# Service difficulty reports: N18243

A list on [N18243](https://openairdocs.org/aircraft/N18243.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 · 121 reports

- [SDR CALA2026012813401](https://openairdocs.org/sdr/CALA2026012813401.md): Unknown · odor · Jan 25, 2026 · N18243 · Boeing 737824 · Air Distribution System
  > BURNING RUBBER ODOR REPORTED BY FA IN THE AFT OF THE ACFT. OPERATED ALL OVENS AND COFFEEMAKERS IN AFT GALLEY; NO ODORS DETECTED IAW AMM 05-51-26.
- [SDR CALA2026011312922](https://openairdocs.org/sdr/CALA2026011312922.md): Seal · missing · Jan 12, 2026 · N18243 · Boeing 737824 · Trailing Edge Flaps
  > FOUND LOWER INBD FLAP BULB SEAL MISSING. REPLACED THE BULB SEAL WITH NEW IAW IPC 27-51-11-01.
- [SDR CALA2025111211159](https://openairdocs.org/sdr/CALA2025111211159.md): Angle · cracked · Nov 8, 2025 · N18243 · Boeing 737824 · Fuselage Miscellaneous Structure
  > L1 DOOR CUTOUT FWD UPPER ANGLE REVEAL CRACKED. REMOVED AND REPLACED THE ANGLE REVEAL IAW SRM 51-40-02-0G-0, & DWG 141A8220.
- [SDR CALA2025110610948](https://openairdocs.org/sdr/CALA2025110610948.md): Skin · cracked · Oct 29, 2025 · N18243 · Boeing 737824 · Leading Edge Devices
  > RIGHT WING LEADING EDGE SLAT NR 5 LOWER SKIN CRACKED AT ACTUATOR FASTENER HOLE. ACCOMPLISHED REPAIR AT RT WING L/E SLAT NR 5 LOWER SKIN, DOUBLER REPAIR IAW SRM 57-42-01-2R-8, STEP 4.H.
- [SDR CALA2025103110779](https://openairdocs.org/sdr/CALA2025103110779.md): Skin · cracked · Oct 29, 2025 · N18243 · Boeing 737824 · Leading Edge Devices
  > LEFT WING LEADING EDGE NR 2 SLAT LOWER SURFACE CRACKED AT ACTUATOR ATTACH POINT. COMPLETED INSTALLATION OF REPAIR PARTS, DOUBLER AND FILLER IAW SRM 57-42-01-2R8, FIG 202, SHEET 2.
- [SDR CALA2025112811576](https://openairdocs.org/sdr/CALA2025112811576.md): Vapor Barrier · cracked · Oct 28, 2025 · N18243 · Boeing 737824 · Fuselage Main, Bulkhead
  > LH VAPOR BARRIER BETWEEN LBL 5" - 14" SEVERAL AREA CRACKED. PERFORMED STOP HOLES AT CRACK ENDS ON LT VAPOR BARRIER CRACKS PER SRM 51-10-02-0G-0, CLEANED AREA PER SOPM 20-30-03 & ACCOMPLISHED FIBERGLASS REPAIR PATCH PER SRM 51-10-02-0G-0.
- [SDR CALA2025102910708](https://openairdocs.org/sdr/CALA2025102910708.md): Stringer · corroded · Oct 27, 2025 · N18243 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY VACUUM WASTE COMPARTMENT BS 867, STRINGER 24L HAD CORROSION. REMOVED AND REPLACED AFT CARGO BAY VACUUM WASTE COMPARTMENT STRINGER FROM BS 867 - 887 IAW SRM 51-40-02-0G-0 AND DWG 146A3230.
