# Service difficulty reports: N24202

A list on [N24202](https://openairdocs.org/aircraft/N24202.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 · 118 reports

- [SDR CALA2026092819871](https://openairdocs.org/sdr/CALA2026092819871.md): Beam · worn · Sep 23, 2026 · N24202 · Boeing 737824 · Wing Miscellaneous Structure
  > STRIKER PLATE FOR FWD RT LATCH ON ECS DOOR 192CR, MISSING. AFTER CLEANING DAMAGE & FINDING IT OUT OF ALLOWABLE DAMAGE LINITS. REMOVED DAMAGE IAW 57-10-13. PERFORMED HFEC IAW NDT PART 6, 51-00-00 PROCEDURE 23, AND NDT PART 6, 51-00-00 PROCEDURE 16. NO DEFCTS N
- [SDR CALA2026092819866](https://openairdocs.org/sdr/CALA2026092819866.md): Latch · worn · Sep 23, 2026 · N24202 · Boeing 737824 · Wing Main, Frame Structure
  > FWD RT LATCH FOR H/P DOOR 192, DOOR WAS WORN INTO CHORD. DAMAGE IS BEYOND ALLOWABLE DAMAGE LIMITS AND WILL REQUIRE SRM REPAIR 57-10-13-2R-3. MARKED MAJOR REPAIR AND RII INITIATED. COMPLIED WITH STEPS 4 A-E 1. REQUIRE NDT CUTOUT FOR CRACKS AND 5/32 HOLE SCAN
- [SDR CALA2026092219639](https://openairdocs.org/sdr/CALA2026092219639.md): Battery Pack · no test · Sep 21, 2026 · N24202 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK AT M1674 FAILED A CAPACITY CHECK. REPLACED THE BATTERY PACK AT M1674, OPS CHKD GOOD IAW MM 33-51-06-960-805.
- [SDR CALA2026092219638](https://openairdocs.org/sdr/CALA2026092219638.md): Battery Pack · no test · Sep 21, 2026 · N24202 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK AT M1676 FAILS CAPACITY CHECK. REPLACED THE BATTERY PACK AT M1676, OPS CHKD GOOD IAW MM 33-51-06-960-805.
- [SDR CALA2026092119624](https://openairdocs.org/sdr/CALA2026092119624.md): Rub Strip · missing · Sep 18, 2026 · N24202 · Boeing 737824 · Trailing Edge Flaps
  > MISSING RUB STRIP IAW GMM 02-30-95. ACCOMPLISHED WITH NEW PART INSTALLED IAW GMM 02-30-95.
- [SDR CALA2026092119622](https://openairdocs.org/sdr/CALA2026092119622.md): Bulb Seal · missing · Sep 18, 2026 · N24202 · Boeing 737824 · Trailing Edge Flaps
  > BULB SEAL MISSING IAW GMM 02-30-95, REF LP 3394334, ACCOMPLISHED WITH NEW PART INSTALLED IAW GMM 02-30-95.
- [SDR CALA2026091419390](https://openairdocs.org/sdr/CALA2026091419390.md): Power Supply · faulted · Sep 11, 2026 · N24202 · Boeing 737824 · Emergency Lighting
  > ROW 15-21 AISLE EMERGENCY LIGHT INOPERATIVE. R & R CHARGER AND BATTERY PACK FOR M1695 IAW AMM 33-51-06. R & R FUSES FOR M1694 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06, OPS CHKD GOOD.
