# Service difficulty reports: N18112

A list on [N18112](https://openairdocs.org/aircraft/N18112.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 · 135 reports

- [SDR CALA2026101620436](https://openairdocs.org/sdr/CALA2026101620436.md): Access Panel · missing · Oct 10, 2026 · N18112 · Boeing 757224 · Engine Thrust Reverser
  > FOUND ACCESS PANEL MISSING ON LT OTBD THRUST REVERSER. REPLACED THE ACCESS PANEL ON LT OTBD THRUST REVERSER. REF IPC: 78-31-20-56 ITEM: 37.
- [SDR CALA2026101620435](https://openairdocs.org/sdr/CALA2026101620435.md): Access Panel · missing · Oct 10, 2026 · N18112 · Boeing 757224 · Engine Thrust Reverser
  > FOUND ACCESS PANEL MISSING ON LT OTBD THRUST REVERSER. REF IPC: 78-31-20-56 ITEM: 41 REPLACED ACCESS PANEL ON LT OTBD THRUST REVERSER. REF IPC: 78-31-20-56 ITEM: 41
- [SDR CALA2026092219652](https://openairdocs.org/sdr/CALA2026092219652.md): Tee Fitting · corroded · Sep 19, 2026 · N18112 · Boeing 757224 · Fuselage Miscellaneous Structure
  > RIGHT LOWER WING TO BODY FAIRING STRUCTURE TEE FITTING HAD CORROSION AT BS 900, RBL20. REMOVED CORROSION AND CHKD LIMITS ON RT LWR WING TO BODY TEE FITTING. FOUND OUT LIMITS. 50% MATERIAL LOSS, MAX ALLOWED 20 IAW SRM 53-00-71-1A-1. REPAIRED AREA IAW SRM 51-7
- [SDR CALA2026092219648](https://openairdocs.org/sdr/CALA2026092219648.md): Access Panel · cracked · Sep 18, 2026 · N18112 · Boeing 757224 · Wing, Plate/Skin
  > LEFT WING LOWER ACCESS PANEL 543BB HAD TWO CRACK INDICATIONS AT HOLE NR 16 AT 3 AND 4 O'CLOCK. FABRICATED, INSTALLED FREEZE PLUG AT HOLE NR 16 IAW EA 757-5720-A46 07 REV-STEP 14 VIA T26/1876291 COMPLIED WITH UAL EC/RA 5720-03682.
- [SDR CALA2026092119630](https://openairdocs.org/sdr/CALA2026092119630.md): Stiffener · corroded · Sep 18, 2026 · N18112 · Boeing 757224 · Wing Miscellaneous Structure
  > LEFT WING T/E CAVITY THROUGH ACCESS PANEL 561FB, AT UPPER PANEL AFT MOUNTING BRACKET HAS FOUR AREAS OF EXFOLIATION, REMOVED AND REPLACED THE STIFFENER. ON LT WING UPPER TRAILING EDGE WSTA 735.80 - 775.10 IAW SRM 51-40-02.
- [SDR CALA2026092119628](https://openairdocs.org/sdr/CALA2026092119628.md): Access Panel · cracked · Sep 18, 2026 · N18112 · Boeing 757224 · Wing, Plate/Skin
  > RIGHT WING LOWER ACCESS PANEL 643BB HAS CRACK INDICATION I N HOLE NR 15 AT 9 O'CLOCK. INSTALLED FREEZE PLUG AT HOLE NR 15 IAW EA 757-5720-13-AY608 REV-. VIA T26/1876294/ COMPLIED WITH ECRA 5720-03683.
- [SDR CALA2026092119620](https://openairdocs.org/sdr/CALA2026092119620.md): Bracket · corroded · Sep 18, 2026 · N18112 · Boeing 757224 · Aerodynamic Fairings
  > RIGHT LWR WING TO BODY FAIRING, BY THE RAM AIR INLET AT BS 880 RBL 20, ONE BRACKET CORRODED. THE BRACKET WAS REMOVED AND REPLACED AND LID WAS REMOVED AND REPLACED IAW DWG 149N7160, REV K IAW SRM 51-40-05-0G, AND SRM 51-40-05-0G.
