Boeing 747-128
Service difficulty reports · 339
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 = '747128' 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 = '747128' 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 EIA990282Skin · corrodedTLV - SWELLING ON EXTERNAL FUSELAGE WITH SHEARED RIVET BETWEEN STATION 660-700 BETWEEN STRINGER 41-43R. REPAIR DOUBLER INSTALLED IAW EO MF-MAN-B47-53-00-88832 REF, BOEING FAX MESSAGE M-7200-99-06866 DATED 8/5/99 AND SRM 53-30-03 FIG 1. (M)SDR EIA990281Skin · corrodedTLV - SWELLING ON RIGHT WING UPPER SKIN, UPPER SURFACE ABOVE FRONT SPAR AT WS 1360. PERFORMED REPAIR PER EO MF-MAN-B47-57-88838 NEW REF BOEING SERVICE ENGINEERING MESSAGE M-7200-99-07260 DATED AUGUST 16, 1999. INSTALLED DOUBLER. (M)SDR EIA990280Chord · crackedTLV - FOUND CRACK IN THE RADIUS OF THE UPPER CHORD OF LEFT WING STATION 669.5 INTERIOR FUEL TANK. CRACKED UPPER CHORD REMOVED. INSTALLED NEW UPPER CHORD IAW SB 57-2273-R2. (M)SDR EIA990279Frame · crackedTLV - FOUND CRACK IN FRAME INNER CHORD AT STATION 1265 LEFT BELOW FLOOR LINE. WEB REPAIR PERFORMED AND INSTRUCTION DETAILED OF THIS WORK ARE NOTED IN EO MF-MAN-B47-53-88847 NEW REF BOEING SERVICE ENG MESSAGE M-7200-99-02111 8/12/99 AND M7200-99-07861 8/30/99.SDR EIA990278Frame · crackedTLV - FOUND CRACK IN FRAME WEB AT STATION 1265 RIGHT JUST ABOVE FLOOR LINE. WEB REPLACEMENT PERFORMED AND INSTRUCTION OF THIS WORK NOTED IN JOB CARD NR 366-53-035M REF IAI SB 366-53-035. DRAWING R05366-53-15-15196-006. (M)SDR EIA990277Spar Web · crackedTLV - DURING THE ACCOMPLISHMENT OF THE TERMINATING OF THE SB 747-57A2266 REV 6 CRACK FOUND AT FASTENER HOLES IN THE FRONT SPAR WEB STATION 660, COMMON TO THE LOWER CHORD. PERFORMED REPAIR IAW IAI EO MF MAN B47-57-88849 AND AS APPROVED BY FAA REPAIR 8110-3 ATTSDR EIA990285Support · corrodedTLV - SWELLING AND OPEN HOLES ON FAIRING SUPPORT AT LOWER FUSELAGE STATION 880 BETWEEN AREA RBL 15 TO RBL 27. SWOLLEN AREA TRIMMED OUT AND DEBURRED. REINFORCED AREA WITH 2 SUPPORTS(7075 T60 .080 THK) PER SRM 53-50-04, FIG 1. ALODINED AND EP PRIMER PROTECTEDSDR EIA990284Fitting · corrodedTLV - FOUND CORROSION ON THE OUTER CHORD SPLICE FITTING AT STATION 1480 LEFT SIDE. REPAIR STRAP INSTALLED IAW IAI EO MF-MAN-B47-53-88841 REV A DATED 9-9-99. (M)SDR EIA990283Bulkhead · crackedTLV - FOUND CRACKS ON PRESSURE BULKHEAD STATION 140 FORWARD SIDE, WL 305 APPROX L AND R BL 33. CRACKED AREA TRIMMED OUT. REINFORCED AREA WITH DOUBLERS AND FILLER 2024-T3 .050 PLUS .032 THK PER SRM 53-10-04 FIG 8D ALODINED AND EP PRIMER PROTECTED PER SRM 51-1SDR EIA980351Wheel · departedDURING LANDING ROLL-OUT, LEFT BODY GEAR ANTI-SKID LIGHT CAME ON, AFTER FURTHER INVESTIGATION THE NR 5 TIRE ASSEMBLY WAS FOUND MISSING, AND THOUGHT TO HAVE DEPARTED AIRCRAFT UPON LANDING. (M)SDR P5CA9800398Angle · corrodedFUSELAGE UPPER BODY FAIRING NR 294FR LOWER SUPPORT ANGLE BETWEEN BS 1370-1400 FOUND CORROSION AROUND FLOAT NUTS. CORROSION REMOVED PER SRM 51-01-01, BLEND OUT NOT WITHIN SRM LIMITS 53-10-01. REPAIRED PER SRM 51-40-04 FIG 3 AND TREATED PER SRM 51-10-02.SDR P5CA9800394Bonding Jumper · corrosionLT WING REAR SPAR WEB HEAVY CORROSION AT ATTACHMENT OF BONDING JUMPER OF NR 2 TANK I/B JETTISON PUMP AREA. REMOVED CORROSION PER SRM 51-10-01 BLEND OUT NOT WITHIN LIMIT 57-10-01. REPAIRED PER BOEING PAO-HKG-98-0073RE-INSTALL FILLERS DOUBLERS AND TREAT AREA.SDR P5CA9800393Skin · corrosionRT WING LOWER SKIN NR 4 MAIN TANK AFT BOOST PUMP HOUSING CUTOUT FOUND HEAVY CORROSION. CORROSION REMOVED BLEND OUT NOT WITHIN SRM LIMIT 57-30-03. REPAIRED PER PAO HKG 98-0068TE AND 0070RE AND SRM 57-30-03 FIG 3.SDR P5CA9800391Panel · delaminationLT HORIZ STAB LOWER T/E FIXED PANEL 334GBL FOUND DELAMINATION. HOT BOND REPAIRED PER SRM 51-40-06 PARA 3.SDR P5CA9800390Skin · corrosionLT BODY GEAR W/W STAT 1350-1380 LOWER FIXED PANEL FOUND CORROSION AT SKIN AND ANGLES. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT 53-10-01.SDR P5CA9800389Support · corrosionLT WING GEAR BEAM FWD SIDE WING FAIRING SUPPORT AFT FACE FOUND CORROSION AT STA 1346 WBL 148. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02 BLENDED OUT WITHIN SRM LIMITS PER 53-10-01.SDR P5CA9800388Door · corrosionLT BODY GEAR STRUT DOOR INNER SKIN FOUND SURFACE CORROSION. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT 52-00-02.SDR P5CA9800387Keel Beam · corrosionLEVEL 1 CORROSION AT LT BODY GEAR WHEEL WELL KEEL BEAM UPPER SURFACE. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMITS 53-30-01.SDR P5CA9800386Splice · corrosionLEVEL 1 CORROSION FOUND AT LT BODY GEAR O/B SPLICE CHORD AT STA 1438. CORROSION REMOVED AND TREATED PER SRM 51-01-01, 51-10-02. BLENDED OUT WITHIN SRM LIMIT 53-10-01.SDR P5CA9800383Web · corrosionLEVEL 1 CORROSION LT WING GEAR W/W STA 1341-1349 UPPER BEAM WEB UPPER SURFACE. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51-10-02 BLENDED OUT WITHIN SRM LIMITS 53-30-01.SDR P5CA9800381Skin · corrosionRT WING GEAR W/W CEILING SKIN AT STA 1320 O/B FOUND CORROSION. REMOVED AND TREATED AS PER SRM 51-10-01, 51-10-02. BLENDED OUT WITHIN SRM LIMIT 53-30-01.SDR P5CA9800426Cowl · delaminationNR 1 ENG NOSE COWL AT THE 5 O'CLOCK POSITION DELAMINATION. NR 1 ENG NOSE COWL ACCOUSTIC PANEL REPAIRED AS PER SRM 54-30-03 FIG 7 AND SRM 54-30-03 FIG 29A.SDR P5CA9800425Fitting · corrosionLEVEL 1 CORROSION FOUND FUSELAGE RT OVERWING LONGERON SPLICE FITTING AT BS 1350, TAPER FILLER. TAPER FILLER REPLACED PER SRM 51-10-01.SDR P5CA9800424Fairing · spongyLT WING I/B T/E FLAP INBD NR 4 CANOE FAIRING SEVEAL AREAS SPONGY DISBONDING AND PUNCHED HOLE FOUND. FIBERGLASS REPAIR PER SRM 51-40-14.SDR P5CA9800423Skin · corrosionLEVEL 1 CORROSION AT BS 880-900 ST 38L. CORROSION REMOVED AND TREATED PER SRM 51-01-01, 51-10-02. BLEND OUT NOT WITHIN LIMITS PER SRM 53-110-01. STRINGER REPAIRED PER SRM 53-10-03 FIG 1.SDR P5CA9800422Support · crackedNR 4 ENG NOSE COWL ANTI-ICE DUCT SUPPORT CRACKED AT STA 180. WELDING CARRIED OUT PER BAC 5975.SDR P5CA9800421Skin · corrosionLEVEL 1 CORROSION FOUND AT RT STA 942 STR 44R. CORROSION REMOVED AND TREATES PER SRM 51-10-01, 51-10-02. BLEND OUT NOT WITHIN SRM LIMIT 53-10-01. REPAIRED PER SRM 53-10-03 FIG 1.SDR P5CA9800420Cowl · delaminatedNR 3 ENGINE INLET COWL LT SIDE PANEL AFT DELAMINATED. REPAIRED PER SRM 51-40-06.SDR P5CA9800419Stabilizer · crackedRT HORIZONTAL STABILIZER SLOT SEAL CRACKED AT FWD LOWER AREA. FIBERGLASS REPAIR CARRIED OUT PER SRM 51-40-15.SDR P5CA9800418Static Wick · corrosionUPPER RUDDER STATIC DISCHARGER 2ND AND 3RD FROM TOP FOUND WITH CORROSION ON ATTACH STRIP. STATIC CHARGE BASE 2ND AND 3RD REPLACED PER SRM 51-01-01.SDR P5CA9800417Spar · corrosionLEVEL 1 CORROSION, FOUND INSIDE HORIZONTAL STAB REAR SPAR UPPER CHORD AND SKIN AREA AT RBL 43.5. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLEND OUT PER SRM LIMIT 55-10-01.SDR P5CA9800416Skin · corrosionRT WING NR 3 MAIN FUEL TANK JETTISON PUMP CUTOUT AREA OF REAR SPAR BONDING ATTACH POINT CORROSION. CORROSION REMOVED AND TREATED PER SRM 51-01-01, 51-10-02. BLEND OUT WITHIN SRM LIMIT 57-10-01.SDR P5CA9800415Angle · corrosionFUSELAGE ACCESS DOOR PANEL NR 192ER MID HINGE LOWER HALF ATTACH ANGLE FOUND CORROSION. ATTACH ANGLE REPLACED AS PER MM 20-50-01.SDR P5CA9800414Angle · corrosionFUSELAGE ACCESS DOOR 192M MID AND AFT HINGE LOWER HALF ATTACH ANGLE FOUND CORROSION. ANGLE REPLACED PER MM 20-50-01.SDR P5CA9800412Cable Cover · crackedMAIN DECK LT STA 1250 SIDEWALL UPPER CONTROL CABLE PULLEY METAL COVER FOUND MOUNTING BRACKET CRACK AND DEFORMED. MOUNTING BRACKET REPLACED AS PER SRM 51-10-01 AND SPEED BRAKE CABLE RIGGING CHECKED PER MM 27-62-02.SDR P5CA9800410Skin · damagedFUSELAGE SKIN DEEP LIGHTNING STRIKE MARK REVEALED AT STA 500 STR 36L. SKIN REPAIRED PER SRM 53-30-03 FIG 1.SDR P5CA9800407Angle · crackedAPU