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 UIEA200700006Seat Track · damagedAFT CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT STA 1780 RBL 25. AFT CARGO SEAT TRACK REPAIRED IAW SRM 53-00-52 REPAIR NR 10 AND EO NR 4453A100.SDR UIEA200700003Attach Fitting · damagedUPON ARRIVAL, FOUND NR 2 CANOE DAMAGED, PUNCTURED HOLE OUTBOARD SIDE, IN ADDITION FOUND FLAP TRACK ATTACH FITTING DAMAGED. TRANSFERRED TO DMI NR M07-003 CDL 27-51-02.SDR P5CA0601506Pdu · inoperativeLE SINGLE DRIVE STATUS MSG NR 3 LED INOP PNEUMATICALLY. REPLACED LE PDU.SDR UIEA200600289Skin · damagedON WALK AROUND FOUND LOWER FWD CARGO DOOR DAMAGED AT THE AFT BOTTOM CORNER AROUND 11 INCH LENGTH ROUND THE AFT CORNER WITH 1.25 OPEN AREA. EDDY CURRENT AND NDT INSP C/W BEFORE AND AFTER INSPECTION ON THE SKIN AND STRUCTURE OF FWD CARGO DOOR AFT BOTTOM CORNER. SDR UIEA200600287Pdu · burned outMAIN DECK PDU 18L INOP. PDU DEVELOPED SMOKE. FOUND ELECTRIC MOTOR BURNED. ITEM TRANSFERRED TO DMI M01-117 MEL 25-53-1 CAT D PDU REMOVED AREA INSPECTED. NO FURTHER DAMAGE NOTED.SDR UIEA200600286Rail · crackedAFT CARGO SIDE RAIL CRACKED.SDR UIEA200600285Rail · crackedAFT CARGO SIDE RAIL DAMAGED.SDR UIEA200600284Rail · damagedFWD CARGO SIDE RAIL CRACKED DUE IMPACT DAMAGE.SDR UIEA200600280Pressure Switch · damagedRTO, DUE TO - BLEED NR 2 EICAS MSG, LOW SPEED (70 KTS) ABORT. REMOVED AND REPLACED OV PRESSURE SWITCH IAW MM 36-12-03, OPS CHECK OK.SDR UIEA200600278Intercostal · crackedA/C M415MC: PERFORMED INTERIM REPAIR TO MAIN DECK SIDE CARGO DOOR INTERCOSTAL CUT-OUT IAW XEO 52-102106, A/C OK FOR CONTINUED OPERATIONS FOR UP TO 6 FLIGHT CYCLES. INTERCOSTAL CUT-OUT WEB REPAIRED IAW SRM 51-70-13 REPAIR FIG 201.SDR P5CA0601501Structure · damagedPILOT REPORT - CHECK FOR BIRDSTRIKE ON SHORT APPROACH, FLEW INTO FLOCK OF BIRDS UNDER AIRCRAFT. ACCOMPLISHED BIRDSTRIKE CONDITIONAL INSPECTION PER AMM 05-51-14-202-001. REPAIRED DAMAGE TO RIGHT INBOARD TRAILING EDGE MID FLAP & AFT FLAP PER 747-400 SRM 57-31-SDR UIEA200600275Manifold · chafedNR 4 ENGINE FUEL NOZZLE MANIFOLD LEAKING AT 12 O'CLOCK POSITION. REMOVED AND REPLACED NR 4 ENGINE RT FUEL MANIFOLD IAW AMM 73-11-10. LEAK CHECK OK.SDR UIEA200600274Powerpack · wornATB:DUE TO MEDIUM/LIGHT VIBRATION IN RUDDER PEDALS. FLIGHT CONTROL VALVES OFF BY 1. YAW DAMPER OFF NO HELP, A/P OFF