- [SDR CALA2026081118467](https://openairdocs.org/sdr/CALA2026081118467.md): Light · sparks · Aug 6, 2026 · N24202 · Boeing 737824 · Exterior Lighting
  > RAMP REPORTS SPARKS, SMOKE, AND FLAMES COMING FROM THE LT HORIZONTAL STAB, ABOUT HALF WAY OUT FROM FUSELAGE. REINSTALLED ORIGINAL LOGO LIGHT, OPENED & COLLARED CB P18-3 A15. REMOVED POWER FROM LIGHT, FIRE DEPARTMENT MEASURED TEMP AT 200F & THERE WERE DEAD B
- [SDR CALA2026042215616](https://openairdocs.org/sdr/CALA2026042215616.md): Bracket · loose · Apr 19, 2026 · N24202 · Boeing 737824 · Emergency Equipment
  > 1R GIRT BAR BRACKET IS LOOSE ADJUSTED THE GIRT BAR RETAINER CLIP ON DOOR 1R,AND VERIFIED THE GIRT BAR STAYS INSIDE THE RETAINER CLIP IN REF TO AMM 25-66-01.
- [SDR CALA2026012613297](https://openairdocs.org/sdr/CALA2026012613297.md): Hook And Loop · damaged · Jan 26, 2026 · N24202 · Boeing 737824 · Passenger Compartment Equipment
  > SEAT 20F EXIT ROW DOOR LOWER SAFTEY STAP COVER WILL NOT STAY ATTACHED HOOK AND LOOP DAMAGED. INSPECTED HOOK AND LOOP ON EXIT ROW 20F DOOR COVER. NO DAMEGE TO HOOK AND LOOP NOTED. SECURED LOWER SAFTEY STRAP IAW AMM 52-22-51-400-801. OKAY FOR SERVICE.
- [SDR CALA2025123012549](https://openairdocs.org/sdr/CALA2025123012549.md): None · no discrepancy · Dec 28, 2025 · N24202 · Boeing 737824 · Standard Practices/Structures
  > BIRD STRIKE ON WINDSHIELD, CLEANED BIRD RESIDUE AND INSPECTED WINDSHIELD AND SURROUNDING STRUCTURE, NO EXTERNAL DAMAGE FOUND. EXTENDED AIRCRAFT FLAPS/SLATS AND EXAMINED THE REST OF THE FUSELAGE AS WELL AS THE ENGINES. NO EVIDENCE OF OTHER BIRD STRIKES OR OBVI
- [SDR CALA2026010212577](https://openairdocs.org/sdr/CALA2026010212577.md): Lens · broken · Dec 26, 2025 · N24202 · Boeing 737824 · Emergency Lighting
  > 29C EMERG PATH LGT BROKEN. LIGHT WORKS OK. MAINTENANCE REQUESTS RELIEF UNDER MEL 3319E. APPROVED PLACED 29C EMERGENCY LIGHT ON MEL 3319E. APPLIED PLACARD. R & R LENS COVER 29C PATH LIGHTING OPS CKS OK AT THIS TIME
- [SDR CALA2025110911023](https://openairdocs.org/sdr/CALA2025110911023.md): Strap · out of position · Nov 7, 2025 · N24202 · Boeing 737824 · Emergency Exits
  > RIGHT OVERWING EXIT DOOR HANDLE COVER PANEL KEEPS FALLING OFF. REPOSITION OVERWING ESCAPE DOOR STRAP COVER ONTO HOOK AND LOOP. COVER STAYS SECURE.
- [SDR CALA2025102110346](https://openairdocs.org/sdr/CALA2025102110346.md): Warning Light · false activation · Oct 20, 2025 · N24202 · Boeing 737824 · Central Warning
  > OIL FILTER BYPASS 3 OCCASIONS ABLE TO GET LIGHT TO EXTINGUISHDURING CLIMB TO 15K OIL DIFFERENTIAL LIGHT ILLUMINATED PROMPTING LEVEL OFF OUR SECOND CLIENT FOR 25,000 FT. THE LIGHT CAME ON AGAIN DURING THE SET TO 8000 FT. IT ILLUMINATED THE THIRD TIME RUSTLE P
- [SDR CALA2025091809038](https://openairdocs.org/sdr/CALA2025091809038.md): Lamp · inoperative · Sep 17, 2025 · N24202 · Boeing 737824 · Emergency Lighting
  > FOUND RH SLIDE OVERWING LIGHT INOP PERFORMED RAR OF RH SLIDE OVERWING LIGHT IAW AMM 33-51-04. OPC GOOD.
