# Service difficulty reports: N57852

A list on [N57852](https://openairdocs.org/aircraft/N57852.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 · 77 reports

- [SDR CALA2026092919977](https://openairdocs.org/sdr/CALA2026092919977.md): Light · loose · Sep 26, 2026 · N57852 · Boeing 757324 · Emergency Lighting
  > ROW 23D EMERGENCY EXIT LIGHT LOOSE IAW 33-51-00, SECURED ROW 23 EMERGENCY EXIT LIGHT.
- [SDR CALA2026092419780](https://openairdocs.org/sdr/CALA2026092419780.md): Lamp · inoperative · Sep 22, 2026 · N57852 · Boeing 757324 · Emergency Lighting
  > EMERGENCY LIGHTS OPS TEST WITH TEST SWITCH, DOOR 2L EMERGENCY EXIT LIGHT INOPERATIVE. R & R DOOR 2L EXTERIOR SLIDE LIGHT LAMP IAW AMM 33-51-06-962-001-002. LIGHT OPS CHKD GOOD. OK TO CONTINUE
- [SDR CALA2026042115555](https://openairdocs.org/sdr/CALA2026042115555.md): Housing · damaged · Apr 20, 2026 · N57852 · Boeing 757324 · Emergency Lighting
  > EMERGENCY PATHWAY LIGHT HOUSING AT 24C IS DAMAGED. REPLACED EMERGECY LIGHT HOUSE AT 24C. OPS CHKS NORMAL. REF IFM 25-21-50 AND AMM 33-51-11-403-070
- [SDR CALA2026012713333](https://openairdocs.org/sdr/CALA2026012713333.md): Frame · cracked · Jan 23, 2026 · N57852 · Boeing 757324 · Fuselage Main, Frame
  > LEFT FRAME AT BS 1580 WAS CRACKED AT PSU SUPPORT, MOST INBD RIVET.
- [SDR CALA2026012713332](https://openairdocs.org/sdr/CALA2026012713332.md): Skin · dented · Jan 23, 2026 · N57852 · Boeing 757324 · Service Doors
  > R4 DOOR SKIN DENTED BELOW AND AFT OF HANDLE. FOUND TO BE OUT OF LIMITS. THE DENT WAS REPAIRED IAW SRM 52-10-01-2R-7.
- [SDR CALA2026012313228](https://openairdocs.org/sdr/CALA2026012313228.md): Floorbeam · corroded · Jan 22, 2026 · N57852 · Boeing 757324 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM BS 1681 APPROX LBL47 TO RBL47 WAS CORRODED ON FWD FLANGE AT SEVERAL NUTPLATE HOLES. THE FLOORBEAM WAS REPAIRED IAW SRM 53-60-51-2R-3 AND ECRA 5360-02091.
- [SDR CALA2026012213172](https://openairdocs.org/sdr/CALA2026012213172.md): Deck Plate · corroded · Jan 21, 2026 · N57852 · Boeing 757324 · Fuselage Main, Structure
  > NUMEROUS AREAS OF HEAVY CORROSION ON AFT DECK PLATE FROM BS 1681 - 1720, LBL 60 - RBL 60. REMOVED, FABRICATED, & INSTALLED DECK PLATE IAW DWG 146N5318, & SRM 51-40-02.
- [SDR CALA2026011613000](https://openairdocs.org/sdr/CALA2026011613000.md): Frame · punctured · Jan 15, 2026 · N57852 · Boeing 757324 · Fuselage Main, Frame
  > PUNCTURE IN FRAME BS 460 BETWEEN STRINGER 11L AND 12L.
