# Service difficulty reports: N289CT

A list on [N289CT](https://openairdocs.org/aircraft/N289CT.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 · 260 reports

- [SDR SWAA2025101323850](https://openairdocs.org/sdr/SWAA2025101323850.md): Slide · detached · Oct 11, 2025 · N289CT · Boeing 7377H4 · Escape Slide
  > FORWARD ENTRY SLIDE HARD TO ARM AND PART OF SLIDE FELL OUT. RE-ATTACHED VELCRO AT BOTTOM OF FWD ENTRY DOOR SLIDE IAW AMM 25-66-01
- [SDR SWAA2025032002743](https://openairdocs.org/sdr/SWAA2025032002743.md): Panel · cracked · Mar 7, 2025 · N289CT · Boeing 7377H4 · Wing Main, Frame Structure
  > PANEL 621PB CRACKED AT FWD I/B END. <[01] CRACK AT FWD I/B END OF PANEL 621PB WAS REPAIRED IAW SRM 51-70-05-2R-6.; [02] VERIFIED CORRECTIVE ACTION #1.
- [SDR SWAA2025032498497](https://openairdocs.org/sdr/SWAA2025032498497.md): Attach Angle · cracked · Feb 21, 2025 · N289CT · Boeing 7377H4 · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL FIN FRONT SPAR; FWD SPRING ANGLE (176A3101-26) CRACKED AT LT ATTACH POINT<[01] REMOVED AND REPLACED VERTICAL FIN FRONT SPAR FWD SPRING ANGLE IAW SRM 51-40-02-0G-0 AND DWG #176A3101 SHEET 4 REV-.
- [SDR SWAA2025032498188](https://openairdocs.org/sdr/SWAA2025032498188.md): Skin · cracked · Feb 20, 2025 · N289CT · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 25' FROM FWD EDGE; 0.6' IN LENGTH (MARKED)<[01] REPAIRED RH LOWER HORIZONTAL STABILIZER SKIN AT STAB STA 193.90; 25' FROM FWD EDGE IAW SRM 55-10-01-2R-11 REPAIR 11.;[02] VERIFIED COMPLETION CORR
- [SDR SWAA2025032497561](https://openairdocs.org/sdr/SWAA2025032497561.md): Stub Frame · cracked · Feb 18, 2025 · N289CT · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK FOUND ON R1 DOOR STUB FRAME 0.7' ABOVE SEAL DEPRESSOR; 0.6' FWD FROM DOOR CUT OUT. L: 0.5' MARKED. <[01] REMOVED CRACKED R1 DOOR STUB FRAME AND REPLACED ALL I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A8370 REV: D; [02] VERIFIED COMPLETION CORRECTIVE ACTI
- [SDR SWAA2025032497558](https://openairdocs.org/sdr/SWAA2025032497558.md): Frame · corroded · Feb 18, 2025 · N289CT · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION ON BS 303 FRAME LBL 56 WL 208. <[01] REPAIRED CORROSION ON BS 303 FRAME LBL 56 WL 208 PER EA 25-153-00457-WIP1; [02] VERIFIED ITEM 1.