- [SDR CALA2025102910702](https://openairdocs.org/sdr/CALA2025102910702.md): Stringer · cracked · Oct 24, 2025 · N18243 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER 27R, BS 540, AFT OF FWD CARGO. ACCOMPLISHED INSTALLATION OF ALL REPAIR PART AND COMMON TO REPAIR AT STR 27, BS 540 AFT OF FWD CARGO IAW SRM 51-40-02 AND ECRA 5330-07630
- [SDR CALA2025102810641](https://openairdocs.org/sdr/CALA2025102810641.md): Channel · corroded · Oct 24, 2025 · N18243 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FOUND CORROSION FWD CARGO COMPARTMENTFLOOR SUPPORT Z CHANNEL S-26L STA 500AD TO 500I. INSTALLED FWD CARGO NEW Z CHANNEL S-26L STA 500A+10" TO 500I IAW B737 SRM 51-40-02 AND DGW 143A7500 & 143A7505. REMOVED AND REPLACED FWD CARGO Z CHANNEL S-26L STA 500A+10"
- [SDR CALA2025102710600](https://openairdocs.org/sdr/CALA2025102710600.md): Seat Track · worn · Oct 24, 2025 · N18243 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND WEAR MARKS MAIN CABIN SEAT TRACK UPPER CROWN EDGES L/H I/B STA 520 LBL 24.75. INSTALLED REPAIR PARTS BETWEEN STA 520 TO STA 500H & LBL 24.75" REF SRM 53-00-52-2R-4. ACCOMPLISHED INSTALLATION OF REPAIR PARTS BETWEEN STA 520 TO STA 500H & LBL 24.75" R
- [SDR CALA2025102710592](https://openairdocs.org/sdr/CALA2025102710592.md): Skin · corroded · Oct 24, 2025 · N18243 · Boeing 737824 · Service Doors
  > FOUND CORROSION R-1 DOOR ASSY LOWER GATE EXTERNAL SKIN AREAS WITH CORROSION. REMOVED AND REPLACED R1 DOOR LOWER GATE ASSEMBLY REF. SRM 51-40-02-0G-0 AND DWG 141A6516.
- [SDR CALA2025102710568](https://openairdocs.org/sdr/CALA2025102710568.md): Skin · corroded · Oct 22, 2025 · N18243 · Boeing 737824 · Service Doors
  > FOUND CORROSION R-1 DOOR ASSY UPPER GATE EXTERNAL SKIN AREAS WITH CORROSION. REMOVED AND REPLACED R1 DOOR UPPER GATE ASSEMBLY REF SRM 51-40-02-0G-0 AND DWG 141A6516.
- [SDR CALA2025102310434](https://openairdocs.org/sdr/CALA2025102310434.md): Pan · corroded · Oct 21, 2025 · N18243 · Boeing 737824 · Fuselage Main, Structure
  > LOWER FUSELAGE POTABLE WATER SERVICE DOOR CUTOUT INSIDE CORROSION IN SEVERAL AREA. REMOVED AND INSTALLED NEW DOUBLER AND PORTABLE WATER SERVICE PAN AT AFT CARGO IAW SRM 51-40-02-0G-0, DWG 147A7221 AND DWG 147A722.
- [SDR CALA2025102410493](https://openairdocs.org/sdr/CALA2025102410493.md): Web · corroded · Oct 20, 2025 · N18243 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT. CARGO DOOR THRESHOLD WEB HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO DOOR THRESHOLD WEB REF B-737 SRM 51-40-02-0G-0 AND DWG 146A8120.
- [SDR CALA2025102310432](https://openairdocs.org/sdr/CALA2025102310432.md): Support Angle · cracked · Oct 20, 2025 · N18243 · Boeing 737824 · Fuselage Miscellaneous Structure
  > LEFT VAPOR BARRIER SUPPORT SIDE ANGLE CRACKED AT BS 663, LBL 5. REMOVED AND REPLACED STIFFENER AT LT VAPOR BARRIER AT BS 663, LBL 5 IAW SRM 51-40-02-0G-0 AND DWG 144A7100.
- [SDR CALA2025102910698](https://openairdocs.org/sdr/CALA2025102910698.md): Fitting · corroded · Oct 17, 2025 · N18243 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO VACUUM WASTE COMPT DUMP CHUTE HOUSING TWO AREA CORROSION. COMPLETED INSTALLATION HOUSING FITTING AT AFT CARGO COMPT DUMP IAW SRM 51-40-02-0G-0, AND DWG 146A7400.
