# Service difficulty reports: N372DA

A list on [N372DA](https://openairdocs.org/aircraft/N372DA.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 · 149 reports

- [SDR DALA2026071004060](https://openairdocs.org/sdr/DALA2026071004060.md): Battery Pack · defective · Jul 10, 2026 · N372DA · Boeing 737832 · Emergency Lighting
  > FOUND ON SVC, EMERGENCY PATH LIGHTING INOP AT SEATS 11-15. REMOVED & REPLACED DEFECTIVE BATTERY PACK (M1676) IAW AMM 33-51 CHECKS NORMAL. (8722117) AIRCRAFT WAS GROUNDED
- [SDR DALA2026070603931](https://openairdocs.org/sdr/DALA2026070603931.md): Oil System · leaking · Jul 2, 2026 · N372DA · Boeing 737832 · APU Oil System
  > APU, PRIOR TO PUSH BACK WITH PACKS ON. A SMELL OF SMOKE ACCOMPANIED WITH A BANGING NOISE IT TAIL. AND VISIBLE SMOKE OBSERVCED BY GROUND CREW. NO ABNORAMAL INDICATIONS IN FLIGHT DECK.: R & R RECIRCULATION AIR FILTERS IAW AMM 21-25. REMOVED AND REPLACED APU, P
- [SDR DALA2025041102817](https://openairdocs.org/sdr/DALA2025041102817.md): Heater · failed · Apr 7, 2025 · N372DA · Boeing 737832 · Heating System
  > (6521792) UPON ENTERING A/C A BURNING ELECTRICAL SMELL WAS DETECTED IN FORWARD GALLEY & FLIGHT DECK. FWD F/A HEATER HAD AN ELECTRICAL SMELL, FWD HEATER TO MEL 21-00-41A.
- [SDR DALA2025040702649](https://openairdocs.org/sdr/DALA2025040702649.md): Shim · installed · Apr 3, 2025 · N372DA · Boeing 737832 · Standard Practices/Structures
  > (LOG 0893520) THIS WORK CARD INSTALLS A NEW SHIM BETWEEN THE RIGHT HAND SIDE OF STA 727 FRAME INNER CHORD AND S-18A WEB. AD 2023-06-15, REQUIRES INSPECTING THE STA 727 FRAME INNER CHORD AT STRINGER S- 18A FOR EXISITNG REPAIRS, INSPECTING THE AREA FOR CRACKING,
- [SDR DALA2025040302550](https://openairdocs.org/sdr/DALA2025040302550.md): Shim · installed · Apr 1, 2025 · N372DA · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0890027) 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 STRINGER S-18A FOR EXISTING REPAIRS, INSPECTING THE AREA FOR CRACKING, AND PER
- [SDR DALA2025040202492](https://openairdocs.org/sdr/DALA2025040202492.md): Skin · damaged · Mar 24, 2025 · N372DA · Boeing 737832 · Fuselage Main, Plate/Skin
  > (LOG 6521776) DURING WALK AROUND FOUND SKIN DAMAGE CORROSION AT VACUUM WASTE CUTOUT 6 O'CLOCK POSITION. ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE SKIN AT STA 917 BETWEEN STR 21L & STR 22L AROUND LAV DUCT VENT NOZZLE ASSY PER DELTA ER/A 625307-14 AND B737-800 S
- [SDR DALA2024121211683](https://openairdocs.org/sdr/DALA2024121211683.md): A/C Pack · odor · Dec 11, 2024 · N372DA · Boeing 737832 · Cabin Cooling System
  > (LOG 6597901) AT GATE WITH APU ONLINE SMELLED AN ODD ODOR THEN THE LEFT PACK LIGHT ILLUMINATED. REPLACED RIGHT PACK ACM IAW B737 AMM 21-51. REPLACED PRIMARY AND SECONDARY HEAT EXCHANGER IAW B737 AMM 21-51. R/R BOTH LEFT AND RIGHT RECIRCULATION AIR FILTER IAW B
- [SDR DALA2024101810185](https://openairdocs.org/sdr/DALA2024101810185.md): Acm · odor · Oct 18, 2024 · N372DA · Boeing 737832 · Cabin Cooling System
  > (LOG 6702420) ON FINAL DESCENT/ APPROACH A DIRTY SOCK SMELL WAS IN THE FLIGHT DECK AS WELL AS BOTH GALLEYS. R/R RT PACK ACM PER B737 AMM 21-51. R/R RECIRC FILTER PER B737 AMM 21-25. PERFORMED ENGINE RUN OF BOTH ENGINES WITH PACKS AT FULL HOT AND FULL COLD AND
- [SDR DALA2024092609450](https://openairdocs.org/sdr/DALA2024092609450.md): Unknown · unknown · Sep 23, 2024 · N372DA · Boeing 737832 · Wing Structure
  > (LOG 0572417) WHILE PERFORMING THE SPLIT SCIMITAR INSTALLATION ON A/C 3702, DELTA WORK CARD 5732-01015-01A-07, STEP 23 (APB TASK CARD 737-8340-11 REV E, OPERATION 240), THERE WAS AN INTERFERENCE ISSUE WITH THE L-8 STRAPS AT RIB 22 ON THE LEFT WING.
