# Service difficulty reports: N57855

A list on [N57855](https://openairdocs.org/aircraft/N57855.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 · 61 reports

- [SDR CALA2026083119028](https://openairdocs.org/sdr/CALA2026083119028.md): A/C Pack · malfunctioned · Aug 26, 2026 · N57855 · Boeing 757324 · Air Conditioning System
  > LEFT PACK OFF LIGHT NOT LIGHT DURING L ENG START. SMELL OF FUEL, POST START WITH PACK OFF. REF TO LP 3111827 FOR WORK PERFORMED, DURING ENG START LT PACK OFF LIGHT WAS ILLUMINATED AND NO FUEL ODOR WAS NOTED, FOLLOWING ENG START WITH PACK OFF / PACK ON OPER
- [SDR CALA2026080518334](https://openairdocs.org/sdr/CALA2026080518334.md): Elec Connector · unsecure · Aug 3, 2026 · N57855 · Boeing 757324 · Light System Wiring
  > PER FLIGHT CREW, AFTER TAKE OFF BEFORE 10,000 FT, CABIN WORK LIGHTS AT ALL 3 FLIGHT ATTENDANT STATIONS FLICKERING & FLASHING WITH SWITCH OFF. ALL OVERHEAD LIGHTS THROUGHOUT CABIN FLICKERING WITH SWITCH OFF. F/A STATED OVERHEAD LIGHTS WERE A ORANGE COLOR. FW
- [SDR CALA2026072818062](https://openairdocs.org/sdr/CALA2026072818062.md): Oven · smoke · Jul 24, 2026 · N57855 · Boeing 757324 · Buffet/Galleys
  > SMOKE CAME OUT OF OVEN 204. OVEN TURNED OFF. SMOKE FIRE FUMES CHECKLIST PERFORMED. SMOKE DISSIPATED. SYSTEMS RESTORED. FLIGHT CREW SMOKE/ODOR QUESTIONAIRE OVEN 204 IS INOP DO TO SMOKE IN CABINE. OPEN CB, AND INOP DECAL. NOC.APPROVED NEF 2520P INOP OVEN 204 CB
- [SDR CALA2026052216452](https://openairdocs.org/sdr/CALA2026052216452.md): Lamp · no test · May 20, 2026 · N57855 · Boeing 757324 · Emergency Lighting
  > EMERGENCY LIGHTS, OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE. DOOR 4L AND 4R EMERGENCY LIGHTS DO NOT ILLUIMINATE WHEN EMERGENCY LIGHTS ARE TESTED. CLEANED 4L AND REPLACED LAMP AT 4R, BOTH CHKD OK IAW AMM 33-51-00
- [SDR CALA2026040315063](https://openairdocs.org/sdr/CALA2026040315063.md): Web · loose · Apr 3, 2026 · N57855 · Boeing 757324 · Nacelle/Pylon, Main Frame
  > NR 2 PYLON UPPER CENTER WEB IS GOUGED FROM LOOSE AND MIGRATING BRACKET 11.25" FROM AFT EDGE OF CENTER WEB AND 5.25" FROM PYLON CENTERLINE. SEE BAM N/R 3300210 AND EC/RA 5450-03117 FOR WORK PERFORMED. MAJOR REPAIR OF NR 2 ENGINE PYLON STRUT UPPER SPAR AFT WEB
- [SDR CALA2026022414048](https://openairdocs.org/sdr/CALA2026022414048.md): Pin · out of adjust · Feb 23, 2026 · N57855 · Boeing 757324 · Fixed Inner Doors
  > FLT DECK DOOR WILL NOT STAY CLOSED EVEN WITH HARD LOCK PIN LOCK PIN WILL NOT PROPERLY ENGAGE. ADJUSTED MECHANICAL CATCH PIN, FLIGHT DECK DOOR CLOSES AND OPENS NORMAL, AND STAYS CLOSED WITH MANUAL LOCK PIN INSTALLED. IAW AMM 52-52-01-400-801-C1. AND AUTOMA
- [SDR CALA2026021813889](https://openairdocs.org/sdr/CALA2026021813889.md): Bulb · inoperative · Feb 8, 2026 · N57855 · Boeing 757324 · Emergency Lighting
  > L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE BULB IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR CALA2025121512127](https://openairdocs.org/sdr/CALA2025121512127.md): Lamp · inoperative · Dec 14, 2025 · N57855 · Boeing 757324 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - MID CABIN CENTER AISLE EMERGENCY EXIT SIGN NEEDS RELAMPED RELAMED AS REQUIRED REF AMM 33-51-10-962-001-002 CK OK
- [SDR CALA2025121512125](https://openairdocs.org/sdr/CALA2025121512125.md): Lamp · inoperative · Dec 14, 2025 · N57855 · Boeing 757324 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - 3L DOOR EMERGENCY EXIT IDENTIFIER REQUIRES RELAMP RELAMED AS REQUIRED REF AMM 33-51-10-962-040 CK OK.
