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 FDEA2020072361532Floorbeam · corrodedFLOOR BEAM LOWER NUT PLATE STRIP IS CORRODED BS 1681.8, LBL39 REMOVED AND REPLACED FLOOR BEAM LWR NUTPLATE STRIP AT BS 1681.8 LBL 39 IAW SRM 51-40-02 AND DWG 146N5693 REV CSDR FDEA2020072361539Seat Track · corrodedRH SEAT TRACK RBL 58.22 CORRORED IN SEVERAL AREAS BETWEEN STA 1080R AND 1180R. REMOVED CORROSION AT RH SEAT TRACK RBL 58.22 SEVERAL AREAS BETWEEN STA. 1080 AND 1180 AND AFTER EVALUATION FOUND SEAT TRACK TO BE OUT OF LIMITS IAW B757 SRM 51-10-02-0G, 53-00-5SDR FDEA202007161542Floorbeam · corrodedMAIN CABIN, FWD RIGHT WET AREA , PRIOR TEE CAP REPAIR HAS CORROSION AT SEAT TRACK AREAS, BS 365 BL 0 TO RBL 64. REMOVED CORROSION, ORIGINAL THICKNESS (.125") REMOVED (.005") REMAINING (.120") CROSSECTIONAL AREA IS LESS THAN 5% WITH A1=.250" AND A2= .0025SDR FDEA2020071761541Floor Support · corrodedFLOOR SUPPORT FITTING UPPER SURFACE IS CORRODED BS 1661.8 - BS 1681.8, RBL 0. REMOVED AND REPLACED CORRODED CHANNEL IAW DWG 146N5576 AND SRM 51-40-03-06, FID 1 SHEET 4 AND SHEET 7.SDR FDEA2020071761540Pressure Deck · corrodedMAIN CABIN PRESSURE DECK UPPER PLATE IS CORRODED BS 1714, LBL 6 - BL9 REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE WITHIN LIMITS IAW SRM 53-60-51-1A, TREATED BARE METAL IAW SRM 514-20-01.SDR FDEA2020071761539Seat Track · corrodedSEAT TRACK RBL 58.22 CORRORED IN SEVERAL AREAS BETWEEN BS 1080 AND 1180.SDR FDEA2020071761538Seat Track · corrodedRH SEAT TRACK RBL 58.22 LIGHT SURFACE CORROSION AROUND NUT PLATES AT FS 1180R.SDR FDEA2020071761536Pressure Deck · corrodedMAIN CABIN PRESSURE DECK UPPER PLATE WAS CORRODED, BS 1685.8 - BS 1688.5. REMOVED THE CORROSION IAW SRM 51-10-02, FOUND TO BE WITHIN LIMITS IAW SRM 53-60-51-1A, TREATED BARE METAL IAW SRM 51-20-01.SDR FDEA2020071761535Floorbeam · corrodedFLOORBEAM UPPER SURFACE WAS CORRODED AT SEVERAL AREAS, BS 1681.8, LBL 4 - LBL 47. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE WITHIN LIMITS IAW SRM 53-60-51-1A, TREATED BARE METAL IAW SRM 51-20-01.SDR FDEA2020071761534Floorbeam · corrodedFLOORBEAM UPPER SURFACE WAS CORRODED, BS 1681.8, RBL 11. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE WITHIN LIMITS IAW SRM 53- 60-51-1A, TREATED BARE METAL IAW SRM 51-20-01.SDR FDEA2020071761532Nut Plate · corrodedFLOORBEAM LOWER NUT PLATE STRIP WAS CORRODED, BS 1681.8, LBL 39. REMOVED AND REPLACED THE FLOORBEAM LWR NUTPLATE STRIP IAW SRM 51-40-02, AND DWG 146N5693, REV C.SDR FDEA2020071081470Line · rupturedLEFT HYD QTY AND PRESSURE WENT TO ZERO.COMPLIED WITH QRH-DECLARED EMERGENCY-UNEVENTFUL LANDING. RAN ENG PER JRH CH 5 AND OPERATED ELECTRIC PUMPS, NO LEAKS NOTED. FOUND FLEX LINE RUPTURE .SDR FDEA2020062321309Collar · brokenR1 DOOR HOLD OPEN LOCK COLLAR BROKEN. REMOVED AND REPLACED RT R1 ENTRY DOOR HOLD OPEN DOOR LOCK REF AMM 52-11-08-8.SDR FDEA2020061091169Frame · crackedCRACK INDICATION FOUND: LT BS1640 AT S-14L AT LOWER I/B FASTENER HOLE AT INTERCOSTAL TEE CLIP. BETWEEN TEE CLIP & CHORD LAYER LOOKING AFT AT 8 O'CLOCK POSITION. (1ST & 2ND LAYER) ACCOMPLISHED EA F-5310-T0354398-P1 FUSELAGE - MAINFRAME - FRAME WEB, STA 1640 S14SDR FDEA2020061091167Latch · brokenR1 DOOR EVACUATION SLIDE LATCH ASSY BROKEN. REMOVED AND REPLACED R-1 DOOR EVACUATION SLIDE CATCH ASSY PER AMM 25-66-01-4 STEP 3.H1 (A).SDR FDEA2020061091164Pan · gougedL1 DOOR HAS GOUGE IN PAN AROUND HANDLE BASE. REMOVED AND REPLACED L-1 PASSENGER DOOR PER AMM 52-11-01-4.SDR FDEA2020060111095Fitting · crackedRIGHT STRUT OB LOWER FWD END HAS A CRACKED CLIP. REMOVED AND REPLACED CLIP PART NR 313N3052-17 IAW DWG NR 313N3052 REV B AND SRM 51-40-02.SDR FDEA2020060111094Nut Plate · corrodedMAIN CABIN FLOORBEAM AT STATION 1681 HAS ONE NUTPLATE STRAP CORRODED AT APPROX RBL 45. REMOVED CORRODED NUTPLATE STRAP IAW SRM 51-40-02. FABRICATED AND INSTALLED NEW NUTPLATE STRAP IAW DWG NR 146N5300 REV E.SDR FDEA2020051870966Adc · faultyPDIS 786 34-14 4200 17MAY20 TYS FACT U LOGPAGES:3215525 REJECTED ON RUNWAY DUE TO NO AIRSPEED ON PILOT/LEFT SIDE. REJECTED AT 78 KTS FACT 17MAY20 12:59 TYS U REPLACED LH CADC AS PER 757 MM 34-12-01-4 AIR DATA COMPUTER - REMOVAL/INSTALLATISDR FDEA2020051320927Transmission · malfunctionedDURING ARRIVAL WHEN WENT TO FLAPS 1 GOT TE FLAP DISAGREE. RAN QRH FLAPS 20 LANDING UTILIZING ALTN FLAP SWITCH. INSTALLED L/H INBOARD TRAILING FLAP TRANSMISSION, REF. B757 AMM27-51-06-4, LEAK AND OPS CHECK GOOD.SDR FDEA2020050860903Floor Support · corrodedCOCKPIT AREA FLOOR SUPPORT BRACKET STA. 324 TO 344 LBL 18 CORRODED REMOVED CORROSION FROM FLOOR SUPPORT STA. 324 TO 344 LBL 18 AND FOUND OUT OF LIMITS IAW SRM 53-00-51-1A DET III FIG 101, REMOVED AND REPLACED BY FABRICATION FLOOR SUPPORT IAW SRM 51-40-05,SDR FDEA2020050860902Floor Support · corrodedCOCKPIT AREA L1 DOOR STA. 365 TO 375 LBL 60 