# Service difficulty reports: N3763D

A list on [N3763D](https://openairdocs.org/aircraft/N3763D.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 · 128 reports

- [SDR DALA2026083104916](https://openairdocs.org/sdr/DALA2026083104916.md): Cover · detached · Aug 28, 2026 · N3763D · Boeing 737832 · Emergency Lighting
  > CENTER EXIT SIGN COVER FELL OFF / INTERIOR. INSTALLED EMERGENCY SIGN COVER AS REQUIRED PER B737 AMM 33-51. (1782840) AIRCRAFT WAS GROUNDED
- [SDR DALA2026011500347](https://openairdocs.org/sdr/DALA2026011500347.md): Wire · detached · Jan 14, 2026 · N3763D · Boeing 737832 · Light System Wiring
  > (LOG 8432328) EMERGENCY LIGHTS INOPERATIVE AT LT OVERWING DOOR (INTERIOR AND EXTERIOR) AND LT AFT FUSELAGE. FOUND POWER WIRE ON LIGHT ASSY AT INSIDE EXIT SIGN UNSOLDERED. SOLDERED IAW BSWPM 20-40. FOUND ELECTRICAL CONNECTOR D12036 UNPLUGGED BEHIND SIDEWALL A
- [SDR DALA2025053004150](https://openairdocs.org/sdr/DALA2025053004150.md): Window Frame · cracked · May 26, 2025 · N3763D · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0987923) CRACK ON UPPER AFT CORNER FRAME OF NO.1 RH WINDOW AT COCKPIT. WINDOW AT COCKPIT WAS REPAIRED PER ER/A 619132-14ADTR REV A.
- [SDR DALA2025052804117](https://openairdocs.org/sdr/DALA2025052804117.md): Frame · corroded · May 24, 2025 · N3763D · Boeing 737832 · Fuselage Main, Frame
  > (LOG 0988241) SEVERAL CORROSION ON FRAME STA. 907 BTW S- 24L AND S-25L AT AFT CARGO COMPARTMENT. FRAME STA. 907 BTW S-24L AND S-25L AT AFT CARGO COMPARTMENT WAS REPAIRED PER ER/A 626212-14 REV. ORIGINAL.
- [SDR DALA2025052704089](https://openairdocs.org/sdr/DALA2025052704089.md): Frame · corroded · May 23, 2025 · N3763D · Boeing 737832 · Fuselage Main, Frame
  > (LOG 0981758) DURING HCK AT QRO, WHILE PERFORMING AFT CARGO COMPARTMENT INSPECTIONS PER WC 5300-2190, CORROSION WAS FOUND AFFECTING THE FUSELAGE FRAME AT STA 907 BETWEEN S-23L AND S-24L. REPAIRED DAMAGE PER ERA 626212-14.
- [SDR DALA2025052704082](https://openairdocs.org/sdr/DALA2025052704082.md): Doubler · damaged · May 22, 2025 · N3763D · Boeing 737832 · Fuselage Main, Plate/Skin
  > (LOG 0980649) MISSING SECTION ON INNER DOUBLER AT EXTERNAL POWER PANEL. REPAIRED PER REPAIR PER B737-800 SRM 53-10-15-2R-5 PROCEDURE 5 REPAIR 5.
