# Service difficulty reports: N14250

A list on [N14250](https://openairdocs.org/aircraft/N14250.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 · 107 reports

- [SDR CALA2026080918413](https://openairdocs.org/sdr/CALA2026080918413.md): Control Panel · faulty · Aug 7, 2026 · N14250 · Boeing 737824 · Communications System
  > ON TAKEOFF ROLL RADIOS WENT STATIC THEN LOUD HUM COULD NOT TRANS OR RECEIVE. DURING T/S NOTED THAT ACP NR 3 VHF 1 MIC SELECTOR SWITCH CHANGE SUDDENLY WITHOUT TOUCHING IT, ACP SWAP WITH FO SIDE, & FAULT CONFIRMED DURING COMMS TEST WITH TOWER & OPS OFFICE. FOU
- [SDR CALA2026042415698](https://openairdocs.org/sdr/CALA2026042415698.md): Skin · damaged · Apr 16, 2026 · N14250 · Boeing 737824 · Wing, Plate/Skin
  > ACCOMPLISH INSP ECTION REQUIREMENTS OF THE RH WING LOWER SKIN REPAIR AREA BETWEE N WSTA 564 ? 591 AT S-9L PER PART 2, TABLE 2
- [SDR CALA2026041715442](https://openairdocs.org/sdr/CALA2026041715442.md): Fitting · cracked · Apr 16, 2026 · N14250 · Boeing 737824 · Fuselage Main, Attach Fittings
  > REMOVE AND REPLACE R/H W/W STA 663.75 S-18A FRAME FITTING. (REF AAR NR 100002905) ACCOMPLISHED ESFR FORM AS PER GMM 04-20-05. REMOVED AND REPLACED RIGHT FRAME PICKLE FORK FITTING AT STA 663.75 STR 18R PER ESR 2 -14631 WI-P1 AND WI-P2. PER EC/RA 5340-02262, A D
- [SDR CALA2026041715439](https://openairdocs.org/sdr/CALA2026041715439.md): Fitting · cracked · Apr 16, 2026 · N14250 · Boeing 737824 · Fuselage Main, Attach Fittings
  > CRACKED: LH W/W STA 663.75 S-18A FRAME FITTING CRACKED. REMOVED AND REPLACED LEFT FRAME PICKLE FORK FITTING AT STA 663.75 STR 18L PER ESR 2- 14631 WI-P1 AND WI-P2. PER EC/RA 5340-02261, A DIP IS REQUIRED T O PERFORM AN INSPECTION OF THE FUSELAGE STA 663.75
- [SDR CALA2026042115561](https://openairdocs.org/sdr/CALA2026042115561.md): Skin · cracked · Apr 15, 2026 · N14250 · Boeing 737824 · Fuselage Main, Plate/Skin
  > CRACK FOUND AT LT INTERNAL SKIN, BELOW 2ND FASTENER HOLE. LOCATED AFT OF BS 663.75 FRAME FITTING ASSY UNDER S18L. CRACK LENGTH: 1.4. ACCOMPLISHED REPAIR TO THE LT INTERNAL SKIN. ACCOMPLISHED REPAIR AT L/H INTERNAL SKIN BELOW 2ND FASTENER HOLE LOCATED
- [SDR CALA2026041315276](https://openairdocs.org/sdr/CALA2026041315276.md): Cargo Track · damaged · Apr 10, 2026 · N14250 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CARGO BAY TIE DOWN ON CARGO RAIL DAMAGED AT STA 500-3" LBL 18. INSTALLED FWD CARGO TRACK FROM BS 500A TO 480, LBL 18 IAW SRM 53-00-53-2R-3 AND SRM 51-40-02-0G-0.
- [SDR CALA2026041215270](https://openairdocs.org/sdr/CALA2026041215270.md): Stringer · corroded · Apr 8, 2026 · N14250 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > AREA AFT OF FWD CARGO CORROSION AT STA 540 STR 26. ACCOMPLISHED REPAIR AT FWD CARGO AFT A/C BAY AREA STR 26L FROM STA 500I TO 540 SUBSTANTIATING THAT COMPLIANCE WITH THE REQUIREMENTS OF ESR-WI _73-14968_ AND ECRA _5330-07734_ WERE ACHIEVED.
