# Service difficulty reports: N8610A

A list on [N8610A](https://openairdocs.org/aircraft/N8610A.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 4 · 171 reports

- [SDR SWAA2026101909356](https://openairdocs.org/sdr/SWAA2026101909356.md): Battery Pack · inoperative · Oct 15, 2026 · N8610A · Boeing 7378H4 · Emergency Lighting
  > RIGHT OVERWING EXIT INTERNAL EMERGENCY LIGHTS WERE INOPERAIVE. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805. OPS TESTED GOOD.
- [SDR SWAA2026082514571](https://openairdocs.org/sdr/SWAA2026082514571.md): Lens · displaced · Aug 21, 2026 · N8610A · Boeing 7378H4 · Emergency Lighting
  > L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT LENS DISPLACED. SECURED THE LENS IAW AMM 33-51-04. LIGHT DOES NOT ILLUMINATE. OK TO CONTINUE IAW MEL 33-14-01. RELAMPED AS REQUIRED 33-51-04.
- [SDR SWAA2026072799239](https://openairdocs.org/sdr/SWAA2026072799239.md): Lens · missing · Jul 22, 2026 · N8610A · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN AT ROW 13ABC MISSING LENS. REPLACED THE LENS IAW AMM 33-51-01
- [SDR SWAA2026071502202](https://openairdocs.org/sdr/SWAA2026071502202.md): Engine · slow · Jul 11, 2026 · N8610A · Boeing 7378H4 · Fuel Controlling System
  > AFTER LANDING NR 1 ENGINE SLOW/ NO RESPONSE TO THRUST LEVER MOVEMENT. PERFORMED EEC BITE IAW FIM 73-00 TASK 801 NO FAULTS AND PERFORMED ENGINE RUN IAW AMM 71-00-00 ALL INDICATIONS NORMAL. ACFT OK FOR SERVICE.
- [SDR SWAA2026071545498](https://openairdocs.org/sdr/SWAA2026071545498.md): Pump · failed · Jul 11, 2026 · N8610A · Boeing 7378H4 · Engine Fuel Pump
  > OTS, NR 1 ENGINE FAILED IN FLIGHT. ATTEMPTED RESTART WITH NO SUCCESS. LANDED SINGLE ENGINE. NO AIRFRAME OR OTHER ABNORMAL ENGINE INDICATIONS PRIOR TO FAILURE. HMU AND FUEL PUMP PACKAGE REMOVED AND REPLACED IAW AMM 73-21-10; 73-11-01. OPS CHECK GOOD. REF TTG8R
- [SDR SWAA2026040784991](https://openairdocs.org/sdr/SWAA2026040784991.md): Skin · debonded · Mar 31, 2026 · N8610A · Boeing 7378H4 · Trailing Edge Flaps
  > DISBOND ON LH OUTBD AFT FLAP UPPER SKIN.<[01] REMOVED LT OTBD AFT FLAP PER AMM 27-51-22. INSTALLED NEW LT OTBD AFT FLAP PER AMM 27-51-22; ACCOMPLISHED RIG PER AMM 27-51-22 AND AMM 27-51-26;
- [SDR SWAA2026040184583](https://openairdocs.org/sdr/SWAA2026040184583.md): Skin · debonded · Mar 29, 2026 · N8610A · Boeing 7378H4 · Trailing Edge Flaps
  > CREW REPORTS NR 1 TE FLAP UPPER FWD CORNER, DEBONDING. RELATIVE TO WS 326. PERFORMED EA 26-157-00859. ACFT OK FOR SERVICE.
- [SDR SWAA2026030976833](https://openairdocs.org/sdr/SWAA2026030976833.md): Sign · cracked · Mar 4, 2026 · N8610A · Boeing 7378H4 · Emergency Lighting
  > FWD ENTRY DOOR EMERGENCY EXIT SIGN CRACKED. R & R FWD ENTRY DOOR EMERGENCY EXIT SIGN IAW AMM 33-51-01.
