# Service difficulty reports: N14735

A list on [N14735](https://openairdocs.org/aircraft/N14735.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 · 127 reports

- [SDR CALA2026062417314](https://openairdocs.org/sdr/CALA2026062417314.md): Unknown · odor · Jun 23, 2026 · N14735 · Boeing 737724 · Air Distribution System
  > VERY MUSTY ODOR FROM ENVIRON SYS IN COCKPIT & CABIN. CABIN CREW REPORTED THEY DID NOT NOTICE ANY SMOKE OR ODOR THROUGHOUT FLIGHT. BURN OUT HAS BEEN REQUESTED TO CORRECT FAULT PER AMM TASK 05-51-26-800-801-C1 SECTION E. COMPLIANCE ON BURNOUT IAW AMM. NO MU
- [SDR CALA2026061117041](https://openairdocs.org/sdr/CALA2026061117041.md): Spar · corroded · Apr 1, 2026 · N14735 · Boeing 737724 · Wing Spar
  > FOUND CORROSION AT RT WING FRONT SPAR AT BOOST PUMP UPPER BONDING STRAP ATTACH AREA. CORROSION AT AT RT WING FRONT SPAR AT BOOST PUMP UPPER BONDING STRAP ATTACH AREA HAS BEEN REPAIRED IAW ESR-WI NO.: 2024262-35-14824
- [SDR CALA2026033014896](https://openairdocs.org/sdr/CALA2026033014896.md): Web · damaged · Mar 25, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > WEB AT STA351 BL "0" HAS SEVERAL ELONGATED FASTENER HOLES. INSTALLED REPAIR AT STA 351, BETWEEN BL 0 AND RBL 10 AS PER SRM 51-40-02-0G-0, AAR ESR-WI 29-14817 REV IR, AND EC/RA #5310-08844 REV. ORIGINAL.
- [SDR CALA2026032714860](https://openairdocs.org/sdr/CALA2026032714860.md): Stiffener · corroded · Mar 25, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > STIFFENER CORRODED OUT OF LIMITS BETWEEN STA 227.8 AND STA 219.8 BL0. FABRICATED STIFFENER AT FWD E&E BETWEEN STA 227.8 TO STA 219.8, BL"0", REF. DRW 141A3504, AND STANDARD BAC5300, AND INSTALLATION ACCOMPLISHED ON AAR N/R S/N#100007959, AND EC/RA #5310-08847
- [SDR CALA2026033014894](https://openairdocs.org/sdr/CALA2026033014894.md): Frame · corroded · Mar 24, 2026 · N14735 · Boeing 737724 · Fuselage Main, Frame
  > FWD E/E ACCESS FRAME STA 227.8 BL 0 WITH CORROSION AREA. TRIMMED OUT CORRODED AREA AT FWD E/E STA 227.8, BL "0", AND INSTALLED REPAIR. THIS IS A CATEGORY B REPAIR AND REQUIRES INSPECTIONS PER EC/RA# 5310-08847 REV. ORIGINAL, PART 1 STEP 2 & 3. REF SRM 51-10-0
- [SDR CALA2026032314747](https://openairdocs.org/sdr/CALA2026032314747.md): Web · cracked · Mar 20, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > FWD E/E COMP WEB CRACKED AT STA 219.8 BL 0. CUT AND REMOVED DAMAGED SECTION ON WEB STA 219.8 BL"O", AT FWD E/E, AND INSTALLED REPAIR REF EC/RA 5310-08843 REV. ORIGINAL, B737 SRM 51-10-02-0G-0, AND 51-40-02-0G-0.
- [SDR CALA2026031614591](https://openairdocs.org/sdr/CALA2026031614591.md): Channel · corroded · Mar 13, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > AFT CARGO LEFT ZEE CHANNELS HAVE CORROSION FROM BS 727A - 847. REPLACED ZEE CHANNEL IAW SRM 51-40-02-0G-0, AND DWG 146A7500.
- [SDR CALA2026031214522](https://openairdocs.org/sdr/CALA2026031214522.md): Shield · corroded · Mar 11, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > AFT CARGO SHIELD CORRODED, RBL 20, BS 767 - 787. REPLACED THE AFT CARGO SHIELD IAW SRM 51-40-02-0G-0, & DWG 146A8127.
