# Service difficulty reports: N75854

A list on [N75854](https://openairdocs.org/aircraft/N75854.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 · 78 reports

- [SDR CALA2026041315287](https://openairdocs.org/sdr/CALA2026041315287.md): Housing · missing · Apr 11, 2026 · N75854 · Boeing 757324 · Emergency Lighting
  > ROW 23 LEFT SIDE EMERGENCY PATH INDICATOR HOUSING/LIGHT MISSING REPLACED EXIT PATH EMERGENCY LIGHT HOUSING AND EMERGENCY LIGHT AT SEAT 23C, TESTS GOOD.
- [SDR CALA2026040815210](https://openairdocs.org/sdr/CALA2026040815210.md): Fire Handle · binding · Apr 7, 2026 · N75854 · Boeing 757324 · Fire Protection System
  > NR 2 ENGINE FIRE HANDLE HARD TO PULL UP OR PUSH DOWN. FLAGGING AS AN SDR. CLEANED DIRTY FIRE HANDLE STEM AT BASE PLATE AND EXERCISED HANDLE UP AND DOWN. AFTER CLEANING HANDLE STEM, HANDLE OPERATION TO BE OF EQUAL TENSION TO OPERATE AS ENG 1. ALSO USED CALIBRAT
- [SDR CALA2026020913638](https://openairdocs.org/sdr/CALA2026020913638.md): Light · damaged · Feb 6, 2026 · N75854 · Boeing 757324 · Emergency Lighting
  > SEAT 22C EMERGENCY LIGHT DAMAGED INSTALLED LIGHT IAW 33-51-11-403-069. LIGHT TEST FUNCTIONS NORMAL.
- [SDR CALA2026020113464](https://openairdocs.org/sdr/CALA2026020113464.md): Target · out of adjust · Jan 29, 2026 · N75854 · Boeing 757324 · Door Warning System
  > INTERMITTENT RT CENTER ENTRY DOOR EICAS ON GROUND. REPEAT WRITEUP, MED R2 DOOR EICAS INTERMITTENT, COMPLIED WITH MEL CARD 5271C. MEL APPROVED FOR DOOR 2R, EICAS INDICATION INTERMITTENT. ADJUSTED THE TARGET TO GET THE CORRECT CLEARANCE BETWEEN THE TARGET AN
- [SDR CALA2026012613277](https://openairdocs.org/sdr/CALA2026012613277.md): Door · unlatched · Jan 26, 2026 · N75854 · Boeing 757324 · Service Doors
  > RIGHT CENTER ENTRY DOOR EICAS C THE RIGHT CENTER ENTRY DOOR IS NOT LATCHED UPON LANDING. DISSAPEARED SHORTLY AFTER. PERFORMED INSPECTION OF PROXIMITY SENSOR AT R2 DOOR IAW AMM 52-71-00-735-053. NO FAULT NOTED. CLEANED UP SENSOR AREA.
- [SDR CALA2025123012534](https://openairdocs.org/sdr/CALA2025123012534.md): Floorbeam · corroded · Dec 28, 2025 · N75854 · Boeing 757324 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON RT OTBD FLOOR STRUCTURE AT BS 1346. FOUND NEAR THE AFT CORNER OF THE EMERGENCY EXIT DOOR. REPAIRED RT OTBD FLOOR STRUCTURE AT BS 1346 IAW EC/RA 5310-08751.
- [SDR CALA2025122912480](https://openairdocs.org/sdr/CALA2025122912480.md): Support · corroded · Dec 23, 2025 · N75854 · Boeing 757324 · Fuselage Miscellaneous Structure
  > INTERIM REPAIR ACCOMPLISHED AT FUSELAGE RT LOWER SUPPORT SPLICE REPAIR BETWEEN BS 1310 AND 1370.
- [SDR CALA2025122912478](https://openairdocs.org/sdr/CALA2025122912478.md): Support · corroded · Dec 23, 2025 · N75854 · Boeing 757324 · Fuselage Miscellaneous Structure
  > INTERIM REPAIR ACCOMPLISHED AT FUSELAGE RT LOWER SUPPORT. SPLICE REPAIR BETWEEN BS 1310 AND 1370.
