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 200200279Skin Panel · corrodedRIGHT WING - CORROSION REPAIR AT FORWARD EDGE OF LOWER FORWARD SKIN PANEL, WS 1390-1498. THE CORROSION WAS IN THE UPPER SURFACE OF THE SUBJECT SKIN, AND IN THE LOWER SURFACE OF THE RT WING FORWARD SPAR LOWER CHORD. THE CORROSION WAS REMOVED BY BLENDING PER BSDR 200200278Skin · damagedREPAIR OF EXISTING REPAIR AT BS 2320, STR 22R. THE EXISTING REPAIR WAS REMOVED FROM THE AIRCRAFT AND DISCARDED, AND THE EXISTING DENT WAS TRIMMED AWAY PER B747 GUIDELINES. THE FUSELAGE SKIN TRIM OUT AND EXISTING FASTENER HOLES COMMON TO THE REPAIR AREA WERE SDR 200200277Skin · damagedFUSELAGE SKIN AT BS 560, STR 37R DAMAGED. A TRIPLER AND DOUBLER INSTALLED PER SRM GUIDELINES.SDR UPS02439735Structure · damagedINSPECTION TYPE: C RT WING LE CAVITY FRONT SPAR LOWER CHORD VERTICAL FLANGE THICKNESS FOUND BLENDED PREVIOUSLY AT OLES 1322, PLS CHK LIMITATION. (20 INCHES O/B WING JACK AREA) RT WING L/E FRONT SPAR LWR CHORD VERTICAL FLANGE AT OLES 1322 IS REPAIRED AS PERSDR UPS02439726Frame · crackedINSPECTION TYPE: C M/D - BS 2231 S25R FRAME CHORD FOUND CRACKED. BS 2231 FRAME CHORD REPAIRED AT STR 24R-26R AS PER HX RS R53-62-34918 (UPS EO B747-5310-17697-A).TO BE CARRY OUT REPEAT INSPECTION IN THE REPAIR AREA AT 3000 CYCLE INTERVALS PER SB 747-53A24SDR UPS02439647Skin · damagedINSPECTION TYPE: C DURING RAP MOD ACCOMPLISH, BS 970-975 STR 40L-41L PREVIOUS REPAIR DOUBLER IS LESS THAN EXISTING SKIN THICKNESS & SHORT EDGE MARGIN FOUND AT CUTOUT AREA. FX SKIN REPAIRED AT BS 970-975 STR 40L-41L AREA AS PER SRM 53-30-03 FIG 1.SDR UPS02439634Attach Angle · corrodedINSPECTION TYPE:C AFT BULK CARGO - BS 2231 S33R FRAME ATTACH ANGLE FOUND COR DAMAGED. COR BLEND OUT 0.63" X 1" X 1" EXCEED SRM LIMIT. ANGLE REPLACED AS PER SRM 51-10-01 P.8.SDR 200200276Floorbeam · damagedBS 340 UPPER DECK FLOOR BEAM - UPPER CHORD - OVERSIZED FASTENER HOLES AT LT FRAME ATTACHMENT. TWO FASTENER HOLES WERE OVERSIZED BEYOND THE LIMITS ALSO THE EDGE MARGIN IN THE FASTENER HOLE COMMON TO THE SUBJECT FLOORBEAM UPPER CHORD AND THE BS 340 FRAME INNER SDR 200200275Floorbeam · damagedBS 360 UPPER DECK FLOORBEAM EXISTING REPAIR STRAP, UPPER FWD FLANGE, LBL 41.7 - 65.2 DAMAGED. A FWD REPAIR ANGLE AND TWO AFT REPAIR ANGLES ALL INSTALLED ON AN UNDERSIDE OF THE BS 360 UPPER DECK FLOORBEAM CHORD.SDR 200200274Skin · corrodedFUSELAGE BILGE SKIN REPAIR, BS 2160-2180, STR 48L TO 48R. THE CORROSION HAS BEEN REMOVED BY TRIMMING THE FUSELAGE SKIN. THE REPAIR IS APPROVED AS A TIME LIMITED REPAIR FOR A MAXIMUM OF 24 MONTHS AFTER 04 SEP 2002, PER ECRA 477-53-067-2.SDR UPS02439636Failsafe · crackedINSPECTION TYPE: C RT BS 800 FRAME AREA FOUND 5 EA FASTENER HOLES CRACKED. REF ATT SKETCH FOR DETAILS. STRAP AND CHORD REPAIRED AS