# Service difficulty reports: N19141

A list on [N19141](https://openairdocs.org/aircraft/N19141.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 3 · 138 reports

- [SDR CALA2026082418821](https://openairdocs.org/sdr/CALA2026082418821.md): Lamp · inoperative · Aug 24, 2026 · N19141 · Boeing 757224 · Emergency Lighting
  > EMERGENCY LIGHTS PANEL BACKLIGHT INOPERATIVE, OVERHEAD EMERGENCY LIGHTS, PAX OXYGEN PANEL LIGHT PLATE DARK. SOLDERED & REPLACED THE LAMPS IN LIGHT PLATE IAW AMM 33-13-01. OPS CHECK GOOD.
- [SDR CALA2026071417789](https://openairdocs.org/sdr/CALA2026071417789.md): Computer · faulty · Jul 12, 2026 · N19141 · Boeing 757224 · Air Collision Avoidance System
  > TCAS RA CLIMBING THRU 5000..CLIMB FOR 2000 FOLLOWED BY DESCEND WITH NO VISIBLE TRAFFIC, WORK WITH FIM 34-45 TASK 801. MTX WORKING ITEM REF LP 9587435 FOR WORK PERFORMED TCAS RA CLIMBING THRU 5000. CLIMB FOR 2000 FOLLOWED BY DESCEND WITH NO VISIBLE TRAFFIC RE
- [SDR CALA2026052116440](https://openairdocs.org/sdr/CALA2026052116440.md): Frame · dented · May 20, 2026 · N19141 · Boeing 757224 · Fuselage Main, Frame
  > AFT CARGO BAY BS 1220, STR 26L, FRAME HAS DENT ON FREE FLANGE AREA. REPAIR PARTS FABRICATED. ACCOMPLISHED BS 1220, STR 26L FRAME REPAIR IAW ECRA 5360-021 45 AND VT MAE EA 757-5360-13-A4444 REV-.
- [SDR CALA2026051416240](https://openairdocs.org/sdr/CALA2026051416240.md): Web · dented · May 13, 2026 · N19141 · Boeing 757224 · Fuselage Main, Plate/Skin
  > STABILIZER COMPARTMENT, THROUGH ACCESS 311AL, CLOSE TO STA 1862.70, STABILIZER CUTOUT, LH SIDE, WEB HAS A DENT. REF NR 145862. REMOVED AND REPLACED DENTED WEB BY NEW WEB PN UA-148N7309-23 FRO M TAB SHOP TRAVELER# T26/1863849 IAW B757-200 SRM 51-40-02-0G-0, R
- [SDR CALA2026051116134](https://openairdocs.org/sdr/CALA2026051116134.md): Threshold · cracked · May 9, 2026 · N19141 · Boeing 757224 · Fuselage Miscellaneous Structure
  > REMOVED AND INSTALLED THRESHOLD ON FWD CARGO COMP. IAW AMM 53-13 -02-004 AND AMM 53-13-02-424-005 NR: 145675 REPLACEMENT OF THRESHOLD WAS DUE TO CRACK NOTED, NEW THRESHOLD FWD CARGO THRESHOLD CRACKED AT PREVIOUS WELD. REMOVED AND INSTALLED THRESHOLD ON FWD C
- [SDR CALA2026051116128](https://openairdocs.org/sdr/CALA2026051116128.md): Support Angle · gouged · May 8, 2026 · N19141 · Boeing 757224 · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL STAB LT SIDE ACCESS PANEL 324AL LOWER SUPPORT ANGLE GOUGED. REMOVED AND REPLACED DAMAGED ANGLE BY NEW ANGLE IAW SRM 51-40-02 RESTORED SURFACE PROTEC ION AT AREA IAW AMM TASK 51-21-15-370-801 STA 1804.81
- [SDR CALA2026051116124](https://openairdocs.org/sdr/CALA2026051116124.md): Skin · cracked · May 8, 2026 · N19141 · Boeing 757224 · Wing, Plate/Skin
  > LEFT WING NR 2 SLAT COVE SKIN AROUND INBD MAIN TRACK CRACKED. REMOVED, FABRICATED, REPLACED COVE. SKIN COMMON TO NR 2 SLAT IAW SRM 51-40-02-0G-1 AND REF DWG 114N7076.
