Boeing 747-123

Service difficulty reports · 2,292

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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 UPS02438120Ground Wire · looseINSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY WEAK AT LIGHT ABOVE UPPER DECK EMERGENCY DOORWAY AREA. FOUND BAD GROUND AT EXIT SIGN ABOVE UPPER DECK EMERGENCY DOORWAY. RESECURED GROUND. OPS CHECK GOOD IAW B747 MM 33-51-00.May 6, 2002 · N674UP · Boeing 747123 · Light System WiringSDR UPS02438119Light · missingINSPECTION TYPE:N/A EMERGENCY LIGHT INOP RT SIDE OF MAIN DECK AFT OF LADDER. FOUND MISSING LIGHT ASSY. INSTALLED LIGHT B747 MM 33-51-00, OPS CHECK GOOD.May 6, 2002 · N674UP · Boeing 747123 · Emergency LightingSDR UPS02438234Stringer · corrodedINSPECTION TYPE:C FWD CARGO COMPT - BS 710 STR 29R STRINGER CORROSION FOUND. BS 670 - 740 STR STRINGER REPLACED AS PER SRM 51-10-01 PG 8.May 3, 2002 · N676UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS02438222Stringer · crackedINSPECTION TYPE:C FWD CARGO COMPT - AFTER STRINGER SPLICE REMOVED STRINGER END FOUND CRACK AT BS 740 STR 28R. STRINGER REPLACED AS PER SRM 51-10-01 PG 8.May 3, 2002 · N676UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS02438331Frame · corrodedINSPECTION TYPE:C FWD CARGO COMPT - BS 700 S28R AREA FRAME I/B CHORD CORRODED. BS 700 RIGHT FRAME CRACK REPAIR AT S28R AS PER RS R-53-22-34798 & EA 747-53-20067.May 2, 2002 · N676UP · Boeing 747123 · Fuselage Main, FrameSDR UPS02438266Attach Angle · corrodedINSPECTION TYPE:C FWD CARGO COMPT - BS 700 S28R WEB I/B ATT ANGLE CORROSION CRACKED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS. FWD CARGO COMPT BS 690-730 S28R WEB I/B ATT ANGLE REPAIRED AS PER SRM 51-40-03 FIG 2.May 2, 2002 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02438344Angle · corrodedINSPECTION TYPE:C RT WLG CANTED BULKHEAD LWR CAP FOUND CORROSION AT RBL 53 BS 1241 TO 1241. THIS REPAIR IS CONSIDERED TIME - LIMITED FOR 24 MONTHS UNTIL AN IMPROVED DRAINAGE MODIFICATION CAN BE INSTALLED IAW BOEING SERVICE BULLETIN 747-51A2054 REV 1 AS PER UPMay 1, 2002 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02438254Bulkhead · crackedINSPECTION TYPE:C NR 2 PYLON REAR ENGINE MOUNT BULKHEAD CRACK FOUND AT AFT WEB APPROX 4 O'CLOCK (VIEW LOOKING FWD). NR 2 PYLON REAR ENGINE MOUNT BULKHEAD REPAIRED AS PER INSTRUCTION ON HAECO REPAIR SCHEME R-54-53-34787.Apr 29, 2002 · N676UP · Boeing 747123 · Nacelle/Pylon, Bulkhead/FirewallSDR UPS02438334Rib · crackedINSPECTION TYPE:C DURING LHW NR 9 L/E FLAP GREASE LUBE AS NR 3 ROTARY ACTUATOR (COUNT FROM O/B) REMOVED, L/E RIB O/B FWD AREA FOUND CORROSION AT ILES 800. L/E RIB AT ILES 800 IS REPLACED AS PER SRM 51-10-01. CORROSION FOUND CRACKED THROUGH AT 2 LOCATIONS.Apr 28, 2002 · N676UP · Boeing 747123 · Leading Edge DevicesSDR UPS02438330Window Frame · corrodedINSPECTION TYPE:C M/D - BS 1840 - 1860 RT BETWEEN S-20R AND S-22R WINDOW FORGINGS FOUND CORRODED AFTER NRC RECTIFICATION. REPAIR WINDOW FORGING AT M/D BS 1840 - 1860 RT BTN S20R - 22R.Apr 26, 2002 · N676UP · Boeing 747123 · Fuselage Main, StructureSDR UPS02438332Support · corrodedINSPECTION TYPE:C M/D - BS 1241 - 1265 RBL 34 SLOPE CANTED BULKHEAD LONGITUDINAL FLOOR TRACK SUPPORT BOTTOM -T- CHORD FINDING HEAVILY CORRODED. M/D BS 1241 - 1265 RBL 34 LONGITUDINAL FLOOR TRACK BOTTOM -T- CHORD REPLACED IAW SRM 51-10-01 PAGE 8.Apr 25, 2002 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02438305Floor Support · corrodedINSPECTION TYPE:C M/D - BS 1220 LBL 