- [SDR DALA2024042504704](https://openairdocs.org/sdr/DALA2024042504704.md): Sensor · inoperative · Apr 21, 2024 · N372DA · Boeing 737832 · Fuel Indicating System
  > SHIP 3702 -DIV- TO CLT DUE TO CENTER TANK FUEL UNUSABLE. CORRECTIVE ACTION: MEL APPLIED. A/C WING TANKS FUELED FOR CONTINUED FLIGHT TO ATL. MAINTENANCE REPLACED RIGHT UFI WDM 28-23 AND REPLACED CENTER PUMP UFI PER AMM 28-22.
- [SDR DALA2024041804540](https://openairdocs.org/sdr/DALA2024041804540.md): None · none · Apr 11, 2024 · N372DA · Boeing 737832 · Standard Practices/Structures
  > (LOG 0288534) ACCOMPLISHED VA 100467MA REV IR IN CONJUNCTION WITH AA 2530-01595
- [SDR DALA2024041804541](https://openairdocs.org/sdr/DALA2024041804541.md): None · none · Apr 1, 2024 · N372DA · Boeing 737832 · Standard Practices/Structures
  > (LOG 0273070) ACCOMPLISHED VA 94701MA REV IR IN CONJUNCTION WITH AA 2540-01414.
- [SDR DALA2022101406645](https://openairdocs.org/sdr/DALA2022101406645.md): None · none · Oct 13, 2022 · N372DA · Boeing 737832 · Air Conditioning System
  > (LOG 2449594) FUMES IN ENTIRE AIRCRAFT DURING MULTIPLE PHASES OF FLIGHT. NO ODOR PRESENT IN A/C. PERF IDLE ENG RUN PER B737 AMM 71-00 WITH PACKS RUNNING, NO ODOR DETECTED. R/R LH & RH RECIRCULATION AIRFILTER IAW B737 AMM 25-25-01.
- [SDR DALA2022101206572](https://openairdocs.org/sdr/DALA2022101206572.md): None · none · Oct 8, 2022 · N372DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2443108) DURING INSPECTION FOUND CRACK WAS NOTED IN LH WINDOW FRAME NO 1 AT TOP OF INSPECTION AREA JUST BELOW UPPER RADIUS. CRACK EXTENDS FROM AFT EDGE OF FRAME APPROX. 1 INCH FWD. REPAIR COMPLIED WITH PER ERA 602196-14AD REV A.
- [SDR DALA2022101006533](https://openairdocs.org/sdr/DALA2022101006533.md): None · none · Sep 11, 2022 · N372DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 8268586) DURING INSPECTION FOUND DAMAGE TO THE UPPER CORNER OF THE LH NO1 FLIGHT DECK WINDOW VERTICAL STANCHIEN. PERMANENT REPAIR COMPLETED / L-1 FLIGHT DECK WINDOW / FRAME / REPLACEMENT / PER ERA 602196-14 REV. ORIG.
- [SDR DALA2022080305354](https://openairdocs.org/sdr/DALA2022080305354.md): Wire · broken · Aug 2, 2022 · N372DA · Boeing 737832 · Emergency Lighting
  > (LOG 8707225) DURING INSPECTION FOUND RH EMERGENCY LIGHT, ON ROW 17 INOP. REPAIRED ELECTRICAL WIRE AND CABLE PER B737-80 SWPM 20-10-13. OPS CHECK OK.
- [SDR DALA2022080305349](https://openairdocs.org/sdr/DALA2022080305349.md): None · none · Aug 1, 2022 · N372DA · Boeing 737832 · Cargo/Baggage Doors
  > (LOG 2345377) DURING INSPECTION FOUND SEVERAL DENTS ON AFT CARGO DOOR EXTERNAL SKIN. EXTERNAL SKIN WAS REPLACED PER B 737-800 SRM 52-30-01-2R PROCEDURE 3, REPAIR 3.
