N18119
Service difficulty reports · 98
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 = 'N18119' 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 = 'N18119' 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 CALA2026102220513None · noneTHE TOMC CONTROLLER AND SENIOR MANAGER CONCUR THAT THE AIRCRAFT CAN BE RELEASED BACK TO SERVICE AFTER EXPERIENCING A DIVERSION OR AIR TURN BACK DUE TO A MECHANICAL REASON LOCKED BY SYSTEM. UNLOCKING AIRCRAFT DIVERTED INTO BOSTON FOR LAV SERVICING. NO MECHANICASDR CALA2026090719290O-Ring · faultyRIGHT HYD QTY, FLUID LOSS RT WING, FOUND NR 11 SPOILER PCA LEAKING AT THE HYDRAULIC RETURN END CAP. O-RING FAILED. CREW SHUT OFF RIGHT HYD IN FLIGHT. HYD LEVEL ON RETURN WAS READING 44 RF. R & R NR 11 PCA IAW AMM 27-61-02-022-001 AND AMM 27-61-02-422-027. SDR CALA2026082518870Bearing · meltedPER FLT CREW, ON TAXI HAVING DIFFICULTY MOVING AND TURNING, MX REQUESTED TO INSPECTREQUIRES FURTHER INSPECTION. AFTER FURTHER GVI DETERMINED THAT UPON LANDING RT NOSE WHEEL BEARINGS FAILED CAUSING WHEEL ASSY TO MELT DOWN BEAR METAL. WHEEL ASSY BORED OVERSIZE SDR CALA2026062317287Light · broken24C FLOOR EMERGENCY LIGHTING DAMAGED PICTURE ADDED SECURED LIGHT HOUSING AND TESTED LIGHT. BOTH THE HOUSING AND THE LIGHT ARE GOOD. TRIM AT SEAT 24C BROKEN, SECURED IN PLACE. EPL WORKS. RESECURED WITH ZIP TIES. APPROVED TRIM AT SEAT 24C PLACED. A PASSENGERSDR CALA2026042215614Cover · unsecureDDOR 1L DOES NOT LOOK FLUSH WHEN CLOSE RESECURED SLIDE COVER OK TO CONTINUESDR CALA2026020413581Access Door · dentedRIGHT AFT FUSELAGE, OTBD SIDE OF THE APU FIRE BOTTLE ACCESS DOOR HAS ONE DENT. ACCOMPLISHED REPAIR IAW ECRA 5380-01438 AND EA 757-5380-13-A4248 WITHOUT DEVIATION. THIS IS A PERMANENT REPAIR WITHOUT LIMITATIONS.SDR CALA2026012713343Frame · dentedAFT CARGO COMPARTMENT BS 1580 LBL 35, FRAME HAS ONE DENT. REPAIRED AFT CARGO COMPARTMENT STA 1580 AT LBL35 FRAME PER EA 75 7-5360-13-A4246 REV- AND EC/RA 5360-02096. ESFR 2895 WC: 13925 1.SDR CALA2026012313226Skin · corrodedLEFT WING TIP, TRIALING EDGE UPPER SKIN SURFACE, SHOWS EVIDENCE OF CORROSION. REMOVED AND REPLACED UPPER PLATE AT LH WING TIP, TRAILING EDGE P ANEL BTW WBL 740 TO WBL 757 IAW SRM 51-40-02-OG-0 AND DWG 119N00030001. RESTORED PROTECTION SURFACE IAW AMM 51 -21-SDR CALA2026012313220Transition Panel · corrodedAFT CARGO BAY BS 1200 - 1280, LT TRANSITION PANEL UPPER AND LOWER SURFACES HAD 12 SPOTS OF CORROSION. REMOVED AND REPLACED THE TRANSITION PANEL IAW SRM 51-40-02-0G-0. DRAWING 