# Service difficulty reports: N8622A, cancelled Feb 28, 2025

A list on [N8622A, cancelled Feb 28, 2025](https://openairdocs.org/deregistered/N8622A-2025-02-28.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 3 · 147 reports

- [SDR SWAA2025012788285](https://openairdocs.org/sdr/SWAA2025012788285.md): Light · cracked · Jan 21, 2025 · N8622A · Boeing 7378H4 · Emergency Lighting
  > FWD BULLNOSE COVE EMERGENCY LIGHT ASSEMBLY CRACKED<[01] UPON FURTHER INVESTIGATION FOUND REPLACED BULLNOSE COVE EMERGENCY LIGHT LENS IS CRACKED. <BR><BR>REPLACED BULLNOSE COVE EMERGENCY LIGHT LENS AND PERFORMED GOOD OPS CHECK IAW AMM 33-51-03-960-803;[02] VERI
- [SDR SWAA2025010774382](https://openairdocs.org/sdr/SWAA2025010774382.md): Scuff Plate · cracked · Dec 6, 2024 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED. REPAIRED AFT CARGO BAY FWD CORNER SCUFF PLATE PER SRM 53-60-15-2R-1. REMOVED FWD CORNER SCUFF PLATE IAW AMM 53-10-02-020-801AT THE AFT CARGO BAY. REPAIRED PER SRM 53-60-15-2R-1 PARA 4.B.(4).
- [SDR SWAA2025010773732](https://openairdocs.org/sdr/SWAA2025010773732.md): Floor Support · corroded · Dec 3, 2024 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FCB SIDEWALL -TO -FLOOR SUPPORT SURFACE HAS CORROSION AT BS500 TO BS500D WL156 LBL22.<[01] FCB SIDEWALL -TO -FLOOR SUPPORT<BR>BS.480+10' TO BS.500I LBL.23 WL.156<BR>REPAIRED IN FAULT TTG8Q00X5VBQ;[02] JOB COMPLETE.
- [SDR SWAA2025010772969](https://openairdocs.org/sdr/SWAA2025010772969.md): Shield · corroded · Dec 1, 2024 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB UNDER ACB FWD SHIELD BS 767-787 RBL 23 (MARKED)<[01] REMOVED AND REPLACED WEB UNDER ACB FWD SHIELD BS 767-787 RBL 23 I.A.W SRM 51-40-02-0G-0 AND DWG 146A0081.;[02] VERIFIED STEP 6 COMPLETE.;[03] VERIFIED ALL STEPS; CORRECTION ACTION ITEM 1; ME
- [SDR SWAA2025010772968](https://openairdocs.org/sdr/SWAA2025010772968.md): Support Angle · corroded · Dec 1, 2024 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB FWD SHIELD SUPPORT ANGLE BS 767-787 RBL 23<[01] REMOVED AND REPLACED ACB FWD SHIELD SUPPORT ANGLE P/N 146A8125-53 BS767 TO BS787 RBL23 IAW SRM 51-40-02 AND DWG 146A0081 REV B;[02] JOB COMPLETE.
- [SDR SWAA2025010872690](https://openairdocs.org/sdr/SWAA2025010872690.md): Floor Support · cracked · Nov 30, 2024 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > INTERCOSTAL B.S. 500B-500C LBL 22 IS CRACKED.<[01] REMOVED AND REPLACED NEW INTERCOSTAL B.S. 500B-500C LBL 22 P/N 143A7510-21 I.A.W SRM 51-40-02-0G-0 AND DWG 143A7505 REV:-;[02] VERIFIED ACTION 1.;[03] JOB COMPLETE.
- [SDR SWAA2025010772528](https://openairdocs.org/sdr/SWAA2025010772528.md): Shield · corroded · Nov 29, 2024 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ACB; SHIELD BS 847+8 RBL 23 HAS CORROSION (MARKED).<[01] REMOVED AND REPLACED ACB; SHIELD BS 847 TO BS867 RBL 23 I.A.W SRM 51-40-02-0G-0 AND DWG 146A0081.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2025010871928](https://openairdocs.org/sdr/SWAA2025010871928.md): Baffle · cracked · Nov 26, 2024 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FCB BAFFLE ASSY ATTACH ANGLE CRACKED AFT SIDE OF BS500H FRAME LBL23 WL156<[01] REMOVED AND REPLACED ANGLE PER REF SRM 51-40-02 AND DWG 143A7505;[02] JOB COMPLETE.
