Boeing 747-123

Service difficulty reports · 2,292

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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 = '747123'
  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.

SDR UPS05443821Frame · crackedFRAME BS 1600 INNER FLANGE CRACKED BTN S-25 / S-26L. INNER FLANGE REPAIRED PER RS R53-62-35240 AND EO B747-5310-21668-A.Jan 6, 2005 · N675UP · Boeing 747123 · Fuselage Main, FrameSDR UPS05443816Frame · crackedFRAME BS 1416 INNER FLANGE CRACKED AT S-22L. M/D FRAME INNER FLANGE REPAIRED AT BS 1416 S-22L AS PER RS : R-53-42-35233 AND ENGINEERING FILE NUMBER : 747-53-20219.Jan 6, 2005 · N675UP · Boeing 747123 · Fuselage Main, FrameSDR UPS05443813Stringer · crackedBS 1476 - 1478 STR 13R STRINGER END FOUND CRACK. STRINGER REPAIRED PER RS 53-41-35250 AND ENGINEERING FILE NUMBER 747-53-20214.Jan 6, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443798Clip · crackedINSPECTION TYPE:C, LOWER FUSELAGE LT INTERNAL NOSE L/G WHEEL WELL VERTICAL BEAM HORIZONTAL STIFFENER ATTACH CLIP FOUND CRACKED AT STA 300 WL 150. STIFFENER ATTACH CLIP REPLACED PER SRM 51-10-01 PG 9.Jan 6, 2005 · N675UP · Boeing 747123 · Fuselage Main, Attach FittingsSDR UPS05443796Stringer Clip · crackedINSPECTION TYPE:C - BS 1160 S15L STRINGER TIE CLIP FOUND CRACKED. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.Jan 6, 2005 · N675UP · Boeing 747123 · Fuselage Main, Attach FittingsSDR UPS05443770Frame · crackedINSPECTION TYPE:C M/D - BS 1372, BETWEEN STR 22 - 23R, FRAME I/B CHORD O/B FACE FOUND CRACK. M/D FRAME I/B CHORD REPAIRED AT BS 1372 BETWEEN S-22R AND S-23R AS PER RS 53-62-35246 AND ENGINEERING FILE NUMBER 747-53-20208.Jan 6, 2005 · N675UP · Boeing 747123 · Fuselage Main, FrameSDR UPS05443765Frame · crackedINSPECTION TYPE:C - FRAME BS 1372 INNER FLANGE CRACKED AT S-22L. INNER FRAME REPAIRED PER RS 53-42-35235 AND ENGINEERING FILE NUMBER 747-53-20205.Jan 6, 2005 · N675UP · Boeing 747123 · Fuselage Main, FrameSDR UPS05443722Stringer · crackedINSPECTION TYPE:C - STR END BS 1484 S-17L CRACKED. CRACKED STRINGER REPAIRED PER RS 53-41-35227 AND ENGINEERING FILE NUMBER 747-53-20203.Jan 6, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443721Stringer · crackedINSPECTION TYPE:C M/D - STR END BS 1476 S-15L CRACKED. CRACKED STRINGER REPAIRED PER RS 53-41-35226 AND ENGINEERING FILE NUMBER 747-53-20202.Jan 6, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443677Spar · crackedINSPECTION TYPE:C, LEFT WING UPPER REAR SPAR OF BODY SPLICE FOUND CRACK AT NR 8 HOLE UPPER SPLICE FITTING RUNNING AFT. BOLT HOLE REWORK AS PER S/B 747-57A2314.Jan 6, 2005 · N675UP · Boeing 747123 · Wing SparSDR UPS05443675Spar · crackedINSPECTION TYPE:C, LT WING UPPER REAR SPAR SIDE OF BODY SPLICE FOUND CRACK