# Service difficulty reports: N24736

A list on [N24736](https://openairdocs.org/aircraft/N24736.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 · 119 reports

- [SDR CALA2026082318812](https://openairdocs.org/sdr/CALA2026082318812.md): Unknown · odor · Aug 22, 2026 · N24736 · Boeing 737724 · Air Distribution System
  > SMOKE ODOR, WHEN WE TURNED ON AIR FROM APU. OPERATED APU BLEED, RAN BOTH PACKS. NO ODOR OF SMOKE. CREW VERBALLY NOTIFIED MX OF NO ODOR OF SMOKE. IAW AMM 49-11-00, TASK 36-00-00-860-803, TASK 21-00-00-800-803.
- [SDR CALA2026082718980](https://openairdocs.org/sdr/CALA2026082718980.md): Pressure Web · cracked · May 14, 2026 · N24736 · Boeing 737724 · Fuselage Main, Structure
  > CRACK FOUND AT VERTICAL PRESSURE WEB BETWEEN RBL 40.00 AND RBL 45.64. CRACK LENGTH 1". (REF AAR N/R 100012821)CUT AND REMOVED DAMAGED PART,FABRICATED AND INSTALLED NEW REPAIR PART, [1] REPAIR WEB, NEW [2], NEW [3] FILLERDOUBLER, [5] SHIM, AT STA 663 FROM RB
- [SDR CALA2026083119110](https://openairdocs.org/sdr/CALA2026083119110.md): Skin · cracked · Apr 18, 2026 · N24736 · Boeing 737724 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT RT HORIZONTAL STAB LOWER SKIN AT HSS 101.90, 13 INCHES FROM REAR SPAR, INBD ROW. CRACK LENGTH 1". ACCOMPLISHED REPAIR ON THE RT HORZ STAB LOWER SKIN IAW SRM 55-10-01-2R-11.
- [SDR CALA2026041615407](https://openairdocs.org/sdr/CALA2026041615407.md): Angle · corroded · Apr 15, 2026 · N24736 · Boeing 737724 · APU Cowling/Containment
  > APU COMPARTMENT LEFT SIDE LOWER FRAME HAS LIGHT CORROSION IN SEVERAL SPOTS. ACCOMPLISHED ESFR FORM AS PER GMM 04-20-05. REMOVED AND REPLACED APU COMPARTMENT LEFT SIDE LOWER FRAME PER SRM 51-40-02-0G-0 AND DWG 148A8600.
- [SDR CALA2026041015249](https://openairdocs.org/sdr/CALA2026041015249.md): Channel · corroded · Apr 9, 2026 · N24736 · Boeing 737724 · Fuselage Miscellaneous Structure
  > AFT CARGO LEFT "Z" CHANNEL HAS CORROSION AT 727A-827 REF AAR N/R 100013217 REMOVED AND REPLACED AFT CARGO LEFT "Z" CHANNEL ASSY AT STA 727A-827, LBL 21 AS PER SRM 51-40-02-0G-0. PENDING ESFRY ENTRY, NO DIPS REQUIRED. WORK ACCOMPLISHED BY V 928495 REMOVED AND R
- [SDR CALA2026040915242](https://openairdocs.org/sdr/CALA2026040915242.md): Floorbeam · corroded · Apr 8, 2026 · N24736 · Boeing 737724 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR STRUCTURE WET AREA BS 328, RBL 45.5, FLOORBEAM HAS CORROSION. CUT THE DAMAGED FLANGES OF THE UPPER TEE OF FLOORBEAM AT MAIN CABIN FLOOR STRUCTURE WET AREA BS 328, FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-51-2R-7.
- [SDR CALA2026040715142](https://openairdocs.org/sdr/CALA2026040715142.md): Skin · cracked · Apr 4, 2026 · N24736 · Boeing 737724 · Leading Edge Devices
  > RIGHT WING LEADING EDGE SLAT # 8 SKIN CRACK AT ACTUATOR ATTACH POINT. FABRICATED AND INSTALLED REPAIR PARTS DOUBLER AND FILLER MATERIAL AT R/WING LEADING EDGE SLAT NR 8 LOWER SKIN AT ACTUATOR ATTACH IAW SRM 57-42-01-2R-8, FIG 202, SHEET 1.
