# Service difficulty reports: N3768

A list on [N3768](https://openairdocs.org/aircraft/N3768.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 · 130 reports

- [SDR DALA2026101605693](https://openairdocs.org/sdr/DALA2026101605693.md): Light · inoperative · Oct 14, 2026 · N3768 · Boeing 737832 · Emergency Lighting
  > DURING SVC. FOUND EMERGENCY EXIT SIGN DOES NOT TURN ON. (9438835) AIRCRAFT WAS GROUNDED
- [SDR DALA2026092905416](https://openairdocs.org/sdr/DALA2026092905416.md): Power Supply · inoperative · Sep 27, 2026 · N3768 · Boeing 737832 · Emergency Lighting
  > FOUND FWD EMERGENCY EXIT INDICATOR LIGHTS INOP, LT AND RT, ON OVERWING EXIT DOORS. FOUND EMERGENCY POWER SUPPLY EIN M1694 INOPERATIVE W/ FUSES BLOWN. R & R BATTERY PACK HOUSING IAW AMM 33-51. FOUND ALL 8 BULBS OF INDICATOR LIGHTS BURNED OUT, R & R THE LAM
- [SDR DALA2026081204640](https://openairdocs.org/sdr/DALA2026081204640.md): Tire · blown · Aug 11, 2026 · N3768 · Boeing 737832 · Tire
  > DECLARED AN EMERGENCY DUE TO NR 2 MAIN LANDING GEAR TIRE FAILURE ON TAKEOFF FROM SLC. REPLACED NR 2 MLG TIRE. (8826166) AIRCRAFT WAS GROUNDED
- [SDR DALA2026081004613](https://openairdocs.org/sdr/DALA2026081004613.md): Diode · broken · Aug 8, 2026 · N3768 · Boeing 737832 · Light System Wiring
  > FOUND 2 INTERIOR EMERGENCY LIGHT SIGNS INOPERATIVE. REMOVED AND REPLACED A BROKEN DIODE ON BATTERY PACK HOUSING IAW AMM 33-50. OPS CHKD GOOD. (8826155) AIRCRAFT WAS GROUNDED
- [SDR DALA2026070703976](https://openairdocs.org/sdr/DALA2026070703976.md): Power Supply · inoperative · Jul 4, 2026 · N3768 · Boeing 737832 · Emergency Lighting
  > EMERGENCY EXIT LIGHT SIGNS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY M1694. OPS TESTED GOOD IAW AMM 33-51. (8619026) AIRCRAFT WAS GROUNDED
- [SDR DALA2026060303372](https://openairdocs.org/sdr/DALA2026060303372.md): Sign · inoperative · Jun 2, 2026 · N3768 · Boeing 737832 · Emergency Lighting
  > LOWER SIDEWALL EXIT SIGNS INOP ON BOTH SIDES IN ROW 17. REMOVED AND REPLACED LOWER SIDEWALL EXIT SIGN ASSY'S ON BOTH SIDES AND REMOVED AND REPLACED M1694 CHARGER PER B737 AMM 33-51. OPS CHECK GOOD. (LOG 8903610 - AIRCRAFT WAS GROUNDED).
- [SDR DALA2026042702649](https://openairdocs.org/sdr/DALA2026042702649.md): Battery Pack · inoperative · Apr 22, 2026 · N3768 · Boeing 737832 · Emergency Lighting
  > BOTH LEFT AND RIGHT OVERWING EMER EXIT LOWER EXIT SIGNS INOP. ON BATTERY PACK (MI694) FOUND FUSE F2 BAD R&R FUSE F2 REF B737 AMM 33-51. ALSO FOUND BOTH EXIT SIGN LIGT ASSY'S BAD. REPLACED BOTH EXIT LIGHT ASSY'S ROW 17 BOTH LIGHT CKS GOOD. REF B737 MM 33-51. OK
- [SDR DALA2026032301947](https://openairdocs.org/sdr/DALA2026032301947.md): Power Supply · no test · Mar 20, 2026 · N3768 · Boeing 737832 · Emergency Lighting
  > DURING SVC CHK FOUND FWD LOWER EMERGENCY EXIT LIGHTS INOP. R/R OW POWER SUPPLY AND LT FWD EMERGENCY LIGHT PER B737 AMM 33-51. LIGHT NOW ILLUMINATES. RT FWD LIGHT STILL INOP. REMOVED AND INSTALLED RT FWD O/W EXIT LT. PER B737 AMM 33-51. OPS NORMAL.
