# Service difficulty reports: N11206

A list on [N11206](https://openairdocs.org/aircraft/N11206.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 · 89 reports

- [SDR CALA2026061617139](https://openairdocs.org/sdr/CALA2026061617139.md): Light · detached · Jun 14, 2026 · N11206 · Boeing 737824 · Emergency Lighting
  > EXIT EMERGNCY LIGHT SEAT 15C TORN OUT REPLACED RED EEPL AT 15C REF AMM 33-51-11 OPS CHECK SAT.
- [SDR CALA2026021013659](https://openairdocs.org/sdr/CALA2026021013659.md): Stator · damaged · Feb 8, 2026 · N11206 · Boeing 737824 · Turbine Section
  > ON CLIMB OUT ENG 1 VIBE IND 4.3. TOMC CONTACTED.RETURN TO KDEN. AT CRUSIE VIB CAME DOWN TO 1.8- 2.3 PER CREW FOUND DAMAGE TO TURBINE BLDS LABOR HOURS UPDATE. PICTURES INCLUDED PICTURES INCLUDED. PICTURES INCLUDED. DUE DAMAGE TO AFT STAGE 4 ATP BLADE STATOR DAM
- [SDR CALA2026010712749](https://openairdocs.org/sdr/CALA2026010712749.md): Light · inoperative · Jan 6, 2026 · N11206 · Boeing 737824 · Emergency Lighting
  > WINDOW LIGHTS FROM 11FED TO 20FED INOPERATIVE. SUSPECT OVERWING EMERGENCY EXIT WINDOW LIGHT AT 20F FAULTY. REMOVED AND REPLACED FWD RT OVERWING EXIT WINDOW LIGHT IAW AMM 33-21-01A. SYSTEM OPS CHECK NORMAL.
- [SDR CALA2025121112019](https://openairdocs.org/sdr/CALA2025121112019.md): Slide · no discrepancy · Dec 7, 2025 · N11206 · Boeing 737824 · Escape Slide
  > R1 DOOR SLIDE PROTRUDING OUT OF BOTTOM OF CASING. INSPECTED SLIDE PACK AT R1 DOOR. SLIDE PACK GIRT BAR AREA NORMAL, NO EXCESS MATERIAL, NO DEFECTS NOTED, IAW AMM 25-66-01-400-801.
- [SDR CALA2025110710981](https://openairdocs.org/sdr/CALA2025110710981.md): Slide · no discrepancy · Nov 5, 2025 · N11206 · Boeing 737824 · Escape Slide
  > L2 SLIDE EXPOSED VISUALLY INSPECTED L2 DOOR SLIDE, NO DISCREPANCIES FOUND, VCK OK. REF: AMM TASK 25-66-01-200-802
- [SDR CALA2025102810626](https://openairdocs.org/sdr/CALA2025102810626.md): Slide · dislodged · Oct 25, 2025 · N11206 · Boeing 737824 · Emergency Equipment
  > RIGHT FWD ENTRY DOOR SLIDE HANGING OUT INSPECTED GIRT AND GIRT BAR, GIRT IS SECURED AND GIRT BAR OPERATES NORMAL. REF AMM 25-66-01.
- [SDR CALA2025091909056](https://openairdocs.org/sdr/CALA2025091909056.md): Lamp · inoperative · Sep 17, 2025 · N11206 · Boeing 737824 · Emergency Lighting
  > RIGHT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-04-960-801, OPS CHECKED GOOD.
- [SDR CALA2025091608953](https://openairdocs.org/sdr/CALA2025091608953.md): O-Ring · leaking · Sep 14, 2025 · N11206 · Boeing 737824 · Hydraulic System, Main
  > LOSS OF HYDRAULIC SYSTEM B PRESSURE AND QUANTITY IN FLIGHT. FOUND B SYS QTY AT ZERO. FOUND LEAK AT B SYS HYD MODULE PLUG. REPLACED PLUG ORING RETORQUED AND SAFTEID. WILL NEED LEAK CHECK WHEN HYDRAULICS ARE RESTORED. FOUND "B" SYSTEM HYDRAULIC RESERVOIR AT 0%
- [SDR CALA2025090808571](https://openairdocs.org/sdr/CALA2025090808571.md): Skin · cracked · Sep 1, 2025 · N11206 · Boeing 737824 · Wing, Plate/Skin
  > LEFT WING LOWER SKIN, STRINGER 9, OTBD MOST FASTENER CRACKED. MAJOR REPAIR, REPAIRED LT WING LOWER SKIN AT STRINGER 9 PER UAL ECRA 5730-03601 REV -.
