# Service difficulty reports: N375DA

A list on [N375DA](https://openairdocs.org/aircraft/N375DA.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 3 · 145 reports

- [SDR DALA2026031601811](https://openairdocs.org/sdr/DALA2026031601811.md): Battery Pack · no test · Mar 12, 2026 · N375DA · Boeing 737832 · Emergency Lighting
  > (LOG 8625215) 2 EMERGENCY BATTERY PACKS FAILED TEST. R/R BATTERY PACKS M1671 AND M1694 PER B737 AMM 33-51. OPS CHECK GOOD.
- [SDR DALA2026012600591](https://openairdocs.org/sdr/DALA2026012600591.md): Battery Pack · inoperative · Jan 24, 2026 · N375DA · Boeing 737832 · Emergency Lighting
  > ON SVC CHECK, FOUND CABIN AFT RT EMERGENCY LIGHTS INOPERATIVE. R & R AFT RT CABIN EMER LIGHTS BATTERY PACK IAW AMM 33-51, OPS CHECKED NORMAL.
- [SDR DALA2025061904612](https://openairdocs.org/sdr/DALA2025061904612.md): Light · inoperative · Jun 15, 2025 · N375DA · Boeing 737832 · Emergency Lighting
  > (LOG 7445530) DURING SVC FOUND EMERGENCY FLOOR PATH LIGHT AT ROW 27 INOP. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT ASSY PER B737 AMM 33-51. OPS CHECKED GOOD.
- [SDR DALA2025052203970](https://openairdocs.org/sdr/DALA2025052203970.md): Transmission · tripped · May 21, 2025 · N375DA · Boeing 737832 · Trailing Edge Flap Actuator
  > SHIP 3705 -DIV- PERFORMED A GO AROUND AND DIVERTED TO MBJ DUE TO FLAPS LOCKED AT 25. CORRECTIVE ACTION: BIT FSEU, INSPECTED FLAP OPERATION AND FLAP COMPONENTS. FOUND SEVERAL FLAP TRANSMISSION TRIP INDICATORS EXTENDED. RESET TRIP INDICATORS AND CHECKED OPERATIO
- [SDR DALA2025032402181](https://openairdocs.org/sdr/DALA2025032402181.md): Frame · none · Mar 21, 2025 · N375DA · Boeing 737832 · Standard Practices/Structures
  > (LOG 0870016) THIS WORK CARD INSTALLS A NEW SHIM BETWEEN THE LEFT SIDE OF STA 727 FRAME INNER CHORD AND S-18A WEB. AD 2023-06-15 REQUIRES INSPECTING THE STA 727 FRAME INNER CHORD AT STRINGERS S-18A FOR EXISTING REPAIRS, INSPECTING THE AREA FOR CRACKING AND PER
- [SDR DALA2025032402180](https://openairdocs.org/sdr/DALA2025032402180.md): Frame · none · Mar 21, 2025 · N375DA · Boeing 737832 · Standard Practices/Structures
  > (LOG 0870000) THIS WORK CARD INSTALLS A NEW SHIM BETWEEN THE RIGHT SIDE OF STA 727 FRAME INNER CHORD AND S-18A WEB. AD 2023-06-15 REQUIRES INSPECTING THE STA 727 FRAME INNER CHORD AT STRINGERS S-18A FOR EXISTING REPAIRS, INSPECTING THE AREA FOR CRACKING. AND P
- [SDR DALA2025020400866](https://openairdocs.org/sdr/DALA2025020400866.md): Skin · corroded · Jan 31, 2025 · N375DA · Boeing 737832 · Fuselage Main, Plate/Skin
  > (LOG 6976703) CORROSION FOUND AT STA 1016 STR 21L & 22L. PERFORMED CUTOUT OF DAMAGED AREA, LOCATED AND DRILLED FABRICATED REPAIR PART. ALL PARTS ALODINED AND PRIMER APPLIED IAW 737 SRM 53-70-01.(2422056) C/W HFEC & LFEC IAW B737SRM 53-70-01-2R PROCEDURE 4. INS
- [SDR DALA2024052805550](https://openairdocs.org/sdr/DALA2024052805550.md): Warning Message · false activation · May 25, 2024 · N375DA · Boeing 737832 · Leading Edge Slat Position Indicating System
  > SHIP 3705 -UFC- PERFORMED GO AROUND DUE TO TRAILING EDGE FLAP ASYMMETRY ON APPROACH AT FLAPS 25. CORRECTIVE ACTION: PERFORMED FSEU BITE CHECK. NO FAULTS. PERFORMED OPERATIONAL TEST OF TRAILING EDGE FLAPS. ALL TESTS PASS. FLAPS OPS CHECK GOOD.
