# Service difficulty reports: N8612K

A list on [N8612K](https://openairdocs.org/aircraft/N8612K.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 · 179 reports

- [SDR SWAA2026081325383](https://openairdocs.org/sdr/SWAA2026081325383.md): Apu · shutdown · Aug 9, 2026 · N8612K · Boeing 7378H4 · APU Core Engine
  > DURING PUSHBACK APU SHUTDOWN AND LOW OIL PRESSURE LIGHT ILLUMINATED. T/S PER FIM 49-90 TASK 803. VERIFIED OIL LEVEL FULL. RESET SYSTEM AND OPS TEST GOOD. THIS CLEARS MEL SP1 REVERSED
- [SDR SWAA2026031177645](https://openairdocs.org/sdr/SWAA2026031177645.md): Battery Pack · inoperative · Mar 8, 2026 · N8612K · Boeing 7378H4 · Emergency Lighting
  > SEVERAL EMERGENCY EXIT LIGHTS AT THE OVERWING EXIT DOORS ARE INOPERATIVE. ONE SMALL EXIT LIGHT ON THE LT SIDE; TWO LARGE LIGHTS ON THE UPPER RT SIDE; AND TWO EXTERIOR LIGHTS INOPERATIVE. RECONNECTED EMERGENCY LIGHT BATTERY PACK AT SEAT ROW 18L IAW AMM 33-51-
- [SDR SWAA2025100320042](https://openairdocs.org/sdr/SWAA2025100320042.md): Light · inoperative · Oct 1, 2025 · N8612K · Boeing 7378H4 · Emergency Lighting
  > R/H EXTERIOR FWD OVERWING EMERGENCY LIGHT INOP. REMOVED & REPLACED LAMP FOR R/H EXTERIOR FWD OVER WING EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2025081403471](https://openairdocs.org/sdr/SWAA2025081403471.md): Flap · loose · Aug 11, 2025 · N8612K · Boeing 7378H4 · Emergency Equipment
  > FORWARD SERVICE DOOR SLIDE BAR FLAP LOOSE. RESECURED FLAP IAW MT 725-61-06.
- [SDR SWAA2025022692783](https://openairdocs.org/sdr/SWAA2025022692783.md): Elevator · out of balance · Feb 3, 2025 · N8612K · Boeing 7378H4 · Elevator Structure
  > DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR LT PN 183A0103-21 SN 005265 FOUND BALANCE WEIGHT PN 183A0210-14 1EA ON BAY 2 PN 183A0210-14 1EA ON BAY 3 1EA 183A0210-15 ON BAY 4 2025-81723<[01] ACCOMPLISHED ELEVATOR BALANCING IAW EA M-22-155-03766.;[02] RII IT
- [SDR SWAA2025022692260](https://openairdocs.org/sdr/SWAA2025022692260.md): Rib · cracked · Feb 1, 2025 · N8612K · Boeing 7378H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA 114.55 AT LT HORIZONTAL STABILIZER 2025-81714<[01] REPLACED RIB AND FASTENERS AT ACCESS PANEL 331B LOCATED LE STA 114.55 AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-40-02;DWG 186A1305 REV:- AND DWG 18
- [SDR SWAA2025022691698](https://openairdocs.org/sdr/SWAA2025022691698.md): Support Angle · cracked · Jan 30, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT OF PANEL 844DZ LOCATED AFT GALLEY SERVICE DOOR (R 2) AT AFT GALLEY AREA 2025-81701<[01] REPACLED ANGLE SUPPORT OF PANEL 844DZ LOCATED AFT GALLEY SERVICE DOOR (R 2) AT AFT GALLEY AREA IAW B737-800 SRM 51-40-05 DWG: 411A2119 SHEET: 71 REV:
- [SDR SWAA2025022691456](https://openairdocs.org/sdr/SWAA2025022691456.md): Support Bracket · cracked · Jan 30, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET BODY STATION 540 AND LBL6 AT KEEL BEAM 2025-81700<[01] REPLACED SUPPORT BRACKET LOC. BODY STATION 540 AND LBL6 AT KEEL BEAM I.A.W. B737-800 SRM 51-40-02;SRM 51-10-02 AND DWG 212A1101 SHEET 7 REV.-;[02] REPLACED SUPPORT BRACKET LOC. BODY
- [SDR SWAA2025022691697](https://openairdocs.org/sdr/SWAA2025022691697.md): Support Bracket · cracked · Jan 30, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET BODY STATION 540 AND RBL6 AT KEEL BEAM 2025-81703<[01] REPLACED SUPPORT BRACKET LOC. BODY STATION 540 AND RBL6 AT KEEL BEAM I.A.W. B737-800 SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DWG 212A1101 SHEET 7 REV.-;[02] REPLACED SUPPORT BRACKET LOC