- [SDR DALA2022080205302](https://openairdocs.org/sdr/DALA2022080205302.md): Skin · dented · Jul 30, 2022 · N372DA · Boeing 737832 · Cargo/Baggage Doors
  > (LOG 2343771) DURING INSPECTION FOUND SEVERAL DENTS ON FWD CARGO DOOR EXTERNAL SKIN. FWD CARGO DOOR EXTERNAL SKIN WAS REPLACED PER B737-800 SRM 52-30-01-2R PROCEDURE 3, REPAIR 3.
- [SDR DALA2022080205299](https://openairdocs.org/sdr/DALA2022080205299.md): Skin · corroded · Jul 30, 2022 · N372DA · Boeing 737832 · Fuselage Main, Plate/Skin
  > (LOG 2342763) DURING INSPECTION CORROSION WAS FOUND ON FUSELAGE SKIN STA 535 BTW RBL7 AND LBL 7. SKIN, KEEL BEAM DOUBLER AND BULKHEAD CHORD, STA 520 TO 540 & S-28L TO S28R WAS REPAIRED PER ER/A 600861-14.
- [SDR DALA2022080105262](https://openairdocs.org/sdr/DALA2022080105262.md): Skin · corroded · Jul 29, 2022 · N372DA · Boeing 737832 · Fuselage Main, Plate/Skin
  > (LOG 2341765) DURING INSPECTION FOUND FUSELAGE / SKIN, KEEL BEAM DOUBLER AND BULKHEAD CHORD, STA. 520 TO 540 & S-28L TO S-28R / CORROSION AND CRACKS. MAINTENANCE REPAIRED DAMAGE PER ERA 600861-14.
- [SDR DALA2022072805204](https://openairdocs.org/sdr/DALA2022072805204.md): None · none · Jul 26, 2022 · N372DA · Boeing 737832 · Fuselage Floor Panel
  > (LOG 2337893) DURING INSPECTION FOUND CORROSION ON BEAM FLOOR STRUCTURE BETWEEN 986.5 AND LBL 18 AND LBL 44. FLOOR STRUCTURE BEAM BETWEEN 986.5 AND LBL 50 AND RBL 50 WAS REPAIRED PER PRI 600481-14 REV 2 AND ERA 600481-14 REV ORIGINAL.
- [SDR DALA2022072505095](https://openairdocs.org/sdr/DALA2022072505095.md): Web · corroded · Jul 23, 2022 · N372DA · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 2332751) DURING INSPECTION FOUND CORROSION ON RH WEB BTWN STA 787/STA 847 AND RBL 20 AT AFT CARGO COMPARTMENT. WEB BTWN STA 787/STA 847 AND RBL 20 AT AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2022072505094](https://openairdocs.org/sdr/DALA2022072505094.md): None · none · Jul 22, 2022 · N372DA · Boeing 737832 · Aerodynamic Fairings
  > (LOG 2322583) DURING INSPECTION FOUND ELONGATED HOLES ON SUPPORT STRUCTURE STA Y=727 BTW RBL 20 AND LBL 20. HOLES ON SUPPORT STRUCTURE STA Y=727 BTW RBL 20 AND LBL 20 WERE REPAIRED PER PRI 600347-14 REV. 2 AND ERA 600347-14AD REV. ORIGINAL.
- [SDR DALA2022072505093](https://openairdocs.org/sdr/DALA2022072505093.md): None · none · Jul 21, 2022 · N372DA · Boeing 737832 · Fuselage Floor Panel
  > (LOG 2330719) AFTER CLEANING SLIDE ANCHOR ( 2EA) (L2, R2 POSITION) WAS FOUND WITH CORROSION. SLIDE ANCHOR (2EA) (L2,R2 POSITION) WERE REPLACED PER B737-800, IPC 11-32-01-03.
- [SDR DALA2022072205072](https://openairdocs.org/sdr/DALA2022072205072.md): None · none · Jul 20, 2022 · N372DA · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 2328915) DURING INSPECTION FOUND CORROSION ON STRINGER 26R, BTW STA 500H AND 500G AT FWD CARGO COMPARTMENT. STRINGER 26R BTW STA 500H AND 500G AT FWD CARGO COMPARTMENT WAS REPAIRED PER. B737-800 SRM. 53-00-03-2R PROCEDURE 1 REPAIR 1.
