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 FDEA2019101092539Striker · delaminatedLMLG DOOR AFT UPSTOP PAD IS WORN. REMOVED AND REPLACED STRIKER PLATE IAW SRM 51-10-02, DWG 149N6002, AND SRM 51-70-06-0G. REMOVED DAMAGED PLIES AND BONDED REPAIR IAW 5010, SRM 51-70-06-0G, AND SRM 52-80-02-2R. SEALED PLATE IAW SRM 51-20-05. RESTORED FINISH SDR FDEA2019101092532Slat Track · corrodedLEFT WING NR 4 SLAT INBD TRACK WORN AND PITTED. REMOVED AND REPLACED THE NR 4 SLAT INBOARD TRACK IAW AMM 27-81-12-4. ADJUSTMENT AND OPS CHECK ACCOMPLISHED ON SNRM N00108.SDR FDEA2019101092529Wedge · corrodedLEFT WING NR 5 SLAT LOWER T/E WEDGE WAS DELAMINATED AT THE INBD AFT CORNER. REPLACED THE SLAT.SDR FDEA2019101092527Attach Angle · corrodedRIGHT WING NR 9 SLAT LOWER T/E WEDGE ATTACH ANGLE IS CORRODED AND THE T/E WEDGE WAS BULGING WITH FASTENERS PULLING THROUGH AT THREE LOCATIONS. REPLACED THE SLAT.SDR FDEA2019101082502Skin · dentedAPU COMPARTMENT RT DOOR OUTER SURFACE IS CREASED. REPAIRED APU RT DOOR OUTER SKIN IAW EA F-5240-T0349703.SDR FDEA2019101082501Skin · dentedAPU COMPARTMENT LT DOOR OUTER SURFACE IS BULGED. REPAIRED APU DOOR OUTER SURFACE IAW EA F-5240-T0349685.SDR FDEA2019101082499Skin · dentedETERIOR FUSELAGE SKIN IS DENTED AT APPROX BS 1630 ON STR17R. REMOVED EFECTED FASTENERS PREFORMED HFEC TO OPEN HOLES AND EFECTED AREA FOUND NO CRACKS. OVERSIZED OPEN HOLES AND INSTALLED NEW FASTENERS IAW EA F-5330-T0349901.SDR FDEA2019101122585Skin · corrodedFWD CARGO DOOR LOWER SKIN CORROSION ON INTERNAL SKIN REMOVED CORROSION ON LOWER INNER SKIN AT LOCATIONS 12" AND 18" FROM FORWARD EDGE AND 12" FROM AFT EDGE AND FOUND TO BE OUTSIDE LIMITS IAW SRM 52-30-01-1A FIG 101 DETAIL V, MAX ALLOWABLE BLEND = 0.006" SDR FDEA201909182278Battery Pack · dischargedMDIS 935 33-50 8397 18SEP19 ABE FACT U L1 DOOR EMERGENCY EXIT LIGHT INOP ON POST FLIGHT CHECK. FACT 18SEP19 15:33 ABE REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY PACK. REF AMM 33-51-07-2. OPS CHECK GOOD. NEW BATTERY PACK MPN -2013-1ASMI, S/N 4286SDR FDEA2019101192588Support · corrodedFORWARD CARGO DOOR EVIDENCE OF BULGING OF LEVELING COMPOUND AT LOWER DOOR AREA REMOVED LEVELLING COMPOUND, CORROSION FOUND AT LOWER DOOR INNER SKIN ,EDGE BEAM AND SPLICES, AND TEE SUPPORTS AT BS 580, BS 589 AND BS 600. COROSION REMOVED AT DOOR INNER SKIN SDR FDEA2019101192587Tee Fitting · corrodedFORWARD CARGO DOOR EVIDENCE