- [SDR SWAA2025022691699](https://openairdocs.org/sdr/SWAA2025022691699.md): Angle · cracked · Jan 30, 2025 · N8612K · Boeing 7378H4 · Wing Miscellaneous Structure
  > CRACK ANGLE LOCATED PANEL 651FB LOWER INBOARD FIXED TRAILING EDGE AT RT WING 2025-81702<[01] REPLACED ANGLE LOCATED PANEL 651FB LOWER INBOARD FIXED TRAILING EDGE AT RT WING IAW B737-800 SRM 51-10-02 ITEM 9 AND DWG 115A2710 SHEET 9 REV A;[02] CORRECTED STEP 1<B
- [SDR SWAA2025030391041](https://openairdocs.org/sdr/SWAA2025030391041.md): Bracket · elongated · Jan 29, 2025 · N8612K · Boeing 7378H4 · Wing Miscellaneous Structure
  > ELONGATED HOLE BRACKET LOCATED IFSS 151 LEADING EDGE INTERNAL CAVITY KRUEGER FLAP AT LT WING 2025-81686<. REPLACED BRACKET LOCATED IFSS 151 LEADING EDGE INTERNAL CAVITY KRUEGER FLAP AT LT WING IAW B737-800 AMM 36-13-01-400-801 STEP 7.G.(8). TORQUE APPLIED 20
- [SDR SWAA2025022691042](https://openairdocs.org/sdr/SWAA2025022691042.md): Frame · cracked · Jan 29, 2025 · N8612K · Boeing 7378H4 · Fuselage Main, Frame
  > CRACK FRAME STA 312 AND BTW STR 5L TO STR 6L AT PASSENGER CABIN 2025-81690<[01] PERFORMED PERMANENT REPAIR ON FRAME STA 312 AND BTW STR 5L TO 6L AT PASSENGER CABIN I.A.W. EA M-22-153-01244. LENGTH OF CRACK IS:0.315? TOOL USED DIGITAL CALIPER P/N: 500-197-30; S
- [SDR SWAA2025022690514](https://openairdocs.org/sdr/SWAA2025022690514.md): Angle · corroded · Jan 28, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ANGLE LOCATED BTW BS767 TO BS787 AT LEVEL STR25R WL156.5 AT AFT CARGO COMPARTMENT 2025-81668<[01] REPLACED ANGLE LOCATED BTW BS767 TO BS787 AT LEVEL STR25R WL156.5 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9; DWG: 146812
- [SDR SWAA2025022690334](https://openairdocs.org/sdr/SWAA2025022690334.md): Web · corroded · Jan 27, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB LOCATED BTW BS492.4 TO BS500 AT LEVEL STR26R WL156.5 AT FWD CARGO COMPARTMENT 2025-81631<[01] REPLACED WEB LOCATED BTW BS492.4 TO BS500A AT LEVEL STR26R WL156.5 AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A0080 SHEET 39 REV.
- [SDR SWAA2025022690332](https://openairdocs.org/sdr/SWAA2025022690332.md): Intercostal · cracked · Jan 27, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BTW BS500E TO BS500F AT LEVEL STR26R FWD CARGO COMPARTMENT 2025-81638 <[01]. REPLACED WEB-INTERCOSTAL LOCATED ON BTW BS500E TO BS500F AT LEVEL STR26R AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A7505 SHEET
- [SDR SWAA2025022690336](https://openairdocs.org/sdr/SWAA2025022690336.md): Support · corroded · Jan 27, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS727 +11 INCHES TO BS747 + 18 INCHES AT LEVEL STR25R WL156.5 AT AFT CARGO COMPARTMENT 2025-81651<[01]. PERFORMED REPAIR LOCATED BTW BS727G TO BS727H AT LEVEL STR25R WL156.5 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 53-00-53-
- [SDR SWAA2025022690326](https://openairdocs.org/sdr/SWAA2025022690326.md): Angle · cracked · Jan 27, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED BS500H AT LEVEL STR26L FWD POSITION AT FWD CARGO COMPARTMENT 2025-81645 <[01]. REPLACED ANGLE-CLIP LOCATED ON BS500H AT LEVEL STR26L FWD POSITION AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A7505 SHEET 108 REV.
