# Service difficulty reports: N765SW

A list on [N765SW](https://openairdocs.org/aircraft/N765SW.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 7 · 303 reports

- [SDR SWAA2023082190977](https://openairdocs.org/sdr/SWAA2023082190977.md): Battery Pack · failed · Aug 18, 2023 · N765SW · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK AT LOCATION M1674 FAILED CAPACITY TEST<[01] R/R M1674 EMERGENCY BATTER PACK PER AMM 33-51-06;[02] ADD PART REMOVAL TO S/O
- [SDR SWAA2023072581652](https://openairdocs.org/sdr/SWAA2023072581652.md): Panel · cracked · Jul 22, 2023 · N765SW · Boeing 7377H4 · Aerodynamic Fairings
  > PANEL 193D CRACKED. CRACK MEASURED 3 IN LENGTH.<[01] REMOVED AND REPLACED FAIRING PANEL 193D PER AMM. 53-51-21.
- [SDR SWAA2023070573575](https://openairdocs.org/sdr/SWAA2023070573575.md): Bulb · inoperative · Jun 30, 2023 · N765SW · Boeing 7377H4 · Emergency Lighting
  > L/H AFT LOWER FUSELAGE EMER LIGHT INOP<[01] R&R L/H AFT LOWER FUSELAGE EMER LIGHT BULB PER AMM 33-51-04.OPS CHECK GOOD
- [SDR SWAA2022122284454](https://openairdocs.org/sdr/SWAA2022122284454.md): Lamp · inoperative · Dec 22, 2022 · N765SW · Boeing 7377H4 · Emergency Lighting
  > INOPERTIVE BULLNOSE EMERGENCY LIGHT 18DEF. RELAMPED PER AMM 33-51-03
- [SDR SWAA2022102462884](https://openairdocs.org/sdr/SWAA2022102462884.md): Flashlight · inoperative · Oct 21, 2022 · N765SW · Boeing 7377H4 · Emergency Equipment
  > FWD GALLEY FLASHLIGHT INOP / [01] REMOVED AND REPLACED FLUSH LIGHT IAW AMM 25-64-00;[02] REMOVED AND REPLACED FLASH LIGHT IAW AMM 25-64-00;[03] REMOVED AN REPLACED FLIS=H LIGHT IAW AMM 25-64-00
- [SDR SWAA2022101258449](https://openairdocs.org/sdr/SWAA2022101258449.md): None · inoperative · Oct 11, 2022 · N765SW · Boeing 7377H4 · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED FWD RH (M1674) BATTERY AND BATTERY CHARGER PACK ASSEMBLY IN REFERENCE TO AMM 33-51-06. OPS CHECK GOOD AT THIS TIME.
- [SDR SWAA2022090649818](https://openairdocs.org/sdr/SWAA2022090649818.md): None · out of position · Sep 3, 2022 · N765SW · Boeing 7377H4 · Emergency Lighting
  > FWD SERVICE SIDE EMERGENCY EXIT LENSE FELL OFF / [01] OK TO CONT PER MEL 25-10-01 SP1B<BR>AUTH#86171;[02] RE-SECURED FWD SERVICE DOOR EMERGENCY EXIT LENSE PER SIP
- [SDR SWAA2022081843182](https://openairdocs.org/sdr/SWAA2022081843182.md): Panel · delaminated · Aug 18, 2022 · N765SW · Boeing 7377H4 · Aerodynamic Fairings
  > PANEL 193 B HAS WORN/DELAMINATED AREAS AT FASTENER HOLE LOCATIONS 6; 8; 10; 11; 13; 14; 17; 22; 33; AND 34. PANEL 193 B HAS WORN/DELAMINATED AREAS AT FASTENER HOLE LOCATIONS 6 8 10 11 13 14 17 22 33 AND 34. / [01] R/R 193B PANEL IAW AMM 53-51-21.
