# Service difficulty reports: N15751

A list on [N15751](https://openairdocs.org/aircraft/N15751.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 · 65 reports

- [SDR CALA2026101220267](https://openairdocs.org/sdr/CALA2026101220267.md): Battery Pack · no test · Oct 7, 2026 · N15751 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK AT M1672 FAILED OPERATION CHECK. REMOVED AND REPLACED M1672 BATTERY IAW AMM 33-51-06 OPS CHK GOOD.
- [SDR CALA2026101220266](https://openairdocs.org/sdr/CALA2026101220266.md): Battery Pack · no test · Oct 7, 2026 · N15751 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK AT M1669 FAILED OPERATION CHECK. REMOVED AND REPLACED M1669 BATTERY PACK IAW AMM 33-51-06 OPS CHK GOOD.
- [SDR CALA2026062917382](https://openairdocs.org/sdr/CALA2026062917382.md): Housing · damaged · Jun 27, 2026 · N15751 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - ROW 29 ABC EPL SHROUD IS DAMAGED AND NOT SECURED TO SEAT REMOVED AND REPLACED THE BROKEN SHROUD. REF CMM 25-21-56.
- [SDR CALA2025111711259](https://openairdocs.org/sdr/CALA2025111711259.md): Smoke Detector · false activation · Nov 15, 2025 · N15751 · Boeing 737724 · Smoke Detection
  > SMOKE ALARM. NO SMOKE NOTICED ALL LAV SMOKE DETECTORS OPS NORMAL, IAW AMM 26-14-00-730-801.
- [SDR CALA2025111311179](https://openairdocs.org/sdr/CALA2025111311179.md): Indicator · faulted · Nov 11, 2025 · N15751 · Boeing 737724 · Trailing Edge Flap Control System
  > FLAPS STUCK BETWEEN 5 AND 10 DEGREES AND WOULD NOT MOVE WITH FLAP HANDLE MOVEMENT. PSEU LIGHT ON. BITE CHECKED PSEU AND FOUND LDG FLAP A FAULT MESSAGE 32-62009 AND LDG FLAP B FAULT WITH MESSAGE 32-62010. AND NO DISPATCH. PERFORMED FSEU BITE. FOUND PROBLEM WIT
- [SDR CALA2025111011030](https://openairdocs.org/sdr/CALA2025111011030.md): Flap System · malfunctioned · Nov 9, 2025 · N15751 · Boeing 737724 · Trailing Edge Flap Control System
  > FLAP LOCK OUT ON 1ST TICK. ATTEMPTED RESEAT OF LEVER, NO HELP. ALTN EXTENSION REQUIRED. PERFORMED OPS CHECK OF NORMAL AND ALTN FLAP CONTROL SYSTEMS IAW AMM 27-51-00-710-801. OPS CHECK GOOD. PERFORMED BITE TEST OF FSEU IAW FIM 27-51 TASK 801. INTERMITTENT INACT
- [SDR CALA2025080107212](https://openairdocs.org/sdr/CALA2025080107212.md): Window Frame · cracked · Jul 30, 2025 · N15751 · Boeing 737724 · Fuselage Main, Structure
  > L3 WINDOW FRAME E-F POST REPAIRED PER ECRA 5310-08654. PERFORM AN INSPECTION OF LT WINDOW FRAME E-F POST REPAIR ON AIRCRAFT IAW PART 2 OF THE LATEST REVISION OF ECRA 5310-08654. MAJOR REPAIR. ACCOMPLISHED ESFR AND PERMANENT REPAIR COMPLIED WITH.
- [SDR CALA2025073107146](https://openairdocs.org/sdr/CALA2025073107146.md): Window Frame · damaged · Jul 30, 2025 · N15751 · Boeing 737724 · Fuselage Main, Structure
  > REPAIR THE RH #3 WINDOW FRAME E-F POST REF TO ECRA 5611-01314 R EV C PART 3. REPAIRED PER ECRA 5310-08655 REPAIR THE R3 WINDOW FRAME E-F POST REF TO ECRA 5611-01314 R EV C PART 3.
