# Service difficulty reports: N24706

A list on [N24706](https://openairdocs.org/aircraft/N24706.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 · 82 reports

- [SDR CALA2026081118458](https://openairdocs.org/sdr/CALA2026081118458.md): Light · detached · Aug 10, 2026 · N24706 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT AT SEAT 28C HAS FALLEN OFF. REMOVED AND REPLACED 28C EMERGENCY LIGHT BOX. OPS CKS GOOD.
- [SDR CALA2026070917642](https://openairdocs.org/sdr/CALA2026070917642.md): Skin · corroded · Jul 8, 2026 · N24706 · Boeing 737724 · Cargo/Baggage Doors
  > (FOUND OUT OF LIMITS) INTERNAL SKIN AT AFT CARGO DOOR APPROX 2'' FROM LOWER EDGE AND 5" FROM FWD EDGE OF DOOR. 241-052 REF AAR N/R 100049974 REPAIR ACOMPLISHED IN REF TO ESR 12-15477 W1. ACCOMPLISHED CAT A REPAIR AT INTERNAL SKIN AT AFT CARGO DOOR APPROX 2'
- [SDR CALA2026071417745](https://openairdocs.org/sdr/CALA2026071417745.md): Skin · cracked · Jun 24, 2026 · N24706 · Boeing 737724 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 157.10, 16" FROM FRONT SPAR, I/B ROW. CRACK LENGTH 1". REF AAR N/R 100049510CATEGORY B REPAIR,
- [SDR CALA2026030514365](https://openairdocs.org/sdr/CALA2026030514365.md): Valve · faulted · Mar 2, 2026 · N24706 · Boeing 737724 · Cabin Pressure Control System
  > CABIN DIFFERENTIAL PRESSURE EXCEEDED. RECOMMENDED VALUES FOR ALTITUDES PER FM1.30.3, FELT ABNORMAL PRESSURE IN CLIMB & DECENT, BOTH PRESSURIZATION CONTROLLERS BITE TEST PASSED IAW AMM 21-31-00. NO FAULTS LATCHED. CREW VERBAL, PRESSURE CHANGE WAS NOTICEABL
- [SDR CALA2026021313769](https://openairdocs.org/sdr/CALA2026021313769.md): Compensator · faulted · Feb 11, 2026 · N24706 · Boeing 737724 · Hydraulic System, Main
  > LOSS OF HYD SYS -A- QTY, 20 PERCENT AT FL290, INDICATIONS NORMAL. WHEN LANDING, QTY JUMPED TO & STABILIZED AT 46% RF, CREW REPORTED NO ISSUE WITH FLT CONTROLS OR STEERING. FOUND NO LEAKS, FLT CREW HAD FLT CONTROL SWITCH GUARD UP, FLIPPED GUARD TO ON, NOTI
- [SDR CALA2025071106472](https://openairdocs.org/sdr/CALA2025071106472.md): Proximity Sensor · faulted · Jul 9, 2025 · N24706 · Boeing 737724 · Landing Gear Position and Warning
  > OVR HD LEFT GEAR GREEN LIGHT REMAINED ILLUMINATED AFTR TAKEOFF AND WOULD NOT RETRACT INDICATION. PREFORMED PSEU BITE FOUND FAULT CODE 32-61007. REF FIM 32-61 TASK 801 DEPINNED THE SENSOR AND REMOVED OLD SENSOR ROUTED NEW HARNESS AND INSTALLED NEW SENSOR S100
- [SDR CALA2025052004836](https://openairdocs.org/sdr/CALA2025052004836.md): Hook · deformed · May 17, 2025 · N24706 · Boeing 737724 · Escape Slide
  > ESCAPE SLIDE PACK BUSTLE LOOSE L1 VISUALLY INSPECTED L1 ESCAPE SLIDE BUSTLE PER AMM 25-61-01 GIRT LENGTH WITHIN LIMITS. FOUND "J" HOOK SLIGHTLY DEFORMED ADJUSTED TO PROPER CONFORMITY MEASUREMENT.
