# Service difficulty reports: N12238

A list on [N12238](https://openairdocs.org/aircraft/N12238.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 · 101 reports

- [SDR CALA2026101320325](https://openairdocs.org/sdr/CALA2026101320325.md): Lamp · faulty · Oct 11, 2026 · N12238 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - EMERGENCY EXIT SIGNS AT DOORS 2L, 2R, AND BOTH FWD OVERWING EXITS HAVE ONE OR MORE BULBS INOP RELAMPED RH FWD OVERWING, AND DOORS 2L AND 2R REF AMM 33-51-01-960-801, FOUND LH FWD OVERWIN
- [SDR CALA2026101320322](https://openairdocs.org/sdr/CALA2026101320322.md): Lamp · inoperative · Oct 11, 2026 · N12238 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - EPL AT SEATS 15ABC, 21ABC, 23ABC, 24ABC AND 34ABC HAVE ONE BULB INOP. RELAMPED REF AMM 33-51-11-960-801, OPC NORMAL PARTS USED: 29-3351-3-0015,QTY:1
- [SDR CALA2025121612169](https://openairdocs.org/sdr/CALA2025121612169.md): Light · no test · Dec 12, 2025 · N12238 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS OPS CHECK, LIGHTS INOPERATIVE AT ROW 15CBA. R & R EMERGENCY LIGHT AT ROW 15CBA IAW AMM 33-51-11. OPS CHECKED GOOD.
- [SDR CALA2025102210418](https://openairdocs.org/sdr/CALA2025102210418.md): Cradle · inoperative · Oct 19, 2025 · N12238 · Boeing 737824 · Emergency Equipment
  > AFT CABIN FLASHLIGHT INOP AFT AC LEFT INBOARD FLASHLIGHT HOLDER TESTER IS INOP. REQUEST MEL 2512A. MEL 2512A APPROVED BY TOMC. DDP CW MEL APPLIED COULD NOT DUPLICATE, AFT FLASHLIGHT OPS CHKS GOOD.
- [SDR CALA2025100609621](https://openairdocs.org/sdr/CALA2025100609621.md): Latch · faulty · Oct 4, 2025 · N12238 · Boeing 737824 · Escape Slide
  > ESCAPE SLIDE INSTALL LATCH ASSEMBLY BROKEN REMOVED AND REPLACED ESCAPE SLIDE LATCH ASSY AT R2 DOOR REF AMM 25-66-01
- [SDR CALA2025090308421](https://openairdocs.org/sdr/CALA2025090308421.md): Bracket · loose · Aug 29, 2025 · N12238 · Boeing 737824 · Service Doors
  > GIRT BAR BRACKET DOOR 2 RIGHT IS LOOSE. ADJUSTED AND TIGHTENED GIRT BAR FLOOR BRAKCET AT DR 2R. OPS CHECKS ARE GOOD AND ACFT IS GOOD TO CONTIUE.
- [SDR CALA2025060505287](https://openairdocs.org/sdr/CALA2025060505287.md): Switch · broken · Jun 2, 2025 · N12238 · Boeing 737824 · Cargo/Baggage Doors
  > DOOR WARNING ANNUNCIATOR IS ON AFT CARGO AFT CARGO LIGHT REF FIM 52-30 TASK 803. FOUND MESSAGE 52-72002 IN AIR MODE. R&R AFT CARGO DOOR WARNING SWITCH S961 PER AMM 52-71-31-400-802. OPS CHECK SATISFACTORY.
- [SDR CALA2025050604495](https://openairdocs.org/sdr/CALA2025050604495.md): Switch · failed · May 1, 2025 · N12238 · Boeing 737824 · Door Warning System
  > AFT CARGO LIGHT CAME ON AT 500 AGL AND STAYED ON FOR TAXI TIL JU ST BEFORE PARKING PERFORMED INSPECTION, DOOR OPONING CLOSING PROPERLY.SUSPECT BAD DOOR IND SWITCH.PILOT SAYS NO ISSUES WITH PRESSURIZATION. REMOVED AND REPLACED AFT CARGO DOOR INDICATION SWITCH
- [SDR CALA2025041803995](https://openairdocs.org/sdr/CALA2025041803995.md): Ground Wire · broken · Apr 17, 2025 · N12238 · Boeing 737824 · Light System Wiring
  > SUPPORT TASK- MAIN CABIN GROUND WIRE PULLED OUT FROM BLOCK AT LH CUSP LINE, STA 683. INSERTED GROUND WIRE IN GD BLOCK 3322DC IAW B737NG WDM 33-51-22 PG1 SH1. OP CHECK OF EEPL PROX LIGHTS GOOD IAW B737NG AMM 33-51-11.
