N17133
Service difficulty reports · 88
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N17133' AND registry_match = 'registration' 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 n_number = 'N17133' AND registry_match = 'registration' 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 CALA2026090719268Skin · crackedLT WING LOWER OTBD INTERSPAR SKIN AT PANEL 543BB IS CRACKED AT HOLE 27 AT THE 12 CLOCK, SEE ECRA 5720-03680 FOR WORK PERFORMED.SDR CALA2026020613614Warning Light · false activationR4 DOOR SLIDE LIGHT ABOVE DOOR ON WITH LEVER IN DISARM POSTION VERFIED DOOR IS DISARMED AND GIRT BAR NOT ENGAGED. SLIDE LIGHT STILL ON. INDICATION PROBLEM FOUND S10224 FAULTY. R & R SENSOR AND OPS TEST OK. IAW AMM 25-66-11/201.SDR CALA2025102010317Lever · unknownDOOR 4R ARMING LEVER IS HAVING ISSUES NO ISSUES FOUND ON DOOR 4R ARMING LEVER, OPERATES NORMALLY, OK FOR SERVICE.SDR CALA2025092409239Indication Sys · false indicationLEFT ENGINE HIGH VIBRATION INDICATION. DEGRADED ENGINE, DID NOT SHUTDOWN. CAPT ADVISED: CLIMBING THRU 32K TO 36K AND SLOWING DOWN A BIT THROUGH SOME MODERATE TURBULENCE, LOOKED DOWN AND SAW VIBRATION INDICATON IN THE AMBER FOR N1, N2, AND N3. FELT NOTHING & SDR CALA2025092209115Accelerometer · faultedLEFT ENGINE N3 VIB WENT TO 5.0 /AMBER/ TWICE FL380 .78 REDUCED T HRUST N3 STABLE AT .8 AS PART OF OTHER TROUBLESHOOTING, REPLACEMENT OF THE #1 ENG AVM HAS BEEN CARRIED OUT, REF AMM 77-31-04-404-017, OPERATIONAL CHECK OK.ACCELEROMETER REPLACED, AND OPERATIONAL SDR CALA2025091608965None · no discrepancy4R SLIDE PRESSURE IN THE RED. PRESSURE GAGE NEEDLE ON THE SLIDE INFLATION CYLINDER ON DOOR 4R IS IN THE GREEN BAND OR NOT MORE THAN 1/2 THE PRESSURE GAGE NEEDLE WIDTH ABOVE OR BELOW THE GREEN BAND AS PER AMM TASK 25-66-01-206-024. OK TO CONTINUESDR CALA2025090908655Line · tangledCANNOT ARM 1L DOOR L1 STATIC LINE GOT CAUGHT BETWEEN DOOR SILL AND GIRT BAR. UNTANGLED AND RESTOWED STATIC LINE. ARMED LIGHT ILUMINATES, OK TO CONTINUE. REF AMM 25-66-10-402-022. ADD 347373, U345365SDR CALA2025073007089Rope · out of positionDOOR 1R SLIDE ARMED LIGHT WILL NOT ILLUMINATE WHILE ARMING DOOR. REMOVED SLIDE COVER TO VIEW, GIRT BAR.FOUND FORWARD GIRT BAR SLIDER INCHES AWAY FROM ENGAGEMENT AND TANGLED WITH ROPING FROM SLIDE. INSERTED SAFETY PIN AS REQUIRED FOUND ONE SIDE OF GIRT BAR USDR CALA2025070906407Potable Water · odorFA REPORTS POTABLE WATER SMELLS LIKE CHEMICALS. POTABLE WATER SYS DRAINED AND FILLED WITH FRESH WATER, WATER FLUSHED THROUGH ALL GALLEY COFFEE MKRS AND TAPS, SYS SERVICED SATIS IAW AMM 38-11-00 REV 136SDR CALA2025061105455None · none4R LIFERAFT PRESSURE NEE DLE IN THE RED NEEDLE WITHIN LIMITS - ON EDGE OF GREEN.SDR CALA2025051204618Switch · out of positionAIRSPEED INDICATORS