# Service difficulty reports: N26232

A list on [N26232](https://openairdocs.org/aircraft/N26232.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 · 99 reports

- [SDR CALA2026082718948](https://openairdocs.org/sdr/CALA2026082718948.md): Fitting · cracked · Jul 30, 2026 · N26232 · Boeing 737824 · Fuselage Main, Frame
  > BS 663.75 FRAME FITTING & FAIL SAFE STRAP AT S18A, CRACKED AT RT TOP LOWER AFT FASTENER ON FRAME FITTING, AFTER CLEAN UP LOCKED BY TOMC FOR MX FERRY TO RFD. FERRY FLIGHT COMPLETED ACCOMPLISHED REPLACEMENT OF RIGHT BS 663.75 REAR SPAR FRAME ASSEMBLY IAW ECRA
- [SDR CALA2026080318228](https://openairdocs.org/sdr/CALA2026080318228.md): Failsafe · damaged · Jul 30, 2026 · N26232 · Boeing 737824 · Fuselage Main, Structure
  > LEFT BS 663.75 FAILSAFE, FRAME FITTING AND FAILSAFE STRAP REQUIRE REPLACEMENT. ACCOMPLISHED REPLACEMENT OF LT BS 663.75 REAR SPAR FRAME ASSEMBLY IAW ECRA 5340-02280 PART 1 AND EO 260383 REV IR.
- [SDR CALA2026073018105](https://openairdocs.org/sdr/CALA2026073018105.md): Battery Pack · inoperative · Jul 29, 2026 · N26232 · Boeing 737824 · Emergency Lighting
  > FOUND EMERGENCY FLOOR LIGHTS FROM ROWS 22-38, INOPERATIVE. PERFORMED FIM 33-50 TASK 801, REMOVED AND REPLACED BATTERY M1670 IAW AMM 33-51-06-960-805, TESTED OK.
- [SDR CALA2026073018101](https://openairdocs.org/sdr/CALA2026073018101.md): Battery Pack · faulty · Jul 28, 2026 · N26232 · Boeing 737824 · Emergency Lighting
  > FOUND LT & RT EXTERNAL LOWER FUSELAGE SLIDE EMERGENCY LIGHTS INOPERATIVE. CHARGED BATTERY PACKS, REPLACED AND PERFORMED OPS TEST IAW AMM 33-51-06-610-802, AMM 33-51-00-720-801 AND AMM 33-51-06-960-805. TEST PASSED.
- [SDR CALA2026072918082](https://openairdocs.org/sdr/CALA2026072918082.md): Skin · cracked · Jul 27, 2026 · N26232 · Boeing 737824 · Fuselage Main, Plate/Skin
  > DURING THE NDT INSPECTION CRACK WERE FOUND ON THE OTBD FASTENER HOLE LOCATED ON THE FUSELAGE UPPER SKIN NEXT TO BS 727 G (FRONT) AND BETWEEN S2L AND S3L (WHERE AFT SKIN FITTING WAS INSTALLED). PERFORMED REPAIR ON UPER FUESELAGE SKIN 2 INCHES TO FWD FROM BS 72
- [SDR CALA2026080318232](https://openairdocs.org/sdr/CALA2026080318232.md): Skin · nicked · Jul 14, 2026 · N26232 · Boeing 737824 · Fuselage Main, Plate/Skin
  > NICK WAS FOUND OUT OF LIMITS ON FUSELAGE SKIN BETWEEN BS 500AD - 500E, STR 27R - 26R. PERFORMED REPAIR AT EXTERNAL FUSELAGE SKIN BETWEEN STA 500D 500E AND STR 27R / STR26R - ALL WORKS WERE ACCOMPLISHED IAW SRM 53-00-01-2R-1, SRM-51-20-01-0G-0,AMM 20-60-07-913
