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.
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
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 UPS00432872Panel · corrodedINSPECTION TYPE:C, MAIN DECK STRESS PANEL CORRODED AT BS 1170 - 1250. NEW STRESS PANEL FITTED.SDR UPS00432868Skin · corrodedINSPECTION TYPE:C, CORROSION ON CENTER WING SKIN UPPER AT BS 1188 RBL 78. SKIN CORROSION CLEANED UP WITHIN LIMITS. NEW SECTION OF CHORD FABRICATED AND FITTED PER SRM 51-10-00.SDR UPS00432864Frame · corrodedINSPECTION TYPE: C, CORROSION ON UPPER SURFACE OF CENTER WING AT BS 1100 RBL 106. NEW SECTION OF CHORD AND REPAIR ANGLES FABRICATED AND FITTED PER Q/NOTE 6/00.SDR UPS00432862Skin · crackedINSPECTION TYPE:C, RIGHT WING CRACKS AND BULGES AT THE FOLLOWING LOCATIONS; WS 528, WS 550, WS 1084, WS 1158, WS 726, WS 1050, WS 905, WS 1110, WS 355, WS 323, WS 311, OLES 1411. CRACKS REPAIRED PER SRM. CORROSION CLEANED OUT OF LIMITS REPAIR ACCOMPLISHED PSDR UPS00432855Frame · corrodedINSPECTION TYPE:C, UPPER SURFACE OF CENTER WING CORRODED AT BS 1120 RBL 78. NEW SECTION OF CHORD AND REPAIR ANGLES FITTED PER Q/NOTE 7/00.SDR UPS00432850Skin · corrodedINSPECTION TYPE:C, CORROSION ON UPPER SURFACE OF CENTER WING SKIN AT BS 1050 LBL 88. CORROSION CLEANED UP OUT OF LIMITS ON SKIN AND FLOORBEAM CHORD. REPAIR ACCOMPLISHED PER Q/NOTE 5/00.SDR UPS00432846Skin · corrodedINSPECTION TYPE:C, CORROSION ON UPPER SURFACE OF CENTER WING SKIN AT BS 1100 RBL 106. REF Q/NOTE 6/00 NEW SECTION OF CHORD FABRICATED AND FITTED.SDR UPS00432857Forging · corrodedINSPECTION TYPE:C, CORROSION ON WINDOW FORGING AT BS 2160 - 2180 RT. REPAIR ACCOMPLISHED PER Q/NOTE 12/00.SDR UPS00432856Forging · corrodedINSPECTION TYPE:C, CORROSION ON WINDOW FORGING BETWEEN STA 2060 AND 2080. REPAIR ACCOMPLISHED PER Q/NOTE 11/00.SDR UPS00432849Forging · corrodedINSPECTION TYPE:C, CORROSION AT FWD EDGE OF WINDOW FORGING BETWEEN STA 2020 AND STA 2040 RHS. CORROSION CLEANED UP. FOUND OUT OF LIMITS. REPAIR ACCOMPLISHED PER Q/NOTE 10/00.SDR UPS00432386Oil Cap · missingINSPECTION TYPE:N/A, ON CLIMBOUT NR 4 ENGINE OIL PRESSURE BEGAN TO FLUCTUATE BETWEEN 35 AND 45 PSI. ENGINE OIL PRESSURE 4 LIGHT ILLUMINATED TO CONFIRM, AT 0715Z , NR 4 ENGINE SHUT DOWN WHEN OIL PRESS BELOW RED ARE CONTINUOUSLY AND OIL PRESS LIGHT ON STEADY, WSDR UPS00432330Light · inoperativeINSPECTION TYPE:N/A, AFT EMERGENCY LIGHT L1854 AT DOOR L1 