BATTERY COMPARTMENT BS 2598 STR 22-STR 23, LT SIDE FITTING FRAME CHORD ATTACH ANGLE FOUND CRACKED. ANGLE REPLACED PER SRM 51-10-01.SDR P5CA9800406Chord · crackedFUSELAGE BS 2598 B/H ATTACH CHORD FOUND CRACKED AT RT STR 11R - STR 12R RIVET HOLES. BULKHEAD CHORD REPAIRED PER SRM 51-40-04.SDR P5CA9800404Skin · corrodedLEVEL 1 CORROSION, FOUND BS 1736 STR 46R-49R FUSELAGE SKIN. CORROSION REMOVED PER SRM 51-10-01 AND TREATED PER SRM 51-10-02. BLEND OUT WITHIN SRM LIMIT 53-30-01.SDR P5CA9800402Stiffener · corrodedLEVEL 1 CORROSION, FOUND FUSELAGE BS 1050 RBL 10 KEEL BEAM O/B FACE ATTACH VERTICAL STIFFENER. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLEND OUT WITHIN SRM LIMITS 53-10-01.SDR P5CA9800400Stringer · corrosionLEVEL 1 CORROSION, FOUND AFT CARGO COMPARTMENT BS 1670-1682 ST 44R. STRINGER REPAIRED IAW RS R-53-11-33645.SDR P5CA9800399Support · corrosionFUSELAGE BODY FAIRING SUPPORT FOUND SLIGHT CORROSION AT BS 1540 LBL 60 - RBL 40. CORROSION REMOVED PER SRM 51-01-01. BLEND OUT NOT WITHING SRM LIMITS 53-10-01 FIG 1, BODY FAIRING SUPPORT REPAIRED PER SRM 53-50-01 AND TREATED PER SRM 51-10-02.SDR P5CA9800397Stringer · corrodedLEVEL 1 CORROSION FOUND AT RT STA 884 STR 44R. CORRSOION REMOVED PER SRM 51-10-01 BLEND OUT NOT WITHIN SRM LIMIT 53-10-03. STRINGER REPAIRED PER SRM 53-10-03 FIG 1 AND TREATED IAW SRM 51-10-02.SDR P5CA9800396Splice · crackedBS 1350 R/H/S OVERWING LONGERON SPLICE FITTING FOUND CRACKED. LONGERON SPLICE FITTING REPLACED IAW SRM 51-01-01.SDR P5CA9800385Skin · corrosionRT WING W/W FWD RT CENTER TANK JETTISON PUMP BONDING JUMPER ATTACH POINT FOUND SKIN CORROSION. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51-10-02 BLENDED OUT PER SRM 57-10-01.SDR P5CA9800380Beam · corrosionLEVEL 1 CORROSION FOUND AT RT WING W/W O/B UPPER LONGITUDINAL BEAM WEB UPPER SURFACE AT STA 1260 WL 180. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51-10-02. BLENDED OUT WITHIN SRM LIMIT 53-30-01.SDR P5CA9800379Skin · delaminationRT WING O/B MID FLAP I/B TOP ACCESS PANEL NR 687LT FOUND LOWER MID AREA SKIN CORROSION AND DELAMINATED. HOT BOND REPAIRS PER SRM 51-40-06 FIG 17.SDR P5CA9800378Frame · crackedUPPER DECK FRAME 680 STR 7AL CUTOUT AREA FOUND CRACKED. DENT SMOOTHED OUT AND TREATED PER SRM 51-10-01 AND 51-10-02.SDR P5CA9800374Bulkhead · crackedFUSELAGE BS140 B/H FWD FACE FOUND CRACKED AT RBL 38 2 PLACES. WEB REPAIRED AS PER SRM 53-10-04 FIG 89.SDR P5CA9800368Door · dentedDOOR 315AL AFT AREA AT RIB FOUND DENTED 12 INCHES LONG. DOOR 315 AL DRESSED PER SRM 51-10-01.
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