# Service difficulty reports: N398DA

A list on [N398DA](https://openairdocs.org/aircraft/N398DA.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 · 116 reports

- [SDR DALA2026082804882](https://openairdocs.org/sdr/DALA2026082804882.md): Bracket · damaged · Aug 27, 2026 · N398DA · Boeing 737832 · Passenger/Crew Doors
  > GIRT BAR BRACKETS DAMAGED, BRACKET THAT HOLDS GIRT BAR IN IS VERY LOOSE. BAR SLIPS IN AND OUT OF BRACKET WITH NO RESISTANCE AT ALL. ADJUSTED AFT RIGHT GIRT BAR BRACKET. (1780171) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026072204291](https://openairdocs.org/sdr/DALA2026072204291.md): Lamp · inoperative · Jul 18, 2026 · N398DA · Boeing 737832 · Emergency Lighting
  > ESCAPE PATH LIGHT AT ROW 31 INOP. RELAMPED, FOUND CONTACT SPLICE DAMAGED AT ROW 31. REPAIRED SPLICE IAW SWPM 20-30-12 PARAGRAPH 17. CHECKS GOOD. (8788657) AIRCRAFT WAS GROUNDED
- [SDR DALA2026070603932](https://openairdocs.org/sdr/DALA2026070603932.md): Battery Pack · inoperative · Jul 3, 2026 · N398DA · Boeing 737832 · Emergency Lighting
  > EMERGENCY LIGHTS OUT ROWS 10-14. R & R BATTERY PACK IAW AMM 33-51-06. (8788603) AIRCRAFT WAS GROUNDED
- [SDR DALA2025122909475](https://openairdocs.org/sdr/DALA2025122909475.md): Line · leaking · Dec 28, 2025 · N398DA · Boeing 737832 · Potable Water System
  > PRES/DE-THE CREW WAS UNABLE TO CONTROL PRESSURIZATION, PERFORMED AN EMERGENCY DESCENT. MAINTENANCE FOUND A WATER LEAK DIRECTLY ABOVE THE OUTFLOW VALVE RENDERING THE VALVE INOPERATIVE, REPLACED A POTABLE WATER LINE AND O-RING. WATER SYSTEM AND AUTO PRESSURIZA
- [SDR DALA2025120108753](https://openairdocs.org/sdr/DALA2025120108753.md): Sign · missing · Nov 26, 2025 · N398DA · Boeing 737832 · Emergency Lighting
  > EMERGENCY EXIT SIGN MISSING BY ROW 21. REPLACED EMERGENCY EXIT SIGN IAW B737 AMM 33-51. OK FOR SVC.
- [SDR DALA2025111808400](https://openairdocs.org/sdr/DALA2025111808400.md): Battery Pack · inoperative · Nov 17, 2025 · N398DA · Boeing 737832 · Emergency Lighting
  > WHILE OPS TESTING PRIOR BATTERY PACK FOR EMER LIGHTS, TWO DIFFERENT SECTIONS WENT OUT. REMOVED AND REPLACED M1695 AND M1670 EMERGENCY BATTERY PACKS REF B737 AMM 33-51.
- [SDR DALA2025111708372](https://openairdocs.org/sdr/DALA2025111708372.md): Battery Pack · no test · Nov 17, 2025 · N398DA · Boeing 737832 · Emergency Lighting
  > ON SVC CHECK, FWD ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. R & R THE EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51.