- [SDR CALA2025121512123](https://openairdocs.org/sdr/CALA2025121512123.md): Lamp · inoperative · Dec 14, 2025 · N57855 · Boeing 757324 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - LEFT OVERWING DOOR EMERGENCY EXIT IDENTIFIERS NEED RELAMPED RELAMED AS REQUIRED REF AMM 33-51-10-962-040 CK OK
- [SDR CALA2025111711235](https://openairdocs.org/sdr/CALA2025111711235.md): Sign · unsecure · Nov 15, 2025 · N57855 · Boeing 757324 · Emergency Lighting
  > OVERHEAD WING EMERGENCY EXIT SIGN IS FALLING OFF THE CEILING. SECURED LIGHT WITH HARDWARE. OPS CHECK EMERGENCY LIGHT REF AMM33-51-01-402. OK FOR SERVICE
- [SDR CALA2025102010282](https://openairdocs.org/sdr/CALA2025102010282.md): Light · intermittent · Oct 20, 2025 · N57855 · Boeing 757324 · Emergency Lighting
  > EMERGENCY LIGHT ABOVE DOOR 2L FLICKERED AND WENT OUT OPS CHECKED EMERGENCY LIGHTING OPS CHECK NORMAL. OPS CHECKED MANUALLY AT DOOR OPS CHECK NORMAL NO FLICKER.
- [SDR CALA2025101309947](https://openairdocs.org/sdr/CALA2025101309947.md): Terminal · damaged · Oct 9, 2025 · N57855 · Boeing 757324 · Electrical Power System Wiring
  > PILOT REPORTS FLAP/SLAT ELEC STATUS MESSAGEFSEU 1 IS UNPOWERED ALSO CAUSING A WARN ELEX STATUS MSG. STALL WARNING RIGHT WILL NOT TEST. UPDATED 20MH, 14GT. FOUND THAT 28VDC IS NOT PRESENT AT THE FSEU & ITS ASSOCIATED 28VDC BREAKER. UPON FURTHER EXAMINATION FOU
- [SDR CALA2025100909852](https://openairdocs.org/sdr/CALA2025100909852.md): Housing · broken · Oct 8, 2025 · N57855 · Boeing 757324 · Emergency Lighting
  > SEAT 9C EMERGENCY PATH LIGHT HOUSING IS BROKEN. REPLACED HOUSING AT SEAT 9C IAW CMM 25-21-50.
- [SDR CALA2025082508095](https://openairdocs.org/sdr/CALA2025082508095.md): Autothrottle Sys · malfunctioned · Aug 22, 2025 · N57855 · Boeing 757324 · Auto Throttle System
  > AUTOTHROTTLE WONT ENGAGE ON TAKEOFF FOUND NO MCDP LAST FLIGHT, FAULTS, CYCLED TMC, FCC'S AND MCP CB'S AS PRECAUTIONARY. PERFORMED MCDP "TMC TEST 02, A/T SERVO TEST 10, A/T DISC SW TEST 12 & FCC TEST 01", AMM REF 22-00-02, ALL TESTS GOOD.