- [SDR CALA2025120411758](https://openairdocs.org/sdr/CALA2025120411758.md): A/C Pack · odor · Dec 3, 2025 · N26232 · Boeing 737824 · Cabin Cooling System
  > NUMBER 2 A/C PACK ODOR & LOW AIR FLOW. PERFORMED VISUAL INSPECTION OF THE RT A/C PACK, NO OBSTRUCTIONS IN THE INTAKE, PERFOMED A/C PACK FLOW CONTROL VALVE OPS TESTED IAW AMM 21-51-00-700-802, OPS CHECKED OK, RAN PACK & AIR CONDITIONING FOR SEVERAL MINUTES, N
- [SDR CALA2025112111390](https://openairdocs.org/sdr/CALA2025112111390.md): Structure · damaged · Nov 20, 2025 · N26232 · Boeing 737824 · Horizontal Stabilizer Structure
  > INSTALL LT HORIZONTAL STAB ASSY IAW AMM 27-41-11-400-801. REMOVED LT HORIZONTAL STAB FOR ACCESS IAW AMM 27-41-11-000-401. BEGAN INSTALLATION OF LH HORIZONTAL STAB IAW AMM 27-41-11-400-801 HARD POINTED AFT PINS & TEMP INSTALLED FWD BOLTS INSTALLED AFT SPAR P
- [SDR CALA2025031102723](https://openairdocs.org/sdr/CALA2025031102723.md): Girt Bar · bent · Mar 6, 2025 · N26232 · Boeing 737824 · Emergency Equipment
  > MAIN CABIN DOOR 1L EMERG ENCY SLIDE GIRT BAR DOES NOT STOW SECUR ELY. FOUND GIRT BAR HOOK BENT OUT OF SHAPE. REFORMED HOOK TO PROPER SHAPE. GIRT BAR STAYS IN PLACE SECURELY. REF AMM 26-66-01.
- [SDR CALA2025021100333](https://openairdocs.org/sdr/CALA2025021100333.md): Support Angle · corroded · Feb 8, 2025 · N26232 · Boeing 737824 · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL FIN L/H SUPPORT ANGLE ON FUSELAGE FOR PANELS 323AL 323BL 323CL HAS CORROSION. REF AAR N/R 9940933. CLEANED CLOSURE ANGLE ON UPPER FUSELAGE BELOW VERT. STAB FROM REF B737 SRM 53-80-71-2R-6. INSTALLED REPAIR ANGLE AND STRAP AS STA 1016 TO 1132, L/H SIDE
- [SDR CALA2025020500299](https://openairdocs.org/sdr/CALA2025020500299.md): Frame · damaged · Feb 5, 2025 · N26232 · Boeing 737824 · Fuselage Main, Frame
  > L/H LOWER FUS ATTACHED ANGLE WORN O/B OF RAM AIR EXIT EXHAUST DUCT. MKD DOT-051 REF. AAR N/R:9940734 REMOVED AND REPLACED FRAME L/H LOWER FUSELAGE O/B OF RAM AIR EXI T EXHAUST DUCT AS PER SRM 51-40-02 REF. AAR N/R:9940734
- [SDR CALA2025013000248](https://openairdocs.org/sdr/CALA2025013000248.md): Door Frame · corroded · Jan 29, 2025 · N26232 · Boeing 737824 · Fuselage Main, Structure
  > R-1 DOOR FWD CUTOUT LOWER PAN FRAME CORROSION AND CRACKED.
- [SDR CALA2025012700200](https://openairdocs.org/sdr/CALA2025012700200.md): Structure · corroded · Jan 23, 2025 · N26232 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWT WET AREA INNER CHORD HAS CORROSION AT STA 293 RBL 52. DOT 251-022 REF AAR N/R 9940374 REMOVED AND REPLACED INNER CHORD AT FWD WET AREA BETWEEN ST 293 TO STA 360 RBL 52 IAW SRM 51-40-02-06-0 AND DWG 141A2310 SHEET 9.