- [SDR DALA2025110508065](https://openairdocs.org/sdr/DALA2025110508065.md): Skin · damaged · Nov 3, 2025 · N398DA · Boeing 737832 · Fuselage Main, Plate/Skin
  > EXTERNAL POWER PANEL CUT OUT DAMAGED. REMOVED INTERNAL CRACK INTERCOSTAL IAW DWG 141A0640. C/W PRI 630191-14 REV ORIG PRI REV 0. ERA 630191-14 HAS BEEN CANCELLED AND NOW WORKING OUT OF THE SRM IAW SRM 53-10 -15-2R, PROCEDURE 5 REPAIR. REMOVED EXISTING FAST
- [SDR DALA2025103007956](https://openairdocs.org/sdr/DALA2025103007956.md): Transmission · faulted · Oct 24, 2025 · N398DA · Boeing 737832 · Trailing Edge Flap Actuator
  > UFC/DE- DECLARED EMERGENCY DUE TO TE FLAP ASYMMETRY. REPLACED NBR 2 FLAP TRANSMISSION, WFFA AND WFFB CONTROL CABLES. PERFORMED CONTROL CABLE TENSION, SAFETY, AND ADJUSTED FLAP. (LP 1268322, 1279340, 1279914)
- [SDR DALA2025081105971](https://openairdocs.org/sdr/DALA2025081105971.md): Elec Connector · damaged · Aug 8, 2025 · N398DA · Boeing 737832 · Light System Wiring
  > (LOG 7056962) SEAT 32 EXIT AISLE LIGHT INOP. REPLACED CONNECTOR ON PSU END IAW B737 SWPM 20-42-01 OP'S CHECKED GOOD.
- [SDR DALA2025071105239](https://openairdocs.org/sdr/DALA2025071105239.md): Battery Pack · no test · Jul 10, 2025 · N398DA · Boeing 737832 · Emergency Lighting
  > (LOG 7440154) DURING SERVICE CHECK FOUND EMERGENCY LIGHTS ON SEATS ROWS 24 AND BACK WERE INOP. REMOVED AND REPLACED BATTERY PACK POWER SUPPLY (M1672) PER B737 AMM 33-51. OPS CHECKS GOOD.
- [SDR DALA2025021001028](https://openairdocs.org/sdr/DALA2025021001028.md): Bulb · inoperative · Feb 10, 2025 · N398DA · Boeing 737832 · Emergency Lighting
  > (LOG 6760114) SEAT ROWS 23-33 FLOOR PROXIMITY ESCAPE PATH LIGHTING INOP. REMOVED AND REPLACED BULBS ON ROW 32, CHECKS GOOD. FOUND PULLED PIN ON ROW 33, INSTALLED PIN REF. B737 AMM 33-51. ALL ROWS CHECK GOOD.
- [SDR DALA2025020700983](https://openairdocs.org/sdr/DALA2025020700983.md): Battery · no test · Feb 7, 2025 · N398DA · Boeing 737832 · Emergency Lighting
  > (LOG 6388497) AFT RT EMERGENCY BATTERY FAILED CAP CHECK. REPLACED BATTERY PACK REF B737 AMM 33-51. OPS CHECK GOOD.
- [SDR DALA2024071207070](https://openairdocs.org/sdr/DALA2024071207070.md): Connector · disconnected · Jul 11, 2024 · N398DA · Boeing 737832 · Light System Wiring
  > (LOG 6167011) EMERG LIGHT AT 33 DEF INOP. T/S IAW B737 WDM 33-51. FOUND CONNECTION UNDER SEAT DISCONNECTED. RECONNECTED, OPS CHK GOOD.
- [SDR DALA2024071207069](https://openairdocs.org/sdr/DALA2024071207069.md): Lamp · inoperative · Jul 11, 2024 · N398DA · Boeing 737832 · Emergency Lighting
  > (LOG 6167010) EMERGENCY LIGHT AT 13 DEF MISSING. RELAMPED AND INSTALLED NEW LENS COVER ON EMERGENCY LIGHT SEAT #13 DEF. OPS CHK GOOD, IAW B737 AMM 33-51.
- [SDR DALA2024062706537](https://openairdocs.org/sdr/DALA2024062706537.md): Pressure Blkhd · cracked · Jun 24, 2024 · N398DA · Boeing 737832 · Fuselage Main, Bulkhead
  > (LOG 0411425) CRACKS (2 E/AS) ON VERTICAL PRESSURE WEB CENTER WING BOX REAR SPAR STA 663 BTW LBL 35.00 AND 45.64 AT W/W. REPAIRED PER B737-800 SRM 57-10-10-2R REPAIR 3 PAR. 5 & SRM 57-10-10-2R REPAIR 6.
