# Service difficulty reports: N15710

A list on [N15710](https://openairdocs.org/aircraft/N15710.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 · 90 reports

- [SDR CALA2026071217712](https://openairdocs.org/sdr/CALA2026071217712.md): Light · damaged · Jul 12, 2026 · N15710 · Boeing 737724 · Emergency Lighting
  > SEAT 15C AFT EMERGENCY LIGHT LENS DAMAGED, LIGHT OPERATES OK. REMOVED AND REPLACED SEAT 15C RED EMER LIGHT AND LENS ASSY IAW AMM 33-51-11-960-802, OPS CHECK NORMAL.
- [SDR CALA2026051816340](https://openairdocs.org/sdr/CALA2026051816340.md): Fseu · faulty · May 14, 2026 · N15710 · Boeing 737724 · Leading Edge Slat Control System
  > FLAP ASYMMETRY WHILE EXTENDING. LEFT FLAP STAYED AT 0. ACCOMPLISHED FSEU BITE, RESULTS MAINT MSG 27-81218 INTERMITENT. CYCLED FLAPS TWICE NO FAULTS NOTED. REF FIM 27-88 TASK 805. REMOVED AND REPLACED FSEU IN REF TO AMM 27-51-01. OPS CHECK GOOD. NO EXISTING
- [SDR CALA2026051516295](https://openairdocs.org/sdr/CALA2026051516295.md): Transmitter · faulted · May 13, 2026 · N15710 · Boeing 737724 · Trailing Flap Position Indicating System
  > NOTICED AT CRUISE THAT R FLAP TE IND HALF WAY BETWEEN 0 AND 1.NO LE OR TE FLAP LIGHTS ON DEBRIEF INBOUND FLT CREW, STATED FLAP HANDLE UP, AT CRUIZE THE TRAILING EDGE FLAP INDICATOR SHOW A SPLIT SEE PHOTOS. AT GATE CYCLE FLAPS WITH HYDRAULICS NEEDLES WERE MARRY
- [SDR CALA2026050415950](https://openairdocs.org/sdr/CALA2026050415950.md): Elec Connector · disconnected · Apr 30, 2026 · N15710 · Boeing 737724 · Light System Wiring
  > EMERGENCY LIGHTS - OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - OVERHEAD EMERGENCY EXIT LIGHT IN CEILING ABOVE ROW 24/25 IS INOP FOUND PLUG DISCONNECTED,SECURED PLUG,ACP OPS CHK AMM 33-51-02-720,OPS CHK GOOD
- [SDR CALA2026042415689](https://openairdocs.org/sdr/CALA2026042415689.md): Vapor Barrier · cracked · Apr 10, 2026 · N15710 · Boeing 737724 · Fuselage Main, Bulkhead
  > FOUND CRACK R/H VAPOR BARRIER WING CTR SECTION REAR SPAR @ RBL 5 STA 663.75 I/B OF RAM AIR EXIT EXHAUST INSTALLED REPAIR PATCH WHERE CRACK WAS FOUND AT R/H VAPOR BARRIER WING CTR SECTION REAR SPAR @ RBL5 STA 663.75 I/B OF RAM AIR EXIT EXHAUST. AS PER SRM-57-
- [SDR CALA2026042415687](https://openairdocs.org/sdr/CALA2026042415687.md): Vapor Barrier · cracked · Apr 10, 2026 · N15710 · Boeing 737724 · Fuselage Main, Bulkhead
  > FOUND CRACK AT WING CTR SECTION REAR SPAR L/H VAPOR BARRIER @ LBL 5 STA 663.75 I/B OF RAM AIR EXIT DUCT. INSTALLED REPAIR PATCH WHERE CRACK WAS FOUND AT WING CTR SECTION REAR SPAR L/H VAPOR BARRIER @ LBL 5 STA 663. AS PER SRM-57-10-10-2R-2 PARAGRAPH 6 FIGU
- [SDR CALA2026041715426](https://openairdocs.org/sdr/CALA2026041715426.md): Drain · corroded · Apr 10, 2026 · N15710 · Boeing 737724 · Water and Waste System
  > WASTE TANK DRAIN ENCLOSURE HAS CORROSION AT THE AFT ANGLE THAT ATTACHES TO THE SKIN AND UNDER THE STAINLESS STEEL RING AT THE DRAIN DUCT. INSTALLED NEW PAN ASSY AT WASTE TANK DRAIN AS PER 51-40-02-0G-0 AND DRAWING 146A7400.
