# Service difficulty reports: N3769L

A list on [N3769L](https://openairdocs.org/aircraft/N3769L.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 · 102 reports

- [SDR DALA2026012200476](https://openairdocs.org/sdr/DALA2026012200476.md): Overheat Sensor · faulted · Jan 20, 2026 · N3769L · Boeing 737832 · Overheat Detection
  > RETURNED TO ATL DUE TO RT WING BODY OVERHEAT. REPLACED M371 AND M1763 OVERHEAT ELEMENTS AND OVERHEAT DETECTION MODULE. CHECKED FOR BLEED AIR LEAKS, NONE FOUND. OPS CHECK GOOD. (LP 7725874)
- [SDR DALA2026010800189](https://openairdocs.org/sdr/DALA2026010800189.md): Check Valve · faulted · Jan 8, 2026 · N3769L · Boeing 737832 · Engine (Turbine/Turboprop)
  > DE- DUE TO RIGHT ENGINE WOULD NOT ADVANCE BEYOND 55% N1 AFTER THROTTLE BACK. INSPECTED MCDS WITH NO FINDINGS. PERFORMED EEC BITE TEST WITH NO FAULTS. CLEARED PS3 LINES, REPLACED 5TH STAGE IP CHECK VALVE AND PT25 SENSOR. (LP 7725822, 1390481)
- [SDR DALA2025091006692](https://openairdocs.org/sdr/DALA2025091006692.md): Stringer · cracked · Sep 9, 2025 · N3769L · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 1189453) CRACK ON UPPER/FWD HOLE AT S-18A WEB STA 727 RIGHT HAND AFT CARGO COMPARTMENT. CRACK ON UPPER/FWD HOLE AT S-18A WEB STA 727 RIGTH HAND AFT CARGO COMPARTMENT (REF. CARD 5311-01251-01B) WAS REPAIRED PER ER/A 628506-14AD REV. ORIGINAL SECTION I: PER
- [SDR DALA2025091006689](https://openairdocs.org/sdr/DALA2025091006689.md): Intercostal · corroded · Sep 9, 2025 · N3769L · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 1189407) CORROSION ON INTERCOSTALS (3 EAS) STA 500D TO 500E S25L,500F TO 500G S25L, 500G TO 500H S25L, AT FWD CARGO COMPARMENT. INTERCOSTAL (3 EAS) WERE REPLACED AND FABRICATE AND REPAIRED: INTERCOSTAL FROM STA 500D TO 500E S25L WAS FABRICATED PER DWG 14
- [SDR DALA2025090906680](https://openairdocs.org/sdr/DALA2025090906680.md): Plate · corroded · Sep 8, 2025 · N3769L · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 1188507) CORROSION OUT OF LIMITS ON LH SIDE PLATE BTW STA 727 TO STA 727J, STA 727J TO STA 847 ALSO RH SIDE PLATE BTW STA 727 TO 727J, STA 727J TO 787. LH SIDE PLATE BTW STA 727 TO STA 847 ALSO RH SIDE PLATE BTW STA 727 TO 787. WERE REPLACED AND INSTALLED
- [SDR DALA2025090906675](https://openairdocs.org/sdr/DALA2025090906675.md): Plate · corroded · Sep 7, 2025 · N3769L · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 1186869) CORROSION ON UP/LOW SURFACE OF SIDE PLATE RH FROM STA 500A TO 500I AT FWD CARGO COMPARMENT. CORROSION LEVEL 2; SIDE PLATE RH FROM STA 500A TO 500I AT FWD CARGO COMPARMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025090906671](https://openairdocs.org/sdr/DALA2025090906671.md): Plate · corroded · Sep 6, 2025 · N3769L · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 1185402) CORROSION OUT OF LIMITS ON UP/LOW SURFACE OF SIDE PLATE LH FROM STA 490 TO 500B. SIDE PLATE LH FROM STA 490 TO 500B +10IN AND SPLICE PLATE AT FWD CARGO COMPARTMEN WAS ADJUSTED, DRILLIND AND REPLACED PER B737-800 SRM 51-40-02-0G PAR 4.B AND 7.D AN
- [SDR DALA2025090806605](https://openairdocs.org/sdr/DALA2025090806605.md): Skin · cracked · Sep 5, 2025 · N3769L · Boeing 737832 · Horizontal Stabilizer, Plate/Skin
  > CRACKS ON LOWER SKIN, STAB STA 101.90 AT LH HORIZONTAL STABILIZER. LOWER SKIN, STAB STA 101.90 AT LH HORIZONTAL STABILIZER WAS REPAIRED PER B 737-800 SRM 55-10-01-2R REPAIR 11.