- [SDR CALA2025082908265](https://openairdocs.org/sdr/CALA2025082908265.md): Elec Connector · disconnected · Aug 28, 2025 · N11206 · Boeing 737824 · Light System Wiring
  > AFT RT OVERWING EXIT EXTERIOR EMERGENCY LIGHT INOPERATIVE. CONNECTED THE ELEC CONNECTOR D12018 TO OVERWING ESCAPE LIGHT L7. OPS TESTED GOOD. IAW AMM 33-51-00 AND WDM 33-51- 14.
- [SDR CALA2025082508075](https://openairdocs.org/sdr/CALA2025082508075.md): Floorbeam · corroded · Aug 18, 2025 · N11206 · Boeing 737824 · Fuselage Main, Floor Beam
  > (B737-53-3-0737) MAIN CABIN FWD WET AREA LT STA 344 LBL50 FLOOR BEAM HAS CORROSION AT GALLEY FITTING AND TRACK. REPAIRED STA 344 FLOORBEAM PER UAL ECRA 5315-01226.
- [SDR CALA2025082007970](https://openairdocs.org/sdr/CALA2025082007970.md): Skin · wrinkled · Aug 16, 2025 · N11206 · Boeing 737824 · Cargo/Baggage Doors
  > AFT CARGO DOOR EXTERIOR SKIN REQUIRES RESKIN. REMOVED AND REPLACED AFT CARGO DOOR SKIN PN: 146A6112-2 IAW SRM 52-30-01-2R-3 SRM 51-40-02 AND DWG 146A6112.
- [SDR CALA2025082007969](https://openairdocs.org/sdr/CALA2025082007969.md): Skin · wrinkled · Aug 15, 2025 · N11206 · Boeing 737824 · Cargo/Baggage Doors
  > FOWARD CARGO DOOR SKIN REQUIRES RESKIN. REMOVED AND REPLACED OUTER DOORE SKIN PN: 143A612Y2 PO 1121069.1 IAW BAC 737-800 SRM 52-30-01-2R-3 REPAIR #3 AND SRM 51-40-02 AND BAC DWG 143A6110 SH 3 REV D.
- [SDR CALA2025082007968](https://openairdocs.org/sdr/CALA2025082007968.md): Floorbeam · corroded · Aug 13, 2025 · N11206 · Boeing 737824 · Fuselage Main, Floor Beam
  > SUPPORT TASK- FLOOR BEAM 947 UNDER LAV MOUNTS 45 L/H AND 45 R/H HAS CORROSION ON UPPER SECTION. CORROSION FOUND UNDER LAV HARD MOUNT AT STA 947.50 LBL AND RBL 51. MATERIAL LOSS MEASURED 100% FOUND TO BE OUT OF LIMITS. REMOVED PREVIOUS T-CAP REPAIR AT STA 9
- [SDR CALA2025081407738](https://openairdocs.org/sdr/CALA2025081407738.md): Floorbeam · corroded · Aug 13, 2025 · N11206 · Boeing 737824 · Fuselage Main, Floor Beam
  > STA 987 FLOORBEAM TEE CAP HAS CORROSION. EVALUATED CORROSION BS 986.5, ORIGINAL THICKNESS 0.150, REMAINING MATERIAL 0.053, REMOVED 0.097. RBL ORIGINAL THICKNESS 0.150, REMAINING MATERIAL 0.091, REMOVED 0.059. FOUND BOTH TO BE OUT OF LIMITS IAW SRM 51-10-08 AN
- [SDR CALA2025081407737](https://openairdocs.org/sdr/CALA2025081407737.md): Seat Track · corroded · Aug 13, 2025 · N11206 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > BS 328, LBL45 HAS CORROSION ON THE END OF SEAT TRACK. REMOVED CORROSION, ORIGINAL THICKNESS 0.135, LOSS 0.0195, REMAINING 0.115 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1 FIG 105 STEP B AND BAC DWG 141A5770 REV 'A'. LOCATED AND DRILLED NEW SEAT TRACK I
