Boeing 757-2T7
Service difficulty reports · 666
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 = '7572T7' 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 = '7572T7' 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 FDEA201607052277Unknown · malfunctionedLOSS OF PRESSURIZATION AT FL 390 FOLLOWING LOSS OF RT ENG BLEED DECLARED EMERGENCY AND DECENDED TO 10,000. PERFORMED RUNUP AND TEST OF BLEED SYSTEMS ON BOTH ENGINES REF MM 36-11-00-5. BOTH BLEEDS PASSED TESTS. PRESSURES AND TEMPS WERE NORMAL DURING AN EXTENSDR FDEA201604301435Track · dirtyLEFT ENTRY DOOR DOES NOT LOCK & ARM PROPERLY. CLEANED & LUBED L1 DOOR GIRT BAR TRACK. OPERATIONS CHECKED NORMAL.SDR FDEA201604211333Girt Bar · dirtyWHEN CLOSING L1 DOOR, GIRT BAR AGAIN CAME LOOSE & DOOR SLIDE WOULD NOT ARM. FOUND GIRT BAR & SLIDES DRY & DIRTY. CLEANED & LUBRICATED SAME, REINSTALLED SLIDE, BUSTLE & GIRT BAR. CHECKS OK IAW 55-66-10-2. ACFT OK FOR SVC.SDR FDEA201604201311Girt Bar · dirtyWHEN CLOSING L1 DOOR, GIRT BAR AGAIN CAME LOOSE & DOOR SLIDE WOULD NOT ARM. FOUND GIRT BAR & SLIDES DRY & DIRTY. CLEANED & LUBRICATED SAME, RE-INSTALLED SLIDE, BUSTLE, & GIRT BAR.SDR FDEA201604201310Girt Bar · out of positionWHILE ATTEMPTING TO CLOSE THE ENTRY DOOR, NOTICED THE SLIDE & GIRT BAR HAD PARTIALLY COME OUT OF THE DOOR. INSTALLED GIRT BAR.SDR FDEA201604191258Proximity Switch · failedR1 ENTRY DOOR SLIDE ARMED LIGHT DOES NOT ILLUMINATE WHEN MOVING HANDLE TO ACTIVATE. R & R R1 DOOR FWD GIRT BAR PROXIMITY SWITCH S10216 IAW AMM 25-66-11-2. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.SDR FDEA201604151225Hinge · brokenRAMP WAS DOING TRAINING ON JET & REPORTED L1 DOOR SLIDE COVER CAME LOOSE. ON INSPECTION FOUND TOP FWD HINGE OF COVER IS BROKEN. PLACED COVER ON ORDER. ITEM WILL REQUIRE COMPOSITE REPAIR IAW WRI 25-60 5905. COMPLIED WITH EA F-2560-T0324743 PT 1 SLIDE COVER SDR FDEA201604131196Girt Bar · dirtyRIGHT FWD ENTRY DOOR SLIDE ARM & DISARM LEVER REQUIRES NUMEROUS ATTEMPTS TO ARM DOOR, IN ORDER TO ACTIVATE SLIDE ARM LIGHT. OLD DISCREPANCY 937 25-60 0005899. CLEANED AND LUBED R1 GIRT BAR AND FLOOR FITTINGS PER AMM 25-66-01-4. CHECKED OPERATION OF ARMING ASDR FDEA201602260696Valve · failedTOTAL LOSS OF CABIN PRESSURE AT FL 390. PREVIOUS HISTORY OF CABIN PRESSURE PROBLEMS. RT ENGINE BLEED & ASSOC EICAS LIGHT ILLUMINATED. FOLLOWED APPROPRIATE QRH. PNEU DUCT PRESSURE, RT SIDE, SLOWLY BUT STEADILY DECREASED & THEN EICAS ILLUMINATED. THEN SUBSESDR FDEA201602230675Bleed Air Sys · malfunctionedAPPROXIMATELY 30 MINUTES AFTER LEVEL OFF, AT FL400 EICAS LT BLEED OFF. COMPLIED WITH QRH, CABIN ALTITUDE MAINTAINED APPROX 30 MINUTES LATER RT BLEED OFF. RAN QRH AFTER COMMENCED DESCENT FROM FL400 TO 10,000, GOT CABIN ALT EICAS, RAN QRH, O2 MASK ON. RESETSDR FDEA201509032782Skin · damagedLIGHTNING STRIKE AT FACTORY SPLICE, BS 660, BETWEEN STRINGERS 28 - 29R. REPAIRED IAW EA F-5330-TO319956 P1.SDR FDEA201509032781Seat Track · corrodedCOURIER