- [SDR SWAA2025010870405](https://openairdocs.org/sdr/SWAA2025010870405.md): Intercostal · cracked · Nov 21, 2024 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD CABIN BS295.5 S-16L WL216.<[01] REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)] AND DGW 141A8180 ID:003 REV: A;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025010870404](https://openairdocs.org/sdr/SWAA2025010870404.md): Stringer · cracked · Nov 21, 2024 · N8622A · Boeing 7378H4 · Fuselage Main, Longeron/Stringer
  > PASSENGER CABIN FED UPPER FRAME BS 312 STR 5L CRACKED<[01] THIS FAULT WILL BE ACCOMPLISHED ON M-22-153-01244 (737-NG - SWA);[02] JOB COMPLETE. REF TTG8Q00XASF0
- [SDR SWAA2025010870073](https://openairdocs.org/sdr/SWAA2025010870073.md): Stringer Clip · cracked · Nov 20, 2024 · N8622A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > ACB; STRINGER CLIP AT BS 727F S-22R HAS A CRACK (MARKED).<[01] REMOVED AND RE INSTALLED ACB; STRINGER CLIP AT BS 727F S-22R I.A.W SRM 51-40-02-0G-0.<BR><BR>NO CRACKS NOTED;[02] VERIFIED ALL STEPS; CORRECTION ACTION ITEM 1; MEASUREMENT FIELD COMPLETE; CARD COMP
- [SDR SWAA2025010770078](https://openairdocs.org/sdr/SWAA2025010770078.md): Support · corroded · Nov 20, 2024 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ACB; AFT BULKHEAD LOWER SUPPORT BS 947 RBL 10 TO 18 HAS CORROSION (MARKED).<[01] REMOVED AND REPLACED AFT BULKHEAD LOWER SUPPORT BS 947 I.A.W SRM 51-40-02-0G-0 AND DWG 149A8117.;[02] JOB COMPLETE.
- [SDR SWAA2025010770077](https://openairdocs.org/sdr/SWAA2025010770077.md): Support · corroded · Nov 20, 2024 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ACB; SIDEPLATE SUPPORT ZEE BS 767 TO 787+5 RBL 23 HAS SEVERAL SPOTS WITH CORROSION (MARKED).<[01] 01 - REMOVED AND REPLACED PER [SRM 51-10-02-0G-0-B00070 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)];[02] VERIFIED ALL RII STEPS COMPLETE.
- [SDR SWAA2025010770079](https://openairdocs.org/sdr/SWAA2025010770079.md): Support · corroded · Nov 20, 2024 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ACB; SIDEPLATE SUPPORT ZEE RBL 23 BS 727 TO 767 WL 157 HAS SEVERAL SPOTS WITH CORROSION AND BS 727I HAS A CRACK (MARKED).<[01] REMOVED AND REPLACED SIDEPLATE SUPPORT ZEE AT ACB RBL 23 BS 727 TO BS 767 WL 157 IAW SRM 51-40-02 AND DWG 146A7500 REV: -;[02] VERIFI
- [SDR SWAA2025010770074](https://openairdocs.org/sdr/SWAA2025010770074.md): Sidewall Support · corroded · Nov 20, 2024 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ACB; SIDEPLATE SUPPORT ZEE LBL 23 BS 727 TO 847 WL 157 HAS SEVERAL SPOTS WITH CORROSION (MARKED).<[01] REMOVED AND REPLACED AFT CARGO BAY L/H FLOOR TO SIDE WALL SUPPORT ANGLE AT BS 727 TO BS 847; LBL-23; WL-157 IAW SRM 51-40-05-0G-0 AND DWG# 146A7500;[02] VERI
- [SDR SWAA2025010769892](https://openairdocs.org/sdr/SWAA2025010769892.md): Shield · cracked · Nov 20, 2024 · N8622A · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > #1 ENG I/B FAN COWL OIL ACCESS DOOR SHIELD CRACKED.<[01] REMOVED AND REPLACED #1 ENG I/B FAN COWL OIL DOOR SHIELD IAW SRM 51-40-02-0G-0 STEP 4 AND 5.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025010861618](https://openairdocs.org/sdr/SWAA2025010861618.md): Attach Angle · cracked · Nov 19, 2024 · N8622A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > BAFFLE ASSEMBLY ATTACH ANGLE IS CRACKED IN FCB BS500G+18 LBL23 WL156.<[01] REMOVED AND REPLACED ANGLE PER REF SRM 51-40-02 AND DWG 143A7505;[02] JOB COMPLETE.
