Boeing 757-33N
Service difficulty reports · 1,195
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 = '75733N' 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 = '75733N' 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 AMTA200600517Liner · corrodedBTWN STA 1380 AND STA 1440 AT BL 21R AND WL 146.9. LINER HAS LITE SURFACE CORROSION. REMOVED CORROSION IAW SRM 53-00-53 MAT THICKNESS .063 LOSS .005 AND FOUND WITHIN LIMITS IAW SRM 53-00-53 FIG 101. TREATED AND PRIMED IAW SRM 51-20-01. (K)SDR AMTA200600520Structure · corrodedAFT CARGO COMPARTMENT CARGO DOOR LOWER CUTOUT INSIDE AREA LINER HAS CORROSION AROUND NUT PLATES APPROX 20 IN TOTAL LENGTH RBL-24, STA 1400-1420. REMOVED CORROSION IAW SRM, ORG THICKNESS IS 050 MAT LOSS .005 FOUND TO BE WITHIN LIMITS. (K)SDR AMTA200600519Support · corrodedAFT PIT RT SIDE LONG SUPPORT UPPER SURFACE HAS CORROSION AND PITTING. NUMEROUS SPOTS ENTIRE LENGTH AND ON SIDES. REMOVED CORROSION IAW CPM, ORG THICKNESS .165 MAT LOSS, .010 WITHIN LIMITS IAW SRM. (K)SDR AMTA200600518Support · corrodedAFT PIT LT SIDE LONG SUPPORT UPPER SURFACE HAS CORROSION AND PITTING NUMEROUS SPOTS ENTIRE LENGTH. REMOVED CORROSION IAW CPM MAT THICK .165 MATERIAL LOSS .010 WITHIN LIMITS IAW SRM. (K)SDR AMTA200600516Structure · corrodedBETWEEN STA 1180+20 AND STA 1200 AT BL22L FLOOR STRUCTURE OF CARGO COMPARTMENT HAS LITE SURFACE CORROSION. REMOVED CORROSION IAW SRM THICKNESS .063 MATERIAL LOSS .002 WITHIN LIMITS IAW SRM. (K)SDR AMTA200600515Structure · corrodedBETWEEN STA 1180+120 AT BL22R FLOOR STRUCTURE OF CARGO COMP HAS LITE SURFACE CORROSION. REMOVED CORROSION IAW SRM ORG THICKNESS ..063. FOUND WITHIN LIMITS IAW SRM. (K)SDR AMTA200600514Anchor · damagedAFT PIT CARGO SYSTEM FWD FLOOR ANCHOR HAS GOUGES, PITTING AND SURFACE CORRODED AROUND 3 ATTACH POINTS AND NUT PLATES HAVE CORROSION. REMOVED CORROSION AND GOUGES IAW CPM ORIGINAL MATERIAL THICKNESS IS .063 AND .040 MATL LOSS AT AREA OF .063 IS .005 WITHIN LIMSDR AMTA200600513Warning Message · activatedRT HF DATALINK STATUS MSG DISPLAYED THE LT HF DATALINK WORKED OK. FOLLOWED FIM MM. NO FAULTS FOUND. (K)SDR AMTA200600508Ecu · unserviceableAPU SHUTDOWN AFTER ARRIVING AT GATE, WOULD NOT REST ART. IAW FIM, BLOCK 26, REPLACED APU ECU IAW AMM. PERFORMED 4 SUCCESSFUL STARTS. PERFORMED ECU BITE. NO FAULTS NOTED. (K)SDR AMTA200600411Attach Bracket · corrodedFWD CARGO LT ATTACH BRACKET HAS CORROSION AROUND FASTENER INSERT HOLES. REMOVED CORROSION AND TREATED IAW EA. (K)SDR AMTA200600410Attach Bracket · corrodedFWD CARGO RT ATTACH BRACKET HAS CORROSION AROUND FASTENER INSERT HOLES. REMOVED AND TREATED IAW EA. (K)SDR AMTA200600412Skin · dented2 SMALL DENTS LT FUSELAGE SECT 43 FS 580 TO FS 584, ABOVE W/L 208.10 REQUIRES PERMENANT REPAIR. REPAIRED IAW EA, THIS IS AN INTERIM REPAIR IAW ER/A SUPPLEMENTAL INSPECTION TO BEGIN AT 20,500 CYCLES. (K)SDR AMTA200600396Starter · unserviceableAPU NO START, FAULT LIGHT ILLUMINATED. REMOVED AND REPLACED APU STARTER IAW AMM. (K)SDR CALA0600198Slide · low pressureTHE BOTTLE PRESSURE FOR THE R-3 DOOR SLIDE WAS FOUND LOW. THE R-3 DOOR SLIDE WAS REPLACED IAW MM 25-66-03.SDR AMTA200600377Switch · unserviceableAPU FAULT LIGHT ILLUMINATED AND APU SHUTDOWN. PERFORMED BITE CHECK ON APU ECU AND READ (FILTER SW (GEN))LIGHT. IAW FIM, REMOVED AND REPLACED DELTA P SWITCH IAW MM. NO FAULTS NOTED. (K)SDR AMTA200600376Control Unit · malfunctionedDURING WALK-AROUND, APU HAD AN AUTO-SHUTDOWN OCCURENCE. REMOVED AND REPLACED ECU FOR APU IAW AMM 49-61-05-2. OPS CHECK GOOD. (K)SDR AMTA200600375Detector · inoperativeSTATUS MSG LT ENG OH LP 1. REMOVED AND REPLACED LOOP, LOOP 2 ASSY IAW AMM26-11-01. OPS CHECK GOOD. (K)SDR AMTA200600357Warning Message · activatedLT FMC FAIL EICAS MESSAGE DISPLAYED. RESET BREAKER FOR LT FMC COMPUTER NO MSG DISPLAYED FMC CHKS NORMAL. (K)SDR AMTA200600355Transceiver · malfunctionedLT HF LING CYCLE TO TUNE. SWAPPED LT AND RT HF TRANSCEIVERS. REPAIRED IAW MM. OPS CHECK NORMAL. (K)SDR AMTA200600337Antenna · failedWX RADAR FAIL DISPLAYED ON EHSI. WX RADAR SELF TEST DISPLAYS WX RADAR FAIL ANTENNA. REMOVED AND REPLACED RADAR ANTENNA DRIVE IAW AMM. CHECK NORMAL. (K)SDR AMTA200600325Wire · looseINTERIOR EMERGENCY LIGHTS ABOVE BOTH OVERWING EXITS RT SIDE ARE OUT. RESOLDERED WIRE BACK ON TERMINAL BLOCK. OPS CHECK NORMAL. (K)SDR AMTA200600272Valve · underservicedAPU AUTOSHUTDOWN. REPLACED DE-OIL SOLENOID IAW AMM. SOLENOID OPERATIVE AND LEAK CHECK-OK. APU OPERATION-OK. (K)SDR AMTA200600203Web · buckledKEEL BEAM WEB (W/W AREA) FWD OF MLG DOOR ACTUATOR MOUNT STRUCTURE IS BUCKLED/WARPED TOWARD THE LT SIDE OF AC AND WEB SECTION BELOW AC LEVEL SUSPENSION POINT IS BUCKLED/WARPED TOWARD THE RT SIDE OF AC. REPAIRED KEEL BEAM AREA IAW EA. (K)SDR AMTA200600190Lens · missingEGRESS LENS MISSING AT L-1 DOOR. INSTALLED LENS COVER AS REQUIRED. (K)SDR AMTA200600179Floor Panel · corrodedCORROSION PITTING APPROX 40 INCH X 43 INCH W AREA OF AFT CARGO FLOOR PANEL FROM BS 1377-1334, BL 20L-20R. REPAIRED IAW SRM AND FOUND WITHIN LIMITS. (K)SDR AMTA200600171Drive Assy · unserviceableWX SYS + WX FAIL MSG`S ILLUMINATED. REPLACED WEATHER RADAR ANTENNA IAW MM. OPS CHECK NORMAL. (K)SDR AMTA200600163Skin · corrodedSURFACE CORROSION ON AC SKIN AT LOWER TCAS ANTENNA STA 450, RBL 2 AND RBL 4 AREA 2 INCHES X 4 INCHES