Boeing 757-224
Service difficulty reports · 3,824
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 = '757224' 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 = '757224' 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 CALA2022122303477Idg · faultedRIGHT AC BUSS OFF EICAS, RIGHT AC MAIN BUSS IS NOT ENERGIZED RT AC BUSS OFF, RESET ONCE. AC BUSS OFF AGAIN 5 MIN LATER. RELATED NOTED FAULTS. PERFORMED BITE CHECK ON BPCU IAW FIM 24-20 TREE 801, FAULT NOTED ON RIGHT GEN POWER SYSTEM DP TRIP AND MAIN BUS/SDR CALA2022122303480Lavatory · inoperativeALL LAVS INOP LAVS. WERE SERVICED . ALL LAVS FUNCTIONAL CHECK NORMAL. A/C BIS.SDR CALA2022121903437Outflow Valve · inoperativeCABIN ALT EICAS AT FL400. RT PACK OFF AUTO 1-2 CONTROLLER INOP. OVBD EX VAL STATUS DECLARE AN EMERGENCY. OUTFLOW VALVE WAS REPLACED AND AMM 05-51-24 PROCEDURE PERFORMED OPS CK GOOD PRESSURE HOLDS PER AMM CALLOUT.SDR CALA2022121903409Skin · dentedSUPPORT TASK- R/H HORIZONTAL STAB UPPER SKIN BETWEEN FORWARD SPAR AND AUX SPAR HAS A DENT AT APPRO STAB STATION 200 TRANSCRIBED FROM HAECO NR 9282966 PERFORMED TAP TEST AND VISUAL, FOUND 3" X 4.25" AREA OF DISBONDE 51-70-10-2R-01. HAECO GSO MECH V899890 INSP SDR FDEA202212152925Skin · noneTHIS NON-ROUTINE CREATED FOR SDR/RDR TRACKING OF AIRCRAFT DAMAGE AT STATION 1681 TO 1720 STRINGERS 23R TO 26R. 0000231760 : ROWLAND, GLEN J - 15-DEC-2022 23:04 ITEM WAS REPAIRED PER E.A. F-5330-T0371948 P1. SEE WO 84864 SEQ #6 FOR MAINTENANCE PERFORMED. TSDR CALA2022121403383Engine · bird ingestionBIRDSTRIKE ON TAKEOFF PERFORM BIRDSTRIKE CONDITIONAL INSPECTION PER AMM PILOT REPORTS ON TAKE OFF RIGHT AT V1 THEY SUPECTED A BIRD 05-51-18-212-001 STRIKE ON E1, ALL CONTROLS FELT NORMAL NO SURGE OR VIBRATION, BUT DID SMELL SOMETHING, PILOT CALLED AIRPORT OPS SDR CALA2022121403391Skin · noneSUPPORT TASK - LW NO. 4 SLAT TE WEDGE IB SIDE PREVIOUS REPAIR FOUND TO BE SEPARATING REF HAECO GSO NR 9286241 ACCOMPLISHED PERMANENT REPAIR OF L/W NO. 4 SLAT TE WEDGE IAW B75 ROTARY ACTUATORS, ACCOMPLISH TORQUE SAFETY AND OPS CHECK, CHECK 7-200 SRM 57-43-02-2RSDR CALA2022121203361Fseu · warning messageTE FLAP DISAGREE EICAS MSG NO EICAS DISAGREE MESSAGE FOUND. PERFORMED FSEU BITE PER FIM NORMALLY. OK TO CONTINUE. 27-51 FAULT TREE 803. FOUND NO HYDRAULIC PRESSURE FAULT ON EXISTING FAULTS. FAULT CODE 302. OPERATED FLAPS SEVERAL TIMES AND FAULT CLEARED. NO FURSDR CALA2022120803332Terminal · brokenL-1 DOOR SLIDE LIGHT INOP. TRANSCIBED FROM HAECO GSO NR 9282919.REMOVED AND REPLACED L-1 DOOR SLIDE LIGHT ASSY AND OPS CHECKED PER AMM 25-66-11-822-011 AND BSWPM 20-84-00 AND WDM 33-51-12.SDR CALA2022120703316None · noneTHE REPAIR INCORPORATED VIA ECRA 5360-01679 IS APPROVED AS TIME- LIMITED FOR 18 MONTHS PENDING THE