Boeing 757-222
Service difficulty reports · 15,539
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 = '757222' 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 = '757222' 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 UALA2012071203750Idg · failedRIGHT GEN DRIVE LIGHT CAME ON AFTER TAKEOFF. DISCONNECTED. AT ARRIVAL, IDG NEEDED BETWEEN 45-50 PUMPS TO OVERFLOW. REPLACED IDG PER MM, ENGINE RUN CHECKED GOOD.SDR UALA2012071203749Actuator · failedLT REVERSER ISOLATION EICAS ON LANDING. LT THROTTLE WILL NOT MOVE. FOUND LT REVERSER HALF NOT STOWED, LOWER ACTUATOR AFT ATTACH HARDWARE MISSING, CHECKED THROTTLES FOUND NO BINDING AND FREE MOVEMENT. LOWER ACTUATOR REPLACED. OPS AND LEAK CHECKS GOOD. AIRCSDR UALA2012071103708Nut · crackedNR 3 AFT TIRE: ONE TIE BOLT NUT IS CRACKED. REPLACED TIRE.SDR UALA2012071103704Skin · damagedEXTERNAL FUSELAGE SKIN DAMAGED BS 511, STR 24L. CUT-OUT DAMAGED SKIN AND FABRICATED A DOUBLER AND FILLER AND INSTALLED PER SRM 53-00-01, REPAIR 2 PER SRM 53-00- 01, RPR 2, FIG. 201 AND TABLE V.SDR UALA2012071003699Check Valve · vibrationDURING DESCENT, VERY NOTICEABLE VIBRATION IN FLOOR FROM ROW 20 TO DOORS 2R AND L. FOUND APU BLEED CHECK VALVE BAD. REMOVED AND REPLACED APU BLEED CHECK VALVE AND BLEED VALVE CLAMPS. GROUND CHECKED GOOD.SDR UALA2012071203765Service Panel · looseDURING DESCENT, VERY NOTICEABLE VIBRATION IN FLOOR FROM ROW 20 TO DOORS 2R&L. FOUND HYD SERVICE PANEL LEADING EDGE LATCHES OUT OF ADJUSTMENT. PANEL VERY LOOSE, ADJUSTED LATCHES.SDR UALA2012070903681Cam · corrodedMAIN CABIN R1 DOOR UPPER AND LOWER CAM PLATES ARE RUSTY. REMOVED DOOR AND CAM PLATES PER MM. PAINT STRIPPED AND CAD PLATE STRIPPED, CADMIUM PLATED, AND REINSTALLED CAM PLATES AND DOOR PER MM.SDR UALA2012071203753Unknown · odorPUNGENT ODOR IN COCKPIT DURING CLIMBOUT AND WENT AWAY. RAN LT & RT PACKS ISOLATED WITH APU AS BLEED SOURCE AND HAD NO ODOR PRESENT. RAN RT & LT PACKS WITH NR 1 & 2 ENGINE BLEEDS AND ISOLATED. ALSO RAN EACH PACK WITH JUST ONE ENGINE AS BLEED SOURCE, NO ODOR PRSDR UALA2012070903653Light · brokenEMERGENCY EXIT ROW 20 ABC EXIT LIGHT FRAME BROKEN DIFFUSER FELL OUT. INTERIM REPAIR MADE GOOD FOR 4 CYCLES. REPLACED DIFFUSER.SDR UALA2012071103717Handle · malfunctionedFLAPS WOULD NOT EXTEND PAST 25 DEGREES. CYCLED HANDLE BACK TO 20 DEGREES THEN MOVED BACK TO 25 WITH NO RESPONSE PAST 20 DEGREES. WENT TO ALTERNATE MODE SET FLAPS TO 20, FLAPS APPEARED TO MOVE A LITTLE. DID NOT TRY TO MOVE FLAPS PAST 20 DEGREES WHILE IN ALTESDR UALA2012070903671Circuit Breaker · malfunctionedCENTER TANK WON'T TAKE FUEL. CYCLED BREAKER AND NOW BOTH VALVES OPENED AND CENTER TANK TAKES FUEL.SDR UALA2012070903670Fitting · gougedMAIN CABIN L2 DOOR MID FRAME OUTBOARD GUIDE FITTING GOUGED. