# Service difficulty reports: N18119

A list on [N18119](https://openairdocs.org/aircraft/N18119.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 98 reports

- [SDR CALA2026102220513](https://openairdocs.org/sdr/CALA2026102220513.md): None · none · Oct 19, 2026 · N18119 · Boeing 757224 · Standard Practices/Structures
  > THE 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 MECHANICA
- [SDR CALA2026090719290](https://openairdocs.org/sdr/CALA2026090719290.md): O-Ring · faulty · Sep 3, 2026 · N18119 · Boeing 757224 · Hydraulic System, Main
  > RIGHT 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 CALA2026082518870](https://openairdocs.org/sdr/CALA2026082518870.md): Bearing · melted · Aug 22, 2026 · N18119 · Boeing 757224 · Nose/Tail Landing Gear
  > PER 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 CALA2026062317287](https://openairdocs.org/sdr/CALA2026062317287.md): Light · broken · Jun 19, 2026 · N18119 · Boeing 757224 · Emergency Lighting
  > 24C 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 PASSENGER
- [SDR CALA2026042215614](https://openairdocs.org/sdr/CALA2026042215614.md): Cover · unsecure · Apr 19, 2026 · N18119 · Boeing 757224 · Escape Slide
  > DDOR 1L DOES NOT LOOK FLUSH WHEN CLOSE RESECURED SLIDE COVER OK TO CONTINUE
- [SDR CALA2026020413581](https://openairdocs.org/sdr/CALA2026020413581.md): Access Door · dented · Jan 26, 2026 · N18119 · Boeing 757224 · Fuselage Main, Plate/Skin
  > RIGHT 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 CALA2026012713343](https://openairdocs.org/sdr/CALA2026012713343.md): Frame · dented · Jan 25, 2026 · N18119 · Boeing 757224 · Fuselage Main, Frame
  > AFT 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 CALA2026012313226](https://openairdocs.org/sdr/CALA2026012313226.md): Skin · corroded · Jan 22, 2026 · N18119 · Boeing 757224 · Wing, Plate/Skin
  > LEFT 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 CALA2026012313220](https://openairdocs.org/sdr/CALA2026012313220.md): Transition Panel · corroded · Jan 22, 2026 · N18119 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT 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 CALA2026012313217](https://openairdocs.org/sdr/CALA2026012313217.md): Plate · corroded · Jan 22, 2026 · N18119 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT 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 CALA2026012313215](https://openairdocs.org/sdr/CALA2026012313215.md): Transition Panel · corroded · Jan 22, 2026 · N18119 · Boeing 757224 · Fuselage Miscellaneous Structure
  > BS 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 CALA2026012313213](https://openairdocs.org/sdr/CALA2026012313213.md): Angle · corroded · Jan 22, 2026 · N18119 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT 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 CALA2026012313195](https://openairdocs.org/sdr/CALA2026012313195.md): Frame · deformed · Jan 21, 2026 · N18119 · Boeing 757224 · Fuselage Main, Frame
  > AFT 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 CALA2026012213166](https://openairdocs.org/sdr/CALA2026012213166.md): Transition Panel · corroded · Jan 21, 2026 · N18119 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT 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 CALA2026012213164](https://openairdocs.org/sdr/CALA2026012213164.md): Transition Panel · corroded · Jan 21, 2026 · N18119 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT 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 CALA2026012213162](https://openairdocs.org/sdr/CALA2026012213162.md): Transition Panel · corroded · Jan 21, 2026 · N18119 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT 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 CALA2026012213160](https://openairdocs.org/sdr/CALA2026012213160.md): Transition Panel · corroded · Jan 21, 2026 · N18119 · Boeing 757224 · Fuselage Miscellaneous Structure
  > (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 1-21-01
- [SDR CALA2026012213156](https://openairdocs.org/sdr/CALA2026012213156.md): Transition Panel · corroded · Jan 21, 2026 · N18119 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT 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 CALA2026012213154](https://openairdocs.org/sdr/CALA2026012213154.md): Transition Panel · corroded · Jan 21, 2026 · N18119 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT 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 CALA2026011312926](https://openairdocs.org/sdr/CALA2026011312926.md): Web · corroded · Jan 12, 2026 · N18119 · Boeing 757224 · Fuselage Miscellaneous Structure
  > BS 1280-1300 CORROSION COMMON TO WEB. REMOVED AND REPLACED THE WEB 146N5425-27 IAW SRM 51-40-20-OG-0 REV 50.