- [SDR SWAA2025032497560](https://openairdocs.org/sdr/SWAA2025032497560.md): Support Angle · corroded · Feb 18, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD ENTRY DOOR THRESHOLD SUPPORT ANGLE BS 320 AND 338 LBL 56 WL 208. <[01] REMOVED AND REPLACED FWD ENTRY DOOR THRESHOLD SUPPORT ANGLE I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A8110 REV A; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASURE
- [SDR SWAA2025032497565](https://openairdocs.org/sdr/SWAA2025032497565.md): Intercostal · cracked · Feb 18, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 380-400 RBL 40 WL 208. <[01] REMOVED AND REPLACED CRACKED INTERCOSTAL WITH NEW AT BS 380-400 RBL 40 WL 208. VERIFIED SRM 53-00-04-1A-1 IS APPLICABLE FOR ALLOWABLE DAMAGE ON CRACKED INTERCOSTAL BS 380-400 RBL 40 WL 208. REMOVED CRACKED I
- [SDR SWAA2025032497573](https://openairdocs.org/sdr/SWAA2025032497573.md): Strap · corroded · Feb 18, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP BS 1028 RBL 18 WL 208. <[01] REMOVED AND REPLACED NEW STRAP BS 1016-1026 RBL 18 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5730 REV:C; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2025032497569](https://openairdocs.org/sdr/SWAA2025032497569.md): Strap · corroded · Feb 18, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP BS 1016-1026 RBL 3 WL 208. <[01] REMOVED AND REPLACED NEW STRAP BS 1016-1026 RBL 3 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5730 REV:C; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2025032497570](https://openairdocs.org/sdr/SWAA2025032497570.md): Strap · corroded · Feb 18, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP BS 1017 LBL 3 WL 208. <[01] REMOVED AND REPLACED STRAP BS1017 LBL3 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 REV:B; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2025032497559](https://openairdocs.org/sdr/SWAA2025032497559.md): Sill Drain · corroded · Feb 18, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD ENTRY DOOR MOP SILL BS 303 LBL 56 WL 208.<[01] REMOVED AND REPLACED FED MOPSILL I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A8110 REV A;[02] VERIFIED CORRECTIVE ACTION. CARD COMPLETE.
- [SDR SWAA2025032497098](https://openairdocs.org/sdr/SWAA2025032497098.md): Stub Frame · cracked · Feb 18, 2025 · N289CT · Boeing 7377H4 · Fuselage Main, Structure
  > FOLDING AND PEELING OFF INTERNAL FUSELAGE SKIN ON UPPER-FWD COUNTER FRAME OF R1 DOOR; DIMENSIONS OF 3' LONG; 1' DEEP; AND 3/32' PEELING OFF.<[01] DURING INSPECTION STUB FRAME FOUND CRACK AND GENERATED CCN TTG8Q00YSN5X THEREFORE DISCREPANCY REPORTED BEING NULL
- [SDR SWAA2025032497564](https://openairdocs.org/sdr/SWAA2025032497564.md): Floor Support · cracked · Feb 18, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 312-328 LBL45 WL 208.<[01] REMOVED CRACKED INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL BS 312-328 LBL45 WL 208.;[02] ALL TASK STEPS COMPLETED;[03] JOB COMPLETE
- [SDR SWAA2025032497562](https://openairdocs.org/sdr/SWAA2025032497562.md): Floor Support · cracked · Feb 18, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 312-328 RBL 30 WL 208.<[01] REMOVED CRACKED INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL BS 312-328 RBL 30 WL 208.;[02] ALL TASKS STEPS COMPLETED;[03] JOB COMPLETE
- [SDR SWAA2025032497082](https://openairdocs.org/sdr/SWAA2025032497082.md): Plate · corroded · Feb 17, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156 <[01]. CORROSION ON AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT LIMITS. REMOVE AND REPLACE R/H FLOOR TO SI
- [SDR SWAA2025032497079](https://openairdocs.org/sdr/SWAA2025032497079.md): Scuff Plate · cracked · Feb 17, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED <[01]. AFT CARGO BAY AFT CORNER SCUFF PLATE REPAIRED PER SRM 53-60-15-2R-1.
- [SDR SWAA2025032097081](https://openairdocs.org/sdr/SWAA2025032097081.md): Support Plate · corroded · Feb 17, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156 <[01]. CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT LIMITS. REMOVE AND REPLACE L/H FLOOR TO SIDEWA
- [SDR SWAA2025031997078](https://openairdocs.org/sdr/SWAA2025031997078.md): Scuff Plate · cracked · Feb 17, 2025 · N289CT · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED <[01]. FWD CARGO BAY FWD CORNER SCUFF PLATE WAS REPAIRED PER SRM 53-30-15-2R-1.
- [SDR SWAA2025031997085](https://openairdocs.org/sdr/SWAA2025031997085.md): Floor Panel · delaminated · Feb 17, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 232AF TOP SURFACE IS DELAMINATED. <[01] CABIN FLOOR PANEL 232AF WITH TOP SURFACE DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.; [02] VERIFIED CORRECTIVE ACTION #1.