CORROSION ON FLOOR SUPPORT BEAM REMOVED CORROSION ON FLOOR SUPPORT AT COCKPIT AREA L1 DOOR STA. 365 TO 375 LBL 60 AND FOUND IT OUT OF LIMITS IAW SRM 51-10-02-0G AND 53-00-51-1A FIG 101 DET III, REMOVED AND REPLACSDR FDEA2020050430887Hydraulic Line · rupturedLOSS OF ALL LEFT HYD FLUID. FOUND L MLG DOWN LOCK ACTUATOR LINE RUPTURED. R&R'D LINE IN REF TO AMM 32-32-02-4. RAN ENGINE AND ENGAGED EDP TO VERIFY PUMP INTEGRITY PER JRH. OPS CHECK GOOD, LEAK CHECK GOOD. OK FOR SERVICESDR FDEA2020050420875Seat Track · corrodedCOCKPIT AREA STA 345 TO 351 RBL 14 SEAT TRACK CORRODEDSDR FDEA2020050420874Floorbeam · crackedFUSELAGE - MAINFRAME - STA 580 FLOOR BEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK AT LBL 45.5 TRIMMED OUT UPPER AFT FLANGE OF FLOOR BEAM SPLICE SEGMENT PER FEDEX DWG SR57- 53-004 REV - , FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX DWG SR57-53-004 REV - SDR FDEA2020050420871Power Supply · failedMDIS 789 33-50 3480 01MAY20 RST OPEN U THE THREE MAIN DECK EMERGENCEY LIGHTS CONTROLLED BY M731 REMAIN ILLUMINATED WITH AIRCRAFT DOWN POWERED. REMOVED AND REPLACED CHARGER / POWER SUPPLY M731 REF MM 33-51-07-SDR FDEA202004300847Light · inoperativeEXTERIOR EXIT DOOR LIGHT OUTSIDE OF L1 DOOR NOT TESTING.SDR FDEA202004300846Light · inoperativeDURING PRE-FLIGHT NOTED EMERGENCY EXIT LIGHT OVER L1 DOOR NOT TESTING. ALONG WITH THE EMERGENCY LIGHT JUST OUTSIDE OF L1 DOORSDR FDEA202004300810Collar · brokenL1 DOOR GUST LOCK BROKEN. REMOVED AND REPLACED L-1 DOOR HOLD-OPEN LOCK COLLAR. IAW 757 M/M 52-11-08-8.SDR FDEA2020043080809Light · inoperativeL1 DOOR EXTERIOR EMERGENCY LIGHT INOP RELAMPED THE L1 DOOR EXTERIOR LIGHT IAW M/M33-51-06-2-1, AND OP'S TESTED NORMAL, THIS CLEARS MEL 33-51-02-02, A/C OK FOR SERVICE.SDR FDEA202004100728Linkage · brokenTHE MAIN CARGO DOOR IS DENTED AND GOUGED ON SKIN AT UPPER FWD CORNER OF DOOR FROM FWD LIFT ACT. LINKAGE BREAKING. COMPLETED REPAIR OF MAIN DECK CARGO DOOR REF B757 SRM 52-30-01-2R.SDR FDEA202003170581Beam · crackedFWD CARGO STA 580 STUB BEAM IS CRACKED. LBL45.5 CUT OUT DAMAGED FLANGE ON FLOOR STUB BEAM STA 580 IAW FEDEX DWG SR57-53-004 REV -. FABRICATED, LOCATED, DRILLED AND INSTALLED ANGLE AND FILLER IAW FEDEX DWG SR57-53- 004 REV -. REF FEDEX EA F-5310-T0352978 P1SDR FDEA202003170582Stringer · corrodedPOPPED RIVET HEAD EXTERIOR FUSELAGE STA 1460 STR 29L. REMOVED RIVETS AT STA 1460,STR 29L IAW B 757 SRM 51-40-02-OG,REMOVED