- [SDR CALA2026040615098](https://openairdocs.org/sdr/CALA2026040615098.md): Floorbeam · corroded · Apr 4, 2026 · N24736 · Boeing 737724 · Fuselage Main, Floor Beam
  > PASSENGER CABIN AFT WET AREA FLOOORBEAM AT BS 947.5, LBL 45 FITTING AREAS FLANGE HAS EXFOLIATION CORROSION. ACCOMPLISHED REPAIR AT AFT WET AREA FLOORBEAM BS 947.5, LBL 45 IAW SRM 53-70-51-2R-5, ESR 4-15014 AND ECRA 5370-01225.
- [SDR CALA2026040615095](https://openairdocs.org/sdr/CALA2026040615095.md): Floor Support · corroded · Apr 3, 2026 · N24736 · Boeing 737724 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR STRUCTURE WET AREA BETWEEN STA 328 TO 294.5 R1 INNER CHORD HAS CORROSION. REMOVED AND REPLACED INNER CHORD AT MAIN CABIN R1 DOOR FLOOR STRUCTURE WET AREA BETWEEN STA 294.5 TO 328 PER SRM 51-40-02-0G-0 AND DWG #141A8310.
- [SDR CALA2026040215042](https://openairdocs.org/sdr/CALA2026040215042.md): Floor Support · corroded · Apr 1, 2026 · N24736 · Boeing 737724 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR STRUCTURE WET AREA BETWEEN STA 312 AND 294.5 L1 INNER CHORD HAS CORROSION (DOT50-008) (REF AAR N/R 100013049) REMOVED AND INSTALLED MAIN CABIN FLOOR STRUCTURE L1 NEW INNER CHORD AS PER REF B737 SRM 51-40-02-0G-0. DWG141A8110.
- [SDR CALA2026040215040](https://openairdocs.org/sdr/CALA2026040215040.md): Floorbeam · corroded · Mar 31, 2026 · N24736 · Boeing 737724 · Fuselage Main, Floor Beam
  > PASSENGER CABIN AFT WET AREA FOUND CORROSION BETWEEN STA. 986.5 AND RBL-45 REF AAR N/R 100013087. REMOVED DAMAGED AREAS, FABRICATED AND INSTALLED, REPAIR PARTS T-FITTING (2EACH), ANGLES REPAIR (2EACH),STRAP (2EACH), RECEIVED SHEAR TIE AS PER REF B737 SRM 53
- [SDR CALA2026040115007](https://openairdocs.org/sdr/CALA2026040115007.md): Floor Support · corroded · Mar 31, 2026 · N24736 · Boeing 737724 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN AFT WET AREA FOUND CORROSION BETWEEN STA. 947.5 & 967 AND LBL-24. REMOVED AND REPLACED NEW FLOOR SUPPORT AT MAIN CABIN AFT WET AREA BETWEEN STA 947.5 AND STA 967 LBL-24 AS PER SRM 51-40-02-0G-0, DWG 147A5650.
- [SDR CALA2026040115006](https://openairdocs.org/sdr/CALA2026040115006.md): Floor Support · corroded · Mar 31, 2026 · N24736 · Boeing 737724 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN AFT WET AREA FOUND CORROSION ON STRUCTURAL ELEMENT LOCATED BETWEEN STA. 967 AND 947.5 RBL-42 REMOVED AND REPLACED NEW FLOOR SUPPORT INTERCOSTAL BETWEEN STA 947 TO STA 967 RBL-50 REF SRM 51-40-02-0G-0 STEP 8.C FIGURE 12 AND DWG#147A5650 SHEETS
- [SDR CALA2026040115005](https://openairdocs.org/sdr/CALA2026040115005.md): Floor Support · corroded · Mar 31, 2026 · N24736 · Boeing 737724 · Fuselage Miscellaneous Structure
  > (CORROSION) PASSENGER CABIN AFT WET AREA FOUND CORROSION AT DOOR R2 FLOOR STRUCTURE ENTRY ANGLE REF AAR N/R 100013086 REMOVED AND REPLACE NEW INNER CHORD R2(ENTRY ANGLE) AT STA 887+2 TO 1006 IAW B737 DWG. 147A8501, SRM 51-40-02-0G-0. INSP HAS BEEN C/W. RE
- [SDR CALA2026041015247](https://openairdocs.org/sdr/CALA2026041015247.md): Angle · corroded · Mar 30, 2026 · N24736 · Boeing 737724 · Passenger/Crew Doors
  > PASSENGER CABIN AFT WET AREA FOUND CORROSION AT ENTRY ANGLE (L2) FLOOR STRUCTURE FROM BS 907 TO BS 992.8. REMOVED AND REPLACED INNER CHORD L2 AT STA 887+2 TO 1006 IAW DWG 147A8501, SRM 51-40-02-0G-0.
