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 FDEA201904171097Skin Panel · dentedDENT ON VERTICAL STABILIZER RT SIDE ON LOWER FWD PANEL, REQUIRES REPAIR IAW SRM 55-30-01AS DENTS RESULT IN DELAM REPAIRED DENT IAW SRM 55-30-01-0I FIG 1 (SHEETS 2 AND 3) AND SRM 55-30-01-2R REPAIR 5 AND SRM 51-70-10-2R REPAIR 2.SDR FDEA201904161067Panel · corrodedENG NR 2 OGV ANNULUS FORMER PANELS MISSING AT THE 6,9 AND 12 O CLOCK POSITION HAVE EVIDENCE OF CORROSION WHERE MISSING. ITEMS CURRENTLY ON OIL AS FOLLOWS: 12 O`CLOCK - 72-30 4464. 6 O'CLOCK 72-30-4323 9 O'CLOCK 73-30-4324 ANNULUS FORMER STRIPS REMOVED AND PITSDR FDEA201904161066Panel · delaminatedENG NR 2 ICE RING PANELS HAVE DE-LAM FROM THE CASING AND HAVE CORROSION UNDERNEATH. REMOVED CORROSION IAW AMM 72-34-10-8-4 AND REPLACED ICE IMPACT PANELS IAW AMM 72-34-10-358-031-R04.SDR FDEA201904151065Acoustic Liner · damagedATRITION LINER DAMAGE ON ENG NR 2 AT 6 O' CLOCK POSITION DAMAGE. REPLACED ENG NR 2 ATTRITION LINERS DUE TO CORROSION DISBOND/CORROSION BELOW IAW AMM 72-34-10-028-122.SDR FDEA201902265424Crease Beam · damagedCREASE BEAM O/B CHORD AT STA. 780 RBL 65 HAS A DOUBLE DRILLED HOLE AT FWD END OF AFT SPLICE SECTION ACCOMPLISHED FREEZE PLUG REPAIRS OF CREASE BEAM O/B CHORD AND FLOOR BEAM STA 780 RBL 65 - 70.5 IAW EA #F5310-T0345116 TITLE : FUSELAGE MAINFRAME-CREASE BSDR FDEA201902150422Splice · corrodedCORRODED CREASE BEAM SPLICE OUTBOARD CHORD STA 780 RBL 65 MAIN CABIN. REMOVED CORRODED CREASE BEAM SPLICE ON O/B CHORD STA 780 RBL 65 IN MAIN CABIN. EVAL DAMAGE FOUND 100% MAT LOSS OUT OF LIMITS FABRICATED AND INSTALLED NEW SPLICE PER DWG 143N5520 REV B AND DWSDR FDEA201902050261Floorbeam · crackedIN MAIN CABIN STUB FLOORBEAM IS CRACKED AT STA 580 LBL 45. CUTOUT AND TRIMMED ENTIRE UPPER AFT FLANGE AT STA 580 FLOOR BEAM SPLICE SEGMENT, FABRICATED REPAIR ANGLE AND RADIUS STRAP LOCATED DRILLED AND TRIMMED TO FINAL SIZE AND INSTALLED REPAIR IAW FEDEX SDR FDEA201901190176Bracket · crackedFAIRING PANEL 198AR SUPPORT STRUCTURE LOWER FWD. CORNER BRACKET FOUND CRACKED OUTSIDE PERMITTED LIMITS IAW SRM 53-00-71-1A ALLOWABLE DAMAGE FIG 101 SHEET 8. DETAIL XII REV 126. REPLACED BRACKET IAW SRM 51-40-02 REV 126.SDR FDEA201901120132Girt Bar · out of adjustPDIS 923 25-60 0328 12JAN19 CDG FACT U LOGPAGES:3011238 L SLIDE ARMED ALLUMINATION LIGHT APEARS INOP ON POSTFLIGHT FACT 12JAN19 18:03 CDG U FOUND THE LEFT DOOR GIRT BAR MECHANISM WORKING IMPROPERLY PER AMM 25-66-10-2 AND AMM 52-11-25/501 THE GIRT BAR ADJUSTED,SDR