Boeing 747-47UF
Service difficulty reports · 3,116
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 = '74747UF' 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 = '74747UF' 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 UIEA2011111000642Seal · brokenFOUND 7TH DESCENT DEVICE SAFETY SEAL BROKEN. (REPLACED DESCENT DEVICE)SDR UIEA2011111500650Structure · damagedDURING A CHECK INSPECTION, FOUND LT INBD FORE FLAP DAMAGED. L/E AREA DAMAGED LENGTH 1.25" FRONT SPAR WEB DAMAGE 8" X 4". LT INBD FORE FLAP REMOVED IAW AMM 27-51-02. INSTALLED NEW LT INBD FORE FLAP IAW AMM 27-51-02. ADJUST IAW AMM 27-51-01. OPS CHECKED OK.SDR UIEA2011110600638Door · damagedDURING WALKAROUND INSP, MX FOUND THE LT WING GEAR DOOR FAIRING - LOWER EDGE CRACKED, MEASURING 7.0 IN. X 2.0 IN. (REF FIG 1) DAMAGE FOUND TO BE BEYOND THE SRM 52-80-02, FIG 101 ALLOWABLE DAMAGE 4 LIMITS IAW SRM 51-70-02, FIG 101 (SHEET 9 OF 41) ALLOWABLE DAMAGSDR UIEA2011110600637Support Channel · damagedWING RIB SUPPORT CHANNEL WAS FOUND DAMAGED AS A RESULT OF THE LT INBD T/E FLAP INCIDENT ON 412. THE DAMAGES WHICH ARE APROX 2" LONG X 0.5" DEEP AND 2.5" LONG X 0.3" DEEP ARE LOCATED ON THE OTBD AND INBD FLANGES OF THE CHANNEL. (SINCE A REPLACEMENT PART COULD SDR UIEA2011102600632Floorboard · damagedDURING A-CHECK INSPECTION, MX REPORTED DAMAGE FOUND TO MAIN DECK - FLOORBOARD PANEL BS 1700 - 2020, LBL 99 AND OTBD GOUGE/DELAMINATION DAMAGE (PART 1 -TIME LIMITED REPAIR SCHEDULE PRIOR TO FURTHER FLIGHT; THIS EO DOCUMENTS THAT A TIME LIMITED REPAIR WAS ACCOMPSDR UIEA2011102600631Fairing · missingDURING WALK AROUND MX FOUND NR 3 ENGINE LT THRUST REVERSER FAIRING TOP SECTION MISSING 3.0" X 4.0" PIECE OF MATERIAL, REF FIG 1 AND FIG 2. (DISPOSITION IS TO PERFORM PERMANENT REPAIR AS DESCRIBED IN PART 1 OF THIS EO. THIS REPAIR IS DERIVED FROM SIMILAR REPAISDR UIEA2011102500630Structure · crackedMAIN DECK TO UPPER DECK STOWABLE CREW LADDER CRACKED - ACCOMPLISH REPAIR TO THE MAIN DECK TO UPPER DECK STOWABLE CREW LADDER CRACK.SDR UIEA2011101900581Fairing · crackedDURING WALKAROUND INSPECTION, MX FOUND THE RT WING GEAR DOOR FAIRING - LOWER EDGE CRACKED, MEASURING 3.0 IN. X 1.5 IN (REF FIG 1). DAMAGE FOUND TO BE BEYOND THE SRM 52-80-02, FIG 101 ALLOWABLE DAMAGE 4 LIMITS IAW SRM 51-70-02, FIG 101 SHEET 9 OF 41. REPAIRESDR UIEA2011101900577Floorboard · gougedDURING WALKAROUND INSPECTION, DAMAGE FOUND TO MAIN DECK FLOORBOARD BS 400 - RBL 60.0 GOUGED AND DELAMINATED. GOUGED AREA MEASURES APPROX 4.5" X 4.5" DAMAGE IS BEYOND LIMITS IAW SRM 53-00-50, FIG 101. REPAIRED IAW THE SRM 