- [SDR CALA2025073107142](https://openairdocs.org/sdr/CALA2025073107142.md): Battery Pack · no test · Jul 30, 2025 · N15751 · Boeing 737724 · Emergency Lighting
  > EMERGENCY PASSENGER CABIN LIGHTS M1674 FAILS BATTERY CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK M01674 AND PERFORMED INSTALLATION TEST IAW B737 A.M.M. 33-51-06-960-805. TEST OK.
- [SDR CALA2025041403776](https://openairdocs.org/sdr/CALA2025041403776.md): Landing Light · damaged · Apr 12, 2025 · N15751 · Boeing 737724 · Exterior Lighting
  > PDA 2 RF LOG 4481684.. LEFT RETRACTABLE LANDING LIGHT LENS AND BULB MISSING ON ARRIVAL... SEE PHOTO... ADDED PHOTO PARTS USED: 29-3342-9-0001,QTY:1 REPLACED LH LANDING LIGHT ASSY PER AMM33-42-02-960-802. OPS CHECKS GOOD. SDR REPORT SUBMITTED.PARTS USED: 29-
- [SDR CALA2025021800376](https://openairdocs.org/sdr/CALA2025021800376.md): Strap · corroded · Feb 17, 2025 · N15751 · Boeing 737724 · Wing Main, Frame Structure
  > REMOVED AND INSTALLED NEW R/W FRONT SPAR LOWER STRAP INBD OF PYLON AT IFSS 155 AS PER SRM 51-40-02-0G-0,DWG 112A4401.REF AAR N/R9935224.WORK ACCOMPLISHED BY V945157.
- [SDR CALA2025021400353](https://openairdocs.org/sdr/CALA2025021400353.md): Strap · gouged · Feb 12, 2025 · N15751 · Boeing 737724 · Fuselage Miscellaneous Structure
  > FOUND 3 EACH LOWER STRAPS WITH GOUGES AT STA 540 LBL STRINGER 23 REF AAR N/R 9935388
- [SDR CALA2025021100337](https://openairdocs.org/sdr/CALA2025021100337.md): Pan · cracked · Feb 7, 2025 · N15751 · Boeing 737724 · Fuselage Miscellaneous Structure
  > REMOVED AND REPLACED PAN ASSY AT DOOR CUT OUT R1 PER REF SRM 51-40-02-0G-0 AND DWG 141A8370.REF AAR N/R 9935718. WORK ACCOMPLISHED BY V894270.
- [SDR CALA2025020500296](https://openairdocs.org/sdr/CALA2025020500296.md): Skin · cracked · Feb 1, 2025 · N15751 · Boeing 737724 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT RIGHT HORIZONTAL STB LOWER SKIN STA 147.90, 24" FROM SPAR, I/B ROW. CRACK LENGTH 0.5" REF AAR N/R 9935073
- [SDR CALA2025012900229](https://openairdocs.org/sdr/CALA2025012900229.md): Floorbeam · corroded · Jan 22, 2025 · N15751 · Boeing 737724 · Fuselage Main, Floor Beam
  > AFT WET ARE STA 992 RBL48 INNER CHORD SEVERAL SPOTS OF CORROSION REF AAR NR9935198 REMOVED AND REPLACED AFT WET ARE STA992RBL48INNER CHORD DUE TO SEVERAL SPOTS OF CORROSION FOUND TO BE OUT OF LIMITS AS PER SRM 53-70-15-17-1 AND SRM 51-40-02-0G-0,DWG:147A8501.
- [SDR CALA2024122701675](https://openairdocs.org/sdr/CALA2024122701675.md): Acm · faulted · Dec 25, 2024 · N15751 · Boeing 737724 · Cabin Cooling System
  > LEFT PACK DRIVING FULL HOT REGARDLESS OF MANUAL CONTROL VALVE. E LEC SMELL NOTED REMOVED AND REPLACED L/H ACM PER REF AMM 21-51-04. OPS CHECK GOOD. NO LEAK NOTED. NO SMELL NOTED.