146N5391. AND RESTORED PROTECTION SURFACE IAW SRM 51-21-01.SDR CALA2026012313217Plate · corrodedAFT CARGO BAY BS 1380 RT FRAME AREA BELOW TRANSITION PANEL HAS CORROSION. AFTER FURTHER EVALUATION FOUND CUT LIMITS FOR EXFOLIATION IAW SRM 51-10-08, AND TWO ANGLES AND TIE DOWN, REMOVED AND REPL ACED THE ANGLE AND TIE DOWN IAW SRM 51-40-02-0G.SDR CALA2026012313215Transition Panel · corrodedBS 1300-1340 LT TRANSITION PANEL HAD CORROSION AND CRACKED. REMOVED AND REPLACED THE TRANSITION PANEL BS 1300-1340 IAW SRM 51-40-02-0G-0, AND RESTORED PROTECTION SURFACE IAW SRM 51-21-01 AND AMM 51-21 -14.SDR CALA2026012313213Angle · corrodedAFT CARGO COMPARTMENT BS 1380, RBL 30, DOOR CUTOUT FRAME ANGLE HAS CORROSION. AFTER FURTHER EVALUATION FOUND OUT OF LIMITS FOR EXFOLIATION AND CRACKS IAW SRM 51-10-08-0G, ANGLE AND INTERCOSTAL REMOVED AND REPLACED IAW SRM 51-40-02 -0G.SDR CALA2026012313195Frame · deformedAFT CARGO COMPARTMENT STA 1320 RBL 35, FRAM HAS ONE DENT. COMPLIED WITH ECRA 5360-02095 AND VTMAE EA 757-5360-13-A4247 RE V. ACCOMPLSIHED FRAME REPAIR BS 1320 RBL 35.SDR CALA2026012213166Transition Panel · corrodedAFT CARGO BAY, BS 1440 RT TRANSITION PANEL AND LOWER SPLICE HAD CORROSION. REMOVED AND REPLACED THE TRANSITION PANEL SPLICE IAW SRM 51-40-02-OG-0.SDR CALA2026012213164Transition Panel · corrodedAFT CARGO BAY, BS 1380-1440 RT TRANSITION PANEL LOWER & UPPER SURFACES HAVE CORROSION. REMOVED AND REPLACED THE TRANSITION PANEL BS 1380 - 1440, RBL 45 IAW SRM 51-40-02-OG-0.SDR CALA2026012213162Transition Panel · corrodedAFT CARGO BAY BS 1300-1320 RT TRANSITION PANEL LOWER SPLICE HAS EXFOLIATION. REMOVED AND REPLACED THE TRANSITION PANEL LOWER SPLICE BS 1310, RBL 45 - 50 IAW SRM 51-40-02-OG-0.SDR CALA2026012213160Transition Panel · corroded(SDR) 53-5300-1-0011: AFT CARGO COMPARTMENT STA 1480 LH TRANSITION PANEL LOWER SURFACE EXFOLIATED. REMOVED AND REPLACED TRANSITION PANEL IAW SRM 51-40-02-OG, & RESTORED SURFACE PROTECTION IAW SRM 5 1-21-01SDR CALA2026012213156Transition Panel · corrodedAFT CARGO COMPARTMENT BS 1200-1300 RT TRANSITIONAL PANEL UPPER & LOWER SURFACES HAD 10 SPOTS WITH CORRSION & 1 CRACK. REMOVED AND REPLACED THE TRANSITION PANEL IAW 51-40-01-0G & DRAWING 146N5391.SDR CALA2026012213154Transition Panel · corrodedAFT CARGO COMPARTMENT BS 1380 RT TRANSITION PANEL HAS EXFOLIATION. AFTER DETAIL INSPECTION, THE EXFOLIATION IS PRESENT IN 100% IAW SRM 51-10-08, REMOVED AND REPLACED TRANSITON PANEL IAW SRM 51-40-02-OG.SDR CALA2026011312926Web · corrodedBS 1280-1300 CORROSION COMMON TO WEB. REMOVED AND REPLACED THE WEB 146N5425-27 IAW SRM 51-40-20-OG-0 REV 50.SDR CALA2025112811533Smoke Warning · false activationLAV SMOKE TWICE IN FLT WENT OUT FA SUSPECT OVEN NEXT TO AFT LAV PLEASE MEET CREW WITH SMOKE/ODOR FORMS AND SEND BACK TO TOMC. IN ADDITION, REF AMM TASK 05-51-58-910-801-C1 CONDITIONAL INSP UNLOCKING LOG PAGE REMOVED ITEMS AND CLEANED OVENS. OPS CHECK GOOD, NO SDR CALA2025110410902Warning Message · illuminatedRIGHT CENTER FUEL PUMP STILL DISPLAYS ON FLOW BAR WHEN DESELECTE D PRESS LIGHT NOT ON MECHANICAL WINDOW THAT SHOWS/HIDES FLOW BAR INOP. PULLED AND COLLARED R FUEL OVRD PUMP BREAKER ON P6. INSTALLED TAPE OVER CENTER FUEL PUMP RIGHT SWITCH, WHEN CLEARING DEFERRASDR CALA2025081807895Blower · faultedAFTER T/O, VIBRATIONS BETWEEN ROWS 2 TO 11. DID NOT SUBSIDE WITH VARYING SPEEDS AT ALT. CREW STATES VIBRATION STARTED AT APPROX 10K FT IN FLT. INCREASED WITH SPEED. ON RETURN BELOW 10K FT VIBRATION IMPROVED BUT NEVER WENT AWAY. VIBRATION FELT IN FLOORBOARD. SDR CALA2025062705976Cover · dented1L SLIDE COVER HAVE A DENT. REPLACED DOOR 1L BUSSELL/ COVER REF AMM 52-11-02-904-004.SDR CALA2025042804282Charger · faultedSTATUS MSG MAIN BAT CHGR. UNABLE COUPLED ILS MAIN BATT CHARGER SWAPPED WITH APU BAT CHARGER AS PER AMM 24-31- 00 MAIN BAT CHARGER ON PN S282T002-6 SN4034 APU BAT CHARGER ON PN S282T002-6 SN C5522 MAIN BATTERY SWAPPED WITH APU BATTERY AS PER AMM 24-31-00 MAIN BSDR CALA2025030502600Girt Bar · fodAIRCRAFT R1 DOOR UNABLE TO DISARM. REMOVED DEBRIS FROM DOOR GIRT BAR OPS CHECKS GOOD OK TO CONTINUE.SDR CALA2025010601782Oven · dirtyCREW REPORTING ONE OF THE TRASH BIN TEMP SENSOR OF EITHER OF THE AFT 2 LAVS INDICATES A GREY DOT ABOVE 200 F. FOR THE AFT 2 LAVS, PERFORM INSPECTION OF THE TEMP STRIP INDICATORS REF AMM 26-24-01-702, CONFIRM THAT THE FIRE EXT BOTTLE FUSIBLE TIPS HAVE NOT MELTESDR CALA2024112002909Skin · dented9B757-57-06-3-0248) DOT 210-18 R/H WING I/B FLAP O/B SIDE HAS MA RK/DENT. REF NR 114209. REPAIRED FLAP LE SKIN IAW SRM 57-53-01-2R-2. VERIFIED INSPECTION PERFORMED RIISDR CALA2024112002908Skin · gouged(B757-57-06-3-0248) R/H WING MAIN FLAP I/B AT MFSTA 153.43 WITH GOUGE. REF NR 114426. REPAIRED FLAP LE SKIN IAW SRM 57-53-01-2R-2. VERIFIED INSPECTION PERFORMED RIISDR CALA2024093000714Fuel Cap · faultyLEFT OVERWING FUEL CAP LEAKING IN FLIGHT REMOVED AND REPLACED LEFT OVERWING FUEL FILL CAP PER B757-200 AMM 28-11-04. B757-200 IPC 28-11-04 ITEM 50 P/N 