- [SDR SWAA2026030575655](https://openairdocs.org/sdr/SWAA2026030575655.md): Handle · loose · Mar 1, 2026 · N8610A · Boeing 7378H4 · Service Doors
  > FORWARD SERVICE DOOR ASSIST HANDLE LOOSE. TIGHTENED THE ASSIST HANDLE IAW AMM 52-41-31-400-802.
- [SDR SWAA2026030575654](https://openairdocs.org/sdr/SWAA2026030575654.md): Pin · disengaged · Mar 1, 2026 · N8610A · Boeing 7378H4 · Light System Wiring
  > SEAT ROW 14FED OVERHEAD EMERGENCY LIGHT INOPERATIVE. ON INVESTIGATION; FOUND PIN B NOT FULLY ENGAGED IN CONNECTOR D14816. TERMINATED IAW WDM 33-51-12 AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-03-960-805, STEP 5.D.(3).
- [SDR SWAA2026030374508](https://openairdocs.org/sdr/SWAA2026030374508.md): Elec Connector · broken · Feb 26, 2026 · N8610A · Boeing 7378H4 · Light System Wiring
  > AFT COVE BULLNOSE HAS BROKEN AISLE LIGHT CONNECTOR. REPLACED AISLE LIGHT CONNECTOR IAW SWPM 20-63-02, & WDM 33-51-14-13. FUNCTIONAL TEST WILL BE PERFORM IN TASK CARD TTG8Q01AJFUK.
- [SDR SWAA2026030374089](https://openairdocs.org/sdr/SWAA2026030374089.md): Cover · broken · Feb 25, 2026 · N8610A · Boeing 7378H4 · Emergency Lighting
  > G1 EMERGENCY LIGHT COVER IS BROKEN. R & R THE EMERGENCY LIGHT COVER IAW AMM 33-51-14-960-802. FUNCTIONAL CHECK PERFORMED ON TASK CARD TTG8Q01AJFUK.
- [SDR SWAA2026030374507](https://openairdocs.org/sdr/SWAA2026030374507.md): Light · cracked · Feb 25, 2026 · N8610A · Boeing 7378H4 · Emergency Lighting
  > LEFT CENTER OVER WING EXIT SIDEWALL PANEL EMERGENCY EXIT LIGHT BACKING IS CRACKED. R & R THE EMERGENCY LIGHT IAW AMM 33-51-14-960-802. FUNCTIONAL CHECK PERFORMED ON TASK CARD TTG8Q01AJFUK.
- [SDR SWAA2025122354586](https://openairdocs.org/sdr/SWAA2025122354586.md): Slide · out of alignment · Dec 21, 2025 · N8610A · Boeing 7378H4 · Escape Slide
  > FORWARD GALLEY SLIDE LOOKS MISALIGNED. RESCURED EXCESS MATERIAL AT BOTTOM OF R1 DOOR SLIDE COMPARTMENT. VERIFIED GIRT BAR OPERATION; GIRT OPS NORMAL AND SLIDE PRESSURE GAUGE IS READABLE THROUGH SLIDE PACK WINDOW IAW AMM 25-66-01.
- [SDR SWAA2025081905343](https://openairdocs.org/sdr/SWAA2025081905343.md): Shield · broken · Aug 17, 2025 · N8610A · Boeing 7378H4 · Emergency Equipment
  > AFT LT OTBD EMERGENCY FLASHLIGHT SHEILD BROKEN. R&R FLASHLIGHT SHEILD REF AMM 25-64-00.