- [SDR DALA2026030301448](https://openairdocs.org/sdr/DALA2026030301448.md): Sign · inoperative · Feb 28, 2026 · N3768 · Boeing 737832 · Emergency Lighting
  > (LOG 8101555) DURING SVC FOUND RIGHT FWD OVERWING ESPACE HATCH VERTICAL EXIT SIGN LIGHT INOPERATIVE. REMOVED EXIT SIGN LIGHT ASSEMBLY PER AMM 33-51. INSTALLED EXIT SIGN LIGHT ASSY RT FWD OVERWING PER AMM 33-21. OPS NORMAL.
- [SDR DALA2026030301447](https://openairdocs.org/sdr/DALA2026030301447.md): Power Supply · no test · Feb 28, 2026 · N3768 · Boeing 737832 · Emergency Lighting
  > (LOG 8101554) DURING SVC, FOUND LEFT FWD OVERWING ESCAPE HATCH VERTICAL EXIT SIGN LIGHT INOP. R&R POWER SUPPLY PER B737 AMM 33-51, AND OPS CHECK NORMAL.
- [SDR DALA2026020200777](https://openairdocs.org/sdr/DALA2026020200777.md): Fuse · open · Jan 28, 2026 · N3768 · Boeing 737832 · Emergency Lighting
  > EMERGENCY EXIT LIGHTED SIGNS ADJACENT TO LT & RT FWD OVERWING EXIT DOORS INOPERATIVE. FOUND BOTH BASE ASSYS WITH OPEN FUSES MARKED F1. R/R BOTH EXIT IDENTIFIER BASES PER B737 AMM 33-51. OPERATION TEST GOOD PER B737 AMM 33-51.
- [SDR DALA2025121109070](https://openairdocs.org/sdr/DALA2025121109070.md): Elec Connector · unsecure · Dec 8, 2025 · N3768 · Boeing 737832 · Light System Wiring
  > (LOG 7798839) ON SERVICE CHECK, FOUND 23DEF SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. FOUND CONNECTOR UNDER CARPET LOOSE, SECURED THE CONNECTOR. LIGHT OPS NORMAL IAW AMM 33-51.
- [SDR DALA2025121109069](https://openairdocs.org/sdr/DALA2025121109069.md): Power Supply · inoperative · Dec 8, 2025 · N3768 · Boeing 737832 · Emergency Lighting
  > (LOG 7798842) DURING SERVICE FOUND POWER SUPPLY FOR INTERIOR EMERGENCY OVERWING LIGHTING TO BE INOPERATIVE. R & R POWER SUPPLY IAW AMM 33-51. OPS CHECKED GOOD.
- [SDR DALA2025121109068](https://openairdocs.org/sdr/DALA2025121109068.md): Light · inoperative · Dec 8, 2025 · N3768 · Boeing 737832 · Emergency Lighting
  > (LOG 7798838) ON SVC CK, FOUND ROW 17 INTERIOR LOWER OVERWING EXIT LIGHT ON BOTH LT & RT SIDE INOPERATIVE. R & R THE LIGHT ASSY IAW AMM 33-51. OPS CHECKED GOOD.
- [SDR DALA2025110608087](https://openairdocs.org/sdr/DALA2025110608087.md): Light · inoperative · Nov 3, 2025 · N3768 · Boeing 737832 · Emergency Lighting
  > ROW 18 DEF LOWER EMERGENCY EXIT SIGN INOPERATIVE. R & R EXIT LED ASSY IAW MM 33-51. CHECKED OK.
- [SDR DALA2026100805571](https://openairdocs.org/sdr/DALA2026100805571.md): Skin · dented · Oct 9, 2025 · N3768 · Boeing 737832 · Fuselage Main, Plate/Skin
  > WHILE ACOMPLISHING A ZONAL INSPECTION, FUSELAGE CROWN SKIN DENTS AT BS 727E TO 727G AND S3L TO S3R. REF ERA 629296-14. (1243111) AIRCRAFT WAS GROUNDED.
- [SDR DALA2025101307469](https://openairdocs.org/sdr/DALA2025101307469.md): Window Frame · cracked · Oct 9, 2025 · N3768 · Boeing 737832 · Fuselage Main, Structure
  > CRACK ON AFT UPPER CORNER FRAME OF NR 1 LT WINDOW AT COCKPIT ON REFERENCE CARD 5311-2003. LT WINDOW FRAME AT COCKPIT WAS REPAIRED PER ER/A 619132-14AD.