38222-3. PERFORMED LEAK CHECK AFTER FUEL SERVICE. LT TANK AT 15000LBS AND NO LEAKS OBSERVED.SDR CALA2024060701733Indicator · bindingTE FLAP DISAGREE STUCK AT 20 UPON CREW DEBRIEF FLAP INDICATOR STUCK AT 20 AT SHUTDOWN POWER FSEU # 28N011-40, NO FAULTS FOUND ON 2/3. FSEU 1 FLAP DISAGREE INSTALLATION TEST AMM 27-58-02-704-010.ALL CHECKED GOOD. X-FER INDICATOR WENT TO PILOT REQUESTED 25. INSPSDR CALA2024050601326None · noneBIRD STRIKE NOTED DURING WALK AROUND ON LH WING ROOT, JUST BESIDE LANDING LIGHT BIRDSTRIKE CLEANED AND AREA INSPECTED IAW AMM 05-51-18 REV 133 20JAN24. NO DAMAGE NOTEDSDR CALA2024042301203Handle · bindingDOOR-MOUNTED ESCAPE SYSTEM DOOR 1R - A EVACUATION SLIDE PROBLEM WAS ENCOUNTERED WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS ARMING LEVER BINDING. EXCESSIVE FORCE NEEDED TO MOVE LEVER TO AR MED POSITION CLEANED DEBRIS FROM BOTTOM DOOR SILL WHERE GIRT BAR ENSDR CALA2024040300959Toilet · inoperativeNO LAVS FLUSHING SERVICED ALL LAVS IN ACCORDANCE WITH AMM 12-17-01-613-001. ALL 4 TOILETS FLUSH.SDR CALA2023112003424Blower · inoperativeCARGO DET AIR STATUS MESSAGE. REMOVED AND REPLACED AFT BLOWER FAN M10464 IAW AMM 26-16-02 OPS CHECK SAT.SDR CALA2023052401635Skin · dentedUNDOCUMENTED DENT DISCOVERED AT BS 1480 + 19 BETWEEN S24R-S25R. DIMENSIONS: 5.00"L X 2.65"W X .125"D AND IS .5" FROM BS 1500 & S24R. PER SRM 53-00-01 ALLOWABLE DAMAGE 1 FIGURE 101 DETAIL III. DENT OUT OF LIMITS. UE DIP FOR INSPECTION REQUIREMENTS TABLE 206/REPSDR CALA2023050901427Frame · crackedCABIN FRAME CRACKED BETWEEN S8RT AND S9RT, AT I/B RIVET FOR PSU RAIL ATTACHMENT AT STA. 1240RT 001234528. INSPECTION REQUIREMENTS ZONE 3 INSPECTION THRESHOLD: AIRFRAME FLIGHT CYCLES, WHICHEVER COMES FIRST. REPEAT 12,000 FLIGHT CYCLES FROM REPAIR INSTALLATION, SDR CALA2023050901426Frame · crackedCABIN FRAME CRACKED AY STA 460 LT BETWEEN S8LT AND S9LT AT PSU RAIL ATTACH BRACKET I/B ATTACH RIVET 001234528. INSPECTION REQUIREMENTS ZONE 3 INSPECTION THRESHOLD: AIRFRAME FLIGHT CYCLES, WHICHEVER COMES FIRST. REPEAT 12,000 FLIGHT CYCLES FROM REPAIR INSTALLATSDR CALA2023050501360Skin · damagedL4 DOOR UPPER DOOR TORQUE TUBE CUTOUT DAMAGED REPAIRED L4 DOOR INNER SKIN DAMAGE STA 1656 BTW HINGE CTR LINE AND BEAM #3 REF ECRA 5210-03284 SEE NR 001262457 FOR ALL WORK PERFORMED. VERIFIED REPAIRED L4 DOOR INNER SKIN DAMAGE STA 1656 BTW HINGE CTR LINE AND BESDR CALA2023021000380Sign · smokeLAVATORY SMOKE EICAS AND ALARM. FOUND PRINTED CIRCUIT BOARD ON NS/FSB SIGN LOOSE MAKING CONTACT