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 P5CA9800362Frame · crackedSTA 720 FRAME FOUND CRACKED AT STR 9L CUTOUT. FRAME REPAIRED AT U/D BS 720 STR 9L PER SRM 53-10-04 FIG 54.SDR P5CA9800361Foreflap · corrosionLT WING INBD FORE FLAP I/B TOP SURFACE PANEL FOUND SURFACE CORROSION AT 3 LOCATIONS. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02.SDR P5CA9800360Frame · crackedUPPER DECK FRAME 540 FOUND CRACKED AT STR 7R AND 7AR AND 8R CUTOUT AREA. FRAME REPAIR AT U/D BS 540 STR 7R, 7AR AND 8R PER SRM 53-10-04 FIG 54.SDR P5CA9800357Frame · crackedUPPER DECK FRAME 600 STR 8L CUTOUT AREA FOUND CRACKED. U/D BS 600 FRAME REPAIR AT STR 8L PER SRM 53-10-04 FIG 54.SDR P5CA9800356Frame · crackedUPPER DECK FRAME 660 STR 7AL CUTOUT AREA FOUND CRACKED. FRAME REPAIRED AT U/D BS 640 STR 7AL PER SRM 53-10-04 FIG 54.SDR P5CA9800351Frame · crackedUPPER DECK FRAME 620 STR 7R CUTOUT AREA FOUND CRACKED. FRAME REPAIRED AT U/D BS 620 STR 7R PER SRM 53-10-04 FIG 54.SDR P5CA9800349Fairing · spongedRT WING #7 FIXED FAIRING MARKED AREA FOUND SPONGED. FIBERGLASS REPAIR AS PER SRM 51-40-15.SDR P5CA9800343Frame · crackedUPPER DECK FRAME 720 FOUND CRACKED AT STR 9R CUTOUT. FRAME REPAIRED AT UD BS 720 STR 9 R PER SRM 53-10-04.SDR P5CA9800322Brace · wornNR 2 ENG DIAGONAL BRACE WORN ON AFT END ON LT SIDE. AREA SMOOTHED OUT AND SHOT PEENED. NO CRACKS NOTED PER SRM 51-10-02, OHM 20-10-03, NDT PT 6 51-00-00 FIG 4.SDR P5CA9800320Flap · crackedLT WING NR 3 L/E FLAP INBD ACTUATING ARM NOSE AREA L/E NOSE BEAM RIB CHORD FLANGE AT LOWER END FOUND CRACK. NOSE BEAM RIB CHORD REPAIRED PER SRM 57-20-03.SDR P5CA9800319Tr Sleeve · damagedNR 1 ENG FAN T/R TRANSLATING SLEEVE AT 9 O'CLOCK POSITION NEEDS REPAIR INSIDE AND OUTSIDE. FILLER REPAIRS CARRIED OUT PER SRM 51-40-06 PARA 2B.SDR P5CA9800291Panel · chippedRT WING L/E UPPER FIXED PNL WS 890-917 T/E FABRIC PATCH FOUND CHIPPED AND GLASS REPAIRED AS PER SRM 51-40-15.SDR P5CA9800281Cowl · dentedNR 2 T/R FAN TRANSLATING COWL AT 9 O'CLOCK POSITION RT SIDE DENTED. REPAIRED AS PER SRM 51-40-00 PARA 2E.SDR P5CA9800279Panel · delaminatedLT WING TOP T/E FIXED PANEL DEBONDED AND A PUNCH HOLD FOUND AT I/B AILERON I/B. FIBERGLASS REPAIRED AS PER SRM 51-40-15.SDR P5CA9800277Stringer · corrosionFWD CARGO COMPARTMENT BS 910-920 STRINGER FOUND CORROSION. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1 REFSRWS 912817.SDR P5CA9800275Skin · dentedDENT FOUND IN SKIN AND SUSPECT SKIN CRACK AT 6 O'CLOCK POSITION AT STA 2618. DENT AREA DRESSED PER SRM 51-10-01 AND TREATED PER SRM 51-01-02 AND CONDITION CHECK FOUND WITHIN SRM 53-30-01 LIMITS.SDR P5CA9800271Skin · dentedDENT FOUND IN RT BODY SKIN AT 6 O'CLOCK POSITION ON SKIN AFT OF STA 2598 WL 212. DENT AREA PATCH REPAIRED AS PER SRM 53-50-03 FIG 4 AND SRWS 912822.SDR P5CA9800270Cowl · disbondedNR 2 LEFT FAN COWL INTERNAL MIDDLE AREA HONEY COMB DISBONDED. HOT BOND REPAIRED AS PER SRM 51-40-06 FIG 17A. HOT BOND REPAIRED AS