# Service difficulty reports: N551WN, cancelled May 23, 2025

A list on [N551WN, cancelled May 23, 2025](https://openairdocs.org/deregistered/N551WN-2025-05-23.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 9 · 405 reports

- [SDR SWAA2024121777662](https://openairdocs.org/sdr/SWAA2024121777662.md): Flashlight · inoperative · Dec 14, 2024 · N551WN · Boeing 73776Q · Emergency Equipment
  > FWD EMERGENCY FLASH LIGHT INOP<[01] R&R FWD EMERGENCY FLASHLIGHT BATTERY PER AMM 25-64-00; OPS CHECK GOOD.
- [SDR SWAA2024080522137](https://openairdocs.org/sdr/SWAA2024080522137.md): Sign · missing · Aug 2, 2024 · N551WN · Boeing 73776Q · Emergency Lighting
  > EMERGENCY EXIT ROW PLACARD CAPT. SIDE MISSING.<[01] INSTALLED MISSING LENS COVER COVER ON CAPT.'S SIDE EMERGENCY EXIT ROW SIGN. PER AMM 33-51-01.
- [SDR SWAA2024073020045](https://openairdocs.org/sdr/SWAA2024073020045.md): Engine · fire · Jul 30, 2024 · N551WN · Boeing 73776Q · Engine (Turbine/Turboprop)
  > FLAMES OBSERVED FROM #1 ENGINE DURING ENGINE START. NO COCKPIT FIRE INDICATIONS. FLAMES EXTINGUISHED AFTER SHUTDOWN<[01] PERFORMED ENG RUN ON #1 ENG NO DEFECTS NOTED GOOD START PER AMM 71-00-00-800-803 FOO
- [SDR SWAA2024052388151](https://openairdocs.org/sdr/SWAA2024052388151.md): Lamp · inoperative · May 21, 2024 · N551WN · Boeing 73776Q · Emergency Lighting
  > FWD SERVICE DOOR EMERGENCY LIGHT INOP<[01] RE-LAMPED FWD SERVICE DOOR EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK NORMAL.
- [SDR SWAA2023113025906](https://openairdocs.org/sdr/SWAA2023113025906.md): Girt Bar · out of adjust · Nov 29, 2023 · N551WN · Boeing 73776Q · Emergency Equipment
  > CREW REPORTED FWD SERVICE DOOR SLIDE GIRT BAR STUCK BETWEEN A/C AND TRUCK.<[01] DISLODGED GIRT BAR. INSTALLED GIRT BAR IN FLOOR BRACKETS. INSPECTED GIRT BAR. NO DAMAGE NOTED REF AMM 25-66-01.
- [SDR SWAA2023062670712](https://openairdocs.org/sdr/SWAA2023062670712.md): Bracket · cracked · Jun 23, 2023 · N551WN · Boeing 73776Q · Galley Doors
  > R2 AFT SERVICE DOORLOWER PAN AFT BRACKET CRACKED<[01] R&R R2 AFT SERVICE DOORLOWER PAN AFT BRACKET PER AMM 52-41-31
- [SDR SWAA2023060255427](https://openairdocs.org/sdr/SWAA2023060255427.md): Slide · out of limits · Jun 1, 2023 · N551WN · Boeing 73776Q · Escape Slide
  > FWD SERVICE DOOR RAFT GAUGE IS RED<[01] REMOVED SLIDE PER THE TASK 725-61-06;[02] INSTALLED SLIDE PER TASK 725-61-06
- [SDR SWAA2023050844448](https://openairdocs.org/sdr/SWAA2023050844448.md): Light · inoperative · May 3, 2023 · N551WN · Boeing 73776Q · Emergency Lighting
  > PASSENGER CABIN ISLE WAY EMERGENCY EXIT LIGHT FOR OVER-WING DOORS IS INOP.<[01] REMOVED AND REPLACED PAX CABIN ISLE WAY EMERGENCY EXIT LIGHT FOR OVER-WING DOORS IAW AMM 33-51-01-960-802 OPS CHECK GOOD;[02] INSPECTED AND VERIFIED CORRECTIVE ACTION. JOB COMPLETE
- [SDR SWAA2023050842890](https://openairdocs.org/sdr/SWAA2023050842890.md): Battery Pack · failed · Apr 28, 2023 · N551WN · Boeing 73776Q · Emergency Lighting
  > BATTERY PACK M2335 AND RELATED EMERGENCY LIGHTS FAIL TEST<[01] REPLACED BATTERY PACK M2335 PER AMM 33-51-06-960-805; PERFORMED GOOD TEST;[02] VERIFIED CORRECTIVE ACTION #1.