- [SDR DALA2022072205071](https://openairdocs.org/sdr/DALA2022072205071.md): Shield · corroded · Jul 19, 2022 · N372DA · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 2327689) DURING INSPECTION FOUND CORROSION ON RH SHIELD BTWN STA 767/STA 787 + 10 AND AT RBL= 20 AT AFT CARGO COMPARTMENT. RH SHIELD WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2022072205070](https://openairdocs.org/sdr/DALA2022072205070.md): None · none · Jul 19, 2022 · N372DA · Boeing 737832 · Fuselage Main, Plate/Skin
  > (LOG 2327628) DURING INSPECTION FOUND RIVET PLUG ON EXTERNAL FUS SKIN BTW STA 362.375 AND STGR 17L. PERMANENT REPAIR ON EXTERNAL FUS SKIN BTW STA 362.375 AND STGR 17L.WAS PERFORMED PER PRI 600313-14.
- [SDR DALA2022072005019](https://openairdocs.org/sdr/DALA2022072005019.md): Stringer · worn · Jul 19, 2022 · N372DA · Boeing 737832 · Fuselage Floor Panel
  > (LOG 2326725) DURING INSPECTION FOUND WEAR ON STA 787/STA 807 AND RBL= 3 AT AFT CARGO COMPARTMENT. STGR ON STA 787/STA 807 AND RBL= 3 AT AFT CARGO COMPARTMENT. WAS REPAIRED PER B737-800 SRM 53-00-53-2R PROCEDURE 2 REPAIR 2.
- [SDR DALA2022072005018](https://openairdocs.org/sdr/DALA2022072005018.md): Rail · worn · Jul 19, 2022 · N372DA · Boeing 737832 · Fuselage Floor Panel
  > (LOG 2326721) DURING INSPECTION FOUND WEAR ON FLOOR STRUCTURE RAIL BTW STA 767/STA 787 AND STA 787/STA 807 RBL8 AT AFT CARGO COMPARTMENT. FLOOR STRUCTURE RAIL BTW STA 767/STA 787 AND STA 787/STA 807 RBL8 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B737-800 SRM 5
- [SDR DALA2022072105053](https://openairdocs.org/sdr/DALA2022072105053.md): None · none · Jul 18, 2022 · N372DA · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 2326322) DURING INSPECTION FOUND CORROSION ON LH SIDE PLATE, BTW STA 418 TO 420 AND 500C TO 500D AT FWD CARGO COMPARTMENT. SIDE PLATE BTW STA 500A APPROX. TO 500D APPROX. AND SIDE PLATE BTW STA 400 TO STA 500+10 WERE REPLACED PER SRM 51-40-02-0G.
- [SDR DALA2022072005022](https://openairdocs.org/sdr/DALA2022072005022.md): Intercostal · corroded · Jul 18, 2022 · N372DA · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 2325147) DURING INSPECTION FOUND CORROSION ON INTERCOSTAL BELOW LH SIDE PLATE BTW STA 460 TO STA 480 AT FWD CARGO COMPARTMENT. INTERCOSTAL WAS REPLACED PER DWG 143A710 REV.C AND B737-800 SRM 51-40-02-0G.
- [SDR DALA2022072005017](https://openairdocs.org/sdr/DALA2022072005017.md): Intercostal · corroded · Jul 17, 2022 · N372DA · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 2325007) DURING INSPECTION FOUND CORROSION ON INTERCOSTAL BETWEEN STA500D-STA500E AND STGR25L-STGR26L, NOTED AFTER REMOVAL OF LH SIDE PLATE, FWD CARGO. CORROSION ON INTERCOSTAL BETWEEN STA500D-STA500E AND STGR25L-STGR26L WAS ATTENDED PER. B737-800 SRM. 51
- [SDR DALA2022072005016](https://openairdocs.org/sdr/DALA2022072005016.md): Intercostal · cracked · Jul 17, 2022 · N372DA · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 2323812) DURING INSPECTION FOUND CRACK ON INTERCOSTAL BELOW LH SIDE PLATE STA 460 AT FWD CARGO COMPARTMENT FLOOR STRUCTURE. INTERCOSTAL BELOW LH SIDE PLATE STA 460 AT FWD CARGO COMPARTMENT WAS REPLACED PER. B737-800 SRM 51-40-02-0G.