NO CHANGES. FOUND UPPER RUDDER HYD RETRACT LINE "B" NUT AND UNION LOOSE BY 2.5 TURN WITH HEAVY LEAK. TIGHTEN BACK IAW MM 27-21-15 OPS AND LEAK CSDR UIEA200600273Line · crackedNR 2 ENGINE SHUTDOWN IN FLIGHT OIL QUANTITY DECREASED TO (0), FOLLOWED SHORTLY BY EICAS MSG ENG 2 OIL PRESSURE. ENGINE WINDMILLING OIL PRESS 8-10PSI. FOUND LUBE AND PUMP MANIFOLD LINE CRACK SERVICED ENGINE OIL. RR LUBE AND PUMP MANIFOLD LINE, OPERATED NR 2 ENGSDR UIEA200600269Fire Loop · malfunctionedIFSD: DUE TO DET FIRE/OHT 2 IN CLIMB REMAINED DISPLAY ENTIRE FLIGHT. STATUS NR 2 ENGINE FIRE LOOP B-RESET. B AND A LOOP CIRCUIT BREAKERS REDUCED, NR 2 THRUST TO IDLE, NO HELP DISPLAYED UNTIL ENGINE SHUTDOWN. ADVISORY, ENG 2 PRECAUTIONARY SHUTDOWN AT 2345, DSDR UIEA200600268Tire · separatedON TAKEOFF FROM HNL NR 8 TIRE TREAD COMPLETELY SEPARATED FROM MAIN CARCASS CAUSING DAMAGE TO 3 WING TO BODY FAIRINGS AFT OF LT BODY GEAR. HONEYCOMB PANELS 193BL,193CL,193DL INCLUDING WTB FRAMES AT STA1540,1580 & 1620. IMPACT DAMAGE TO ELEC CONDUIT ON RT BLG SDR UIEA200600267Mechanism · dirtyEICAS MESSAGE FLAPS DRIVE WHILE RUNNING QRH AFTER 2 MINUTES FLAPS DRIVE CHANGED TO FLAPS PRIMARY EICAS. PER FIM 27-51-00 LUBE ALL BALL SCREWS AS PER AMM 12-21-20. CLEANED ALL FLAP DRIVE MECHANISMS AND SERVICED FLAP ANGLE GEAR BOXES AS PER AMM 12-13-13, 1-1/2SDR UIEA200600252Transmitter · failedNR 2 ENGINE OIL PRESSURE DROPPED AND STABILIZED BELOW 10 PSI AFTER LEVEL OFF, INFLIGHT SHUT DOWN. REMOVED AND REPLACED PRESSURE XMITTER. RUN ENGINE, OPS CHECKED NORMAL AS PER AMM 79-32-00.SDR UIEA200600224Seat Track · crackedN415MC AT PIK FOR MSG-3, CHECK C-4 & A-4. AS PER N/ROUTINE 163 FWD CARGO SEAT TRACK AT BS 560 LBL 45.5 HAS 6 INCH CRACK AND N/ROUTINE 188 FWD CARGO SEAT TRACK AT BS 560, LBL 25 HAS TWO HOLES. NR 4453A083 WAS GENERATED. FOR N/ROUTINE 163 REPAIR ACCOMPLISHED SDR UIEA200600223Shim · migratedN415MC AT PIK FOR MSG-3 CHECK C-4 & A-4. AS PER N/ROUTINES 168, 169 AND 210, AFT AND FWD CARGO DOORS HINGE SHIMS MIGRATED. XEO 53-082906 WAS GENERATED. REPAIR ACCOMPLISHED TO THE AFT & FWD CARGO DOOR HINGE SHIMS MIGRATION AS PER SRM 51-20-08 AND 50 PERCENT SDR UIEA200600222Fan Blade · lack of lubeN415MC AT PIK FOR MSG-3, C-4&A-4 CHECK. AS PER N/ROUTINE 154, NR 1 ENGINE S/N 704-916 FAN BLADES REMOVED FOR LUBRICATION. IT WAS FOUND, FAN DISKS