- [SDR CALA2025041803978](https://openairdocs.org/sdr/CALA2025041803978.md): Charger · no test · Apr 17, 2025 · N12238 · Boeing 737824 · Emergency Lighting
  > SUPPORT TASK- SEAT EEPL LIGHTS FROM OVERWING AFT INOP. REMOVED AND REPLACED SEAT EEPL LIGHTS FROM OVERWING AFT IAW B737NG AMM B737NG 35-51-11-960-801. REMOVED AND REPLACED M1694 BATTERY CHARGER ASSY IAW B737NG AMM 33-51-06-960-806. OP CHECK GOOD IAW B737NG A
- [SDR CALA2025042104043](https://openairdocs.org/sdr/CALA2025042104043.md): Rib · cracked · Apr 12, 2025 · N12238 · Boeing 737824 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER HINGE RIB AT RUDDER STATION 56.48 (17SA1204) IS CRACKED. REPAIRED VERTICAL STAB T/E HINGE RIB IAW HAECO REO-G25412 STAGE 3 AND UNITED ECRA SFR DATA ENTERED. REPAIRED VERTICAL STAB T/E HINGE RIB IAW HAECO REO-G25412 STAGE 3 AND UNITED ECR
- [SDR CALA2025042104042](https://openairdocs.org/sdr/CALA2025042104042.md): Skin · cracked · Apr 10, 2025 · N12238 · Boeing 737824 · Wing, Plate/Skin
  > EA 5725-01143 OPS 001 LH WING LOWER SKING AT STRINGER 9 FWD AND AFT O/B FASTENERS ARE CRACKED ON LOWER SKIN CRACKS; RUNNING FWD TO AFT DIRECTION. WSTA 564.5 APPROX. REPAIRED LH WING LOWER SKIN PER UNITED ECRA 5720-03517. PERFORM AN INSPECTION PER PART 2 OF T
- [SDR CALA2025040403538](https://openairdocs.org/sdr/CALA2025040403538.md): Skin · no discrepancy · Apr 1, 2025 · N12238 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > R/H HORIZONTAL STABILIZER LOWER SKIN AT STA 92.70 REQUIRE SKIN CUT-OUT FOR ACCESS TO RIB WEB REPAIRS.
- [SDR CALA2025040303487](https://openairdocs.org/sdr/CALA2025040303487.md): Floorbeam · corroded · Apr 1, 2025 · N12238 · Boeing 737824 · Fuselage Main, Floor Beam
  > SUPPORT TASK FLOOR BEAM AT STA 967 HAS CORROSION NEAR FLOORBOARD HOLE AT RIB 30, COMPLETED REPAIRED FLOOR BEAM AT STA 967 IAW HAECO REO-G25391 STAGE 7 AND ECRA: 5375-01014. CATEGORY A REPAIR WITH NO TIME INTERVALS.
- [SDR CALA2025040303486](https://openairdocs.org/sdr/CALA2025040303486.md): Floorbeam · corroded · Apr 1, 2025 · N12238 · Boeing 737824 · Fuselage Main, Floor Beam
  > STA 986 FLOOR BEAM IS CORRODED AT LBL 35 PREVIOUS REPAIR, COMPLETED REPAIRED FLOOR BEAM AT STA 986 IAW B737-800 SRM 53-70-51-2R-4. THIS IS A CATEGORY A REPAIR
- [SDR CALA2025040303485](https://openairdocs.org/sdr/CALA2025040303485.md): Floor Support · corroded · Apr 1, 2025 · N12238 · Boeing 737824 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) FLOOR SUPPORT AT STA 951 TO 967 RBL35 IS CORRODED ON THE UPPER SURFACE. COMPLETED REMOVED AND REPLACED FLOOR SUPPORT IAW BAC DWG 147A5760 REV- AND B737-800 SRM 51-40-02.
- [SDR CALA2025040403530](https://openairdocs.org/sdr/CALA2025040403530.md): Skin · cracked · Mar 31, 2025 · N12238 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION FOUND: NO.1 MARKED, R/H HORIZONTAL LOWER SKIN STAB. STA 147.90.900 INCHES L, I/B OF I/B ROW OF RIVETS, 8.25 INCHES FWD OF AFT SPAR. TRANSCRIBED FROM HAECO GSO NR 9287038 ESFR COMPLETED
- [SDR CALA2025032803291](https://openairdocs.org/sdr/CALA2025032803291.md): Structure · corroded · Mar 27, 2025 · N12238 · Boeing 737824 · Fuselage Structure (General)
  > R2 DOOR CUTOUT LOWER CHORD UPPER SURFACE IS CORRODED, FROM STA 947-992 RBL 48.