- [SDR CALA2025072406878](https://openairdocs.org/sdr/CALA2025072406878.md): Girt Bar · fod · Jul 20, 2025 · N57855 · Boeing 757324 · Emergency Equipment
  > L1 DOOR HARD TO ARM, NO SLIDE LIGHT ILLUMINATION. REMOVED DEBRIS FROM GIRT BAR FITTINGS, DIRT AND CATERING CART PLASTIC LOCKS, AND LUBED. OPENED AND CLOSED DOOR 1L AND ARMED SLIDE WITH NO ISSUES AND SLIDE LIGHT ILLUMINATED. REPEATED 3 TIMES AND HAD FLIGHT
- [SDR CALA2025070706272](https://openairdocs.org/sdr/CALA2025070706272.md): Static Inverter · warning message · Jul 5, 2025 · N57855 · Boeing 757324 · Electrical Power System
  > STBY INVERTER STATUS MESSAGE. REPLACED STATIC INVERTER MM 24-33-03, OPS CHECK GOOD.
- [SDR CALA2025062005743](https://openairdocs.org/sdr/CALA2025062005743.md): Light · loose · Jun 19, 2025 · N57855 · Boeing 757324 · Emergency Lighting
  > REPORTED BY FLIGHT ATTENDANT: SEAT MOUNTED EMERGENCY EXIT LIGHT AT 21C IS BENT EXIT ASSY LIGHT WAS LOOSE. SECURED EMERGENCY EXIT LIGHT. OPS GOOD AT THIS TIME.
- [SDR CALA2025032503168](https://openairdocs.org/sdr/CALA2025032503168.md): None · none · Mar 23, 2025 · N57855 · Boeing 757324 · Standard Practices/Structures
  > DEACTIVATION OF SLIDE PERFORMED INSTALLED SAFETY SLIDE PIN AT POSITION (L3) DOOR IN THE SLIDE INFLATION BOTTLE REGULATOR ON SLIDE PACK ACCOMPLISHED SAFETY SLIDE PIN AT POSITION (L3) DOOR IN THE SLIDE INFLATION BOTTLE REGULATOR ON SLIDE PACK REMOVED & STOWED AW
- [SDR CALA2025012702071](https://openairdocs.org/sdr/CALA2025012702071.md): Connector · damaged · Jan 24, 2025 · N57855 · Boeing 757324 · Light System Wiring
  > 1 OVER WING ON LOWER SEAT, EXIT RED EMERGENCY LIGHT INOP. FOUND PINS PUSHED BACK ON RED EMERGENCY LIGHT. OPS CHECK GOOD.
- [SDR CALA2025012702070](https://openairdocs.org/sdr/CALA2025012702070.md): Light · detached · Jan 24, 2025 · N57855 · Boeing 757324 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ASSEMBLY FOR SEAT 26C FELL OFF. FOUND SEAT BRACKET THAT HOLDS EMERGENCY LIGHT BROKEN. REPLACED. OPS CHECK GOOD. PARTS USED: 58-2523-3-0048,QTY:1
- [SDR CALA2025010601801](https://openairdocs.org/sdr/CALA2025010601801.md): Light · faulty · Jan 2, 2025 · N57855 · Boeing 757324 · Emergency Equipment
  > DOOR 4R SLIDE LIGHT WAS ILLUMINATED ON GROUND. NOT ILLUMINATE D AT CRUI ZE. DOOR 4R SLIDE LIGHT GND CHK OK, BUT SINCE THE GRIPE IS IN AIR LIKE TO DEFER IT PER MEL 2566V. VERIFIED GIRT BAR AT DOOR 4R ENGAGEMENT CHECKING OK PER MEL CARD 25200 MAINTENANCE PROC
- [SDR CALA2025010301774](https://openairdocs.org/sdr/CALA2025010301774.md): Warning Message · false activation · Jan 1, 2025 · N57855 · Boeing 757324 · Door Warning System
  > L CTR ENT DOOR EICAS MSG DURING CRUISE. PRESSURIZATION NORMAL. SEE LONG HISTORY, DOOR OPERATION SMOOTH & NORMAL, SLIDE LIGHT ON WHEN DOOR ARMED. REQUEST MEL WITH L2 DOOR MODE SELECTOR IN ARMED POSITION CONFIRMED SLIDE LIGHT ON AND ARMED CONDITION INDICATOR "KN
- [SDR CALA2024122601655](https://openairdocs.org/sdr/CALA2024122601655.md): Door · unknown · Dec 23, 2024 · N57855 · Boeing 757324 · Passenger/Crew Doors
  > RECHECKED 2L DOOR FOR CLOSURE AND ARMED. 2L DOOR VERIFIED CLOSED LATCHED AND SLIDE ARMED.
