# Service difficulty reports: N33714

A list on [N33714](https://openairdocs.org/aircraft/N33714.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 · 88 reports

- [SDR CALA2026092119598](https://openairdocs.org/sdr/CALA2026092119598.md): Tape · peeling · Sep 17, 2026 · N33714 · Boeing 737724 · Vertical Stabilizer
  > SPEED TAPE HAS PEELED BACK ON VERTICAL STAB. FOUND VERTICLE STAB ANTENNA EROSION COATING PEELING. ACCOMPLISHED PART 1 OF ECRA 5530-01432. INSPECT INTERM REPAIR AT INTERVALS NOT TO EXCEED 2 DAYS AND PERFORM A PERMANENT REPAIR WITHIN 10 DAYS DUE TO VERTICAL S
- [SDR CALA2026070517536](https://openairdocs.org/sdr/CALA2026070517536.md): Filter · odor · Jul 3, 2026 · N33714 · Boeing 737724 · Air Distribution System
  > ODOR IN AFT CABIN AT CRUISE SDR ADDED. UPDATED WITH FORM REF LP 9479753 FOR CORRECTIVE ACTION PERFORM SMOKE/ODOR IN THE FLIGHT DECK/CABIN - CONDITIONAL INSPECTION PER AMM 05-51-26-800-801-C1 PERFORMED SMOKE AND ODOR INSPECTION, RAN BOTH ENGINES, PACKS AND APU
- [SDR CALA2026060816922](https://openairdocs.org/sdr/CALA2026060816922.md): Door Frame · cracked · Jun 6, 2026 · N33714 · Boeing 737724 · Fuselage Main, Structure
  > L1 DOOR AFT UPPER INNER CORNER BENT. REMOVED FASTENER AND STRAIGHTENED MATERIAL IAW AVO 0814-06052026-1 STEPS 1 AND 2. READY FOR HFE. INSPECTION PER STEPS 3 AND 4. DURING REMOVAL OF FASTENER FOUND CRACK AT HOLE, PERFORMED HFEC OF DAMAGED AREA, CONFIRMED CRACK
- [SDR CALA2026042915815](https://openairdocs.org/sdr/CALA2026042915815.md): Placard · missing · Apr 27, 2026 · N33714 · Boeing 737724 · Placards and Markings
  > PDA 2 MLG SERVICING CHART IN LEFT MAIN WHEEL WELL MISSING, BROKEN OFF. INSTALLED NEW PLACARD REF SRM 51-40-02PARTS USED: 29-1122-3-0008,QTY:1
- [SDR CALA2026020413577](https://openairdocs.org/sdr/CALA2026020413577.md): Blower · faulted · Feb 1, 2026 · N33714 · Boeing 737724 · Waste Disposal System
  > ALL LAVS WILL NOT FLUSH REQUEST MEL PER 3802E. APPROVED DEFER PER MEL 3802E. REMIVED AND REPLACE AFT CARGO LAV VACUUM BLOWER IAW AMM 38-32-05. OPS CHECK GOOD.
- [SDR CALA2026010512653](https://openairdocs.org/sdr/CALA2026010512653.md): Light · inoperative · Jan 2, 2026 · N33714 · Boeing 737724 · Emergency Lighting
  > AFT OVERHEAD EXIT SIGN IN GALLY AS IT LOWER RIGHT HAND LIGHT INOPERATIVE. REPLACED THE LAMP, NO HELP, CHECKED FUSES IN BATTERY TRAY ALL IN GOOD CONDITION, ALL WIRING FROM HOUSING IN GOOD CONDITION. REQUEST LIGHT ASSY. R & R THE LAMP ASSY IAW AMM 33-51-01, OP
- [SDR CALA2025111711229](https://openairdocs.org/sdr/CALA2025111711229.md): Battery Pack · no test · Nov 12, 2025 · N33714 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1675 FAILED CAPACITY CHECK.POWER SUPPLY - BATTERY PACK CAPACITY CHECK POWER SUPPLY - BATTERY PACK CAPACITY CHECK - REPLACED BATTERY PACK IN M1675 POWER SUPPLY. RE-RAN CAPACITY CHECK ON M1675, LASTED ONLY 10 MINUTES. CONTINUED DISC
- [SDR CALA2025102110330](https://openairdocs.org/sdr/CALA2025102110330.md): Bracket · cracked · Oct 16, 2025 · N33714 · Boeing 737724 · Wing Miscellaneous Structure
  > LH WING LOWER SKIN, BETWEEN RIB 7-8 AND S 8-9 HYDRAULIC LINES BRACKET BROKEN. REPLACED CRACKED BRACKET AT LEFT WING LOWER SKIN BETWEEN RIB 7&8 REFERENCE SRM 51-40-02-0G-0, DWG 272A9125-1.
