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 EIA2007088Support Beam · corrodedRT WING INBOARD LEADING EDGE SUPPORT BEAM FOUND WITH EXFOLIATION CORROSION. REMOVED SUPPORT BEAM HFEC INSPECTION CARRIED OUT ON CUT OUT AREA. NIL CRACKS NOTED. REPAIR CARRIED OUT PER N482EV-07-0004/SRM 51-40-04.SDR EIA2007089Skin · debondedFOUND FUSELAGE SKIN FWD OF STA 2460 BETWEEN 17L AND 18L DISBONDED APPROX 2"X". REPAIR CARRIED OUT PER N482EV-07-0006(SRM53-30-04 FIG 3)APPROVED PER BOEING MESSAGE 1-310403476-4.SDR KCSA071136Bulkhead · crackedNR 4 PYLON NAC STA 221.9 BULKHEAD UPPER CHORD CRACKED IN RADIUS.SDR EIA2007080Stringer · corrodedFOUND STRINGER 47L BETWEEN BS 740 TO BS 780 CORRODED. DAMAGED SECTION OF STRINGER CUT AND REMOVED. SPLICE SECTION FABRICATED PER SRM 53-10-03 REPAIR PARTS INSTALLATION CARRIED OUT PER B747 SRM 51-30-02 & 53-10-03 FIG 1.SDR EIA2007078Stringer · corrodedFOUND STRINGER CORRODED AT CEC CUTOUT AREA BS 760-780 STR 47L. DAMAGED SECTION OF STRINGER CUT AND REMOVED. FABRICATED PER SAMPLE. REPAIR SECTION FABRICATED PER SRM 53-10-03 FIG 1. REPAIR PARTS INSTALLATION CARRIED OUT PER B747 SRM 51-30-02, SRM 53-10-03 FSDR EIA2007092Stringer · damagedFOUND STRINGER 24A BODY STATION 140-190 WITH OVERSIZE HOLES. REMOVED STRINGER AND FABRICATED AND INSTALLED PER B747 SRM 53-10-03.SDR EIA2007084Stringer · corrodedFOUND STRINGER CORRODED AT CENTER ELECTRONIC COMPARTMENT CUTOUT AREA BS760-780 STRINGER 47L. DAMAGED SECTION OF STRINGER CUT AND REMOVED. REPAIR SPLICE SECTION FABRICATED PER SRM 53-10-03 FIG 1. REPAIR PARTS INSTALLED PER SRM 51-30-02 & 53-10-03 FIG 1.SDR EIA2007083Skin · corrodedEVIDENCE OF CORROSION FOUND AT STA 810, WL 91 BETWEEN S45R AND S46R. CORROSION REMOVED AS PER SRM 51-10-01 FOUND OUT OF LIMITS PER SRM 53-30-01. CARRIED OUT REPAIRS PER N482EV-07-003(BOEING 1-307245973)SDR EIA2007086Stringer · corrodedSTRINGER FOUND CORRODED AT STA 800 STRINGER 45L. DAMAGED SECTION OF STRINGER CUT AND REMOVED FABRICATED SPLICE SECTION PER SRM 53-10-03 REPAIR PARTS INSTALLED PER SRM 51-30-02/SRM 53-10-03 FIG 1.SDR EIA2007079Light · inoperativeFOUND DOOR 5R CEILING EMERGENCY LIGHT INOPERATIVE. DOOR 5R CEILING EMERGENCY ASSY AND BATTERY ASSY REPLACED AND CHECKED SATISFACTORY PER B747 MM 33-51-00.SDR EIA20070073Frame · damagedNOSE GEAR WELL STA 340, LEFT WL 150 FOUND BASE AND HOLES DAMAGED 1/2" BY 1/2" BEYOND SRM 53-10-01 PAGE 3 FIG 1 LIMIT. CHORD FABRICATED BY WORKSHOP INSTALLED PER BOEING 747 SRM 51-30-02.SDR EIA2007063Unknown · odorSTRONG ELECTRICAL SMELL NOTED ON SHORT FINAL NO SMOKE NOTED ALL CB CHECKED CLOSED ELECTRICAL SYSTEM VOLTS AND FREQ LOADS NORMAL. ALL SYSTEMS TROUBLESHOT NO DEFECTS NOTED NOW OR ON NEXT FLIGHT.SDR EIA2007087Keelbeam · crackedWEB CRACKED NEAR RIVET HOLE AT STA 1002 KEEL BEAM LT SIDE SECOND ROW OF RIVETS. KEEL BEAM WEB REPAIRED PER SRM 53-10-09 FIG 4.SDR EIA2007091Shear Tie · out of limitsFOUND FRAME SHEAR TIE AT BODY STATION 200-220 BETWEEN STRINGER 35L & 34L WITH TOO LARGE A GAP TO NEW SKIN REPLACEMENT. FABRICATED SHEAR TIE PER B747 SRM 53-10-04 INSTALLED PER SRM 51-30-02.SDR EIA2007093Stringer · damagedFOUND STRINGER 28AL BETWEEN BODY STATION 180-200 WITH OVERSIZED HOLES. REMOVED STRINGER 28AL FROM BODY STATION 180-200. FABRICATED PER B747 SRM 53-10-03 FIG 3.SDR EIA2007090Shear Tie · crackedFOUND FRAME SHEAR TIE AT BODY STATION 220 BETWEEN STRINGER 30L AND 29L CRACKED. SHEAR TIE REMOVED AND FABRICATED PER SRM 53-10-04 INSTALLED PER SRM 51-30-02.SDR EIA2007085Shear Tie · crackedFOUND FRAME SHEAR TIE AT BS 180 BETWEEN STRINGER 34L AND 35L CRACKED. SHEAR TIE REMOVED AND FABRICATED PER SRM 53-10-04 AND INSTALLED PER SRM 51-30-02.SDR EIA2007077Seat Track · damagedSTA 543 SEAT TRACK DAMAGED AT RBL 11. SEAT TRACK REMOVED AND SENT TO WORKSHOP FOR CROWN AND FLANGE TRIMMING. PRIMER APPLIED. SEAT TRACK INSTALLED AS PER B747 SRM 51-30-02, SRM 53-10-05 FIG 4.SDR EIA2007082Seat Track · corrodedSEAT TRACK FOUND CORRODED AT LBL 11 STA 470. SEAT TRACK REMOVED AS PER SRM 51-30-01. SEAT TRACK TRIMMED AND PRIMER APPLIED PER SOPM 20-41-01. SEAT TRACK INSTALLED PER SRM 53-10-05 FIGURE 4.SDR EIA2007076Seat Track · corrodedSEAT TRACK FOUND CORRODED AT LBL11 STA 470. SEAT TRACK REMOVED AS PER B747 SRM 51-30-02. SEAT TRACK TRIMMED AND PRIMER APPLIED AS PER B747 SOPM 20-41-02. SEAT TRACK INSTALLED PER B747 SRM 53-10-05 FIG 4.SDR EIA2007075Attach Fitting · corrodedNUMBER 4 FLAP TRACK FWD FITTING MATING SURFACE OF BEARING FOUND WITH PITTING CORROSION. BEARING REMOVED AS PER SB 747-57-2325 FIG 30. FITTING HOLE FOUND PITTED AND BORING ACCOMPLISHED PER SB 747-57-2325 STEP 7. CARRIED OUT FPI NIL CRACKS FOUND. CHAMFER CARSDR EIA2007081Spar · corrodedCORROSION FOUND AT TOP CHORD ASSY AT LT WING IN FRONT OF SPOILER NR 5 & NR 6. BEAM ASSY UPPER "T" CHORD REMOVED FROM WBL 285-WBL345. FABRICATED AS PER SRM 51-40-04 FIG 3. REPAIR CARRIED OUT PER B747 SRM 51-40-04 FIG 3.SDR EIA2007094Shear Tie · misinstalledFOUND FRAME SHEAR TIE AT BODY STATION 240 BETWEEN STRINGER 34A AND 36 WITH TOO BIG A GAP AFTER SKIN REPLACEMENT. SHEAR TIE REMOVED AND FABRICATED PER B747 SRM 53-10-04, INSTALLED PER SRM 51-30-02.SDR EIA2007052Stringer · damagedBS 460 STRINGER 14R EXISTING DOUBLER REMOVED FOR OPEN HOLE HFEC OF REPAIR. REMOVED AND REPLACED DOUBLER AT BS 460 STRINGER 14R PER ECRA 485-53-185-2.SDR WRNA200700015Skin · gougedDURING C-CHECK, 2 GOUGES IN SKIN WERE FOUND OUT OF LIMITS AT FUSELAGE STA 560 BETWEEN