# Service difficulty reports: N14235

A list on [N14235](https://openairdocs.org/aircraft/N14235.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 CALA2026062517322](https://openairdocs.org/sdr/CALA2026062517322.md): Oven · odor · Jun 23, 2026 · N14235 · Boeing 737824 · Buffet/Galleys
  > OVEN 204 EMITTS ACRID ELETRICAL SMELL WHEN HEATED. NO SMOKE OR FIRE. FOUND BURNED FOOD RESIDUE ON INSIDE OF OVEN DOOR. CLEANED AFFECTED AREA ON OVEN DOOR. OPS CHECKED OVEN AT 350 DEGREES FOR 20 MIN. NO BURN SMELL OR ODOR. ACFT OK FOR SERVICE.
- [SDR CALA2026060416826](https://openairdocs.org/sdr/CALA2026060416826.md): Skin · cracked · Jun 3, 2026 · N14235 · Boeing 737824 · Wing, Plate/Skin
  > LEFT WING LOWER SKIN AT S9, DURING HFEC INSPECTION CRACK WAS FOUND AT OTBD MOST FASTENER. PERFORMED PERMANENT REPAIR ON LH WING LOWER SKIN AT S-9 IAW EA 5725-01143 REV A.
- [SDR CALA2026010512657](https://openairdocs.org/sdr/CALA2026010512657.md): Skin · dented · Jan 2, 2026 · N14235 · Boeing 737824 · Cargo/Baggage Doors
  > DAMAGE FROM BAGGAGE CART AT FWD CARGO DOOR. BS 440+7 - 440+13.7, S20R-2 - S20R+2.4. DENT IS WITHIN LIMITS IAW SRM 52-30-01-1A-1 SEC 4, PARA B, SUBSECTION (4) FIG 103, ALLOWABLE DAMAGE 1, DETAIL F. DENT IS 7.00 INCHES LONG, 4.250 WIDE,.320 DEEP. NO CRACKS
- [SDR CALA2026010512656](https://openairdocs.org/sdr/CALA2026010512656.md): Skin · damaged · Jan 2, 2026 · N14235 · Boeing 737824 · Fuselage Main, Plate/Skin
  > DAMAGE FROM BAGGAGE CART AT RT SIDE OF FUSELAGE. BS 344-2 - 360+3, S20R-1 - S20R+10.5. MEASUREMENTS: HEIGHT: 7.3" WIDTH: 20.75" DEPTH: 0.24". INSPECTED AREA, THE DAMAGE BS 344 -360, S20R - S21R. STR 20R APPEARS TO BE BENT, CAUSING THE ATTACHING CLIPS ON BOTH
- [SDR CALA2026010512655](https://openairdocs.org/sdr/CALA2026010512655.md): Stringer · bent · Jan 2, 2026 · N14235 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > WHILE INSPECTING EXTERNAL FUSELAGE SKIN DAMAGE FROM STA 344 TO STA 360, FOUND STRINGER 20R BENT FROM STA 344 TO STA 360. REPAIRED STRINGER 20R FROM STA 344 TO STA 360 AS PER SRM 53-00-03-2R-1 TYPE 1 STRINGER, WITH THE DEVIATIONS PROVED IN EC/RA 5310-08761 AND
- [SDR CALA2025111911348](https://openairdocs.org/sdr/CALA2025111911348.md): Unknown · odor · Nov 18, 2025 · N14235 · Boeing 737824 · Air Distribution System
  > DUR FLT FAINT SMOKE SMELL BTW ROWS 12-21 AIRCRAFT LEFT. SMELL DISSIPATED AFTR 5 MINS FLIGHT AND CABIN CREW COMPLETED FORM 46-6020. DEBRIEFED FLIGHT AND CABIN CREW ON ASSOCATED SMOKE/ODOR IN CABIN. INSPECTED AREAS SUSECTED TO CAUSE CONCERN REF AMM TASK 05-51-
- [SDR CALA2025111111130](https://openairdocs.org/sdr/CALA2025111111130.md): Girt Bar · no discrepancy · Nov 10, 2025 · N14235 · Boeing 737824 · Emergency Equipment
  > FA REPORTS LEFT GIRT BAR CLIP ON DOOR 1R LOOSE. INSPECTED BOTH J HOOKS FOR GIRT BAR ON 1R, J HOOKS ARE SECURED, NO DEFECTS NOTED. REF AMM TASK 25-66-01- 200-802.