- [SDR SWAA2022080137105](https://openairdocs.org/sdr/SWAA2022080137105.md): O-Ring · leaking · Jul 30, 2022 · N765SW · Boeing 7377H4 · Hydraulic System, Main
  > DURING FLIGHT AT 29K FEET WE LOST HYDRAULIC SYS B FLUID WENT TO ZERO AND TOTAL LOSS OF PRESSURE / [01] REF TTG8Q00DVGLL ALT BRAKE SELECTOR VALVE LEAKING. MT 729-PPRD-01-01 HYDRO SYSTEM FLUSH / FILTER R/R B SYSTEM. NO METAL OR DEBRIS NOTED. TTG8Q00DVGR3 ' B ' E
- [SDR SWAA2022080136782](https://openairdocs.org/sdr/SWAA2022080136782.md): Selector Valve · leaking · Jul 30, 2022 · N765SW · Boeing 7377H4 · Hydraulic System, Main
  > DURING FLIGHT AT 29K FEET WE LOST HYDRAULIC SYS B FLUID WENT TO ZERO AND TOTAL LOSS OF PRESSURE / [01] REF TTG8Q00DVGLL ALT BRAKE SELECTOR VALVE LEAKING. MT 729-PPRD-01-01 HYDRO SYSTEM FLUSH / FILTER R/R B SYSTEM. NO METAL OR DEBRIS NOTED. TTG8Q00DVGR3 ' B ' E
- [SDR SWAA2022080137104](https://openairdocs.org/sdr/SWAA2022080137104.md): Selector Valve · leaking · Jul 30, 2022 · N765SW · Boeing 7377H4 · Hydraulic System, Main
  > DURING FLIGHT AT 29K FEET WE LOST HYDRAULIC SYS B FLUID WENT TO ZERO AND TOTAL LOSS OF PRESSURE / [01] REF TTG8Q00DVGLL ALT BRAKE SELECTOR VALVE LEAKING. MT 729-PPRD-01-01 HYDRO SYSTEM FLUSH / FILTER R/R B SYSTEM. NO METAL OR DEBRIS NOTED. TTG8Q00DVGR3 ' B ' E
- [SDR SWAA2022070524810](https://openairdocs.org/sdr/SWAA2022070524810.md): Light · loose · Jul 1, 2022 · N765SW · Boeing 7377H4 · Emergency Lighting
  > EXIT LIGHT COVER FELL OFF ON TAKEOFF (MIDDLE OF AIRCRAFT). WILL NOT STAY SECURED. / [01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW MM 33-51-01. OPS A CHECK GOOD.
- [SDR SWAA2022040690679](https://openairdocs.org/sdr/SWAA2022040690679.md): Light · failed · Apr 2, 2022 · N765SW · Boeing 7377H4 · Emergency Lighting
  > FWD OVERHEAD EXIT SIGN FELL OFF / [01] SECURED LENS PER SIP/AMM 33-51-01. OK FOR SERVICE
- [SDR SWAA2022010457003](https://openairdocs.org/sdr/SWAA2022010457003.md): Battery Pack · inoperative · Dec 30, 2021 · N765SW · Boeing 7377H4 · Emergency Lighting
  > INOP BATTERY EMERGENCY LIGHT AFT GALLEY AREA RH; 2021-549938 / [01] REPLACED BATTERY PACK ON AFT GALLEY AREA ON RH SIDE P/N OFF: D717-01-100SWA S/N OFF: 19023 P/N ON: D717-01-100SWA S/N ON: 310687 AND PERFORMED OPERATIONAL TEST OF THE NEW BATTERY PACK IAW B73
- [SDR SWAA2022010452051](https://openairdocs.org/sdr/SWAA2022010452051.md): Shock Mount · broken · Dec 10, 2021 · N765SW · Boeing 7377H4 · Escape Slide
  > BROKEN FWD SERVICE DOOR SLIDE SHOCK MOUNT AT PASSENGER CABIN (1 EA); 2021-549919 / [01] REPLACED SLIDE SHOCK MOUNT LOC. FWD SERVICE DOOR AT PASSENGER CABIN (1 EA) I.A.W B737-700 SRM 51-40-02 AND 51-10-02 PARAGRAPH 9; [02] CERTIFIED WORK PERFORMED
- [SDR SWAA2022010451586](https://openairdocs.org/sdr/SWAA2022010451586.md): Gusset · cracked · Dec 8, 2021 · N765SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK GUSSET LOCATED BS 500D STR 19R FWD CARGO COMPARTMENT. REPLACED GUSSET LOCATED BS 500D STR 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. DGW: 143A7902 REV: E.