HAVE NO EVIDENCE OF LUBRICANT. INSPECTION PERFORMED IAW MM 72-31-00, 206 TABLE 601 NR 1 DOVETAILS ON FAN DISK HSDR UIEA200600221Skin · corrodedN415MC AT PIK FOR MSG-3 CHECK C-4 & A-4. AS PER N/ROUTINE 105 LEFT WING UPPER SURFACE WS 752-779 FIVE BLENDED & RESURFACED AREAS ON THE OUTER AREA. FWD MOST DEPTH TO BE CHECKED. FWD BLEND OUT CHECKED BETWEEN WS 752 - WS 779. MAX DEPTH OF BLEND OUT = 0.017 SDR UIEA200600227Light · inoperativeMAIN DECK ZONE-A LEFT CEILING EMERGENCY LIGHT FOUND INOP. TRANSFERRED TO DEFERRED ITEM M06-087.SDR UIEA200600220Fairing · damagedN493MC WAS AT PIK FOR A-2 CHECK. AS PER NON-MEL 06-068 AND N/ROUTINE 41. A HOLE WAS FOUND IN LEADING EDGE OF RIGHT WING BODY FAIRING AT STA 840. INTERIM REPAIR CARRIED OUT AS PER SRM 53-00-70 (NOTE B). TAP TEST ON EVERY CHECK AND PERMANENT REPAIR WILL BE CSDR UIEA200600214Tire · failedRTO: DUE TO TIRE FAILURE AT ROTATION ON TAKEOFF FROM NBO, BRAKE TEMP EICAS AT TOC. PERFORMED CHECKLIST, CVR C/B PULLED. FOUND NR 4 TIRE BURST. C/O SINGLE FLAT SPOT INSP OR BLOWN TIRE CHECK IAW AMM 05-51-25 ALL SATISFACTORY. REMOVED AND REPLACED NR 4 WHEEL SDR UIEA200600210Shim · migratedC-4 & A-4 CHECK AT PIK., FWD CARGO DOOR FWD ACTUATOR ARM FITTING HAS MIGRATING SHIMS. AFT CARGO DOOR AFT ACTUATOR ARM FITTING HAS MIGRATING SHIMS. ENGG HAS GENERATED XEO 53-081406 PART-1 OF XEO 53-081406 HAS ALREADY ACCOMPLISHED DURING C-CHECK AT PIK ON 15THSDR UIEA200600209Shim · migratedC-4 & A-4 CHECK AT PIK. AFT PIT DOOR HINGE SEGMENTS 1 THRU 12 HAVE MIGRATING SHIMS. AS PER BOEING MESSAGE 1-218612791-2 DATED 11TH AUG 2006, XEO 52-081106 GENERATED. PART-1 ACCOMPLISHED DURING C-CHECK AT PIK. PART-2 WILL BE ACCOMPLISHED (DVI) EVERY 2A CHECSDR UIEA200600206Skin · damagedN496MC AT PIK FOR MSG C-4 & A-4 CHECK. AS PER N/R 39, ON INDUCTION OF A/C FOUND LT I/B T/E FORE FLAP LEADING EDGE DAMAGED, I/B OF NR 3 CANOE. OFF S/N 000532. RECT:LT, I/B T/E FORE FLAP REPLACED AS PER AMM 27-51-02. ON P/N 65B39011-93C & ON S/N 000492.SDR UIEA200600208Steering Sys · malfunctionedRTO: DUE TO T/O WARNING. BODY GEAR STEERING, RETURNED TO BLOCKS. PRESENT LEG FAULT SHOWS RIGHT BODY GEAR STEERING RIGHT. ACTUATOR EXTENSION UNCOMMANDED AS PREVIOUS MEL 32-53-1. CONFIRM BODY GEAR STEERING ACTUATORS DEACTIVATED AND LOCKED PER MEL 32-53-2. BSDR UIEA200600203Torque Tube · shearedDURING