- [SDR CALA2025090908674](https://openairdocs.org/sdr/CALA2025090908674.md): Contact · shorted · Sep 6, 2025 · N14235 · Boeing 737824 · Lighting System
  > GATE RETURN, WHEN SETTING TAKE OFF PWR ADIRU LIGHTS ILLUMINATED, MCP FLICKERED FOLLOWED WITH NUMEROUS WARNING LIGHTS ILLUMINATED ON THE OVERHEAD PANEL. TOMC ADVISED GATE RETURN MCP ALL LIGHTS ON. ALSO NUMBERS FLASHING 8 ON DISPLAY WINDOWS. FIRE PANEL SHOWING
- [SDR CALA2025090108318](https://openairdocs.org/sdr/CALA2025090108318.md): Pcb · not reported · Aug 28, 2025 · N14235 · Boeing 737824 · Flight Compartment Lighting
  > SEVERAL ANNUNCIATIONS ON OVHD PANEL CENTER INSTRUMENT PANEL AND MCP. WOULD REF WDM 31-52-75 AND IF NO FAULTS. REPLACE R33/R34 AS A PRECAUTION. GND TESTED OK AFTER ARRIVAL, REPLACED R33, MASTER TEST RELAY, AND R34, MASTER DIM RELAY. PERFORMED OP TESTED OK I
- [SDR CALA2025081107559](https://openairdocs.org/sdr/CALA2025081107559.md): Skin · cracked · Aug 7, 2025 · N14235 · Boeing 737824 · Leading Edge Devices
  > RIGHT WING NR 8 SLAT LOWER SURFACE AT ACTUATOR ATTACH POINT CRACKED. ACCOMPLISHED PERMANENT REPAIR AT SLAT NR 8 NOSE SKIN LOWER SURFACE IAW SRM 57-42-01-2R-8 FIGURE 202 ALTERNATIVE 1. NO FURTHER ACTION REQUIRED.
- [SDR CALA2025081407755](https://openairdocs.org/sdr/CALA2025081407755.md): Window Frame · cracked · Aug 6, 2025 · N14235 · Boeing 737824 · Fuselage Main, Structure
  > EA 5310-08195 REV B CRACK FOUND AT LH SIDE NUMBER 3 WINDOW FRAME POST 4TH HOLE FROM THE BOTTOM. ACCOMPLISHED ON THE LT NR 3 WINDOW POST FRAME E-F IAW ECRA 5310-08666 PART 1. AFTER 49900 TOTAL AIRCRAFT FLIGHT CYCLES (FC), BUT BEFORE 50000FC PERFORM AN INSP
- [SDR CALA2025081407746](https://openairdocs.org/sdr/CALA2025081407746.md): Spar · corroded · Aug 6, 2025 · N14235 · Boeing 737824 · Wing Spar
  > LEFT WING L/E TO FRONT SPAR APPROXIMATELY RIB 26 HAS CORROSION. ACCOMPLISHED INTERIM REPAIR CATEGORY B AT LEFT WING FRONT SPAR LOWER CHORD BETWEEN OFSS 700 AND OFSS 710 AS PER EC/RA 5720-03555 PART 1 PARAGRAPH 1.