- [SDR CALA2025091108771](https://openairdocs.org/sdr/CALA2025091108771.md): Connector · damaged · Sep 9, 2025 · N24202 · Boeing 737824 · Hydraulic Power System Wiring
  > -A- SYSTEM HYD EMDP ELEC CONNECTOR DAMAGED. ON INSP, FOUND HYD PUMP A CONNECTOR (D2664) DAMAGED. REMOVED CONNECTOR D2664 & CLEANED WIRES & CONTACTS, INSPD ALL CONTACTS & FOUND CONTACTS TO BE GOOD. STARTED INSTALL OF CONNECTOR & ABLE TO GET 18AWG WIRES TERMIN
- [SDR CALA2025091008738](https://openairdocs.org/sdr/CALA2025091008738.md): Elec Connector · damaged · Sep 8, 2025 · N24202 · Boeing 737824 · Hydraulic Power System Wiring
  > B SIDE HYD OVHT LIGHT ILLUMINATED. FOUND ELEC HYD PUMP B CONNECTOR (D2666) DAMAGED. REMOVED ALL OLD CONTACTS AND RETERMINATED ALL WIRES WITH NEW CONTACTS AND INSTALLED IN CONNECTOR D2666 IAW WDM 29-11-12-1 & VERIFYING CONTINUITY BACK TO R318 IN THE P91 PANE
- [SDR CALA2025080507330](https://openairdocs.org/sdr/CALA2025080507330.md): Light · no test · Aug 4, 2025 · N24202 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK. ONE RED EMERGENCY LIGHT INOPERATIVE AT 20C. REPLACED LIGHT ASSY, GROUND OPS NORMAL.
- [SDR CALA2025070906408](https://openairdocs.org/sdr/CALA2025070906408.md): Unknown · smoke · Jul 9, 2025 · N24202 · Boeing 737824 · Air Distribution System
  > ON T/O ROLL, SMOKE WITH BURNING ODOR CAME FROM CA SIDE AIR VENTS. R EJ T/O AND SMOKE DISSIPATED CREW ADVISED LOW SPEED ABORT LESS THAN 20 KTS. PER FODM CAPTAIN REPORTED RTO BETWEEN 100 AND 110 KTS. PERFORMED SMOKE CABIN/FLIGHT DECK CONDITIONAL INSPECTION. REF
- [SDR CALA2025022400431](https://openairdocs.org/sdr/CALA2025022400431.md): Skin · cracked · Feb 21, 2025 · N24202 · Boeing 737824 · Wing, Plate/Skin
  > PER ECRA 5725-01156 PART 1, STEP 3 - AFTER MAY 18, 2026, BUT BEFORE JUNE 18, 2026, PLANNING TO CONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS OF THE INTERIM REPAIR INSTALLED ON THE RIGHT WING OUTBOARD LOWER SKIN PANEL BETWEEN WSTA 564.5 & 591.5 AT STR L-9
- [SDR CALA2025022400412](https://openairdocs.org/sdr/CALA2025022400412.md): Spar · cracked · Feb 19, 2025 · N24202 · Boeing 737824 · Fuselage Main, Structure
  > CENTER WING REAR SPAR L/H VAPOR BARRIER HAS 10" CRACKED O/B OF HYD A SYSTEM RETURN FILTER. APPLIED REPAIR PATCH ON L/H VAPOR BARRIER O/B HYD A SYSTEM RETURN FILTER AT CENTER WING REAR ESFR:1038460 SPAR. CRACK LENGTH 10" AS PER B737-800 SRM 57-10-10-2R-2.