- [SDR CALA2025101309940](https://openairdocs.org/sdr/CALA2025101309940.md): Slide · unraveled · Oct 10, 2025 · N15710 · Boeing 737724 · Escape Slide
  > L2 SLIDE HAS EXCESSIVE MATERIAL BETWEEN GIRT BAR AND SLIDE HOUSING. R & R AFT L, DOOR SLIDE IAW AMM 25-66-01-400-801.
- [SDR CALA2025052104879](https://openairdocs.org/sdr/CALA2025052104879.md): Slide · out of tolerance · May 18, 2025 · N15710 · Boeing 737724 · Escape Slide
  > R1 SLIDE SKIRT HANGING OUT OF THE BOTTOM PERFORMED R1 DOOR SLIDE PACK REPACKING REF AMM 25-66-01. ADD 347944, U384621 C/W RII REQUIREMENTS FOR R1 DOOR SLIDE
- [SDR CALA2025021802367](https://openairdocs.org/sdr/CALA2025021802367.md): Girt Bar · unlaced · Feb 15, 2025 · N15710 · Boeing 737724 · Emergency Equipment
  > RQST DOOR 1R SLIDE INSPECTION FOR EXCESS MATERIAL SHOWING PER F/ A POSITIONED GIRT Z FOLD REF AMM 25-66-01-400-803 FIG 401. OPENED AND CLOSED UNARMED DOOR,OK.ARMED AND DISARMED GIRT ARM,OK.
- [SDR CALA2024121201480](https://openairdocs.org/sdr/CALA2024121201480.md): Battery Pack · no test · Dec 9, 2024 · N15710 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR) {MULT-33-3-0004} - M1672 BATTERY FAILS CAPACITY CHECK REPLACED EMERG BATTERY PACK AT #M1672, OPS CHK GOOD PER MM# 33-51-06-960-805.
- [SDR CALA2024121201479](https://openairdocs.org/sdr/CALA2024121201479.md): Battery Pack · faulted · Dec 9, 2024 · N15710 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR) {MULT-33-3-0004} - BATTERY M1670 FAILS CAPACITY CHECK REPLACED EMERG BATTERY PACK AT #M1670, OPS CHK GOOD PER MM# 33-51-06-960-805.
- [SDR CALA2024101100813](https://openairdocs.org/sdr/CALA2024101100813.md): Seal · missing · Oct 11, 2024 · N15710 · Boeing 737724 · Elevator Miscellaneous Structure
  > PDA 2 LEFT ELEVATOR OUTBD LOWER HINGE SEAL MISSING PICS SDR UPDATE REPLACED LT ELEVATOR OUTBD BOTTOM SEAL REF MM 27-31-11-400-801
- [SDR CALA2024072600286](https://openairdocs.org/sdr/CALA2024072600286.md): Window Post · cracked · Jul 23, 2024 · N15710 · Boeing 737724 · Fuselage Main, Structure
  > RT 3 WINDOW HAS EVIDENCE OF FRAME CRACK ON FWD POST. NEED IDT QC TO VERIFY THE CRACK VERIFIED #3R FWD. WINDOW POST CRACKED THROUGH FASTENER HOLE REF NTM 6-51-00-00-23. REMOVED RT 3 WINDOW TO FOM REF EA5310-08195-004 REV ORIG REPLACED R3 WINDOW SEAL AND INSTAL
- [SDR CALA2023092002834](https://openairdocs.org/sdr/CALA2023092002834.md): Fire Bottle · unknown · Sep 18, 2023 · N15710 · Boeing 737724 · Extinguishing System
  > FOUND SAFETY RELEASE CAP ATTCHED TO ENGINE FIRE BOTTLES REMOVED SAFETY RELEASE CAP FROM BOTH FIRE BOTTLES REF AMM26-21-01. VERIFIED BOTH FIRE BOTTLES SAFTEY RELEASE CAPS HAVE BEEN REMOVED. INSPECTED BOTH FIRE BOTTLES FOR INSTALLATION, SERVICABILITY AND HYDOST
- [SDR CALA2023091402787](https://openairdocs.org/sdr/CALA2023091402787.md): Door · not seated · Sep 12, 2023 · N15710 · Boeing 737724 · Landing Gear Doors
  > CREW VERBAL: REPORTS ON T/O WHEN GEAR HANDLE MOVED TO UP, HAD GEAR DISAGREE. UP AND DOWN ILLUMINATED. FOLLOWED QRH, NO CHANGE WHEN ALT GEAR DOOR CHECKED. ALT GEAR DOOR FOUND NOT FLUSH. CONTINUED WITH AIR RETURN IAH. RESEAT ALT GEAR DOOR PANEL OPS SWING ALL 3