- [SDR CALA2025080607383](https://openairdocs.org/sdr/CALA2025080607383.md): Floorbeam · corroded · Aug 1, 2025 · N14235 · Boeing 737824 · Fuselage Main, Floor Beam
  > FOWARD WET AREA STA.294.5 RBL 10" FLOORBEAM STRUCTURE HAS CORROSION. ACCOMPLISHED ESFR FORM AS PER UAL GMM 04-20-05.REMOVED AND REPLACED UPPER T-CHORD AT FLOORBEAM STA 294.5 BETWEEN LBL 35 TO RBL 57 REF SRM 53-10-51-2R-16 AND SRM 51-40-02-0G-0 PARAGRAPH 4 AN
- [SDR CALA2025080507321](https://openairdocs.org/sdr/CALA2025080507321.md): Floorbeam · corroded · Aug 1, 2025 · N14235 · Boeing 737824 · Fuselage Main, Floor Beam
  > FORWARD WET AREA BS 328, RBL 46, FLOORBEAM HAS CORROSION. REMOVED AND REPLACED FLOORBEAM SECTION BS 328 BETWEEN RBL 0 AND RBL 56 IAW SRM 53-10 51-2R-7 AND SRM SRM 51-40-02-0G-0 PARAGRAPH 7.D.
- [SDR CALA2025080807489](https://openairdocs.org/sdr/CALA2025080807489.md): Structure · corroded · Jul 31, 2025 · N14235 · Boeing 737824 · Fuselage Main, Structure
  > AFT WET AREA. EXFOLIATION CORROSION ON SEVERAL SPOTS OF RT INNER CHORD BETWEEN BS 947.5 -1006. REMOVED AND REPLACED INNER CHORD AT RT AFT WET AREA BETWEEN STA 890 TO STA 1006 PER SRM 51-40-02-0G-0, 51-40-03-0G-0 AND DWGS 147A8501, 147A0004.
- [SDR CALA2025080407232](https://openairdocs.org/sdr/CALA2025080407232.md): Stringer · corroded · Jul 31, 2025 · N14235 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND AT AREA AFT OF AFT CARGO COMPT S-21R BETWEEN STA 967-986.5. ACCOMPLISHED CATEGORY A REPAIR AT STRINGER S-21R BETWEEN STA 967 AND 986.5 AS PER SRM 53-70-03-2R-1 AND SRM 53-00-03-2R-1 FIGURE 201 FOR DAMAGE ON STRINGER FREE FLANGE. NO FURTHER ACT
- [SDR CALA2025080107208](https://openairdocs.org/sdr/CALA2025080107208.md): Floorbeam · corroded · Jul 31, 2025 · N14235 · Boeing 737824 · Fuselage Main, Floor Beam
  > AFT WET AREA. EXFOLIATION CORROSION AT SEVERAL SPOTS ON FLOOR BEAM UPPER SURFACE BS 986.5 RBL7 TROUGHT RBL47. REMOVED AND REPLACED EXISTING REPAIR T - CHORD AT STA 986.5 RBL 8 TO RBL 50 REF SRM 53-70-51-2R-4 AND SRM 51-40-02-0G-0.
