# Service difficulty reports: N774SW, cancelled Oct 4, 2024

A list on [N774SW, cancelled Oct 4, 2024](https://openairdocs.org/deregistered/N774SW-2024-10-04.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 6 · 290 reports

- [SDR SWAA2022121381038](https://openairdocs.org/sdr/SWAA2022121381038.md): Panel · damaged · Dec 13, 2022 · N774SW · Boeing 7377H4 · Aerodynamic Fairings
  > WING TO BODY FAIRING PANEL 193B HAS ELONGATED & CRACKED HOLES. R & R THE FAIRING PANEL 193B IAW AMM.53-51-21.
- [SDR SWAA2022060614177](https://openairdocs.org/sdr/SWAA2022060614177.md): Light · inoperative · Jun 1, 2022 · N774SW · Boeing 7377H4 · Emergency Lighting
  > FO SIDE EMERGENCY EXIT WINDOW LIGHT INOP (WING) / [01] OK TO CONTINUE PER MEL 33-2-03 SP1B C/W. R AND R BULB AND FUSE FO SIDE EMERGENCY EXIT WINDOW LIGHT IAW AMM 33-51-04
- [SDR SWAA2022052509394](https://openairdocs.org/sdr/SWAA2022052509394.md): Bracket · cracked · May 19, 2022 · N774SW · Boeing 7377H4 · Trailing Edge Flaps
  > I/B T/E SUPPORT BRACKET FOR PANEL 551EB L/H WING IS CRACK. / [01] REMOVED I/B TRAILING EDGE SUPPORT BRACKET FOR ACCESS PANEL 551 EB AS PER BOEING 737 SRM 51-40-02;[02] VERIFIED STEP 1.;[03] CORRECTION: REMOVED AND REPLACED I/B TRAILING EDGE SUPPORT BRACKET(CLI
- [SDR SWAA2022052509215](https://openairdocs.org/sdr/SWAA2022052509215.md): Girt Lacing · out of adjust · May 18, 2022 · N774SW · Boeing 7377H4 · Escape Slide
  > CUSTOMER REQUEST- L1 DOOR SLIDE HAS EXCESSIVE GIRT HANGING DOWN. / [01] READJUSTED L1 DOOR SLIDE GIRT REF B737 AMM 25-66-01-400-803;[02] VERIFIED 1;COMPLETE
- [SDR SWAA2022052508857](https://openairdocs.org/sdr/SWAA2022052508857.md): Angle · cracked · May 17, 2022 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > SUPPORT ANGLE AT VAPOR BARRIER LH STA 663 CRACKED / [01] LOCATED AND DRILLED NEW SUPPORT ANGLE AT VAPOR BARRIER L/H STA 663 PER REF B737-700 SRM51-40-05-0G-0.;[02] VERIFIED STEP 1. OK TO TREAT AND PRIMER.;[03] TREATED AND PRIMED NEW HOLES ON NEW ANGLE PER REF
- [SDR SWAA2022052508625](https://openairdocs.org/sdr/SWAA2022052508625.md): Vapor Barrier · cracked · May 14, 2022 · N774SW · Boeing 7377H4 · Wing Main, Frame Structure
  > L/H STA 663 VAPOR BARRIER CRACKED AT LBL 10 LOWER CORNER. STOP DRILL CRACK AS PER B737 SRM 51-70-04-2R-10; ACCOMPLISH DRY OUT ON DAMAGE AREA OF L/H VAPOR BARRIER FOUND NO WATER AS PER B737 SRM 51-70-04-2R-0 SECTION 4-D-9; REPAIRED 9' CRACK ON THE L/H VAPOR BAR
- [SDR SWAA2021111643351](https://openairdocs.org/sdr/SWAA2021111643351.md): Lens · broken · Nov 12, 2021 · N774SW · Boeing 737* · Emergency Lighting
  > CUSTOMER WALK: FORWARD CABIN EMERGENCY EXIT LENS FALLING WONT STAY UP CLIP LOCK BROKEN.; / [01] SECURED FORWARD CABIN EMERGENCY EXIT LENS AS PER B737 AMM 33-51-01-960-801; [02] STEP 1 VERIFIED
- [SDR SWAA2021111642174](https://openairdocs.org/sdr/SWAA2021111642174.md): Slide · out of position · Nov 10, 2021 · N774SW · Boeing 737* · Escape Slide
  > R2 DOOR SIDE SCURT TOUCHING SCUFF PLATE WHEN CLOSED; / [01] REPOSITIONED R2 DOOR SLIDE SKIRT PER B737 AMM 25-66-01-400-803; [02] VERIFIED STEP 1.
