# Service difficulty reports: N35204

A list on [N35204](https://openairdocs.org/aircraft/N35204.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 2 · 94 reports

- [SDR CALA2026033014916](https://openairdocs.org/sdr/CALA2026033014916.md): Pitot Tube · faulted · Mar 26, 2026 · N35204 · Boeing 737824 · Pitot/Static System
  > FEEL DIFF PRESS LIGHT ON AFTER TAKEOFF FULL NOSE UP TRIM FOR LA NDING REF FIM 27-31 TASK 815. FLUSHED OUT R/H ELEV PITOT. NO CLOGS NOTED. L/H PITOT HAS OBSTRUCTION. REMOVED ELEVATOR PITOT PROBE REF AMM 27-31-94-000-801. CONDUCTED ELEVATOR PITOT STATIC FLUSHI
- [SDR CALA2025110710985](https://openairdocs.org/sdr/CALA2025110710985.md): Slide · unpacked · Nov 6, 2025 · N35204 · Boeing 737824 · Escape Slide
  > F/A REPORTS DOOR 1R HAS EXCESS SLIDE MATERIAL LOOSE. REMOVED AND REPACKED Z FOLD ON DOOR 1R ESCAPE SLIDE AND REINSTALLED DOOR 1R ESCAPE SLIDE IN REF TO AMM 25-66-01, NO FURTHER DEFECTS AT THIS TIME VERIFIED INSTALL OF DOOR SLIDE 1R RII REF GMM 09-25-05.
- [SDR CALA2025081407761](https://openairdocs.org/sdr/CALA2025081407761.md): Structure · no discrepancy · Aug 9, 2025 · N35204 · Boeing 737824 · Standard Practices/Structures
  > PERFORM AN INSPECTION PER PART 2 OF THE LATEST REVISION OF ECRA 5311-03385 ON OR BEFORE 29-JULY-2027 REF LP 5753762 FOR INTERIM REPAIR.
- [SDR CALA2025080407235](https://openairdocs.org/sdr/CALA2025080407235.md): Stub Beam · damaged · Jul 31, 2025 · N35204 · Boeing 737824 · Fuselage Main, Structure
  > STA 616 LH STUB BEAM HAS AN ELONGATED HOLE. REPAIRED BS616 L/H STUB BEAM AS REQ IAW REO-G25531 REV IR AND ECRA NO. 5311-03385 REV-.
- [SDR CALA2025081407754](https://openairdocs.org/sdr/CALA2025081407754.md): Skin · corroded · Jul 29, 2025 · N35204 · Boeing 737824 · Fuselage Main, Plate/Skin
  > AFT PIT LT SIDE, FUSELAGE SKIN CORRODED AROUND THE LAVATORY EXHAUST VENT ATTACHMENT BETWEEN BS 907 AND BS 927 AND BETWEEN STRINGERS S19L AND S22L. ACCOMPLISHEDD INTERIM REPAIR OF THE AFT PIT LT SIDE, FUSE SKIN IAW ECRA 5370-01182 PT1.
- [SDR CALA2025071406498](https://openairdocs.org/sdr/CALA2025071406498.md): Skin · cracked · Jul 9, 2025 · N35204 · Boeing 737824 · Passenger/Crew Doors
  > R-2 DOOR, INNER UPPER SKIN, UPPER CENTER LIGHTENING HOLE IS CRACKED. REPAIRED R-2 DOOR INNER UPPER SKIN REFERENCE UNITED EC/RA# 5210-03403.
- [SDR CALA2025070906383](https://openairdocs.org/sdr/CALA2025070906383.md): Crease Beam · corroded · Jul 8, 2025 · N35204 · Boeing 737824 · Fuselage Main, Structure
  > MAIN CABIN CREASE BEAM INNER CHORD UPPER SURFACE HAS CORROSION AT STA 294, RBL 53. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER ECRA 5321-01330 REV H. ORIGINAL MAT.094, REMOVED.017, REMAINING.077. INSTALLED NEW CREASE BEAM IAW SRM 51-
- [SDR CALA2025071706651](https://openairdocs.org/sdr/CALA2025071706651.md): Floorbeam · corroded · Jul 1, 2025 · N35204 · Boeing 737824 · Fuselage Main, Floor Beam
  > AFT WET AREA RT FLOORBEAM BS 947 HAS SURFACE CORROSION. DAMAGE FOUND TO BE OUT OF LIMITS PER B737-800 SRM 53-70-51-1A-1. REMOVED AND T-ANGLE REPAIR PER B737-800 SRM 51-40-02. REFABRICATED AND REPLACED T-ANGLE REPAIR PER B737-800 SRM 53-70-51-2R-5.