- [SDR CALA2025073007076](https://openairdocs.org/sdr/CALA2025073007076.md): Battery Pack · no test · Jul 29, 2025 · N14235 · Boeing 737824 · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INOP. (REF AAR N/R 9986389) REMOVED & REPLACED BATTERY PACKS AT POSITIONS M1672 & M1673 AS PER AMM 33-51-06-02. PERFORMED INSTALLATION TEST AS PER B737 AMM 33-51-06-02 (SUBTASK 33-51-06-710-004). TEST FOUND NORMAL, NO DEFECTS NOTED. RE
- [SDR CALA2025072806978](https://openairdocs.org/sdr/CALA2025072806978.md): Angle · corroded · Jul 26, 2025 · N14235 · Boeing 737824 · APU Cowling/Containment
  > CORROSION APU BAY. AFT BULKHEAD. LOWER ANGLE FOR SEAL RETAINER, DOT 260 001 FOR REF N/R 9985897 REMOVED AND REPLACED CORROSION APU BAY. AFT BULKHEAD. LOWER ANGLE FOR SEAL RETAINER, DOT 260 001. AFT BULKHEAD. LOWER ANGLE FOUND EXFOLIATION OUT OF LIMITIS. REMOV
- [SDR CALA2025072806977](https://openairdocs.org/sdr/CALA2025072806977.md): Waste Tank · corroded · Jul 26, 2025 · N14235 · Boeing 737824 · Waste Disposal System
  > AFT CARGO WASTE TANK COMP CORROSION AT DUMP CHUTE BASE BETWEEN S STA 847-867 REMOVED AND REPLACED WASTE TANK DRAIN NEW PAN ASSY AT AFT CARGO WASTE TANK AT DUMP CHUTE BASE BETWEEN STA 847-867 IN REF SRM 51-40-02-0G-0 AND DWG 146A7401 ESFR TRANSACTION COMPLETED
- [SDR CALA2025063006074](https://openairdocs.org/sdr/CALA2025063006074.md): Skin · cracked · Jun 28, 2025 · N14235 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT LOWER SKIN OF RIGHT HORIZONTAL STABILIZER AT STAB STA 92.70, 12" FROM REAR SPAR, I/B ROW. CRACK LENGTH: 0.468". REPAIRED CRACK FOUND AT LOWER SKIN OF RIGHT HORIZONTAL STABILIZER AT STAB STA 92.70, 12" FROM REAR SPAR, I/B ROW. IN REF SRM 55-10-
- [SDR CALA2025032603194](https://openairdocs.org/sdr/CALA2025032603194.md): Handle · no discrepancy · Mar 23, 2025 · N14235 · Boeing 737824 · Flight Compartment Windows
  > COCKPIT EMERGENCY ESCAPE HANDLE OUTSIDE NOT FLUSH. CREW STOWED HANDLE. FOUND HANDLE FLUSH CREW STOWED HANDLE. FOUND HANDLE FLUSH.
- [SDR CALA2025013002134](https://openairdocs.org/sdr/CALA2025013002134.md): Hook And Loop · worn · Jan 27, 2025 · N14235 · Boeing 737824 · Doors
  > 20F EXIT ROW VELCROW COMING NEEDS REPLACING FOUND DEBRIS IN OVERWING EXIT LIFT STRAP COVER VELCRO, CLEANED DEBRIS AND RESECURED COVER IN REF AMM 52-22-00
- [SDR CALA2024062400062](https://openairdocs.org/sdr/CALA2024062400062.md): Skin · damaged · Jun 19, 2024 · N14235 · Boeing 737824 · Cargo/Baggage Doors
  > RAMP REPORT DURING CARGO REMOVAL DOOR WAS SCRATCHED FWD CARGO DOOR. SCRATCH MEASURED 5.5" VERTICALLY, BLENDED TO A SMOOTH CONTOUR REF SRM 52-30-01-1A-1. REQUEST HFEC INSP OF REWORKED AREA FOR CRACKS AND CHECK REMAINING THICKNESS. PERFORMED HFEC. NO CRACKS IA
- [SDR CALA2024053101659](https://openairdocs.org/sdr/CALA2024053101659.md): Toilet · leaking · May 28, 2024 · N14235 · Boeing 737824 · Waste Disposal System
  > AFT LAV AREA CARPET SOAKED POSSIBLE LAV LEAK REQUEST MEL FOR LAVATORY " E " AS UNUSABLE COMPLIED WITH DDP PLACED LAVATORY "E" ON MEL AS INOP DO NOT USE, COMPLIED WITH DDP. R&R LAV E REF AMM 38-32-01 OPS CHECK GOOD NO LEAKS.
