Boeing 747-251F

Service difficulty reports · 400

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 = '747251F'
  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.

SDR 0601186716Frame · crackedDURING L-CHECK AND ACCOMPLISHMENT OF EM 5310-01357-01A FOUND CRACKS IN TENSION TIE FRAME FASTENER HOLES AT BS 860 LT. REPAIRED PER EA 67-206266.May 29, 2006 · N616US · Boeing 747251F · Fuselage Main, FrameSDR 0601156716Frame · crackedDURING L-CHECK AND ACCOMPLISHMENT OF EM 5310-01357-01A FOUND CRACK IN TENSION TIE FRAME FASTENER HOLE AT BS 920 RT. REPAIRED PER EA 67-206256.May 29, 2006 · N616US · Boeing 747251F · Fuselage Main, FrameSDR 0601136716Frame · crackedDURING L-CHECK FOUND CRACK IN FRAME CUTOUT AT BS 880 S9R. REPAIRED PER EA 67-206264.May 29, 2006 · N616US · Boeing 747251F · Fuselage Main, FrameSDR 0601126716Skin · corrodedDURING L-CHECK FOUND CORROSION ON RT WING LOWER SKIN AT WS 1530. REPAIRED PER EA 67-206259.May 27, 2006 · N616US · Boeing 747251F · Wing, Plate/SkinSDR 0601146716Frame · crackedDURING L-CHECK AND ACCOMPLISHMENT OF EM 5310-01357-01A FOUND CRACK IN TENSION TIE FRAME FASTENER HOLE AT BS 940 RT. REPAIRED PER EA 67-206260.May 26, 2006 · N616US · Boeing 747251F · Fuselage Main, FrameSDR 0601116716Frame · crackedDURING L-CHECK AND ACCOMPLISHMENT OF MOD PER EM 5310-01319-02K FOUND CRACK IN UPPER DECK FRAME WEB CHORD AT BS 420 S12R. REPAIRED PER EA 67-206251.May 24, 2006 · N616US · Boeing 747251F · Fuselage Main, FrameSDR 0601036740Housing · brokenAFTER GEAR RETRACTION ON TAKEOFF, NR 4 HYDRAULIC QUANTITY LOW LIGHT ILLUMINATED, AND INDICATOR WENT TO 0. CREW FOLLOWED COM PROCEDURE. DUMPED FUEL, RETURNED TO ANC, AND LANDED WITHOUT INCIDENT. ANC MAINTENANCE FOUND RIGHT CENTRAL CONTROL ACTUATOR FILTER HOUMay 18, 2006 · N640US · Boeing 747251F · Hydraulic System, MainSDR 0600936719Strap · crackedDURING L-CHECK FOUND CRACK IN NR 2 PYLON BULKHEAD STRAP AT NAC STA 224 AND SKIN CRACK AT NAC STA 221.9. REPAIRED PER EA 67-206237 SECT I, SECTION II CALLS FOR REPEAT INSPECTIONS AT L-CHECK INTERVALS OR 18 MONTHS WHICHEVER COMES FIRST.Apr 29, 2006 · N619US · Boeing 747251F · Nacelle/Pylon, Bulkhead/FirewallSDR 0600866719Strap · crackedDURING L-CHECK FOUND CRACK IN UPPER DECK FLOORBEAM REINFORCEMENT STRAP AT BS 440 LBL 38 AND LBL 43. REPAIR ACCOMPLISHED AS PER SECTION I OF EA 67-206233, SECTION II PERMANENT REPAIR IS TO BE ACCOMPLISHED BY OR BEFORE APRIL 29, 2007.Apr 29, 2006 · N619US · Boeing 747251F · Fuselage Main, Floor BeamSDR 0600946719Bulkhead · crackedDURING L-CHECK FOUND CORROSION ON CANTED BULKHEAD WEB AT BS 1241 RBL 37.5. REPAIRED