STR 37R AND STR 38R. BLENDED OUT DAMAGE AREA OF OUTER SKIN IAW EA 01-07013.SDR EIA2007054Skin · crackedFUSELAGE SKIN CRACKED AT BS 340 BETWEEN STRINGERS 6L-7L. REMOVED DAMAGE, NDT'D AREA, FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-30-03 PAGES 77-78D.SDR EIA2007053Pressure Panel · crackedNOSE WHEEL WELL WEB CRACKED BETWEEN STA 265-280 LT SIDE AT WL 160. REMOVED DAMAGE, NDT'D AREA, FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-10-04 FIGURE 116 PAGES 708-711.SDR EIA2007051Battery Pack · dischargedUPPER DECK SERVICE DOOR EMERGENCY LIGHT INOP. REPLACE BATTERY PACK, OPS CHECK GOOD PER MM 34-44-01.SDR WRNA200700037Skin · gougedDURING C-CHECK, FOUND EXTERNAL FUSELAGE SKIN GOUGED AT STA 2576 BETWEEN STR 42R AND 46R. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-03 FIG 28.SDR EIA2007014Lamp · inoperativeNR 4 LOWER AFT SMOKE DETECTOR WILL NOT TEST. RELAMPED PER 12-16-02, OPS CHK GOOD.SDR WRNA200700039Door Frame · crackedDURING C-CHECK, A CRACK WAS FOUND ON WEB AND DOUBLER ON R-1 DOOR EDGE FRAME AT STA 488 BETWEEN STR 25 AND 26 USING HFEC. REMOVED DOUBLER AND DAMAGED SECTION OF WEB, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-04 FIG 92.SDR WRNA200700010Ball Screw · failedDURING C-CHECK, HORIZONTAL STABILIZER BALL SCREW AND BALL NUT FAILED FREE PLAY CHECK. REMOVED STABILIZER DRIVE MECHANISM, CHECKED WEAR OF PINS AND FITTINGS, FOUND IN TOLERANCE IAW 747 MM 27-41-06. REINSTALLED DRIVE MECHANISM PER 747 MM 27-41-06 AND PERFORMED BSDR WRNA200700034Rib · crackedDURING C-CHECK, THE LOWER RIB CORD OF NR 4 FUEL TANK ACCESS PANEL 652AB, WS 972 WAS FOUND CRACKED FROM RADIUS BLOCK TO RADIUS BLOCK. REMOVED LOWER RIB CORD IAW SRM 51-30-00, FABRICATED NEW RIB CORD IAW DRAWING 65B01073 AND INSTALLED RIB CORD IAW SRM 51-30-02SDR WRNA200700007Mount · crackedDURING C-CHECK, WHILE ACCOMPLISHING ULTRASONIC INSPECTION OF NR 4 STRUT REAR ENGINE MOUNT THRUST LINKIAW 747 MM 71-21-03, THE FORWARD BORE HAD A CRACK INDICATION AT O/B LUG BORE EDGE.SDR WRNA200700033Skin · damagedDURING C-CHECK, THE O/B SKIN OF NR 3 PYLON WAS FOUND DAMAGED AT APPROX STA 221.9 JUST BELOW MID SPAN. REMOVED DAMAGE IAW SRM 54034-03, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 54-34-03 FIG 25, SRM 51-10-02 AND SOPM 20-42-02.SDR WRNA200700032Bulkhead · dentedDURING C-CHECK, A SMALL DENT WAS FOUND IN THE AFT PRESSURE BULKHEAD AT STA 2360 APPROX WL 200, LBL 30. REMOVED DAMAGED SECTION OF BULKHEAD WEB, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-04 FIG 9, SRM 51-10-01 AND AMM 51-21-00.SDR WRNA200700017Skin · damagedDURING C-CHECK, NR 3 PYLON INBOARD SKIN DOUBLER WAS FOUND WORN UNDER FORESHIELD NEAR NAC STA 221. FABRICATED AND INSTALLED REPAIR PARTS IAW