OPENING OF MAIN DECK SIDE CARGO DOOR THE FWD PULL IN HOOK ACTUATOR ACTIVATION ROD SHEARED AT THE TORQUE TUBE END AND PUNCTURED THE CARGO DOOR SKIN.SDR UIEA200600202Structure · delaminatedDELAM & PUNCTURE DAMAGE TO RT I/B FORE FLAP 60 INCHES FROM I/B EDGE & 12 INCHES FROM TE.SDR UIEA200600201Skin · gouged2 AREAS OF DAMAGE TO UPPER SURFACE LEADING EDGE LT O/B TE AFT FLAP CAUSED BY MID FLAP COVE PANEL SUPPORT BRACKETS, 0.050 DEPTH X .5 DIA. 15 IN FROM O/B EDGE AND 0.040 DEPTH X .5 DIA. 35 IN FROM O/B EDGE, PANEL THICKNESS .120SDR UIEA200600186Thrust Reverser · delaminatedMINOR LIGHTNING STRIKE, EXIT TO NR 2 ENGINE LT TRANSLATING COWL CAUSING DELAMINATION TO CARBON FIBRE MEASURING 0.5 INCH AXIAL BY 2.5 NR CIRCUMFRENTIAL ON TRAILING EDGE AT 8 O/C POSITION AFT LOOKING FORWARD.SDR UIEA200600184Actuator · malfunctionedNR 2 ENGINE FUEL CONTROL STATUS MSG, AFTER LOW SPEED ABORT. ENGINE NR 2 N1 78.5 MAX AT T/O ROLL OTHER ENGINES NORMAL. REMOVED AND REPLACED RT VSV ACTUATOR IAW AMM 75-31-02, DUE ON VISUAL INSP FOUND CLEVIS END DETACHED FROM ACTUATOR ASSY. ENGINE TEST 12 COMPSDR UIEA200600172Generator · disintegratedNR 1 APU GENERATOR BEARING MSG DURING T/S CHECK, BURNING SMELL INSIDE CABIN SUSPECT APU FIRE. FLT CREW FOLLOW QRH AND FIRE HANDLE PULLED AND FIRE BOTTLE DISCHARGED. APU COMPARTMENT CHECKED AND FOUND HEATING DAMAGE. NR 1 GEN DISINTEGRATED CAUSING DEBRIS IMPASDR UIEA200600157Solenoid · inoperativeON DEPARTURE, GEAR WOULD NOT RETRACT, NO MESSAGES. QRH ACTIONED, NO IMPROVEMENT. ATB, SEVERAL ATTEMPT, GEAR LOCK OVRD WOULD NOT MOVE. TRANSFERRED TO DMI PG 81157 DMI M06-065 MEL 32-31-01 CAT "C". LANDING GEAR SOLENOID INOP. ALL LG GRD TEST OK AS PER MM 32-SDR UIEA200600147Skin · puncturedLEFT AFT T/E FLAP LOWER SKIN HAS A PUNCTURE MARK LOCATED 125 INCHES FROM I/B & 9 INCHES FWD OF AFT EDGE. PUNCTURE MARKS REPAIRED IAW ATLAS AIR SRM 747-400F 57-53-01 PG 102 REF D & F REVISION 43 FIG 101.SDR UIEA200600145Skin · puncturedRIGHT I/B FORE FLAP LOWER SKIN 4 PUNCTURE MARKS ALL APPROX .100 DIA LOCATED AT 1) 65.5 INCHES FROM I/B EDGE & 6.75 INCHES FROM AFT. 2) 64.5 INCHES FROM I/B EDGE & 9.5 INCHES FROM AFT EDGE. 3) 60 INCHES FROM I/B EDGE & 14 INCHES FROM AFT EDGE. 4) 56.5 INCHES SDR UIEA200600146Skin · crackedLEFT TRAILING EDGE I/B MID FLAP HAS PREVIOUS REPAIR THAT HAS CRACKED ON I/B END 6 