- [SDR CALA2025121612147](https://openairdocs.org/sdr/CALA2025121612147.md): Door Sill · mechanic error · Dec 14, 2025 · N57852 · Boeing 757324 · Fuselage Main, Structure
  > L2 DOOR SILL INNER CHORD IS MISS-DRILLED AT DRAIN PAN ATTACH HOLES REMOVE AND REPLACE INNER CHORD PART # 143N8328-53 PER DRAWING 143N8322 AND SRM 51-40-02. ADD EMP:U407139 UPDATED SFR INFORMATION. L2 DOOR SILL INNER CHORD IS MISDRILLED INNER CHORD 143N8328-53
- [SDR CALA2025092209085](https://openairdocs.org/sdr/CALA2025092209085.md): Cartridge · crushed · Sep 14, 2025 · N57852 · Boeing 757324 · Fuselage Main, Structure
  > TAIL STRIKE REPORTED ON ARRIVAL.DPI POPPED. PERFORMED PART OF TAIL STRIKE INSPECTION PER AMM 05-51-32-212-011. FOUND POPPET POPPED. RESET POPPET. INSPECTED EXTERNAL FUSELAGE FROM AREA NEAR AFT BULKHEAD OF AFT CARGO PIT TO TAIL, INSPECTED APU BAY, INSPECTED LOW
- [SDR CALA2025082208047](https://openairdocs.org/sdr/CALA2025082208047.md): Lamp · inoperative · Aug 21, 2025 · N57852 · Boeing 757324 · Emergency Lighting
  > EMERGENCY LIGHTS OPS TEST WITH THE TEST SWITCH PROCEDURE, MULTIPLE EMERGENCY EXIT IDENTIFIER SIGNS REQUIRE LAMPS. REPLACED THE LAMPS 23 EA IN VARIOUS LOCATIONS IAW AMM 33-51-01-962-001-002 & 33-51-10-962-040 CK OK.
- [SDR CALA2025072907043](https://openairdocs.org/sdr/CALA2025072907043.md): Lamp · inoperative · Jul 28, 2025 · N57852 · Boeing 757324 · Emergency Lighting
  > LEFT WING AFT EMERGENCY LIGHT INOP. RELAMPED OVERWING EXTERIOR EMERGENCY EXIT LIGHT AND OPS CHECKED IAW AMM 33-51-00 OPS CHECK GOOD.
- [SDR CALA2025050504439](https://openairdocs.org/sdr/CALA2025050504439.md): Lamp · inoperative · May 2, 2025 · N57852 · Boeing 757324 · Emergency Lighting
  > EMERGENCY LIGHTS - GENERAL VISUAL INSPECTION (ADDED BY EC0300-01601) PROCEDURE - EXIT MARKER R/H OVERWING EXIT AFT DOOR, NEEDS RELAMPED EXIT IDENTIFIER SIGN AT R/H OVERWING EXIT AFT DOOR, REF AMM 33-51-10. OP CHECK GOOD.PARTS USED: 3071BPE, QTY:3
- [SDR CALA2025031402818](https://openairdocs.org/sdr/CALA2025031402818.md): Slide · inoperative · Mar 14, 2025 · N57852 · Boeing 757324 · Escape Slide
  > CATERING REPORTS SOMETHING WRONG WITH AFT SERVICE DOOR. REOPENING NEW L/ P DUE TO CLOSING BY MISSTAKE L/P 4139067. REMOVED THE L-4 ESCAPE SLIDE REF AMM TASK 25-66-01-004-154 AND PER STEP 6 CYLINDER SAFETY PIN INSTALLED IN OLD SLIDE INFLATION CYLINDER VALVE ON
- [SDR CALA2025031402817](https://openairdocs.org/sdr/CALA2025031402817.md): Cover · damaged · Mar 14, 2025 · N57852 · Boeing 757324 · Escape Slide
  > DURING INSTALL OF DOOR 4L FOUND SLIDE COVER DAMAGED. REPAIRED DAMAGED AREA REF CMM 25-00-66 REPAIR 1-1. READY FOR SERVICE.
