Boeing 747-SR-46
Service difficulty reports · 412
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 = '747SR46' 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 = '747SR46' 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 UPS05444876Stiffener · crackedINSPECTION TYPE: C, SECONDARY INSPECTION FOUND OUT LT NLG WW TUNNER S/W AT BS 280 WL 150 STIFFENER FWD O/B FASTENER HOLE CRACKED. NLG LT WW TUNNER INTERIOR STIFFENER AT BS 280-300 WL 150 REPLACED AS PER SRM 51-10-01 PG 8.SDR UPS05444345Battery · dischargedINSPECTION TYPE:6A EMERGENCY LIGHT AT STA 2280 L/H HAS A BAD BATTERY. LIGHT FLASHES ON A AND THEN OFF WHEN TURNED ON. REPLACED BATTERY PACK. EMERGENCY LIGHT OPERATION CHECKS OKAY I.A.W. B 747 MM 33-51-00 ADJ/TEST.SDR EIA2005041Keelbeam · corrodedKEEL BEAM RIGHT LOWER CHORD CORROSION BS 1335-1345 WL 100 RBL 10. CORROSION REMOVED PER SRM 53-10-01, REPAIR PARTS FABBED AND INSTALLED PER ECRA 478-51-173-1.SDR EIA2005040Keelbeam · corrodedKEEL BEAM BS 1355-1365 LBL 10 WL 100 CORROSION. CORROSION REMOVED PER SRM 53-10-01, REPAIR FABBED AND INSTALLED PER ECRA 478-51-173-1.SDR EIA2005039Keelbeam · corrodedBS 1375-1380 WL 95-100 LBL 10 KEEL BEAM CORROSION. CORROSION REMOVED PER SRM 63-10-01, REPAIR PARTS FABBED AND INSTALLED PER ECRA 478-51-173-1.SDR EIA2005038Stringer · crackedBS 2260 STR 43R INNER CHORD CRACK. DAMAGE REMOVED, REPAIR FABBED AND INSTALLED PER ECRA 478-51-173-1.SDR EIA2005037Frame · crackedBS 1840 STR 11R FRAME CRACKED. DAMAGE REMOVED, FABBED AND INSTALLED REPAIR PER ECRA 478-51-173-1.SDR EIA2005036Keelbeam · corrodedBS 1360 KEEL BEAM LWR ANGLE UPPER SURFACE CORROSION WL 95, LBL 10. CORROSION REMOVED PER SRM 53-10-01, FABBED AND INSTALLED REPAIR PER SRM 51-10-01 AND 51-30-02.SDR EIA2005035Stringer Clip · crackedBS 820 LT TENSION TIE CRACKED STR 10AL - 10L. DAMAGE REMOVED, FABBED AND INSTALLED REPAIR PER ECRA 478-51-173-1.SDR EIA2005034Frame · crackedBS 1780 STR 13R FRAME CRACKED. DAMAGE REMOVED, REPAIR PARTS FABBED AND INSTALLED PER SRM 53-10-04.SDR EIA2005033Frame · crackedBS 880 LT STR 8L - 9L TENSION TIE FRAME CRACKED. DAMAGED AREA REMOVED, REPAIR FABBED AND INSTALLED PER ECRA 478-51-173-1.SDR EIA2005032Stringer Clip · crackedBS 800 STR 11L TENSION TIE CRACK. DAMAGE REMOVED, REPAIR FABBED AND INSTALLED PER ECRA 478-51-173-1.SDR UPS05443640Light · inoperativeCREW STAIRS EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS PER MM 33-51-07.SDR EIA2004149Battery Pack · inoperativeU/D SILL LIGHT ON CREW EXIT DOOR INOP. REPLACED UPPER DECK BATTERY PACK ASSY IAW MM 33-51-04.SDR EIA2004147Bulb · inoperativeAFT EMERGENCY LIGHT BULB AT L1 DOOR MAIN CARGO DECK INOP. RELAMPED AFT EMERGENCY LIGHT BULB AT L1 DOOR MAIN CARGO DECK. GRN CHECKED NORMAL IAW MM 33-51-00.SDR SIMA200629203Floor Support · crackedUPPER DECK, FLOOR SUPPORT UPPER CHORD OPEN