- [SDR CALA2025012300190](https://openairdocs.org/sdr/CALA2025012300190.md): Floorbeam · corroded · Jan 21, 2025 · N26232 · Boeing 737824 · Fuselage Main, Floor Beam
  > AFT WET AREA FLOOR BEAM UPPER SURFACE AROUND LAV FITTING HAS CORROSION AT STA 947.5 RBL.52. REF AAR N/R 9940373.
- [SDR CALA2025012300189](https://openairdocs.org/sdr/CALA2025012300189.md): Floorbeam · corroded · Jan 21, 2025 · N26232 · Boeing 737824 · Fuselage Main, Floor Beam
  > AFT WET AREA FLOOR BEAM UPPER SURFACE HAS CORROSION AROUND LAV FITTING STA 947.5 LBL 50. REF AAR N/R 9940368.
- [SDR CALA2025012300188](https://openairdocs.org/sdr/CALA2025012300188.md): Floorbeam · corroded · Jan 21, 2025 · N26232 · Boeing 737824 · Fuselage Main, Floor Beam
  > AFT WET AREA FLOOR BEAM SURFACE SEVERAL SPOTS HAS CORROSION STA 986.5 BETWEEN LBL 45 TO RBL 45. REF AAR N/R 9940361.
- [SDR CALA2025011500125](https://openairdocs.org/sdr/CALA2025011500125.md): Door Frame · cracked · Jan 14, 2025 · N26232 · Boeing 737824 · Fuselage Main, Structure
  > L-1 DOOR CUTOUT CRACK UPPER CHORD AT STA 312, BETWEEN S-5L AND S-6L. ACCOMPLISHED REPAIR AT STA 312 STR 5L-6L IAW B737-800 SRM 53-10-07-2R-1.
- [SDR CALA2025011300100](https://openairdocs.org/sdr/CALA2025011300100.md): Floor Support · corroded · Jan 11, 2025 · N26232 · Boeing 737824 · Fuselage Miscellaneous Structure
  > L-1 Z FLOOR SUPPORT HAS CORROSION BETWEEN STA 328 TO STA 344 LBL 61. (REF AAR N/R 9940429) REMOVED AND REPLACED DAMAGED L-1 Z FLOOR SUPPORT BETWEEN STA 328 AND STA 344 LBL 61 AS PER B737-800 SRM 51-40-02-0G-0. REMOVED AND REPLACED DAMAGED L-12 FLOOR SUPPORT
- [SDR CALA2024100900796](https://openairdocs.org/sdr/CALA2024100900796.md): Window Post · cracked · Oct 5, 2024 · N26232 · Boeing 737824 · Fuselage Main, Structure
  > SUSPECT 2 CRACKS ON L3 FWD WINDOW POST 2ND SCREW UP FROM BOTTOM FWD. SEE ATTACHED PHOTO HFEC INSPECTION REQUIRED, REF SRM 56-10-02-1A-3 PARA. 4 A. FIG 102. CRACK ON 2ND SCREW UP ON LEFT WINDOW POST BETWEEN WINDOWS L2 AND L3. VERIFIED WITH HFEC 1 EA CRACK THAT
- [SDR CALA2024100700755](https://openairdocs.org/sdr/CALA2024100700755.md): Electrical Box · faulty · Oct 3, 2024 · N26232 · Boeing 737824 · Electrical Power System Wiring