- [SDR SWAA2025022690327](https://openairdocs.org/sdr/SWAA2025022690327.md): Angle · cracked · Jan 27, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED BS500H AT LEVEL STR26L AFT POSITION AT FWD CARGO COMPARTMENT 2025-81644 <[01]. REPLACED ANGLE-CLIP LOCATED ON BS500H AT LEVEL STR26L AFT POSITION AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A7505 SHEET 108 REV.
- [SDR SWAA2025022690328](https://openairdocs.org/sdr/SWAA2025022690328.md): Angle · cracked · Jan 27, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED BS500H AT LEVEL STR26R AFT POSITION AT FWD CARGO COMPARTMENT 2025-81643 <[01]. REPLACED ANGLE-CLIP LOCATED ON BS500H AT LEVEL STR26R AFT POSITION AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A7505 SHEET 108 REV.
- [SDR SWAA2025022690329](https://openairdocs.org/sdr/SWAA2025022690329.md): Angle · cracked · Jan 27, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED BS500H AT LEVEL STR26R FWD POSITION AT FWD CARGO COMPARTMENT 2025-81642 <[01]. REPLACED ANGLE-CLIP LOCATED ON BS500H AT LEVEL STR26R FWD POSITION AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A7505 SHEET 108 REV.
- [SDR SWAA2025022690341](https://openairdocs.org/sdr/SWAA2025022690341.md): Support Angle · cracked · Jan 27, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS867 AT LEVEL STR 27L AT AFT CARGO COMPARTMENT 2025-81657 <[01]. REPLACED ANGLE - SUPPORT LOCATED BS867 AT LEVEL STR 27L AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9 DWG 149A8102 SHEET 19 REV A AND SRM 51-40-02; [02]
- [SDR SWAA2025022690339](https://openairdocs.org/sdr/SWAA2025022690339.md): Web · corroded · Jan 27, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB LOCATED BTW BS767 TO BS794.3 AT LEVEL STR 25R WL 156.5 AT AFT CARGO COMPARTMENT 2025-81652 CORROSION WEB LOCATED BTW BS767 TO BS794.3 AT LEVEL STR 25R WL 156.5 AT AFT CARGO COMPARTMENT<[01] REPLACED WEB LOCATED BTW BS767 TO BS794.3 AT LEVEL STR 2
- [SDR SWAA2025022690338](https://openairdocs.org/sdr/SWAA2025022690338.md): Support Angle · cracked · Jan 27, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BTW BS907 TO BS927 AND STR25R TO STR27R AT AFT CARGO COMPARTMENT 2025-81658<[01] REPLACED ANGLE AND FASTENERS LOCATED BTW BS907 TO BS927 AND STR25R TO STR27R AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG 147A7221 SHEE
- [SDR SWAA2025022690325](https://openairdocs.org/sdr/SWAA2025022690325.md): Angle · cracked · Jan 27, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED BS500G AT LEVEL STR26L FWD POSITION AT FWD CARGO COMPARTMENT 2025-81646<[01] REPLACED ANGLE-CLIP LOCATED ON BS500G AT LEVEL STR26L FWD POSITION AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A7505 SHEET 108 REV. -<B
- [SDR SWAA2025022690330](https://openairdocs.org/sdr/SWAA2025022690330.md): Angle · cracked · Jan 27, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED BS500G AT LEVEL STR26R AFT POSITION FWD CARGO COMPARTMENT 2025-81641<[01] REPLACED ANGLE-CLIP LOCATED ON BS500G AT LEVEL STR26R AFT POSITION AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A7505 SHEET 108 REV. -<BR><