HOLES CRACKED AT BS380, 400, 420, 520, 540, 600, 660, AND 720. REPAIR OPEN HOLES PER SB 747-53A2452. REPETITIVE INSPECTION ECRA 477-53-105-1.SDR AWXA200601495Floor Support · crackedUPPER DECK, FLOOR SUPPORT UPPER CHORD OPEN HOLES CRACKED AT BS380, 400, 420, 520, 540, 600, 660, AND 720. REPAIR OPEN HOLES PER SB 747-53A2452. REPETITIVE INSPECTION ECRA 477-53-105-1.SDR EIA2004125Stringer · crackedUPPER DECK STRINGER CRACKED AT BS 746, STR L3. REPAIRED STRINGER PER SRM 53-10-03, FIG 10.SDR EIA2004113Floor Support · crackedUPPER DECK, FLOOR SUPPORT UPPER CHORD OPEN HOLES CRACKED AT BS380, 400, 420, 520, 540, 600, 660, AND 720. REPAIR OPEN HOLES PER SB 747-53A2452. REPETITIVE INSPECTION ECRA 477-53-105-1.SDR EIA2004112Frame · crackedMULTIPLE DEFECTS (CRACKS) ON LT AND RT SIDE BS 2231 FRAME ASSY AT MED NR 5L/R FWD EDGE CUTOUT AREA. TRIM OUT DAMAGED PORTION, SPLICE REPLACEMENT SECTION OF FRAME STRAP AND REVEAL PANEL ON RHS AND5. BOEING MESSAGE: I-OJHBI, I-P3MEM, AND I-P8ZPI. REPETITIVESDR EIA2004111Skin · corrodedFUSELAGE SKIN BULGED AT SB/T STA 2180 TO STA 2200, STR 44R. CORRODED SKIN TRIMMED OUT. REMOVE AND DISCARD EXISTING DOUBLER OVERLAPPING STR 46R LAP JOINT. TRIM OUT CORRODED OVERLAPPING SKIN. INTL REPAIR DOUBLER PER EN AND EA53-0825. BOEING MESSAGE I-PC15E,SDR EIA2004119Skin · corrodedBULGE FROM CORROSION ON SKIN AT AFT LWR CORNER OF AFT CARGO DOOR. TRIM OUT CORROSION PER SRM 51-10-01. HFEC INSPECTED. REINFORCE ENTIRE DAMAGED AREA WITH TWO OUTER DOUBLERS PER EN EA 52-0048. BOEING MESSAGE, 1-P48WC, 1-PBPA2, AND 1-P1QFU. TIME LIMITED REPSDR EIA2004117Skin · crackedRT BLG I/B STRUT DOOR FOUND CORROSION AND CRACK ON EXT FACE OF OUTER DOOR-SKIN AT AFT EDGE. TRIM CORROSION AND CRACK IN 0.040 OUTER SKIN AT BS 1483.7, RBL 55.6, AND INSTALLED REPAIR DOUBLER BONDED TO FILLER. INSTALLED THREE (3) ROWS OF BLIND RIVETS AROUND THSDR EIA2004124Frame · crackedCRACK AT END OF MAIN DECK FRAME AT FASTENER HOLE, BS 340, S-16L. REPAIRED FRAME PER SRM 53-10-04, FIG 85.SDR EIA2004118Skin · corrodedFOUND CORROSION ON UPPER CENTER SKIN SECTION AT STA 1140, RBL 100, MAIN DECK. CORROSION BLENDED FROM SKIN PAD ON UPPER SURFACE OF UPPER SKIN PANEL NR 2 AT S-14, JUST O/B RBL 98.58 FLOORBEAM. INSPECTED AREA AND DETERMINED CORROSION AND CRACK FREE. SHOT PEENESDR EIA2004120Keelbeam · corrodedCORROSION CRACK, KEEL BEAM, RT LWR CHORD IB LEG AT STA 1313. TRIM 5.0 INCHES INBOARD LWR FLANGE OF VERTICAL AND HORIZONTAL LEGS. HFEC INSPECTED, FOUND CRACK AND CORROSION FREE. SHOT PEENED AND REFINISHED PER EN EA 53-0827. BOEING MESSAGE 1-OJ18O, 1-OUNOI, SDR EIA2004110Fairing · corrodedLT WING LEADING EDGE WING ROOT ALUMINUM NOSE CAP (D-FAIRING) AT LALDG LIGHT LWR AREA FOUND CORROSION. CORROSION REMOVED, HFEC INSP TO INSURE CORROSION CRACK FREE. APPLIED FINISH PER BOEING MESSAGE NR I-OYSCJ, I-OW4AE, TEC-XMN-04-01388C. EN