SHOWING/RED LINING AT 268 KNOTS CREW DEBRIEF REPORTS AIRSPEED INDICATON ON ALL FLIGHT DECK INDICATORS MATCHED. ON TAKEOFF AIRSPEED WAS NORMAL WITH FLAPS DOWN, CREW RETRACTED FLAPS AND NOTICED AIRSPEED RED FLAG SHOWED AT 268 KNOTS. WHEN CREWSDR CALA2025041403772Arming Lever · out of positionDOOR 4L ARMING LEVER NOT POSITIONED PROPERLY VERIFIED DOOR 4L ARMED CORRECTLY, ARMED LIGHT VERIFIED, ARMED NUCKLE VERIFIED, GIRT BAR ENGAGMENT VERIFIED,. NO DEFECTS NOTED AT THIS TIME.SDR CALA2025031702848Skin · puncturedFOUND HOLE ON NUMBER 1 ENGINE PYLON FORWARD OF PRECOOLER. THIS LOGPAGE IS FOR ESFR REPORTING PURPOSES. SEE BAM N/R 2414981 FOR WORK PERFORMED. ADDED ESFR INFORMATION.SDR CALA2025022402444Skin · dentedFUSELAGE SKIN DENTED AT APPROX STA 382 ON STRINGER 8R. DENT REPAIRED IAW ECRA 5310-08503 AT IHC BASE VISIT ON NON-ROUTINE 2377794. CATEGORIZED AS MAJOR REPAIR AND RII INSPECTED. ESFR CREATED. DMG LP 3782513 CREATED PER ECRA PART F AND DENT DOT APPLIED. DIP LP SDR CALA2025022402439Doubler · noneDISCREPANCIES BETWEEN INSTALLATION DRAWING AND EXISTING FASTENER LOCATIONS DURING LAYOUT OF L1 DOOR SURROUND STRUCTURE DOUBLER PREVENTIVE MODIFICATION L1 DOOR SURROUND STRUCTURE DOUBLER PREVENTIVE MODIFICATION ACCOMPLISHED IAW EA 5330-04213 OP 4 REV D WITH DEVSDR CALA2024082600498Relief Valve · missingSIGNIFICANT AMT OF WATER IN AFT CABIN AFTER TAKEOFF DURING TROUBLESHOOTING FOUND PRESSURE RELEIF VALVE OF WATER HEATER LAVATORY M BROKEN OFF. REMOVED WATER HEATER LAV M REF AMM TASK 38-13-51-004-001 AND STOWED IN LAVATORY M. R/R WATER HEATER IN LAV M IAW AMM 3SDR CALA2024080700386Adc · failedL AIR DATA COMP FAIL REPLACED LEFT ADC,,OPS CKS NORMAL..REF MM 34-12-01 AND 34-12-00..ALL TESTS AND INDICATIONS ARE NORMAL ACCOMPLISHED IDT PER GMM 09-10-05.SDR CALA2024051401469Oven · odorMID GALLEY OVEN #305 HAS A BURNING SMELL WHEN OPERATING. MID GALLEY OVEN HAS A BURNING SMELL WHEN IS WORKING. NO SMOG COMPLIED WITH NEF DISPOSITION. OVEN AT MID GALLEY INOP AND DETECTED. REQUEST NEF PLACED ON NEF NOC DATE: 13-MAY-24- TOMC APPROVES NEF 2520P OVSDR CALA2024032700882Seal · missingLEFT WING INBOARD FLAP AERODYNAMIC RUBBER SEAL DEPARTED AIRCRAFT. SEAL MEASURES 39.4 INCHES IN LENGHT. INSPECTED AND FOUND SEAL TO BE MISSING FROM A/C. INSTALLED NEW AERODYNAMIC SEAL ON LEFT WING FLAP INBOARD TRACK REF AMM 27-51-00.SDR CALA2023111503365Clutch · out of adjustLOW SPEED REJECTED T.O. 50 KIAS DUE TO SPOILERS EICAS MESSAGE WILL NOT ALWAYS DRIVE TO THE DEPLOY POSITION AND DOES NOT ALWAYS STOW WHEN THROTTLE LEVER IS MOVED FWD. YOU CAN SEE AND HEAR SPEEDBRAKE HANDLE ACTUATOR DRIVE, BUT HANDLE DOES NOT ALWAYS MOVE INSSDR CALA2023080402428Fseu · unknownSTATUS MESSAGE FLAP/SLAT ELEC REPEAT WRITEUP INSPECTED LT LE SLAT XMT AND CANNON PLUG BACKSHELL NO DEFECT PARTS USED: 19-2758-9-0002,QTY :1 NOTED. RIGG CHECKED SLAT XMT FOUND TO BE WITHIN LIMITS. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1247594 SN OFF 2801SDR CALA2023080402427Slat · warning messageLEADING EDGE SLAT SYSTEM EICAS MSG LE SLAT ASYM SHOWS WITH THE F LAP LEVER AT 1; BOTH FLAP POINTERS INDICATE 1/2 FSEU 1 BITE HAD INTERMITTENT FAILURE OF THE LEFT LE POSITION TRANSMITTER REF FIM 27-81 TASK 804 AND FIM 27-51 TASK 805. RESET FLAPS AND SLATS FROM SDR CALA2023052901679Slide · unwanted deployDOOR 1R SLIDE DEPLOYED REPLACED DEPLOYED SLIDE. SLIDE FAILED TO REMAIN ATTACHED TO AIRCRAFT AFTER DEPLOYMENT / CATERING FAILED TO VERIFY DOOR WAS DISARMED BEFORE OPENING. MECHANIC LATER VERIFIED THAT DOOR 1L WAS ALSO STILL ARMED AFTER ARRIVAL AT GATE.SDR CALA2023041401124Fuse · openAFT 2 BULLNOSE EMERGENCY LIGHTS ON RIGHT SIDE DO NOT LIGHT DURING EMERGENCY LIGHT TEST. SUPPORT TASK NSA EMX NR 00209. FUSES AT EMERGENCY POWER SUPPLY. REMOVED AND REPLACED FUSE IAW B757 AMM 33-51-07 PERFORMED OPS CHECK GOOD IAW B757 AMM 33-51-07.SDR CALA2023041401114Switch · inoperativeEMERGENCY LIGHTING TEST SWITCH ABOVE L2 DOOR DOES NOT INITIATE TEST. EMERGENCY LIGHTING FUNCTIONS NORMALLY. SUPPORT TASK NSA EMX NR 00004SDR CALA2023032000795Seat Track · corrodedMAIN CABIN SEAT TRACK BETWEEN STA 1186 AND STA 1320 LBL 45.50 HAS CORROSION IN THE BOTTOM OF THE TRACK SUPPORT TASK NSA EMX N/R 00099 REMOVED FLOOR PANELS 251 JF, 241JF, 241HF,251BF, 251CF,251DF, 2 LICE CHANNEL IAW B757-200 SRM 53-00-52-2R-3 REINSTALLED FLOOR SDR CALA2023020600336Winglet · damagedHIT BY A/C LEFT WING TIP RIPPED OFF WHEN AIRCRAFT WAS TOWED UNDER RIGHT ADDED IMAGES REMOVED LEFT WINGLET. REF AMM 57-31-02-000-801-C2 PERFOMED INSPECTION PER AMM 05-51-36-200-801 FROM STEP C1 TO C5 COMPLIED WITH H.F.E.C IN STEPS 1C6-11 OF AMM:05-51-36-200-801SDR CALA2023010400027Indicator · intermittentFO AIRSPEED INDICATOR READ SLOW WITH INTERMITTENT FLAG RPL FO MACH AIRSPEED INDICATOR MM34-13-02-404-004. INSPECTED ACFT FOR HIGH ENERGY STOP PER AMM TASK 05-51-14-212-001 FOUND NO DEFECTS ON ACFT.SDR CALA2022092302437Flapper Valve · damagedPDA 2 DISCOVERED AFTER LANDING AND ETOPS PDC THAT THE LOWER PRESS RELIEF VALVE ON UPPER FLAPPER DOOR MISSING. REMOVED AND REPLACED LOWER PRESSURE RELIEF VALVE REF AMM 21-32-01-402-009 COMPLETED STEPS UP. VAVLE REPLACEMENT REQUIRES STATIC SYSTEM LEAK CHECK. LEASDR CALA2022050901192None · faulty*EMERGENCY*TRAILING EDGE FLAP EICAS ON APPROACH WHEN GOING FROM FLAPS 20 TO 25. FLAPS REMAINED STUCK AT FSEU 1 BITE SHOWED FLAP LD RELIEF ON LAST FLT LEG AND NO CURRENT FAULTS. PERFORMED FIM 27-51 FAULT TREE 818. NO FAULTS FOUND AFTER CYCLING FLAPS & SYSTEM SDR CALA2021122902457Skin · corrodedBS 1500-1520 S28R-29R CORROSION COMMON TO BLANKING