Boeing 757-224
Service difficulty reports · 3,824
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 = '757224' 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 = '757224' 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 CALA0400485Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 720 FROM RBL 58.2 TO LBL 58.2. REPAIRED IAW ECRA 5320-01753, SRM 51-10-02, FIGURE 12, PARAGRAPH 6 AND 51-40-02, FIGURE 3 AND 12.SDR CALA0400484Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 740 FROM RBL 9 TO LBL 4. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 203.SDR CALA0400483Skin · corrodedINSPECTION FOUND INTERNAL FUSELAGE SKIN CORRODED AT BS 778 BETWEEN LBL 6 AND RBL 6. THE CORRODED AREA OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-01 FIGURE 204.SDR CALA0400475Attach Fitting · corrodedINSPECTION FOUND FORWARD CARGO DOOR CUTOUT LOWER SILL THRESHOLD FORWARD, SECOND, AND THIRD ATTACH FITTINGS AT LOWER FORWARD CORNER CORRODED. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0400466Circuit Card · faultyTHE FLIGHT ATTENDANTS REPORTED SMOKE/HAZE AND SMOKEY ODOR IN CABIN WHILE AT CRUISE. THE QRH PROCEDURE FOR SMOKE IN CABIN WAS COMPLETED AND THE GALLEY AND VIDEO EQUIPMENT CIRCUITS WERE DEACTIVATED. THE HAZE CEASED, BUT THE ODOR REMAINED. THE AIRCRAFT LANDED SDR CALA0400459Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1640 BETWEEN LBL 9 AND RBL 14, WL 208. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 203.SDR CALA0400408Socket · faultyPASSENGERS IN ROW 21 - 23 AIRCRAFT LEFT AND RIGHT REPORTED A FAINT SMELL OF RUBBER WHICH COMES AND GOES. FOUND BURNED CONTACT AT FLUORESCENT FIXTURE AT 21 ABC. PULLED AND COLLARED C/B AND PLACARD LIGHT SYSTEM.SDR CALA0400372Frame · dentedINSPECTION FOUND FRAME DENTED IN TWO PLACES AT BS 1600. THE DENTS WERE LOCATED BETWEEN S25L AND S26L AND BETWEEN S23L AND S24L. THE FRAME WAS REPAIRED IAW ECRA 5311-01188.SDR CALA0400339Fan · failedTHE FLIGHT CREW SMELLED A BURNING ODOR IN THE CABIN WHILE ON DESCENT INTO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT RECIRCULATION FAN AT FAULT. THE FAN WAS REMOVED AND REPLACED IAW MM 21-25-01.SDR CALA0400318Slide · out of rigCARRIER DEPLOYMENT WAS INTERMITTENT DURING RIGHT OFF WING SLIDE DEPLOYMENT FUNCTION TEST. THE RIGHT OFF WING SLIDE DOOR WAS RIGGED AND ADJUSTED IAW MM 25-65-09, PARAGRAPH 3D, ITEMS 9-14.SDR CALA0400320Valve · leakingTHE FLIGHT ATTENDANTS REPORTED AN ELECTRICAL SMELL IN THE AFT CABIN WHILE IN FLIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED SAFELY. MAINTENANCE FOUND THE LEADING EDGE SLAT POWER DRIVE UNIT CONTROL VALVE MODULE LEAKING HYDRAULIC FLUID. THE ODOR OBSSDR CALA0400311Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 378, RBL 10. REPAIRED IAW ECRA 5320-01747.SDR CALA0400310Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER SURFACE CORRODED AT BS 700, LBL 58.2. REPAIRED IAW ECRA 5320-01746.SDR CALA0400309Floorbeam · corrodedINSPECTION FOUND TOP SURFACE OF FLOORBEAM CORRODED AROUND FASTENER HOLES AT BS 1640, BL 0 TO LBL 24.5. REPAIRED IAW ECRA 5320-01749.SDR CALA0400308Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AT BS 680, RBL 16 TO LBL 16. REPAIRED FLOORBEAM IAW SRM 53-00-51, FIGURE 203.SDR CALA0400307Intercostal · corrodedINSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AT BS 684, RBL 15. THE INTERCOSTAL WAS