N747BC
Service difficulty reports · 134
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N747BC' AND registry_match = 'registration' 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 n_number = 'N747BC' AND registry_match = 'registration' 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 UIEA2026032800112Indication Sys · faultedENGINE NR 3 OIL PRESSURE WENT TO ZERO. EICAS ENG 3 OIL PRESS, RAN QRH CHKLIST WHICH READ ENGINE SHUTDOWN. TEMP WAS 95 & QTY WAS 16. R & R ENG 3 & ENG RUN OK IAW AMM 71-00-00. C/W WO 158637 REV 0 & W/C L-71-099-02-01. OPS TEST PASS. NO DEFECTS NOTED.SDR UIEA2026022000064Server · inoperativeCARGO CAMERA SYSTEM UNAVAILABLE INOP(<P>REMOVED AND REPLACED VIDEO SEVER UNIT IAW AMM 23-75-05/401. OPS CHECK ALL CAMERAS NORMAL. EFB/CCAM OPS TEST OK</P>)SDR UIEA2025051200598Beam · corrodedCORROSION - BEAM L/H WING L/E LOWER PNL FWD SUPPORT BEAM INNER FACE ILES 757.(<P>1. BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV 60. 2. PFM NDT INSP REFER TO JOB CARD ATTACHING SHEET 0473658. 3. MEASURED REWORK AREA D= 0.001", L= 0.7", W= 0.5", IT WASSDR UIEA2025051200599Beam · corrodedCORROSION - BEAM L/H WING OUTBD L/E LOWER PNL FWD SUPPORT BEAM INNER FACE OLES 1552.(<P>1. BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV 60. 2. PFM NDT INSP REFER TO JOB CARD ATTACHING SHEET 0473659. 3. MEASURED REWORK AREA D= 0.003", L= 0.5", W= 0.4",SDR UIEA2025051200600Beam · corrodedCORROSION - BEAM L/H WING OUTBD L/E LOWER PNL FWD SUPPORT BEAM INNER FACE OLES 1497.(<P>1. BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV 60. 2. PFM NDT INSP REFER TO JOB CARD ATTACHING SHEET 0473660. 3. MEASURED REWORK AREA D= 0.003", L= 0.45", W= 0.4"SDR UIEA2025051200601Battery Pack · inoperativeFOUND EMER LIGHT POWER PACK INOP, M14533, M14532, X317.(<P>1. REPLACED M14333, M14532, X317 BATTERIES AND LIGHT ASSY IAW AMM 33-51-04-902-001-001 & AMM 33-51-06-004-046. 2. PERFORMED LIGHT TEST AND THE RESULT WAS SATISFACTORY.</P>)SDR UIEA2024072500751Brake Sys · faultedEICAS MESSAGE WITH MASTER WARNING: CONFIG PARKING BRAKE WITH BRAKES RELEASED, CAUSED CREW RTO AT APPROX 40KTS GROUND SPEED. HOT BRAKE TEMP IS 2 UNITS 15 MINUTES LATER(<P>FOLLWED FIM 32-44 FAULT TREE AND FIM 31-51-805. CYCLED BRAKES AND TESTED PER AMM 32-44-00-SDR UIEA2023121901004Unknown · unknownA PUNCTURED HOLE ON THE FUSELAGE SKIN NEAR STA 1241, BETWEEN S-105L & S-106L(<P>1) ACCOMPLISHED EI T2023A53M-3476 REV 1. 2) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2023121901005Lamp · unknownFOUND M14534 EMERGENCY BATTERY PACK FAIL AND X317 EMERGENCY BATTERIES FAIL(<P>1) IAW AMM 33-51-04-902-001-001 REV 109 R/R EMERGENCY BATTERY PACK AT M14534 AND PERFORMED POWER SUPPLY TEST, THE RESULT WAS SATISFACTOR. 