- [SDR CALA2026092119611](https://openairdocs.org/sdr/CALA2026092119611.md): Failsafe · corroded · Sep 18, 2026 · N18112 · Boeing 757224 · Fuselage Main, Structure
  > AFT CARGO AFT BULKHEAD AT BS 1681 AND S28L TO S29L HAS EXFOLIATION. REMOVED AND REPLACED 146N1038-7 FAIL SAFE VIA T26/1876248 IAW SRM 51-40-02-0G.
- [SDR CALA2026092119590](https://openairdocs.org/sdr/CALA2026092119590.md): Access Panel · cracked · Sep 17, 2026 · N18112 · Boeing 757224 · Wing, Plate/Skin
  > LEFT WING LOWER ACCESS PANEL 543BB HAS CRACK INDICATION IN HOLE NR 18 AT 9 O'CLOCK. INSTALLED FREEZE PLUG IN HOLE NR 18 IAW EA 757-5720-13-A4607, STEP 14, REV-. COMPLI D WITH ECRA 5720-03682.
- [SDR CALA2026092119588](https://openairdocs.org/sdr/CALA2026092119588.md): Access Panel · cracked · Sep 17, 2026 · N18112 · Boeing 757224 · Wing, Plate/Skin
  > LEFT WING LOWER ACCESS PANEL 543BB HAS CRACK INDICATION IN HOLE NR 20 AT 8 O'CLOCK. INSTALLED FREEZE PLUG IN HOLE NR 20 IAW EA 757-5720-13-A4607, STEP 4, REV-. COMPLI D WITH ECRA 5720-03682-44-0008.
- [SDR CALA2026091819546](https://openairdocs.org/sdr/CALA2026091819546.md): Bracket · cracked · Sep 17, 2026 · N18112 · Boeing 757224 · Fuselage Main, Attach Fittings
  > RIGHT WW CUTOUT OTBD BRACKET THAT ATTACH PROXIMITY SENSOR OF THE MLG DOOR HAD ONE CRACK AND TWO GOUGES. REMOVED AND REPLACED RT WW PROXIMITY SENSORS BRACKET IAW SRM 51-40-02-OG.
- [SDR CALA2026091819544](https://openairdocs.org/sdr/CALA2026091819544.md): Channel · cracked · Sep 17, 2026 · N18112 · Boeing 757224 · Fuselage Miscellaneous Structure
  > LEFT MLG WW BULKHEAD BS 1180 CHANNEL SUPPORT, LBL 45 CRACKED. REMOVED THE CHANNEL ASSY IAW SRM 51-40-02, AND INSTALLED A NEW CHANNEL ASSY IAW SRM 5 1-40-02. APPLIED CIC IAW AMM 51-00-59.
- [SDR CALA2026092119586](https://openairdocs.org/sdr/CALA2026092119586.md): Access Panel · cracked · Sep 16, 2026 · N18112 · Boeing 757224 · Wing, Plate/Skin
  > RIGHT WING LOWER ACCESS PANEL 643BB HAS CRACK INDICATION IN HOLE NR 2 AT 5 O'CLOCK. INSTALLED FREEZE PLUG COMMON TO HOLE NR 2 AT RT WING LWR ACCESS PANEL 6 43BB, SKIN LOCATION IAW EA 757-5720-13-A4608, STEP 14. FABRICATION ACCOMPLISHED VIA T26/1876293 WC 61
- [SDR CALA2026092119584](https://openairdocs.org/sdr/CALA2026092119584.md): Access Panel · cracked · Sep 16, 2026 · N18112 · Boeing 757224 · Wing, Plate/Skin
  > RIGHT WING LOWER ACCESS PANEL 643BB HAS CRACK INDICATION IN HOLE NR 5 AT 7 O'CLOCK. INSTALLED FREEZE PLUG HOLE NR 5 IAW EA 757-5720-13-A4608, REV-, STEP 14. VIA T26/1876292. FABRICATION ACCOMPLISHED T26/1876292 ON WC 6100815272/18159. COMPLIED WITH ECRA 5720