FDEA2018122643608Transmitter · failedTWO HOURS INTO FLIYHT AT FL370 EPR ON BOTH ENGINES INDICATES 1.76 HOWEVER N1 LEFT 78.1% N1 RIGHT 96.3%. EGT LEFT 500C EGT R 637C.FUEL FLOW LEFT 2.6K FUEL FLOW R 4.8K.SUSPECT BAD EPR INPUT PROM LEFT ENGINE REMOVED ASDR FDEA2018122193563Slide · dislodgedAFTER WE WERE COMPLETELY READY FOR START THE TNT FEDEX REP REENTERED THE AIRCRAFT WITHOUT US KNOWING IT. DURING THIS PROCESS OR OPENING THE DOOR "ARMED " FROM THE OUTSIDE. SEATING FOR THE SLIDE WAS PUT OUT OF ALIGNEMENT RELEASED FOR SERVICE PER MEL : 52-SDR FDEA201811283389Placard · loosePOST FLIGHT L1 DOOR SLIDE ARM/DISARM CONDITION INDICATOR RED/GREEN PLACARD LOOSE. RESECURED L1 DOOR ARM/DISARM CONDITION INDICATOR PLACARD, DOOR ARM/DISARM OPS CHK OK.SDR FDEA201811223343Light · inoperativeCOCKPIT CEILING EMERGENCY LIGHT WILL NOT TEST. RELAMPED AND OPS CHECK NORMAL REF MM 33-51-09-3. A/C OK FOR SERVICE.SDR FDEA2018111653217Girt Bar · out of adjustPDIS 923 52-10 0074 14NOV18 MUC OPEN U LOGPAGES:2711946 L1 DOOR SLIDE ARMED LIGHT INOP. FACT 16NOV18 02:00 CDG PERFORMED ADJUSTEMENT OF THE L1 DOOR GIRT BAR IAW SDR FDEA2018110133071Girt Bar · dirtyL1 DOOR WAS HARD TO ARM AND DISARM. INSPECTED AND CLEANED THE GIRT BAR MECHANISM AND FLOOR FITTINGS FROM MATERIAL. CHECKED THE L1 DOOR ARMING MECHANISM AND OPS IAW AMM 25-66-10-2 AND AMM 25-66-01-6. FOUND GOOD.SDR FDEA2018110293077Lamp · inoperativeL1 SLIDE ARM LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-06-2-1. OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE.SDR FDEA2018081492011Bushing · bentL1 DOOR DIFFICULT TO DISARM. L1 DOOR WILL NOT OPEN. APEARS THAT GIRT BAR HAS DROPPED FROM BOTTOM OF DOOR AND WAS JAMMED ALONG THE FLOOR. REPLACED THE L1 DOOR GIRT BAR FORWARD MECHANISM SPRING, BUSHINGS AND BOLT. OPS CHECKED GOOD IAW AMM 52-11-25-5.SDR FDEA201807201792Eva System · failedWHILE PERFORMING EO F-2560-E0323178 FOUND CAPT'S EVAS BLOWER NOT TESTING. R&R CAPT'S EVAS TESTS GOOD REF MM25-62-00-4.SDR FDEA201806291599Bracket · crackedLOWER FWD CORNER BRACKET FOUND CRACKED ON LT CANTED BEAM BEHIND THE ACCESS PANEL 197AL. FABRICATED NEW BRACKET PART NUMBER 149N7553-25 IAW SRM 51-30-01 REV 124, DRAWING 149N7553 SHEET 1 REV C AND GMM 7-0-100.SDR FDEA201806151498Idg · failedACFT ELECTRICAL SYSTEM WENT IRRADIC, COCKPIT LIGHTS BEGAN FLICKERING, LOWER EICAS WENT BLACK. NUMEROUS EICAS MESSAGES ENSUED BUT MAIN ONES REMAINED. EVERYTHING CAME BACK ON WHEN THE RIGHT ENGINE WAS SHUTDOWN. REMOVED AND REPLACED THE RIGHT ENGINE IDG IAW SDR FDEA201806111448Switch · dirtyLEFT ENTRY DOOR SLIDE ARMED LIGHT WILL NOT ILLUMINATE WHEN SLIDE LEVER IS IN ARMED POSITION. CLEANED DOOR ARMING MECHANISM/SWITCH AS PER AMM 25-66-01 AND 52-11-25-5. OPS CHECKED MULTIPLE TIMES. PASSED. OKAY FOR SERVICE.SDR FDEA201806011374Light · inoperativeUPON LANDING DISCOVERED LEFT ENTRY DOOR SLIDE LIGHT NOT ILLUMINATED. OPENING AND RE-CLOSING DOOR DID NOT FIX IT. RELAMP CHKD OK IAW SWPM 20-84-00 AND CKD IAW SUBTASK 52-11-00-822-046. RELAMPED BULB. OPS CHECK OK.SDR FDEA2018052311267Latch · damagedL1 DOOR DIFFICULT TO CLOSE FROM THE INSIDE. FOUND AFT UPPER CAM FOLLOWER BEARING DAMAGE AND AFT UPPER AND LOWER CAM FITTING LATCHES DAMAGE. REPLACED LATCH FITTING AND CAM BEARING,DOOR ADJUSTED AND OPS CHECKED OK.SDR FDEA201805181257Cylinder · leakingUPON ARRIVAL, THE L1 ENTRY DOOR EMERGENCY POWER RESERVOIR INDICATION WAS ZERO PSI. REMOVED AND REPLACED L1 ENTRY DOOR EMERGENCY POWER RESERVOIR IAW MM 52-11-30-4. OK FOR SERVICESDR FDEA201802030301Spring · unsecureCREW VERBAL DOOR 1L HOLD OPEN LOCK NOT WORKING CORRECTLY. FOUND SPRING ON HOLD OPEN LOCK TRIGGER CAME OFF. SECURED SPRING ON TRIGGER. HOLD OPEN LOCK OPERATION CHECK OK PER AMM 52-11-00-2.SDR FDEA201802030300Spring · unsecureCREW VERBAL DOOR 1L HOLD OPEN LOCK NOT WORKING CORRECTLY. FOUND SPRING ON HOLD OPEN LOCK TRIGGER CAME OFF. SECURED SPRING ON TRIGGER. HOLD OPEN LOCK OPERATION CHECK OK PER AMM.SDR FDEA201711213290Floorbeam · crackedSTA 580 LBL 45.5 FLOORBEAM IS CRACKED. SEEN FROM FORWARD CARGO. COMPLIED WITH EA # F-5310-T0336514 P1,FUSELAGE-MAINFRAME-STA 580 FLOOR BEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.SDR FDEA201711183275Seat Track · corrodedMAIN DECK BETWEEN STA 1620 - 1640 LBL 45.5 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION ON SEAT TRACK IAW B 757 SRM 51-10-02-0G,EVALUATED AREA,ORIGINAL MAT. 0.070",MAT. REMAINING 0.015",MAT. LOSS 0.055" FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-52SDR FDEA201711183274Cusp Web · corrodedMAIN DECK BETWEEN STA 980 - 1000 RT SIDE CUSP WEB CORRODED. REMOVED CORROSION AND EVALUATED CUSP WEB AT STA 980 - 1000 RT, ORIGINAL MAT .056", MAT REM .048" FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A DET III FIG 101. FORMED, LOCATED, DRILLED AND TRIMMED NEWSDR FDEA201711183273Cusp Web · corrodedMAIN DECK STA 978 LT SIDE CUSP WEB CORRODED. REMOVED CORROSION AND EVALUATED CUSP WEB MAIN DECK AT STA 978 LT, ORIGINAL MAT .056", MAT REM .044" FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A DET II FIG 101. FORMED, LOCATED, DRILLED