# Service difficulty reports: N7861J

A list on [N7861J](https://openairdocs.org/aircraft/N7861J.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 · 195 reports

- [SDR SWAA2026081923403](https://openairdocs.org/sdr/SWAA2026081923403.md): Wire Harness · broken · Aug 15, 2026 · N7861J · Boeing 73779P · Fire Protection System Wiring
  > NR 2 ENGINE -A- FIRE DETECTION LOOP INOP T/S PER FIM 26-10 TASK 801. FOUND ENGINE #2 LOOP A CORE LEFT HARNESS BROKEN AT LOOP ELEMENT. REMAINING HARNESS TOO SHORT FOR REPAIR. REQUIRES HARNESS CHANGE/CORE HARNESS MOD. REMAINS ON MEL. OPENED ENGINE PER AMM 71
- [SDR SWAA2026051297922](https://openairdocs.org/sdr/SWAA2026051297922.md): Limiter · failed · May 11, 2026 · N7861J · Boeing 73779P · Hydraulic System, Main
  > LOSS OF SYS B HYD PRESSURE AND FLUID. FOUND O-RING ON TRAILING EDGE FLAP FLOW LIMITER TORN. O-RINGS REPLACED & REPLACED TRAILING EDGE FLAP FLOW LIMITER REF AMM 27-51-67 & SVC'D B SYS REF AMM 12-12-00. NO LEAKS NOTED AT THIS TIME.
- [SDR SWAA2026051297935](https://openairdocs.org/sdr/SWAA2026051297935.md): O-Ring · torn · May 11, 2026 · N7861J · Boeing 73779P · Hydraulic System, Main
  > LOSS OF SYS B HYD PRESSURE AND FLUID. FOUND O-RING ON TRAILING EDGE FLAP FLOW LIMITER TORN. O-RINGS REPLACED & REPLACED TRAILING EDGE FLAP FLOW LIMITER REF AMM 27-51-67 & SVC'D B SYS REF AMM 12-12-00. NO LEAKS NOTED AT THIS TIME.
- [SDR SWAA2026031178260](https://openairdocs.org/sdr/SWAA2026031178260.md): Pump · inoperative · Mar 10, 2026 · N7861J · Boeing 73779P · Hydraulic Pump (Electric/Engine), Main
  > LOSS OF HYDRAULIC B SYSTEM, NO OVERWEIGHT LANDING. REMOVED AND INSTALLED DUE TO HYDRAULIC LOSS, B ELECTRIC PUMP, B SYSTEM HYD FILTER, & TRAILING EDGE FLAP FLOW TRANSMITTER.
- [SDR SWAA2026031178667](https://openairdocs.org/sdr/SWAA2026031178667.md): Filter · inoperative · Mar 10, 2026 · N7861J · Boeing 73779P · Hydraulic System, Main
  > LOSS OF HYDRAULIC B SYSTEM, NO OVERWEIGHT LANDING. REMOVED AND INSTALLED DUE TO HYDRAULIC LOSS, B ELECTRIC PUMP, B SYSTEM HYD FILTER, & TRAILING EDGE FLAP FLOW TRANSMITTER.
- [SDR SWAA2026031178668](https://openairdocs.org/sdr/SWAA2026031178668.md): Limiter · leaking · Mar 10, 2026 · N7861J · Boeing 73779P · Hydraulic System, Main
  > LOSS OF HYDRAULIC B SYSTEM, NO OVERWEIGHT LANDING. REMOVED AND INSTALLED DUE TO HYDRAULIC LOSS, B ELECTRIC PUMP, B SYS HYDLAULIC FILTER, & TRAILING EDGE FLAP FLOW TRANSMITTER.
- [SDR SWAA2025102217859](https://openairdocs.org/sdr/SWAA2025102217859.md): Rib · cracked · Sep 24, 2025 · N7861J · Boeing 73779P · Horizontal Stabilizer, Spar/Rib
  > CRACK ON FRONT SPAR UPPER FLANGE INSPAR RIB 120.30 LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON RIB IAW EA 25-155-02690-WIP1 REV A, EA 25-155-02690, AND SRM 55-10-09-2R, REPAIR 5.
- [SDR SWAA2025102217089](https://openairdocs.org/sdr/SWAA2025102217089.md): Vapor Barrier · cracked · Sep 22, 2025 · N7861J · Boeing 73779P · Fuselage Main, Bulkhead
  > TWO CRACKS ON VAPOR BARRIER BS 663.75 LH SIDE MAIN WHEEL WELL COMPARTMENT. THIS FAULT IS RESOLVED ON FAULT TTG8Q01564Z0.
- [SDR SWAA2025102315280](https://openairdocs.org/sdr/SWAA2025102315280.md): Sill Drain · corroded · Sep 16, 2025 · N7861J · Boeing 73779P · Fuselage Main, Structure
  > CORROSION LOWER SILL LOCATED BETWEEN STA794.3 TO STA847 AND RBL24 WL156 AT AFT CARGO COMPARTMENT. REPLACED LOWER SILL LOCATED BETWEEN STA794.3 TO STA847 AND RBL24 WL156 AT AFT CARGO COMPARTMENT IAW SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 146A8340; SHEE
- [SDR SWAA2025102314819](https://openairdocs.org/sdr/SWAA2025102314819.md): Support Bracket · cracked · Sep 15, 2025 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL LBL 6 AT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET LOCATED BS540 AT LEVEL LBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND DWG 212A1101; SHEET 3 REV-.