- [SDR CALA2025102310430](https://openairdocs.org/sdr/CALA2025102310430.md): Intercostal · cracked · Oct 17, 2025 · N18243 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN FWD WET AREA INTERCOSTAL UPPER ANGLE CRACKED AT LBL 10" BETWEEN STA 380-400. INSTALLED NEW MAIN CABIN FWD WET AREA INTERCOSTAL UPPER ANGLE AT LBL 10" BETWEEN BS 380-400 IAW SRM 51-40-02-0G-0 & DWG 143A5400,
- [SDR CALA2025112811575](https://openairdocs.org/sdr/CALA2025112811575.md): Skin · corroded · Oct 16, 2025 · N18243 · Boeing 737824 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN EXTERNAL STA 540 BL 0" BULGE EVIDENCE OF CORROSION. ACCOMPLISHED REPAIR AT LOWER FUSELAGE SKIN PANEL STA 500H TO 540 BETWEEN STR 27L TO STR 27R IAW ECRA 5330-07635.
- [SDR CALA2025101610181](https://openairdocs.org/sdr/CALA2025101610181.md): Angle · worn · Oct 15, 2025 · N18243 · Boeing 737824 · Vertical Stabilizer Miscellaneous Structure
  > LOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323BR SUPPORT ANGLE SEVERAL AREA WORN. REMOVED AND REPLACED LOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323BR SUPPORT AFT ANGLE REF SRM 51-40-02-0G-0 AND DWG 148A8300.
- [SDR CALA2025101610180](https://openairdocs.org/sdr/CALA2025101610180.md): Angle · worn · Oct 15, 2025 · N18243 · Boeing 737824 · Vertical Stabilizer Miscellaneous Structure
  > LOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323BL SUPPORT ANGLE SEVERAL AREA WORN. REMOVED AND REPLACED LOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323BL SUPPORT AFT ANGLE REF B-737 SRM 51-40-02-0G-0 AND DWG 148A8300.
- [SDR CALA2025101610179](https://openairdocs.org/sdr/CALA2025101610179.md): Angle · worn · Oct 15, 2025 · N18243 · Boeing 737824 · Vertical Stabilizer Miscellaneous Structure
  > LOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323AR SUPPORT ANGLE SEVERAL AREA WORN. REMOVED AND REPLACED LOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323AR SUPPORT FWD ANGLE IAW SRM 51-40-02-0G-0 AND DWG 147A0030.
- [SDR CALA2025101610178](https://openairdocs.org/sdr/CALA2025101610178.md): Angle · cracked · Oct 15, 2025 · N18243 · Boeing 737824 · Vertical Stabilizer Miscellaneous Structure
  > LOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323AL SUPPORT ANGLE CRACKED REF AAR N/R 99954672 REMOVED AND REPLACED LOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323AL SUPPORT FWD ANGLE REF B-737 SRM 51-40-02-0G-0 AND DWG 147A0030. REMOV
- [SDR CALA2025102610544](https://openairdocs.org/sdr/CALA2025102610544.md): Floor Support · corroded · Oct 14, 2025 · N18243 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AFT WET AREA BELOW CABIN FLOOR S-21L UPPER FLAGE STA 947+10". INSTALLED REPAIR ANGLE ON STRNGER S-21L & STA 947+10" AT MAIN CABIN AFT WET AREA REF 53-00-03-2R-1, FIGURE 201.
- [SDR CALA2025101710223](https://openairdocs.org/sdr/CALA2025101710223.md): Door Frame · cracked · Oct 14, 2025 · N18243 · Boeing 737824 · Fuselage Main, Structure
  > UPON REMOVAL OF R1 DOOR INNER CHORD FOUND FWD STUB FRAME LOWER CORNER CRACKED BS 296, WL 210. COMPLETED INSTALLATION OF FWD LOWER STUB FRAME IAW SRM 51-40-02-0G-0, AND DWG 141A8370.
- [SDR CALA2025102910694](https://openairdocs.org/sdr/CALA2025102910694.md): Structure · corroded · Oct 12, 2025 · N18243 · Boeing 737824 · Passenger/Crew Doors
  > L1 DOOR INNER CHORD BS 312 IS CRACKED. REMOVED AND REPLACED INNER CHORD AT L1 DOOR IAW SRM 51-40-02 AND DWG 141A8110.