  > DATA WAS LOST ON ALL DISPLAY UNITS 2-4 SECS AT A TIME REMOVED AND REPLACED DEU1 IN REF TO AMM 31-62-21-400-801, OP CHECKED GOOD. INSTALLED REQUIRED SOFTWARE IN REF TO AMM 31-62-21-470-802 PARTS USED: 29-3162-9-0002, QTY:1 ROTABLE PARTS CHANGE WAS INDICATED -
- [SDR CALA2024050201295](https://openairdocs.org/sdr/CALA2024050201295.md): Landing Gear · faulted · Apr 29, 2024 · N26232 · Boeing 737824 · Nose/Tail Landing Gear
  > REJECTED TAKEOFF DUE TO UNCOMMANDED NOSEWHEEL DEFLECTION. REQUES T INSPECTION. PER FLT CREW, RTO AT APPROX 10 KTS, AC VEERED RIGHT ON TAKEOFF GROUND TIME AND LABOR HOUR INFORMATION UPDATE ONLY. SPOKE TO PILOTS, SAID AIRCRAFT VEERED RIGHT IMMEDIATELY AFTER THIS
- [SDR CALA2023062802063](https://openairdocs.org/sdr/CALA2023062802063.md): Forging · cracked · Jun 27, 2023 · N26232 · Boeing 737824 · Fuselage Main, Structure
  > REF L/P4949126. RH FWD COCKPIT WINDOW POST CRACKED RIGHT WINDOW POST PERMANENTLY REPAIRED ON EA 5310-04554 REV. B OP 004. VERIFIED REPAIR OF R/H WINDOW POST IAW EA 5310-04554 REV B OP 004
- [SDR CALA2023062802062](https://openairdocs.org/sdr/CALA2023062802062.md): Forging · cracked · Jun 27, 2023 · N26232 · Boeing 737824 · Fuselage Main, Structure
  > REF L/P4949126. LH FWD COCKPIT WINDOW POST CRACKED LEFT WINDOW POST PERMANENTLY REPAIRED ON EA 5310-04554 REV. B OP 003. VERIFIED REPAIR IAW EA 5310-04554, REV. B OP 003
- [SDR CALA2022080501976](https://openairdocs.org/sdr/CALA2022080501976.md): Pseu · warning light · Aug 5, 2022 · N26232 · Boeing 737824 · Main Landing Gear
  > PSEU LT ON TO ROLL. RTO INITIATED. PERFORMED PSEU BITE. FOUND NO EXISTING FAULTS. LAST LEG REPORT MSG 27-62001 SPDBRK DN FAULT SHOWS. PERFORMED PSEU GROUND TEST AND PSEU SPEED BREAK TEST PER FIM TASK 27-62 TASK 808. ALL TEST PASSED WITH NO FAULTS RECORDED. OK
- [SDR CALA2022051801276](https://openairdocs.org/sdr/CALA2022051801276.md): Window · obstructed · May 17, 2022 · N26232 · Boeing 737824 · Flight Compartment Windows
  > LOUD RUSHING AIR SOUND FROM CAPT SIDE SLIDING WINDOW-UPPER L COR NER L2 WINDOW FOUND CAPT HEADSET JACK STUCK IN TOP AFT WINDOW FRAME WITH WINDOW IN THE CLOSED POSITION. REMOVED HEADSET JACK FROM WINDOW FRAME PRESSURIZED AIRCRAFT TO 3 PSI DIFF. NO LEAKS NOTED.