- [SDR SWAA2025022690331](https://openairdocs.org/sdr/SWAA2025022690331.md): Angle · cracked · Jan 27, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED BS500G AT LEVEL STR26R FWD POSITION AT FWD CARGO COMPARTMENT 2025-81640<[01] REPLACED ANGLE-CLIP LOCATED ON BS500G AT LEVEL STR26R FWD POSITION AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A7505 SHEET 108 REV. -<B
- [SDR SWAA2025022690337](https://openairdocs.org/sdr/SWAA2025022690337.md): Access Panel · cracked · Jan 27, 2025 · N8612K · Boeing 7378H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK BLADE ACCESS PANEL 333AT BLADE AT LT HORIZONTAL STABILIZER 2025-81654<[01] REPLACED BLADE ON ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 186A3101 SHEET 24 REV -<BR><BR>MEASURE OF CRACK ON SUPPORT
- [SDR SWAA2025022692416](https://openairdocs.org/sdr/SWAA2025022692416.md): Access Panel · corroded · Jan 27, 2025 · N8612K · Boeing 7378H4 · Wing, Plate/Skin
  > CORROSION ACCESS PANEL 632RB FUEL TANK RING RT WING 2025-81639<[01] REPLACED ACCESS PANEL 632RB FUEL TANK RING RT WING IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 110A0110 SHEET 41; REV-.<BR><BR>RING CLAMP INSTALLATION TO BE ACCOMPLISHED SEE: TTG
- [SDR SWAA2025022689888](https://openairdocs.org/sdr/SWAA2025022689888.md): Gusset · cracked · Jan 26, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK GUSSET LOCATED BS 500I AT LEVEL STR 24L AT FWD CARGO COMPARTMENT 2025-81600 <[01]. REPLACED GUSSET LOCATED BS 500I AT LEVEL STR 24L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG 143A7902 REV:B SHEET 256 AND SHEET 257. SEE INDIVIDUAL SIGN OF
- [SDR SWAA2025022689886](https://openairdocs.org/sdr/SWAA2025022689886.md): Gusset · cracked · Jan 26, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK GUSSET LOCATED BS 500I AT LEVEL STR 22L AT FWD CARGO COMPARTMENT 2025-81599 <[01]. REPLACED GUSSET LOCATED BS 500I AT LEVEL STR 22L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9. AND DRAWING # 143A7902 SHEET 256 REV: B. SEE INDIVIDUAL SIGN O
- [SDR SWAA2025022689887](https://openairdocs.org/sdr/SWAA2025022689887.md): Gusset · cracked · Jan 26, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK GUSSET LOCATED BS 500I AT LEVEL STR 21L AT FWD CARGO COMPARTMENT 2025-81598 <[01]. REPLACED GUSSET AND FASTENERS LOCATED BS 500I AT LEVEL STR 21L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 256 AND REV-
- [SDR SWAA2025022689889](https://openairdocs.org/sdr/SWAA2025022689889.md): Gusset · cracked · Jan 26, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON GUSSET LOCATED BS 500I AT LEVEL STR 19R AT FWD CARGO COMPARTMENT 2025-81597 <[01]. REPLACED GUSSET LOCATED BS 500I AT LEVEL STR 19R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG: 143A7902 SHEET: 256 REV: B. SEE IN
- [SDR SWAA2025022689540](https://openairdocs.org/sdr/SWAA2025022689540.md): Angle · cracked · Jan 25, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE FLOOR STRUCTURE LOCATED BETWEEN STA380 TO STA400 AND LBL52 AT PASSENGER CABIN 2025-81541 CRACK ANGLE FLOOR STRUCTURE LOCATED BETWEEN STA380 TO STA400 AND LBL50 AT PASSENGER CABIN<[01] REPLACED ANGLE FLOOR STRUCTURE LOCATED BETWEEN STA380 TO STA400
- [SDR SWAA2025022689545](https://openairdocs.org/sdr/SWAA2025022689545.md): Angle · cracked · Jan 25, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE FLOOR STRUCTURE LOCATED BETWEEN STA380 TO STA400 AND LBL13 AT PASSENGER CABIN 2025-81543<[01] REPLACED ANGLE FLOOR STRUCTURE LOCATED BETWEEN STA380 TO STA400 AND LBL13 AT PASSENGER CABIN AND FASTENERS IAW B737-800 SRM 51-10-02 ITEM 9 AND DWG:143A54