- [SDR SWAA2025010861622](https://openairdocs.org/sdr/SWAA2025010861622.md): Attach Angle · cracked · Nov 19, 2024 · N8622A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > BAFFLE ASSEMBLY ATTACH ANGLE IS CRACKED IN FCB BS500H LBL23 WL156.<[01] REMOVED AND REPLACED ANGLE PER REF SRM 51-40-02 AND DWG 143A7505;[02] JOB COMPLETE.
- [SDR SWAA2025010861619](https://openairdocs.org/sdr/SWAA2025010861619.md): Attach Angle · cracked · Nov 19, 2024 · N8622A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > BAFFLE ASSEMBLY ATTACH ANGLE IS CRACKED IN FCB BS500H RBL23 WL156.<[01] REMOVED AND REPLACED ATTACH ANGLE P/N 143A7502U158 LOT 1568341-1 AT FCB BS500H RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A7505;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025010861627](https://openairdocs.org/sdr/SWAA2025010861627.md): Attach Angle · cracked · Nov 19, 2024 · N8622A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACKED BAFFLE ASSEMBLY ATTACH ANGLE IN FCB BS500F+18 RBL23 WL156.<[01] REMOVED AND REPLACED ATTACH ANGLE P/N 143A7502U158 LOT 1568341-1 AT FCB BS500F+18 RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A7505;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025010872363](https://openairdocs.org/sdr/SWAA2025010872363.md): Shield · corroded · Nov 19, 2024 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FCB AFT SHIELD FROM BS480 +13 TO BS500+16 RBL24 WL156.<[01] REMOVED AND REPLACED AFT SHIELD ASSY. AT FCB BETWEEN BS.492.4 - BS.500A RBL 24 WL 156 IAW B-737-800 SRM 51-10-02; SRM 51-40-02 & DWG#143A0080 REV: -;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025010861628](https://openairdocs.org/sdr/SWAA2025010861628.md): Attach Angle · cracked · Nov 19, 2024 · N8622A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > BAFFLE ASSEMBLY ATTACH ANGLE IS CRACKED IN FCB BS440 LBL18 WL156.<[01] REMOVED AND REPLACED ANGLE PER REF SRM 51-40-02 AND DWG 143A7505;[02] JOB COMPLETE.
- [SDR SWAA2025010861625](https://openairdocs.org/sdr/SWAA2025010861625.md): Stringer Clip · corroded · Nov 19, 2024 · N8622A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CLIP AT BS 1006 S-9L HAS A CORROSION (MARKED).<[01] FABRICATED STRINGER CLIP 9L AT BS 1006 AND INSTALLED PER SRM 51-40-02; DWG#147A3500; DWG 147A3287.TASK CARD COMPLETED.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025010761620](https://openairdocs.org/sdr/SWAA2025010761620.md): Floor Support · corroded · Nov 19, 2024 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS WITH CORROSION ON FCB SIDEWALL TO FLOOR SUPPORT NUTPLATE HOLES FROM BS500A+12 TO BS500H+15 RBL24 WL156.<[01] MEASUREMENT TABLE ITEM 22 'NO' INCORRECT BY AMT; PHOTO IS CURRENTLY IN THE ATTACHMENT; SO AMT MUST EDIT TO 'YES'.;[02] REMOVED AND REPLA
- [SDR SWAA2025010761626](https://openairdocs.org/sdr/SWAA2025010761626.md): Attach Angle · cracked · Nov 19, 2024 · N8622A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > BAFFLE ASSEMBLY ATTACH ANGLE IS CRACKED IN FCB BS500G+18 RBL23 WL156. REMOVED AND REPLACED ATTACH ANGLE P/N 143A7502U154 LOT 1582135-3 AT FCB BS500G+18 RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A7505.
