Boeing 747-46NF
Service difficulty reports · 1,079
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 = '74746NF' 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 = '74746NF' 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 UIEA2026091000864Coalescer Bag · odorELECTRICAL BURNING ODOR IN DESCENT. R & R WATER SEPARATOR COALESCER BAG ON PACK 1, 2, & 3, AND PERFORMED CH 5 INSP IAW AMM 21-51-05. OPS CHKD OK.SDR UIEA2026090500853Shutoff Valve · faultedBLEED 3 EICAS DURING CLIMB. REMOVED AND REPLACED ENG 3 PRV, OPS CHECK NORMAL AND ENG RUN OK IAW AMM 36-11-19, AMM 71-00-00 AND IPC 36-11-05-02A.SDR UIEA2026081400759Control Module · faultedGEAR DISAGREE MESSAGE. LANDING GEAR LEVER WOULD NOT GO UP AFTER T/O. LANDING GEAR STAYED IN DOWN POSITION. RETURNED TO AIRPORT. : TRANSFER TO DMI 257550 PER MEL 32-30-01 CAT C. LANDING GEAR CONTROL MODULE WAS REPLACED. OPS CHECK PERFORMED. OPS CHECKED GOOD IASDR UIEA2026072400646Generator · faultedCREW SET UP IAW DDG 49-11-01. CREW ISOLATED THAT LT PNEUMATIC & RT UTILITY. CREW STARTED NR 4 ENG. DURING START, AT THE TIME, NR 4 ENG GOING TO TAKE OVER POWER BY GEN FROM ENGINE. THE ACFT STARTED TO SHED LOAD POWER. THEN LT SIDE WHICH IS POWERED BY LT EXT POSDR UIEA2026072400654Radar · faultedRADAR INTERMITTENT AND INAUCCURATE, NOT PAINTING ANY WEATHER. PERFORMED OPERATIONAL TEST PER AMM 33-43-00/501. NO ISSUES NOTED AT THE TIME.SDR UIEA2026071300593Circuit Card · faultedMAIN DECK FIRE WARNING - NO EICAS MSG. SWAPED THE A4 WITH A29 CIRCURT CARD & PFMD GND TEST ,TEST PASSED IAW AMM 26-10-01 (NOW D00132 IN A4 POSITION,D00883 IN A29 POSITION)SDR UIEA2026063000563Impeller · damagedFUEL IMBALANCE 2 - 3 STATUS MESSAGE. ACCOMPLISHED FIM 28-22 TASK 925, NO FINDING. TANK DIVE ACCOMPLISHED, FOUND A JET LEAK FROM OVRD PUMP DISCH CHECK VLV. R/R DISCHARGE CHECK VALVE PER AMM 28-31-11/401, CHECK OK. FURTHER T/S NEEDED. DETAILS ARE LISTED LP 209SDR UIEA2026041900218Oil System · leakingENG #1 OIL QTY DROPPED TO 1 AFTER T/O, FOLLOW WITHIN 20 MINS BY ENG OIL PRESS ADVISORY MSG. QRH FOLLOWED, AND ENG #1 WAS SHUT DOWN. WITHIN 15 MINS OF ENG SHUTDOWN, HYD PRESS SYSTEM 1 CAUTION MSG, QRH FOLLOWED HYD SYSTEM 1 SHUT DOWN. REMOVED AND REPLACED SDR UIEA2026040200120Strap · wornFOUND HOLE WEAR 1 EA AT B52231 S-17L -8 REPAIR FRAME STRAP(<P>REMOVED REPAIR FRAME STRAP AT B52231 S-17L AS PER SRM 51-40-02. FABRICATED -8 REPAIR FRAME STRAP AT B52231 S-17L AS PER BOEING SR SPI-TLS-26-0017-03B. INSTALLED -8 REPAIR FRAME STRAP AT BS52231 S-17SDR UIEA2026040200121Bulkhead Web · crackedCRACK SIGNAL INDICATION AT L/H AFT INNER CHORD IN ACCORDANCE WITH EO 4453C127 OPEN HOLE HEEL INSPECTION (2EA) REMOVED HI-LOK 10 EA TO PERFORM S.B 747 53A2467 & 53A2427 AT B.S 2598 L/H LOWER BULKHEAD AS PER SPI-TLS-26-0016. PERFORMED OPEN HOLE HFEC INSP AT STASDR UIEA2026040100118Keelbeam · corrodedLOWER FUSELAGE STA 1460 KEELBEAM STRUCTURE CORROSION (BETWEEN BOTH BODY L/G DOOR) REMOVED BOTH PANEL AT LWR FUSELAGE BS 1460 KEEL BEAM IAW SRM 51-40-02. PERFORMED BLEND OUT CORROSION