- [SDR SWAA2023050930096](https://openairdocs.org/sdr/SWAA2023050930096.md): Intercostal · cracked · Apr 22, 2023 · N551WN · Boeing 73776Q · Fuselage Miscellaneous Structure
  > AFT CARGO BAY INTERCOSTAL AT BS 927-947 RBL 20 IS CRACKED<[01] REMOVED INTERCOSTAL AT AFT CARGO BAY BETWEEN BS 927 - BS 947 RBL 20 IAW SRM 51-40-02.<BR>MEASURED CRACK ON WEB: L=.6' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 PARAGRAFH 4.
- [SDR SWAA2023050930095](https://openairdocs.org/sdr/SWAA2023050930095.md): Support · broken · Apr 21, 2023 · N551WN · Boeing 73776Q · Trailing Edge Flaps
  > L/W WING STA 220; CLIP ON LOWER REAR SPAR FOR PANEL SUPPORT 551FB IS BROKEN.<[01] REMOVED AND REPLACED L/W WING STA 220; CLIP P/N 115A5552-1 ON LOWER REAR SPAR FOR PANEL SUPPORT 551FB IAW SRM 51-40-02 AND AIPC 57-50-00-23;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2023050830094](https://openairdocs.org/sdr/SWAA2023050830094.md): Scuff Plate · cracked · Apr 21, 2023 · N551WN · Boeing 73776Q · Fuselage Miscellaneous Structure
  > FWD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACKED RADIUS ON FWD CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-30-15-2R-1 PARA 4.B. (2) AND (4)<BR>EQUIP USED: WELDING MACHINE E10583. CAL DUE 01/2024;[02
- [SDR SWAA2023050929680](https://openairdocs.org/sdr/SWAA2023050929680.md): Doubler · corroded · Apr 20, 2023 · N551WN · Boeing 73776Q · Fuselage Main, Plate/Skin
  > CORROSION ON DOUBLER UNDER VERTICAL FIN AT WL 308 BS 1016+23 RBL 8.<EVALUATED DAMAGE ON DOUBLER UNDER VERTICAL FIN AT WL 308; BS 1016+23; RBL 8. MAXIMUM MATERIAL LOSS 0.8' X 0.8' X 0.004' ORIGINAL THICKNESS 0.040' REMAINING THICKNESS 0.036' FOUND TO BE OUT OF
- [SDR SWAA2023050929182](https://openairdocs.org/sdr/SWAA2023050929182.md): Stiffener · cracked · Apr 19, 2023 · N551WN · Boeing 73776Q · Horizontal Stabilizer Structure
  > L/H HORIZONTAL STAB INSPAR RIB 4 (STAB STA 120.30) HAS A CRACKED 4TH STIFFENER.<[01] SRM 55-10-09-2R-4 IS APPLICABLE TO THIS REPAIR.;[02] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 120.30 RIB 4RT VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[03] HFEC
- [SDR SWAA2023050928364](https://openairdocs.org/sdr/SWAA2023050928364.md): Support · cracked · Apr 17, 2023 · N551WN · Boeing 73776Q · Fuselage Miscellaneous Structure
  > WING CENTER SECTION - BREAK DOWN SUPPORT HAS CRACK BS 540 LBL 38.25 WL 208<[01] REMOVED WING CENTER SECTION - BREAK DOWN SUPPORT BS 540 LBL25 TO LBL 45 WL 208 DUE TO NO ALLOWABLE DAMAGE FOUND FOR THIS ITEM; IAW SRM 51-10-02 AND SRM 51-40-02;[02] LOCATED AND D
- [SDR SWAA2023050928363](https://openairdocs.org/sdr/SWAA2023050928363.md): Support · cracked · Apr 17, 2023 · N551WN · Boeing 73776Q · Fuselage Miscellaneous Structure
  > WING CENTER SECTION - BREAK DOWN SUPPORT HAS CRACK BS 540 LBL 1.5 WL 208<[01] REMOVED WING CENTER SECTION - BREAK DOWN SUPPORT BS 540 BL0 TO LBL 25 WL 208 DUE TO NO ALLOWABLE DAMAGE FOUND FOR THIS ITEM; IAW SR 51-10-02 AND SRM 51-40-02;[02] REMOVED WING CENTE