- [SDR SWAA2021111542172](https://openairdocs.org/sdr/SWAA2021111542172.md): Scuff Plate · cracked · Nov 10, 2021 · N774SW · Boeing 737* · Fuselage Miscellaneous Structure
  > AFT CARGO CENTER SCUFF PLATE CRACKED; AFT CARGO CENTER SCFF PLATE CRACKED / [01] RECEIVED NEW SCUFF PLATE PART #146A8342-8 TO BE INSTALLED ON WORK ORDER #TTG8Q0032BDK; [02] VERIFIED STEP # 1.
- [SDR SWAA2021111641203](https://openairdocs.org/sdr/SWAA2021111641203.md): Light · inoperative · Nov 7, 2021 · N774SW · Boeing 737* · Emergency Lighting
  > R1 DOOR EXTERIOR EMERGENCY LIGHT INOP.; / [01] RELAMPED R1 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF. B737 AMM 33-51-04-960-801. TEST OK; [02] VERIFIED STEP 1.
- [SDR SWAA2021111641206](https://openairdocs.org/sdr/SWAA2021111641206.md): None · missing · Nov 7, 2021 · N774SW · Boeing 737* · Emergency Lighting
  > EMERGENCY EXIT SIGN LENS MISSING AT G4 GALLEY; / [01] REPLACED EMERGENCY EXIT SIGN LIGHT ASSEMBLY AND PERFORMED TEST FOR NEW ASSEMBLY AS PER B737 AMM 33-51-01960-802. TEST OK.; [02] VERIFIED STEP 1
- [SDR SWAA2021111641197](https://openairdocs.org/sdr/SWAA2021111641197.md): Skin · inoperative · Nov 6, 2021 · N774SW · Boeing 737* · Emergency Lighting
  > L2 DOOR LOWER EMERGENCY INDICATOR EXIT SIGN INOP.; / [01] PERFORMED BATTERY PACK REPLACEMENT AT M1673 L2 DOOR (S/N ON: 36688); AND ACCOMPLISHED OPS CHECK AS PER B737 AMM 33-51-06-960-805; TEST FOUND NORMAL.; [02] VERIFIED COMPLETE
- [SDR SWAA2021111641198](https://openairdocs.org/sdr/SWAA2021111641198.md): Light · inoperative · Nov 6, 2021 · N774SW · Boeing 737* · Emergency Lighting
  > EMERGENCY OVERHEAD BIN LIGHTS INOP AT POSITIONS: 14L/H THRU 23L/H AND 22R/H.; / [01] WORK TO BE ACCOMPLISHED IN ITEM TTG8Q0096A91; OPS CHECK FOUND NORMAL AS PER B737 AMM 33-51-06-960-805.; [02] VERIFIED
- [SDR SWAA2021111641199](https://openairdocs.org/sdr/SWAA2021111641199.md): Light · inoperative · Nov 6, 2021 · N774SW · Boeing 737* · Emergency Lighting
  > L2 DOOR EXTERIOR EMERGENCY LIGHT INOP.; / [01] WORK TO BE ACCOMPLISHED IN ITEM TTG8Q009A91; OPS CHECK FOUND NORMAL AS PER B737 AMM 33-51-06-960-805.; [02] VERIFIED
- [SDR SWAA2021111641201](https://openairdocs.org/sdr/SWAA2021111641201.md): Sign · burned out · Nov 6, 2021 · N774SW · Boeing 737* · Emergency Lighting
  > R/H OVER-WING EMERGENCY EXIT INDICATOR SIGN HAS 1 BULB BURNED OUT.; / [01] REPLACED EXIT SIGN; LAMP AT R/H OVER WING INDICATOR; AS PER B737 AMM 33-51-01-960-801; TEST FOUND NORMAL.; [02] VERIFIED NORMAL
- [SDR SWAA2021111041200](https://openairdocs.org/sdr/SWAA2021111041200.md): None · inoperative · Nov 6, 2021 · N774SW · Boeing 737* · Emergency Lighting
  > R2 DOOR UPPER EMERGENCY INDICATOR EXIT SIGN INOP.; / [01] WORK TO BE ACCOMPLISHED IN ITEM TTG8Q0096A91; OPS CHECK FOUND NORMAL AS PER B737 AMM 33-51-06-960-805.; [02] VERIFOED