- [SDR CALA2026042115567](https://openairdocs.org/sdr/CALA2026042115567.md): Skin · damaged · Apr 3, 2026 · N14250 · Boeing 737824 · Fuselage Main, Plate/Skin
  > IAW C/R DURING AAI INSPECTION NO RECORDS FOUND FOR THE REPAIR AND DTA REQUIREMENTS OF THE EXTERNAL FUSELAGE DOUBLER REPAIR AT STA 907-927 AND STR 6R-8R. ACOMPLISHED REPAIR AT FUSELAGE SKIN BETWEEN BS 907-927 BTWN S6R & 9R.
- [SDR CALA2026042115565](https://openairdocs.org/sdr/CALA2026042115565.md): Skin · corroded · Apr 3, 2026 · N14250 · Boeing 737824 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE INTERNAL SKIN CORRODED AROUND RIVET TAIL BETWEEN STR 27L-27R, BS 520. ACCOMPLISHED LOWER FUSELAGE SKIN REPAIR FROM BS 500H+10 - 540 BETWEEN S27R - 27R IAW ESR-WI 10-14655 AND ECRA 5330-07728.
- [SDR CALA2026040615094](https://openairdocs.org/sdr/CALA2026040615094.md): Cargo Track · corroded · Apr 3, 2026 · N14250 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CARGO COMP CORROSION AT CARGO RAIL 5 EACH FASTENER HOLES STA 500I - 500H, RBL 14. ACCOMPLISHED REPAIR AT FWD CARGO COMPT TRACK RAIL FROM STA 500I TO STA 500H RBL 14 REF SRM 53-00-53-2R-3 AND DWG 143A7501.
- [SDR CALA2026042115569](https://openairdocs.org/sdr/CALA2026042115569.md): Skin · corroded · Apr 2, 2026 · N14250 · Boeing 737824 · Fuselage Main, Plate/Skin
  > CORROSION AT RH LOWER FUSELAGE EXTERNAL SKIN BY DRAG LINK BS 540 BTWN S21-22R. ACCOMPLISHED A REPAIR IAW ESR 14681, ECRA 5710-02968.
- [SDR CALA2026042115563](https://openairdocs.org/sdr/CALA2026042115563.md): Floorbeam · damaged · Apr 2, 2026 · N14250 · Boeing 737824 · Fuselage Main, Floor Beam
  > FLIGHT DECK FLOORBEAM FASTENER HOLE ELONGATE BS 259.5, RBL 7. ACCOMPLISHED A FLOOR SUPPORT REPAIR IAW ESR-14897 AND ECRA 5310-08851
- [SDR CALA2026040114999](https://openairdocs.org/sdr/CALA2026040114999.md): Skin · misrepaired · Mar 30, 2026 · N14250 · Boeing 737824 · Service Doors
  > AS PER C/R DURING AAI INSPECTION THE R-1 DOOR EXTERNAL SKIN REPAIR FOUND TO BE UNSATISFACTORY DUE TO POOR WORKMANSHIP AND GOUGES AT THE INTERNAL STRUCTURE REF ECRA 5210-02699 AND LP 4766966 REF AAR N/R 100003587 ACCOMPLISHED REPAIR ON R1-DOOR IN REF WITH SRM 5
- [SDR CALA2026033114964](https://openairdocs.org/sdr/CALA2026033114964.md): Floorbeam · corroded · Mar 29, 2026 · N14250 · Boeing 737824 · Fuselage Main, Floor Beam
  > CABIN AFT WET AREA HAS CORROSION AT UPPER SURFACE BEAM ST 947.5 UNDER THE HARD POINT FITTING RBL 51. ACCOMPLISHED REPAIR OF THE UPPER TEE SECTION OF THE FLOORBEAM BS 947.5 FROM LBL 60 TO RBL 60 IAW SRM 53-70-51-2R-5, ESR 11-14649-WI-P1.
- [SDR CALA2026041515396](https://openairdocs.org/sdr/CALA2026041515396.md): Floor Support · corroded · Mar 27, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CORROSION: MAIN CABIN FWD WET AREA CORROSION AROUND FITTING AT FLOOR SUPPORT STA 294.5-3" RBL 12". ACCOMPLISHED REPAIR AT STA 277 RBL 23, SUBSTANTIATING THAT COMPLIANCE WITH THE REQUIREMENTS OF ESR-WI 52-14862 AND ECRA _5310-08849_ WERE ACHIEVED.
- [SDR CALA2026040915231](https://openairdocs.org/sdr/CALA2026040915231.md): Skin · corroded · Mar 26, 2026 · N14250 · Boeing 737824 · Fuselage Main, Plate/Skin
  > CORROSION: LOWER FUSELAGE WATER SERVICE DOOR CUTOUT INNER SKIN CORROSION AROUND HINGES. REMOVED AND REPLACED DOUBLER PER REF 51-40-02-0G-0 AND DWG147A7221.