- [SDR CALA2026051116122](https://openairdocs.org/sdr/CALA2026051116122.md): Skin · cracked · May 8, 2026 · N19141 · Boeing 757224 · Wing, Plate/Skin
  > NUMBER 10 SLAT OTBD COVE SKIN CRACKED NEAR 652BB COVER PANEL. REMOVED, FABRICATED, INSTALLED COVE SKIN COMMON TO NR 10 SLAT OTBD IAW SRM 51-40-02-0G AND DWG 114N4075.
- [SDR CALA2026051116120](https://openairdocs.org/sdr/CALA2026051116120.md): Skin · cracked · May 8, 2026 · N19141 · Boeing 757224 · Wing, Plate/Skin
  > RIGHT WING, NR 10 SLAT, INNER SURFACE, CLOSE TO INBD TRACK, SKIN HAS A CRACK. REMOVED, FABRICATED, INSTALLED COVE SKIN COMMON TO NR 10 SLAT IAW SRM 51-40-02-0G AND DWG 114N4075.
- [SDR CALA2026051016092](https://openairdocs.org/sdr/CALA2026051016092.md): Skin · cracked · May 7, 2026 · N19141 · Boeing 757224 · Leading Edge Devices
  > RIGHT WING, NR 8 SLAT, INNER SURFACE SKIN HAS A CRACK. REMOVED, FABRICATED, REINSTALL NEW COVE SKIN O/T NO. 8 SLAT IAW DWG 114N4077 AND SRM 51-40-02-0G MATERIAL 7075 T6.056 THICK, NO DEVIATION IAW OPS CHECK AMM 27-81-02-424-021.
- [SDR CALA2026051016090](https://openairdocs.org/sdr/CALA2026051016090.md): Angle · cracked · May 7, 2026 · N19141 · Boeing 757224 · Fuselage Miscellaneous Structure
  > LEFT MLG W/W STA 1037 BEAM ANGLE CRACKED AT LBL 64 BEHIND ACCESS PANEL 197AL. THE ANGLE WAS REMOVED IAW B757-300 SRM 51-40-02-0G, ANGLE WAS FABRICATED IAW DWG 149N7553 REV N AND PL LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05-0G, NEW ANGLE WAS TREATED PRIME
- [SDR CALA2026050816079](https://openairdocs.org/sdr/CALA2026050816079.md): Transition Panel · corroded · May 7, 2026 · N19141 · Boeing 757224 · Fuselage Miscellaneous Structure
  > FWD CARGO BETWEEN STA 620 TO 640 RT TRANSITION PANEL WITH CORROSION. REMOVED AND REPLACED TRANSITION PANEL IAW SRM 51-40-02-0G-0, & SRM 51-40-05-06-0.
