Boeing 757-204
Service difficulty reports · 676
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 = '757204' 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 = '757204' 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 WX0A2014010671810Battery Pack · inoperativeEMERGENCY LIGHTS INOPERATIVE IN CABIN AT L2 DOOR & FWD UPPER OVERWING EXITS. R & R BATTERIES IAW AMM-33-53-00. OPS CHECKED GOOD.SDR WX0A071789Skin · corrodedEXFOLIATION CORROSION FOUND ON EIGHT EACH AREAS AROUND FASTENERS, NR 8 SLAT LE SKIN. REPLACED NR 8 SLAT.SDR WX0A2014122071788Skin · damagedEVIDENCE OF FUEL SEEPAGE FROM LT WING UPPER SKIN FASTENERS, THREE PLACES AT APPROXIMATELY WS 681.5, STRINGERS 12 & 8. REPLACED FASTENERS IAW EA 757-5730-18-A5001.SDR WX0A2014122071787Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER FLANGE HAS CORROSION, 100% MATERIAL LOSS IAW SRM 53-00-01 FIG 101. REPAIRED IAW SRM 53-00-51 REPAIR 10 & EA 757-5130-18- A4997 P1, P2.SDR WX0A071786Skin · dentedAFT CARGO DOOR EXTERNAL SKIN HAS 2 DENTS ON LOWER EDGE SIDE. PART REPAIRED, LEAVE AS IS IAW EA 757-5236-18-A4989.SDR WX0A2014122000083Skin · dentedDENT IN CROWN SKIN APPROXIMATELY BS 271 AT ACFT CENTERLINE. FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 SHEET 4. REPAIRED IAW EA 757-5310-18-A6998.SDR WX0A2014122071784Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER FLANGE IS CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL 3. REPAIRED IAW SRM 53-00-51 FIG 201 REPAIR 1.SDR WX0A071785Floor Support · corrodedMAIN CABIN FLOOR STATION 1314 UPPER FLOOR SUPPORT FRAME HAS CORROSION. REMOVED CORROSION BY BLEND METHOD & REMAINING MATERIAL THICKNESS FOUND OUT OF LIMITS IAW B757-200 SRM 53-60-13 FIG 101. R & R PART IAW B757-200 SRM 51-40-05 PG 13 & SRM 51-40-02.SDR WX0A071771Battery · dischargedONE EACH AFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. R & R AFFECTED EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00-902-037 CHECKED OK.SDR WX0A071782Floorbeam · corrodedMAIN CABIN FLOOR BEAM UPPER CAP & LOWER SURFACE HAS CORROSION AT FASTENER HOLES STATION 1320 LT OTBD END. PART REPAIRED IAW B757-200 SRM 53-00-51 REPAIR 8.SDR WX0A071781Floorbeam · corrodedMAIN CABIN FLOOR BEAM UPPER CAP IS CORRODED AT STATION 1320 RBL 48 TO RBL 60. REPAIRED IAW B757-200 SRM 53-00-51 REPAIR 8.SDR WX0A071758Battery Pack · dischargedLEFT INBD AFT EMERGENCY FLASHLIGHT INOPERATIVE. R & R LT INBD AFT CABIN EMERGENCY FLASHLIGHT & BATTERY PACK IAW AMM 25-60-00, OPERATIONS CHECKED GOOD.SDR FDEA201311182818Frame · crackedFWD M.E.C. CUT OUT FRAME BS 231 ON FWD SIDE