- [SDR DALA2023051203791](https://openairdocs.org/sdr/DALA2023051203791.md): Unknown · unknown · May 10, 2023 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 4031418) DURING INSPECTION CRACK WAS FOUND IN THE FAILSAFE STRAP AT FRAME STA 663.75. REPAIRED ON N/R CARD 1 PER ERA 607703-14AD REV ORIG.
- [SDR DALA2023050803554](https://openairdocs.org/sdr/DALA2023050803554.md): Unknown · unknown · May 5, 2023 · N375DA · Boeing 737832 · Fuselage Main, Plate/Skin
  > (LOG 2753206) WHILE REMOVING AND REPLACING THE LH STA 663.75 PICKLE FORK FITTING TOOLING DAMAGE OCCURRED TO THE CENTER WING REAR SPAR WEB (111A1101-2) AND THE REAR SPAR TERMINAL FITTING (112A1511-201) AT THE HOLE COMMON TO THE OUTBOARD BOTTOM MOST FASTENER OF
- [SDR DALA2023050803553](https://openairdocs.org/sdr/DALA2023050803553.md): Unknown · unknown · May 5, 2023 · N375DA · Boeing 737832 · Fuselage Main, Plate/Skin
  > (LOG 2753155) DURING INSPECTIONS FOR CRACKING OF THE FS663 PICKLE FORK FITTINGS PER EM 5300-01157, MAINTENANCE FOUND A CRACK ON THE FAILSAFE STRAP COMMON TO THE LH FS663 PICKLE FORK FITTING. MAINTENANCE REPAIRED CRACK PER ERA 607710-14AD.
- [SDR DALA2023050503504](https://openairdocs.org/sdr/DALA2023050503504.md): Unknown · unknown · May 3, 2023 · N375DA · Boeing 737832 · Fuselage Structure (General)
  > (LOG 2749886) DURING INSPECTIONS FOR CRACKING OF THE FS663 PICKLE FORK FITTINGS PER EM 5300-01157, MAINTENANCE FOUND A CRACK ON THE FAILSAFE STRAP (P/N: 225A3523-3) COMMON TO THE LH FS663 PICKLE FORK FITTING. MAINTENANCE REPAIRED DAMAGE PER ERA 607842-14AD.
- [SDR DALA2023050503503](https://openairdocs.org/sdr/DALA2023050503503.md): Unknown · unknown · May 3, 2023 · N375DA · Boeing 737832 · Fuselage Structure (General)
  > (LOG 2749844) DURING INSPECTIONS FOR CRACKING OF THE FS663 PICKLE FORK FITTINGS PER EM 5300-01157, MAINTENANCE FOUND A CRACK ON THE FAILSAFE STRAP (P/N: 144A2412-3) COMMON TO THE LH FS663 PICKLE FORK FITTING. MAINTENANCE REPAIRED CRACK PER ERA 607711-14AD.
- [SDR DALA2023050503497](https://openairdocs.org/sdr/DALA2023050503497.md): Unknown · unknown · May 2, 2023 · N375DA · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 2748441) DURING INSPECTIONS FOR CRACKING OF THE FS663 PICKLE FORK FITTINGS PER EM 5300-01157, MAINTENANCE FOUND A CRACK IN THE FAILSAFE STRAP (P/N: 225A3523-3) COMMON TO THE LH FS663 PICKLE FORK FITTING. CRACK REPAIRED PER ERA 607841-14AD.
- [SDR DALA2022122308317](https://openairdocs.org/sdr/DALA2022122308317.md): Frame · cracked · Dec 21, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > DURING INSPECTION FOUND A CRACK AT FRAME BS 727B STRINGER 1, WHILE INSTALLING FASTENER. COMPLIED WITH ERA 604528-14 REV. ORIGINAL.
- [SDR DALA2022120607857](https://openairdocs.org/sdr/DALA2022120607857.md): Control Unit · inoperative · Dec 3, 2022 · N375DA · Boeing 737832 · Emergency Equipment
  > ATB/DE - DUE TO ELEC LIGHT AND LOSS OF STANDBY POWER. REPLACED STANDBY PWR CONTROL UNIT & #3 TR UNIT. INSPECTED CIRCUIT BREAKER PANELS FOR DEFECTS AND ODOR. PERFORMED POWER CHECKS. OPS CHECKED GOOD AND RTS.