- [SDR SWAA2025051970988](https://openairdocs.org/sdr/SWAA2025051970988.md): Door Frame · corroded · May 14, 2025 · N8610A · Boeing 7378H4 · Fuselage Main, Structure
  > AFT LEFT LAVATORY DOOR POST HAS EVIDENCE OF CORROSION AT LOWER SIDE<[01] REMOVED LH AFT LAV DOOR; AND AFT DOOR FRAME TRIM. REMOVED CORRODED SECTION OF THE AFT DOOR FRAME. NO FURTHER CORROSION NOTED. FABRICATED REPAIR PART AND INSTALLED ON AFT DOOR FRAME PER CM
- [SDR SWAA2025041422625](https://openairdocs.org/sdr/SWAA2025041422625.md): Light · inoperative · Apr 8, 2025 · N8610A · Boeing 7378H4 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT AFT OF R/H WING INOP<[01] RELAMPED EXTERIOR EMERGENCY LIGHT AFT OF R/H WING IAW AMM 33-51-04
- [SDR SWAA2025031104138](https://openairdocs.org/sdr/SWAA2025031104138.md): Flap System · locked · Mar 11, 2025 · N8610A · Boeing 7378H4 · Trailing Edge Flap Control System
  > ON APPROACH FLAP INDICATION WAS 10 WHILE FLAP HANDLE WAS AT 30. WE EXECUTED A GO AROUND AND RAN THE TRAILING EDGE FLAP DISAGREE CHECKLIST. WE EXTENDED THE FLAPS WITH THE ALTERNATE FLAPS SWITCH AND THE EXTENDED TO 15 AT A NORMAL RATE WITH NO ASYMMETRY. LANDED A
- [SDR SWAA2025021395098](https://openairdocs.org/sdr/SWAA2025021395098.md): Handle · out of adjust · Feb 12, 2025 · N8610A · Boeing 7378H4 · Service Doors
  > FWD GALLEY SERVICE DOOR HANDLE CAM CONTACTING LOWER 4 FASTENERS.<[01] FWD GALLEY SERVICE DOOR HANDLE ADJUSTED REF. AMM 52-41-00 AND REMOVED AND REPLACED FASTENERS REF. SRM 51-40-02.
- [SDR SWAA2025013191303](https://openairdocs.org/sdr/SWAA2025013191303.md): Panel · delaminated · Jan 30, 2025 · N8610A · Boeing 7378H4 · Aerodynamic Fairings
  > PANEL 193AL HAS DELAMINATION<[01]. EVALUATED DAMAGE ON PANEL 193AL. FOUND PUNCTURE LENGTH.5''; WIDTH.3''; DEPTH 0.05''. APPLIED TEMPORARY SEAL PER SRM 53-40-70-1A-1. INSPECTED PER [SRM 53-40-70-1A-1-B00369 (DAMAGE NOT MORE THAN 1 PLY DEEP - SEAL WITH SPEED
- [SDR SWAA2025011582423](https://openairdocs.org/sdr/SWAA2025011582423.md): Intercostal · elongated · Jan 2, 2025 · N8610A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE WEB - INTERCOSTAL LOC BTW BS500B TO BS500C AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-764828<[01] REPLACED WEB - INTERCOSTAL LOC BTW BS500B TO BS500C AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 AND DWG 143A7505 SHEET
- [SDR SWAA2025011582424](https://openairdocs.org/sdr/SWAA2025011582424.md): Intercostal · elongated · Jan 2, 2025 · N8610A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE WEB - INTERCOSTAL LOC BTW BS500G TO BS500H AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-764829<[01] REPLACED WEB - INTERCOSTAL LOC BTW BS500G TO BS500H AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 AND DWG 143A7505 SHEET
- [SDR SWAA2025011582422](https://openairdocs.org/sdr/SWAA2025011582422.md): Intercostal · elongated · Jan 2, 2025 · N8610A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE WEB - INTERCOSTAL LOC BTW BS500C TO BS500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-764827<[01] REPLACED WEB - INTERCOSTAL LOC BTW BS500C TO BS500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AN