- [SDR CALA2024122401632](https://openairdocs.org/sdr/CALA2024122401632.md): Bulb · no test · Dec 23, 2024 · N57855 · Boeing 757324 · Emergency Lighting
  > FOUND DOOR R3 EMERGENCY SLIDE LIGHT INOP. RELAMPED EMERGENCY SLIDE LIGHT FOR DOOR R3 REF AMM 33-51-06. OPS CHECK GOOD.PARTS USED: 99-3351-3-0014,QTY:1
- [SDR CALA2024121201489](https://openairdocs.org/sdr/CALA2024121201489.md): Seal · damaged · Dec 9, 2024 · N57855 · Boeing 757324 · Fire Detection
  > R ENGINE OVERHEAT REPEAT WRITE UP. T/S REF. B757-3 FIM 26-11 FAULT TREE 802. ENG. 2 OVER HEAT LOOPS 1 & 2 ARE WITHIN LIMITS PER TABLE 101 OF FIM. REF LOGPAGE 3129533 FOR PRIOR T/S OF RH ENG OVHT PERFORMED FIM 26-11 FAULT TREE 803 FROM FAULT ISOLATION BLOCK BL
- [SDR CALA2024120603024](https://openairdocs.org/sdr/CALA2024120603024.md): Skin · cracked · Dec 4, 2024 · N57855 · Boeing 757324 · Passenger/Crew Doors
  > FAULT: EA5330-04213 REVISION D OPERATION 004 OVERVIEW, 01 E/A FA STENER HOLE COMMON TO THE MIDIFICATION AREA HAVE CRACK. L1 DOOR CUTOUT BEARSTRAP AND SKIN REPAIR WORKED PER UAL EC/RA#:5 310-08471 AND VT MAE EA 757-5310-13-A3723 REV-
- [SDR CALA2024120202998](https://openairdocs.org/sdr/CALA2024120202998.md): Frame · corroded · Nov 30, 2024 · N57855 · Boeing 757324 · Fuselage Main, Frame
  > B757-53-3-0526 AFT CARGO COMPT. STA 1440 S-29R AND S-30 FRAME HA S EXFOLIATED CORROSION ON THE LOWER WEB.
- [SDR CALA2024120202992](https://openairdocs.org/sdr/CALA2024120202992.md): Stringer · corroded · Nov 29, 2024 · N57855 · Boeing 757324 · Fuselage Main, Longeron/Stringer
  > B757-53-3-0526 STR-Z154 AFT CARGO COMPARTMENT BTWN STA 1440/1460 BTWN STR 29R FACTORY SPLICE IS EXFOLIATED. REMOVED AND REPLACED SPLICE AT AFT CARGO COMPT. BETWEEN STA 1440 TO STA 1460 AND STR 29RH IAW B757-300 SRM 51-40-02-0G-0.