- [SDR CALA2025081307691](https://openairdocs.org/sdr/CALA2025081307691.md): Crease Beam · corroded · Aug 12, 2025 · N11206 · Boeing 737824 · Fuselage Main, Structure
  > SUPPORT TASK- R2 DOOR CREASE BEAM HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED R2 DOOR CREASE BEAM P/N: 147A854048 PO: 1124776.2 IAW B737-800 DRW: 147A8540 REV. B, SRM 51-40-05, SRM 51-40-02, ORIGINAL CREASE BEAM FOUND CORROSION 60% OF MATERIAL OUT
- [SDR CALA2025073107139](https://openairdocs.org/sdr/CALA2025073107139.md): Skin · dented · Jul 29, 2025 · N11206 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STAB L/E HAS DENT AT HSS 107 THAT REQUIRES A PERMANENT REPAIR PER SRM 55-10-01-1A-1. REMOVED DAMAGE IAW SRM 55-10-01-2R-1 REPAIR 1, FIG 202, FABRICATED DOUBLER REPAIR IAW SRM 55-10-01-2R-1 REPAIR 1 FIG 202. ALODINED & PRIMED REPAIR DOUBLER
- [SDR CALA2025072907033](https://openairdocs.org/sdr/CALA2025072907033.md): Stringer · corroded · Jul 24, 2025 · N11206 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > FWD PIT STRINGER IS CORRODED INSIDE U-CHANNEL AT APPROX BS 500G+7 S26L, UNDERNEATH. REMOVED CORROSION BS 500G+7 S26LT, ORIGINAL MAT. THICKNESS.045, MAT. REMAINING.035, MAT. LOSS.010 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1 & SRM 53-30-01. REMOVED STR
- [SDR CALA2025072907030](https://openairdocs.org/sdr/CALA2025072907030.md): Web · damaged · Jul 9, 2025 · N11206 · Boeing 737824 · Fuselage Main, Structure
  > FLIGHT COMPARTMENT FLOOR STRUCTURE BETWEEN BS 250-260 LBL 17 TO RBL3 HAS DENT AT MULTIPLE PLACES. REMOVED 2 EACH DAMAGED AREAS BETWEEN STA 250 TO 260 LBL2 AND LBL13 IAW SRM 53-10-51-2R-2, REPAIR 2 SECTION 41 FLOOR WEB FIG 203. INSTALLED REPAIR DOUBLER BETWEEN
- [SDR CALA2025050604497](https://openairdocs.org/sdr/CALA2025050604497.md): Switch · faulted · May 2, 2025 · N11206 · Boeing 737824 · Door Warning System
  > DOOR LIGHT WITH MASTER CAUTION AT 100FEET BEFORE LANDING.UNKOWN WHICH DOOR. DUE TO HISTORY. REQUEST FWD CARGO DOOR INDICATION BE PLACED ON MEL 5203D. DDP CW. INTERROGATED PSEU AND NOTED MESSAGE # 52-72001. FAULT IS INTERMITTENT. SUSPECT FAULTY PROX SENSOR S96
- [SDR CALA2025041803982](https://openairdocs.org/sdr/CALA2025041803982.md): Oven · dirty · Apr 16, 2025 · N11206 · Boeing 737824 · Buffet/Galleys
  > OVEN SMOKING OR SPARKING 205 LIGHT SMOKE EMITTED FROM BOTTOM/LEFT SIDE OF OVEN WHEN COOKNG. PREFORMED CONDITIONAL INSPECTION IAW AMM 05-51-26-800-801-C1 FOUND TO BE BURNT FOOD FROM OVEN 205 NO OTHER DEFECTS NOTED.