- [SDR CALA2026033114971](https://openairdocs.org/sdr/CALA2026033114971.md): Support Angle · corroded · Mar 30, 2026 · N24736 · Boeing 737724 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN AFT WET AREA FLOOR STRUCTURE FOUND CORROSION BERWEEN STA. 986.5 +8 AND LBL-31. REMOVED AND INSTALLED NEW SUPPORT ANGLE AT BS 986.5+8, LBL 31 IAW SRM 51-40-02-0G-0 AND DWG 147A5700.
- [SDR CALA2026032714863](https://openairdocs.org/sdr/CALA2026032714863.md): Floor Support · cracked · Mar 25, 2026 · N24736 · Boeing 737724 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR STRUCTURE WET AREA BETWEEN STA 328 AND 344 LBL 30. FLOOR SUPPORT HAS CRACK. REMOVED AND REPLACE FLOOR SUPPORT (INTERCOSTAL) AT MAIN CABIN FLOOR STRUCTURE WET AREA BETWEEN STA 328 AND STA 344, LBL 30 PER BOEING DRAWING 141A5410-16, SRM 51-40-0
- [SDR CALA2026032414805](https://openairdocs.org/sdr/CALA2026032414805.md): Floorbeam · corroded · Mar 23, 2026 · N24736 · Boeing 737724 · Fuselage Main, Floor Beam
  > PASSENGER CABIN AFT WET AREA FLOOR STRUCTURE FOUND CORROSION BETWEEN STA. 947.5 AND RBL-20 REF AAR N/R 100013085 REMOVED, FABRICATED NEW REPAIR PARTS (T CHORD, 2 ANGLE S, 2 STRAPS) AND REINSTALLED AT LBL 4 TO RBL 55 STA 947.5 REF B737-700 SRM 51-40-02-0G-0, S
- [SDR CALA2026032414804](https://openairdocs.org/sdr/CALA2026032414804.md): Floor Support · cracked · Mar 21, 2026 · N24736 · Boeing 737724 · Fuselage Miscellaneous Structure
  > (59-5305-1-0003) MAIN CABIN FLOOR STRUCTURE WET AREA FLOOR SUPPORT AT BL0 BETWEEN STA 277 AND 294.5 HAS CRACK.REF AAR NR 100013045. REMOVED AND REPLACED FLOOR SUPPORT(INTERCOSTAL) AT MAIN CABIN FLOOR STRUCTURE WET AREA AT BLO BETWEEN STA 277 AND STA 294.5 PE
- [SDR CALA2026011512974](https://openairdocs.org/sdr/CALA2026011512974.md): Battery Pack · no test · Jan 14, 2026 · N24736 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACKS, M1674 FAILED FUNCTIONAL CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1674, IAW AMM 33-51-06-960-806. TEST CHECKS GOOD.
- [SDR CALA2026011512972](https://openairdocs.org/sdr/CALA2026011512972.md): Window Frame · cracked · Jan 13, 2026 · N24736 · Boeing 737724 · Fuselage Main, Structure
  > L3 WINDOW FRAME, 5TH HOLE UP FROM BOTTEM CRACKED. PERFORMED REPAIR ON L3 WINDOW FRAME IAW EO 250467 REV. P1, EO 250467 REV. P2, EO 250467 REV. P2 RED LINE, EO 250467 REV. IR AND EC/RA 5310-08766.