- [SDR CALA2025071706650](https://openairdocs.org/sdr/CALA2025071706650.md): Crease Beam · corroded · Jun 30, 2025 · N35204 · Boeing 737824 · Fuselage Main, Structure
  > MAIN CABIN CREASE BEAM INNER CHORD UPPER SURFACE HAS CORROSION FROM BS 294-348, LBL60. REMOVED CORROSION IAW B737-800 SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER EC/RA 5321-01330 REV A, ORIGINAL THICKNESS.125" REMOVED.045", REMAINING.080". REMOVED AND R
- [SDR CALA2025071706649](https://openairdocs.org/sdr/CALA2025071706649.md): Stop Fitting · worn · Jun 26, 2025 · N35204 · Boeing 737824 · Passenger/Crew Doors
  > (SUPPORT TASK) L-2 DOOR, UPPER FWD DOOR STOP FITTING IS GOUGED. EVALUATED DAMAGE AND FOUND OUT OF LIMITS IAW SRM 52-10- 90-1A-1. REMOVED AND REPLACED UPPER FWD STOP FITTING PN#147A6128 U53 IAW SRM 51-40-02 AND DWG 147A6125 REVB. RESTORED SURFACE PROTECTION I
- [SDR CALA2025070106106](https://openairdocs.org/sdr/CALA2025070106106.md): Crease Beam · corroded · Jun 26, 2025 · N35204 · Boeing 737824 · Fuselage Main, Structure
  > AFT WET AREA RH DOOR CREASE BEAM HAS MULTIOPLE SPOTS OF CORROSION. REMOVED CORROSION ORG THICKNESS.180 REMOVED.105 REMAINING.075 AND FOUND TO BE OUT OF LIMITS PER EC/RA 5321-01330 REV A AND SRM 53-70-15-1A-1. REMOVED CREASE BEAM PER B737-800 SRM 51-40-02.
- [SDR CALA2025070106105](https://openairdocs.org/sdr/CALA2025070106105.md): Floor Support · corroded · Jun 26, 2025 · N35204 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 946 RBL 50 SUPPORT HAS CORROSION, WITH 100% MATERIAL LOSS ON UPPER SURFACE. REMOVED AND REPLACED INTERCOSTAL AT ST STA.949 - STA 967 RBL50 PER B737-800 SRM 51-40-02 AND BAC DWG 147A5762
- [SDR CALA2025071506571](https://openairdocs.org/sdr/CALA2025071506571.md): Service Panel · corroded · Jun 25, 2025 · N35204 · Boeing 737824 · Fluid Service Doors
  > (SUPPORT TASK) AFT CARGO COMPARTMENT,WASTE SERVICE PAN HAS CORROSION.
- [SDR CALA2025062706002](https://openairdocs.org/sdr/CALA2025062706002.md): Web · corroded · Jun 25, 2025 · N35204 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT, SILL PLATE INNER WEB HAS EXFOLIATED CORROSION. REMOVED AND REPLACED AFT CARGO COMP SILL PLATE, LOCATED AND DRILLED, IAW B737-800 SRM 51-40-02, 51-40-05.
- [SDR CALA2025062305813](https://openairdocs.org/sdr/CALA2025062305813.md): Floor Support · cracked · Jun 20, 2025 · N35204 · Boeing 737824 · Fuselage Miscellaneous Structure
  > (B737-53-3-0737) MAIN CABIN FWD WET AREA, MACHINED INTERCOSTAL FROM STA 344-360 BL 0 HAS 2EA POSSIBLE CRACKS IN UPPER FLANGE AT FLOOR PANEL ATTACH HOLES. REMOVED AND REPLACED MACHINED INTERCOSTAL IAW DWG NO. 141A540010 REV B AND SRM 51-40-02.
- [SDR CALA2024080800390](https://openairdocs.org/sdr/CALA2024080800390.md): Pump · malfunctioned · Aug 5, 2024 · N35204 · Boeing 737824 · Fuel Boost Pump
  > CENTER TANK LEFT FUEL PUMP INOP. CENTER TANK RIGHT BOOST PUMP ON MEL 2802D ON LOG PAGE 8819950. PLACING BOTH CENTER FUEL TANK BOOST PUMPS ON MEL 2802E. LOG PAGE 8819950 CLEARED. CENTER FUEL TANK QTY 4.75. T/S PER FIM 28-22 TASK 822-C1. FOUND STATUS CODE 2 ON
- [SDR CALA2024042201187](https://openairdocs.org/sdr/CALA2024042201187.md): Web · damaged · Apr 18, 2024 · N35204 · Boeing 737824 · Fuselage Miscellaneous Structure
  > E & E BAY WEB BS 323.7 TO 351.2 DAMAGED.