- [SDR SWAA2025010761616](https://openairdocs.org/sdr/SWAA2025010761616.md): Sidewall Support · corroded · Nov 19, 2024 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS WITH CORROSION ON FCB SIDEWALL TO FLOOR SUPPORT NUTPLATE HOLES AT BS500A+16 TO BS500C+13; BS500+6 TO BS500I LBL23 WL156. REMOVED AND REPLACE FCB SIDEWALL SUPPOT BS 480 TO BS 500I IAW SRM 51-10-02-0G-0 DWG 143A7505; DWG 143A7500. THE DAMAGE WA
- [SDR SWAA2025010661342](https://openairdocs.org/sdr/SWAA2025010661342.md): Floor Panel · pulled · Nov 19, 2024 · N8622A · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 241KF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241KF WITH UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 146A5810 ID:0
- [SDR SWAA2025010861337](https://openairdocs.org/sdr/SWAA2025010861337.md): Seal · cracked · Nov 18, 2024 · N8622A · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > RT. HORIZONAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED RT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
- [SDR SWAA2025010861338](https://openairdocs.org/sdr/SWAA2025010861338.md): Seal · cracked · Nov 18, 2024 · N8622A · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > LT. HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED LT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
- [SDR SWAA2025010761021](https://openairdocs.org/sdr/SWAA2025010761021.md): Scuff Plate · cracked · Nov 17, 2024 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] CORNER AFT SCUFF PLATE REPAIRED ON THE AFT CARGO BAY PER SRM 53-60-15-2R-1 PARA 4.B.(4). APPLIED TREAT AND PRIMED AT INNER SURFACES OF SCUFF PLATE PER SOPM 20-40-03 & SOPM 20-41-02.
- [SDR SWAA2025010860469](https://openairdocs.org/sdr/SWAA2025010860469.md): Fairlead · debonded · Nov 16, 2024 · N8622A · Boeing 7378H4 · Elevator Structure
  > CUSTOMER REQUEST: 'EMPENAGE ELEVATOR LH - TAB UPPER IB SURFACE FAIRING DISBONDED'<[01] RE-BONDED LH ELEVATOR TAB UPPER I/B FAIRING PER DWG 183A8100-3 FL 10 AND BAC 5010 TYPE 70.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025010660029](https://openairdocs.org/sdr/SWAA2025010660029.md): Floor Panel · pulled · Nov 15, 2024 · N8622A · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 231RF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231RF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 143A5810 ID:0531.;[02] JOB COMP
- [SDR SWAA2024090433090](https://openairdocs.org/sdr/SWAA2024090433090.md): Lamp · inoperative · Sep 1, 2024 · N8622A · Boeing 7378H4 · Emergency Lighting
  > R/H SIDE FWD EMERGENCY EXTERIOR LIGHT INOP<[01] REPLACED R/H FWD EXTERIOR EMERGENCY LIGHT LAMP IAW AMM 33-51-04. OPS. CHECK GOOD.
- [SDR SWAA2024080521664](https://openairdocs.org/sdr/SWAA2024080521664.md): Power Supply · inoperative · Aug 2, 2024 · N8622A · Boeing 7378H4 · Emergency Lighting
  > AFT ENTRY EXTERNAL EMERGENCY LIGHT INOP<[01] RELAMPED; NO HELP. R&R?D POWER SUPPLY PER AMM 33-51-06
- [SDR SWAA2024072918246](https://openairdocs.org/sdr/SWAA2024072918246.md): Light · inoperative · Jul 27, 2024 · N8622A · Boeing 7378H4 · Emergency Lighting
  > L/H AFT OUTTER EMERGENCY LIGHT INOP<[01] RELAMPED OUTTER EMERGENCY LIGHT IAW AMM 33-51-04. LAMP WORKING AT THIS TIME.