- [SDR CALA2023042601259](https://openairdocs.org/sdr/CALA2023042601259.md): Skin · damaged · Apr 25, 2023 · N15710 · Boeing 737 · Horizontal Stabilizer, Plate/Skin
  > R/H STABILIZER LOWER SKIN NEEDS ACCESS HOLE CUT AT STA 92.70 #2 RIB STIFFENER FOR ACCESS FOR RIB REPAIR, TRANSFERRED FROM NR# 001359383. INITIATING DIP TO PERFORM INITIAL DETAILED VISUAL AND LFEC 9000 FLIGHT CYCLES AFTER INITIAL INSPECTION. INSPECTION AT 5600
- [SDR CALA2022080501968](https://openairdocs.org/sdr/CALA2022080501968.md): Thermocouple · warning light · Aug 4, 2022 · N15710 · Boeing 737724 · Fuel Control/Turbine Engines
  > HIGH EGT 903 NO 1 REPEAT WRITEUP ADDED PICS, NO FAULTS NOTED. REMOVED AND REPLACED CORE ENGINE HARNESS CJ9 REF AMM PARTIALLY INSTALLED CJ10 HARNESS. REQUIRES ROUTING AND CHECK FOR FINISHED INSTALLATION OF CJ10 HARNESS AND SAFETY WIRED 73-21-06-400-803.REQURES
- [SDR CALA2021122002413](https://openairdocs.org/sdr/CALA2021122002413.md): Radar · warning message · Dec 20, 2021 · N15710 · Boeing 737724 · Doppler System
  > PWS WARNING AS TO THRUST WAS APPLIED UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PERFORMED FIM 34-43 TASK 815 FOR PREDICTIVE WINDSHEAR, NO FAULTS SPEED REJECTED TAKE OFF LESS THAN 60 KTS. REALIGNED ADIRU''S FOU
- [SDR CALA2021022200208](https://openairdocs.org/sdr/CALA2021022200208.md): Battery Pack · faulty · Feb 21, 2021 · N15710 · Boeing 737724 · Emergency Lighting
  > BULLNOSE LIGHTING ON OVERHEAD BINS ON RT SIDE BETWEEN ROWS 10 AN 22 DIM. SPT 5867958 TROUBLESHOT AND FOUND FAULTY BATTERY PACK AND BATTERY CHARGER. REMOVED AND REPLACED BATTERY PACK, SN 146212 AN BATTERY CHARGER SN5917 WITH NEW BATTERY PACK SN 253349 AND BATT
- [SDR CALA2021022200205](https://openairdocs.org/sdr/CALA2021022200205.md): Fitting · cracked · Feb 19, 2021 · N15710 · Boeing 737724 · Wing, Center Box
  > SHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED LP 5866779 B737-57- 4-1262. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 6.14 IAW UNITED EC/RA 5714-01201 REV ORIGINAL SSFR REPORT, FORM 46-0024 ENTERED BY UAL, 2/19/2021 ACCOMPLISHED INSPECTION.
- [SDR CALA2021022200204](https://openairdocs.org/sdr/CALA2021022200204.md): Fitting · cracked · Feb 19, 2021 · N15710 · Boeing 737724 · Wing, Center Box
  > SHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED LP 5867921 B737-57 -4-1262. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 15.04 IAW UNITED ECIRA 5714-01201 REV ORIGINAL. SSFR REPORT FORM 46-0024 ENTERED BY UAL, 2-19-2021 ACCOMPLISHED INSPECTION.
- [SDR CALA2021022200203](https://openairdocs.org/sdr/CALA2021022200203.md): Fitting · cracked · Feb 19, 2021 · N15710 · Boeing 737724 · Wing, Center Box
  > SHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED LP 5867920 B737-57 -4-1262. REMOVED AND REPLACED ECIRA 5714-01201 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED, 2-19-2021 ACCOMPLISHED INSPECTION.