- [SDR SWAA2025012381111](https://openairdocs.org/sdr/SWAA2025012381111.md): Support Bracket · cracked · Dec 27, 2024 · N8610A · Boeing 7378H4 · Aerodynamic Fairings
  > CRACK SUPPORT BRACKET BODY STATION 540 AND LBL 6 AT KEEL BEAM 2024-764808<[01] REPLACED SUPPORT BRACKET LOCATED ON BS 540 AND LBL6 AT KEEL BEAM. IAW B737-800 SRM 51-40-02.;[02] CERTIFIED WORK PERFORMED
- [SDR SWAA2025012380929](https://openairdocs.org/sdr/SWAA2025012380929.md): Plate · cracked · Dec 26, 2024 · N8610A · Boeing 7378H4 · Fuselage Main, Structure
  > CRACK ON CORRUGATED PLATE LOCATED IRSS 215 AT TRAILING EDGE AT LT WING 2024-764797<[01] REPLACED CORRUGATED PLATE LOCATED IRSS 215 AT TRAILING EDGE AT LT WING IAW B737-800 SRM 51-10-02 ITEM 9 MEASURE OF CRACK IS 0.500 IN TOOL USED DIGITAL CALIPER: P/N: 500-197
- [SDR SWAA2025012480359](https://openairdocs.org/sdr/SWAA2025012480359.md): Plate · broken · Dec 22, 2024 · N8610A · Boeing 7378H4 · Wing Main, Frame Structure
  > BROKEN CORRUGATED PLATE LOC ON IRSS 143 AT REAR SPAR LT WING 2024-764768<[01] REPLACED CORRUGATED PLATE LOC ON IRSS 143 LT WING IAW B737-800 SRM 51-40-02 AND DRAWING 115A2001 SHEET 49 REV:-.<BR>?SEE INDIVIDUAL SIGN OFF BELOW?.;[02] TASK COMPLETED<BR><BR>SEE IN
- [SDR SWAA2025012280354](https://openairdocs.org/sdr/SWAA2025012280354.md): Nut · deteriorated · Dec 22, 2024 · N8610A · Boeing 7378H4 · Service Doors
  > DETERIORATED NUT ON ASSIST HANDLE AT AFT SERVICE DOOR (2EA) 2024-764740<[01] REPLACED NUT ON ASSIST HANDLE AT AFT SERVICE DOOR (2EA) IAW SOPM 20-50-01 REV. 38 AND DWG 411A2204 REV A SHEET 65;[02] REPLACED NUT ON ASSIST HANDLE AT AFT SERVICE DOOR (2EA) IAW SOPM
- [SDR SWAA2025012280353](https://openairdocs.org/sdr/SWAA2025012280353.md): Nut · deteriorated · Dec 22, 2024 · N8610A · Boeing 7378H4 · Service Doors
  > DETERIORATED NUT ON ASSIST HANDLE AT FWD SERVICE DOOR 2024-764739<[01] REPLACED NUT ON ASSIST HANDLE AT FWD SERVICE DOOR IAW B737-800 AMM 52-41-31-400-802 STEP 3.F ITEM (2);[02] JOB COMPLETED
- [SDR SWAA2025012180357](https://openairdocs.org/sdr/SWAA2025012180357.md): Rib · cracked · Dec 22, 2024 · N8610A · Boeing 7378H4 · Wing, Rib/Bulkhead
  > CRACK ON DEFLECTION CONTROL RIB TRAILING EDGE AT LT WING 2024-764746<[01] TOOL USED STEP 6 EDDY CURRENT EQUIPMENT PN: NORTEC 600D SN: 240497907 DUE DATE: 27-AUG-25;[02] PERFORMED REPAIR ON DEFLECTION CONTROL RIB TRAILING EDGE AT LT WING IAW B737-800 SRM 57-51-
- [SDR SWAA2025012080355](https://openairdocs.org/sdr/SWAA2025012080355.md): Angle · cracked · Dec 22, 2024 · N8610A · Boeing 7378H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED ORSS 317 AT LT WING 2024-764745<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 317 AT LT WING IAW B737-800 SRM 51-40-02 AND DWG 115A3712 SHEET 5 REV -;[02] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 317 AT LT WING IAW B737-800