- [SDR DALA2022072005015](https://openairdocs.org/sdr/DALA2022072005015.md): Intercostal · corroded · Jul 16, 2022 · N372DA · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 2322462) DURING INSPECTION FOUND CORROSION ON INTERCOSTAL BETWEEN STA500C-STA500D AND STGR25L-STGR26L. INTERCOSTAL BETWEEN STA500C-STA500D AND STGR25L-STGR26L WAS REPLACED PER B737-800 SRM 51-40-05-0G AND DWG 147A7510 REV B.
- [SDR DALA2022071804949](https://openairdocs.org/sdr/DALA2022071804949.md): Intercostal · corroded · Jul 15, 2022 · N372DA · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 2321984) DURING INSPECTION FOUND CORROSION ON INTERCOSTAL BETWEEN STA500B-STA500C AND STGR25L-STGR26L, NOTED AFTER REMOVAL OF LH SIDE PLATE, FWD CARGO. INTERCOSTAL BETWEEN STA500B-STA500C AND STGR25L-STGR26L WAS REPLACED PER B737-800 SRM 51-40-05-0G AND D
- [SDR DALA2022071804948](https://openairdocs.org/sdr/DALA2022071804948.md): Intercostal · corroded · Jul 15, 2022 · N372DA · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 2321979) DURING INSPECTION FOUND CORROSION ON INTERCOSTAL BETWEEN STA500-STA500A AND STGR25L-STGR26L. CORROSION 2 INTERCOSTAL BETWEEN STA500-STA500A AND STGR25L-STGR26L WAS REPLACED PER B737-800 SRM 51-40-05-0G AND DWG 147A7510 REV B.
- [SDR DALA2022071804947](https://openairdocs.org/sdr/DALA2022071804947.md): Web · corroded · Jul 15, 2022 · N372DA · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 2321663) DURING INSPECTION FOUND CORROSION ON WEB (UPPER/ LOWER SURFACE), BTW STA 986 TO 1016 AND LBL36. CORROSION 2 WEB WAS REPLACED PER DWG 147A5712 SHEET 21 REV.- PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2022071804946](https://openairdocs.org/sdr/DALA2022071804946.md): Web · corroded · Jul 15, 2022 · N372DA · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 2321658) DURING INSPECTION FOUND CORROSION ON WEB (UPPER/ LOWER SURFACE), BTW STA 986 TO 1016 AND RBL36. LEVEL CORROSION 2 WEB WAS REPLACED PER DWG 147A5712 SHEET 21 REV.- PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2022071804945](https://openairdocs.org/sdr/DALA2022071804945.md): Floorbeam · corroded · Jul 15, 2022 · N372DA · Boeing 737832 · Fuselage Main, Floor Beam
  > (LOG 2321604) DURING INSPECTION FOUND CORROSION OUT OF LIMITS ON FLOORBEAM STA 344 BTW RBL 0 TO RBL 20. FLOORBEAM STA 344 BTW RBL 0 TO RBL 20 WAS REPAIRED PER B737-800 SRM 53-10-51-2R REPAIR 10.
- [SDR DALA2022071804944](https://openairdocs.org/sdr/DALA2022071804944.md): Plate · corroded · Jul 15, 2022 · N372DA · Boeing 737832 · Fuselage Floor Panel
  > (LOG 2321551) DURING INSPECTION FOUND CORROSION ON RH SIDE PLATE BTWN STA 727/STA 767 AND RBL= 21 AT AFT CARGO COMPARTMENT. SIDE PLATE BTWN STA 727/STA 767 AND RBL=21 AT AFT CARGO COMPARTMENT. WAS REPLACED PER B737-800, SRM 51-40-02-0G.
- [SDR DALA2022071504900](https://openairdocs.org/sdr/DALA2022071504900.md): None · none · Jul 14, 2022 · N372DA · Boeing 737832 · Fuselage Floor Panel
  > (LOG 2320279) DURING INSPECTION FOUND CORROSION ON FLOOR BEAM STA 947.5 RBL 5. FLOOR BEAM STA 947.5 RBL 5 WAS REPAIRED PER B-737-800 SRM 53-70-51-2R REPAIR 5.