- [SDR DALA2025090806604](https://openairdocs.org/sdr/DALA2025090806604.md): Slat Track · corroded · Sep 4, 2025 · N3769L · Boeing 737832 · Leading Edge Devices
  > CORROSION ON INBD MAIN TRACK OF SLAT # 1 AT LH WING. INBD MAIN TRACK OF SLAT # 1 AT LH WING WAS REPLACED PER B737-800 AMM 27-81-21.
- [SDR DALA2025090806599](https://openairdocs.org/sdr/DALA2025090806599.md): Skin · corroded · Sep 4, 2025 · N3769L · Boeing 737832 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE EXTERIOR SKIN BETWEEN S-27L AND S-27R AT STA 540. FUSELAGE EXTERIOR SKIN BETWEEN S-27L AND S-27R AT STA 540. WAS REPAIRED PER ER/A 628368-14 REV. ORIGINAL SECTION: I PERMANENT REPAIR AND PRI 628368-14, REV 3.
- [SDR DALA2025090406554](https://openairdocs.org/sdr/DALA2025090406554.md): Keelbeam · damaged · Sep 3, 2025 · N3769L · Boeing 737832 · Fuselage Main, Keel
  > (LOG 1179813) DURING HCK AT QRO, WHILE PERFORMING A ZONAL INSPECTION OF THE KEEL BEAM FROM STA 540 TO STA 727 PER WC 5300-2539, CORROSION WAS FOUND AFFECTING THE DOUBLER INSTALLED BETWEEN STA 500H TO 540 & S-26L TO S-26R, SUBSEQUENTLY AN INTERNAL INSPECTION WA
- [SDR DALA2025090106430](https://openairdocs.org/sdr/DALA2025090106430.md): Stanchion · cracked · Aug 31, 2025 · N3769L · Boeing 737832 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, A CRACK WAS FOUND RUNNING HORIZONTALLY ACROSS THE VERTICAL STANCHION (C-D POST) COMMON TO WINDOW FRAMES OF THE LH (P/N 141A8811) AND/OR RH (P/N 141A8811) NO. 1 DECK WINDOWS. UPPER AFT CORNER FRAME OF 1 RIGHT WINDOW WAS REPAIRED PER ER/A 61
- [SDR DALA2025090106429](https://openairdocs.org/sdr/DALA2025090106429.md): Seat Track · corroded · Aug 31, 2025 · N3769L · Boeing 737832 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL 45 STA 727H+16. AREA IS OUT OF LIMITS PER B737-800 SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 PROCEDURE 1, PAR. 4. A. (2) (A) FIG. 103 DETAIL A. SEAT TRACK LBL 45 STA 727H+16 WAS REPAIRED PER B737-800 SRM 53-00-52-2R PROCEDURE 5, REPAIR
- [SDR DALA2025083106425](https://openairdocs.org/sdr/DALA2025083106425.md): Frame · cracked · Aug 30, 2025 · N3769L · Boeing 737832 · Fuselage Main, Frame
  > DURING HCK AT QRO, WHILE PERFORMING PASSENGER COMPARTMENT INSPECTION PER WC 5300-2342, CRACKS WERE FOUND AFFECTING SEVERAL FUSELAGE FRAMES, COMMON TO STRINGER 8 AIR CONDITIONING (AC) SUPPORT BRACKET ATTACHMENT FASTENER HOLE. TRIMMED OUT DAMAGED AREAS, FABRIC
- [SDR DALA2025083006417](https://openairdocs.org/sdr/DALA2025083006417.md): Seat Track · corroded · Aug 30, 2025 · N3769L · Boeing 737832 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION OUT OF LIMITS ON SEAT TRACK RBL 24 BTW STA 500H+10 TO 520. SEAT TRACK RBL 24 BTW STA 500H+10 TO 520 WAS FABRICATED PER B737-800 SRM 53-00-52-2R PROCEDURE 4, REPAIR 4, AND BAC1520-2789 REV. (B).AND INSTALLED PER B737-800 SRM 51-40-02-0G PAR 4.B AND
- [SDR DALA2025083006416](https://openairdocs.org/sdr/DALA2025083006416.md): Frame · cracked · Aug 30, 2025 · N3769L · Boeing 737832 · Fuselage Main, Frame
  > DURING HCK AT QRO, WHILE PERFORMING PASSENGER COMPARTMENT INSPECTION PER WC 5300-2342, CRACKS WERE FOUND AFFECTING SEVERAL FUSELAGE FRAMES, COMMON TO STRINGER 8 AIR CONDITIONING (AC) SUPPORT BRACKET ATTACHMENT FASTENER HOLE. REMOVED DAMAGED AREAS AND FABRICA