- [SDR CALA2022040800927](https://openairdocs.org/sdr/CALA2022040800927.md): Control Panel · inoperative · Apr 7, 2022 · N26232 · Boeing 737800* · Fire Protection System
  > RTO AT 110KTS FOR FIRE BELL 3 FIRE HANDLE LTS ILLM + WHEEL WELL AND OVRHT FAULT/ LOG AT THIS POINT IN TIME. PERFORMED WHEEL WELL,WING AND LOWER AFT BDY OHVT DETECTION SYS OPS TEST ( REF AMM 26-18-00-710-801, ENGINE FIRE DETECTION OPS TEST AMM 26-11-00-710-801
- [SDR CALA2022033100817](https://openairdocs.org/sdr/CALA2022033100817.md): Fitting · none · Mar 28, 2022 · N26232 · Boeing 7378 · Wing Structure
  > B737-06-3-3467 LT WING O/B FLAP O/B ROLLER GUIDE HAS SEVERAL WEA R MARKS ON UPPER & LWR SURFACE REMOVED & REPLACED OB FLAP OB DEFLECTOR RIB ON LH WING REF SRM 5 1-40-02. SEE PARTIAL WORK FOR WORK ACCOMPLISHED. DATA WAS TRANSC RIBED FROM PAPER DOC AERSALE WO 35
- [SDR CALA2022032500786](https://openairdocs.org/sdr/CALA2022032500786.md): Rib · damaged · Mar 25, 2022 · N26232 · Boeing 737800* · Wing Structure
  > B737-06-3-3467 LT WING O/B FLAP O/B ROLLER GUIDE HAS SEVERAL WEA R MARKS ON UPPER & LWR SURFACE REMOVED & REPLACED OB FLAP OB DEFLECTOR RIB ON LH WING REF SRM 5 1-40-02. SEE PARTIAL WORK FOR WORK ACCOMPLISHED. DATA WAS TRANSC RIBED FROM PAPER DOC AERSALE WO 35
- [SDR CALA2022031700686](https://openairdocs.org/sdr/CALA2022031700686.md): Battery Pack · no test · Mar 16, 2022 · N26232 · Boeing 7378 · Lighting System
  > (MULT-33-3-0004) EMERGENCY LIGHT SYSTEM FAILED BATTERY PACK CAPA CITY CHECK REMOVED & REPLACED EMERGENCY LIGHT SYSTEM POWER SUPPLIES "M1670, M1672, M1673 & M1676" IAW AMM 33-51-06-960-806. OPS CHECK GOOD IAW AMM 33-51-06-710-005. DATA WAS TRANSCRIBED FROM PAPE
- [SDR CALA2022030900617](https://openairdocs.org/sdr/CALA2022030900617.md): Channel · corroded · Mar 8, 2022 · N26232 · Boeing 737800* · Fuselage Structure (General)
  > (SUPPORT TASK) FLOOR SUPPORT BS 991-1015 LBL31 CORRODED IN AFT M AIN CABIN REMOVED CORRODED FLOOR SUPPORT AND INSTALLED NEW FLOOR SUPPORT P /N 147A5710U16 IAW BOEING DWG #1417A5700 REV "A". DATA WAS TRANS CRIBED FROM PAPER DOC AERSALE WO 3545 NR 25760 ACP BY M
- [SDR CALA2022022400499](https://openairdocs.org/sdr/CALA2022022400499.md): Sensor · failed · Feb 24, 2022 · N26232 · Boeing 737800* · Flight Control System
  > LE FLAPS EXT FLICKERD ON TAKEOFF INIT PWR UP GOT TAKEOFF CONFIG WRN ABORTED T/O APPX 10KTS UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. ACCOMPLISH FSEU BITE, CONTACT TOMC. PER FIM 27-88 TASK 805 FOUND RECENT LEG
- [SDR CALA2022012600241](https://openairdocs.org/sdr/CALA2022012600241.md): Battery Pack · unserviceable · Jan 26, 2022 · N26232 · Boeing 737824 · Lighting System
  > EMERGENCY LIGHTS INOP FWD LEFT SIDE. REMOVED AND REPLACED SERVICEABLE BATTERY PACK M1675 PERFORMED OPS CHECK IAW B737-800 AMM 33-51-06-960-805 AND 33-51-00-720-801 TEST GOOD. DATA WAS TRANSCRIBED FROM EMX NR 00131, WORK ACCOMPLISHED BY V921080, INSPECTED BY
- [SDR CALA2022012600228](https://openairdocs.org/sdr/CALA2022012600228.md): Fitting · cracked · Jan 24, 2022 · N26232 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRACKED. NSAEMX N/R 00095. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 32.40 REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U379153, IAW B737-800 SRM 51-40-02 AND B737NG AMM 51-31-00 A