- [SDR CALA2025101410069](https://openairdocs.org/sdr/CALA2025101410069.md): Structure · corroded · Oct 12, 2025 · N18243 · Boeing 737824 · Service Doors
  > R1 DOOR INNER CHORD HAS CORROSION AT STA 328-2". REMOVED AND REPLACED INNER CHORD AT R1 DOOR IAW SRM 51-40-02 AND DWG #141A8310
- [SDR CALA2025101410068](https://openairdocs.org/sdr/CALA2025101410068.md): Floorbeam · corroded · Oct 12, 2025 · N18243 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN CABIN AFT WET AREA CORROSION AT FLOORBEAM STA 947.5 LBL 53". ACCOMPLISHED REPAIR AT LT AFT WET AREA FLOORBEAM 947.5" LBL 53" PER B737-800 SRM 53-70-51-2R-5 AND SRM 51-40-02-0G-0
- [SDR CALA2025101410056](https://openairdocs.org/sdr/CALA2025101410056.md): Floorbeam · corroded · Oct 7, 2025 · N18243 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN CABIN AFT WET AREA CORROSION AT FLOORBEAM AROUND FITTING STA 947.5 RBL 52" (REF AAR N/R 99954162) ACCOMPLISHED REPAIR AND INSTALLED REPAIR PARTS AT MAIN CABIN AFT WET AREA FLOORBEAM BS 947.5" RBL 34" TO RBL 60" PER SRM 53-70-51-2R-5 AND ECRA 5370-01201.
- [SDR CALA2025100909838](https://openairdocs.org/sdr/CALA2025100909838.md): Floor Support · corroded · Oct 5, 2025 · N18243 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA, FOUND CORROSION AT FLOOR SUPPORT BS 947.5 +2", LBL 51. INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND 147A5650.
- [SDR CALA2025100809793](https://openairdocs.org/sdr/CALA2025100809793.md): Floorbeam · corroded · Oct 5, 2025 · N18243 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN CABIN AFT WET AREA CORROSION AT FLOOR BEAM PREVIOUS REPAIRSTA 986.5 RBL 45"-LBL 45". REMOVED AND INSTALLED REPAIR PARTS (T-CHORD -1, ANGLES -2, ANGLES -3, STRAP -4) AT STA 986.5 FROM LBL 51 TO RBL 51 IAW SRM 53-70-51-2R-4.
- [SDR CALA2025100609658](https://openairdocs.org/sdr/CALA2025100609658.md): Floor Support · corroded · Oct 4, 2025 · N18243 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FLOOR STRUCTURE PANEL SUPPORT AT STA 312-4" RBL12" IS CORRODED AT BOLT HOLE. REMOVED AND INSTALLED NEW FLOOR PANEL SUPPORT AT STA 312-4" RBL 12" PER SRM 51-40-02-0G-0 AND DWG 141A5410
- [SDR CALA2025100609650](https://openairdocs.org/sdr/CALA2025100609650.md): Floor Support · corroded · Oct 3, 2025 · N18243 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA CORROSION AT FLOOR SUPPORT STA 986.5+7" RBL 38". INSTALLED FLOOR SUPPORT AT AFT WET AREA STA 986.5 +7 RBL 38" IAW SRM 51-40-02-0G-0 AND DWG 147A5700.
- [SDR CALA2025100609649](https://openairdocs.org/sdr/CALA2025100609649.md): Web · corroded · Oct 3, 2025 · N18243 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA CORROSION AT FLOOR WEB STA 986.5+2" LBL 34". REMOVED AND REPLACED WEB AT LT AFT WET AREA BETWEEN STA 986.5" TO STA 1016" PER B737-800 SRM 51-40-02-0G-0 AND DWG 147A8501 AND DWG 147A5700.
- [SDR CALA2025100109498](https://openairdocs.org/sdr/CALA2025100109498.md): Floor Support · corroded · Sep 29, 2025 · N18243 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA, CORROSION ON FLOOR SUPPORT BS 986.5+5, LBL 33. EVALUATED AREA. FOUND CORRSION OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SEM 51-40-02-0G-0 AND DWG 147A5700.
- [SDR CALA2025100109496](https://openairdocs.org/sdr/CALA2025100109496.md): Floor Support · corroded · Sep 29, 2025 · N18243 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA CORROSION AT FLOOR SUPPORT, BS 1016, RBL 33. EVALUATED AREA, FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 147A5700.