RESULTS OF A DAMAGER TOLERANCE ANALYSIS (DTA). REMOVE THE AIRCRAFT FROM SERVICE ON OR BEFORE MA Y 09, 2024, UNLESS ANOTHER 8110-3 FORM IS RECEIVED FINDING APPRO SDR CALA2022112503229A/C Pack · failedRAPID DEPRESSURIZATION DUE TO R AND L PACK FAIL ALSO R ENG BLEED OFF. THE 450 TEMP SENSOR PASSED THE HEALTH CHECK WITH NO ISSUES. REPLACED #1 HI STAGE PILOT. COMPLETED INSTALLATION AND OPERATIONAL CHECKS. R&R RT PACK COMPRESSOR OUTLET TEMP SENSOR. BITE PASS. CSDR CALA2022112503215Frame · damagedTHE REPAIR INCORPORATED VIA ECRA 5362-01040 IS APPROVED AS TIME- LIMITED FOR 18 MONTHS PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE AIRCRAFT FROM SERVICE ON OR BEFORE MA Y 15, 2024, UNLESS ANOTHER 8110-3 FORM IS RECEIVED FINDING APPRO VSDR CALA2022112103180Seal · missingPDA 2 LEFT WING OUTBD MAIN FLAP SEAL COMPLETELY MISSING AT INBOARD END ( WHERE INBD. & OUTBD FLAPS MEET ) -- SEE PHOTO PHOTO ADDED SEAL MISSING IS 42 INCHES LONG ... REF IPC 57-53-10-51 ITEM 100 INSTALLED NEW SEAL AT INBOARD END OF OUTBD MAIN FLAP LEFT WING ..SDR CALA2022111703164Light · inoperativeEMERGENCY EXIT LIGHT AT ROW SEAT ROW 20 CENTER CEILING HAS PARTIAL ILLUMINATION. DATA TRANSCRIBED FROM NSA EMX N/R 00003. REMOVED AND REPLACED LAMPS AT EMERGENCY EXIT LIGHT AT ROW 20 AND INSPECTED BY V932931. CENTER CEILING PANEL IAW B757-ALL AMM 33-51-01-712-SDR CALA2022111703163Line · looseC HYD QTY STATUS MSG AT FL370 1 HOUR FROM LAN DING. FOLLOWED CHC KLIST ISOLATED SYS. .43 RF FOUND RETURN LINE BETWEEN RT CTR PUMP AND EMP CASE DRAIN DUAL FILTER MODULE LOOSE. TIGHTENED FITTING PER AMM 29-00-98. SERVICED SYSTEM TO FULL PER AMM 12-12-01. LEAK CKSDR CALA2022111603141Frame · dentedFWD PIT R/H AT STA 740 STR 24 FRAME IS DENTED TOP SIDE, DENT WAS FOUND TO BE IN FREE FLANGE ON FRAME BS 740 S24R, DENTS ARE NOT PERMITED IN FREE FLANGE. OUT OF LIMITS IAW SRM 53-00-07. COMPLETED REPAIR ON FRAME IAW SRM 53-00-07.SDR CALA2022111403130Lamp · inoperativeEMERGENCY EXIT LIGHT AT L1 DOOR OH HAS PARTIAL ILLUMINATION. REMOVED L1 EMERGENCY EXIT LIGHT LENS AND REPLACED BAD LAMPS . REINSTALLED EMERGENCY EXIT LIGHT LENS. OPERATION CHECK GOODSDR CALA2022110403031Warning Message · false activationRUDDER RATIO LIGHT ILLUMINATED ON ARRIVAL THERE WAS NO FAULT BALLS ON EITHER RUDDER RATION MODULES, PERFORMED THE TEST , BOTH SYSTEMS CHK OK PER REF 27-21 FAULT TREE 809.SDR CALA2022110203022Floor Support · corroded(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 400 RBL 40 FLOOR SUPPORT CORRODED ON UPPER SURFACE. TRANSCRIBED HAECO GSO NR 9282307. REMOVED DAMAGE TO GUTTER SUPPORT STA 400 RBL 40 MAT. 063 REMOVED AND BAC DWG 141N5162 REV. A REMOVED DOT HAECO GSO MECH V935SDR CALA2022110203010Floorbeam · corroded(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 