- [SDR CALA2025121612155](https://openairdocs.org/sdr/CALA2025121612155.md): Retainer · unsecure · Dec 14, 2025 · N75854 · Boeing 757324 · Fuselage Main, Structure
  > L1 DOOR CUTOUT UPPER SECTION,A SEAL RETAINER ATTACH SCREWS GOUGING STRUCTURE.( MKD) SEE BAM NR003003202 FOR WORK COMPLETED ECRA5300-01838. SRF AND SDR FORM ARE C/W LP7279301 DUPLICATED AS IS THIS LP VERIFIED
- [SDR CALA2025121612153](https://openairdocs.org/sdr/CALA2025121612153.md): Strap · worn · Dec 14, 2025 · N75854 · Boeing 757324 · Fuselage Main, Structure
  > L1 DOOR CUTOUT UPPER SECTION,A SEAL RETAINER ATTACH SCREWS GOUGING STRUCTURE.( MKD) SEE BAM NR#003003202 FOR WORK PERFORMED AND COMPLETED PER ECRA 5300-01838 MISS MAJOR REPAIR MARK AS YES, SEE LP7279695 FOR CORRECTION
- [SDR CALA2025121112029](https://openairdocs.org/sdr/CALA2025121112029.md): Floorbeam · corroded · Dec 9, 2025 · N75854 · Boeing 757324 · Fuselage Main, Floor Beam
  > FWD WET AREA, FLOORBEAM, BS 365.25 HAS CORROSION AND TOOLING DAMAGE, BETWEEN BL 0 AND RT END. REPAIRED.
- [SDR CALA2025112711510](https://openairdocs.org/sdr/CALA2025112711510.md): Deck Plate · corroded · Nov 25, 2025 · N75854 · Boeing 757324 · Fuselage Main, Structure
  > FWD EDGE OF DECK PLATE STA 1681 AS CORROSION IN SEVERAL SPOTS. MAJOR REPAIR. REMOVED AND REPLACE AFT DECK PLATE PO# 536354 PER DRAWING 146N5300 AND SRM 51-41-02.
- [SDR CALA2025111911345](https://openairdocs.org/sdr/CALA2025111911345.md): Deck Plate · corroded · Nov 18, 2025 · N75854 · Boeing 757324 · Fuselage Main, Structure
  > FWD EDGE OF DECK PLATE AT STA 1681 HAS CORROSION IN SEVERAL AREAS. SEE IMAGES. REPLACED DECK PLATE PER BOEING DWG NO:. 146N300 AND BOEING 757 SRM 51-40-02
- [SDR CALA2025111911343](https://openairdocs.org/sdr/CALA2025111911343.md): Floorbeam · corroded · Nov 18, 2025 · N75854 · Boeing 757324 · Fuselage Main, Floor Beam
  > CORROSION FOUND AROUND NUPLATE HOLE ON UPPER PART OF FLOOR BEAM AT STA 1681 RBL-32 PERFORMED BOEING 757 SRM 53-60-51-2R-3 REPAIR COMPLETED BOEING 757 SRM 53-60-51-2R-3 REPAIR
- [SDR CALA2025111811307](https://openairdocs.org/sdr/CALA2025111811307.md): Door Sill · corroded · Nov 16, 2025 · N75854 · Boeing 757324 · Fuselage Main, Structure
  > R2 DOOR LOWER MAIN SILL INNER CHORD IS CORRODED AT SEVERAL AREAS FROM BS 680 - 743. REPLACED R2 Z-ANGLE AT BS 680 - 780 IAW SRM 51-40-02.