- [SDR CALA2024042201151](https://openairdocs.org/sdr/CALA2024042201151.md): Angle · cracked · Apr 18, 2024 · N35204 · Boeing 737824 · Fuselage Main, Structure
  > E&E COMPARTMENT DOOR CUTOUT FRAME/WEB, LH SIDE FWD CORNER EXTRUSION ANGLE IS CRACKED L/P IS FOR ESFR PURPOSES SEE NR 1952113 ESFR CREATED ESFR # 1035845
- [SDR CALA2024040200924](https://openairdocs.org/sdr/CALA2024040200924.md): Panel · missing · Mar 29, 2024 · N35204 · Boeing 737824 · Nacelle/Pylon, Main Frame
  > NR 1 ENGINE PYLON PANEL HEAT SHIELD COATING MISSING FROM LOWER SECTION OF PANEL - APPROXIMATLY 10 SQ INCHES. REMOVED ENG 1 INBD AFT PYLON ACEESS PANEL FOR MX AT IAH. INSTALLED #1 ENGINE INBOARD PYLON PANEL REF AMM 54-53-01.
- [SDR CALA2023021000383](https://openairdocs.org/sdr/CALA2023021000383.md): Door · missing · Feb 10, 2023 · N35204 · Boeing 7378 · Nose/Tail Landing Gear Strut/Axle
  > PDA 3 RIGHT NLG DOOR LEADING EDGE EROSION BOOT MISSING -- SEE PHOTO PHOTO ADDED IF NEEDED ECRA 5280-01284 REV-B IS AVAILABLE FOR DEFERRAL.... PARTS ADDED TO LOG.. REF IPC 32-22-11-05 ITEM 275 PARTS USED: 00-0609-3-7367,QTY:1 29-3222-3-0008,QTY:1 REPLACED
- [SDR CALA2023011000081](https://openairdocs.org/sdr/CALA2023011000081.md): Position Sensor · inoperative · Jan 10, 2023 · N35204 · Boeing 737824 · Landing Gear Position and Warning
  > NOSE GEAR INDICATES DOWN AFTER T/O. QRH DONE. DIVERTING TO IAH. REMOVED AND REPLACED NOSE LANDING GEAR DOWN POSITION SENSOR S853. OPS CHECK NORMAL.
- [SDR CALA2022092102423](https://openairdocs.org/sdr/CALA2022092102423.md): Skin · cracked · Sep 19, 2022 · N35204 · Boeing 737 · Horizontal Stabilizer Structure
  > C-SCAN CRACK INDICATIONB LH HORIZONTAL STABILIZER APPROX STA 117, 10.5" FROM AFT SPAR. TRANSCRIBED FROM AERSALE NRC 23739 EMP STAMP# ALD011. INITIAL DVI AND LFEC EVERY 9,00 FLT CYC THEREAFTER IAW SRM 55-10-01, INSPECTION THRESHOLD AT 56,00 TOTAL FLT CYC AND TH
- [SDR CALA2022081602071](https://openairdocs.org/sdr/CALA2022081602071.md): Handle · loose · Aug 16, 2022 · N35204 · Boeing 737824 · Passenger/Crew Doors
  > DOOR 1L ASSIST HANDLE LOOSE.TIGHTEN THE HANDLE OK TO USE.