- [SDR DALA2022090906014](https://openairdocs.org/sdr/DALA2022090906014.md): None · none · Sep 8, 2022 · N375DA · Boeing 737832 · Passenger/Crew Doors
  > (LOG 8938126) DURING INSPECTION FOUND DOOR 1 RIGHT ASSIST HANDLE TO OPEN, CLOSE DOOR IS BROKEN. REPLACED DOOR ASSIST BUNDLE PER B737 AMM 52-11.
- [SDR DALA2022072505098](https://openairdocs.org/sdr/DALA2022072505098.md): Brake Assy · fire · Jul 21, 2022 · N375DA · Boeing 737832 · Landing Gear Brake System
  > SHIP 3705 -BRAKE/FIRE- #2 BRAKE FIRE DISCOVERED BY MAINTENANCE DURING WALK AROUND. SELF-EXTINGUISHED. CORRECTIVE ACTION: REPLACED #2 BRAKE AND WHEEL ASSEMBLY. PERFORMED AXLE BOROSCOPE. NO TROUBLE FOUND.
- [SDR DALA2022070104600](https://openairdocs.org/sdr/DALA2022070104600.md): None · none · Jul 1, 2022 · N375DA · Boeing 737832 · Fuselage Floor Panel
  > (LOG 2301474) DURING INSPECTION FOUND CORROSION ON FLOOR SUPPOR FROM STA 787 TO STA 827 ABOVE STRINGER 26RH AT AFT CARGO COMPARTMENT. FLOOR SUPPORT FROM STA 787 TO STA 827 ABOVE STRINGER 26RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2022070104604](https://openairdocs.org/sdr/DALA2022070104604.md): None · none · Jun 30, 2022 · N375DA · Boeing 737832 · Fuselage, Seat/Cargo Attach Fittings
  > (LOG 2300560) DURING INSPECTION FOUND DAMAGE T: BROKEN ON SEAT TRACK CROWN ON LBL 24.75 BTW STA 727 H AND 727 I. AT PASSENGER CABIN. SEAT TRACK ON LBL 24.75 BTW STA 727 H AND 727 I. AT PASSENGER CABIN WAS REPAIRED PER B737-800 SRM 53-00-52-2R PROCEDURE 5, REPA
- [SDR DALA2022063004551](https://openairdocs.org/sdr/DALA2022063004551.md): Power Supply · inoperative · Jun 29, 2022 · N375DA · Boeing 737832 · Emergency Lighting
  > (LOG 2298173) REMOVE POWER SUPPLY P/N: D717-02-001 FROM A/C 3705 TO BE INSTALLED ON A/C 3701 TO ATTEND NRC 00878,THEN INSTALL SERVICEABLE PART ON A/C 3705. EMERGENCY POWER SUPPLY WAS REPLACED PER B-737/800 AMM 33-51, OPS SATISFACTORY TEST.
- [SDR DALA2022063004550](https://openairdocs.org/sdr/DALA2022063004550.md): Power Supply · inoperative · Jun 28, 2022 · N375DA · Boeing 737832 · Emergency Lighting
  > (LOG 2298067) DURING FUNCTIONAL CHECK - EMERGENCY LIGHTING, POWER SUPPLY DOES NOT CHARGE BATTERY PACK. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY.
- [SDR DALA2022063004549](https://openairdocs.org/sdr/DALA2022063004549.md): None · none · Jun 28, 2022 · N375DA · Boeing 737832 · Aerodynamic Fairings
  > (LOG 2296821) DURING INSPECTION WEAR PANEL SUPPORT STRUCTURE P/N 149A7593 -WAS FOUND. PANEL SUPPORT STRUCTURE P/N 149A7593 WAS REPAIRED PER ERA 599812-14AD REV. ORIGINAL.
- [SDR DALA2022063004548](https://openairdocs.org/sdr/DALA2022063004548.md): Light · inoperative · Jun 27, 2022 · N375DA · Boeing 737832 · Emergency Lighting
  > (LOG 2296128) DURING INSPECTION EMER RH LIGHT (RIGHT STA 627.5) WAS FOUND BURNT. LIGHT ASSEMBLY WAS REPLACED PER B737-800 AMM 33-51-01. OPS TEST OK.
