Boeing 747-121

Service difficulty reports · 3,030

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 = '747121'
  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 EIA2000250Web · crackedFOUND NOSE W/W TUNNEL, RIGHT BS 300 VERTICAL BEAM WEB BETWEEN 1ST AND 2ND CLIP FROM TOP FOUND TWO EACH STANDOFF HOLES CRACKED. RIGHT BS 300 VERTICAL BEAM WEB REPLACED PER SB747-53A-2293. (M)Sep 3, 2000 · N480EV · Boeing 747121 · Fuselage Miscellaneous StructureSDR EIA2000251Clip · crackedFOUND NOSE WHEEL WELL TUNNEL, RIGHT BS 300 VERTICAL BEAM 2ND CLIP FROM TOP CRACKED. RIGHT BS 300 VERTICAL BEAM 2ND CLIP REPLACED PER SB747-53A-2293. (M)Sep 3, 2000 · N480EV · Boeing 747121 · Fuselage Miscellaneous StructureSDR EIA2000252Clip · crackedFOUND NOSE WHEEL WELL TUNNEL, LEFT BS 320 VERTICAL BEAM 2ND CLIP FROM TOP CRACKED. LEFT BS 320 VERTICAL BEAM 2ND CLIP REPLACED PER SB747-53A-2293. (M)Sep 3, 2000 · N480EV · Boeing 747121 · Fuselage Miscellaneous StructureSDR EIA2000253Web · crackedFOUND NOSE WHEEL WELL TUNNEL RIGHT BS 320 VERTICAL BEAM WEB BETWEEN 1ST AND 2ND CLIP FROM TOP CRACKED. RIGHT BS 320 VERTICAL BEAM WEB REPLACED PER SB747-53A-2293. (M)Sep 3, 2000 · N480EV · Boeing 747121 · Fuselage Miscellaneous StructureSDR EIA2000244Stringer · crackedFOUND BS 2200 STRINGER 14R END CRACKED. BS 2200 RIGHT STRINGER 14R REPAIRED PER SRM 53-10-03 FIG 2 AND SRWS 917614. (M)Sep 3, 2000 · N480EV · Boeing 747121 · Fuselage Main, Longeron/StringerSDR EIA2000254Channel · crackedFOUND BS 900 RIGHT OUTBOARD CEILING LEVEL TENSION TIE AFT CHANNEL CRACKED. REPAIRED PER SB747-53-2371. (M)Sep 3, 2000 · N480EV · Boeing 747121 · Fuselage Miscellaneous StructureSDR EIA2000255Channel · crackedFOUND BS 860 LEFT OUTBOARD CEILING PANEL AREA TENSION TIE AFT CHANNEL CRACKED. REPAIRED PER SB747-53-2371 FIG 3. (M)Sep 3, 2000 · N480EV · Boeing 747121 · Fuselage Miscellaneous StructureSDR EIA2000256Channel · crackedFOUND BS 760 LEFT OUTBOARD CEILING PANEL AREA TENSION TIE AFT CHANNEL CRACKED. REPAIRED PER SB747-53-2088 FIG 7. (M)Sep 3, 2000 · N480EV · Boeing 747121 · Fuselage Miscellaneous StructureSDR EIA2000257Channel · crackedFOUND BS 860 RIGHT OUTBOARD CEILING PANEL AREA TENSION TIE AFT CHANNEL CRACKED. REPAIRED PER SB747-53-2371 FIG 3. (M)Sep 3, 2000 · N480EV · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS00434047Angle · crackedINSPECTION TYPE:C, RT WING T/E SPOILER SUPPORT BEAM WEB CRACKED AFT OF 6 FLAP TRANSMISSION. REPAIR ACCOMPLISHED, SPLICE REPAIR USING 15.5 PH CRES ANGLES IAW QUERY NOTE 102/000 FORM 8110 ISSUED.Sep 2, 2000 · N691UP · Boeing 747121 · SpoilersSDR UPS00434119Flange · crackedINSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT OLES 1453. REPAIR CARRIED OUT IAW SRM 57-20-03.Aug 25, 2000 · N691UP · Boeing 747121 · Wing Miscellaneous StructureSDR UPS00433619Indicator · reads lowINSPECTION TYPE:N/A, DURING FLAP EXTENSION O/B FLAPS FAILED TO MOVE. SPLIT T.E. FLAP CHECKLIST ACCOMPLISHED. LT NEEDLE ON O/B FLAP IND IS OFF SCALE LOW. REMOVED AND REPLACED O/B FLAP POSITION INDICATOR AND TESTED PER MM 27-58-00 CHKS OK. P/N ON/OFF: 9801-Aug 23, 2000 · N681UP · Boeing 747121 · Trailing Flap Position Indicating SystemSDR UPS00434110Forging · corrodedINSPECTION TYPE:C, PLEASE REPLACE CORRODED WINDOW FORGINGS AT BS 240 - 260 LT SIDE IAW SRM. WINDOW FORGING REMOVED IAW SRM 51-30-02 NEW FORGING FITTED SRM 51-30-02 & QUERY NOTE N691UP 11/2000.Aug 9, 2000 · N691UP · Boeing 747121 · Fuselage Main, StructureSDR UPS00434039Forging · crackedINSPECTION TYPE:C, REPLACE CRACKED WINDOW FORGING BS 1460 - 1480 RT SIDE. WINDOW FORGING REPLACED