- [SDR DALA2022071504899](https://openairdocs.org/sdr/DALA2022071504899.md): None · none · Jul 13, 2022 · N372DA · Boeing 737 · Aerodynamic Fairings
  > (LOG 2318632) DURING INSPECTION FOUND ELONGATED HOLES AND WEAR ON SETLEMENT AREA ON AFT EDGE AT ACCESS PANEL 193D. REPAIRED PER B737-800 S.R.M. 51-70-05-2R PROCEDURE REPAIR GENERAL, PER B737-800 S.R.M. 51-70-05-2R PROCEDURE 8 REPAIR 8 IN REFERENCE PER B737-80
- [SDR DALA2022071504897](https://openairdocs.org/sdr/DALA2022071504897.md): None · none · Jul 13, 2022 · N372DA · Boeing 737832 · Fuselage Floor Panel
  > (LOG 2318005) DURING INSPECTION FOUND CORROSION ON RH SIDE PLATE BTW STA 420 TO STA 500C RBL 24. AT FWD CARGO COMPARTMENT. SIDE PLATE RH SIDE BTW STA 420 TO STA 500C RBL 24. AT FWD CARGO COMPARTMENT WAS REPLACE PER. B737-800, SRM 51-40-02-0G.
- [SDR DALA2022071504896](https://openairdocs.org/sdr/DALA2022071504896.md): None · none · Jul 12, 2022 · N372DA · Boeing 737832 · Fuselage Floor Panel
  > (LOG 2317793) DURING INSPECTION FOUND CORROSION ON LH SIDE PLATE BTWN STA 727/STA 847 AND LBL= 21 AT AFT CARGO COMPARTMENT. LH SIDE PLATE BTWN STA 727/ STA 847 AND LBL= 21 AT AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2022071104819](https://openairdocs.org/sdr/DALA2022071104819.md): Frame · cracked · Jul 11, 2022 · N372DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2314989) DURING INSPECTION FOUND CRACK ON FRAME AT SUPPORT BRACKET INBD RIVET HOLE BTW STA 907 AND STRINGERS 8L - 9L. CRACK ON FRAME AT SUPPORT BRACKET INBD RIVET HOLE BTW STA 907 AND STRINGERS 8L - 9L WAS REPAIRED PER AMDS 2526-01236-03A.
- [SDR DALA2022071104818](https://openairdocs.org/sdr/DALA2022071104818.md): Intercostal · corroded · Jul 10, 2022 · N372DA · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 2313589) DURING INSPECTION FOUND CORROSION ON INTERCOSTAL, BTW LBL 51 AND STA 947 TO 967 AT PASSENGER CABIN. INTERCOSTAL, BTW LBL 51 AND STA 947 TO 967 AT PASSENGER CABIN WAS REPLACED AT NRC 00745.
- [SDR DALA2022071104817](https://openairdocs.org/sdr/DALA2022071104817.md): Floor Support · corroded · Jul 9, 2022 · N372DA · Boeing 737832 · Fuselage Floor Panel
  > (LOG 2313483) DURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT BTW FS: 951 AND LBL 27 TO LBL 50 AT PASSENGER CABIN. FLOOR SUPPORT WAS REPLACED AT NRC 00745.
- [SDR DALA2022070604694](https://openairdocs.org/sdr/DALA2022070604694.md): None · none · Jul 5, 2022 · N372DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2307613) DURING INSPECTION FOUND CRACK ON FRAME AT SUPPORT BRACKET INBD RIVET HOLE BTW STA 727B AND STRINGERS 8L - 9L. FRAME BTW STA 727B AND STRINGERS 8L - 9L WAS REPAIRED PER. A.A. AD. CARD 2526-01236-02A.
- [SDR DALA2022070604693](https://openairdocs.org/sdr/DALA2022070604693.md): None · none · Jul 5, 2022 · N372DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2307606) DURING INSPECTION FOUND CRACK ON FRAME AT SUPPORT BRACKET INBD RIVET HOLE BTW STA 500C AND STRINGERS 8L - 9L. FRAME BTW STA 500C AND STRINGERS 8L - 9L WAS REPAIRED PER. A.A. AD. CARD 2526-01236-02A.
- [SDR DALA2022070604692](https://openairdocs.org/sdr/DALA2022070604692.md): None · none · Jul 5, 2022 · N372DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 2307604) DURING INSPECTION FOUND CRACK ON FRAME AT SUPPORT BRACKET INBD RIVET HOLE BTW STA 827 AND STRINGERS 8L - 9L. FRAME BTW STA 827 AND STRINGERS 8L - 9L WAS REPAIRED PER. A.A. // AD. CARD 2526-01236-02A.

Next page: https://openairdocs.org/aircraft/N372DA/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 = 'N372DA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N372DA/reports

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