- [SDR CALA2025090908665](https://openairdocs.org/sdr/CALA2025090908665.md): None · none · Sep 6, 2025 · N75854 · Boeing 757324 · Standard Practices/Structures
  > DUE TO L2 DOOR SLIDE REPLACEMENT THE FOLLOWING TECHS WORKING THE SLIDE REPLACEMENT ARE REQUIRED TO WATCH THE MTISE VIDEO FOUND IN QUICK TIP, ESCAPE SLIDES. B757 PASSENGER DOOR SLIDE REMOVE AND INSTALL. U118164, U181306, AND U416899. LIST THE EMPLOYEE FILE NUMB
- [SDR CALA2025081107570](https://openairdocs.org/sdr/CALA2025081107570.md): Sleeve · cut · Aug 9, 2025 · N75854 · Boeing 757324 · Ignition System
  > FOUND CUT ON TEFLON SLEEVE ON NR 1 ENGINE LOCATED BETWEEN 6-7 O'CLOCK. FOUND NO DAMAGED TO KEVLAR WRAP. TEFLON SLEEVE TEAR IS MEASURED TO BE 20"X16". UNABLE TO PERFORM REPAIR DUE TO REMOVAL REQUIREMENTS OF COMPONENTS. DAMAGE IS OKAY TO CONTINUE AS LONG IT IS
- [SDR CALA2025061005417](https://openairdocs.org/sdr/CALA2025061005417.md): Seal · damaged · Jun 7, 2025 · N75854 · Boeing 757324 · Engine Bleed Air System
  > FOUND DAMAGE ON THE LH WING LEADING EDGE DUCT VAPOR SEAL, NEED TO BE REPLACE M&E:19-3611-3-0027, PN BOE2049-0001 REPLACED VAPOR SEAL REF AMM TASK 36-11-01-404-109-001. LEAK CHECK GOOD.
- [SDR CALA2025051904784](https://openairdocs.org/sdr/CALA2025051904784.md): Sign · broken · May 16, 2025 · N75854 · Boeing 757324 · Emergency Lighting
  > FA REPORTS EMERGENCY EXIT SIGNED IN MIDDLE ISLE AT DOOR 2 HANGING MID AISLE OVERHEAD EXIT SIGN. SIGN HAS BEEN REMOVED FROM CIELING PANEL A/C SIDE CONNECTOR JUST LAYING IN PLACE. SIGN BROKEN, REQUIRES RR REPLACED THE DR 2L EXIT SIGN ASSY AND OPS CHECK GOOD AT
- [SDR CALA2025041103682](https://openairdocs.org/sdr/CALA2025041103682.md): Slide · unknown · Apr 8, 2025 · N75854 · Boeing 757324 · Escape Slide
  > DOOR 2L EMERGENCY POWER RESERVER HAS BEEN PINNED FOR REMOVAL OF ESCAPE SLIDE REF LOGPAGE 4438790 PER AMM 25-66-01-004-154 REMOVED DOOR 2 LEFT EMERGENCY POWER RESERVOIR PINS. VERIFIED L2 DOOR EMERGENCY RESERVOIR SAFETY PIN REMOVED.
- [SDR CALA2025040703572](https://openairdocs.org/sdr/CALA2025040703572.md): Lamp · inoperative · Apr 1, 2025 · N75854 · Boeing 757324 · Door Warning System
  > DOOR 1L SLIDE ARMED LIGHT WILL NOT ILLUMINAT E WHEN ARMED. RELAMPED DOOR ARMED LIGHT, LIGHT OPS CHECKED OK WHEN DOOR 1L WAS ARMED.
- [SDR CALA2024103000969](https://openairdocs.org/sdr/CALA2024103000969.md): Spring · faulty · Oct 27, 2024 · N75854 · Boeing 757324 · Doors
  > L-1 DOOR SLIDE ARM/DISARM HANDLE GREEN SIGN SPRING IS BROKEN REMOVED AND REPLACED SPRING PER AMM 52-11-02.PARTS USED: 19-5211-3-0415, QTY:1
- [SDR CALA2024072200262](https://openairdocs.org/sdr/CALA2024072200262.md): Fan · faulty · Jul 21, 2024 · N75854 · Boeing 757324 · Air Distribution Fan
