# Service difficulty reports: N732SW, cancelled Sep 16, 2024

A list on [N732SW, cancelled Sep 16, 2024](https://openairdocs.org/deregistered/N732SW-2024-09-16.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 8 · 363 reports

- [SDR SWAA2022122083606](https://openairdocs.org/sdr/SWAA2022122083606.md): Tray · dislodged · Dec 20, 2022 · N732SW · Boeing 7377H4 · Passenger Compartment Equipment
  > ROW 12D TRAY TABLE IS DISLOCATED FROM THE ATTACHMENT ARM. REATTACHED SEAT 12D TRAY TABLE TO ATTACHMENT ARM IAW CMM 25-21-42.
- [SDR SWAA2022120879553](https://openairdocs.org/sdr/SWAA2022120879553.md): Flap · disconnected · Dec 7, 2022 · N732SW · Boeing 7377H4 · Escape Slide
  > CREW REPORTS FWD SERVICE DOOR MOUNTED SLIDE YELLOW FLAP ON RT SIDE NOT ATTACHED TO Z FOLD CORRECTLY. INSTALLED YELLOW FLAP TO DOOR SLIDE Z FOLD IAW MM 25-66-01; WITH NO OTHER DEFECTS.
- [SDR SWAA2022081742366](https://openairdocs.org/sdr/SWAA2022081742366.md): Light · out of position · Aug 16, 2022 · N732SW · Boeing 7377H4 · Emergency Lighting
  > FRONT LEFT FLOOR PHOTO ILLUMINATION STRIP UNSTUCK FROM THE FLOOR / [01] RESECURED PHOTO ILLUMINATION STRIP PER CMM 25-00-66
- [SDR SWAA2022061317192](https://openairdocs.org/sdr/SWAA2022061317192.md): Circuit Breaker · popped · Jun 10, 2022 · N732SW · Boeing 7377H4 · Air Distribution System
  > SMOKE AND FUMES IN CABIN. QRH - SMOKE FIRE FUMES CHECK LIST COMPLETE. RETURN TO GATE / [01] C/W CONDITIONAL INSP AMM 05-51-56. FOUND RECIRC FAN CB POPPED. REF NONROUTINE TTG8Q00CYHKJ FOR FAN ASSY R&R
- [SDR SWAA2022051607382](https://openairdocs.org/sdr/SWAA2022051607382.md): Panel · cracked · May 12, 2022 · N732SW · Boeing 7377H4 · Aerodynamic Fairings
  > REF L/P 1995181; DAMAGE TO PANEL 194 GL; MINOR CRACK (2ND) / [01] COMBINED THIS MINOR CRACK INTO THE FIRST CRACK PER ENGINEERING AND SRM 53-60-70-1A-1 FIG 104
- [SDR SWAA2022051206327](https://openairdocs.org/sdr/SWAA2022051206327.md): Girt Bar · out of position · May 10, 2022 · N732SW · Boeing 7377H4 · Emergency Equipment
  > FWD SERVICE DOOR SLIDE GIRT BAR NEEDS TO BE RESECURED / [01] REPOSITIONED GIRT BAR PER MM25-66-01.
- [SDR SWAA2022032285430](https://openairdocs.org/sdr/SWAA2022032285430.md): Light · out of position · Mar 18, 2022 · N732SW · Boeing 737* · Emergency Lighting
  > RT. SIDE EMERGENCY EXIT LENS WONT STAY IN PLACE. / [01] REPLACED RT SIDE EMER. EXIT LIGHT ASSY PER AMM 33-51-04; CHECK GOOD.
- [SDR SWAA2022020868970](https://openairdocs.org/sdr/SWAA2022020868970.md): Light · failed · Feb 4, 2022 · N732SW · Boeing 737* · Emergency Lighting
  > F/O SIDE EXIT SIGN FELL OFF IN THE EXIT ROW.; / [01] RESECURED SIGN PER MM: 33-51-11.