AND TRIMMED SHEAR WEB (CUSP SDR FDEA201711173261Seat Track · corrodedMAIN DECK BETWEEN BS 1360 - 1383, LBL 58.22 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-10-02-0G, EVALUATED THE AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, DETAIL VII, FIG 101. REMOVED THE DAMAGED SEAT TRACK, TRIMMED, AND DRILLED SDR FDEA201711173258Floorbeam · corrodedMAIN DECK BS 1640 BETWEEN BL 0 - LBL 58.22 FLOORBEAM TEE CORRODED. REMOVED CORROSION IAW SRM 51-10-02-0G, LBL 38 TO LBL 58.22, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A, FIG 101, DETAL VI. CUT-OUT THE DAMAGED FLOORBEAM UPPER TEE, FABRICATED ANGLES,SDR FDEA201711173260Crease Beam · corrodedMAIN DECK BETWEEN STA 900 - 1040 LBL 64 CREASE BEAM CORRODED. REMOVED CORROSION AND EVALUATED CREASE BEAM AT MAIN CABIN STA 900-1040 LBL 64 ORIGINAL MAT .070" MAT REMAINING .046" FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A DET III FIG 101. REMOVED AND REPLACSDR FDEA201711173259Crease Beam · corrodedMAIN DECK BETWEEN STA 900-1040 RBL 64 CREASE BEAM CORRODED. REMOVED CORROSION AT MAIN CABIN CREASE BEAM STA 900 AT 1040 RBL 64 AND FOUND TO BE OUT OF LIMITS ORIGINAL MAT .070" MATERIAL REM . 050" IAW SRM 53-40-13-1A DET III FIG 101. REMOVED AND REPLACED CREASSDR FDEA201711173257Cusp Web · corrodedMAIN DECK STA 1110 LBL 70 CUSP WEB CORRODED. REMOVED CORROSION AT CUSP WEB MAIN DECK STA 1110 LBL 70 AND EVALUATED ORIGINAL MAT .063" MAT REM .030" FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A DET III FIG 101. FORMED, LOCATED, DRILLED AND TRIMMED NEW SHEAR WESDR FDEA201711153244Web · corrodedMAIN DECK WEB BETWEEN BS 1640 - 1680, LBL 54 CORRODED. REMOVED THE CORROSION IAW SRM 51-10-02-0G, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A, DETAIL VIII, FIG 101. REMOVED THE WEB, FABRICATED AND INSTALLED A NEW WEB IAW DWG 657N4304, REV - AND SRMSDR FDEA201711153243Crease Beam · corrodedMAIN DECK CREASE BEAM BETWEEN BS 1610 - 1620, LBL 64 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13-1A, DET II. CUT OUT THE DAMAGE AREA BS 1570 TO 1630 IAW SRM 53-00-13-2R, LOCATED, DRILLED, AND TRIMMED A NEW CREASE BEAM SECTION,SDR FDEA201711153242Crease Beam · corrodedMAIN DECK BETWEEN BS 1370 - 1415, LBL 64 CREASE BEAM CORRODED. D. REMOVED THE CORROSION. FOUND OUT OF LIMITS IAW SRM 53-60-13-1A, DET II AND III, CUT OUT DAMAGE SECTION FROM BS 1480 TO 1360 IAW SRM 53-00-13-2R. LOCATED AND DRILLED A NEW CREASE BEAM, CHANNESDR FDEA201711103319Stringer · corrodedCORROSION BS 1434 STR 26L STRINGER AT AFT CARGO