OF CORROSION ON DOOR INNER SKIN AT LOWER CUTOUT AREA 12" FROM FORWARD EDGE OF CARGO DOOR COROSION REMOVED AT DOOR INNER SKIN AT LOWER CUTOUT AREA LOCATED 12" FROM FORWARD EDGE OF DOOR AND,AREA FOUND TO BE OUTSIDE LIMITS IAW SRM SDR FDEA2019101192586Skin · corrodedFORWARD CARGO DOOR EVIDENCE OF CORROSION ON DOOR INNER SKIN AT LOWER CUTOUT AREA 12" FROM AFT EDGE OF CARGO DOOR COROSION REMOVED AT DOOR INNER SKIN AT LOWER CUTOUT AREA LOCATED 12" FROM AFT EDGE OF DOOR AND,AREA FOUND TO BE OUTSIDE LIMITS IAW SRM 52-30-01SDR FDEA201908141881Slat · delaminatedPER EA F-5750-E033693 REV B P9 STEP 6 #9 LE SLAT TO BE REMOVED AND REPAIRED/REPLACED DUE TO DELAMINATION FOUND ON PREVIOUS REPAIRS. (REF WRI 57-50/7700) COMPLETED OPS CK AND TEST OF SLAT LE SYSTEM REF. AMM 757-200-27-81-02SDR FDEA2019081541880Skin · delaminatedDELAMINATION FOUND ON THE NR 6 SLAT PREVIOUS REPAIRS. IAW EA F-5750-E033693 REV B P9 STEP 6, THE NR 5 LE SLAT REMOVED, REPAIRED AND REPLACED.SDR FDEA2019081541881Skin · delaminatedDUE TO DELAMINATION FOUND ON PREVIOUS REPAIRS OF THE SLAT. IAW EA F-5750-E033693 REV B P9 STEP 6 REMOVED, REPAIRED, AND REPLACED.SDR FDEA201907231672Rvdt · out of adjustAIRCRAFT ROLLS RIGHT AT LIFTOFF. AIRCRAFT ROLLS 1 UNIT LEFT DURING FLIGHT WHEN THE FLIGHT SPOILERS ARE DEPLOYED. TROUBLESHOT PER FRMFIM 27-61 FAULT TREE 804, STEP 1 CLEARANCE CHECKS CHECKED NORMAL. STEP 2 FOUND #7 SPOILER PCA RVDT OUT OF TOLERANCE. ADJUSTSDR FDEA201907081509Battery · dischargedDURING PRE-DEPARTURE CHECK, FOUND NUMEROUS EMERGENCY EXIT SIGNS AND R1 EXTERIOR LIGHT INOP. ATTEMPTED TO CHARGE EMERGENCY LIGHT BATTERIES USING SHIP'S POWER FOR 1 HOUR. NO HELP. REMOVED AND REPLACED #2 EMERGENCY LIGHT BATTERY ASSY IN REF TO AMM 33-51-07-2. SDR FDEA201906261414Reservoir · failedDURING L ENTRY DOOR DISARM, F.O. NOTED THAT DOOR LIGHT WAS EXTINGUISHED AND "KNUCKLEBUSTER" WAS RETRACTED AFTER MOVING ARMING HANDLE TO DISARMWHEN HE TRIED TO CRACK THE DOOR, HE NOTICED THAT THE DOOR JAMMED AND THE ARMING HANDLE WAS CLOSER NOW TO ARMED THAN DISDR FDEA201905161081Computer · malfunctionedAUTO THROTTLES WOULD NOT ENGAGE ON TAKE OFF. REJECTED T/O AND RETURNED TO GATE AFTTER CALLING GOC/MOC RELEASED FOR SERVICE PER MEL : 22-30-01 CATEGORY : C EXPIRATION : 26MAY19 "MEL 22-30-01: THRUST MANAGEMENT SYSTEM/AUTOTHROTTLE SYSTEM - INOP." THRUST MANAGEMESDR FDEA201903090565Guide Arm · out of positionUNABLE TO CLOSE