- [SDR DALA2025052704077](https://openairdocs.org/sdr/DALA2025052704077.md): Channel · corroded · May 21, 2025 · N3763D · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0978726) CORROSION ON LH ZEE CHANNEL SIDEPLATE AT FLOOR STRUCTURE BTW STA 727-847 AND LBL 21 AT AFT CARGO COMPARTMENT. ZEE CHANNEL SIDEPLATE (LH) BTW STA 727-847 LBL 21 AT AFT CARGO COMPARTMENT, WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025052704071](https://openairdocs.org/sdr/DALA2025052704071.md): Channel · corroded · May 21, 2025 · N3763D · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0977252) CORROSION ON RH ZEE CHANNEL SIDEPLATE AT FLOOR STRUCTURE BTW STA 727-767 AND RBL 21 AT AFT CARGO COMPARTMENT. RH ZEE CHANNEL SIDEPLATE AT FLOOR STRUCTURE BTW STA 727-767 AND RBL 21 AT AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0
- [SDR DALA2025052203967](https://openairdocs.org/sdr/DALA2025052203967.md): Fitting · corroded · May 20, 2025 · N3763D · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0976989) CORROSION WAS FOUND ON FITTING BTW STA. 907 AND BTW S-24L TO S-25L ALSO CORROSION WAS FOUND ON SUPPORT STA 927 BTW S-24L TO S-25L. FITTING BTW STA. 907 AND BTW S-24L TO S-25L AND SUPPORT STA 927 BTW S-24L TO S-25L WERE REPLACED PER B737-800 SRM 5
- [SDR DALA2025052203965](https://openairdocs.org/sdr/DALA2025052203965.md): Shear Tie · corroded · May 20, 2025 · N3763D · Boeing 737832 · Fuselage Internal Mounting Structure
  > (LOG 0976497) CORROSION ON SHEAR TIE BTW STGR 25L-26L AND STA 847 AT AFT CARGO COMPARTMENT (INSIDE OF WASTE TANK ENCLOUSURE AREA WAS FOUND. SHEAR TIE BTW STGR 25L -26L AND STA 847 AT AFT CARGO COMPARTMENT WAS REPLACED PER B737- 800 SRM 51-40-02-0G.
- [SDR DALA2025052203964](https://openairdocs.org/sdr/DALA2025052203964.md): Intercostal · corroded · May 20, 2025 · N3763D · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0976456) AFTER REMOVED INTERCOSTAL ON STA 907 TO 927 BTW S-24L TO S-25L WAS FOUND EXFOLIATION ON PART. INTERCOSTAL ON STA 907 TO 927 BTW S-24L TO S-25L WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025052103915](https://openairdocs.org/sdr/DALA2025052103915.md): Shear Tie · corroded · May 19, 2025 · N3763D · Boeing 737832 · Fuselage Internal Mounting Structure
  > (LOG 0974774) CORROSION WAS FOUND ON SHEAR TIE (2 EAS) ON STA 927 AND STA 907. SHEAR TIE (2 EAS) ON STA 927 AND STA 907 WERE REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025052103914](https://openairdocs.org/sdr/DALA2025052103914.md): Stringer · corroded · May 19, 2025 · N3763D · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 0974698) CORROSION ON STGR 25L STA 810 AT AFT CARGO COMPARTMENT. STGR 25L STA 810 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B737-800 SRM 53-00-03-2R PROCEDURE 1 REPAIR 1.
- [SDR DALA2025052003885](https://openairdocs.org/sdr/DALA2025052003885.md): Channel · corroded · May 17, 2025 · N3763D · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0971714) AFTER ZEE CHANNEL SIDEPLATE REMOVAL WAS FOUND CORROSION ON UPPER FLANGE OF INTERCOSTAL BTW. STA 747 AND 767 ABD S-25R AT AFT. CARGO COMPARTMENT. INTERCOSTAL BTW. STA 747 AND 767 ABD S-25R AT AFT. CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51
- [SDR DALA2025052003875](https://openairdocs.org/sdr/DALA2025052003875.md): Intercostal · corroded · May 17, 2025 · N3763D · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0970323) CORROSION ON INTERCOSTAL BTW STA 847-867 AND STGR 25L-26L AT AFT CARGO COMPARTMENT (INSIDE OF WASTE TANK ENCLOUSURE AREA). INTERCOSTAL BTW STA 847-867 AND STGR 25L-26L AT AFT CARGO COMPARTMENT (INSIDE OF WASTE TANK ENCLOUSURE AREA) WAS REPLACED P
- [SDR DALA2025052003874](https://openairdocs.org/sdr/DALA2025052003874.md): Intercostal · corroded · May 16, 2025 · N3763D · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 0969844) AFTER REMOTION OF SIDE PLATES CORROSION WAS FOUND ON INTERCOSTALS BTW STA 500A + 10 TO 500 I STGR 26L AT FWD CARGO COMPARTMENT. INTERCOSTALS (1EA) BTW STA 500H TO STA 500I WAS REPAIRED AND REPLACED PER B737-800 SRM 53-30-53-2R-1, B737-800 SRM 51
- [SDR DALA2025052003872](https://openairdocs.org/sdr/DALA2025052003872.md): Stringer Splice · corroded · May 16, 2025 · N3763D · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 0969522) CORROSION WAS FOUND ON STGR SPLICE ON STA 887 AND STGR 24L AT AFT CARGO COMPARTMENT. STGR SPLICE ON STA 887 AND STGR 24L AT AFT CARGO COMPARTMENT WAS FABRICATED AND REPLACED PER BAC1498-268 REV (-) AND B737-800 SRM 51-40-02-0G.