- [SDR CALA2026031214521](https://openairdocs.org/sdr/CALA2026031214521.md): Channel · corroded · Mar 10, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > CORROSION AT SEVERAL SPOTS AND A CRACK AT FWD CARGO LT ZEE CHANNEL, BS 400 - 500D. REPLACED THE FWD CARGO ZEE CHANNELS IAW SRM 51-40-02-0G-0, AND DWG 143A7500.
- [SDR CALA2026031214520](https://openairdocs.org/sdr/CALA2026031214520.md): Shield · corroded · Mar 10, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > CORROSION AT SEVERAL SPOTS AT FWD CARGO BILGE FLOOR STRUCTURE SHIELD. BS 492 - 500A, STRINGER 26R. REPLACED FWD CARGO BILGE FLOOR STRUCTURE SHIELD IAW SRM 51-40-02-0G-0 AND DWG 143A8126.
- [SDR CALA2026031814637](https://openairdocs.org/sdr/CALA2026031814637.md): Frame · cracked · Mar 6, 2026 · N14735 · Boeing 737724 · Fuselage Main, Frame
  > FRAME 727D CRACKED AT OVERHEAD BIN ATTACH BRACKET INBD FASTENER S8L AND S9L. INSTALLED REPAIR AT FRAME 727D BETWEEN S8L AND S9L IAW SRM 51-40-02-0G-0 & EC/RA 5310-07665, REV ORIGINAL.
- [SDR CALA2026031014465](https://openairdocs.org/sdr/CALA2026031014465.md): Rib · cracked · Mar 6, 2026 · N14735 · Boeing 737724 · Horizontal Stabilizer, Spar/Rib
  > EA 5510-01843 REV I OP 002 - (CRACK) R/H HORIZONTAL STABILIZER INSPAR RIBS AT STAB 120.30, SECOND STIFFINER FROM FRONT SPAR, LOWER VERTICAL STIFFINER TRANSITION RADIUS CRACKED. DOT J-14. REF AAR N/R 100007797. INSTALLED REPAIR AT R/H HORIZONTAL STABILIZER INSP
- [SDR CALA2026031014461](https://openairdocs.org/sdr/CALA2026031014461.md): Skin · dented · Mar 5, 2026 · N14735 · Boeing 737724 · Cargo/Baggage Doors
  > REPLACE AFT CARGO DOOR SKIN. REMOVED AND REPLACED AFT CARGO DOOR EXTERNAL SKIN PER SRM 51-40-02-0G-0,SRM 52-30-01-2R-3 AND DWG#146A6110. REMOVED AND REPLACED AFT CARGO DOOR EXTERNAL SKIN IAW SRM 51-40-02-0G-0, SRM 52-30-01-2R-3, AND DWG 146A6110.
- [SDR CALA2026030614380](https://openairdocs.org/sdr/CALA2026030614380.md): Attach Angle · cracked · Mar 4, 2026 · N14735 · Boeing 737724 · Fuselage Main, Attach Fittings
  > VAPOR BARRIER ATTACH ANGLE BS 663, LBL 5 CRACKED. INSTALLED THE VAPOR BARRIER ATTACH ANGLE AND REPAIR SPLICE BS 663, LBL 3 - LBL 20 IAW SRM 57-10-10-2R-5.
- [SDR CALA2026030614379](https://openairdocs.org/sdr/CALA2026030614379.md): Angle · corroded · Mar 4, 2026 · N14735 · Boeing 737724 · APU Cowling/Containment
  > APU COMPARTMENT BULKHEAD LOWER HORIZONTAL ANGLE HAD CORROSION. APU COMPARTMENT BULKHEAD BS 1088 LOWER HORIZONTAL ANGLE REMOVED AND REPLACED IAW SRM 51-40-02-0G-0, PARAGRAPH 9, AND DWG 148A2410.
- [SDR CALA2026030414315](https://openairdocs.org/sdr/CALA2026030414315.md): Support Angle · cracked · Mar 4, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > CRACK AT RIGHT AIRCONDITION BAY AFT WALL MID SUPPORT ANGLE. VAPOR BARRIER BS 663.75 BTWN RBL 6 - RBL 30, THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02-0G-0, AND DWG 111A1000.