- [SDR SWAA2022010451587](https://openairdocs.org/sdr/SWAA2022010451587.md): Gusset · cracked · Dec 8, 2021 · N765SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK GUSSET LOCATED BS 500D STR 19L FWD CARGO COMPARTMENT; 2021-549916 / [01] REPLACED GUSSET LOCATED BS 500D STR 19L FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02-0G-0 STEP9 AND DWG 143A7902 REV:E. PART USED P/N: 143A9481-6. P/0: 2021-118586. SEE INDIVID
- [SDR SWAA2022010450232](https://openairdocs.org/sdr/SWAA2022010450232.md): Web · corroded · Dec 4, 2021 · N765SW · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION WEB LOCATED BS196.5 TO BS203.8 AND LBL 9; WL148.5 AT LOWER FUSELAGE; 2021-549878 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 21-JAN-22; TEMPERATURE CHART RECORD P/N: KT8P2; S/N: 19021963; DUE DATE: 14-MAY
- [SDR SWAA2022010549814](https://openairdocs.org/sdr/SWAA2022010549814.md): None · cracked · Dec 3, 2021 · N765SW · Boeing 737 · Horizontal Stabilizer, Spar/Rib
  > SUPPLEMENTAL INFORMATION: CRACK INSPAR RIB LOC STAB STA 129.50 AT 35 INCH FROM FRONT SPART LT HORIZONTAL STAB (1 E/A); 2021-549836 / [01] TOOL USED. EDDY CURRENT EQUIPMENT. P/N: NORTEC 500D. S/N: N500X12101V022233. DUE DATE: 02-JUN-22.; [02] TOOL USED: EDDY C
- [SDR SWAA2022010550229](https://openairdocs.org/sdr/SWAA2022010550229.md): Access Panel · cracked · Dec 3, 2021 · N765SW · Boeing 737 · Wing Miscellaneous Structure
  > SUPPLEMENTAL INFORMATION: CRACK ACCESS PANEL 651GB CORRUGATED PLATE AT RT WING; 2021-549847 / [01] REPLACED CORRUGATED PLATE ON ACCESS PANEL 651GB AT RT WING. I.A.W B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 115A2001 REV:A SHEET 7; [02] INSTALLED CORRUGAT
- [SDR SWAA2022010549976](https://openairdocs.org/sdr/SWAA2022010549976.md): Stringer · cracked · Dec 3, 2021 · N765SW · Boeing 737 · Wing, Longeron/Stringer
  > SUPPLEMENTAL INFORMATION: CRACK INTERNAL CAVITY STRINGER U-8 UPPER SURFACE BETWEEN RIB 19 TO RIB 20 AT LT WING; 2021-549843 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020. DUE DATE: 21-JAN-22.; [02] PERFORMED REPAIR UPPER STRING
- [SDR SWAA2022010549598](https://openairdocs.org/sdr/SWAA2022010549598.md): Access Panel · cracked · Dec 2, 2021 · N765SW · Boeing 737 · Wing Miscellaneous Structure
  > SUPPLEMENTAL INFORMATION: CRACK ACCESS PANEL 532NB FUEL TANK FLOAT AT LT WING; 2021-549811 / [01] FAULT RESOLVED ON OTHER FAULT REPLACED FUEL TANK FLOAT ON ACCESS PANEL 532NB AT LT WING ON TTG8Q009MYPM; [02] TASK CARD COMPLETED
- [SDR SWAA2022010549813](https://openairdocs.org/sdr/SWAA2022010549813.md): Rib · cracked · Dec 2, 2021 · N765SW · Boeing 7377H4 · Vertical Stabilizer, Spar/Rib
  > CRACK DORSAL FIN RIB 8 AT VERTICAL STABILIZER; 2021-549833 / [01] REPLACED RIB 8 AND FASTENERS LOC. DORSAL FIN AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 174A1008 SHEET 2 REV.C. REPLACED RIB 8 AND FASTENERS LOC. DORSAL FIN AT VERTICAL STABILIZE