- [SDR SWAA2025012379911](https://openairdocs.org/sdr/SWAA2025012379911.md): Rib · cracked · Dec 21, 2024 · N8610A · Boeing 7378H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK ON RIB ACCESS PANEL 331B LOCATED LE STA105.26 AT LT HORIZONTAL STABILIZER 2024-764729<[01] REPLACED RIB AND FASTENERS LOCATED ON L/E STA 105.26 AT LT HORIZONTAL STABILIZER. IAW B737-800 SRM 51-40-02 AND DWG# 186A1001 SHEET 19 AND REV -.;[02] REPLACED RIB
- [SDR SWAA2025012379912](https://openairdocs.org/sdr/SWAA2025012379912.md): Rib · cracked · Dec 21, 2024 · N8610A · Boeing 7378H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK ON RIB ACCESS PANEL 331B LOCATED LE STA114.55 AT LT HORIZONTAL STABILIZER 2024-764730<[01] REPLACED RIB & FASTENERS LOCATED ON L/E STA 114.55 AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-40-02 AND DWG# 186A1001 SHEET 19 AND REV -.;[02] REPLACED RIB &
- [SDR SWAA2025012379910](https://openairdocs.org/sdr/SWAA2025012379910.md): Support Angle · cracked · Dec 20, 2024 · N8610A · Boeing 7378H4 · Fuselage Internal Mounting Structure
  > CRACK SUPPORT ANGLE LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN 2024-764690<[01] TOOLS USED TEMPERATURE CONTROLLER P/N: 38615K71; S/N: AE-40585; DUE DATE: 26-JUL-25.;[02] TOOLS USED: POWER PACK: P/N: FMK0003223; S/N: PE0412/63335; DUE DATE: 17
- [SDR SWAA2025012179559](https://openairdocs.org/sdr/SWAA2025012179559.md): Shear Plate · corroded · Dec 19, 2024 · N8610A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION BILGE AREA SHEAR PLATE BTW BS 500 TO BS 500A AT LEVEL S 26R AND WL 154.5 AT FWD CARGO COMPARTMENT 2024-764668<[01] REPLACED SHIELD PLATE BTW BS 492.4 TO BS 500A AT LEVEL STR 26R AND WL 154.5 AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9;
- [SDR SWAA2025012179555](https://openairdocs.org/sdr/SWAA2025012179555.md): Support Channel · corroded · Dec 19, 2024 · N8610A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION CHANNEL SUPPORT ZEE LOCATED BTW BS 500C TO BS 500G AT LEVEL S 26L AT WL 154.5 AT FWD CARGO COMPARTMENT 2024-764656<[01] THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EAM-22-153-01550;[02] THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (
- [SDR SWAA2025012179558](https://openairdocs.org/sdr/SWAA2025012179558.md): Shield · corroded · Dec 19, 2024 · N8610A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB (SHIELD) LOCATED BTW BS794 TO 767 RBL 21 WL 156.5 AT AFT CARGO COMPARTMENT 2024-764657<[01] REPLACED WEB(SHIELD)AND FASTENERS LOCATED BETWEEN BS767 TO BS 794 RBL21 AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DRAWING 146A0081 SHEET 49 REV
- [SDR SWAA2025012179552](https://openairdocs.org/sdr/SWAA2025012179552.md): Channel · corroded · Dec 19, 2024 · N8610A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION CHANNEL SUPPORT ZEE LOCATED BTW BS 500H TO BS 500I AT LEVEL S 26L AND WL 154.5 AT FWD CARGO COMPARTMENT 2024-764658<[01] TOOL USED ON STEP 4 UT EQUIPMENT. P/N: 45MG; S/N: 232017609; CAL DUE DATE: 08-OCT-25;[02] THE DAMAGE WAS REPAIRED PER SRM 53-00-5