- [SDR CALA2024111901180](https://openairdocs.org/sdr/CALA2024111901180.md): Lamp · inoperative · Nov 16, 2024 · N15751 · Boeing 737724 · Emergency Lighting
  > WINDOW LIGHT ABOVE EMERGENCY EXIT INOP AT ROW 21A. REPLACED LAMP PER AMM 33-21-00-960-807. OP 'S CHK OK.
- [SDR CALA2024032200843](https://openairdocs.org/sdr/CALA2024032200843.md): Target · unsecure · Mar 21, 2024 · N15751 · Boeing 737724 · Leading Edge Slat Position Indicating System
  > LEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED ON DESCENT THEN ACTIONED QRH. DEBREIFED INBOUND CREW & RAN FLAPS UP & DOWN NO HELP LEADING TRANSIT LIGHT STILL ON UNLOCKING ACCOMPISHED LEADING EDGE FLAP AND SLAT PROXIMITY SENSOR TEST AMM 27-88-11-700-801 FOUND N
- [SDR CALA2024011200085](https://openairdocs.org/sdr/CALA2024011200085.md): Engine · vibration · Jan 10, 2024 · N15751 · Boeing 737724 · Engine (Turbine/Turboprop)
  > ENGINE VIBRATION, VIBRATION HIGH ENGINE 2 MODERATE TO XCESSIVEVIBRATION ENG 2 AT CRZ STABILZD WITH NO AB IND RECURRED IN DESCENT ENG2 SN. 888650 (TSI=3004/ CSI= 1441) REMOVED MCD'S. FOUND METAL SHAVINGS IN REAR MCD. SEE PICS. (COPIED TEXTAND PIX FROM L/P 6781
- [SDR CALA2023110303268](https://openairdocs.org/sdr/CALA2023110303268.md): Light · inoperative · Oct 31, 2023 · N15751 · Boeing 737724 · Emergency Lighting
  > ROW 29ABC EMERGENCY STOWBIN LIGHT INOP RELAMPED. OPS CK GOOD
- [SDR CALA2023032000798](https://openairdocs.org/sdr/CALA2023032000798.md): Window Frame · cracked · Mar 17, 2023 · N15751 · Boeing 737* · Fuselage Main, Structure
  > SUSPECT CRACK IN R3 WINDOW FRAME ON FWD. SIDE 2ND FASTENER FROM BOTTOM PERFORMED HFEC SURFACE INSPECTION OF L3 WINDOW FRAME AT SECOND FASTENER HOLE FROM THE BOTTOM OF FWD FRAME EDGE AND VERIFIED CRACK EMINATING AFT.200 FROM FASTENER EDGE. REF 737 NTM PART 6-5
- [SDR CALA2023032000797](https://openairdocs.org/sdr/CALA2023032000797.md): Window Frame · cracked · Mar 17, 2023 · N15751 · Boeing 737* · Fuselage Main, Structure
  > SUSPECT CRACK IN L3 WINDOW FRAME ON FWD. EDGE 2ND FASTENER FROM THE BOTTOM PERFORMED HFEC SURFACE INSPECTION OF L3 WINDOW FRAME AT SECOND FASTENER HOLE FROM THE BOTTOM OF FWD FRAME EDGE AND VERIFIED CRACK ACROSS FASTENER HOLE TO EDGES.REF 737 NTM PART 6-51-00-
- [SDR CALA2023031300721](https://openairdocs.org/sdr/CALA2023031300721.md): Window Frame · cracked · Mar 13, 2023 · N15751 · Boeing 737* · Window/Windshield System
  > SUSPECT CRACK IN R3 WINDOW FRAME ON FWD. SIDE 2ND FASTENER FROM BOTTOM PERFORMED HFEC SURFACE INSPECTION OF L3 WINDOW FRAME AT SECOND FASTENER HOLE FROM THE BOTTOM OF FWD FRAME EDGE AND VERIFIED CRACK EMINATING AFT.200 FROM FASTENER EDGE. REF 737 NTM PART 6-5