- [SDR DALA2025101307468](https://openairdocs.org/sdr/DALA2025101307468.md): Window Frame · cracked · Oct 9, 2025 · N3768 · Boeing 737832 · Fuselage Main, Structure
  > CRACK WAS FOUND OF: 0.375IN LENGTH ON RT WINDOW FRAME RADIUS AREA IN REF. CARD 5311-2003. RH WINDOW FRAME WAS REPAIRED PER ER/A 619132-14ADTR REV, A.
- [SDR DALA2025101007400](https://openairdocs.org/sdr/DALA2025101007400.md): Skin · corroded · Oct 9, 2025 · N3768 · Boeing 737832 · Fuselage Main, Plate/Skin
  > CORROSION ON INB SKIN FUSELAGE AND DOUBLER SUPPORT(NATS AIRPHONE ANTENNA) STA 747,STA 757 AND STA 797 BTWN S27L TO 27R (BILGIE AREA) CARGO COMPARMENT C2.
- [SDR DALA2025101007399](https://openairdocs.org/sdr/DALA2025101007399.md): Skin · dented · Oct 9, 2025 · N3768 · Boeing 737832 · Fuselage Main, Plate/Skin
  > THREE DENTS BETWEEN STA 727F+7 TO 727E AND S2R - S3R, ALSO 8 DENTS BTW STA 727E +15 TO 727G STGR 2L/3L AT EXTERNAL FUSELAGE SKIN. FUSELAGE SKIN (VIASAT) BTW STA 727E TO 727G STGR 3L/3R WAS REPAIRED PER PRI 629345-14 REV 0 TO 4 AND ERA 629345-14AD REV. ORIGINAL
- [SDR DALA2025101007398](https://openairdocs.org/sdr/DALA2025101007398.md): Skin · dented · Oct 9, 2025 · N3768 · Boeing 737832 · Fuselage Main, Plate/Skin
  > THREE DENTS BETWEEN STA 727F+7 TO 727E AND S2R - S3R. FUSELAGE SKIN BTW STA 727E TO 727G STGR 3L /3R WAS REPAIRED PER PRI 629296-14 REV 0 TO 3 AND ERA 629296-14AD REV. A.
- [SDR DALA2025101007397](https://openairdocs.org/sdr/DALA2025101007397.md): Window Frame · cracked · Oct 9, 2025 · N3768 · Boeing 737832 · Fuselage Main, Structure
  > CRACK ON AFT UPPER CORNER FRAME OF NO.1 LH WINDOW AT COCKPIT ON REFERENCE CARD 5311-2003. LH WINDOW FRAME AT COCKPIT WAS REPAIRED PER ER/A 619132-14AD.
- [SDR DALA2025101007396](https://openairdocs.org/sdr/DALA2025101007396.md): Window Frame · cracked · Oct 9, 2025 · N3768 · Boeing 737832 · Fuselage Main, Structure
  > CRACK WAS FOUND OF: 0.375IN LENGTH ON RH WINDOW FRAME RADIUS AREA IN REF. CARD 5311-2003. RH WINDOW FRAME WAS REPAIRED PER ER/A 619132-14ADTR REV, A.
- [SDR DALA2025101007395](https://openairdocs.org/sdr/DALA2025101007395.md): Plate · corroded · Oct 8, 2025 · N3768 · Boeing 737832 · Fuselage Miscellaneous Structure
  > CORROSION ON SIDE PLATE FLOOR STRUCTURE SUPPORT UPPER SURFACE (BILGE AREA) (STA 727 TO STA 727F+10)(STA 727F+10 TO STA 767) BTWN S26R AND S25R AND (STA 727 TO STA 727F +10)(STA 727F+10 TO STA 787+10) AND (STA 787+10 TO STA 847) BTWN S26L AND S25L CARGO COMPAR
- [SDR DALA2025101007393](https://openairdocs.org/sdr/DALA2025101007393.md): Plate · corroded · Oct 8, 2025 · N3768 · Boeing 737832 · Fuselage Miscellaneous Structure
  > CORROSION ON RT SIDEPLATE FROM STA 500A TO STA 500I AT FWD CARGO COMPARTMENT. SIDE PLATE STA 500A TO 500I WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025100907378](https://openairdocs.org/sdr/DALA2025100907378.md): Plate · corroded · Oct 7, 2025 · N3768 · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 1239881) CORROSION ON LH SIDEPLATE FROM STA 500 TO STA 500I AT FWD CARGO COMPARTMENT. LH SIDEPLATE FROM STA 500 TO STA 500I AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025100707297](https://openairdocs.org/sdr/DALA2025100707297.md): Skin · corroded · Oct 6, 2025 · N3768 · Boeing 737832 · Fuselage Main, Plate/Skin
  > (LOG 1237864) CORROSION ON CUT OUT OF FUSELAGE SKIN UNDER PAN (VACCUM WASTE TANK) BTW STA 847 TO 867 AND STGR 23LH-25LH AT AFT CARGO COMPARTMENT.