- [SDR SWAA2023050928225](https://openairdocs.org/sdr/SWAA2023050928225.md): Panel · pulled · Apr 16, 2023 · N551WN · Boeing 73776Q · Trailing Edge Flaps
  > PANEL 661BB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PARA 4B( REPAIRED PER SRM 51-70-04-2R-9 AS DIRECTED BY SRM 57-51-01-2R-1 PARA 4C AND TABLE 202. <BR><BR>REMOVED DAMAGE TO ALL FASTENER HOLES O
- [SDR SWAA2023050928226](https://openairdocs.org/sdr/SWAA2023050928226.md): Panel · pulled · Apr 16, 2023 · N551WN · Boeing 73776Q · Wing, Plate/Skin
  > PANEL 561AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED) FOUND PANEL TO BE 661AB. PANEL 561AB FASTENER HOLES WILL BE REPAIRED ON FAULT TTG8Q00KCULF<OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PARA 4B(5).REPAIRED PER SRM 51-70-04-2R-9 AS DIRECT
- [SDR SWAA2023050927775](https://openairdocs.org/sdr/SWAA2023050927775.md): Skin · debonded · Apr 15, 2023 · N551WN · Boeing 73776Q · Fuselage Main, Plate/Skin
  > PANEL 191FR OUTER SKIN IS DISBONDED. (MARKED)<[01] IDENTIFIED PANEL 191FR IAW SRM 53-30-70-0I-1; FIGURE 2; SHEET 1; TABLE 2; ITEM 4.<BR><BR>CLEANED PANEL FOR EVALUATION IAW AMM 51-21-11-150-815 PARA 17. C.<BR><BR>VISUALLY EXAMINED DAMAGE AND TAP TESTED WITH DI
- [SDR SWAA2023050827777](https://openairdocs.org/sdr/SWAA2023050827777.md): Floor Panel · pulled · Apr 15, 2023 · N551WN · Boeing 73776Q · Fuselage Floor Panel
  > FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL IAW SRM 53-00-50-0I-1 FIGURE 4. DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL WITH BMS4-23 TYPE II LOT 1508290-1 USING BMS5-107 LOT AK2KP8383K-1 RESIN WI
- [SDR SWAA2023050827778](https://openairdocs.org/sdr/SWAA2023050827778.md): Floor Panel · pulled · Apr 15, 2023 · N551WN · Boeing 73776Q · Fuselage Floor Panel
  > FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241AF IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. FLOOR PANEL IS DAMAGED BEYOND ECONOMICAL REPAIR; AND EXCEEDS ALLOWABLE DAMGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. FLOOR P
- [SDR SWAA2023050827779](https://openairdocs.org/sdr/SWAA2023050827779.md): Floor Panel · pulled · Apr 15, 2023 · N551WN · Boeing 73776Q · Fuselage Floor Panel
  > FLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241BF IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. FLOOR PANEL IS DAMAGED BEYOND ECONOMICAL REPAIR; AND EXCEEDS ALLOWABLE DAMGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. FLOOR P
- [SDR SWAA2023050827780](https://openairdocs.org/sdr/SWAA2023050827780.md): Floor Panel · pulled · Apr 15, 2023 · N551WN · Boeing 73776Q · Fuselage Floor Panel
  > FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL WITH BMS4-17 LOT 1522265-1 USING BMS5-107 LOT AK2KP8383K-1 RESIN WITH THE INSERTS; CURED THE RESIN UNDER A HEAT LAMP USING T
