# Service difficulty reports: N36207

A list on [N36207](https://openairdocs.org/aircraft/N36207.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 · 102 reports

- [SDR CALA2026090419236](https://openairdocs.org/sdr/CALA2026090419236.md): Bleed Valve · faulted · Sep 1, 2026 · N36207 · Boeing 737824 · APU Core Engine
  > DUE TO ACFT DIVERSION DUE TO APU BLEED NOT TURNING OFF AFTER A BLEEDS OFF TAKE OFF, ETOPS V-FLT REQUIRED, APPLYING PLA 06921. REMOVED AND REPLACED APU BLEED VLV I.A.W. AMM 49-52-11-400-801. LEAK CHK AND OPS CHECK COMPLETE. NO FURTHER DEFECTS NOTED. PARTS USED:
- [SDR CALA2026080318225](https://openairdocs.org/sdr/CALA2026080318225.md): Skin · gouged · Aug 2, 2026 · N36207 · Boeing 737824 · Fuselage Main, Plate/Skin
  > SKIN REPAIR ON ORIGINAL LP 9727321 COMPLETED ESFR PER GMM 04-20-05 VERIFIED SFR COMPLETED PER GMM 04-20-05. DIP CREATED ON LP 9824565. ALL STEPS FOR GMM 04-20-05 HAVE BEEN COMPLIED WITH AND ESFR FOR LP 9727321 HAVE BEEN UPDATED AND VERIFIED.
- [SDR CALA2026072718039](https://openairdocs.org/sdr/CALA2026072718039.md): Skin · gouged · Jul 26, 2026 · N36207 · Boeing 737824 · Fuselage Main, Plate/Skin
  > RAMP REPORTS GOUGE ON LT FUSELAGE UNDER CAPTAIN'S SIDE WINDOW. DENT LOCATED BTWN BS 251.5 - 259.5, & STRINGERS 19-20L.. REMOVED SCRATCH IAW SRM 53-00-01-1A-1, PAR 2.E, & PAR 4.B(2)(D), FIG 103 DETAIL C. PERFORM HFEC AFTER BLENDED AT BS 245.5 8" ABOVE STR 1
- [SDR CALA2025081507801](https://openairdocs.org/sdr/CALA2025081507801.md): Transceiver · inoperative · Aug 15, 2025 · N36207 · Boeing 737824 · Weather Radar System
  > RADAR WAS WORKING MOST OF FLT, THEN RECEIVED WXR FAIL MSG. PERFORM FIM 34-43 TASK 801. REMOVED AND REPLACED WX RADAR R/T UNIT IAW AMM 34-43-41-000-801. WX RADAR SYSTEM TEST GOOD OK FOR SERVICE.
- [SDR CALA2025071606616](https://openairdocs.org/sdr/CALA2025071606616.md): Floorbeam · corroded · Jul 14, 2025 · N36207 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN CABIN, BS 344, BL 0 - LBL 12 FLOORBEAM CORRODED ON UPPER SURFACE. ACCOMPLISHED PERMANENT REPAIR IAW G25507 STAGE 5, REO-G25507 REV IR, AND ECRA 5310-08638, CATEGORY A REPAIR.
- [SDR CALA2025071606615](https://openairdocs.org/sdr/CALA2025071606615.md): Floorbeam · corroded · Jul 13, 2025 · N36207 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN CABIN BS 344, LBL 55, FLOORBEAM CORRODED ON UPPER SURFACE. ACCOMPLISHED PERMANENT REPAIR IAW REO-G25507, STAGE 4, REO-G25507 REV IR, AND ECRA 5310-08638. CATAGORY A REPAIR.
- [SDR CALA2025071606614](https://openairdocs.org/sdr/CALA2025071606614.md): Window Frame · cracked · Jul 13, 2025 · N36207 · Boeing 737824 · Fuselage Main, Structure
  > LEFT NR 3 WINDOW FRAME CRACKED, FOUND IN HOLE NR 3. ACCOMPLISHED PERMANENT REPAIR TO THE WINDOW FRAME IAW EA-5310-01895-003 AND REO G25486, STAGE 1 AND 5310-08641.
