# Service difficulty reports: N744SW, cancelled Sep 18, 2024

A list on [N744SW, cancelled Sep 18, 2024](https://openairdocs.org/deregistered/N744SW-2024-09-18.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 · 318 reports

- [SDR SWAA2022071929626](https://openairdocs.org/sdr/SWAA2022071929626.md): Scuff Plate · cracked · Jul 15, 2022 · N744SW · Boeing 7377H4 · Fuselage Main, Structure
  > RAMP AGENTS REPORT AFT CARGO CENTER THRESHOLD SCUFF PLATE CRACKED. / [01] R&R'ED AFT CARGO SCUFF PLATE PER AMM 53-11-02. NO DAMAGE NOTED UNDERNEATH.;[02] PER EE# 67870 ADDITIONAL REFERENCE ADDED FOR CORRECTIVE ACTION;<BR>R&R'ED AFT CARGO SCUFF PLATE PER AMM 53
- [SDR SWAA2022051005297](https://openairdocs.org/sdr/SWAA2022051005297.md): Slide · loose · May 6, 2022 · N744SW · Boeing 7377H4 · Escape Slide
  > FOWARD ENTRY DOOR SLIDE FELT FROM COMPARTMENT / [01] REPACKED SLIDE INTO COMPARTMENT IAW AMM 25-66-01;OK FOR SERVICE
- [SDR SWAA2022012462636](https://openairdocs.org/sdr/SWAA2022012462636.md): Light · inoperative · Jan 20, 2022 · N744SW · Boeing 7377H4 · Emergency Lighting
  > AFT RIGHT SERVICE DOOR EXTERIOR EMERGENCY LIGHT IS INOP; / [01] REMOVED AND REPLACED THE AFT RIGHT EMERGENCY LIGHT POWER SUPPLY PER AMM 33-51-06. OPERATIONAL CHECK IS NORMAL.
- [SDR SWAA2021090212616](https://openairdocs.org/sdr/SWAA2021090212616.md): Megaphone · no test · Aug 29, 2021 · N744SW · Boeing 7377H4 · Emergency Equipment
  > AFT MEGAPHONE WILL NOT TEST; / [01] REMOVED AND REPLACED AFT MEGAPHONE IAW AMM 25-64-00. OP CHECK GOOD
- [SDR SWAA2021051271525](https://openairdocs.org/sdr/SWAA2021051271525.md): Skin · cracked · May 5, 2021 · N744SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE CRACK INDICATION AT BS 520 +13 AND S4R; REPAIRED PER EA 211531243
- [SDR SWAA2021051169225](https://openairdocs.org/sdr/SWAA2021051169225.md): Skin · cracked · May 5, 2021 · N744SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R; ISSUED EA 2115301243WIP1 AS A SUBTASK TO THE FAULT.
- [SDR SWAA2021051168968](https://openairdocs.org/sdr/SWAA2021051168968.md): Skin · cracked · May 5, 2021 · N744SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE CRACK INDICATION AT BS 500A +11 AND S4R
- [SDR SWAA2021051070442](https://openairdocs.org/sdr/SWAA2021051070442.md): Skin · cracked · May 5, 2021 · N744SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R; / COMPLIED WITH EA
- [SDR SWAA2021051070441](https://openairdocs.org/sdr/SWAA2021051070441.md): Skin · cracked · May 5, 2021 · N744SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE CRACK INDICATION AT BS 500A +11 AND S-4R; /
- [SDR SWAA2021051070440](https://openairdocs.org/sdr/SWAA2021051070440.md): Skin · cracked · May 5, 2021 · N744SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R; / C/W STEP3.DO A HIGH FREQUENCY EDDY CURRENT (HFEC) HOLE PROBE INSPECTION OF ANY ADDITIONAL EXISTING FASTENER HOLES COMMON TO THE REPAIR AREA PER 737 NDT PART 6; 51-00-00 PROCEDURE 16 USING A 0.030' NOTCH STAN
- [SDR SWAA2021051069940](https://openairdocs.org/sdr/SWAA2021051069940.md): Skin · cracked · May 5, 2021 · N744SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R; /
- [SDR SWAA2021051069667](https://openairdocs.org/sdr/SWAA2021051069667.md): Skin · cracked · May 5, 2021 · N744SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE CRACK INDICATION AT BS 500A +11 AND S-4R; /
- [SDR SWAA2021051069666](https://openairdocs.org/sdr/SWAA2021051069666.md): Skin · cracked · May 5, 2021 · N744SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R; /
- [SDR SWAA2021042866237](https://openairdocs.org/sdr/SWAA2021042866237.md): Battery · inoperative · Apr 24, 2021 · N744SW · Boeing 7377H4 · Emergency Equipment
  > AFT MEGAPHONE INOP / REPLACED AFT MEGAPHONE BATTERIES REF AMM 25-68-00. OPS CHECK GOOD.