INOP. RELAMPED AFT LIGHT, OPS CHECKS GOOD.SDR UPS00432062Acm · leakingOIL FUMES IN FLIGHT DECK, ON TAXI, NR 2 AIR CONDITIONING PACK PRODUCED BURNING ODOR NR 1 ACM LEAKING OIL. DEFERRED NR 1 ACM INOPERATIVE PER MEL.SDR EIA2000014Skin · damagedKSEA - DURING GROUND HANDLING IN SEA, AIRCRAFT EMPANNAGE WAS STRUCK JUST FORWARD OF BS 2598 BUTT JOINT AND STRINGER 46L LAP SPLICE, CAUSING APPROX 2 INCH BY 2 INCH PUNCTURE RUNNING ALONG AND ACROSS SKIN SEAM. STRINGER 46L ALSO SUSTAINED A 1 INCH CRACK RUNNINGSDR EIA2000006Blade · damagedNFFN - DURING POST-FLIGHT WALK AROUND INSPECTION, FOUND NR 1 ENGINE WITH NUMEROUS DAMAGED FAN BLADES. FOUND BLADES 1, 25, 27, 31, 33, 11, 34, 13, 42, 22 DAMAGED OUT OF LIMITS. REPLACED A TOTAL OF 18 FAN BLADES PER WORKCARD F7208. RII ACCOMPLISHED. (M)SDR 20000330SH017Blade · bentDURING WALKAROUND INSPECTION, SEVEN N1 FAN BLADES WERE FOUND BENT BEYOND LIMITS ON NR 1 ENGINE. AIRCRAFT WAS GROUNDED NAN. FAN BLADES WERE REPLACED AND TEST RUN CARRIED OUT BY EVERGREEN. (X)SDR UPS00431251Light · inoperativeLEFT FWD ENTRY DOOR FWD EMERGENCY LT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CK GOOD.SDR UPS99431229Skin · crackedINSPECTION TYPE:N/A, LEFT O/B TRAILING EDGE FLAP WHEEL END HAD 10 INCH CRACK. REMOVED AND REPLACED AFT O/B TRAILING EDGE FLAP PER 747 MM 27-51-06, OPS CHECK GOOD.SDR UPS99431162Torque Tube · brokenNR 4 L/E PANEL RIGHT DROOPED AND SPLIT FROM INBD TO OUTBOARD SEGMENT. REMOVED AND REPLACED NR 4 L/E TORQUE TUBE IAW MM 27-81-05. FUNCTIONAL TEST OF L/E DEVIC ES PERFORMED. OPS CHECK NORMAL.SDR UPS99431068Smoke Detector · inopINTERMITTENT ZONE 5 MAIN CARGO DECK FIRE LIGHT ILLUMINATED DURING CLIMB-OUT OF PHL. DEFERRED PER MEL 26-11. REMOVED AND REPLACED B SMOKE DETECTOR AND A8 SMOKE DETECTOR CARD. OP'S CHECK GOOD PER MM 26-10-00. POSITIONS 14 TO 15A VOID. REFERENCE LOG PAGE 148SDR UPS99431001Connector · contaminatedAPPROX 2 HRS INTO FLIGHT, NR 4 START VALVE LIGHT CAME ON THE WENT OUT CAME ON AGAIN, THEN SHUT DOWN NR 4 ENGINE PER AOM. LIGHT WENT OUT. MX FOUND CONNECTORS AT START VALVE OIL SOAKED AND SHORTED. CLEANED CONNECTORS. SYSTEM OPS CHECK NORMAL. THIS CLEARS M1SDR UPS99430728Sign · inopINSPECTION TYPE:N/A, L1 DOOR EMERGENCY EXIT SIGN INOP. REPLACED EMERGENCY EXIT SIGN, OPS CHECK GOOD.SDR UPS99430630Marker Beacon · inopINSPECTION TYPE:N/A, MARKER BEACON INOP.SDR UPS99430528Safety Valve · failedRIGHT BODY GEAR DOOR OPENED DURING DESCENT, 