Boeing 747-200B
Service difficulty reports · 48
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 = '747200B' 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 = '747200B' 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 1119200701Tire · failedON TO ROLL, AIRCRAFT AIRFRAME SHUDDERED AT 155KTS. CONTINUED TAKEOFF, REPORTED TO TOWER POSSIBLE BLOWN TIRE. DEBRIS CONFIRMED ON RUNWAY. ALL SYSTEMS INCLUDING BRAKE TEMPS GOOD, CONTINUED. (25) MINUTES INTO FLIGHT, NR 1 HYDRAULIC SYSTEM FAILURE - RETURNED TSDR 0331200702Engine · bird ingestionAT ROTATION NR 2 ENG VIB ANNUNICATOR LIGHT & ENG VIB LIGHT FOR NR 2 ENG ILLUM, ACCOMPANIED BY VIB & ABNORMAL SOUND. NR 2 ENG SECURED IAW CHECKLIST, NO VIB NOTED AFTER SHUTDOWN. FUEL JETTISON, ACFT RETURNED WITHOUT FURTHER INCIDENTS. ON POSTFLIGHT INSPECTIOSDR EIA2007061Smoke Detector · no testNR 5 A LOOP SMOKE DETECTOR WILL NOT TEST. REPLACED SMOKE DETECTOR PER 26-14-01, TEST OK.SDR 0312200701Hose · wornAFTER TAKEOFF, WITH LG RETRACTED, OBSERVED HYDRAULIC SYSTEM NR 4 LOOSE WITH BOTH NR 4 EDP, ADR LOW PRESSURE ON. AOM 2-2-55 AND 2-2-59 FOLLOWED, RETURNED TO DEPARTURE.FOUND LT WING GEAR DOOR ACTUATOR HYDRAULIC LINE WORN. REMOVED AND REPLACED HYDRAULIC LINE, SDR 1023200603Warning Light · illuminatedON DEPARTURE (GYD), JUST AFTER V1, NR 1 ENGINE VIBE LIGHT ILLUMINATED, VIBE METER NR 1 OFF SCALE HIGH, INCLUDING VIBRATION AS WELL. ENGINE SHUT DOWN, FUEL DUMP, AND RETURNED TO (GYD).CORRECTIVE ACTIONS, PENDING.SDR 1017200602Engine · power lossDURING CLIMB FROM (ELLX) AT AROUND FL 180 FT, NR 1 THROTTLE IS AT FORWARD STOP TO MAINTAIN CLIMB THRUST. IN CRUISE NR 1 THROTTLE IS AT 1.5 UNITS - (4) KNOBS AHEAD OF ENGINES 2, 3, 4. NOTE ALL ENGINE PARAMETERS NORMAL AT LOW ALT, BELOW 189 THROTTLE POSITIONS SDR 0925200603Compressor · stalledDURING TO ROLL (SKBO), APPROX. 125 KTS., NR 4 ENGINE COMPRESSOR STALLED - ABORTED TO, RETURN TO GATE. FINDINGS - CORRECTIVE ACTIONS - TBD.SDR 0808200601Engine · noneON TAKEOFF AT SGES (AGT), NR 3 ENGINE BEGAN TO VIBRATE AND AMBER ENGINE VIB LIGHT CAME ON. ENGINE SHUTDOWN AND PROCEDURE TO COMPLETE THE HIGH ENGINE VIBRATION RB211 CHECKLIST. DISCREPANCY DUE TO BIRDSTRIKE/INJESTION. PERFORMED CONDITIONAL ENGINE BIRDSTRIKE SDR EIA2006160Smoke Detector · no testNR 5 LOWER LOBE SMOKE DETECTOR, NO TEST. REPLACED SAME.SDR 0623200604Control Wheel · bindingON CLIMBOUT BEFORE LEVEL FLT WITH FLAPS EXTENDED CONTROL WHEEL BINDING & ABRUPT YAWING MOTIONS WITH MINOR VIBRATION & RUMBLE EXPERIENCED AT FLAPS 10.5 DEGREE WITH AP ENGAGED. BINDING WAS STILL PRESENT WITH MINIMUM YAWING MOTION ON APPROACH (MIA). BINDING & YSDR 0622200603Rivet · shearedAFTER DEPARTURE FROM MIA, AILERONS DURING MANUAL CLIMB APPEARED HEAVY AND WERE BINDING. ALTITUDE 350/AUTOPILOT A & B NORMAL. DURING DESCENT AUTOPILOT A&B TURN RATE NORMAL. AUTOPILOT C