- [SDR CALA2026011512971](https://openairdocs.org/sdr/CALA2026011512971.md): Window Frame · cracked · Jan 12, 2026 · N24736 · Boeing 737724 · Fuselage Main, Structure
  > R3 WINDOW FRAME CUTOUT EDGE MARGIN OUT OF LIMITS IAW EA 5310- 08195, REV C. PERFORMED REPAIR TO THE R3 WINDOW FRAME E-F POST IAW EC/RA 5310-08770.
- [SDR CALA2025092409204](https://openairdocs.org/sdr/CALA2025092409204.md): Switch · malfunctioned · Sep 21, 2025 · N24736 · Boeing 737724 · Door Warning System
  > LEFT OVERWING DOOR LIGHT HAS FLASHED TWICE DOOR IS SECURED & VERIFIED BY FA.S. FOUND LOW SWITCH DISAGREE MSG 52-72020. ITEM HAS HISTORY. DOOR VERIFIED CLOSED. REQUESTING MEL. MEL COMPLIED WITH PERFORMED PSEU BITE TEST & RECONFIRMED 52-72020 LT OVRWG SW DISAG
- [SDR CALA2025071706675](https://openairdocs.org/sdr/CALA2025071706675.md): Start Valve · faulted · Jul 16, 2025 · N24736 · Boeing 737724 · Engine Start Valves/Controls
  > NUMBER 2 START VALVE OPEN LIGHT FLASHING ON TAKEOFF REMOVED ENG #2 START VALVE & PULLED ASSOCIATED CB REF AMM TASK 80-11-03-000-801-F00 UPDATED LABOR AND GROUND TIME. REMOVED AND REPLACED THE NUMBER 2 ENGINE STARTER SHUTOFF VALVE IN REF TO AMM 80-11-03-400-801
- [SDR CALA2025052704983](https://openairdocs.org/sdr/CALA2025052704983.md): Skin · dented · May 25, 2025 · N24736 · Boeing 737724 · Cargo/Baggage Doors
  > MULTIPLE DENTS FOUND ON AFT CARGO DOOR EXTERNAL REPAIR DOUBLER DURING D CHECK AT AAR-MIA.WORK REPAIR ACCOMPLISHED PER AAR NON-ROUTINE 99878446 AND ECRA 5231-01134 REV A PART 1 STEPS 1 THRU 6. INSPECTION DIP INITIATED FOR ON OR BEFORE THE ACCUMULATION OF 50,00
- [SDR CALA2025050204420](https://openairdocs.org/sdr/CALA2025050204420.md): Battery Pack · discharged · Apr 30, 2025 · N24736 · Boeing 737724 · Emergency Lighting
  > CABIN EMERGENCY ISLE PATH LIGHTING AT SEAT ROWS 3 THROUGH 11 INOP. CHARGED EMERGENCY EXIT BATTERY PACKS PER AMM 33-51-06-610-802. ALL EMERCENGY EXITS LIGHTS CHECKED GOOD.
- [SDR CALA2025042404193](https://openairdocs.org/sdr/CALA2025042404193.md): Connector · disconnected · Apr 23, 2025 · N24736 · Boeing 737724 · Light System Wiring
  > EMERGENCY LIGHT AT 26ABC INOP. RECONNECTED CONNECTOR D11334.
- [SDR CALA2025031102692](https://openairdocs.org/sdr/CALA2025031102692.md): Light · inoperative · Mar 7, 2025 · N24736 · Boeing 737724 · Emergency Lighting
  > EMG EXIT LIGHT BROKEN. INVESTIGATE EMERGENCY EXIT INSTALLATION AT SEAT ROW 31C AND CONFIRM THAT INSTALLATION IS ACCEPTABLE PER AMM 33-51-02/201. REPLACED SEAT 31C EMERGENCY LIGHT ASSEMBLY. OPS CK OK
- [SDR CALA2025012402032](https://openairdocs.org/sdr/CALA2025012402032.md): None · none · Jan 23, 2025 · N24736 · Boeing 737724 · Standard Practices/Structures
  > OIL LEAK SPOTTED BOTTOM INSIDE LEFT ENG COWL DURING PREFLIGHT SUBSTANCE HAD SMELL AND CONSISTANCY OF TYPE I DEICING FLUID. INSPECTED FAN INLET SECTION AND DID NO OBSERVE ANY LEAKS AT THIS TIME.
