Boeing 747-249F
Service difficulty reports · 501
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 = '747249F' 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 = '747249F' 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 0202446743Shear Tie · crackedDuring "M" check found cracks in shear tie at BS 520 between S8L and S10L. Repaired per EA 67-191111.SDR P5CA0200686Autopilot Sys · malfunctionedB-AUTOPILOT WILL NOT ACCEPT STEERING COMMANDS IN HDG OR INS MODE. ALSO INOP IN MANUAL. TRANSFERRED TO DEFERRED MX ITEM.SDR P5CA0200685Wire · broken"A" AUTOPILOT WILL NOT ACCEPT STEERING COMMANDS IN HDG OR INS MODES. ALSO INOP IN MANUAL. TRANSFERRED TO DEFERRED MX ITEM ID #036042 CTR #29299 IAW MEL 02-22-2-1 IN CONSULT W/ MTC & PLACARD INSTALLED. JFK MX FOUND BROKEN WIRE AT PINS 9 & 10 ON CONNECTOR DB193 SDR P5CA0200690Acoustic Panel · damagedAPU EXHAUST ACOUSTIC LINER DAMAGED AT 01:30 O'CLOCK POSITION. APU LINER REMOVED & REPLACED IAW MM 49-81-02.SDR P5CA0200689Shroud · crackedCRACKS FOUND ON NR 1 ENG TURBINE COOLING SHROUD AT 8 & 2 O'CLOCK POSITIONS. RT (2 CRACKS) NR 1 IS 5 INCHES LONG & NR 2 IS 2 INCHES LONG. LT (4 CRACKS) NR 1 IS 3 INCHES LONG, NR 2 IS 5 INCHES LONG, NR 3 IS 1.5 INCH LONG & NR 4 IS 1.5 INCH LONG. ALSO BRACKET SDR P5CA0200688Panel · crackedCRACK 15" LONG FOUND RH WING UPPER SKIN LE FIXED PANEL AT WS 834 TO WS 862. PANEL SHOWS 15 X 30 IN. SQ AREA DELAMINATED. LEADING EDGE FIXED PANEL AT WS 834 TO WS 862 REMOVED & NEW PANEL INSTALLED IAW SRM 51-10-01, PG 8, SECT 6, PARA A-B-C. ALSO SRM 51-30-02.SDR P5CA0200687Door · crackedA 2 INCH LONG CRACK FOUND ON APU INLET DOOR OUTSIDE LOWER FORWARD CORNER. COMPOSITE REPAIR CARRIED OUT WITH REF TO SRM 51-40-06. AREA PROTECTED WITH REF TO SRM 51-21-01.SDR P5CA0200682Web · crackedFOUR CRACKS FOUND ON NR 2 ENG PYLON, AFT ENGINE MOUNT BULKHEAD FRAME, VERTICAL WEB STATION 221.9. (1. CRACK ON FRONT OUTBOARD WEB, 3 INCHES LONG. 2. CRACK ON FRONT OUTBOARD WEB, 1 INCH LONG. 3. CRACK ON FRONT INBOARD WEB, 3.5 INCH LONG. 4. CRACK ON FRONT OUSDR P5CA0200683Web · crackedTHREE CRACKS FOUND ON NR 3 ENG PYLON, AFT ENGINE MOUNT BULKHEAD FRAME, VERTICAL WEB STATION 221.9. (1. CRACK ON FRONT OF OUTBOARD WEB, 2 INCHES LONG. 2. CRACK ON FRONT OUTBOARD WEB, 1 INCH LONG. 3. CRACK ON FRONT OUTBOARD WEB, 3 INCHES LONG). BULKHEAD LOWERSDR P5CA0200681Web · crackedCRACK 8 INCHES LONG FOUND NR 2 ENG PYLON FORWARD LOWER SPAR FLOOR WEB AT STA 270, MID SPAR (PANEL 452CL). COMPLETED REPAIRS IAW BOEING REPAIR SCHEME DWGS PAO-LGB-02-00056F, 55F, 54H, 53F & 52H.SDR P5CA0200680Mount · corrodedLEVEL 1 CORROSION FOUND ON ENG UPPER REAR MOUNT BULKHEAD FITTING LOWER LUGS WHILE REMOVING NR 2 ENG REAR UPPER MOUNT FOR REPAIRS. ACCOMPLISHED SB 747-54A2200. COATED MOUNT W/ BMS 14-4, TYPE 2. COATING IAW 747-A2200 SERMATECH ENGINEERING BULLETIN 249.SDR P5CA0200679Mount · wornNR 2 ENG AFT UPPER ENG MOUNT BENT ON ALIGNMENT HOLE, MOUNT ASSY WORN. REMOVED & REPLACED AFT ENG MOUNT IAW MM 71-21-03.SDR P5CA0200678Web · crackedCRACK 3.5" LONG FOUND #3 PYLON WEB BETWEEN RIVET HOLES BELOW STIFFNER (STA 211.42, MID SPAR WEB). DOUBLER REPAIR FABRICATED IAW SRM 54-14-03, PG 20. THE RIVETS WERE REMOVED PLUS FURTHER 3 EITHER SIDE OF CRACK. 