- [SDR SWAA2021040260405](https://openairdocs.org/sdr/SWAA2021040260405.md): Slide · pulled · Mar 29, 2021 · N744SW · Boeing 7377H4 · Escape Slide
  > CREW REPORTS:L1 DOOR SLIDE GIRL BAR MATERIAL PULLED OUT EXCESSIVE / REPOSITION SLIDE AND POSITIONS GIRL MATERIAL FOR L1 SLIDE ASSY ALL PER MT 7255-61-06 ALL C/W ALL NOW GOOD
- [SDR SWAA2020122137210](https://openairdocs.org/sdr/SWAA2020122137210.md): Engine · power loss · Dec 16, 2020 · N744SW · Boeing 7377H4 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE N1 ROLLED BACK APPROX 15% AT CRUISE AND THEN RECOVERED AFTER 5-7 SECS AND HAD ASSOCIATED GRUMBLING NOISE FOR REMAINDER OF FLIGHT. NO EEC LIGHT AND NO HIGH VIBE IND.
- [SDR SWAA2020092418217](https://openairdocs.org/sdr/SWAA2020092418217.md): Sign · missing · Sep 24, 2020 · N744SW · Boeing 7377H4 · Emergency Lighting
  > INTERIOR: EMERGENCY LIGHT EXIT MISSING BULB AT AFT SERVICE DOOR. RELAMPED AND PERFORMED GOOD TEST OF AFT SERVICE DOOR EMERGENCY EXIT SIGN, PER AMM 33-51-01-960-801.
- [SDR SWAA2020092418216](https://openairdocs.org/sdr/SWAA2020092418216.md): Sign · missing · Sep 24, 2020 · N744SW · Boeing 7377H4 · Emergency Lighting
  > INTERIOR: EMERGENCY LIGHT EXIT MISSING BULB AT LT OVERWING DOOR AT UPPER SIGN. RELAMPED AND PERFORMED GOOD TEST OF LT OVERWING UPPER EMERGENCY EXIT SIGN, PER AMM 33-51-01-960-801.
- [SDR SWAA2020092418215](https://openairdocs.org/sdr/SWAA2020092418215.md): Sign · missing · Sep 24, 2020 · N744SW · Boeing 7377H4 · Emergency Lighting
  > INTERIOR: EMERGENCY LIGHT EXIT MISSING BULB AT L1 AND LT OVERWING. RELAMPED AND PERFORMED GOOD TEST OF LT OVERWING EMERGENCY EXIT SIGN. REPLACED AND PERFORMED GOOD TEST OF L1 EMERGENCY EXIT SIGN LIGHT ASSEMBLY, PER AMM 33-51-01-760-801 AND AMM 33-51-01-960-8
- [SDR SWAA2021081615934](https://openairdocs.org/sdr/SWAA2021081615934.md): Floor Splice · corroded · Sep 14, 2020 · N744SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** AFT CARGO BAY FLOOR SPLICE CORRODED AT BS 727D. RBL14; WL156 / RECEIVED NEW/SERVICABLE AFT CARGO BAY FLOOR SPLICE AT BS 727D TO BE INSTALLED ON JPANEL-141-CLOSE. 57609U 15SEP20
- [SDR SWAA2021080315933](https://openairdocs.org/sdr/SWAA2021080315933.md): Splice Plate · corroded · Sep 14, 2020 · N744SW · Boeing 7377H4 · Fuselage Floor Panel
  > ***CORROSION*** AFT CARGO BAY FLOOR SPLICE CORRODED AT BS 767+5. / RECEIVED SERVICEABLE REPLACEMENT PART; PO NUMBER 801448. REPLACEMENT SPLICE PLATE TO BE INSTALLED WITH FLOOR PANELS ON JPANEL-141-CLOSE. 57133U 14SEP20
- [SDR SWAA2020092416076](https://openairdocs.org/sdr/SWAA2020092416076.md): Battery Pack · faulty · Sep 14, 2020 · N744SW · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY SLIDE LIGHT AT FWD SERVICE DOOR ONLY ILLUMINATES FOR A FEW SECONDS. REMOVED AND INSTALLED NEW. PERFORMED A GOOD INSTALLATION TEST OF THE M01674 BATTERY PACK, PER AMM 33-51-06-960-805.