PER RS R53-22-34910 & UPS EO NR B747-5310-17666-A. ** TO BE CONTINUEOUS PERFORMING REPEAT INSPECTION PER SB 747-53A2451 EVERSDR UPS02439635Failsafe · crackedINSPECTION TYPE:C LT BS 800 FRAME S16 AREA, ONE FASTENER HOLE FOUND CRACKED AT STRAP 1/8 INCHES RUNNING FWD AND AFT, CRACK AT ANGLE 0.040 INCH RUNNING FWD REF ATT SKETCH FOR DETAILS. BS 800 FRAME CRACKED AREA REPAIRED PER RS R53-22-34910. ** TO BE CONTINUESDR UPS02439170Light · inoperativeINSPECTION TYPE:N/A FORWARD MOST LEFT SIDE EMERGENCY LIGHT IN COURIER COMPARTMENT IS INOP. REMOVED AND REPLACED LEFT SIDE EMERGENCY LIGHT.SDR UPS02438663Bulkhead · crackedINSPECTION TYPE:SPC NR 2 PYLON REAR ENGINE MOUNT BULKHEAD CRACK FOUND AT AFT WEB DOUBLER APPROX .1875 INCH IN LENGTH. NR 2 PYLON REAR ENGINE MOUNT BULKHEAD REPAIRED AS PER R54-53-34828.SDR UPS02438661Bulkhead · crackedINSPECTION TYPE:SPC NR 1 PYLON REAR ENGINE MOUNT BULKHEAD CRACK FOUND AT AFT WEB DOUBLER APPROX .25 INCH IN LENGTH. NR 1 PYLON REAR ENGINE MOUNT BULKHEAD REPAIRED AS PER HX RS 54-53-34828.SDR UPS02438662Bulkhead · crackedINSPECTION TYPE:SPC CRACK REVEALED AT NR 4 PYLON REAR ENGINE MOUNT BULKHEAD FWD SIDE I/B DOUBLER, THE CRACK INITIATED FROM ONE FASTENER HOLE PROPAGATED UPWARD TO THE EDGE CRACK LENGTH .1875 INCH. NR 4 PYLON REAR MOUNT BULKHEAD REPAIRED AS PER HX RS R-54-53-34SDR 200200265Floorbeam · puncturedDURING B-CHECK A PUNCTURE WAS FOUND IN THE BS 380 FLOORBEAM WEB P/N 65B10929-506 AT APPROXIMATELY LBL 57. THE DAMAGE WAS TRIMMED OUT, HFEC INSPECTION PERFORMED AND DOUBLERS AND FILLERS FABRICATED AND INSTALLED PER ECRA 478-53-137-02.SDR 200200264Floorbeam · crackedDURING B-CHECK, A CRACKED FLOOR PANEL ATTACH HOLE COMMON TO THE BS 380 UPPER DECK FLOORBEAM UPPER CHORD WAS DISCOVERED P/N 65B10929-18 AT RBL 65.0. THE CRACKED UPPER CHORD IS BEING REPAIRED BY INSTALLING 2 STRAPS PER ECRA.SDR 200200245Vane · crackedLEFT HAND NR 4 CASCADE VANE WAS CRACKED AT AFT ATTACH AREA. REPLACED CASCADE VANE IN ACCORDANCE WITH B747 M/M 78-31-07.SDR 200200244Attach Fitting · brokenLEFT HAND INBOARD FORE FLAP, INBOARD DRIVE LINK ATTACH FITTING WAS BROKE COMPLETELY THROUGH. REPLACED ATTACH FITTING IN ACCORDANCE WITH SRM 57-30-02.SDR UPS01436842Fitting · crackedINSPECTION TYPE:A LT INBOARD FORE FLAP CENTER SUPPORT FITTING HAS A CRACK AROUND IT. REPLACED LT INBOARD FORE FLAP PER MM 27-51-02.SDR UPS01436214Battery Pack · dischargedINSPECTION TYPE:N/A 2 EMERGENCY EXIT DOOR SLIDE LIGHTS INOP. REMOVED AND REPLACED CREW DOOR BATTERY PACK IAW B747 MM 33-51-04, OPS CHECKS GOOD.SDR ERKR200100135Splice · corrodedLEFT AND RIGHT BS 1241 REAR SPAR- ANGLE SPLICE. THIS ECRA SPLICES IN A NEW SECTION OF 65B10821-1 ANGLE ON BOTH SIDES UP TO THE INBOARD EDGES OF THE BULKHEAD FITTINGS. REPAIR IS ACCOMPLISHED USING A SPLICE ANGLE AT LBL 80 AND