Boeing 747 212B
Service difficulty reports · 2,202
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 = '747212B' 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 = '747212B' 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 UPS05445379Bulkhead · corrodedINSPECTION TYPE:C L/G - RBLG W/W STA 1480 BULKHEAD FWD FACE FOUND SURFACE CORROSION AROUND L/G RETRACT ACTUATOR UPPER MOUNT AREA. BS 1480 BULKHEAD CORRODED. TIME LIMITED REPAIR AT RBL 85 WL 156 AREA AS PER H HX RS R53-43-35364 AND UPS EO B747-5310-22826-A. SDR UPS05445290Frame · corrodedFX FRONT BODY FAIRING SUPPORT UPPER SURFACE FOUND SURFACE CORROSION AT STA 880 RBL 0 TO RBL 1". CORROSION BLEND OUT 0.080" BY 1" BY 1" EXCEED SRM 53-50-01 FIG 5 LIMITS, FRAME WEB REPAIRED AT BS 880 BL 0" TO RBL 1" FWD SIDE AREA AS PER SRM 53-50-04 FIG 1.SDR UPS05445272Fitting · corrodedLT WING UPPER REAR SPAR SIDE OF BODY SPLICE NR 6 FASTENER HOLE FOUND CORROSION AT UPPER SPLICE FITTING APPROX 0.030" IN LENGTH RUNNING FORWARD O/B, CORROSION BLEND OUT 0.030" IN LENGTH. LEFT NR 6 BOLT HOLE BUSHING REPAIRED AS PER EO NR B747-5740-17032.SDR UPS05445271Fitting · crackedBS 1241 REAR SPAR CRACK INDICATION REVEALED AT UPPER SPLICE FITTING LOWER SURFACE AT NR 6 HOLE. CRACK LENGTH 0.060". RT NR 6 BOLT HOLE BUSHING REPAIRED AS PER EO NR B747-5740-17032.SDR UPS05445270Fitting · crackedRT BS 1241 WING UPPER REAR SPAR SIDE-OF-BODY KICK FITTING AREA FOUND HOLE NR 2 CRACKED AT KICK FITTING APPROX 0.060". RH NR 2 BOLT HOLE BUSHING REPAIRED AS PER EO NR B747-5740-17032.SDR UPS05445311Skin · dentedINSPECTION TYPE:C FX LT LOWER FUSELAGE EXTERNAL SKIN SURFACE SUSPECT DENT MARK AT STA 1980 TO STA 2000 STR 43L TO STR 44L. FX BS 1986 TO BS 1998.5 BETWEEN STR 43L TO STR 44L SKIN REPAIRED AS PER SRM 53-30-03 FIG 1 SUBSEQUENT INSPECTIONS ARE NECESSARY FOR CAT SDR EIA2005152Controller · malfunctionedNR 3 ENGINE ON DESCENT FL 350 WOULD NOT RESPOND TO PUSH-UP. RESTART REQUIRED ALL PAREMETERS WERE NORMAL RESTART OK. NR 3 EVC REPLACED AND TRIMMED PER MMS 71-00-00 AND 75-31-01 RESPONCE NORMAL.SDR UPS05445355Stiffener · crackedLT KEEL BEAM VERTICAL WEB SURFACE EXTERNAL ATT STIFFENER FOUND CRACKED AT STA 1460 LBL 9, CRACK LENGTH .625. STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.SDR UPS05445390Bear Strap · corrodedINSPECTION TYPE:C FX LOWER FUSELAGE EXTERNAL SKIN SURFACE FWD LAVATORY SERVICE PAN FWD ATT PLATE FOUND CORRODED AT LT STA 545 STR 46L TO STR 47L. CORROSION BLEND OUT THROUGH WHOLE THICKNESS .5 X 1 INCH. FX BS 540 BETWEEN STR 46L TO STR 47L LAV SVC PAN ATTACHSDR UPS05445208Skin · dentedINSPECTION TYPE:N/A SEVERAL