1640 BL0 FLOOR B EAM PREVIOUS T CAP REPAIR CORRODED ON UPPER SURFACE, TRANSCRIBED FROM HAECO GSO N/R 9282336 ACCOMPLISHED T-CAP REPAIR IAW B757-200 SRM 53-00-51-2R-10 REPAIR 10 AND B757-200 SRM 51-0-02-0G-0. CATSDR CALA2022103103001Floor Support · corroded(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 400 RBL 40 FLOOR SUPPORT CORRODED ON UPPER SURFACE. TRANSCRIBED HAECO GSO NR 9282307.SDR CALA2022103103000Floor Support · corroded(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 1660 TO 1680 LBL 60 GUTTER SUPPORT CHANEL CORRODED ON UPPER SURFACE. DOT: R726. TRANSCRIBED FROM HAECO NR 9282335.SDR CALA2022103102994Floorbeam · corroded(SUPPORT TASK) MAIN CABIN FLOORBEAM STA 1681 HAS CORROSION ON UPPER SURFACE UNDER AFT DECK PLATE AT APPROX LBL47. TRANSCRIBED FROM HAECO GSO NRC# 9288277SDR CALA2022102802983Floorbeam · corroded(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 363 RBL 58 FLOORBEAM UPPER SURFACE CORRODED TRANSCRIBED FROM HAECO GSO NR 9282303.SDR CALA2022102802979Skin · damagedFWD LWR CARGO DOOR 10 INCHES FROM LWR END HAS A BLENDED AREA. RE PORTED BY V921224 REPAIRED DAMAGED AREA IAW B757-200 SRM 52-30-01-2R-4CATAGORY "B" REPAIR REQUIRES REPEAT INSPECTIONS PER NOTES B & C. REF NON-ROUT INE 151186-0800-0010 FOR DETAILSSDR CALA2022102702971Floor Support · corrodedLOG PAGE OPENED FOR SFR TRACKING,REF MRO LOG PAGE 151186-0100-00 96 ON FLOOR SUPPORT STRUCTURE, REF SSFR FORM 46-0024. FLOOR SUPPORT STRUCTURE STA 400 RBL 61 CORRODED- REMOVED AND REPLACED SUPPORT PER ECRA 5316-01011. ALL WORK PER AMES NRC 151186-0100-0096. FOSDR CALA2022102702962Floor Support · corrodedFLOOR SUPPORT STRUCTURE STA 377-395 RBL 65 CORRODED FOR SFR TRACKING ONLY REF AMES NRC 151190-0100-0052 FOR ESFR TRACKING PURPOSES ONLY FLOOR STRUCTURE STA 377-395 RBL 65 CORRODED-REMOVED AND REPLACED FLOOR SUPPORT AT STA 377-395 IAW SRM 51-40-02 PAR 7. FOR SFSDR CALA2022102702961Seat Track · corroded(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 720 TO STA 760 R BL 45 SEAT TRACK CORRODED IN SEVERAL SPOTS REF HAECO GSO NR 9282 325. BLENDED CORROSSION AT 720 RBL45, REMINING THICKNESS .025 FOUND T O BE OUT OF LIMITS PER B757-200 SRM 51-40-02 INSTALLED NEW SSDR CALA2022102702954Support Channel · corroded(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 346 RBL 62 GUTT ER SUPPORT CHANNEL CORRODED AT R1. TRANSCRIBED FROM HAECO GSO NRC# 9282302 REMOVED AND REPLACED SUPPORT P/N 141N5160-78 IAW BOEING DWG# 141 N5160 REV B AND B757-200 SRM 51-40-02. HAECO GSO MECHSDR CALA2022102702950Engine · unserviceableIN THE CLIMB FROM 340- 360. LEFT ENGINE DID NOT PRODUCE SUFFICIE NT PWR LEFT FF 2.5 CLIMB BEYOND 340. BOTH ENGINES PERFORMED NORMAL DURING ROLLOUT, TAKEOFF, AND CLIMB. IDT INSPECTION