RBL 80. ADDITIONALLY THE TAPERSHSDR ERKR200100134Beam · crackedCRACKED UPPER T-CHORD OF RT WING T/E BEAM AT WING 235.20. THE CRACK WAS FOUND IN THE UPPER T-WING TRAILING EDGE BEAM AT WBL 235.20. THE REPAIR WAS ACCOMPLISHED BY REMOVING AND REPLACING THE DAMAGED AREA OF THE CHORD WITH NEWLY FABRICATED CHORD, REPAIR STRAPSSDR ERKR200100133Shear Tie · crackedCRACKED SHEAR TIE AT LIGHTENING HOLES BETWEEN STA 340-STA 360, WL.199.80. THE CRACK WAS FOUND AT A LIGHTENING HOLE IN SHEAR TIE LOCATED BETWEEN STA 340 AND STA 360, WL 199.80. REMOVED AND REPLACED THE DAMAGED SHEAR TIE PER ECRA 478-53-125-2.SDR EIA2001224Yoke · failedMZJ-EAC - DURING C-CHECK, CHAFING DAMAGE IN THE AREA OF MID FLAP CARRIAGE DUE TO FAILURE OF YOKE ON LEFT INBOARD MID FLAP. REPAIRED PER ECRA 478-57-103-1. (M)SDR UPS01435749Rib · crackedINSPECTION TYPE:C3 RT - CORROSION CRACK IS REVEALED AT ILES 630.72 RIB AS MARKED. RT RIB WAS REPAIRED AS PER SRM 51-40-02 AFTER CORROSION REMOVED AS PER SRM 51-10-01.SDR UPS01435700Door Frame · crackedINSPECTION TYPE:C3 CABIN - R5 DOOR FWD LOWER CORNER FOUND CRACKED. R5 DOOR FWD LOWER CORNER REPAIRED AS PER SRM 52-10-02 FIG 1B.SDR UPS01435701Beam · crackedINSPECTION TYPE:C6 CRACK REVEALED ON THE FWD BOTTOM OF HORIZONTAL BEAM OF DOOR 2L. 2L DOOR FWD BOTTOM OF HORIZONTAL BEAM REPAIRED AS PER SRM 52-10-02 FIG 10.SDR UPS01435697Support · corrodedINSPECTION TYPE:C3 FX - STA 1404 LBL 16 - RBL 16 KEEL BEAM PANEL SUPPORT FIND WITH CORRODED. SUPPORT REPLACED AS PER 51-10-01.SDR UPS01435695Pressure Panel · crackedINSPECTION TYPE:C3 NOSE WHEEL WELL VERTICAL BEAM LT BS 300 FRAME WEB FOUND NR 2 STAND OFF HOLE CRACK (COUNT FROM TOP APPROX. 1/4 INCH IN LENGTH AT 7 O/C POSN AS MARKED. (LOOKING FWD) VERTICAL BEAM WEB REPLACED IAW BOEING SB 747-53A2293, PROCEDURE 3 PART IV PESDR UPS01435691Support · corrodedINSPECTION TYPE:C3 AFT CARGO - STA 1913 BALLMAT SUPPORT SURFACE CORR AT RBL 30, RBL 40 & RBL 60. REPAIR AS PER SRM 51-40-03 FIG 1.SDR UPS01435703Support · corrodedINSPECTION TYPE:C3 FX - STA 1426 LBL 16 - RBL 16 KEEL BEAM PANEL SUPPORT FOUND WITH CORRODED. SUPPORT REPLACED AS PER SRM 51-10-01.SDR UPS01435702Floorbeam · crackedINSPECTION TYPE:C3 M/D - BS 2240 LBL 40-75 FLOORBEAM UPPER SURFACE FOUND CORROSION FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 9.SDR UPS01435699Support · corrodedINSPECTION TYPE:C3 FX - STA 1465 LBL 16 - RBL 16 KEEL BEAM PANEL SUPPORT FOUND WITH CORRODED. ***CPCP*** SUPPORT REPLACED AS PER SRM 51-10-01.SDR UPS01435693Fitting · crackedINSPECTION TYPE:C3 M/D - R3 DOOR FWD CUTOUT NR 6 STOP FITTING CRACKED. NR 6 STOP FITTING REPLACED AS PER SRM 51-10-01. `SDR UPS01435692Support · corrodedINSPECTION TYPE:C3 FX - BODY FAIRING SUPPORT UPPER & LWR SURFACE CORR AT STA 1480 FROM LBL 55 - RBL 40. STA 1480 LBL 55 - RBL 