- [SDR DALA2025100607242](https://openairdocs.org/sdr/DALA2025100607242.md): Floor Support · corroded · Oct 4, 2025 · N3768 · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 1234689) CORROSION ON FLOOR SUPPORT STA 800,809,843 BETWEEN S26R TO DOOR JAMB (BILGIE AREA) CARGO COMPARMENT C2. CARGO COMPARMENT C2 WAS FABIRCATED AND REPLACED PER DWG 146A8128 REV. B AND B737-800 SRM 51-40-02-0G.
- [SDR DALA2025100607240](https://openairdocs.org/sdr/DALA2025100607240.md): Shield · corroded · Oct 4, 2025 · N3768 · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 1234618) CORROSION ON RH SHIELD BTW STA 847 TO 867 BTW STRG 25R/26R AT AFT CARGO COMPARMENT. RH SHIELD BTW STA 847 TO 867 BTW STRG 25R/26R AT AFT CARGO COMPARMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025100607239](https://openairdocs.org/sdr/DALA2025100607239.md): Skin · cracked · Oct 4, 2025 · N3768 · Boeing 737832 · Horizontal Stabilizer, Plate/Skin
  > CRACK ON LOWER SKIN STAB STA 101.90 AT LH HORIZONTAL STABILIZER. LOWER SKIN STAB STA 101.90 AT LH HORIZONTAL STABILIZER WAS REPAIRED PER B737-800 SRM 55-10-01-2R REPAIR 11.
- [SDR DALA2025100607243](https://openairdocs.org/sdr/DALA2025100607243.md): Frame · corroded · Oct 3, 2025 · N3768 · Boeing 737832 · Fuselage Main, Frame
  > (LOG 1232618) DURING CURRENT H CHECK AT TECHOPS MX QRO, WHILE ACCOMPLISHING BASE ZONAL INSPECTIONS, THE FUSELAGE FRAME WEB AT BSTA 847 FWD FACE WAS FOUND CORRODED BETWEEN S-25L AND S-26L. MAINTENANCE REPAIRED DAMAGER PER ERA 629195-14.
- [SDR DALA2025100607238](https://openairdocs.org/sdr/DALA2025100607238.md): Frame · corroded · Oct 3, 2025 · N3768 · Boeing 737832 · Fuselage Main, Frame
  > CORROSION ON FRAME OF STA 847 BTW STGR 25LH TO 24LH AT AFT CARGO COMPARTMENT. CORROSION ON FRAME OF STA 847 BTW STGR 25LH TO 24LH AT AFT CARGO COMPARTMENT WAS REPAIRED PER PRI 629195-14 REV. 2. AND ER/A 629195-14 REV. ORIGINAL.