AT NR 1 HOLE AT SPAR CHORD (REFER FIGURE FOR DETAILS ). HOLE REPAIRED AS PER S/B 747-57A2314.Jan 6, 2005 · N675UP · Boeing 747123 · Wing SparSDR UPS05443673Spar · crackedINSPECTION TYPE:C, LT WING UPPER REAR SPAR SIDE OF BODY SPLICE FOUND CORROSION CRACK AT HOLE NR 4 AT INTERNAL SPLICE FITTING (REFER FIGURE FOR DETAILS ). HOLE REPAIRED AS PER SB 747-57A2317.Jan 6, 2005 · N675UP · Boeing 747123 · Wing SparSDR UPS05443729Stringer Clip · crackedINSPECTION TYPE:C M/D - BS 1640 LT STR 3L TIE CLIP FOUND CRACKED. M/D BS 1640 STR 3L TIE CLIP REPLACED IAW SRM 51-10-01 PAGE 9.Jan 5, 2005 · N675UP · Boeing 747123 · Fuselage Main, Attach FittingsSDR UPS05443719Frame · crackedINSPECTION TYPE:C, NR 4 NACELLE STRUT REAR MOUNT BULKHEAD FWD OUTBOARD FRAME WEB FOUND CRACKED (REFER ATTACH SKETCH FOR LOCATION). REAR ENG MOUNT BULKHEAD FRAME REPAIRED PER RS R54-53-35228 AND ENGINEERING FILE NUMBER 747-54-20050.Jan 5, 2005 · N675UP · Boeing 747123 · Nacelle/Pylon, Frame/Spar/RibSDR UPS05443651Stringer · crackedINSPECTION TYPE:C - BS 1680 LT S-L8 STRINGER FOUND CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 4.Jan 5, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443799Bulkhead · crackedINSPECTION TYPE:C, LEFT BLG WHEEL WELL AFT BULKHEAD STA 1480 APU DUCT PASSING HOLE CUTOUT SUSPECT CRACKED AT 10:30 POSITION AS MARKED. LEFT BS 1480 BULKHEAD WEB APU DUCT CUTOUT REPAIR CARRIED OUT AS PER EO B747-5310-C APPENDIX B FIG 4 AND DWG 144U2602.Jan 4, 2005 · N675UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS05443718Rib · crackedINSPECTION TYPE:C, RT WING NR 23 O/B ARM I/B RIB O/B FACE -D- POINT AREA SUSPECT CRACK. RIB REPAIRED AS PER RS R-57-41-35223 AND EO B747-5740-21619-A.Jan 4, 2005 · N675UP · Boeing 747123 · Wing, Rib/BulkheadSDR P5CA0501300Warning Light · illuminatedDURING FULL THRUST T/O AT 650', NR4 ENGINE FAILED WITH FIRE INDICATION. SHUT DOWN ENGINE AND FIRED BOTTLES. REPLACED LEFT AND RIGHT FIRE BOTTLES PER MM 26-21-03. ALL TESTS OK.Dec 30, 2004 · N858FT · Boeing 747123 · Fire DetectionSDR P5CA0501299Engine · failedDURING FULL THRUST T/O 650' NR 4 ENGINE FAILED WITH FIRE INDICATION. SHUT DOWN ENGINE AND FIRED BOTTLES. REPLACED NR 4 ENG PER WC 7100-002. RUN UP OK.Dec 30, 2004 · N858FT · Boeing 747123 · Powerplant SystemSDR P5CA0401295Pump · leakingNR 4 HYDRAULIC QUANTITY WENT TO ZERO IN CLIMB. FOUND HYDRAULIC LEAK ON NR 4 ENG EDP. REMOVED EDP AND INSTALLED HYDRAULIC PUMP FROM THE NR 3 ADP POSITION. OPS AND LEAK CHECK OK. NR 3 ADP DEACTIVATED PER MEL 29-2A.Dec 28, 2004 · N858FT · Boeing 747123 · Hydraulic Pump (Electric/Engine), MainSDR P5CA0401290Tire · leakingNR 4 TIRE FOUND WITH SCREW IMBEDDED AND LEAKING AIR. REPLACED WHEEL ASSY PER MM 32-45-01. SPIN & LEAK CHECK OK.Dec 20, 2004 · N858FT · Boeing 747123 · TireSDR UPS04443610Pump · inoperativeCREW SHUTDOWN NR 2 ENGINE IN FLIGHT DUE TO ENGINE NOT RESPONDING. CREW RESTARTED AND ENGINE PERFORMED NORMALLY. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL PER MM 73-21-01 AND 73-11-01. PERFORMED ADJ AND TEST PER MM 71-00-00 OPS CK LEAK CK GOOD.Dec 15, 2004 · N676UP · Boeing 747123 · Engine Fuel PumpSDR P5CA0401285Module · malfunctionedAFTER LANDING TOWER REPORTED SUSPECTED BLOWN TIRES. AT BLOCKS, FOUND NR 10 & 12 TIRES BLOWN. ON CONDITIONAL INSPECTION FOUND DAMAGE TO RT UPPER AFT WING/BODY FAIRING BETWEEN STA 1540 AND 1580. ALSO FOUND DAMAGE TO RT INBD TRAILING EDGE MID FLAP. REPLACED NDec 12, 2004 · N858FT · Boeing 747123 · Brake Anti-Skid SectionSDR P5CA0401281Chain · contaminatedDURING STAB TRIM CHECK STAB TRIM BINDING IN BOTH ELECTRICAL & MANUAL. CLEANED DEBRIS ON STAB TRIM CONTROL WHEEL CHAIN, INDICATIONS CHECKED NORMAL.Dec 5, 2004 · N858FT · Boeing 747123 · Stabilizer Control SystemSDR P5CA0401280Window · crackedON CLIMBOUT FROM ANCHORAGE THE R1 WINDOW STARTED ARCING & CRACKING. A 15 INCH CRACK DEVELOPED ON THE TOP EDGE OF THE WINDOW. FUEL WAS JETTISONED & A/C RETURNED TO ANCHORAGE. REMOVED & REPLACED R1 WINDOW.Nov 19, 2004 · N858FT · Boeing 747123 · Flight Compartment WindowsSDR P5CA0401275Seal · failedDURING CRUISE AT FL 36.0, NR 1 ENGINE OIL PRESSURE FLUCTUATING 40-35 PSI WITH OIL PRESSURE LIGHT DOING SAME. OIL PRESSURE WENT TO 25 PSI WITH STEADY LOW OIL PRESSURE LIGHT ON, ENGINE SHUTDOWN, WINDMILLING OIL PRESSURE 15-20 PSI. REPLACED STARTER SEAL PER AMMNov 16, 2004 · N858FT · Boeing 747123 · Turbine Engine Oil SystemSDR UPS04443493Light · inoperativeAFT EMERGENCY EXIT LIGHT INOP AT ENTRY DOOR. RELAMPED, OP'S CHECKED GOOD.Nov 14, 2004 · N676UP · Boeing 747123 · Emergency LightingSDR 04053Engine · failedON T/O FROM HNL, NR 4 ENGINE LOSS AT 200 FT WITH LOUD BANG AND BRIGHT FLASH. EGT WENT TO 1100 DEGREES, ENGINE OIL PRESSURE APPROX 10 PSI FOR 5 MIN, THEN WENT TO 5PSI. RETURNED TO HNL. BOROSCOPED NR 4 ENGINE LP AND HP COMP SECTIONS AND FOUND EVIDENCE OF BIRDOct 24, 2004 · N717CK · Boeing 747123 · Engine (Turbine/Turboprop)SDR UPS04443426Floorbeam · crackedINSPECTION TYPE: SPV, SEAT TRACK SUPPORTS HAVE ELONGATED MOUNTS HOLES AT STA 1920, 1940, LBL 98.58. REMOVED 2EA DAMAGED SUPPORT ANGLES. FABBED ANGLE 69B04527 PER DWG STA 1920 ATTACH ANGLE CRACKED. FABBED AND INSTALLED REPAIR PER SRM 51-40-03. NDT VERIFIED Oct 19, 2004 · N675UP · Boeing 747123 · Fuselage Main, Floor BeamSDR P5CA0401256Skin · corrodedRT WING UPPER SKIN HAS CORROSION AT WING STATION 697 MID SPAR. BLENDED OUT CORROSION, WITHIN LIMITS IAW SRM 57-30-01 AND 57-30-03.Oct 19, 2004 · N858FT · Boeing 747123 · Wing, Plate/SkinSDR P5CA0401257Skin · delaminatedRT WING FIXED L/E UPPER SKIN B/W