  > SMOKE/ODOR IN THE CABIN AFTER TAKE-OFF. ACCOMPLISHED RECIR FAN OPERATIONAL TEST PER AMM TASK 21-25-00-005-040. TESTED OK. NO FAULTS FOUND. MUST WORK AMM SMOKE/ODOR IN THE FLIGHT DECK AND/OR CABIN CONDITIONAL INSPECTION (ADDED BY EC0500-01014) REFERENCE: TASK
- [SDR CALA2024060501705](https://openairdocs.org/sdr/CALA2024060501705.md): Intercostal · dented · May 30, 2024 · N75854 · Boeing 757324 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FR 1480 BETWEEN S-25L TO S-26L FOUND 2 EA DENTS. TRANSCRIBED FROM MAE NR 99133. PERFORM INSPECTIONS PER PART 2 OF THE LATEST REVISION OF ECRA 5360-01813 ON OR BEFORE 30,500 TOTAL AIRCRAFT FLIGHT CYCLES. ACCOMPLISHED REPAIR PER ECRA 5360-0
- [SDR CALA2023071002197](https://openairdocs.org/sdr/CALA2023071002197.md): Fan · unknown · Jul 9, 2023 · N75854 · Boeing 757324 · Air Distribution Fan
  > L RECIR FAN CAUTION MSG FAN IS FAILED REFERENCE B757 FIM 21-20 FAULT TREE 803 INFO ONLY: FLAGGED LOGPAGE FOR SDR REPORTING. ESFR WILL NEED FOUND LEFT RECIRCULATION FAN CONTROL CIRCUIT BREAKER OPEN ON P70 COMPLETED. PANEL. RESET CIRCUIT BREAKER RECIRC FAN RAN F
- [SDR CALA2023021000386](https://openairdocs.org/sdr/CALA2023021000386.md): Cover · missing · Feb 10, 2023 · N75854 · Boeing 757* · Doors
  > PDA 3 DOOR 2L UPPER HINGE COVER FOUND MISSING ON ARRIVAL. NO DAMAGE TO AIRCRAFT NOTED. PLACED ON CDL. REF GMM 02-30-95.
- [SDR CALA2022120703311](https://openairdocs.org/sdr/CALA2022120703311.md): None · none · Dec 6, 2022 · N75854 · Boeing 757324 · Standard Practices/Structures
  > THE REPAIR INCORPORATED VIA ECRA 5310-08079 IS APPROVED AS TIME LIMITED UNTIL 37,500 TOTAL AIRCRAFT FLIGHT CYCLES PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE AIRCRAFT FROM SERVICE ON OR BEFORE 37,500 TOTAL AIRCRAFT FLIGHT CYCLES, UNLES
- [SDR CALA2022120703310](https://openairdocs.org/sdr/CALA2022120703310.md): None · none · Dec 6, 2022 · N75854 · Boeing 757324 · Standard Practices/Structures
  > THE REPAIR INCORPORATED VIA ECRA 5360-5360-01680 STATION 1440 FUSELAGE FRAME BETWEEN S-29R AND S-29L STRINGERS IS APPROVED AS TI ME LIMITED UNTIL 50,000 TOTAL AIRCRAFT FLIGHT CYCLES PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE AIRCRA FT
- [SDR CALA2022120703307](https://openairdocs.org/sdr/CALA2022120703307.md): None · none · Dec 5, 2022 · N75854 · Boeing 757324 · Standard Practices/Structures
  > THE REPAIR INCORPORATED VIA EC/RA 5360-01678 BS 1420 FRAME, S24L & S27L. APPROVED AS TIME LIMITED UNTIL 25,600 TOTAL AIRCRAFT FLIGHT CYCLES PENDING THE RE SULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE ACFT FROM SERVICERE 25,600 TOTAL AIRCRAFT FLIGHT CYC
- [SDR CALA2022120503304](https://openairdocs.org/sdr/CALA2022120503304.md): Frame · dented · Dec 5, 2022 · N75854 · Boeing 757324 · Fuselage Main, Frame