- [SDR DALA2024062506477](https://openairdocs.org/sdr/DALA2024062506477.md): Retainer · cracked · Jun 23, 2024 · N398DA · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0409603) CRACK ON LH NO.1 WINDSHIELD RETAINER (LH UPPER CORNER) AT FWD FUSELAGE. CRACK ON LH NO.1 WINDSHIELD RETAINER (LH UPPER CORNER) AT FWD FUSELAGE WAS REPAIRED PER PRI 618217-14 REV 0 AND REV 1 AND ER/A 618217-14AD REV. ORIGINAL.
- [SDR DALA2024062106308](https://openairdocs.org/sdr/DALA2024062106308.md): Doubler · corroded · Jun 20, 2024 · N398DA · Boeing 737832 · Fuselage Main, Plate/Skin
  > (LOG 0403864) CORROSION ON INTERNAL PRODUCTION DOUBLER BS 757 AND BS 797 BTW STRINGER 27LH-27RH AT AFT CARGO COMPARTMENT. INTERNAL PRODUCTION DOUBLER BS 757 AND BS 797 BTW STRINGER 27LH-27RH AT AFT CARGO COMPARTMENT WERE REPAIRED PER ER/A 618489-14 REV. ORIGIN
- [SDR DALA2024062006257](https://openairdocs.org/sdr/DALA2024062006257.md): Skin · gouged · Jun 19, 2024 · N398DA · Boeing 737832 · Fuselage Main, Plate/Skin
  > (LOG 0402873) GOUGE ON SKIN BTW STA 360 AND STA 370. S-28R TO S-27R APPROX AT EXTERNAL FUSELAGE. SKIN BTW STA 360 AND STA 370. S-28R TO S-27R APPROX AT EXTERNAL FUSELAGE WAS REPAIRED PER ERA 618224-14.
- [SDR DALA2024062006254](https://openairdocs.org/sdr/DALA2024062006254.md): Access Panel · corroded · Jun 18, 2024 · N398DA · Boeing 737832 · Buffet/Galleys
  > (LOG 0400834) CORROSION ON ACCESS PANELS OF GALLEY 4. ACCESS PANELS OF GALLEY 4 (2EAS) PN: 9354078-7 AND PN: 9354078-8 WAS FABRICATED AND INSTALLED PER ER/A NO. 618835-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR AND PRI ER/A 618835-14 REV 0.
- [SDR DALA2024062006253](https://openairdocs.org/sdr/DALA2024062006253.md): Floorbeam · cracked · Jun 18, 2024 · N398DA · Boeing 737832 · Fuselage Main, Floor Beam
  > (LOG 0400936) CORROSION ON FLOOR SUPPORT ANGLE BTW STA 277 AND LBL-10 TO RBL-10 AT COCKPIT. FLOOR SUPPORT ANGLE BTW STA 277 AND LBL-10 TO RBL-10 WAS REPAIRED PER ERA 618349-14.
- [SDR DALA2024061806183](https://openairdocs.org/sdr/DALA2024061806183.md): Access Door · corroded · Jun 14, 2024 · N398DA · Boeing 737832 · Buffet/Galleys
  > (LOG 0393878) CORROSION ON TRIM UNDER OF THE DOOR ACCESS A417 (1EA) AND A423 (1EA) AT GALLEY 4. CORRODED TRIMS UNDER OF THE DOOR ACCESS A417 (1EA) AND A423 (1EA) AT GALLEY 4 WERE REPLACED BY MANUFACTERED TRIMS (2 EAS) PER PRI 618436-14 REV. 0, PRI 618436-14 RE
- [SDR DALA2024061706142](https://openairdocs.org/sdr/DALA2024061706142.md): Window Frame · cracked · Jun 11, 2024 · N398DA · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0388387) FUSELAGE OPENING FRAME LH NO. 1 WINDOW FRAME UPPER CORNER CRACKED. REPAIRED CRACK PER ERA 618217-14.