IS CRACKED. FABRICATED AND INSTALLED REPAIR IAW EA F-5310-T0303943 P1.SDR WX0A2013111300752Fuse · blownAFT LEFT POWER SUPPLY FOR EMERGENCY LIGHTS FUSE BLOWN. R & R AFT EMERGENCY POWER SUPPLY ASSY IAW MM 33-51-07. OPS CHECKED GOOD.SDR FDEA201310262622Window · failedTHE LT FWD WINDOW STARTED ARCHING IN FLIGHT. TURNED WINDOW HEAT OFF IAW THE QRH. WINDOW SHATTERED ABOUT FIVE MINUTES LATER. REMOVED AND INSTALLED NEW L1 WINDOW IAW MM 56-11-01-4 .SDR FDEA201310092454Windshield · crackedL1 WINDOW OUTER LAYER CRACKED AT FLT LV 400 -60C, AFTER 2.5 HRS OF FLIGHT. INSTALLED NEW L-1 WINDOW, FIRST TORQUE COMPLETED AT 2119Z. R & R L1 WINDSHIELD IAW AMM 56-11-01-4.SDR FDEA201309192251Power Supply · inoperativeDURING SERVICE CHECK, THE RT SIDE EMERGENCY LIGHTS INOPERATIVE DURING TEST. R & R RT POWER SUPPLY FOR THE EMERGENCY LIGHTS IAW MM REF 25-22-02. OP`S CHECKED GOOD.SDR WX0A2013090571685Battery · inoperativeFLASHLIGHT INOPERATIVE AT L2 DOOR. REPLACED BATTERY IAW MM, OPS CHECKED GOOD 25-64-00.SDR WX0A201308130002Light · inoperativeDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX REPLACED THE EMERGENCY LIGHT ASSY AS REQUIRED. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. ACFT RETURNED TSDR WX0A201308010051Light · no testDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX REPLACED EMERGENCY LIGHT ASSY. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. ACFT RETURNED TO SERVICE.SDR FDEA201307171580Structure · damagedCLIMBING THROUGH 11,000 MSL, HEARD A LOUD PRESSURIZATION BUMP. CABIN RATE CLIMBING AT 2000 FPM AND CABIN ALT CLIMBING. LEVELED AT APPROX 14000 MSL AND STARTED DESCENT TO 10,000 AT APPROX 11000 MSL CABIN, ALT 1 EICAS. COMPLIED WITH QRH, SELECTED AUTO 2 AND SDR FDEA201306261400Wire · brokenEMERGENCY LIGHT GUARD HAS BROKEN CAP WIRE. R & R EMERGENCY LIGHTS PANEL IAW MM CH 33-51-08-4 EMERGENCY LIGHTS SWITCH. CHECKED GOOD ON GROUND OK FOR SERVICE.SDR FDEA201306111250Line · leakingLOST LEFT HYD QTY AND LEFT HYD SYS PRESSURE AFTER POWER UP FOR TAKEOFF. RUDDER RATIO ON EICAS AND POWER TRANSFER UNIT ON STATUS CAME UP AS WELL. NO NOSE WHEEL STEERING AVAILABLE AFTER PTU AUTOMATICALLY CAME ON. APPEARS LOST ALL FLUID IN LEFT HYD. INSTALLSDR FDEA201306061208Slide · dislodgedWHEN THE LT DOOR OPENED THE SLIDE FELL OUT OF THE BOX. INSTALLED L1 DOOR SLIDE USING AMM 25-66-01-4. COVER INSTALLED. OPS CHECKED GOOD.SDR FDEA201305130977Crease Beam · misrepairedCREASE BEAM MISREPAIRED. REMOVED AND REPLACED CREASE BEAM LOCATED BS 1040 TO 1180 IAW SRM 51-40-02 & PG 30.SDR FDEA201305030904Girt Bar · out of adjustR1 DOOR