EA-57-0428, REPETSDR EIA2004121Spar · crackedCRACK AT NAC STA 210, LOWER SPAR WEB, CENTER AREA, NR 1 PYLON. REPAIR LWR SPAR WEB PER SRM 54-10-03, FIG 2, SPAR WEB FABRICATED IAW SRM 54-10-03, FIG 2.SDR EIA2004116Tie · crackedCRACKS IN TENSION TIE TO FRAME JOINTS AT LOCATION BS 800 TENSION TIE, LEFT AND RT S-11L. BOTH ENDS OF TENSION TIE CHANNELS WERE TRIMMED AND NEW SEGMENTS AND SPLICE PARTS INSTALLED PER EN 53-0824. BOEING MESSAGE NR 1-OUMRW, 1-OOHR4, AND 1-P8ZM7 WITH FAA 8110-SDR EIA2004115Frame · crackedCRACKS IN TENSION TIE TO FRAME JOINTS AT LOCATION BS 840 FRAME, LEFT SIDE S-10L. HOLE IN FRAME OVERSIZED TO REMOVE CRACKS AND FREEZE PLUGS INSTALLED. REPAIR DOUBLER INSTALLED INCORPORATING EXISTING PRODUCTION DOUBLER PER EN 53-084 BOEING MESSAGE NR 1-OUMRW, SDR EIA2004122Structure · corrodedBULGING CORROSION LEFT WING JUST AFT NR 12 K-FLAP, LOWER LEADING EDGE AT FIXED COMPOSITE FAIRING. SUSPECT INT METAL STRAP CORROSION. REMOVED CORROSION PER SRM 51-10-01, REWORK AREA 3 IN LONG BY .5 IN WIDE, BY 0.04 IN DEEP IS OUT OF SRM 57-20-01, FIG 1 LIMIT.SDR EIA2004123Web · crackedCRACK IN STA 40 RT SUPPORT WEB, STA 2220-2240, BULK CARGO DISCHARGE COMPARTMENT. WEB REPLACED PER SRM 51-30-02, AND 51-10-01.SDR EIA2004114Tie · crackedCRACK FOUND IN TENSION TIE TO FRAME JOINTS AT LOCATION B880 FRAME, LT SIDE, S-9L. FRAME HOLE OVERSIZED TO REMOVE CRACKS AND FREEZE PLUGS INSTALLED. REPAIR DOUBLER INSTALLED INCORPORATING EXISTING PRODUCTION DOUBLER PER EN 53-084 BOEING MESSAGE NR 1-OUMRW, 1-SDR EIA2004109Splice · crackedLEFT WING UPPER SIDE OF BODY SPLICE, LT WING AT REAR SPAR OPEN HOLE NR 4 FOUND CRACK. HOLE CONCENTRICALLY REAMED 1.375 IN DIAMETER IN SPLICE FITTING ONLY. OPEN HOLE HFEC INSP PERFORMED. FREEZE PLUG FAB'D AND INSTALLED COMMON TO SPLICE FITTING ONLY PER SRM 5SDR UPS04443073Battery Pack · inoperativeEMERGENCY LIGHT INOPERATIVE, PASSENGER AREA. REPLACED BATTERY PACK, OPS CHECK GOOD.SDR UPS04442923Switch · jammedINSPECTION TYPE:N/A EMERGENCY LIGHTING SWITCH JAMS. INSTALLED NEW EMERGENCY CONTROL MODULE PER AMM 33-51-09 AND EO B747-3350-20899A, OPS CHECKED NORMAL.SDR EIA2004012Light · inoperativeMAIN CARGO DECK EMERGENCY EXIT LIGHT GOES OUT AFTER 10 SECONDS. REPLACED LIGHT ASSY.SDR UPS04442053Intercostal · crackedINSPECTION TYPE: C, BELOW FLOOR INTERCOSTAL WEB CRACKED AT BS 2220 S-37R AS MARKED. BS 2220 S-37R BELOW FLOOR INTERCOSTAL WEB REPLACED AS PER SRM 51-10-01 PG 8.SDR UPS04442045Strap · corrodedINSPECTION TYPE: C, BS 1241 LEFT WING REAR SPAR LOWER SPLICE FOUND CORROSION AT HOLE -A- ALL LAYERS APPROX 12 O/C POSITION AND APPROX 0.030 INCH DEEP. CORROSION REMOVED AND BOLT HOLE FINAL OVERSIZE TO 0.907 INCH PER EO B747-5710-12138-G, HFEC INSPECTED RESULSDR EIA2004011Shield · tornNR 4 ENGINE LOWER I/B PYLON SKIRT FIRE SHEILD WORN THROUGH FROM NAC STA. 