- [SDR DALA2025082806368](https://openairdocs.org/sdr/DALA2025082806368.md): Seat Track · corroded · Aug 26, 2025 · N3769L · Boeing 737832 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 3769, CORROSION OUT OF LIMITS ON SEAT TRACK LBL 24 BTW STA 500H+10 TO 520. CORRECTIVE ACTION: CORROSION LEVEL 2: SEAT TRACK LBL24 BTW STA 500H+10 TO 520 WAS REPLACED PER B737-800 SRM 51-40-02-0G. (LP 1165607)
- [SDR DALA2025082806365](https://openairdocs.org/sdr/DALA2025082806365.md): Seat Track · corroded · Aug 26, 2025 · N3769L · Boeing 737832 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 3769, CORROSION OUT OF LIMITS ON SEAT TRACK LBL 45 BTW STA 500H+10 TO 520. CORRECTIVE ACTION: CORROSION LEVEL 2. SEAT TRACK LBL 45 BTW STA 500H+10 TO 520 WAS FABRICATED PER BAC 1520-2789 REV. (B) AND B737-800 SRM 53-00-52-2R PROCEDURE 4, REPAIR 4 AND
- [SDR DALA2025082806364](https://openairdocs.org/sdr/DALA2025082806364.md): Seat Track · corroded · Aug 26, 2025 · N3769L · Boeing 737832 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 3769, CORROSION OUT OF LIMITS ON SEAT TRACK RBL 45 BTW STA 500H+10 TO 520. CORRECTIVE ACTION: CORROSION LEVEL 2 - SEAT TRACK RBL 45 BTW STA 500H+10 TO 520 WAS FABRICATED PER BAC1520-2789 REV. (B) AND B737-800 SRM 53-00-52-2R PROCEDURE 4, REPAIR 4, AND
- [SDR DALA2025082806362](https://openairdocs.org/sdr/DALA2025082806362.md): Receptacle · cracked · Aug 25, 2025 · N3769L · Boeing 737832 · Fuselage Main, Structure
  > AIRCRAFT 3769, CRACK ON INNER STRAP ON GROUND POWER RECEPTACLE AT LOWER FUSELAGE. CORRECTIVE ACTION: GROUND POWER RECEPTACLE AT LOWER FUSELAGE WAS REPAIRED PER B737-800 SRM 53-10-15-2R PROCEDURE 5 REPAIR 5. (LP 1163677)
- [SDR DALA2025082806361](https://openairdocs.org/sdr/DALA2025082806361.md): Receptacle · cracked · Aug 25, 2025 · N3769L · Boeing 737832 · Fuselage Main, Structure
  > AIRCRAFT 3769, CRACK ON INNER STRAP ON GROUND POWER RECEPTACLE AT LOWER FUSELAGE. CORRECTTIVE ACTION: GROUND POWER RECEPTACLE AT LOWER FUSELAGE WAS REPAIRED PER B737-800 SRM 53-10-15-2R PROCEDURE 5 REPAIR 5. (LP 1163662)
- [SDR DALA2025082806356](https://openairdocs.org/sdr/DALA2025082806356.md): Floorbeam · corroded · Aug 25, 2025 · N3769L · Boeing 737832 · Fuselage Main, Floor Beam
  > AIRCRAFT 3769, CORROSION OUT OF LIMITS ON FLOOR BEAM STA 986.5 BTW LBL 45 TO LBL 46. CORRECTIVE ACTION: PREVIOUS REPAIR ON BEAM STA 986 BTW LBL 25/50 WAS REPLACED PER B737-800 SRM 51-40-02-0G. (LP 1163445)
- [SDR DALA2025081906185](https://openairdocs.org/sdr/DALA2025081906185.md): Pressure Deck · cracked · Aug 18, 2025 · N3769L · Boeing 737832 · Fuselage Main, Structure
  > CRACK OF 2.000IN (LENGTH) PRESSURE DECK WEB ON LH SIDE STA 663.0 BTW LBL35.0/LBL45.0. PRESSURE DECK WEB ON LH SIDE STA 663.0 BTW LBL35.0 TO LBL45.0 WAS REPAIRED PER B737-800 SRM 57-10-10-2R REPAIR 3. PRESSURE DECK WEB ON LH SIDE STA 663.0 BTW LBL 35.0/LBL45.0
- [SDR DALA2025081806143](https://openairdocs.org/sdr/DALA2025081806143.md): Angle · corroded · Aug 15, 2025 · N3769L · Boeing 737832 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE BTW STA 980 TO 960 LBL 54 AT PAX CABIN. ANGLE BTW STA 980 TO 960 LBL 54 AT PAX CABIN WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025041502937](https://openairdocs.org/sdr/DALA2025041502937.md): Battery Pack · inoperative · Apr 11, 2025 · N3769L · Boeing 737832 · Emergency Lighting
  > (LOG 6764025) AFT LEFT DOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED ASSOCIATED BATTERY PACK IN REF B737 AMM 33-51. OPS TEST GOOD AT THIS TIME.