- [SDR CALA2024052201557](https://openairdocs.org/sdr/CALA2024052201557.md): Vent · cracked · May 15, 2024 · N14235 · Boeing 737824 · Fuselage Main, Plate/Skin
  > WASTE TANK FUSELAGE VENT EXHIBITS CRACKS AND CORROSION EXTERNALLY ON EXTERIOR SKIN AFT OF STATION # 907 SECTION # 47 REMOVED WASTE TANK ENCLOUSER PANELS. REF AMM 25-52-20. REMOVED POTABLE WATER TANK. REF AMM 38-11-01-00-801. REPAIR DAMAGED AREA PER SRM 53-70-0
- [SDR CALA2024040300958](https://openairdocs.org/sdr/CALA2024040300958.md): Landing Gear · unknown · Mar 31, 2024 · N14235 · Boeing 737824 · Landing Gear Retraction/Extension System
  > NOSE GEAR CAME DOWN WITH GEAR LEVER IN OFF POSITION DURING AFTER TAKEOFF PROCEDURE RIGGING, COULD NOT DUPLICATE THE ISSUE LIKE MIDNIGHTS DID. RECONNECTED LG DOORS AND CYCLED GEAR SEVERAL MORE TIMES WITH NO ISSUES. VERIFIED CABLE RIG TENSION ONLY.RII 09-25-05
- [SDR CALA2024040300957](https://openairdocs.org/sdr/CALA2024040300957.md): Landing Gear · unknown · Mar 31, 2024 · N14235 · Boeing 737824 · Landing Gear Retraction/Extension System
  > NOSE GEAR CAME DOWN WITH GEAR LEVER IN OFF POSITION DURING AFTER TAKEOFF PROCEDURE RIGGING, COULD NOT DUPLICATE THE ISSUE LIKE MIDNIGHTS DID. RECONNECTED LG DOORS AND CYCLED GEAR SEVERAL MORE TIMES WITH NO ISSUES. VERIFIED CABLE RIG TENSION ONLY.RII 09-25-05
- [SDR CALA2023092702878](https://openairdocs.org/sdr/CALA2023092702878.md): Uplock Sensor · worn · Sep 25, 2023 · N14235 · Boeing 737824 · Landing Gear Retraction/Extension System
  > RIGHT GEAR RED LIGHT GEAR HANDLE UP RAN CHECKLIST EVENTUALLY G OT 3 DOWN AND LOCK PER CREW ON GEAR RETRACTION GOT RED RIGHT GEAR LIGHT ONLY. WITH THEGEAR LEVER IN THE OFF POSITION THEY GOT BOTH THE RED AND GREEN RIGHT GEAR LIGHT. PERFORMED MANUAL EXTENSION SAM
- [SDR CALA2023012500201](https://openairdocs.org/sdr/CALA2023012500201.md): Light · damaged · Jan 24, 2023 · N14235 · Boeing 737824 · Emergency Lighting
  > SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROW 34ABC DAMAGED. REMOVED AND REPLACED WHITE LIGHT ASSY REF MM 33-51-11. OPS CK OK. PARTS USED: BR9644-11,QTY:1 VERIFIED IDT REQUIREMENTS AND PROPER OPERATION OF LIGHT
- [SDR CALA2022120803334](https://openairdocs.org/sdr/CALA2022120803334.md): Structure · cracked · Dec 8, 2022 · N14235 · Boeing 737824 · Cargo/Baggage Doors
  > AFTER EVALUATING DMG ROUTINE CARD AT AFT CARGO DOOR FWD LOWER CO RNER FOUND POSSIBLE CRACK (REF: AAR NR 99952238) PLACED ON DIP PER TABLE 202 INSPECTION AT 22,500 FC AND REPEAT INSPECTIONS AT INTERVALS OF 1,400 FC ON CATEGORY B REPAIR. WORK ACCOMPLISHED ON AAR
- [SDR CALA2022081602083](https://openairdocs.org/sdr/CALA2022081602083.md): Circuit Breaker · not seated · Aug 16, 2022 · N14235 · Boeing 737824 · Leading Edge Slat Position Indicating System
  > PSEU ILLUMINATED UPON RECALL PERFORMED BITE TEST OF PSEU AND FOUND FAULTS: 31-52105, 31-52111, 32-64004, ALSO FOUND MAINTENANCE MESSAGE ON FSEU 27-53279. FOUND CIRCUIT BREAKER A12 ON P6-2 OPEN. RESET C/B A12. OPERATED FLAPS AND SLATS THRU SEVERAL CYCLES NO FA