- [SDR CALA2026033014899](https://openairdocs.org/sdr/CALA2026033014899.md): Housing · corroded · Mar 26, 2026 · N14250 · Boeing 737824 · Fuselage Main, Structure
  > CORROSION SPOTS AROUND LAV WASTE TANK INTERNAL DRAIN FLANGE AND HOUSING B.S. 847- B.S. 867. REMOVED AND REPLACED LAV WASTE HOUSING REF SRM 51-40-02-0G-0 AND DWG 146A7400.
- [SDR CALA2026033014893](https://openairdocs.org/sdr/CALA2026033014893.md): Floorbeam · corroded · Mar 23, 2026 · N14250 · Boeing 737824 · Fuselage Main, Floor Beam
  > FLIGHT DECK FLOOR SUPPORT UPPER SURFACE CORROSION BS 270 BETWEEN LBL 10" TO RBL 10" REF AAR N/R 100003259 INSTALLED REPAIR ANGLE AND REPAIR STRAP AT FLIGHT DECK FLOOR SUPPORT UPPER STA 270 REF B737-800 SRM 51-40-02-0G-0 & ECRA 5321-01566. INSTALLED REPAIR A
- [SDR CALA2026041515401](https://openairdocs.org/sdr/CALA2026041515401.md): Floorbeam · corroded · Mar 20, 2026 · N14250 · Boeing 737824 · Fuselage Main, Floor Beam
  > CABIN AFT WET AREA HAS CORROSION AT BEAM BS 986.5, LBL 44 UPPER SURFACE FASTENER HOLE. ACCOMPLISHED REPAIR OF THE UPPER T-CHORD SECTION OF THE FLOOR BEAM 986.5" FROM LBL 52" TO RBL 52" PER SRM 53-70-51-2R-4 AND ESR 12 14659-WI-P1. COMPLIANCE WITH THE REQUIREM
- [SDR CALA2026032314741](https://openairdocs.org/sdr/CALA2026032314741.md): Seat Track · worn · Mar 20, 2026 · N14250 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > CHAFE ON TOP OF SEAT TRACK LBL 45 BS 540. REPAIRED THE SEAT TRACK IAW SRM 53-00-52-2R-3.
- [SDR CALA2026032314739](https://openairdocs.org/sdr/CALA2026032314739.md): Channel · corroded · Mar 20, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > RIGHT ZEE CHANNEL BS 490 TO 500H HAS CORROSION. REMOVED AND REPLACED THE ZEE CHANNEL IAW SRM 51-40-02-0G-0, AND DWG 143A7500.
- [SDR CALA2026032314738](https://openairdocs.org/sdr/CALA2026032314738.md): Floorbeam · dented · Mar 20, 2026 · N14250 · Boeing 737824 · Fuselage Main, Floor Beam
  > DENTS ON FLIGHT DECK FLOOR B.S. 259 LBL. 15" - RBL. 4". REPAIR ACCOMPLISHED PER SRM 51-10-51-2R-2 AND DWG 141A0631.
- [SDR CALA2026032414802](https://openairdocs.org/sdr/CALA2026032414802.md): Support Angle · worn · Mar 19, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FOUND GOUGES AFT CARGO COMPARTMENT L/H SIDEWALL SUPPORT ANGLE FASTENER HOLES STA 727D BETWEEN S-21L & S-24L. REF AAR N/R 100003361 REMOVED AND INSTALLED NEW AFT CARGO COMPARTMENT L/H SIDEWALL SUPPORT ANGLE AT STA 727D BETWEEN S-19L & S-25L PER SRM 51-40-02-0G
- [SDR CALA2026032414801](https://openairdocs.org/sdr/CALA2026032414801.md): Channel · punctured · Mar 18, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT. R/H 'Z' CHANNEL BETWEEN STAS 727F & 727G PUNCTURED. REF AAR N/R 100003328 REMOVED AND REPLACED NEW AFT CARGO COMPT. R/H 'Z' CHANNEL BETWEEN STAS 727F & 727G PER SRM 51-40-02-0G-0, DWG# 146A7500. ESFR ENTRY REMOVED AND REPLACED AFT CARGO COMPT
- [SDR CALA2026032314731](https://openairdocs.org/sdr/CALA2026032314731.md): Seat Track · worn · Mar 18, 2026 · N14250 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN GOUGE AT SEAT TRACK CROWN TOP RBL 24.75 STA 540. ACCOMPISHED REPAIR AT SEAT TRACK STA 540 RBL 24.75 AS REQUIRED PER SRM 53-00-52-2R-3. ACCOMPLISHED REPAIR AT SEAT TRACK STA 540 RBL 24.75 AS REQUIRED IAW SRM 53-00-52-2R-3.