- [SDR CALA2026092119582](https://openairdocs.org/sdr/CALA2026092119582.md): Access Panel · cracked · Sep 16, 2026 · N18112 · Boeing 757224 · Wing, Plate/Skin
  > RIGHT WING LOWER ACCESS PANEL 643BB HAS MULTIPLE CRACK INDICATIONS IN HOLE NR 19 AT 2 TO 3 O'CLOCK. INSTALLED FREEZE PLUG IN HOLE NR 19 IAW EA 757-5720-13-A4608 REV -, STEP 14. FABRICATION ACCOMPLISHED VIA T26/1876293 ON WC 6100815 272/18159. COMPLIED WITH EC
- [SDR CALA2026092119580](https://openairdocs.org/sdr/CALA2026092119580.md): Access Panel · cracked · Sep 16, 2026 · N18112 · Boeing 757224 · Wing, Plate/Skin
  > RIGHT WING LOWER ACCESS PANEL 643BB HAS CRACK INDICATION IN HOLE NR 27 AT 1 O'CLOCK. INSTALLED FREEZE PLUG AT HOLE NR 27 IAW EA 757-5720-13-A4608 REV - STEP 14, FABRICATION ACCOMPLISHED VIA T26/1876293 /6100815272/18 159. COMPLIED WITH ECRA 5720-03683.
- [SDR CALA2026092119576](https://openairdocs.org/sdr/CALA2026092119576.md): Access Panel · cracked · Sep 16, 2026 · N18112 · Boeing 757224 · Wing, Plate/Skin
  > LEFT WING LOWER ACCESS PANEL 543BB HAS CRACK INDICATION IN HOLE NR 27 AT 11 O'CLOCK. INSTALLED FREEZE PLUG AT HOLE 27 IAW EA 757-5720-13-A4607 STEP 14 VIA T26/1876291 PER WC 6100815268/18155. COMPLIED WITH ECRA 5720-03682.
- [SDR CALA2026092119574](https://openairdocs.org/sdr/CALA2026092119574.md): Access Panel · cracked · Sep 16, 2026 · N18112 · Boeing 757224 · Wing, Plate/Skin
  > LEFT WING LOWER ACCESS PANEL 543BB HAS 2EA CRACK INDICATIONS IN HOLE NR 28 AT 12 AND 2 O'CLOCK. INSTALLED FREEZE PLUG IN HOLE NR 28 IAW EA 757-5720-13-A4607 REV- STEP 14. FABRICATION ACCOMPLISHED VIA WC 6100815268 / 18155 & T26/ 187691. COMPLIED WITH ECRA UA
- [SDR CALA2026092119572](https://openairdocs.org/sdr/CALA2026092119572.md): Access Panel · cracked · Sep 16, 2026 · N18112 · Boeing 757224 · Wing, Plate/Skin
  > LEFT WING LOWER ACCESS PANEL 543BB HAS CRACK INDICATION IN HOLE NR 22 AT 12 O'CLOCK. INSTALLED FREEZE PLUG IN HOLE NR 22 IAW EA 757-5720-13-A4607, REV-, STEP 14. FABRICATION ACOMPLISHED VIA T26/1876291 WC 6100815268/18 155. COMPLIED WITH UAL ECRA 5720-0368
- [SDR CALA2026091719502](https://openairdocs.org/sdr/CALA2026091719502.md): Frame · dented · Sep 15, 2026 · N18112 · Boeing 757224 · Fuselage Main, Frame
  > AFT CARGO THROUGH SIDEWALL PANEL AT STA 1560, RT FRAME HAS A DENT, STR 25R - 26R. REPAIR ACCOMPISHED IAW ECRA 5360-02211 AND EA 757-5360-13-A4610, REV, EA 8110-3.