- [SDR CALA2024102400922](https://openairdocs.org/sdr/CALA2024102400922.md): Governor · faulty · Oct 24, 2024 · N57852 · Boeing 757324 · Turbine Governor
  > R ENG FAILURE ON DESCENT AT 16000 FT DEBRIEF CREW, ENGINE 2 FLAMED OUT, SELF SHUTDOWN. APPROXIMATELY 15MN WINDMILL AND NOTICED ABOUT 2PSI OIL PRESSURE. REF TO LOG 9641578 AND 9633254 FOR CORRECTIVE ACTIONS (FFG & HP FUEL PUMP R&R). UPDATING SDR PER GMM04-20-1
- [SDR CALA2024072402095](https://openairdocs.org/sdr/CALA2024072402095.md): Skin · dented · Jul 23, 2024 · N57852 · Boeing 757324 · Fuselage Main, Plate/Skin
  > B757-06-3-0221 2 DENTS LWR AFT FUSELAGE STA 1480 AT KEEL BEAM DO OR. DOT 140-005. EVALUATED DENTS AT LWR AFT FUSELAGE STA 1480 DENT #1 L=1.870" W= 53-00-01-2R-28..900" D=0.017" A/Y=52.9", DENT #2 L=1.480" W=.860" D=0.012" A/Y= 66.1, DENTS FOUND TO BE OUT OF L
- [SDR CALA2023102703203](https://openairdocs.org/sdr/CALA2023102703203.md): Unknown · unknown · Oct 25, 2023 · N57852 · Boeing 757324 · Electrical Power System
  > L GEN CONT OFF LIGHT SWITCH CYCLED RESET L GE N CONT SWITCH PER QRH CREW STATED NO EICAS MSGS PRESENT AND RESET WAS SUCCESSFUL. PERFORMED BPCU BIT PROCEEDURE IAW B757 FIM 24-20 TREE 801. NO FAULT MSGS RECORDED. A/C OK FOR SERVICE
- [SDR CALA2023082102607](https://openairdocs.org/sdr/CALA2023082102607.md): Yaw Damper · inoperative · Aug 20, 2023 · N57852 · Boeing 757324 · Auto Flight System
  > MACH/SPD TRIM MSG FLAGGED FOR SDR REF. FIM 27-09 TASK 814. NO EXISTING FAULTS IN EITHER LEFT OR RIGHT YAW DAMPER STAB TRIM MODULE. REPLACED R/H YAW DAMPER MODULE PER AMM 22-21-04 OPERATIONAL TEST GOOD, NO FAULTS NOTED AT THIS TIME. PARTS USED: 64-2221-9-0003,
- [SDR CALA2022053001398](https://openairdocs.org/sdr/CALA2022053001398.md): None · none · May 27, 2022 · N57852 · Boeing 757 · Electrical Power System
  > THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL REPORT SUBMITTED ON 5/30/22. HYD GEN ON EICAS S THE HYDRAULIC DRIVEN GENERATOR IS IN OPERATION HYD GEN IN CONTINUOUS OPERATION REQUEST MEL COMPLIED WITH. HMG INOP REF MEL 2425J C/W MEL. DISPATCH DESK: 38 NAME:
- [SDR CALA2020100901168](https://openairdocs.org/sdr/CALA2020100901168.md): Fire Detector · out of limits · Oct 9, 2020 · N57852 · Boeing 757324 · Fire Detection
  > ENGINE FIRE DETECTION FIRE PROTECTION SYSTEM FAIL LGT ON. EICAS MESSAGE FIRE/OVHT SYS DISPLAYED. EICAS STATUS MESSAGE (01=L, 02= R) ENG OH LP 1 AND LP 2 DISPLAYED 01 FIRE/OVHT SYS EICAS WARNING DISPLAYED L ENG OH LP 1 AND 2 STATUS DISPLAYED. ADDING CREW PHOTO
- [SDR CALA2020072701074](https://openairdocs.org/sdr/CALA2020072701074.md): Latch · no test · Jul 22, 2020 · N57852 · Boeing 757324 · Escape Slide
  > R4 DOOR SLIDE LATCH BLOCK WILL NOT PASS PULL TEST.