- [SDR CALA2022061301496](https://openairdocs.org/sdr/CALA2022061301496.md): Axle · departed · Jun 13, 2022 · N14235 · Boeing 737824 · Nose/Tail Landing Gear Attach Section
  > PDA 1 ON TAXI OUT, LEFT NLG WHEEL AND AXLE DEPARTED AIRCRAFT. COMPLETED REMOVAL OF THE NOSE LANDING GEAR FOR REPLACEMENT. REF INSTALLED BOTH NOSE LANDING GEAR WHEELS ON THE NLG REF AMM AMM 32-21-00-000-801. 32-45-21, WHEELS NOT SAFETIED, AWAITING NEW WHEEL WAS
- [SDR CALA2022032100714](https://openairdocs.org/sdr/CALA2022032100714.md): Frame · cracked · Mar 19, 2022 · N14235 · Boeing 737800* · Fuselage Main, Plate/Skin
  > F/O''S UPPER OUTBOURD CORNER WINDOW FRAME IS CRACKED. LOCK FOR MX FERRY PHOTO ADDED RAMS REQUITED LOGPAGE UNLOCKED FOR UPDATE COMPLETED STEPS B1&2 OF AVO9568 REF NDT PART 6 51-00-01. CORRECTION: COMPLETED STEPS B3 & B4 OF AVO9568 REF NDT PART 6 INSPECTION EVAL
- [SDR CALA2021061400867](https://openairdocs.org/sdr/CALA2021061400867.md): Proximity Sensor · inoperative · Jun 14, 2021 · N14235 · Boeing 737824 · Leading Edge Slat Position Indicating System
  > *DECLARED EMERGENCY* LE FLAP TRANSIT LITE T/S REF FIM 27-51-801 FOUND LEADING EDGE FLAP EXTEND PROX SENSOR BAD F2 R&R PROX SENSOR REF MM 27-88-11-400-802 OPS NORMAL
- [SDR CALA2020032700737](https://openairdocs.org/sdr/CALA2020032700737.md): Wire · broken · Mar 27, 2020 · N14235 · Boeing 737824 · Fire Protection System Wiring
  > WING-BODY OVERHEAT LIGHT LIGHT ON THIS IS A REPEAT WRITEUP BITE ON WING BODY OVERHEAT CTL. SHOWED CODE 44, AFT CARGO OVERHEAT ALARM. PERFORMED CONTINUITY CHECK OF CARGO BIN LOOPS WAS BAD PER TABLE 301 FIM TASK 26-18-00 P 301. NEED TO ISOLATE WHICH LOOP IS BAD
- [SDR CALA2019102981839](https://openairdocs.org/sdr/CALA2019102981839.md): Bulkhead Web · canning · Oct 25, 2019 · N14235 · Boeing 737824 · Fuselage Main, Bulkhead
  > REF EA 5310-04639 REV E OP002 AFT BULKHEAD WEB EVVIDENCE OF OIL CAN CONDITION AT BS1016 S-13R WL232.5 IN I/B SIDE FROM OUTER PERIMETER L-2.0 W-1.218 AND D-0.020 ACCOMPLISHED REPAIR AT APB WEB BS1016, S13R WL232.5 14IN FROM OUTER PERMITER I.A.W RES-WI NO.201518
- [SDR CALA2019102981838](https://openairdocs.org/sdr/CALA2019102981838.md): Bulkhead · corroded · Oct 25, 2019 · N14235 · Boeing 737824 · Fuselage Main, Bulkhead
  > CORROSION FOUND AT LT W/W AFT BULKHEAD AREA AT STA 727 ADJECENT TO ELECTRICAL FEED THRU SUPPORT NEAR ENGINE FIRE BOTTLES REF AAR N/R 99848687 ACCOMPLISHED LT WHEEL WELL STA 727 WEB REAPIR PER AAR RES 2015189-46 REV IR AND UNITED ECRA 5311-02284 ADD EMP:V891438
- [SDR CALA2019102501814](https://openairdocs.org/sdr/CALA2019102501814.md): Rib · cracked · Oct 23, 2019 · N14235 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > L/H HORIZONTAL STAB NO.1 RIB HAS CRACKS ON THE LOWER SIDE OF EACH STIFFENER (4 EACH) (REF N/R 99848214) REPAIRED L/H HORIZONTAL STAB NO.1 RIB AT VERTICAL STIFFENER NO.1 AS PER REF B737-800 SRM 55-10-09 FIG 02 REPAIR 4.