- [SDR CALA2025071506574](https://openairdocs.org/sdr/CALA2025071506574.md): Skin · cracked · Jul 3, 2025 · N36207 · Boeing 737824 · Wing, Plate/Skin
  > TWO CRACK INDICATIONS LT WING LOWER LE SKIN SURFACE BETWEEN WSTA 564.5 AND WSTA 591.5, NR 1 EMANATING FROM LOWER FWD SPAR CHORD FASTENER, THRU FWD ROW O/B S-9 FASTENER MARKED 5,500"L. NR 2 EMANATING FROM OB AFT S-9 ROW FASTENER.150"L.
- [SDR CALA2025070806332](https://openairdocs.org/sdr/CALA2025070806332.md): Strap · cracked · Jul 3, 2025 · N36207 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CRACK INDICATIONS FOUND RT SIDE BS639 I/B STUD BEAM STRAP, AFT LOWER HOLE, IN I/B STRAP AT 3 AND 5 O'CLOCK POSITIONS AS VIEWED FROM O/B. REMOVED AND REPLACED SUTB BEAM CRACKED STRAP IAW BAC DWG 144A1705 REV B AND UAL ECRA 5340-02235 AND EA5340-02153 ESFR COMP
- [SDR CALA2025062005736](https://openairdocs.org/sdr/CALA2025062005736.md): Floorbeam · corroded · Jun 19, 2025 · N36207 · Boeing 737824 · Fuselage Main, Floor Beam
  > (SUPPORT TASK) MAIN CABIN FLOOR BEAM REPAIR REQUIRES -8 AND -9 FILLERS TO BE REMADE. REMOVED STIFFENER 1EA AND 2EA FILLERS, FABRICATED MAT ID, ALODINED,PRIMED AND INSTALLED 2EA FILLERS. AND REINSTALL 1EA STIFFENER PER HAECO PROGRESSIVE REO-G25491, STAGE 6, A
- [SDR CALA2025062005733](https://openairdocs.org/sdr/CALA2025062005733.md): Floorbeam · corroded · Jun 18, 2025 · N36207 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR BEAM AT STA 986 RBL 43 R LBL43 CORRODED ON UPPER SURFACE IN MULTIPLE AREAS REMOVED OLD REPAIR FLOOR BEAM AT STA986 IAW B737-800 AND LOCATED AND DRILLED NEW T-CHORD ANGLES AND STRAPS IAW B737-800 SRM 53-70-51-2R-4 SRM 51-40-05. INSTALLED NEW
- [SDR CALA2025062005732](https://openairdocs.org/sdr/CALA2025062005732.md): Door Sill · corroded · Jun 14, 2025 · N36207 · Boeing 737824 · Fuselage Main, Structure
  > (B737-53-3-0711) MAIN CABIN R2 LOWER INNER CHORD CORRODED ON UPP ER SURFACE IN MULTIPLE AREAS REMOVED AND REPLACED LOWER INNER SILL CHORD REMOVED R2 LOWER INNER CHORD, RECIVED NEW R2 INNER LOWER CHORD M AT ID PO# 1122020.1 IAW B737-800 SRM 51-40-02 DWG NO. 14
- [SDR CALA2025062005731](https://openairdocs.org/sdr/CALA2025062005731.md): Skin · dented · Jun 14, 2025 · N36207 · Boeing 737824 · Cargo/Baggage Doors
  > CUSTOMER REQUEST - FWD CARGO DOOR, HAS MULTIPLE DENTS THAT REQUIRE EVAL REPAIR DOUBLER INSTALLED PREVIOUSLY ON SKIN. REMOVED AND REPLACED FWD CARGO DOOR OUTER SKIN IAW B737 SRM 52-30-01-2R-3 REPAIR NO.3 REMOVED AND REPLACED LEVELING COMPOUND IAW ECRA 5235-01