AREA AT LWR FUSELAGE BS 1460 KEELBEAM IAW SRM 51-10-02. ACCOMPLISHED FPI INSDR UIEA2026022600069Valve · inoperativeEQUIPMENT COOLING MESSAGE. SUSPECT FLT DECK FLOW REG VALVE INOP. OPENED FLOOR PANEL AND MANUALLY MOVED VALVE TO OPEN. TRANSFER TO DMI 248403 PER MEL 21-61-13 CAT C. R & R FD FLOW REG VALVE AS PER AMM 21-61-09 & AIPC 21-21-06. OPS AND LEAK CHK GOOD. DMI 24840SDR UIEA2026021600053Shear Tie · crackedFOUND CRACK ON SHEAR TIE AT BS 1000 RBL 33.99. REMOVED DAMAGE SHEAR TIE IAW SRM 51-40-02-0G-0 REV 115. INSTALL NEW SHEAR TIE IAW EI T2026A53M-210 REV 0 AND EO 4453C024 PART 8 REV 4. ACCOMPLISH EI T2026A53M-210 REV 1. JOB COMPLETED AND CONDITION CHECK NORMSDR UIEA2026021600054Web · corrodedFOUND RT WING INBD FORE FLAP INTERNAL INBD SIDE WEB CRACKED. REMOVED DAMAGED WEB IAW SRM 51-40-02-0G-0 REV 105. 2. INSTALL A NEW WEB IAW EI T2026A57M-236 REV 0 AND DWG 65B39038 SH7 REV -. ACCOMPLISH EI T2026A57M-236 REV 1. JOB COMPLETED AND CONDITION CHECK NSDR UIEA2026021600055Seat Track · corrodedFOUND M/D CGO SUBSTITUTE SEAT TRACK CRACK AT STA 1633 RBL 75.92. ACCOMPLISHED WORK SHEET 60030 AND IAW SRM 53-00-52-2R-13 REV 105 AND DWG 65B38751 SH62 REV A ,SH75 REV -. JOB COMPLETED.SDR UIEA2026021600056Seat Track · corrodedCRACK - ON M/D FLOOR SUBSTITUTE SEAT TRACK AT STA 2070 RBL 75.92. ACCOMPLISHED WORK SHEET 60035 AND IAW SRM 53-00-52-2R-13 REV 105. JOB COMPLETED.SDR UIEA2026021600057Seat Track · corrodedFOUND M/D CARGO SUBSTITUTE SEAT TRACK CRACKED AT BS 1507, RBL 75.92. ACCOMPLISHED WORK SHEET NO: 60029 IAW SRM 53-00-52-2R-13 REV 105 AND DWG 65B38251 SH62 REV A & SH75 REV-. JOB COMPLETED.SDR UIEA2026021600058Seat Track · corrodedCORROSION ON M/D SEAT TRACK BS 700, RBL 33.99. PERFORM EI T2026A53M-256 REV 0 AND W/S NO: 60039 (SRM 53-00-52-2R-6 REV 105). ACCOMPLISH EI NO: T2026A53M-216 REV 1. 3. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR UIEA2026021600059Cargo Track · corrodedFOUND M/D CARGO TRACK CORRODED AT BS 1519, RBL 11.33. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 105. REPAIR DAMAGE AREA IAW EI T2026A53M-227 REV 0 AND W/S 60036 (SRM 53-00-52-2R-12 REV 105). INSTALL ACCESS FASTENERS IAW SRM 51-40-0SDR UIEA2026021600060Door Sill · not reportedFWD LWR CARGO DOOR SURROUND LWR MAIN SILL WEB & OTR CHORD, LATCH SUPPORT FITTING PART 1 TIME LIMITED REPAIR STA 580 REQUIRES EO PART 2 HFEC INSPECTION & EO PART 3 REQUIRES A SECOND TIME LIMITED REPAIR & EO PART 4 PERMANENT REPAIR ALL WITHIN 10 CALENDAR DAYS PESDR UIEA2026021600061Actuator · faultedFND FUNCTION FAIL AT R/H WLG ALTERNATE EXTENSION ROTARY ACTUATOR. REPLACED RT WLG ALTERNATE ROTARY ACTUATOR IAW AMM 32-36-01-004-001 REV 115 & AMM 32-36-01-404-009 REV 115 & STEP A TO F(4). 