PER EA 67-206232.Apr 27, 2006 · N619US · Boeing 747251F · Fuselage Main, BulkheadSDR 0600956719Floorbeam · crackedDURING L-CHECK FOUND CRACK IN UPPER DECK FLOORBEAM FLANGE AT BS 240. REPAIRED PER EA 67-206225.Apr 21, 2006 · N619US · Boeing 747251F · Fuselage Main, Floor BeamSDR 0600676718Control Panel · smokeWHILE AT CRUISE, ACARS SCREEN WENT BLANK, AND THEN STARTED TO SMOKE. FLIGHT CREW PULLED ACARS C/B'S SMOKE STOPPED AND DISSIPATED. FLIGHT CONTINUED ON AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED ACARS CONTROL PANEL. OPS CHECKED GOOD, AIRCRApr 4, 2006 · N618US · Boeing 747251F · Data Transmission Auto CallSDR 0600226716Floorbeam · crackedDURING H-CHECK, FOUND CRACK ON UPPER DECK FLOORBEAM FASTENER HOLE AT BS 340 RBL 42. REPAIRED IAW EA 67-165190.Jan 20, 2006 · N617US · Boeing 747251F · Fuselage Main, Floor BeamSDR 0600186716Actuator · failedAFTER TAKEOFF NR 3 HYDRAULIC SYSTEM QUANTITY WENT TO NEAR ZERO. AIRCRAFT DUMPED 150,000 LBS OF FUEL AND RETURNED TO ANC, AND LANDED WITHOUT INCIDENT. ANC MAINTENANCE REMOVED AND REPLACED RUDDER ACTUATOR, AND NR 3 ENG HYDRAULIC PUMP. OPERATIONAL CHECKED OK, Jan 20, 2006 · N616US · Boeing 747251F · Rudder Control SystemSDR 0501766739None · noneABORTED TAKEOFF BECAUSE PILOT FELT SOMETHING WAS WRONG WITH THE RUDDER, BUT IS WAS JUST A STRONG CROSS WIND. NRT MAINTENANCE CHECKED ALL MAIN WHEEL BRAKES AND FOUND OK. RUDDER OPERATION CHECKED OK. NO TROUBLE FOUND, AIRCRAFT RETURNED TO SERVICE.Dec 17, 2005 · N639US · Boeing 747251F · Aircraft StructuresSDR 0501466718Control Panel · failedDURING CRUISE THE PMS (PERFORMANCE MANAGEMENT SYSTEM) WENT BLANK. SMELLED ELECTRICAL SMOKE, AND SMOKE WAS VISIBLE FROM PEDESTAL AROUND PMS BASE. FLIGHT CREW PUT ON O2 MASKS AND GOGGLES, REFERRED TO RED CHECK LIST AND COM PROCEDURE. FOUND PMS CDU C/B POPPED,Sep 24, 2005 · N618US · Boeing 747251F · Flight Management Computing Hardware SystemSDR 0501576718Frame · corrodedDURING L-CHECK FOUND CORROSION AND CRACK ON FRAME IN LT BLG WHEEL WELL AT BS 1146. REPAIRED IAW EA 67-165244.Sep 16, 2005 · N618US · Boeing 747251F · Fuselage Main, FrameSDR 0501566718Frame · crackedDURING L-CHECK FOUND CRACK IN FRAME AT BS 380 S27R AND S28R. REPAIRED IAW EA 67-165241.Sep 15, 2005 · N618US · Boeing 747251F · Fuselage Main, FrameSDR 0501406717Frame · corrodedDURING L-CHECK FOUND CORROSION ON FRAME LOWER CHORD AT BS 400 BETWEEN S40L AND S41L. REPAIRED PER EA 67-165239.Aug 19, 2005 · N617US · Boeing 747251F · Fuselage Main, FrameSDR 0501346717Frame · crackedDURING L-CHECK FOUND CRACKS IN FRAME AT BS 380 S24L. REPAIRED PER EA 67-165232.Aug 