- [SDR CALA2026031914686](https://openairdocs.org/sdr/CALA2026031914686.md): Channel · corroded · Mar 17, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CARGO LT ZEE CHANNEL, BS 396 - 500H HAS CORROSION. REMOVED AND REPLACED THE LT ZEE CHANNEL BS 396 - 500I IAW SRM 51-40-02-0G-0 AND DWG 143A7500.
- [SDR CALA2026032414800](https://openairdocs.org/sdr/CALA2026032414800.md): Door Frame · corroded · Mar 16, 2026 · N14250 · Boeing 737824 · Fuselage Main, Structure
  > CORROSION- APU COMPT LT DOOR FRAME FWD SECTION HAS CORROSION. REF AAR NR 100003292 REMOVED AND REPLACED APU COMPARTMENT L/H DOOR FRAME ANGLE REF B737-800 SRM 51-40-02-0G-0 AND DWD 148A8600.WORK ACCOMPLISHED BY V949481 INSP 258 ESFR CREATED AND SENT REMOVED AND
- [SDR CALA2026090119162](https://openairdocs.org/sdr/CALA2026090119162.md): Pressure Blkhd · cracked · Mar 14, 2026 · N14250 · Boeing 737824 · Fuselage Main, Bulkhead
  > CRACK FOUND AT VERTICAL PRESSURE WEB AT LBL 40.00 - LBL45.64. COMPLETED INSTALLATION OF ALL FASTENER ON REPAIR AREA IAW SRM 57-10-10-2R PARAGRAPH 5.L. AND 51-40-02-0G-0 PARAGRAPH 8.
- [SDR CALA2026041715458](https://openairdocs.org/sdr/CALA2026041715458.md): Pressure Web · cracked · Mar 14, 2026 · N14250 · Boeing 737824 · Fuselage Main, Bulkhead
  > CRACK FOUND AT VERTICAL PRESSURE WEB BS 663 AT RBL 40 - RBL45.64. INSTALLED 100-% FASTENERS AT RT SIDE VERTICAL PRESSURE WEB REPAIR FROM RBL-25 TO RBL-50 BS 663 REF SRM 57-10-10-2R-3 STEP 5.L TABLE 202 FIGURE 204 CATEGORY B REPAIR INSPECTION REQUIREMENTS FOR
- [SDR CALA2026040915230](https://openairdocs.org/sdr/CALA2026040915230.md): Crease Beam · corroded · Mar 11, 2026 · N14250 · Boeing 737824 · Fuselage Main, Structure
  > CORROSION: MAIN CABIN CORROSION AT RH CREASE BEAM WEB STA 807-827. INSTALLED NEW CREASE BEAM WEB AT MAIN CABIN R/H STA 807 TO STA 827 AS PER SRM 51-40-02-0G-0 AND DWG 146A5900.
- [SDR CALA2026031614590](https://openairdocs.org/sdr/CALA2026031614590.md): Shield · corroded · Mar 11, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FOUND CORRODED AFT CARGO BAY FLOOR SUPPORT SHIELD S25R BETWEEN BS 767 & 787. INSTALLED A NEW SHIELD IAW SRM 51-40-02-0G-0, & DWG 146A0081.
- [SDR CALA2026031614589](https://openairdocs.org/sdr/CALA2026031614589.md): Shield · corroded · Mar 11, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY INTERCOSTAL BETWEEN BS 787 DOOR CUTOUT FWD FRAME, BELOW FLOOR SUPPORT SHIELD HAS CORROSION. INSTALLED NEW INTERCOSTAL UNDER SHIELD AT AFT CARGO COMPT INTERCOSTAL DOOR CUT OUT FLOOR SUPPORT SHIELD STA 787 PER REF SRM 51-40-02-0G-0 AND DWG146A0081.