- [SDR SWAA2022012462627](https://openairdocs.org/sdr/SWAA2022012462627.md): Light · inoperative · Jan 20, 2022 · N732SW · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY?S FAILED CAPACITY TEST AT LOCATIONS M1672; M1673; M1669; M1670; M1668; EMERGENCY LIGHT ATTERY?S FAILED CAPACITY TEST AT LOCATIONS M1672; M1673; M1669; M1670; M1668 / [01] REPLACED EMERGENCY LIGHT BATTERY?S AT LOCATIONS M1672; M1673; M1
- [SDR SWAA2022012462635](https://openairdocs.org/sdr/SWAA2022012462635.md): Seal · cracked · Jan 20, 2022 · N732SW · Boeing 7377H4 · Horizontal Stabilizer Structure
  > HORIZONTAL STABILIZER R/H UPPER SLIDER SEAL CRACKED. REMOVED AND REPLACED R/H FWD UPPER SLIDING SEAL PER AMM 53-31-31.
- [SDR SWAA2022012462634](https://openairdocs.org/sdr/SWAA2022012462634.md): Seal · cracked · Jan 20, 2022 · N732SW · Boeing 7377H4 · Horizontal Stabilizer Structure
  > HORIZONTAL STABILIZER L/H UPPER SLIDER SEAL CRACKED. REMOVED AND REPLACED L/H FWD UPPER SLIDING SEAL PER AMM 53-31-31
- [SDR SWAA2021111542799](https://openairdocs.org/sdr/SWAA2021111542799.md): Panel · cracked · Nov 11, 2021 · N732SW · Boeing 737* · Aerodynamic Fairings
  > FOUND 6 FASTENER HOLES WITH CRACKS.; FOND 6 FASTENER HOLES WITH CRACKS ON 194E PANEL. / [01] REPLACED 194E PANEL
- [SDR SWAA2021061679203](https://openairdocs.org/sdr/SWAA2021061679203.md): Support Web · corroded · Jun 1, 2021 · N732SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB FLOOR-TO-SIDEWALL SUPPORT WEB; BS 787-796; WL 160; / BLENDED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT WEB BS 787-792; RBL 22; WL 160. BLENDED 1'X1'X.020'; ORIGINAL THICKNESS IS.063'. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1.;INSTALL
- [SDR SWAA2021061679202](https://openairdocs.org/sdr/SWAA2021061679202.md): Web · corroded · Jun 1, 2021 · N732SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB FLOOR-TO-SIDEWALL SUPPORT WEB; BS 847-856; RBL 22; WL 160; / APPLIED A CHEMICAL CONVERSION COATING IAW SRM 51-20-01-0G-0 AND PRIMED NEW WEB IAW SOPM 20-41-02 AND DWG 146A8322; OK TO INSTALL;BLENDED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT W
- [SDR SWAA2021061778861](https://openairdocs.org/sdr/SWAA2021061778861.md): Gusset · cracked · May 31, 2021 · N732SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > GUSSET AT BS 500D COMMON TO STR22L LBL53 WL170 IS CRACKED; / ACCOMPLISHED STEP 8.;INSTALLED NEW GUSSET AT BS500D STR22L LBL53 WL170 IAW SRM 51-40-02 AND DWG #143A7902.;LOCATED; DRILLED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING AND PRIMERED NEW GUSSET AT
- [SDR SWAA2021061778860](https://openairdocs.org/sdr/SWAA2021061778860.md): Gusset · cracked · May 31, 2021 · N732SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > GUSSET AT BS 500D COMMON TO STR21L LBL58 WL178 IS CRACKED; / VERIFIED ALL WORK ACCOMPLISHED THIS CARD;VERIFIED INSTALLATION OF NEW GUSSET AT BS 500D STR-21L IAW SRM 51-40-02-0G-0 AND DWG 143A7902.;VERIFIED LOCATE AND DRILL OF NEW GUSSET AT BS 500D STR- 21L IA
- [SDR SWAA2021061778128](https://openairdocs.org/sdr/SWAA2021061778128.md): Gusset · cracked · May 29, 2021 · N732SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > GUSSET AT BS500D COMMON TO STR19R IS CRACKED AT RBL60 WL192; / CERTIFIED STEP 8;LOCATED AND DRILLED NEW GUSSET FOR BS 500D STR 19 RBL 60 WL 192 IAW SRM 51-40-05-0G-0 OK TO INSTALL;REMOVED AND REPLACED CRACK DAMAGED GUSSET AT BS 500D STR 19 RBL 60 WL 192 IAW S