- [SDR CALA2025102110329](https://openairdocs.org/sdr/CALA2025102110329.md): Bracket · broken · Oct 16, 2025 · N33714 · Boeing 737724 · Wing Miscellaneous Structure
  > RH WING LOWER SKIN, BETWEEN RIB 7-8 AND S 8-9 HYDRAULIC LINES BRACKET BROKEN. REPLACED CRACKED HYDRAULIC LINES BRACKET P/N 2729125-13 ON THE RIGHT-WING LOWER SKIN BETWEEN RIB 7&8 REFERENCE DWG 2729125-1, SRM 51-40-02-0G-0. ESFR NO. 2175; (WORK ACCOMPLISHED BY
- [SDR CALA2025072907027](https://openairdocs.org/sdr/CALA2025072907027.md): Slide · damaged · Jul 26, 2025 · N33714 · Boeing 737724 · Escape Slide
  > GIRT BAR SLIDE RUBBER BACKING IS PEELING OFF ACCOMPLISHED ESCAPE SLIDE PACK CHECK AT DOOR 2L IAW AMM 25-66-01-200-802. NO DAMAGE FOUND THAT WOULD CAUSE THE SLIDE PACK TO OPERATE INCORRECTLY. OK F/SVC
- [SDR CALA2024110701063](https://openairdocs.org/sdr/CALA2024110701063.md): Screw · loose · Nov 5, 2024 · N33714 · Boeing 737724 · Emergency Equipment
  > L1 GIRT BAR LOOSE BRACKETS TIGHTENED LOOSE SCREW ON FLOOR-MOUNTED BRACKET AND APPLIED ADHESIVE. L1 FOWARD FLOOR-MOUNTED BRACKET SECURED AS REQUIRED. REF AMM TASK 25-66-02-400-801.
- [SDR CALA2024102102680](https://openairdocs.org/sdr/CALA2024102102680.md): Splice · corroded · Oct 18, 2024 · N33714 · Boeing 737724 · Fuselage Main, Structure
  > (SUPPORT TASK) FUSELAGE INTERNAL SPLICE CORRODED INSIDE E&E COMPARTMENT STA 360 STR28L. FOUND 2 EACH STRINGER SPLICES TO BE CORRODED. REMOVED AND REPLAC ED SPLICE 141A8513-48 AND SPLICE 141A8513-50 IAW BOEING DRAWING 140A9101 REV A.
- [SDR CALA2024102102685](https://openairdocs.org/sdr/CALA2024102102685.md): Stringer · damaged · Sep 28, 2024 · N33714 · Boeing 737724 · Fuselage Main, Longeron/Stringer
  > EXTERNAL WALKAROUND INSPECTION {B737-06-3-0550} - FOUND 4 DISHED RIVET HEADS WITH SKIN BULGING BETWEEN RIVETS AT FUSELAGE EXTERIOR SKIN AT BS 365 TO 369, STR 26 LH. LOCKED FOR FERRY FLIGHT PERFORMED BOROSCOPE INSPECTION OF AFFECTED STRINGER (LH #26), IN AREA
- [SDR CALA2024061701810](https://openairdocs.org/sdr/CALA2024061701810.md): Sealant · missing · Jun 17, 2024 · N33714 · Boeing 737724 · Aerodynamic Fairings
  > SEALANT ON UPPER FWD LEFT WING TO BODY FAIRING PEELING OFF. SHOULD BE RIGHT WING. RE-APPLIED SEALANT REF MM 53-51-21 AND 51-31-00.