SEAT RBL 10, SEAT TRACK CORRODED. COMPLIED WITH EA F-5310-138503 P2.SDR FDEA201509022760Skin · damagedLIGHTNING STRIKE LOCATED LOWER FUSELAGE STATION 514, STRINGER 28R. BLENDED LOWER FUSELAGE IAW SRM 53-00-01-2R, OUT OF LIMITS IAW SRM 53-00-01-1A. REPAIRED AREA IAW SRM 53-00-01-2R REPAIR 15.SDR FDEA201509022755Skin · damagedLIGHTNING STRIKE LOWER SKIN BS 549, STRINGER 28R. COMPLIED WITH EA F-5330-T0319926 P1.SDR FDEA201508292719Frame · dentedBS 321.25 FRAME DENTED AT BL 0, FWD E & E BAY DOOR CUT OUT. COMPLIED WITH EA F-5310-T0319779 P1.SDR FDEA201508042459Proximity Sensor · obstructedWITH R1 DOOR CLOSED & ARMED SLIDE ARM, LIGHT ABOVE DOOR WILL NOT ILLUMINATE. INSPECTED R1 DOOR GIRT BAR PROX SENSOR & TARGET FOUND DEBRI & SEALANT, GREASE STUCK BETWEEN BOTH THE SENSORS & TARGETS WITH DOOR CLOSED & ARMED. CLEANED BOTH SIDES GIRT BARS & SENSOSDR FDEA201507292437Proximity Sensor · obstructedR1 DOOR IS NOT ARMING WHILE FULLY CLOSED. TROUBLE SHOT IAW FIM 25-66-00 FAULT TREE 802. FOUND BOTH GIRT BAR PROX SENSORS COVERED IN GREASE. CLEANED SENSOR, NO HELP. SUSPECT ONE OF THE PROX SENSORS BAD. OPERATED R1 DOOR, SEVERAL ARMING & DISARM CYCLES. OPSDR FDEA201507232346Proximity Sensor · dirtyR1 DOOR IS NOT ARMING WHILE FULLY CLOSED. CLEANED GIRT BAR PROXIMITY SENSORS.SDR FDEA201507112216Fitting · wornDOOR VERY DIFFICULT TO CLOSE & ARM. R & R THE FWD & AFT DOOR LATCH FITTINGS DUE TO WEAR IAW AMM CH 52-11-37-4, ALSO ADJUSTED THE CENTERING GUIDE PIN IAW AMM CH 52-11-00-5. DOOR CLOSES PROPERLY & ARMS NORMALLY. CHECKED GIRT DOOR MECHANISM IAW AMM CH 52-11-25SDR FDEA201507072161Stop · looseLEFT ENTRY DOOR SLIDE WON'T ARM WHILE T/R COMPARED THE STOP THAT WAS INDICATED AS BEING LOOSE ON THE L1 DOOR WITH THE RT DOOR IT ALSO HAD PLAY IN IT. FOUND THAT THE CAMS WHERE NOT LINING UP WITH THE SLOT ON THE GIRT BAR SLID LOCKS SO DID THE GIRT BAR MECHANISDR FDEA201507012138Girt Bar · disconnectedFOUND GIRT BAR ON DOOR L1 DISCONNECTED FROM FWD SIDE OF MECHANISM. REINSTALLED GIRT BAR SLIDER L1 DOOR SLIDE. CHECKED GOOD IAW MM 25-66-10-2.SDR FDEA201506041694Hydraulic Line · blownCLIMBING THROUGH 13000 FT, EICA LT HYD QTY ON STATUS PAGE. LT HYD QTY WAS BELOW .48 & WAS CONTINUING TO GO LOWER. RETURNED & LOWERED LG WHILE WE STILL HAD FLUID. ALT LE & TE FLAP EXTENSION. UNEVENTFUL LANDING, NO NWS SO TOW IN TO GATE OF RUNWAY. NOTE, HYDSDR FDEA201504221274Servo · malfunctionedAFTER TAKEOFF RUDDER STARTED CYCLING LT TO RT. RUDDER CYCLE BECAME MORE VIOLENT THE FASTER WE WENT. SLOWED TO 220KTS & LEVELED OFF AT 15000'. STATUS MSG, RUDDER PCU. NO QRH TO LOOK AT, RETURNED TO LAND. REPLACED YAW DAMP MODULE & YAW DAMP SERVO.SDR FDEA201504191260Girt Bar · unsecureL1 DOOR GIRT BAR PARTIALLY HANGING OUT WITH A METAL PIECE LOOSE & UNATTACHED ON ENTRY DECK. RELEASED FOR SERVICE IAW MEL 52-11-01-A CATEGORY B EXPIRATION 18 APR 15 MEL 52-11-01-A. L1 DOOR SLIDE MISSING. DOOR SLIDE REMOVED & PLACED IN HOLD BEHIND RCB. INSTALSDR FDEA201504161243Window · unsecureDURING TAKEOFF, LT WINDOW CAME OPEN AT 40 KTS, STOPPED & CLOSED WINDOW, TAXIED BACK FOR TAKEOFF. CAPTAIN CLOSED & LATCHED LT SLIDING WINDOW BEFORE TAKEOFF. VERIFIED THAT THE LT SLIDING WINDOW WAS CLOSED & LATCHED UPON ARRIVAL. NO HISTORY LAST 90 DAYS. OKSDR FDEA201502210563Girt Bar · deployedL1 ESCAPE SLIDE GIRT BAR DEPLOYED. R & R GIRT BAR IAW AMM 25-66-10-2.SDR FDEA201502120521Contact · dirtyON CLOSING & ARMING THE L1 DOOR, WE DID NOT OBSERVE THE SLIDE LIGHT ILLUMINATE. OUND CONTACTS AT SLIDE LIGHT DIRTY.CLEANED CONTACTS REINSTALLED SLIDE LIGHT, OPS CHECK GOOD IAW S.M.P.SDR FDEA201502100509Light · inoperativeLEFT EXTERIOR EMER LIGHT INOPERATIVE ON POST FLIGHT. RELAMPED LT EXTERIOR EMER LIGHT IAW MM 33-51-06-02-1. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.SDR FDEA201501130158Indicator · poppedON FINAL PLACED FLAPS FROM 15 DEGREES TO 20 DEGREES. RECEIVED TE FLAP DISAGREE EICAS. THE FLAP HANDLE WAS IN 20 DEGREE DETENT WITH 17.5 APPROX FLAPS INDICATED ON FLAP INDICATOR. COMPLETED QRH PROCEDURE & LANDED FLAPS 20 VREF 20. TROUBLE SHOT IAW FIM 27-51SDR FDEA201410193301Slide · unsecureUPON OPENING RT FWD ENTRY WITH DOOR DISARMED THE ESCAPE SLIDE FELL OUT OF COMPARTMENT ONTO STAIR SURFACE. R & R R1 DOOR ESCAPE SLIDE IAW MM 25-66-01-4. ALSO SERVICED PAX DOOR EMER POWER RESERVOIR IAW MM 12-15-10-3.SDR FDEA201408012034Skin · delaminatedLEFT WING INBD TE AFT FLAP UPPER SURFACE TABS DELAMINATED AT APPROX WS 200. REMOVED DAMAGED AREA. SANDED, CLEANED & PREPPED. APPLIED REPAIR, REFINISHED & TOP COATED IAW SRM 51-70-04 PARA 4G AMM 51-21-10-7.SDR FDEA201407281993Skin · crackedNR 1 ENGINE INBD AFT THRUST REVERSER HAS A CRACK IN THE SKIN. REPAIRED IAW EA F-5450-T0309968.SDR FDEA201407251978Skin · dentedLOWER FUSELAGE SKIN HAS A DENT AT BS 1666 BETWEEN STRINGERS 24 - 25L. REPAIRED IAW EA F-5330-T0309871 PT 1.SDR FDEA201407191869Skin · damagedRIGHT SIDE OF FUSELAGE HAS A CREASE AT BS 1530 BETWEEN STRINGER 24R & 25R. CUTOUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR DOUBLER IAW B757 SRM 51-40-02, 53-00-01 REPAIR 16, 51-20-01, & 51-40-08.SDR FDEA201407191868Skin · dentedRIGHT SIDE OF FUSELAGE HAS A DENT AT BS 1495 BETWEEN STRINGER 24R & 25R. CUT OUT DAMAGED SKIN, FABRICATED DOUBLER AND INSTALLED REPAIR DOUBLER AT BS 1495 BETWEEN STR 24R - 25R IAW B757 SRM 53-00-01 REPAIR 16, 51-40-02, 51-20-01 & 51-40-08.SDR FDEA201407171841Skin · dentedLOWER FUSELAGE SKIN HAS A DENT AT BS 1582 BETWEEN STRINGERS 27 & 28L. CUT OUT DAMAGE. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM REV112 53-00-01 REPAIR 16, 51-40-02, 51-20-01 AND 51-40-05.SDR FDEA201407171837Skin · gougedLOWER FUSELAGE IS GOUGED AT BS 612 STRINGER 26R. COMPLIED WITH EA F-5330-TO309868 REV NR PSP1 FUSELAGE PLATES & SKINS STATION 612 STRINGER 26R AT C1 DOOR CUT OUT GOUGE.SDR FDEA201406121458Coupling · lack of lubeRECEIVED TE DISAGREE DURING APPROACH TO LANDING. CONFIGURATION STOPPED AROUND 17 - 18 