- [SDR DALA2025100607237](https://openairdocs.org/sdr/DALA2025100607237.md): Door Sill · corroded · Oct 3, 2025 · N3768 · Boeing 737832 · Fuselage Main, Structure
  > CORROSION ON LOWER SILL CHORDS RH OF R2 DOOR BTW STA 986.5 TO STA 847 AT W2 ORIGINAL THICKNESS: 0.080 INCHES AND MINIMUM REMAINING THICKNESS IS 0.056 INCHES. THEREFORE, IS OUT LIMITS PER B737-800 SRM-53-70-15. LOWER SILL CHORDS RH OF R2 DOOR BTW STA 986.5 TO S
- [SDR DALA2025100607236](https://openairdocs.org/sdr/DALA2025100607236.md): Skin · corroded · Oct 3, 2025 · N3768 · Boeing 737832 · Fuselage Main, Plate/Skin
  > DURING H CHECK AT TECHOPS MX (QRO), WHILE ACCOMPLISHMENT OF TASK CARD 5300-2422, THE FUSELAGE SKIN WAS FOUND CORRODED AT LOWER FORWARD CORNER OF CUT OUT LAVATORY SERVICE ACCESS DOOR BETWEEN BSTA 847 AND BSTA 867 AND BETWEEN S-23L AND S-25L. MAINTENANCE REPAIRE
- [SDR DALA2025100307199](https://openairdocs.org/sdr/DALA2025100307199.md): Frame · corroded · Oct 3, 2025 · N3768 · Boeing 737832 · Fuselage Main, Frame
  > (LOG 1231613) CORROSION ON FRAME OF STA 907 BTW STGR 24LH TO STGR 23LH AT AFT CARGO COMPARTMENT. FRAME OF STA 907 BTW STGR 24LH TO STGR 23LH AT AFT CARGO COMPARTMENT WAS REPAIRED PER ER/A 629014-1 REV ORIGINAL. SECTION I: REPAIR INSTRUCTIONS AND PRI 629014-1 R
- [SDR DALA2025100307198](https://openairdocs.org/sdr/DALA2025100307198.md): Stringer · corroded · Oct 2, 2025 · N3768 · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 1231070) CORROSION ON STGR 25LH BTW STA 827 TO STA 847 AT AFT CARGO COMPARTMENT. STGR 25LH BTW STA 827 TO STA 847 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B737-800 SRM 53-00-03-2R PROCEDURE 1. REPAIR 1.
- [SDR DALA2025100307197](https://openairdocs.org/sdr/DALA2025100307197.md): Frame · damaged · Oct 2, 2025 · N3768 · Boeing 737832 · Fuselage Main, Frame
  > (LOG 1230927) PERFORM LEFT HAND STA 727 FRAME INNER CHORD 737 REPAIR; RII; SECTION 02. LEFT HAND STA 727 FRAME INNER CHORD 737 REPAIR; RII; SECTION 02 WAS PERFORMED IN ACCORDANCE AMDS 5311-01251-02A.
- [SDR DALA2025100307196](https://openairdocs.org/sdr/DALA2025100307196.md): Frame · damaged · Oct 2, 2025 · N3768 · Boeing 737832 · Fuselage Main, Frame
  > PERFORM RIGHT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02. RIGHT HAND STA 727 FRAME INNER CHORD 737 REPAIR; RII; SECTION 02 WAS PERFORMED IN ACCORDANCE AMDS 5311-01251-02B.
- [SDR DALA2025100207169](https://openairdocs.org/sdr/DALA2025100207169.md): Skin · cracked · Oct 2, 2025 · N3768 · Boeing 737832 · Horizontal Stabilizer, Plate/Skin
  > (LOG 1229629) CRACK (3 EAS) ON LOWER SKIN STAB STA 101.90, 138.70 AND 147.90 AT RH HORIZONTAL STABILIZER. LOWER SKIN STAB STA 101.90, 138.70 AND 147.90 AT RH HORIZONTAL STABILIZER WAS REPAIRED PER B737-800 SRM 55-10-01-2R PROCEDURE 11 REPAIR 11.
- [SDR DALA2025100207166](https://openairdocs.org/sdr/DALA2025100207166.md): Floor Support · corroded · Sep 28, 2025 · N3768 · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 1223364) CORROSION ON FLOOR STRUCTURE OF STA 947 AND RBL49 AT W2. FLOOR STRUCTURE (UPPER CORD) OF STA 947 AND RBL49 AT W2, WAS REPAIRED PER B737-800 SRM 53-70-51-2R PROCEDURE 5 REPAIR 5.
- [SDR DALA2025100207165](https://openairdocs.org/sdr/DALA2025100207165.md): Floor Support · corroded · Sep 28, 2025 · N3768 · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 1223162) CORROSION ON FLOOR SUPPORTS (2EAS) BTW STA 967 TO STA 987 OF RBL 18 AND LBL 18 (UPPER AND LOWER SURFACE) AT W2. FLOOR SUPPORTS (2EAS) BTW STA 967 TO STA 987 OF RBL 18 AND LBL 18 AT W2 WERE REPLACED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025093007089](https://openairdocs.org/sdr/DALA2025093007089.md): Floorbeam · corroded · Sep 25, 2025 · N3768 · Boeing 737832 · Fuselage Main, Floor Beam
  > (LOG 1218233) CORROSION ON FLOOR STRUCTURE (PREVIOUS REPAIR) OF STA 986.5 BTW RBL45 TO LBL45 (UPPER AND LOWER SURFACE) AT W2. FLOOR STRUCTURE (T-CHORD) OF STA 986.5 BTW RBL45 TO LBL45 (UPPER AND LOWER SURFACE) AT W2 WAS REPAIRED PER ER/A 585014-14 REV ORIGINAL
- [SDR DALA2025092907040](https://openairdocs.org/sdr/DALA2025092907040.md): Stringer · corroded · Sep 25, 2025 · N3768 · Boeing 737832 · Fuselage Main, Longeron/Stringer
  > (LOG 1217532) CORROSION ON STGR 24LH BTW STA 877 TO STA 897 AT AFT CARGO COMPARTMENT. STGR 24LH BTW STA 877 TO STA 897 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B737-800 SRM 53-00-03-2R PROCEDURE1 REPAIR 1.