2) IAW AMM 33-51-06-004-046 AND 33-51-06-404SDR UIEA2023052300521Unknown · unknownFOUND BRACKET DAMAGE 5 EACH AT R/H UPR W-T-B FAIRING PNL 292DR(<P>1) IAW AMM 53-51-01-004-001 REV107 RMV PNL FITTING. 2) FABRICATED PARTS AND INSTALL PARTS IAW EI NO T2023A53M-1137 REV1 3) JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2023052300520Battery Pack · unknownFOUND THE EMERGENCY LIGHT INOP. EQUIPT M14529, L6510, L1845, L1846, M3430, L6504, L6512, L6502 & X317(<P>1) IAW AMM 33-31-04-902-001-001 REV 107 REPLACED BATTERY PACK OF EMERGENCY LIGHT (M14533) AND CONDITION CHECK NORMAL. 2) IAW AMM 33-31-06-000-801 & AMM 33-SDR UIEA2023052300519Unknown · unknownCORROSION - FOUND FUSELAGE KEEL BEAM LOWER CHORD CORROSION AT STA 1032 LBL 9(<P>1) BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV 54. 2) PFM EI T2023A53M-1156 REV 0. 3) PFM NDT INSP REFER TO JOB CARD ATTACHING SHEET 0412623 & DATA SHEET 8252368-1 4) ACCSDR UIEA2023052300518Unknown · unknownCORROSION - #2 ENG LH CORE COWL OUTER SURFACE(<P>1) REPAIR DAMAGE AREA IAW EI T2023A71M-1181 REV 0. 2) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2023052300517Strap · unknownCORROSION - FND RH WING FIXED L/E UPPER CHORD AREA STRAP CORROSION AT OLES 1535(<P>1) REMOVE DAMAGE PART IAW SRM 51-40-02-06-0 REV 54. 2) INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 54, DWG 112U3640 SHEET 1 REV B, DWG 112U3620, SHEET 1 REV - AND DWG 65B10652, SSDR UIEA2023052300516Unknown · unknownCORROSION - SKIN #4 ENG LH CORE COWL COOLING AIR EXHAUST AREA AT NAC STA 230(<P>1) REPAIR DAMAGE AREA IAW EI T2023A71M-1210 REV 2. 2) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2023052300515Bracket · unknownFORWARD LOWER WING TO BODY FAIRING LOWER PANEL RIB SUPPORT BRACKET CORROSION STA 920, WBL 0(<P>1) REMOVE DAMAGE BRACKET (2 EA) IAW SRM 51-40-02-0G-0 REV 54. 2) INSTALL NEW BRACKET (2 EA) IAW SRM 51-40-02-0G-0 REV 54, DWG 65B06704 SH2 REV F AND 65B04118 SH2 REVSDR UIEA2023052300514Splice · unknownCORROSION - FOUND FUSELAGE KEEL BEAM SPLICE TEE CORROSION AT STA 1210 RBL 9(<P>1) REMOVE DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 54. 2) FABRICATE PARTS IAW EI T2023P53M-1154 REV 0. 3) INSTALL PARTS IAW SRM 51-40-02-0G-0 REV 54 & DWG 149U7010 SH 4 REV A. 4) JOB SDR UIEA2023052300513Unknown · unknownLOWER AFT WING TO BODY FAIRING 193BL PANEL FWD SUPPORT RIB SKIN CORROSION STA 1480(<P>1) REMOVE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 54. 2) INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 54 & DWG 65B15085 SH 4 REV L. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</PSDR UIEA2023052300512Unknown · unknownLIGHTNING STRIKE - FOUND FUSELAGE SKIN SURFACE HAVE LIGHTNING STRIKE AT STA 580, BETWEEN S-42L AND S-43L(<P>1) ACCOMPLISHED EI T2023A53M-1111 REV 0. 