- [SDR SWAA2020092416075](https://openairdocs.org/sdr/SWAA2020092416075.md): Lamp · inoperative · Sep 14, 2020 · N744SW · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT AFT OF RIGHT SIDE FLAP IS OUT. RELAMPED AND PERFORMED GOOD TEST OF RIGHT AFT SLIDE EMERGENCY LIGHT, PER AMM 33-51-04-960-801. 59019U 14SEP20.
- [SDR SWAA2020092416074](https://openairdocs.org/sdr/SWAA2020092416074.md): Wire · disconnected · Sep 14, 2020 · N744SW · Boeing 7377H4 · Light System Wiring
  > EXIT SIGN ABOVE AFT ENTRY DOOR IS INOP. PERFORMED CONTINUITY TEST FROM CONNECTOR D2982 TO D10744 AND GROUND, PER WDM 33-51-14 AND FOUND WIRE W3142-0474-20 DISCONNECTED FROM GD3814-DC. TERMINATED AND REINSERTED WIRE W3142-0474-20 INTO GD3814-DC AND PERFORMED
- [SDR SWAA2020092818356](https://openairdocs.org/sdr/SWAA2020092818356.md): Skin · dented · Sep 9, 2020 · N744SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT AT BS 578+4.5'; 1.5' ABOVE S-4R. REPAIRED FUSELAGE SKIN DENT AT BS 578+4.5'; 1.5' ABOVE S-4R, PER EA 20-153-01719 REV IR AND ER 20-03260 REV IR.
- [SDR SWAA2020092417810](https://openairdocs.org/sdr/SWAA2020092417810.md): Skin · dented · Sep 8, 2020 · N744SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT AT BS 203.8+4.5'; 4' BELOW S-17L. FUSELAGE SKIN DENT AT BS 203.8+4.5'; 4' BELOW S-17L. REPAIRED IAW ATS ER 20-03255 REV IR DATED 23-SEP-2020 AND PER EA NO:20-153-01830 REV IR. 55981U 23SEP20.
- [SDR SWAA2020092417624](https://openairdocs.org/sdr/SWAA2020092417624.md): Skin · dented · Sep 8, 2020 · N744SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT AT BS 827+8.5; 3.8' ABOVE S-7L. REPAIRED FUSELAGE SKIN DENT AT BS 827+8.5; 3.8' ABOVE S-7L, PER 737-700 SRM 53-00-01-2R-3 (REPAIR 3).
- [SDR SWAA2021081714476](https://openairdocs.org/sdr/SWAA2021081714476.md): Attach Bracket · broken · Sep 7, 2020 · N744SW · Boeing 7377H4 · Wing, Attach Fittings
  > ATTACH BRACKET FOR PANEL 551FB AT IRSS 209 ALONG LOWER REAR SPAR CORD IS BROKEN / REMOVED ATTACH BRACKET FOR PANEL 551FB IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED HOLES IN NEW BRACKET IAW SRM 51-40-05-0G-0 FIGURE 4 SHEET 2. VERIFIED CORRECT FASTNER APPLICATIO
- [SDR SWAA2021081614440](https://openairdocs.org/sdr/SWAA2021081614440.md): Cargo Track · corroded · Sep 7, 2020 · N744SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** ON TRACK TIEDOWN AT FWD CARGO BAY BS500 LBL18 WL157. / REMOVED AND INSTALLED NEW TRACK TIEDOWN AT FWD CARGO BAY AT BS396 TO BS500D LBL 18; WL 157 ITEM # 7535311 IAW SRM 53-30-53-01-2; SRM 53-00-53-1A-2 SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG
- [SDR SWAA2021081514455](https://openairdocs.org/sdr/SWAA2021081514455.md): Shield · corroded · Sep 7, 2020 · N744SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON FWD SHIELD AT FWD CARGO BAY BS420 - BS440 RBL24 WL157. / REMOVED AND REPLACED SHIELD AT FWD CARGO BAY LOCATED BS420-BS440 RBL24 WL157 ITEM 7530143 IAW SRM 51-40-02 ITEM 4.B AND DWG # 143A0080 59202U 10SEP20.