EXCESSIVE TURN RATES IN BOTH LEFT AND RIGHT TURNS. NOTICE MINOR VIBRATIOSDR 0609200602Valve · leakingON GROUND, FUEL SPILL THRU RT WING, AFTER REFUELING AIRCRAFT. FOLLOW PROCEDURES IN FUELING MANUAL FOR FUEL SPILLAGE. DURING INSPECTION, FOUND BOTH THE NR 2 AND NR 3 DRAIN VALVE LEAKING. REPLACED BOTH VALVES, CLEAN FUEL TANKS, INSPECTED, AND CLOSED TANK PLATSDR EIAA2006038Indicator · failedDURING FLIGHT, NR 2 EGT FAILED TO 0 ON DESCENT, INTERMITTENT FAILURE, SEEMED TO FAIL DURING POWER REDUCTION NEVER GOT AN OFF FLAG. CHECKED CONNECTORS ON HARNESS AND PYLON ON NR 2 ENG AND P-2 PANEL. COULD NOT DUPLICATE, ALL WIRE CHECKS WERE NORMAL COMPARED TOSDR 740002Engine · shutdownNR 2 ENGINE SHUTDOWN FOR UNKNOWN REASON, ACCOMPANIED BY A LOUD BANG. QRH CHECKLIST ACCOMPLISHED. AIRCRAFT RETURNED TO PANC.SDR 1022200501Window · crackedRIGHT FORWARD NR 1 WINDOW HAS DELAMINATION AND POSSIBLE CRACK. INSPECTED WINDOW, AND FOUND ACCEPTABLE FOR FLIGHT IAW MEL 56-1-1, NR 1 WINDOW OUTER GLASS PLY CRACKED ONLY, AND VISIBILITY THROUGH ASSOCIATED WINDSHIELD IS ACCEPTABLE, AND VISION IS NOT IMPAIRED OSDR UPS01435784Brake Assy · inoperativeWHILE EXITING RAMP NO NORMAL BRAKES AVAILABLE MOMENTARILY. INSPECTED ALL SYSTEM FOR LEAKS, NONE FOUND. PERFORMED OPERATION OF BRAKE SYSTEM ON NR 4, NR 1 AND RESERVE SYSTEM. FOUND NORMAL IAW MM 32-40-00. OK FOR SERVICE.SDR UPS01435638Wire · damagedINSPECTION TYPE:N/A EMERGENCY LIGHT INOP UPPER DECK EXIT FWD PANEL REPAIRED PULLED WIRE, OPS CK GOODSDR UPS01435326Fire Detector · malfunctionedINSPECTION TYPE:N/A NR 4 ENGINE FIRE DETECTION LIGHT ILLUMINATED REMOVED AND REPLACED NR 4 ENGINE UPPER AFT TEST DECTECTOR ASSY. I.A.W. MMNL 26-11-00. OPERATIONAL CHK SYSTEM NORMAL.SDR UPS01434803Spar Cap · corrodedINSPECTION TYPE:IN PER EO-13738A REPAIR RT WING LWR SKIN FWD ANGLE ATTACH CHORD. *S/D* REPAIR ACCOMPLISHED PER EO -13738A.SDR UPS00434524Light · inoperativeINSPECTION TYPE:N/A AFT EMERGENCY EXIT LIGHT AT CREW ENTRY DOOR L1 IS INOP R&R BATTERY ASSY PER 33-50-00 OPS CK OKSDR UPS00434521Battery Pack · dischargedINSPECTION TYPE:N/A AFT EMERGENCY LIGHT AT CREW ENTRY DOOR L1 IS INOP EMERGENCY LIGHT BY CREW STAIRS (AFT) INOP R/R BATTERY ASSY ONLY, PER 33-50-00 OPS CHK OKSDR UPS00434525Stringer · corrodedINSPECTION TYPE:N/A AFT CARGO COMPT CORROSION ON STR 49 RH BETWEEN STA 1920 TO 1960 CORRODED PORTION STRINGER REMOVED. FABRICATED NEW STRINGER AND REINF ORCEMENT IAW SRM 53-10-23 FIG 2 ACCOMPLISHED REPAIR IAW SRM 53-10-03SDR UPS00434268Light · inoperativeINSPECTION TYPE:N/A, L1 DOOR AFT EMERGENCY LIGHT IS INOP. RELAMPED, OPS CHECKS GOOD.SDR UPS00433554Indicator · malfunctionedINSPECTION TYPE:N/A, AIR TURNBACK - ALL FOUR ENG N1 INDICATORS NOT EFFECTIVE FOR AIRCRAFT. REMOVED AND REPLACED INDICATORS. TPCR FILED FOR PROPER EFFECTIVITY REFERENCE LOG PAGES 418722, 418723, AND 418724.SDR