- [SDR CALA2020072701073](https://openairdocs.org/sdr/CALA2020072701073.md): Latch · no test · Jul 22, 2020 · N57852 · Boeing 757324 · Escape Slide
  > ESCAPE SLIDE LATCH ASSEMBLY ON R1 DOOR FAILS PULL TEST LP 700132 5 SPT
- [SDR CALA2020072001067](https://openairdocs.org/sdr/CALA2020072001067.md): Lamp · inoperative · Jul 19, 2020 · N57852 · Boeing 757324 · Emergency Lighting
  > EMERGENCY LIGHT ON LT SIDE OF FUSELAGE LOWER AFT OF WING INOPERATIVE. REPLACED THE LAMP AND OPS CHECKED GOOD IAW AMM 33-51-06.
- [SDR CALA2020030200568](https://openairdocs.org/sdr/CALA2020030200568.md): Skin Panel · chafed · Mar 1, 2020 · N57852 · Boeing 757324 · Fuselage Main, Plate/Skin
  > B757-53-3-0586 SUPPORT BRACKET CHAFING INTO FUSELAGE SKIN PANEL AT STA 1800 AND STR 17R. REF ST.ENGINEERING NON ROUTINE 0089005. ACCOMPLISHED A CAT "A"PERMANENT SPLICE REPAIR ON FUSELAGE SKIN P ANEL AT STA 1800 STR 17R IAW B757-3 SRM 53-80-70 REPAIR 4 FIG 20 1
- [SDR CALA2020030600567](https://openairdocs.org/sdr/CALA2020030600567.md): Skin · damaged · Mar 1, 2020 · N57852 · Boeing 757324 · Rudder, Plate/Skin
  > THE VERTICAL STABILIZER LOWER RUDDER TRAILING EDGE IS DAMAGED. R EF. ST. ENGINEERING N/R 0087783 ACCOMPLISHED A PERMANENT REPAIR ON VERTICAL STABILIZER LWR RUDDE R TRAILING EDGE IAW B757-3 SRM 51-40-02 PARA 11, 55-40-01 TABLE 1, 51-70-04 PARA 5.D. WORK ACCOMPL
- [SDR CALA2020022400460](https://openairdocs.org/sdr/CALA2020022400460.md): Frame · gouged · Feb 16, 2020 · N57852 · Boeing 757324 · Fuselage Main, Frame
  > (MULT-20-3-0019) MAIN CABIN RH STA 1280 FRAME GOUGED 4EA PLACES STR 10-14. 103-116. REF ST-SAA NR0087486 ACCOMPLISHED PART 1 INTERIM REPAIR ON FUSELAGE FRAME AT STA 1280 BETWEEN STR 9R TO STR 14R IAW EC/RA 5360-01548.AREA FREE OF FOD WORK ACCOMPLISHED BY V9197
- [SDR CALA2020021700443](https://openairdocs.org/sdr/CALA2020021700443.md): Stringer · cracked · Feb 13, 2020 · N57852 · Boeing 757324 · Fuselage Main, Longeron/Stringer
  > (B757-53-3-0546)MAIN CABIN STA 780+24 STRINGER 16R CRACKED. 103- 119 ST. ENGINEERING N/R 0087493 REMOVED AND REPLACED STR 16R AT STA 780+24 IAW B757-3 SRM 51-40- 02 FIG 4 AND BOEING DWG 143N3500 REV E.
- [SDR CALA2020021700442](https://openairdocs.org/sdr/CALA2020021700442.md): Stringer · cracked · Feb 13, 2020 · N57852 · Boeing 757324 · Fuselage Main, Longeron/Stringer
  > (B757-53-3-0546)MAIN CABIN STA 780+24 STRINGER 16L CRACKED.103-1 17 REF. ST. ENGINERRING N/R 0087491 REMOVED AND REPLACED STR 16L AT STA 780+24 IAW B757-3 SRM 51-40- 02 AND BOEING DWG 143N3500 REV E.