- [SDR DALA2022062704491](https://openairdocs.org/sdr/DALA2022062704491.md): Skin · cracked · Jun 25, 2022 · N375DA · Boeing 737832 · Passenger/Crew Doors
  > (LOG 2293419) DURING INSPECTION FOUND CRACK ON INTERNAL CUTOUT OF LOWER INTERNAL SKIN IN AFT ENTRY DOOR (L-2) AT 5 INCH LOWER EDGE AND 8 INCH FROM AFT EDGE. DAMAGE ON INTERNAL CUTOUT OF LOWER INTERNAL SKIN IN AFT ENTRY DOOR (L-2) AT 5 INCH LOWER EDGE AND 8 INC
- [SDR DALA2022062704489](https://openairdocs.org/sdr/DALA2022062704489.md): Frame · cracked · Jun 23, 2022 · N375DA · Boeing 737832 · Passenger/Crew Doors
  > (LOG 2289915) DURING INSPECTION FOUND CRACK FWD SIDE FRAME SKIN AT FWD ENTRY DOOR L1. FWD SIDE FRAME SKIN AT FWD ENTRY DOOR L1 WAS REPAIRED PER ER/A: 599957-14.
- [SDR DALA2022062404455](https://openairdocs.org/sdr/DALA2022062404455.md): Plate · out of limits · Jun 23, 2022 · N375DA · Boeing 737832 · Fuselage Floor Panel
  > (LOG 2290830) DURING INSPECTION FOUND LH FLOOR SUPPORT SCREW HOLES (ABOVE STRINGER 25LH/RH) BETWEEN STA 400 AND 500I OF FORWARD CARGO COMPARTMENT FLOOR STRUCTURE WITH ORIGINAL THICKNESS = 0.040" AND REMAINING THICKNESS ON STATIONS BOTH SIDES (LH/RH) ON STA 500
- [SDR DALA2022062704488](https://openairdocs.org/sdr/DALA2022062704488.md): Frame · cracked · Jun 22, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2288381) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 867 BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 867 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.
- [SDR DALA2022062704487](https://openairdocs.org/sdr/DALA2022062704487.md): Stringer · corroded · Jun 21, 2022 · N375DA · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 2288374) DURING INSPECTION FOUND CORROSION ON STRINGER RBL 3 BTW STA 767 TO STA 687 AY AFT CARGO COMPARTMENT. RH SIDE CHANNEL SPLICE WAS REPLACED PER B737-800 SRM 53-00-53-2R REPAIR 2.
- [SDR DALA2022062404454](https://openairdocs.org/sdr/DALA2022062404454.md): Frame · cracked · Jun 21, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2288188) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 500D BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 500D BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.
- [SDR DALA2022062404453](https://openairdocs.org/sdr/DALA2022062404453.md): Frame · cracked · Jun 21, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2288177) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 827 BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 727 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.
- [SDR DALA2022062404452](https://openairdocs.org/sdr/DALA2022062404452.md): Frame · cracked · Jun 21, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2288161) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 727B BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 727B BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.
- [SDR DALA2022062404451](https://openairdocs.org/sdr/DALA2022062404451.md): Frame · cracked · Jun 21, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2288152) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 500C BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 500C BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.
- [SDR DALA2022062404450](https://openairdocs.org/sdr/DALA2022062404450.md): Frame · cracked · Jun 21, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2288043) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 500A BTW S-8 AND S-9. AD. CRACKS ON LH FUSELAGE FRAME STA 500 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.
- [SDR DALA2022062404449](https://openairdocs.org/sdr/DALA2022062404449.md): Frame · cracked · Jun 21, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2288030) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 480 BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 480 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.
- [SDR DALA2022062404448](https://openairdocs.org/sdr/DALA2022062404448.md): Frame · cracked · Jun 21, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2288018) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 440 BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 440 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.
- [SDR DALA2022062404447](https://openairdocs.org/sdr/DALA2022062404447.md): Frame · cracked · Jun 21, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2288000) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 400 BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 400 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.
- [SDR DALA2022062404446](https://openairdocs.org/sdr/DALA2022062404446.md): Frame · cracked · Jun 21, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2287988) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 380 BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 380 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.
- [SDR DALA2022062404445](https://openairdocs.org/sdr/DALA2022062404445.md): Plate · corroded · Jun 21, 2022 · N375DA · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 2287380) DURING INSPECTION FOUND OUT OF LIMITS RH SIDE PLATE IN STA 727 TO 767 AT AFT CARGO COMPARTMENT. RH SIDE PLATE IN STA 727 TO 767 AT AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2022062304386](https://openairdocs.org/sdr/DALA2022062304386.md): Trim Panel · corroded · Jun 20, 2022 · N375DA · Boeing 737832 · Buffet/Galleys
  > (LOG 2286144) DURING INSPECTION FOUND CORROSION IN TRIMS IN THE ACCESSES A417 AND A423 AT GALLEY 4. TRIMS IN THE ACCESSES A417 AND A423 AT GALLEY 4 WERE REPLACED PER PRI 600184-14 REV. 0 AND ERA 600184-14 REV. ORIGINAL.