UPS00433344Flap · malfunctionedINSPECTION TYPE:N/A, FLAPS WON''T DRIVE TO COMMANDED POSITION.SDR UPS00433745Cap · crackedINSPECTION TYPE:C, RT WING - TRAILING EDGE SUPPORT BEAM UPPER CAP DEEP CORROSION AND A LONG CRACK WERE FOUND AT THE UPPER AFT FLANGE OF THE UPPER CHORD. REPAIR ACCOMPLISHED PER IAI EO 89310 AND AS APPROVED BY FAA-8110-3 FORM. THE CHORD AT WBL 360 TRIMMED OUSDR UPS00433247Angle · corrodedINSPECTION TYPE:C, REINFORCING ANGLE AT BS 360 RT BETWEEN STR 3 A AND STR 10 IS CORRODED. ANGLE FABRICATED IAW SRM 51-20-01 AND REPLACED IAW SRM 51-30-02.SDR UPS00433073Support Bracket · damagedINSPECTION TYPE: C, FUSELAGE WING TO BODY FAIRING SUPPORT BRACKET CRACKED AT BS 1265, BELOW LOWER REAR SPAR SPLICE RT. DAMAGE REMOVED AND REPAIR CARRIED OUT IAW SRM 51-40-03 FIG 1.SDR UPS00433072Support Bracket · crackedINSPECTION TYPE: C. WING TO BODY SUPPORT CRACKED AT BS 1265, BELOW REAR SPAR SPLICE LT SIDE. DAMAGE REMOVED AND REPAIR CARRIED OUT IAW SRM 51-40--03 FIG 1SDR UPS00433341Spar · corrodedINSPECTION TYPE:C REF NRC 44298572 44298580 44298584 44298590, PLEASE REPLACE LEFT I/B MIDFLAP ASSY DUE CORROSION ON FRONT SPAR LOWER CHORD AND UPPER SURFACE DOUBLER PLATE. LT MIDFLAP ASSY REPLACED PER MM 27-51-01.SDR UPS00433060Stiffener · crackedINSPECTION TYPE: C. CRACK IN NOSE WHEEL WELL AT BS 300 RBL 22 . CRACK IN STIFFENER. NOSE WHEEL WELL CRACKED STIFFENER REPLACED STIFFENER IAW SRM 51-300-02SDR UPS00433064Angle · crackedINSPECTION TYPE: C. CRACK FOUND IN ANGLE AT BS 486 STR 26 LT IN FWD CARGO HOLD. ANGLE REPLACED IAW SRM 51-30-02SDR UPS00433059Seat Track · crackedINSPECTION TYPE: C. SEAT TRACK CRACKED BS 440 AND BS460 RBL 64. SECTION OF SEAT TRACK REPLACED FROM BS 430 TO BS 460 IAW SRM 53-10-0 5, FIG. 1A, DETAIL 1VSDR UPS00433061Strap · crackedINSPECTION TYPE: C. FRAME TIE DOWN STRAP BROKEN FWD OF RT OUTFLOW VALVE BS 2020 LBL 15. NEW TIE DOWN STRAP FABRICATED AND INSTALLED IAW 51-30-02 AND SRM 5 1-20-1SDR UPS00433067Angle · crackedINSPECTION TYPE: C. FWD CARGO BAY TWO CRACKED ANGLES ON WEATHER RADAR TRAY BS 380 RT SIDE NOSE WW, CRACKED ANGLES REMOVED IAW SRM 51-30-02. NEW ANGLES FABRICATED IAW BAC 5300. NEW ANGLES INSTALLED IAW SRM 51-30-02SDR UPS00433269Frame · crackedINSPECTION TYPE:C, UPPER DECK FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STRINGER AT BS 500 AT STR 10 RT. REPAIR CARRIED OUT IAW QUERY NOTE 34/200 AND SRM 51-10-06. TRIM OFF FRAME SEGMENT AND FABRICATE DOUBLER PENETRANT INSP ALL NEW PARTS APPROVED 8110 ISSSDR UPS00433315Rivet · looseINSPECTION TYPE:C, LOOSE RIVETS IN TORQUE TUBE DRIVES AT VARIOUS LOCATIONS I/B END NR 15 KRUEGER FLAP, I/B AND O/B OF NR 1 L/E PDU, I/B AND O/B OF NR 3 PDU RT, OUTPUT OF L/E NR 4 PDU, I/B AND O/B OF NR 3 LT PDU, TORQUE TUBE AT NR 5 VCF, TORQUE TUBE AT NR 4 VCFSDR UPS00433325Channel · corrodedINSPECTION TYPE:C, RT WING