- [SDR CALA2020021640411](https://openairdocs.org/sdr/CALA2020021640411.md): Bracket · cracked · Feb 8, 2020 · N57852 · Boeing 757324 · Cargo/Baggage Doors
  > B757-52-3-0103 FWD CARGO DOOR,FWD AND AFT (UPPER)CORNER BRACKETS ARE CRACKED. (96-19) REF.ST. ENGINEERING N/R 0087139 REMOVED AND REPLACED FWD CARGO DOOR FWD AND AFT UPPER CORNER BRA CKETS; P/N: 69-53919U5,BATCH NO:0003603133,PO NO:SAG2090051 AND P/N: 69-53919
- [SDR CALA2020021200376](https://openairdocs.org/sdr/CALA2020021200376.md): Skin · gouged · Feb 7, 2020 · N57852 · Boeing 757324 · Passenger/Crew Doors
  > SUPPORT TASK EA 5210-01361 REV G R1 DOOR SKIN DOUBLER THROUGH LI GHTNING HOLE GOUGE AS MARKED 034-004.REF. ST. ENGINEERING N/R 0087711 CHECKED LIMITS TO GOUGE AT R1 DOOR SKIN DOUBLER,THROUGH LIGHTING HOLE; L=.50" W=.25" D=.023". OUT OF LIMITS IAW B757-300 SRM
- [SDR CALA2020020800346](https://openairdocs.org/sdr/CALA2020020800346.md): Skin · chafed · Feb 5, 2020 · N57852 · Boeing 757324 · Fuselage Main, Plate/Skin
  > B757-53-3-0586 SUPPORT BRACKET CHAFING INTO AFT FUSELAGE SKIN PA NEL STA 1800 STR 17L REF. ST. ENGINEERING N/R 0086941 CUT DAMAGE SECTION OF FUSELAGE SKIN PANEL (HORZ. STAB FWD CUTOUT FAIRING SKIN) AT STA 1800 STR 17L AND ACCOMPLISHED A CATEGORY "A" PERMANENT
- [SDR CALA2020020870335](https://openairdocs.org/sdr/CALA2020020870335.md): Seal Depressor · dented · Feb 3, 2020 · N57852 · Boeing 757324 · Cargo/Baggage Doors
  > B757-52-3-0103 FWD CARGO DOOR,AFT SEAL DEPRESSOR IS DENTED. (96- 18) REF. ST. ENGINEERING N/R 0087138 FOUND 1EA DENT OUT OF LIMITS ON FWD CARGO DOOR AFT SEAL DEPRESSO R,DENT 1,L=2.5,W=.80,D=.040 IAW B757-300 SRM 52-30-02-A1 FIG. 10 1.REMOVED AND INSTALLED NEW
- [SDR CALA2020020870334](https://openairdocs.org/sdr/CALA2020020870334.md): Seal Depressor · dented · Feb 3, 2020 · N57852 · Boeing 757324 · Cargo/Baggage Doors
  > B757-52-3-0103 AFT CARGO DOOR,FWD SEAL DEPRESSOR HAS A 2" WIDE D ENT. (96-12) REF. ST ENGINEERING N/R 0087124 FOUND 1EA DENT OUT OF LIMITS ON AFT CARGO DOOR FWD SEAL DEPRESSO R,DENT 1 L=2.0,W=.50,D=.105 IAW B757-300 SRM 52-30-02 A1 FIG. 10 1.REMOVED AND INSTAL
- [SDR CALA2020020870333](https://openairdocs.org/sdr/CALA2020020870333.md): Angle · corroded · Feb 3, 2020 · N57852 · Boeing 757324 · Fuselage Main, Structure
  > B757-53-3-0593 FUSELAGE CUTOUT SUPPORT STRUCTURE FOR APU AIR INL ET DOOR HOUSING ASSY HAS CORROSION. RL024 REF. ST.ENGINEERING N/ R 0086925 FOUND CORROSION OUT OF LIMITS ON APU AIR INLET SUPT STRUCTURE BE TWEEN STA 1787-1825 AND S-3R TO 6R,UPPER ANGLE L=28.5 W
- [SDR CALA2020020870331](https://openairdocs.org/sdr/CALA2020020870331.md): Rib · dented · Feb 3, 2020 · N57852 · Boeing 757324 · Cargo/Baggage Doors