INCHES FROM EDGE. DAMAGE REMOVED & REPAIR LAYED UP 7 CURED IAW B747-400F SRM 51-70-06 REPAIR 5A (1), PARA 4 A, C, E (1) (D) PG 13 REVISION 43.SDR UIEA200600138Windshield · delaminatedDURING ROUTINE MAINTENANCE MSG3 C-4 CHECK IN PIK, ON INSPECTION OF THE COCKPIT WINDOWS, IT WAS OBSERVED THAT NR 3 RT WINDOW HAD DELAMINATED IN THE UPPER AFT CORNER, REQUIRING REPLACEMENT. WINDOW ASSY REPLACED, AND AIRCRAFT RETURNED TO SERVICE.SDR UIEA200600139Door · puncturedRT MAIN LANDING GEAR DOOR DAMAGED (PUNCTURED) APPROX 4" X 2" 21" ABOVE THE BOTTOM EDGE.SDR UIEA200600140Repair · debondedNR 4 ENG INBOARD T/R TRANSLATING SLEEVE PREVIOUS REPAIR AT 9 O'CLOCK WAS DISBONDED.SDR UIEA200600141Tire · disintegratedT/O ABORT: TIRE FAILURE, REJECTED AT APPROX 80KTS. SEVERE VIBRATION, A/C LEANING TO THE RT. VOICE RECORDER C/B OPENED. FOUND NR 9 & NR 10 TIRES BURST AND DISINTEGRATED. NR 9 & NR 10 TIRES AND MAIN WHEELS REPLACED, TEMP TO FACILITATE A/C TOWING OFF RUNWAY. SDR UIEA200600134Flap · chafedLEFT HAND OUTBOARD AFT FLAP END WEAR/CHAFE MARK. RANGING IN DEPTH FROM 0.002' TO 0.013'AND FROM 8"X1" IN DIAMETER TO 2"X1".SDR UIEA200600135Sleeve · crackedINBOARD THRUST REVERSER TRANSLATING SLEEVE CRACKED.SDR UIEA200600133Panel · crackedNR 1 PYLON STRUT FAIRING PANEL 4541R CRACKED.SDR UIEA200600129Panel · missingON ARR, FOUND ON ENGINE NR 2 INBOARD PYLON PANEL 462RL MISSING. INSP LT FLAPS AND STABILIZER NO DAMAGE FOUND. REPLACED PANEL 462RL ON ENGINE NR 2, OK FOR SERVICE.SDR UIEA200600125Skin · gougedRIGHT TRAILING EDGE AFT FLAP HAS A GOUGE ON THE UPPER SURFACE APPROX ONE INCH LONG, .125 INCH DEEP AND .250 WIDE. LOCATED 3 FEET OUTBOARD OF NR 7 TRACK CANOE. FOUND DURING C-4 CHECK AT PIK, N/ROUTINE NR 148. GOUGE REPAIRED IAW SRM 57-53-01 FIG 101. COVE PASDR UIEA200600124Skin · dentedRT INBOARD AFT FLAP HAS A DENT ON THE UPPER SURFACE APPROX ONE SQUARE INCH AND APPROX .250 DEEP,12 INCHES OUTBOARD OF NR 6 FLAP TRACK CANOE. FOUND DURING C-4 CHECK, N/ROUTINE NR 147. PERMANENT REPAIR CARRIED OUT TO DAMAGE AREA AS PER SRM 51-70-10 FIG 203 ANDSDR UIEA200600123Panel · chippedFLYING PANEL ON THE RIGHT HAND WING INBOARD TRAILING EDGE PREVIOUS REPAIR REQUIRES RE-WORK. AREA MARKED LOCATION IS APPROX WBL 220. NON ROUTINE NR 145. EXISTING REPAIR REMOVED AND A NEW REPAIR INSTALLED IAW SRM 51-70-06.
Back to Boeing 747-47UF