L1 DOOR. FOUND GUIDE ARM CAM FOLLOWER PINS OUT OF TRACK AND BOLTS BACKED OUT OF SUPPORT BRACKET AT SERRATED PLATE. REINSTALLED GUIDE ARM PER AMM 52-11-04-2.SDR FDEA201902220479Sensor · obstructedRIGHT ENTRY DOOR DOESN'T SHOW OPEN ON EICAS. FOUND SENSOR S10090 PLUNGER ON RIGHT ENTRY DOOR COVERED WITH ICE, CLEARED ICE AWAY AND DOOR OPS CHECKS GOOD PER AMM 52-71-00-5.SDR FDEA201902150419Warning Message · false activationTE FLAP DISAGREE EICAS MSG WHEN SELECTING FLAPS 25. COMPLIED WITH QRH AND LANDED WITH FLAPS 20. PERFORMED FSEU BITE CHECK IAW 757 FIM 27-51 FIG104B. NO EXISTING FAULTS AND BITE CHECK GOOD ON ALL 3 UNITS. CHECKED TRANSMISSIONS FOR TRIPED INDICATORS ANDSDR FDEA201812053438Handle · looseL1 CREW ENTRY DOOR HANDLE LOOSE. FOR CLARITY, THE DOOR ASSIST HANDLE IS LOOSE, NOT THE DOOR CLOSING HANDLE. FOUND UPPER BOLT LOOSE ON ASSIST HANDLE AND RESECURED BOLT AND REINSTALLED ASSIST HANDLE REF AMM 51-11-00-0. OK FOR SERVICE.SDR FDEA201811283390Slide · detachedDURING DE-PLANING, L1 DOOR DISARM WHILE RAMP PERSONAL WERE OPENING L1 DOOR ESCAPE SLIDE DETACHED FROM HOUSING. REVERSED MEL AND RE-INSTALLED L-1 DOOR ESCAPE SLIDE IAW AMM 25-66-01-4 AND SAFETY PIN REMOVED. GIRT BAR ANDSDR FDEA201811143213Warning System · false activationTE FLAP DISAGREE EICAS MSG. CYCLED FLAPS 3 TIMES, NO FAULTS AND ALL INDICATIONS NORMAL PER FIM 27-51 FAULT TREE 803. ALSO REVIEWED TECH TIP 18-0042. OPS CK NORMAL, A/C OK FOR SERVICE.SDR FDEA201809292745Not Reported · malfunctioned2ND ATTEMPT, AC HELD STATIONARY TO APPROX 1.15 EPR. BRAKES RELEASED AND AIRCRAFT PRECEDED TO THE RIGHT. FULL LEFT RUDDER APPLIED AND AIRCRAFT DID RESPOND TO INPUT. T/O WAS ABORTED AT LOW SPEED. PILOT DEBRIEF REVEALED PROBLEM WITH RUDDER STEERING WHILE TAXING OSDR FDEA2018100282743Strut · not reported2ND ATTEMPT- AC HELD STATIONARY TO APPROX 1.15 EPR. BRAKES RELEASED AND AIRCRAFT PRECEDED TO THE RIGHT. FULL LEFT RUDDER APPLIED AND AIRCRAFT DID RESPOND TO INPUT. T/O WAS ABORTED AT LOW SPEED SUSPECT OVERSERVICED NOSE GEAR IN CONJUNCTION WITH A VERY FULL AFTSDR FDEA201809052351Detector · inoperativeWHILE PRE FLIGHTING AIRCRAFT WITH APU RUNNING AND PACKS ON, RECEIVED WHEEL WELL FIRE WARNING. AIRCRAFT WAS EVACUATED AND FIRE TRUCKS CALLED. NO APU AIR DUCT LEAKS NOTED REF WDM 26-17-11, FOUND RIGHT WHEEL WELL DETECTOR ELEM T205 WITH LOW RESISTANCE FROM THE CESDR FDEA2018080761930Attach Bracket · crackedAFT