53-00-50, REPAIR 1.SDR UIEA2011101300568Handle · damagedDURING WALKAROUND INSPECTION, MX REPORTED DAMAGE FOUND TO MAIN DECK TO FWD E/E COMPARTMENT ACCESS DOOR HANDLE. REPLACED THE DAMAGED DOOR HANDLE.SDR UIEA2011092900530Sleeve · crackedDURING MX WALKAROUND, FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, BETWEEN APPROX THE 9 TO 10 O'CLOCK POSITION ON THE NR 2 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 12" LONG . IAW SRM 54-41-30 THE LENGTH OF THE CRACK IS OUT OF LIMITS. STOP DRILLED ENDSDR UIEA2011092900531Floorboard · delaminatedDURING WALKAROUND INSPECTION, MX REPORTED DAMAGE FOUND TO MAIN DECK FLOORBOARD BS 1720 LBL 117.4 DAMAGE IS BEYOND THE SRM 53-00-50-1A-1, FIG 101. REPAIRED IAW THE SRM 53-00-50, REPAIR 1.SDR UIEA2011092600526Motor · burnedCAPT SEAT ELECTRIC FUNCTION FAILED. SLIGHT ELECTRICAL BURN ODOR. TURNED POWER SWITCH OFF. (VERIFIED MANUAL ADJUSTMENT WORKS. ELECTRIC MOTOR BELIEVED TO BE UNSERVICEABLE. TRANSFERRED TO DMI 26719 IAW MEL 25-11-2-1.)SDR UIEA2011091900512Structure · damagedDURING MX, RT OTBD WING - WBL 1131.2 SUSTAINED GROUND DAMAGE. LOCATED 4.0 IN. OTBD FROM FUEL JETTISON NOZZLE AT THE WING T/E WEDGE MEASURING 12.0 X 9.0 IN. (REF FIG 1). (DISPOSITION WAS MADE TO PERFORM AN INTERIM REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONSDR UIEA2011091300477Structure · damagedFLIGHT CREW ADVISED MX UPON ARRIVAL, THEY NOTICED DAMAGE TO THE LT OTBD MID FLAP TRAILING EDGE.SDR UIEA2011090900491Skin · damagedDURING LOADING OPERATIONS, THE LOWER LOBE - FWD CARGO DOOR EXTERNAL SKIN - BS670 LWR AFT CORNER AREA WAS DAMAGED BY LOADER INTERFERING WHILE CLOSING THE DOOR, THE DAMAGED CORNER MEASUREMENTS FIG 1 (SHEET 3 OF 3). THE DAMAGE EXCEEDS THE SRM 52-30-01, FIG 101 ASDR UIEA2011082700474Skin · puncturedDURING WALKAROUND, MX FOUND THE NR 4 RT THRUST REVERSER CORE COWL HAS 2 PUNCTURES IN THE SKIN LOCATED ABOVE THE ACCESS PANEL AND BLOWOUT DOOR. DAMAGE TO THE ACCESS PANEL AND BLOWOUT DOOR HINGES, LATCHES AND LANYARDS. REPAIRED.SDR UIEA2011082300458Fire Warning · false indicationPRIOR TO LANDING, HAD A FALSE MAIN DECK FIRE WARNING INDICATION. WARNING TERMINATED AFTER 30 SECONDS. PERFORMED FIRE DETECTION SYS TEST IAW MM 26-14-00. PASSED WITH NO DEFECTS FOUND.SDR UIEA2011082100464Duct · crackedDURING TROUBLESHOOTING, MX REPORTED LOWER LOBE - FWD CARGO COMPARTMENT RT BS 600 INBD EXHAUST VALVE DUCT WITH MULTIPLE CRACK DAMAGE. ACCOMPLISHED REPAIR.SDR P5CA2011081800455Thrust Reverser · damagedFOUND DAMAGE TO THE NR 3 ENG RT THRUST REV 4 INCHES WIDE BY 2 INCHES LONG & NBSP; FROM A