18, 2005 · N617US · Boeing 747251F · Fuselage Main, FrameSDR 0501336717Frame · crackedDURING L-CHECK FOUND CRACK IN FRAME AT BS 400 S23L. REPAIRED PER EA 67-165233.Aug 18, 2005 · N617US · Boeing 747251F · Fuselage Main, FrameSDR 0501326717Skin · crackedDURING L-CHECK FOUND CRACK IN FUSELAGE SKIN BETWEEN BS 2060 - 2080 S31R-33R. REPAIRED PER EA 67-165234.Aug 9, 2005 · N617US · Boeing 747251F · Fuselage Main, Plate/SkinSDR 0501096717Fire Loop · malfunctionedDURING CRUISE, APU FIRE LIGHT B LOOP ILLUMINATED WITH BELL. THEN SELECTED LOOP A. AIRCRAFT CONTINUED ON TO ANC AND LANDED WITHOUT INCIDENT. ANC MAINTENANCE PUT APU FIRE LOOP B ON MEL. 18JUL05 SIN MAINTENANCE R&R UPPER FIRE DETECTOR ELEMENTS LOOP A & B. OPJul 14, 2005 · N617US · Boeing 747251F · Fire DetectionSDR 0501146718Fuel Cell · leakingDURING TAKE-OFF THERE WAS A STRONG FUEL ODOR IN COCKPIT. SMELL CLEARED ONCE PACKS WERE TURNED ON. AIRCRAFT CONTINUED ON TO DESTINATION AND LANDED WITHOUT INCIDENT. ANC MAINTENANCE FOUND LEAK ON SEAM 15 INCHES AHEAD OF NR 2 SUMP DRAIN, AND SEALED EXTERNAL TAJul 8, 2005 · N618US · Boeing 747251F · Fuel StorageSDR 0501016717Wire · chafedDURING CRUISE, APU FIRE LIGHT ILLUMINATED WITH BELL. LIGHT AND BELL EXTINGUISHED WHEN FAULT TEST WAS ACCOMPLISHED. AIRCRAFT CONTINUED ON TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE PUT APU FIRE LOOP B ON MEL. MAINTENANCE FOUND CHAFED WIRE AND REPJul 8, 2005 · N617US · Boeing 747251F · Fire DetectionSDR 0501136718Odor · detectedDURING ROTATION AT TAKE-OFF, THERE WAS A STRONG SMELL OF FUEL ODOR. SMELL CLEARED IN 2-3 MINUTES AFTER PACK ACTIVATION. AIRCRAFT CONTINUED ON TO DESTINATION AND LANDED WITHOUT INCIDENT. SIN MAINTENANCE CHECKED FOR FUEL LEAKS, NONE FOUND. AIRCRAFT OK FOR REJul 7, 2005 · N618US · Boeing 747251F · Air Distribution SystemSDR 0501086740Frame · crackedDURING L-CHECK FOUND CRACK IN FRAME WEB AT BS 460 S12L. REPAIRED PER EA 67-165219.Jul 4, 2005 · N640US · Boeing 747251F · Fuselage Main, FrameSDR 0501076740Frame · crackedDURING L-CHECK FOUND CRACK IN FRAME AT BS 460 S14L. REPAIRED PER EA 67-165222.Jul 2, 2005 · N640US · Boeing 747251F · Fuselage Main, FrameSDR 0501286717Pressure Panel · crackedDURING LINE CHECK FOUND CRACK IN RIGHT HAND NOSE WHEEL WELL SIDE PANEL WEB. REPAIRED PER EA 67-204659.Jun 18, 2005 · N617US · Boeing 747251F · Fuselage Main, BulkheadSDR 0500776719Light · inoperativeDURING CLIMB-OUT, SMOKE FILLED FLIGHT DECK. AIRCRAFT RETURNED TO SIN AND LANDED WITHOUT INCIDENT. SIN MAINTENANCE FOUND FE PANEL LIGHT CB POPPED. FE DIMMER WAS BURNED. MEL'D COCKPIT LIGHTS, AND COLLARED BREAKER