CARGO BAY, BS 1420 - 1440, BETWEEN STRINGERS 28R - 29R INTERCOSTAL FWD ATTACH BRACKET WAS FOUND CRACKED.SDR FDEA2018080311880Doubler · corrodedCORROSION ON FRAME DOUBLER STA 730 S- 5L.SDR FDEA201804050857Coupling · leakingABOUT 25 MINUTES INTO FLIGHT, RECEIVED A RT ENGINE OVERHEAT EICAS MESSAGE & RT ENGINE OVERHEAT LIGHT. COMPLIED WITH QRH AND LIGHT WENT OUT AFTER ABOUT 3 MINUTES WITH RIGHT THRUST LEVER AT IDLE. ALL ENGINE INSTRUMENT INDICATIONS WERE NORMAL. LANDED WITH RSDR FDEA201803220754Detector · malfunctionedFL380/.80 MACH RT ENGINE OVERHEAT. RAN QRH REDUCED RT THRUST LEVER TO IDLE OPERATED REMAINDER OF FLIGHT WITH REDUCED THRUST ON R ENGINE (BELOW1.3 EPR). REMOVED AND REPLACED RIGHT ENGINE NACELLE OVERHEAT DETECTORS TS5074 AND TS5073 IAW AMM 26-11-01-4. RAN THESDR FDEA201803060601Bottle · emptyAT BLOCK IN FOUND WHEN THE L1 DOOR WAS CRACKED OPEN. WHEN RAMP AGENT TRIED TO OPEN THE DOOR, THE GIRT BAR JAMMED IN OPENING. THE L1 DOOR WAS STUCK HALFWAY OPEN. INSPECTED THE DOOR IAW MM 52-11-00-6. THE GIRT BAR ENGAGES AND DISENGAGES NORMALLY. OPS CHECSDR FDEA201802130380Fitting · crackedMAIN CABIN BELOW FLOOR, SEEN FROM FWD CARGO BAY. FLOOR BEAM STUB FITTING CRACKED, AFT FLANGE BS 580, LBL 45. COMPLIED WITH EA F-5310-T0338208, P1.SDR FDEA201802200380Fitting · crackedMAIN CABIN BELOW FLOOR SEEN FROM FWD CARGO COMPT FLOORBEAM STUB FITTING CRACKED AFT FLANGE STA 580 LBL.45. COMPLIED WITH EA F-5310-T0338208 P1. FUSELAGE MAINFRAME STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.SDR FDEA201711243304Power Supply · failedDURING A POST FLIGHT, FOUND THE R1 DOOR SLIDE EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE POWER SUPPLY IAW AMM 33-51-07-2, PAR 5,6. OPS CHECKED GOOD. ACFT OK FOR SERVICE.SDR FDEA201709222676Gust Lock · crackedL1 DOOR GUST LOCK COLLAR BROKEN. R & R THE L1DOOR HOLD OPEN LOCK COLLAR IAW MM 52-11-08-8.SDR FDEA201709202657Firewall · gougedAPU BAY RT SIDE FIREWALL HAS A GOUGE. ON EVALUATION FOUND THE APU FIREWALL TO BE 100% MATERIAL LOSS IAW IAW SRM 53-80-08-1A. REPAIRED THE FIREWALL IAW SRM 53-80-08-2R REPAIR 2.SDR FDEA201709072465Light · inoperativeSLIDE ARM LIGHT DOES NOT WORK ON DOOR L1. REF TO MEL 52-11-01-A WRI 52-10/6642.SDR FDEA201708292409Stringer · corrodedAFT CARGO, CORROSION ON THE UPPER SECTION OF STRINGER 29R, BS 1410. FOUND OUT LIMIT IAW SRM 53-00-03-1A FIG.101 , REMOVED AND REPLACED THE STRINGER IAW SRM 