DEGREES. TROUBLE SHOT FLAP DISAGREE IAW FIM WITH NO MSG ON EICAS OR FSEU. GREASED TORQUE TUBE COUPLINGS & LIMITERS IAW AMM. PERFORMED OPERATIONS CHECK OF FLAPS IAW AMM WISDR FDEA201402150325Seal Depressor · damagedUNABLE TO ARM 1R DOOR, COULD NOT OPEN DOOR WITH HANDLE. FOUND IN THE UPPER FWD CORNER ABOUT A 3 INCH SECTION PEALING & JAMMING THE DOOR. REMOVED DAMAGED UPPER SEAL DEPRESSOR SEGMENT. FABRICATED NEW SEAL DEPRESSOR CORROSION PROTECTED REPAIR SEGMENT IAW SRM. SDR FDEA201312283064Seal · out of positionFOUND ACOUSTIC SEAL OUT OF TRACK ON L1 DOOR. REINSTALLED ACOUSTIC SEAL IN TRACK IAW MM 25-21-06-4.SDR FDEA201312203027Slide · inoperativeLEFT FWD CABIN DOOR WAS NOT DISARMED PROPERLY BEFORE BEING OPENED FROM INSIDE, SLIDE FELL ONTO CREW STAIRS. L1 DOOR SLIDE INOPERATIVE. R & R EMERGENCY POWER RESERVOIR BOTTLE FOR L1 DOOR IAW AMM 12-15-10-3. R & R L1 DOOR SLIDE PACK ASSEMBLY IAW AMM25-66-01-SDR FDEA201310262623Controller · failedLEFT FORWARD WINDOW HEAT ELEMENT GLOWING, SPARKING ENROUTE. TURNED OFF LT FWD WINDOW HEAT ARCING CEASED. R & R THE L1 WINDOW HEAT CONTROLLER PER MM 30-41-01-4.SDR FDEA201309112178Bulb · inoperativeEMERGENCY EXIT UNARMED LIGHT HALF UNLIT. REPLACED BULBS AND CHECKED NORMAL.SDR FDEA201308171925Lamp · burned outLEFT FWD ENTRY DOOR SLIDE LIGHT INOPERATIVE. REPLACED LAMPS, OP CHECKED GOOD.SDR FDEA201306151296Gust Lock · inoperativeDOOR GUST LOCK INOPERATIVE. INSTALLED NEW L1 DOOR HOLD OPEN LOCK. OPS CHECKED NORMAL IAW MM-52-11-08-8.SDR FDEA201305060925Circuit Card · failedLT ENGINE OVERHEAT AT CRUISE (FLT 380). HAD ASSOCIATED CAUTIOM LIGHT, EICAS AND MASTER CAUTION . PERFORMED QRH PROCEDURE INCLUDING ENG SHUTDOWN. LIGHT REMAINED ON ENTIRE TIME. CREW ADVISED THAT ENG WAS SHUTDOWN APPROX 1 HR WITH ENGINE OIL PRESS AT 7 TO 9 PSDR FDEA201302150355Light · missingLT SLIDE ILLUMINATION LIGHT IS MISSING (LIGHT IS 1" SQUARE) (ARMED LIGHT) ORIGINAL PLAN DATE WAS ENTERED. RELEASED FOR SERVICE IAW MEL: 25-66-05-A CATEGORY: C EXPIRATION: 18FEB13 "MEL 25-66-05-A: L1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS- INOP VERIFY AND RESDR FDEA201212204342Unknown · unknownTWICE, A LOWER ALTITUDE WAS SELECTED AND ACFT FAILED TO DESCEND, OVER RODE WITH VERTICAL SPEED. COULD NOT CONFIRM ANY FAULTS LAST FLIGHT. NO PREVIOUS HISTORY PAST 30 DAYS. PERFORMED MCDP GROUND TESTS 30 & 40 IAW MM 22-00-02-2. NO DISCREPANCIES NOTED. OK SDR FDEA201209113286Line · leakingLOST LEFT HYD QTY IN FLIGHT. COMPLETED ALTERNATE GEAR EXTENSION AND ALTERNATE FLAPS EXTENSION. R & R PRESSURE AND RETURN LINES ON LT MLG DOWNLOCK ACTUATOR IAW AMM 32-32-02-4 AND SMP. SERVICED LT SYS HYD RESERVIOR IAW AMM 12-12-01-3. CHECKED FILTER DPI'S. SDR FDEA201209053229Pressure Switch · failedCARGO DOOR STATUS MESSAGE RECEIVED ENROUTE. REMOVED AND REPLACED SHUTOFF VALVE PRESSURE SWITCH PER FIM 52-72-02-00. SYSTEM LEAK AND OPS CHECKED NORMAL PER AMM 52-30-00. OK FOR SERVICE.
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