- [SDR CALA2026031614587](https://openairdocs.org/sdr/CALA2026031614587.md): Shield · corroded · Mar 6, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR CUTOUT AFT SHIELD CORRODED. IAW AAR N/R 100002995 INSTALLED SHIELD AT FWD CARGO DOOR CUTOUT AT BS 500 - 500A IAW SRM 51-40-02-0G-0 & DWG 143A0080. REMOVED AND REPLACED SHIELD IAW SRM 51-40-02-0G-0, AND DWG 143A0080.
- [SDR CALA2026030914410](https://openairdocs.org/sdr/CALA2026030914410.md): Door Frame · cracked · Mar 4, 2026 · N14250 · Boeing 737824 · Fuselage Main, Structure
  > CRACKED: MAIN CABIN R1 DOOR CUTOUT CRACKED AT FWD LOWER DOOR FRAME. REMOVED AND REPLACED NEW FRAME ASSY AT MAIN CABIN R1 DOOR CUTOUT FWD AND LOWER SRM 51-40-02-0G-0 AND DWG 141A8370.
- [SDR CALA2026030314234](https://openairdocs.org/sdr/CALA2026030314234.md): Web · corroded · Feb 28, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA CORRODED FLOOR SUPPORT, LBL 31, BS 986.5+3. REMOVED AND REPLACED THE LT WEB FROM BS 986.5" & 1016, LBL 31 IAW SRM 51-40-02-0G-0 AND DWG 147A5700.
- [SDR CALA2026030214206](https://openairdocs.org/sdr/CALA2026030214206.md): Floor Support · corroded · Feb 28, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA CORROSION AT FLOOR SUPPORT LBL 15" BETWEEN STA 967-947.5. REMOVED AND REPLACED FLOOR SUPPORT AT MAIN CABIN AFT WET AREA LBL 15" BETWEEN STA 947.5" AND STAQ 967" IAW SRM 51-40-02-0G-0 AND DWG 147A5650.
- [SDR CALA2026030214204](https://openairdocs.org/sdr/CALA2026030214204.md): Floorbeam · cracked · Feb 28, 2026 · N14250 · Boeing 737824 · Fuselage Main, Floor Beam
  > CRACKED: MAIN CABIN FWD WET AREA HAS CRACK AT LH INNER CHORD BS 309. INSTALLED 100% FASTENERS LT INNER CHORD AT L1 DOOR AREA IAW SRM 51-40-02-0G-0 AND DWG 141A8110.
- [SDR CALA2026030214194](https://openairdocs.org/sdr/CALA2026030214194.md): Stringer · corroded · Feb 27, 2026 · N14250 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMP EXFOLIATION CORROSION AT STA STR 25R STA 500G. INSTALLATION OF NEW FWD CARGO COMP STRINGER 25R AND REPAIR SPLICES FROM STA 500D+10" TO 500G+10" PER SRM 53-00-03-2R-1 AND DWG#143A3241.
- [SDR CALA2026030214192](https://openairdocs.org/sdr/CALA2026030214192.md): Floor Support · corroded · Feb 27, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA CORROSION AT FLOOR SUPPORT EDGE RBL 17" 986.5-2". REMOVED AND REPLACED FLOOR SUPPORT AT MAIN CABIN AFT WET AREA RBL 17" BETWEEN STA 967" AND STA 986.5" REF B737 SRM 51-40-02-0G-0 AND DWG 140A9870.
- [SDR CALA2026030214190](https://openairdocs.org/sdr/CALA2026030214190.md): Floor Support · corroded · Feb 27, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA CORROSION AT FLOOR SUPPORT HOLES LBL 15" BETWEEN STA 967-986.5. REMOVED AND REPLACED FLOOR SUPPORT AT MAIN CABIN AFT AREA LBL 15" BETWEEN STA 967" AND STA 986.5" REF B737 SRM 51-40-02-0G-0 AND DWG 140A9870.
- [SDR CALA2026030214188](https://openairdocs.org/sdr/CALA2026030214188.md): Floor Support · corroded · Feb 27, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CABIN AFT WET AREA HAS CORROSION AT UPPER WEB BRACKET ANGLE BETWEEN STA 986.5 AND STA 1006 RBL39. REMOVED AND REPLACED BRACKET ANGLE AT AFT WET AREA BETWEEN STA 986.5" AND STA 1006 RBL 39" REF B737 SRM 51-40-02-0G-0 AND DWG 147A5700.
- [SDR CALA2026030214186](https://openairdocs.org/sdr/CALA2026030214186.md): Web · corroded · Feb 27, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CABIN AFT WET AREA HAS CRACK AT UPPER WEB 967 STA 1016, LBL 32. INSTALLED NEW WEB BETWEEN STA 986.5 TO STA 1016 & BL 0" TO LBL 27.95" IAW B737 SRM 51-40-02 AND DWG 147A5700.