REQUIRES OPS CHECK OF ARM AND DISARM. ADJUSTED THE R1 DOOR GIRT BAR FLOOR FITTING IAW FIM 52-11 FAULT TREE 813, AMM 52-11-25-5. R1 DOOR SLIDE ARM AND DISARM OPS CHECKS GOOD.SDR FDEA201304300888Sensor · out of adjustLT FWD ENTRY DOOR LIGHT & EICAS MESSAGE COMES ON INFLIGHT. LT FWD ENTRY DOOR WARNING SENSOR SYS ADJUSTMENT CARRIED OUT IAW AMM 52-71-00, REV 106 FOUND GOOD. TESTING OF DOOR WARNING SYS FOR NR 1 PASSENGER DOOR FOUND GOOD IAW AMM 52-71-00, REV 106.SDR FDEA201304250858Skin · damagedFOUND SCRIBE LINE ON SKIN AT BS 439.625 TO 560.875 IN LAP JOINT SEAM AT S19R. REPAIRED IAW EA 757-5331-16-F4105, REV, AND 496583220001. CAT "A" MAJOR REPAIR.SDR FDEA201304240852Skin · dentedFUSELAGE SKIN DENT AT STA 1545 BELOW STRINGER 26L. SKIN REPAIRED IAW EA 757-5361-16-F4167, REV-, AND 49659150001. CAT "B" MAJOR REPAIR.SDR FDEA201304180800Pseu · faultedAFTER NORMAL LANDING, RECEIVED NUMEROUS EICAS ALERTS THAT CLEARED BEFORE THEY COULD BE READ, BELIEVE THEY WERE DOOR RELATED. ESTIMATE IT WAS SIX ALERTS, NO CURRENT FAULTS AND PILOT STATED THAT FAULTS WERE MOMENTARY. R & R PSEU REF AMM 32-09-04-4 AS PRECAUSDR FDEA201304180799Pseu · malfunctionedDURING DESCENT, RECEIVED MOMENTARY "GEAR NOT DOWN" EICAS WARNING. ALTITUDE WAS APPROX 30,000 FT WARNING ONLY APPEARED ONE TIME AND LASTED ONLY A FEW SECONDS. NO EICAS FAULTS ON GROUND AND PILOT STATED THAT FAULTS WERE MOMENTARY IN FLIGHT. R & R PSEU REF 3SDR FDEA201304150783Spar · corrodedIAW EO F-2822-7-5009 PART 3, STEP B1. C (PAGE 16 OF 33). CORROSION AT RT AFT WING SPAR SURFACE. REMOVED AND SPAR WEB THICKNESS FOUND LESS THAN THE MINIMUM. IAW EO F-2822-7-5009, PART 3, STEP B1. C (PAGE 16 OF 33). CORROSION AT RT AFT WING SPAR SURFACE REMOVSDR FDEA201304120775Skin · damagedFOUND SCRIBE LINE AT BS 781.031 S14R. REPAIRED IAW EA F-5330-T0300304A. CAT. "B" MAJOR REPAIR.SDR FDEA201304120774Skin · damagedFOUND VERTICAL SCRIBE LINE AT BS 759.031 IN LAP JOINT SEAM AT S14R. REPAIRED IAW EA F-5330-T0300304A. CAT."B' MAJOR REPAIR.SDR FDEA201304050726Skin · dentedCARGO DOOR OUTER SKIN AFT LOWER CORNER DENTED. REPAIRED IAW EA F-5230-166052 PART 1. MAJOR REPAIR.SDR FDEA201304050727Unknown · malfunctionedREPEAT PROBLEM CAUSING GO-AROUND AND DIVERT AT 500FT AGL WITH THREE GEAR INDICATIONS DOWN AND LOCKED THE GPWS AURAL "TOO LOW GEAR" BEGAN. GO AROUND INITIATED. NO QRH RELIEF FOR SITUATION. DIVERTED FOR LOW APPROACH VISUAL GEAR CHECK, SITUATION STILL PRESENTSDR FDEA201304030718Skin · dentedFUSELAGE EXTERIOR SKIN DENTED BS 1698 AND 1 INCH BELOW S15L. REPAIRED IAW EA F-5330-162939 PART 1. MAJOR REPAIR.SDR