- [SDR SWAA2021061778127](https://openairdocs.org/sdr/SWAA2021061778127.md): Gusset · cracked · May 29, 2021 · N732SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > GUSSET AT BS500D COMMON TO STR 19L IS CRACKED LBL 60; WL 192; / CERTIFIED FOR STEP 8;CORRECT STEP 7 APPLIED CIC TO REPAIR AREA IAW AMM 51-21-91-620-802;LOCATED AND DRILLED NEW GUSSET FOR BS 500D STR 19 LH WL 192 IAW SRM 51-40-05-0G-0 OK TO INSTALL;VERIFIED CO
- [SDR SWAA2021061775010](https://openairdocs.org/sdr/SWAA2021061775010.md): Support Angle · cracked · May 19, 2021 · N732SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED WATER TANK SUPPORT ANGLE TO BS 947 BULKHEAD SUPPORT AT BS 947 LBL 11 WL 178; / INSTALLED NEW WATER TANK BULKHEAD SUPPORT ANGLE BS 947; LBL 11; WL 178 IAW SRM 51-40-02-0G-0; DWG# 149A8103.;LOCATED AND DRILLED NEW WATER TANK SUPPORT ANGLE TO BS947 BULKH
- [SDR SWAA2021052474518](https://openairdocs.org/sdr/SWAA2021052474518.md): Support · corroded · May 19, 2021 · N732SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY AFT R/H BULKHEAD SUPPORT BS 947 RBL 24 WL 178; / EVALUATED CORROSION ON BULKHEAD SUPPORT BS 947 RBL 24 WL 178 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM. FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM REMOVED R/H BS 9
- [SDR SWAA2021061773362](https://openairdocs.org/sdr/SWAA2021061773362.md): Cargo Track · corroded · May 15, 2021 · N732SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RAIL AT AFT CARGO BAY BS927 RBL8 WL175. MARKED; / CORRECTION REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS927 RBL8 WL175 NOT BS754;REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS754 RBL8 WL175 IN A 2'X.90' AREA; ORIGINAL THICKNESS.063; REMAINING T
- [SDR SWAA2021061772876](https://openairdocs.org/sdr/SWAA2021061772876.md): Floor Support · corroded · May 13, 2021 · N732SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON INTERCOSTAL AT AFT CARGO BAY BS927- BS947 RBL13 WL172. MARKED; / INSTALLED NEW ACB INTERCOSTAL BS 927-947; LBL 13; WL 172 IAW SRM 51-40-02-0G-0; DWG# 147A7500;LOCATED; DRILLED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING; AND PRIMED NEW A
- [SDR SWAA2021061774086](https://openairdocs.org/sdr/SWAA2021061774086.md): Attach Angle · cracked · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage Main, Bulkhead
  > FWD SIDE OF BS 663 VAPOR BARRIER RH SIDE UPPER ATTACH ANGLE UPPER END CRACKED; / ACCOMPLISHED STEP 4 VERIFIED FASTENER INSTALLATION RII; COMPLETED ALL STEPS; VERIFIED EA IS COMPLETE (WIP 1)
- [SDR SWAA2021061772364](https://openairdocs.org/sdr/SWAA2021061772364.md): Cargo Track · cracked · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACKED TRACK AT AFT CARGO BAY BS727E LBL17 WL156.; / ASSIGNED PART TO JOB;EVALUATED CRACK ON CARGO TRACK BS 727E LBL 17 WL 156; CRACK FOUND TO BE 0.25 WITH ALLOWABLE DAMAGE OF 0.10. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;INSTALLED ACB CARGO TRACK BS
- [SDR SWAA2021061776938](https://openairdocs.org/sdr/SWAA2021061776938.md): Skin · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION AROUND FWD FASTENER HOLE OF ADF #1 ANTENNA; CORROSION ON ACFT SKIN AROUND FWD; CENTER; FASTENER HOLE; OF ADF #1 ANTENNA BS 674; RBL 4; WL 308 / COMPLETED STEPS 4-8; COMPLETED AMT STEPS OF 21-153-01387-WIP1 (N732 - ATS(PAE) - REPAIR - FUSELAGE CROWN
- [SDR SWAA2021061778126](https://openairdocs.org/sdr/SWAA2021061778126.md): Attach Angle · cracked · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage Main, Bulkhead
  > FWD SIDE OF BS 663 VAPOR BARRIER RH SIDE UPPER ATTACH ANGLE UPPER END CRACKED; / ACCOMPLISHED STEPS 1 AND 2; VERIFIED STEPS 1 AND 2.