2. PERFORMED OPERATION TEST IAW AMM 32-36-01-404-009 REV 115 STEP F(SDR UIEA2026020500030Winglet · damagedRT WINGLET TIP T/E CORNER FOUND WORN. RT WINGLET TIP T/E CORNER LIGTHNING STRIKE DAMAGED AREAS REPAIRED IAW RI-57-30-18090 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2025111001295Tire · failed#8 MLG BLEW OUT TOWER REPORTED SMOKE & TIRE DEBRIS ON RUNWAY. R & R NR 8 MWA IAW AMM 32-45-01 & IPC 32-45-03-02. C/W BLOWN TIRE CHAP 5 INSP IAW AMM 05-51-25. R & R NR 7 MWA IAW AMM 32-45-01. R & R NLG STEERING CYLINDER IAW AMM 32-53-11. OPS CHKD NORMAL. NO SDR UIEA2025110701293Wheel · damagedNR 3 MAIN TIRE DAMAGED. REPLACED NR 3 AND 4 MLG WHEEL ASSY IAW AMM 32-45-01/401. PRESS & LEAK CHK OK.SDR UIEA2025102801282Fire Warning · false activationCREW REPORTED DURING CRUISE, CARGO FIRE MAIN DECK ZONE 11 EICAS MSG. FOUND MESSAGE 26330/26331 NOT ACTIVE. CREW CONFIRMED NO ACTUAL SMOKE/FIRE ON MAIN DECK. CARGO CONSISTS OF FLOWERS. SMOKE DETECTOR TEST PASSED PER AMM 26-14-01. NO FURTHER DEFECTS NOTEDSDR UIEA2025102601281Exhaust Fan · odorSMOKE SMELL IN COCKPIT. R & R COOLING EXHAUST FAN PER AMM 21-58-01. OPS CHK NORMAL.SDR UIEA2025101001267Indication Sys · faultedFLIGHT CREW REPORTED NR 4 HYD QTY INDICATION ERRATIC IN FLIGHT. PERFORMED WIRING CHECK BETWEEN DW 3112C PIN 2 AND DM7838EA PIN G15, DM 7838BA PIN D15, CHECKS NORMAL. R & R NR 4 HYD IM AND GROUND TEST PASS IAW AMM 29-11-42, WDM 27-62-11 & AIPC 29-11-42-01B, APSDR UIEA2025090401161Actuator · faultedOUTFLOW VALVE R EICAS MSG. REMOVED & REPLACED RT OUTFLOW VALVE ACTUATOR ASSY, RT ICU & DIODE IAW AMM 21-31-10/401, 21-31-07/401, SWPM 20-40, AIPC 21-31-01-01 & AIPC 21-31-10-01. OPS CHKD OK.SDR UIEA2025082501136Skin · corrodedCORROSION - SKIN, LH AFT LWR FUSELAGE SKIN STA 1732, S42L(<P>1) REPAIR THE DAMAGE IAW SRM 53-00-01-2R-1 REV 104 & W/S 50620. 2) CONDITION CHK NORMAL AND JOB COMPLETED</P>)SDR UIEA2025082501137Hinge Fitting · crackedCRACK - FITTING, INBD LWR SIDE OF LH WING #6 SPOILER MID HINGE FITTING(<P>1) REPAIRED DAMAGE AREA IAW W/S 50588 & SRM 57-51-13-2R-1 REV 104. 2) CONDITION CHK NORMAL AND JOB COMPLETED.</P>)SDR UIEA2025082501138Not Entered · not reportedCMR REQUEST CLARIFICATION FUSELAGE FASTENERS TYPE ON RH BODY SKIN NEAR STA 440, S26R(<P>1) ACCOMPLISHED EI T2025A53M-1774 REV 1. 2) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2025082501139Skin · corrodedCORROSION ON LH FUSELAGE OUTER SKIN NEAR STA 1700, S42L(<P>1) REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV 104. 2) REPAIR DAMAGE SKIN IAW EI T2025A53M-1733 REV 104. 3) JOB COMPLETED AND CONDITION CHK NORMAL</P>)SDR UIEA2025081001118Tire · failedAT LANDING, #1 TIRE BLEW. FLAT SPOT FOUND. CREW HAD AUTOBRAKE SET AT 4 MINIMUM LEVEL DUE TO NO AUTOSPOILER AND BRAKE ROD. ONCE DISENGAGED, CREW MANUAL BRAKE DID NOT EXCEED LEVEL 2. A/C TAXIED & TOWED IN WITH BLOWN TIRE. R & R #1 MWA IAW AMM 32-45-01/401 & AIPSDR UIEA2025062800817Longeron Fitting · crackedLEFT BS 1480 LONGERON EXTENSION FITTING FOUND CRACKED. CRACK LONGERON EXTENSION FITTING REPAIRED AS PER ATLAS AIR EO 4453A818 REV 20 PART 7. NO FURTHER DEFECTS NOTED.SDR UIEA2025062800818Doubler · crackedMAIN DECK - L1 ENTRY DR UPR HINGE DOUBLER FND CRACKED. DOUBLER REPLACED AS PER SRM 51-10-02 AND NEW DOUBLER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW DOUBLER INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.SDR