PLATE AND SKI N. REF AMES ILN N/R 139533-0100-0139 ON OR BEFORE 21,664 TOTAL AIRCRAFT FLIGHT CYCLES. PERFORM REPEAT REF AMES ILN N/R 139533-0100-0139 FOR DETAILS OF WORK ACCOMPLISH INSPECTIONS EVERY 3000 FLIGHSDR CALA2021122902456Skin · corrodedBS 1500-1520 S28L-29L CORROSION COMMON TO BLANKING PLATE AND SKI N. REF AMES ILN N/R 139533-0100-0139 ON OR BEFORE 21,664 TOTAL AIRCRAFT FLIGHT CYCLES. PERFORM REPEAT REF AMES ILN N/R 139533-0100-0139 FOR DETAILS OF WORK ACCOMPLISH INSPECTIONS EVERY 3000 FLIGHSDR CALA2021122702452Skin · corrodedBS 1500-1520 S28R-29R CORROSION COMMON TO BLANKING PLATE AND SKI N. REF AMES ILN N/R 139533-0100-0139 ON OR BEFORE 21,664 TOTAL AIRCRAFT FLIGHT CYCLES. PERFORM REPEAT REF AMES ILN N/R 139533-0100-0139 FOR DETAILS OF WORK ACCOMPLISH INSPECTIONS EVERY 3000 FLIGHSDR CALA2021122702451Skin · corrodedBS 1500-1520 S28L-29L CORROSION COMMON TO BLANKING PLATE AND SKI N. REF AMES ILN N/R 139533-0100-0139 ON OR BEFORE 21,664 TOTAL AIRCRAFT FLIGHT CYCLES. PERFORM REPEAT REF AMES ILN N/R 139533-0100-0139 FOR DETAILS OF WORK ACCOMPLISH INSPECTIONS EVERY 3000 FLIGHSDR CALA2021121702382Beam · corrodedREF AMES NR 0200-0109 B757-53-3-0581 UPPER CABIN FLOOR BEAM PREVIOUS REAPIR AT STA 1640 BL0 IS CORRODED. REMOVED OLD REPAIR AND INSTALLED NEW REAPIAR INCORPERATING , BLEND OUIT ON N/R 139533.0200.0121 IAW B757 SRM 53-00-51 REAPIAR #8 SEE PARTIAL WORK ON BACK ASDR CALA2021121702381Skin · bulgedAFT FUSELAGE LOWER EXTERNAL SKIN STA 1519, S28L - S29L SKIN BULG E FWD OF BLANKING PLATE. MARKED REPAIRED IAW B757 SRM 53-00-01 REPAIR 29. SEE PARTIAL WORK ACCOM PLISHED. ADD EMP:V931850SDR CALA2021121502373Floor Support · corrodedREF AMES NR 0200-0223, FLOOR SUPPORT STRUCTURE AT STA 365 RBL 46 FOUND TO BE CORRODED. BLENDED CORROSION IAW B757 SRM 53-00-51-1A-1 FOUND TO BE OUT OF LIMITS, INSTALLED NEW FLOOR SUPPORT BEAM IAW B757 SRM 51-40-02 P AR 7 ADD EMP:V921495SDR CALA2021121502372Floorbeam · corrodedREF AMES NR 0200-0110, UPPER CABIN FLOOR SUPPORT STRUCTURE CORRO DED STA 330 BL0-RBL30. REMOVED DAMAGE ORIGINAL THICKNESS .060" REMOVED .010" FOUND TO B E OUT OF LIMITS IAW B757 SRM 53-00-51 DETAIL VI REPLACED PN 141N 5160-V81 IAW B757 SRM 51-40-02 PARA 4, 7 ASDR CALA2021121502371Web · damagedREF AMES NR 0200-0252, UPPER CABIN WEB BETWEEN STA 324-344 AT RB L30 HAS A LOWER HOLE DAMAGED LOCATED ON AFT STIFFENER AT STA 330 REMOVED AND REPLACED WEB PN 141N5150-82 IAW B757 SRM 51-40-02 PA RA 4,5,7 AND BOEING DWG 141N5150 ADD EMP:V931851SDR CALA2021121402366Web · crackedREF AMES NR 0100-0123, WEB CRACKED @ STA 400 RBL 46 NEEDS REMOVE D FOR REPLACEMENT. REMVOED & REPLACED WEB STA 400 RBL 4G IAW BOEING DWG 141N5150 RE V ABD B757 SRM 51-40-02. ADD EMP:V931845SDR CALA2021121302355Floor Panel · corrodedREF AMES NR 