- [SDR CALA2024120202991](https://openairdocs.org/sdr/CALA2024120202991.md): Channel · corroded · Nov 29, 2024 · N57855 · Boeing 757324 · Fuselage Miscellaneous Structure
  > B757-53-3-0526 STR-Z154 AFT CARGO COMPT STA 1460 BTWN STR 29R/30 HAS SHEAR TIE WITH CORROSION. REMOVED AND REPLACED SHEAR TIE AT AFT CARGO COMPT. STA 1460 BETW AND INSTALLED PARTS FOR ACCESS BY EVALUATION FRAME. EEN STR 29RH TO 30 IAW B757-300 SRM 51-40-02-0G-
- [SDR CALA2024120202990](https://openairdocs.org/sdr/CALA2024120202990.md): Stringer · corroded · Nov 29, 2024 · N57855 · Boeing 757324 · Fuselage Main, Longeron/Stringer
  > B757-53-3-0526 STR-Z154 AFT CARGO COMPARTMENT STA 1420/1440 STR 29R HAS CORROSION IN 4EA POINTS. REMOVED AND REPLACED STRINGER 29R STA 1420 TO STA 1440 P/N 146N3 SRM 51-40-02-0G DRAWING 146N3300 SRM 51-20-01. INSTALLED NEW STRINGER CLIP P/ N 146N2005-133 TRAV
- [SDR CALA2024120202989](https://openairdocs.org/sdr/CALA2024120202989.md): Intercostal · corroded · Nov 29, 2024 · N57855 · Boeing 757324 · Fuselage Miscellaneous Structure
  > B757-53-3-0526 STR-Z154 AFT CARGO COMPARTMENT STA1420/1440 BTWN STR 28R/29R HAS INTERCOSTAL WITH CORROSION. REMOVED AND REPLACED INTERCOSTAL AFT CARGO COMPT. STA 1420 TO ST A 1440 AND BETWEEN STR 28RH TO STR 29RH IAW B757-300 SRM 51-40-0 2-0G-0.
- [SDR CALA2024112902985](https://openairdocs.org/sdr/CALA2024112902985.md): Panel · corroded · Nov 27, 2024 · N57855 · Boeing 757324 · Fuselage Miscellaneous Structure
  > SUPPORT TASK - AFT CARGO COMPT. SIDE PANEL FROM STA 1420 TO STA 1540 LH SIDE HAS EXFOLIATED CORROSION. (REPAIR OR REPLACE).
- [SDR CALA2024112502931](https://openairdocs.org/sdr/CALA2024112502931.md): Structure · corroded · Nov 22, 2024 · N57855 · Boeing 757324 · Fuselage Miscellaneous Structure
  > B757-53-3-0499: EXTERIOR LOWER FUSELAGE BS 900 BETWEEN LBL45 TO RBL45 SPOTS WITH CORROSION. DOT 68-95 REF NR 113682. PERFORMED T-CHORD REPAIR AT LOWER FUSELAGE BS 900 BETWEEN RBL45 TO LBL45 IAW B757-300 SRM 51-70-12-0G-0 FIG 1.
- [SDR CALA2024112202920](https://openairdocs.org/sdr/CALA2024112202920.md): Floorbeam · damaged · Nov 21, 2024 · N57855 · Boeing 757324 · Fuselage Main, Floor Beam
  > PERFORMED T-CHORD REPAIR AT LOWER FUSELAGE BS 900 BETWEEN RBL45 TO LBL 45 IAW B757-300 SRM 51-70-12-0G-0 FIG 1 PERFORMED T-CHORD REPAIR AT LOWER FUSELAGE BS 900 BETWEEN RBL45 TO LBL 45 IAW B757-300 SRM 51-70-12-0G-0 FIG 1
- [SDR CALA2024050601330](https://openairdocs.org/sdr/CALA2024050601330.md): Fairing · missing · May 4, 2024 · N57855 · Boeing 757324 · Turbine Engine Compressor Section
  > FOUND #1 ENG. OUTBOARD LOWER COMPRESSOR FAIRING MISSING WHICH CAUSED DAMAGE TO MULTIPLE ITEM IN BOTH C DUCTS. PANEL DIMENSIONS ARE APPROX. 27X27.5 INCHES. REF TASK 72-03-01-424-006-R00 AND TORQUED BOLTS REF TASK 70-51-00-912-001-R00 REPLACED COMPRESSOR FAIRING
- [SDR CALA2024022600547](https://openairdocs.org/sdr/CALA2024022600547.md): Terminal Block · shorted · Feb 22, 2024 · N57855 · Boeing 757324 · Communications System Wiring
  > RADIO VHF1/2 INOP UNCONTROLLABLE CREW REPORTED: L VHF/HF COMMUNICATION CONTROL PANEL (TUNING PANEL) KEPT CHANGING TO 120.500 AUTOMATICLLY AND R TUNING PANEL TO 118.200. CENTER PANEL KEPT THE SELECTED FREQUENCY. ENGINEERING UPDATE: SELECTION BETWEEN FREQUENCY S