- [SDR SWAA2021061772386](https://openairdocs.org/sdr/SWAA2021061772386.md): Angle · cracked · May 12, 2021 · N732SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > RIGHT WING T/E PNL JUST AFT OF #2 PYLON VERT ANGLE IS CRACKED.; / REMOVED AND REPLACED VERT ANGLE (FITTING; 115A2953-2) ON RIGHT WING T/E PANEL JUST AFT OF #2 PYLON IAW SRM 51-40-02-0G-0 PARA. 4 AND 9; AND AIPC 57-50-00-25.; VERIFIED REPLACEMENT OF VERT ANGLE
- [SDR SWAA2021061772381](https://openairdocs.org/sdr/SWAA2021061772381.md): Floor Support · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS727A+18 LBL3 WL150; / CORRECTED LOCATION 727A TO 727B;INSTALLED NEW INTERCOSTAL IN ACB BS727+18 LBL3 WL150 IAW SRM 51-40-02 AND DWG #146A7510.;LOCATED; DRILLED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING; AND PRI
- [SDR SWAA2021061772378](https://openairdocs.org/sdr/SWAA2021061772378.md): Cargo Track · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** ON RAIL AROUND FASTENER HOLE AT AFT CARGO BAY BS727+10 RBL3 WL156.; / REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS727+10 RBL3 WL156 IN A 2'X.90' AREA; ORIGINAL THICKNESS.063; REMAINING THICKNESS.055; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-
- [SDR SWAA2021061772377](https://openairdocs.org/sdr/SWAA2021061772377.md): Cargo Track · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TRACK TIEDOWN AT AFT CARGO BAY BS727B LBL17 WL156.; / REMOVED CORROSION ON TOP SURFACE OF TRACK TIE DOWN BS 727B LBL17 WL 156; REMOVED 0.025 FROM MAX ALLOWABLE OF 0.020 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DEPTH GAU
- [SDR SWAA2021061772376](https://openairdocs.org/sdr/SWAA2021061772376.md): Cargo Track · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TRACK TIEDOWN AT AFT CARGO BAY BS727A LBL17 WL156.; / REMOVED CORROSION ON TOP SURFACE OF TRACK TIE DOWN BS 727A LBL17 WL 156; REMOVED 0.025 FROM MAX ALLOWABLE OF 0.020 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DEPTH GAU
- [SDR SWAA2021061772375](https://openairdocs.org/sdr/SWAA2021061772375.md): Cargo Track · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RAIL AROUND FASTENER HOLE AT AFT CARGO BAY BS727B+3 LBL12 WL156.; / ADDING INSTALLATION REFERENCES TO STEP 10; ALSO USING DWG 146A7500 AND DWG 146A0061;CORRECTED LOCATION 727+4 TO 727B+10;ET INSPECTED CUT EDGE IAW 737 NDTM PART 6 51-00-00 PROCEDU
- [SDR SWAA2021061772373](https://openairdocs.org/sdr/SWAA2021061772373.md): Cargo Track · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TRACK TIEDOWN AT AFT CARGO BAY BS727D LBL17 WL156.; / REMOVED CORROSION ON TOP SURFACE OF TRACK TIE DOWN BS 727D LBL 17 WL 156; REMOVED 0.025 FROM MAX ALLOWABLE OF 0.020 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DEPTH GA
- [SDR SWAA2021061772372](https://openairdocs.org/sdr/SWAA2021061772372.md): Cargo Track · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RAIL AT AFT CARGO BAY BS754 LBL8 WL157.; / COMPLETE;ET INSPECTED TRIM IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED.<BR><BR>IS000450 N500D;FABRICATED REPAIR SECTION OF RAIL AT AFT CARGO BAY BS727E - BS747+12 LBL8 WL157; MADE FROM BAC