REQUREMENTS FOR R&R OF ENGINE #1 HP FUEL PUMP AND VERIFIED THAT IDT ITEMS ASSDR CALA2022102702945Plate · corroded(SUPPORT TASK) MAIN CABIN AFT DECK PLATE HAS CORROSION AT APPROX . STA 1685 BL 0, TRANSCRIBED FROM HAECO GSO N/R 9288278 REMOVED CORROSION ON AFT DECK PLATE PER B757-200 SRM 51-10-02. O 200 SRM 53-60-51-2R-2. HAECO GSO MECH V934114 INSP QC194 RIGINAL MATERIALSDR CALA2022102702944Seat Track · corroded(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 720 TO STA 760 R BL24 SEAT TRACK CORRODED IN SEVERAL SPOTS. TRANSCRIBED FROM HAE CO GSO NRC# 9282323 BLENDED SEAT TRACK, REMOVED .030, FOUND TO BE OUT OF LIMITS PER 95-030 REV A. HAECO GSO MECH V932674 INSP QC4SDR CALA2022102702942Flap · noneACCOMPLISHED DVI OF RIGHT HAND INBOARD FLAP FOUND REPAIR ON UPPE R SURFACE IN GOOD CONDITION 37" UP FROM TRAILING EDGE AND 16" IN BOARD FROM OUTBOARD EDGE TO CENTER OF REPAIR, REPAIR IS 4" X 16" , TRANSCRIBED FROM HAECO GSO N/R 9284205 REPAIRED R/H INBOARD FLASDR CALA2022101802841Frame · chafedUPPER CABIN FUSELAGE FRAME AT STA 1640 STRINGER 6R IS CHAFFED. R EPORTED BY V921209 REPAIRED UPPER CABIN FUSELAGE FRAME @ STA 1640 BETWEEN STR 5R & 6R IAW AMES DOCUMENT 47527REA02 AND UAL EC/RA 5302-01035. REF NO N-ROUTINE 151186-0200-0129 FOR DETAILSSDR CALA2022101402805Fairing · missingPDA 1 DURING 1C VISIT AT GSO, FOUND ON ARRIVAL #2 ENGINE INBD COMPRESSOR GAS FAIRING, WITH THE MAJORITY OF THE PANEL MISSING. EVIDENCE OF THE PANEL IS ONLY AT THE UPPER FORWARD SECTION. REPLACED GAS PATH FAIRING.SDR CALA2022101402804Fairing · missingPDA 1 DURING 1C VISIT UPON ARRIVAL AT GSO FOUND #2 ENGINE OUTBD COMPRESSOR FAIRING WITH LARGE SECTION OF THE PANEL MISSING. REPLACED GAS PATH FAIRING.SDR CALA2022101202783Seat Track · corrodedUPPER CABIN SEAT TRACK STATION 720-760 RBL 45 HAS CORROSION ON MULTIPLE AREAS OF THE HORIZONTAL FLANGES. GENERATING ITEM: W/C 19-5330-1-2802. REMOVED SECTION OF SEAT TRACK ASSY FROM STA.720-760 RBL 45 AND INSTALLED SERVICEABLE SEAT TRACK SUPPORT IAW 757-200 SRSDR CALA2022101202782Floor Support · corrodedUPPER CABIN FLOOR SUPPORT STA 760 RLB 65 IS CORRODED. BLENDED CABIN FLOOR SUPPORT INBD CHORD STA 760 RBL 65, FOUND OUT OF LIMITS IAW B757-200 SRM 53-30-13-1A-1 DETAIL VIII. REPAIRED INBD CHORD IAW B757-200 SRM 53-00-13-2R-1 REPAIR 1.SDR CALA2022101002761Fseu · faultyTE FLAP DISAGREE. ALT LE AND TE FLAPS USED AND FLAP ISLN VAL MESSAGE APPEARED AT 20 DEGREE FLAP. REPLACED FSEU 1. NO HELP. RAN FLAPS UP AND DOWN HYDRAULICALLY AND FOUND STATUS MSG FLAP ISLN VAL.FOLLOWED FIM 27-51 FAULT TREE 818 AND REPLACED PRESSURE SWITCH ONSDR CALA2022101002749Frame · crackedFUSELAGE FRAME AT STA 800 BELOW STRINGER 8L IS CRACKED AT ATTACH BRACKET RIVET. REPORTED BY V921209 REPAIRED FASELAGE FRAME AT STA 