- [SDR CALA2026030414313](https://openairdocs.org/sdr/CALA2026030414313.md): Attach Angle · worn · Mar 4, 2026 · N14735 · Boeing 737724 · Fuselage Main, Attach Fittings
  > WEAR AT LOWER FUS ATTACH ANGLE OTBD OF RT RAM AIR EXIT EXHAUST. LOWER FUSELAGE ATTACH ANGLE WAS FOUND TO BE OUT OF LIMITS, ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02-0G-0 AND DWG 149A7216.
- [SDR CALA2026030514345](https://openairdocs.org/sdr/CALA2026030514345.md): Floor Support · corroded · Mar 3, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > AFT WET AREA FLOOR SUPPORT, BS 947.5 - 967.5, LBL 24 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0 & DWG 147A5650.
- [SDR CALA2026031214514](https://openairdocs.org/sdr/CALA2026031214514.md): Skin · dented · Feb 28, 2026 · N14735 · Boeing 737724 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN DENTED BS 1016+3 AND BELLOW STRINGER 13L INSTALLED A REPAIR, BS 1016, STRINGER 13L IAW SRM 51-40-02-0G-0 AND SRM 53-80-01-2R-6 FIGURE 202 DETAIL A.
- [SDR CALA2026030314228](https://openairdocs.org/sdr/CALA2026030314228.md): Channel · corroded · Feb 28, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY, RT ZEE CHANNELS HAVE CORROSION. REPLACED THE AFT CARGO RT ZEE CHANNEL FROM BS 727 - 767 IAW SRM 51-40-02-0G-0, AND DWG 146A7500.
- [SDR CALA2026022614107](https://openairdocs.org/sdr/CALA2026022614107.md): Floor Support · cracked · Feb 25, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > FWD WET AREA FLOOR SUPPPORT BS 294.5 - 312, RBL 15, CRACKED ON UPPER SURFACE. R & R THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 141A5400.
- [SDR CALA2026022614099](https://openairdocs.org/sdr/CALA2026022614099.md): Floorbeam · corroded · Feb 24, 2026 · N14735 · Boeing 737724 · Fuselage Main, Floor Beam
  > CORROSION - FWD WET AREA FLOORBEAM TEE WITH SURFACE CORROSION SPOTS AT BS 294.5 RBL 18 & RBL 28. AT BS 294.5 UPPER CHORD CORROSION BETWEEN RBL 18 AND RBL 28 FOUND OUT OF LIMITS, REPAIR MAIN CABIN FWD WET AREA FLOOR BS 294.5 BETWEEN RBL25 - LBL21 IAW SRM 53-10
- [SDR CALA2026022614092](https://openairdocs.org/sdr/CALA2026022614092.md): Tie Down · corroded · Feb 24, 2026 · N14735 · Boeing 737724 · Fuselage Main, Structure
  > L1 DOOR TIE DOWN FITTING AT STA 312 HAS EXFOLIATING CORROSION REF AAR N/R 100007609. REMOVED AND REPLACED FITTING L1 DOOR FWD AT STA 312 IAW SRM 51-40-02-0G -0, AND AIPC 53-42-00-29. LOGPAGE 8010828 ESFR ENTERED. REMOVED AND REPLACED FITTING L1 DOOR FWD AT
- [SDR CALA2026022414038](https://openairdocs.org/sdr/CALA2026022414038.md): Floor Support · corroded · Feb 23, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > FWD WET AREA FLOOR STRUCTURE FLOOR SUPPORT BS 312 - 328, LBL 11 WITH SCRATCH ON UPPER SURFACE. REMOVED AND REPLACED FLOOR SUPPORT AT MAIN CABIN FWD WET AREA STA 312 TO STA 328 LBL 11 REF. SRM 51-40-02-0G-0 AND DWG 141A5400.
- [SDR CALA2026022614072](https://openairdocs.org/sdr/CALA2026022614072.md): Floorbeam · corroded · Feb 22, 2026 · N14735 · Boeing 737724 · Fuselage Main, Floor Beam
  > AFT WET AREA FLOORBEAM, BS 947.5, RBL 50 HARD POINT AREA CORRODED IN SPOTS. THE FLOORBEAM WAS REMOVED AND INSTALLED A TEE ANGLE REPAIR IAW SRM SRM-53-70-21-2R-5, SRM 51-40-02-0G-0, & DWG 147A8501.