- [SDR CALA2021022200202](https://openairdocs.org/sdr/CALA2021022200202.md): Fitting · cracked · Feb 19, 2021 · N15710 · Boeing 737724 · Wing, Center Box
  > SHEAR FITTING AT STA 540 RBL 40.87 IS CRACKED LP 5867918 B737-57 -4-1262. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 40.87 IAW UNITED ERIRA 5717-01201. SSFR REPORT, FORM 46-0024 ENTERED, ACCOMPLISHED INSPECTION.
- [SDR CALA2021022200201](https://openairdocs.org/sdr/CALA2021022200201.md): Fitting · cracked · Feb 19, 2021 · N15710 · Boeing 737724 · Wing, Center Box
  > SHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED LP 5867917 B737-57 -4-1262. REMOVED AND REPLACED SHEAR FITTING IAW UNITED EC/RA 5714-01201 REV ORIGINAL. SSFR REPORT, FORM 46-0024 ENTERED, ACCOMPLISHED INSPECTION.
- [SDR CALA2021022200200](https://openairdocs.org/sdr/CALA2021022200200.md): Fitting · cracked · Feb 19, 2021 · N15710 · Boeing 737724 · Wing, Center Box
  > SHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED LP 5867916 B737-57- 4-1262. REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 6.14 IAN UNITED ECIRA 5714-01201 REV ORIGINAL. SSFR REPORT, FORM 46-0024 ENTERED.
- [SDR CALA2021022200199](https://openairdocs.org/sdr/CALA2021022200199.md): Fitting · cracked · Feb 19, 2021 · N15710 · Boeing 737724 · Wing, Fuselage Attach Fittings
  > SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED LP 5867915 B737-57 -4-1262. REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 15.04 IAN UNITED ECIRA 5714-01201 REV ORIGINAL. SSFR REPORT, 46-0024, ENTERED BY UAL INSPECTION U354653, 2/19/2021 ACCOMPLISHED INSPECT
- [SDR CALA2021022200198](https://openairdocs.org/sdr/CALA2021022200198.md): Fitting · cracked · Feb 19, 2021 · N15710 · Boeing 737724 · Wing, Attach Fittings
  > SHEAR FITTING AT STA 540 LBL 32.40 IS CRACKED LP 5867914 B737-57 -4-1262. REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 32.40 AND WASTE TUBE SUPPORT BRACKET IAW UNITED ECIRA 5714-01201 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U35
- [SDR CALA2021022200197](https://openairdocs.org/sdr/CALA2021022200197.md): Fitting · cracked · Feb 19, 2021 · N15710 · Boeing 737724 · Wing, Fuselage Attach Fittings
  > SHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED LP 5867913 B737-57 -4-1262. REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 40.87 IAW UNITED ECIRA 5714-01201 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354653, 2/19/2021 ACCOMPLISHED IN
- [SDR CALA2021022200196](https://openairdocs.org/sdr/CALA2021022200196.md): Fitting · cracked · Feb 19, 2021 · N15710 · Boeing 737724 · Wing, Attach Fittings
  > SHEAR FITTING AT STA 540 LBL 54.60 IS CRACKED B737-57-4-1262. REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 54.60 IAW UNITED ECIRA 5714-01201 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354653, 2/19/2021 ACCOMPLISHED INSPECTION.
- [SDR CALA2020101601184](https://openairdocs.org/sdr/CALA2020101601184.md): Battery Pack · discharged · Oct 13, 2020 · N15710 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1668 INOP. REPLACED BATTERY PACK M1668 AS PER AMM 33-51-06-960-805. OPS CHECKS GOOD. LOG CLEARED.
- [SDR CALA2020101601183](https://openairdocs.org/sdr/CALA2020101601183.md): Battery Pack · discharged · Oct 13, 2020 · N15710 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1670 INOP. REPLACED BATTERY PACK AT M1670 AS PER AMM 33-51-06-960-805. OPS CHECKS GOOD. LOG CLEARED.
- [SDR CALA2020101601182](https://openairdocs.org/sdr/CALA2020101601182.md): Battery Pack · discharged · Oct 13, 2020 · N15710 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1672 INOP. REPLACED BATTERY PACK AT M1672 AS PER AMM 33-51-06-960-805. OPS CHECKS GOOD. LOG CLEARED.