- [SDR CALA2025042404204](https://openairdocs.org/sdr/CALA2025042404204.md): Selector · out of position · Apr 21, 2025 · N24706 · Boeing 737724 · Hydraulic System, Main
  > HYD SYS A AND B BOTH LOST QTY DURING FLT ABOUT 1PERCNT EVERY 10 MIN FLIGHT CREW LOGGED QUANTIES AND TIMES CREW ALSO INDICATED PRESSURE ON BOTH SYSEMS WERE CONSISTANT AND NORMAL. INFO: CDS BITE SHOWED NO ASSOCIATED FAULTS FOUND RSERVOIR FILL SELECTOR VALVE ON
- [SDR CALA2025040103366](https://openairdocs.org/sdr/CALA2025040103366.md): Wire · broken · Mar 24, 2025 · N24706 · Boeing 737724 · Light System Wiring
  > FOUND ROW 23ABC PATHWAY EMERGENCY LIGHT INOP REF AMM 33-51-11 RELAMPED SEAT EMERGENCY LIGHT AND REPLACED ASSEMBLY, NO HELP DF PER MEL TOMC APPROVES C/W DDP FOUND SEAT WIRE HARNESS WITHBROKEN LOCKING TAB AND DISCONNECTED UNION AT BASE OF SEAT 23ABC REF 737 SWPM
- [SDR CALA2025032503154](https://openairdocs.org/sdr/CALA2025032503154.md): Light · no test · Mar 23, 2025 · N24706 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - FOUND SEAT 24 ABC LOWER SEAT EMERGENCY LIGHT INOP. SECURED CONNECTOR D12054 AT SEAT ROW 24 ABC. ALL EMER LIGHTS CHECK OK REF WDM 33-51-22
- [SDR CALA2025030302560](https://openairdocs.org/sdr/CALA2025030302560.md): None · none · Mar 3, 2025 · N24706 · Boeing 737724 · Standard Practices/Structures
  > INPUTING ESFR
- [SDR CALA2024112701321](https://openairdocs.org/sdr/CALA2024112701321.md): Skin · damaged · Nov 20, 2024 · N24706 · Boeing 737724 · Fuselage Main, Plate/Skin
  > INSPECT (GENERAL VISUAL) LAVATORY SERVICE PANEL(S) FOR, BUT NOT LIMITED TO: {B737-38-3-0129} - FASTENERS PULLING THRU LAV PANEL FRAME STRUCTURE LOCKING FOR MX FERRY FLIGHT 2 SEPARATE AREAS OF BULGING METAL AT LOWER FWD AND AFT CORNERS OF LAV DOOR REPAIR. FWD
- [SDR CALA2024111301133](https://openairdocs.org/sdr/CALA2024111301133.md): None · none · Nov 14, 2024 · N24706 · Boeing 737724 · Standard Practices/Structures
  > REMOVED L1 DOOR ESCAPE SLIDE TO F.O.M. RENDER SAFE ESCAPE SLIDE CHECKLIST COMPLETE REINSTALLED L1 DOOR ESCAPE SLIDE I.A.W. AMM 25-66-00. SLIDE PACK NEVER OPENED. REMOVE AND REPLACE COMPLETE VERIFIED INSTALLATION AND OPPERATION. QC#U223821
- [SDR CALA2023081402502](https://openairdocs.org/sdr/CALA2023081402502.md): Fitting · cracked · Aug 13, 2023 · N24706 · Boeing 737724 · Fuselage Main, Attach Fittings
  > AT D1 CHECK IN IAH, CRACKS WERE FOUND DURING EA 5310-07660 OP 1 & 2 INSPECTION OF STA 727 & S-18A WEB AT LH UPPER, LH LOWER AND RH LOWER HOLE LOCATIONS. AN INTERIM REPAIR WAS ACCOMPLISHED REPLACING THE CRACKED FITTINGS AND OVERSIZING FASTENER HOLES DUE TO HOLE
- [SDR CALA2023081402501](https://openairdocs.org/sdr/CALA2023081402501.md): Stringer · corroded · Aug 12, 2023 · N24706 · Boeing 737724 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STR 22R AT STA 1006 R/H SIDE UNDER AFT WET AREA...REF BAM N/R# 1517657 FOR WORK ACCOMPLISHED PART 2 OF THE LATEST REVISION OF EC/RA 5330-07118 ON OR BEFORE 09-FEB-2025. INTERIM REPAIR ACCOMPLISHED AT FUSELAGE SKIN STA 1006 BETWEEN S-21R & S-