- [SDR CALA2026022414032](https://openairdocs.org/sdr/CALA2026022414032.md): Door Frame · corroded · Feb 21, 2026 · N14735 · Boeing 737724 · Fuselage Main, Structure
  > L1 DOOR CUTOUT INNER CHORD UPPER SURFACE WITH SEVERAL CORROSION AREAS. REMOVED AND REPLACED LEFT INNER CHORD AT MAIN CABIN FWD WET AREA IAW REF. SRM 53-10-15-1A-1, 51-40-02-0G-0, AND DWG # 141A8110. L1 INNER CHORD FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-
- [SDR CALA2026022314011](https://openairdocs.org/sdr/CALA2026022314011.md): Floorbeam · corroded · Feb 21, 2026 · N14735 · Boeing 737724 · Fuselage Main, Floor Beam
  > CORRODED AFT WET AREA FLOORBEAM UPPER TEE ANGLE, BS 986, BL 0 TO RBL 45 HAD SEVERAL CORROSION SPOTS. THE FLOORBEAM UPPER TEE WAS REMOVED AND INSTALLED A REPAIR IAW SRM 53-70-51-2R-4, SRM 51-40-02-0G-0, & DWG 147A5700.
- [SDR CALA2026022313988](https://openairdocs.org/sdr/CALA2026022313988.md): Floor Support · corroded · Feb 20, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > AFT WET AREA FLOOR SUPPORT ANGLE AT STA 947.5 - 967.5 LBL 51 WITH CORROSION SPOTS. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW B737-700 SRM 51-40-02-0G-0 & DWG 147A5650.
- [SDR CALA2026022313987](https://openairdocs.org/sdr/CALA2026022313987.md): Floor Support · corroded · Feb 20, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > AFT WET AREA FLOOR SUPPORT ANGLE AT STA 947.5 + 4 LBL 42 WITH CORROSION SPOTS. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW B737-700 SRM 51-40-02-0G-0 & DWG 147A5650.
- [SDR CALA2026022313985](https://openairdocs.org/sdr/CALA2026022313985.md): Floor Support · corroded · Feb 20, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > AFT WET AREA FLOOR SUPPORT ANGLE AT STA 986.5 +6 LBL 37 WITH CORROSION SPOTS. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IN REF TO B737-700 SRM 51-40-02-0G-0 & DWG 147A5700.
- [SDR CALA2026022313983](https://openairdocs.org/sdr/CALA2026022313983.md): Door Frame · corroded · Feb 20, 2026 · N14735 · Boeing 737724 · Fuselage Main, Structure
  > L2 DOOR CUTOUT INNER CHORD WITH SEVERAL CORROSION SPOTS. REMOVED AND REPLACED L2 INNER CHORD IAW SRM 51-40-02-0G-0 AND DWG 147A8501.
- [SDR CALA2026092319705](https://openairdocs.org/sdr/CALA2026092319705.md): Bulkhead Web · cracked · Feb 19, 2026 · N14735 · Boeing 737724 · Fuselage Main, Bulkhead
  > VERTICAL PRESSURE DECK WEB CRACKED 4 INCH BELOW HORIZONTAL DECK AT STA 663 RBL 34. INSTALLED A REPAIR IAW SRM 57-10-10-2R-3, ALTERNATIVE 2.
- [SDR CALA2026031814636](https://openairdocs.org/sdr/CALA2026031814636.md): Structure · corroded · Feb 19, 2026 · N14735 · Boeing 737724 · Service Doors
  > R2 DOOR CUTOUT INNER CHORD WITH SEVERAL CORROSION AREAS ON UPPER SURFACE. REMOVED AND REPLACED R2 INNER CHORD IAW SRM 51-40-02-0G-0 AND DWG 147A8501. REMOVED AND REPLACED R2 INNER CHORD IAW SRM 51-40-02-0G-0 AND DWG 147A8501.