  > B757-52-3-0103 AFT CARGO DOOR LWR RIBS,(1ST AND 2ND) INNER FLANG E IS DENTED. (96-59) REF. ST. ENGINEERING N/R 0087422 FOUND 2EA DENTS OUT OF LIMITS ON AFT CARGO DOOR LWR RIB''S INNER FLANGE,DENT 1 L=4.0,W=.80,D=.200 DENT 2 L=5.0,W=.80,D=.350 IAW B 757-300 SRM
- [SDR CALA2020020870330](https://openairdocs.org/sdr/CALA2020020870330.md): Crease Beam · corroded · Feb 3, 2020 · N57852 · Boeing 757324 · Fuselage Main, Structure
  > B757-53-3-0557 RH CREASE BEAM INNER CHORD HAS CORROSION ON UPPER SURFACE,LEADING UNDER DRAIN PAN,FROM STA 730-STA 740.(96-86) RE F. ST. ENGINEERING N/R 0087599 FOUND CORROSION REMOVAL OUT OF LIMITS ON CABIN CREASE BEAM INNER CHORD AT STA 730-740 RBL 60,L=6.0 W
- [SDR CALA2020020700329](https://openairdocs.org/sdr/CALA2020020700329.md): Crease Beam · corroded · Feb 3, 2020 · N57852 · Boeing 757324 · Fuselage Main, Structure
  > B757-53-3-0557 LH CREASE BEAM INNER CHORD HAS CORROSION ON UPPER SURFACE LEADING UNDER DRAIN PAN AT L-2 SILL,STA 735. (96-81) RE F ST. ENGINEERING N/R 0087573 FOUND CORROSION REMOVAL OUT OF LIMITS ON CABIN CREASE BEAM INNER CHORD AT STA 735-733 CBL 60,L=2.0,W=
- [SDR CALA2020020700327](https://openairdocs.org/sdr/CALA2020020700327.md): Stringer · cracked · Jan 28, 2020 · N57852 · Boeing 757324 · Fuselage Main, Longeron/Stringer
  > (B757-53-3-0546)MAIN CABIN STA 780+36 STRINGER 16R CRACKED. 103- 120 ST. ENGINEERING N/R 0087494 TRIMMED-OUT DAMAGE ON STR 16R AT MAIN CABIN STA 780+36 TO A 1.01 1" X 0.781" X 0.25" R CUTOUT AND ACCOPLISHED A CAT "A" PERMANENT REINFORCING REPAIR IAW B757-300 S
- [SDR CALA2020020200296](https://openairdocs.org/sdr/CALA2020020200296.md): Stringer · cracked · Jan 28, 2020 · N57852 · Boeing 757324 · Fuselage Main, Longeron/Stringer
  > (B757-53-3-0546)MAIN CABIN STA 780+36 STRINGER 16L CRACKED REF. ST. ENGINEERING N/R 0087492 TRIMMED-OUT CRACK ON STR 16L AT STA 780+36 TO A 1.011" X 0.781" X 0.25" R AND ACCOMPLISHED A PERMANENT CAT "A" REINFORCING REPAI R IAW B757-300 SRM 53-30-03 REPAIR 1 FI
- [SDR CALA2019071501198](https://openairdocs.org/sdr/CALA2019071501198.md): Socket · burned · Jul 14, 2019 · N57852 · Boeing 757324 · Passenger Compartment Lighting
  > ELECTRICAL BURNING ODOR AROUND ROW 30 FOUND CEILING LIGHT ASSY ABOVE ROW 32-33 A,B,C STOW BIN WITH BURNT SOCKET. FOUND LEFT CEILING FLOURESCENT LIGHT AFT SOCKET ABOVE ROW 33 TO BE DEFECTIVE. REMOVED LIGHT BULB, DISCONNECTED FLOURESCENT LIGHT BALLAST, AND CAPP
- [SDR CALA2019021700251](https://openairdocs.org/sdr/CALA2019021700251.md): Skin · damaged · Feb 13, 2019 · N57852 · Boeing 757324 · Fuselage Main, Plate/Skin
