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 CALA2024052801596Controller · faultyN2 OVERSPD ON DEPT MAX N2 103 ON RT ENG PIC UPDATE. #2 ENG AT TAKEOFF. N2 RED 103.2 :05, EGT AMBER 795. :07.9. MAX 796 WITH EPR .05 HIGHER ON RIGHT ENGINE. NO LOSS OF POWER NOTED BY CREW. PHOTOS OF ENGINE EXCD AND EICAS MESS PAGES. NOTED ''R ENG SURGE BITE'' MSDR CALA2024052001531Channel · crackedREF AMES NR 170224-0200-0211 GEN ITEM 53-5310-1-2626 CRACK FOUND THROUGH FASTENER ON FRAME IN UPPER CABIN R/H SIDE ST A 1580 FOR OVER HEAD BIN ATTACH BRACKET ABOVE STR 9 REPAIRED CRACK THROUGH FASTNER ON FRAME IN UPPER CABIN R/H SIDE STA 1580 ABOVE STRINGER 9 SDR CALA2024051301462Floor Support · crackedCABIN FLOOR SUPPORT CRACKED IN MULTIPLE SPOTS FROM BS1420-1440. REMOVED AND REPLACED FLOOR SUPPORT AT BS 1420-1440 BL0 IAW BOEIN G 757 SRM 51-40-02 PAR 4, SEE BACK FOR PARTIALLED WORK.SDR CALA2024051301461Floor Support · crackedCABIN FLOOR SUPPORT CRACKED IN MULTIPLE SPOTS FROM BS1320-1340 AT BL0 IN CEILING AREA OF ALC MARKED IN RED. REMOVED AND REPLACED CABIN FLOOR SUPPORT AT BS 1320-1370 AT BLO IAW BOEING 757 SRM 51-40-02 PAR 4. SEE BACK AND PARTIALLED WORKSDR CALA2024051301460Floor Support · crackedCABIN FLOOR SUPPORT CRACKED IN MULTIPLE SPOTS FROM BS1260-1300 AT BL0 IN CEILING AREA OF ALC MARKED IN RED. REMOVED AND REPLACED CABIN FLOOR SUPPORT AT BS 1260-1300BLO IAW BOEING 757 SRM 51-40-02 PAR 4. SEE BACK FOR PARTIAL WORK.SDR CALA2024050701366Floor Panel · crackedREF AMES NR 170224-0100-0069 GEN ITEM EA 5100-02244 REV G OP 003 ALC FLOOR PANEL 153AF CRACKEDSDR CALA2024050701365Panel · crackedREF AMES NR 170224-0100-0068 GEN ITEM EA 5100-02244 REV G OP 003 ALC PANEL 151AF HAS A CRACKSDR CALA2024050701358Support Rib · crackedFOUND CRACKED SUPPORT RIB AT STATION 365.25, JUST ABOVE WIRING B UNDLE #91177 REF AMES NR 170224-0100-0064SDR CALA2024050101279Adiru · failedAT FLT 340 FO A/S FAIL MOMENTS LATER CPT A/S FAILED C/W QRC INSPECT DRAIN TRAPS FOR ANY WATER, NO DEFECTS, R/R ADIRU L PER AMM 34-26-01, PERFORMED GROUND TEST 30, TEST GOOD PARTS USED: 60-3421-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1564274 SSDR CALA2024041501085Flap System · faultedTE FLAP DISAGREE ON FINAL. SMALL SPLIT. FLGHT CREW REPORTED FLAP LEVER WAS NOT IN THE DETENT AFTER LANDING, FOUND NO EXISTING OR LAST FLT FAULTS ON FSEU''S. STOWED FLAPS AND SLATS ELECTRICALLY AND THAN CYCLED FLAPS IN NORMAL MODE SEVERAL TIMES. REF FIM 27-51 FSDR CALA2024032800901Fmc · failedRIGHT FMC FAIL LIGHT IS ON LP 7452038 MEL 3461AK WAS CLEARED. MUST REPLACE R FMC REF AMM34-61-01-024-001-002 UNLOCKED TO CLEAR WITH R FMC R&R FMC IN SFO WITH TT# 1524492 AC 0862 REF