- [SDR CALA2026030214182](https://openairdocs.org/sdr/CALA2026030214182.md): Floor Support · corroded · Feb 27, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CABIN AFT WET AREA HAS CORROSION AT UPPER SURFACE INTERCOSTAL BETWEEN BS 947.5 AND BS 967, LBL 49.5. REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 947.5" AND STA 967, LBL 49.5" REF SRM 51-40-02-0G-0 AND DWG 147A5650.
- [SDR CALA2026030214180](https://openairdocs.org/sdr/CALA2026030214180.md): Floor Support · corroded · Feb 27, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CABIN AFT WET AREA HAS CORROSION BETWEEN BS 986.5 AND BS 1006, LBL 42, LBL 36 UPPER SURFACE WEB BRACKET ANGLE. REMOVED AND REPLACED BRACKET ANGLE AT AFT WET AREA BETWEEN STA 986.5" AND STA 1006" LBL 42" REF SRM 51-40-02-0G-0 AND DWG 147A5700.
- [SDR CALA2026030214178](https://openairdocs.org/sdr/CALA2026030214178.md): Floorbeam · corroded · Feb 27, 2026 · N14250 · Boeing 737824 · Fuselage Main, Floor Beam
  > FORWARD WET AREA FLOORBEAM AT STA312 LBL43 HAS SPOT OF COROSSION. INSTALLED THE REPAIR PARTS (( T-CHORD [1], STRAPS [2], [3] AND ANGLES [4] [5])) AT MAIN CABIN FWD FLOOR STRUCTURE STA 312" BETWEEN LBL 27" TO LBL 63" IAW SRM 53-10-51-2R-12 AND SRM 53-10-51-2
- [SDR CALA2026030214177](https://openairdocs.org/sdr/CALA2026030214177.md): Threshold · corroded · Feb 27, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous Structure
  > (COROSSION) INNERCHORD NEXT TO PAX DOOR THRESHOLD HAVE AREAS OF COROSSION. INSTALLED 100% FASTENERS NEW RIGHT INNER CHORD AT MAIN CABIN FWD FLOOR STRUCTURE RBL 57 BETWEEN BS 270 TO 360 IAW SRM 51-40-02-0G-0 AND DWG 141A8310.
- [SDR CALA2026010812791](https://openairdocs.org/sdr/CALA2026010812791.md): Lens · broken · Jan 6, 2026 · N14250 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS OPERATIONAL CHECK, ROW 11, SEAT C, PROXIMITY LIGHT NEEDS TO BE SECURED OR REPLACED. REPLACED BROKEN LENS CAP AND SECURED. OPS CKD OK.
- [SDR CALA2025110610968](https://openairdocs.org/sdr/CALA2025110610968.md): Rib · cracked · Nov 5, 2025 · N14250 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STAB TIP DAMAGED. REMOVED REMAINING UPPER AND LOWER TRAILING EDGE PANEL AND CLOSURE RIB FITTING IAW AVO15975, STEP 1-2. REMOVED AND REPLACED RIB FITTING, UPPER AND LOWER TRAILING EDGE PANELS AND TIP CAP FAIRING IAW SRM 51-40-02, DWG 182A5
- [SDR CALA2025102110362](https://openairdocs.org/sdr/CALA2025102110362.md): Light · loose · Oct 19, 2025 · N14250 · Boeing 737824 · Emergency Lighting
  > ROW 10 FLOOR SEAT MOUNTED EXIT LIGHT NEEDS RESECURED. - EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK. REMOVED AND REPLACED LIGHT ASSY IAW AMM 33-51-11, LIGHTS OPS CHECK GOOD.
- [SDR CALA2025032803274](https://openairdocs.org/sdr/CALA2025032803274.md): Elec Connector · damaged · Mar 26, 2025 · N14250 · Boeing 737824 · Light System Wiring
  > IN SEAT EMERGENCY LIGHTS INOP AT SEATS 7-14.EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR) {MULT-33-3-0004} - SLAVED IN A NEW CHARGER AT #M1676, NO HELP. CONTINUEING WITH TROUBLESHOOTING, REFERRED TO WM #33-51-21. TROUBLESHOT DOWN TO NO EME

Next page: https://openairdocs.org/aircraft/N14250/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 = 'N14250' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N14250/reports

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