- [SDR DALA2025032702258](https://openairdocs.org/sdr/DALA2025032702258.md): Fuel Control · malfunctioned · Mar 24, 2025 · N3769L · Boeing 737832 · Fuel Control/Turbine Engines
  > SHIP 3769 -DIV- TO PDX DUE TO RIGHT ENGINE SUSPECTED STALL. CORRECTIVE ACTION: BSI SHOWS NO DAMAGE TO COMPRESSOR. REPLACING HMU, FUEL PUMP, EEC AND BLOWING OUT PS3 LINE. FOQA DATA SHOWS ENGINE DID NOT STALL BUT FAILED TO ACCELERATE AFTER BOTH ENGINES WERE THRO
- [SDR DALA2024090308674](https://openairdocs.org/sdr/DALA2024090308674.md): Battery Pack · inoperative · Sep 2, 2024 · N3769L · Boeing 737832 · Emergency Lighting
  > (LOG 6154562) RT SIDE OVER WING EMER EXIT LIGHTS INOP. REPLACED RT OVERWING EMERGENCY EXIT LIGHT BATTERY PER B737 AMM 33-51. OPS CHCK NORMAL.
- [SDR DALA2024082708479](https://openairdocs.org/sdr/DALA2024082708479.md): Window Frame · cracked · Aug 27, 2024 · N3769L · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0524113) LHS NO. 3 FLIGHT COMPARTMENT WINDOW FRAME LOWER FWD CORNER CRACK. COMPLIED WITH E/RA 620400-14AD REV. ORIG.
- [SDR DALA2024070206722](https://openairdocs.org/sdr/DALA2024070206722.md): None · none · Jun 29, 2024 · N3769L · Boeing 737832 · Escape Slide
  > (LOG 6023000) GATE AGENT OPENED ARMED DOOR SLIDE DID NOT DEPLOY. INSPECTED L1 DOOR ESCAPE SLIDE. IAW B737 AMM 25-66. NO DEFECTS NOTED, SLIDE DID NOT DEPLOY. A/C OK FOR SVC.
- [SDR DALA2024042204618](https://openairdocs.org/sdr/DALA2024042204618.md): Unknown · unknown · Apr 19, 2024 · N3769L · Boeing 737832 · Standard Practices/Structures
  > (LOG 5287102) 10 KTS PRIOR TO V1 FELT AN ABRUPT SHIFT IN HE AIRPLANE SUSPECTED BLOWN TIRE, HOWEVER ALL TIRE ARE INTACT. PERFORMED GVI OF GEAR + FLIGHT CONTROLS. NO ITEMS NOTED.
- [SDR DALA2023111609453](https://openairdocs.org/sdr/DALA2023111609453.md): Unknown · unknown · Nov 14, 2023 · N3769L · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0065254) WHILE AT SEA, MTC REPORTED A BLURRY LH NO.1 FLIGHT DECK WINDOW. UPON TROUBLESHOOTING, 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.
- [SDR DALA2023111609452](https://openairdocs.org/sdr/DALA2023111609452.md): Unknown · unknown · Nov 14, 2023 · N3769L · Boeing 737832 · Fuselage Main, Structure
  > (LOG 0065572) FOUND CRACK ON CAPTS #1 WINDOW FRAME AT UPPER OUTBOARD CORNER. REPAIRED PER ERA 613708-14.