- [SDR SWAA2025022689548](https://openairdocs.org/sdr/SWAA2025022689548.md): Floor Support · cracked · Jan 25, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA277 TO STA294.5 AND BL0 AT FWD GALLEY AREA 2025-81549<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA277 TO STA294.5 AND BL0 AT FWD GALLEY AREA IAW B737-800 SRM 51-10-02 ITEM 9 AND DR
- [SDR SWAA2025022689543](https://openairdocs.org/sdr/SWAA2025022689543.md): Floor Support · cracked · Jan 25, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA344 TO STA360 AND BL0 AT FWD GALLEY AREA 2025-81547<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA344 TO STA360 AND BL0 AT FWD GALLEY AREA IAW B737-800 SRM 51-10-02 ITEM 9. AND DRAWI
- [SDR SWAA2025022689415](https://openairdocs.org/sdr/SWAA2025022689415.md): Lens · missing · Jan 25, 2025 · N8612K · Boeing 7378H4 · Emergency Lighting
  > MISSING EMERGENCY LIGHT LENS ON SIDEWALL 231ZKW AT PASSENGER CABIN. 2025-81498<[01] INSTALLED EMERGENCY LIGHT LENS ON SIDEWALL 231ZKW AT PASSENGER IAW B737-800 AMM 33-51-01-960-802 STEP 3.C.(10);[02] INSTALLED EMERGENCY LIGHT LENS ON SIDEWALL 231ZKW AT PASSENG
- [SDR SWAA2025022689541](https://openairdocs.org/sdr/SWAA2025022689541.md): Handle · worn · Jan 25, 2025 · N8612K · Boeing 7378H4 · Service Doors
  > WEAR NUT ASSIST HANDLE ON LINING DOORWAY AFT GALLEY AREA (2EA) 2025-81548. WEAR NUT ASSIST HANDLE ON LINING DOORWAY RH AFT GALLEY AREA (2EA)<[01] REPLACED NUT ASSIST HANDLE ON LINING DOORWAY RH AFT GALLEY AREA (2EA) I.A.W. B737-800 AMM 25-21-25-420-801 STEP 3.
- [SDR SWAA2025022689542](https://openairdocs.org/sdr/SWAA2025022689542.md): Floorbeam · cracked · Jan 25, 2025 · N8612K · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CRACK INNER CHORD LOCATED STA303.9 AND LBL55 FWD GALLEY AND LAV 2025-81546<[01] STEP 2. EDDY CURRENT EQUIPMENT USED P/N: NORTE 600D; S/N: 210138103 AND DUE DATE: 10-JUN-25.;[02] PERFORMED DETAIL VISUAL INSPECTION ON INNER CHORD LOCATED ON BS303.9 AND LBL55 AT
- [SDR SWAA2025022689544](https://openairdocs.org/sdr/SWAA2025022689544.md): Access Panel · elongated · Jan 25, 2025 · N8612K · Boeing 7378H4 · Wing, Plate/Skin
  > ELONGATED HOLE ACCESS PANEL 195CR LOCATED AT RT WING 2025-81556<[01] TOOL USED ULTRASONIC FLAW DETECTOR PN. EPOCH 650; SN. 201036102; DUE DATE 25-OCT-25;[02] TOOL USED: MULTIMETER P/N: FLUKE 87; S/N: 58430097; DUE DATE: 17-JUN-25; HUMIDITY/TEMPERATURE CHART RE
- [SDR SWAA2025022689125](https://openairdocs.org/sdr/SWAA2025022689125.md): Handle · out of adjust · Jan 23, 2025 · N8612K · Boeing 7378H4 · Passenger/Crew Doors
  > WEAR NUT IN HANDLE ASSIST AT FWD ENTRY DOOR (4EA) 2025-81461<[01] REPLACED NUT IN HANDLE ASSIST AT FWD ENTRY DOOR (4EA) IAW B737-800 AMM-52-11-31-400-802 STEP 3.G ITEM (2);[02] TASK CARD COMPLETED <BR>REPLACED NUT IN HANDLE ASSIST AT FWD ENTRY DOOR (4EA) IAW B
- [SDR SWAA2025022689124](https://openairdocs.org/sdr/SWAA2025022689124.md): Floorbeam · corroded · Jan 23, 2025 · N8612K · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON EXISTING REPAIR T-CHORD LOCATED ON FLOOR BEAM BS947.5 LBL4 AT AFT GALLEY AREA 2025-81437<[01] REPLACED EXISTING REPAIR LOCATED ON STA 947.5 FROM LBL8 TO RBL60 AFT GALLEY AREA I.A.W B737-800 SRM 53-70-51-2R-5; REPAIR 5. SEE INDIVIDUAL SIGN OF BELOW