- [SDR CALA2022012600227](https://openairdocs.org/sdr/CALA2022012600227.md): Fitting · cracked · Jan 24, 2022 · N26232 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRACKED. NSA EMX N/R 00096. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 15.04 REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U379153, IAW B737-800 SRM 51-40-02 AND B737NG AMM 51-31-00
- [SDR CALA2022012600226](https://openairdocs.org/sdr/CALA2022012600226.md): Fitting · cracked · Jan 24, 2022 · N26232 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 40.87 IS CRACKED. NSA EMX N/R 00091. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 40.87 REPORT, 46-0024, ENTERED BY UAL INSPECTION U379153, 01/24/2022. IAW B737-800 SRM 51-40-02 AND B737NG AMM 28
- [SDR CALA2022012600225](https://openairdocs.org/sdr/CALA2022012600225.md): Fitting · cracked · Jan 24, 2022 · N26232 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 32.40 IS CRACKED.NSA EMX N/R 00092. REMOVED AND REPLACED SHEAR FITTING AT STA 540 AND LBL 32.40 IAW REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U379153, B737-800 SRM 51-40-02 AND B737NG AMM 51-31-00 AND B
- [SDR CALA2022012600224](https://openairdocs.org/sdr/CALA2022012600224.md): Fitting · cracked · Jan 24, 2022 · N26232 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 15.04 IS CRACKED. NSA EMX N/R 00093. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 15.04 REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U379153, IAW B737-800 SRM 51-40-02 AND B737NG AMM 51-31-00
- [SDR CALA2022012600223](https://openairdocs.org/sdr/CALA2022012600223.md): Fitting · cracked · Jan 24, 2022 · N26232 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKED. NSA EMX N/R 00097. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U379153, IAW B737-800 SRM 51-40-02 AND B737NG AMM 51-31-00 AN
- [SDR CALA2022012600222](https://openairdocs.org/sdr/CALA2022012600222.md): Fitting · cracked · Jan 24, 2022 · N26232 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 6.14 IS CRACKED. NSA EMX N/R 00094. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 6.14 REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U379153, IAW B737-800 SRM 51-40-02 AND B737NG AMM 51-31-00 AN
- [SDR CALA2019070501146](https://openairdocs.org/sdr/CALA2019070501146.md): Power Supply · inoperative · Jul 5, 2019 · N26232 · Boeing 737824 · Emergency Lighting
  > EEL PATH LIGHTING BET SEAT ROW 7 TO SEAT ROW 14 INOP. REPLACED M1676 PWR SUPPLY REF AMM 33-51-06. OPS CHECKED OK. ACP IDT INSP OF REPLACING EMERGENCY PWR UNIT REF GMM 09-10-05 AND AMM 33-51-06. OPS CK GOOD.
- [SDR CALA2019030800357](https://openairdocs.org/sdr/CALA2019030800357.md): Bulkhead · corroded · Mar 4, 2019 · N26232 · Boeing 737824 · Fuselage Main, Bulkhead
  > MAIN CABIN APB STA 1016 AT STR 4 LT HAS CORROSION, REF FLEET CYC LE LOG PAGE 9649104. LOG PAGE IS FOR DIP AND ESFR ONLY REPAIRED PER ECRA 5310-07581. SEE FLEET CYCLE LOG PAGE 9649104 FOR DETAILS OF WORK ACCOMPLISHED. INITIATED A DIP TO ACCOMPLISH INSPECTION R