- [SDR DALA2024061406085](https://openairdocs.org/sdr/DALA2024061406085.md): Stiffener · cracked · Jun 11, 2024 · N398DA · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0387578) CRACK STIFFENER STA 540 RBL=6 THROUGH ACCESS PANEL 192E AT LOWER FUSELAGE. STIFFENER STA 540 RBL=6 THROUGH ACCESS PANEL 192E AT LOWER FUSELAGE WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2024061005935](https://openairdocs.org/sdr/DALA2024061005935.md): Channel · corroded · Jun 8, 2024 · N398DA · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0383629) CORROSION ON INNER ZEE CHORD OF DOOR L2 LOWER SILL AREA BTW STA 930-992 AT PAX CABIN. INNER ZEE CHORD OF DOOR L2 LOWER SILL AREA BTW STA 930-992 WAS REPLACED PER B737-800 SRM 51-40-02-0G PARA 4 (B) AND 51-40-02-0G PARA 7 (C) AND 51-40-2-0G.
- [SDR DALA2024061005933](https://openairdocs.org/sdr/DALA2024061005933.md): Floorbeam · corroded · Jun 8, 2024 · N398DA · Boeing 737832 · Fuselage Main, Floor Beam
  > (LOG 0383359) CORROSION ON FLOOR SUPPORTS BTW STA 992 AND LBL=35-45, ALSO 2EAS BTW STA 992-1016 AND RBL=35-45. FLOOR SUPPORTS BTW STA 992 AND LBL=35-45, ALSO 2EAS BTW STA 992-1016 AND RBL=35-45 WERE FABRICATED AND REPLACED PER DWG 147A5710 REV 0 AND DWG 147A57
- [SDR DALA2024061005930](https://openairdocs.org/sdr/DALA2024061005930.md): Plate · corroded · Jun 8, 2024 · N398DA · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0382476) CORROSION ON SIDE PLATES RH BTW STA 500A AND STA 500 I AT FWD CARGO COMPARTMENT. SIDE PLATES RH BTW STA 500A AND STA 500 I WAS REPAIRED B737-800 SRM 53-00-53-2R REPAIR 5.
- [SDR DALA2024061005929](https://openairdocs.org/sdr/DALA2024061005929.md): Door Sill · corroded · Jun 8, 2024 · N398DA · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0382460) CORROSION ON INNER ZEE CHORD OF DOOR R2 LOWER SILL AREA BTW STA 930-992 AT PAX CABIN. INNER ZEE CHORD OF DOOR R2 LOWER SILL AREA BTW STA 930-992 WAS REPLACED PER B737-800 SRM 51-40-02-0G PARA 4 (B) AND 51-40-02-0G PARA 7 (C) AND 51-40-02-0G.
- [SDR DALA2024061005928](https://openairdocs.org/sdr/DALA2024061005928.md): Frame · cracked · Jun 7, 2024 · N398DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 0382144) FRAME AT A/C RAIL BRACKETS - INSP/MOD; SEC. 01. ON STA=500C BTW S8R AND S9R AT PAX CABIN CRACK WAS FOUND OF 0.5IN. LENGTH. SUMMARY OF NRC 00511. SEC. 01. ON STA=500C BTW S8R AND S9R WAS REPAIRED UNDER AMDS 2526-01236-02B.
- [SDR DALA2024061005908](https://openairdocs.org/sdr/DALA2024061005908.md): Floorbeam · corroded · Jun 7, 2024 · N398DA · Boeing 737832 · Fuselage Main, Floor Beam
  > (LOG 0380695) CORROSION ON FLOOR BEAM STA 986 LBL=50 TO RBL=50 AT PAX CABIN. FLOOR BEAM STA 986 LBL= 50 TO RBL=50 WAS REPAIRED PER B737-800 SRM 53-70-51 -2R REPAIR 4.