- [SDR CALA2023031300720](https://openairdocs.org/sdr/CALA2023031300720.md): Window Frame · cracked · Mar 13, 2023 · N15751 · Boeing 737* · Window/Windshield System
  > SUSPECT CRACK IN L3 WINDOW FRAME ON FWD. EDGE 2ND FASTENER FROM THE BOTTOM PERFORMED HFEC SURFACE INSPECTION OF L3 WINDOW FRAME AT SECOND FASTENER HOLE FROM THE BOTTOM OF FWD FRAME EDGE AND VERIFIED CRACK ACROSS FASTENER HOLE TO EDGES.REF 737 NTM PART 6-51-00-
- [SDR CALA2022100302638](https://openairdocs.org/sdr/CALA2022100302638.md): Skin · cracked · Oct 3, 2022 · N15751 · Boeing 737724 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT FRAME 737C BETWEEN STR 2L AND 2R CRACK DAMAGE.FOR REPAIR OF SKIN FRAME AT 737C BETWEEN FRAME 2L AND 2R (WORK ACCOMPLISHED BY V920656 AND AAR QC V923046) ADD EMP:V920656 COMPLIED WITH EC/RA 5331-02969 & EC/RA 5331-02968 FOR REPAIR OF SKIN FRAM
- [SDR CALA2022100302614](https://openairdocs.org/sdr/CALA2022100302614.md): Skin · unknown · Oct 2, 2022 · N15751 · Boeing 737724 · Fuselage Main, Plate/Skin
  > ON OR BEFORE AUGUST 27, 2023, PERFORM AN INSPECTION OF THE EXTERNAL DOUBLER/TRIPLER REPAIRS TO THE FUSELAGE SKIN AT STA 727C, STR 3L ? 3R IN ACCORDANCE WITH PART 2 OF THE LATEST REVISION OF ECRA 5331-02969. 727C, STR 3L ? 3R ON AIRCRAFT N15751 IN ACCORDANCE WI
- [SDR CALA2022100302613](https://openairdocs.org/sdr/CALA2022100302613.md): Skin · unknown · Oct 2, 2022 · N15751 · Boeing 737724 · Fuselage Main, Plate/Skin
  > ON OR BEFORE JUNE 26, 2023, OR THE ACCUMULATION OF 28,974 TOTAL AIRCRAFT FLIGHT CYCLES, WHICHEVER COMES FIRST, PERFORM AN INSPECTION OF THE EXTERNAL DOUBLER/TRIPLER REPAIR TO THE FUSELAGE SKIN AT STA 747 - 787, STR 1 - 4L ON AIRCRAFT N15751 IN ACCORDANCE WITH
- [SDR CALA2022083102230](https://openairdocs.org/sdr/CALA2022083102230.md): Skin · none · Aug 30, 2022 · N15751 · Boeing 737 · Wing Structure
  > DURING A C CHECK AT AAR-RFD, HEAVY CORROSION WAS FOUND ON THE LO WER SURFACE OF THE WING CENTER SECTION FORWARD LOWER SKIN PANEL (P/N 111A4102-7) AT STA 540 UNDER THE LEFT-HAND DRAG LINK (P/N 1 43A0062-27) (REF AAR RFD NR 99939586) PERFORMED REPAIR OF CORROSIO
- [SDR CALA2022082902213](https://openairdocs.org/sdr/CALA2022082902213.md): Skin · corroded · Aug 29, 2022 · N15751 · Boeing 737 · Wing Structure
  > HEAVY CORROSION WAS FOUND ON THE LOWER SURFACE OF THE WING CENTER SECTION FORWARD LOWER SKIN PANEL AT STA 540 UNDER THE LEFT-HAND DRAG LINK. PERFORMED REPAIR OF CORROSION FOUND ON LEFT WING CENTER SECTION LOWER PANEL BS540 AND COMPLIED WITH EA 220206 AND EC/RA
- [SDR CALA2022082902201](https://openairdocs.org/sdr/CALA2022082902201.md): Battery · none · Aug 27, 2022 · N15751 · Boeing 737 · Lighting System
  > EMERGENCY LIGHTS CAPACTIY CHECK NO GOOD ON BATTERIES M1674 AND M 1669 (REF AAR NR 99939054).