- [SDR CALA2023122903751](https://openairdocs.org/sdr/CALA2023122903751.md): Floorbeam · corroded · Dec 7, 2023 · N33714 · Boeing 737724 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR BEAM HAS CORROSION ON UPPER SURFACE AT BS 947, LBL 53.
- [SDR CALA2023122803745](https://openairdocs.org/sdr/CALA2023122803745.md): Floorbeam · corroded · Dec 5, 2023 · N33714 · Boeing 737724 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR SUPPORT STRUCTURE HAS CORROSION AT BS 986 LBL 3 7-43.
- [SDR CALA2023090802733](https://openairdocs.org/sdr/CALA2023090802733.md): Proximity Sensor · faulty · Sep 5, 2023 · N33714 · Boeing 737724 · Landing Gear Position and Warning
  > RED AND GREEN NOSE GEAR LITES STAYED ILLUMINATED AFTER RETRACTION. PSEU MSG 32-61013 NOSE DOWN DISAGREE AND 32-61004 NOSE DOWN "A" FAULT. PSEU BITE FAULTS NOSE DOWN A FAULT. MESSAGE #32-61004, PER FIM REPLACED NLG DOWN SENSOR S0845 REF AMM 32-61-51. SWUNG NOS
- [SDR CALA2023061601864](https://openairdocs.org/sdr/CALA2023061601864.md): Window · cracked · Jun 14, 2023 · N33714 · Boeing 737724 · Flight Compartment Windows
  > CREW REPORTED SMALL FIRE AT FO''S WINDSHIELD HEAT TERMINALS. MUST REPLACE WINDSHIELD HEAT CONTROLLER AND INSPECT SURROUNDING AREA FOR DAMAGE. MUST COMPLETE SDR (ESFR FORM) MARKING SDR Y
- [SDR CALA2023042401226](https://openairdocs.org/sdr/CALA2023042401226.md): Skin · damaged · Apr 21, 2023 · N33714 · Boeing 737 · Cargo/Baggage Doors
  > GROUND CREW HIT FORWARD CARGODOOR WITH AIRSTART. LARGE HOLE NEAR FORWARD CARGO DOOR BELOW HANDLE. TRIMMED OUT DAMAGE AND SUBMITED TO EWR-ESC ALSO PARTIALLY REMOVED AFT SKIN FOR ACCESS. ACCOMPLISHED H.F.E.C. OF SKIN CUTOUT IAW AVO10690 REV. A AND NDT COMPLIE
- [SDR CALA2021102201953](https://openairdocs.org/sdr/CALA2021102201953.md): None · failed · Oct 22, 2021 · N33714 · Boeing 737724 · Autopilot Computer
  > BOTH AUTOPILOTS INOP CWS A AND B INOP R&R STAB TRIM INTERLOCK RELAY R 850 REF WDM 27-41-12. NO HELP PERFORMED LAND VERIFY TEST, TEST FAILED, PER DFCS SUMMARY - NEED MORE TROUBLESHOOTING. SUSPECT LRU IS ''STAB TRIM RLY'', (FCC-A/B INTERFACE, J1C-D03). PER FIM 2
- [SDR CALA2020121401369](https://openairdocs.org/sdr/CALA2020121401369.md): Pan · corroded · Dec 12, 2020 · N33714 · Boeing 737724 · Fuselage Miscellaneous Structure
  > REF LOG PAGE 9760918 FOR LAV PAN CORROSION. ACCOMPLISH A PERMANENT REPAIR, PER PART 3 OF ECRA 5331-02688 ON OR BEFORE 11-DECEMBER-2022. PLANNING TO CONTACT ENGINEERING AFTER 11-AUGUST-2022 BUT BEFORE 11-SEPTEMBER-2022 FOR PERMANENT REPAIR.