- [SDR DALA2024061005906](https://openairdocs.org/sdr/DALA2024061005906.md): Frame · cracked · Jun 6, 2024 · N398DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 0379876) FRAME AT A/C RAIL BRACKETS - INSP/MOD; SEC. 01. ON STA=867 BTW S8R AND S9R AT PAX CABIN CRACKS WERE FOUND OF: 01) 0.3IN. LENGTH AND 02) 0.4IN. SUMMARY OF NRC 00515: SEC. 01. ON STA=867 BTW S8R AND S9R WAS REPAIRED UNDER AMDS 2526-01236-02B.
- [SDR DALA2024061005905](https://openairdocs.org/sdr/DALA2024061005905.md): Frame · cracked · Jun 6, 2024 · N398DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 0379858) STA=500A BTW S8R AND S9R AT PAX CABIN CRACKS WERE FOUND OF: 01) 0.5IN. LENGTH AND 02) 0.5IN. SUMMARY OF NRC 00510: SEC. 01. ON STA=500A BTW S8R AND S9R WAS REPAIRED UNDER AMDS 2526-01236-02B.
- [SDR DALA2024060605840](https://openairdocs.org/sdr/DALA2024060605840.md): Frame · cracked · Jun 6, 2024 · N398DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 0379073) INSPECTION WAS PERFORMED ON FRAME AT A/C RAIL BRACKETS - INSP/MOD; SEC. 01. ON STA=500D BTW S8R AND S9R AT PAX CABIN CRACK WAS FOUND OF 0.3IN. LENGTH. SUMMARY OF NRC 00512: SEC. 01. ON STA=500D BTW S8R AND S9R WAS REPAIRED UNDER AMDS 2526-01236-0
- [SDR DALA2024060605839](https://openairdocs.org/sdr/DALA2024060605839.md): Frame · cracked · Jun 6, 2024 · N398DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 0379006) INSPECTION WAS PERFORMED ON FRAME AT A/C RAIL BRACKETS - INSP/MOD; SEC. 01. ON STA=827 BTW S8R AND S9R AT PAX CABIN CRACKS WERE FOUND OF: 01) 0.1IN. LENGTH AND 02) 0.2IN. LENGTH. SUMMARY OF NRC 00514: SEC. 01. ON STA=827 BTW S8R AND S9R WAS REPAI
- [SDR DALA2024060605838](https://openairdocs.org/sdr/DALA2024060605838.md): Frame · cracked · Jun 6, 2024 · N398DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 0378865) INSPECTION WAS PERFORMED ON FRAME AT A/C RAIL BRACKETS - INSP/MOD; SEC. 01. ON STA=500F BTW S8R AND S9R AT PAX CABIN CRACK WAS FOUND OF 0.3IN. LENGTH. SUMMARY OF NRC 00513: SEC. 01. ON STA=500F BTW S8R AND S9R WAS REPAIRED UNDER AMDS 2526-01236-0
- [SDR DALA2024060605835](https://openairdocs.org/sdr/DALA2024060605835.md): Floor Support · corroded · Jun 5, 2024 · N398DA · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0378472) CORROSION ON FLOOR SUPPORTS 2EA BTW STA 951-967 AND LBL=22-50 AT PAX CABIN. FLOOR SUPPORTS (2EA) BTW STA 951-967 AND LBL=22-50 WERE REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2024060605834](https://openairdocs.org/sdr/DALA2024060605834.md): Shear Web · corroded · Jun 5, 2024 · N398DA · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0378465) CORROSION ON RH SHEAR WEB STA 992 AND RBL=35-40 PAX CABIN FLOOR STRUCTURE. RH SHEAR WEB STA 992 AND RBL=35-40 PAX CABIN FLOOR STRUCTURE WAS MANUFACTURED AND REPLACED PER B737-800 SRM 51-40-02-0G PAR 4 AND PAR. 7 AND DWG-147A5712.