2) ACCOMPLISHED EI T2023A53M-1111 REV 1 AND EI ATTACHED TO W/O F225279(035) 3) JOB COMPLETED AND CONDITION CHECSDR UIEA2023052300511Unknown · unknownKEEL BEAM SIDE WALL SKIN CORROSION AT STA 1060 LBL 9 LEFT SIDE (PANEL 191EL INSIDE)(<P>1) BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV 54. 2) PERFORM EI T2023A53M-1156 REV 0. 3) PERFORM NDT INSPECTION REFER TO JOB CARD ATTACHING SHEET 0412622 & DATA SSDR UIEA2023052300510Stiffener · unknownKEEL BEAM SIDE WALL STIFFENER CORROSION STA 1010 RH SIDE (PANEL 192AR INSIDE)(<P>1) REMOVED THE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 54. 2) FABRICATED PART IAW EI T2023P53M-1132 REV 0. 3) INSTALL FABRICATED PART IAW SRM 51-40-02-0G-0 REV 54 AND DWG 65B01828 SSDR UIEA2023052300509Angle · unknownCORROSION - FOUND GROUNDING BRACKET CORROSION AT UNDER CENTER WING KEEL BEAM STA 1220 LBL 9(<P>1) REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0 REV 54. 2) FABRICATED PART IAW EI T2023A53M-1150 REV 1. 3) INSTALLED FABRICATED PART IAW SRM 51-40-02-0G-0 REV 54 AND BOSDR UIEA2023052300508Unknown · unknownLIGHTNING STRIKE - FOUND FUSELAGE SKIN SURFACE HAVE LIGHTNING AT STA 666 BETWEEN S-42L AND S-43L(<P>1) ACCOMPLISH EI NO. T2023A53M-1111 REV 0. 2) ACCOMPLISHED EI NO T2023A53M-1111 REV 1 AND EI ATTACHED TO W/O NO. 8225279. 3) JOB COMPLETED AND CONDITIONAL CHECKSDR UIEA2023052300507Unknown · unknownDISBOND - R/H WING OUTBD AFT FLAP TOP PANEL(<P>1) CUT OUT THE DISBOND MATERIALS AND CLEAN. MEASURE THE CUT OUT (L =2" W= 1". 39" FROM INBD EDGE 5.5" FROM AFT EDGE. BOND THE FILLER AND EXTERNAL DOUBLER (L= 4.2", W=4") WITH FILM ADHESIVE CURE AT 250„‰ FOR 90 MISDR UIEA2023052300506Unknown · unknownCORROSION - FOUND FUSELAGE SKIN CORROSION STA 1700 - STA 1720, S46L - S47L(<P>1) ACCOMPLISH EI T2023A53M-1148 REV 0. 2) ACCOMPLISH EI T2023A53M-1148 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2023052300505Unknown · unknownEXISTING UNDOCUMENTED REPAIR ON AFT CARGO DOOR OUTBD SKIN FWD SIDE(<P>1) PERFORM EXTERNAL AND INTERNAL DVI AND NDT INSPECTION REFER TO JOB CARD ATTACHING SHEET 0398151. 2) ACCOMPLISH EI T2023A53M-1140 REV 0. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2023052300504Unknown · unknownLIGHTNING STRIKE - FOUND FUSELAGE SKIN SURFACE HAVE LIGHTNING STRIKE AT STA 680 S42L(<P>1) ACCOMPLISH EI T2023A53M-1111 REV 0. 2) ACCOMPLISH EI T2023A53M-1111 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2023052300503Unknown · unknownLIGHTNING STRIKE - FOUND FUSELAGE SKIN SURFACE HAVE LIGHTNING STRIKE AT STA 460 BETWEEN S40L AND 241L(<P>1) ACCOMPLISH EI T2023A53M-1119 REV 0. 