- [SDR SWAA2021081314452](https://openairdocs.org/sdr/SWAA2021081314452.md): Support · corroded · Sep 7, 2020 · N744SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** IN AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT AT B.S. 727-767; R.B.L. 21; W.L. 154. / REMOVED AND REPLACED SIDEWALL SUPPORT AT ACB BS727-767 WL154 AS PER SRM 51-40-02-0G-0 AND DRAWING # 146A7502. EVALUATED SIDEWALL SUPPORT AND FOUND TO BE OUT O
- [SDR SWAA2021081314453](https://openairdocs.org/sdr/SWAA2021081314453.md): Support · corroded · Sep 7, 2020 · N744SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** IN AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT AT B.S. 727-847; L.B.L. 21; W.L. 154. / REMOVED AND REPLACED FLOOR SIDEWALL SUPPORT AT ACB BS727-847 LBL27 WL154 AS PER SRM 51-40-02-0G-0 AND DRAWING #146A7502. EVALUATED FLOOR SIDEWALL SUPPORT AND
- [SDR SWAA2021081214432](https://openairdocs.org/sdr/SWAA2021081214432.md): Boot · damaged · Sep 7, 2020 · N744SW · Boeing 7377H4 · Aerodynamic Fairings
  > NOSE RADOME BOOT IS DAMAGED / REMOVED DAMAGED RADOME BOOT AND INSTALLED A NEW RADOME BOOT IAW. AMM 53-52-00-400-802. 6042U 14SEP20. AND AMM 53-52-00-000-802 6042U 14SEP20.
- [SDR SWAA2021072014466](https://openairdocs.org/sdr/SWAA2021072014466.md): Attach Angle · bent · Sep 7, 2020 · N744SW · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > AFT SHIELD HAS BENT ATTACH ANGLE AT FWD CARGO BAY BS500A RBL25 WL157. / FABRICATED NEW FCB AFT SHIELD ATTACH ANGLE BS500A RBL-25 WL-157 MADE FROM BAC1503 - 100179 7075-T6511 LOT# 1442201-2 EXTRUSION IAW SRM 51-40-05 AND DWG # 143A8124 SENT TO OSS FOR HEAT TREA
- [SDR SWAA2021071514464](https://openairdocs.org/sdr/SWAA2021071514464.md): Support Angle · corroded · Sep 7, 2020 · N744SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FWD CARGO BAY BS500D LBL22 TO RBL22 WL157. / REMOVED AND REPLACED ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FCB BS500D LBL22 TO RBL22 ITEM 7530142 PO # 798181 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 5
- [SDR SWAA2021071514465](https://openairdocs.org/sdr/SWAA2021071514465.md): Support Angle · corroded · Sep 7, 2020 · N744SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT FWD CARGO BAY BS500D RBL25 WL157. / REMOVED AND REPLACED ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT FCB BS 500D S-19R - S-26R. ITEM 7530202 PO # 800475 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-
- [SDR SWAA2021071414444](https://openairdocs.org/sdr/SWAA2021071414444.md): Attach Angle · cracked · Sep 7, 2020 · N744SW · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 RBL25 WL156. / REMOVED AND REPLACED ON INTERCOSTAL ATTACH ANGLE AT FCB BS 400 RBL 25 NEW P/N 143A7502-156 PO# 802611. LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 143A7505 80641U 14SEPT20
- [SDR SWAA2021071414448](https://openairdocs.org/sdr/SWAA2021071414448.md): Attach Angle · cracked · Sep 7, 2020 · N744SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500B FWD SIDE LBL25 WL156. / REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCB BS 500B FWD SIDE LBL25 IAW SRM 51-40-02-0G-0 AND DWG 143A7505
- [SDR SWAA2021052614469](https://openairdocs.org/sdr/SWAA2021052614469.md): Gusset · cracked · Sep 7, 2020 · N744SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / REMOVED AND REPLACED ON FCB AFT BULKHEAD SUPPORT GUSSET BS 500D S-19L P/N 143A9481-6 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02 AND DWG 143A7902 80641U 15SEPT20
- [SDR SWAA2021052614470](https://openairdocs.org/sdr/SWAA2021052614470.md): Gusset · cracked · Sep 7, 2020 · N744SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED / REMOVED AND REPLACED ON FCB AFT BULKHEAD SUPPORT GUSSET BS 500D S-19R P/N 143A948-5 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02 AND DWG 143A7902 80641U 16SEPT20
- [SDR SWAA2020092814447](https://openairdocs.org/sdr/SWAA2020092814447.md): Attach Angle · cracked · Sep 7, 2020 · N744SW · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS 500C FWD SIDE RBL 25 WL 156. REMOVED AND REPLACED NEW ON INTERCOSTAL ATTACH ANGLE AT FCB BS 500C RBL 25 P/N 143A7502U160 PO NR 802622. LOCATED AND DRILLED, IAW SRM 51-40-05; SRM 51-40-02 AND DWG 143A7505.