- [SDR CALA2025061705619](https://openairdocs.org/sdr/CALA2025061705619.md): Floorbeam · corroded · Jun 14, 2025 · N36207 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN CABIN STA 328 FLOORBEAM RBL55 CORRODED ON UPPER SURFACE. SRM 53-10-51 2R-7 PGS.1-30 REMOVED CORROSION ON FLOOR BEAM STA 328 RBL55 ORIG.125 DEPTH.021 REMAINING MATERIAL.104. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51. REPAIRED THE FLOORBEAM IAW SRM 53-
- [SDR CALA2025080807488](https://openairdocs.org/sdr/CALA2025080807488.md): Skin · dented · Jun 10, 2025 · N36207 · Boeing 737824 · Cargo/Baggage Doors
  > AFT CARGO DOOR, MULTIPLE DENTS IN THE OUTER SKIN REQUIRES EVALUATION. REMOVED DENTED OUTER SKIN AND INSTALLED A NEW OUTER SKIN IAW DWG 146A6110 REV: A, SRM 51-40-02. ALODINED, PRIMED TOP COATED, & STENCILED OUTER SKIN IAW AMM 51-21-41, 51-21-72, 51-21-99 & 2
- [SDR CALA2025061105459](https://openairdocs.org/sdr/CALA2025061105459.md): Transition Panel · corroded · Jun 8, 2025 · N36207 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT R/H TRANSITION PANEL FROM STA 500A-500I IS CORRODED ESFR INFO UPDATED REMOVED CORROSION ORIGINAL MAT.040 REMOVED.007 OUT OF LIMITS REMAINING.033 IAW B737-800 SRM 53-00-53. LOCATED AND DRILLED IAW B737-800 SRM 51-10-05. ALODINED AND PRI
- [SDR CALA2025071506568](https://openairdocs.org/sdr/CALA2025071506568.md): Deck Plate · dented · Jun 5, 2025 · N36207 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FLIGHT COMPARTMENT FLOOR WEB IS DEFORMED JUST FWD OF THE FLIGHT DECK ENTRY AT APPROX STA 256 BETWEEN APPROX LBL10 AND BL4. REMOVED INCOMING REPAIR DOUBLER AND FILLER, REMOVED DAMAGED AREA AT LBL3 BETWEEN BS 250 AND 260. INSTALLED NEW REPAIR DOUBLER 1 EACH, 1
- [SDR CALA2025060505295](https://openairdocs.org/sdr/CALA2025060505295.md): Support · corroded · Jun 3, 2025 · N36207 · Boeing 737824 · Fuselage Miscellaneous Structure
  > (B737-53-3-0711) MAIN CABIN LAV SUPPORT INTERCOSTAL STA 947 - 967 RBL 45 CORRODED ON UPPER SURFACE. REMOVED AND REPLACED INTERCOSTAL STA 947 TO 967 RBL45 IAW B737-800 SRM 51-40-02 AND BAC DWG 147A5760 REV:-. EVALUATED ORIG.080 DEPTH.045 REMAINING.035 FOUND
- [SDR CALA2025060505293](https://openairdocs.org/sdr/CALA2025060505293.md): Floor Support · corroded · Jun 3, 2025 · N36207 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN LAV SUPPORT INTERCOSTAL STA 947-967 LBL 25 CORRODED ON UPPER SURFACE REMOVED AND EVALUATED CORROSION AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51. REMOVED AND REPLACED FLOOR SUPPORT IAW B737-800 SRM 51-40-02 SRM 53-70-51, BOEING DWG NO.