APPROX. BLENDED SURFACE CORROSION ON SKIN DOUBLER LOWER TCAS ANTENNA STA 450, RBL 2 AND 4 MATERIAL REMOVED RANGED FROM .001 TO .003 MEASURES THICKNESS FOUND TSDR AMTA200600164Bracket · corrodedCORRODED ON RADOME UPPER BRACKET AT 12 OCLOCK POSITION ON INTERNAL SIDE AT AFT END STA 199, RBL 3 AREA .75 X .75. REMOVED CORROSION FROM RADOME BRACKET ORIGINAL THICK .075. MATERIAL REMOVED .003 FOUND TO BE WITHIN LIMITS SRM. TREATED AND PRIMED. (K)SDR AMTA200600162Floor Support · corrodedAFT CARGO SIDEWALL FLOOR SUPPORT FROM STA 1480 TO 1540 LT SIDE IS CORRODED. REMOVED MINOR CORROSION ON SIDEWALL FLOOR SUPPORT STA 1480-1540, LT SRM. ORIGINAL THICKNESS .063 IAW SRM DETAIL VII INLINITS AFTER .005 REMOVAL OF MATERIAL DETAIL V TREATED AND PRIMESDR AMTA200600161Floor Panel · crackedAFT CARGO COMPT BETWEEN STA 1377 AND 1480 FLOOR PANEL HAS A CRACK. STOP DRILLED CRACK AND INSTALLED 2EA RIVETS ON FLOOR PANEL AT AFT CARGO BETWEEN STA 1377 AND 1480 IAW SRM. CRACK FOUND TO BE WITHIN LIMITS ACTUAL LENGTH 1 INCH. FILLED CRACK WITH SEALANT. (KSDR AMTA200600160Skin · corrodedUPPER FUSELAGE HAS CORROSION AROUND FASTENER HOLES AT ATA ANRENNA LOCATION STA 537 AND LBL 5, APPROX .125 X .5 ON EACH HOLE. REMOVED CORROSION AT STA 537, LBL 5 IAW SRM. ORIGINAL MATERIAL THICKNESS .040 MATERIAL LOSS IS .001-.002 WITHIN LIMITS OK TO TREAT ARSDR AMTA200600166Radar · failedSTATUS MSG WXR SYS AND HSI MSG WXR FAIL IS ILLUMINATED IN FLIGHT, WX TEST MODE ILLUMINATED ANT RT. BOTH CAPT AND FO SIDE ILLUMINATED. PERFORMED FIM TO SHEET 4 BLOCK 2, SYSTEM TEST OK, NO FAULTS. ALSO INSPECTED AND CLEANED AIR FILTER IAW MM. NO HISTORY 90 DSDR AMTA200600143Engine · fluctuatesRT ENGINE, (.1) EPR LOWER AND 40 DEGREES C, EGT HIGHER THAN THE LT ENGINE WITH OTHER PARAMETERS MATCHING. PRIOR TO DESCENT EPR FLUCTUATED (.15) EPR TOWARDS THE NORMAL (HIGHER SETTING). REDUCED THRUST TO MID POINT AND ENG STABILIZED. (K)SDR CALA0500435Fan · inoperativeA SMOKY ODOR WAS REPORTED IN THE COCKPIT AND CABIN WHILE ON DESCENT INTO LAS. THE ODOR CLEARED WITHIN 2-3 MINUTES. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED INSPECTIONS IAW MM 05-51-58 AND LOCATED THE SOURCE OF THE ODOR AS COMING FROM A FASDR AMTA200501062Ground Wire · looseLEFT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. SECURED GROUND STUD 4554 WIRE IAW WDM. LIGHTS OPS CHECK NORMAL. (K)SDR AMTA200500944Terminal · looseLOOP ONE EICAS MSG LT ENG. FOUND TERMINAL LOOSE AT LOOP TS5033. TIGHTENED AS REQUIRED. FIRE LOOP OPS CHECK NORMAL IAW AMM. (K)SDR AMTA200500936Card · unserviceableEICAS MSG (L ENG OH LLP1). REMOVED AND REPLACED LT ENG AUTO FIRE HEAT DET CARD IAW MM. RAN LT ENG, OPS