2) ACCOMPLISH EI T2023A53M-1119 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2023052200494Unknown · unknownDISBOND - R/H WING OTBD AFT FLAP TOP PANEL UPPER SURFACE WBL 700(<P>1) CUT OUT THE DISBOND MATERIALS AND CLEAN. MEASURE THE CUT OUT (L =5" W= 2". 3/5" FROM OUTBD EDGE 4.4" FROM AFT EDGE. INSTALL THE REPAIR CORE WITH COMPOUND CURE AT 250„‰ FOR 90 MINUTES WITH SDR UIEA2022070700729None · none4 UN-COMMANDED LEFT YAW EVENTS WHILE IN CRUISE. EICAS YAW DAMPER UPPER AND YAW DAMPER UPPER STS MSG(<P>PLACED UPPER YAW DAMPER ON MEL 22-21-01.</P>)SDR UIEA2019110105827Skin · bulgedBULGE ON THE RH SIDE FUSELAGE SKIN AT STA 730, BETWEEN S-43R TO S-44R. (<P>REPAIRED THE DAMAGED AREA IAW SRM 53-00-01-2R-1 REPAIR 1 REV. 43 AND EI NO. T2019A53M-4039 REV. 1. REPAINTED THE RE-WORKED AREA IAW AMM 51-24-11-477-083 REV. 96. JOB COMPLETED AND CONDISDR UIEA2019110105828Snubber · failedFOUND R1 DOOR ROTARY SNUBBER FAIL (INDICATOR OUT OF LIMITS).(<P>REMOVED AND REPLACED R1 DOOR ROTARY SNUBBER ASSY IAW AMM TASK 52-11-10-004-001 REV. 96 AND TASK 52-11-10-404-005 REV. 96. JOB COMPLETED AND CONDITION CHECKS NORMAL.</P>)SDR UIEA2019110105829Splice Plate · corrodedCORROSION - PLATE, L/H WING L/E TO FRONT SPAR CAVITY AT OLES 1545.50.(<P>REMOVED DAMAGED PART IAW SRM 51-40-02 REV. 43. FABRICATED NEW PART IAW EI NO T2019P57M-4063 REV. 0. INSTALLED NEW FABRICATED PART IAW SRM 51-40-02 REV. 43 AND DWG 65B11862 SH2 REV F. JOB SDR UIEA2019090805456Light · inoperativeMAIN DECK CEILING EMERGENCY LIGHT LEFT SIDE APPROX 430 INOP. RELAMPED, TESTED GOOD.SDR UIEA201908215228Tru · arced#4 AC DISTRIBUTION CB TRIPPED AFTER TAKEOFF, 500'. MULTIPLE MALFUNCTIONS. FOUND SIGNS OF ELECTRICAL ARCING AT THE #4 AC DISTRIBUTION CB AND #4 TR/CB. REMOVED AND REPLACED #4 AC DISTRIBUTION C/B AND TR C/B REF AMM 24-22-02 AND SWPM 20-30-00. ALSO REMOVED AND RSDR UIEA2019081905214Circuit Breaker · trippedAC DIST CB 3C4 TRIPPED IN FLIGHT, MULTIPLE MALFUNCTIONS. AFTER TURNING OFF AC POWER, CLEANED AND INSPECTED INSIDE OF P6 PANEL AREA PER AMM 20-60-02-04. AFTER TURNING ON AC POWER, CYCLED AC DISTRIBUTION CB ON P6 3C4. NO CB'S POP-UP. AC GENERATION OPS TEST C/OUSDR UIEA2018080301620Rvdt · faultyUPPER EICAS "FLAPS DRIVE" MESSAGE. TRAILING EDGE FLAPS STATUS MSG. FOUND RIGHT HAND OUTBOARD RVDT INDICATION FLUCTUATES. REMOVED AND REPLACED OUTBOARD RVDT IAW AMM 27-58-01. OPS CHECKED NORMAL PER AMM 27-58-01-725-050.SDR UIEA2018062601256Skin · brokenCRACK AND BROKEN ON NR 4 PYLON RIGHT SIDE ACCESS DOOR SURROUND SKIN AND DOUBLER. REPAIR CRACK AREA IAW EI NO T2018A54M-2819 REV 1 2. JOB COMPLETED AND COND CHK NML.SDR UIEA2018062601257Seat Track · crackedCRACK SEAT TRACK. FWD MAIN DECK FLOOR PANEL BELOW AT BS 260, RBL 56. REPAIR SEAT TRACK IAW SRM 53-00-52 REPAIR 