- [SDR CALA2026031714612](https://openairdocs.org/sdr/CALA2026031714612.md): Web · corroded · Feb 19, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > CORROSION - AFT WET AREA WEB UPPER SURFACE AT STA 986.5 + 1 RBL 33 WITH CORROSION SPOTS. REF AAR N/R 100007269 AT AFT WET AREA WEB STA 986.5+1 & RBL 33. REMOVED AND REPLACED WEB IN REF TO B737-700 SRM 51-40-02-0G-0 & DWG 147A5700. REMOVED AND REPLACED WEB IN
- [SDR CALA2026030214147](https://openairdocs.org/sdr/CALA2026030214147.md): Floor Support · corroded · Feb 18, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > FWD WET AREA FLOOR SUPPORT BS 294.5-312, RBL 10 WITH CORROSION AT FASTENER HOLES. REMOVED AND REPLACED THE FLOOR SUPPORT AT FWD WET AREA FLOOR STRUCTURE BETWEEN BS 294.5 TO BS 312, RBL 10 IAW SRM 51-40-02-0G-0 AND DWG 141A5410.
- [SDR CALA2026022013933](https://openairdocs.org/sdr/CALA2026022013933.md): Floor Support · corroded · Feb 18, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > FWD WET AREA FLOOR SUPPORT BS 312-328, RBL 10 CORRODED AT FASTENER HOLES. REMOVED & REPLACED FLOOR SUPPORT BETWEEN BS 312 - 328, RBL 10, SRM 51-40-02-0G-0, AND DWG 141A5410.
- [SDR CALA2026031214513](https://openairdocs.org/sdr/CALA2026031214513.md): Floorbeam · cracked · Feb 17, 2026 · N14735 · Boeing 737724 · Fuselage Main, Floor Beam
  > AIR CONDITIONING DISTRIBUTION BAY AFT OF FWD CARGO BS 540 CENTER RT FLOORBEAM CRACKED. REF AAR N/R 100007543, R & R THE FLOORBEAM IAW SRM 51-40-02-0G-0, HOLE SIZES SRM 51-40-05-0G-0.
- [SDR CALA2026022313974](https://openairdocs.org/sdr/CALA2026022313974.md): Floor Support · scratched · Feb 17, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > SCRATCH - FWD WET AREA FLOOR STRUCTURE FLOOR SUPPORT STA 328 - 344 LBL 11 WITH SCRATCH ON UPPER SURFACE. REF AAR N/R 100007400 REMOVED AND REPLACED FWD WET AREA FLOOR SUPPORT STA328 TO STA344, LBL11, REF. SRM 51-40-02-0G-0, DWG #141A5400.
- [SDR CALA2026022013930](https://openairdocs.org/sdr/CALA2026022013930.md): Floorbeam · cracked · Feb 17, 2026 · N14735 · Boeing 737724 · Fuselage Main, Floor Beam
  > AIR CONDITIONING DISTRIBUTION BAY, AFT OF FWD CARGO BS 540 CENTER LEFT FLOORBEAM CRACKED BS 540 BL 0 - LBL 24. REMOVED AND REPLACED FLOORBEAM ANGLE IAW SRM 51-40-02-0G-0,
- [SDR CALA2026021113698](https://openairdocs.org/sdr/CALA2026021113698.md): Floor Support · corroded · Feb 10, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > FWD WET AREA FLOOR STRUCTURE FLOOR SUPPPORT BS 294.5 -312, RBL 41 WITH SURFACE CORROSION SPOT. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02 -G-0, SRM 51-40-05-0G-0, SRM 51-20-01-0G-0, AND AMM 51-21-72-370-804.
- [SDR CALA2026021113697](https://openairdocs.org/sdr/CALA2026021113697.md): Floor Support · cracked · Feb 10, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous Structure
  > FWD WET AREA FLOOR STRUCTURE UPPER ANGLE BS 380 - 400, BL 0 CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0.
- [SDR CALA2025120811828](https://openairdocs.org/sdr/CALA2025120811828.md): Girt Bar · no discrepancy · Dec 5, 2025 · N14735 · Boeing 737724 · Emergency Equipment
  > 1R GIRT BAR DIFFICULT TO OPERATE. EXCESSIVE DRAG PERFORMED OPERATIONAL CHECK OF DOOR 1R IAW AMM 52-00-00, OPS CHECKED GOOD, DOOR CLOSES FINE. PERFORMED ESCAPE SLIDE PACK CHECK OF DOOR 1R IAW AMM 25-66-01, OPS CHECK GOOD, GIRT BAR STOWED CORRECTLY.