DENTS IN CREW EMERGENCY ESCAPE HATCH OUTER SKIN S/M. DOOR REMOVED FOR REPAIR S/M SHOP. FABRICATED NEW SKIN IAW 52-20-01 OK TO INSTALL INNER AND OUTER SKIN. INSTALLED OUTER SKIN PER SRM 51-36-02. FINISHED INSTALLATION OF INNER SKSDR EIA2005149Light · inoperativeUPPER DECK EXIT DOOR EMERGENCY FLOOD LIGHT INOP. REPLACED UPPER DECK DOOR EMERGENCY EXIT SIGN ASSY, SYSTEM OPS CHECK NORMAL IAW MM 33-51-00.SDR UPS05444898Engine · failedNR 3 ENGINE FAILED. REPLACED NR 3 ENGINE IAW TASK CARD 5000, 5016. OPS CHECK GOOD.SDR EIA2005135Pump · leakingNR 1 HYD SYS SLOWLY LOST HYD QUANTITY AT TO GAGE SHOWED 9 GAL. GAGE SHOWED SLOW LOSS APPROX 2 HRS AFTER T/O. DID LEAK/LOSS PROCEDURES BUT LEAK CONTINUED, SYSTEM DEPRESSURIZED AND ADP OFF REMAINDER OF FLIGHT. REMOVED AND REPLACED NR 1 ENG HYDRAULIC PUMP PER SDR EIA2005133Light · inoperativeR5 AND L5 DOOR EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. RELAMPED R5 AND REMOVED AND REPLACED EMERGENCY LIGHT ASSY ON L5, IAW MM 33-51-07, OPS CK GOOD.SDR EIA2005146Fire Loop · chafedINTERMITTENT FIRE WARNING INDICATION ON APU DURING FLIGHT. PULLED A LOOP CB FOR APU FOR FIRE WARNING SYSTEM WHICH STOPPED INTERMITTENT FIRE WARNING. FOUND WIRING ON APU A LOOP FIRE WARNING CONNECTION CHAFING WITH STRUCTURE. REPAIR PER STANDARD PRACTICE 20-3SDR EIA2005145Circuit Card · malfunctionedINTERMITTENT FIRE WARNING INDICATION ON APU DURING FLIGHT. OCCURS WITH LOOP SELECTOR IN BOTH A OR B. ACCOMPLISHED FIRE TEST ON APU, APU TEST NORMAL. PULLED APU FIRE HANDLE AS PRECAUTIONARY. RERACKED APU FIRE WARNING CARD, OPS CK GOOD.SDR EIA2005143Fire Warning · activatedAPU FIRE DETECTION AND PILOTS FIRE LIGHTS COME ON MOMENTARILY AND INTERMITTENTLY DURING CRUISE. APU FIRE WARNING, OPS CK OK IAW MM 26-11-00.SDR EIA2005131Light · inoperativeUPPER DECK EMERGENCY LIGHT AT LOCATION STA 405 INOP. LIGHT ASSY REPLACED PER MM 33-51-00 OPS CKD OK.SDR EIA2005129Skin · bulgedBULGED BELLY SKIN AT TWO (2) LOCATIONS, STA 2160 BL 0 AND RBL 12. ACCOMPLISHED SKIN REPAIR PER B 747-SRM 53-03-03 AND STRINGER REPAIR PER B 747 SRM 53-10-03.SDR EIA2005128Skin · bulgedSKIN BULGED ON FUSELAGE BELLY STA 2180 BL 0. SKIN REPLACEMENT COMPLIED WITH PER B 747 SRM 53-30-03 IN CONJUNCTION WITH NON-ROUTINE CARD 1095.SDR UPS05444681Battery Pack · inoperativeEMERGENCY BATTERY PACK INOP FOR AFT 2 CEILING LIGHTS IN UPPER DECK. REPLACED EMERGENCY BATTERY PACK M335. OPS CHECK GOOD PER 33-51-00 PG 501.SDR UPS05444693Connector · dirtyNR 4 ENG A- LOOP DISPLAYED INTERMITTENT FAULT LIGHTS AND BELL TEMPERATURE WAS IN RED BANK BUT FLUCTUATED SOMEWHAT. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN PROCEDURE. TEMP STAYED IN HIGH ORANGE TO RED BAND. FOUND LOWER RIGHT A- LOOP CONNECTORS SOAKED WITH SDR EIA2005127Light · inoperativeL5 DOOR AFT EMERGENCY EXIT LIGHT FOUND INOP. REMOVED AND REPLACED LIGHT ASSY IAW MM 33-51-05.SDR EIA2005123Seat Track · brokenM/D BS 1883 RBL 11, SEAT TRACK FLANGE FOUND BROKEN. M/D BS 1870 TO BS 1950 RBL 11, SEAT TRACK REPAIRED PER SRM 53-10-05, FIG 14.SDR EIA2005122Rib · crackedLT WING SURGE TANK WS 1516, RIB LOWER CHORD AT STRINGER 6 AREA FOUND CRACKED AS MARKED. LT WING SURGE TANK, WS 1516 RIB LOWER CHORD REPLACED AT STRINGER 6 AREA PER SRM 57-10-05, FIG 4.SDR EIA2005121Seat Track · corrodedM/D BS 996 RBL 33, SEAT TRACK, RT FLANGE FOUND CORROSION. SEAT TRACK AT BS 990 TO BS 1000, RBL 33, SECTIONAL REPLACED PER SRM 53-10-05, FIG 1A.SDR EIA2005120Seat Track · corrodedM/D BS 1000, LBL 33, SEAT TRACK OUTBOARD FLANGE FOUND CORROSION. M/D BS 990 TO BS 1000, LBL 33, SEAT TRACK SECTIONAL REPLACED PER SRM 53-10-05 FIG 1A.SDR EIA2005119Seat Track · corrodedM/D BS 1535 TO BS 1545, LBL 33, SEAT TRACK CROWN FOUND CORROSION. M/D BS 1480 TO BS 1550, SEAT TRACK SECTIONAL REPLACED PER SRM 53-10-05, FIG 1A.SDR EIA2005118Seat Track · unknownM/D BS 610 TO BS 620 LBL 33, SEAT TRACK RT-05, FIG 1A.SDR EIA2005117Floorbeam · corrodedCORROSION REVEALED ON UPPER DECK FLOORBEAM, UPPER CHORD AT BS 420 RBL 68, PER ATTACH FIG. UPPER DECK BEAM, UPPER CHORD REPAIRED PER SB 747-53A2452.SDR EIA2005116Shear Tie · crackedM/D BS 1780 STRINGER 4R TO 5R, SHEAR TIE FOUND CRACKED. CRACKED SHEAR TIE REPLACED PER SRM 51-10-01.SDR EIA2005115Shear Tie · crackedM/D BS 1800 STRINGER 4R TO 5R SHEAR TIE FOUND CRACKED. CRACKED SHEAR TIE REPLACED PER SRM 51-10-01.SDR EIA2005114Shear Tie · crackedM/D BS 1820 STRINGER 4R TO 5R SHEAR TIE FOUND CRACKED. CRACKED SHEAR TIE REPLACED PER SRM 21-10-01.SDR EIA2005113Shear Tie · crackedM/D BS 1860 STRINGER 4R TO 5R SHEAR TIE FOUND CRACKED. CRACKED SHEAR TIE REPLACED PER SRM 51-10-01.SDR EIA2005112Shear Tie · crackedM/D BS 1920 STRINGER 4R TO 5R, SHEAR TIE FOUND CRACKED. CRACKED SHEAR TIE REPLACED PER SRM 51-10-01SDR EIA2005111Bulkhead · corrodedFX BS 1480 KEEL BEAM BOX BULKHEAD, FWD FACE BETWEEN RBL2 AND LBL2, FOUND CORROSION. REPAIRED PER HAECO REPAIR SCHEME R-53-49-35300.SDR EIA2005110Strap · crackedM/D RT BS 800 FRAME STRAP BETWEEN STRINGER 25R AND 26R FRAME INNER CHORD STRAP FOUND CRACKED. RT BS 800 FRAME STRAP BETWEEN STRINGER 25R AND 26R, DOUBLER REPAIRED PER SRM 51-40-01, FIG 1.SDR EIA2005109Shear Tie · crackedM/D STA 1880 RT STRINGER 4 TO 5, SHEAR TIE FOUND CRACKED. CRACKED SHEAR TIE