- [SDR DALA2025051903821](https://openairdocs.org/sdr/DALA2025051903821.md): Plate · corroded · May 15, 2025 · N3763D · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0966714) CORROSION ON SIDE PLATE STA 500A+10-500I STR26L. SIDE PLATE STA 500A+10-500I STR26L WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025051903818](https://openairdocs.org/sdr/DALA2025051903818.md): Angle · cracked · May 14, 2025 · N3763D · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0965872) CRACKED LH AND RH ANGLES ON AFT BULKHEAD OF AIR CONDITIONING BAYS COMMON TO MAIN WHEEL WELLS AT STA 663.75 AND REAR SPAR ATTACHMENT ANGLE ON CENTER FUSELAGE. LH AND RH ANGLES ON AFT BULKHEAD OF AIR CONDITIONING BAYS COMMON TO MAIN WHEEL WELLS AT
- [SDR DALA2025051503766](https://openairdocs.org/sdr/DALA2025051503766.md): Fitting · corroded · May 13, 2025 · N3763D · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0964437) WORK SHOP INTERIOR MONUMENTS: FLOOR FITTINGS 4(EA) WITH CORROSION GALLEY #7. FLOOR FITTINGS 4(EA) WITH CORROSION GALLEY #7 WERE FABRICATED AND INSTALLED PER PRI 626215-14 REV 0 AND ERA 626215-14 REV. ORIGINAL.
- [SDR DALA2025051503764](https://openairdocs.org/sdr/DALA2025051503764.md): Stringer · corroded · May 13, 2025 · N3763D · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 0964226) CORROSION WAS FOUND ON STGR 24L BTW STA 907-927 AT AFT CARGO COMPARTMENT. STGR 24L BTW STA 907-927 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B737-800 SRM 53-00-03-2R PROCEDURE 1 REPAIR 1.
- [SDR DALA2025051503763](https://openairdocs.org/sdr/DALA2025051503763.md): Plate · corroded · May 13, 2025 · N3763D · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0964162) CORROSION ON SIDE PLATE STA 400-500A STR26L. SIDE PLATE STA 400-500A STR26L WAS DRILLED AND ADJUSTED PER B737-800 SRM 51-40-05-0G AND REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025051503762](https://openairdocs.org/sdr/DALA2025051503762.md): Not Reported · damaged · May 13, 2025 · N3763D · Boeing 737832 · Wing Structure
  > (LOG 0963092) PERFORM PERMANENT REPAIR IN ACCORDANCE SRM 57-10-10-2R PROCEDURE 3. PERMANENT REPAIR IN ACCORDANCE B737-800 SRM 57-10-10-2R PROCEDURE 3, REPAIR 3 ALTERNATIVE 2 WAS PERFORMED.
- [SDR DALA2025051503761](https://openairdocs.org/sdr/DALA2025051503761.md): Box Beam · corroded · May 12, 2025 · N3763D · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0962932) CORROSION ON BEAM BOX BELOW ATTACH FITTING STA 291.5 BTW RBL 40 AT (FLOOR STRUCTURE) W1. BEAM BOX BELOW ATTACH FITTING STA 291.5 BTW RBL 40 AT (FLOOR STRUCTURE) W1 WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025051503760](https://openairdocs.org/sdr/DALA2025051503760.md): Strap · corroded · May 12, 2025 · N3763D · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0962675) CORROSION ON STRAP (UPPER SKIN) BTW STA 787- 847 AND STGR 25R-26R AT AFT CARGO COMPARTMENT. STRAP (UPPER SKIN) FROM STA.767 TO STA.867 AND STGR 25R-26R AT AFT CARGO WAS FABRICATED PER DWG 146A8128-1 REV C AND REPLACED PER B737-800 SRM 51-40-02 -0
- [SDR DALA2025051503759](https://openairdocs.org/sdr/DALA2025051503759.md): Stringer · cracked · May 12, 2025 · N3763D · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 0962458) CRACK ON S-16L INTERNAL SIDE STA 294.5 NEAR L1 ENTRY DOOR AT PASSENGER COMPARTMENT. S-16L INTERNAL SIDE STA 294.5 NEAR L1 ENTRY DOOR AT PASSENGER COMPARTMENT WAS REPAIRED PER B737-800 SRM 53-00-03-2R PROCEDURE 1, REPAIR 1.