- [SDR CALA2025080807487](https://openairdocs.org/sdr/CALA2025080807487.md): Transition Panel · corroded · Jun 2, 2025 · N36207 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT RT TRANSITION PANEL FROM BS 727F - 767 WAS CORRDOED. REMOVED CORROSION ON AFT CARGO RT TRANSITION PANEL BS 727E+10 - 767 IAW SRM 51-10-02. ORIGINAL THICKNESS.040, REMOVED UP TO.025 REMAINING.015, FOUND TO BE OUT OF LIMITS IAW SRM 53
- [SDR CALA2025080807486](https://openairdocs.org/sdr/CALA2025080807486.md): Floor Support · corroded · Jun 2, 2025 · N36207 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SUPPORT TASK: AFT CARGO COMPARTMENT R/H FLOOR SUPPORT AT BS 727A - 727B RBL 6 IS CORRODED ON INBOARD SURFACE REMOVED CORROSION ON FLOOR SUPPORT, ORIGINAL MAT'L.045", REMAINING.031" OUT OF LIMITS IAW SRM 53-60-53-01-2 AND SRM 53-00-04-2A-1, LOCATED AND DRILL
- [SDR CALA2025070206133](https://openairdocs.org/sdr/CALA2025070206133.md): Floor Support · corroded · May 28, 2025 · N36207 · Boeing 737824 · Fuselage Miscellaneous Structure
  > (B737-53-3-0711) MAIN CABIN STA 344 TO 328 LBL 22 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PN 141A5730 PER B737-800 SRM 51-40-02 AND DWG 141A5730 REV B. REMOVED AND REINSTALLED STIFFENER PER B737-800 SRM 51-40-02.
- [SDR CALA2025070206132](https://openairdocs.org/sdr/CALA2025070206132.md): Floor Support · cracked · May 28, 2025 · N36207 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 344 TO STA 328 LBL 47 INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL PN 141A5410U141 PER B737-800 SRM 51-40-02 AND BAC DWG 141A5900 REV -.
- [SDR CALA2025070206131](https://openairdocs.org/sdr/CALA2025070206131.md): Floor Support · corroded · May 28, 2025 · N36207 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 344-328 LBL 43 FLOOR SUPPORT CORRODED ON UPPER SURFACE. REMOVED AND REINSTALLED FLOOR STIFFENER, REMOVED AND REPLACED FLOOR SUPPORT PN 141A5770U3 PER B737-800 SRM 51-40-02 AND BOEING DWG 141A5730 REV B.
- [SDR CALA2025053005119](https://openairdocs.org/sdr/CALA2025053005119.md): Intercostal · cracked · May 25, 2025 · N36207 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 312 TO LBL 46 INTERCOSTAL CRACKED REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN STA 312 TO STA 328 LBL 46 PER DWG 141A5400 PART #141A54104139 PO #1121452-1. REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN STA 312 TO STA 328 LBL 46 PER DWG 141A5
- [SDR CALA2025061105456](https://openairdocs.org/sdr/CALA2025061105456.md): Channel · corroded · May 23, 2025 · N36207 · Boeing 737824 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) FWD CARGO COMPARTMENT L/H TRANSITION PANEL FROM STA 500B-500I CORRODED TRANSCRIBED FROM HAECO GSO NR 9286634 SFR COMPLETED REMOVED CORROSION ORIGINAL MAT'L.040, REMOVED.020 OUT OF LIMITS, REMAINING.020 IAW B737-800 SRM 53-00-53. LOCATED AND
- [SDR CALA2025052104888](https://openairdocs.org/sdr/CALA2025052104888.md): Floor Support · cracked · May 15, 2025 · N36207 · Boeing 737824 · Fuselage Miscellaneous Structure
  > (B737-53-3-0711) MAIN CABIN STA 277-294.5 BLO INTERCOSTAL CRACKED TRANSCRIBED FROM HAECO GSO NR 9286425 REMOVED AND REPLACED 141A5410U139 INTERCOSTAL AT STATION 277- 294.5 BL0 PER B737-53-3-0711 SRM 51-40-02 REF HAECO GSO MECH V951638 INSP QC340 SFR INFO UPDA
- [SDR CALA2025031402827](https://openairdocs.org/sdr/CALA2025031402827.md): Slide · unsecure · Mar 14, 2025 · N36207 · Boeing 737824 · Escape Slide
  > 2L SLIDE PACK FALLING OUT INSPECTED SLIDE 2L, SLIDE IS NOT HANGING OR HAS NO EXCESSIVE MATERIAL SHOWING REF AMM 25-66-01. NO DEFECTS NOTED.