96 LONGITUDINAL FLOOR SUPPORT TRACK SUPPORT WEB BOTTOM -T- CHORD HEAVY CORROSION. FLOOR LONGITUDINAL TRACK BOTTOM CHORD REPAIRED PER RS R53-45-34793. BEYOND SRM 53-10-01 ALLOWABLE.Apr 25, 2002 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02438173Stringer · crackedINSPECTION TYPE:C M/D BS 2178 LT NR 1 STRINGER END CRACKED. BS 2178 S1L, STRINGER SEGMENT REPAIR AS PER SRM 53-10-03 FIG 4 AND FINISHED PAINT TOUCH UP PER MM 51-24-11.Apr 24, 2002 · N676UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS02438337Fitting · crackedINSPECTION TYPE:C 3 EA FASTENER HOLES FOUND CRACK ON THE BATH TUB FITTING OF LT SIDE BS 980 STR 38L. LT STA 980 S38L BATHTUB FITTING REPAIRED AS PER RS R53-23-34791. A PERMANENT REPAIR TO THE BATHTUB FITTING IS TO BE ACCOMPLISHED WITHIN 18 MONTHS. CONTINUE Apr 23, 2002 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02438302Floorbeam · crackedINSPECTION TYPE:C LT BS 340 UPPER DECK FLOORBEAM ONE EACH FASTENER HOLE CRACK REVEALED AT UPPER CHORD LAYER THROUGH THICKNESS. U/D BS 340 FLOORBEAM UPPER CHORD PARTIALLY REPLACED FROM LBL 35 TO LT MOST O/B IAW HAECO RS R-53-15-34801 AND DWG 141U0044 SHEET 2 FApr 23, 2002 · N676UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS02438268Fitting · crackedINSPECTION TYPE:C CRACK REVEAL ON THE FASTENER HOLE OF THE FITTING INSIDE WING CENTER TANK COMMON TO LT SIDE BATHTUB FITTING RUNNING UPWARD APPROX .125" LONG. LT SIDE STA 983 S38L INSIDE DRY BAY BATHTUB DRAG FITTING REPLACED AS PER SRM 51-30-02.Apr 23, 2002 · N676UP · Boeing 747123 · Wing, Center BoxSDR UPS02438267Skin · crackedINSPECTION TYPE:C 2 EACH FASTENER HOLES FOUND CRACK ON LT BS 980 S38L SKIN PANEL. FX BS 980 LT STR SKIN REPAIRED AS PER SRM 53-30-03 FIG 60 AT BS 975 - 983 LT BETWEEN STR 37 - 39L.Apr 23, 2002 · N676UP · Boeing 747123 · Fuselage Main, Plate/SkinSDR UPS02438235Stiffener · corrodedINSPECTION TYPE:C AFT CARGO COMPT - BS 1800 S-34R AREA FRAME ATT STIFFENER CORRODED. AFT CARGO COMPT BS 1800 S-34R AREA FRAME ATT STIFFENER REPLACED AS PER SRM 51-10-01 PG 8.Apr 23, 2002 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02438190Angle · crackedINSPECTION TYPE:C M/D - NLG PRESSURE DECK UPPER SURFACE ANGLE FOUND CRACKED. ANGLE REPLACED AS PER SRM 51-10-01.Apr 23, 2002 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02438189Angle · crackedINSPECTION TYPE:C M/D - NLG PRESSURE DECK UPPER SURFACE ANGLE FOUND CRACKED. ANGLE REPLACED AS PER SRM 51-10-01.Apr 23, 2002 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02438188Floor Support · corrodedINSPECTION TYPE:C M/D BS 150-160 LBL 50 MOST O/B FLOOR SUPPORT CORRODED. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2.Apr 23, 2002 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02438353Pressure Panel · corrodedINSPECTION TYPE:C RT WLG W/W PRESSURE DECK PANEL CORROSION AT RBL 56 - 58 BS 1342 - 1344. CORROSION REMOVED IAW SRM 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1. PRESSURE DECK WEB REPAIRED AS PER SRM 53-10-07 FIG 2.Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02438352Pressure Panel · corrodedINSPECTION TYPE:C RT WLG W/W PRESSURE DECK WEB CORROSION AT BS 1341 - 1343 RBL 54 - 56. CORROSION REMOVED IAW 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1.Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02438351Door Frame · corrodedINSPECTION TYPE:C FWD CARGO DOOR BS 575 BETWEEN NR 1, NR 3 FRAME UPPER MASTER LATCH T/T INTERIOR AREA FOUND CORROSION (COUNT FROM FWD) AS MARKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT NOT WITHIN SRM LIMIT 52-00-02 FIG 1. FWD CARGO DOOR INTApr 22, 2002 · N676UP · Boeing 747123 · Cargo/Baggage DoorsSDR UPS02438295Stiffener · corrodedINSPECTION TYPE:C LWLG - BS 1241 BULKHEAD LBL 87 CENTER TANK TRANSFER VALVE BONDING JUMPER ATTACHMENT VERT STIFFENER CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 57-10-01 LIMITS. LWLG BS 1241 LBL 87 VERTICAL STIFFENER REPLACED AS PApr 22, 2002 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02438349Bulkhead · corrodedINSPECTION TYPE:C RT WLG W/W CANTED BULKHEAD WEB CORRODED AROUND DRAIN HOSE ADAPTOR AT BS 1241 - 1243 RBL 36 - 39. REPAIRED AS PER HAECO RS R-53-48-34796. THE REPAIR IS CONSIDERED TIME-LIMITED TO 24 MONTHS UNTIL AN IMPROVED DRAINAGE MODIFICATION CAN BE INSTApr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02438348Bulkhead · crackedINSPECTION TYPE:C M/D - BS 1241 RBL 35 CANTED PRESSURE BULKHEAD FOUND CRACKED. RT WLG W/W CANTED BULKHEAD WEB REPAIRED AT BS 1241 RBL 16 - RBL 47 AS PER RS R-53-48-34796.Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02438347Pressure Panel · corrodedINSPECTION TYPE:C M/D - BS 1241 RBL 76 CANT PRESSURE DECK FOUND CORRODED. BLEND OUT CORROSION DEPTH 0.015, WIDTH 4", LENGTH 6". THE BONDED DOUBLER REPAIRED AS PER HAECO RS R-53-48-34796. THIS REPAIR IS CONSIDERED TIME-LIMITED TO 24 MONTHS UNTIL AN IMPROVED Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02438343Angle · corrodedINSPECTION TYPE:C RT MLG W/W CANTED BULKHEAD LOWER CAP ANGLE UPPER EDGE CORRODED AT RBL 78 - 83 BS 1241 - 1242. THIS REPAIR IS CONSIDERED TIME - LIMITED FOR 24 MONTHS UNTIL AN IMPROVED DRAIN AGE MODIFICATION CAN BE INSTALLED IAW BOEING SERVICE BULLETIN 747-51Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02438342Pressure Panel · corrodedINSPECTION TYPE:C LT MLG - BS 1241 BULKHEAD OVERRIDE JETTISON PUMP BONDING STRIP ATTACHMENT CORRODED. AS RS R-53-43-34797 IS TIME LIMITED REPAIR FOR 18 MONTHS, WAN 681694 RAISED AS FOLLOW - UP TO CARRY OUT PERMANENT REPAIR AS PER EO B747-5710-16852-A WITHIN 1Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02438341Pressure Panel · corrodedINSPECTION TYPE:C RT MLG W/W OVERRIDE JETTISON PUMP CUTOUT AND BONDING ATTACHMENT CORROSION FOUND AT STA 1241 RBL 90 - 96 WL 140 - 148. AS PER R-53-43-34797 IS THE LIMITED REPAIR FOR 18 MONTHS, WAN 681694 RAISED AS FOLLOW - UP TO CARRY OUT PERMANENT REPAIR ASApr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02438340Frame · crackedINSPECTION TYPE:C RT BS 990 AT STR 38 RING CHORD ONE EACH FASTENER HOLE FOUND TWO CRACKS AS MARKED. FOR DETAIL PLS REFER ATTACH SKETCH. LOWER CHORD SEGMENT REPAIRED PER SB 747-53-2362 FIG 9 AND CHORD LOCAL FABRICATED PER RS 53-43-34792 AREA REPAIRED FOR RT OApr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, FrameSDR UPS02438339Fitting · corrodedINSPECTION TYPE:C HEAVY CORROSION REVEALED AT UPPER AND LOWER FASTENER HOLES OF BATH TUB FITTING AT BS 990 S38R. PLEASE REFER FIG. RT SIDE STA 980 S38R BATHTUB FITTING PERMANENT REPAIR CARRIED OUT AS PER RS R53-23-34791. CONTINUE INSPECTION PLANS ON THE RT Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02438338Spar · crackedINSPECTION TYPE:C RT BS 990 FRONT SPAR WEB ONE EACH FASTENER HOLE COMMON TO BATH TUB FITTING CRACK REVEALED AT FRONT SPAR WEB LAYER FOR DETAIL PLS REFER ATTACHED SKETCH. RT BS 990 FRONT SPAR WEB CRACKED HOLE OVERSIZED TO 0.660" AND FREEZE PLUG INSTALLED AND DApr 22, 2002 · N676UP · Boeing 747123 · Wing, Center BoxSDR UPS02438333Panel · crackedINSPECTION TYPE:C M/D - BS 1241 RT CLOSURE PNL FOUND CRACKED. CLOSURE PANEL REPLACED PER EO B747-5310-2758-E APPENDICES -E- AT RT SIDE ONLY.Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, Plate/SkinSDR UPS02438309Frame · crackedINSPECTION TYPE:C U/D - BS 760 STR 6-8R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04.Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, FrameSDR UPS02438308Bulkhead · corrodedINSPECTION TYPE:C M/D - BS 2141 RBL 76 CANT PRESSURE DECK FOUND CORRODED. BOND SKIN TRIMMED AS PER SRM 51-10-01. REPAIR PARTS FABRICATED AS PER RS R53-48-34796.Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02438307Skin · corrodedINSPECTION TYPE:C M/D - WING CENTER SECTION SURFACE FOUND CORRODED. WING CENTER SECTION CORRODED SKIN REPAIRED AT BS 1220 LBL 97 AS PER RS R57-14-34799.Apr 22, 2002 · N676UP · Boeing 747123 · Wing, Center BoxSDR UPS02438299Frame · crackedINSPECTION TYPE:C U/D - BS 960 S-5R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 54.Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, FrameSDR UPS02438298Frame · crackedINSPECTION TYPE:C U/D - BS 760 S-7L AND S-8L AREA FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 54.Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, FrameSDR UPS02438297Stringer · crackedINSPECTION TYPE:C U/D - BS 990 S-9L STRINGER END SPLICE AREA FOUND CRACKED. STRINGER REPAIRED SRM 53-10-03 FIG 4.Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS02438294Frame · crackedINSPECTION TYPE:C U/D BS 960 S8L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 54.Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, FrameSDR UPS02438163Frame · corrodedINSPECTION TYPE:C, BULK CARGO BS 2120 RT FRAME WEB FOUND CORROSION BETWEEN STR 28R AND STR 29R. BS 2120 S28R S29R FRAME WEB REPAIRED AS PER SRM 53-10-04 FIG 39. BLEND OUT CORROSION DEPTH 0.030', WIDTH 1', LENGTH 1'.Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, FrameSDR UPS02438274Frame · crackedINSPECTION TYPE:C M/D - BS 960 S-5L FRAME FOUND CRACKED. SIDE FRAME REPAIRED AS PER SRM 53-10-04 FIG 54.Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, FrameSDR UPS02438271Door Frame · crackedINSPECTION TYPE:C M/D - R2 DOOR FWD FRAME FOUND CRACKED AT LOWER HINGE CUTOUT AREA. R2 DOOR FWD FRAME LOWER HINGE CUTOUT AREA REPAIRED PER HAECO RS R-52-11-34782.Apr 22, 2002 · N676UP · Boeing 747123 · Passenger/Crew DoorsSDR UPS02438264Door Frame · crackedINSPECTION TYPE:C M/D - R3 DOOR FWD FRAME FOUND CRACKED AT NR 1 STOP FITTING AREA. FRAME REPAIRED AS PER SRM 52-10-02 FIG 8.Apr 22, 2002 · N676UP · Boeing 747123 · Passenger/Crew DoorsSDR UPS02438263Stop Fitting · crackedINSPECTION TYPE:C R1 DOOR FWD LOWER STOP FITTING FOUND CRACKED. R1 DOOR FWD LOWER STOP FITTING REPLACED AS PER SRM 51-10-01 PG 8.Apr 22, 2002 · N676UP · Boeing 747123 · Passenger/Crew DoorsSDR UPS02438253Frame · crackedINSPECTION TYPE:C BS 2240 BETWEEN S49L AND S50L FRAME CRACK. FRAME REPAIRED AS PER SRM 53-10-04 FIG 71.Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, FrameSDR UPS02438246Stringer · corrodedINSPECTION TYPE:C BULK CARGO - BS 2116 - 2120 RT STR 40 STR END FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS. BS 2110 - 2130 STR 40R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS02438245Stringer · crackedINSPECTION TYPE:C BS 2180 S-32R STRINGER END CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 2.Apr 22, 2002 · N676UP · Boeing 747123 · Fuselage Main, Longeron/Stringer
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