- [SDR CALA2019102981834](https://openairdocs.org/sdr/CALA2019102981834.md): Bulkhead Web · cracked · Oct 22, 2019 · N14235 · Boeing 737824 · Fuselage Main, Bulkhead
  > UPPER VAPOR BARRIER APPEARS TO BE CRACKED APPROX 3IN LONG NEAR B SYS HYD RESERVOIR IN RIGHT WHEEL WELL. NEED TO VERIFY UPPER VAPOR BARRIER IS CRACKED PER NDTINSP CW NDT PART 6, REF 51-00-00-23, NOTED A 2.5 INCH CRACK IN RIGHT WW AREA VAPOR BARRIER. E/WIZ HAS B
- [SDR CALA2019102501809](https://openairdocs.org/sdr/CALA2019102501809.md): Floor Support · corroded · Oct 22, 2019 · N14235 · Boeing 737824 · Fuselage Miscellaneous Structure
  > LEFT SIDE FLOOR SUPPORT ANGLE IS CORRODED BETWEEN 927-993 JUST INBOARD OF L2 DOOR. (REF NR 99847955) REMOVED AND REPLACED FLOOR SUPPORT ANGLE "CREASE BEAM CHORD" AT MAIN CABIN L2 DOOR JUST INBOARD REF B737-800 SRM 51-40-02.
- [SDR CALA2019102501805](https://openairdocs.org/sdr/CALA2019102501805.md): Web · corroded · Oct 22, 2019 · N14235 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT DOOR CUTOUT LOWER SILL WEB CORRORED (REF NR 99847849) REMOVED AND REPLACED LOWER SILL WEB AT FWD CARGO COMPT DOOR IAW B737-800 SRM 51-40-02 AND DWG 143A8330.
