# Service difficulty reports: N38727

A list on [N38727](https://openairdocs.org/aircraft/N38727.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 · 75 reports

- [SDR CALA2026070917632](https://openairdocs.org/sdr/CALA2026070917632.md): Light · inoperative · Jul 8, 2026 · N38727 · Boeing 737724 · Emergency Lighting
  > EMERGENCY EXIT WINDOW LIGHT INOP. AT 21F. REMOVE AND REPLACE EMERGENCY EXIT WINDOW LIGHT. AT 21F. OPS CHECK GOOD.
- [SDR CALA2025110310838](https://openairdocs.org/sdr/CALA2025110310838.md): Wire · shorted · Oct 29, 2025 · N38727 · Boeing 737724 · Light System Wiring
  > L2 DOOR, EMERGENCY EXIT LIGHT SIGN DOES NOT ILLUMINATE. M1672 BATTERY PACK REMOVED AND DISCONNECTED FROM D10744. AFT GALLEY CEILING LIGHT ASSEMBLY(M01678) REMOVED AND DISCONNECTED FROM D11460. D40100P AND J DISCONNECTED. D40044 P & J DISCONNECTED. TROUBLESHOOT
- [SDR CALA2025103110773](https://openairdocs.org/sdr/CALA2025103110773.md): Battery Pack · no test · Oct 29, 2025 · N38727 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1675 FAILED CAPACITY CHECK. REPLACED THE M1675 BATTERY, OPS CHKD GOOD IAW MM 33-51-06-960-805.
- [SDR CALA2025103110772](https://openairdocs.org/sdr/CALA2025103110772.md): Battery Pack · no test · Oct 29, 2025 · N38727 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1672 FAILED CAPACITY CHECK. REPLACED THE M1672 BATTERY, OPS CHKD GOOD IAW MM 33-51-06-960-805.
- [SDR CALA2025103110771](https://openairdocs.org/sdr/CALA2025103110771.md): Battery Pack · no test · Oct 29, 2025 · N38727 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1668 FAILED CAPACITY CHECK. REPLACED THE M1668 BATTERY, OPS CHKD GOOD IAW MM 33-51-06-960-805.
- [SDR CALA2025100709753](https://openairdocs.org/sdr/CALA2025100709753.md): Skin · corroded · Sep 30, 2025 · N38727 · Boeing 737724 · Fuselage Main, Plate/Skin
  > AFT LAV SERVICE PANEL COUTOUT AFT LOWER CORNER SKIN IS BULGING AND RIVETS PULLING THROUGH. AFT LAV SVC PNL CORROSION. PERFORMED REPAIR TO THE FUSELAGE SKIN P/N'S 146A3231-4,146A3201- 7 AND INTERNAL DOUBLER BETWEEN STA 807-887 AND S19L - S24R IAW EC/RA 5360-0
- [SDR CALA2025091508884](https://openairdocs.org/sdr/CALA2025091508884.md): Window Frame · cracked · Aug 25, 2025 · N38727 · Boeing 737724 · Fuselage Main, Structure
  > FOUND DAMAGE CRACK AT THE R3 WINDOW FRAME POST HOLE 5, REF TO EA 5310-08195 REV C OP 004. (REF AAR NR 1000043323). ACCOMPLISHED REPAIR OF HOLE # 5 AT THE RH # 3 WINDOW FRAME POST IAW ECRA #:5310-08676.
- [SDR CALA2025101510115](https://openairdocs.org/sdr/CALA2025101510115.md): Window Frame · cracked · Aug 22, 2025 · N38727 · Boeing 737724 · Fuselage Main, Structure
  > RIGHT NR 3 WINDOW FRAME E-F POST CRACKED AT 5TH LOWER FASTENER HOLE. PERFORMED INTERIM REPAIR TO THE 5TH FASTENER HOLE FROM THE BOTTOM OF THE R3 WINDOW FRAME E-F POST IAW PART 1.