- [SDR CALA2020101601181](https://openairdocs.org/sdr/CALA2020101601181.md): Battery Pack · discharged · Oct 13, 2020 · N15710 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1675 INOP. REPLACED BATTERY PACK AT M1675 AS PER AMM 33-51-06-960-805. OPS CHECKS GOOD. LOG CLEARED.
- [SDR CALA2020030700591](https://openairdocs.org/sdr/CALA2020030700591.md): Skin · dented · Mar 5, 2020 · N15710 · Boeing 737724 · Fuselage Main, Plate/Skin
  > (B737-53-4-1557) DENT FOUND AT UPPER FUSELAGE EXTERNAL SKIN JUST OFF OF STA 767 BETWEEN STR 2R AND 3R REF AAR NR 99877030 STA767, BETWEEN STR2-3R OF FUSELAGE AS PER RES-WI-2015702-2IR & UNITED EC/RA 5331-02634. ACCOMPLISHED REPAIR AT UPPER SKIN CROWN AREA PERM
- [SDR CALA2020030700582](https://openairdocs.org/sdr/CALA2020030700582.md): Spar · corroded · Mar 4, 2020 · N15710 · Boeing 737724 · Wing Spar
  > LT WING L/E STRUCTURE,SHOW SIGNS OF SURFACE CORROSION AT FRONT SPAR LWR CHORD UPPER SURFACE W.S. 300.0 APROX.THROUGH ACCESS 521DB,FOUND DURING PANEL CLOSING(MKD 26-017) REF AAR NR 99877098 ACCOMPLISHED REPAIR AT L/W L/E FRONT SPAR ATTACH STRAP STA OSS 63 AS PE
- [SDR CALA2020022980506](https://openairdocs.org/sdr/CALA2020022980506.md): Skin · cracked · Feb 21, 2020 · N15710 · Boeing 737724 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER LOWER INSPAR SKIN STA 92.70 AT 11 INCHES FROM REAR SPAR HAS CRACK APPROX. 1" IN LENGTH. REF AAR NR 99876898 ACCOMPLISHED REPAIR AT L/H HORIZONTAL STAB LOWER SKIN STA 92.70 AT 11 INCHES FROM REAR SPAR IAW B737-700 SRM 55-10-01 REPAIR
- [SDR CALA2019110901936](https://openairdocs.org/sdr/CALA2019110901936.md): Wire · damaged · Nov 6, 2019 · N15710 · Boeing 737724 · Ice/Rain Protection System Wiring
  > LEFT ELEV PITOT LIGHT ON. TROUBLESHOT LH ELEV PITOT REF FIM 30-31-00-810-805, FOUND OPEN CONTINUITY REF STEP F. 2 AT PIN 40 OF CONNECTOR D644. PITOT PROBE REQS REPLACEMENT. REF FIM 30-31-00-810-805 STEP F2(B) FOUND PIN SEPERATED FROM PIN ON WIRE W7102-2001B-20
- [SDR CALA2017121204408](https://openairdocs.org/sdr/CALA2017121204408.md): Sign · unsecure · Dec 12, 2017 · N15710 · Boeing 737724 · Emergency Lighting
  > EMERGENCY EXIT SIGN DANGLING FROM THE CEILING IN OVERWING POSITION. REINSTALLED EXIT SIGN.
- [SDR CALA2017120804357](https://openairdocs.org/sdr/CALA2017120804357.md): Battery · faulty · Dec 8, 2017 · N15710 · Boeing 737724 · Emergency Equipment
  > FWD CABIN OUTBD EMERGENCY FLASHLIGHT WILL NOT BLINK. REPLACED BATTERY FOR FWD OUTBD EMERGENCY FLASHLIGHT. LIGHT TESTS GOOD.
- [SDR CALA2017061901912](https://openairdocs.org/sdr/CALA2017061901912.md): Light · inoperative · Jun 19, 2017 · N15710 · Boeing 737724 · Emergency Lighting
  > LT EMERGENCY OVERWING SLIDE LAMP INOP. REPLACED LAMP REF AMM 33-51-04. OPERATIONAL CHECK NORMAL.
- [SDR CALA2017051501451](https://openairdocs.org/sdr/CALA2017051501451.md): Light · inoperative · May 15, 2017 · N15710 · Boeing 737724 · Emergency Lighting
  > LEFT OVERWING EMERGENCY LIGHT INOP. RELAMPED LEFT WING OVERWING EMERGENCY LIGHT REF AMM 33-51-0 4-960-801. OPS CHECKED GOOD.