- [SDR CALA2020021200403](https://openairdocs.org/sdr/CALA2020021200403.md): Fitting · cracked · Feb 10, 2020 · N33714 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 15.04. IAW B73 7 700 SRM 51-40-02 AND DWG NO 111A2000. SSFR REPORT, FORM 46-002 4, ENTERED BY UAL INSPECTION U241010, 2/10/2020 INSPECTION ACCEPTED
- [SDR CALA2020021200387](https://openairdocs.org/sdr/CALA2020021200387.md): Fitting · cracked · Feb 8, 2020 · N33714 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT 540 RBL 6.14 IAW B737-700 SRM 51-40-02 AND DWG NO 111A2000. SSFR REPORT, FORM 46-0024, ENT ERED BY UAL INSPECTION U241010, 2/8/20 INSPECTION ACCEPTED
- [SDR CALA2020021200386](https://openairdocs.org/sdr/CALA2020021200386.md): Fitting · cracked · Feb 8, 2020 · N33714 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 LBL 32.40 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 3240 IAW B737- 700 SRM 51-40-02 AND DWG NO 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U241010, 2/8/2020 INSPECTION ACCEPTED
- [SDR CALA2020021200385](https://openairdocs.org/sdr/CALA2020021200385.md): Fitting · cracked · Feb 8, 2020 · N33714 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 15-04 IAW B737 -700 SRM 51-40-02 AND ECRA NO 5714-01063. SSFR REPORT, FORM 46-0 024, ENTERED BY UAL INSPECTION U241010, 2/8/20 INSPECTION ACCEPTED
- [SDR CALA2020021200392](https://openairdocs.org/sdr/CALA2020021200392.md): Fitting · cracked · Feb 8, 2020 · N33714 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 6.14 IAW B737 700 SRM. 51-40-02 AND ECRA 5714-01061. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U241010, 2/8/20. INSPECTION ACCEPTED
- [SDR CALA2020021200389](https://openairdocs.org/sdr/CALA2020021200389.md): Fitting · cracked · Feb 8, 2020 · N33714 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 32.40 IAW B737-700 SRM 51-40-02 AND ECRA NO 5714-01064.
- [SDR CALA2020021200384](https://openairdocs.org/sdr/CALA2020021200384.md): Fitting · cracked · Feb 8, 2020 · N33714 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED LP 5865973 SPT REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 40.87 IAW B737 -700 SRM 51-40-02 AND ECRA 5714-01062.
- [SDR CALA2020021200383](https://openairdocs.org/sdr/CALA2020021200383.md): Fitting · cracked · Feb 8, 2020 · N33714 · Boeing 737724 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA. 540 RBL 54.60 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 54.60 IAW B737 -700 SRM 51-40-02 AND ECRA NO 5724-01065. SSFR REPORT, FORM 46-0 024, ENTERED BY UAL INSPECTION U241010, 2/8/20 INSPECTION ACCEPTED
- [SDR CALA2020021200394](https://openairdocs.org/sdr/CALA2020021200394.md): Fitting · cracked · Feb 8, 2020 · N33714 · Boeing 737724 · Wing Miscellaneous Structure
  > SHEAR FITTING AT STA 540 RBL 40.87 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540, RBL 40.87. IAW B7 37 700. SRM 51-60-02 AND DWG NO. 111A 2000. SSFR REPORT, FORM 46 -0024, ENTERED BY UAL INSPECTIONU241010, 2/8/2020 INSPECTION ACCEPTED
- [SDR CALA2018020900538](https://openairdocs.org/sdr/CALA2018020900538.md): Lamp · failed · Feb 9, 2018 · N33714 · Boeing 737724 · Passenger Compartment Lighting
  > READING LIGHT AT SEAT 22D PRODUCED A LITTLE SMOKE, BECAME INOPERATIVE AND STOPPED SMOKING. REPLACED THE LAMP. OPS CHECKED OK.
- [SDR CALA2018010700091](https://openairdocs.org/sdr/CALA2018010700091.md): Flashlight · inoperative · Jan 7, 2018 · N33714 · Boeing 737724 · Emergency Equipment
  > EMERGENCY FLASHLIGHT AFT RIGHT HAND INBD INOP. REPLACED EMERGENCY FLASHLIGHT AFT RT HAND INBD. NOW OK FOR SERVICE.