FDEA201304030717Skin · dentedFUSELAGE EXTERIOR SKIN DENTED AT BS 1717.5 AND 0.5 INCHES BELOW S14L. REPAIRED IAW EA F-5330-162939 PART 1. MAJOR REPAIR.SDR FDEA201304030716Skin · dentedAFTER PAINTING OBSERVED FUSELAGE EXTERIOR SKIN HAS A DENT AT BS 1695 AND 1 INCH ABOVE S15L. REPAIRED IAW EA F-5330-162939 PART 1. MAJOR REPAIR.SDR FDEA201304030719Skin · dentedFUSELAGE EXTERIOR SKIN HAS A PROTRUDING DENT AT BS 746 THREE INCHES ABOVE S25R. REPAIRED IAW SRM 53-00-01, FIG.201, REPAIR 16, REV.108. CAT B, MAJOR REPAIR.SDR FDEA201304020702Stringer · corrodedAREA AFT OF AFT CARGO BS 1681-1701, S22R HAS CORROSION ON UPPER FLANGE. REPAIR CARRIED OUT ON CORRODED PART OF STRINGER S-22R AT STA 1681-STA 1701, IAW SRM 53-00-03 FIG.201 DETAIL I REPAIR 2 REV.108. REPAIR IS MAJOR.SDR FDEA201304020704Skin · gougedRT INBD MAIN FLAP WEDGE LWR SURFACE IS GOUGED BY AFT OTBD CANOE FAIRING. REPAIRED RT INBD MAIN FLAP WEDGE IAW SRM 51-70-10, REPAIR 4. MAJOR REPAIR.SDR FDEA201304020703Skin · chafedLT OUTBD FLAP, TOP INBD PANEL CHAFED. REPAIRED IAW SRM 51-70-10 FIG 201 REP 4.SDR FDEA201303290685Shear Tie · damagedFOUND 0.200 GAP IN BETWEEN SKIN AND SHEAR TIE AT BS 1701 BETWEEN STRINGER 15 - 16 LEFT, ONLY ALLOWED FOR UP TO 0.040 MAXIMUM GAP. REMOVED AND REPLACED WITH NEW SHEAR TIE FABRICATED AS PER DWG 140N2002 SHT.4 REV.B AND INSTALLED AS PER DWG 146N1026 SHT.2 REVSDR FDEA201303290696Light · inoperativeR1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R LIGHT IAW AMM 33-51-06-2-1. OPS CHECKED OK.SDR FDEA201303290689Crease Beam · crackedAT STA 1140 LT SIDE CREASE BEAM HAS A CRACK THAT BROKEN IN TWO AT STATION 1140, LT SIDE, CREASEBEAM WAS CRACKED AT FASTENER HOLE, WHICH IS NOT ALLOWED IAW SRM 53-40-13, FIG. 101, NOTE "D", PAGE 102. R & R CREASEBEAM IAW SRM 51-40-02, DWG 144N5214, BS 1140, WLSDR FDEA201303280682Crease Beam · corrodedCABIN RT FLOOR CREASE BEAM HAS CORROSION AND CRACKS FROM STA 1560 -1640, RBL 64.SDR FDEA201303280681Crease Beam · corrodedCABIN RT FLOOR CREASE BEAM HAS CORROSION AND CRACKS FROM STA 1560 -1640, RBL 64.SDR FDEA201303280683Crease Beam · corrodedCABIN RT FLOOR CREASE BEAM HAS CORROSION AND CRACKS FROM BS 1580-1640, RBL64. FOUND OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DETAIL VII. R & R CREASE BEAM WITH A NEW ONE, FABRICATED IAW SRM 51-40-02 & DWG 146N5590, BS 1580-1640, RBL64 CAT "A", MAJOR REPSDR FDEA201303260657Skin · dentedFUSELAGE EXTERIOR SKIN HAS A DENT AT BS 1700 AND 1 INCH ABOVE S15L. REPAIRED IAW EA F-5330-162939 PART 1. MAJOR REPAIR.
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