- [SDR CALA2025022600444](https://openairdocs.org/sdr/CALA2025022600444.md): Skin · gouged · Feb 11, 2025 · N24202 · Boeing 737824 · Nacelle/Pylon, Plate/Skin
  > NRO.2 EG INBOARD PYLON ATTACH WING LANDIENG EDGE FILLET PANEL HAS DEEP GOUGE REF ARR N/R 9934107 REMOVED AND REPLACED SKIN CLOSEOUT 611A AT R/W L/E INBOARD OF PYLON AS PER B737-800 SRM 51-40-02-0G-0 AND DWG# 116A4008. WORK ACCOMPLISHED BY V918489 REMOVED AND R
- [SDR CALA2025022600448](https://openairdocs.org/sdr/CALA2025022600448.md): Fitting · gouged · Feb 10, 2025 · N24202 · Boeing 737824 · Wing Miscellaneous Structure
  > R/W FLAP SUPPORT FAIRING #6 AFT BULKHEAD FITTING GOUGED. REF AAR N/R 9933952 REMOVED AND REPLACED FITTING AT FLAP FAIRING. # 6 REF B 737-800 SRM 51-40-02-0G-0, DWN 113A9350. WORK ACCOMPLISHED BY V903523. ESFR NO.1038497. SIGNED U057326.
- [SDR CALA2025022600450](https://openairdocs.org/sdr/CALA2025022600450.md): Skin · gouged · Feb 8, 2025 · N24202 · Boeing 737824 · Nacelle/Pylon, Plate/Skin
  > L/W L/E I/B OF PYLON SKIN GOUGED REF AAR N/R 9934263 REMOVED AND REPLACED SKIN AT L/W L/E INBOARD OF PYLON AS PER B73 37-800 SRM 51-40-02-0G-0 AND DWG# 116A4008. REMOVED AND REPLACED SKIN AT L/W L/E INBOARD OF PYLON AS PER B737-800 SRM 51-40-02-0G-0 AND DWG#
- [SDR CALA2025021200342](https://openairdocs.org/sdr/CALA2025021200342.md): Access Door · gouged · Feb 7, 2025 · N24202 · Boeing 737824 · Accessory Compartment Doors
  > LOWER WING CENTER SECTION PNEUMATIC SERVICE PORT ACCESS DOOR 192DR EDGES FWD DEEP GOUGES MKD DOT 148 (REF AAR N/R 9934287) REMOVED AND REPLACED LOWER WING CENTER SECTION PNEUMATIC SERVICE ACCESS DOOR 192DR PER SRM 51-40-02-0G-0.
- [SDR CALA2025022400420](https://openairdocs.org/sdr/CALA2025022400420.md): Stiffener · cracked · Feb 4, 2025 · N24202 · Boeing 737824 · Fuselage Miscellaneous Structure
  > LOWER FUS. CENTER WING REAR SPAR STIFFENER LOWER RADIUS CRACKED AT LBL 25 STA 663.75 O/B OF L/H RAM AIR EXIT EXHAUST REF AAR N/R 9933669 REMOVED AND REPLACED LOWER FUS. CENTER WING REAR SPAR STIFFENER AT LBL 25 STA 663.75 O/B OF L/H RAM AIR EXIT EXHAUST AS PE
- [SDR CALA2025021000323](https://openairdocs.org/sdr/CALA2025021000323.md): Pressure Deck · dented · Feb 4, 2025 · N24202 · Boeing 737824 · Fuselage Main, Structure
  > FLIGHT DECK FLOOR SKIN PANEL DENTS AT LBL 11 STA 259 AND STA 277 REF AAR N/R 9933688 ACCOMPLISHED FLIGHT DECK FLOOR WEB REPAIR AT LBL 11 STA 259 - STA 277 AS PER SRM 53-10-51-2R-2. WORK ACCOMPLISHED BY V928495 ACCOMPLISHED FLIGHT DECK FLOOR WEB REPAIR AT LBL
- [SDR CALA2025021100338](https://openairdocs.org/sdr/CALA2025021100338.md): Skin · dented · Feb 3, 2025 · N24202 · Boeing 737824 · Cargo/Baggage Doors
  > FWD CARGO DOOR EXT SKIN HAS SEVERAL DENTS. (REF AAR N/R 9933840)
- [SDR CALA2025021000322](https://openairdocs.org/sdr/CALA2025021000322.md): Attach Angle · worn · Feb 3, 2025 · N24202 · Boeing 737824 · Fuselage Main, Attach Fittings