- [SDR CALA2022082902195](https://openairdocs.org/sdr/CALA2022082902195.md): Skin · none · Aug 26, 2022 · N15751 · Boeing 737 · Vacuum System
  > BEGIN REPAIR AT L/H SIDE AT WASTE TANK VACUMM HOLE (REF AAR NR 9 9939552) 31-02932 INITIATE 2ND DIP FOR PLANNING TO CONTACT ENG FOR INSCPE CTION REQUIREMENTS ON REPAIR ON OR BEFORE JAN 10, 2024 (WORK ACC OMPLISHED BY V920656 AND V895387) COMPLIED WITH EC/RA 53
- [SDR CALA2022050901188](https://openairdocs.org/sdr/CALA2022050901188.md): None · faulty · May 9, 2022 · N15751 · Boeing 737 · Navigation System
  > TEMP PROBE LIGHT LIGHT ON PROBE P/N NIS EWR 29-3421-3-0006 GASKET P/N 29-3412-3-0007 AVIONICS UPDATE THERE IS NO POWER TO THE TAT PROBE AVIONICS T/S PER SSM 24-51-11 PG1 FOUND NO PWR TO TCAS AND TAT PROBE C/B'' TROUBLE SHOOTING CONTINUES SUSPECT LOST OF POWE
- [SDR CALA2022050901169](https://openairdocs.org/sdr/CALA2022050901169.md): Shift Mechanism · failed · May 6, 2022 · N15751 · Boeing 73771Q · Auto Flight System
  > STAB TRIM LITE ILLUMINATED IN FLIGHT WITH A SPEED TRIM FAILURE BOTH AIRCFAFT HAD TO BE FLOWN BY HAND NO AUTOPILOT PERFORMED STAB TRIM TEST, COLUMN SWITCHING MODULES AND NEUTRAL SHIFT SENSOR FAILED SEVERAL TIMES. FURTHER T/S REQUIRED. REF L/P 8537413, FOUND PHA
- [SDR CALA2019102901851](https://openairdocs.org/sdr/CALA2019102901851.md): Drain Mast · sheared · Oct 27, 2019 · N15751 · Boeing 73771Q · Aircraft Fuel Distribution System
  > PDA 2 REF LOG PAGE 3676794; AIRCRAFT ARRIVED IN SAT WITH LOWER 13 INCHES OF APU FUEL LINE SHROUD DRAIN MAST MISSING. MAST P/N IS 346A2801-3. CORRECTIVE ACTION IS REPLACEMENT OF DRAIN MAST, REF L/P 3676794
- [SDR CALA2019062101005](https://openairdocs.org/sdr/CALA2019062101005.md): Bulkhead Web · cracked · Jun 18, 2019 · N15751 · Boeing 73771Q · Fuselage Main, Bulkhead
  > FOUND 4EA.CRACKS ON RIGHT CENTER WING REAR SPAR VERTICAL RESSURE WEB1 CRACK STA.RBL 25-31.83. 1 CRACK STA RBL 31.83-40.2 CRACK S STA RBL 40-45.64. ALL CRACKS VERIFIED WITH HFEC AND CRCKS MARKED. REMOVED DAMAGED SECTION OF PESSURE DECK WEB AND INSTALLED REPAIR
- [SDR CALA2019062101002](https://openairdocs.org/sdr/CALA2019062101002.md): Frame · worn · Jun 18, 2019 · N15751 · Boeing 73771Q · Fuselage Main, Frame
  > AFT CARGO FRAME STA 747 RBL 15 BETWEEN STR 25R AND 26R ELONGATED HOLE WHERE SIDE PANEL ATTACHES. FRAME REPAIRED REF ECRA 5310-07631
- [SDR CALA2019062210994](https://openairdocs.org/sdr/CALA2019062210994.md): Frame · cracked · Jun 18, 2019 · N15751 · Boeing 73771Q · Fuselage Main, Frame
  > MAIN CABIN UPPER LOBE FUSELAGE FRAME AT STA 440 BETWEEN S-8R AND S-9R HAS CRACK AT I/B FASTENER HOLE FOR AC OUTLET EXTRUSION SUPPORT BRACKET (REPAIR PER W/C SEQ #1655 FIG 3 STEP 9) REPAIRED CABIN FRAME AT STA 440 STR8R PER ECRA 5310-07627.