AND WILL REPLACE DIMMER IN NRT. NRT MAINTENAMay 16, 2005 · N619US · Boeing 747251F · Flight Compartment LightingSDR 0500656718Skin · crackedDURING OVERNIGHT LINE CHECK, FOUND CRACK IN FUSELAGE SKIN AT BS 1705 S34L. REFERENCE SB 747-53A2487, AD 2002-23-15 AND AD 2004-07-22. REPAIRED PER EA 67-192649.Apr 28, 2005 · N618US · Boeing 747251F · Fuselage Main, Plate/SkinSDR 0500586739Frame · crackedDURING LINE CHECK AND IN COMPLIANCE WITH AD 2005-04-51, FOUND CRACK IN FRAME AT BS 460 S12L. REPAIRED PER EA 67-203103.Mar 7, 2005 · N639US · Boeing 747251F · Fuselage Main, FrameSDR 0500246730Frame · crackedDURING LINE CHECK FOUND CRACK IN FRAME AT BS 440 STRINGER 10L. REPAIRED PER EA 67-203062.Feb 27, 2005 · N640US · Boeing 747251F · Fuselage Main, FrameSDR 0500196729Engine · overheatedSHORTLY AFTER TAKEOFF, THE NR 4 ENGINE NACELLE TEMPERATURE BEGAN TO INCREASE FOLLOWED BY THE FIRE WARNING ANNUNCIATION. THE CREW FOLLOWED COM PROCEDURES AND WHEN POWER WAS REDUCED THE FIRE WARNING CEASED AND THE NACELLE TEMPERATURE BEGAN TO DECREASE. THE NR Feb 14, 2005 · N629US · Boeing 747251F · Engine (Turbine/Turboprop)SDR 0402256719Frame · crackedDURING L-CHECK, FOUND CRACK IN FRAME AT BS 380 S24R. REPAIRED PER EA 67-165180.Dec 24, 2004 · N619US · Boeing 747251F · Fuselage Main, FrameSDR 0402236719Frame · crackedDURING L-CHECK FOUND CRACK IN FRAME AT BS 400 S23L. REPAIRED PER EA 67-165182.Dec 23, 2004 · N619US · Boeing 747251F · Fuselage Main, FrameSDR 0401436718Engine · fireDURING TAXI IN, THE NR 2 ENGINE FIRE WARNING ANNUNCIATED. THE CREW SHUT DOWN THE ENGINE AND DISCHARGED THE LT FIRE BOTTLE FOR NR 2 ENGINE. THE FIRE WARNING CEASED. NO OTHER ABNORMAL ENGINE INDICATIONS WERE OBSERVED. MAINTENANCE INSPECTION FOUND EVIDENCE OF A Aug 24, 2004 · N618US · Boeing 747251F · Engine (Turbine/Turboprop)SDR 0401166729Floorbeam · crackedDURING L-CHECK AND ARMAR FOUND CRACK IN FLOORBEAM WEB AT BS 380 BETWEEN S12L & S13L. REPAIRED PER EA 67-165144.Jul 9, 2004 · N629US · Boeing 747251F · Fuselage Main, Floor BeamSDR 0401226717Frame · crackedDURING H-CHECK FOUND CRACK IN FRAME WEB AT BS 360 S24L. REPAIRED PER EA 67-165134.May 31, 2004 · N617US · Boeing 747251F · Fuselage Main, FrameSDR 0400696718Bulkhead · crackedDURING H-CHECK FOUND CRACK IN BULKHEAD CHORD AT BS 1000 FROM 36L TO 40L. REPAIRED PER EA 67-165121.May 5, 2004 · N618US · Boeing 747251F · Fuselage Main, BulkheadSDR 0400726718Floorbeam · crackedDURING H-CHECK FOUND CRACK IN UPPER DECK FLOORBEAM CHORD AT BS 520. REPAIRED PER EA 67-165122.May 4, 2004 · N618US · Boeing 747251F · Fuselage Main, Floor BeamSDR 0400716718Floorbeam · crackedDURING H-CHECK FOUND CRACK IN UPPER DECK FLOORBEAM CHORD AT BS 420 BETWEEN LBL 8 AND RBL 58. REPAIRED PER EA 67-165119.May 4, 2004 · N618US · Boeing 747251F · Fuselage Main, Floor BeamSDR 0400736718Fitting · crackedDURING H-CHECK FOUND CRACK IN NOSE CARGO DOOR FRAME CLOSURE FITTING. REPAIRED PER EA 67-165115.Apr 30, 2004 · N618US · Boeing 747251F · Fuselage Main, Attach FittingsSDR 0400496740Warning Light · false indicationDURING TAKEOFF, THE BRAKE OVERHEAT LIGHT ILLUMINATED. AIRCRAFT ABORTED TAKEOFF AT 120 KNOTS AND RETURNED TO THE GATE WITHOUT INCIDENT. VISUALLY INSPECTED AND OPERATIONALLY CHECKED THE BRAKING SYSTEM WITH NO FAULTS FOUND.Mar 24, 2004 · N640US · Boeing 747251F · Landing Gear Brake SystemSDR 0400246716Circuit Card · malfunctionedDURING APPROACH, THE RED LANDING GEAR LIGHT ILLUMINATED WHILE THE LANDING GEAR INDICATED DOWN AND LOCKED. RECYCLED THE LANDING GEAR AND THE RED LANDING GEAR LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. RESEATED THE GPWS AND THE PRIMARY AND ALTERNATFeb 4, 2004 · N3260 · Boeing 747251F · Landing Gear Position and WarningSDR 0400186740Bulkhead · corrodedDURING H-CHECK FOUND CORROSION ON LOWER BULKHEAD CHORD AT BS 1000 S 41L. REPAIRED PER EA 67-165093.Jan 2, 2004 · N640US · Boeing 747251F · Fuselage Main, BulkheadSDR 0467400018Bulkhead · corrodedDURING H-CHECK FOUND CORROSION ON LOWER BULKHEAD CHORD AT BS 1000 S 41L. REPAIRED PER EA 67-165093.Jan 2, 2004 · N640US · Boeing 747251F · Fuselage Main, BulkheadSDR 0302056718Amplifier · faultyDURING CRUISE, THE NR 5 MAIN DECK CARGO SMOKE DETECTION SYSTEM INDICATED A FIRE. THE OVERHEAD CARGO FIRE LIGHT ILLUMINATED AND THE MASTER FIRE WARNING ACTIVATED. VISUALLY INSPECTED CARGO ON MAIN DECK WITH NO SIGNS OF FIRE OR SMOKE. AIRCRAFT CONTINUED TO DESNov 15, 2003 · N618US · Boeing 747251F · Smoke DetectionSDR 0301696718Computer · inoperativeDURING CLIMB THE LOWER YAW DAMPER LIGHT ILLUMINATED BRIEFLY AND THE AIRCRAFT WAS DIFFICULT TO CONTROL IN HEADING. SLOWED AIRCRAFT TO 270 KNOTS AND TURNED OFF LOWER YAW DAMPER BUT AIRCRAFT WAS STILL DIFFICULT TO CONTROL IN HEADING. AIRCRAFT DECLARED AN EMERGENCSep 4, 2003 · N618US · Boeing 747251F · Autopilot SystemSDR 0301556717Terminal · damagedDURING CLIMB WITH NR 4 ENGINE FIRE LOOP -A- ON MEL, THE FAULT DETECTION ANNUNCIATOR ILLUMINATED FOR THE NR 4 ENGINE B-FIRE DETECTOR. AIRCRAFT RETURNED TO ANC AND LANDED WITHOUT INCIDENT. REPLACED TERMINALS FOR (A) AND (B) FIRE LOOPS AND REPLACED THE RIGHT SIDEAug 9, 2003 · N617US · Boeing 747251F · Smoke Detection
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