- [SDR CALA2025120411781](https://openairdocs.org/sdr/CALA2025120411781.md): Windshield · failed · Dec 1, 2025 · N14735 · Boeing 737724 · Flight Compartment Windows
  > FO OUTTER PANE SHATTERED. PERFORMED R1 WINDOW REMOVAL IAW AMM 56-11-11-000-801 UP TO AND INCLUDING STEP (11) SUBTASK (56-11-11-020-031). REMOVED AND REPLACED THE R1 WINDSHIELD IAW AMM 56-11-11. LEAK CHECKED GOOD. OK FOR SERVICE.
- [SDR CALA2025111811290](https://openairdocs.org/sdr/CALA2025111811290.md): Window Frame · damaged · Nov 16, 2025 · N14735 · Boeing 737724 · Fuselage Main, Structure
  > FOUND DAMAGE POSSIBLE LIGHTNING STRIKE ON THE L3 WINDOW FRAME POST, NR 2 HOLE REQUIRE FURTHER EVALUTION. ACCOMPLISHED PERMANENT REPAIR ON L3 WINDOW FRAME POST IAW EO 250412 REV IR & ECRA 5310-08724.
- [SDR CALA2025101309928](https://openairdocs.org/sdr/CALA2025101309928.md): Switch · dirty · Oct 10, 2025 · N14735 · Boeing 737724 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS COMES ON AND OFF IN FLIGHT CHECKED AND CLEANED EMERGENCY LIGHT SWITCHES ON P5 PANEL AND AFT FAP, SWITCHES SECURE AND DID NOT CAUSE LIGHT TO GO ON AND OFF. OPERATIONALY CHECKED LIGHT WITH SAME SWITCHES AND LIGHTS OP NORMAL REF AMM 33-51-0
- [SDR CALA2025070806327](https://openairdocs.org/sdr/CALA2025070806327.md): Slide · out of adjust · Jul 5, 2025 · N14735 · Boeing 737724 · Escape Slide
  > 1R DOOR INSIDE SLIDE MATERIAL SHOWING. RE-POSITIONED 1R DOOR GIRT BAR AND BUSTLE/COVER ASSEMBLY REF AMM TASK 25-66-01-200-802. EXCESS SLIDE MATERIAL NO LONGER SHOWING OUTSIDE OF THE BUSTLE/COVER ASSEMBLY.
- [SDR CALA2024112701316](https://openairdocs.org/sdr/CALA2024112701316.md): None · no discrepancy · Nov 25, 2024 · N14735 · Boeing 737724 · Standard Practices/Structures
  > DOOR 1R DISARMING BRACKET IS TIGHT INSPECTED DOOR SLIDE ARMING SYSTEM, NO FAULTS NOTED. DISARM BRACKETS ALSO CK GOOD.
- [SDR CALA2024111101105](https://openairdocs.org/sdr/CALA2024111101105.md): Battery Pack · no test · Nov 10, 2024 · N14735 · Boeing 737724 · Emergency Lighting
  > FOUND M1672 AND M1673 BATTERY PACK FAIL FUNCTIONAL CHECK IAW JOBCARD EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR) {MULT-33-3-0004} - REMOVED AND REPLACED EMERGENCY BATTERY PACK M1672 AND M1673 IAW AMM 33-51-06-960-805 OPS CHECK GOOD
- [SDR CALA2024103000972](https://openairdocs.org/sdr/CALA2024103000972.md): Slide · out of adjust · Oct 28, 2024 · N14735 · Boeing 737724 · Escape Slide
  > FA REPORTS DOOR 1R HAS MATERIAL COMING OUT OF BOTTOM WORRIED ABOUT INTEGRITY ADJUSTED SLIDE PACK REF AMM 52-11-00. OPS CHECK GOOD.
- [SDR CALA2024030500639](https://openairdocs.org/sdr/CALA2024030500639.md): Panel · missing · Mar 2, 2024 · N14735 · Boeing 737724 · Fuselage Main, Structure
  > PDA FAIRING 193AL FWD OF LH WHEEL WELL FOUND MAJORITY OF PANEL MISSING FROM AIRCRAFT. REPLACEMENT PANEL ARRIVED PRE-DRILLED, AND HOLES DO NO ALIGN WITH NUTPLATES, INSTALLED REPLACEMENT PANEL.

Next page: https://openairdocs.org/aircraft/N14735/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 = 'N14735' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N14735/reports

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