- [SDR CALA2025032103054](https://openairdocs.org/sdr/CALA2025032103054.md): Scuff Plate · cracked · Mar 20, 2025 · N12238 · Boeing 737824 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK PARTS RACK) R1 SCUFF PLATE CRACKED IN FORWARD CORNER CLEANED AND WELDED AREA IAW B737-800 SRM 53-10-15 REPAIR 2 USING ERTI-5 TIT FILL ROD PO NO. 6343.1 FLOURSCENT PENETRANT INSPECTION OF WELD ACCOMPLISHED IAW BAC SOPM 20-20-02. NO CRACKS NOTED.
- [SDR CALA2025032003006](https://openairdocs.org/sdr/CALA2025032003006.md): Floor Panel · dented · Mar 19, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 231UF DENTED AND CRUSHED ON EDGE. RECEIVED NEW FLOOR PANEL 231UF NO. 143A5810-12 P.O NO.1113242.1 APPLICABLE TO AIRCRAFT PER B737-800 AIPC 53-21-00-24A PREFORMED FIT CHECK PER B737-800 AMM 53-21-00-400-801 STEPS 3.F.(7)(
- [SDR CALA2025032003005](https://openairdocs.org/sdr/CALA2025032003005.md): Floor Panel · dented · Mar 19, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 232PF DENTED AND CRUSHED ON EDGE. RECEIVED NEW FLOOR PANEL 143A5810-8 P.O NO. 113242.3 APPLICABLE TO AIRCRAFT PER B737-800 AIPC 53-21-00 PREFORMED FIT CHECK IAW B737-800 AMM 53-21-00-801 STEPS 3.F.(7)(8) ESFR COMPLETED
- [SDR CALA2025032003004](https://openairdocs.org/sdr/CALA2025032003004.md): Floor Panel · dented · Mar 19, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 231YF DENTED AND CRUSHED ON EDGE. RECEIVING NEW FLOOR PANEL PN NO. 29-5321-3-0126 PO NO. 1113650.2 PN: 5320DC14858-251 IAW B737-800 AMM 53-21-00. FIT CHECK GOOD ESFR COMPLETED
- [SDR CALA2025032003003](https://openairdocs.org/sdr/CALA2025032003003.md): Floor Panel · dented · Mar 19, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 232FF DENTED AND METAL HONEY COMB CRUSHED ON EDGE. TRANSCRIBED FROM HAECO GSO NR 9286470 RECEIVED NEW FLOOR PNL 232FF 143A5810-90 P.O NO. 1113321.1 APPLICABLE TO AIRCRAFT PER B737-800 AIPC 53-21-00-42A PREFORMED FIT CHECK
- [SDR CALA2025032003002](https://openairdocs.org/sdr/CALA2025032003002.md): Floor Panel · dented · Mar 19, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 232YAF DENTED AND CRUSHED ON EDGE. RECEIVED NEW FLOOR PNL 232YAF 141A5810-162 P.O NO.1113660.1 APPLICABLE TO AIRCRAFT PER B737-800 AIPC 53-21-00-47 PREFORMED FIT CHECK IAW B737-800 AMM 53-21-00 STEPS 3.F.(7)(8) ESFR COMP
- [SDR CALA2025032003001](https://openairdocs.org/sdr/CALA2025032003001.md): Floor Panel · dented · Mar 19, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 231VF DENTED AND CRUSHED ON EDGE. RECEIVED NEW FLOOR PNL 231VF 143A5810-8 P.O NO.1113242.2 APPLICABLE TO AIRCRAFT PER B737-800 AIPC 53-21-00 PREFORMED FIT CHECK IAW B737-800 AMM 53-21-00-400-801 STEPS 3.F(7)(8) ESFR COMPL
- [SDR CALA2025032002998](https://openairdocs.org/sdr/CALA2025032002998.md): Deck Plate · dented · Mar 19, 2025 · N12238 · Boeing 737824 · Fuselage Main, Structure
  > (B737-53-3-0733) COCKPIT FLOOR APPROXIMATELY STA259.5 LBL17 TO RBL5 HAS DENTS. INSTALLED REPAIR DOUBLER BETWEEN STA. 254 TO 260 LBL15.33 TO LBL1 AND REINSTALLED REMOVED RIVETS STA 247 TO 254 LBL15.33 TO RBL4.1 IAW B737-800 SRM 51-70-13-2R-2 REPAIR 2, B737-80