- [SDR CALA2017033100757](https://openairdocs.org/sdr/CALA2017033100757.md): Window Frame · damaged · Mar 27, 2017 · N15710 · Boeing 737724 · Fuselage Main, Structure
  > WINDOW FRAME DAMAGED. CUTOUT DAMAGED AREA AND ACCOMPLISHED REPAIR IAW EC/RA 5310-07094.
- [SDR CALA2017032500714](https://openairdocs.org/sdr/CALA2017032500714.md): Skin · dented · Mar 25, 2017 · N15710 · Boeing 737724 · Fuselage Main, Plate/Skin
  > STA 807 BLO BETWEEN STR 27L AND STR 27R DENT FOUND OUT OF LIMITS PER SRM 53-00-01 AD5 DENT GOES ACROSS FRAME. REPAIRED REF ECRA 5330-06006 REPAIRED DENT AT STA 807 IAW ECRA 5330-06006.
- [SDR CALA2017032400688](https://openairdocs.org/sdr/CALA2017032400688.md): Skin · dented · Mar 23, 2017 · N15710 · Boeing 737724 · Fuselage Main, Plate/Skin
  > RT FUSELAGE SKIN DENTED 39 INCHES AFT OF AFT CARGO DOOR CUTOUT BETWEEN STRINGERS 20 AND 21R 2.75 INCHES WIDE AND.114 DEEP. INSTALLED REPAIR DOUBLER IAW ECRA 5360-01460, PART 1.
- [SDR CALA2017031700615](https://openairdocs.org/sdr/CALA2017031700615.md): Skin · cracked · Mar 17, 2017 · N15710 · Boeing 737724 · Fuselage Main, Plate/Skin
  > CRACK DETECTED IN SKIN AROUND FASTENER BS 540 BETWEEN STRINGERS 22 AND 23L. REPAIRED IAW EA 5310-05878, REV.D.
- [SDR CALA2017031700614](https://openairdocs.org/sdr/CALA2017031700614.md): Bulkhead Web · cracked · Mar 17, 2017 · N15710 · Boeing 737724 · Fuselage Main, Bulkhead
  > PERFORMED HFEC OF BS 540 BULKHEAD WEB AND FRAME BETWEEN STRINGERS 22 & 23R. A CRACK INDICATION WAS FOUND. REPAIRED IAW EA 5310-05878 REV D, OP05.
- [SDR CALA2017031700606](https://openairdocs.org/sdr/CALA2017031700606.md): Beam · cracked · Mar 15, 2017 · N15710 · Boeing 737724 · Service Doors
  > R1 DOOR LOWER BEAM HAS A ONE CRACK AT RADIUS COMMON TO THE TORQUE BOX ATTACH POINT. REMOVED AND REPLACED THE BEAM IAW ECRA 5210-02824.
- [SDR CALA2017031200580](https://openairdocs.org/sdr/CALA2017031200580.md): Beam · cracked · Mar 11, 2017 · N15710 · Boeing 737724 · Passenger/Crew Doors
  > R1 DOOR UPPER BEAM HAS A 1" CRACK AT RADIUS COMMON TO THE TORQUE BOX ATTACH POINT. SEE TYPICAL LOCATION ECRA 5210-02824 FIG 2. P/N 1416536-15 REPLACED BY 141A6536-21 OR EQUIVALENT. REMOVED AND REPLACED R1 DOOR UPPER BEAM. REF: ECRA 5210-02824 AND SRM 51-40-02.
- [SDR CALA2017031000555](https://openairdocs.org/sdr/CALA2017031000555.md): Pressure Panel · cracked · Mar 7, 2017 · N15710 · Boeing 737724 · Fuselage Main, Bulkhead
  > REPAIRED LT MLG W/W VERTICAL PRESSURE DECK CRACK AT LBL 45.64 TO LBL 40.0 BETWEEN WL 192.0 AND WL 200.6 AND REPAIRED SECONDARY VAPOR BARRIER AS REQUIRED REF 57-10-10 REPAIR 3 ALT 2. THIS REPAIR IS ALSO BECOMES THE FINAL CORRECTIVE ACTION FOR CRACK DISCREPANCY

Next page: https://openairdocs.org/aircraft/N15710/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 = 'N15710' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N15710/reports

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