- [SDR DALA2024060605833](https://openairdocs.org/sdr/DALA2024060605833.md): Floorbeam · corroded · Jun 5, 2024 · N398DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 0378086) A.A. / AD (ET) INSPECTION WAS PERFORMED ON FRAME AT A/C RAIL BRACKETS - INSP/MOD; SEC. 01. ON STA=727B BTW STR-8L AND STR-9L AT PAX CABIN CRACKS WERE FOUND OF: 01) 0.2IN. LENGTH AND 02) 0.1IN. LENGTH. SUMMARY OF NRC 00527: SEC. 01. ON STA=727B BT
- [SDR DALA2024060605832](https://openairdocs.org/sdr/DALA2024060605832.md): Floorbeam · corroded · Jun 5, 2024 · N398DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 0378082) INSPECTION WAS PERFORMED ON FRAME AT A/C RAIL BRACKETS - INSP/MOD; SEC. 01. ON STA=500A BTW STR-8L AND STR-9L AT PAX CABIN CRACKS WERE FOUND OF: 01) 0.2IN. LENGTH AND 02) 0.3IN. LENGTH. STA=500A BTW STR-8L AND STR-9L WAS REPAIRED UNDER AMDS 2526-
- [SDR DALA2024060605831](https://openairdocs.org/sdr/DALA2024060605831.md): Floorbeam · corroded · Jun 5, 2024 · N398DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 0378078) INSPECTION WAS PERFORMED ON FRAME AT A/C RAIL BRACKETS - INSP/MOD; SEC. 01. ON STA=380 BTW STR-7L AND STR-8L AT PAX CABIN CRACKS WERE FOUND OF: 01) 0.2IN. LENGTH AND 02) 0.3IN. LENGTH. SUMMARY OF NRC 00524: SEC. 01. ON STA=380 BTW STR-7L AND STR-
- [SDR DALA2024060605830](https://openairdocs.org/sdr/DALA2024060605830.md): Floorbeam · corroded · Jun 5, 2024 · N398DA · Boeing 737832 · Fuselage Main, Floor Beam
  > (LOG 0378065) CORROSION ON FLOOR BEAM STA STA 947 AND LBL= 53 TO RBL 53 AT PAX CABIN. FLOOR BEAM STA 947 AND LBL=53 TO RBL 53 WAS REPAIRED PER B737-800 SRM 53-70-51-2R PROCEDURE 5 REPAIR 5.
- [SDR DALA2024060605829](https://openairdocs.org/sdr/DALA2024060605829.md): Frame · cracked · Jun 5, 2024 · N398DA · Boeing 737832 · Fuselage Main, Frame
  > (LOG 0377286) INSPECTION WAS PERFORMED ON FRAME AT A/C RAIL BRACKETS - INSP/MOD; SEC. 01. ON STA=500C BTW STR-8L AND STR-9L AT PAX CABIN CRACK WAS FOUND OF 0.1IN. LENGTH. SUMMARY OF NRC 00526: SEC. 01. ON STA=500C BTW STR-8L AND STR-9L WAS REPAIRED UNDER AMDS
- [SDR DALA2024060605822](https://openairdocs.org/sdr/DALA2024060605822.md): Plate · corroded · Jun 4, 2024 · N398DA · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0375517) CORROSION ON SIDE PLATES LH BTW STA 500E TO STA 500F AT FWD CARGO COMPARTMENT. SIDE PLATES LH BTW STA 500E TO STA 500F AT FWD CARGO COMPARTMENT WAS REPAIRED PER B737-800 SRM 53-00-53-2R PROCEDURE 5 REPAIR 5.
- [SDR DALA2024060405760](https://openairdocs.org/sdr/DALA2024060405760.md): Support · cracked · Jun 2, 2024 · N398DA · Boeing 737832 · Main Landing Gear
  > (LOG 0372053) CRACK ON SUPPORT OF SHOCK STRUT AT LH MLG. REPAIRED PER B737-800 SRM 51-70-11-2R REPAIR GENERAL.