- [SDR SWAA2021061772371](https://openairdocs.org/sdr/SWAA2021061772371.md): Cargo Track · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RAIL AT AFT CARGO BAY BS754 RBL3 WL157.; / REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS754 RBL3 WL157 IN A 2'X.90' AREA; ORIGINAL THICKNESS.063; REMAINING THICKNESS.053; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4(A) 2 FIG.103 DEPTH
- [SDR SWAA2021061772369](https://openairdocs.org/sdr/SWAA2021061772369.md): Support · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727B - BS767 RBL21 WL157.; / CORRECTIVE ACTION 9 WAS ENTERED IN ERROR CERTIFIED WORK PERFORMED FOR CORRECTIVE ACTION 11;OK TO INSTALL ACB RH FLOOR TO SIDEWALL SUPPORT BS727 TO BS 767.;REMOVED CORROSION
- [SDR SWAA2021061772367](https://openairdocs.org/sdr/SWAA2021061772367.md): Cargo Track · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RAIL AT AFT CARGO BAY BS727D+6 RBL8 WL156.; / REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS727D+6 RBL8 WL156 IN A 2'X.90' AREA; ORIGINAL THICKNESS.063; REMAINING THICKNESS.051; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4(A) 2 FIG.103
- [SDR SWAA2021061772366](https://openairdocs.org/sdr/SWAA2021061772366.md): Cargo Track · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RAIL AT AFT CARGO BAY BS727D+6 RBL3 WL156.; / COMPLETE;ET INSPECTED TRIM IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED.<BR><BR>IS000450 N500D;INSTALLED RAIL SECTION AND SPLICE AT AFT CARGO BAY FROM BS727+4 - BS747+10 RBL3 WL156 IAW S
- [SDR SWAA2021061772363](https://openairdocs.org/sdr/SWAA2021061772363.md): Cargo Track · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RAIL AROUND FASTENER HOLE AT AFT CARGO BAY BS727E+3 RBL8 WL157.; / COMPLETED;ET INSPECTED TRIM IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED.<BR><BR>IS000450 N500D;INSTALLED RAIL SECTION AND SPLICES AT AFT CARGO BAY FROM BS727C+10 -
- [SDR SWAA2021061772362](https://openairdocs.org/sdr/SWAA2021061772362.md): Cargo Track · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TRACK TIEDOWN AT AFT CARGO BAY BS747 LBL17 WL157.; / REMOVED CORROSION ON TOP SURFACE OF TRACK TIE DOWN; REMOVED 0.025 FROM MAX ALLOWABLE OF 0.020 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DEPTH GAUGE ID ATS1225 S/N UNKN
- [SDR SWAA2021061771524](https://openairdocs.org/sdr/SWAA2021061771524.md): Skin · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION ON ACFT SKIN AROUND AFT LEFT FASTENER HOLE OF ADF # 1 ANTENNA; CORROSION ON ACFT SKIN AROUND AFT; LEFT; FASTENER HOLE OF ADF #1 ANTENNA; BS 702; RBL 3; WL 308 / EVALUATED DAMAGE REMOVAL ON FUSELAGE SKIN AT BS 702; RBL 3; WL 308. MAX DEPTH OF DAMAGE
- [SDR SWAA2021061771522](https://openairdocs.org/sdr/SWAA2021061771522.md): Skin · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION AROUND FWD FASTENER HOLE OF ADF #1 ANTENNA; CORROSION ON ACFT SKIN AROUND FWD; CENTER; FASTENER HOLE; OF ADF #1 ANTENNA BS 674; RBL 4; WL 308 / EVALUATED DAMAGE REMOVAL ON FUSELAGE SKIN AT BS 674; RBL 4; WL 308. MAX DEPTH OF DAMAGE REMOVAL FOUND TO
- [SDR SWAA2021061672382](https://openairdocs.org/sdr/SWAA2021061672382.md): Intercostal · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON INTERCOSTAL AT AFT CARGO BAY BS727A+2 LBL17 WL150; / INSTALLED NEW INTERCOSTAL IN ACB BS727A+2 LBL17 WL150 IAW SRM 51-40-02 AND DWG #146A7500.;LOCATED; DRILLED; AND DEBURRED NEW INTERCOSTAL AT BS 727A+2 LBL17 WL150 IAW SRM 51-40-05 AND DWG