- [SDR DALA2025092907037](https://openairdocs.org/sdr/DALA2025092907037.md): Floor Support · corroded · Sep 25, 2025 · N3768 · Boeing 737832 · Fuselage Miscellaneous Structure
  > (LOG 1216598) CORROSION ON FLOOR SUPPORTS (2EAS) BTW STA 947 TO STA 967 OF RBL 47 AND LBL47 (UPPER AND LOWER SURFACE) AT W2. FLOOR SUPPORTS (2EAS) BTW STA 947 TO STA 967 OF RBL 47 AND LBL47 (UPPER AND LOWER SURFACE) AT W2 WERE REPLACED PER B737-800 SRM 51-40-0
- [SDR DALA2025092907034](https://openairdocs.org/sdr/DALA2025092907034.md): Frame · cracked · Sep 23, 2025 · N3768 · Boeing 737832 · Fuselage Main, Frame
  > (LOG 1214060) CRACK ON FRAME STA 380 BTW STGR 7L TO 8L AT PAX CABIN. FRAME STA 380 BTW STGR 7L TO 8L AT PAX CABIN WAS REPAIRED PER B737-800 SRM 53-00-07-2R PROCEDURE 1 REPAIR 1.
- [SDR DALA2025092907029](https://openairdocs.org/sdr/DALA2025092907029.md): Seat Track · broken · Sep 23, 2025 · N3768 · Boeing 737832 · Fuselage, Seat/Cargo Attach Fittings
  > (LOG 1213723) BROKEN SEAT TRACK FROM STA 500C TO STA 500D LBL 24.75 AT PASSENGER CABIN. SEAT TRACK FROM STA 500C TO STA 500D LBL 24.75 AT PASSENGER CABIN WAS REPAIRED B737-800 SRM 53-00-52-2R PROCEDURE 4 REPAIR 4.
- [SDR DALA2025092306936](https://openairdocs.org/sdr/DALA2025092306936.md): Floor Support · corroded · Sep 22, 2025 · N3768 · Boeing 737832 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS BTW STA 312 TO 344 LBL12 AT CPAX. FLOOR SUPPORTS BTW STA 312 TO 344 LBL12 AT CPAX WERE REPLACED AND INSTALLED PER B737-800 SRM 51-40-02-0G.
- [SDR DALA2025091506759](https://openairdocs.org/sdr/DALA2025091506759.md): Floorbeam · corroded · Sep 13, 2025 · N3768 · Boeing 737832 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAMS STA 328 RBL50 AT CPAX. FLOOR BEAM STA 328 RBL50 AT CPAX PER WAS REPAIRED B737-800 SRM 53-10-51-2R PROCEDURE 8 REPAIR 8.
- [SDR DALA2025091506758](https://openairdocs.org/sdr/DALA2025091506758.md): Floorbeam · corroded · Sep 13, 2025 · N3768 · Boeing 737832 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAMS STA 294 BL0 AT CPAX. FLOOR BEAM STA 294 BL0 AT CPAX WAS REPAIRED PER B737-800 SRM 53-10-51-2R PROCEDURE 14 REPAIR 14.
- [SDR DALA2025091506757](https://openairdocs.org/sdr/DALA2025091506757.md): Skin · dented · Sep 12, 2025 · N3768 · Boeing 737832 · Fuselage Main, Plate/Skin
  > PERFORM REVALUATION OF DENT FUSELAGE SKIN SECTION 41 BTW STA 224.8/235.8 STGR 21-L/23-L". FUSELAGE SKIN SECTION 41 BTW STA 224.8/235.8 STGR 21-L/23-L WAS REPAIRED PER B737-800 SRM 53-10-01-2R PROCEDURE 8 REPAIR 8.

Next page: https://openairdocs.org/aircraft/N3768/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 = 'N3768' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N3768/reports

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