- [SDR CALA2025042204131](https://openairdocs.org/sdr/CALA2025042204131.md): Window · sparks · Apr 15, 2025 · N11206 · Boeing 737824 · Flight Compartment Windows
  > WINDOW HEAT OVERHEAT LIGHT LIGHT ON L SIDE VISIBLE SPARKS FROM LOWER REAR CORNER. INSPECTED WINDOW, PLACED WINDOW HEAT ON MEL INSPECTED WINDOW, PLACED WINDOW HEAT ON MEL. CREW STATED SPARKS EXTENDED TO BACK OF MOUNTED IPAD REF FIM 30-41 TASK 801, FOUND FAU
- [SDR CALA2025041403791](https://openairdocs.org/sdr/CALA2025041403791.md): Proximity Sensor · faulty · Apr 10, 2025 · N11206 · Boeing 737824 · Trailing Flap Position Indicating System
  > LE FLAP TRANSIT LGT IN FLIGHT FLAPS UP. LE 1 SHOWS EXENDED WITH FLAPS UP. PERFORMED BITE TEST FOR FLAP AND SLAT BOX REF AMM 27-51 TASK801. AND FOUND FAULT. ADD PIC INSTALLED R-Y-B SPLICES FOR SENSOR S169. REF WDM 27-81-11-901. FOUND SENSOR S169 FAULTY WHILE T
- [SDR CALA2025021002261](https://openairdocs.org/sdr/CALA2025021002261.md): Battery Pack · discharged · Feb 6, 2025 · N11206 · Boeing 737824 · Emergency Lighting
  > FIRST CLASS AND MID CABIN AISLE EMERGENCY LIGHT INOP LET BATTERIES CHARGE REF FIM 33-50 TASK 801, OPS CK GOOD
- [SDR CALA2025020302180](https://openairdocs.org/sdr/CALA2025020302180.md): Overheat Sensor · faulted · Jan 30, 2025 · N11206 · Boeing 737824 · Overheat Detection
  > RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED ON CLI MBOUT EXTINGUIS HED AFTER RUNNING CHECKLIST C/W OVERHEAT DETECTION CONTROL MODULE MEMORY AND READ PROCEDURE FOUND MAINT. ADV. LIGHT ON ALONG WITH CODE 64 AND 97 REF AMM 26-18-01-740-801 T/S REF FIM 26-18 TASK 8
- [SDR CALA2024101800861](https://openairdocs.org/sdr/CALA2024101800861.md): Anti-Ice Valve · faulty · Oct 16, 2024 · N11206 · Boeing 737824 · Engine Anti-Icing System
  > COWL VALVE OPEN LIGHT STAYS ON BRIGHT WHEN THE ENG ANTI-ICE SWIT CH IS MOVED TO ON ENG-1 ENG 1 COWL OPEN LIGHT ON WHEN ENG ANTI ICE ON AMBER TAI ON INST PANEL VALVE ANTI ICE #1 ENGINE ROTABLE PART CHANGE. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1405558 SN O
- [SDR CALA2024050701349](https://openairdocs.org/sdr/CALA2024050701349.md): None · none · May 3, 2024 · N11206 · Boeing 737824 · Standard Practices/Structures
  > REPORTING SSFR FOR LEFT HAND WINDOW POST EA 5310-04554 OP 003 UPDATE SSFR FOR EA 5310-04554 OP 003 FOR LEFT HAND WINDOW POST UAL QC UPDATED SSFR FOR AC 0206 FOR LEFT HAND WINDOW POST ON EA 5310-04554 OP 003
- [SDR CALA2024050701348](https://openairdocs.org/sdr/CALA2024050701348.md): None · none · May 3, 2024 · N11206 · Boeing 737824 · Standard Practices/Structures
  > REPORTING SSFR FOR AC 0206 RIGHT WINDOW POST REF EA 5310-04554 UPDATE FOR SSFR FPR EA 5310-04554 OP 004 UAL QC COMPLETED SSFR FOR RIGHT HAND WINDOW POST EA 5310-04554 O P 004
- [SDR CALA2023092902919](https://openairdocs.org/sdr/CALA2023092902919.md): Coupling · worn · Sep 26, 2023 · N11206 · Boeing 737824 · Trailing Edge Flap Actuator
  > FLAP ASYMMETRY/LOCKOUT AT APPROX 25 DEGREES CREW DEBRIEF FLAP ASYMMETRY ON APPROACH WITH FLAPS AT 25 DEGREES. EXTENDED FLAPS TO 30 AND FLAPS LOCKED OUT. FLAP INDICATION SHOWS ASYMMETRY AND LOW HYD LEVEL B SYSTEM. PERFORMED FSEU BITE REF FIM 27-51 TASK 801 WITH
- [SDR CALA2023050301332](https://openairdocs.org/sdr/CALA2023050301332.md): Packing · leaking · May 3, 2023 · N11206 · Boeing 7378 · Autopilot Computer
  > HYDRAULIC FLUID QUANTITY INDICATION SHOWS RF (76%) SYSTEM A SYS A HYD SLOWLY DECREASES APPROX 1 PCT DECREASED TO30 PCT. LEAKING FROM REDUCER ON AUTOPILOT ELEVATOR ACTUATOR. LEAK OBSERVED FROM LEFT ELEVATOR PCU AT THIS TIME. DISCONNECTED HYDRAULIC PRESSURE LINE