- [SDR CALA2026050716052](https://openairdocs.org/sdr/CALA2026050716052.md): Support · damaged · May 5, 2026 · N19141 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT. STA. 1200, LBL 24.75 CEILING PLATE SUPPORT BROKEN. CEILING SUPPORT WAS REMOVED IAW B757-200 SRM 51-40-02-0G NEW SUPPORT WAS FABRICATED, LOCATED AND DRILLED IAW SRM 51-20-05-0G SUPPORT WAS TREATED, PRIMED AND PAINTED IAW AMM 51-21-04, AMM 5
- [SDR CALA2026050516007](https://openairdocs.org/sdr/CALA2026050516007.md): Support Bracket · cracked · May 3, 2026 · N19141 · Boeing 757224 · Fuselage Miscellaneous Structure
  > FWD CARGO STA 740 RH SIDE SUPPORT BRACKET THAT ATTACH SIDWALL IS BENT. CHANNEL SUPPORT AND 06EA NUTPLATE WERE REMOVED IAW B757-200 SRM 51-40-02-0G, PART FABRICATION PERFORMED IN-HOUSE, HEAT TREATMENT ACCOMPLISHED, HARDNESS: 84, CONDUCTIVITY: 48.0, IAW BA C560
- [SDR CALA2026050515973](https://openairdocs.org/sdr/CALA2026050515973.md): Splice Angle · corroded · May 1, 2026 · N19141 · Boeing 757224 · Fuselage Miscellaneous Structure
  > ACCESS PANEL 139CL FORWARD KEEL BEAM REQUIRE FURTHER CLEANING AT PANEL ATTACH FRAMES AND CHECK ON CORROSION. CLEANED AREA IAW BOEING SOPM 20-30-03, REMOVED CORROSION ON LH A ND RH TEE BEAM BTW 995-1040 IAW B757-200 SRM 51-10-02-0G-0. ORIG INAL THICKNESS.130
- [SDR CALA2026050515971](https://openairdocs.org/sdr/CALA2026050515971.md): Splice Angle · corroded · May 1, 2026 · N19141 · Boeing 757224 · Fuselage Miscellaneous Structure
  > ACCESS PANEL 139AL FORWARD KEEL BEAM REQUIRE FURTHER CLEANING AT PANEL ATTACH FRAMES AND CHECK ON CORROSION. CLEANED AREA IAW SOPM 20-30-03. REMOVED CORROSION IAW SRM 51-10-02-0G-0. ORIGINAL THICKNESS.130", REMAINING THI CKNESS.123" FOUND TO BE WITHIN LIMI
- [SDR CALA2026050515969](https://openairdocs.org/sdr/CALA2026050515969.md): Splice Angle · corroded · May 1, 2026 · N19141 · Boeing 757224 · Fuselage Miscellaneous Structure
  > ACCESS PANEL 139BL FORWARD KEEL BEAM REQUIRE FURTHER CLEANING AT PANEL ATTACH FRAMES AND CHECK ON CORROSION. CLEANED AREA IAW BOEING SOPM 30-30-03, REMOVED CORROSION ON LH A ND RH TEE BEAM BTW STA 965-995 IAW 51-10-02-0G-0. ORIGINAL THICK NESS.130" REMAINING
- [SDR CALA2026050515966](https://openairdocs.org/sdr/CALA2026050515966.md): Support · cracked · May 1, 2026 · N19141 · Boeing 757224 · Fuselage Miscellaneous Structure
  > LEFT CEILING SUPPORT AT STA 1640-1681 CRACKED IN NUMEROUS LOCATIONS. REMOVED AND REPLACED LT CEILING SUPPORT AT BS 1640-1681, IAW SRM 51-40-02-0G -0 AND SRM 51-40-05-0G-0.
- [SDR CALA2026050415964](https://openairdocs.org/sdr/CALA2026050415964.md): Support · cracked · May 1, 2026 · N19141 · Boeing 757224 · Fuselage Miscellaneous Structure
  > RT CEILING SUPPORT AT STA 1640-1681 CRACKED. REMOVED AND REPLACED L/H CEILING SUPPORT AT BS 1640-1681 BY NEW PART IAW B757-200 SRM 51-40-02AND SRM 51-40-05.
- [SDR CALA2026043015885](https://openairdocs.org/sdr/CALA2026043015885.md): Floorbeam · corroded · Apr 29, 2026 · N19141 · Boeing 757224 · Fuselage Main, Floor Beam
  > LOWER FUSELAGE AT BS 900 LBL 0 TO RBL 12 T-CHORD WITH EXFOLIATED AND DELAMINATED. REPAIRED T-CHORD ON LOWER FUSELAGE WTB STRUCTURE AT STA 900 LBL 12 - RBL 12 IAW SRM 51-70-12-0G-0.