- [SDR CALA2025112811533](https://openairdocs.org/sdr/CALA2025112811533.md): Smoke Warning · false activation · Nov 24, 2025 · N18119 · Boeing 757224 · Smoke Detection
  > LAV 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 CALA2025110410902](https://openairdocs.org/sdr/CALA2025110410902.md): Warning Message · illuminated · Nov 1, 2025 · N18119 · Boeing 757224 · Fuel Boost Pump
  > RIGHT 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 DEFERRA
- [SDR CALA2025081807895](https://openairdocs.org/sdr/CALA2025081807895.md): Blower · faulted · Aug 14, 2025 · N18119 · Boeing 757224 · Smoke Detection
  > AFTER 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 CALA2025062705976](https://openairdocs.org/sdr/CALA2025062705976.md): Cover · dented · Jun 23, 2025 · N18119 · Boeing 757224 · Escape Slide
  > 1L SLIDE COVER HAVE A DENT. REPLACED DOOR 1L BUSSELL/ COVER REF AMM 52-11-02-904-004.
- [SDR CALA2025042804282](https://openairdocs.org/sdr/CALA2025042804282.md): Charger · faulted · Apr 24, 2025 · N18119 · Boeing 757224 · Battery/Charger System
  > STATUS 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 B
- [SDR CALA2025030502600](https://openairdocs.org/sdr/CALA2025030502600.md): Girt Bar · fod · Mar 3, 2025 · N18119 · Boeing 757224 · Emergency Equipment
  > AIRCRAFT R1 DOOR UNABLE TO DISARM. REMOVED DEBRIS FROM DOOR GIRT BAR OPS CHECKS GOOD OK TO CONTINUE.
- [SDR CALA2025010601782](https://openairdocs.org/sdr/CALA2025010601782.md): Oven · dirty · Jan 2, 2025 · N18119 · Boeing 757224 · Buffet/Galleys
  > CREW 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 MELTE
- [SDR CALA2024112002909](https://openairdocs.org/sdr/CALA2024112002909.md): Skin · dented · Nov 19, 2024 · N18119 · Boeing 757224 · Trailing Edge Flaps
  > 9B757-57-06-3-0248) 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 RII
- [SDR CALA2024112002908](https://openairdocs.org/sdr/CALA2024112002908.md): Skin · gouged · Nov 19, 2024 · N18119 · Boeing 757224 · Trailing Edge Flaps
  > (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 RII
- [SDR CALA2024093000714](https://openairdocs.org/sdr/CALA2024093000714.md): Fuel Cap · faulty · Sep 30, 2024 · N18119 · Boeing 757224 · Fuel Storage
  > LEFT 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 CALA2024060701733](https://openairdocs.org/sdr/CALA2024060701733.md): Indicator · binding · Jun 7, 2024 · N18119 · Boeing 757224 · Trailing Flap Position Indicating System
  > TE 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. INSP
- [SDR CALA2024050601326](https://openairdocs.org/sdr/CALA2024050601326.md): None · none · May 2, 2024 · N18119 · Boeing 757224 · Standard Practices/Structures
  > BIRD 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 NOTED
- [SDR CALA2024042301203](https://openairdocs.org/sdr/CALA2024042301203.md): Handle · binding · Apr 20, 2024 · N18119 · Boeing 757224 · Service Doors
  > DOOR-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 EN
- [SDR CALA2024040300959](https://openairdocs.org/sdr/CALA2024040300959.md): Toilet · inoperative · Mar 31, 2024 · N18119 · Boeing 757224 · Waste Disposal System
  > NO LAVS FLUSHING SERVICED ALL LAVS IN ACCORDANCE WITH AMM 12-17-01-613-001. ALL 4 TOILETS FLUSH.
- [SDR CALA2023112003424](https://openairdocs.org/sdr/CALA2023112003424.md): Blower · inoperative · Nov 19, 2023 · N18119 · Boeing 757200 · Detection System
  > CARGO DET AIR STATUS MESSAGE. REMOVED AND REPLACED AFT BLOWER FAN M10464 IAW AMM 26-16-02 OPS CHECK SAT.