  > LOWER FUS. ATTACH ANGLE WORN O/B OF L/H RAM AIR EXIT EXHAUST MKD DOT 031. (REF AAR N/R 9933670)
- [SDR CALA2025020500301](https://openairdocs.org/sdr/CALA2025020500301.md): Skin · dented · Feb 3, 2025 · N24202 · Boeing 737824 · Cargo/Baggage Doors
  > AFT CARGO DOOR EXT SKIN HAS SEVERAL DENTS. (REF AAR N/R 9933841)
- [SDR CALA2025022400421](https://openairdocs.org/sdr/CALA2025022400421.md): Attach Angle · cracked · Jan 27, 2025 · N24202 · Boeing 737824 · Fuselage Main, Attach Fittings
  > R/H VAPOR BARRIER I/B UPPER ATTACHED ANGLE CRACKED @ RBL 7 STA R/H VAPOR BARRIER I/B UPPER ATTACHED ANGLE CRACKED @ RBL 7 STA REMOVED AND REPLACED RH VAPOR BARRIER UPPER ATTACH ANGLE AT STA 663.75 663.75 PER SRM 51-40-02-0G-0 AND DWG#111A1000 REF AAR N/R 9933
- [SDR CALA2025012700215](https://openairdocs.org/sdr/CALA2025012700215.md): Strap · cracked · Jan 25, 2025 · N24202 · Boeing 737824 · Service Doors
  > AS PER T/C 29-5241-2706 FWD R1 DOOR STRAP HAS CRACK ON UPPER AREA REF AAR N/R 9933925 REMOVED AND REPLACED DEPPRESOR(DOOR STRP) AT R1 DOOR AREA AS PER REF B737 SRM 51-40-02=0G-0 AND DWG # 141A8370.
- [SDR CALA2025011700136](https://openairdocs.org/sdr/CALA2025011700136.md): Floorbeam · corroded · Jan 16, 2025 · N24202 · Boeing 737824 · Fuselage Main, Floor Beam
  > AFT CABIN WET AREA FLOOR SUPPORT BEAM UPPER CAP CORR. LBL 29 TO RBL 33 STA 986.5 MKS DOT 089 REF AAR N/R 9933829
- [SDR CALA2025011700137](https://openairdocs.org/sdr/CALA2025011700137.md): Spar · cracked · Jan 15, 2025 · N24202 · Boeing 737824 · Fuselage Main, Bulkhead
  > CRACK FOUND AT LOWER FUSELAGE CENTER WING BOX REAR SPAR STA 663 VERTICAL PRESSURE WEB DECK BETWEEN LBL40- LBL 31.83 (CRACK LENGTH 1") REF AAR N/R 9933560
- [SDR CALA2025011600130](https://openairdocs.org/sdr/CALA2025011600130.md): Floor Support · corroded · Jan 15, 2025 · N24202 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FLOOR SUPPORT INNER CHORD L-2 DOOR LOWER SILL FOUND CORRODED FROM STA 951 TO STA 992.8 MKD DOT 087 REF AAR N/R 9933826
- [SDR CALA2025022400413](https://openairdocs.org/sdr/CALA2025022400413.md): Floor Support · cracked · Jan 14, 2025 · N24202 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED AT FASTENER HOLE LBL 30 BETWEEN STA 312 AND 328. REMOVED AND REPLACED INTERCOASTAL AT FWD CABIN WET AREA FLOOR SUPPORT LBL 30 BETWEEN STA 312 AND 328 ESFR:1038461 PER REF SRM 51-40-02-0G-0 AND DWG# 141A5
- [SDR CALA2025011400116](https://openairdocs.org/sdr/CALA2025011400116.md): Floor Support · cracked · Jan 11, 2025 · N24202 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CABIN WET AREA FLOOR SUPPORTNINNER CHORD APPEARS CRACK REF AAR N/R 9933798
- [SDR CALA2025011500120](https://openairdocs.org/sdr/CALA2025011500120.md): Floorbeam · corroded · Jan 8, 2025 · N24202 · Boeing 737824 · Fuselage Main, Floor Beam
  > AFT CABIN WET AREA FLOORBEAM UPPER CAP CORRODED FROM LBL 4 TO RBL 50 STA 947.75.