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REPLACED MAIN CABIN L2 DOOR FRAME OTBD GUIDE FITTING IAW AMM. DOOR OPS CHECK GOOD.SDR UALA2012071103730Feeder Cable · inoperativeEMERGENCY LIGHTS INOPERATIVE ROW 8A-12A. REPLACED BROKEN FEEDER CABLE, OPS CHECKED NORMAL.SDR UALA2012071103732O-Ring · leakingNR 1 ENGINE FMU LEAKING PROFUSELY AT BLUE END CAP. NOTED PACKING PROTRUDING. ORDERED NEW PACKING. RAN 5 MIN IDLE NO LEAKS NOTED. REPLACED LEAKING O-RING FUEL CONTROL WITH NEW.SDR UALA2012071103731Unknown · odorSTRONG RAW FUEL ODOR AND VISIBLE VAPOR IN CABIN AFTER ENGINE START. ACCOMPLISHED HIGH POWER ENG RUNS AND APU OPS CHK ISOLATING ALL BLEED SOURCES INDIVIDUALLY. UNABLE TO DUPLICATE OIL ODOR IN CABIN. NO VISIBLE VAPOR IN CABIN. ACFT OK FOR SERVICE.SDR UALA2012070903694Skin · dentedFUSELAGE SKIN DENTED BETWEEN BS 1600-1620 AT STR 15R-16R. DENT LOCATION AT 1510, APPROX DENT CORRECTLY LOCATED AT BS 1595. CORRECTED LOCATION DUE TO ERROR DURING INITIAL EVALUATION. EVALUATED DENT AND FOUND OUT OF SRM LIMITS. CUT OUT DAMAGE AND ACCOMP NDT SDR UALA2012070903692Floorbeam · corrodedFLOORBEAM AT BS 1640 CORRODED AT BL 0. REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF SRM LIMITS. REMOVED FLOORBEAM UPPER TEE FROM LBL 9.5 TO RBL 68. ACCOMPLISHED NDT OF TRIMMED EDGE AND EXISTING FASTENER HOLES AND HOLES COMMON TO REPAIR. NO CRACKS FOUNSDR UALA2012070903691Shear Tie · corrodedSHEAR TIE CORRODED AT BS 1320 BETWEEN 27 AND 28L IN AFT CARGO. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-40-02. MAJOR REPAIRSDR UALA2012070903690Web · corrodedAFT CARGO BAY BILGE AREA WEB AT BS 1360 STR 27 LT HAS CORROSION, FABRICATED AND INSTALLED NEW WEB PER SRM 53-60-04 AND 51-40-05.SDR UALA2012070903667Skin · dentedFUSELAGE SKIN DENTED BS 1595 STR 15-16R. EVALUATED DENT AND FOUND OUT OF SRM LIMITS. CUT OUT DAMAGE AND ACCOMP NDT OF CUT OUT AND OPEN HOLES COMMON TO REPAIR REF NDTM 51-00-19 (PART 6). FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR REF SRM 53-00-01 REPSDR UALA2012070903666Floorbeam · corrodedFLOORBEAM AT BS 1640 CORRODED AT BL 0. REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF SRM LIMITS. REMOVED FLOORBEAM UPPER TEE FROM LBL 9.5 TO RBL 68. ACCOMPLISHED NDT OF TRIMMED EDGE AND EXISTING FASTENER HOLES AND HOLES COMMON TO REPAIR. NO CRACKS FOUNSDR UALA2012070903665Shear Tie · corrodedSHEAR TIE CORRODED AT BS 1320 BETWEEN STRINGERS 27 AND 28L, AFT CARGO BAY. REMOVED AND REPLACED SHEAR TIE IAW SRM. MAJOR REPAIR.SDR UALA2012070903664Web · corrodedAFT CARGO BAY BILGE AREA WEB AT BS 1360 STR 27L HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED NEW WEB.SDR CALA2014040390761Mount Bracket · damagedLEFT WING INB FLAP, OTBD AFT