- [SDR CALA2022122603483](https://openairdocs.org/sdr/CALA2022122603483.md): Power Supply · defective · Dec 23, 2022 · N11206 · Boeing 737824 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS INOP AT ROWS 15-21 INCLUDING LEFT FORWARD EMERGENCY EXIT DOOR LIGHT AND RIGHT FORWARD EMERGENCY EXIT DOOR LIGHT. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06. NO HELP. PROBLEM CONTINUES. REINSTALLED ORIGINAL BATTERY PACK. NEEDS NEW
- [SDR CALA2022120203272](https://openairdocs.org/sdr/CALA2022120203272.md): Warning Horn · false activation · Dec 2, 2022 · N11206 · Boeing 737824 · Central Warning
  > REJECTED TAKEOFF AT 130 KNOTS FOR TAKEOFF CONFIG LIGHT AND HORN. NOTHING OUT OF PLACE. PERFORMED HIGH ENERGY STOP INSPECTION FOR CAUTION RANGE IAW AMM 05-51-07-210-801. NO DAMAGE NOTED PERFORMED HIGH ENERGY STOP INSPECTION FOR CAUTION RANGE IAW AMM 05-51-07-
- [SDR CALA2022111403126](https://openairdocs.org/sdr/CALA2022111403126.md): Lamp · inoperative · Nov 12, 2022 · N11206 · Boeing 737824 · Emergency Lighting
  > L-1 DOOR EMERGENCY LIGHT EXTERIOR IS INOP - SUPPORT TASK NSA EMX NR 00124
- [SDR CALA2022111103100](https://openairdocs.org/sdr/CALA2022111103100.md): None · none · Nov 11, 2022 · N11206 · Boeing 737824 · Standard Practices/Structures
  > DISPLACE SEAT ROW 15 ABC TO FOM - REINSTALL ON THIS CARD (IDT) - SUPPORT TASK NSA EMX NR 00013 REMOVED AND REINSTALLED SEAT ROW 15ABC IAW B737NG AMM 25-22-00-0 SYSTEM IAW B737NG AMM 23-34-00-710-801. IN SEAT POWER SUPPLY SYS CHECKED EMERGENCY LIGHT SEAT 15 ABC
- [SDR CALA2022110703053](https://openairdocs.org/sdr/CALA2022110703053.md): Fitting · cracked · Nov 5, 2022 · N11206 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STATION 540 AND LBL 6.14 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA. 540 LBL 6.14 IAW SRM 51-40-02 AND DWG 11A2000 REV ORGINAL.
- [SDR CALA2022110703058](https://openairdocs.org/sdr/CALA2022110703058.md): Fitting · cracked · Nov 5, 2022 · N11206 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STATION 540 AND LBL 32.40 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 AND LBL 32.40 IAW SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL
- [SDR CALA2022110703057](https://openairdocs.org/sdr/CALA2022110703057.md): Fitting · cracked · Nov 5, 2022 · N11206 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRA CKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 AND RBL 32.40 IAW SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL
- [SDR CALA2022110703056](https://openairdocs.org/sdr/CALA2022110703056.md): Fitting · cracked · Nov 5, 2022 · N11206 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 AND RBL 15.04 IAW SRM 51-40-02 AND DWG 111A2000 REV. ORIGINAL
- [SDR CALA2022110703055](https://openairdocs.org/sdr/CALA2022110703055.md): Fitting · cracked · Nov 5, 2022 · N11206 · Boeing 737824 · Fuselage Miscellaneous Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRAC KED. SUPPORT TASK NSA N/R 00082 REMOVED AND REPLACED SHEAR FITTING AT STA. 540 AND RBL 6.14 AND HANGER IAW SRM 51-40-02 AND DWG 111A2000 REV. ORIGINAL.
- [SDR CALA2022110703054](https://openairdocs.org/sdr/CALA2022110703054.md): Fitting · cracked · Nov 5, 2022 · N11206 · Boeing 737824 · Wing Miscellaneous Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 15.04 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA. 540 AND LBL 15.04 AND HANGER IAW SRM 51-40-02 AND BAC DWG 111A2000 REV. ORIGINAL.
- [SDR CALA2022093002567](https://openairdocs.org/sdr/CALA2022093002567.md): Battery Pack · none · Sep 29, 2022 · N11206 · Boeing 737 · Lighting System
  > EMERGENCY BATTERY PACKS M1694 INOP (REF. AAR NR 99945400).