WING STATION 570 AND 600 LWR SURFACE DELAMINATED. REMOVED PANEL REPAIRED AND REINSTALLED IAW SRM 51-30-02.Oct 19, 2004 · N858FT · Boeing 747123 · Wing, Plate/SkinSDR P5CA0401255Stringer · crackedAFT CARGO COMPARTMENT LT BS 1600 STRINGER 39L AND STRINGER 40L CRACKED. STOP DRILLED, FABRICATED DOUBLER AND INSTALLED IAW SRM 53-10-04.Oct 19, 2004 · N858FT · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS04443428Seat Track · damagedINSPECTION TYPE: SPV, MAIN DECK SEAT TRACK REMOVED ALONG LBL 98.58 FROM STA 1840-1920. TRIMMED OUT DAMAGED SEAT TRACK & FABBED REPLACEMENT SECTION REF SRM 53-10-05 FIG 1A, DETAIL II. FABRICATED SPLICE FITTING 69B02537-15 PER DWG. FABRICATED 69B04238-1,-3 FIOct 18, 2004 · N675UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS04443425Floorbeam · damagedINSPECTION TYPE: SPV, FLOORBEAM 65B38095 STA 1900, LBL 98.58, SEAT TRACK ATTACH HOLES FOUND OVERSIZED FWD HOLE 0.350, AFT HOLE 0.390. REMOVED AFT ATTACH ANGLE, REAMED BEAM HOLES FWD 0.389, AFT 0.432 PER EO. FAB & INSTALLED 2EA FREEZE PLUGS PER SKETCH & SRM Oct 18, 2004 · N675UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS04443424Floorbeam · damagedINSPECTION TYPE: SPV, FLOORBEAM 65B38096 STA 1920 LBL 98.58, SEAT TRACK ATTACH HOLES FOUND OVERSIZED, FWD & AFT HOLES 0.380. REAMED BEAM HOLES TO; FWD 0.389, AFT 0.432 PER EO. FAB & INSTALLED FREEZE PLUGS PER SKETCH & SRM 51-10-08. FAB FWD FITTING 69B04238 Oct 18, 2004 · N675UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS04443423Floorbeam · damagedINSPECTION TYPE: SPV, FLOORBEAM 65B38093, STA 1860 LBL 98.58, SEAT TRACK ATTACH HOLES FOUND OVERSIZED. FWD HOLE 0.350, AFT HOLE 0.410. REMOVED AFT TRACK ATTACH ANGLE. REAMED BEAM HOLES TO 0.389 & 0.432 PER EO. FAB & INSTALLED FREEZE PLUGS PER SKETCH AND SROct 18, 2004 · N675UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS04443422Floorbeam · damagedINSPECTION TYPE: SPV, FLOORBEAM 65B38094 STA 1880, LBL 98.58 SEAT TRACK ATTACH HOLES FOUND OVERSIZED, FWD HOLE 0.340, AFT HOLE 0.380. REMOVED AFT ATTACH ANGLE, REAMED HOLES IN BEAM TO 0.389 PER EO. FAB & INSTALLED FREEZE PLUGS PER SKETCH. REAMED OVERSIZED TOct 18, 2004 · N675UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS04443421Floorbeam · damagedINSPECTION TYPE: SPV, FLOORBEAM 65B38092, STA 1840 LBL 98.58, SEAT TRACK ATTACH HOLES FOUND OVERSIZED, FWD HOLE 0.330 IN, AFT HOLE 0.390 IN. REAMED HOLES TO 0.389 AND 0.432. FABRICATED AND INSTALLED FREEZE PLUGS PER EO. REPLACED 65B38120-1 FITTING DUE TO OOct 18, 2004 · N675UP · Boeing 747123 · Fuselage Main, Floor BeamSDR P5CA0401254Stringer · crackedFUSELAGE STRINGER 9R HAS CRACKS AT BODY STATIONS 1372 AND 1394. REMOVED SHEAR TIE CLIPS, REMOVED STRINGER 11R FOR ACCESS, REMOVED STRINGER INSTALLATION AND INSTALLED NEW