2 OF FURTHER ROWS OF FASTENERS PITCHED FORWARD SDR P5CA0200677Ground Wire · brokenNR 2 ENGINE PYLON HYD S/O VALVE GROUND WIRES, PYLON STA 270, BROKEN. REPAIRED GROUND WIRES IAW SWP 20-11-15.SDR P5CA0200676Skin · crackedFOUND 1" CRACK IN LOWER SKIN FUSELAGE AT STA 2390, LBL70. FABRICATED REPAIR PLATE & DRILLED FASTENER HOLES. APPLIED ALODINE TO CUT EDGES OF REPAIR PLATE & REPAIR SKIN AREA. PRIMED FAYING SURFACES. INSTALLED REPAIR PLATE W/ FASTENERS. USED BMS 5-95 TO SEALSDR P5CA0200672Bearing · failed#2 APU GENERATOR BEARING FAILURE LIGHT ILLUMINATED & GRND CREW REPORTED SMOKE EMANATING FROM APU. FIRE HANDLE PULLED & BOTTLE DISCHARGED AS A PRECAUTION. VISUAL INSPECTION OF APU COMPARTMENT BY MX & F/E SHOWED DAMAGE ONLY TO THE #2 GENERATOR. NO FIRE OR DAMAGESDR 0201206743Hydraulic Line · leakingDURING FLIGHT, LOST HYDRAULIC FLUID IN THE NR 2 HYDRAULIC SYSTEM. PERFORMED COM PROCEDURES AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE HYDRAULIC RETURN LINE AT THE RIGHT INBOARD AILERON POWER CONTROL UNIT. OPERATIONALSDR P5CA0200651Flap Track · corrodedFOUND LIGHT CORROSION, AREA 600, ON UPPER FLAP TRACKS AND CENTER TOGGLE ROLLERS ON NR 5, 6, 7 & 8 FLAP TRACKS. REMOVED CORROSION AND RETREATED IAW MM 27-51-22 & 27-51-23, PAGE 801.SDR P5CA0200650Flap Track · corrodedLEVEL 1 CORROSION: FOUND LIGHT CORROSION, AREA 500, ON UPPER FLAP TRACKS AND CENTER TOGGLE ROLLERS ON NR 1, 2, 3 & 4 FLAP TRACKS. REMOVED CORROSION AND RETREATED IAW MM 27-51-22 & 27-51-23, PAGE 801.SDR P5CA0200649Bolt · wornWORN LT WING BODY GEAR, AREA 751; SUPPORT ROD BOLT WORN. REMOVED BOLTS/BUSHINGS AND CLEANED UP. REASSEMBLED IAW MM 32-13-00 WITH LUBRICATION AND NEW WASHERS INSTALLED TO CORRECT ITEM. FOUND DOOR TO ROD BEARINGS AND BOLTS NOW WITHIN LIMITS. OK FOR SERVICE.SDR P5CA0200640Switch · out of adjustTAKEOFF WARNING HORN WHEN POWER IS ADVANCED. ADJUSTED SPEED BRAKE DOWN SWITCH IAW 31-26-05. OPS CHECK NORMAL.SDR P5CA0200628Transmitter · faultyON APPLICATION OF PWR AT T/O NR 3 ENG NOT ACCELERATING TO 1.58 EPR SETTING. T/O DISCONTINUED. REMOVED AND REPLACED TT2 SENSOR PER 73-21-04. LEAK CKS GOOD BUT NO HELP. ON ENG RUN IDLE TO 80 PERCENT, N1 TOOK 4.5 SECS, EPR LAGGED AND STABILIZED - TOOK 10 SECSSDR P5CA0200627Control Unit · out of rigNR 3 ENG WOULD NOT ACHIEVE T/O THRUST. 