- [SDR CALA2024123101726](https://openairdocs.org/sdr/CALA2024123101726.md): Battery Pack · no test · Dec 27, 2024 · N24736 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1673 FAILED CAPACITY CHECK.....EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR) {MULT-33-3-0004} - REPLACED BATTERY PACK AS PER MM 33-51-06, OPS CKS GOOD
- [SDR CALA2024123101725](https://openairdocs.org/sdr/CALA2024123101725.md): Battery Pack · no test · Dec 27, 2024 · N24736 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1668 FAILED CAPACITY CHECK....EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR) {MULT-33-3-0004} - REPLACED BATTERY PACK AS PER MM 33-51-06, OPS CKS GOOD
- [SDR CALA2024123001708](https://openairdocs.org/sdr/CALA2024123001708.md): Battery Pack · no test · Dec 27, 2024 · N24736 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1672 FAILED CAPACITY CHECK.....EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR) {MULT-33-3-0004} - REPLACED BATTERY PACK AS PER MM 33-51-06, OPS CKS GOOD
- [SDR CALA2024123001705](https://openairdocs.org/sdr/CALA2024123001705.md): Battery Pack · inoperative · Dec 27, 2024 · N24736 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1675 FAILED CAPACITY CHECK.....EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR) {MULT-33-3-0004} - REPLACED BATTERY PACK AS PER MM 33-51-06, OPS CKS GOOD
- [SDR CALA2024123001703](https://openairdocs.org/sdr/CALA2024123001703.md): Battery Pack · inoperative · Dec 27, 2024 · N24736 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1670 FAILED CAPACITY CHECK.....EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR) {MULT-33-3-0004} - REPLACED BATTERY PACK AS PER MM 33-51-06, OPS CKS GOOD
- [SDR CALA2024112101230](https://openairdocs.org/sdr/CALA2024112101230.md): Sensor · dirty · Nov 21, 2024 · N24736 · Boeing 737724 · Auto Flight System
  > DURING TAKEOFF AT APPROX 80KTS THE TAKEOFF CFG WARNING SOUNDED WITH LE FLAPS LIGHT ILLUMINATED. DIGITAL FLIGHT CONTROL SYSTEM (DFCS) BITE PROCEDURE AND FIM 22-12 TASK 812, AND AMM 22-11-30-820-801. ACCOMPLISHED A DIGITAL FLIG HT CONTROL SYSTEM (DFCS) BIT
- [SDR CALA2024110400995](https://openairdocs.org/sdr/CALA2024110400995.md): Module · faulty · Nov 2, 2024 · N24736 · Boeing 737724 · Landing Gear System
  > GEAR DID NOT RETRACT ON TAKEOFF.NOR DID IT COME UP WITH LANDING GEAR OVERIDE. SPEEDBRAKE DID DEBRIEFED CREW, THEY SAID WHEN LIFTING GEAR HANDLE, THEY COULD NOT GET IT TO RAISE ALL THE WAY, IT WOULD ONLY GO UP MAYBE AN INCH. THEY TRIED WITH THE OVERIDE AND IT S
- [SDR CALA2024091000612](https://openairdocs.org/sdr/CALA2024091000612.md): Proximity Sensor · faulted · Sep 7, 2024 · N24736 · Boeing 737724 · Leading Edge Slat Position Indicating System