- [SDR SWAA2025022688795](https://openairdocs.org/sdr/SWAA2025022688795.md): Support Angle · cracked · Jan 22, 2025 · N8612K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED STA727B AND LBL51 CEILING AREA AT AFT CARGO COMPARTMENT 2025-81408 <[01]. PERFORM HAND LAY-OUT ON REPAIR AREA LOCATED SUPPORT ANGLE BTW BS727A MORE 16? TO BS727B MORE 5? CEILING AREA AFT CARGO COMPARTMENT IAW B737-800 SRM 57-70-1
- [SDR SWAA2025022688270](https://openairdocs.org/sdr/SWAA2025022688270.md): Skin · debonded · Jan 21, 2025 · N8612K · Boeing 7378H4 · Trailing Edge Flaps
  > CUSTOMER REQUEST - DEBONDED OB AFT FLAP LOWER SURFACE AT LT WING. 2025-81322<[01] TOOL USED ON STEP 3 ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 15-OCT-25;[02] TOOL USED: HOTBONDER: P/N: HCS9200B S/N: 16122983 DUE DATE: 15-FEB-25;[0
- [SDR SWAA2025022687825](https://openairdocs.org/sdr/SWAA2025022687825.md): Light · inoperative · Jan 20, 2025 · N8612K · Boeing 7378H4 · Emergency Lighting
  > BROKEN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH SIDE AT PASSENGER CABIN (9 EA) 2025-81259<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH SIDE AT PASSENGER CABIN (9 EA) IAW B737-800 AMM 33-51-15-400-802;[02] REPLACED STRIP PHOTOLUMIN
- [SDR SWAA2025022687826](https://openairdocs.org/sdr/SWAA2025022687826.md): Light · inoperative · Jan 20, 2025 · N8612K · Boeing 7378H4 · Emergency Lighting
  > BROKEN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE AT PASSENGER CABIN (9 EA) 2025-81260<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE AT PASSENGER CABIN (9 EA) IAW B737-800 AMM 33-51-15-400-802;[02] REPLACED STRIP PHOTOLUMIN
- [SDR SWAA2025012087354](https://openairdocs.org/sdr/SWAA2025012087354.md): Battery Pack · inoperative · Jan 18, 2025 · N8612K · Boeing 7378H4 · Emergency Lighting
  > R/H MULTIPLES EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT ROW 8DEF REF AMM 33-51-06.OPS CHECK GOOD
- [SDR SWAA2024112671271](https://openairdocs.org/sdr/SWAA2024112671271.md): Seal · cracked · Nov 25, 2024 · N8612K · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT; AFT; UPPER SLIDING SEAL IS CRACKED ON THE HORIZONTAL STABILIZER.<[01] R&R RH HORIZONTAL STAB AFT UPPER SLIDING SEAL REF. SRM 51-40-02.
- [SDR SWAA2024020850274](https://openairdocs.org/sdr/SWAA2024020850274.md): Light · unsecure · Feb 8, 2024 · N8612K · Boeing 7378H4 · Emergency Lighting
  > CABIN LIGHTED FLOOR STRIP IS LIFTING NEAR ROW 12<[01] SECURED LIGHTED FLOOR STRIP IAW AMM 33-51-15
- [SDR SWAA2023090897342](https://openairdocs.org/sdr/SWAA2023090897342.md): Unknown · unknown · Sep 6, 2023 · N8612K · Boeing 7378H4 · Engine Collector/Tailpipe/Nozzle
  > GROUND CREW REPORTS #1 ENGINE TAILPIPE FIRE. FIRE EXTINGUISHED PRIOR TO QRH STEP 2 MOTOR ENGINE.<[01] PERFORMED GVI OF #1 ENGINE IAW AMM 71-00-00. DUE TO OBSERVED CANDLE FIRE IN EXHAUST PLUG. A/C OK FOR SERVICE DUE TO NO DAMAGE TO FLAME ARRESTOR (SECTION F; PA

Next page: https://openairdocs.org/aircraft/N8612K/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 = 'N8612K' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8612K/reports

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