- [SDR CALA2025031902958](https://openairdocs.org/sdr/CALA2025031902958.md): Skin · corroded · Mar 18, 2025 · N12238 · Boeing 737824 · Fuselage Main, Plate/Skin
  > SUPPORT TASK: E&E BAY BETWEEN STA 360 - 382 STR 27L IS CORRODED. ON INSPECTION FOUND EXFOLIATED CORROSION.002 LOSS. REMOVED CORRODED SECTION OF STRINGER FROM STA 368 388. FABRICATED NEW REPAIR STRINGER SECTION. REPAIR SPLICES AND SHIMS IAW B737 SRM 53-00-53-
- [SDR CALA2025031902956](https://openairdocs.org/sdr/CALA2025031902956.md): Channel · corroded · Mar 18, 2025 · N12238 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SUPPORT TASK: FWD CARGO COMPARTMENT R/H TRANSITION PANEL FROM STA 500A - 500I IS CORRODED. DOT:X496. TRANSCRIBED FROM HAE CO NR 9286426 UPDATED TO ADD SDR INFORMATION
- [SDR CALA2025031902955](https://openairdocs.org/sdr/CALA2025031902955.md): Floor Panel · dented · Mar 18, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 232DF DENTED AND METAL HONEY COMB CRUSHED ON EDGE. RECEIVED NEW FLOOR PNL 232DF NO. 142A5810-1 P.O NO. 1113233.1 APPLICABLE TO AIRCRAFT PER B737-800 IAPC 53-21-00-24A PREFORMED FIT CHECK IAW B737-800 AMM 53-21-00-400-801
- [SDR CALA2025031902954](https://openairdocs.org/sdr/CALA2025031902954.md): Floor Panel · dented · Mar 18, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 241CF DENTED AND CRUSHED ON EDGE. TRANSCRIBED FROM HAECO GSO NR 9286485 RECEIVED NEW FLOOR PNL 241CF NO. 144A5810-12 P.O. NO. 1113242.4 APPLICABLE TO AIRCRAFT PER B737-800 AIPC 53-21-00-24A PREFORMED FIT CHECK IAW B737-800
- [SDR CALA2025031902953](https://openairdocs.org/sdr/CALA2025031902953.md): Floor Panel · dented · Mar 18, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 241BF DENTED, DELAM AND CRUSHED ON EDGE. RECEIVED NEW FLOOR PANEL 241BF 144A5810-37 P.O NO.1113733.1 APPLICABLE TO AIRCRAFT PER B737-800 AIPC 53-21-00 PREFORMED FIT CHECK IAW B737-800 AMM 53-21-00-400-801 STEPS 3.F.(7)(
- [SDR CALA2025031902952](https://openairdocs.org/sdr/CALA2025031902952.md): Floor Panel · dented · Mar 18, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 242DF DENTED AND CRUSHED ON EDGE. TRANSCRIBED FROM HAECO GSO NR 9286490 RECEIVED NEW FLOOR PNL 242DF 144A5810-3 P.O NO. 1113233.3 APPLICABLE TO AIRCRAFT PER B737-800 AIPC 53-21-00-24A PREFORMED FIT CHECK IAW B737-800 AMM 5
- [SDR CALA2025031902951](https://openairdocs.org/sdr/CALA2025031902951.md): Strap · corroded · Mar 18, 2025 · N12238 · Boeing 737824 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) FLOOR SUPPORT STRAP AT STA 1006 TO 1016 RBL15 HAS CORROSION ON UPPER SURFACE. REMOVED STRAP MATERIAL ID FOR STRAP.071 7075-T6 PO NO.1078610.1 IAW B737-800 SRM 51-40-02 BAC DWG 147A5700 REV AA AND FABRICATED STRAP IAW BAC DWG 147A5714, APPLIE
- [SDR CALA2025031902950](https://openairdocs.org/sdr/CALA2025031902950.md): Web · corroded · Mar 18, 2025 · N12238 · Boeing 737824 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) STA 1016 RBL 30 WEB CORRODED ON AFT SIDE OF LAV MOUNT. RECIEVED NEW WEB PART NO. 147A5712-2 PO NO. 1113738 AND REMOVED AND REPLACED WEB ON AFT SIDE OF LAV MOUNT STA 1016 RBL30 IAW B737-800 SRM 51-40-02 BAC DWG NO. 147A5700 REV:-