  > LEADING EDGE FLAPS TRANSIT LIGHT STAYS ON 2 AFTER TAKEOFF LE FLAPS TRANSIT LIGHT REMAINED ON WITH FLAPS AT 5. DEBRIEFED FLIGHT CREW. FLAPS 5 TAKEOFF, ON CLIMBOUTRECIEVED OVERHEAD IN FO ANNUNC PNL, FOUND #2 LE KRUGER FLAP ILLUMINATED AMBER IN TRANSIT, CREW RAN
- [SDR CALA2024072502098](https://openairdocs.org/sdr/CALA2024072502098.md): Skin · corroded · Jul 19, 2024 · N24736 · Boeing 737724 · Fuselage Main, Plate/Skin
  > FOUND CORROSION AROUND THE LAVATORY EXHAUST PORT PICTURES ADDED UPDATE PERFORMED HFEC PER 737 NDT PART6, PROCEDURE 23,ALONG CUT OUT EDGES. NO DEFECTS NOTED. PERFORMED STEPS A-D PARA 4 OF SRM 53-70-01-2R-3. HFEC REQUIRED AROUND EDGE OF DAMAGE TRIM OUT REF SRM
- [SDR CALA2023062101952](https://openairdocs.org/sdr/CALA2023062101952.md): Panel · corroded · Jun 19, 2023 · N24736 · Boeing 737724 · Wing Structure
  > TWO AREAS OF CORROSION FOUND ON THE RH WING LOWER WINGTIP PANEL BETWEEN WBL 616.75 TO 658.17 WHILE AT GYR C-CHECK. BOTH LOCATION S WERE BLENDED AND ONE LOCATION REQUIRED A CUTOUT AND DOUBLER RE INFORCEMENT. THE REPAIR IS CONSIDERED AN INTERIM REPAIR AND REQU I
- [SDR CALA2023061901922](https://openairdocs.org/sdr/CALA2023061901922.md): Skin · corroded · Jun 17, 2023 · N24736 · Boeing 737724 · Wing, Plate/Skin
  > CORROSION ON THE RH WING AT FRONT SPAR LEADING EDGE TO WING LOWER ATTACH STRAP AT KRAS 180 WAS FOUND AT GYR. INTERIM SPLICE REPAIR WAS ACCOMPLISHED FROM KRAS 173 TO KRAS 197 AND REQUIRES PERMANENT REPAIR. PLANNING TO CONTACT ENGINEERING AFTER 16 MONTHS BUT BEF
- [SDR CALA2023061901920](https://openairdocs.org/sdr/CALA2023061901920.md): Skin · corroded · Jun 17, 2023 · N24736 · Boeing 737724 · Wing, Plate/Skin
  > RH WING LOWER SURFACE HAS CORROSION AT TWO LOCATIONS APPROXIMATELY 3" I/B OF WINGLET AND 28" FWD OF WING T/E AND APPROXIMATELY 29" I/B OF WINGLET AND 25" FWD FROM WING T/E. PERFORMED PERMANENT REPAIRS IAW ECRA 572101477 TO RH WING LOWER SURFACE CORROSION AT TW
- [SDR CALA2023061901919](https://openairdocs.org/sdr/CALA2023061901919.md): Unknown · corroded · Jun 17, 2023 · N24736 · Boeing 737724 · Wing Main, Frame Structure
  > (SUPPORT TASK) RH WING INSIDE LEADING EDGE COVE AT APPROXIMATE WING STATION 180 - CORROSION NOTED ON FRONT SPAR LOWER CHARD REPAIR WAS ACCOMPLISHED FROM KRAS 173 TO KRAS 197 AND REQUIRES EC/RA 5720-03341 (LATEST REVISION) ON OR BEFORE 18 MONTHS FROM PERMANENT
- [SDR CALA2023060501761](https://openairdocs.org/sdr/CALA2023060501761.md): Window Frame · cracked · Jun 4, 2023 · N24736 · Boeing 737724 · Fuselage Main, Structure
  > (SUPPORT TASK) THIS NR GENERATED FOR ESFR REPORTING ONLY L/H NO 1 WINDOW FRAME HAS CRACK EA 5310-04554 REV B
- [SDR CALA2023060201740](https://openairdocs.org/sdr/CALA2023060201740.md): Skin · cracked · Jun 1, 2023 · N24736 · Boeing 737724 · Horizontal Stabilizer, Plate/Skin