- [SDR SWAA2023050827781](https://openairdocs.org/sdr/SWAA2023050827781.md): Floor Panel · pulled · Apr 15, 2023 · N551WN · Boeing 73776Q · Fuselage Floor Panel
  > FLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIGURE 4 TABLE 4 UNDER SEAT LOW TRAFFIC SECTION 44.<BR>MULTIPLE PULLED STRANDS; DENTS & OTHER DEFECTS EXCEED THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-0
- [SDR SWAA2023050827782](https://openairdocs.org/sdr/SWAA2023050827782.md): Floor Panel · pulled · Apr 15, 2023 · N551WN · Boeing 73776Q · Fuselage Floor Panel
  > FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 SHEET 1; FIGURE 4; TABLE 4.<BR><BR>UPON INVESTIGATION; PANEL DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM<BR>53-00-50-1A-1 PAR. 4. E. & 4. F.<BR><B
- [SDR SWAA2023050827784](https://openairdocs.org/sdr/SWAA2023050827784.md): Floor Panel · pulled · Apr 15, 2023 · N551WN · Boeing 73776Q · Fuselage Floor Panel
  > FLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 232SF IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. FLOOR PANEL IS DAMAGED BEYOND ECONOMICAL REPAIR; AND EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. FLOOR
- [SDR SWAA2023050927757](https://openairdocs.org/sdr/SWAA2023050927757.md): Stringer Clip · corroded · Apr 14, 2023 · N551WN · Boeing 73776Q · Fuselage Main, Attach Fittings
  > CORROSION ON STRINGER CLIP AT ACB BS827 LBL6 WL157.<[01] FOUND TO BE WITH NO LIMITS PER SRM 53-00-53-1A2;[02] REMOVED STRINGER CLIP IAW SRM 51-40-02;[03] RECEIVED NEW STRINGER CLIP LOCATED AND DRILLED<BR>AT ACB BS827 LBL6 WL 157<BR>P/N 146A1010-10 LOT# 1478113
- [SDR SWAA2023050927747](https://openairdocs.org/sdr/SWAA2023050927747.md): Support · corroded · Apr 14, 2023 · N551WN · Boeing 73776Q · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT SPLICE AT ACB BS727D+6 LBL20 TO RBL20 WL156.<[01] THIS PART DOES NOT ALLOWABLE DAMAGE LIMITS; IT HAS TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] RECEIVED NEW SPLICE STRIP ASSY AT
- [SDR SWAA2023050927769](https://openairdocs.org/sdr/SWAA2023050927769.md): Stringer · cracked · Apr 14, 2023 · N551WN · Boeing 73776Q · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-26R WL153. MARKED<[01] CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-26R WL153 FOUND TO BE OUT OF LIMITS DUE TO CRACKS ARE NOT ALLOWED IAW SRM 53-00-03-1A-1.<BR>CUT AND REMOVED THE DAMAGED PART OF
- [SDR SWAA2023050927768](https://openairdocs.org/sdr/SWAA2023050927768.md): Stringer · cracked · Apr 14, 2023 · N551WN · Boeing 73776Q · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-27R WL150. MARKED<[01] CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-267R WL150 FOUND TO BE OUT OF LIMITS DUE TO CRACKS ARE NOT ALLOWED IAW SRM 53-00-03-1A-1.<BR>CUT AND REMOVED THE DAMAGED PART OF