- [SDR DALA2022083105855](https://openairdocs.org/sdr/DALA2022083105855.md): None · none · Aug 27, 2022 · N3769L · Boeing 737832 · Fuselage Main, Bulkhead
  > (LOG 2383375) DURING INSPECTION FOUND CRACK ON BULKHEAD (VAPOR BARRIER) AT STA 663 BTW LBL 31.83 AND LBL 40.00. REPAIR ON BULKHEAD (VAPOR BARRIER) ON STA 663 BTW LBL 31.83 AND LBL 40.00 WAS PERFORMED PER B737-800 SRM 57-10-10-2R-2.
- [SDR DALA2022020200695](https://openairdocs.org/sdr/DALA2022020200695.md): None · none · Jan 30, 2022 · N3769L · Boeing 737832 · Fixed Inner Doors
  > (LOG 8236484) COCKPIT DOOR OPENED ON T/O ROLL. PERFORMED COCKPIT DOOR LOCK TEST PER B737 AMM 52-51-21-700-801 SEVERAL TIMES WITH NO FAILURE. NO 180 DAY HISTORY.
- [SDR DALA2022010800152](https://openairdocs.org/sdr/DALA2022010800152.md): Battery Pack · inoperative · Jan 4, 2022 · N3769L · Boeing 737832 · Emergency Lighting
  > (LOG 8060386) DURING INSPECTION FOUND LEFT OVERWING EXIT SIGNS DO NOT ILLUMINATE WITH FORWARD UPPER DOOR. EXIT SIGNS DO NOT ILLUMINATE AS WELL. REMOVED AND REPLACED LT OVERWING EXIT SIGN BATTERY PACK AND CHARGER. OPS CHECKS GOOD.
- [SDR DALA2021121607836](https://openairdocs.org/sdr/DALA2021121607836.md): None · none · Dec 14, 2021 · N3769L · Boeing 737832 · Fuselage, Landing Gear Attach Fittings
  > (LOG 2052397) DURING INSPECTION FOUND LEFT MLG- O/B UPPER H BLOCK ATTACH LUG HAS CORROSION AROUND BUSHING ON O/B SIDE. REPAIRED PER B737 SRM 57-20-90.
- [SDR DALA2021121607835](https://openairdocs.org/sdr/DALA2021121607835.md): None · none · Dec 14, 2021 · N3769L · Boeing 737832 · Fuselage, Landing Gear Attach Fittings
  > (LOG 20523960) DURING INSPECTION FOUND LEFT MLG- I/B LOWER ATTACH LUG HAS CORROSION AROUND I/B SIDE OF BUSHING. REPAIRED PER B737 SRM 57-20-90.
- [SDR DALA2021121607834](https://openairdocs.org/sdr/DALA2021121607834.md): None · none · Dec 14, 2021 · N3769L · Boeing 737832 · Fuselage, Landing Gear Attach Fittings
  > (LOG 2052394) DURING INSPECTION FOUND RT MLG FORWARD TRUNNION INBOARD LOWER BUSHING BORE CORRODED ON I/B SIDE. REPAIRED PER B737 SRM 57-20-90.
- [SDR DALA2021121607833](https://openairdocs.org/sdr/DALA2021121607833.md): None · none · Dec 14, 2021 · N3769L · Boeing 737832 · Fuselage, Landing Gear Attach Fittings
  > (LOG 2052392) DURING INSPECTION FOUND RT MLG FORWARD TRUNNION I/B UPPER BUSHING BORE CORRODED ON I/B SIDE. REPAIRED PER B737 SRM 57-20-90.
- [SDR DALA2021121607832](https://openairdocs.org/sdr/DALA2021121607832.md): None · none · Dec 14, 2021 · N3769L · Boeing 737832 · Fuselage, Landing Gear Attach Fittings
  > (LOG 2052390) DURING INSPECTION FOUND RT MLG FORWARD TRUNNION O/B LOWER BUSHING BORE CORRODED ON O/B SIDE. REPAIRED PER B737 SRM 57-20-90.
- [SDR DALA2021121607831](https://openairdocs.org/sdr/DALA2021121607831.md): None · none · Dec 14, 2021 · N3769L · Boeing 737832 · Fuselage, Landing Gear Attach Fittings
  > (LOG 2052388) DURING INSPECTION FOUND RT MLG FORWARD TRUNION O/B UPPER BUSHING BORE CORRODED ON O/B SIDE. REPAIRED PER B737 SRM 57-20-90.
- [SDR DALA2021121607830](https://openairdocs.org/sdr/DALA2021121607830.md): None · none · Dec 14, 2021 · N3769L · Boeing 737832 · Fuselage, Landing Gear Attach Fittings
  > (LOG 2052387) DURING INSPECTION FOUND LEFT MLG- I/B UPPER H BLOCK ATTACH LUG HAS CORROSION AROUND I/B SIDE OF BUSHING. REPAIRED PER B737 SRM 57-20-90.