FAIRING, FWD INBD MOUNT BRACKET HAS PULLED RIVETS & ELONGATED HOLE. ACCOMPLISHED A FREEZE PLUG STRAP REPAIR. ACFT WILL BECOME NON-AIRWORTHY ON OR BEFORE 20JUL14 UNLESS NEW 8100-9 RECEIVED.SDR UALA2012070903656Guard · faultyEMERGENCY LIGHTS SWITCH COVER DOES NOT ARM SWITCH WHEN CLOSED. REPLACED P5 PANEL EMERGENCY LIGHT SWITCH GUARD.SDR UALA2012070903658Fitting · gougedMAIN CABIN L1 DOOR SLIDE OUTBOARD BAYONET FITTING AREA DEEPLY GOUGED. REMOVED AND REPLACED MAIN CABIN L-1 DOOR SLIDE ASSY PER MM.SDR UALA2012070903655Door · stuckRT OVERWING EMERGENCY SLIDE DOOR WOULD NOT OPEN WITH MANUAL HANDLE. FOUND DOOR WAS SEALED WITH OVER SPRAYED PAINT, PAINT WAS FOUND BETWEEN DOOR SEAL AND DOOR, LWR FWD LOCATION. REMOVED OLD GREASE FROM DOOR LATCH TUBE AND RE-LUBED. PERFORMED MANUAL AND PNEUMSDR UALA2012070903652Controller · failedNR 2 ENGINE 14TH STAGE HPC UNIT FAILED TEST. REMOVED AND REPLACED NEW SERVICEABLE HPC FOR NR 2 ENGINE ON NR 9975046.SDR UALA2012070903651Pump · failedLEFT AC ELECTRIC HYDRAULIC PUMP FAIL, THE RECEPTACLE PIN DIAMETER CHECK PER CARD WORK INSTRUCTIONS. REMOVED AND REPLACED LT HYD PUMP PER AMM.SDR UALA2012070603648Pseu · faultyEICAS GEAR DISAGREE ON FINAL WITH NORMAL GEAR DOWN GREEN LIGHTS ON. SECOND EXTENSION NORMAL. ACCOMPLISHED PSEU BITE. FAULTED 16 DIFFERENT SENSORS. GEAR DISAGREE MSG COMING FROM PSEU. REPLACED PSEU PER MM AND RELAY K10266 PER WDM. OPS CHECK GOOD. NO FAULSDR UALA2012070603649Gate · crackedDOOR 2R UPPER HINGE CUTOUT CRACKED AND SMC5 DOOR 1R UPPER GATE CRACKED. REMOVED DOOR 2R. ACCOMPLISHED CHECK. REPAIRED PER MM.SDR UALA2012070503583Gate · crackedDR 2R HAS CRACK .25 LONG AT UPPER HINGE CUTOUT. ALSO FOUND R1 DOOR UPPER GATE CRACKED AT SECOND RIVET.SDR C8GA20120710008Gcu · malfunctionedRIGHTT GEN OFF DISPLAYED ON TAKEOFF, CONDITION RETURNED TO NORMAL ON RESET. REMOVED AND REPLACED RIGHT GCU AND TESTED GOOD.SDR UALA2012070603633Lock · faultyMAIN CABIN L1 DOOR HOLD OPEN ASSEMBLY CLUTCH WORN. REMOVED AND REPLACED MAIN CABIN L1 DOOR HOLD OPEN LOCK ASSY PER MM 52-11-08 ON NON ROUTINE 40215.SDR UALA2012070603632Bolt · unsecureMAIN CABIN L1 DOOR EMERGENCY POWER ASSIST PRESSURE RESERVOIR CABLE HAS LOOSE BOLT AT BOTTLE. SUPPLEMENTAL DATA UPDATE, SECURED MAIN CABIN L1 DOOR EMERGENCY POWER ASSIST PRESS RESERVOIR CABLE AND BOTTLE BOLTS PER MM ON NON ROUTINE 40240.SDR UALA2012070503620Girt Bar · obstructedL2 DOOR WILL NOT ARM. CLEANED DOOR SILL AREA, ARMED DOOR THREE TIMES, CHECKED OK.SDR UALA2012070503618Gate · corrodedR4 DOOR LOWER GATE HAS CORROSION ON BOTTOM LIP. INSTALLED LOWER GATE.SDR UALA2012070503617Gate · corrodedL1 LOWER GATE CORRODED. INSTALLED LOWER GATE REF MM 52-11-38 STEP 3,D 5-7.SDR UALA2012070503604Circuit Card · faultyFALSE