WITH LAV S COMPOSITE WALL WHICH OVERHEATED AND CREATED SMOKE IN THE LAV. REPLACED NS/FSB SIGN REF AMM 33-24-00-962-081. OP'S CHECK GOOD REF AMM 33-24-00-710-801.SDR CALA2023012000162Battery Pack · inoperativeR&R EMERGENCY LIGHT BATERY PACK LOCATED IN GALLEY AREA LIGHT PANEL BETWEEN L3 AND R3 DOOR. BATTERY PACK DID NOT HOLD CHARGE REMOVED AND REPLACED EMERGENCY LIGHT BATERY PACK LOCATED IN GALLEY AREA LIGHT PANEL BETWEEN L3 AND R3 DOOR. IAW AMM 33-51-07 REV. 130SDR CALA2023012000161Battery Pack · inoperativeR&R EMERGENCY LIGHT BATERY PACK LOCATED AFT OF THE GALLEY AREA LIGHT PANEL BETWEEN L1 AND R1 DOOR. BATTERY PACK DID NOT HOLD CHARGE REMOVED AND REPLACED EMERGENCY LIGHT BATERY PACK LOCATED AFT OF THE GALLEY AREA LIGHT PANEL BETWEEN L1 AND R1 DOOR. IAW AMM 35-5SDR CALA2018121702587Acm · inoperativeACRID SMELL IN CLIMBOUT BOTH IN CABIN AND COCKP IT...HIGH ENGINE VIBRAT ION ON RIGHT ENGINE 2.7 RECIEVED A/C, FLT AND CABIN CREWS FILLED OUT SMOKE/ ODOR QUESTIONAIRE 46.6020 AND RESULTS SENT TO TOMC. C/W AMM 05-51-58-910-801C SMOKE/ODOR CONDITIONAL INSPECTION SDR CALA2018121102553Transmitter · inoperativeRT ENG VIB IND IN AMBER BAND HIGHEST NOTED APROX 3.4 REF FIM 77-31-00-815-807-R04 BLOCK 27 REPLACEMENT OF VIBRATION ACCELEROMETER. REPLACED ACCELEROMETER REF AMM 77-31-01-404-020-ROO. VIBRATION CKS GOOD HIGHEST VIB NOTED AT .07 DURING ENG RUN. ADD EMP:U00548SDR CALA2018081731793Power Supply · inoperativeSEVERAL BULL NOSE EMERGENCY LIGHTS WERE INOPERATIVE THROUGHOUT THE CABIN. REPLACED THE POWER SUPPLY 736 IAW AMM 33-51-07. LIGHTS OPS CHECKED OK.SDR CALA2018081731792Power Supply · inoperativeR4 DOOR EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE POWER SUPPLY IAW AMM 3-51-07. LIGHT OP CHECKED OK.SDR CALA2018081731791Wire · shortedCABIN SEAT EMERGENCY LIGHTS WERE INOPERATIVE ON THE LEFT SIDE OF THE ACFT FROM ROWS 8 TO 30. FOUND WIRES SHORTED AT SEAT 11ABC. CAPPED AND STOWED THE WIRES. LIGHTS FROM ROWS 8 THRU 30 WORK OK.SDR CALA2018020900550Sign · detachedLEFT OVERWING EMERGENCY EXIT SIGN FOUND DETACHED.SDR CALA2018012600311Altimeter · out of toleranceAT 360 CAPTAIN`S ALTIMETER 36100, FIRST OFFICER`S 360, STBY 349. REPLACED INDICATOR IAW MM 34-13-06-404 -002.SDR CALA2017122504594Controller · failedOVENS NR 1 AND 2 IN 1ST CLASS BOTH OVERHEAT WITH ASSOCIATED ELECTRICAL WIRE ODOR. REMOVED AND REPLACED THE OVEN TEMP CONTROLLERS. RAN BOTH OVENS FOR 10 MINUTES ON HIGH, NO METALLIC ODORS NOTED.
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