PER SRM 51-40-06 FIG 17A.SDR P5CA9800269Fairing · spongyLEFT WING NR 2 CANOE FAIRING MIDDLE LOWER AREA FOUND SPONGY. FIBERGLASS REPAIRED PER SRM 51-40-14.SDR P5CA9800268Foreflap · damagedRT WING O/B FLAP NOSE AREA NR 8 FLAP TRACK I/B FOUND SPONGED AS MARKED APPROX 4 BY 6 INCHES. FIBERGLASS REPAIRED AS PER SRM 51-40-14.SDR P5CA9800266Door · crackLT W/G I/B STRUT DOOR, FWD END FAIRING FWD EDGE FOUND FABRIC CRACK. FIBERGLASS REPAIRED AS PER SRM 51-40-06 APRA 2E.SDR P5CA9800265Door · debondedLT W/G I/B STRUT DOOR AFT EXTERIOR SKIN FOUNDED DEBONDED AT I/B EDGE. FIBERGLASS REPAIRED PER SRM 51-40-06 PARA 2E.SDR P5CA9800264Fairing · delaminationFUSELAGE BODY FAIRING EXTERIOR MID AREA FOUND DELAMINATION FAIRING 192KR. BODY FAIRING FIBERGLASS REPAIRED PER SRM 51-40-14.SDR P5CA9800263Support · corrosionLEVEL 1 CORROSION, FOUND AT FUSELAGE BODY FAIRING SUPPORT AT BS 1620 LBL O THROUGH 60. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT AND REPAIRED PER 53-50-04.SDR P5CA9800262Support · corrosionLEVEL 1 CORRSOION, FOUND FUSELAGE BODY FAIRING SUPPORT AT BS 1580 LBL LEFT 0 THROUGH 245. REMOVED CORROSION AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMITS 53-30-01.SDR P5CA9800261Support · corrosionLEVEL 1 CORROSION, FOUND ON NUTPLATE SUPPORT RT STA 1130 AT UPPER WING TO BODY FILLET FAIRING AREA. CORROSION REMOVED AS PER SRM 51-10-01 AND TREATED AS PER 51-10-02.SDR P5CA9800260Skin · corrosionLEVEL 1 CORROSION, FOUND LEFT WING MIDSPAR AREA WS 557-586 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT PER 57-30-01.SDR P5CA9800259Skin · corrosionLEVEL 1 CORROSION, FOUND LEFT WING MIDSPAR AREA WS 520-530 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51-10-02. BLENDED OUT PER SRM 57-30-01.SDR P5CA9800258Skin · corrosionLEVEL 1 CORROSION, FOUND LEFT WING MIDSPAR AREAS WS 469-499 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT PER 57-30-01.SDR P5CA9800257Skin · corrosionLEVEL 1 CORROSION, FOUND LEFT WING MIDSPAR AREA WS 440-455 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLEND OUT WITHIN SRM LIMIT 57-30-01.SDR P5CA9800256Skin · corrosionLEVEL 1 CORROSION FOUND LEFT WING SPANWISE BEAM NR 3 AREA WS 350 - 380 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-70-02. BLENDED OUT WITHIN SRM LIMIT 57-30-01.SDR P5CA9800255Skin · corrosionLEVEL 1 CORROSION, FOUND LT WING MID SPAR AREA WS 382-411 AND WBL 150-235 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT 57-30-01.SDR P5CA9800254Skin · corrosionLEVEL 1 CORROSION FOUND LT WING LOWER SKIN O/B SURFACE AT MID SPAR BETWEEN PANEL 554GB AND 555 AB. REMOVED CORROSION AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMITS PER 57-30-01.SDR P5CA9800253Skin · corrosionLEVEL 1 CORROSION FOUND AT LT WING O/B LOWER SKIN T/E AREA PREVIOUS REWORK AREA O/B AILERON MID AREA. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02 BLEND OUT WITHIN SRM LIMIT 57-30-01.SDR P5CA9800252Skin · corrosionLEVEL 1 CORROSION LT WING FRONT SPAR WS 1112-1155 UPPER SURFACE. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51-10-02. BLENDED OUT WITHIN SRM LIMIT 57-30-01.SDR P5CA9800251Skin · corrosionLEVEL 1 CORROSION FRONT SPAR AREA WS 660-680 UPPER SURFACE. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT 57-30-01.SDR P5CA9800250Skin · corrosionLEVEL 1 CORROSION LT/W MIDSPAR W/S 614-642 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT 57-30-01.SDR P5CA9800244Support · corrodedFUSELAGE BODY FAIRING SUPPORT FOUND SLIGHT CORROSION AT BS 1620 LBL 0 TO 60. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. REPAIRED PER SRM 53-50-04.SDR P5CA9800243Skin · corrosionLEVEL 1 CORROSION FUSELAGE SKIN AT BS 1620 TO 1680 STR 40L STR 43R. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51-10-02 BLEND OUT WITHIN SRM LIMIT PER SRM 53-30-01.SDR P5CA9800242Stiffener · crackedFUSELAGE KEEL BOX ATTACH VERTICAL STIFFENER FOUND CRACKED AT BS 1000. STIFFENER REPAIRED AS PER SRM 51-10-01.SDR P5CA9800241Skin · crackedONE EACH CRACK FOUND ON THE FASTENER HOLE OF SKIN LONGITUDINAL LAP SPLICE AT BS 785 STR 392 OUTER SKIN AREA RUNNING FORWARD APPROX 0.51 LONG. RT STR 382 LAP REPAIRED AS PER SRM 53-30-03 FIG 17.SDR P5CA9800240Web · corrosionLEVEL 1 CORROSION FOUND LT W/G W/W INBD WEB AT STA 1241 WL 155. REMOVED AND TREATED AS PER SRM 5110-01, 51-10-02. BLEND OUT AND REPAIRED PER SRM 51-40-04.SDR P5CA9800239Skin · corrosionLEVEL 1 CORROSION FOUND ON FUSELAGE SKIN BS 2355 TO 2365 STR 46L TO 46R. REMOVED CORROSION AND TREATED PER SRM 51-10-01 AND 51-10-02 BLEND OUT WITHIN SRM LIMIT 53-30-01.SDR P5CA9800354Frame · crackedUPPER DECK FRAME 640 8R CUTOUT AREA FOUND CRACKED. FRAME REPAIRED AT U/D STA 640 STR 84 SRM 53-10-04 FIG 54.SDR P5CA9800333Fairing · delaminatedFUSELAGE BODY FAIRING 193G AND 194G EXTERIOR LAYER FOUND CRACKED AND DELAMINATED. AREA REPAIRED PER SRM 51-24-11.SDR P5CA9800330Skin · damagedNR 3 ENG NOSE COWL RT AFT LOWER ACOUSTIC PANEL OUTER SKIN DAMAGED, ACOUSTIC PANEL REPAIRED FIBERGLASS REPAIR PER SRM 51-30-02.SDR P5CA9800321Skin · corrosionLT WING GEAR O/B STRUT DOOR INNER SKIN LOWER EDGE FOUND CORROSION. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02.SDR P5CA9800316Bulkhead · corrosionLEVEL 1 CORROSION, FOUND ON NR 3 ENG BULKHEAD TO FIREWALL FWD LT CORNER AREA IN STRUCTURE (FWD ING MOUNT BULKHEAD STRUCTURE). SURFACE CORROSION REMOVED ON FWD BULKHEAD AT FIREWALL FWD LWR LT CORNER PER SRM 51-10-01 AND 51-10-02.SDR P5CA9800314Skin · disbondedLT WING I/B FOREFLAP I/B PANEL FOUND SKIN DISBONDED AT CORROSION REWORK LOCATION 2 BY 10 INCHES. HOT BOND REPAIRED PER SRM 51-40-06 FIG 17 AND FIG 17A.SDR P5CA9800312Skin · corrodedRT WING I/B T/E FOREFLAP L/E LOWER SURFACE BETWEEN NR 5 AND NR 6 FLAP TRACKS HAS LIGHT SURFACE CORROSION ON SKIN PANEL. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02 AND FILLER REPAIRED PER SRM 51-40-06.
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