- [SDR SWAA2021111738631](https://openairdocs.org/sdr/SWAA2021111738631.md): Doubler · corroded · Oct 31, 2021 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AT FWD CARGO COMP BILGE AREA M2134 'NATS AIRPHONE ANTENNA' DOBBLER BETWEEN STA 500 AND 500A STGR 28L AND STGR 28R.INSTALLED PROTECTION OF EWIS AT FWD CARGO IAW AMM 20-60-07-913-801. REMOVED EXTERIOR COVER DOUBLE PLATE ATTACHED WITH 6 (EA) FAST
- [SDR SWAA2021111632322](https://openairdocs.org/sdr/SWAA2021111632322.md): None · missing · Oct 21, 2021 · N774SW · Boeing 737* · Passenger Compartment Equipment
  > EMERGENCY EXIT DOOR L & R SIDE INDICATOR ASSY -LIGHTED EXIT FOUND MISSING; / [01] INSTALLED EMERGENCY EXIT DOOR L/H SIDE AND R/H SIDE INDICATOR ASSY LIGHT AS PER BOEING 737-700 AMM 33-51-01-960-801.; [02] VERIFIED INSTALL. TEST ON CARD TTG8Q0033A01
- [SDR SWAA2021111731584](https://openairdocs.org/sdr/SWAA2021111731584.md): Intercostal · cracked · Oct 19, 2021 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ENG 2 O/B FAN COWL INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL AT NR 2 ENGINE O/B FAN COWL IAW SRM 51-40-02-0G-0.
- [SDR SWAA2021111731793](https://openairdocs.org/sdr/SWAA2021111731793.md): Access Panel · delaminated · Oct 19, 2021 · N774SW · Boeing 7377H4 · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON ACCESS PANEL 431ER EDGE DELAMINATED. PREPARED PANEL 431ER FOR REPAIR OF THE FIBER GLASS IAW SRM 51-70-062R-7. REPAIRED AT PANEL 431ER IAW SRM 51-70-06-2R-7. RESTORED FINISH AT #2 PYLON ACCESS PANEL 431ER IAW AMM 51-21-73-370-803.
- [SDR SWAA2021111730939](https://openairdocs.org/sdr/SWAA2021111730939.md): Channel · corroded · Oct 18, 2021 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT R/H FLOOR SUPPORT Z CHANNEL NUTPLATES BETWEEN BS 767 & 787. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP. ON REWORKED AREA IAW NDT PART 4 51-00-00 PROC. 3. MIN THICKNESS.028'. EVALUATED REWORKED
- [SDR SWAA2021111730941](https://openairdocs.org/sdr/SWAA2021111730941.md): Support · corroded · Oct 18, 2021 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY BILGE FRAME SUPPORT UPPER FLANGE BS 787, S26R. REMOVED CORROSION IAW SRM 51-10-02-0G-0. EVALUATED REWORKED AREA ORG MAT 0.088 MAT REMOVED 0.042 MAT REMAINING 0.046 FOUND TO BE OUT OF LIMITS IAW B737-7 SRM 53-00-53-1A-2 REMOVED AT A
- [SDR SWAA2021111728694](https://openairdocs.org/sdr/SWAA2021111728694.md): Stringer · corroded · Oct 11, 2021 · N774SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND AFT FUSELAGE INTERNAL STINGER 27L, BS 1006 & 1016. REMOVED CORROSION AT AFT FUSELAGE & FOUND OUT OF LIMITS DUE TO ITS ALL THE WAY THROUGH STRINGER BLOWN OUT IAW SRM 51-10-02-0G-0. FABRICATED A NEW STRINGER IAW SRM 53-00-03-2R-1, FIGURE 205.