- [SDR SWAA2024062404366](https://openairdocs.org/sdr/SWAA2024062404366.md): Fan · burned · Jun 21, 2024 · N8622A · Boeing 7378H4 · Air Distribution Fan
  > ABOUT 2 HOURS INTO FLIGHT FA'S REPORT BURNING SMELL SIMILAR TO OR BURNT HAIR THE SMELL WAS MOST NOTICED FROM ROW 19-24 AND IN FRONT & BACK GALLEY SMELL WAS INTERMITTENT STRONG FOR A FEW MIN MINUTES THEN GONE COMPLETELY CAME AND WENT SEVERAL TIMES. COMPLIED W
- [SDR SWAA2024010236762](https://openairdocs.org/sdr/SWAA2024010236762.md): Battery · inoperative · Dec 31, 2023 · N8622A · Boeing 7378H4 · Emergency Lighting
  > LEFT AFT AISLE EMERGENCY LIGHTS OUT<[01] REPLACED AFT EMERGENCY LIGHT BATTERY REF AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2023103110358](https://openairdocs.org/sdr/SWAA2023103110358.md): Floor Panel · cracked · Oct 12, 2023 · N8622A · Boeing 7378H4 · Fuselage Floor Panel
  > L/H FLIGHT COMPARTMENT CONSOLE PANEL 211FW SKIN CRACKED MKD DOT<[01] MEASUREENTS;[02] REPAIRED DAMAGE AREA AT L/H FLIGHT COMPARTMENT CONSOLE PANEL 211FW AS PER AMM 25-00-00-340-801.;[03] VERIFIED STEPS 1 AND 2
- [SDR SWAA2023103109837](https://openairdocs.org/sdr/SWAA2023103109837.md): Doubler · cracked · Oct 11, 2023 · N8622A · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > EXTERNAL GROUND POWER DOOR CUTOUT LOWER DOUBLER SKIN CRACKED; MISSING A PIECE OF SKIN<[01] ACCOMPLISH EXTERNAL GROUND POWER DOOR CUTOUT LOWER DOUBLER SKIN REPAIR AS PER SRM 53-10-15-2R-4 AND BOEING DRAWING#141A8701.;[02] VERIFIED STEP 1;[03] ACCOMPLISHED EXTER
- [SDR SWAA2023103109838](https://openairdocs.org/sdr/SWAA2023103109838.md): Floor Support · cracked · Oct 11, 2023 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR CENTER WING BOX FLOOR SUPPORT BREAK CRACKED AT STA 540 LBL 1 WL 208.1<[01] INSTALLED MAIN CABIN FLOOR CENTER WING BOX FLOOR SUPPORT BREAK AT STA 540 LBL 1 WL 208.1 PART NUMBER 143A5240U33 AS PER SRM 51-40-02-0G-0.;[02] REMOVED AND REPLACED MAI
- [SDR SWAA2023103109839](https://openairdocs.org/sdr/SWAA2023103109839.md): Floor Support · cracked · Oct 11, 2023 · N8622A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR CENTER WING BOX FLOOR SUPPORT BREAK CRACKED AT STA 540 RBL 1 WL 208.1<[01] INSTALLED MAIN CABIN FLOOR CENTER WING BOX FLOOR SUPPORT BREAK AT STA 540 RBL 1 WL 208.1. PART NUMBER 143A5240U34 AS PER SRM 51-40-02-0G-0.;[02] REMOVED AND REPLACED MA
- [SDR SWAA2023103109645](https://openairdocs.org/sdr/SWAA2023103109645.md): Access Panel · corroded · Oct 10, 2023 · N8622A · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > CORROSION AT LOWER FUS AFT LAVATORY SERVICE ACCESS PANEL 145AL AT BONDING WIRE ATTACHING POINT MKD DOT<[01] REMOVED CORROSION;AS PER SRM51-10-02-OG-0;CHECK LIMITS FOUND OUT OF LIMITS AS PER SRM 52-40-01-1A-4.AT LOWER FUS AFT LAVATORY SERVICE ACCESS PANEL 145AL
- [SDR SWAA2023103109624](https://openairdocs.org/sdr/SWAA2023103109624.md): Handle · loose · Oct 10, 2023 · N8622A · Boeing 7378H4 · Passenger/Crew Doors