LIGHTNING STRIKE AT 5 O'CLOCK POS. (COMPLIED WITH LIGHTNING STRIKE INSP PER AMM 05-51-13. ACCOMPLISHED EO 4478A184 (FAA FORM 8110-3 DATED 17AUG2011): TIME LIMITEDSDR UIEA2011081700455Sleeve · crackedDURING MX WALKAROUND, FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, BETWEEN APPROX THE 9 TO 12 O'CLOCK POSITION ON THE NR 3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 11" LONG AND IS JUST IN FRONT OF NAC STA 349.236. IAW SRM 54-41-30 THE LENGTH OF THE CSDR UIEA2011081500454Ecu · inoperativeCREW REPORTED "STARTER CUTOUT 2 CAUTION MESSAGE" AND "ENGINE 2 START VALVE" MESSAGE. (REPLACED START VALVE AND ECU, ALL OPERATIONAL CHECKS SATISFACTORY)SDR UIEA2011080700432Skin · damagedDURING MX WALKAROUND, MX FOUND DAMAGE TO THE NR 2 ENG RT THRUST REVERSER TRANSLATING COWL EXTERNAL SKIN OUTER FINISH DAMAGE. THE DAMAGE IS LOCATED IN NEAR THE REVERSER COWL SKIN T/E (REF FIG 1-3): PERFORMED A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK ISDR UIEA2011073000395Start Valve · inoperativeSTARTER CUTOUT 2 EICSA MSG. MSG WOULD NOT GO OUT. REPLACED NR 2 ENG START VALVE IAW 80-11-02. CHECKED NORMAL IAW AMM. MSG CLEARED.SDR UIEA2011072700372Panel · deformedDURING WALK-AROUND INSPECTION, MX REPORTED RT INBD MID FLAP - T/E OF COVE PANEL - DEFORMATION WBL168.55, MEASURING 5.0 IN. LONG X 0.250 IN. DEPTH (UPWARD DEFLECTION) (REF FIG 1).SDR UIEA2011072700373Panel · deformedDURING WALK-AROUND INSP, MX REPORTED RT INBD MID FLAP - T/E OF COVE PANEL - DEFORMATION WBL259.55, MEASURING 10.0 IN. LONG X 0.5 IN. DEPTH UPWARD DEFLECTION REF FIG 2.SDR UIEA2011072700374Panel · deformedDURING WALK-AROUND INSPECTION, MX REPORTED RT INBD MID FLAP - T/E OF COVE PANEL - DEFORMATION (4 PLACES) WBL347.55, MEASURING 4.0 IN. LONG X 0.375 IN. DEPTH (UPWARD DEFLECTION) (REF FIG 3). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED ISDR UIEA2011072700375Panel · deformedDURING WALK-AROUND INSP, MX REPORTED RT INBD MID FLAP -T/E OF COVE PANEL -DEFORMATION WBL435.55, MEASURING 5.0 IN. LONG X 0.250 IN. DEPTH (UPWARD DEFLECTION) (REF FIG 4). DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUSDR UIEA2011070600347Structure · damagedDURING LOADING OPERATIONS, THROUGH THE NOSE CARGO DOOR, LOADER DROPPED CAUSING DAMAGE TO BS 260, LBL10.75 & RBL 10.75, WL 195.8 - CANTED BULKHEAD STIFFENERS (2 EA.), CONSISTING IN EDGE CRACKS MEASURING 1.5 AND 2.5 INCHES LONG (REF FIG 1). DAMAGE TO THE STIFFENSDR P5CA2011070300059Tension Tie · crackedTHE FORWARD CHANNEL OF TENSION TIE AT BODY STATION 760 WAS FOUND TO BE CRACKED AT 3 HOLES. ACCOMPLISHED CATEGORY B