- [SDR SWAA2021111728693](https://openairdocs.org/sdr/SWAA2021111728693.md): Hinge · corroded · Oct 11, 2021 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AT UPPER FUSELAGE UNDER VERTICAL FIN AREA BETWEEN VERTICAL STAB. FWD HINGE & AFT HINGE. OTBD S1L & 1R. REMOVED CORROSION AT UPPER FUSELAGE UNDER VERTICAL FIN AREA IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP. ON REWORKED AREAS IAW NDT PART 4
- [SDR SWAA2021111728691](https://openairdocs.org/sdr/SWAA2021111728691.md): Panel · delaminated · Oct 9, 2021 · N774SW · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > PANEL 192BL HAS EDGES DELAMINATED IN TWO SPOTS. REMOVED DAMAGED PLIES & PREPARED THE DAMAGED AREA TO APPLY FABRIC REPAIR PLIES NO WATER NOTE AT ACCESS PANEL 192BL IAW SRM 51-70-04-2R-10 PARAGRAPH 4 B & C. APPLIED FABRIC REPAIR PLIES AT ACCESS PANEL 192BL IAW
- [SDR SWAA2021111727968](https://openairdocs.org/sdr/SWAA2021111727968.md): Stiffener · cracked · Oct 7, 2021 · N774SW · Boeing 7377H4 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STAILIZER INSPAR RIB ASSY #4 STIFFENER #2 LOWER CRACK NOTED. PERFORMED HFEC INSP ON STIFFENER#2 LOWER CHORD IAW B737 NDT P6 51-00-00 PROC.23; 2EA CRACKS NOTED. PERFORMED ROTO INSP ON STIFFENER#2 LOWER 8EA EXISTING HOLES IAW NDT P6 51-00-00 PR
- [SDR SWAA2021111727969](https://openairdocs.org/sdr/SWAA2021111727969.md): Stiffener · cracked · Oct 7, 2021 · N774SW · Boeing 7377H4 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STAILIZER INSPAR RI ASSY #4 STIFFENER #4 LOWER CRACK NOTED / REMOVED DAMAGED AT LT HORIZONTAL STAB #4 RIB #4 STIFFENER LOWER IAW 7 SRM 55-10-09-2R REPAIR 4. NO CRACKS NOTED. INSTALLED REPAIR AT#4 RIB STIFFENERS #4 AT L/H HORIZONTAL STAB IA
- [SDR SWAA2021111726866](https://openairdocs.org/sdr/SWAA2021111726866.md): Rib · cracked · Oct 5, 2021 · N774SW · Boeing 7377H4 · Vertical Stabilizer, Spar/Rib
  > DORSAL FIN FWD RIB CRACKED; / [01] REMOVED DORSAL FIN FWD RIB AS PER B737-700 SRM 5-40-02-0G-0; [02] LOCATED AND DRILLED NEW RIB ASSEMBLY AS PER B737-700 SRM 51-40-05-0G-0; [03] VERIFIED STEP 2. OK TO INSTALL ON DORSAL FUN.; [04] INSTALLED NEW RIB AT DORSAL F
- [SDR SWAA2021111626860](https://openairdocs.org/sdr/SWAA2021111626860.md): Web · cracked · Oct 5, 2021 · N774SW · Boeing 737* · Wing Main, Frame Structure
  > CRACK FOUND AT EXTERNAL WHEEL WELL WEB LOCATED AT RT SIDE STA 663 BETWEEN RBL 31.83 & RBL 40.00. CRACK LENGTH: 0.512'. / [01] INSTALLED EWIS PROTECTION AT EXTERNAL WHEEL WEB AT R/H SIDE STA 663 BETWEEN RBL 31.83 AND RBL 40.00 IN REFERENCE B-737 AMM20-60-07-91
- [SDR SWAA2021111725744](https://openairdocs.org/sdr/SWAA2021111725744.md): Panel · delaminated · Oct 3, 2021 · N774SW · Boeing 7377H4 · Nacelle/Pylon Structure
  > NO-2 PYLON ACCESS PANEL 441EL EDGE AREA DELAMINATED MKD DOT; / [01] PREPARED FOR REPAIR AT PANEL 441 EL AS PER B737-700 SRM. 51-70-06-2R-7; [02] VERIFIED STEP 1; OK TO INSTALL REPAIR PLIES; [03] REPAIRED AT PANEL 441 EL AS PER B737-700 SRM 51-70-06-2R-7 MATER