UIEA2025063000819Lug · cracked1 EA CRACK WAS FOUND ON BS 1000 RBL 11.33 INTERCOSTAL LUG FITTING. INTERCOSTAL LUG FITTING REPLACED AS PER ATLAS AIR EO 4453C024 REV.4 PART 7 STEP 3. NO FURTHER DEFECTS NOTED.SDR UIEA2025063000820Lug · cracked1 EA CRACK WAS FOUND ON BS 1000 LBL 11.33" INTERCOSTAL LUG FITTING. INTERCOSTAL LUG FITTING REPLACED AS PER ATLAS AIR EO 4453C024 REV.4 PART 3 STEP 3. NO FURTHER DEFECTS NOTED.SDR UIEA2025070100821Fairing · delaminatedRIGHT WING I/B MID FLAP L/E FAIRING FOUND DELAMINATION AT I/B 13". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.SDR UIEA2025070100822Fairing · delaminatedRIGHT WING I/B AFT FLAP MID L/E FAIRING FOUND DELAMINATION AT O/B 180". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.SDR UIEA2025070100823Fairing · delaminatedLEFT WING I/B MID FLAP L/E FAIRING FOUND DELAMINATION AT O/B 70". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.SDR UIEA2025070100824Fairing · delaminatedRIGHT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION AT I/B 39". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.SDR UIEA2025070100825Fairing · delaminatedRIGHT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION AT I/B 12". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.SDR UIEA2025070100826Fairing · puncturedLEFT WING I/B FORE FLAP MID L/E FAIRING FOUND PUNCH HOLE FROM I/B 133". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. C. NO FURTHER DEFECTS NOTED.SDR UIEA2025070100827Fairing · delaminatedRIGHT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION AT O/B 180". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.SDR UIEA2025070100828Fairing · chafedRHW I/B AFT FLAP I/B L/E FAIRING FOUND CHAFING. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5.G. NO FURTHER DEFECTS NOTED.SDR UIEA2025070300830Power Supply · no testFUNCTIONAL TEST EMERGENCY LIGHTS BATTERY PACKS FOR CAPACITY (15 MIN. MINIMUM). FOUND EMERGENCY LT L1533, L5733, L5767 & M4915 WENT OFF IN LESS THAN 15 MINUTES. EMERGENCY LT POWER PACK M5169 REPLACED AND OPERATION CHECKED NORMAL IAW AMM 33-51-04.SDR UIEA2025070500835Lamp · inoperativeDOOR L1 FWD EMERGENCY SILL LT L1853 FOUND INOP. DOOR L1 FWD EMERGENCY SILL LT L1853 LAMP REPLACED AND TEST NORMAL IAW AMM 33-51-05.SDR UIEA2025070700844Seat Track · crackedM/D STA753 TO STA757 LBL11" SEAT TRACK FOUND CRACKED. SEAT TRACK CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR12 FIG 201. NO FURTHER DEFECTS NOTED.SDR UIEA2025070700846Seat Track · chafedM/D STA 1980 TO STA 1985 RBL 11.33" SEAT TRACK CROWN CHAFED. CHAFED AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT AREA MEASURED L:6" X W:0.3" X D:0.007" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NSDR UIEA2025070700847Seat Track · chafedM/D STA 2020 TO STA 2026 RBL 11 SEAT TRACK CROWN CHAFED. CHAFED AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT AREA MEASURED L:7" X W:0.3" X D:0.008", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO
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