- [SDR CALA2026091619466](https://openairdocs.org/sdr/CALA2026091619466.md): Channel · corroded · Sep 13, 2026 · N18112 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF L2 MIDDLE SCUFF PLATE, FOUND BRACKET WITH CORROSION. R & R 3 EA CHANNEL TRAVELED #T26/1876249 BAT CH#0004324241 IAW B757-200 SRM 51-40-02-OG-0 AT L2 SOFT PLATE AR EA AND RESTORED CIC AT AREA IAW B757-200 AMM 51-24-03 SFR:4329 R EF:NR#18279
- [SDR CALA2026091519451](https://openairdocs.org/sdr/CALA2026091519451.md): Support Bracket · cracked · Sep 13, 2026 · N18112 · Boeing 757224 · Fuselage Miscellaneous Structure
  > LEFT MLG W/W, PRESS/CD FILTER MOD L SYS BRACKET SPRT IS CRACKED. DOT 23-004(). REF:NR#18074 ESFR INFORMATION ENTERED. REMOVED AND REPLACED 271N2062-9 FILTER NODULE BRACKET IAW B757 S RM 51-40-02-0G VIA T26/1876675. REF SFR 4328 AND NR 18074.
- [SDR CALA2026091519441](https://openairdocs.org/sdr/CALA2026091519441.md): Strap · corroded · Sep 12, 2026 · N18112 · Boeing 757224 · Fuselage Miscellaneous Structure
  > APU INLET DOOR EXT SURFACE FWD STRAP HAS EXFOLIATION. REMOVED AND REPLACED FWD STRAP ON BS 1787.45, S3-6R, APU INLET CUTOUT IAW SRM 51-40-00.
- [SDR CALA2026091519439](https://openairdocs.org/sdr/CALA2026091519439.md): Strap · corroded · Sep 12, 2026 · N18112 · Boeing 757224 · Fuselage Miscellaneous Structure
  > APU INLET CUT OUT AFT STRAP HAS CORROSION, BS 1825, S3 - 6R. ACCOMPLISHED REPAIR ON APU INLET CUTOUT AFT BS 1825, STR 3 - 6RM IAW SRM 53-80-15-2R-1, REPAIR 1.
- [SDR CALA2026091519437](https://openairdocs.org/sdr/CALA2026091519437.md): Retainer · cracked · Sep 12, 2026 · N18112 · Boeing 757224 · Fuselage Main, Structure
  > RIGHT W/W FWD CUT OUT SEAL RETAINER HAD TWO CRACKS. PANEL 198BR WAS REMOVED TO GAIN ACCESS IAW SRM 51 -40-02-OG, SUPPORT CHANNEL WAS REMOVED SRM 51-40-02-OG, REPLACED SUPPORT. CHANNEL IAW SRM 51-40-02, & INSTALLED NEW BRACKET IAW SRM 51-40-02, AND REINSTALL
- [SDR CALA2026091519435](https://openairdocs.org/sdr/CALA2026091519435.md): Angle · corroded · Sep 12, 2026 · N18112 · Boeing 757224 · Fuselage Miscellaneous Structure
  > APU INLET DOOR EXT SURFACE LWR STRAP HAS EXFOLLIATION. REMOVED AND REPLACED APU INLET DOOR EXT ANGLES IAW SRM 51-40-02-OG.
- [SDR CALA2026091519433](https://openairdocs.org/sdr/CALA2026091519433.md): Strap · corroded · Sep 12, 2026 · N18112 · Boeing 757224 · Fuselage Miscellaneous Structure
  > APU INLET CUT OUT UPPER STRAP HAS CORROSION, BS 1787-1825, STR 3R. DAMAGE ANGLES WERE REMOVED AND REPLACED IAW SRM 5 1-40-02-OG.
- [SDR CALA2026091019349](https://openairdocs.org/sdr/CALA2026091019349.md): Support Bracket · cracked · Sep 8, 2026 · N18112 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT CARGO SUPPORT BRACKET THAT ATTACH SIDEW ALL PANEL IN STA 1560 LH SIDE BEND. REMOVED FABRICATED AND REPLACED ONE EACH 453N1801-41 AFT C ARGO SIDEWALL SUPPORT BRACKET IAW B757-200 SRM 51-40-02-OG
- [SDR CALA2026090719265](https://openairdocs.org/sdr/CALA2026090719265.md): Bracket · cracked · Sep 4, 2026 · N18112 · Boeing 757224 · Fuselage Main, Attach Fittings
  > LEFT MLG WW, BS 1040, LBL 64.9 ANGLE BRACKET WAS CRACKED AT INBD SIDE. REMOVED AND INSTALLED A NEW ANGLE BRACKET IAW SRM 51-40-02-0G-0, APPLIED SURFACE PROTECTION IAW AMM 51-21-14-370-801 AND AMM 51-21-15-370-801.