- [SDR CALA2019062100993](https://openairdocs.org/sdr/CALA2019062100993.md): Frame · cracked · Jun 18, 2019 · N15751 · Boeing 73771Q · Fuselage Main, Frame
  > MAIN CABIN UPPER LOBE FUSELAGE FRAME AT STA 747 BETWEEN S-8R AND S-9R HAS CRACK AT I/B FASTENER HOLE FOR AC OUTLET EXTRUSION SUPPORT BRACKET (REPAIR PER W/C SEQ #1655 FIG 3 STEP 9) REPAIRED CABIN FRAME AT STA 747 STR8R PER ECRA 5310-07620.
- [SDR CALA2019062210992](https://openairdocs.org/sdr/CALA2019062210992.md): Frame · cracked · Jun 18, 2019 · N15751 · Boeing 73771Q · Fuselage Main, Frame
  > MAIN CABIN UPPER LOBE FUSELAGE FRAME AT STA380 BETWEEN S-8R AND S-9R HAS CRACK AT I/B FASTENER HOLE FOR AC OUTLET EXTRUSION SUPPORT BRACKET.
- [SDR CALA2019062210999](https://openairdocs.org/sdr/CALA2019062210999.md): Frame · worn · Jun 18, 2019 · N15751 · Boeing 73771Q · Fuselage Main, Frame
  > AFT CARGO FRAME STA 727C RBL 15 BETWEEN STR 25R AND 26R ELONGATED HOLE WHERE SIDE PANEL ATTACHES. FRAME REPAIRED REF ECRA 5310-07631, SEE FLEETCYCLE L/P 9672870 FOR ALL WORK PERFORMED. ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE THE AIRCRAFT REACHES 75000
- [SDR CALA2019062210998](https://openairdocs.org/sdr/CALA2019062210998.md): Frame · cracked · Jun 18, 2019 · N15751 · Boeing 73771Q · Fuselage Main, Frame
  > MAIN CABIN UPPER LOBE FUSELAGE FRAME AT STA 727D BETWEEN S-8L AN D S-9L HAS CRACK AT I/B FASTENER HOLE FOR AC OUTLET EXTRUSION SU PPORT BRACKET (REPAIR PER W/C SEQ #1655 FIG 3 STEP 9) REPAIRED MAIN CABIN UPPER LOBE FUSELAGE FRAME STATION 727D BETWE EN S-8L AND
- [SDR CALA2019062210991](https://openairdocs.org/sdr/CALA2019062210991.md): Frahm · cracked · Jun 17, 2019 · N15751 · Boeing 73771Q · Fuselage Main, Frame
  > MAIN CABIN UPPER LOBE FUSELAGE FRAME BS 727D BETWEEN S-8L AND S-9L WAS CRACK AT I/B FASTENER HOLE FOR AC OUTLET EXTRUSION SUPPORT BRACKET.
- [SDR CALA2019062100990](https://openairdocs.org/sdr/CALA2019062100990.md): Frame · cracked · Jun 17, 2019 · N15751 · Boeing 73771Q · Fuselage Main, Frame
  > FRAME AT BS 500A BETWEEN S-8R AND S-9R CRACKED AT I /B FASTENER HOLE AC OUTLET EXTRUSION SUPPORT BRACKET. REPAIRED THE FRAME IAW ECRA 5 311-02138 AND EA 5310-04716 REV I OP1 FIG 3.
- [SDR CALA2019062210989](https://openairdocs.org/sdr/CALA2019062210989.md): Frame · cracked · Jun 17, 2019 · N15751 · Boeing 73771Q · Fuselage Main, Frame
  > FRAME AT STA 480 BETWEEN S-8R AND S-9R CRACK AT I/B FASTENER HOLE AC OUTLET EXTRUSION SUPPORT BRACKET. REPAIRED FUSELAGE FRAME IAW ECR A 5311-02138 AND EA5310-04716 REV I OP1 FIG 3.