- [SDR SWAA2023050927755](https://openairdocs.org/sdr/SWAA2023050927755.md): Intercostal · corroded · Apr 14, 2023 · N551WN · Boeing 73776Q · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOASTAL AT ACB BS847+9 RBL6 WL159.<[01] VERIFY APPLICABILITY PER SRM53-60-15-0I-1 AND SRM 53-60-15-1A-1<BR>REMOVED CORROSION AT DISCREPANCY AREA L=3'; W=1.5' PER SRM 51-10-02-0G-0 AND SRM 53-60-15-1A-1;[02] VERIFIED CORRECTIVE ACTION 1.;[03]
- [SDR SWAA2023050927748](https://openairdocs.org/sdr/SWAA2023050927748.md): Support · corroded · Apr 14, 2023 · N551WN · Boeing 73776Q · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB LBL21 BS727A - BS807 WL156.<[01] SRM 53-60-53-0I-2 IDENTIFICATION AND SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 ARE APPLICABLE;[02] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT UPPER SURFACE 03 EACH LOCATIONS L=19';
- [SDR SWAA2023050927751](https://openairdocs.org/sdr/SWAA2023050927751.md): Attach Angle · corroded · Apr 14, 2023 · N551WN · Boeing 73776Q · Fuselage Main, Attach Fittings
  > CORROSION ON INTERCOSTAL TO WEB ATTACH ANGLE BS767+2; 767+5; 767+9; 767+16; 767+19 RBL21 WL156.<[01] FOUND TO BE OUT OF LIMITS EXFOLIATED CORRODED WITH MORE THE 50 % OF MATERIAL LOST IWA B 737-700 SRM 53-60-15 REMOVED DAMAGE PART PER SRM 51-40-02;[02] SRM 53-6
- [SDR SWAA2023050927749](https://openairdocs.org/sdr/SWAA2023050927749.md): Sidewall Support · corroded · Apr 14, 2023 · N551WN · Boeing 73776Q · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB RBL21 BS727B+4; BS727C+14 - BS767 WL156.<[01] VERIFY APPLICABILITY PER SRM 53-60-53-0I-2 AND SRM 53-00-53-1A-2.<BR>REMOVED CORROSION ON DISCREPANCY AREA L=0.800';W=0.700';D=0.010'. FOUND TO BE OUT OF LIMITS IAW SRM
- [SDR SWAA2023050927764](https://openairdocs.org/sdr/SWAA2023050927764.md): Shield · corroded · Apr 14, 2023 · N551WN · Boeing 73776Q · Fuselage Miscellaneous Structure
  > CORROSION ON AFT SHIELD AT FWD CARGO BAY BS500 RBL24 WL156.<[01] AFT SHIELD AT FORWARD CARGO BAY LOCATED BETWEEN BS492.4- BS500A RBL 24 WL 156 NOT HAS ENTRIES ALLOWABLE DAMAGE IN SRM. MUST BE REPAIR BY REPLACEMENT IAW SRM 51-10-02 PARAGRAPH 9.C.;[02] VERIFIED
- [SDR SWAA2023050927750](https://openairdocs.org/sdr/SWAA2023050927750.md): Cargo Track · corroded · Apr 14, 2023 · N551WN · Boeing 73776Q · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TRACK AT ACB BS787+12 RBL14 WL157.<FOUND TO OUT OF LIMITS ORIGINAL MATERIAL.070 REMAINING MATERIAL.060 ALLOWABLE DAMAGE LIMITS IS.007.;[13] UPDATED CORRECTIVE ACTION 5. REMOVED NUTPLATE PER B737-700 SRM 51-40-02-0G-0.;[14] OBTAINED LOCATED AND
- [SDR SWAA2023050927762](https://openairdocs.org/sdr/SWAA2023050927762.md): Sidewall Support · corroded · Apr 14, 2023 · N551WN · Boeing 73776Q · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS400 - BS500D LBL23 WL156.<OUT OF LIMITS; WILL BE REPAIR BY REPLACEMENT PER SRM 51-10-02 PARAG. 9.C;[05] RECEIVED EXTRUSION P/N BAC1496-444 LOT. 1524635-1. LOCATED AND DRILLED (2EA) EXTRUSION (FORMED CHANNEL) ON F