53-00-03-1A, FIG 101 , 51-4040-02-OG AND DWG 146N3300 REV. F.SDR FDEA201708252357Beam · crackedSTUB BEAM AT BS 580 IS CRACKED. REMOVED AND REPLACED STUB BEAM IAW SRM 51-40-02-0G, AND DWG 657N4311, REV -.SDR FDEA201706211727Warning System · false activationON CLIMBOUT FROM KLAX PASSING 5000 IAS DISAGREE EICAS. CONTINUE CLIMB AND ALT DISAGREE EICAS ILUMINATED. COMPLETED QRH AND DIVERTED TO KLAX . NOTE: WORSE CASE SPLITS WERE APROXX 500' LOW ON FO SIDE VERSUS CAPT AND APPROX 15 KNOTS SLOWER ON FO SIDE AT FL230. CSDR FDEA201706201714Power Supply · inoperativeL1 DOOR INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY M731 AND BATTERY PACK IAW AMM 33-51-07-2. OPS CHECKED GOOD. OK FOR SERVICE.SDR FDEA201703140872Battery Pack · dischargedDURING EMERGENCY LIGHT TEST, L/H EMERGENCY EXIT SIGN AND SLIDE LIGHT WOULD NOT TEST. REMOVED AND REPLACED POSITION 1 EMERGENCY LIGHT POWER SUPPLY BATTERY PACK, OPS CK GOOD.SDR FDEA201611083902Pan · gougedL1 DOOR PAN GOUGED AT AFT LWR RADIUS. REMOVED AND REPLACED GOUGED DOOR PAN IAW SRM 51-40-02, AND DRAWING 141N6100.SDR FDEA201608032790Fitting · crackedMAIN CABIN FLOORBEAM ST 580, LBL 45.5, STUB FRAME EXISTING MOD FOUND CRACKED AT AFT FACE. R & R STUB FRAME FITTING, PN: 5316913, PO 935FB-00010 AT BS 580, LBL 45.5 IAW SRM 51-40-02-0G AND DWG: 657N4311, REV-1.SDR FDEA201608032795Intercostal · corrodedCORROSION FOUND AT MAIN EQUIPMENT CENTER INTERCOSTAL AT BS 456 O/B SIDE OF STRINGER 26L. FORMED, LOCATED AND DRILLED NEW INTERCOSTAL AT MAIN EQUIPMENT CENTER FROM BS 440 TO BS 456, OTBD SIDE OF STR 26L IAW DWG 143N822, REV A, 143N8248, REV R, SRM 51-40-05.SDR FDEA201608012714Door Frame · corrodedMAIN EQUIPMENT CENTER DOOR CUTOUT FRAME, LOWER SIDE HAS CORROSION AT STA 460, STR 30. REMOVED AND REPLACED CHORD P/N 143N8211-6 PER EA F-5310-TO327283 P1. THIS IS A MAJOR REPAIR.SDR FDEA201607252614Shear Web · crackedMAIN CABIN SHEAR WEB BS 580 LBL 46.5 FOUND CRACKED. FOUND CRACK EXTENDING FROM FASTENER HOLE. COMPLIED WITH EA F-5310-T0327046 PART 1. FUSELAGE MAINFRAME, LBL 45, SHEAR WEB CRACK AT STA 580, LBL 45.5, PERMANENT REPAIR,SDR FDEA201607132383Window · failedRIGHT FORWARD WINDOW SHATTERED IN FLIGHT. NO AIR LEAK, NO INNER PANE DEFORMATION, RT WINDOW R1 WAS REMOVED USING AMM 56-11-01-4.
INSTALLED R1 WINDOW AND TORQUED IAW AMM 56-11-01-4. AVIONICS INSTALLING INNER WINDOW TRIM, WIRING AND COMPLETING OPS CHECKS.
Back to Boeing 757-2T7