- [SDR SWAA2021111725737](https://openairdocs.org/sdr/SWAA2021111725737.md): Gusset · cracked · Oct 2, 2021 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO L/H STA 500D S-19L GUSSET BRACKET CRACK.; / [01] REMOVED GUSSET AT FWD CARGO DOOR L/H STA 500D S19L B737-700 ARM 51-40-02-0G-0; [02] LOCATED. HOLE AND NEW GUSSET B737-700 SRM 51-40-05-0G-0; [03] VERIFIED DRILL OF NEW; OK TO INSTALL; [04] INSTALLED G
- [SDR SWAA2021111725738](https://openairdocs.org/sdr/SWAA2021111725738.md): Gusset · cracked · Oct 2, 2021 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO R/H STA 500D S-19R GUSSET BRACKET CRACK.; / [01] REMOVED GUSSET AT FWD CARGO R/H SAT 500D S-19 B737-700 ARM 51-40 -02 0G-0; [02] LOCATED HOLE NEW GUSSET PER B737-700 IN REF SRM 51-40)05; [03] VERIFIED NEW GUSSET DRILL; OK TO INSTALL; [04] INSTALLED
- [SDR SWAA2021111725727](https://openairdocs.org/sdr/SWAA2021111725727.md): Panel · deformed · Oct 1, 2021 · N774SW · Boeing 7377H4 · Fuselage Floor Panel
  > PANEL 211AF OUT OF SHAPE. LOCATED AND DRILLED NEW PART REF B-737-700 SRM 41-40-05-0G-0; [02] VERIFIED NEW PART.INSTALLATION ON CARD TTG8Q002YL6X
- [SDR SWAA2021111725191](https://openairdocs.org/sdr/SWAA2021111725191.md): Panel · delaminated · Oct 1, 2021 · N774SW · Boeing 7377H4 · Aerodynamic Fairings
  > ACCESS PANEL 193D AFT EDGE DELAMINATED. / [01] PREPARED FOR REPAIR PLIES THE AREA AT PANEL 193D AS PER B737-700 SRM51-70-04-2R-9; [02] OK TO INSTALL REPAIR.; [03] REPAIRED AT PANEL 193 D AS PER B737-700 SRM 51-70-04-2R-9. MATERIAL USED PO.1731939 AND PO. 1694
- [SDR SWAA2021111725206](https://openairdocs.org/sdr/SWAA2021111725206.md): Channel · corroded · Oct 1, 2021 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BILGE AREA, LT SIDE ZEE CHANNEL, BS 727D+9 - 847. REMOVED CORROSION IAW SRM 51-51-10-02-0G-0. PERFORMED UT THIKNESS INSP. ON REWORKED AREA IAW NDT PART 4 51-00-00 PROC. 4. MIN THICKNESS.035'. ORIGINAL THICKNESS 0.040'' AFTER REWORKE
- [SDR SWAA2021111725731](https://openairdocs.org/sdr/SWAA2021111725731.md): Skin · corroded · Oct 1, 2021 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > LIGHT CORROSION AT AFT PRESSURE DOME FWD SIDE BS 1016, CIRCUMFERENTIAL SKIN SPLICE BETWEEN STRINGERS 26L TO 26R. REMOVED SKIN ATTACH RIVETS AT AFT PRESSURE DOME IAW SRM 53-80-08-1A-1 CORROSION FOUND OUT OF LIMITS IAW SRM 53-80-08-1A-1. REMOVED SPLICE ANG
- [SDR SWAA2021111725215](https://openairdocs.org/sdr/SWAA2021111725215.md): Splice · corroded · Oct 1, 2021 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BILGE AREA; FLOOR-PANEL SPLICE AT STA#727D+5; SPOTS OF CORROSION. DOT#208-16<REMOVED CORROSION AT AFT CARGO BILGE AREA FLOOR PANEL SPLICE AT STA 727.5 CORROSION IS ALL THE WAY THROUGH THE TEE IS OUT OF LIMITS IAW B737-7 SRM 51-10-02-0G-0 CORROSION OU