- [SDR SWAA2025011579562](https://openairdocs.org/sdr/SWAA2025011579562.md): Web · corroded · Dec 19, 2024 · N8610A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB - INTERCOSTAL LOCATED BTW BS747 TO BS767 RBL21 WL 156.5 AFT CARGO COMPARTMENT. REPLACED WEB LOCATED BTW BS 747 TO BS 767 RBL 21 WL 156 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9; SRM 51-40-02 DWG: 146A7500 SHEET: 236 REV: - AND D
- [SDR SWAA2025011579564](https://openairdocs.org/sdr/SWAA2025011579564.md): Support Angle · cracked · Dec 19, 2024 · N8610A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS867 AT LEVEL STR27L AT AFT CARGO COMPARTMENT 2024-764669<[01] REPLACED ANGLE - SUPPORT LOCATED FLOOR STRUCTURE STA 867 AT LEVEL STR 27L AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02-0G AND 51-40-02 AND DWG 149A8102 SHEET: 1
- [SDR SWAA2025011579561](https://openairdocs.org/sdr/SWAA2025011579561.md): Support · corroded · Dec 19, 2024 · N8610A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS727F TO BS767 RBL21 WL156.5 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE AND CLIP ZEE-SUPPORT(1E/A) BTW BS727F TO BS767 RBL21 WL156.5 AT AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-6 REPAIR 6; SRM 51-40-02 AND DWG 146A750
- [SDR SWAA2025011579563](https://openairdocs.org/sdr/SWAA2025011579563.md): Strap · corroded · Dec 19, 2024 · N8610A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION STRAP LOCATED BS767 BTW LBL21 TO RBL21 WL 156.5 AT AFT CARGO COMPARTMENT 2024-764667<[01] REPLACED STRAP LOCATED BS767 BTW LBL21 TO RBL21 WL 156.5 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 AND DWG 146A7500 REV-;[02] CORRECTED STEP 1<BR>REPLA
- [SDR SWAA2025011579560](https://openairdocs.org/sdr/SWAA2025011579560.md): Support · corroded · Dec 19, 2024 · N8610A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS727D TO BS807 LBL21 WL156.5 AT AFT CARGO COMPARTMENT. ZEE CHANNEL SIDEPLATE ( SUPPORT ZEE) LOCATED BTW BS 727C+11 TO BS 787+ 11. SPLICE SIDEPLATE 4EA LOCATED BTW BS 727D TO BS 727E. BTW BS 727H TO BS 727I. BTW BS 727I TO B
- [SDR SWAA2025012379162](https://openairdocs.org/sdr/SWAA2025012379162.md): Balance Weight · out of balance · Dec 18, 2024 · N8610A · Boeing 7378H4 · Elevator Structure
  > DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR LT PN: 183A0103-25 SN: 006113 FOUND BALANCE WEIGHTS PN: 183A0210-15 (1 EA) ON BAY 4 PN: 183A0210-14 (1EA) ON BAY 3 PN: 183A0210-14 (1 EA) ON BAY 2 2024-764623<[01] ACCOMPLISHED ELEVATOR BALANCING IAW EA M-22-155-
- [SDR SWAA2025012379163](https://openairdocs.org/sdr/SWAA2025012379163.md): Balance Weight · out of balance · Dec 18, 2024 · N8610A · Boeing 7378H4 · Elevator Structure
  > DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR RT PN: 183A0103-26 SN: 006328 FOUND BALANCE WEIGHTS PN: 183A0210-15 (1 EA) ON BAY 4 PN: 183A0210-14 (1EA) ON BAY 3 PN: 183A0210-14 (1 EA) ON BAY 2 2024-764624<[01] ACCOMPLISHED ELEVATOR BALANCING IAW M-22-155-037