- [SDR CALA2022072701884](https://openairdocs.org/sdr/CALA2022072701884.md): Harness · damaged · Jul 27, 2022 · N35204 · Boeing 737824 · Equipment/Furnishings Wiring
  > FOUND DANAGED EPL HARNESS P/N BR9635-30-24 THAT RUNS FROM SEAT ROW 34ABC TO 36ABC. SUPPORT TASK GOOD IAW B737-800 AMM 25-22-00-710-027 REMOVED THE DAMAGED SECTION OF WIRES AND SPLICED WIRES IAW SWPM 20-30-12 AT STA 792 BETWEEN SEAT ROWS 34ABC & 35ABC. OPS CKD
- [SDR CALA2022072701899](https://openairdocs.org/sdr/CALA2022072701899.md): Harness · chafed · Jul 26, 2022 · N35204 · Boeing 737824 · Lighting System
  > EPL WIRING BETWEEN SEAT ROWS 34 & 35 ABC IS DAMAGED CAUSING THE AFT CABIN EMERGENCY LIGHTS TO APPEAR WEAK. (REF. N/R 000149). SUPPORT TASK NSA EMX N/R 00153. REPAIRED DAMAGED EEPL SEAT TO SEAT CABLE WITH 2 EA SPLICES AT REPORT, FORM 46-0024, ENTERED BY UAL INS
- [SDR CALA2022072701896](https://openairdocs.org/sdr/CALA2022072701896.md): Power Supply · inoperative · Jul 26, 2022 · N35204 · Boeing 737824 · Emergency Lighting
  > AFT CABIN SEATS EMERGENCY LIGHT BATTERY PACK IS WEAK. SUPPORT TASK NSA EMX N/R 00149. TROUBLESHOT AND FOUND BAD EMERGENCY POWER SUPPLY AT STA 952 LEFT 00153. PERFORMED THE EMERGENCY ESCAPE PATH LIGHTING OPERATIONAL ENTERED BY UAL INSPECTION U354653, DATE 26JU
- [SDR CALA2022072001838](https://openairdocs.org/sdr/CALA2022072001838.md): Fitting · cracked · Jul 20, 2022 · N35204 · Boeing 737 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRAC KED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 ACCOMPLISHED BY V905004, AND INSPECTED BY V932009. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/R 0
- [SDR CALA2022072001837](https://openairdocs.org/sdr/CALA2022072001837.md): Fitting · cracked · Jul 20, 2022 · N35204 · Boeing 737 · Wing Structure
  > B737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 6.14 IS CRAC KED REMOVED AND REPLACED SHEAR FITTING AT STATION 54-0 AND LBL 6.14 INSPECTED BY V932009. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/R 00113 AND HANGER N/R 5867202
- [SDR CALA2022072001836](https://openairdocs.org/sdr/CALA2022072001836.md): Fitting · cracked · Jul 20, 2022 · N35204 · Boeing 737 · Wing Structure
  > B737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRA CKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 32.40 ACCOMPLISHED BY V905004, AND INSPECTED BY V932009. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/R
- [SDR CALA2022072001835](https://openairdocs.org/sdr/CALA2022072001835.md): Fitting · cracked · Jul 20, 2022 · N35204 · Boeing 737 · Wing Structure
  > B737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 40.87 IS CRA CKED REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 RBL 40.87 SSFR REPORT FORM 46-0024 ENTERED BY UAL INSPECTION U301243 IAW B737-800 SRM 51-40-02 AND DWG 111A2000 REV ORIGINAL DATA WAS DA
- [SDR CALA2022072001834](https://openairdocs.org/sdr/CALA2022072001834.md): Fitting · cracked · Jul 20, 2022 · N35204 · Boeing 737 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 LBL32.40 IS CRACKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 32.40 ACCOMPLISHED BY V905004, AND INSPECTED BY 932009. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/R 00115
- [SDR CALA2022072001833](https://openairdocs.org/sdr/CALA2022072001833.md): Fitting · cracked · Jul 20, 2022 · N35204 · Boeing 737 · Wing Structure
  > B737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRA CKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 15.04 ACCOMPLISHED BY V905004, AND INSPECTED BY V932009. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/R
- [SDR CALA2022072001832](https://openairdocs.org/sdr/CALA2022072001832.md): Fitting · cracked · Jul 20, 2022 · N35204 · Boeing 737 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 54.60 IS CRA CKED REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 AND SSFR REPORT, FORM 46-0024,ENTERD BY UAL INSPECTION U301243, RBL 54.60 IAW B737-800. SRM 51-40-02 AND DWG NO. 111A2000. 7-15-2022 REV
- [SDR CALA2022072001831](https://openairdocs.org/sdr/CALA2022072001831.md): Fitting · cracked · Jul 20, 2022 · N35204 · Boeing 737 · Wing Structure
  > B737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 15.04 IS CRA CKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 15.04 ACCOMPLISHED BY V905004, AND INSPECTED BY V932009. IAW B737-800 SRM 51-40-02 AND BAS DWG 111A2000 REV ORIGINAL SEE NSA EMX N/R
- [SDR CALA2022072001830](https://openairdocs.org/sdr/CALA2022072001830.md): Fitting · cracked · Jul 20, 2022 · N35204 · Boeing 737824 · Wing Structure