EA 01-07019.SDR WRNA200700011Attach Angle · crackedDURING C-CHECK, FOUND FLOOR ATTACH ANGLE FOR L-1 DOOR FRAME CRACKED, STA 441. REPLACED ANGLE PER 747 SRM 51-30-02SDR WRNA200700009Shear Web · crackedDURING C-CHECK, FOUND A 1 INCH CRACK IN SHEAR WEB BETWEEN S-10A AND S10 LEFT SIDE BS 820, WL 330, LBL 80. REPLACED SHEAR WEB IAW B747 SRM 51-30-02 AND DRAWING 65B9661.SDR WRNA200700008Shear Web · crackedDURING C-CHECK, FOUND A 1 INCH CRACK IN SHEAR WEB, BETWEEN S-10A AND S-10 RIGHT SIDE BS 820, WL 332, RBL 80. REPLACED SHEAR WEB IAW B747 SRM 51-30-02 AND DRAWING 65B09661.SDR WNRA200700038Angle · damagedDURING C-CHECK, HFEC INSPECTION, NR 1 PYLON BULKHEAD, STA 221 FORWARD SIDE, INBOARD ANGLE MISSING PIECE AT UPPER HORIZONTAL FLANGE. FABRICATED AND INSTALLED DOUBLER'S IAW SRM 54-14-03 FIG 13 AND EA 01-07016.SDR WRNA200700036Skin · dentedDURING C-CHECK, FUSELAGE SKIN WAS FOUND DENTED AT STA 228 STR 17L. CUT OUT DAMAGE IAW SRM 53-30-03 FIG 1, FABRICATED REPAIR IAW SRM 53-30-03 FIG 1 AND INSTALLED PER SRM 53-30-01 FIG 1.SDR WRNA200700035Skin · dentedDURING C-CHECK, FOUND 3 DENTS IN FUSELAGE SKIN AT STA 265 BETWEEN STR 10A L AND 11L. REMOVED DAMAGED, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-30-03 FIG 1. THIS IS A CATEGORY -C- REPAIR AND WILL REQUIRE RE-INSPECTION AT 1,000 HOUR INTERVALS, LIFE LIMSDR WRNA200700030Skin · gougedDURING C-CHECK, FUSELAGE SKIN WAS FOUND GOUGED AT STA 665 BETWEEN STR 40R AND 41R. REMOVED GOUGE IAW SRM 53-30-01 DETAIL II AND INSTALLED REPAIR DOUBLE IAW SRM 53-30-03 FIG 1.SDR WRNA200700019Skin · bulgedDURING C-CHECK, FUSELAGE SKIN WAS FOUND BULGED AT STA 2348 AT STRINGER 51R. REPAIRED STRINGER, FAILSAFE STRAP, SHEAR TIE, FRAME WEB AND FRAME IAW SRM, 53-10-02, 53-10-03 FIG 1, 51-40-04, MM 51-21-00, KM DRAWING 531007003-1 AND EA 01-07017.SDR WRNA200700018Skin · damagedDURING C-CHECK, EXTERNAL FUSELAGE SKIN WAS FOUND CREASED FROM STA 1770 TO STA 1850 & 41L TO 46L. REPLACED SKIN SECTION IAW SRM 53-30-03 FIG 19 AND EA 01-07014.SDR WRNA200700016Fuel Tank · corrodedDURING C-CHECK, CORROSION WAS FOUND AT LOWER CENTER TANK SKIN AT STA 1265 LBL 117. REPAIRED IAW SRM 57-30-01 AND EA 01-07018.SDR WRNA200700002Seat Track · crackedDURING 'C' CHECK, CAPTAINS AFT INBD SEAT TRACK WAS FOUND CRACKED, CRACKED VERIFIED WITH HFEC. REPLACED CAPTAINS AFT INBD SEAT TRACK IAW 747 MM 20-51-1.SDR WRNA200700001Seat Track · crackedDURING C-CHECK, FIRST OFFICERS AFT INBOARD SEAT TRACK WAS FOUND CRACKED, VERIFIED WITH HFEC. REPLACED SEAT TRACK IAW B747 MM 20-51-1SDR WRNA200700004Attach Fitting · brokenDURING C-CHECK, FOUND NR 5 SPOILER CENTER ATTACH FITTING BROKEN AFT OF WS 680 IN FLAP WELL.
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