REPLACED IAW SRM 51-40-02, FIGURE 12.SDR CALA0400292Wire · chafedMAINTENANCE NOTICED SMOKE WHEN POWERING UP THE AIRCRAFT TO ACCOMPLISH A GEAR SWING WHILE THE AIRCRAFT WAS IN HEAVY CHECK AT YXX. WHEN MAINTENANCE FOUND THE SOURCE OF THE SMOKE THE FIRE HAD SELF EXTINGUISHED. EVIDENCE OF FIRE EXISTED FROM THE HEAT DAMAGE AND SDR CALA0400288Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT FASTENER HOLE, BS 377.7, LBL 58, WBL 208.10. REPAIRED IAW SRM 53-00-51.SDR CALA0400287Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 365, RBL 18. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 203.SDR CALA0400284Battery · inoperativeTHE R-2 DOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. A NEW BATTERY PACK WAS INSTALLED IAW MM 33-51-07.SDR CALA0400283Charger · inoperativeINSPECTION FOUND R-1 DOOR EMERGENCY LIGHTS INOPERATIVE. THE EMERGENCY LIGHT BATTERY CHARGER AT STA 340 (IN OVERHEAD AT FORWARD LAV & COCKPIT DOOR) WAS FOUND AT FAULT. THE CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07.SDR CALA0400276Actuator · inoperativeTHE RIGHT OFF WING ESCAPE SLIDE CARRIER DID NOT DEPLOY WHEN 1500 PSI NITROGEN WAS APPLIED DURING TESTING. MAINTENANCE FOUND THE RIGHT WING ESCAPE SLIDE ACTUATOR AT FAULT. THE ACTUATOR WAS REMOVED AND REPLACED AND A FUNCTIONAL CHECK WAS PERFORMED IAW MM 25-65SDR CALA0400218Skin · damagedTHE PREVIOUS SKIN BLENDOUT AT STATIC PORT AREA, BS 540 BETWEEN S22R AND S23R WAS FOUND BEYOND LIMITS. THE DAMAGE WAS REPAIRED IAW SRM 53-00-01, FIGURE 209. A DIP WAS ISSUED TO REINSPECT THE REPAIR WITHIN 37,500 FLIGHT CYCLES AND AGAIN EACH SUBSEQUENT 12,000 SDR CALA0400214Frame · dentedINSPECTION FOUND AFT CARGO COMPARTMENT RT SIDEWALL FRAME DENTED ON TOP SURFACE AT BS 1340, S26R. REPAIRED IAW SRM 51-70-11, FIGURE 1.SDR CALA0400212Frame · dentedINSPECTION FOUND MAIN FRAME DENTED AT BS 1600, STRINGERS 23L TO 26L. A REPAIR WAS INSTALLED IAW ECRA 5311-01188. A DIP WAS ISSUED TO ACCOMPLISH A PERMANENT REPAIR WITHIN 60 DAYS.SDR CALA0400204Skin · crackedINSPECTION FOUND TWO CRACKS IN THE LT WING FIXED L/E SKIN AT OSS 421 T0 471. THE CRACKS WERE 3 INCH AND 5 INCH LONG. REPAIRED IAW EA 5731-01010, REV D.SDR CALA0400198Skin · crackedINSPECTION FOUND A 9 INCH CRACK IN RT WING LEADING EDGE SKIN AT STA OSS 425. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D.SDR CALA0400192Stop Fitting · corrodedINSPECTION FOUND FORWARD CARGO DOOR LOWER STOP FITTINGS NR 2 AND NR 3 CORRODED AT STA 572. THE FITTINGS WERE REPLACED IAW SRM 51-40-02.SDR CALA0400174Support Fitting · corrodedINSPECTION FOUND FORWARD CARGO DOOR CUTOUT LOWER SILL UPPER AFT SUPPORT FITTING CORRODED. THE SUPPORT FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0400164Sill · corrodedINSPECTION FOUND THE FORWARD CARGO DOOR LOWER SILL UPPER SURFACE CORRODED AT AFT SECTION BEHIND THE SCUFF PLATE SUPPORT BRACKET, STA 580. REPAIRED IAW SRM 51-40-02.SDR CALA0400161Skin · crackedINSPECTION FOUND A 3 INCH CRACK IN RT WING UPPER FIXED L/E SKIN LOCATED I/B OF SLAT NR 7 AT WS 418. REPAIRED IAW ECRA 5721-01119.SDR CALA0400160Skin · crackedINSPECTION FOUND TWO 3.5 INCH CRACKS IN LT WING UPPER L/E SKIN PANEL AT WS 539 BETWEEN NR 3 AND NR 4 SLATS. REPAIRED IAW ECRA 5721-01120.SDR CALA0400148Skin · crackedINSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STA 1620-1640, S21R, JUST BELOW AND FORWARD OF R-3 DOOR. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 214. A DIP WAS ISSUED TO INSPECT FASTENERS EVERY 1,000 FLIGHT CYCLES AND TO PERFORM A PERMANENT REPASDR CALA0400104Frame · dentedINSPECTION FOUND FRAME DENTED AT BS 1460, S27L. THE FRAME WAS REPAIRED IAW SRM 53-00-07, FIGURE 201.SDR CALA0400096Skin · damagedINSPECTION FOUND THREE CREASES IN FUSELAGE SKIN FROM S24R - S26R, STA 1787, WL 138.5. REPAIRED IAW ECRA 5330-03323.SDR CALA0400095Skin · crackedINSPECTION FOUND MULTIPLE CRACKS IN LT WING L/E SKIN AT O/B END OF NR 4 SLAT, OSS 430. THE LONGEST CRACK WAS SIX INCHES. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D, SEQ 399.SDR CALA0400040Skin · crackedINSPECTION FOUND A 9 INCH CRACK IN LT WING LEADING EDGE SKIN AT OSS 450.0. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D.SDR CALA0400039Skin · crackedINSPECTION FOUND A 9 INCH CRACK IN RT WING LEADING EDGE SKIN AT OSS 441.0. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D.SDR CALA0400021Engine · making metalSMOKE WITH OILY ODOR REPORTED IN CABIN & NR 1 ENG AUTO SHUTDOWN. A/C DIVERTED & LANDED WITHOUT INCIDENT. INSP OF NR 1 ENG FOUND CHIP DETECTORS COVERED IN METAL, ENG OIL QTY ZERO, & DAMAGE TO NR 1 ENG FAN & COWL. A/C OUT OF SERVICE FOR REMOVAL OF NR 1 ENG. SDR CALA0300706Skin · crackedINSPECTION FOUND A 4.5 INCH CRACK IN RIGHT WING FIXED LEADING EDGE SKIN BETWEEN OSS 397 AND OSS 421. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D, OP 4 AND SRM 57-41-01.SDR CALA0300704Skin · crackedINSPECTION FOUND A 6.25 INCH CRACK IN RT WING FIXED L/E SKIN AT STA OSS 421- OSS 471. THE SKIN WAS REPLACED IAW EA 5731-01010, REV D, OP 3.SDR CALA0300644Skin · puncturedINSPECTION FOUND AFT FUSELAGE EXTERNAL SKIN PUNCTURED JUST BELOW LEFT STATIC PORT AT STA 1365, S23-24L. REPAIRED SKIN IAW SRM 53-00-01, FIGURE 204 AND 51-10-01, FIGURE 7.SDR CALA0300640Skin · gougedINSPECTION FOUND RT TRAILING EDGE O/B MAIN FLAP NOSE SKIN GOUGED AT WBL 558. THE FLAP NOSE SKIN WAS REPAIRED IAW SRM 57-53-01 FIGURE 202.SDR CALA0300626Frame · puncturedINSPECTION FOUND AFT CARGO PIT FRAME PUNCTURED AT BS 1340, S25R. REPAIRED IAW SRM 51-70-11.SDR CALA0300624Skin · crackedINSPECTION FOUND A 6 INCH CRACK IN RT WING L/E SKIN PANEL AT WS 421.5. THE SKIN PANEL WAS REMOVED AND REPLACED IAW EA 5731-01010, OP 3.SDR CALA0300580Connector · corrodedTHE LT EMERGENCY ESCAPE SLIDE FAILED TEST 1. TROUBLESHOOTING PER FIM 25-65-00 FOUND CANNON PLUG D40828 AT LT EMERGENCY HATCH DISARM PANEL HAD LITE SURFACE CORROSION ON SEVERAL PINS. THE CONNECTOR WAS CLEANED AND RECONNECTED AND SYSTEM TESTED NORMAL.SDR CALA0300542Skin · dentedINSPECTION FOUND LT FUSELAGE SKIN DENTED AT BS 730, STRINGER 16L. THE SKIN WAS REPAIRED IAW ECRA 5330-03281.SDR CALA0300541Skin · corrodedINSPECTION FOUND RT I/B MAIN FLAP SKIN PANEL CORRODED ON LOWER SURFACE. REPAIRED SKIN IAW ECRA 5750-03811.SDR CALA0300537Skin · crackedINSPECTION FOUND AN 8 INCHES CRACK IN LT WING FIXED LEADING EDGE SKIN AT OSS 421-471. THE SKIN WAS REPAIRED IAW ECRA 5721-01010, REV. D.SDR CALA0300519Slide · out of adjustTHE RT OFF WING SLIDE SYSTEM FAILED DURING FUNCTION TEST WHILE AIRCRAFT WAS IN (C) CHECK AT LTN. THE DOOR AND SLIDE CARRIER FAILED TO DEPLOY DURING FUNCTION TEST AS PRESCRIBED BY CO WORK CARD 19-2560-1-7602(MPD-25-65-00-05B, MRB-25-020. THE LOCK FITTING, CONTR
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