- [SDR CALA2025022002382](https://openairdocs.org/sdr/CALA2025022002382.md): Pseu · malfunctioned · Feb 16, 2025 · N36207 · Boeing 737824 · Landing Gear Position and Warning
  > PSEU LIGHT AFTER LDG UPON ARRIVAL, LIGHT WAS OFF IN COCKPIT. PROCEEDED WITH BITE CHECK AS PER FIM 32-09 TASK 801.FOUND 2 FAULTS IN EXISTING FAULTS 32-64003 AND 52-72023. REQUEST DEFERRAL. MEL 3217C REJECTED DUE TO SECOND CODE 52-72023 NOT APPLICABLE PER THIS M
- [SDR CALA2025021102293](https://openairdocs.org/sdr/CALA2025021102293.md): Switch · faulty · Feb 9, 2025 · N36207 · Boeing 737824 · Door Warning System
  > INBOUND FLIGHT CREW REPORT PSEU LIGHT ON AFTER LANDING. LIGHT WENT AWAY AFTER TAXI IN. ACP PSEU BITE TEST. FAULT MSG 52-72023. R FWD OW SWITCH DSGR R FWD OVERWING SWITCH DISAGREE MSG INTERMITTENT. REQUESTING MEL 5203P. TOMC OK COMPLIED WITH MEL 5302P. ACP PSEU
- [SDR CALA2024022100492](https://openairdocs.org/sdr/CALA2024022100492.md): Flap · dented · Feb 17, 2024 · N36207 · Boeing 737824 · Leading Edge Devices
  > BIRDSTRIKE/FOD. AT 2037Z FELT STRIKE UNDER AND ON RT SIDE OF FUSELAGE UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID V900885 MAC RELATED WORK ORDER 000000003097366 AND PRTR G
- [SDR CALA2024021500431](https://openairdocs.org/sdr/CALA2024021500431.md): Warning Light · illuminated · Feb 11, 2024 · N36207 · Boeing 737824 · Passenger/Crew Doors
  > CREW REPORTS DOOR 2L INDICATION LIGHT ON DURING TAKEOFF. PERFORMED PSEU ENTRY AND GALLEY SERVICE DOOR MONITORED PROBLEM - FAULT ISOLATION PER FIM 52-10 TASK 801. NO FAULTS FOUND. INSPECTED DOOR 2L PROX SWITCH. NO DAMAGE FOUND. OPS CHECK GOOD.
- [SDR CALA2023091302776](https://openairdocs.org/sdr/CALA2023091302776.md): Door · unknown · Sep 10, 2023 · N36207 · Boeing 737824 · Doors
  > AFT ENTRY DOOR LIGHT ON DURING TAKEOFF ROLL REJECTED TAKEOFF PLACED ON MEL. PLACED ON MEL. C/W PLACRD. TOMC APPROVED. ACCOMPLISHED COOL DOWN PERIOD PER AMM TASK 05-51-07-210-801 CHECKED TIRE PRESSURE NO FAULT NOTED.OPS CHECK GOOD. OK FOR SERVICE. REVERSED ME
- [SDR CALA2023062101958](https://openairdocs.org/sdr/CALA2023062101958.md): Flap · warning light · Jun 18, 2023 · N36207 · Boeing 7378 · Flight Control System
  > FLAP DISAGREE INITIAL EVALUATION FLAP DISAGREE NOT INDICATED AND FLAP POSITION AGREES WITH FLAP SETTING. CYCLED FLAPS FULL UP AND FULL DOWN, NO DISAGREE FOUND, REF AMM27-51-00.