- [SDR DALA2025051503757](https://openairdocs.org/sdr/DALA2025051503757.md): Tee Fitting · corroded · May 11, 2025 · N3763D · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0960692) CORROSION ON TEE FITTING AT STA 992.8 STR 11LH AT PAX CABIN. ANGLE AT STA 992.8 STR 11LH AT PAX CABIN WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025051203671](https://openairdocs.org/sdr/DALA2025051203671.md): Angle · corroded · May 10, 2025 · N3763D · Boeing 737832 · Fuselage Miscellaneous Structure
  > CORROSION ON CHORD ANGLE FROM STA 360 TO STA 291 BTW RBL 57 AT (FLOOR STRUCTURE) W1. CHORD ANGLE BTW STA 360 TO STA 251, RBL 57 AT (FLOOR STRUCTURE) W1 WAS REPLACED PER B737-800 SRM 51-40-02-0G PAR 4. AND 51-40-02-0G PAR 7.D.
- [SDR DALA2025051203660](https://openairdocs.org/sdr/DALA2025051203660.md): Floorbeam · corroded · May 9, 2025 · N3763D · Boeing 737832 · Fuselage Main, Floor Beam
  > (LOG 0956562) CORROSION ON FLOOR BEAM UPPER FLANGE BELOW ATTACH FITTING STA 947.5 BTW RBL 50 AT (FLOOR STRUCTURE) W2 FLOOR BEAM UPPER FLANGE BELOW ATTACH FITTING STA 947.5 BTW RBL 50 AT (FLOOR STRUCTURE) W2 WAS REPAIRED ALTERNATIVE 2 PER B737-800 SRM 53-70-51-
- [SDR DALA2025051203659](https://openairdocs.org/sdr/DALA2025051203659.md): Pressure Deck · cracked · May 8, 2025 · N3763D · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0955933) CRACK OF 1.000 IN LENGTH ON LH VERTICAL PRESSURE DECK WEB STA 663.0 BTW LBL38.0 AND LBL 45.0. VERTICAL PRESSURE DECK WEB STA 663.0 BTW LBL38.0 AND LBL 45.0 WAS REPAIRED PER B737-800 SRM B737-800 SRM 57-10-10-2R PROCEDURE 3 REPAIR 3.
- [SDR DALA2025050903630](https://openairdocs.org/sdr/DALA2025050903630.md): Plate · corroded · May 8, 2025 · N3763D · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0956286) CORROSION ON SIDE PLATE STA 500D+10-500I STR26R. SIDE PLATE STA 500D+10-500I STR26R WAS ADJUSTED AND DRILLED PER B737-800 SRM 51-40-05-0G AND REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025050903629](https://openairdocs.org/sdr/DALA2025050903629.md): Box Beam · corroded · May 8, 2025 · N3763D · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0956265) CORROSION ON BEAM BOX STA 937.5 BTW LBL 51 AT (FLOOR STRUCTURE) W2. BEAM BOX STA 937.5 BTW LBL 51 AT (FLOOR STRUCTURE) W2 WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025050903628](https://openairdocs.org/sdr/DALA2025050903628.md): Plate · corroded · May 8, 2025 · N3763D · Boeing 737832 · Fuselage Floor Panel
  > (LOG 0956226) CORROSION ON SIDE PLATE STA 500D+10-500I STR26R. SIDE PLATE STA 500D+10-500I STR26R WAS ADJUSTED AND DRILLED PER B737-800 SRM 51-40-05-0G AND REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025050903626](https://openairdocs.org/sdr/DALA2025050903626.md): Plate · corroded · May 8, 2025 · N3763D · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 0955881) CORROSION SIDE PLATE STA 500-500D+10 STR 26R AT FWD CARGO COMPARMENT. SIDE PLATE STA 500-500D +10 STR 26R AT FWD CARGO COMPARMENT WAS ADJUSTED, DRILLED AND COUNTERSINK PER B737-800 SRM 51-40-05-0G AND SRM 51-40-08-0G AND REPLACED PER B737-800 SRM
- [SDR DALA2025050903625](https://openairdocs.org/sdr/DALA2025050903625.md): Seat Track · corroded · May 8, 2025 · N3763D · Boeing 737832 · Fuselage, Seat/Cargo Attach Fittings
  > (LOG 0955840) CORROSION ON SEAT TRACK (PREVIOUS REPAIR) LBL 45 STA 520. REPAIRED OF SEAT TRACK LBL 45 STA 510H+ 11 TO STA 520. CPAX WAS REPLACED PER B737-800 SRM 53-00-52-2R PROCEDURE 4 REPAIR 4.