  > B737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 40.87 IS CRA CKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 40.87 ACCOMPLISHED BY V905004, AND INSPECTED BY V932009. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/R
- [SDR CALA2022072001814](https://openairdocs.org/sdr/CALA2022072001814.md): Fitting · cracked · Jul 20, 2022 · N35204 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 54.60 IS CRA CKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 54.60 ACCOMPLISHED BY V905004, AND INSPECTED BY V932009. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/R
- [SDR CALA2022071801777](https://openairdocs.org/sdr/CALA2022071801777.md): Fitting · cracked · Jul 15, 2022 · N35204 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKED
- [SDR CALA2022071801776](https://openairdocs.org/sdr/CALA2022071801776.md): Fitting · cracked · Jul 15, 2022 · N35204 · Boeing 737824 · Wing Structure
  > B737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 6.14 IS CRACKED
- [SDR CALA2022071801775](https://openairdocs.org/sdr/CALA2022071801775.md): Fitting · cracked · Jul 15, 2022 · N35204 · Boeing 737824 · Wing Structure
  > B737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 15.04 IS CRACKED
- [SDR CALA2022071801782](https://openairdocs.org/sdr/CALA2022071801782.md): Fitting · cracked · Jul 15, 2022 · N35204 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 54.60 IS CRACKED
- [SDR CALA2022071801781](https://openairdocs.org/sdr/CALA2022071801781.md): Fitting · cracked · Jul 15, 2022 · N35204 · Boeing 737824 · Wing Structure
  > B737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 40.87 IS CRACKED
- [SDR CALA2022071801779](https://openairdocs.org/sdr/CALA2022071801779.md): Fitting · cracked · Jul 15, 2022 · N35204 · Boeing 737824 · Wing Structure
  > B737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRACKED
- [SDR CALA2022071801778](https://openairdocs.org/sdr/CALA2022071801778.md): Fitting · cracked · Jul 15, 2022 · N35204 · Boeing 737824 · Wing Structure
  > B737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRA CKED
- [SDR CALA2022071501756](https://openairdocs.org/sdr/CALA2022071501756.md): Fitting · cracked · Jul 14, 2022 · N35204 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 LBL32.40 IS CRACKED
- [SDR CALA2022071501755](https://openairdocs.org/sdr/CALA2022071501755.md): Fitting · cracked · Jul 14, 2022 · N35204 · Boeing 737824 · Wing Structure
  > B737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 40.87 IS CRA CKED
- [SDR CALA2022071501753](https://openairdocs.org/sdr/CALA2022071501753.md): Fitting · cracked · Jul 14, 2022 · N35204 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 54.60 IS CRACKED
- [SDR CALA2022040800929](https://openairdocs.org/sdr/CALA2022040800929.md): Tire · damaged · Apr 7, 2022 · N35204 · Boeing 737824 · Tire Tube
  > PDA 1 REFERENCE #3 TIRE CAME APART WHICH CLASSIFIES AS A PDA EVENT REMOVED AND REPLACED #3 MLG TIRE FOR TREAD LOSS INSPECTION COMPLETION.#3 TIRE WAS REPLACED
- [SDR CALA2022040800920](https://openairdocs.org/sdr/CALA2022040800920.md): Tire · damaged · Apr 7, 2022 · N35204 · Boeing 737824 · Nose/Tail Landing Gear Attach Section
  > FOUND ON ARRIVIAL TO GATE,RH MLG,INBD TIRE SHREDDED,FLAT, AND MISSING INBD PLIES. REMOVED AND REPLACED #3 MLG TIRE IAW AMM 32-45-11-400-801. REF LOG PAGE 8337559 FOR TREAD LOSS INSPECTION COMPLETION. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1987286 SN OFF 03
- [SDR CALA2022040600895](https://openairdocs.org/sdr/CALA2022040600895.md): None · missing · Apr 6, 2022 · N35204 · Boeing 737 · Wing, Control Surface Attach Fittings
  > PDA 3 LEFT WING #2 SLAT HAS ONE FASTENER HEAD BROKEN OFF/MISSING AND ANOTHER LOOSE AT ACTUATOR ATTACH POINT -- SEE PHOTO PHOTO ADDED PHOTO ADDED PHOTO ADDED UPDATE -- ONE FASTENER MISSING AND 3 FASTENERS LOOSE -- SEE PHOTO INSTALLED MISSING HI LOCK AND TIGHTEN
- [SDR CALA2021101101848](https://openairdocs.org/sdr/CALA2021101101848.md): None · contaminated · Oct 11, 2021 · N35204 · Boeing 737824 · Hydraulic Power Accumulator, Main
  > *EMERGENCY DECLARED* LOSS OF SYS A HYD QTY FOLLOWED BY LOSS OF SYS A PRESSURE INFLIG HT RUN THRU. AN ADDITIONAL 30 SECONDS TO 1 MINUTE ELAPSED BEFORE EMDP SELECTED OFF. DEBRIEF OF F/O. HE STATED THAT AT CRUISE THE MASTER CAUTION CAME MATL AND LABOR UPDATED ON

Next page: https://openairdocs.org/aircraft/N35204/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 = 'N35204' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N35204/reports

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