  > FWD CABIN ENTRY L-1 DOOR EXTERNAL HANDLE HAS PLAY MKD DOT<[01] ADJUSTMENT WILL BE PERFORMED IN TC TTG8Q00NXNTU;[02] VERIFIED STEP 1
- [SDR SWAA2023103109657](https://openairdocs.org/sdr/SWAA2023103109657.md): Panel · delaminated · Oct 10, 2023 · N8622A · Boeing 7378H4 · Wing, Plate/Skin
  > PANEL 621HB (PANEL 621HB PANEL ASSEMBLY - LOWER LEADING EDGE ACCESS - RIGHT WING) WITH DELAMINATED LE CORNER.<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #621HB AS MARKED AS PER B737 SRM 57-41-01-2R-1; B737 SRM 51-70-04-2R-13 PARAG (4-D-G) AND B737 S
- [SDR SWAA2023103109658](https://openairdocs.org/sdr/SWAA2023103109658.md): Panel · delaminated · Oct 10, 2023 · N8622A · Boeing 7378H4 · Wing, Plate/Skin
  > PANEL 621VB (PANEL 621VB PANEL ASSEMBLY - LOWER LEADING EDGE ACCESS - RIGHT WING) WITH DELAMINATED LE CORNER.<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #621VB AS MARKED AS PER B737 SRM 57-41-01-2R-1; B737 SRM 51-70-04-2R-13 PARAG (4-D-G) AND B737 S
- [SDR SWAA2023103109659](https://openairdocs.org/sdr/SWAA2023103109659.md): Panel · delaminated · Oct 10, 2023 · N8622A · Boeing 7378H4 · Wing, Plate/Skin
  > PANEL 621XB (PANEL 621XB PANEL ASSEMBLY - LOWER LEADING EDGE ACCESS - RIGHT WING) WITH DELAMINATED LE CORNER.<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #621XB AS MARKED AS PER B737 SRM 57-41-01-2R-1; B737 SRM 51-70-04-2R-13 PARAG (4-D-G) AND B737 S
- [SDR SWAA2023103109656](https://openairdocs.org/sdr/SWAA2023103109656.md): Panel · debonded · Oct 10, 2023 · N8622A · Boeing 7378H4 · Wing, Plate/Skin
  > PANEL 621JB (PANEL 621JB PANEL ASSEMBLY - LOWER LEADING EDGE ACCESS - RIGHT WING) WITH DISBONDED LE CORNER.<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #621JB AS MARKED AS PER B737 SRM 57-41-01-2R-1; B737 SRM 51-70-04-2R-13 PARAG (4-D-G) AND B737 SRM
- [SDR SWAA2023103109651](https://openairdocs.org/sdr/SWAA2023103109651.md): Rib · cracked · Oct 10, 2023 · N8622A · Boeing 7378H4 · Wing, Rib/Bulkhead
  > R/W REAR SPAR T/E FIXED DEFLECTION CONTROL PANEL ATTACHED TO DEFLECTION RIB CRACKED AT LOCATION ' A' MKD DOT<[01] ACCOMPLISHED REPAIR OF R/W REAR SPAR T/E FIXED DEFLECTION CONTROL PANEL RIB TAB AS PER SRM 57-51-02-2R-3; SRM 57-51-02-2R-1.;[02] VERIFIED STEP 1
- [SDR SWAA2023092102055](https://openairdocs.org/sdr/SWAA2023092102055.md): Flashlight · inoperative · Sep 19, 2023 · N8622A · Boeing 7378H4 · Emergency Equipment
  > FWD OUTBOARD FLASHLIGHT INOP.<[01] REPLACED FLASHLIGHT PER AMM 25-64-00.
- [SDR SWAA2023041726967](https://openairdocs.org/sdr/SWAA2023041726967.md): Seal · cracked · Apr 13, 2023 · N8622A · Boeing 7378H4 · Horizontal Stabilizer Structure
  > TAIL LEFT STABILIZER FORWARD UPPER SLIDING SEAL CRACKED<[01] R&R TAIL LEFT STABILIZER FORWARD UPPER SLIDING SEAL REF AMM 53-31-31.

Next page: https://openairdocs.org/deregistered/N8622A-2025-02-28/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 = 'N8622A' AND deregistration_id = 'N8622A-2025-02-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N8622A-2025-02-28/reports

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