENT BS 560 - LBL - 225, WL 118 SEAT TRACK CRACKED. REPAIRED BY SPLICED IN SECTION OF SEAT TRACK IAW 400 SRM 53-00-52, PG. 251SDR P5CA0200625Nozzle · cracked#3 ENGINE EXHAUST NOZZLE OUTER SKIN IS CRACKED ON THE RIGHT SIDE TOP. REMOVED & REPLACED EXHAUST NOZZLE AS PER 78-11-01.
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