1.58 MAX PWR WAS APPLIED, THRUST LEVER WAS MOVED TO FIREWALL THRUST W/ MAX EPR OF 1.38. OTHER PARAMETERS NORMAL WHEN ASSOCIATED W/ & EPR SETTING OF 1.38 ENG RUN TO MAX POWER FOR OPS CK INTO WIND (250/11). ENG SLOW TO RSDR P5CA0200629Wire · brokenRT BODY GEAR LEFT REAR (NR 11) ANTI-SKID LIGHT CAME ON AND WOULD NOT RESET. WHEEL ASSY RETORQUED FOR PRECAUTION PER MM 32-45-01. NR 11 BRAKE DEACTIVATED PER MEL. REPAIRED BROKEN WIRES AT TRANSDUCER ELECT CONNECTION PER MM STANDARD PRACTICES. REACTIVATED NRSDR P5CA0200623Switch · malfunctioned#3 ENGINE OIL PRESSURE LITE ON PILOT'S FWD ANNUNCIATOR PANEL ILLUMINATED. ALT PROCEDURES CHECK LIST ACCOMPLISHED - OIL PRESS, QUANTITY NORMAL - FILTER BYPASS LIGHT EXTINGUISHED. REMOVED & REPLACED LOW OIL PRESS SWITCH PER MM 79-33-01. PERFORMED WINDMILL INSPSDR P5CA0100622Seal · leakingAT APPROX. 15 MIN. INTO CRUISE (FL 33.0), #4 OIL QTY RAPIDLY DROPPED TO ZERO. FWD CAUTION PANEL LOW OIL PRESSURE LIGHT CAME ON. PRECAUTIONARY ENG SHUTDOWN ACCOMPLISHED PER ABNORMAL PROCEDURES. UPON INSPECTION FOUND GEARBOX N2 FULL OF OIL W/ TANK EMPTY.REPAIRESDR P5CA0100621Flap · delaminatedLEFT INBOARD T/E FLAP HAS 4 AREA OF SLIGHT DELAMINATION. REPAIRED PER SRM 20-11-14.SDR P5CA0100620Retainer · tornNR 1 ENGINE PYLON SAILBOAT DOOR, INBOARD SIDE, LOWER FWD END, HAS A 6 INCH RIP IN SEAL RETAINER. REPAIRED PER SRM 51-40-00.SDR P5CA0100619Doubler · torn#2 PYLON INBD SIDE, AFT END, ABOVE AFT MOUNT, HAS A 1" RIP IN DOUBLER. REPAIRED PER SRM 54-12-01 & SRM 51-40-00.SDR P5CA0100618Bearing · wornL/BODY GEAR STRUT DOOR LINK ROD ATTACH FITING BEARING WORN. REMOVED & REPLACED FITTING/BEARING PER MM 32-14-06.SDR 0104646743Smoke Detector · dirtyDuring flight, the #5 main deck cargo smoke detector light illuminated accompanied with alarm lights and fire bell. Aircraft continued to destination and landed without incident. Cleaned both detectors. Operational check good.SDR P5CA0100613Fairing · damagedL/H HORIZONTAL STABILIZER STA 560 OUTBOARD TIP - AFT WEDGE 6" SECTION BROKEN OFF. REMOVED & REPLACED T/E & BOTTOM ACCESS PANELS PER SRM 51-10-01.SDR P5CA0100606Web · crackedNOSE GEAR WHEEL WELL FRAME WEB CRACKED, APPROX. 1/8" LONG, BY INSULATION HOLES FIRST & FOUR FROM FLOOR CHORD ANGLE ON RIGHT SIDE. OPENED HOLES TO 7/16", RE-INSPECTED BY H.F.E.C. - NO INDICATIONS. REPAIRED IAW BOEING SERVICE LETTER PAO-LGB-01-0015514, SB74752SDR P5CA0100601Transformer · malfunctionedSMELLED SMOKE IN COCKPIT. FOUND PILOT'S BACKGROUND LIGHT C/B OPEN & MAIN PANEL BACKGROUND LIGHT CONTROL KNOB VERY HOT. (NEXT TO THUNDERSTORM LIGHT SWITCH). SMOKE WENT AWAY. REPLACED TRANSFORMER. OPS NORMAL.SDR 0103536743Controller · failedDURING CLIMB, AN ELECTRICAL BURNING SMELL EMITTED IN THE COCKPIT. AIRCRAFT DIVERTED TO NRT AND LANDED WITHOUT INCIDENT. REPLACED THE R1 WINDOW HEAT CONTROLLER, R1 WINDOW, APU BATTERY CHARGER, AND CLEANED AN INSTRUMENT COOLING DUCT. OPERATIONAL CHECK GOOD.SDR 0100572Skin · bulgedMAIN DECK CARGO DOOR EXTERNAL SKIN BULGING AT LATCH ACCESS PANEL CUT OUT (2ND FROM FWD). DAMAGED AREA TRIMMED OUT AND A FILLER AND STRAP INSTALLED PER BOEING TELEX SIA-SIN -01-00947H FAA FORM 8110-3 DATED JUNE 21.SDR P5CA0100585Intercostal · corrodedLEVEL 1 CORROSION - BULK CARGO FLOOR INTERCOSTAL AT STA 2040 RBL 23 FOUND