- [SDR CALA2023081402495](https://openairdocs.org/sdr/CALA2023081402495.md): Unknown · damaged · Aug 11, 2023 · N24706 · Boeing 737724 · Fuselage Structure (General)
  > DAMAGE FOUND ON R2 DOOR CUT-OUT OUTER CHORD IN TWO SPOTS BTWN STA 965 TO STA 983 LOG PAGE CREATED FOR SFR REPORTING. SFR #1033393 CREATED. REPAIR COMPLETED AT IHC HEAVY D CHECK VISIT ON BAM NR 1482301 & 1482299 PER ECRA 5370-01086. DIP LP 5432529 & 5432657 CR
- [SDR CALA2023080902461](https://openairdocs.org/sdr/CALA2023080902461.md): Web · damaged · Aug 8, 2023 · N24706 · Boeing 737724 · Service Doors
  > ELONGATED HOLES AT R2 DOOR WEB ABOVE R2 Z-ANGLE BTWN STA 887 TO STA907. REMOVED DAMAGED SECTION OF WEB, FABRICATED REPAIR PIECES,TREATE D,PRIMED,INSTALLED REPAIR PIECES, REINSTALLED WEB IN REF TO ECRA 5311-03044 NEED DIP INFO. GENERATED DIP FOR FURTHER INSPECT
- [SDR CALA2022090702300](https://openairdocs.org/sdr/CALA2022090702300.md): None · missing · Sep 5, 2022 · N24706 · Boeing 737 · Trailing Flap Position Indicating System
  > TRAILING EDGE FLAP BULB SEAL LEFT WING INBOARD FLAP LOWER SEAL IS MISSING UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INSTALL LIFT WING TRAILING EDGE BULB SEAL PER AMM 27-81-11-910-801-C1
- [SDR CALA2022090502275](https://openairdocs.org/sdr/CALA2022090502275.md): None · missing · Sep 5, 2022 · N24706 · Boeing 737 · Trailing Flap Position Indicating System
  > THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 9/05/22. TRAILING EDGE FLAP BULB SEAL LEFT WING INBOARD FLAP LOWER SEAL IS MISSING. INSTALL LEFT WING TRAILING EDGE BULB SEAL. OPS CHECKS GOOD.
- [SDR CALA2020020200289](https://openairdocs.org/sdr/CALA2020020200289.md): Fitting · cracked · Jan 27, 2020 · N24706 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED. L/P 6471106. SUPP ORT TASK REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D DWG. 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPE CTION U358176, 1/27/20 INSPECTION ACCEPTED
- [SDR CALA2020020200288](https://openairdocs.org/sdr/CALA2020020200288.md): Fitting · cracked · Jan 27, 2020 · N24706 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 RBL 40.87 IS CRACKED. L/P 6471110. SUPP ORT TASK REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D DWG 111A2000.
- [SDR CALA2020020200287](https://openairdocs.org/sdr/CALA2020020200287.md): Fitting · cracked · Jan 27, 2020 · N24706 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED. L/P 6471107. SUPP ORT TASK REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D ECRA NO. 5714-01048.
- [SDR CALA2020020200286](https://openairdocs.org/sdr/CALA2020020200286.md): Fitting · cracked · Jan 27, 2020 · N24706 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED. L/P 6471109. SUPP ORT TASK REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D ECRA NO. 5714-01049. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U358176, 1/27/20 INSPECTION ACCEPTED
- [SDR CALA2020020200285](https://openairdocs.org/sdr/CALA2020020200285.md): Fitting · cracked · Jan 27, 2020 · N24706 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED. L/P 6471111. SUPP ORT TASK REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D ECRA NO. 5714-01050.