- [SDR CALA2025031902949](https://openairdocs.org/sdr/CALA2025031902949.md): Floor Support · corroded · Mar 18, 2025 · N12238 · Boeing 737824 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) FLOOR SUPPORT BETWEEN STA 294 TO 312 RBL 10 HAS CORROSION ON UPPER SURFACE. TRANSCRIBED FROM HAECO GSO NR 9286609 EVALUATED FLOOR SUPPORT BETW STA 294 TO 312 RBL10, ORIGINAL MATERIAL 0.080 REMAINING MATERIAL 0.050 MATERIAL LOSS 0.030. FOUND TO
- [SDR CALA2025031902948](https://openairdocs.org/sdr/CALA2025031902948.md): Floor Support · corroded · Mar 18, 2025 · N12238 · Boeing 737824 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) FLOOR SUPPORT STRAP AT STA 1006 TO 1016 LBL2 HAS CORROSION ON UPPER SURFACE. TRANSCRIBED FROM HAECO GSO NR 9286578 REMOVED STRAP MATERIAL ID FOR STRAP.071 7075-T6 PO NO. 1078610. 1 IAW B737-800 SRM 51-40-02 BAC DWG NO. 147A5700 REV AA FABRICAT
- [SDR CALA2025031802923](https://openairdocs.org/sdr/CALA2025031802923.md): Support Angle · corroded · Mar 17, 2025 · N12238 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SUPPORT TASK Z-ANGLE AT STA 992 LBL 30 HAS CORROSION, REMOVED AND REPLACED Z ANGLE AT STA 992 LBL 30 IAW B737-800 SRM 51-40-02 AND BAC DWG 147A5700 REV A.
- [SDR CALA2025031802925](https://openairdocs.org/sdr/CALA2025031802925.md): Door Frame · corroded · Mar 16, 2025 · N12238 · Boeing 737824 · Fuselage Main, Structure
  > L2 DOOR CUTOUT LOWER CHORD UPPER SURFACE IS CORRODED AT STA 992, LBL 48. L2 DOOR CUTOUT LOWER INNER CHORD.
- [SDR CALA2025031802924](https://openairdocs.org/sdr/CALA2025031802924.md): Floorbeam · corroded · Mar 16, 2025 · N12238 · Boeing 737824 · Fuselage Main, Floor Beam
  > SUPPORT TASK STA 328 FLOOR BEAM HAS CORROSION ON UPPER SURFACE BETWEEN RBL 0 TO RBL 45, STRAP REPAIR ON ONE SIDE OF FLANGE APPROX RBL15 STA328. THIS REPAIR WAS CUT OUT AND REPLACED WITH NEW T-CHORD SECTION.
- [SDR CALA2025031702863](https://openairdocs.org/sdr/CALA2025031702863.md): Floor Panel · dented · Mar 15, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 231WF DENTED AND CRUSHED O N EDGE. RECEIVED NEW FLOOR PNL 231WF P.O NO. 111487.2 APPLICABLE TO AIRCRAFT PER B737-800 AIPC 58-21-00-24A PREFORMED FIT CHECK IAW B737-800 AMM 53-21-00-400-801 STEP 3F(7)(8) ESFR COMPLETED
- [SDR CALA2025031702862](https://openairdocs.org/sdr/CALA2025031702862.md): Floor Panel · dented · Mar 15, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 231ZF DENTD AND CRUSHED ON EDGE TRANSCRIBED FROM HAECO GSO NR 9286479 RECEIVED NEW FLOOR PNL 231ZF P.O NO. 1113312.2 APPLICABLE TO AIRCRAFT PER B737-800 AIPC 53-21-00-24A PREFORMED FIT CHECK IAW B737-800 AMM 53-21-00-400-
- [SDR CALA2025031702861](https://openairdocs.org/sdr/CALA2025031702861.md): Floor Panel · corroded · Mar 15, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 222YAF HAS CORRODED INSERTS. RECEIVED NEW FLOOR PANEL 141A5810-2 P.O NO. 1113515.1 APPLICABLE TO AIRCRAFT PREFORMED FIT CHECK IAW B737-800 AMM 53-21-00-400-801 STEPS 3F(7)(8) ESFR COMPLETED
- [SDR CALA2025031702860](https://openairdocs.org/sdr/CALA2025031702860.md): Floor Panel · dented · Mar 15, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 231RF DENTED AND CRUSHED ON EDGE. RECEIVED NEW FLOOR PNL 231RF PNL NO. 143A5810-42 P.O. NO. 111323 3.2 APPLICABLE TO AIRCRAFT PER B737-800 AIPC 53-21-00-24A PREFORMED FIT CHECK IAW B737-800 AMM 53-21-00-400-801 STEP 3F(7)