0200-0125 B757-53-3-0575 AFT FLOOR PANEL PRESSURE WEB STA 1715 BL0-LBL40 IS CORRODED. BLENDED CORROSIONON AFT FLOOR PANEL BOEING DWG 146N5300 W/MESH FABRICATED PART PRESSURE WEB FOUND TO BE OUT OF B757 SRM 146N5318-11. SEE PARTIAL WORK ON BACK ANDSDR CALA2021121002320Floorbeam · corrodedREF AMES NR 0200-0122 B757-53-3-0575 FLOOR SUPPORT STRUCTURE STA 1660-1680 BL0 CORRODED. BLENDED, ON FLOOR SUPPORT STRUCTURE STA 1660-1680 BL0, FOUND OUT OF LIMITS. REMOVED AND REPLACED IAW B757 SRM 51-40-02 PARA 7 ADD EMP:V921265SDR CALA2021121002319None · corrodedREF AMES NR 0200-0119 B757-53-3-0575 AFT L/H LAV THE AFT O/B MOUNT IS CORRODED STA 1640. BLENDED, AFT L/H LAV O/B MOUNT. FOUND TO BE OUT OF LIMITS IAW B757 SRM 51-40-02 PARA 7 (SEE BACK AND PWS 1 OF 1 FOR WORK ACCOMPLISHED). REPLACE IAW B757 SRM 51-40-02 PARA SDR CALA2021121002318Floorbeam · corrodedREF AMES NR 0200-0109 B757-53-3-0581 UPPER CABIN FLOOR BEAM PREVIOUS REAPIR AT STA 1640 BL0 IS CORRODED. REMOVED OLD REPAIR AND INSTALLED NEW REAPIAR INCORPERATING , BLEND OUIT ON N/R 139533.0200.0121 IAW B757 SRM 53-00-51 REAPIAR #8 SEE PARTIAL WORK ON BACK ASDR CALA2021121002317Floor Support · deterioratedREF AMES NR 0100-0131 "CAUTION LIFT COVER, MAKE..." PLACARD ON INT. OF FLIGHT DECK DOOR DETERIORATED. P/N 0FG3100A29M01. REMOVED AND REPLACED FLOOR SUPPORT PN 146N5447 IAW B757 SRM 51-40-02 PARA 7 SEE REVERSER FOR PARTIAL WORK DETAILS ADD EMP:V931851SDR CALA2021120802276Skin · corrodedAFT FUSELAGE EXTERNAL SKIN STA 1519, S28R - S29R ( BLANKING PLAT E REMOVED ) CORROSION AND EXPOSED METAL. REPAIRED IAW B757 SRM 53-00-01 REPAIR 29. SEE PARTIAL WORK ACCOM PLISHED ADD EMP:V931850SDR CALA2021112902184Floor Support · corrodedFLOOR SUPPORT STRUCTURE AT STA 365 RBL 25 FOUND TO BE CORRODED. REF AMES ILN N/R 139533-0200-0224. REMOVED AND REPLACED FLOOR SUPPORT STA 365 RBL 25 IAW SRM 51-40- 02 AND BOEING DWG 141N5130. SEE AMES ILN N/R 139533-0200-0224 FOR DETAILS OF WORK ACCOMPLISH ED.SDR CALA2021111702127Skin · bulgedAFT FUSELAGE LOWER EXTERNAL SKIN STA 1519, S28L - S29L SKIN BULG E FWD OF BLANKING PLATE. MARKED REPAIRED IAW B757 SRM 53-00-01 REPAIR 29. SEE PARTIAL WORK ACCOM PLISHED. ADD EMP:V931850SDR CALA2021111702126Skin · corrodedAFT FUSELAGE EXTERNAL SKIN STA 1519, S28R - S29R ( BLANKING PLAT E REMOVED ) CORROSION AND EXPOSED METAL. REPAIRED IAW B757 SRM 53-00-01 REPAIR 29. SEE PARTIAL WORK ACCOM PLISHED ADD EMP:V931850SDR CALA2021070501025Oven · shortedAFT GALLEY OVEN 411 SMOKED CB PULLED SMOKE LINGERED ON FOR 15 MI N THEN SLOWLY DISSIPATED CONDUCTED TASK 05-51-58-910-801-C1. INSTALLED OVEN AT POSITION 411. PER AMM TASK 25-34-00-400-801-C3. RAN OVEN FOR 15 MIN. OPS CHK GOOD. ADD EMP:181152 ROTABLE PARTS CHAN
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