  > RH HORZ STAB LOWER SKIN CRACKED AT STA 138.70 AT 7TH DRAIN HOLE FROM INBOARD END. CRACK BLENDED OUT AND CONFIRMED BY HFEC AND REPAIR ACCOMPLISHED PER SRM 55-10-01-2R-11 REPAIR 11. PER SAME SRM ITEM 5 TABLE 204 REPAIR IS A CAT B WHICH REQUIRES DVI AND LFEC INSP
- [SDR CALA2023053101726](https://openairdocs.org/sdr/CALA2023053101726.md): Skin · cracked · May 30, 2023 · N24736 · Boeing 737724 · Horizontal Stabilizer, Plate/Skin
  > RT HORZ STAB: LOWER SKIN RT SIDE 7TH DRAIN HOLE AT STABILIZER STA 138.70 C SCAN CRACK
- [SDR CALA2022120203264](https://openairdocs.org/sdr/CALA2022120203264.md): Flap System · malfunctioned · Dec 2, 2022 · N24736 · Boeing 737724 · Trailing Edge Flap Control System
  > *EMERGENCY*TE FLAP ASSYM 2 DEGREES LOCKED. CK''D NORMAL. CK''D SYNCHRO INPUTS (AMM 27-59-00-730-801), TEST IAW AMM 27-59-00-730-801. OPS CHECK GOOD. VERIFIED #3 SKEW SENSOR READING LOW. REPLACED LH INBD FLAP OTBD SENSOR IAW AMM 27-59-01-000-803 AND 27-59-01-4
- [SDR CALA2022101202762](https://openairdocs.org/sdr/CALA2022101202762.md): Push-Pull Cable · unserviceable · Oct 11, 2022 · N24736 · Boeing 737724 · Landing Gear Door Retract Section
  > ALL 3 RED LDG GEAR LIGHT ON WITH ALL 3 GREEN ALSO AND 3 GREEN O VHD PANEL WENT TO HOLD DID QRH 7-45399-3 SHOWS 1 AVAILABLE EWR IF NEEDED. LOCKED DUE TO EMERGENCY DECLARED LOCKED PER TOMC SM. UNLOCKED FOR UPDATE DEBRIEFED CREW CYCLED GEAR HANDLE AND CHECKED
- [SDR CALA2021072601192](https://openairdocs.org/sdr/CALA2021072601192.md): Control Panel · faulted · Jul 26, 2021 · N24736 · Boeing 737724 · Fire Detection
  > FAULT LIGHT ILLUM IN ALL POSITIONS IN FLIGHT AND ON GROUND WITH ENGINES RUNNING OHMED OUT ENGINE 1 LOOP B. AND HARNESS. FROM M279 ALL VALUES WITHIN LIMITS REF FIM TASK 26-10-T805. REPLACED FIRE DETECTION PANEL IN COCKPIT REF AMM 26-00-01-000-801 ADD EMP:13769
- [SDR CALA2020070401041](https://openairdocs.org/sdr/CALA2020070401041.md): Drive Unit · defective · Jul 4, 2020 · N24736 · Boeing 737724 · Weather Radar System
  > WX RADR INOP. RUMBLING NOISE FM RADOME AREA NOTABLE IN CPIT AND BY F/A IN CABIN. REPLACED DRIVE PEDESTAL UNIT PER AMM 34-43-11. OPS NORMAL ROTABLE PARTS CHANGE WAS INDICATED - TT 1142362 SN OFF 0752 UNIT, DRIVE PED OFF 99-3443-9-0004 0752 ON 99-3443-9-0004
- [SDR CALA2020051100961](https://openairdocs.org/sdr/CALA2020051100961.md): Skin · dented · May 10, 2020 · N24736 · Boeing 737724 · Horizontal Stabilizer, Plate/Skin
  > EA 5100-02345 REV E OP 016 LT HORIZONTAL STABILIZER LOWER SKIN FOUND REINFORCING REPAIR 5" FROM FRONT SPAR L/E SIZE 30.5" X 15" INC BETWEEN RIB -1 ND RIB 3. EVALUATE REPAIR PER THE SRM. REF AAR NR 99878327 REMOVED AND REPLACED WITH NEW REPAIR DOUBLER AT LT HOR

Next page: https://openairdocs.org/aircraft/N24736/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 = 'N24736' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N24736/reports

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