PIT. REMOVED DAMAGED ON STRINGER 26L STA 1434,EVAL ORINAL MAT. 0.080",MAT. LOSS 0.080",MAT. REMAINING 0.000",FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-03-1A FIG 101,DETAIL II AND B DWG. # 140N1530 REV. SDR FDEA201710303112Warning System · false activationAT BCN ON T/O ROLL WHEN T/O POWER BEING SET, RECEIVED MASTER WARNING LTS AND "SPOILERS" DISPLAYED ON EICAS. RTO PERFORMED AT 20 KTS. PERFORMED SPOILER CONTROL MODULE BITE PER FIM 27-09 FT 807. SCM 1R SHOWED "R HYD PRESS LOW" AS AN ACTIVE FAULT. PRESSURIZESDR FDEA201710213021Door · lack of lubeL1 DOOR IS HARD TO OPEN AND CLOSE. LUBRICATED THE DOOR IAW MM 12-21-18-3. OPERATED THE DOOR IAW MM 52-11-00-2. OPS CHECKED NORMAL. OK FOR SERVICE.SDR FDEA201708162242Light · inoperativeDURING PREFLIGHT, FOUND BOTH GREEN POSITION LIGHTS INOPERATIVE. FOUND CONNECTOR D07086 BROKEN ON TRANSFORMER. THE CONNECTOR WAS REPLACED IAW SWPM 20-60-06, NO HELP. THE TRANSFORMER T10044 WAS REPLACED IAW AMM 33-43-03. LIGHT STILL NOT WORKING. REPLACED THSDR WX0A20170731281Engine · failedEMERGENCY DECLARED, RIGHT ENGINE FAILED. R&R #2 ENGINE.SDR FDEA201707061861Sensor · out of adjustLEFT FWD ENTRY DOOR WHEN OPEN, DOES NOT SHOW OPEN ON THE OVERHEAD PANEL OR EICAS SCREEN. CLEANED AND ADJUSTED THE L1 ENTRY DOOR SENSOR IAW AMM 52-71-00-5. OPS CHECKED GOOD.SDR FDEA201706281781Battery · thermal runawayAPU BATTERY THERMAL RUNAWAY. REPLACED APU BATTERY CHARGER AND APU BATTERY IAW AMM 24-31-04 & AMM 24-31-03 PERFORMED TEST OF APU BATTERY CHARGER AND APU BATTERY IAW AMM 24-31-04 & AMM 24-31-03SDR FDEA201705081372Skin · dentedDENT ON EXTERIOR UPPER FUSELAGE BS 453, STRINGER 7R. REPAIRED IAW EA F-5330-T0333088 P1, AND SRM 53-00-01-2R, REPAIR 15.SDR FDEA201705021335Skin · dentedLOWER FUSELAGE HAS A SERIES OF PROTRUDING DENTS ALONG PRODUCTION SPLICE BS 660, STRINGERS 21 - 24L. REPAIRED IAW EA F-5330-T0332951.SDR FDEA201705021334Strut · crackedLEFT ENGINE STRUT TO DIAGONAL BRACE FITTING, HORIZONTAL FLANGE,OTBD SIDE CRACKED.SDR FDEA201704281291Fitting · crackedLEFT ENGINE STRUT TO DIAGONAL BRACE FITTING, HORIZONTAL FLANGE, OTBD SIDE, INBD, AFT HOLE CRACKED IN ALUMINUM LAYER. REPAIRED IAW EO F-5450-7-5006.SDR FDEA201703301012Door · detachedDURING POST FLIGHT INSPECTION, THE CAPTAIN'S ESCAPE ROPE ACCESS DOOR HAD FALLEN OFF OF CEILING PANEL. FOUND THE ACCESS DOOR LOWER LATCH BROKEN. REPLACED THE LATCH, INSPECTED THE DOOR AND NO FURTHER DEFECTS WERE NOTED. FOUND ESCAPE ROPE TO BE PROPERLY STOW
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