IAW SRM 51-30-02.Aug 7, 2000 · N691UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS00434127Beam · crackedINSPECTION TYPE:C, VERTICAL STABILIZER T/E CRACK ON TRAILING EDGE BEAM AT FIN STA 245 RT. REPAIRED TRAILING EDGE BEAM WEB IAW SRM 55-30-06.Aug 4, 2000 · N691UP · Boeing 747121 · Vertical StabilizerSDR UPS00434126Web · crackedINSPECTION TYPE:C, LOWER RUDDER L/E FAIRING, TWO WEBS CRACKED AT FOLLOWING LOCATIONS RT RUD STA 147 AND LT RUD STA 32. WEB AT RT RUD STA 147 REPAIRED IAW SRM 51-40-02 FIG 2 2. NEW WEB FABRICATED IAW EO100921 AND FITTED IAW SRM 51-30-02.Aug 4, 2000 · N691UP · Boeing 747121 · Rudder StructureSDR UPS00434124Intercostal · crackedINSPECTION TYPE:C, CONTROL CABIN INTERCOSTAL IS CRACKED AT BS 360 - 380 BETWEEN STR 1 AND 2 RT. CRACKED INTERCOSTAL REMOVED AND NEW INTERCOSTAL FABRICATED AND FITTED IAW SRM 51-30-02.Aug 2, 2000 · N691UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS00433726Fitting · corrodedINSPECTION TYPE:C, RT HORIZONTAL STABILIZER INTERIOR CORROSION FOUND ON A RIGHT ANGLE FITTING AT STAB STA 243, BETWEEN REAR SPAR AND S1 UPPER SURFACE. PLEASE INVESTIGATE NEW FITTING, FABRICATED IAW E0100940 AND FITTED IAW SRM 51-30-02.Aug 2, 2000 · N691UP · Boeing 747121 · Horizontal Stabilizer StructureSDR UPS00434122Stiffener · crackedINSPECTION TYPE:C, AIR COND CRACK IN RAM AIR DUCT STIFFENER AT BS 960. NEW STIFFENER FABRICATED IAW BAC5300 AND FITTED IAW SRM 51-30-02.Aug 1, 2000 · N691UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS00434099Rib · crackedINSPECTION TYPE:C, RT WING UPPER FLANGE FOUND CRACKED BY NDT INSP ON L/E RIB AT OLES 1411.85. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 28, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434097Flange · crackedINSPECTION TYPE:C, RT WING UPPER FLANGE FOUND CRACKED ON L/E RIB AT OLES 1421.35. REPAIRED RIB IAW SRM 57-20-03 FIG 1.Jul 28, 2000 · N691UP · Boeing 747121 · Wing Miscellaneous StructureSDR UPS00434095Rib · crackedINSPECTION TYPE:C, RT WING UPPER FLANGE ON L/E RIB AT OLES 1525.45 FOUND CRACKED. RIB REPLACED IAW SRM 51-30-02.Jul 28, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434093Rib · crackedINSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT OLES 1534.95. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 28, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434092Rib · wornINSPECTION TYPE:C, TAIL VERTICAL FIN LWR L/E SECTION OF RIB WORN AT CONTACT AREA WITH DORSAL FIN. RIB REPLACED IAW SRM 51-30-02.Jul 28, 2000 · N691UP · Boeing 747121 · Elevator, Spar/RibSDR UPS00434091Frame · crackedINSPECTION TYPE:C, APU COMPT FRAME CRACKED RT SIDE BS 2675 WL 310. FRAME REPAIRED IAW SRM 51-40-03 USING 2024 T3 .040.Jul 28, 2000 · N691UP · Boeing 747121 · Fuselage Main, FrameSDR UPS00434089Spar · corrodedINSPECTION TYPE:C, LT HORZ STAB REAR SPAR UPPER CHORD CORRODED AT STAB BL 380. CHORD REPAIRED IAW QUERY NOTE 56/200.Jul 26, 2000 · N691UP · Boeing 747121 · Horizontal Stabilizer, Spar/RibSDR UPS00434086Rib · crackedINSPECTION TYPE:C, CRACKED RIB UPPER CHORD ON LT HORZ STAB BEHIND R/SPAR AT STAB BL 39 1. CHORD REPAIRED IAW SRM 51-40-03.Jul 26, 2000 · N691UP · Boeing 747121 · Horizontal Stabilizer, Spar/RibSDR UPS00434083Beam · crackedINSPECTION TYPE:C, TAIL VERTICAL STABILIZER T/E BEAM SUPPORTS FOUND CRACKED AT RUD STA 132 LT, RT, 157 LT, 267 LT RT ,282 LT & RT, 307 LT & RT, 332 RT AND 367 RT. REPAIRS TO STAB (VERTICAL) T/E BEAM SUPPORTS REPAIRED IAW SRM 51-40-03 AND Q/NOTE 54/2000 CLOSUJul 26, 2000 · N691UP · Boeing 747121 · Vertical StabilizerSDR UPS00434033Rib · crackedINSPECTION TYPE:C, RT WING L/E CRACKING ON UPPER FLANGE OF L/E RIB AT OLES 1390.75. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 26, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434101Door Frame · crackedINSPECTION TYPE:C, DOOR 4 LT REMOVED FOR REPAIR OF FWD FRAME DAMAGE. NR 4 DOOR FWD FRAME REPAIRED IAW SRM 52-10-02 FIG 13. MATERIAL AIS I301 .050 HFEC INSP ACCOMPLISHED ON CRACK ENDS REPAIR PIECE CAD PLATED.Jul 25, 2000 · N691UP · Boeing 747121 · Fuselage Main, StructureSDR UPS00434035Rib · crackedINSPECTION TYPE:C, RT L/E CRACKING ON UPPER FLANGE ON L/E RIB AT OLES 1493.45. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434031Rib · crackedINSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 1048.25. NEW RIB INSTALLED RIB REPLACED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434029Rib · crackedINSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 705.55. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434026Rib · crackedINSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 974.05. REPAIR CARRIED OUT IAW SRM 57-20-03 FIG 1.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434022Rib · crackedINSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 1014.95. NEW RIB INSTALLED IAW 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434021Rib · crackedINSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 964.55. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434019Rib · crackedINSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 852.45. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434018Rib · crackedINSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 878.55. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434017Rib · crackedINSPECTION TYPE:C, LT WING UPPER FLANGE ON L/E RIB AT ILES 889.5. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434015Rib · crackedINSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIBS AT ILES 928.96. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434014Rib · crackedINSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 928.96. NEW RIB INSTALLLED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434013Rib · crackedINSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 938.45. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434012Rib · crackedINSPECTION TYPE:C, RT WING UPPER FLANGE ON L/E RIB AT ILES 1024.45. CRACKS REPAIRED IAW SRM 57-20-03 FIG 3 USING 2024 T3 X 0.125.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434010Rib · crackedINSPECTION TYPE:C, LT WING UPPER FLANGE OF L/E RIB CRACKED AT ILES 756.95. REPAIR CARRIED OUT IAW SRM 57-20-03 FIG 1. FASTENERS FITTED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434009Rib · crackedINSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 768.45. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434008Rib · crackedINSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 1014.95. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434007Rib · crackedINSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 974.05. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434006Rib · crackedINSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 802.6. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434005Rib · crackedINSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED AT ILES 964.55 L/E RIB CRACKS. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS00434004Rib · crackedINSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 842.96. NEW RIB INSTALLED IAW SRM 51-30-02.Jul 25, 2000 · N691UP · Boeing 747121 · Wing, Rib/Bulkhead
Back to Boeing 747-121