- [SDR SWAA2023050927767](https://openairdocs.org/sdr/SWAA2023050927767.md): Intercostal · cracked · Apr 14, 2023 · N551WN · Boeing 73776Q · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT AREA AFT OF FCB BS500D+18 RBL31 S-25R WL159.<[01] REMOVED INTERCOSTAL AT AREA AFT OF FCB BS500D+18 RBL31 S-25R WL159 IAW SRM 51-40-02.-;[02] RECEIVED NEW INTERCOSTAL HFAB53-AN-011 (7075T0#0.032'') PER DWG# 143A9803-58 HEAT TREATED TO T62
- [SDR SWAA2023050927758](https://openairdocs.org/sdr/SWAA2023050927758.md): Attach Angle · corroded · Apr 14, 2023 · N551WN · Boeing 73776Q · Fuselage Main, Attach Fittings
  > CORROSION ON ATTACH ANGLE AT ACB BS727E LBL7 WL152.<[01] FOUND TO BE WITH NO LIMITS IAW SRM 53-00-53-1A-2;[02] PART TO BE REPAIR BY REPLACEMENT PEER SRM 51-10-02 PARAGRAPH 9.C;[03] REMOVED ATTACH ANGLE AT ACB BS 727E LBL7 WL 152 IAW SRM 51-40-02;[04] RECEIVED
- [SDR SWAA2023050827765](https://openairdocs.org/sdr/SWAA2023050827765.md): Attach Angle · cracked · Apr 14, 2023 · N551WN · Boeing 73776Q · Fuselage Main, Attach Fittings
  > FWD CARGO BAY BAFFLE ATTACH ANGLE CRACKED BS500A FWD SIDE LBL25 WL155.<[01] VERIFIED APPLICABILITY FOR SRM 51-10-02 PARAG 9.REPAIRABLE BY REPLACEMENT.;[02] PRIOR TO REMOVAL FOUND PART HAS NOT ALLOWABLE DAMAGE ON SRM;PART WILL BE REPAIRABLE BY REPLACEMENT;PER S
- [SDR SWAA2023050827766](https://openairdocs.org/sdr/SWAA2023050827766.md): Attach Angle · cracked · Apr 14, 2023 · N551WN · Boeing 73776Q · Fuselage Main, Attach Fittings
  > FWD CARGO BAY BAFFLE ATTACH ANGLE CRACKED BS500B FWD SIDE RBL25 WL155.<[01] VERIFIED APPLICABILITY FOR SRM 51-10-02 PARAG 9.REPAIRABLE BY REPLACEMENT.;[02] PRIOR TO REMOVAL;FOUND PART HAS NOT ALLOWABLE DAMAGE ON SRM;PART WILL BE REPAIRABLE BY REPLACEMENT;PER S
- [SDR SWAA2023050827319](https://openairdocs.org/sdr/SWAA2023050827319.md): Frame · cracked · Apr 13, 2023 · N551WN · Boeing 73776Q · Fuselage Main, Frame
  > CRACK ON PASSENGER CABIN FRAME AT BS 727B STRINGER BETWEEN 8L-9L.(MARKED)<[01] FORMED ANGLE REPAIR PART B PER EA 1-A53-12114 APPENDIX REV A OK TO HEAT AND TRAET;[02] MATERIAL ID 7075-0.050 LOT # 1517365-2;[03] REMOVED DAMAGE PER EA 1-A53-12114;[04] WORK ACCOM
- [SDR SWAA2023050926587](https://openairdocs.org/sdr/SWAA2023050926587.md): Pulley · cracked · Apr 12, 2023 · N551WN · Boeing 73776Q · Fuselage Structure (General)
  > CRACK ON ST B PULLEY ATTACH ANGLE AT BS 1040 RBL 8 ABOVE STRINGER 25R.(MARKED)<[01] VERIFIED APPLICABILITY FOR SRM 51-10-02 PARAG. 9; REPAIRABLE BY REPLACEMENT.;[02] REMOVED STB PULLEY ATTACH CLIP AT BS 1040 RBL 8 ABOVE STRINGER 25R PER SRM 51-40-02.;[03] FABR
- [SDR SWAA2023050926303](https://openairdocs.org/sdr/SWAA2023050926303.md): Stiffener · cracked · Apr 12, 2023 · N551WN · Boeing 73776Q · Horizontal Stabilizer Structure