- [SDR SWAA2021111725214](https://openairdocs.org/sdr/SWAA2021111725214.md): Angle · corroded · Oct 1, 2021 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BILGE AREA; FLOOR-PANEL SPLICE AT STA#772 CORROSION. REMOVED CORROSION AFT CARGO BILGE AREA FLOOR PANEL SPLICE AT STA772IAW B737 SRM51-10-02-0G-0. VERIFIED 1 PERFORMED UT THICKNESS INSP. ON REWORKED AREA @ AFT CARGO BILGE AREA FLOOR-PANEL SPLICE @ ST
- [SDR SWAA2021111725735](https://openairdocs.org/sdr/SWAA2021111725735.md): Web · cracked · Oct 1, 2021 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT WET AREA FLOOR WEB AT BS 1016+8', RBL 30 CRACKED. REMOVED AFT WET AREA FLOOR WEB IAW SRM 51-40-02-G-0. LOCATED AND DRILLED A NEW WEB IAW SRM 51-40-05-0G-0. FABRICATED A NEW WEB IAW SRM 53-70-51-01-1, WEBS & STRAPS DWG 147A5744. TREATED AND PRIMED T
- [SDR SWAA2021111725193](https://openairdocs.org/sdr/SWAA2021111725193.md): Channel · corroded · Oct 1, 2021 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BILGE AREA; R/H SIDE 'Z' CHANNEL FROM BS 727 TO 767. REMOVED CORROSION BILGE AREA R/H Z CHANEL IAW SRM 51-10-02-0G-0. PERFORMED UT THIKNESS INSP. ON REWORKED AREA IAW NDT PART 4 51-00-00 PROC. 3. MIN THICKNESS.030'. ORIGINAL THICKNESS 0.040''
- [SDR SWAA2021111725204](https://openairdocs.org/sdr/SWAA2021111725204.md): Structure · corroded · Oct 1, 2021 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BILGE AREA; FLOOR STRUCTURE BETWEEN BS 727- 727A, LBL 4 - RBL 8. AROUND FASTENER HOLES. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP IAW NDT P4 51-00-00 PROC.3; MIN THK. NOTED 0.051'. EVALUATED REWORKED AREA O
- [SDR SWAA2021111725197](https://openairdocs.org/sdr/SWAA2021111725197.md): Channel · corroded · Oct 1, 2021 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BILGE AREA; R/H SIDE 'Z' CHANNEL FROM STA#867 TO STA#887; SPOTS OF CORROSION AROUND FASTENER HOLES. REMOVED CORROSION AFT CARGO BILGE AREA R/HZ CHANNEL. FOUND OUT LIMITS EXFOLIATION CORROSION AREA IAW SRM 51-10-02-0G-0 VERIFIED 1 PERFORMED UT THIKNE
- [SDR SWAA2021111740658](https://openairdocs.org/sdr/SWAA2021111740658.md): Stiffener · cracked · Oct 1, 2021 · N774SW · Boeing 7377H4 · Horizontal Stabilizer Structure
  > REMOVE LEFT HAND HORIZONTAL STABILIZER IN SPAR RIB ASSY #5 FOR ACCESS TO STIFFENER #3 REPAIR.; REMOVE LEFT HAND HORIZONTAL STAILIZER IN SPAR RI ASSY #5 FOR ACCESS TO STIFFENER #3 REPAIR. / [01] REMOVED L/H HORIZONTAL STAB IN SPAR RIB #5 STIFFENERS #3 IAW B737
- [SDR SWAA2021111725221](https://openairdocs.org/sdr/SWAA2021111725221.md): Stiffener · cracked · Oct 1, 2021 · N774SW · Boeing 7377H4 · Horizontal Stabilizer Structure
  > RIGHT HORIZONTAL STAB INSPAR RIB ASSY NR 4 HSS 120.30. STIFFENER #2 LOWER AREA CRACK NOTED. REMOVED CRACK ON STIFFENER 2 RIB 4 RT HORIZONTAL STAB IAW SRM 55-10-09 -2R REPAIR4. VERIFIED STEP 1 PERFORMED ROTO INSP ON REWORKED AREA 4EA EXISTING HOLES AT LOWER C