- [SDR CALA2022093002568](https://openairdocs.org/sdr/CALA2022093002568.md): Battery Pack · none · Sep 29, 2022 · N11206 · Boeing 737 · Lighting System
  > EMERGENCY BATTERY PACK M1695 INOP (REF. AAR NR 9945399).
- [SDR CALA2022072001839](https://openairdocs.org/sdr/CALA2022072001839.md): None · missing · Jul 20, 2022 · N11206 · Boeing 737 · Trailing Edge Flaps
  > PDA 3 RIGHT WING MAIN INBD T/EDGE FLAP COMPLETELY MISSING SEAL AT OUTBD END LOWER POSITION -- SEE PHOTO PHOTO ADDED INSTALLED NEW SEAL AT OUTBD END LOWER POSITION OF INBOARD MAIN FLAP ON RIGHT WING. REF IPC 27-51-11-01.
- [SDR CALA2022050201122](https://openairdocs.org/sdr/CALA2022050201122.md): None · faulty · May 2, 2022 · N11206 · Boeing 737 · Attitude Gyro and Indicating System
  > SPD LIM AMBER FLAG ON CA SIDE. STICK SHAKER INTERMITENT. HORIZO NTAL FD INOP DURING CLIMBOUT. REMOVED AND REPLACED CAPTAIN SIDE (LEFT) AOA SENSOR REF AMM AOA PARTS ENTRY 34-21-05 UP TO AND INCLUDING STEPS G. (7). NEXT STEP IS (8) ROTABLE PARTS CHANGE WAS INDI
- [SDR CALA2021091701597](https://openairdocs.org/sdr/CALA2021091701597.md): Proximity Sensor · failed · Sep 17, 2021 · N11206 · Boeing 737824 · Leading Edge Slat Position Indicating System
  > LE FLAPS TRANSIT LIGHT ILLUMINATED AT FLAPS 10 AND REMAINED ON A T FLAPS 15 UNTIL RETRACTD FSEU BITE CAPTURED LEG-0 SL1 PROX INBOARD MSG 27-81201 INTRMTNT WHEN RUN FLAPS UP & DWN AT UNIT 1 LE MID EXTEND #1 SLAT JERKS AN D AT UNIT 10 LE FULL EXTEND #1 SLAT JE
- [SDR CALA2021090101465](https://openairdocs.org/sdr/CALA2021090101465.md): Light · damaged · Aug 31, 2021 · N11206 · Boeing 737824 · Emergency Lighting
  > SEAT MOUNTED EMERGENCY LIGHT AT ROW 32ABC LENS IS DAMAGED. REMOVED AND REPLACED WHITE LIGHT ASSY REF MM 33-51-11 AND CONFIGURATION DRAWING 3350DD14743. OPS CK OK. VERIFIED IDT REQUIREMENTS
- [SDR CALA2019102301794](https://openairdocs.org/sdr/CALA2019102301794.md): Handle · unsecure · Oct 21, 2019 · N11206 · Boeing 737824 · Passenger/Crew Doors
  > L1 FWD ENTRY DOOR LIGHT ILLUMINATED AT APPROX 9OKTS VERIFIED WITH INFLIGHT CREW THAT DOOR WAS NOT CLOSED ALL THE WAY. OPERATED DOOR, MANIPULATED HANDLE AND HANDLE STAYED IN PLACE AND LOCKED. NO OTHER DEFAULTS NOTED.
- [SDR CALA2019072801259](https://openairdocs.org/sdr/CALA2019072801259.md): Brake Disc · separated · Jul 27, 2019 · N11206 · Boeing 737824 · Brake
  > DURING #2 TIRE CHANGE NOTICED WHEEL EXTREMLY HOT UPON INSP FOUND #2 BRAKE DISC SEPERATED REMOVED AND REPLACED #2 MLG BREAK REF AMM 32-41-41 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1264009 SN OFF 0633 IPC REFERENCE # 32-41-41-01-085 BRAKE, MLG, CAR OFF 60-3
- [SDR CALA2019042600646](https://openairdocs.org/sdr/CALA2019042600646.md): Lock Fastener · missing · Apr 24, 2019 · N11206 · Boeing 737824 · Leading Edge Devices
  > PDA 3 REF L/P 3062264 FOR HI-LOK MISSING FROM #4 SLAT. REF L/P 3062264 FOR INSTALLATION OF FASTENER P/N HL111 6-4.

Next page: https://openairdocs.org/aircraft/N11206/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 = 'N11206' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N11206/reports

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