180.00 TO NAC STA. 265.94. NR 4 ENG LWR I/B SKIN REPAIRED PER SRM 54-30-03 FIG 35 & 36 PG 111-118.SDR UPS04442048Fitting · crackedINSPECTION TYPE:C LLEFT WING REAR SPAR LOWER KICK FITTING HOLE -C- FOUND CRACKED APPROX 0.040 INCH. LOWER KICK FITTING HOLE -C- OVERSIZED TO 1.000 INCH TO REMOVE CRACK. HFEC INSPECTED CONFIRM CRACK FREE. FASTENER HOLE BUSHING REPAIRED PER RS R-57-12-35122. SDR UPS04442047Fitting · crackedINSPECTION TYPE:C RIGHT WING REAR SPAR LOWER KICK FITTING HOLE -C- FOUND CRACKED APPROX 0.040 INCH. KICK FITTING HOLE -C- OVERSIZED TO 0.937 INCH TO REMOVE CRACK. HFEC INSPECTED CONFIRM CRACK FREE FASTENER HOLE BUSHING REPAIRED AND BOLT BACB30US14K45X INSTALSDR UPS04442046Strap · damagedINSPECTION TYPE: C, REF EO B747-5310-1093M LEFT BS 1241 FWD HOLE FOUND A BUSHING IN BULKHEAD FORGING. LEFT BS 1241 FWD HOLE FORGING OLD BUSHING REMOVED. HFEC INSPECTED, RESULT NO CRACK FOUND. BUSHING FABRICATED AND INSTALLED PER RS R53-43-35119. BOLT BACBSDR UPS04442044Skin · damagedINSPECTION TYPE: C, REF EO - B747-5310-1093M LT BS 1241 AFT HOLE FOUND A BUSHING IN SKIN. LEFT BS 1241 AFT HOLE SKIN OLD BUSHING REMOVED. HFEC INSPECTED RESULT, NO CRACK FOUND. BUSHING FABRICATED AND INSTALLED PER RS R53-43-35119. BOLT BACB30US12K40 INSTASDR UPS04442043Bushing · crackedINSPECTION TYPE: C, REF EO B747-5310-1093-M RT SIDE BS 1241 FWD HOLE HAS BEEN OVERSIZED TO 1 INCH AND HAS A BUSHING INSTALLED. OLD BUSHING REMOVED AND HFEC INSPECTED RESULT CONFIRM CRACK FREE ON ALL LAYERS. BUSHING REPAIRED ON LONGERON AND ON SKIN. SPLICE SDR UPS04442020Stringer Clip · crackedINSPECTION TYPE: C, AFT OF BULK CARGO COMPT - RT STA 2240 STRINGER 46 TIE CLIP FOUND CRACK. DEFECTIVE AREA STRINGER TIE CLIP REPLACED AS PER SRM 51-10-01 PAGE 8.SDR UPS04442039Frame · crackedINSPECTION TYPE:C AFT OF BULK CARGO COMPT- RT STA 2240 FRAME CRACKED BETWEEN STR R38 & STR R40 AREA. AFT OF BULK CARGO COMPT - RT STA 2240 FRAME STR 35R TO STR 40R REPLACED AS PER RS R53-62-35127 AND ENGINEERING FILE 747-53-20173.SDR UPS04442042Fitting · crackedINSPECTION TYPE: C, CRACK FOUND AT NR 1 DIA BRACE UNDERWING ATTACHED FITTING'S MOST AFT HOLE OF THE O/B ROW, CRACK LENGTH .125 INCH LONG APPROX AT THE UPPER SURFACE. CRACKED HOLE REPAIRED PER RS R57-04-35118 AND EO B747-5740-20132-A.SDR UPS04442021Shear Tie · crackedINSPECTION TYPE: C, AFT CARGO COMPT - STA 1840 IN BETWEEN STR 51L AND STR 51R SHEAR TIE FOUND CRACKED. DEFECTIVE AREA SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3.SDR UPS04442002Fitting · crackedINSPECTION TYPE: C, BS 1241 LT WING REAR SPAR UPPER SPLICE FITTING FOUND CRACKS AT HOLE NR 5. BS 1241 LT WING REAR UPPER SPLICE FITTING HOLE NR 5 REAMED TO REMOVE CRACKS. HFEC INSPECTED RESULT CRACK FREE. FINAL HOLE DIAMETER IS 1.000 INCH AND BUSHING INSTA
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