  > EA 5310-07582 REV A FRAME 1420 INSIDE THE AFT CARGO COMPARTMENT NEAR S-26L HAS TWO DENTS ON TOP OF THE FRAME FLANGE, DAMAGE MARK ED IN RED. DENTS FOUND TO BE OUT OF LIMITS PER 53-00-07-1A-1 FIG 1. REPAIRE D FRAME AT STA 1420 L/H PER EA 757-5360-13-A3083 REV A
- [SDR CALA2021110502037](https://openairdocs.org/sdr/CALA2021110502037.md): None · inoperative · Nov 4, 2021 · N75854 · Boeing 757324 · Auto Flight System
  > CAPTAIN STATED, ON INITIAL LEVEL OFF AT 5000 FT OUT OF HNL, LEFT AUTO THROTTLE UNABLE TO RETARD THRUST BACK TO MATCH RIGHT ENGINE. AFTER AUTO THROTTLE DISCONNECTION UNABLE TO MANUALLY RETARD THROTTLE TO MATCH RIGHT SIDE ALSO. LEFT THROTTLE WAS 20 PERCENT N1 HI
- [SDR CALA2020112501303](https://openairdocs.org/sdr/CALA2020112501303.md): Panel · inoperative · Nov 25, 2020 · N75854 · Boeing 757324 · Fixed Inner Doors
  > UNABLE TO LOCK FLIGHT DECK DOOR. REPLACED DOOR SWITCH CONTROL PANEL, REF AMM 52-52-01-000-801C9. OPERATIONS CHECKED GOOD, REF AMM 52-52-01-700-801C3. TRACKING TAG NR 113608 8. S/N OFF 0014 S/N ON 0048. ROTABLE PARTS CHANGE WAS INDICATED-TT NR 1136088 SN O
- [SDR CALA2020040300758](https://openairdocs.org/sdr/CALA2020040300758.md): Frame · corroded · Mar 31, 2020 · N75854 · Boeing 757324 · Fuselage Main, Frame
  > (B757-06-3-0242) CORROSION ON AFT CARGO FRAME FWD SIDE AT STA 14 20 BETWEEN STR 28L - 29R. REF ST-SAA NR 0088725 ACCOMPLISHED INTERIM REINFORCING REPAIR ON AFT CARGO FRAME AT ST COMPLISHED A 1420 BETWEEN STR 29R - 28L IAW EC/RA 5360-01553 PART1. WORK AC AND PA
- [SDR CALA2020032700694](https://openairdocs.org/sdr/CALA2020032700694.md): Frame · dented · Mar 22, 2020 · N75854 · Boeing 757324 · Fuselage Main, Frame
  > (B757-53-3-0492) DENT ON FWD CARGO FRAME UPPER FLANGE AT STA 540 BETWEEN STR 24L-25L. RG42() REF ST-SAA NR 0091847 EEN STR 24L-25L TO 1.180"L X 1.040"W X 0.5"R & ACCOMPLISHED A IN TERIM RE-INFORCING REPAIR IAW EC/RA 5310-07771 REV-PART1. SEE SU PPLEMENT 95126
- [SDR CALA2020032700696](https://openairdocs.org/sdr/CALA2020032700696.md): Floorbeam · corroded · Mar 22, 2020 · N75854 · Boeing 757324 · Fuselage Main, Floor Beam
  > B757-53-3-0554 FLOOR BEAM AT STA 377.7" MAIN CABIN HAS CORROSION ON UPPER SURFACE FROM BL-0 TO LBL 24-5 AT SEAT TRACK. ST-SAA F REF NR0089135 REMOVED CORROSION ON MAIN CABIN FLOORBEAM AT STA 377.7 BET LBL 2 4.5 AND BL0 L=22.00 W=2.0 D=0.22. BLEND OUT FOUND OU
- [SDR CALA2020032700693](https://openairdocs.org/sdr/CALA2020032700693.md): Frame · dented · Mar 22, 2020 · N75854 · Boeing 757324 · Fuselage Main, Frame
  > (B757-53-3-0492) DENT ON FWD CARGO FRAME UPPER FLANGE AT STA 520 STR 24L. RG41() REF ST-SAA NR 0088857 24L (1.680"X1.040"X0.5"R) & ACCOMPLISHED A INTERIM RE-INFORCING REPAIR IAW EC/RA 5332-01023 REV-PART 1. WORK ACCOMPLISHED TRIMMED-OUT DENT ON FWD CARGO FRAME
- [SDR CALA2020040300757](https://openairdocs.org/sdr/CALA2020040300757.md): Stringer · cracked · Mar 18, 2020 · N75854 · Boeing 757324 · Fuselage Main, Longeron/Stringer