- [SDR CALA2023052401635](https://openairdocs.org/sdr/CALA2023052401635.md): Skin · dented · May 23, 2023 · N18119 · Boeing 757224 · Fuselage Main, Plate/Skin
  > UNDOCUMENTED 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/REP
- [SDR CALA2023050901427](https://openairdocs.org/sdr/CALA2023050901427.md): Frame · cracked · May 8, 2023 · N18119 · Boeing 757224 · Fuselage Structure (General)
  > CABIN 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 CALA2023050901426](https://openairdocs.org/sdr/CALA2023050901426.md): Frame · cracked · May 8, 2023 · N18119 · Boeing 757200 · Fuselage Structure (General)
  > CABIN 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 INSTALLAT
- [SDR CALA2023050501360](https://openairdocs.org/sdr/CALA2023050501360.md): Skin · damaged · May 3, 2023 · N18119 · Boeing 757224 · Passenger/Crew Doors
  > L4 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 BE
- [SDR CALA2023021000380](https://openairdocs.org/sdr/CALA2023021000380.md): Sign · smoke · Feb 10, 2023 · N18119 · Boeing 757200 · Standard Practices/Structures
  > LAVATORY 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 CALA2023012000162](https://openairdocs.org/sdr/CALA2023012000162.md): Battery Pack · inoperative · Jan 19, 2023 · N18119 · Boeing 757224 · Emergency Lighting
  > R&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. 130
- [SDR CALA2023012000161](https://openairdocs.org/sdr/CALA2023012000161.md): Battery Pack · inoperative · Jan 19, 2023 · N18119 · Boeing 757224 · Emergency Lighting
  > R&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 35-5
- [SDR CALA2018121702587](https://openairdocs.org/sdr/CALA2018121702587.md): Acm · inoperative · Dec 15, 2018 · N18119 · Boeing 757224 · Cabin Cooling System
  > ACRID 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 CALA2018121102553](https://openairdocs.org/sdr/CALA2018121102553.md): Transmitter · inoperative · Dec 10, 2018 · N18119 · Boeing 757224 · Engine Vibration Analyzer
  > RT 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:U00548
- [SDR CALA2018081731793](https://openairdocs.org/sdr/CALA2018081731793.md): Power Supply · inoperative · Aug 12, 2018 · N18119 · Boeing 757224 · Emergency Lighting
  > SEVERAL BULL NOSE EMERGENCY LIGHTS WERE INOPERATIVE THROUGHOUT THE CABIN. REPLACED THE POWER SUPPLY 736 IAW AMM 33-51-07. LIGHTS OPS CHECKED OK.
- [SDR CALA2018081731792](https://openairdocs.org/sdr/CALA2018081731792.md): Power Supply · inoperative · Aug 12, 2018 · N18119 · Boeing 757224 · Emergency Lighting
  > R4 DOOR EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE POWER SUPPLY IAW AMM 3-51-07. LIGHT OP CHECKED OK.
- [SDR CALA2018081731791](https://openairdocs.org/sdr/CALA2018081731791.md): Wire · shorted · Aug 12, 2018 · N18119 · Boeing 757224 · Light System Wiring
  > CABIN 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 CALA2018020900550](https://openairdocs.org/sdr/CALA2018020900550.md): Sign · detached · Feb 9, 2018 · N18119 · Boeing 757224 · Emergency Lighting
  > LEFT OVERWING EMERGENCY EXIT SIGN FOUND DETACHED.
- [SDR CALA2018012600311](https://openairdocs.org/sdr/CALA2018012600311.md): Altimeter · out of tolerance · Jan 26, 2018 · N18119 · Boeing 757224 · Altimeter, Barometric/Encoder
  > AT 360 CAPTAIN`S ALTIMETER 36100, FIRST OFFICER`S 360, STBY 349. REPLACED INDICATOR IAW MM 34-13-06-404 -002.
- [SDR CALA2017122504594](https://openairdocs.org/sdr/CALA2017122504594.md): Controller · failed · Dec 25, 2017 · N18119 · Boeing 757224 · Buffet/Galleys
  > OVENS 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.

Next page: https://openairdocs.org/aircraft/N18119/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N18119/reports

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