- [SDR CALA2025101510114](https://openairdocs.org/sdr/CALA2025101510114.md): Window Frame · cracked · Aug 22, 2025 · N38727 · Boeing 737724 · Fuselage Main, Structure
  > RH NO. 3 WINDOW FRAME E-F POST CRACKED AT 5TH LOWER FASTENER HOLE - INTERIM REPAIR AT THE REPAIRED AREA OF THE RIGHT HAND #3 WINDOW FRAME E-F POST, REPAIRED AREA OF THE RH #3 WINDOW FRAME E-F POST REF ECRA 5310-08676.
- [SDR CALA2025073107145](https://openairdocs.org/sdr/CALA2025073107145.md): Lens · missing · Jul 30, 2025 · N38727 · Boeing 737724 · Emergency Lighting
  > SEAT 1B EMERG LIGHT COVER MISSING. REPLACED FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 1B, CHECKS OK. REF AMM 33-51-11.
- [SDR CALA2025062305781](https://openairdocs.org/sdr/CALA2025062305781.md): Window · arced · Jun 23, 2025 · N38727 · Boeing 737724 · Flight Compartment Windows
  > WINDOW 2 BEGAN ARCING EXTERIOR PANE R2 CRACKED AND DAMAGED THIS IS FOR R1 WINDOW R&R. UPDATING M&L TO REFLECT (35MH AND 22GT) ACP E-LOTO, REMOVED 2 EACH EFIS PANELS REF AMM31-62-12-000-801, REMOVED DFCS CONTROL PANEL REF AMM22-11-34-000-801, REMOVED RH WINSHEI
- [SDR CALA2025041603916](https://openairdocs.org/sdr/CALA2025041603916.md): Computer · malfunctioned · Apr 14, 2025 · N38727 · Boeing 737724 · Auto Throttle System
  > ON TAKEOFF ROLL THRUST LEVERS SPLIT AND AUTO THROTTLES DISENGAGED. BITE OF AT SHOWS ASM2 AT DISC RATE MON. REF FIM 22-32 TASK 819. CURRENT FAULT BITE AND SERVO MOTOR TEST SHOWS NO FAULTS. DUE TO INFLIGHT FAULTS AND FLIGHT CREW REPORT. REPLACED ASM #2 REF AMM
- [SDR CALA2025031702867](https://openairdocs.org/sdr/CALA2025031702867.md): Module · faulted · Mar 12, 2025 · N38727 · Boeing 737724 · Flight Control System
  > CREW REPORTED FLIGHT CONTROL B SYS HYD OVERHEAD LIGHT ON FOLLOWED QRH TURNED ON STDBY RUDDER ADDING WHAT CREW SENT IN ON E-MAIL,ON DEPARTURE MASTER CAUTION ILLUMINATED WITH FLT CONT LIGHT AND LOW PRESSURE LIGHT ON OVERHEAD PANEL ON FLT CONT B SIDE. FLYING PIL
- [SDR CALA2025021702342](https://openairdocs.org/sdr/CALA2025021702342.md): Proximity Sensor · faulted · Feb 13, 2025 · N38727 · Boeing 737724 · Leading Edge Slat Position Indicating System
  > LEADING EDGE SLATS TRANSIT LIGHT STAYS ON 7 ON FLAP RETR SLAT 7 TRAN SIT LT STAYED ON W/ASS A LE FLAPS TRANSI T LT ON. SLIGHT ASSEMETRY/ROLL. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED. PER
- [SDR CALA2025011501910](https://openairdocs.org/sdr/CALA2025011501910.md): Light · inoperative · Jan 12, 2025 · N38727 · Boeing 737724 · Emergency Lighting
  > SEAT 23C EMERGENCY PATH LIGHTING MODULE IS BRKN OFF FROM SEAT. L T NOT WORKING. SWAPPED LIGHTS AT 23C WITH 34C - EMERGENCY LIGHT AT 34C REQUIRES REPLACEMENT. REPLACED BROKEN LIGHTING MODULE AT SEAT 34C,OPS CHECKED GOOD.