- [SDR CALA2026043015883](https://openairdocs.org/sdr/CALA2026043015883.md): Intercostal · cracked · Apr 29, 2026 · N19141 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT. BS 1200 CEILING AREA BL 0, INTERCOSTAL WEB IN FWD CORNER IN FWD CORNER CRACKED. THE DAMAGED INTERCOSTAL WAS REMOVED AND REPLACED, NEW INTE RCOSTAL WAS POSITIONED AND DRILLED IAW SRM 51-40-05-0G, AND NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40
- [SDR CALA2026042815766](https://openairdocs.org/sdr/CALA2026042815766.md): Angle · cracked · Apr 25, 2026 · N19141 · Boeing 757224 · Aerodynamic Fairings
  > RT MLG W/W FAIRING STRUCTURE ANGLE CORNER AT STA 1094 CRACKED. NR# 145213 ESFR INFORMATION ENTERED REMOVED AND REPLACED ANGLE CORNER AT RT MLG W/W FAIRING STRUCTURE AT BS 1094 IAW B757-200 SRM 51-40-02-0G-0.
- [SDR CALA2026042815749](https://openairdocs.org/sdr/CALA2026042815749.md): Angle · cracked · Apr 24, 2026 · N19141 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT CARGO CEILING BS 1420 - 1440, RBL 14.25 CRACKED CEILING ANGLE COMMON TO INTERCOSTAL. REMOVED AND REPLACED CEILING ANGLE AT AFT CARGO CEILING BS 1420 - 1440, RBL 14.25 COMMON TO INTERCOSTAL. IAW SRM 51-40-02-OG-0.
- [SDR CALA2026042415674](https://openairdocs.org/sdr/CALA2026042415674.md): Angle · cracked · Apr 22, 2026 · N19141 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT CARGO CEILING STA 1580 RBL 14.25: CRACKED CEILING ANGLE COMMON TO INTERCOSTAL. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G -0, APPLIED CIC IAW AMM 51-24-03-277-008.
- [SDR CALA2026022614071](https://openairdocs.org/sdr/CALA2026022614071.md): O-Ring · damaged · Feb 25, 2026 · N19141 · Boeing 757224 · Emergency Equipment
  > ONE EMERGENCY FLASHLIGHT HAS A DAMAGED O-RING AT FWD FLIGHT ATTENDANT SEAT. REMOVED & REPLACED FLASHLIGHT.
- [SDR CALA2026010612723](https://openairdocs.org/sdr/CALA2026010612723.md): Apu · faulted · Jan 5, 2026 · N19141 · Boeing 757224 · APU Core Engine
  > AFTER STARTING APU & DISCONNECTING GROUND POWER, CREW & PAX SAW & SMELLED SMOKE. WAS WHITE & HAD A BURNING ELECT ODOR. APU SHUTDOWN AUTOMATICALLY & CREW POWERED DOWN ADDITIONAL SYS. PERFORMED APU MAGNETIC CHIP DETECTOR INSP, FOUND METAL ON COMPRESSION BEARIN
- [SDR CALA2026010512668](https://openairdocs.org/sdr/CALA2026010512668.md): Slide · faulty · Jan 1, 2026 · N19141 · Boeing 757224 · Escape Slide
  > LEVEL-2 CHRONIC DOOR L4 ARMING ISSUES. DUE REPEATED FAULTS OF D OOR L4 HARD TO ARM WITH REPEAT FINDINGS OF GIRT MATERIAL IMPENDI NG WITH ARMING FUNCTION. ALONG WITH REPEATED FINDINGS OF DAMAGE TO BUSTLE ASSY. THESE FAULTS STARTED AFTER THIS SLIDE WAS RECENT LY
- [SDR CALA2025110310852](https://openairdocs.org/sdr/CALA2025110310852.md): Girt Bar · out of adjust · Oct 31, 2025 · N19141 · Boeing 757224 · Emergency Equipment
  > L4 DOOR WILL NOT ARM, GIRT BAR WAS CLEANED ON FLOOR AND ADJUSTED MECHANISM IAW AMM 25-66-00. OPS CHECKED ARMED-DISARMED LEVER, DOOR SLIDE WAS SATISFACTORY. OK TO CONTINUE.