REPAIR IAW 747-400 SRM 53-20-30 REPAIR 1. REPEAT DETAILED VISUAL INSPECTION REQUIRED EVERY 300 FLIGHT CYCLES ACCORDING TO TABLE 203. TRACKED SDR P5CA2011070300062Rib · wornRIGHT INBOARD TRAILING EDGE MID-FLAP INBOARD SPRING SEAL RIB FOUND TO BE WORN. SPRING SEAL RIB REPAIRED IAW HX RS 57-55-37144 REV A.SDR P5CA2011070300060Tension Tie · crackedTHE FORWARD CHANNEL OF TENSION TIE AT BODY STATION 720 WAS FOUND TO BE CRACKED AT ONE HOLE. ACCOMPLISHED CATEGORY B REPAIR IAW 747-400 SRM 53-20-30 REPAIR 1. REPEAT DETAILED VISUAL INSPECTION REQUIRED EVERY 300 FLIGHT CYCLES ACCORDING TO TABLE 203. TRACKED SDR UIEA2011062400325Actuator · inoperativeEICAS "OUTFLOW VALVE L" AT 6000 FT ON TAKEOFF. PASSING THROUGH 11,500 FT "CABIN ALT" EICAS HORN AND LIGHTS. COULD NOT CONTROL PRESSURIZATION RETURNED TO DEPARTURE. REPLACED LT OUTFLOW VALVE ACTUATOR ASSY IAW MM. OPS TEST PASSED. MESSAGE CLEARED.SDR UIEA2011062100446Skin · delaminatedRT WING INBD FORE FLAP MID AREA L/E FOUND DELAMINATED. REPAIRED IAW SRM 51-70-07. REF PROCESS CARD CONTROL SEQUENCE NT FIM 500284-1 FOR DETAILS.SDR UIEA2011062100445Bulb · inoperativeM/D STAIRWAY EMERGENCY LIGHT FOUND 1 EA BULB INOP AND COVER LOOSE. STAIRWAY EMERGENCY LIGHT 1 EA BULB REPLACED AND COVER REPLACED. OPS TEST C/O RESULT NORMAL.SDR UIEA2011061500314Engine · vibrationON TAKE-OFF ROLL, ENGINE VIBE 4 SHOWED 5.2. FELT A VIBRATION WHEN SELECTING MAX THRUST (VISUALLY INSPECTED INLET/EXHAUST OF ENGINE, MAG CHIP DETECTOR AND & NBSP; ENGINE LPT AREA COMPONENTS AMD VIBRATION PICKUP CONNECTOR & NBSP; ALL IAW FIM 71-00. PERFORMED BSDR UIEA2011060900295Web · crackedDURING THE "C CHECK", CRACK DAMAGE TO 65B12457-14 CLOSEOUT WEB ASSY WAS DOCUMENTED IAW NRC 50396. THE ACTION REQUIRED TO CLOSE NRC 50396 WAS TO REPAIR THE CRACK DAMAGE IAW SB 747- 53-2329, REV 2, FIG 3. (2 REPAIR SHEETS 23 INCH BY 12 INCH MADE 2024-T3 OR 7075SDR UIEA2011060700287Fairing · crackedDURING A-CHECK, ON NR2 ENGINE RT T/R TRANSCOWL, AFT FAIRING WAS FOUND WITH A CRACK APPROX 2.45 INCHES IN LENGTH. (DISPOSITION WAS MADE TO PERFORM REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS. PERMANENT REPAIR AS DECRIBED IN PART 2 WILL BE PERFORMED AT 15,0SDR UIEA2011060600293Stiffener · deformedDURING A C3-CHECK INSPECTION, THE MLG W/W TOP PRESSURE DECK STIFFENERS AT BS 1398.75 LOWER FLANGE WERE FOUND DEFORMED AT RBL 46 AND RBL 45.5 RESPECTIVELY AS SHOWN ON FIGURE 1. AT BS1398.75 THE DEFORMATION IS APPROX BETWEEN RBL 44 AND RBL 47. THE WEB IS ALSO SDR UIEA2011060600292Stiffener · deformedDURING A C3-CHECK INSP, THE MLG W/W TOP PRESSURE