- [SDR CALA2020020200284](https://openairdocs.org/sdr/CALA2020020200284.md): Fitting · cracked · Jan 27, 2020 · N24706 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED. L/P 6471112 SUPPOR T TASK REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D ECRA NO. 5714-01047.SSFR REPORT, FORM 46-0024, ENTERED BY UAL U358176, 1/27/20 INSPECTION ACCEPTED
- [SDR CALA2020020200283](https://openairdocs.org/sdr/CALA2020020200283.md): Fitting · cracked · Jan 27, 2020 · N24706 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 LBL 54.60 IS CRACKED. L/P 6471114. SUPP ORT TASK REMOVED AND REPLACED SHEAR FITTING IAW 737-700. SRM 51-40-02 AND DWG NO. 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INS PECTION U358176, 1/27/20 INSPECTION ACCEPTED
- [SDR CALA2020020200282](https://openairdocs.org/sdr/CALA2020020200282.md): Fitting · cracked · Jan 27, 2020 · N24706 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED. L/P 6471113. SUPP ORT TASK REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D DWG 111A2000.
- [SDR CALA2019042200630](https://openairdocs.org/sdr/CALA2019042200630.md): Thermocouple · failed · Apr 22, 2019 · N24706 · Boeing 737724 · Engine Indicating System
  > R-ENG EGT OVERTEMP DURIN G CLIMB THRU 15000 FT. ARC TURNED AMBE R. MAX EG T SEEN WAS 918C. ENG 2 BITE TEST, MSG NMBR: 77-20872 THE TOP LEFT EGT SIGNAL 77-21-00-810-804-F00 THE TOP LEFT EGT SIGNAL (T495S4) IS OUT OF RANGE - FAULT ISOLATION (T495S4)IS OUT OF R
- [SDR CALA2019032900485](https://openairdocs.org/sdr/CALA2019032900485.md): Circuit Breaker · tripped · Mar 28, 2019 · N24706 · Boeing 737724 · Waste Disposal System
  > ALL 3 TOILETS ARE NOT FLUSHING. FOUND VACUUM WASTE CB POPPED ON P18-3 PANEL. PER FIM 38-30-00-810-811 CB 1423 WAS NOT CLOSED ON ARRIVAL. VERIFIED M1188 MODULE AT AFT GALLEY SECURE, LCM IN AFT PIT SECURE AND HARNESS, ALL LAV HARNESS SECURE UNDER SINKS. SYSTEM O
- [SDR CALA2017061101792](https://openairdocs.org/sdr/CALA2017061101792.md): Frame · cracked · Jun 10, 2017 · N24706 · Boeing 737724 · Fuselage Main, Frame
  > INNER PART OF FRAME AT BS 235.8 IS CRACKED AT FASTENER HOLE FOR EXTERNAL POWER RECEPTACLE BOX ATTACH LOCATION. INSTALLED A REPAIR IAW EC/RA 5310-07150. BS 235.8 FROM RBL 30 TO RBL 40.
- [SDR CALA2017060901751](https://openairdocs.org/sdr/CALA2017060901751.md): Pressure Panel · cracked · Jun 7, 2017 · N24706 · Boeing 737724 · Fuselage Main, Bulkhead
  > PERFORMED HFEC AT CENTER WING REAR SPAR VERTICAL PRESSURE WEB AND FOUND CRACK AT APPROX WL 196.0 AND LBL 42.0. INSTALLED REPAIR PER EC/RA 5710-02610 AND SRM 57-10-10, REPAIR 3, ALTERNATIVE 2.
- [SDR CALA2016072900468](https://openairdocs.org/sdr/CALA2016072900468.md): Battery Pack · discharged · Jul 29, 2016 · N24706 · Boeing 737724 · Emergency Lighting
  > LAST 4 ROWS ON LEFT SIDE EMERGENCY AISLE LIGHTING IS INOPERATIVE. R & R EMERGENCY BATTERY PACK REF AMM 33-51-06-9 60-805. LOCATED AT RT SIDE OVERHEAD AFT GALLEY CEILING. OPS CHECK GOOD.