- [SDR CALA2025080707420](https://openairdocs.org/sdr/CALA2025080707420.md): Collar · loose · Aug 6, 2025 · N18243 · Boeing 737824 · Emergency Equipment
  > DOOR 2R GIRT BAR COLLAR IS LOOSE. DOOR 2R SLIDE GIRT BAR STOP RELEASE DAMAGED. REPLACED GIRT BAR QUICK RELEASE STOP PER IPC 25-66-00-08 ITEM 400, AND OPERATED GIRT BAR.
- [SDR CALA2025073107124](https://openairdocs.org/sdr/CALA2025073107124.md): Slide · no discrepancy · Jul 29, 2025 · N18243 · Boeing 737824 · Escape Slide
  > L1 DOOR SLIDE HAS THE CHAIN CONNECTION HANGING LOOSE IN THE MIDDLE WHEN GIRT BAR IS ARMED. C/O AMM TASK 03-25-66-200-801, ESCAPE SLIDE - GENERAL VISUAL INSPECTION. FOUND NO FAULTS. AIRCRAFT OKAY FOR SERVICE.
- [SDR CALA2025063006050](https://openairdocs.org/sdr/CALA2025063006050.md): Skirt · out of position · Jun 27, 2025 · N18243 · Boeing 737824 · Escape Slide
  > SLIDE MATERIAL DOOR 1R PROTRUDING OUT BOTTOM OF SLIDE HOUSING REPOSITIONED SKIRT. REF AMM 25-66-01-401. OK FOR SERVICE. ABOVE ITEM IS RII ITEM. VERIFIED R1 DOOR SLIDE INSTALLATION PER REF AMM 25-66-01-401. L/P CLEARED
- [SDR CALA2025041603895](https://openairdocs.org/sdr/CALA2025041603895.md): Girt Bar · unsecure · Apr 14, 2025 · N18243 · Boeing 737824 · Emergency Equipment
  > MATERIAL ON GIRT BAR TOUCHING FLOOR TUCKED THE GIRT MATERIAL IN SLIDE PACK R1 REF AMM 25-66-01-400-803; OK TO USE.
- [SDR CALA2025040303475](https://openairdocs.org/sdr/CALA2025040303475.md): Girt Bar · undamaged · Mar 31, 2025 · N18243 · Boeing 737824 · Emergency Equipment
  > DOOR 1R SLIDE HAS EXCESS MATERIAL HANGING DOWN REF TASK 25-66-01-400-803 FOR CHECKING GIRT BAR Z-FOLD MATERIAL LENGTH, FOUND WITH IN LIMITS
- [SDR CALA2025031702871](https://openairdocs.org/sdr/CALA2025031702871.md): Light · no test · Mar 16, 2025 · N18243 · Boeing 737824 · Emergency Lighting
  > WHITE FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 15C INOP REMOVED AND REPLACED WHITE FLOOR PROXIMITY EMERGENCY LT ASSY AT SEAT 15C. OPS CHK NORMAL. REF. AMM 33-51-11. REMOVED AND REPLACED WHITE FLOOR PROXIMITY EMERGENCY LT ASSY AT SEAT 15C. OPS CHK NORMAL. REF. A
- [SDR CALA2025030302534](https://openairdocs.org/sdr/CALA2025030302534.md): Indication Sys · false activation · Feb 28, 2025 · N18243 · Boeing 737824 · Landing Gear Position and Warning
  > PER FLIGHT CREW, DURING APPROACH, FLAPS 15, OBSERVED GEAR INDICATION DISAGREEMENT. GEAR INDICATION SHOWED 3 RED AND 3 GREEN ON P-2 CENTER PANEL. OVERHEAD P-5 INDICATION DISPLAYED 3 GREEN. PILOT FLEW SECOND APPROACH WITH SAME INDICATIONS. PILOT REPORTED HE CYCL
- [SDR CALA2024121601523](https://openairdocs.org/sdr/CALA2024121601523.md): Wire · damaged · Dec 12, 2024 · N18243 · Boeing 737824 · Light System Wiring
  > EMERGENCY EXIT LIGHTS ON CLOSET DOOR IN FWD GALLEY INOP. DISCONNECTED AND RECONNECTED WIRE SPLICE, FWD MONUMENT LIGHT NOW OPS CHECKS GOOD OK TO CONTINUE. REF AMM 33-51-14 DISCONNECTED AND RECONNECTED WIRE SPLICE, FWD MONUMENT LIGHT NOW OPS CHECKS GOOD OK TO
- [SDR CALA2024090902400](https://openairdocs.org/sdr/CALA2024090902400.md): Fuse · failed · Sep 8, 2024 · N18243 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK FAILS TEST SUPPORT TASK NSA EMX NR 00258. REMOVED AND REPLACE FUSE F2 AND F3 ON M1694 BATTERY CHARGER AND PERFORMED EMERGENCY LIGHTS OPERATIONAL CHECK IAW B737NG AMM 33-51-00. OPS CHECK GOOD.