- [SDR CALA2019030400341](https://openairdocs.org/sdr/CALA2019030400341.md): Frame · cracked · Mar 1, 2019 · N26232 · Boeing 737824 · Fuselage Main, Frame
  > FUSELAGE FRAME IS CRACKED @ PSU RAIL ATTACH POINT AT STA 380 BETWEEN STR 8R AND 9R. SEE FLEETCYCLE LOG PAGE 9648812 FOR INDIVIDUAL STEP SIGN OFFS. LOG PAGE UPDATE FOR CHANGING CLOSING REQUIREMENT TO RII AND A MAJOR REPAIR CATEGORY. AT FS 380: REPAIRED FUSELAGE
- [SDR CALA2019030100328](https://openairdocs.org/sdr/CALA2019030100328.md): Spar · corroded · Feb 28, 2019 · N26232 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > LT HORIZ STAB REA SPAR UPPER T CHORD CORRODED JUST O/B OF STAB STA 57.99 AS VIEWED FROM ACCESS PANEL 332EB. REF FLEET CYCLE LOG PAGE 9648561. LOG PAGE IS FOR DIP AND ESFR ONLY. REPAIRED PER ECRA 5510-02869. SEE FLEET CYCLE LP 9648561 FOR DETAILS OF WORK ACCOMP
- [SDR CALA2019030100304](https://openairdocs.org/sdr/CALA2019030100304.md): Pressure Panel · cracked · Feb 26, 2019 · N26232 · Boeing 737824 · Fuselage Main, Bulkhead
  > RT CENTER WING BOX REAR SPAR VERTICLE PRESSURE WEB IS CRACKED AT RBL 40.00 TO RBL 45.64 WL 192 TO WL 200.6. REF FLEET CYCLE LOG PAGE 9647078. LOG PAGE IS FOR DIP ONLY. REPAIRED PER SRM 57-10-10, REPAIR 3, ALTERNATIVE 2. SEE FLEET CYCLE LP 9647078 FOR WORK PER
- [SDR CALA2017110603956](https://openairdocs.org/sdr/CALA2017110603956.md): Lens · missing · Nov 6, 2017 · N26232 · Boeing 737824 · Emergency Lighting
  > EXIT/SALIDA SIGN MISSING DOOR 2L NEAR STATION 402. INSTALLED EMERGENCY LIGHT LENS AT DOOR 2L IAW AMM 33-51-01.
- [SDR CALA2017110603955](https://openairdocs.org/sdr/CALA2017110603955.md): Plate · broken · Nov 6, 2017 · N26232 · Boeing 737824 · Emergency Lighting
  > EMERGENCY EXIT LIGHT COVER AT DOOR 2L FELL OFF. REPLACED BROKEN BASE PLATE, SYSTEM CHKS OK.
- [SDR CALA2017110303922](https://openairdocs.org/sdr/CALA2017110303922.md): Slide · unserviceable · Nov 3, 2017 · N26232 · Boeing 737824 · Escape Slide
  > DOOR 2R NEEDS INSPECTION. REPLACED AFT RT SLIDE PER AMM 26-66-01.
- [SDR CALA2017071402219](https://openairdocs.org/sdr/CALA2017071402219.md): Oven · sparks · Jul 14, 2017 · N26232 · Boeing 737800* · Buffet/Galleys
  > OVEN SMOKING OR SPARKING 205. REPLACED OVEN
- [SDR CALA2015092100786](https://openairdocs.org/sdr/CALA2015092100786.md): Pump · faulty · Sep 20, 2015 · N26232 · Boeing 737824 · Hydraulic Pump (Electric/Engine), Main
  > NUMBER 1 ENG HYD PUMP WILL NOT PRESSURIZE IAW ITEM D OF AMM 29-11-00-700-801. REPLACED NR 1 EDP.
- [SDR CALA2015082400695](https://openairdocs.org/sdr/CALA2015082400695.md): Light · inoperative · Aug 22, 2015 · N26232 · Boeing 737824 · Emergency Lighting
  > SUPPORT TASK EXTERIOR EMER LIGHT AT L1 DOOR NOT ILLUMINATING. REPLACED LAMP FOR EXTERIOR EMER LIGHT AT L1 DOOR IAW AMM 33-51-04. OPERATIONS CHECKED OK.

Next page: https://openairdocs.org/aircraft/N26232/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 = 'N26232' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N26232/reports

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