CHECKED OK. (K)SDR AMTA200500924Fire Warning · false activationL ENG FIRE LP 1 DISPLAYED. PERFORMED FIM TASK AND VISUALLY EXAMINED LT ENG FIRE LOOPS/HARNESSES WITH NO DEFECTS NOTED. AS PRECAUTION REMOVED AND REPLACED FIRE/OVERHEAT CARD M 10224 IAW MM. OPS CHECK GOOD. (K)SDR AMTA200500926Sensor · unserviceableNR 1 ENG STATUS MESSAGE (L ENG FIRE LP 1) DISPLAYED. REMOVED AND REPLACED LOOP TS5035 IAW WDM. L ENG FIRE LOOP 1, OPS CHECK GOOD IAW. (K)SDR AMTA200500925Fire Warning · false activationSTATUS MSSG L ENG FIRE LP 1, COMPLETED CONTINUITY CHECKS ON LOOP SYSTEM AND SWAPPED P54 CARDS M681 WITH M682. STATUS MSG CLEAR. ALL CHECKS NORMAL IAW WD. (K)SDR AMTA200500884Eec · unserviceableRT ENGINE LIMITER INOP LIGHT ILLUM. EICAS MSG AND R ENG LIMITER DISPLAYED. PERFORMED FIM 73-21-00, FIG 103A, FAULT CODE (BF) FOUND ON EEC, ONLY FAULT FOUND, IAW FIM REMOVED AND REPLACED RT ENGINE EEC IAW 73-21-07-4, ENGINE RUN-UP AND TAXI. OPS CHECK NORMAL.SDR AMTA200500883Fire Loop · malfunctionedEICAS STATUS MESSAGE: L ENGINE FIRE LOOP 1. ACCOMPLISHED TEST IAW FIM 26-11-00. OPS OK. (K)SDR AMTA200500882Fire Loop · malfunctionedEICAS STATUS MESSAGE INFLIGHT LT ENGINE FIRE LOOP 1. REMOVED AND REPLACED CONNECTOR IAW RRECMM. PERFORMED AMM 26-10-00 FIRE/OVERHEAT LOGIC SYSTEM TEST. CHECKED GOOD. (K)SDR AMTA200500853Fire Loop · looseEICAS STATUS MSG L ENG FIRE LOOP 1, DISPLAYED. SECURED TEMP SENSE LINE, RAN ENGINE. OPS CHECK NORMAL. NO EICAS MSG. (K)SDR AMTA200500854Line · looseEICAS MSG LT ENG OVHT DISPLAYED WITH ENG OVHT ILLUMINATED. LGT EXTIN AFTER THRUST REDUCTION. FOUND NR 1 ENG TEMP SENSOR SENSE LINE LOOSE ON FAN AIR MODULATING VALVE, SECURED IN PLACE, RAN ENGINE, OPS CHECK NORMAL. (K)SDR AMTA200500654Detector · unserviceableAFTER ENGINE SHUTDOWN, STATUS MSG (R ENG OH LP2). REMOVED AND REPLACED RT ENGINE. OVERHEAT DETECTOR (NACELLE) IN A/W AMM. OPS CHECK NORMAL. (K)SDR AMTA200500641Generator · unserviceableRT GENERATOR DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUMINATED. GEN DRIVE DISCONNECTED. REMOVED AND REPLACED IDG IAW MM. LK AND OPS CHECK GOOD. (K)SDR AMTA200500634Seal · unserviceableON TAKEOFF AND CLIMB OUT, LT HIGH STAGE BLEED LIGHT ILLUMINATED ACCOMPANIED WITH EICAS MESSAGE RETURNED TO DEPARTURE. T/S IAW FIM, FOUND HPSOV BUTTERFLY SEAL BROKEN. REPLACED IAW FIM MM, LEAK CHECK GOOD. (K)SDR AMTA200500507Shim · migratedSHIMS MIGRATING IN NR 1 ENGINE MID-SPAR BULKHEAD AT OB AFT LOWER ATTACH BOLT UPPER SURFACE. REPAIRED DAMAGE IAW ERA. (K)SDR AMTA200500506Skin · gougedSEVERAL GOUGES FOUND UNDER PANEL AREA 321AL. REPAIRED DAMAGE IAW ERA. (K)
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