- [SDR CALA2025022600447](https://openairdocs.org/sdr/CALA2025022600447.md): Floor Support · corroded · Jan 6, 2025 · N24202 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CORR. AT FASTENERS HOLES LBL 50 BETWEEN STA 947.75 AND 967. REMOVED AND REPLACED INTERCOSTAL FROM STA 947.5 TO STA 967 AT LBL 50.68 AS PER B737-800 SRM 51-40-02-0G-0 AND DWG# 147A5650.
- [SDR CALA2025022400415](https://openairdocs.org/sdr/CALA2025022400415.md): Floor Support · cracked · Jan 6, 2025 · N24202 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CABIN FLOOR SUPPORT INTERCOSTAL CRACKED AT LBL 15 BETWEEN STA 380 AND 400. REMOVED AND REPLACED FWD CABIN FLOOR SUPPORT ESFR:1038463 INTERCOSTAL AT LBL 15 BETWEEN STA 380 & 400 AS PER REF B737 SRM 51-40-02-0G-0 & DWG # 143A5400.
- [SDR CALA2025022400414](https://openairdocs.org/sdr/CALA2025022400414.md): Floor Support · cracked · Jan 6, 2025 · N24202 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CABIN FLOOR SUPPORT INTERCOSTAL CRACKED AT RBL 13 BETWEEN STA 380 AND 400. REMOVED AND REPLACED FWD CABIN FLOOR SUPPORT ESFR:1038462 INTERCOSTAL AT RBL 13 BETWEEN STA 380 & 400 AS PER REF B737 SRM 51-40-02-0G-0 & DWG # 143A5400.
- [SDR CALA2024120403018](https://openairdocs.org/sdr/CALA2024120403018.md): Skin · cracked · Dec 3, 2024 · N24202 · Boeing 737824 · Wing, Plate/Skin
  > ACCOMPLISH A PERMANENT REPAIR ON THE RH WING LOWER SKIN BETWEEN WSTA 564 AND WSTA 591 PRIOR TO 02 JULY 2026 SKIN AROUND THE OUTBOARD FASTENER OF STRINGER R-9 BETWEEN WS 564.5 AND WS 591.5 REF NR 002323616 FOUND A CRACK THAT PROPAGATES 0.8" FWD OF THE FASTENER
- [SDR CALA2024120303007](https://openairdocs.org/sdr/CALA2024120303007.md): Skin · cracked · Dec 2, 2024 · N24202 · Boeing 737824 · Fuselage Main, Plate/Skin
  > PERFORMED INTERIM REPAIR TO LH WING OUTBD LOWER SKIN PANEL CRACK BETWEEN WSTA 564.5 - 591.5 AT S-9L REFER TO EC/RA 5725-01152. REQUIREMENTS PER PART 2 OF EC/RA 5725-01152 ON OR BEFORE 25 MAY 2026. DIP TO BE INITIATED A DTA DIP TO STATE: ON THE LH WING LOWER SK
- [SDR CALA2024082802301](https://openairdocs.org/sdr/CALA2024082802301.md): Window Frame · cracked · Aug 26, 2024 · N24202 · Boeing 737824 · Fuselage Main, Structure
  > REF.EA5310-04554 OP002-TYPICAL CRACK FOUND ON RT #1 WINDOW FRAME UPPER AFT CORNER. ACCOMPLISHED RH #1 WINDOW FRAME PERMANENT REPAIR / PREVENTIVE / TRIPLER AS A PERMANENT REPAIR. MODIFICATION IAW EA#5310-04554 REV."C"OP-004,WHICH REQUIRES TO REF. AAR N/R:9