- [SDR CALA2026090719262](https://openairdocs.org/sdr/CALA2026090719262.md): Bracket · cracked · Sep 4, 2026 · N18112 · Boeing 757224 · Fuselage Main, Attach Fittings
  > LEFT MLG WW BS 1040, BY OTBD SIDE OF LBL 64.9, ANGLE BRACKET IS CRACKED. REMOVED AND INSTALLED NEW ANGLE BRACKET, IAW SRM 51-40-02-0G-0 DWG 149N7553, APPLIED SURFACE PROTECTION IAW AMM 51-21-14-370-801 AND AMM 51-21-15-370-801.
- [SDR CALA2026090719260](https://openairdocs.org/sdr/CALA2026090719260.md): Door Frame · cracked · Sep 4, 2026 · N18112 · Boeing 757224 · Fuselage Main, Structure
  > NLG WHEEL WELL. DOOR CUTOUT RT SIDE AT BS 275 HAS ONE GUSSET REINFORCEMENT PLATE IS BENT. REMOVED AND REPLACED FOR NEW GUSSET REINFORCEMENT PLATE IAW SRM 51-40-02-0G-0.
- [SDR CALA2026090719258](https://openairdocs.org/sdr/CALA2026090719258.md): Gusset · cracked · Sep 4, 2026 · N18112 · Boeing 757224 · Fuselage Main, Structure
  > NLG WHEEL WELL. DOOR CUTOUT R.H SIDE AT BS 324 HAS 2EA GUS SET REINFORCEMENT PLATES CRACKED. REMOVED AND REPLACED 02EA GUSSETS REINFORCEMENT WITH NEW GUSSETS IAW SRM 51-40-02-0G.
- [SDR CALA2026090419246](https://openairdocs.org/sdr/CALA2026090419246.md): Support Bracket · corroded · Sep 2, 2026 · N18112 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT CARGO SUPPORT BRACKET THAT ATTACH SIDEWALL PANEL IN LT SIDE FRAME 1360 WITH CORROSION. REMOVED AND REPLACED SUPPORT BRACKET THAT ATTACHED SIDEWALL PANE L, AT AFT CARGO IN LT SIDE FRAME BS 1360 IAW SRM 51-40-02-OG-0.
- [SDR CALA2026090419244](https://openairdocs.org/sdr/CALA2026090419244.md): Support Bracket · cracked · Sep 2, 2026 · N18112 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT CARGO LT SIDE SUPPORT BRACKET THAT ATTACH SIDEWALL PANEL IN STA 1200 WITH DENTS AND CRACKED. REMOVED AND REPLACED SUPPORT SIDEWALL PANEL BS 1200 2/H FOR CRACK IAW SRM 51-40-02-0G-0 T26 / 1875858, TREATED PR IMED SRM 51-00-59.
- [SDR CALA2026090319206](https://openairdocs.org/sdr/CALA2026090319206.md): Strap · cracked · Sep 2, 2026 · N18112 · Boeing 757224 · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE, BTWN BS 365.25 & BS 377.7, LBL 24.75, FLOOR STRAP CRACKED. CUTOUT DAMAGE, FATRICATED NR 1 STRAP, 1 FILLER, & INSTALLED THE STRAP & FILLER IAW SRM 53-00- 51-2R-12, PAGE 2, DETAIL IV.
- [SDR CALA2026032314734](https://openairdocs.org/sdr/CALA2026032314734.md): Unknown · odor · Mar 19, 2026 · N18112 · Boeing 757224 · Buffet/Galleys
  > STRONG ACRID ODOR WHEN USING AFT GALLEY OVEN NR 2. OPS AFT GALLEY MIDDLE OVEN FOR 10 MINUTES IAW AMM 25-34-00. NO ODORS OR DEFECTS NOTED. OK FOR SERVICE.