  > (B757-53-3-0562) STRINGER 16R IN MAIN CABIN AT STA 780+36 IS CRACKED. REF ST-SAA NR 0088556. INSTALLED PERMANENT REPAIR FUSELAGE STRINGER 16R BETWEEN STA 780 +40 AND 780+60 IAW ECRA 5330-06744 REV. WORK ACCOMPLISHED, INSPECTED. INSPECTION COMPLETED AND ACCETED
- [SDR CALA2020032100667](https://openairdocs.org/sdr/CALA2020032100667.md): Frame · dented · Mar 18, 2020 · N75854 · Boeing 757324 · Fuselage Main, Frame
  > (B757-53-3-0524) 2 EA DENTS ON AFT CARGO FRAME UPPER FLANGE AT S TA 1400 BETWEEN STR 25L - 26L. REF ST-SAA NR 0088763. PLACED ON DIP PER ECRA 5360-01552, PLANNING TO CONTACT ENGUNEERI NG AFTER 32600 CYCLES BUT BEFORE 33600 CYCLES FOR INSPECTION REQ UIREMENTS
- [SDR CALA2020032100657](https://openairdocs.org/sdr/CALA2020032100657.md): Frame · dented · Mar 15, 2020 · N75854 · Boeing 757324 · Fuselage Main, Frame
  > (B757-53-3-0524) DENT ON AFT CARGO FRAME UPPER FLANGE AT STA 144 0 BETWEEN STR 25L - 26L. REF ST-SAA NR 0088762 CHECKED LIMITS TO DENT ON AFT CARGO FRAME UPPER FLANGE AT STA 14 40 BETWEEN S25L AND S26L L=1.30 W=.80 D=.028 OUT OF LIMITS IAW B 757-3 SRM 53-00-07
- [SDR CALA2020030700574](https://openairdocs.org/sdr/CALA2020030700574.md): Depressor · dented · Mar 1, 2020 · N75854 · Boeing 757324 · Cargo/Baggage Doors
  > (B757-06-3-0354) FWD CARGO DOOR INTERNAL AFT FRAME SEAL DEPRESSO R IS BENT AND DENTED.REF ST-SAA NR 0088445. MEASURED AND FOUND DENT ON FWD CARGO DOOR INTERNAL AFT FRAME SEA L DEPRESSOR TO BE OUT OF LIMITS (L= 3.5" X W= 1.0" X D=.270", A /Y= 12.96 < 30) IAW B
- [SDR CALA2020022980518](https://openairdocs.org/sdr/CALA2020022980518.md): Stringer · cracked · Feb 26, 2020 · N75854 · Boeing 757324 · Fuselage Main, Longeron/Stringer
  > (B757-53-3-0560) STRINGER 16L IN MAIN CABIN IS CRACKED AT STA 78 0+24. REF ST-SAA NR 0088550. REMOVED AND REPLACED STRINGER SECTION FROM PRODUCTION SPLICE AT STA 780 TO STA 780+24 STR 16L IAW DWG 143N3100 AND B757-3 SRM 51 -40-02 AND B757-3 SRM 51-40-05 RESTOR
- [SDR CALA2020022980517](https://openairdocs.org/sdr/CALA2020022980517.md): Stringer · cracked · Feb 26, 2020 · N75854 · Boeing 757324 · Fuselage Main, Longeron/Stringer
  > (B757-53-3-0562) STRINGER 16R IN MAIN CABIN AT STA 780+24 IS CRACKED. REF ST-SAA NR 0088554. REMOVED AND REPLACED 16R STRINGER SECTION FROM PRODUCTION SPLICE LOCATION AT STA 776 TO STA 780+24 IAW B757-3 SRM 51-40-02 DWG 1 43N3100 B757-3 SRM 51-40-05 RESTORED C
- [SDR CALA2020022400478](https://openairdocs.org/sdr/CALA2020022400478.md): Stringer · cracked · Feb 20, 2020 · N75854 · Boeing 757324 · Fuselage Main, Longeron/Stringer
  > B757-53-3-0560 STRINGER 16L IN MAIN CABIN AT STA 780 + 36 IS CRACKED. (96-11) REF VT-SAA N/R 0088553 REPAIRED STRINGER 16L IN MAIN CABIN AT STA 780+36 IAW B757-300 S RM 53-30-03 REPAIR 1, PG 201, FIG 201.