- [SDR CALA2024010500034](https://openairdocs.org/sdr/CALA2024010500034.md): Thrust Reverser · damaged · Jan 2, 2024 · N57855 · Boeing 757324 · Engine Thrust Reverser
  > FOUND CRACK ON NO. 1 ENG COWLING O/B T/R REF LOG PAGE 6708820. UPON OPENING TRANSLATING SLEEVE, FOUND O/B CASCADE VANE MISSING FROM T/R. SEE LOG PAGE 6708820 FOR PHOTOS. HIGHLIGHTED SDR MARKER.UPPER ACOUSTIC PANEL SIZE ESTIMATE, BASED OFF MEASURING FROM THE MO
- [SDR CALA2024010400018](https://openairdocs.org/sdr/CALA2024010400018.md): Thrust Reverser · cracked · Jan 2, 2024 · N57855 · Boeing 757324 · Engine Thrust Reverser
  > FOUND CRACK ON NO. 1 ENG COWLING O/B T/R REF LOG PAGE 6708820. UPON OPENI NG TRANSLATING SLEEVE, FOUND O/B CASCADE VANE MISSING FROM T/R. SEE LOG PAGE 6708820 FOR PHOTOS. MISSING UPPER ACOUSTIC PANEL SIZE ESTIMATE, BASED OFF MEASURING FROM THE MOUNTING POINTS
- [SDR CALA2023072602330](https://openairdocs.org/sdr/CALA2023072602330.md): O2 Generator · activated · Jul 16, 2023 · N57855 · Boeing 757324 · Passenger Oxygen System
  > WHEN INSPECTING THE P/N AND S/N OF THE OXYGEN GENERATORS, THE OXYGEN GENERATOR OF ROW 43 DEF WAS FOUND ACTIVATED. (ST NR 70848). O2 GENERATOR AT ROW 43 DEF REPLACED PER AMM 35-21-04-404-013 ON ST ENGINEERING N/R 70848 PARTS USED: 29-3522-3-0010,QTY:1
- [SDR CALA2023022700568](https://openairdocs.org/sdr/CALA2023022700568.md): Door Seal · none · Feb 27, 2023 · N57855 · Boeing 757* · Emergency Exits
  > LOUD SQUEL COMING FROM R OVRWING EXIT REMOVED DOOR AND REPOSITION DOOR SEAL PER AMM 52-09-03-404-014. PRESSURIZE ACFT NO LEAKS ADD EMP:U235110,U234513,U393561
- [SDR CALA2022031400637](https://openairdocs.org/sdr/CALA2022031400637.md): None · cracked · Mar 11, 2022 · N57855 · Boeing 757* · Fuselage Main, Plate/Skin
  > CABIN FRAME STA. 760LH CRACKED AT I/B FASTENER AT PSU RAIL. REPAIRED DAMAGE REF SRM 53-00-07-2R-8. DO THE INSPECTIONS AS GIV EN IN TABLE 203/REPAIR8 ZONE 2 OF SRM 53-00-07-2R-8 ITEM ENTERED TO TRACK REPETITIVE INSPECTIONS. CLEARED RII BUY BACK IN ERROR. INSPEC
- [SDR CALA2022031000631](https://openairdocs.org/sdr/CALA2022031000631.md): None · cracked · Mar 10, 2022 · N57855 · Boeing 757* · Fuselage Main, Plate/Skin
  > CABIN FRAME STA 780+20 LH SIDE CRACKED AT I/B FASTENER AT PSU RAIL (FRAME MARKED) CYCLES FROM REPAIR INSTALLATION, OR 50,000 AIRFRAME FLIGHT INTERVAL 12;000 FLIGHT CYCLES. CYCLES, WHICHEVER COMES FIRST. METHOD DETAIL VISUAL INSPECTION. REPAIRED FRAME PER SRM 5
- [SDR CALA2022030700577](https://openairdocs.org/sdr/CALA2022030700577.md): Frame · dented · Mar 4, 2022 · N57855 · Boeing 757* · Fuselage Main, Plate/Skin
  > PLANNING TO CONTACT ENGINEERING AFTER 03-JAN-2023 BUT BEFORE 03-FEB-2023 FOR THE PERMANENT REPAIR OF EC/RA 5311-02776.? REFERENCE LOG PAGE #8115543. REFERENCE LOG PAGE #8115543. PLANNING TO CONTACT ENGINEERING AFTER 03-JAN-2023 BUT BEFORE 03-FEB-2023 FOR THE P
- [SDR CALA2022030700576](https://openairdocs.org/sdr/CALA2022030700576.md): Skin · corroded · Mar 4, 2022 · N57855 · Boeing 757* · Fuselage Structure (General)
  > FUSELAGE SKIN AT STA. 1844 BETWEEN STR. 28LAND 29L CORRODED( VIEWED INSIDE TAIL COMP.) (INFORMATION ONLY FOR SFR INPUT.) PERFORMED REPAIR ON DAMAGED FUSELAGE SKIN REF. ECRA 5380-01325... SEE FLEETCYCLE LOG PAGE 9800429 FOR WORK ACCOMPLISHED.