- [SDR SWAA2025031997096](https://openairdocs.org/sdr/SWAA2025031997096.md): Floor Panel · delaminated · Feb 17, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 221FF TOP SURFACE IS DELAMINATED. <[01] CABIN FLOOR PANEL 221FF TOP SURFACE WITH DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2025031997090](https://openairdocs.org/sdr/SWAA2025031997090.md): Floor Panel · delaminated · Feb 17, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241ACF HAS TOP SURFACE DELAMINATION. <[01] CABIN FLOOR PANEL 241ACF WITH TOP SURFACE DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025031997092](https://openairdocs.org/sdr/SWAA2025031997092.md): Floor Panel · delaminated · Feb 17, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241UF HAS TOP SURFACE DELAMINATION. <[01] CABIN FLOOR PANEL 241UF; WITH TOP SURFACE DELAMINATION; WAS REPAIRED IAW SRM 53-00-50-2R-0.; [02] ITEM 1 SHOULD READ: CABIN FLOOR PANEL 241UF; WITH TOP SURFACE DELAMINATION; WAS REPLACED WITH A NEWLY
- [SDR SWAA2025031997080](https://openairdocs.org/sdr/SWAA2025031997080.md): Shield · corroded · Feb 17, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] CORROSION ON AFT CARGO BAY R/H SHIELD; FOUND TO BE OUT LIMITS. REMOVE AND REPLACE R/H SHIELD; BS 767 TO BS 794 IAW SRM 51-40-02-0G-0; SRM 51-40-0
- [SDR SWAA2025031997087](https://openairdocs.org/sdr/SWAA2025031997087.md): Cargo Track · cracked · Feb 17, 2025 · N289CT · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO BAY CARGO TRACK IS CRACKED BS747 AND BS727E RBL13 WL156<[01] REMOVED AND REPLACED AFT CARGO BAY CARGO TRACK BS727+4 - BS887 RBL13 WL156 IAW SRM 51-40-02-0G-0; DWG 146A7500 REV:-; DWG 147A7500 REV:- AND DWG 146A0061 REV:A;[02] REPAIRED AS PER SRM 53-
- [SDR SWAA2025032496721](https://openairdocs.org/sdr/SWAA2025032496721.md): Structure · corroded · Feb 16, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON INNER CHORD AT BS 698 RBL 63 WL 208. (MARKED) <[01] REFER TO FAULT TTG8Q00YQ2WS WHERE EA 25-153-00417 WAS ADDED AS A SUBTASK; [02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2025032095952](https://openairdocs.org/sdr/SWAA2025032095952.md): Panel · cracked · Feb 14, 2025 · N289CT · Boeing 7377H4 · Wing Main, Frame Structure
  > PANEL 621YB CRACKED ON O/B FWD. END <[01] PANEL 621YB WITH CRACK ON O/B FWD END WAS REPAIRED PER SRM 51-70-05-2R-6.
- [SDR SWAA2025031995954](https://openairdocs.org/sdr/SWAA2025031995954.md): Floor Panel · debonded · Feb 14, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231JF HAS DISBONDED TOP SURFACE. <[01] CABIN FLOOR PANEL 231JF DISBONDED TOP SURFACE REPAIRED IAW SRM 53-00-50-2R-0; [02] CORRECTION TO ITEM 1: FABRICATED NEW CABIN FLOOR PANEL 231JF IAW SRM 53-00-50-2R-0.; [03] VERIFIED CORRECTIVE ACTION ITE
- [SDR SWAA2025031995955](https://openairdocs.org/sdr/SWAA2025031995955.md): Floor Panel · delaminated · Feb 14, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 242DF HAS DELAMINATED TOP SURFACE. <[01] REPLACED DAMAGED 242DF FLOOR PANEL WITH SERVICEABLE PANEL P/N:144A5810-150 IAW SRM 51-10-02-0G-0 PARA 9.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025031995959](https://openairdocs.org/sdr/SWAA2025031995959.md): Floor Panel · debonded · Feb 14, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241EF HAS DISBONDED TOP SURFACE. <[01] CABIN FLOOR PANEL 241EF WITH DISBONDED TOP SURFACE WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.; [02] VERIFIED CORRECTIVE ACTION #1.