- [SDR CALA2024062100052](https://openairdocs.org/sdr/CALA2024062100052.md): Controller · inoperative · Jun 21, 2024 · N38727 · Boeing 737724 · Cabin Temperature Control System
  > AIRCRAFT IS HOT. CANNOT BE COOLED ON GND OR AIR UNTIL REACHING CRUISE. BITE TEST CABIN TEMP CONTROL, CTC HAS NO POWER TO BIT TEST, REST SYS, NO HELP. R & R CABIN TEMP CONTROLLER PER AMM 21-61-01 OPS CHKD GOOD. PERFORMED TEST, BOTH PACKS & SELECTING CABIN TEM
- [SDR CALA2024012200167](https://openairdocs.org/sdr/CALA2024012200167.md): Window Frame · cracked · Jan 19, 2024 · N38727 · Boeing 737724 · Fuselage Main, Structure
  > AC 0727, LEFT-HAND NO. 3 WINDOW FRAME POST E-F CRACK INTERIM REPAIR. LEFT-HAND NO. 3 WINDOW FRAME (POST E-F) REPAIR ON AIRCRAFT N38727 PER PART 2 OF THE LATEST REVISION OF ECRA 5611-01336. AFTER OCTOBER 14, 2025, BUT BEFORE NOVEMBER 14, 2025, PLANNING TO CONTA
- [SDR CALA2023122103706](https://openairdocs.org/sdr/CALA2023122103706.md): Intercostal · cracked · Dec 19, 2023 · N38727 · Boeing 737724 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT BETWEEN STA 480 TO STA 500, L 21 STRINGER, LONGITUDINAL LAP SPLICE IS CRACK SEE DOT (103-43). REF AAR N/R 9216662. REMOVED AND REPLACED INTERCOSTAL (143A7550-11) AT FORM ATTACHED OP-84 FOR ACCOMPLISHMENT OF HEAT FWD CARGO COMPARTMENT STA
- [SDR CALA2023120803603](https://openairdocs.org/sdr/CALA2023120803603.md): Window Frame · cracked · Dec 6, 2023 · N38727 · Boeing 737724 · Fuselage Main, Structure
  > FOR SDR TRACKING PURPOSE ONLY "737NG LH #1 WINDOW FRAME INSPECTION AND PREVENTATIVE MOD" REF AAR N/R 9217043.
- [SDR CALA2023112703484](https://openairdocs.org/sdr/CALA2023112703484.md): Skin · cracked · Nov 22, 2023 · N38727 · Boeing 737724 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 129.50, 17 FROM FRONT SPAR I/B ROW. CRACK LENGTH 1.218 REF N/R 9216514 REPAIRED CRACK AT LEFT HORIZONTAL STABALIZER LOWER SKIN STA. ACCOMPLISHED BY V938928. 129.50, 17" FROM FRONT SPAR I/B ROW IN
- [SDR CALA2023060501752](https://openairdocs.org/sdr/CALA2023060501752.md): Shutoff Valve · leaking · Jun 2, 2023 · N38727 · Boeing 737724 · Aircraft Fuel Distribution System
  > DIVERT FOR SUSPECTED FUEL LEAK LEAKS. PERFORMED CROSSFEED VALVE FUNCTIONAL TEST IN REF TO MM28-22-00-7 ING FLOAT VALVE REF MM28-13-11. NO DEFECTS NOTED. NO UNWANTED TR ROTABLE PARTS CHANGE WAS INDICATED - TT # 1101271 SN OFF 1424 PERFORMED BOOST PUMP PRESSUR
- [SDR CALA2022101002758](https://openairdocs.org/sdr/CALA2022101002758.md): Pcu · false activation · Oct 10, 2022 · N38727 · Boeing 737724 · Aileron Tab Control System
  > UNCOMMANDED ROLLL LEFT AND RIGHT AT 2500FT PERFORMED DFCS FLIGHT FAULTS CHK, NO FAULTS BOTH A/B SYSTEMS. CURRENT STS- NO FAULTS FOR A/P. PEFORMED DFCS LAND VERIFY BITE I.A.W. AMM 22-11-00, "PASSED". ENGAGED & DISENGAGED A/P''S MULTI- PLE TIMES WITH NO KICKBACK
- [SDR CALA2022071301714](https://openairdocs.org/sdr/CALA2022071301714.md): Stop Fitting · cracked · Jul 9, 2022 · N38727 · Boeing 737724 · Cabin Cooling System
  > RIGHT PACK EXHAUST DIFFUSER DOOR STOP (L-ANGLE) CRACKED AND BENT -- SEE SAFETY BULLETIN PHOTO,S.. PHOTO,S ADDED
- [SDR CALA2021080901281](https://openairdocs.org/sdr/CALA2021080901281.md): Indicator · faulted · Aug 9, 2021 · N38727 · Boeing 737724 · Airspeed/Mach Indicator