- [SDR CALA2023050501366](https://openairdocs.org/sdr/CALA2023050501366.md): Seal · missing · May 5, 2023 · N36207 · Boeing 737824 · Trailing Edge Flaps
  > PDA 2 LEFT I/B FLAP, O/B BULB SEAL IS MISSING FROM TRACK. SEAL MISSING IS ROUGHLY 24IN LONG. NEEDS LOWER BULB SEAL M&E 42-2751-3-0005, REF IPC 27-51-11-01. ALTERNATE P/N FOR LOWER BULB SEAL IS 113A2100-13, M&E ITEM # 335. MF PN# 113A2172-603. 29-2751-3-0023.
- [SDR CALA2022112303195](https://openairdocs.org/sdr/CALA2022112303195.md): Proximity Switch · faulted · Nov 23, 2022 · N36207 · Boeing 737824 · Leading Edge Slat Control System
  > LE FLAPS TRANSIT LIGHT STAYED ON AFTER FLAP RETRACTION LE DEVICE NUMBER 4 ACP BITE OF FSEU NO EXISTING FAULTS FOUND. FOUND FAULT HISTORY FLT LEG 0 F4 PROX EXTEND WITH MSG 27-81223 & FLT LEG -001 R 28VAC EXC INV MSG 27-53280. PARTS USED: 1-899-29,QTY:1 CW F
- [SDR CALA2022102402934](https://openairdocs.org/sdr/CALA2022102402934.md): Oil System · warning light · Oct 24, 2022 · N36207 · Boeing 737824 · Engine Oil Quantity
  > ENGINE OIL QUANTITY INDICATION LOW ENGINE 2 ENG 2 OIL QTY READS ZERO BUT OIL PRESS IS 42 AND OIL TEMP IS 97. ENG VIB IS.4 W/NO FLUCTUATIONS. REMOVED AND REPLACED # 2 ENGINE.OK FOR SERVICE.
- [SDR CALA2022082202133](https://openairdocs.org/sdr/CALA2022082202133.md): Rib · corroded · Aug 20, 2022 · N36207 · Boeing 737824 · Horizontal Stabilizer Structure
  > EA 5510-01843 REV H OP 001: LH HORZ STAB AT RIB 147.9 HAD RELEVANT INDICATION OF CRACK DURING C-SCAN. REF BY PEMCO NR.12666.0378 STALLED REPAIR DOUBLER REPAIR IAW SRM 55-10-01-2R-11 REPAIR 11. L FLIGHT CYCLES WITH REPEAT INSPECTIONS EVERY 9000 FLIGHT CYCLES 51
- [SDR CALA2021122002402](https://openairdocs.org/sdr/CALA2021122002402.md): Fitting · cracked · Dec 17, 2021 · N36207 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 40.87 IS CRA CKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 40.87 V842476, 12/17/2021. DATA WAS TRANSCRIBED FROM NSA EMX NR 00121, IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL S
- [SDR CALA2021122002401](https://openairdocs.org/sdr/CALA2021122002401.md): Fitting · cracked · Dec 17, 2021 · N36207 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 54.60 IS CRA CKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 54.60 V842476, 12/17/2021. DATA WAS TRANSCRIBED FROM NSA EMX NR 00120, IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL S
- [SDR CALA2021122002400](https://openairdocs.org/sdr/CALA2021122002400.md): Fitting · cracked · Dec 17, 2021 · N36207 · Boeing 737824 · 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 V842476, 12/17/2021. DATA WAS TRANSCRIBED FROM NSA EMX NR 00118, IAW B737-800 SRM 51-40-02 AND BAC DWG 11A2000 REV ORIGINAL SE
- [SDR CALA2021122002399](https://openairdocs.org/sdr/CALA2021122002399.md): Fitting · cracked · Dec 17, 2021 · N36207 · Boeing 737824 · 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 540 AND LBL 6.14 V842476, 12/17/2021. DATA WAS TRANSCRIBED FROM NSA EMX NR 00119, IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE
- [SDR CALA2021122002398](https://openairdocs.org/sdr/CALA2021122002398.md): Fitting · cracked · Dec 17, 2021 · N36207 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 32.40 IS CRA CKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL32.40 V842476, 12/17/2021, DATA WAS TRANSCRIBED FROM NSA EMX NR 00117, IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SE
- [SDR CALA2021122002397](https://openairdocs.org/sdr/CALA2021122002397.md): Fitting · cracked · Dec 17, 2021 · N36207 · Boeing 737824 · Wing Structure
  > B737-57-1262 SHEAR FITTING AT STATION 540 AND LBL 40.87 IS CRACK ED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 40.87 V842476, 12/17/2021. DATA WAS TRANSCRIBED FROM NSA EMX NR 00016, IAW IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL
- [SDR CALA2021122002405](https://openairdocs.org/sdr/CALA2021122002405.md): Fitting · cracked · Dec 17, 2021 · N36207 · Boeing 7378 · 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 V842476, 12/17/2021. DATA WAS TRANSCRIBED FROM NSA EMX NR 00124, IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE
- [SDR CALA2021122002404](https://openairdocs.org/sdr/CALA2021122002404.md): Fitting · cracked · Dec 17, 2021 · N36207 · Boeing 7378 · 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 V842476, 12/17/2021. DATA WAS TRANSCRIBED FROM NSA EMX NR 00123, IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL S
- [SDR CALA2021122002403](https://openairdocs.org/sdr/CALA2021122002403.md): Fitting · cracked · Dec 17, 2021 · N36207 · Boeing 7378 · 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 V842476, 12/17/2021. DATA WAS TRANSCRIBED FROM NSA EMX NR 00122, IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL S
- [SDR CALA2019111101962](https://openairdocs.org/sdr/CALA2019111101962.md): Proximity Sensor · failed · Nov 11, 2019 · N36207 · Boeing 737824 · Landing Gear Position and Warning
  > ON DEPARTURE AFTER GEAR RETRACTION WE GOT A RIGHT GEAR DOWN IND ICA TION GEAR DISAGREEMENT AFTER DEBRIEF, CREW ONLY HAD FWD PANEL GEAR LIGHT ON THE OVER HE AD WAS OFF AND THE GEAR HANDLE WAS IN THE OFF POSITION. PSEU OVR HD LIGHT WAS OFF UNTIL LANDING. HAD 2
- [SDR CALA2019071801208](https://openairdocs.org/sdr/CALA2019071801208.md): Door Frame · damaged · Jul 11, 2019 · N36207 · Boeing 737824 · Fuselage Main, Structure
  > STA 303.9 AT STRINGER 8L AT FWD ENTRY DOOR FRAME DAMAGED. STA 303.9 FRAME LOCATED AT STRINGER 8L FWD ENTRY DOOR REPAIRED IN ACCORDANCE WITH EC/RA 5311-02185. ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE JULY 10, 2021. PLANNING CONTACT ENGINEERING AFTER MAY 10, 2
- [SDR CALA2019071301185](https://openairdocs.org/sdr/CALA2019071301185.md): Stringer · corroded · Jul 11, 2019 · N36207 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > AFT SECTION OF AFT CARGO - FOUND CORROSION ON STRINGER BETWEEN FRAMES 947 AND 967 LBL. STRINGER 25L BETWEEN STA 947 AND STA 967 REPAIRED IN ACCORDANCE WITH SRM 53-00-03 REPAIR 1 AND EC/RA 5311-02198. REFERENCE HANGAR NON ROUTINE 9675935 VERIFIED ECRA 5311-0219

Next page: https://openairdocs.org/aircraft/N36207/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 = 'N36207' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N36207/reports

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