- [SDR CALA2019102501804](https://openairdocs.org/sdr/CALA2019102501804.md): Rib · cracked · Oct 22, 2019 · N14235 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > IN REF TO EA 5510-01843 REV G OP 002 L/H HORIZ. STAB IN-SPAR RIB STA 92.70 VERTICAL STIFFENER NO.4 CRACKS AT LWR TRANSITION RADIUS MKD. (REF N/R 99848208) REPAIRED L/H HORIZONTAL STAB IN-SPAR RIB STA 92.70 VERTICAL STIFFENER NO.4 AS PER REF B737 SRM 55-10-09 F
- [SDR CALA2019102501803](https://openairdocs.org/sdr/CALA2019102501803.md): Rib · cracked · Oct 22, 2019 · N14235 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > REF TO EA 5510-01843 REV G OP 02 L/H HORIZ. STAB INSPAR RIB STA 92.70 VERTICAL STIFFENER NO.3 CRACKS AT LWR TRANSITION RADIUS MKD (REF N/R 99848207) REPAIRED L/H HORIZONTAL STAB INSPAR RIB STA 92.70 VERTICAL STIFFENER NO.3 AS PER REF B737-8 SRM 55-10-09 FIG 20
- [SDR CALA2019102501802](https://openairdocs.org/sdr/CALA2019102501802.md): Rib · cracked · Oct 22, 2019 · N14235 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > REF TO EA 5510-01843 REV G OP 02. L/H HORIZ. STAB. INSPAR RIB STA 92.70 VERTICAL STIFFENER NO.2 CRACKS AT LWR TRANSITION RADIUS MKD (REF N/R 99848206) REPAIRED L/H HORIZONTAL STAB INSPAR RIB STA 92.70 VERTICAL STIFFENER NO.2 AS PER REF B737-800 SRM 55-10-09 FI
- [SDR CALA2019102501801](https://openairdocs.org/sdr/CALA2019102501801.md): Stringer · corroded · Oct 22, 2019 · N14235 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION AT AFT WET AREA, STRINGER 22R BETWEEN STA 1006 AND STA 1016 CLOSER TO STA 1016 JUST AT THE END OF THE FITTING BELOW FLOOR WEB AREA. (REF NR 99848703) INSTALLED REPAIR PARTS AT AFT WET AREA STRINGER 22R BETWEEN STA 986.5 TO STA 1016 IAW B737-800
- [SDR CALA2019102311789](https://openairdocs.org/sdr/CALA2019102311789.md): Skin · corroded · Oct 19, 2019 · N14235 · Boeing 737824 · Cargo/Baggage Doors
  > AFT CARGO COMPT DOOR INTERNAL T/E WEB SKIN HAS 1EA SPOT EXFOLIATION CORROSION AND 3EA SPOTS SURFACE CORROSION REF AAR N/R99847994 REMOVED AND REPLACED INNER SKIN AT AFT CARGO COMPT DOOR REF B737 SRM 51-40-02 AND DWG 146A6110.
- [SDR CALA2019102311785](https://openairdocs.org/sdr/CALA2019102311785.md): Fitting · cracked · Oct 18, 2019 · N14235 · Boeing 737824 · Fuselage Main, Attach Fittings
  > CENTER WING FUEL TANK UPPER R/H SURFACE AT STATION 540 HAS I/B BRACKET AFT END CRACKED REF AAR N/R 99848702 REMOVED AND REPLACED NEW BRACKET AT CENTER WING FUEL TANK UPPER R/H SURFACE STATION 540I/B REF B737 SRM 51-40-02 DWG 111A2000 AND AMM 51-31-00
- [SDR CALA2019102311784](https://openairdocs.org/sdr/CALA2019102311784.md): Angle · cracked · Oct 18, 2019 · N14235 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN FLOOR SUPPORT ANGLE APPEARS CRACKED AT FASTNER HEAD AT RBL55 STA 616 REF AAR N/R 99848350 INSTALLED REPAIR AT R/H MAIN FLOOR INNER CHORD STA 616 HOLE FASTNER FROM STA 601-639 RBL 55 AS PER RES WI2015189-51 AND ECRA 5315-01134.
- [SDR CALA2019102311783](https://openairdocs.org/sdr/CALA2019102311783.md): Floorbeam · corroded · Oct 18, 2019 · N14235 · Boeing 737824 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT CROSSBEAM AT 987 HAS CORROSION AT NUT PLATE 47IN RIGHT OF CENTER LINE REF AAR N/R 99847940 FLOOR SUPPORT CROSSBEAM AT 987 STA RBL 7.98 TO RBL 50 REPAIRED IN REF B737 SRM 53-70-51 REPAIR 4 REPAIR ALYERNATIVE 2 FIG 205 FROM PAGE 214 TO PAGE 229 ADD

Next page: https://openairdocs.org/aircraft/N14235/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 = 'N14235' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N14235/reports

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