- [SDR CALA2025031702859](https://openairdocs.org/sdr/CALA2025031702859.md): Floor Panel · dented · Mar 15, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 241EF DENTED AND CRUSHED ON EDGE. RECEIVED NEW FLOOR PNL 241EF NO. 144A5810-10 P.O NO. 1113242.5 APPLICABLE TO AIRCRAFT PER AIPC B737-800 AIPC 53-21-00 PREFORMED FIT CHECK PER B737-800 AMM 53-21-00-400-801 STEPS 3.F(7)(8)
- [SDR CALA2025031702858](https://openairdocs.org/sdr/CALA2025031702858.md): Floor Support · corroded · Mar 15, 2025 · N12238 · Boeing 737824 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) FLOOR SUPPORT BETWEEN STA 328 TO 344 LBL 5 HAS CORROSION ON UPPER SURFACE FWD SIDE. REMOVED AND REPLACED NEW FLOOR SUPPORT/PANEL BREAK IAW B737-800 SRM 51-40-02-0G-0 AND BAC DWG 1415400 REV:- AND 141A5410 REV:A, EVALUATED CORROSION AREAS, ORIGI
- [SDR CALA2025031702857](https://openairdocs.org/sdr/CALA2025031702857.md): Floor Support · corroded · Mar 15, 2025 · N12238 · Boeing 737824 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) FLOOR SUPPORT STA 312 TO 320 RBL10 HAS CORROSION ON UPPER SIDE. EVALUATED FLOOR SUPPORT BETWEEN STA 312 TO 320 RBL10 ORIGINAL MATERIAL THICKNESS 0.080, REMAINING THICKNESS 0.055, MATERIAL LOSS 0.025, OUT OF LIMITS IAW B737-800 SRM 53-10-51-1A-
- [SDR CALA2025031702856](https://openairdocs.org/sdr/CALA2025031702856.md): Floor Panel · dented · Mar 15, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 232SF DENTED AND CRUSHED ON EDGE. RECEIVED NEW FLOOR PNL 232SF PO: 1113312.2 PN: 5320DC14858-150 APPLICABLE TO ACFT IAW B737-800 AIPC 53-21-00. AND FIT CHK GOOD IAW B737-800 AMM 53-21-00-400-801 STEP 3.F(7)(8) ESFR COMPLET
- [SDR CALA2025031402807](https://openairdocs.org/sdr/CALA2025031402807.md): Skin · dented · Mar 12, 2025 · N12238 · Boeing 737824 · Cargo/Baggage Doors
  > SUPPORT TASK--N/R CREATED DUE TO N/R 36023; LOG PAGE 9286023 WAS CLOSED IN ERROR. THIS N/R IS CREATED SO UAL CAN COMPLETE ESFR. COMPLETED LOG PAGE OPENED TO DOCUMENT SFR FOR LP 4074059, CLOSED IN ERROR ALL WORK ACCOMPLISHED ON NON-ROUTINE NO. 36023 LOG PAGE
- [SDR CALA2025031302760](https://openairdocs.org/sdr/CALA2025031302760.md): Floor Panel · dented · Mar 12, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 232RF DENTED AND CRUSHED ON EDGE. TRANSCRIBED FROM HAECO GSO NR 9286481 RECEIVED NEW FLOOR PNL 144A5810-151 P.O NO.1113650.3 APPLICABLE TO AIRCRAFT PER B737-800 AIPC 53-21-00-42A PREFORMED FIT CHECK IAW B737-800 AMM 53-21-
- [SDR CALA2025031302759](https://openairdocs.org/sdr/CALA2025031302759.md): Floor Panel · dented · Mar 12, 2025 · N12238 · Boeing 737824 · Fuselage Floor Panel
  > (SUPPORT TASK) MAIN CABIN FLOOR PANEL 231YAF IS DENTED AND CRUSHED ON EDGE TRANSCRIBED FROM HAECO GSO NR 9286455 ESFR COMPLETE

Next page: https://openairdocs.org/aircraft/N12238/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 = 'N12238' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N12238/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.