- [SDR CALA2019122102257](https://openairdocs.org/sdr/CALA2019122102257.md): Wire · detached · Dec 20, 2019 · N57855 · Boeing 757324 · Light System Wiring
  > ELEC BURNING SMELL AND SUBSEQUENT SHOWER OF SPARKS FROM CAPTAINS LEFT GLARESHIELD FOUND LOOSE WIRE ON BACK OF RHEOSTAT(507). NEED RHEOSTAT PART #86A2EZ8BA0689 FAULT CONFIRMED, LOOSE WIRE. REMOVED AND REPLACED RHEOSTAT SWITCH. SECURED ALL WIRES AND OPS CHECK G
- [SDR CALA2019011200064](https://openairdocs.org/sdr/CALA2019011200064.md): Floor Support · corroded · Jan 10, 2019 · N57855 · Boeing 757324 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT CORRODED BS 345 LBL 20. 8-22 REF. N/R:99828815 REMOVED AND REPLACED CABIN FLOOR SUPPORT CORRODED AT F.S 345 LBL 20 IN REF. DRWG#141N5170-56 REF. N/R:99828815 INSPECTION COMPLIED WITH.
- [SDR CALA2017121904526](https://openairdocs.org/sdr/CALA2017121904526.md): Lens · loose · Dec 19, 2017 · N57855 · Boeing 757324 · Emergency Lighting
  > CREW REPORTED, EMERGENCY EXIT LIGHT LENS AT L2 DOOR FELL OFF. REPLACED LENS, EMERGENCY EXIT LIGHT AT L2 DOOR OPS CHECK NORMAL.
- [SDR CALA2016010800034](https://openairdocs.org/sdr/CALA2016010800034.md): Skin · dented · Jan 7, 2016 · N57855 · Boeing 757324 · Fuselage Main, Plate/Skin
  > RIGHT LOWER FUSELAGE SKIN SHOWS DENT DAMAGE, JUST FWD OF BS 740 RT, BETWEEN STRINGERS 24 & 25 RT. REQUIRED INITIATE DIP FOR REINSPECTION ON CYCLE 37500. DAMAGE AREA 1 1/16 X 1 1/2 WITH A DOUBLER 8 1/4 X 8 3/4. ACCOMPLISHED REPAIR IAW SRM 53-00-01 REPAIR 3 W
- [SDR CALA2015123001046](https://openairdocs.org/sdr/CALA2015123001046.md): Floorbeam · corroded · Dec 28, 2015 · N57855 · Boeing 757324 · Fuselage Main, Floor Beam
  > AFT PASS CABIN, STATION 1640, LBL 9" - RBL 4", FLOORBEAM SCREW HOLES, 3 EA HAVE CORROSION. CORROSION OUT OF LIMITS, ACCOMPLISHED REPAIR IAW SRM 51-10-02, 53-00-51, 51-20-01 & 53-00-51.

Next page: https://openairdocs.org/aircraft/N57855/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 = 'N57855' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N57855/reports

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