- [SDR CALA2025102110345](https://openairdocs.org/sdr/CALA2025102110345.md): Fire Loop · faulted · Oct 19, 2025 · N19141 · Boeing 757224 · Fire Detection
  > MULTIPLE INTERMITTENT RT ENGINE FIRE WARNINGS DURING CLIMB/CRUISE. RT ENGINE FIRE LOOP 2 INITIALLY INOPERATIVE IAW MEL, FIRE WARN WOULD HAVE WENT OFF DUE TO FAULT IN LOOP 1. FOUND POSITIVE FIX FOR RT ENG. FIRE LOOP 2. MEL CLEARED. NO FAULTS NOTED FOR RT ENG
- [SDR CALA2025092409205](https://openairdocs.org/sdr/CALA2025092409205.md): Bottle · no discrepancy · Sep 21, 2025 · N19141 · Boeing 757224 · Emergency Equipment
  > DOOR 2L SLIDE GAUGE IN THE RED PAST THE GREEN BAND. INSPECTED INFLATION CYLINDER ON DOOR 2L REF AMM 25-66-01-206-024, NEEDLE IS NOT MORE THAN HALF THE WIDTH OFF THE GREEN MARKER, PRESSURE REMAINS STABLE. OK FOR SERVICE.
- [SDR CALA2025091508875](https://openairdocs.org/sdr/CALA2025091508875.md): Fuse · inoperative · Sep 12, 2025 · N19141 · Boeing 757224 · Emergency Lighting
  > EMERGENCY LIGHTS, OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE, DOOR 3R EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY FUSE IAW AMM 33-51-07-962-071 OPS CHECKED GOOD. REPLACE LIGHT ASSEMBLY AS REF. AMM 33-51-06-962-049-001.
- [SDR CALA2025091508894](https://openairdocs.org/sdr/CALA2025091508894.md): Girt Bar · fod · Sep 10, 2025 · N19141 · Boeing 757224 · Emergency Equipment
  > DOOR 4R SLIDE LIGHT INOPERATIVE. REMOVED DEBRIS FROM GIRT BAR AREA. SLIDE LIGHT OPS NORMAL
- [SDR CALA2025091108781](https://openairdocs.org/sdr/CALA2025091108781.md): Lamp · inoperative · Sep 10, 2025 · N19141 · Boeing 757224 · Emergency Lighting
  > INOP SLIDE LIGHT IS ON DOOR 3R. REPLACED 3R SLIDE LIGHT OPS CHECK GOOD IAW AMM 33-51-06.
- [SDR CALA2025081107530](https://openairdocs.org/sdr/CALA2025081107530.md): Unknown · odor · Aug 10, 2025 · N19141 · Boeing 757224 · Air Distribution System
  > STRONG ODOR OF OIL IN COCKPIT, ON INSPECTION OF FLIGHT DECK VENT, TRACE OF OIL SMELL COMING FORM VENTS OK TO CONTINUE.
- [SDR CALA2025073107177](https://openairdocs.org/sdr/CALA2025073107177.md): Wire · broken · Jul 30, 2025 · N19141 · Boeing 757224 · Light System Wiring
  > EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - AISLE PATH LIGHTING AT ROW 31 DOES NOT ILLUMINATE. FOUND BROKEN GROUND WIRE AT SPLICE LOCATED UNDER SEAT ROW 31. RESPLICED WIRE UNDER SEAT ROW 31 IN REF. SWPM 20-30-12 AND DRAWING BR2013-P-75
- [SDR CALA2025062305805](https://openairdocs.org/sdr/CALA2025062305805.md): Battery Pack · no test · Jun 22, 2025 · N19141 · Boeing 757224 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - DOOR 3L EMERGENCY LIGHT IS INOP RELAMP NO HELP, REF AMM 33-51-06-962-001-001. UPON FURTHER INSPECTION, REMOVED AND REPLACED RESPECTED BATTERY, LIGHT CAME ON OPPOSITE GOOD OK FOR OPERATION.