- [SDR SWAA2025012078981](https://openairdocs.org/sdr/SWAA2025012078981.md): Web · cracked · Dec 18, 2024 · N8610A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK FLOOR STRUCTURE WEB LOCATED BTW BS 380 TO BS 400 AT LBL 13 AT PASSENGER CABIN 2024-764625<[01] REPLACED FLOOR STRUCTURE WEB (UPPER CHORD ANGLE) LOCATED BTW BS 380 TO BS 400 AT LBL 13 AT PASSENGER CABIN IAW DRAWING 143A5400 REV-B AND B737-800 SRM 51-10-02
- [SDR SWAA2025012378551](https://openairdocs.org/sdr/SWAA2025012378551.md): Frame · cracked · Dec 17, 2024 · N8610A · Boeing 7378H4 · Fuselage Main, Frame
  > CRACK FRAME ON BS 312 BETWEEN S-5L AND S-6L AT FWD GALLEY AREA 2024-764593<[01] REPAIRED FRAME ON BS 312 BETWEEN S-5L AND S-6L AT FWD GALLEY AREA IAW B737-800 EA EA-GENERAL M-22-153-01244<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] STEP 1 CORRECTED:<BR>REPAIRED FRA
- [SDR SWAA2025012378744](https://openairdocs.org/sdr/SWAA2025012378744.md): Gusset · cracked · Dec 17, 2024 · N8610A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > BROKEN ANGLE GUSSET LOCATED ON BS 500I AT STR 19R AT FWD CARGO COMPARTMENT 2024-764608<[01] REPLACED ANGLE GUSSET AND FASTENERS LOCATED ON BS 500I AT STRINGER 19R AT FWD CARGO COMPARTMENT IAW BOEING 737-800 SRM 51-40-02; BOEING 737-800 SRAND BOEING 737-800 DWG
- [SDR SWAA2025012178553](https://openairdocs.org/sdr/SWAA2025012178553.md): Fastener · deteriorated · Dec 17, 2024 · N8610A · Boeing 7378H4 · Emergency Equipment
  > DETERIORATED GIRT BAR FITTING HARDWARE ON AFT ENTRY AND GALLEY AT AFT GALLEY AREA 2024-764576<[01] REPLACED GIRT BAR FITTING HARDWARE ON AFT ENTRY AND GALLEY AT AFT GALLEY AREA IAW B737-800- AMM 25-66-02-400-801;[02] CERTIFIED WORK PERFORMED.
- [SDR SWAA2025012178554](https://openairdocs.org/sdr/SWAA2025012178554.md): Fastener · deteriorated · Dec 17, 2024 · N8610A · Boeing 7378H4 · Emergency Equipment
  > DETERIORATED HARDWARE GIRT BAR FITTING IN ENTRY AND SERVICE DOOR AT FWD GALLEY AREA 2024-764587<[01] REPLACED HARDWARE GIRT BAR FITTING IN ENTRY AND SERVICE DOOR AT FWD GALLEY AREA IAW B737-800 AMM 25-66-02-400-801;[02] REPLACED HARDWARE GIRT BAR FITTING IN EN
- [SDR SWAA2025012378182](https://openairdocs.org/sdr/SWAA2025012378182.md): Stiffener · corroded · Dec 16, 2024 · N8610A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION STIFFENER LOCATED BTW BS947.5 TO BS967 RBL 50 WL 208.1 AT AFT GALLEY AREA 2024-764549<[01] TOOL USED P/N: 45MG; S/N: 130066401; CAL DUE: 21-OCT-25.;[02] REPLACED STIFFENER AND FASTENERS LOCATED BTW BS947.5 TO BS967 RBL 50 WL 208.1 AT AFT GALLEY AREA

Next page: https://openairdocs.org/aircraft/N8610A/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 = 'N8610A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8610A/reports

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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.