IPC EQUIPMENT AND SOFTWARE INSTL- MAIN ELECTRONICS EQPT CTR FMC REFERENCE: CYCSDR CALA2024032500855Skin · crackedLEFT WING FIXED LEADING EDDGE ABOVE THE PYLON IS CRACKED. PART IS CURRENTLY RMOVED FROM THE AIRCRAFT.SDR CALA2024032100803Unknown · crackedGEN ITEM; EA 5310-07582 REV A OP 003 7837 A STRINGER CLIP IS CRACKED. LOCATED AT THE FWD SIDE OF B STA FRAME1460 S-26L REPORT ED BY V921214 REMOVED & REPLACED STRINGER CLIP FLOOR SUPPORT IN THE ALC AT STA 1460 LEFT SIDE IAW B757 SRM 51-40-02 PARA 7. SEE BACK FSDR CALA2024031500736Floor Panel · crackedREF AMES NR 169356-0100-0067 GENERATING ITEM: 53-5330-1-2802///A FT LOWER CARGO HAS 6 INCH CRACK APPROXIMATELY IN FIXED FLOOR PAN EL IN-BETWEEN STATIONS 1280-1300 JUST ABOVE STRINGERS S-26R, MAR KED WITH STREAMER 3254 INSTALLED REPAIR DOUBLE ON THE ALC TRANSISDR CALA2024031400731Warning Message · false activationRT GEN CONT ON OVRHD AND RT GEN OFF EICAS AND ASSOCIATED MSGS. SVC IDG PER AMM 12-13-03 RESET BPCU PER FIM 24-20 RAN #2 ENG NO FAULTS RETURNEDSDR CALA2024030800664Engine · damagedDUE TO #2 ENGINE IFSD ACCOMPLISH INSPECTION PER AMM 71-00-00-206-015-R00. LOUD BANG AND JOLT COMING FROM NUMBER 2 ENGINE , THEN ALL OILS INDICATING WENT TO 0. AT THAT POINT CREW SHUTDOWN ENGINE. SEE PHOTOS FROM CAPTAIN. PER FLIGHT CREW DURNG CRUISE ALTITUDE 33SDR CALA2024030600644Transmitter · intermittentMAIN LT, RT, AND CNTR C HYD QTY DECREASED. QTY STABLE WITH SYS PUMPS OFF QTY DECREASED TO 0.02. FLUTUATED W/PUMPS ON STABLE AT 1.06 W/PUM PS OFF AFTR 5 MINS OFF PLACE CTR HYD QTY FLUCIATION ON MEL 2933F. VERFIED CTR HYD QTY WAS AT PROPER OPS LEVEL AT PANEL. SDR CALA2024022300509Battery Pack · dischargedDOORS 2L & 2 R EMERGENCY LIGHTS INOP REMOVED & AND REPLACED M11486 IAW AMM 33-51-07. OPERATION NORMAL.SDR CALA2024020800363Anti-Ice Valve · inoperativeLEFT ENG ANTI ICE EICAS L ENG ANTI ICE YELLOW VALVE LIGHT WITH SWIT CH SELECTED ON UPDATE. MARKED AS SDR REPLACED LEFT ENG TAI VALVE (WITHOUT VALVE POSITION INDICATOR) REF AMM 30-21-03-404-016, UP TO STEP 3 E (15). NEEDS ENGINE RUN FOR OPS AND LEAK CHECK. ADD SDR CALA2024020100273Bleed Valve · faultyDISTRIBUTION EICAS MESSAGE L (R) ENG BLEED OFF DISPLAYED. BLEED AIR (01=L ENG, 02=R ENG) OFF LIGHT ON WITH ENGINE RUNNING AND SW ITCH ON. DUCT PRESSURE WAS ZERO R TRIED TO CYCLE WITH CRH PROCEDURES BUT FAILED AGAIN RT ENGINE BLEED PRESSURE REGULATING AND SHUTOSDR CALA2024012300182Battery Pack · inoperativeSTA 351 WL 289 RBL 1 , MOUNTED ON CEILING PANEL JUST TO RIGHT OF THE FWD ENTRY LIGHT PANEL, EMERGENCY LIGHT EXIT INOP. REMOVED AND REPLACED BATTERY PACK M730 IAW AMM 33-51-07-022-023- 002 AND 33-51-07-862-029-002. PERFORMED OPS