- [SDR CALA2024082802304](https://openairdocs.org/sdr/CALA2024082802304.md): Window Frame · cracked · Aug 14, 2024 · N24202 · Boeing 737824 · Fuselage Main, Structure
  > AFTER REMOVING L/H WINDSHIELD, FOUND OUTBOARD POST CRACKED. LOG LOCKED FOR FERRY FLIGHT UNLOCKING FOR ITEM TO BE WORKED ACCOMPLISHED L/H NO.1 WINDOW PERMANENT REPAIR / PREVENTATIVE PERMANENT REPAIR MODIFICATION AS PER EA 5310-04554 REV C. REMOVE THE NO.1 WIND
- [SDR CALA2024050601325](https://openairdocs.org/sdr/CALA2024050601325.md): Hub Cap · missing · May 5, 2024 · N24202 · Boeing 737824 · Wheel/Ski/Float
  > PDA 1 REF. LP 7872896 #1 MLG TIRE HUB CAP AND BOLTS ARE MISSING AND DEPARTED THE AIRCRAFT. ADDED PICTURE
- [SDR CALA2023042801278](https://openairdocs.org/sdr/CALA2023042801278.md): Transmitter · inoperative · Apr 28, 2023 · N24202 · Boeing 7378 · Leading Edge Slat Control System
  > NO FLAP DEPLOYMENT ON APPROACH. NO LEADING EDGE FLAP TRANSIT LIGHT FLAP PRIMARY OR MOVEMENT OF FLAPS PER PROCEDURE 1. FIM POINTS TO WIRING/TRANSMITTER. RAN FLAPS IN PRIMARY AND ALTERNATE NO FLAP MOVEMENT. SLATS MOVED DURING ALTERNATE OPERATION. ALTERNATE FLAPS
- [SDR CALA2023031300724](https://openairdocs.org/sdr/CALA2023031300724.md): Lamp · inoperative · Mar 13, 2023 · N24202 · Boeing 7378 · Lighting System
  > RIGHT AFT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. RE-LAMPED OVERWING LIGHT REF MM 33-51-04. OPS CK OK. PARTS USED: 767,QTY:1
- [SDR CALA2022112303197](https://openairdocs.org/sdr/CALA2022112303197.md): Transmitter · inoperative · Nov 23, 2022 · N24202 · Boeing 737824 · Leading Edge Slat Control System
  > CREW REPORTS THE FLAPS DID NOT MOVE WHEN SELECTED. HAD TO USE ALTERNATE FLAPS FOR LANDING. REMOVED AND REPLACED L/H FLAP POSITION TRANSMITTER I.A.W. AMM 27-58-01-400-801. OPS CHECKS AND ALL ASSOCIATED TESTS C/W AND CHK GOOD. PERFORMED LAND VERIFY. TESTS PASSE
- [SDR CALA2022101202780](https://openairdocs.org/sdr/CALA2022101202780.md): Position Sensor · inoperative · Oct 12, 2022 · N24202 · Boeing 737824 · Drag Control Actuator
  > LEFT FLAP NEEDLE IS BOUNCING INTERMITANTLY BETWEEN 6 OCLOCK AND 12 OCLOCK POSITION ON GAUGE PERFORMED BITE OF FSEU REF FIM 27-61 TASK 801 LAST FLT SHOWS OK FAULT 27-52259 AND 27-52261. PERFORMED FIM 27-61 TASK 813 AND ROTABLE PARTS CHANGE WAS INDICATED - TT #

Next page: https://openairdocs.org/aircraft/N24202/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 = 'N24202' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N24202/reports

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