Boeing 747-121

Service difficulty reports · 3,030

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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 = '747121'
  ORDER BY difficulty_date DESC"

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SDR UPS03440605Frame · crackedINSPECTION TYPE: C, BS 540 LT STR 24L FRAME FOUND CRACKED. FRAME REPAIRED AS PER RS R53-22-35011 REFER NRC FF76313 FOR DETAIL. AND ENGR FILE NBR 747-53-20135.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, FrameSDR UPS03440604Skin · crackedINSPECTION TYPE: C, AFT CARGO DOOR CUTOUT FWD UPPER CORNER FOUND BEAR STRAP CRACK APPROX 3/16 INCHES LONG FROM EDGE. AFT CARGO DOOR CUTOUT FWD CUTOUT UPPER CORNER REPAIRED AS PER SRM 53-30-03 FIG 62 AND REFER NRC 6407 FOR WORK DETAIL. CAT B REPAIR REQUIREApr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS03440596Rib · corrodedINSPECTION TYPE: C, RT WING - NR 20 VC FLAP O/B I/B ROTARY ACTUAOTR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 4 , 5 ( VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND EO B747-5740-18687-AApr 13, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440590Rib · corrodedINSPECTION TYPE: C, RT WING - NR 19 VC FLAP O/B I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 6 ( VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO B747-5740-18687-A.Apr 13, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440584Forging · corrodedINSPECTION TYPE: C, BS 620 - 640 RT WINDOW FORGING FOUND CORROSION AT CUTOUT SKIN AFT AREA. CORROSION BLEND OUT (0.028 X 1 X 1 INCHES). WINDOW FORGING REINSTALLED AS PER SRM 51-30-02.Apr 13, 2003 · N681UP · Boeing 747121 · Flight Compartment WindowsSDR UPS03440575Seat Track · corrodedINSPECTION TYPE: C, SEAT TRACK FOUND CORROSION. CORROSION BLEND OUT ( 0.050 X 5/8 X 2 INCHES). M/D SEAT TRACK REPAIRED AT BS 770-850 LBL 98 AS PER SRM 53-10-05 FIG 1A.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS03440572Frame · crackedINSPECTION TYPE: C, BS 960, BET S7-8R FRAME FOUND CRACK. FRAME REPAIRED AS PER SRM 53-10-04.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, FrameSDR UPS03440571Frame · crackedBS 540 LT STR 25L FRAME FOUND CRACKED. FRAME REPAIRED AS PER HX RS R53-22-35011 & UPS RA 747-53-20135 REF NRC FF76313 FOR DETAIL.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, FrameSDR UPS03440566Longeron · crackedINSPECTION TYPE: C, BS 1002-1004- S2R, STR END FOUND CRACK. BS 1002 - 1004 S2R STRINGER REPAIRED AS PER HX RS R53-21-35017 & UPS RA 747-53-20138.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR UPS03440558Frame · crackedINSPECTION TYPE: C, M/D - BS 580 LT STRINGER 24L FRAME FOUND CRACKED. FRAME REPAIRED AT BS 580 BETWEEN S23L TO S25L AS PER SRM 53-10-04 FIG.35.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, FrameSDR UPS03440554Longeron · crackedM/D - BS 1235 S8L STRINGER END CRACKED. BS 1235 S8L STRINGER REPAIRED AS PER HX RS R53-21-35017 & UPS RA 747-53-20138.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR UPS03440551Stringer · crackedINSPECTION TYPE: C, BS 1000 - 1020, S6L STRINGER CRACKED. BS 1000 S-6L STRINGER REPAIRED AS PER HX RS R53-21-35017 AND ENGINEERING FILE NUMBER ; 747-53-20138.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR UPS03440541Floorbeam · corrodedINSPECTION TYPE: C, FLOORBEAM UPPER STRUCTURE CORROSION. FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 3. CORROSION BLEND OUT 0.060 X 2 X 2 INCHES. EXCEED SRM LIMIT.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS03440538Frame · crackedINSPECTION TYPE: C, BS 540 LT BET STRINGER 22L AND 23L FRAME INNER CHORD FOUND CRACKED. FRAME REPAIRED AS PER HX RS R53-22-35011 AND ENGINEERING FILE NUMBER 747-53-20135.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, FrameSDR UPS03440535Seat Track · corrodedINSPECTION TYPE: C, SEAT TRACK FOUND CORROSION AT BS 480 - 485 RBL 65. SEAT TRACK REPAIRED AT U/D BS 480 - 530 RBL 65 AS PER SRM 53-10-05 FIG 1A. CORROSION BLEND OUT 0.045 X 1 X 8 INCHES. EXCEED SRM LIMIT.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS03440534Seat Track · corrodedINSPECTION TYPE: C, BS 820 - 860 LBL 11 SEAT TRACK RT LIP FOUND CORRODED. BS 810 - 890 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14. CORROSION BLEND OUT 0.050 X 1 X 10 INCHES. EXCEED SRM LIMIT.