L/E CORROSION ON L/E FALSE WORK SUPPORT CHANNEL AT OLES 1373 4 AND OLES 1444. CORROSION REMOVED DEPTH 10, AREA RE-PROTECTED IAW SRM 51-10-02.SDR UPS00433301Strap · corrodedINSPECTION TYPE:C, RT WING L/E CORROSION ON L/E LOWER IN SPAR SKIN EXT AT OLES 1116 RT. REPAIR CARRIED OUT IAW Q/NOTE 8/2000 AND SRM 57-30-03 FIG 4. BLENDED OUT CORROSION / SPLICE REPAIR.SDR UPS00433300Channel · corrodedINSPECTION TYPE:C, RT WING L/E CORROSION ON L/E LOWER FALSE WORK PANEL FWD OF SUPP CHANNEL AT SEVERAL LOCATIONS AT OLES 1066 OUT TO NR 4 ENG. REPAIR CARRIED OUT IAW QUERY NOTE 4/2000 AND SRM 51-30-01 AND 51-30 -06. REMOVED CORRODED BEAM SECTION AND SPLICE INSDR UPS00433302Panel · corrodedINSPECTION TYPE:C, RIGHT WING L/E LOWER FALSE WORK PANEL IS BULGING AT O/B WING JACK PAD LOCATION. REPAIR CARRIED OUT IAW QUERY NOTE 7/2000 AND SRM 57-30-01 AND 57-30-03. BLENDED OUT CORRODED AREA AND INSTALLED FILLER AND RETURNED AREA TO ORIGINAL DIMENSIOSDR UPS00433267Floorbeam · corrodedINSPECTION TYPE:C, MAIN DECK CORROSION ON UPPER DECK FLOORBEAM WEB AT BS 460 RBL 60. REPAIRED IAW QUERY NOTE N521 UP/3/2000 AND SRM 53-10-07 FIG 11. CUT OUT CORRODED AREA AND SPLICED IN FABRICATED WEB. APPROVED 8110 ISSUED FOR THIS REPAIR.SDR UPS00432609Line · not closedINSPECTION TYPE:C, AIR TURNBACK DUE TO FAILURE OF AIRSPEED AND ALTIMETER SYSTEM. AFTER DEBRIEF WITH CREW, FLS COMPLETED AN INSPECTION OF A/C, FOUND CAPT''S AND F/O''S PITOT DRAIN LINES UNCAPPED IN THE E & E BAY. THE FLAP SYS WAS OVERSPED. *S/D* CAPPED PITOSDR UPS00432530Frame · crackedINSPECTION TYPE:C 44, UPPER DECK, FRAME CRACKED AT STRINGER CUTOUT AT STA 500 LT, STR 11L. PLEASE REPAIR/RECTIFY. REPAIR ACCOMPLISHED IAW APPROVED REPAIR PER 8110-3. ALL THE ACTIVE CRACK TIPS WERE ELIMINATED. REINFORCING DOUBLERS AND FILLERS WERE INSTALLEDSDR UPS00432510Stringer · corrodedINSPECTION TYPE:C 44, FWD CARGO, EVIDENCE OF CORROSION FOUND ON STRINGER AT BS 984 STR 38 LT. STRINGER FABRICATED PER WORK SHOP ORDER E0169804 AND INSTALLED IAW SRM 51-30-02. REPAIR ACCOMPLISHED IAW SRM 53-10-03.SDR UPS00432520Frame · crackedINSPECTION TYPE:C 44, MAIN DECK, FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 240 STR 14 LT. REPAIR CARRIED OUT IAW SRM 53-10-04, FIG 14 AND CONTINUE WITH INSPECTIONS IN ACCORDANCE WITH SB 53A2265.SDR UPS00432519Frame · crackedINSPECTION TYPE:C 44, MAIN DECK, FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 200 STR 14. REPAIR CARRIED OUT IAW SRM 53-10-04 AND APPROVED 8110-3, DETAILS OF REPAIR TEXT AS FOLLOWS. THESE CRACKED FRAMES WERE REPAIRED BY STOP DRILLING CRACKS AND INSTSDR UPS00432518Frame · crackedINSPECTION TYPE:C 44, MAIN DECK, FUSELAGE FRAME WEB CRACKED AT CUTOUT FOR STR AT BS 200 STR 14 RT. REPAIR CARRIED OUT IAW SRM 53-10-04 AND APPROVED REPAIR DETAILED I N 8110-3.
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