- [SDR DALA2022062304384](https://openairdocs.org/sdr/DALA2022062304384.md): Frame · cracked · Jun 20, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2286321) DURING INSPECTION FOUND CRACKS ON RH FUSELAGE FRAME STA 440 BTW S-8 AND S-9 (INBD FASTENER HOLE OF SUPPORT BRACKET. CRACKS ON RH FUSELAGE FRAME STA 440 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-04B.
- [SDR DALA2022062304383](https://openairdocs.org/sdr/DALA2022062304383.md): Seat Track · corroded · Jun 20, 2022 · N375DA · Boeing 737832 · Fuselage, Seat/Cargo Attach Fittings
  > (LOG 2286294) DURING INSPECTION FOUND CORROSION OUT OF LIMITS SEAT TRACKS STA 727+17 OUTBD RH SIDE SEAT TRACK. SEAT TRACKS STA 727+17 OUTBD RH SIDE SEAT TRACK WAS REPAIRED PER B737-800 SRM 53-00-52-2R PROCEDURE 5.
- [SDR DALA2022062304382](https://openairdocs.org/sdr/DALA2022062304382.md): Frame · cracked · Jun 20, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2286284) DURING INSPECTION FOUND CRACKS ON RH FUSELAGE FRAME STA 480 BTW S-8 AND S-9 (INBD & OUTBD FASTENER HOLES OF SUPPORT BRACKET. CRACKS ON RH FUSELAGE FRAME STA 480 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-04B.
- [SDR DALA2022062304381](https://openairdocs.org/sdr/DALA2022062304381.md): Frame · cracked · Jun 20, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2286216) DURING INSPECTION FOUND CRACK ON RH FUSELAGE FRAME STA 500F BTW S-8 AND S-9 (INBD FASTENER HOLE OF SUPPORT BRACKET. CRACKS ON RH FUSELAGE FRAME STA 500F BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02B.
- [SDR DALA2022062304380](https://openairdocs.org/sdr/DALA2022062304380.md): Frame · cracked · Jun 20, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2286207) DURING INSPECTION FOUND CRACKS ON RH FUSELAGE FRAME STA 400 BTW S-8 AND S-9 (INBD FASTENER HOLE OF SUPPORT BRACKET. CRACKS ON RH FUSELAGE FRAME STA 400 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02B.
- [SDR DALA2022062304379](https://openairdocs.org/sdr/DALA2022062304379.md): Frame · cracked · Jun 20, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2286195) DURING INSPECTION FOUND CRACK ON RH FUSELAGE FRAME STA 827 BTW S-8 AND S-9 (INBD FASTENER HOLE OF SUPPORT BRACKET. CRACKS ON RH FUSELAGE FRAME STA 827 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02B.
- [SDR DALA2022062304378](https://openairdocs.org/sdr/DALA2022062304378.md): Frame · cracked · Jun 20, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2286174) DURING INSPECTION FOUND CRACK ON RH FUSELAGE FRAME STA 727B BTW S-8 AND S-9 (INBD FASTENER HOLE OF SUPPORT BRACKET). CRACKS ON RH FUSELAGE FRAME STA 727B BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02B.
- [SDR DALA2022062304377](https://openairdocs.org/sdr/DALA2022062304377.md): Frame · cracked · Jun 20, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2286166) DURING INSPECTION FOUND CRACKS ON RH FUSELAGE FRAME STA 500C BTW S-8 AND S-9 (INBD & OUTBD FASTENER HOLES OF SUPPORT BRACKET. CRACKS ON RH FUSELAGE FRAME STA 500C BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02B.
- [SDR DALA2022062304376](https://openairdocs.org/sdr/DALA2022062304376.md): Frame · cracked · Jun 20, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2286136) DURING INSPECTION FOUND CRACK ON RH FUSELAGE FRAME STA 500H BTW S-8 AND S-9 (INBD FASTENER HOLE OF SUPPORT BRACKET). CRACKS ON RH FUSELAGE FRAME STA 500H BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02B.
- [SDR DALA2022062304375](https://openairdocs.org/sdr/DALA2022062304375.md): Frame · cracked · Jun 20, 2022 · N375DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2286104) DURING INSPECTION FOUND CRACKS ON RH FUSELAGE FRAME STA 500A BTW S-8 AND S-9 (INBD & OUTBD FASTENER HOLES OF SUPPORT BRACKET. CRACKS ON RH FUSELAGE FRAME STA 500A BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02B.

Next page: https://openairdocs.org/aircraft/N375DA/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 = 'N375DA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N375DA/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.