6 FIG 201 ALTERNATIVE 2 REV 39 AND DWG NO 14115257 542 REV B. COND CHK NML AND JOB COMPLETED.SDR UIEA2018062601258Cargo Track · wornWEAR DAMAGE ON MAIN DECK ROLLER TRAY CARGO RAIL AND ENTRANCE GUIDES AT BL98.20. ACCOMPLISHED EI NR T2018A53M-3252 REV 0. JOB COMPLETED AND COND CHK NML.SDR UIEA2018062601261Skin · corrodedCORROSION ON NR 3 ENG LT CORE COWL SKIN BETWEEN INSTA 222..5 AND INSTA 230.5. RMV CORROSION PANEL IAW SRM 51-40-02-06-0 REV 39. INSTALL NEW PANEL AND REPAIR CORROSION AND REPAIR CORROSION AREA IAW EI NO T2018A71M-2843 REV 2.3. JOB COMPLETED AND COND CHK NML.SDR UIEA2018062601262Motor · failedTHE RT WLG ALTERNATE EXTENSION MOTOR FUNCTION TEST FAIL. IAW AMM 32-36-01-004 REV92 AND AMM32-36-01-404-009 REV92 RPL RT WLG ALTERNATE EXTENSION MOTOR 2. IAW AMM 32-36-00-705-009 REV92 PFM WLG ALTERNATE EXTENSION SYSTEM OPERATION TEST 3. COND CHK NML.SDR UIEA2018062601263Battery · dischargedFOUND EMER SLIDE LIGHT AT M/D L1 DOOR INOP. IAW AMM 33-51-06-000-801 AND 33-31-06-400-801 REV 92 REPLACED LIGHT BATTERY. IAW AMM 33-51-00-T151-105 REV 92 REV 92 PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST AND THE RESULT WAS SATISFACTORY.SDR UIEA2018062601264Battery · dischargedFOUND M/D EMERGENCY LIGHT INOP. IAW AMM 33-51-07--902-001-001 REV 92 REPLACED 3 EMERGENCY LIGHT POWER SUPPLY BATTERIES AND CONDITION CHECK NORMAL. IAW AMM 33-51-04-902-001-001 REV 92 STEP E PERFORMED POWER SUPPLY TEST AND THE RESULT WAS SATISFACTORY.SDR UIEA2016121901032Web · crackedCRACK ON WEB OF MAIN DECK CARGO FLOOR NEAR BS1790 LBL 101. REPAIR THE DAMAGE AREA IAW EI T2016-A53M2862 REV 1.SDR UIEA2016121901033Actuator · inoperativeTHE RT MLG ALTERNATE EXTENSION ACTUATOR CANNOT SHUT OFF IAW AMM 32-36-01-004-001 AND AMM 32-36-01-404-009 REV 87. STEP 3A - 3F REPLACED THE MLG ALTERNATE EXTENSION ACTUATOR IAW AMM 32-36-00-705-009 REV87 PFM OPERATION TEST FOR MLG ALTERNATE EXTENSION SYS, RESUSDR UIEA2016121901034Thermal Switch · inoperativeFOUND THERMAL SWITCH FUNCTION NOT WORKING, TOTAL 12EA.(<P>1) IAW AMM 26-18-02-004-001, 25-26-18-02-404-011 REV87 REPLACED THERMAL SWITCH TOTALL 12EA. 2) TRANSFER TEST TO T/C L260180101 AND NRC 456.
SDR UIEA2016121901036Transfer Valve · inoperativeFOUND RT WING JETTISON TRANSFER VALVE FAILED DURING GROUND TEST IAW AMM 28-31-04-004-001 REV87 AND AMM28-31-04-404-010 REV 87. REPLACED THE TRANSFER VALVE IAW AMM 28-31-00-715-066 REV 87SDR UIEA2016121901037Web · crackedCRACK ON WEB OF MAIN DECK CARGO FLOOR NEAR BS 870. LBL 101. REPAIRED IAW T2016A53M-2908 REV. 1.SDR UIEA2016121901038Skin · nickedTWO NICKS ON SEC 47 FUSELAGE SKIN NEAR BS 2340+20 AND STRINGER 101R. REPAIRED IAW T2016A53M-2846 REV. 1.
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