  > *DECLARED EMERGENCY* IAS DISAGREE.CAPT SIDE IAS 235.FO SIDE IAS 247 CAPT SIDE APPEARS CORRECT.FL380. SAT-50. LOCKED BY TOMC SR MANAGER DUE TO EMERGENCY BEING DECLARED FOR LANDING UNLOCKING FOR UPDATE. LOOKED AT CAPT AND F/O PITOT PROBE, NO NOTICEABLE BLOCKAGE
- [SDR CALA2021043000579](https://openairdocs.org/sdr/CALA2021043000579.md): Fitting · cracked · Apr 29, 2021 · N38727 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA540 RBL40.87 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 40.87. IAW B73 7-700 SRM 51-60-02 ECRA 5714-01208. REV ORIGINAL.
- [SDR CALA2021043000578](https://openairdocs.org/sdr/CALA2021043000578.md): Fitting · cracked · Apr 29, 2021 · N38727 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA540 RBL54.60 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 54.60. IAW SRM 51-40-02 AND ECRA 5716-01219 REV ORIGINAL.
- [SDR CALA2021043000577](https://openairdocs.org/sdr/CALA2021043000577.md): Fitting · cracked · Apr 29, 2021 · N38727 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA540 RBL54.60 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 54.60. IAW SRM 51-40-02 AND ECRA 5716-01219 REV ORIGINAL.
- [SDR CALA2021043000582](https://openairdocs.org/sdr/CALA2021043000582.md): Fitting · cracked · Apr 29, 2021 · N38727 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA540 RBL6.14 IS CRACKED-N/R6 227155 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 6.14 IAW B737- 700 SRM 51-40-02 AND ECRA 5714-01208. REV ORIGINAL.
- [SDR CALA2021043000581](https://openairdocs.org/sdr/CALA2021043000581.md): Fitting · cracked · Apr 29, 2021 · N38727 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA540 RBL15.04 IS CRACKED-N/R 6227154 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 15.04 IAW B737 -700 SRM 51-40-02 AND ECRA 5714-01209 REV ORIGINAL.
- [SDR CALA2021043000580](https://openairdocs.org/sdr/CALA2021043000580.md): Fitting · cracked · Apr 29, 2021 · N38727 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA540 RBL32.40 IS CRACKED-N/R 6227153 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 32.40 IAW B737 -700 SRM 51-40-02 ECRA 5714-01209 REV ORIGINAL.
- [SDR CALA2021043000576](https://openairdocs.org/sdr/CALA2021043000576.md): Fitting · cracked · Apr 29, 2021 · N38727 · Boeing 737724 · Fuselage Main, Attach Fittings
  > B737-57-4-1262-SHEAR FITTING AT STA540 LBL6.14 IS CRACKED-N/R 6227150 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 6.14 IAW B737- 700 SRM 51-40-02 AND ECRA 5714-01209 REV ORIGINAL.
- [SDR CALA2021043000575](https://openairdocs.org/sdr/CALA2021043000575.md): Fitting · cracked · Apr 29, 2021 · N38727 · Boeing 737724 · Fuselage Main, Attach Fittings
  > B737-57-4-1262-SHEAR FITTING AT STA540 LBL15.04 IS CRACKED-N/R 6227149 REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 LBL 15.04. IAW B737-700 SRM 51-40-02 AND ECRA 5714-01208. REV ORIGINAL. SS FR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651 4
- [SDR CALA2021043000574](https://openairdocs.org/sdr/CALA2021043000574.md): Fitting · cracked · Apr 29, 2021 · N38727 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT BS 540, LBL 32.4 WAS CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02 AND ECRA 5714-01208. REV ORIGINAL.