800 BETWEEN STRING 8L-9LSDR CALA2022101002748Frame · crackedFUSELAGE FRAME AT STA 1540 BELOW STRINGER 8L IS CRACKED AT ATTAC H BRACKET RIVET. REPORTED BY V921209 REPAIRED FUSELAGE FRAME AT STA 1540 BETWEEN STRINGERS 8L-9L PER B757-200 SRM 53-00-07 REPAIR 8. SEE NR 151186-0200-0131 FOR DETA ILSSDR CALA2022101002747Frame · crackedFUSELAGE FRAME AT STA 1120 BELOW STRINGER 8R IS CRACKED AT ATTACH BRACKET RIVET. REPORTED BY V921209 REPAIRED FUSELAGE FRAME AT STA 1120 BETWEEN S8R & S9R.SDR CALA2022101002746Floorbeam · corrodedUPPER CABIN FLOORBEAM STA 720 RBL30 TO RBL65 UPPER SURFACE HAS CORROSION ON PREVIOUS REPAIR. UPDATED TO INCLUDE SDR REQUIRED. ADD EMP:V921726, V921224 REMOVED CORRODED UPPER CABIN FLOORBEAM STRAP AT STA 720 FROM LBL65 TO RBL65 AND INSTALLED SERVICEABLE NEW STRSDR CALA2022101002745Seal Depressor · chafedAFT CARGO DOOR SEAL DEPRESSOR ON LOWER PART OF THE DOOR IS CHAFED. GENERATING ITEM: 19-0630-1-2012. INSTALLED SERVICEABLE AFT CARGO DOOR LOWER SEAL DEPRESSOR EDGE BEAM REF SRM B757-51-40-02 PAR 4-7. WORK PERFORMED IN ILN AMES W/O 151186-0800-0028 V921503.SDR CALA2022100702738Warning Light · illuminatedLEFT HYD QTY EICAS MSG WHEN ACFT WAS ON THE RUNWAY AND THROTTLES MOVED UP. SHOWED .27 THEN RECOVERED. PER CREW THE ACFT WAS 3 KNOTS OR LESS WHEN EVENT OCCURRED.NO LOW PRESSURE OR OVERHEAT INDICATIONS. PERFORMED LEFT HYDRAULIC SYSTEM QUANTITY CHECK. REF AMM 29-SDR CALA2022100702737Depressor · chafedAFT CARGO DOOR SEAL DEPRESSOR ON LOWER PART OF THE DOOR IS CHAFED. GENERATING ITEM: 19-0630-1-2012. INSTALLED SERVICEABLE AFT CARGO DOOR LOWER SEAL DEPRESSOR EDGE BEAM REF SRM B757-51-40-02 PAR 4-7. WORK PERFORMED IN ILN AMES W/O 151186-0800-0028 V921503.SDR CALA2022100702735Skin · bentAFT CARGO DOOR FWD LOWER CORNER AREA BENT. INSTALLED NEW DOUBLER AND FILLER ON AFT CARGO DOOR LOWER FWD CORNER DOOR SKIN IAW B757-200 SRM 52-30-01-2R REPAIR 4.SDR CALA2022100602728Actuator · inoperativeUNABLE TO ADJUST RUDDER TRIM IN FLIGHT- AUTOPILOT ON OR OFF-NO D IFFERENCE GROUND TEST OF RUDDER TRIM SHOWS TRIM INTERMITTANTLY COMPLETELY INOP. FOLLOWED FIM 27-21 FAULT TREE 805, ELECTRICAL CHECKS AT TRIM ACT CANNON PLUG D1746 CHECK GOOD. FIM INDICATES TRIMSDR CALA2022100602711Floorbeam · corrodedUPPER CABIN FLOORBEAM STA 720 RBL30 TO RBL65 UPPER SURFACE HAS CORROSION ON PREVIOUS REPAIR. UPDATED TO INCLUDE SDR REQUIRED. ADD EMP:V921726, V921224 REMOVED CORRODED UPPER CABIN FLOOR BEAM STRAP AT STA 720 FROM LBL65 TO RBL65 AND INSTALLED SERVICEABLE NEW STSDR CALA2022100602707Floor Support · corroded(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 720 RBL 20 TO RB L 50 UPPER STRAP CORRODED ON UPPER SURFACE. TRANSCRIBED FROM HA ECO GSO NRC# 9282322
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