- [SDR CALA2019061700959](https://openairdocs.org/sdr/CALA2019061700959.md): Frame · cracked · Jun 15, 2019 · N15751 · Boeing 73771Q · Fuselage Main, Frame
  > MAIN CABIN UPPER LOBE FUSELAGE FRAME AT STA 380 BETWEEN S-8L AND S-9L HAS CRACK AT I/B FASTENER HOLE FOR AC OUTLET EXTRUSION SUPP ORT BRACKET (REPAIR PER W/C SEQ #1655 FIG 3 STEP 9) REF FLEETCYCLE N/R 9666842 REPAIRED FRAME STA 380 S-7L AND S-8L PER EC/RA # 53
- [SDR CALA2019061400952](https://openairdocs.org/sdr/CALA2019061400952.md): Frame · damaged · Jun 14, 2019 · N15751 · Boeing 73771Q · Fuselage Main, Frame
  > AFT CARGO FRAME STA 727D RBL 15 BETWEEN STR 25R AND 26R ELONGATED HOLE WHERE SIDE PANEL ATTACHES. FRAME REPAIRED AS REF ECRA 5310-07631 SEE FLEETCYCLE L/P 9672871 FOR WORK PERFORMED. VERIFIED ACCOMPLISHMENT OF FRAME REPAIR REF ECRA 5310-07631
- [SDR CALA2019061400951](https://openairdocs.org/sdr/CALA2019061400951.md): Frame · damaged · Jun 14, 2019 · N15751 · Boeing 73771Q · Fuselage Main, Frame
  > AFT CARGO FRAME STA 727A RBL 15 BETWEEN STR 25 R AND 26 R ELONGATED HOLE WHERE SIDE PANEL ATTACHES. FRAME REPAIRED AS REF ECRA 5310-07631 SEE FLEETCYCLE L/P 9672868 FOR WORK PERFORMED. VERFIED ACCOMPLISHMENT OF FRAME REPAIR REF. EC/RA 5310-07631
- [SDR CALA2019061400950](https://openairdocs.org/sdr/CALA2019061400950.md): Frame · damaged · Jun 14, 2019 · N15751 · Boeing 73771Q · Fuselage Main, Frame
  > AFT CARGO FRAME STA 767 RBL 15 BETWEEN STR 25R AND 26R ELONGATED HOLE WHERE SIDE PANEL ATTACHES. FRAME REPAIRED AS REF ECRA 5310-07631 SEE FLEETCYCLE L/P 9672873 FOR ALL WORK PERFORMED. VERIFIED ACOMPLISHMENT OF FRAME REPAIR REF. EC/RA 5310-07631
- [SDR CALA2019061400949](https://openairdocs.org/sdr/CALA2019061400949.md): Frame · damaged · Jun 14, 2019 · N15751 · Boeing 73771Q · Fuselage Main, Frame
  > AFT CARGO FRAME STA 727E RBL 15 BETWEEN STR 25R AND 26R ELONGATED HOLE WHERE SIDE PANEL ATTACHES. FRAME REPAIRED AS REF ECRA 5310-07631 SEE FLEETCYCLE L/P 9672872 FOR ALL WORK PERFORMED. VERIFIED ACCOMPLISHMENT OF FRAME REPAIR REF. EC/RA 5310-07631
- [SDR CALA2019061400953](https://openairdocs.org/sdr/CALA2019061400953.md): Frame · worn · Jun 14, 2019 · N15751 · Boeing 73771Q · Fuselage Main, Frame
  > AFT CARGO FRAME STA 727B RBL 15 BETWEEN STR 25R AND 26R ELONGATE D HOLE WHERE SIDE PANEL ATTACHES. FRAME REPAIRED AS REF ECRA 5310-07631 REF FLEETCYCLE L/P 9672869 FOR ALL WORK PERFORMED. VERIFIED ACCOMPLISHMENT OF FRAME REPAIR REF ECRA 5310-07631

Next page: https://openairdocs.org/aircraft/N15751/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 = 'N15751' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N15751/reports

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