FLAP WARNING, RTFL. TROUBLESHOT PER FIM 32 09 03. FOUND LOGIC CARD NUMBER 011 BAD IN PROX SWITCH ELECT UNIT. REMOVED AND REPLACED LOGIC CARD PER AMM AND RAN TEST OF PROX SWITCH ELECT UNIT. ALL CHECKED GOOD. OK TO CONTINUE.SDR UALA2012070503606Torque Tube · corrodedRT MAIN FLAP FAILSAFE TORQUE TUBE SHOWS SIGNS OF CORROSION. REPAIRED RT WING FAILSAFE TORQUE TUBE PER CMM 57-53-43.SDR UALA2012070503605Torque Tube · corrodedLEFT INBD MAIN FLAP TORQUE TUBE FAILSAFE SHOWS SIGNS OF CORROSION. REPAIRED THE FAILSAFE TORQUE TUBE PER CMM 57-53-43, REFERENCE R03846, 8130-3, 016-A004726 49. WORK WAS ACCOMPLISHED AT SFO.SDR UALA2012070303546Skin · damagedEXTERIOR UPPER FUSELAGE STA 700, BETWEEN STA 3L AND 4L HAS A DEEP BLENDED OUT AREA. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN, HFEC CUT SKIN AND SURROUNDING HOLES, INSTALLED REPAIR DOUBLERS AND FILLER PER ECRA 5531-01609.SDR UALA2012070303545Frame · corrodedAFT CARGO FRAME HAS CORROSION AT STA 1440 AND RBL4. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION, JUST OUT OF SRM LIMITS, TREATED, PRIMED, INSTALLED REPAIR DOUBLER PER ECRA 5360-01209.SDR UALA2012070503603Igniter · arcedNR 1 ENGINE LOWER IGNITER AND LEAD SHOW EVIDENCE OF ARCING. REPLACED LOWER IGNITER AND LEAD ASSY.SDR UALA2012070503611Skin · damagedEXTERIOR UPPER FUSELAGE BS 1450 SPLICE BETWEEN STR 3L AND 4L HAS A BLENDED OUT AREA. TRIMMED OUT DAMAGED SKIN. HFEC INSPECTED SURROUNDING FASTENER HOLES AND TRIMMED OUT AREA. INSTALLED REPAIR DOUBLERS AND FILLERS. PLANNING TO CONTACT ENGINEERING AFTER 3000SDR UALA2012070303567Door · out of positionA & K LAV O2 MASK DOORS DID NOT OPEN DURING MASK DROP. CONNECTED QUICK DISCONNECT FOR A LAV O2 MASK DOOR. REPOSITIONED O2 MASK DOOR OF K LAV BOTH LAV O2 MASK DOORS OPEN IAW MM.SDR UALA2012070303568Wire · disconnectedEMERGENCY LIGHT AT FWD CLOSET IS INOPERATIVE. CONNECTED EMERGENCY LIGHT, OPS CHECKED GOOD.SDR UALA2012070303564Floorbeam · corrodedAFT CARGO BAY FLOOR STRUCTURE, AFT SIDE OF FRAME AT BS 1380 HAS CORROSION FROM RBL 13 TO RBL 17. REMOVED CORROSION OUT OF SRM LIMITS ON THE END OF FRAME. HFEC INSPECTION SURROUNDING FASTENER HOLES AND REWORKED AREA, TREATED, PRIMED, INSTALLED FASTENERS PER ESDR UALA2012070303544Skin · damagedEXTERIOR UPPER FUSELAGE STA 1450 SPLICE BETWEEN STR 3L AND 4L HAS A BLENDED OUT AREA. MAJOR REPAIR ACCOMPLISHED. TRIMMED OUT AREA, INSTALLED REPAIR DOUBLERS AND FILLERS.SDR UALA2012070203533Valve · malfunctionedRIGHT ENGINE HI STAGE EICAS MSG ON TAKEOFF ROLL. ABORTED TAKEOFF AT 80 KTS. CREW STATES DURING TAKEOFF ROLL LIGHT CAME ON APPX 40-50 KTS LIGHT DID NOT EXTINGUISH AND FINAL SPEED REACHED WAS APPROX 80-90 KTS WHEN TAKEOFF ABORTED. COMPLIED WITH MEL 3611D. RE
Back to Boeing 757-222