- [SDR CALA2017102703781](https://openairdocs.org/sdr/CALA2017102703781.md): Window Frame · cracked · Oct 25, 2017 · N33714 · Boeing 737724 · Fuselage Main, Structure
  > CRACK FOUND ON THE L1 WINDOW FRAME. THE WINDOW FRAME REPAIRED IAW ECRA 5311-01879.
- [SDR CALA2017102703779](https://openairdocs.org/sdr/CALA2017102703779.md): Window Frame · cracked · Oct 24, 2017 · N33714 · Boeing 737724 · Fuselage Main, Structure
  > CRACK FOUND ON THE R1 WINDOW FRAME. REPAIRED IAW ECRA 5311-01880, STEP D 8.
- [SDR CALA2017102003659](https://openairdocs.org/sdr/CALA2017102003659.md): Skin · bulged · Oct 19, 2017 · N33714 · Boeing 737724 · Fuselage Main, Plate/Skin
  > BULGE IN FUSELAGE SKIN, FWD AND ABOVE EXTERNAL POWER PANEL. REPAIRED IAW EC/RA 5330-06208.
- [SDR CALA2017101303584](https://openairdocs.org/sdr/CALA2017101303584.md): Bulkhead Web · cracked · Oct 12, 2017 · N33714 · Boeing 737724 · Fuselage Main, Bulkhead
  > BS 663 BULKHEAD WEB HAS A ONE INCH CRACK BETWEEN LBL 45.64 - 40.92. REPAIRED IAW SRM 57-10-10, REP 3, ALT 2
- [SDR CALA2016102800830](https://openairdocs.org/sdr/CALA2016102800830.md): Slide · unsecure · Oct 28, 2016 · N33714 · Boeing 737724 · Escape Slide
  > DOOR 1L 2 FOOT OF SLIDE LOOSE ON BOTTOM OF PACK. REPACKED 1L DOOR SLIDE IAW MM 25-66-01-401-801. OPS CHECKS GOOD OK TO CONTINUE.
- [SDR CALA2016090900645](https://openairdocs.org/sdr/CALA2016090900645.md): Slide · loose · Sep 9, 2016 · N33714 · Boeing 737724 · Escape Slide
  > L1 DOOR SLIDE LOOSE. INSTALLED THE SLIDE IAW AMM 25-66-01-400-803 DOOR OPS NORMAL GIRT BAR OPS NORMAL.
- [SDR CALA2016082200560](https://openairdocs.org/sdr/CALA2016082200560.md): Motor · failed · Aug 22, 2016 · N33714 · Boeing 737724 · Stabilizer Control System
  > ELECTRIC TRIM FAILED WITH AUTOPILOT ON DURING CLIMBOUT, RECEIVED A STAB OUT OF TRIM LIGHT. RAN QRH AND THEN RAN ELECTRIC STABILIZER TRIM INOPERATIVE QRH. REPLACED STABILIZER TRIM MOTOR IAW AMM27-41-71-401. ACCOMPLISHED MOTOR TRIM TEST IAW AMM27-41-71-700-
- [SDR CALA2015120400967](https://openairdocs.org/sdr/CALA2015120400967.md): Charger · inoperative · Dec 2, 2015 · N33714 · Boeing 737724 · Emergency Lighting
  > SUPPORT TASK, EMER AISLE LIGHTS IN AFT CABIN INOPERATIVE. TROUBLE SHOT SYS, FOUND EMER LIGHTS BATTERY CHARGER BAD. REMOVED CHARGER, PN D717-02-030, SN 4494. INSTALLED NEW CHARGER, PN D717-02-030 & SN 5617. SYS OPERATIONS CHECKED GOOD IAW AMM 33-51-06. R &
- [SDR CALA2013082800589](https://openairdocs.org/sdr/CALA2013082800589.md): Pressure Panel · cracked · Aug 26, 2013 · N33714 · Boeing 737724 · Fuselage Main, Bulkhead
  > CENTER WING BOX REAR SPAR VERTICAL PRESSURE WEB STATION 663, CRACKED TWO PLACES, 1/4" CRACK AT RBL 35 & AMP; WL 196 1 1/4" CRACK AT RBL 43 AND WL 197. ACCOMPLISHED, IAW SRM 57-10-10, REPAIR 3 PG 204, FIG 204.