- [SDR CALA2026013013442](https://openairdocs.org/sdr/CALA2026013013442.md): Unknown · odor · Jan 29, 2026 · N18112 · Boeing 757224 · Air Distribution System
  > ODOR OF FUEL AND RUBBER BURNING BEFORE AND AFTER ENGINE START, CONFIGURED AIRCRAFT FOR FLIGHT, CONFIGURATION WITH ALL DOORS CLOSED, ALL PUMPS ON FOR OVER 30MIN, NO ABNORMAL ODORS NOTED, PERFORMED OUTSIDE VISUAL INSPECTION, NO FAULTS NOTED. COULD NOT DUPLICAT
- [SDR CALA2025111111136](https://openairdocs.org/sdr/CALA2025111111136.md): None · no discrepancy · Nov 10, 2025 · N18112 · Boeing 757224 · Standard Practices/Structures
  > FWD CABIN CALL LIGHT ON OVERHEAD PANEL NOT LIGHTING UP WHEN CALLED, ALSO NO EICAS CABIN CALL RESET FLIGHT ATTENDANCE PHONE L1 DOOR LIGHT, AND EICAS MESSAGE IN FLIGHT DECK OPERATE CORRECTLY IAW AMM 23-19-00N
- [SDR CALA2025100309578](https://openairdocs.org/sdr/CALA2025100309578.md): None · none · Oct 2, 2025 · N18112 · Boeing 757224 · Standard Practices/Structures
  > RIGHT OVERWING SLIDE DEACTIVATED AND PANELS OPENED. IAW AMM - 25-65-00-002-001. RIGHT OVERWING SLIDE REACTIVATED AND CLOSED PANELS. ARMED RT OVER WING SLIDE REF AMM 25-65-00. VERIFIED RH OVER WING SLIDE REACTIVATED AND ARMED PER RII REQUIREMENTS
- [SDR CALA2025061605558](https://openairdocs.org/sdr/CALA2025061605558.md): Door · faulted · Jun 14, 2025 · N18112 · Boeing 757224 · Fixed Inner Doors
  > FLIGHT DECK DOOR WILL NOT STAY CLOSED ROBBED DAMAGED PIN BUSHING FROM AIRCRAFT 139. INSTALLED PER AMM 52-52-01. OPS CHECK GOOD
- [SDR CALA2025052805032](https://openairdocs.org/sdr/CALA2025052805032.md): Stringer · corroded · May 27, 2025 · N18112 · Boeing 757224 · Fuselage Main, Longeron/Stringer
  > ABB; STRINGER S26R CORRODED UNDER RIGHT TRANSITION PANEL AT STA. 1615. REPAIRED AFT CARGO COMP STRINGER STA 1600-1620 AT S26R REF ECRA 5360-01958. ISSUED DIP FOR PART 2 INSPECTION REQUIREMENTS L/P 4988313. VERIFIED AFT CARGO COMP STRINGER STA 1600-1620 AT S26
- [SDR CALA2025052704982](https://openairdocs.org/sdr/CALA2025052704982.md): Strap · damaged · May 17, 2025 · N18112 · Boeing 757224 · Passenger/Crew Doors
  > RII INSPECTION REQUIRED DOUBLER PREVENTATIVE MOD TO THE L1 DOOR SURROUND FWD UPPER CORNE R WAS INSTALLED PER EA 5330-04213 REV D WITH DEVIATIONS NOTED IN ECRA 5330-07534. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF ECRA 5330-07534 AT FUSELAGE REINFORCED
- [SDR CALA2025051504693](https://openairdocs.org/sdr/CALA2025051504693.md): Floor Support · corroded · May 14, 2025 · N18112 · Boeing 757224 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR L/H SIDE BETWEEN STA. 1020 TO 1040, S-17, O/B ANGLE UNDER FLOOR BOARD 241FFA HAS CORROSION. FABRICATED AND REPLACED INNER CHORD STA 1020-1040 AT S17 LT.REF DWG 144N5152 AND DWG 144N5140.