- [SDR CALA2016072900470](https://openairdocs.org/sdr/CALA2016072900470.md): Light · inoperative · Jul 29, 2016 · N24706 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHTS NOT ARMED, LIGHT INDICATOR BULBS BURNED OUT. RELAMPED, CKS GOOD.
- [SDR CALA2015102600870](https://openairdocs.org/sdr/CALA2015102600870.md): Light · inoperative · Oct 24, 2015 · N24706 · Boeing 737724 · Emergency Lighting
  > RIGHT OVERWING EXIT, EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED & ADJUSTED THE LIGHT RECEPTACLE IAW AMM 33-51-06-960-805. SYS CHECKED GOOD IAW AMM 33-51-06-960-805, PN 767.
- [SDR CALA2015030200136](https://openairdocs.org/sdr/CALA2015030200136.md): Bulkhead · damaged · Mar 1, 2015 · N24706 · Boeing 737724 · Fuselage Main, Bulkhead
  > DAMAGED FASTENER HOLES ON INTERIOR SURFACE AT STATION 540 BULKHEAD CHORD BETWEEN STRINGER 22R & 23R, FIVE EACH MARKED. REPAIRED OVERSIZED FASTENER HOLES BY INSTALLING FREEZE PLUG, DOUBLER & TRIPLER IAW ECRA 5310-06416.
- [SDR CALA2014071600945](https://openairdocs.org/sdr/CALA2014071600945.md): Slide · unknown · Jul 16, 2014 · N24706 · Boeing 737724 · Escape Slide
  > INBOUND CREW PIREP SOMETHING HANGING FROM SLIDE. REMOVED SLIDE FROM DOOR & ACCIDENTALLY BLOWN ON REINSTALLATION IN SHROUD. REPLACED SLIDE ASSEMBLY R2 DOOR & REINSTALLED GIRT BAR ASSEMBLY IAW MM 25-66-01401. SAFETY PIN REMOVED & STOWED IN POUCH. DOOR & GIRT
- [SDR CALA2014070100861](https://openairdocs.org/sdr/CALA2014070100861.md): Slide · unwanted deploy · Jul 1, 2014 · N24706 · Boeing 737724 · Escape Slide
  > IN FLIGHT CLIMBING TO FL400 AFT LT DOOR SLIDE DEPLOYED & AFT DOOR LIGHT ILLUMINATED. ACFT REMAINED PRESSURIZED. DIVERTED TO NEAREST AIRPORT. INSPECTED L2 DOOR IAW AMM 52-13-00-200-801 AFT ENTRY DOOR CHECK & 52-13-00-700-805 AFT ENTRY DOOR SYS TESTED ONE TIM
- [SDR CALA2013012800068](https://openairdocs.org/sdr/CALA2013012800068.md): Battery Pack · inoperative · Jan 27, 2013 · N24706 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHTS ROWS 3-7 INOPERATIVE, TROUBLESHOT AND REPLACED BATTERY PACK IN SIDEWALL. OPS CHECKED GOOD IAW AMM 33-51-06-960-805.
- [SDR CALA2012100400643](https://openairdocs.org/sdr/CALA2012100400643.md): Frame · cracked · Oct 4, 2012 · N24706 · Boeing 737724 · Fuselage Main, Frame
  > FRAME BS 787, CRACKED AT FASTENER, RADIUS GOOD. REPAIRED IAW EA 5310-04716, REV C, OP1 SEE FLEET CYCLE FOR ALL WORK PERFORMED.
- [SDR CALA2012082400530](https://openairdocs.org/sdr/CALA2012082400530.md): Floorbeam · corroded · Aug 23, 2012 · N24706 · Boeing 737724 · Fuselage Main, Floor Beam
  > BS 947.5 FLOORBEAM AT RBL 48 UNDER AFT OTBD LAV MOUNT CORRODED. REPAIRED FLOORBEAM IAW SRM 53-70-51 AND ECRA 5321-01805.