CHECK GOOD.SDR CALA2024012200164Frame · crackedEA5311-01827 REV E OP 002 FRAME 1640 R/H SIDE, HAS A SMALL CRACK ON THE FRAME INNER CHORD FLANGE BY THE INNER CHORD STRAP AREA LOCATED JUST BELOW S-14R. ELB REPORTING FOR SDR. REPAIRED 1640 R/H FRAME 146N8711-72 IAW MAE EA 757-5360-13-A3474 DATED JAN 10 2024 ASDR CALA2024012200163Skin · crackedR/H OUTBOARD MAIN FLAP OUTBOARD LOWER SKIN CRACK REPAIR ON ST ENGINEERING NON ROUTINE 86900 AS PER SRM 57-53-01-2R-4 REPAIR 4 REQUIRES DIP TO REINSPECT BLIND FASTENERS EVERY 3000 FLIGHT CYCLES. IF ANY EVIDENCE OF PULLED OR LOOSE RIVETS, THE RIVETS MUST BE REPLSDR CALA2023120803585Bleed Valve · leakingR ENG HI STAGE CAUTION UPON APPLIYING TAKEOFF POWER STATUS AND ECS/MSG SHOW NO FAULTS, UPPER EICAS ADVISORY MSG DISPLAYED "R ENG HI STAGE". AUTO EVENT SHOWS - RIGHT ENG HI STAGE, ADDED PHOTOS. INFO UPDATE FOR RH ENGINE HI STAGE VALVE NO CLAMPS OR LINES WERE DISDR 2023FA0000544Case · crackedDURING INDUCTION AT STANDARDAERO, SAN ANTONIO FOR A SHOP VISIT. A CRACK OF APPROXIMATELY 4.5" WAS FOUND IN THE REAR FAN CASE AT THE 12 O'CLOCK POSITION AFT OF THE FRONT ENGINE MOUNT. PICTURES WILL BE EMAILED TO 9-AMC-SDR-PROGMGR@FAA.GOV AFTER SUBMITTING THIS RSDR CALA2023083002667Unknown · inoperativeAUTOPILOT EICAS MSG WITH L AP ENGAGED. NO CONTROL ISSUES. ENGAGE D R AP AND NO MSG. FL235 M.75 MCDP FLIGHT FAULTS SHOWS "A/P CTN STAB L/FCC L". MCDP TEST 65 T/S PER FIM: 22-04 FAULT TREE 825. REPLACED L FCC PER AMM: FAILED; "STAB TRIM FCC L FAIL" AND "STAB TRISDR CALA2023081602543Line · damagedGEAR DOOR INDICATION AFTER TAKEOFF. MSG CLEAR AFTER QRH PROCEDURE. LIFTED AC OFF GROUND USING JACKS REF MM 07-11-01-852-016. TILT ACTUATOR REF LP 5353105 FOUND BRAIDED HYD LINE ON TRUNK POSITION ACTURATOR SPLIT AND LEAKING FLUID. UPDATE, FOUND ON RIGHT MAIN GESDR CALA2023071902283Indicator · faultyON TAKEOFF ROLL CAPT AIR SPEED INDICATOR FLAG APPEARED. T/O REJ ECTED AT 8 0KTS. CAPT''S MACH AIRSPEED INDICATOR FLUCTUATING WITH AIRCRAFT PARKED. REPLACED CAPT''S MACH AIRSPEED INDICATOR REF AMM 34-13-02-404-004, CKS GOOD. PARTS USED: 75-3111-9-0001,QTY :1 RSDR CALA2023071202230Spoiler · unknownRUDDER TRIM EXCESSIVE LEFT IN FLIGHT CRUISE. A/C SETTLED AROUND 9 DEGREES IN CRUISE. NO VIBRATIONS NOTED DURING FLIGHT. A/C SLIGHT LEFT ROLL ON TAKEOFF. PILOTS NOTICED HAVING TO ADD T/S PER FIM 27-21 FAULT TREE 812 UPTO BLOCK 33 RECONNECTED RT C/W FIM 27-21-00SDR CALA2024070901986Skin · dentedFOUND DENT AFT OF LAVATORY SERVICE DOOR NEAR OLD STUCTURAL REPAIR NEAR BS 1580, BETWEEN STR 30 AND 29R. RIVET IN DENT IS FIRST RIVET TO THE RIGHT OF STR 30. DENT SIZE DEPTHS. IS 2.25 X 1.375 X .050 DEPTH. ACP STEPS 1,2,3, AND 