- [SDR CALA2025041003676](https://openairdocs.org/sdr/CALA2025041003676.md): Girt Bar · unpacked · Apr 7, 2025 · N18112 · Boeing 757224 · Emergency Equipment
  > DOOR 4R WILL NOT ARM FOUND GIRT MATERIAL UNPACKED AROUND GIRT BAR. REPACKED MATERIAL IN SLIDE. OK TO CONTINUE. DOOR ARMS/DISARMS.
- [SDR CALA2025032603200](https://openairdocs.org/sdr/CALA2025032603200.md): Slide · unknown · Mar 25, 2025 · N18112 · Boeing 757224 · Escape Slide
  > REMOVE ESCAPE SLIDE PREPARE FOR REMOVAL - INSTALLED R4 DOOR ESCAPE SLIDE SAFETY PIN. REMOVED AND STOWED R4 DOOR ESCAPE SLIDE SAFETY PIN. C.W IDT INSP REQUIREMENTS REF GMM 09-10-05
- [SDR CALA2025032503167](https://openairdocs.org/sdr/CALA2025032503167.md): Warning Message · false activation · Mar 24, 2025 · N18112 · Boeing 757224 · Door Warning System
  > RIGHT WING SLIDE EICAS MSG ON FINAL APP ON ARRIVAL HAD NO MSG SHOWN BUT HAD INTERMITTENT S10374 FAULT, NO PREVIOUS HISTORY, PERFORMED PSEU TARGET TEST, TEST PASSED. AND NOMORE FAULT ON PSEU.
- [SDR CALA2025032403122](https://openairdocs.org/sdr/CALA2025032403122.md): Girt Bar · iced · Mar 21, 2025 · N18112 · Boeing 757224 · Emergency Equipment
  > DOOR 1L UNABLE TO DISARM. FOUND ICE IN GIRT BAR AREA, CLEANED AND LUBED GIRT AREA, SLIDE ARMS AND DISARMS FREELY. SLIDE ARMING AND DISARMING NORMAL AS PER AMM. 25-66-00 / 201.
- [SDR CALA2025032003017](https://openairdocs.org/sdr/CALA2025032003017.md): Proximity Sensor · faulted · Mar 16, 2025 · N18112 · Boeing 757224 · Emergency Equipment
  > LVL1 CHRONIC HIST OF DOOR 4L ARM LIGHT INTERMITTENT STAY ON W/ D OOR DISARMED. CYCLED HANDLE & CLEARED DEBRIS CHK GOOD BUT ISSUE REPEAT. WHEN WORKING W/ DOOR ARM/DISARM SYS, PLS REF SLIDE SAFET Y CHKLIST TO PREVENT OF SLIDE DEPLOYMENT. DUE TO REPEAT ISSUE, T E
- [SDR CALA2025012301996](https://openairdocs.org/sdr/CALA2025012301996.md): Indicator · malfunctioned · Jan 19, 2025 · N18112 · Boeing 757224 · Door Warning System
  > 4L DISARM LT WILL NOT GO OUT FOUND SLIDE LIGHT EXTINGUISHED ON INITAIL DOO INSPECTION. ARMED AND DISARMED DOOR MULTIPLE TIMES AND SLLIDE LIGHT OPERATED NORMALLY. DOOR DISARMED AND ARMED NORMALLY ALSO. COULD NOT DUPLICATE AND DOOR ARMING DISARMING CHECK NORM
- [SDR CALA2024121901582](https://openairdocs.org/sdr/CALA2024121901582.md): Door · no discrepancy · Dec 16, 2024 · N18112 · Boeing 757224 · Passenger/Crew Doors
  > 4R WILL NOT DISARM OPS CHECKED 4R DOOR, ARMED & DISARMED NORMALY VERIFIED NORMAL INDICATIONS. PER AMM TASK 52-11-00. OK FOR SERVICE

Next page: https://openairdocs.org/aircraft/N18112/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 = 'N18112' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N18112/reports

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