- [SDR SWAA2022010449600](https://openairdocs.org/sdr/SWAA2022010449600.md): Angle · cracked · Dec 2, 2021 · N765SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK ANGLE - CLIP LOCATED ON BS 500C AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT; 2021-549817 / [01] REPLACED CLIP AND FASTENERS LOCATED ON BS 500C AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02. DGW: 143A7505 REV: A.; [
- [SDR SWAA2022010449601](https://openairdocs.org/sdr/SWAA2022010449601.md): None · cracked · Dec 2, 2021 · N765SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOC ON BS 400 AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT; 2021-549819 / [01] REPLACED CLIP AND FASTENERS LOC ON BS 400 AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. DWG: 143A7505 REV: B; [02] REPLACED
- [SDR SWAA2022010449812](https://openairdocs.org/sdr/SWAA2022010449812.md): Support · corroded · Dec 2, 2021 · N765SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 AT LEVEL STR 25R RBL 21 AT AFT CARGO COMPARTMENT; 2021-549830 / [01] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 AT LEVEL STR 25R RBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A75
- [SDR SWAA2022010549416](https://openairdocs.org/sdr/SWAA2022010549416.md): None · cracked · Dec 1, 2021 · N765SW · Boeing 737 · Fuselage Miscellaneous Structure
  > SUPPLEMENTAL INFORMATION: CRACK FLOOR STRUCTURE PLATE LOCATED ON BS 540 BTW BL 0 TO LBL 25 AT PASSENGER CABIN; 2021-549793 / [01] REPLACED FLOOR STRUCTURE PLATE LOCATED ON BS 540 BTW BL 0 TO LBL 25 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-40-02;SRM 51-10-02
- [SDR SWAA2022010549415](https://openairdocs.org/sdr/SWAA2022010549415.md): Plate · cracked · Dec 1, 2021 · N765SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FLOOR STRUCTURE PLATE LOCATED ON BS 540 BTW BL 0 TO RBL 25 AT PASSENGER CABIN; 2021-549792 / [01] REPLACED FLOOR STRUCTURE PLATE LOCATED ON BS 540 BTW BL 0 TO RBL 25 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DWG 143A0060;
- [SDR SWAA2022010449414](https://openairdocs.org/sdr/SWAA2022010449414.md): Stringer · corroded · Dec 1, 2021 · N765SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 23L BS 540 AT WL 164 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR STRINGER 23L BETWEEN BS500D TO BS540 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1; REPAIR 1 FIG 206.
- [SDR SWAA2022010449413](https://openairdocs.org/sdr/SWAA2022010449413.md): Stringer · corroded · Dec 1, 2021 · N765SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 26L LOCATED ON BS 540 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR STRINGER 26L BETWEEN BS500D TO BS540 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1.