AND REINSTALLED STRINGER SPLICE AT STA 1452 TO 1468 IAW B 757 SRM 51-40-02-OG.FOUND CORROSION ON STRINGER SECTION,29L 100% MAT. LOSS,SDR FDEA2020031760578Power Supply · inoperativeFOUND DURING PREFLIGHT, INTERIOR EMERGENCY LIGHT ABOVE L1 DR INOP. REMOVED AND REPLACED M731 POWER SUPPLY PER MM 33-51-07-2, OPS CK GOOD. CLEARED MEL. OK FOR SERVICE.SDR FDEA2020031760577Power Supply · inoperativeFOUND DURING PREFLIGHT, EXTERIOR EMERGENCY SLIDE LIGHT AFT OF L1 DR INOP REMOVED AND REPLACED M731 POWER SUPPLY PER MM 33-51-07-2, OPS CK GOOD. CLEARED MEL. OK FOR SERVICE.SDR CALA2020032100659Skin · corrodedIN AFT CARGO AFT BULKHEAD ABOVE WATER DRAIN MAST HAS CORROSION REMOVE MAST AND CHECK LIMITS. (REF AAR NR 9759301) REMOVED DRAIN MAST. REMOVED CORROSION, HFEC AREA, NO CRACK ON DEFECT FOUND, TREATED, PRIMED AND TOP COAT AREA. FILL ALL VOIDS WITH POTTING COMPOUNSDR CALA2020032100648Skin · corrodedCORROSION DAMAGE FOUND ON THE THE FUSELAGE SKIN AFT LAV SERVICE PAN, AT BS 1701 AND BETWEEN STRINGER 28R AND 29R. REMOVED AFT SE RVICE PAN. REMOVED CORROSION AND FABRICATED AND INSTALLED RPR DOUBLER PER ECRA 5331-02645. ALL WORK ACCOMPLISHED ON AAR-MIA NR 9759SDR FDEA2020031200520Angle · corrodedAFTER REMOVING C1 DOOR LOWER CENTER DEPRESSOR,FOUND #3 ANGLE CORRODED,LOKING FWD TO AFT AT APPROX. STA 588.93 EVALUATED FWD CARGO DOOR LOWER #3 ANGLE 100% MATERIAL LOSS DUE TO CORR. OUT OF LIMITS IAW B 757,SRM 52-30-02-1A,DETAIL VI. REMOVED,FABRICATED AND SDR FDEA2020031200519Angle · corrodedAFTER REMOVING C1 DOOR LOWER CENTER DEPRESSOR,FOUND #4 ANGLE CORRODED,LOKING FWD TO AFT AT APPROX. STA 600. EVALUATED FWD CARGO DOOR LOWER #4 ANGLE,ORIF. MAT=.050",REM. MAT= .024",MAT LOSS=.026" FOUND TO BE OUT OF LIMITS IAW B 757 SRM 52-30-02-1A,DETAIL VISDR FDEA2020031200522Angle · corrodedAFTER REMOVING C1 DOOR LOWER CENTER DEPRESSOR,FOUND #1 ANGLE CORRODED,LOKING FWD TO AFT AT APPROX. STA 572.53 EVALUATED FWD CARGO DOOR LOWER # 1 ANGLE 100% MATERIAL LOSS DUE TO COORR. OUT OF LIMITS IAW B 757 SRM 52-30-02-1A DET VI. REMOVED,FABRICATED AND ISDR FDEA2020031200521Angle · corrodedAFTER REMOVING C1 DOOR LOWER CENTER DEPRESSOR,FOUND #2 ANGLE CORRODED,LOKING FWD TO AFT AT APPROX. STA 580. EVALUATED FWD CARGO DOOR LOWER #2 ANGLE 100% MATERIAL LOSS DUE TO CORR. OUT OF LIMITS IAW B 757 SRM 52-30-02-1A DET.VI. REMOVED,FABRICATED AND INSTSDR FDEA2020031200518Angle · corrodedAFTER REMOVING C1 DOOR