- [SDR CALA2025051304647](https://openairdocs.org/sdr/CALA2025051304647.md): Governor · faulty · May 10, 2025 · N19141 · Boeing 757224 · Engine Fuel Distribution
  > LEFT ENG FAILED TO GET 1.60 EPR ON TAKEOFF ONLY REACHED 1.30 REJ ECTED AT 80KTSPERFORMED FIM 77-11 FAULT TREE 805. REMOVED AND REPLACED E1 EPR TRANSMITER IN REFF WITH AMM TASK 77-11-01. REQUIRES HIGH POWER RUN DUE TO E1 EPR DID NOT PASS 1.3.PARTS USED: 19-771
- [SDR CALA2025032002999](https://openairdocs.org/sdr/CALA2025032002999.md): Battery · discharged · Mar 20, 2025 · N19141 · Boeing 757224 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - EXTERIOR RIGHT OVERWING EGRESS AFT EMERGENCY LIGHT (2 TOTAL) WILL NOT TEST. REF WDM 33-51-14-902, FOUND CONNECTOR M10699J AT SEAT ROW 28DEF (SEE PICTURE). NEED BATTERY PACK ME#75-3351-3-0041
- [SDR CALA2025032002992](https://openairdocs.org/sdr/CALA2025032002992.md): Bulb · inoperative · Mar 18, 2025 · N19141 · Boeing 757224 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - EXTERIOR AT DOOR 2L EMERGENCY LIGHT WILL NOT TEST EVEN AFTER LIGHT BULB (767) REPLACEMENT. REF WDM 33-51-15-902, LOCATED M736 & M737 JUST BEHIND AFT GLY AREA LIGHT. SWAPPED CONNECTOR BUT NO
- [SDR CALA2025022402433](https://openairdocs.org/sdr/CALA2025022402433.md): Cooling Fan · shorted · Feb 21, 2025 · N19141 · Boeing 757224 · Air Distribution Fan
  > STRONG ELECTRICAL BURN SMELL IN FLIGHT FOUND CB FWD EQUIP COOL SUPPLY FAN 1 (F17) ON THE P6 PANEL POPPED. RESET CB PER GMM 05-30-05 AND PERFORMED OPS TEST OF FWD EQUIP COOL SUPPLY FAN REF AMM 21-58-06. CB IMMEDIATELY POPS WHEN EQUIP COOLING SWITCH IS DEPRESSED
- [SDR CALA2025021002270](https://openairdocs.org/sdr/CALA2025021002270.md): Girt Bar · fod · Feb 6, 2025 · N19141 · Boeing 757224 · Emergency Equipment
  > DOOR 1R VERY STICKY AND HARD TO DISARM AND ARM. INSPECTED R1 DOOR PER AMM 52-11-01. FOUND PAPER IN THE GRIT BAR REMOVED UNWANTED MATERIAL. OPERATIONAL CHECK GOOD ON DOOR DISARMING AND ARMING.
- [SDR CALA2025020402197](https://openairdocs.org/sdr/CALA2025020402197.md): Lanyard · out of position · Feb 2, 2025 · N19141 · Boeing 757224 · Escape Slide
  > 2L UNABLE TO ARM OR DISARM REMOVED OBSTRUCTION, SLIDE LANYARD, FROM GIRT BAR TRACK. ARMED AND REARMED DOOR 2L. FLIGHT CREW ARMED AND DISARMED DOOR 2L. NO COMPLAINTS. DOOR 2L ARMS AND DISARMS. NO DEFECTS NOTED.
- [SDR CALA2025012301995](https://openairdocs.org/sdr/CALA2025012301995.md): Girt Bar · fod · Jan 19, 2025 · N19141 · Boeing 757224 · Emergency Equipment
  > DOOR 1R WILL NOT ARM REMOVED DEBREE UNDER GIRT BAR AREA,ARM AND DISARM DOOR OPS CHECKS NORMAL,SUBTASK 25-66-01-094-102 ITEM 6 OK TO CONTINUE
- [SDR CALA2025010600028](https://openairdocs.org/sdr/CALA2025010600028.md): Charger · inoperative · Jan 3, 2025 · N19141 · Boeing 757224 · Emergency Lighting
  > DURING CABIN WALK AROUND FOUND EMERGENCY LIGHT INOP FROM SEAT ROW 32-41 REMOVED AND REPLACED BATTERY ASSY. IAW B757-200 AMM 33-51-07. OPERATIONAL CHECK GOOD.