4. ONE RIVET IS WITHIN HALF SDR CALA202306070368Hose · damaged***EMERGENCY DECLARED*** L HYD SYS PRESS CAUTION ILLUMINATED ON FINAL APP. EMERG DECLARE D. FOUND HOLE ON HYDRAULIC HOSE TO DOWN LOCK ACTUATOR. REMOVED AND REPLACED HYDRAULIC HOSE TO DOWN LOCK ACTUATOR IN REF WITH AMM 32-32-02. SERVICED LEFT HYDRAULIC SYSTEMSDR CALA2023051201484Fairing · missingRIGHT WING NO. 6 FLAP TRACK AFT FAIRING FWD LH ATTACH PLATE IS MISSING. SEE PIC AFT FLAP TRACK FAIRING REMOVED. FLAP TRACK FAIRING REMOVED PER CDL27C 486,DELIVERED TO LAX STORES RIGHTWING #6 AFT FLAP FAIRING, ADD EMP:U107479,U232924 DISPATCH DESK: 3355 TOMC APSDR CALA2023012300188Transmitter · faultedSPOKE TO FLT CREW IN SFO LT SYS 83 ,CENTER 93 ,RT SYS 98 . ALL NORMAL DURING FLT, MLG DOWN CENTER WENT TO ZERO . ALSO CENTER SYS PRESSURE WENT TO ZERO 88%. SERVICED CENTER HYD SYS TO 89% FROM 32%.PRESSURIZED ALL HYD SYS, NO LEAKS FOUND ON ACFT. AFT OF HORIZSDR CALA2023011800146Transceiver · inoperativeHF 1 UNABL 2 TRNSMT 15 MIN AFTER TAKOFF HF2 UNABL TO TRNSMT 28MI N AFTER TAKOFF 3) REPLACE BOTH COUPLERS AS PRECAUTIONARY. DUE TO HISTORY OF HF ISSUES, PLS PERFORM 1) HF TEST PER AMM TASK 23-11-00-735-009-001, 2) CHECK HF ANTENNA BONDING PER TASK 23-11-04-766-SDR CALA2023011800144Door · missingEXTERNAL AIR DOOR MISSING RIGHT SIDE HIGH PRESSURE PNEUMATIC DOOR IS MISSING. PLACED ON CDL. BACW10UC81P WASHERS, 9 EA BACW10BP2NDP WASHERS, 8 EA PLH508CD NUTS AND LISTED PARTS ON M&L. DISPATCH DESK: 3304 NAME: DATE: 15-JAN-23- EXTERNAL AIR DOOR MISSING. DEFESDR CALA2023011600130Access Door · missingPDA 1, RIGHT SIDE HIGH PRESSURE PNEUMATIC DOOR IS MISSING. RIGHT SIDE HIGH PRESSURE PNEUMATIC DOOR IS MISSING. INSTALLED NEW PART EXTERNAL AIR DOOR. OPS CK GOOD.SDR CALA2022080101930Battery Pack · inoperativeDOOR 3 EMER EXIT LGTS INOP REPLACED BATTERY PACKS OVER DOORS 4LEFT & 4RIGHT.SDR CALA2022080101924Engine · unknownSMOKE SEEN AROUND RIGHT ENGINE WE THEN SHUT THE ENGINE DOWN SMOKE STOPPEDSDR CALA2022072001849Brake Sys · warning messageRTO ON 17L AT 125KTS DUE TO HIGH EGT ON BOTH ENGS. BRAKE TEMPS 8 TOGW 229.4 CREW REPORTED A/C WAS ON 1HR BEFORE DEPARTURE, #1 ENG EGT SHOWED 117 BEFORE MOTORING, AND #2 ENG EGT SHOWED 120 BEFORE MOTORING. AT TOP OF COLD RANGE. ALL TIRES WITHIN NORMAL WEAR LIMISDR CALA2022070801674Engine · warning messageFL380 R ENG OVHT EICAS. REDUCED PWR HALF AND SHUT ENG BLD VALVE W NO EFF ECT. WENT IDLE W RT TH. T/S IN PROGRESS.SDR CALA2022061301498Proximity Sensor · out of adjustAT 80KNOTS ON TAKEOFF ROLL LEFT AFT ENTRY DOOR EICAS MESSAGE CAME O N L3 DOOR INDICATION CAME ON, BUT NOW EXTINGUISHED COMPLIED WITH COMPLIED WITH MEL . MEL. REQUEST APPROVAL. L4 