- [SDR CALA2012081500504](https://openairdocs.org/sdr/CALA2012081500504.md): Intercostal · corroded · Aug 15, 2012 · N24706 · Boeing 737724 · Fuselage Miscellaneous Structure
  > BS 260 LATERAL INTRECOSTAL CORRODED AT LBL 10 - RBL 10. REPAIRED IAW ECRA 5321-01807.
- [SDR CALA2012081700511](https://openairdocs.org/sdr/CALA2012081700511.md): Frame · cracked · Aug 15, 2012 · N24706 · Boeing 737724 · Fuselage Main, Frame
  > FRAME BS 907, CRACKED AT FASTENER, RADIUS GOOD. REPAIRED IAW ECRA5310-05570.
- [SDR CALA2012081700510](https://openairdocs.org/sdr/CALA2012081700510.md): Frame · cracked · Aug 15, 2012 · N24706 · Boeing 737724 · Fuselage Main, Frame
  > FRAME BS 907, CRACKED AT BRACKET FASTENER RADIUS GOOD. REPAIRED FRAME AT 907 IAW ECRA 5310-0557.
- [SDR CALA2012081700509](https://openairdocs.org/sdr/CALA2012081700509.md): Frame · cracked · Aug 15, 2012 · N24706 · Boeing 737724 · Fuselage Main, Frame
  > FRAME BS 827, CRACKED AT BRACKET FASTENER. RADIUS GOOD. ALL WORK COMPLETE.
- [SDR CALA2012081700508](https://openairdocs.org/sdr/CALA2012081700508.md): Floor Support · corroded · Aug 15, 2012 · N24706 · Boeing 737724 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT INTERCOSTAL CORRODED FROM STA 260-270 RBL5 -LBL5. R & R IAW EC/RA 5321-01566.
- [SDR CALA2012081500505](https://openairdocs.org/sdr/CALA2012081500505.md): Skin · cracked · Aug 15, 2012 · N24706 · Boeing 737724 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STAB LOWER SKIN SURFACE SHOWS CRACK INDICATION WITH C- SCAN AT STA 129.50 2 EA CRACKS MEASURED WITH HFEC CRACK LENGTH 1.5 AND.25 MARKED INSTALLED REPAIR REF SRM 55-10-01, REPAIR 11.
- [SDR CALA2012081300502](https://openairdocs.org/sdr/CALA2012081300502.md): Intercostal · corroded · Aug 12, 2012 · N24706 · Boeing 737724 · Fuselage Miscellaneous Structure
  > BS 270, LATERAL INTERCOSTAL CORRODED AT LBL10-RBL10. REPAIRED INTERCOSTAL IAW ECRA 5321-01566.
- [SDR CALA2012080300495](https://openairdocs.org/sdr/CALA2012080300495.md): Frame · cracked · Aug 2, 2012 · N24706 · Boeing 737724 · Fuselage Main, Frame
  > FRAME BS 867, FRAME CRACKED AT FASTENER HOLE BETWEEN STR 8 AND 9R. FRAME REPAIRED IAW EA 5310-04716 REV C, OP 1, FIG 3.
- [SDR CALA2012080200492](https://openairdocs.org/sdr/CALA2012080200492.md): Frame · cracked · Aug 2, 2012 · N24706 · Boeing 737724 · Fuselage Main, Frame
  > FRAME 867L CRACKED AT BRACKET FASTENER, RADIUS GOOD REPAIRED IAW EA 5310-04716, REV C, OP1.
- [SDR CALA2012080100491](https://openairdocs.org/sdr/CALA2012080100491.md): Frame · cracked · Aug 1, 2012 · N24706 · Boeing 737724 · Fuselage Main, Frame
  > FRAME 827R CRACKED AT FASTENER BETWEEN STR 8 AND STR 9R. REPAIRED FRAME 827 R IAW EA 5310-04716 REV C, OP 1, FIG 3.

Next page: https://openairdocs.org/aircraft/N24706/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 = 'N24706' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N24706/reports

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