DECK STIFFENERS AT BS 1393.5 & NBSP; LOWER FLANGE WERE FOUND DEFORMED AT RBL 46 AND RBL 45.5 RESPECTIVELY AS SHOWN ON FIG 1. AT BS1393.5 THE DEFORMATION IS APPROX BETWEEN RBL 44 AND RBL 48. THE WEB IS ALSO DEFSDR UIEA2011060400273Structure · damagedDURING LOADING OPERATIONS, ENGINE PALLET CAUSED DAMAGE TO FLOORBOARD PANELS BS1500 - BS1625, LBL 85.65 GOUGES/PUNCTURE DAMAGE (REF FIG 1). THE HOLE IS APPROX 30 INCHES LONG BY 2.5 IN. WIDE.SDR UIEA2011060100270Cdu · inoperativeRIGHT CDU INOP, FROZEN ON POSITION REPORT (REPLACED RT CDU IAW MM 34-61-02, ALL OPERATES NORMAL ).SDR UIEA2011051700259Inlet · erodedDURING WALK-AROUND INSP, MX FOUND THE NR 3 RT FAN COWL L/E WITH EROSION DAMAGE, MEASURING 0.350 IN. WIDE X 1.5 FT. LONG (REF FIG 1). THE DAMAGE IS BEYOND THE ALLOWABLE DAMAGE LIMITS IAW SRM 54-25-01 (ALLOWABLE DAMAGE 1). (DISPOSITION WAS MADE TO PERFORM A TISDR UIEA2011051300258Actuator · failedGEAR FAILED TO RETRACT DUE TO "GEAR TILT" (BODY L/GEAR TRUCK POSITIONING ACTUATOR AND FWD ATTACH BOLT REPLACED IAW MM. LT BODY GEAR AND WHEEL WELL AREA INSPECTED AND NO DAMAGE EVIDENT.)SDR P5CA2011051200054Acoustic Panel · dentedNUMBER 2 ENGINE NOSE COWL INLET HAS DENTS TO THE ACOUSTIC PANELS AT THE 3 AND 6 O'CLOCK POSITIONS. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1136 AND SRM 54-15-01.SDR P5CA2011051000036Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 475.928 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.SDR UIEA2011050900256Sleeve · crackedDURING MX WALKAROUND, MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 9 O'CLOCK POSITION ON THE NR 3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 3" LONG AND IS APPROX .5" FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LENGTH OF TSDR UIEA2011043000253Light · sparksFLIGHT DECK ACCESS LIGHT; BEHIND COCKPIT DOOR BULKHEAD WOULD NOT SHUTOFF THEN BEGAN TO SPARK (BULB REMOVED AND LEADS DISCONNECTED FROM LIGHT ASSY.)SDR UIEA2011042600252Skin · damagedDURING WALK-AROUND INSP, MX REPORTED DAMAGE WAS FOUND TO THE RT FUSELAGE SKIN BS1937, BELOW S37R (THE DAMAGE IS BEYOND THE SRM 53-00-01, FIGURE 101 ALLOWABLE DAMAGE 1, DETAIL III LIMITS. TIME LIMITED REPAIR ACCOMPLISHED AS DESCRIBED IN PART 1 WORK INSTRUCTIONSDR UIEA2011042600250Skin · dentedDURING WALK-AROUND INSPECTION AT ANC, MX REPORTED DAMAGE WAS FOUND TO THE RT FUSELAGE SKIN BS1928.5, BELOW S38R; 1 INCH DIAMETER. EO 4453A552 (THE DAMAGE IS BEYOND THE SRM 53-00-01, FIGURE 101 ALLOWABLE DAMAGE 1, DETAIL III LIMITS. TIME LIMITED REPAIR ACCOM
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