- [SDR SWAA2025031995961](https://openairdocs.org/sdr/SWAA2025031995961.md): Floor Panel · debonded · Feb 14, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 232FF HAS DISBONDED TOP SURFACE. <[01] CABIN FLOOR PANEL 232FF DISBONDED TOP SURFACE REPAIRED IAW SRM 53-00-50-2R-0.; [02] CORRECTION TO ITEM 1: FABRICATED NEW CABIN FLOOR PANEL 232FF IAW SRM 53-00-50-2R-0.; [03] VERIFIED CORRECTIVE ACTION IT
- [SDR SWAA2025031995963](https://openairdocs.org/sdr/SWAA2025031995963.md): Floor Panel · delaminated · Feb 14, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 242BF HAS DELAMINATED TOP SURFACE. <[01] REPLACED DAMAGED 242BF FLOOR PANEL WITH SERVICEABLE PANEL P/N:144A5810-149 IAW SRM 51-10-02-0G-0 PARA 9.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025031995967](https://openairdocs.org/sdr/SWAA2025031995967.md): Floor Panel · debonded · Feb 14, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231ZF HAS DISBONDED TOP SURFACE. <[01] CABIN FLOOR PANEL 231ZF; WITH DISBONDED TOP SURFACE; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION #1.
- [SDR SWAA2025031995962](https://openairdocs.org/sdr/SWAA2025031995962.md): Floor Panel · debonded · Feb 14, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231MF HAS DISBONDED TOP SURFACE. <[01] 231MF FLOOR PANEL DISBOND DAMAGE ON UPPER AND LOWER SURFACE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]. ATTACHE
- [SDR SWAA2025031995957](https://openairdocs.org/sdr/SWAA2025031995957.md): Floor Panel · delaminated · Feb 14, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 242AF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 242AF WITH DELAMINATED TOP SURFACE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2025031995964](https://openairdocs.org/sdr/SWAA2025031995964.md): Floor Panel · delaminated · Feb 14, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231XF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 231XF; WITH TOP SURFACE DELAMINATION; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025031995958](https://openairdocs.org/sdr/SWAA2025031995958.md): Floor Panel · delaminated · Feb 14, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241AF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 241AF WITH DELAMINATED TOP SURFACE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0127.; [02] VERIFIED CORRECTIVE
- [SDR SWAA2025031995965](https://openairdocs.org/sdr/SWAA2025031995965.md): Floor Panel · delaminated · Feb 14, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231YF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 231YF WITH DELAMINATED TOP SURFACE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025031995966](https://openairdocs.org/sdr/SWAA2025031995966.md): Floor Panel · delaminated · Feb 14, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241BF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 241BF WITH DELAMINATED TOP SURFACE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2025031995956](https://openairdocs.org/sdr/SWAA2025031995956.md): Floor Panel · delaminated · Feb 14, 2025 · N289CT · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 232RF HAS DELAMINATED TOP SURFACE. <[01] DAMAGE TO CABIN FLOOR PANEL 232RF WAS BEYOND ECONOMICAL REPAIR; FABRICATED NEW PANEL IAW SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2025032495947](https://openairdocs.org/sdr/SWAA2025032495947.md): Strap · corroded · Feb 13, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP AT MID CABIN BS696 RBL67 WL203. MARKED <[01] REJECTED; AMT REQUEST FOR NDI TO VERIFY REMAINING THICKNESS OF PART. AMT DID PROVIDE STRUCTURE ID/DRAWING AS REQUIRED IAW 737 NDTM PART 4; 51-00-00; PROC 2 STEP 4. C.; [02] EDIT: 'DID NOT PROVIDE