- [SDR 39NR2013082620](https://openairdocs.org/sdr/39NR2013082620.md): Pressure Panel · cracked · Aug 26, 2013 · N33714 · Boeing 737724 · Fuselage Main, Bulkhead
  > DURING INSPECTION OF BS 663 VERTICAL PRESSURE WEB FOUND TWO CRACKS. REPAIRED VERTICAL PRESSURE WEB IAW SRM 57-10-10, REPAIR NR 3.
- [SDR CALA2013071700496](https://openairdocs.org/sdr/CALA2013071700496.md): Wire Harness · shorted · Jul 16, 2013 · N33714 · Boeing 737724 · Light System Wiring
  > SEAT EMERGENCY LIGHTING INOPERATIVE AT SEAT 26C. R & R WIRE HARNESS IAW IFM 25-25-99 AND SWP 20-10-13. OPS CHECKED GOOD.
- [SDR CALA2013022700134](https://openairdocs.org/sdr/CALA2013022700134.md): Frame · cracked · Feb 26, 2013 · N33714 · Boeing 737724 · Fuselage Main, Frame
  > CRACK INDICATION NOTED ON FRAME BS 706 BETWEEN STRINGER S8-S9L, FRAME HAS BEEN REPAIRED IAW EC/RA 5310-05641.
- [SDR CALA2013022700133](https://openairdocs.org/sdr/CALA2013022700133.md): Frame · cracked · Feb 26, 2013 · N33714 · Boeing 737724 · Fuselage Main, Frame
  > CRACK INDICATION NOTED AT FRAME BS 907L BETWEEN STRINGER S8-9L. FRAME HAS BEEN REPAIRED IAW EC/RA 5310-05641.
- [SDR CALA2013022700132](https://openairdocs.org/sdr/CALA2013022700132.md): Frame · cracked · Feb 26, 2013 · N33714 · Boeing 737724 · Fuselage Main, Frame
  > CRACK INDICATION NOTED AT FRAME BS 907, RT BETWEEN S8-9R. FRAME 907 REPAIRED IAW EC/RA 5310-05641.
- [SDR CALA2012121900864](https://openairdocs.org/sdr/CALA2012121900864.md): Floorbeam · corroded · Dec 15, 2012 · N33714 · Boeing 737724 · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 328 RBL 16" CORRODED OUT OF LIMITS. FLOORBEAM REPAIRED IAW ECRA 5321-01827.
- [SDR CALA2012121000855](https://openairdocs.org/sdr/CALA2012121000855.md): Frame · cracked · Dec 8, 2012 · N33714 · Boeing 737724 · Fuselage Main, Frame
  > CRACK INDICATION NOTED AT FRAME BS 867 BETWEEN STRINGER S8-S9L DURING MFEC INSPECTION. INSTALLED REPAIR IAW EA 5310-04716, REV D OP 1.
- [SDR CALA2012120700852](https://openairdocs.org/sdr/CALA2012120700852.md): Frame · cracked · Dec 7, 2012 · N33714 · Boeing 737724 · Fuselage Main, Frame
  > CRACK INDICATION NOTED AT FRAME BS 747L STRINGER S8-S9. REPAIRED FRAME IAW EA 5310-04716, REV D, OP 1.
- [SDR CALA2012120500848](https://openairdocs.org/sdr/CALA2012120500848.md): Frame · cracked · Dec 5, 2012 · N33714 · Boeing 737724 · Fuselage Main, Frame
  > CRACK INDICATION NOTED AT FRAME BS 500C BETWEEN S-8 AND 9R. DURING MFEC INSPECTION. FRAME BS 500C HAS BEEN REPAIRED IAW EA 5310-04716, REV A, FIG 3.

Next page: https://openairdocs.org/aircraft/N33714/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 = 'N33714' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N33714/reports

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