  > CRACK INDICATIONS ON L/H H-STAB RIB 4 STIFFENERS 2 & 3 LOWER RADII.<REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 120.30 RIB 2ND AND 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[03] HFEC REQUEST ON 2ND AND 3RD VERTICAL STIFFENER ON CUT OUT EDGES; W
- [SDR SWAA2023050926302](https://openairdocs.org/sdr/SWAA2023050926302.md): Web · cracked · Apr 11, 2023 · N551WN · Boeing 73776Q · Fuselage Main, Attach Fittings
  > INTERNAL - HORIZONTAL PRESSURE DECK WEB STA 663 TO STA 675 - LBL 30 TO LBL 45. MULTIPLE CRACKS NOTED. MARKED AREAS.<[01] SRM 53-40-51-2R-2 REPAIR 2 IS APPLICABLE TO THIS A/C;[02] CUT AND REMOVED THE DAMAGED PART OF WEB IAW SRM 53-40-51-2R-2 REPAIR 2 STEP 4C(3)
- [SDR SWAA2023050926299](https://openairdocs.org/sdr/SWAA2023050926299.md): Vapor Barrier · cracked · Apr 11, 2023 · N551WN · Boeing 73776Q · Fuselage Main, Keel
  > WING CENTER SECTION - LH VAPOR BARRIER HAS A CRACK BS 663 LBL 15 WL 148 (MARKED)<DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PAR.4 D(1) TO BE REPAIRED IAW SRM 51-70-04-2R-10 AS DIRECTED BY SRM 57-10-10-2R-2 PAR.1 C(NOTE)<BR><BR>REMOVED DAMAGED
- [SDR SWAA2023050925704](https://openairdocs.org/sdr/SWAA2023050925704.md): Panel · pulled · Apr 10, 2023 · N551WN · Boeing 73776Q · Trailing Edge Flaps
  > PANEL 561CB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4.B(5).WILL BE REPAIRED IAW SRM 51-70-04-2R-9 PER SRM 57-51-01-2R-1 PARA 2.B(2) AND TABLE 202.<BR>REMOVED ALL DAMAGE AT FASTENER HOLES TO.5' DI
- [SDR SWAA2023050925703](https://openairdocs.org/sdr/SWAA2023050925703.md): Panel · pulled · Apr 10, 2023 · N551WN · Boeing 73776Q · Trailing Edge Flaps
  > PANEL 561AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4.B(5).REPAIRED IAW SRM 51-70-04-2R-9 PER SRM 57-51-01-2R-1 PARA 2.B(2) AND TABLE 202.REMOVED ALL DAMAGE AT FASTENER HOLES TO.5' DIAMETER; CLEA
- [SDR SWAA2023050825699](https://openairdocs.org/sdr/SWAA2023050825699.md): Battery Pack · inoperative · Apr 10, 2023 · N551WN · Boeing 73776Q · Emergency Lighting
  > REMOVE EMERGENCY LIGHTS BATTERY PACK M1675 FOR USE ON A/C 8574 **CORRECTED FAULT DESCRIPTION **REMOVE EMERGENCY LIGHTS BATTERY PACK M1675 FOR USE ON A/C 8527<[01] REMOVED BATTERY PACK M1675 IAW AMM 33-51-06-960-805 STEP E. (1 - 4);[02] INSTALLED SERVICEABLE EM
- [SDR SWAA2022121280250](https://openairdocs.org/sdr/SWAA2022121280250.md): Lens · missing · Dec 10, 2022 · N551WN · Boeing 73776Q · Emergency Lighting
  > OVER WING EXIT SIGN; RIGHT SIDE MISSING / [01] INSTALLED RT SIDE OVER WING EXIT SIGN LEN ONLY PER AMM 33-51-01; OPS CHECK EMERGENCY LIGHT; LIGHT CHECK OUT GOOD

Next page: https://openairdocs.org/deregistered/N551WN-2025-05-23/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 = 'N551WN' AND deregistration_id = 'N551WN-2025-05-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N551WN-2025-05-23/reports

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