  > AT EXTERNAL FUSELAGE BETWEEN STA 600 AND 620 ABOVE STR 17 LEFT EXISTING REPAIR HAS A DENT AT LOWER AFT CORNER. REF. AAR N/R:9753852 REMOVED EXISTING REPAIR DOUBLER CUT-OUT DAMAGED AREA,FABRICATED NEW DOUBLER,REPAIR AT STA 600 AND 620 STR#17 LEFT,REF.RES-WI 201
- [SDR CALA2018020200438](https://openairdocs.org/sdr/CALA2018020200438.md): Cover · damaged · Feb 2, 2018 · N57852 · Boeing 757324 · Escape Slide
  > R1 DOOR SLIDE COVER DAMAGED. REPAIRED THE SLIDE COVER IAW AMM 25-00-00-300,
- [SDR CALA2018011200157](https://openairdocs.org/sdr/CALA2018011200157.md): Light · inoperative · Jan 12, 2018 · N57852 · Boeing 757324 · Passenger Compartment Equipment
  > POWER LIGHT AT SEAT 10D INOPERATIVE. INSTALLED A NEW LIGHT ASSEMBLY.
- [SDR CALA2017120104267](https://openairdocs.org/sdr/CALA2017120104267.md): Light · unknown · Dec 1, 2017 · N57852 · Boeing 757324 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS IN ENTIRE CABIN CAME ON AND STAYED ON IN F LIGHT FOUND EMERGENCY LIGHTS TESTED GOOD.AMM 33-51-00-715-044. THINK M AYBE THE ATTENDANT''S SWITCH WAS IN THE ON POSTION DURING FLIGHT. THIS WOULD CAUSE THE LIGHT TO BE ON PER AMM 33-51-00 DESCR
- [SDR CALA2017103003865](https://openairdocs.org/sdr/CALA2017103003865.md): Light · inoperative · Oct 30, 2017 · N57852 · Boeing 757324 · Emergency Lighting
  > ROW SEAT 33FED EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP IAW AMM 33-51-05.
- [SDR CALA2017090803085](https://openairdocs.org/sdr/CALA2017090803085.md): Slider · binding · Sep 8, 2017 · N57852 · Boeing 757324 · Passenger/Crew Doors
  > L4 DOOR ARMING LEVER HARD TO ARM. LUBED THE DOOR SLIDER, OPS CHECKED GOOD, NO DEFECTS NOTED.
- [SDR CALA2017090803084](https://openairdocs.org/sdr/CALA2017090803084.md): Lens · broken · Sep 8, 2017 · N57852 · Boeing 757324 · Emergency Lighting
  > SEAT 19C EMERGENCY LIGHT LENS BROKEN. REPLACED THE LENS. LIGHT WORKS NORMALLY. OPS CHECKED GOOD IAW AMM 33-00-00.
- [SDR CALA2017081102615](https://openairdocs.org/sdr/CALA2017081102615.md): Lamp · inoperative · Aug 11, 2017 · N57852 · Boeing 757324 · Emergency Lighting
  > R2 DOOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-51-06.
- [SDR CALA2017072102303](https://openairdocs.org/sdr/CALA2017072102303.md): Unknown · odor · Jul 21, 2017 · N57852 · Boeing 757324 · Air Distribution System
  > CREW REPORTS ELECTRICAL SMELL AROUND ROWS 22-25 INSPECTED ABOVE CEILING PANEL ROWS 19-23 NO ISSUES NOTED. PACK RUN WITH NO ISSUES. CRAWLED AROUND SEAT MOUNTS AND LOOKED AT SEAT POWER BOXES AND SMELLED A LITTLE BIT OF ELECTRICAL BUT NO EVIDENCE OF BURNS OR CURR

Next page: https://openairdocs.org/aircraft/N57852/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 = 'N57852' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N57852/reports

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