40 BODY FAIRING SUPPORT REPLACED AS PER SRM 51-10-01 P.8.SDR UPS01435677Door Frame · crackedINSPECTION TYPE:C3 M/D - R2 DOOR FWD CUTOUT REVEAL FOUND CRACKED. NR 2 RT DOOR LWR REVEAL AND FRAME INNER CHORD STRAP REPAIRED AS PER SRM 53-10-04 FIG 84.SDR UPS01435674Frame · crackedINSPECTION TYPE:C3 CABIN - FRAME FOUND CRACK AT STA 560 BETWEEN STR 23L TO STR 24L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 11.SDR UPS01435673Support · corrodedINSPECTION TYPE:C3 FX - BODY FAIRING SUPPORT SURFACE CORROSION AT LBL 58 FROM STA 1170-1230. LT STA 1170-1230 LBL 58 BODY FAIRING SUPPORT SURFACE REPLACED AS PER SRM 51-40-04 FIG 1.SDR UPS01435672Support · corrodedINSPECTION TYPE:C3 FX - AFT BODY FAIRING SUPPORT SURFACE CORROSION AT STA 1540 FROM LBL 40 - RBL 60 AS MARKED. SUPPORT REPAIRED AS PER SRM 53-50-04 FIG 2.SDR UPS01435698Skin · corrodedINSPECTION TYPE:C3 FX - EXTERIOR SKIN STA 2160 STR 46R CORR CRACK REVEALED ***CPCP*** FX - EXTERIOR SKIN AT STA 2160 STR-46R REPAIRED AS PER SRM 53-30-03 FIG 1.SDR UPS01435689Beam · crackedINSPECTION TYPE:C3 CRACK REVEALED ON THE FWD BOTTOM OF HORIZONTAL BEAM OF DOOR 4L. 4L DOOR FWD BOTTOM OF HORIZONTAL BEAM REPAIRED AS PER SRM 52-10-02 FIG 10.SDR UPS01435678Floor Support · corrodedINSPECTION TYPE:C3 BULK CARGO COMPT - FLOOR SUPPORT CORROSION REVEALED AT STA 1940, LBL 55 AS MARKED. FLOOR SUPPORT BETWEEN STA 1920 TO STA 1950 LBL 55 REPAIRED AS PER 53-10-07 FIG 20.SDR UPS01435676Stringer · corrodedINSPECTION TYPE:C3 AFT CARGO - BILGE AREA STA 1750 STR 51R SURFACE CORROSION. AFT CARGO - BS 1750-1770 STR 51R REPAIRED AS PER SRM 53-10-03 FIG 8.SDR UPS01435671Frame · crackedINSPECTION TYPE:C3 NR 4 PYLON PYLON AFT TORQUE BULKHEAD O/B VERTICAL CHORD, CRACK FOUND AT 2ND FASTENER HOLE (FROM LOWER) RUNNING O/B APPROX. 0.100 INCH LONG. NR 4 PYLON AFT TORQUE BULKHEAD O/B VERTICAL CHORD CRACKED HOLE O/SIZE FASTENER INSTALLED WITH FREESDR UPS01435641Floor Support · corrodedINSPECTION TYPE:C3 BULK CARGO COMPT - FLOOR PANEL SUPPORT LOWER SURFACE FOUND CORROSION AT STA 1920 LBL0 AS MARKED. FLOOR PANEL SUPPORT REPAIRED AT BULK CARGO COMPTMENT BETWEEN STA 1920 TO 1925 BL 0.SDR UPS01435663Floor Support · crackedINSPECTION TYPE: C3, AFT CARGO BAY- FLOOR PANEL SUPPORT FOUND CRACK AT STA 1976 RBL 30 AS MARKED. FLOOR PANEL SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20.SDR UPS01435668Floor Support · crackedINSPECTION TYPE:C3 M/D - BS 1350-1370 LBL 116 MOST O/B LONGITUDINAL FLR SUPPORT FOUND CRACKED AS MARKED. M/D BS 1350-1370 LBL 116 FLOOR SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 1.SDR UPS01435667Channel · crackedINSPECTION TYPE:C3 CABIN - ''U'' CHANNEL I/B FLANGE FOUND CRACKED AT STA 994-995 LBL 75. U CHANNEL REPLACED AS PER SRM 51-10-01.
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