CORRODED. CORROSION REMOVED AND INSPECTED. FOUND WITHIN LIMITS AS PER SRM 51-10-01 & SRM 53-10-01. BLENDED SURFACES, REPROTECTED AND REPLACED ANCHOR NUT AS PER SRM 51-10-02 & SRM 51-3SDR P5CA0100584Intercostal · corrodedLEVEL 1 CORROSION - BULK CARGO FLOOR INTERCOSTAL AT STA 2040 LBL 23 FOUND CORRODED. CORROSION REMOVED AND INSPECTED. FOUND WITHIN LIMITS AS PER SRM 51-010-01 & SRM 53-10-01. BLENDED SURFACES, RE-PROTECTED AND REPLACED ANCHOR NUT AS PER SRM 51-10-02 & SRM 51SDR P5CA0100583KeelbeamLEVEL 1 CORROSION - KEEL BEAM LOWER PANEL SUPPORT STRUCTURE CORRODED AT RBL 15 FROM STA 1273 TO 1352. INSPECT AREA AS PER SRM 51-10-01. BLENDED OUT CORROSION AS PER 53-10-01 FOUND W/IN LIMIT OF 20% THICK. AREA RE-PROTECTED W/ ALODINE & PRIMER AS PER SRM 51-10-SDR P5CA0100582KeelbeamLEVEL 1 CORROSION - KEEL BEAM LOWER PANEL SUPPORT BEAM CORRODED AT STA 1391 LBL 15 TO RBL 15. BLENDED OUT CORROSION AS PER 53-10-01. CLEANED OUT DEPTH W/IN LIMIT OF 20% THICKNESS. RE-PROTECTED W/ ALODINE & PRIMER AS PER SRM 51-10-02. DIMENSIONS ARE MATERIAL THSDR P5CA0100581Floorbeam · corrodedLEVEL 1 CORROSION, FOUND MAIN DECK FLOORBEAM CORROSION ON TOP FLANGE AT STA 2260 RBL 41. REPAIR CARRIED OUT AS PER 53-11-23 & SRM 51-40-04.SDR 0100579Threshold · corrodedCORROSION FOUND AT STA 460 - 480 NR 1 RT FWD ENTRY DOOR THRESHOLD PLATE UNDERNEATH FLOORBEAM. REPAIR CARRIED OUT AS PER SRM 51-40-02.SDR 0100577Floorbeam · corrodedCORROSION FOUND ON MAIN DECK FLOORBEAM STA 2240 RBL 54 TOP OF CHORD. REPAIR CARRIED OUT AS PER SRM 53-11-23 & SRM 51-40-04.SDR 0100576Structure · corrodedCORROSION FOUND BEHIND ATTACHMENT FLANGE OF WING TO BODY FAIRING SUPPORT RIB AT STA 1480 LBL 75 TO LBL 90. REMOVED CHORD AND AFFECTED AREA PER IAW SRM 53-10-01 AND SRM 51-30-00.SDR 0100575Support · corrodedCORROSION FOUND ON KEEL BEAM LOWER PANEL SUPPORT STRUCTURE AT RBL 15 FROM STA 1391 TO STA 1437. BLENDED OUT CORROSION AS PER SRM 51-10-01.SDR 0100573Nut · corrodedLEVEL 1 CORROSION FOUND ON AIRCON PANEL SUPPORT STRUCTURE AT LOWER SURFACE AT RBL 53 STA 1170 & 1152. REMOVED AND REPLACED CORRODED ANCHOR NUT, BLEND OUT CORROSION AS PER SRM 53-10-01.SDR 0100571Support · corrodedLEVEL 1 CORROSION AT STA 500 - 520 LBL 37 FLOORBEAM SUPPORT STRUCTURE SPLICE INTERCOSTAL. REPAIR CARRIED OUT AS PER SRM 53-10-05.SDR 0100578Balance Weight · corrodedCORROSION FOUND ON LEFT O/B ELEVATOR BALANCE WEIGHT. NUT BLAST PER 747 SL-55-07 FINISH PER 747-32-55-07.SDR P5CA0100569Slide · defectiveRT UPPER DECK SLIDE BLOWN BY MAINTENANCE AND ONLY HALF INFLATED. REPLACED U/D RIGHT SLIDE ASSIST BOTTLE. REMOVED AND REPLACED U/D RIGHT SLIDE FOUND SHEARED CABLE. P/N ON 7A1248-36 S/N ON G476.SDR P5CA0100466Fire Warning · activatedNR 2 ENG FIRE DET LIGHT AND FAULT LIGHT CAME ON A-LOOP WITH A FIRE WARNING. ENGINE SHUT DOWN AND BOTTLE FIRED. REPLACED NR 2 LFT FIRE BOTTLE. P/N ON 33603903P, S/N M2621
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