- [SDR SWAA2022010549024](https://openairdocs.org/sdr/SWAA2022010549024.md): Plate · broken · Nov 30, 2021 · N765SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > BROKEN TRAILING EDGE CORRUGATED PLATE LOCATED WS180.00 INTERNAL AREA OF ACCESS PANEL 651EB AT RT WING; 2021-549676 / [01] REPLACED CORRUGATED PLATE LOCATED WS180.00 INTERNAL AREA OF ACCESS PANEL 651EB AT RT WING. I.A.W B737-700 SRM 51-40-02; 51-10-02 ITEM 9 A
- [SDR SWAA2022010549025](https://openairdocs.org/sdr/SWAA2022010549025.md): Plate · broken · Nov 30, 2021 · N765SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > BROKEN TRAILING EDGE CORRUGATED PLATE LOCATED WS204.25 INTERNAL AREA OF ACCESS PANEL 651EB AT RT WING; 2021-549674 / [01] REPLACED CORRUGATED PLATE LOCATED WS204.25 INTERNAL AREA OF ACCESS PANEL 651EB AT RT WING. IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND
- [SDR SWAA2022010549030](https://openairdocs.org/sdr/SWAA2022010549030.md): Bracket · broken · Nov 30, 2021 · N765SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > BROKEN SUPPORT BRACKET LOCATED IRSS140 REAR SPAR UPPER AREA AT LT WING; 2021-549710 / [01] REPLACED SUPPORT BRACKET LOCATED IRSS140 REAR SPAR UPPER AREA AT LT WING IAW B737-700 SRM 51-10-02-0G-0 STEP 9; [02] TASK COMPLETED
- [SDR SWAA2022010549032](https://openairdocs.org/sdr/SWAA2022010549032.md): Angle · broken · Nov 30, 2021 · N765SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > BROKEN ANGLE TRAILING EDGE LOCATED ORSS174 REAR SPAR UPPER AREA AT RT WING; 2021-549722 / [01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS174 REAR SPAR UPPER AREA AT RT WING I.A.W B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 SEE INDIVIDUAL SIGNOFFS BELOW.
- [SDR SWAA2022010449027](https://openairdocs.org/sdr/SWAA2022010449027.md): Stringer · cracked · Nov 30, 2021 · N765SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER 26R, AT BS 540 IN FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR STRINGER 26R LOCATED BTW BS500D TO BS540 IAW SRM B737-700 53-00-03-2R-1 REPAIR 1.
- [SDR SWAA2022010449026](https://openairdocs.org/sdr/SWAA2022010449026.md): Stringer · cracked · Nov 30, 2021 · N765SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 24R LOCATED AT BS 540 AND WL 160 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR STRINGER 24R BETWEEN BS500D TO BS540 AND WL 160 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1.
- [SDR SWAA2022010449029](https://openairdocs.org/sdr/SWAA2022010449029.md): Stringer · corroded · Nov 30, 2021 · N765SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 25R AT BS 540 AND WL 156 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR LOCATED STRINGER 25R BETWEEN BS500C TO BS540 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1.
- [SDR SWAA2022010449023](https://openairdocs.org/sdr/SWAA2022010449023.md): Stringer · corroded · Nov 30, 2021 · N765SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 22R LOCATED AT BS 540 AND WL 168 AT FWD CARGO COMPARTMENT; 2021-549688. PERFORMED PERMANENT REPAIR LOCATED STRINGER 22R BETWEEN BS500C TO BS540 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1.
- [SDR SWAA2022010449022](https://openairdocs.org/sdr/SWAA2022010449022.md): Stringer · corroded · Nov 30, 2021 · N765SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 23R LOCATED AT BS 540. WL164 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR STRINGER 23R BETWEEN BS500D TO BS540 WL154 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1.