- [SDR SWAA2025032495948](https://openairdocs.org/sdr/SWAA2025032495948.md): Strap · corroded · Feb 13, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP AT MID CABIN BS703 RBL64 WL203. MARKED <[01] REJECTED; AMT REQUEST FOR NDI TO VERIFY REMAINING THICKNESS OF PART. AMT DID PROVIDE STRUCTURE ID/DRAWING AS REQUIRED IAW 737 NDTM PART 4; 51-00-00; PROC 2 STEP 4. C.; [02] EDIT: 'DID NOT PROVIDE
- [SDR SWAA2025032495942](https://openairdocs.org/sdr/SWAA2025032495942.md): Strap · corroded · Feb 13, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP AT MID CABIN BS707 RBL63 WL203. MARKED <[01] REJECTED; AMT REQUEST FOR NDI TO VERIFY REMAINING THICKNESS OF PART. AMT DID NOT PROVIDE STRUCTURE ID/DRAWING AS REQUIRED IAW 737 NDTM PART 4; 51-00-00; PROC 2 STEP 4. C.; [02] REMOVED CORROSION O
- [SDR SWAA2025032495945](https://openairdocs.org/sdr/SWAA2025032495945.md): Structure · corroded · Feb 13, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON INNER CHORD AT MID CABIN BS696; BS704 RBL63 WL208. MARKED <[01] REMOVED CORROSION IN MULTIPLE AREAS AREAS BS695 RBL63 WL 208 BLEND WAS.080'X.070'X.003; BS696 RBL63 WL 208 WAS.009'X.007'X.003'; BS704 RBL63 WL 208 WAS 1'X.080'X.004'; BS 706 RBL63
- [SDR SWAA2025032495946](https://openairdocs.org/sdr/SWAA2025032495946.md): Strap · corroded · Feb 13, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP AT MID CABIN BS692 RBL62 WL203. MARKED <[01] REJECTED; AMT REQUEST FOR NDI TO VERIFY REMAINING THICKNESS OF PART. AMT DID PROVIDE STRUCTURE ID/DRAWING AS REQUIRED IAW 737 NDTM PART 4; 51-00-00; PROC 2 STEP 4. C.; [02] EDIT: 'DID NOT PROVIDE
- [SDR SWAA2025012086531](https://openairdocs.org/sdr/SWAA2025012086531.md): Mount Bracket · cracked · Jan 16, 2025 · N289CT · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > R/H A/C BAY FWD PNEUMATIC APU BLEED AIR TO PACK VALVE DUCT MOUNT BRACKET CRACKED JUST OTBD OF KEEL BEAM BOX STRUCTURE. (SEE PIC)<[01] REMOVED AND REPLACED PER AMM 20-50-11.
- [SDR SWAA2025012086512](https://openairdocs.org/sdr/SWAA2025012086512.md): Bracket · cracked · Jan 16, 2025 · N289CT · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > RIGHT MLG WHEEL WELL; FWD. BULKHEAD; ABOVE BOOST PUMP; BRACKET CRACKED<[01] REMOVED AND REPLACED RIGHT MLG WHEEL WELL FWD BULKHEAD; ABOVE BOOST PUMP BRACKET IN REF SRM 51-10-02 AND 51-40-02.
- [SDR SWAA2025011686522](https://openairdocs.org/sdr/SWAA2025011686522.md): Handle · loose · Jan 16, 2025 · N289CT · Boeing 7377H4 · Service Doors
  > R1 DOOR INTERIOR HANDLE LOOSE<[01] TIGHTENED R1 DOOR INTERIOR HANDLE PER AMM 52-41-11.
- [SDR SWAA2025011686524](https://openairdocs.org/sdr/SWAA2025011686524.md): Handle · loose · Jan 16, 2025 · N289CT · Boeing 7377H4 · Service Doors
  > R1 DOOR ASSIST HANDLE LOOSE<[01] TIGHTENED R1 DOOR ASSIST HANDLE PER AMM 52-41-31.
- [SDR SWAA2025011686508](https://openairdocs.org/sdr/SWAA2025011686508.md): Door · cracked · Jan 16, 2025 · N289CT · Boeing 7377H4 · Landing Gear Doors
  > LEFT MLG CENTER GEAR DOOR CRACKED AT FORWARD ATTACH POINT<[01] REMOVED LEFT MLG CENTER AND LOWER/INNER DOOR ASSEMBLY IN REF AMM 32-13-11.

Next page: https://openairdocs.org/aircraft/N289CT/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 = 'N289CT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N289CT/reports

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