- [SDR DALA2021121607829](https://openairdocs.org/sdr/DALA2021121607829.md): None · none · Dec 14, 2021 · N3769L · Boeing 737832 · Fuselage, Landing Gear Attach Fittings
  > (LOG 2052384) DURING INSPECTION FOUND LEFT MLG- O/B LOWER H BLOCK ATTACH LUG HAS CORROSION AROUND O/B SIDE OF BUSHING. REPAIRED PER B737 SRM 57-20-90.
- [SDR DALA2020051802407](https://openairdocs.org/sdr/DALA2020051802407.md): Smoke Detector · activated · May 16, 2020 · N3769L · Boeing 737832 · Smoke Detection
  > SMOKE ALARM SOUNDED AT CRUISE WITH PASSENGER IN FIRST CLASS LAV. PASSENGER SMELLED AND APPEARED LIKE HE WAS SMOKING IN THE LAV WHEN DOOR OPENED ALARM STOP SOUNDING. INSPECTED SMOKE DETECTOR AND FOUND IT WAS NOT TAMPERED WITH. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2020012750662](https://openairdocs.org/sdr/DALA2020012750662.md): Antenna · corroded · Jan 24, 2020 · N3769L · Boeing 737832 · Communications System
  > DURING INSPECTION, FOUND THE FORWARD PASSENGER TELEPHONE ANTENNA BS 757 BTW S-27L TO S-27R WAS CORROED ON THE SETTLEMENT AREA. THE CORROSION WAS REMOVED IAW ETI-37-20-300 REV 1 AND ERA 584735-14 SECTION 1 REV. ORIG.
- [SDR DALA2020012750661](https://openairdocs.org/sdr/DALA2020012750661.md): Doubler · corroded · Jan 24, 2020 · N3769L · Boeing 737832 · Fuselage Main, Structure
  > DURING INSPECTION FOUND CORROSION ON FITTING DOUBLER BS 797 BTW S-27L TO S-27R IN THE AFT CARGO COMPARTMENT. THE DOUBLER WAS REPAIRED IAW ETI-37-20-300, REV 1, AND ERA 584735-14, SECTION 1, REV ORIG.
- [SDR DALA2020012750660](https://openairdocs.org/sdr/DALA2020012750660.md): Doubler · corroded · Jan 24, 2020 · N3769L · Boeing 737832 · Fuselage Main, Structure
  > DURING INSPECTION FOUND CORROSION ON FITTING DOUBLER BS 757 BTW STRINGERS 27L - 27R IN THE AFT CARGO COMPARTMENT. FITTING DOUBLER WAS REPAIRED IAW ETI-37-20-300, REV 1, AND ERA 584735-14, SECTION 1, REV ORIG.
- [SDR DALA2020012100425](https://openairdocs.org/sdr/DALA2020012100425.md): Intercostal · corroded · Jan 21, 2020 · N3769L · Boeing 737832 · Fuselage Miscellaneous Structure
  > DURING INSPECTION FOUND SEVERE CORROSION ON INTERCOSTAL RT 500H AT FWD CARGO COMPARTMENT. THE INTERCOSTAL WAS REPAIRED IAW SRM 51-70-11-2R, AND SRM 51-40-02.
- [SDR DALA2020122410422](https://openairdocs.org/sdr/DALA2020122410422.md): Rib · cracked · Jan 20, 2020 · N3769L · Boeing 737832 · Horizontal Stabilizer, Spar/Rib
  > DURING INSPECTION, FOUND CRACKS ON THE INTERNAL RIB IN THE LEFT HORIZONTAL STABILIZER HSS 92.7. THE RIB WAS REPAIRED IAW SRM 55-10-09, REP 4, AND SRM 51-40-02.
- [SDR DALA2020012100423](https://openairdocs.org/sdr/DALA2020012100423.md): Rib · cracked · Jan 20, 2020 · N3769L · Boeing 737832 · Horizontal Stabilizer, Spar/Rib
  > DURING INSPECTION, FOUND A CRACKED INTERNAL RIB IN THE RIGHT HORIZONTAL STABILIZER STA 129.5. THE RIB WAS REPAIRED IAW SRM 55-10-09-2R, PROCEDURE 5, AND SRM 51-40-02.

Next page: https://openairdocs.org/aircraft/N3769L/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 = 'N3769L' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N3769L/reports

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