- [SDR SWAA2021061672380](https://openairdocs.org/sdr/SWAA2021061672380.md): Intercostal · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON INTERCOSTAL AT AFT CARGO BAY BS727A+18 RBL3 WL150; / INSTALLED NEW INTERCOSTAL IN ACB BS727A+18 RBL3 WL150 IAW SRM 51-40-02 AND DWG #146A7510.;LOCATED; DRILLED; DEBURRED; AND APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-40-05 AND DWG #146
- [SDR SWAA2021061672379](https://openairdocs.org/sdr/SWAA2021061672379.md): Cargo Track · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** ON RAIL AROUND FASTENER HOLE AT AFT CARGO BAY BS727+13 RBL3 WL156.; / REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS727+13 RBL3 WL156 IN A 2'X.90' AREA; ORIGINAL THICKNESS.063; REMAINING THICKNESS.054; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-
- [SDR SWAA2021061672374](https://openairdocs.org/sdr/SWAA2021061672374.md): Attach Angle · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORROSION ON ATTACH ANGLE AT AFT CARGO BAY BS727D+10 RBL6 WL151.; / PRIMERED ATTACH ANGLE PER SRM 51-21-72-370-804; OK TO INSTALL.;REMOVED ATTACH ANGLE IN ACB BS727D+10 RBL6 WL151 IAW SRM 51-40-02.;REFERENCE ESR: 21-01944; FABRICATED ATTACH ANGLE BS 727D+ 10
- [SDR SWAA2021061672368](https://openairdocs.org/sdr/SWAA2021061672368.md): Attach Angle · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORROSION ON ATTACH ANGLE AT AFT CARGO BAY BS727D+10 LBL6 WL151.; / CORRECTION TO STEP 7; SHOULD BE AMM NOT SRM.;INSTALLED ATTACH ANGLE BS 727D+ 10; LBL 6;WL 151 PER SRM51-40-02-0G-0; DWG 146A7730.;PRIMERED ATTACH ANGLE PER SRM 51-21-72-370-804; OK TO INSTALL
- [SDR SWAA2021061672365](https://openairdocs.org/sdr/SWAA2021061672365.md): Cargo Track · corroded · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RAIL AT AFT CARGO BAY BS727D+6 LBL3 WL156.; / APPLIED CHEMICAL CONVERSION COATING AND PRIMERED REPAIR PARTS @ BS 727D+6 LBL3 WL156 IAW SRM 53-00-53-2-2R.;ET INSPECTED CUT EDGE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED.<BR><BR>CAL
- [SDR SWAA2021051772384](https://openairdocs.org/sdr/SWAA2021051772384.md): Attach Angle · cracked · May 12, 2021 · N732SW · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > FWD SIDE OF BS 663 VAPOR BARRIER RH SIDE UPPER ATTACH ANGLE UPPER END CRACKED. INSTALLED EWIS PROTECTION IAW AMM 20-60-07-913-801. REMOVED DAMAGE ON THE VAPOR BARRIER RH UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5. CONFORMED -1 REPLACEMENT ANGLE AND -2 SPLICE A
- [SDR SWAA2021081371513](https://openairdocs.org/sdr/SWAA2021081371513.md): Web · corroded · May 11, 2021 · N732SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON WEB AT AFT CARGO BAY BS809 RBL19 WL159.; / BS 847; RBL 19; WL 159 IAW SRM 51-40-02-0G-0.; [09] RECEIVED WEB PER P.O. #825119.; [10] VERIFIED STEP 9.; [11] RECEIVED WEB PER P.O. # 825689.; [12] LOCATED; DRILLED;DEBURRED WEB PER SRM 51-40-05

Next page: https://openairdocs.org/deregistered/N732SW-2024-09-16/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 = 'N732SW' AND deregistration_id = 'N732SW-2024-09-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N732SW-2024-09-16/reports

---
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.