- [SDR SWAA2021111725220](https://openairdocs.org/sdr/SWAA2021111725220.md): Stiffener · cracked · Oct 1, 2021 · N774SW · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STAB INSPAR RIB 4, HSS 120.30. STIFFENER 4 LOWER AREA CRACKED. REMOVED CRACK IAW SRM 55-10-09-2R REPAIR 4. HFEC INSP IAW NDT P6 51-00-00 PROC.23 CRACK NOTED. ROTO INSP IAW NDT P6 51-00-00 PROC.16 CRACK NOTED. REMOVED CRACK ON WEB & HOLE I
- [SDR SWAA2021111725219](https://openairdocs.org/sdr/SWAA2021111725219.md): Stiffener · cracked · Oct 1, 2021 · N774SW · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STABILIZER INSPAR RIB ASSY. #4 (STAB STA 120.30); STIFFENER #3 LOWER AREA CRACK NOTED. REMOVED CRACK IAW SRM 55-10-09-2R REPAIR 4. PERFORMED HFEC INSP ON REWORKED AREA WEB IAW B737 NDT P6 51-00-00 PROC.23 CRACK NOTED. PERFORMED ROTO INSP ON
- [SDR SWAA2021111725211](https://openairdocs.org/sdr/SWAA2021111725211.md): Stiffener · cracked · Oct 1, 2021 · N774SW · Boeing 7377H4 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER INSPAR RIB 5, STIFFENER 3 LOWER AREA, CRACK NOTED. REMOVED PAINT FOR ACCESS FASTENER UPPER AND LOWER SKIN IAW AMM 51-21-11-150-801. REMOVED STAB NR 5 RIB IAW SRM 51-40-02-0G-0. REMOVED CRACK FROM NR 5 RIB STIFFENER 3 IAW SRM 55-10-
- [SDR SWAA2021111725210](https://openairdocs.org/sdr/SWAA2021111725210.md): Stiffener · cracked · Oct 1, 2021 · N774SW · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STAB INSPAR RIB NR 4, STIFFENER 3 LOWER AREA CRACKED. REMOVED DAMAGED IAW SRM 55-10-09-2R, REPAIR 4. PERFORMED HFEC INSP ON STIFFENER IAW NDT P6 51-00-00 PROC.23, CRACK NOTED. PERFORMED ROTO INSP ON STIFFENER IAW NDT P6 51-00-00 PROC.16
- [SDR SWAA2021111625729](https://openairdocs.org/sdr/SWAA2021111625729.md): Angle · cracked · Oct 1, 2021 · N774SW · Boeing 737* · Fuselage Miscellaneous Structure
  > CABIN FLOOR INTERCOSTAL AT ABOUT BL-0 BETWEEN STA 380-400 UPPER SURFACE CRACKED; / [01] REMOVED UPPER ANGLE AT CABIN FLOOR INTERCOSTAL ABOUT BL-0 BETWEEN STATION 380 & 400 AS PER SRM 51-40-02-G-0.; [02] LOCATED AND DRILLED NEW ANGLE AS PER SRM 51-40-05-0G-0.;
- [SDR SWAA2021111725031](https://openairdocs.org/sdr/SWAA2021111725031.md): Panel · delaminated · Sep 30, 2021 · N774SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PANEL 241XF DELAMINATED; / [01] REMOVED DAMAGED AREA AND PREPARED AREA FOR REPAIR AT PANEL 241XF AS PER B737 SRM 53-00-50-2R-1; [02] REPAIRED DAMAGED AREA AT PANEL 241XF AS PER B737 SRM 53-00-50-2R-1; [03] REPAIRED DELAMINATED AREA AT PANEL 241XF AS PER B737

Next page: https://openairdocs.org/deregistered/N774SW-2024-10-04/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 = 'N774SW' AND deregistration_id = 'N774SW-2024-10-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N774SW-2024-10-04/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, except the copies of manufacturers’ service documents, which belong to their rights holders.