- [SDR CALA2021043000573](https://openairdocs.org/sdr/CALA2021043000573.md): Fitting · cracked · Apr 29, 2021 · N38727 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02 AND ECRA 5714-01209.
- [SDR CALA2021043000572](https://openairdocs.org/sdr/CALA2021043000572.md): Fitting · cracked · Apr 29, 2021 · N38727 · Boeing 737724 · Fuselage Main, Attach Fittings
  > B737-57-4-1262-SHEAR FITTING AT STA 540 LBL 54.60 IS CRACKED-622 7146 REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02 AND ECRA 5716-01208.
- [SDR CALA2019063001104](https://openairdocs.org/sdr/CALA2019063001104.md): Thermocouple · malfunctioned · Jun 28, 2019 · N38727 · Boeing 737724 · Engine (Turbine/Turboprop)
  > EGT EXCEED 965 DEGREEES AFTER TAKEOFF. EGT NORM AFTER THROTTLE R ETARDED PER CREW VERBAL, # 2 ENGINE. BY VERBAL FROM CREW AIRCRAFT WAS NOT IN AN OVERWEIGHT CONDITION AT LANDING. 73-10322, 77-20862, 77-20872, 75-10362, 775-30412, 77-20872, 75-20462, AND 75-3041
- [SDR CALA2019030400350](https://openairdocs.org/sdr/CALA2019030400350.md): Skin · dented · Mar 3, 2019 · N38727 · Boeing 737724 · Fuselage Main, Plate/Skin
  > NOTE THIS DAMAGED TRANSFERED FROM LOGPAGE 9006123. DENT IN FUSELAGE SKIN, STA. 827-847, STR. 25LT-27RT. VERIFIED REMOVAL OF DAMAGED MATERIAL. PERFORMED HFEC AROUND CUTO UTS. REF: NDT P6 51-00-00-23. ALSO PERFORMED THICKNESS CHECK 0.002"REMOVED FROM BURNISHED A
- [SDR CALA2018092401978](https://openairdocs.org/sdr/CALA2018092401978.md): Module · faulty · Sep 21, 2018 · N38727 · Boeing 737724 · Air Data Computer
  > CAPT AND F/O UNRELIABLE AIRSPEED/ALTIMETER AND ENG LIGHT ON. AIR SPEED DISAGREE BY200 KTS CREW REPORTS CAPT AIRSPEED DROPPED TO 80KTS. EEC BITE FLT HISTORY SHOWS MSG 73-31641 & 73-31642 ADIRU TOTAL PRESSURE DISAGREE FLUSHED CAPT & F/O PITOT SYSTEM PER AMM 34-1
- [SDR CALA2017122204571](https://openairdocs.org/sdr/CALA2017122204571.md): Door Frame · corroded · Dec 21, 2017 · N38727 · Boeing 737724 · Fuselage Main, Structure
  > L1 DOOR FRAME CORRODED AT BS 303.9 JUST ABOVE UPPER DOOR HINGE. REPAIRED THE DOOR FRAME BETWEN STRINGERS 9L AND 10L IAW ECRA 5311-01889.
- [SDR CALA2017121804498](https://openairdocs.org/sdr/CALA2017121804498.md): Hinge · corroded · Dec 18, 2017 · N38727 · Boeing 737724 · Fuselage, Door Hinge
  > FOUND CORROSION ON THE L1 DOOR UPPER HINGE FITTING. REMOVED AND REPLACED UPPER FUSELAGE HINGE FITTING AT L1 DOOR P/N 141A8186-4 PER SRM 51-40-02 REF BOEING DWG # 141A8180.
- [SDR CALA2017121804497](https://openairdocs.org/sdr/CALA2017121804497.md): Fitting · corroded · Dec 18, 2017 · N38727 · Boeing 737724 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON S10 LT FITTING. FABRICATED NEW FITTING.
- [SDR CALA2017112104176](https://openairdocs.org/sdr/CALA2017112104176.md): Bulkhead · cracked · Nov 21, 2017 · N38727 · Boeing 737724 · Fuselage Main, Bulkhead
  > PRESSURE BULKHEAD CRACKED, RBL 31.8 TO RBL 40. INSTALLED A REPAIR IAW SRM 57-10-10, REPAIR 3, ALTERNATIVE 2.