- [SDR CALA2024100400753](https://openairdocs.org/sdr/CALA2024100400753.md): Probe · faulted · Oct 2, 2024 · N19141 · Boeing 757224 · Engine Indicating System
  > R ENG PROBE HEAT STATUS AFTER ENG START SUSPECT RT ENG PROBE M&E 19-7321-3-0002 MEL 3034B DISPATCH ADVISES THERE IS ICING NEAR BOS. ON DEFERRAL R&R ENG 2 P1 PROBE PER AMM TASK 73-21-04 AND OPS CHECKED GOOD AND PERFORMED IDLE RUN TO MAKE MSG DID NOT COME BACK
- [SDR CALA2024080100343](https://openairdocs.org/sdr/CALA2024080100343.md): Computer · faulty · Jul 30, 2024 · N19141 · Boeing 757224 · Weather Radar System
  > ACFT DIVERTED WITH MULTPLE GPWS RELATED FAULTS REMOVED AND REPLACED THE GPWS COMPUTER REF AMM 34-46-01 LOADED CURRENT TERRAIN DB VERSION 640 REF AMM 34-46-00 OPS CHECKS NORMAL.PARTS USED: 64-3446-9-0002,QTY:1 PARTS USED: 64-3446-9-0002,QTY:1 ROTABLE PARTS C
- [SDR CALA2024032700883](https://openairdocs.org/sdr/CALA2024032700883.md): Access Panel · missing · Mar 26, 2024 · N19141 · Boeing 757224 · Nacelle/Pylon, Plate/Skin
  > OIL FILLER DOOR MISSING UPON ARRIVAL. #1 ENGINE L/H OIL FILLER ACCESS PANEL. REPLACED MISSING OIL FILLER DOOR IN REFERENCE TO AMM 71-11-04-308-075-R00. AIPC REF 71-11-04-03.
- [SDR CALA2023122203709](https://openairdocs.org/sdr/CALA2023122203709.md): Cover · out of position · Dec 21, 2023 · N19141 · Boeing 757224 · Escape Slide
  > WHEN SQUIB TEST BUTTON PRESSED TO NUMBER "1" POSITION BOTH WING SLIDE LIGHTS DO NOT ILLUMINATE. UPON FURTHER INVESTIGATION FOUND L/H AND R/H OVERWING SLIDE ARMING PANELS IN WRONG POSITIONS. SWAPPED PANELS TO PROPER CONFIGURATION REF AMM 25-65-11. AS STATED IN
- [SDR CALA2023121803661](https://openairdocs.org/sdr/CALA2023121803661.md): Liner · incorrect · Dec 15, 2023 · N19141 · Boeing 757224 · Emergency Exits
  > LEFT OVERWING ARM/DISABLE HANDLE COVER FOUND TO BE IN CLOSE AND FLUSH POSTION WITH SLIDE DISARMED LEFT OVERWING DISABLE HANDLE COVER FOUND TO BE IN THE INCORRECT LINING INSTL-HATCHWAY LS REFERENCE: 52-22-02-25 ITEM 280 POSITION. DOOR HANDLE WILL NOT BE ABLE TO
- [SDR CALA2023071002213](https://openairdocs.org/sdr/CALA2023071002213.md): Unknown · unknown · Jul 7, 2023 · N19141 · Boeing 757200 · Fuselage Structure (General)
  > OPENED AMES WORK PACK N19141-2 FOR 8C + GEAR MAINTAINENCE CHECK.

Next page: https://openairdocs.org/aircraft/N19141/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 = 'N19141' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N19141/reports

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