- [SDR DALA2025050903624](https://openairdocs.org/sdr/DALA2025050903624.md): Box Beam · corroded · May 8, 2025 · N3763D · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0954583) CORROSION ON BEAM BOX STA 937.5 BTW RBL 51 AT (FLOOR STRUCTURE) W2. BEAM BOX STA 937.5 BTW RBL 51 AT (FLOOR STRUCTURE) W2 WAS REPLACED PER SRM 51-40-02-0G.
- [SDR DALA2025050903621](https://openairdocs.org/sdr/DALA2025050903621.md): Floorbeam · corroded · May 8, 2025 · N3763D · Boeing 737832 · Fuselage Main, Floor Beam
  > (LOG 0954506) CORROSION ON FLOOR SUPPORT STA 955.0 BTW RBL 34 TO RBL 49 AT (FLOOR STRUCTURE) W2. SUPPORT STA 955.0 BTW RBL 34 TO RBL 49 AT (FLOOR STRUCTURE) W2 WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025050903613](https://openairdocs.org/sdr/DALA2025050903613.md): Attach Angle · cracked · May 6, 2025 · N3763D · Boeing 737832 · Fuselage Main, Attach Fittings
  > (LOG 0952267) CRACK WAS FOUND ON OPEN FASTENER HOLE IN THE ATTACH ANGLE NEXT TO THE DRAIN HOLE/SLOT AT 9HRS O LOCK POS. AT VERTICAL PRESSUERE DECK WEB. ASTENER HOLE IN THE ATTACH ANGLE NEXT TO THE DRAIN HOLE/SLOT AT 9HRS O LOCK POS. AT VERTICAL PRESSURE DECK W
- [SDR DALA2025050903612](https://openairdocs.org/sdr/DALA2025050903612.md): Attach Angle · cracked · May 6, 2025 · N3763D · Boeing 737832 · Fuselage Main, Attach Fittings
  > (LOG 0952236) CRACK WAS FOUND OF: 0.625IN LENGTH ON LH ATTACH ANGLE AT THE DRAIN HOLE/SLOT OF VERTICAL PRESSUERE DECK WEB. LH ATTACH ANGLE AT THE DRAIN HOLE/SLOT OF VERTICAL PRESSUERE DECK WEB WAS REPAIRED PER B737-800 SRM 57-10-10-2R PROCEDURE 6 REPAIR 6.
- [SDR DALA2025050803579](https://openairdocs.org/sdr/DALA2025050803579.md): Floorbeam · corroded · May 4, 2025 · N3763D · Boeing 737832 · Fuselage Main, Floor Beam
  > (LOG 0948600) CORROSION ON FLOOR BEAM UPPER FLANGE STA 328 BTW RBL 48 TO RBL 38 AT (FLOOR STRUCTURE) W1. FLOOR BEAM UPPER FLANGE STA 328 BTW RBL 48 TO RBL 38 AT (FLOOR STRUCTURE) W1 WAS REPAIRED PER B737-800 SRM 53-10-51-2R PROCEDURE 11.