- [SDR SWAA2022010548687](https://openairdocs.org/sdr/SWAA2022010548687.md): Access Panel · cracked · Nov 29, 2021 · N765SW · Boeing 7377H4 · Wing, Control Surfaces
  > CRACK ACCESS PANEL 561AB HOLES AT LT WING; 2021-549546 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: 15331932; DUE DATE: 26-OCT-22; [02] HOT BONDER PN: HCS9200B-AV; SN: 18196021; DUE DATE: 14/DEC/21.; [03] SCALE P/N: 1863T62; S/N: AE-40571; DUE DATE: 19-MAY-22
- [SDR SWAA2022010548688](https://openairdocs.org/sdr/SWAA2022010548688.md): Access Panel · cracked · Nov 29, 2021 · N765SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ACCESS PANEL 561BB HOLES AT LT WING; 2021-549549 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: 15331932; DUE DATE: 26-OCT-22; [02] HOT BONDER PN: HCS9200B-AV; SN: 18196021; DUE DATE: 14/DEC/21.; [03] SCALE P/N: 1863T62; S/N: AE-40571; DUE DATE: 19-MAY-22
- [SDR SWAA2022010548179](https://openairdocs.org/sdr/SWAA2022010548179.md): Support Angle · cracked · Nov 28, 2021 · N765SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BS695 AND RBL24.75 LOWER POSITION CENTER SECTION; 2021-549498 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22 TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE:
- [SDR SWAA2022010548182](https://openairdocs.org/sdr/SWAA2022010548182.md): Support Angle · cracked · Nov 28, 2021 · N765SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BS695 AND LBL24.75 LOWER POSITION CENTER SECTION; 2021-549500 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE 22 JAN 22; P/N P3015GOES00000 S/N 112820025 DUE DATE 22 JAN 22.; [02] REPLACED SUPPORT
- [SDR SWAA2022010448177](https://openairdocs.org/sdr/SWAA2022010448177.md): Support Angle · cracked · Nov 28, 2021 · N765SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BS695 AND BL0 LH SIDE CENTER SECTION; 2021-549495 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22 TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.;
- [SDR SWAA2022010448181](https://openairdocs.org/sdr/SWAA2022010448181.md): Support Angle · cracked · Nov 28, 2021 · N765SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BS695 AND BL0 RH SIDE CENTER SECTION; 2021-549493. REPLACED SUPPORT ANGLE LOCATED BS695 AND BL0 RH SIDE CENTER SECTION I.A.W B737-700 SRM 51-40-02 AND DWG 273A9110; SHEET 5; REV A; [03] VERIFIED TASK COMPLETE. TASK RII.
- [SDR SWAA2022010448185](https://openairdocs.org/sdr/SWAA2022010448185.md): Support Angle · cracked · Nov 28, 2021 · N765SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BS695 AND RBL24.75 VERTICAL POSITION CENTER SECTION; 2021-549502. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS695 AND RBL24.75 VERTICAL POSITION CENTER SECTION I.A.W. B737-700 SRM 51-10-02 AND DWG 111A6002; SHEET 10; REV. A.; R
- [SDR SWAA2022010448176](https://openairdocs.org/sdr/SWAA2022010448176.md): Scuff Plate · cracked · Nov 28, 2021 · N765SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON AFT CORNER SCUFF PLATE LOCATED BS 492 AT FWD CARGO COMPARTMENT; 2021-549491 / [01] TOOL USED; DIGITAL CALIPER P/N:500-197-30 S/N:A21142022 DUE DATE: 02-OCT-22.; [02] REPAIRED BY WELDING AFT CORNER SCUFF PLATE LOCATED BS 492 AT FWD CARGO COMPARTMENT I
- [SDR SWAA2022010448178](https://openairdocs.org/sdr/SWAA2022010448178.md): Scuff Plate · cracked · Nov 28, 2021 · N765SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON FWD CORNER SCUFF PLATE LOCATED BS 440 AT FWD CARGO COMPARTMENT; 2021-549494 / [01] TOOL USED; DIGITAL CALIPER; P/N:500-197-30 S/N:A21142022 DUE DATE:02-OCT-22.; [02] REPAIRED BY WELDING FWD CORNER SCUFF PLATE LOCATED BS 440 AT FWD CARGO COMPARTMENT I
- [SDR SWAA2022010448186](https://openairdocs.org/sdr/SWAA2022010448186.md): Scuff Plate · cracked · Nov 28, 2021 · N765SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON AFT CORNER SCUFF PLATE LOCATED BS 847 AT AFT CARGO BAY. REPAIRED BY WELDING AFT CORNER SCUFF PLATE LOCATED BS 847 AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1.
- [SDR SWAA2021120248183](https://openairdocs.org/sdr/SWAA2021120248183.md): Scuff Plate · cracked · Nov 28, 2021 · N765SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON FWD CORNER SCUFF PLATE LOCATED BS 792 AT AFT CARGO BAY. REPAIRED BY WELDING FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1.

Next page: https://openairdocs.org/aircraft/N765SW/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 = 'N765SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N765SW/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.