- [SDR DALA2024060405758](https://openairdocs.org/sdr/DALA2024060405758.md): None · none · May 31, 2024 · N398DA · Boeing 737832 · Standard Practices/Structures
  > (LOG 0370351) IN REF. A.A. WORDCARD (A.D) 2526-01236-01A, STEP 3.E.: ER/A NUMBER 502901-14AD ON LH FRAMES EXISTING REPAIR STA 400, 440 AND 480 IS NOT ADDRESSED BY ER/A 502904-14AD LISTEN IN FIGURE 6. SUMMARY OF NRC 00251: LH FRAMES EXISTING REPAIR ON STA 400,
- [SDR DALA2024060405757](https://openairdocs.org/sdr/DALA2024060405757.md): Skin · damaged · May 31, 2024 · N398DA · Boeing 737832 · Passenger/Crew Doors
  > (LOG 0370267) BENT AND CRACKS ON FORWARD ENTRY DOOR (L1) EXTERNAL SKIN AT LOWER HINGE CUT OUT. FORWARD ENTRY DOOR (L1) WAS REPAIRED PER B737-800 SRM 52-10-01-2R REPAIR 5.
- [SDR DALA2024052605514](https://openairdocs.org/sdr/DALA2024052605514.md): Skin · damaged · May 25, 2024 · N398DA · Boeing 737832 · Passenger/Crew Doors
  > AIRCRAFT 3728, BENT AND CRACKS ON FORWARD ENTRY DOOR (L1) EXTERNAL SKIN AT LOWER HINGE CUT OUT. CORRECTIVE ACTION: EXTERNAL SKIN AT LOWER HINGE CUT OUT ON FORWARD ENTRY DOOR (L1) WAS REPAIRED PER B737-800 SRM 52-10-01-2R REPAIR 5. (LP 0360201)
- [SDR DALA2024052605512](https://openairdocs.org/sdr/DALA2024052605512.md): Skin · cracked · May 25, 2024 · N398DA · Boeing 737832 · Horizontal Stabilizer, Plate/Skin
  > AIRCRAFT 3728, CRACK AT LOWER SKIN OF LH HORIZONTAL STABILIZER BETWEEN STAB STA 147.90. CORRECTIVE ACTION: LOWER SKIN OF LH HORIZONTAL STABILIZER BETWEEN STAB STA 147.90. WAS REPAIRED PER B 737-800 SRM 55-10-01-2R-11. DEFERRED TO MONITOR. (LP 0358903)
- [SDR DALA2024052305480](https://openairdocs.org/sdr/DALA2024052305480.md): Skin · cracked · May 23, 2024 · N398DA · Boeing 737832 · Horizontal Stabilizer, Plate/Skin
  > AIRCRAFT 3728, CRACK AT LOWER SKIN OF RH HORIZONTAL STABILIZER BETWEEN STAB STA 138.7 AND STAB STA 147.9. CORRECTIVE ACTION: LOWER SKIN OF RH HORIZONTAL STABILIZER BETWEEN STAB STA 138.7 AND STAB STA 147.9 WAS REPAIRED PER B737-800 SRM 55-10-01-2R-11. (LP 0355
- [SDR DALA2023091207467](https://openairdocs.org/sdr/DALA2023091207467.md): Transmitter · inoperative · Sep 12, 2023 · N398DA · Boeing 737832 · Trailing Edge Flap Control System
  > SHIP 3728 -UFC/DE- DUE TO FLAP ASYMMETRY ON APPROACH. CORRECTIVE ACTION: FSEU FAULT CODE 27-52260 (TE FLAP SNSR R). REPLACED RIGHT TE FLAP POSITION TRANSMITTER. OPS CHECKS GOOD.

Next page: https://openairdocs.org/aircraft/N398DA/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 = 'N398DA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N398DA/reports

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