STRINGER IAW SRM 51-30-02 , REMOVE STRINGERS AND SHEAR TIE CLIPS.Oct 18, 2004 · N858FT · Boeing 747123 · Fuselage Main, Longeron/StringerSDR P5CA0401253Flap Track · corrodedNR 6 FLAP TRACK AFT ATTACHMENT IB BLOCK OB HOLE CORRODED ON WING AT STA 353. REMOVED CORROSION, OPEN HOLE HFEC PERFORMED OK, REPAIRED IAW SRM 51-10-01.Oct 18, 2004 · N858FT · Boeing 747123 · Trailing Edge FlapsSDR P5CA0401262Skin · delaminatedLEFT WING STATION 382 UPPER SURFACE ON TOP PANEL BY STRUT DELAMINATED & CRACKED. REMOVE PANEL & REBONDED, REINSTALLED PER SRM 51-10-09.Oct 17, 2004 · N858FT · Boeing 747123 · Wing, Plate/SkinSDR P5CA0401261Skin · canningBS 2360 TO 2380 STRINGER LEFT IS OIL CANNING. PERFORM HFEC, NO CRACKS. REMOVED AND REPLACED SKIN PER SRM 51-10-02.Oct 17, 2004 · N858FT · Boeing 747123 · Fuselage Main, Plate/SkinSDR UPS04443337Bulb · inoperativeMAIN CARGO DECK CEILING EMERGENCY LIGHT FWD OF L1 DOOR HAS ONE BULB INOPERATIVE AND VERY DIM. REMOVED AND REPLACED MAIN CARGO DECK CEILING EMERGENCY LIGHT JUST FWD OF L1 DOOR IAW MM 33-51-07. OPS CKS NORMAL.Oct 12, 2004 · N675UP · Boeing 747123 · Emergency LightingSDR P5CA0401250Attach Fitting · crackedRIGHT WING L/E AFT ATTACHED FRAME (FSSI) TO WING FRONT SPAR UPPER CHORD HAS CRACKED AFT FSSI 335. REMOVED CRACK T-ANGLE & INSTALLED NEW T-ANGLE PER SRM 51-30-02.Oct 11, 2004 · N858FT · Boeing 747123 · Wing, Attach FittingsSDR P5CA0401249Frame · crackedAFT CARGO COMPT SECONDARY FRAME B/W STA 1740 & 1760 LBL 30 IS CRACKED. REMOVED DAMAGE FRAME & INSTALLED NEW FRAME PER SRM 51-30-02.Oct 11, 2004 · N858FT · Boeing 747123 · Fuselage Main, FrameSDR P5CA0401248Skin · delaminatedRIGHT I/B ELEVATOR LWR SURFACE SKIN HAS DELAMINATION. REMOVED DAMAGE AREA, INSTALLED NEW PER SRM 51-40-04.Oct 11, 2004 · N858FT · Boeing 747123 · Elevator, Plate/SkinSDR P5CA0401247Stringer · crackedFUSELAGE STRINGER AT 10R HAS CRACK B/W STA 1372-1392. REMOVED DAMAGE AREA, REPLACED WITH NEW STRINGER AS PER SRM 53-10-03.Oct 11, 2004 · N858FT · Boeing 747123 · Fuselage Main, Longeron/StringerSDR P5CA0401246Frame · crackedMAIN DECK CEILING AREA FRAME WEB STA 960 STR 5R CRACKED. STOP DRILL CRACK PER SRM 51-30-02, 53-10-04, 51-00-00.Oct 11, 2004 · N858FT · Boeing 747123 · Fuselage Main, FrameSDR P5CA0401245Panel · crackedRIGHT WING I/B FIXED T/E LWR PNL, I/B EXTENDED CHORD HAS CRACK 2 INCHES LONG AT WS 440. REMOVE CHORD INSTALLED NEW CHORD AS PER SRM 51-30-02.Oct 11, 2004 · N858FT · Boeing 747123 · Wing, Plate/SkinSDR P5CA0401239Beam · crackedBULK CARGO COMPT, LONGITUDNAL BEAM AT STA 2040-2060-2080 LBL 30 IS CRACKED. REMOVED DAMAGE SECTION, FABRICATED NEW PART & INSTALLED PER SRM 51-40-04.Oct 1, 2004 · N858FT · Boeing 747123 · Fuselage Main, Longeron/Stringer
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