- [SDR SWAA2020092414468](https://openairdocs.org/sdr/SWAA2020092414468.md): Stringer · cracked · Sep 7, 2020 · N744SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS 540 S-23R WL 167. CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS 540 - S-23R. REPAIRED, IAW ATS ER 20-03242 REV IR DATED 21-SEP-2020 AND PER EA NO:20-153-01783 REV IR 55981U 22SEP20.
- [SDR SWAA2020092414467](https://openairdocs.org/sdr/SWAA2020092414467.md): Stringer · cracked · Sep 7, 2020 · N744SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS 540 S-27L WL151. CRACKED STRINGER AT BS 540 S-27L WL151 WAS REPAIRED, IAW SRM 53-00-03-2R-1 REPAIR 1.
- [SDR SWAA2020092414446](https://openairdocs.org/sdr/SWAA2020092414446.md): Skin · bent · Sep 7, 2020 · N744SW · Boeing 7377H4 · Passenger/Crew Doors
  > FORWARD ENTRY DOOR UPPER AFT DOOR SKIN IS BENT. REPAIRED FORWARD ENTRY DOOR UPPER AFT DOOR SKIN, PER SRM 52-00-01-2R-2.
- [SDR SWAA2021062414427](https://openairdocs.org/sdr/SWAA2021062414427.md): Scuff Plate · cracked · Sep 5, 2020 · N744SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR AFT CORNER SCUFF PLATE IS CRACKED / LOCATED AND DRILLED FWD CARGO AFT CORNER SCUFF PLATE IAW SRM 51-40-05-0G-0 SCUFF PLATE TO BE INSTALLED ON CUSTOMER CARD # 753-140-00-01Y 56334U 17SEP20
- [SDR SWAA2021062414426](https://openairdocs.org/sdr/SWAA2021062414426.md): Scuff Plate · cracked · Sep 5, 2020 · N744SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR FWD CORNER SCUFF PLATE IS CRACKED / LOCATED AND DRILLED NEW FWD CARGO BAY FWD CORNER SCUFF PLATE IAW SRM 51-40-05-0G-0 SCUFF PLATE TO BE INSTALLED ON CUSTOMER CARD # 753-140-00-01Y 56334U 17SEP20
- [SDR SWAA2021072014423](https://openairdocs.org/sdr/SWAA2021072014423.md): Attach Angle · cracked · Sep 4, 2020 · N744SW · Boeing 7377H4 · Wing, Attach Fittings
  > RIGHT WING FIXED T/E PANEL LOWER WEB ATTACH ANGLE CRACKED; JUST IB OF DEFLECTION RIB ORSS278. MARKED / REMOVED AND REPLACED RIGHT WING FIXED T/E PANEL LOWER WEB ATTACH ANGLE. JUST IB OF DEFLECTION RIB P/N 115A6260-2 IAW. AIPC 57-42-51-02 AND SRM 51-40-02 88920
- [SDR SWAA2021041314397](https://openairdocs.org/sdr/SWAA2021041314397.md): Skin · dented · Sep 4, 2020 · N744SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > TRANSFERRED FROM CARD V262886=FUSELAGE EXTERNAL SKIN DENT AT STA. 1006 + 3.5'; 2.5' BELOW STR. 16R HAS ADDITIONAL GOUGE DAMAGE NOTED IN DENTED AREA. / FUSELAGE EXTERNAL SKIN DENT AT BS 1006+3.5' BELOW STRINGER 16R REPAIRED IAW EA 20-153-01763 REV IR AND ATS ER
- [SDR SWAA2020092814419](https://openairdocs.org/sdr/SWAA2020092814419.md): Seat Track · damaged · Sep 4, 2020 · N744SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MECHANICAL DAMAGE ON SEAT TRACK AT PASSENGER CABIN BS 520 LBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK AT PASSENGER CABIN FROM BS 480-520 LBL 45 WL 208, AS PER SRM 51-40-02-0G-0 AND DRAWING NR 143A5300. SEAT TRACK WAS EVALUATED AND FOUND TO BE OUT OF LIMIT
- [SDR SWAA2020092814418](https://openairdocs.org/sdr/SWAA2020092814418.md): Seat Track · damaged · Sep 4, 2020 · N744SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MECHANICAL DAMAGE ON SEAT TRACK AT PASSENGER CABIN BS 520 LBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK AT PASSENGER CABIN FROM BS 480-520 LBL 25 WL 208, AS PER SRM 51-40-02-0G-0 AND DRAWING NR 143A5300. SEAT TRACK WAS EVALUATED AND FOUND TO BE OUT OF LIMIT

Next page: https://openairdocs.org/deregistered/N744SW-2024-09-18/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 = 'N744SW' AND deregistration_id = 'N744SW-2024-09-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N744SW-2024-09-18/reports

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