3000 FT, 220KTS. BOTH PRIMARY AND ALTERNATE SHOWED DOOR OPENED. THE DOOR DID CLOSE AFTER LANDING GEAR WAS EXTENDED. FOUND BODY RT BODY GEAR DOOR SAFETY VALVE BYPASSING TOG 36550. REMOVED AND REPLACED BODY GEAR DOSDR EIA990190Engine · shut downVHHH - THE NR 1 ENGINE SHUT DOWN ON CLIMB-OUT. ENGINE WAS RESTARTED AND RUN AT PARTIAL POWER UNTIL EGT REACHED 750. ENGINE WAS SHUT DOWN AT THAT POINT FOR REMAINEDER OF FLIGHT. (M)SDR UPS99430163Heat Duct · dirtyINSPECTION TYPE:N/A, AFT LWR CARGO COMPARTMENT FIRE WARNING ACCOMPLISHED LWR CARGO COMP SMOKE DET TEST, CKD OK. THOROUGHLY INSPECTED LOWER AFT CARGO COMP, NO EVIDENCE OF FIRE FOUND. WHEN INSPECTING CGO COMPT HEAT DUCT, FOUND PLASTIC TRASH STICKING TO THE DUCSDR UPS99430164Skin · corrodedINSPECTION TYPE:N/A, FUSELAGE SKIN LT SIDE OF LAV DUMP HAS CORROSION AND POPPED HI-LOK RIVET HEADS. REMOVED CORROSION AND ACCOMPLISHED EO B747 5330 11468 A.SDR UPS99430085Motor · badLT NR 2 L/E FLAP WOULD NOT RETRACT VIA, THE ALTERNATE METHOD. REPLACED LT NR 2 L/E FLAP ALT DRIVE ELECTRIC MOTOR PER MM 27-81-03. OPS CKS OK.SDR UPS99430008Skin · dentINSPECTION TYPE:IN, DENT 3 FOOT FWD OF AFT CARGO DOOR. REMOVED DAMAGE IAW SRM 53-30-03. INSTALLED DOUBLER IAW SRM 53-30-03, PAINTED TO MATCH A/C COLOR SCHEME.SDR UPS99429804Module · inoperativeINSPECTION TYPE:N/A, EMERGENCY LIGHTS UNARMED ANNUNCIATOR ILLUMINATED WHEN SWITCH PLACED TO ARMED POSITION. REPLACED EMERGENCY LIGHT CONTROL PANEL PER M/M 33-51-09, OPS CKS OK.SDR EIA990115Module · brokenSYD - NR 2 HYD QTY 1 GALLON, ACCOMPLISHED ABNORMAL PROCEDURE HYD SYSTEM LEAK/LOSS JETTISON 40K FUEL, LANDING WT 604.9. FOUND BROKEN CHECK VALVE, HOUSING NR 2 HYD PRESS MODULE SERVICE MODULE INSTALLED PER RMM 29-51-23 AND LEAK CHECKED OK. NR 2 HYD RES SERVICED SDR TWRA9912Hatch Assy · looseON TAKEOFF COCKPIT ESCAPE HATCH ASSY CAME OUT OF CLOSE AND LOCKED POSITION UNABLE TO RECLOSE IN FLIGHT. INSPECTED DOOR, NO DAMAGE FOUND. (M)SDR EIA990170Frame · crackedHKG - DURING C-CHECK, THE BS 340 FRAME WEB ON BOTH LEFT AND RIGHT STRINGER 24A WAS FOUND CRACKED. REPAIRED PER HAECO REPAIR SCHEME NR R-53-12-34025. (M)SDR EIA990167Splice · crackedDURING C-CHECK, THE FRAME SPLICE WEB AT BS 1265 LBL 120 WAS FOUND CRACKED. REPAIRED FRAME SPLICE WEB. (M)SDR EIA990166Frame · crackedDURING C-CHECK, THE RIGHT FRAME, INBOARD CHORD ATTACH WEB WAS FOUND CRACKED AT BS 1265. REPLACED WITH NEW. (M)SDR EIA990165Frame · crackedHKG - DURING C-CHECK, THE M/D NR 3 DOOR FORWARD FRAME CHORD AT BS 1265, RBL 120 WAS FOUND CRACKED. REPAIRED NR 3 DOOR FORWARD FRAME CHORD. (M)SDR EIA990164Stringer · crackedHKG - DURING C-CHECK, THE M/D S17R AT BS 1485 WAS FOUND CRACKED. REPAIRED S17R. (M)SDR EIA990163Stringer · crackedHKG - DURING C-CHECK, THE M/D BS 1478 STRINGER 6L, STRINGER END WAS FOUND CRACKED. REPAIRED CRACKED AREA. (M)SDR EIA990155Stringer · crackedDURING C-CHECK ON M/D AT BS 1485, STRINGER 15R WAS FOUND CRACKED. INSTALLED NEW STRINGER. (M)SDR EIA990071Splice · crackedHKG - DURING C-CHECK, MAIN DECK BS 1000 STRINGER 7R ATTACH SPLICE FOUND CRACKED, NRC 6958. REPLACED SPLICE FITTING IAW SRM 51-10-01. (M)SDR EIA990157Stringer · crackedDURING C-CHECK ON M/D AT BS 1959, STRINGER 3R END WAS FOUND CRACKED. INSTALLED NEW STRINGER. (M)SDR EIA990156Stringer · crackedDURING C-CHECK ON M/D AT STATION 1959 AT STRINGER 2L, END CRACKED. INSTALLED NEW STRINGER. (M)SDR EIA990154Stringer · crackedDURING C-CHECK ON M/D AT BS 1959 STRINGER 4R, STRINGER END WAS FOUND CRACKED. INSTALLED NEW STRINGER. (M)SDR EIA990153Stringer · crackedDURING C-CHECK ON M/D AT BS 1959 S3L, STRINGER END WAS FOUND CRACKED. INSTALLED NEW STRINGER. (M)SDR EIAA990160Outlet · crackedDURING C-CHECK AT STATION 570, EQUIPMENT COOLING OUTLET, 3 FASTENER HOLED WERE FOUND CRACKED. REPAIRED, REFERENCE THE FOLLOWING DOCUMENTS. 1) NRC 7192, 2) CWS 123457, 3) COMP WORK PROCESS CARD Z52E013 4) BOEING TELEX EVR-HKG-99-0023 RE 2/9/99, 1024 TE 2/18/9SDR EIA990169Frame · crackedDURING C-CHECK, THE S25L FRAME WAS FOUND CRACKED AT STATION 380. REPLACED WITH NEW. (M)SDR EIA990168Bulkhead · crackedDURING C-CHECK, THE LEFT BS 1480 BULKHEAD AND STRINGER INTERFACE WERE FOUND CRACKED AT STRINGER 34. REPAIRED BULKHEAD AND STRINGER INTERFACE. (M)SDR EIAA990075Stringer · crackedHKG - DURING C-CHECK, MAIN DECK BS 1478 STRINGER 6L, BS 1485 STRINGER 15R AND 17R, STRINGER ENDS FOUND CRACKED. NRC 7235, 7230 AND 7231 RESPECTIVELY. REPAIRED IAW RS R-53-41-34003, 8110-3 AND ECRA. (M)SDR EIAA990028Frame · crackedHKG - DURING C-CHECK, MAIN DECK AT BS 340 FRAME FOUND CRACKED AT STRINGER 24A LEFT SIDE, NRC 6388. REPAIRED IAW RS R-53-12-34024, 8110-3 AND ECRA. (M)SDR EIAA990027Frame · crackedHKG - DURING C-CHECK, UPPER DECK, BS 340 FRAME UPPER CHORD FOUND CRACKED AT STRINGER 0, NRC 6306. REPAIRED IAW SRM 51-40-03. (M)
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