- [SDR CALA2017082802921](https://openairdocs.org/sdr/CALA2017082802921.md): Altimeter · malfunctioned · Aug 28, 2017 · N38727 · Boeing 737724 · Altimeter, Barometric/Encoder
  > CAPT ALTIMETER CLIMBED APPROX 900 FT AND RETURNED IN APPROX ONE SECOND. PERFORMED BIT/OP TEST OF LEFT AND RIGHT HAND ADIR'S UNITS. NO FAULTS FOUND SYS GROUND TEST GOOD IAW AMM 34-21-00.
- [SDR CALA2013081900579](https://openairdocs.org/sdr/CALA2013081900579.md): Stringer Splice · corroded · Aug 17, 2013 · N38727 · Boeing 737724 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE CORRODED S24L AT BS 887. STRINGER SPLICE WAS REPLACED REF DWG 147A3287 AND SRM 51-40-02.
- [SDR CALA2013081900578](https://openairdocs.org/sdr/CALA2013081900578.md): Stringer · corroded · Aug 17, 2013 · N38727 · Boeing 737724 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY STRINGER CORRODED BEYOND LIMITS BS 867 S24L. R & R STRINGER REF DWG 146A3230 AND SRM 51-40-02.
- [SDR CALA2013081600571](https://openairdocs.org/sdr/CALA2013081600571.md): Intercostal · corroded · Aug 16, 2013 · N38727 · Boeing 737724 · Fuselage Miscellaneous Structure
  > AFT CARGO BS 847-867, BETWEEN STRINGERS S25-26L, FOUND HEAVY IGC CORROSION AT INTERCOSTAL LOCATED FWD OF WASTE TANK. DAMAGE ON AFT CARGO INTERCOSTAL FOUND TO BE OUT OF LIMITS, REMOVED, FABRICATED, AND INSTALLED REF SRM 53-00-53, 51-40-02.
- [SDR CALA2013081600570](https://openairdocs.org/sdr/CALA2013081600570.md): Floorbeam · corroded · Aug 15, 2013 · N38727 · Boeing 737724 · Fuselage Main, Floor Beam
  > FLOORBEAM, BS 1016 AT LBL 32 CORRODED ON AFT FLANGE. REPAIRED IAW ECRA 5310-05843
- [SDR CALA2013081600569](https://openairdocs.org/sdr/CALA2013081600569.md): Floorbeam · corroded · Aug 15, 2013 · N38727 · Boeing 737724 · Fuselage Main, Floor Beam
  > AFT WET AREA, FLOORBEAM BS 986.5. TOP AREA AT RBL 12 CORRODED AROUND FASTERNER HOLE. REPAIRED IAW ECRA 5310-05842.
- [SDR CALA2013081600568](https://openairdocs.org/sdr/CALA2013081600568.md): Angle · corroded · Aug 15, 2013 · N38727 · Boeing 737724 · Passenger/Crew Doors
  > AFT WET AREA L-2 DOOR, ZEE ANGLE HAS SURFACE CORROSION LOCATED BETWEEN BS 947.5 AND BS986.5 ALONG THE SURFACE. REMOVED, VERIFIED AND INSTALLED L-2 DOOR ZEE ANGLE REF DWG 147A8540-1 AND SRM 51-40-02.
- [SDR CALA2013081200559](https://openairdocs.org/sdr/CALA2013081200559.md): Angle · corroded · Aug 11, 2013 · N38727 · Boeing 737724 · Fuselage Miscellaneous Structure
  > AFT WET AREA, R2 DOOR ZEE ANGLE HAS SURFACE CORROSION LOCATED BETWEEN BS 947.5 AND 962 IN SEVERAL AREAS ALONG THE SURFACE. REMOVED, VERIFIED, TRANSFERED HOLES AND INSTALLED ZEE ANGLE IAW DWG 147A8540-1 AND SRM 51-40-02.

Next page: https://openairdocs.org/aircraft/N38727/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 = 'N38727' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N38727/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