REPLACED PER SRM 51-10-01, P 9.SDR EIA2005108Shear Tie · crackedM/D BS 1940 RT STRINGER 4 TO 5 SHEAR TIE FOUND CRACKED. CRACKED SHEAR TIE REPLACED PER SRM 51-10-01, P9.SDR EIA2005107Cargo Track · corrodedM/D BS 1680-1700 LBL 11 TIE DOWN TRACK FLANGE FOUND CORROSION AS MARKED. M/D BS 1680-1730 LBL 11 TIE DOWN TRACK REPAIRED PER SRM 53-10-05, FIG 14.SDR EIA2005106Stringer · damagedFX - DURING BS 980 LT SKIN REPAIR, FOUND STRINGER 37L AND SKIN HAD A METALLIC PLUG INSTALLED PREVIOUSLY. REPAIRED STRINGER 37L AT BS 970- BS 983, AND REPAIRED SKIN AT BS 950 TO BS 990, BETWEEN STRINGER 36L AND 39L PER HAECO REPAIR SCHEME R-53-21-35304.SDR EIA2005105Skin · crackedNDT - LT FUSELAGE SKIN UNDER DRAG SPLICE FITTING AT BS980, STRINGER 38L. FOUND ONE EACH FASTENER HOLE CRACKED. SKIN REPAIRED AT SA 950-990, BTN STRINGER 36L AND STRINGER 39L, PER SRM 53-3-03 FIGURE 60, AND HAECO REPAIR SCHEME, R53-21-35304.SDR EIA2005100Stringer · crackedFUSELAGE BS 393 STRINGER 44L ONE EACH FASTENER HOLE FOUND CRACKED RUNNING FOWARD LOWER 1/8 INCH APPROX AND 3/16 INCH AFT. STRINGER PLATE REPAIRED PER SB 747-53-2305.SDR EIA2005006Splice · crackedBS 400 NLG W/W AFT CORNER FOUND CRACKED AT SPLICE PLATE. SPLICE PLATE REPAIRED PER SB 747-53-2305.SDR EIA2005099Floorbeam · crackedBS 600 UPPER DECK FLOOR BEAM UPPER CHORD HORIZONAL FLANGE FASTENER HOLE AT RBL 27 FOUND CRACKED APPROX .0030 INCH IN LENGTH RUNNING AFT. CRACKED FASTENER HOLE FURTHER OVERSIZED TO .31 INCH. FOUND CRACK FREE CONDITION. THE HOLE REPAIRED PER SB53A2452 PT 3 RESDR EIA2005103Power Supply · inoperativeFOUR (4) EXIT DOOR EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLIES AND OPS CHECKED IAW MM 33-51-00.SDR EIA2005102Skin · crackedBS 2230 RT NR 5 DOOR FWD CUTOUT BETWEEN STRINGER 24R AND 25R FOUND CRACKED. BS 2230 RT NR 5 DOOR FWD REVEAL BETWEEN STRINGER 24R AND 25R REPAIRED PER SRM 53-10-04 FIGURE 34.SDR EIA2005101Web · crackedLEFT BS 488 NR 1 MAIN ENTRY DOOR CRACK FOUND AT BS 488 WEB AND DOUBLER. THE WEB AND DOUBLER REPAIRED PER SRM 53-10-04 FIGURE 92.SDR EIA2005098Skin · crackedLEFT BS 1708 AT STRINGER 34L ONE EACH FASTENER HOLE FOUND CRACKED AT 9 O'CLOCK POSITION 2ND LAYER .0625 INCH APPROX IN LENGTH. THE CRACK TRIMMED AND NDT CONFIRMED CRACK FREE CONDITION. THE SKIN REPAIRED PER EIA EO 53-474-1701-03.SDR EIA2005097Skin · crackedLEFT BS 1730 AT STRINGER 34L ONE EACH FASTENER HOLE FOUND CRACKED AT 2ND LAYER 8 O'CLOCK POSITION .0625 INCH APPROX IN LENGTH. THE CRACK TRIMMED OFF AND NDT CONFIRMED CRACK FREE CONDITION. SKIN REPAIRED PER EIA EO 53-747-1701-03.
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