- [SDR CALA2020011000119](https://openairdocs.org/sdr/CALA2020011000119.md): Actuator · malfunctioned · Jan 9, 2020 · N75854 · Boeing 757324 · Drag Control Actuator
  > SPOILER EICAS ADVISORY MSG AND ASSOCIATED OVERHEAD SPOILER LIGHT ILLUMINATED. ACFT IS EXPERIENCING LEFT HAND TURN TENDENCY WHILE HAND FLYING. FUEL FLOW AND BURN IS HIGHER THAN ANTICIPATED AT EACH WAYPOINT. REF. FIM 27-61-00-815-802, BOX [1] ASKS IS THERE A PCA
- [SDR CALA2019111101964](https://openairdocs.org/sdr/CALA2019111101964.md): Warning Message · false activation · Nov 11, 2019 · N75854 · Boeing 757324 · Trailing Edge Flap Control System
  > TE FLAP DISAGREE TE FLAP LOCKOUT AT 22 DEGREES PERFORMED BITE OF FSEU REF FIM 27-50-00. MAINT CODE 217. FLA FAIL. CYCLED FLAPS SLATS SEVERAL TIMES. OPS CK NORMAL. PERFORMED FLA TEST REF FIM 27-51-00. OPS CK NORMAL. REMOVED AND REPLACED #1 AND #2 FSEU, GET HAR
- [SDR CALA2019082601437](https://openairdocs.org/sdr/CALA2019082601437.md): Engine · vibration · Aug 26, 2019 · N75854 · Boeing 757324 · Engine (Turbine/Turboprop)
  > LEFT ENG VIBS REACHED 2.8 REDUCED THRUST AND VIBS STAYED BELOW 2.5 REF FIM 71-05-00-815-808-ROO, BLOCKS 1, 2 & 3 #1 ENG EXAMINATION SHOWED NO ANOMOLIES. PER BLOCK 4, WITH VIBE AT 2.8 UNITS, ENG IS OK FOR SVC BUT VIBRATION SURVEY TEST 6 MUST BE DONE NLT 5 FLT
- [SDR CALA2019072801262](https://openairdocs.org/sdr/CALA2019072801262.md): Heater · malfunctioned · Jul 27, 2019 · N75854 · Boeing 757324 · Emergency Exits
  > SIDEWALL AT 21F BETWEEN WINDOWS VERY HOT PLACE ON MEL 2145M. RT OVERWING EMERGENCY EXIT HATCHES RIGHT OVRWNG EXIT DOOR HEATER PLACED ON MEL2145M, P/N 116941-2, M&E 19-5222-3-0043, IPC 52-22-02-25 ITEM 95. HEATER IS NIS IN HNL.
- [SDR CALA2019060400883](https://openairdocs.org/sdr/CALA2019060400883.md): Wheel · broken · Jun 3, 2019 · N75854 · Boeing 757324 · Wheel/Ski/Float
  > 11" X 4" SECTION OF OUTBOARD LH NLG WHEEL ASSY BROKE AWAY DURING GATE ENTRY RESULTING IN TIRE GOING FLAT. NO INJURIES, NO FLIGHT IRREGULARITY AS RON AIRCRAFT. BOTH NOSE TIRES CHANGED. INITIAL INSPECTION OF FULLY RECOVERED PART INDICATES MATALLURGY FAILURE.
- [SDR CALA2018090401880](https://openairdocs.org/sdr/CALA2018090401880.md): Skin · damaged · Aug 31, 2018 · N75854 · Boeing 757324 · Fuselage Main, Plate/Skin
  > SKIN DAMAGED AT FUSELAGE STA 1681.80 STRINGER 20RT. ACCOMPLISHED REPAIR AT SKIN DAMAGED AT FUSELAGE STA1681.80 STG 2 0RT AS PER WORK INSTRUCTIONS RES NR 2013922-4 AND EC/RA 5331-022 54.
- [SDR CALA2018010700084](https://openairdocs.org/sdr/CALA2018010700084.md): Engine · abnormal · Jan 7, 2018 · N75854 · Boeing 757324 · Engine (Turbine/Turboprop)
  > STRONG MUSTY ODOR ON DESCENT. REMOVED AND REPLACED NR 1 ENGINE REF WC 19-7100-1-0900.

Next page: https://openairdocs.org/aircraft/N75854/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 = 'N75854' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N75854/reports

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