- [SDR DALA2025050603489](https://openairdocs.org/sdr/DALA2025050603489.md): Frame · not reported · May 2, 2025 · N3763D · Boeing 737832 · Fuselage Main, Frame
  > (LOG 0945663) ACCOMPLISH AMDS 5311-01251-02B - RIGHT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02. COMPLIED WITH AMDS CARD 5311-01251-02B. INSTALL A NEW SHIM R/H SIDE STA 727 FRAME INNER CHORD S-18A. (AD 2023-06-15) (BOEING SERVICE BULLETIN 737-
- [SDR DALA2025050603488](https://openairdocs.org/sdr/DALA2025050603488.md): Frame · not reported · May 2, 2025 · N3763D · Boeing 737832 · Fuselage Main, Frame
  > (LOG 0945659) ACCOMPLISH AMDS 5311-01251-02A - LEFT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02. COMPLIED WITH AMDS CARD 5311-01251-02A. INSTALL A NEW SHIM L/H SIDE STA 727 FRAME INNER CHORD S-18A. (AD 2023-06-15) (BOEING SERVICE BULLETIN 737-5
- [SDR DALA2025010600100](https://openairdocs.org/sdr/DALA2025010600100.md): Battery Pack · no test · Jan 5, 2025 · N3763D · Boeing 737832 · Emergency Lighting
  > (LOG 5648384) RIGHT OVERWING DOOR EXIT LIGHTS INOP. R/R M1695 BATTERY PACK REF B737 AMM 33-51. OPS CHECK GOOD AT THIS TIME.
- [SDR DALA2024090408726](https://openairdocs.org/sdr/DALA2024090408726.md): Battery Pack · inoperative · Sep 3, 2024 · N3763D · Boeing 737832 · Emergency Lighting
  > (LOG 6156343) EMERGENCY LIGHTS OUT SEAT ROWS 11-15. R & REPLACED POWER SUPPLY BATTERY PACK AT SEAT ROW 11 DEF. OPS CKS OK.
- [SDR DALA2024071907295](https://openairdocs.org/sdr/DALA2024071907295.md): Stanchion · cracked · Jul 16, 2024 · N3763D · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0450960) DURING B-CHECK IN CVG, MTC DISCOVERED DAMAGE CONSISTING OF A CRACK RUNNING HORIZONTALLY ACROSS THE VERTICAL STANCHION (C-D POST) COMMON TO WINDOW FRAME (P/N 141A8811-5) OF THE LH NO. 1 FLIGHT DECK WINDOW. MAINTENANCE REPAIRED CRACK PER ERA 619401
- [SDR DALA2024071607193](https://openairdocs.org/sdr/DALA2024071607193.md): Window Frame · cracked · Jul 12, 2024 · N3763D · Boeing 737832 · Fuselage Main, Structure
  > (LOG 5620560) DURING WORK CARD 5600-2492 FOUND SUSPECTED CRACK ON CAPTAIN WINDOW STRUCTURE. REPAIRED CRACK PER ERA 619401.
- [SDR DALA2024071207071](https://openairdocs.org/sdr/DALA2024071207071.md): Window Frame · cracked · Jul 12, 2024 · N3763D · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0442593) CAPTAIN WINDSHIELD NO. 1 WINDOW FRAME UPPER OTBD CORNER CRACKED. REPAIRED CRACK PER ERA 619401-14.
- [SDR DALA2024070506772](https://openairdocs.org/sdr/DALA2024070506772.md): Battery Pack · no test · Jul 1, 2024 · N3763D · Boeing 737832 · Emergency Lighting
  > (LOG 5620513) ROW 23 EMERGENCY BATTERY PACK NOT WORKING. R&R BATTERY PACK AT ROW 23. ALL EMERGENCY LIGHTS OPERATIVE AND OPS NORMAL AT THIS TIME PER B737 AMM 33-51.
- [SDR DALA2024042504702](https://openairdocs.org/sdr/DALA2024042504702.md): Apu · odor · Apr 24, 2024 · N3763D · Boeing 737832 · Airborne Auxiliary Power Unit (APU) System
  > (LOG 5302761) STRONG ODOR MUSTY DIRTY SOCK ON DESCENT STARTING AT 4000 FT UNTIL LANDING. REPLACED APU PER B 737 AMM 49.
- [SDR DALA2024032603778](https://openairdocs.org/sdr/DALA2024032603778.md): Pressure Blkhd · cracked · Mar 24, 2024 · N3763D · Boeing 737832 · Fuselage Main, Bulkhead
  > (LOG 0260709) DURING INBOUND WALK AROUND- CRACK APPROX 2 INCHES IN LENGTH IN LN RIGHT WHEEL WELL PRESSURE BULKHEAD, LOCATION TO THE LEFT OF FLIGHT RECORDER ACCAROMETER M517. INSTALLED DOUBLER WET WITH SEALANT. APPLIED FILLET SEAL TO DOUBLER. RESTORED COATINGS

Next page: https://openairdocs.org/aircraft/N3763D/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 = 'N3763D' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N3763D/reports

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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.