LOWER CENTER DEPRESSOR,FOUND #5 ANGLE CORRODED,LOKING FWD TO AFT AT APPROX. STA 607.47 EVALUATED FWD CARGO LOWER #5 ANGLE 100% MATERIAL LOSS DUE TO CORR. OUT OF LIMITS IAW B 757 SRM 52-30-02-1A DET VI REMOVED,FABRICATED AND INSTALLEDSDR FDEA2020030650496Skin · gougedR / WING OB FLAP L/E UPPER SKIN GOUGE. REMOVED GOUGE ON RT WING O/B FLAP L/E FOUND O/B BLENDOUT TO BE OUT LIMITS IAW B757 SRM 57-53-01-1A FIG 101 DET. VI AND SRM 51-10-02-OG,CUT OUT DAMAGE AREA AND INSTALLED REPAIR DOUBLERS,STRAPS AND REPAIR PLATE IAW B75SDR FDEA2020022860409Sensor · inoperativePDIS 780 32-30 4516 26FEB20 MEM OPEN U LOGPAGES:2877688 AFTER TAKEOFF, GEAR DISAGREE EICAS WITH AMBER GEAR LIGHT. GEAR EXTENDED NORMAL. NO EMERGENCY DECLARED. SHGN 26FEB20 22:32 MEM U DEBRIEFED FLIGHT CREW. DURING GEAR RETRACT RECEIVED GSDR FDEA202002240381Strap · damagedAFT. CARGO COMPT. AFT. BULKHEAD BETWEEN BS.1681, AND BS. 1701, INTERCOSTAL WEB LOWER FLANGE HAS 26EA. DRILL OFF RIVETS SHANKS, AND MISSING STRAP, AT BL0. FORMED, LOCATED, DRILLED, FABRICATED AND INSTALLED AFT CARGO STA 1681-1701 BL0 INTERCOSTAL WEB LWR FLSDR FDEA202002240380Intercostal · damagedAFT. CARGO COMPT. AFT. BULKHEAD INTERCOSTAL LOWER FLANGE HAS 1EA. DAMAGED FASTENER HOLE, AT BL0 BETWEEN BS. 1681, AND BS.1701 EVALUATED INTERCOSTAL LWR FLANGE (CHANNEL) BL0 STA 1681-1701 OUT OF LIMITS IAW B757 SRM 51-10-02 AND 53-00-04-1A FIG 101. REMOVESDR FDEA202002210364Seat Track · corrodedSEAT TRACK AT STA 1180 LBL45.5 HAS CORROSION REMOVED CORR ON SEAT TRACK STA 1180 LBL45.5 IAW B757 SRM 51-10-02. 100% MAT LOSS DUE TO EXFOILIATION OUT OF LIMITS IAW B757 SRM 53-60-52-1A FIG 101. REMOVE, F FABRICATED AND INSTALLED NEW SEAT TRACK IAW B757 SSDR FDEA2020022100362Cylinder · inoperativeL1 DOOR EMERGENCY POWER RESERVOIR AT 0 PSI. REMOVED AND REPLACED LEFT #1 DOOR EMERGENCY POWER ASSIST RESERVOIR PER MM 52-11-30-4. PART REPLACED WAS A HR TEXTRON, ENTRANCE DOOR EMERGENCY POWER SDR FDEA20200221361Slide · damagedAFTER BLOCK IN FO DISARMED THE SLIDES AND CRACKED THE DOOR OPEN. WHEN GROUND CREW OPENED THE DOOR, THE SLIDE PARTIALLY DETAINED BUT DID NOT DEPLOY. INSTALLED L1 DOOR ESCAPE SLIDE ASSEMBLY IAWSDR FDEA202002140341Lamp · inoperativeL1 DOOR EXTERIOR EMER EXIT LIGHT INOP RELAMPED L1 DOOR EXT EMER EXIT LIGHT (SLIDE LIGHT) USING LAMP P/N 767 LIGHT CHECKS GOOD. REF B757 AMM 33-51-06-2-1. OK FOR SERVICE
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