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS03440533Stringer · crackedINSPECTION TYPE: C, BS 1394 S11L STRINGER CRACKED. BS 1385 - 1410 STR 11L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 5.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR UPS03440532Frame · crackedINSPECTION TYPE: C, BS 960 FRAME CRACKED AT STR 9L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 54.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, FrameSDR UPS03440531Frame · crackedINSPECTION TYPE: C, BS 960 FRAME CRACKED BTN S11-12L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 4.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, FrameSDR UPS03440530Frame · crackedINSPECTION TYPE: C, BS 560 LT STR 24L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, FrameSDR UPS03440529Frame · crackedINSPECTION TYPE: C, BS 1640 S-13L FRAME CRACKED. M/D FRAME REPAIRED AT BS 1640 BTN STR 12L AND STR 14L AS PER SRM 51-40-03 FIG 2.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, FrameSDR UPS03440499Clip · corrodedBS 1040 STR 4L TIE CLIP CORROSION. BS 1040 STR 4L TIE CLIP REINSTALL AS PER SRM 51-30-02. CORROSION BLEND OUT 0.040 X 1 X 1 INCHES. EXCEED SRM LIMIT.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS03440498Floorbeam · corrodedINSPECTION TYPE:N/A M/D - BS 760 LBL 40 FLOORBEAM UPPER SURFACE FOUND CORRODED. FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 3. CORROSION BLEND OUT 0.060 X 2 X 2 INCHES, EXCEED SRM LIMIT.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS03440497Stringer · crackedBS 1474 S-12L STRINGER END CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR UPS03440492Structure · corrodedM/D - HAT SECTION FWD FLANGE CORROSION. CORRODED HAT SECTION REPLACED AS PER SRM 51-10-01 PAGE 8. CORROSION BLEND OUT 0.030 X 1 X 1 INCHES. EXCEED SRM LIMIT.Apr 13, 2003 · N681UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS03440624Shear Tie · crackedINSPECTION TYPE: C M/D - BS 1500 RH STR 12R TO 13R, SHEAR TIE BRACKET FOUND CRACKED. SHEAR TIE REPLACED AS PER SRM 51-10-01 PAGE 8.Apr 12, 2003 · N681UP · Boeing 747121 · Fuselage Main, StructureSDR UPS03440618Rib · corrodedINSPECTION TYPE: C LHW, NR 9 VC FLAP O/B I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 3 ( VIEW FROM I/B ). RIB MOUNT BOLT HOLE BORE EXCEED LIMIT AFTER CORR BLEND OUT. SUPPORT RIB REPLACED AS PER SRM 51-10-01 PAGE 8Apr 12, 2003 · N681UP · Boeing 747121 · Leading Edge DevicesSDR UPS03440609Frame · crackedINSPECTION TYPE: C, BS 2060 BET STR 25-26L, FRAME WEB FOUND CRACK. FRAME WEB REPAIRED AT BS 2060 BTN STR 25L AND STR 26L AS PER SRM 53-10-04 FIG 39.Apr 12, 2003 · N681UP · Boeing 747121 · Fuselage Main, FrameSDR UPS03440600Rib · corrodedINSPECTION TYPE: C, RT WING - NR 19 VC FLAP I/B O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 1 TO 8. (VIEW FROM I/B). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER HX RS 57-41-35014 AND UPS EO 747-5740-1Apr 12, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440599Rib · corrodedINSPECTION TYPE: C, RT WING - NR 23 VC FLAP I/B O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 1 TO 8. ( VIEW FROM I/B ) BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND EO B747-5740-18687-AApr 12, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440598Rib · corrodedINSPECTION TYPE: C, LT WING - NR 10 VC FLAP O/B I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 3,4,5 & 6. (VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER HX RS 57-41-35014 AND UPS EO B747-5Apr 12, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440595Rib · corrodedINSPECTION TYPE: C, LT WING - NR 9 VC FLAP O/B O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 2,3 & 6. (VIEW FROM I/B). BOLT HOLES CORROSION REVEALED REMOVED AND INTERIM REPAIRED AS PER HX RS 57-41-35014 AND UPS EO BApr 12, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440593Rib · corrodedINSPECTION TYPE: C, LT WING - NR 9 VC FLAP I/B O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 1,2,3,6,7 & 8 (VIEW FROM I/B). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER HX RS 57-41-35014 AND UPS EO B747-Apr 12, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440592Rib · corrodedINSPECTION TYPE:C LT WING - NR 8 VC FLAP I/B I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 1,2,6 & 8. (VIEW FROM I/B). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER HX RS 57-41-35014 & UPS EO B747-5740-186Apr 12, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440591Rib · corrodedINSPECTION TYPE: C, LT WING - NR 8 VC FLAP I/B O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 2,3,4,6,7 & 8 (VIEW FROM I/B). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER HX RS 57-41-35014 AND UPS EO B747-Apr 12, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440589Rib · corrodedINSPECTION TYPE: C, LT WING - NR 7 VC FLAP O/B O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLE BORE AREA FOUND CORROSION AT HOLE NR 4 ( VIEW FROM I/B). BOLTS HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER HX RS 57-41-35014 AND UPS EO B747-5740-18687-Apr 12, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440587Rib · corrodedINSPECTION TYPE: C LT WING, NR 7 VC FLAP O/B I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 6 & 7 ( VIEW FROM I/B). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER HX RS 57-47-35014 AND UPS EO B747-5740-1868Apr 12, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440585Frame · crackedINSPECTION TYPE: C, BS 540 BET S24-25R FRAME FOUND CRACK. M/D BS 540 STR 24R - STR 26R FRAME REPAIRED AS PER SRM 51-40-03 FIG 1.Apr 12, 2003 · N681UP · Boeing 747121 · Fuselage Main, FrameSDR UPS03440582Rib · corrodedINSPECTION TYPE: C, LT WING - NR 6 VC FLAP I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 2 & 3 ( VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO B747-5740-18687-A.Apr 12, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440581Rib · corrodedINSPECTION TYPE: C, LT WING, NR 5 VC FLAP O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 5 AND 6 ( VIEW FROM I/B ). BOLT HOLE CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO B747-5740-18687-AApr 12, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440580Rib · corrodedLT WING - NR 4 VC FLAP I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 1, 3, 4, 6 & 8. ( VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO B747-5740-18687-A.Apr 12, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440579Rib · corrodedINSPECTION TYPE: C, LT WING - NR 4 VC FLAP O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 1, 2, 4, 5, 7 & 8 ( VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO B747-5Apr 12, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440578Rib · corrodedINSPECTION TYPE: C, LT WING - NR 3 VC FLAP O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 2 & 3 ( VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO B747-5740-18687-A.Apr 12, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440577Rib · corrodedINSPECTION TYPE: C, LT WING - NR 2 VC FLAP O/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 1, 2, 3, 4, 5 AND 6 ( VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO 747-Apr 12, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440576Rib · corrodedINSPECTION TYPE: C, LT WING, NR 2 VC FLAP I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NO.1, 2, 3 & 4 ( VIEW FROM I/B ). BOLT HOLES CORROSION REMOVED AND INTERIM REPAIRED AS PER RS 57-41-35014 AND UPS EO B747-5740-18Apr 12, 2003 · N681UP · Boeing 747121 · Trailing Edge FlapsSDR UPS03440573Stringer Clip · corrodedINSPECTION TYPE: C, BS 540 LT STRINGER 15L, 16L & 17L TIE CLIP FOUND CORRODED. CORROSION BLEND OUT ( 0.009 X 1 X 3 INCHES) AT M/D BS 540 LT STR 15L TO 17L EXCEEDS LIMITATION. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG.8.Apr 12, 2003 · N681UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS03440567Frame · crackedINSPECTION TYPE: C, BS 620 LT STRINGER 24L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG.35.Apr 12, 2003 · N681UP · Boeing 747121 · Fuselage Main, FrameSDR UPS03440564Frame · crackedINSPECTION TYPE: C, BS 760, BET STR 14 - 15R FRAME FOUND CRACKED. FRAME REPAIRED AS PER RS R-53-22-35013 AND ENGINEERING FILE NUMBER 747-53-20132.Apr 12, 2003 · N681UP · Boeing 747121 · Fuselage Main, FrameSDR UPS03440563Frame · crackedINSPECTION TYPE: C, BS 740 BET S24-25R FRAME FOUND CRACK. BS 740 STR 24R - STR 26R FRAME REPAIRED AS PER SRM 53-10-04 FIG.35Apr 12, 2003 · N681UP · Boeing 747121 · Fuselage Main, FrameSDR UPS03440562Support Bracket · corrodedINSPECTION TYPE: C, KEELBEAM PANEL SUPPORT BRACKET FOUND SURFACE CORROSION AT STA 1095 LBL 9. CORROSION BLEND OUT (0.040 X 1 X 1 INCHES) SUPPORT BRACKET REPLACED AS PER SRM 51-10-01 P.8Apr 12, 2003 · N681UP · Boeing 747121 · Fuselage Miscellaneous Structure
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