DOOR INDICATION INTERMITTENT CORRECTION L4 DOOR. VERY SMALL MOVEMENT OF L4 DOOR HSDR CALA2022061001478Skin · noneNUMEROUS BLEND OUTS LOCATED ON LWR AFT FUSELAGE SKIN, STA 1300-1460, STRINGER 25R TO 26L. INFO ONLY INFO ONLY: SEE NR 5715602 (MCO) FOR PREVIOUS REPAIRS & CORRECT IVE ACTION. AREA IDENTIFIED PER GMM 06-35-05 LOG PAGE WAS CONVERTED TO ELB FORMAT ON APR 27, 2016SDR CALA2022021800438Light · inoperativeEMERGENCY BULL NOSE LIGHTS AT SEATS 22,24 AND 27ABC AND EXTERIOR LEFT WING OVERWING EXIT DOOR FWD AND AFT LIGHTS INOP. SUSPECT PWR SPLY AND/OR BATT AT M11383 REF WDM 33-51-14. RMVD SLAVED IN NEW PWR SPLY, NO HELP. BATT ON AOG LWR DADO PANEL AT ROW 22 LH. PARTSSDR CALA2022021400386Cover · missingDOOR-MOUNTED ESCAPE SYSTEM DOOR 3L - A EVACUATION SLIDE PROBLEM WAS ENCOUNTERED WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS FA REPORTS EMERGENCY TEST SWITCH PLASTIC PROTECTIVE COVER MISS ING AT DOOR 3L PICTURED ADDED ITEM DOES NOT REQUIRE GUARD,SEE IPC 3SDR CALA2022021400374Unknown · odorFUMES ENTIRE FLIGHT. WENT AWAY AS SOON AS ENGINES SHUTDOWN REPORT FILED BY CAPTAIN FLIGHT CREW AND FLIGHT ATTENDANTS REPORTED UPON ENGINE SHUT DOWN, OIL SMELL IN CABIN DOOR 2 AREA. AFTER ARRIVAL APPROX 40MINS, STARTED APU BLEED & PACKS TURN ON, OIL SMELL STILLSDR CALA2022021400367Frame · cracked(SUPPORT TASK) CRACK FOUND ON LOWER INBD HOLE FWD LAYER AT STA 1 640 L/H FRAME ON THE INTERCOSTAL TEE CLIP. TRANSCRIBED FROM HAEC O GSO TASK CARD 9281318 RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE UNLESS ANOTHER 8100-9 FORM IS RECEIVED FINDING APSDR CALA2022020800342Intercostal · crackedSUPPORT TASK MAIN CABIN FLOOR STA 345 TO STA 365 INTERCOSTAL WEB CRACKED ON INSTALL, TRANSCRIBED FROM HAECO GSO NON ROUTINE 9281 700. REMOVED DAMAGED INTERCOSTAL, SUPPORT ANGLES AND PULLEY BRACKET I MARKED IAW BAC 5307, INSTALLED INTERCOSTAL AND SUPPORT ANGLESSDR CALA2022020700332Intercostal · crackedSUPPORT TASK STA 1640 STR 10L WEB CRACKED AT AFT CTR HOLE ON INS TALL. WEB PN 146N8738-15, TRANSCRIBED FROM HAECO GSO NON ROUTINE 9281722 FABRICATED INTERCOSTAL WEB 146N8738-15 AND INSTALLED IAW B757-30 0 SRM 51-40-02 AND BAC DWG 146N8738 REV G. HAECO GSO MECHSDR CALA2022020700328Beam · corrodedB757-53-3-0479 FLOOR BEAM 365.25 UPPER T-CAP BETWEEN RBL 24.75 T O RBL 45.5 SURFACE CORROSION, TRANSCRIBED FROM HAECO GSO NON ROU TINE 9281118 ACCOMPLISHE T-CAP REPAIR AT STA 365.25 FROM RBL 24.75 - RBL 45.5 IAW B757-300 SRM 53-00-51-2R-1 AND HAECO REO G23586 SDR CALA2022013100276Floorbeam · corroded(SUPPORT TASK) FLOOR BEAM STA 345 UPPER T CAP BETWEEN LBL G-24 H AS SURFACE CORROSION
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