- [SDR CALA2024090902399](https://openairdocs.org/sdr/CALA2024090902399.md): Wire Harness · missing · Sep 8, 2024 · N18243 · Boeing 737824 · Light System Wiring
  > EPL AISLE LIGHT HARNESS AT SEAT ROW 7ABC TO 14ABC MISSING ALL BUT ONE CONNECTION. SUPPORT TASK NSA EMX NR 00217 INSTALLED EEPL AISLE LIGHT HARNESS AND PERFORMED EMERGENCY LIGHTS OPERATIONAL CHECK IAW B737NG AMM 33-51-00. OPS CHECK GOOD.
- [SDR CALA2024090902401](https://openairdocs.org/sdr/CALA2024090902401.md): Skin · cracked · Aug 10, 2024 · N18243 · Boeing 737824 · Wing, Plate/Skin
  > L/H LOWER WING SKIN BETWEEN RIBS 19-20 AND STRNG 9 END FASTNER HAS CRACK IN SKIN. SUPPORT TASK NSA EMX N/R00090.
- [SDR CALA2024072300270](https://openairdocs.org/sdr/CALA2024072300270.md): Control Valve · faulty · Jul 15, 2024 · N18243 · Boeing 737824 · Cabin Cooling System
  > PRESSURIZATION CANNOT KEEP THE CORRECT CABIN PRESSURE AC DID NOT PRESSURIZE MANUAL MODE DID NOT CONTROL OUTFLOW VALVELOG PAGE LOCKED BY TOMC. BITE TEST OF DCPC 1 & 2 PER FIM TASK 21-31 TASK 801. DCPC 1 & 2 FAULT HISTORY RECORDED ON FLIGHT LEG OO, FAULT CODE 00
- [SDR CALA2024071602049](https://openairdocs.org/sdr/CALA2024071602049.md): Flex Line · leaking · Jul 13, 2024 · N18243 · Boeing 737824 · Engine Bleed Air System
  > LEFT BLEED TRIP OFF LIGHT ILLUMINATED, CREW TRIED RESET, NO JOY. TO PRSOV, REF IPC 36-11-51-02A, ITEM #30. NEEDS ENGINE RUN ABOVE BLEED SHIFT TO CONFIRM FIX, TEST #5 AMM 71-00-00-700-813-F00, OF POWER PLANT TEST REFERANCE TABLE. CREW STATED IT WAS A NO BLEED
- [SDR CALA2024071001991](https://openairdocs.org/sdr/CALA2024071001991.md): Receiver · inoperative · Jul 8, 2024 · N18243 · Boeing 737824 · Global Positioning System
  > GPS L INOP TROUBLESHOT IAW FIM 34-31 TASK 801 FOUND BREAKER P6-1 A13 TO BE POPPED ATTEMPTED RESET WOULDN''T RESET. REPLACED MMR #2 IAW AMM 34-31-42-000/400-801 OPS CHECK GOOD.
- [SDR CALA2023103103254](https://openairdocs.org/sdr/CALA2023103103254.md): Anti-Ice Valve · inoperative · Oct 29, 2023 · N18243 · Boeing 737824 · Engine Anti-Icing System
  > NUMBER 1 ENGINE COWL ANTI ICE ILLUMINATED ON TAKEOFF ROLL. PIREP ENGINE #1 COWL ANTI ICE ILLUMINATED AT HIGH POWER SETTINGS. WHEN THRUST WAS RETARDED, LIGHT EXTINGUISHED. SECURED NO 1 ENGINE ANTI ICE VALVE IN OPEN POSITION PER MEL. ELECTRICAL CONNECTOR DP1302

Next page: https://openairdocs.org/aircraft/N18243/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 = 'N18243' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N18243/reports

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