- [SDR SWAA2025102314816](https://openairdocs.org/sdr/SWAA2025102314816.md): Tie Clip · cracked · Sep 15, 2025 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK TIE CLIP BS 277 AND STRINGER 10R PASSENGER CABIN. REPLACED TIE CLIP AND FASTENERS LOC.BS 277 AND STRINGER 10R PASSENGER CABIN IAW SRM 51-40-02; SRM B737-700 51-10-02 PARAGRAPH 9; DWG 141A1110 SHEET:18 REV:- AND DWG 141A8380 SHEET:14 REV-.
- [SDR SWAA2025102314813](https://openairdocs.org/sdr/SWAA2025102314813.md): Support Angle · cracked · Sep 15, 2025 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE BETWEEN BS 291.5 TO BS 294.5 AT LEVEL STRINGER 17R PASSENGER CABIN. REPLACED SUPPORT ANGLE LOC. BETWEEN BS 291.5 TO BS 294.5 AT LEVEL STRINGER 17R PASSENGER CABIN IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, DWG 141A8310 SHEET 25; REV.
- [SDR SWAA2025102314821](https://openairdocs.org/sdr/SWAA2025102314821.md): Support Bracket · cracked · Sep 15, 2025 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL RBL 6 AT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET LOCATED BS540 AT LEVEL RBL 6 AT AIR CONDITIONING BAY IAW SRM 51-40-02-0G-0.
- [SDR SWAA2025102214625](https://openairdocs.org/sdr/SWAA2025102214625.md): Vapor Barrier · cracked · Sep 15, 2025 · N7861J · Boeing 73779P · Fuselage Main, Bulkhead
  > CRACK ON VAPOR BARRIER BS 663.75 LH SIDE MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR BARRIER BS 663.75 LH SIDE MAIN WHEEL WELL COMPARTMENT IAW SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2025102214626](https://openairdocs.org/sdr/SWAA2025102214626.md): Light · deteriorated · Sep 15, 2025 · N7861J · Boeing 73779P · Emergency Lighting
  > DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHT LT SIDE 7 EA AND RT SIDE 7 EA. REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING IAW AMM 33-51-15-400-802.
- [SDR SWAA2025102314618](https://openairdocs.org/sdr/SWAA2025102314618.md): Strap · corroded · Sep 14, 2025 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION STRAP LOCATED BETWEEN BS787 TO BS794 AND WL154 FROM STR25R TO STR26R AFT CARGO COMPARTMENT. REPLACED STRAP LOCATED BETWEEN BS787 TO BS794 AND WL154 FROM STR25R TO STR26R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0
- [SDR SWAA2025102314619](https://openairdocs.org/sdr/SWAA2025102314619.md): Strap · corroded · Sep 14, 2025 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION STRAP LOCATED BETWEEN BS794 TO BS807 AND WL154 FROM STR25R TO STR26R AFT CARGO COMPARTMENT. REPLACED STRAP LOCATED BETWEEN BS794 TO BS807 AND WL154 FROM STR25R TO STR26R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0
- [SDR SWAA2025102314554](https://openairdocs.org/sdr/SWAA2025102314554.md): Access Panel · cracked · Sep 14, 2025 · N7861J · Boeing 73779P · Fuselage Main, Structure
  > CRACK ANGLE ACCESS PANEL 844DZ AT AFT GALLEY DOOR. REPLACED ANGLE ACCESS PANEL 844DZ AT AFT GALLEY DOOR DUE TO ALLOWABLE DAMAGE NOT FOUND IN SRM 52-10-02-1A-4; MEASURE OF CRACK IS: 0.310'. ANGLE REPLACED IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DRAWIN
- [SDR SWAA2025102214613](https://openairdocs.org/sdr/SWAA2025102214613.md): Cargo Track · cracked · Sep 14, 2025 · N7861J · Boeing 73779P · Fuselage, Seat/Cargo Attach Fittings
  > CRACK TRACK LBBL 17.24 LOCATED BS767 AFT CARGO COMPARTMENT. REPAIRED CARGO TRACK LOC LBL17.24 BTW BS 747 TO BS 787 IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3.
- [SDR SWAA2025102314161](https://openairdocs.org/sdr/SWAA2025102314161.md): Support · cracked · Sep 13, 2025 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK CHANNEL SUPPORT LOCATED STA727 AND RBL 3 AT AFT CARGO COMPARTMENT. REPLACED CHANNEL SUPPORT LOCATED STA727 AND RBL 3 AT AFT CARGO COMPARTMENT IAW B737 700 SRM 51-10-02-0G STEP 9 AND DWG 144A2600 SHEET 566 REV -.
- [SDR SWAA2025102314157](https://openairdocs.org/sdr/SWAA2025102314157.md): Gusset · damaged · Sep 13, 2025 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
  > ELONGATED HOLE GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT. REPLACED GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 143A7902; SHEET: 174; REV-.
- [SDR SWAA2025102314160](https://openairdocs.org/sdr/SWAA2025102314160.md): Web · corroded · Sep 13, 2025 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION SHIELD WEB FLOOR STRUCTURE LOCATED BETWEEN STA767 TO STA794.3 AND RBL21 WL156 AT AFT CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS LOC. ON FLOOR STRUCTURE BETWEEN STA767 TO STA794.3 AND RBL21 WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM51-
- [SDR SWAA2025102214154](https://openairdocs.org/sdr/SWAA2025102214154.md): Rib · cracked · Sep 13, 2025 · N7861J · Boeing 73779P · Horizontal Stabilizer, Spar/Rib
  > CRACKED INSPAR RIB LOCATED STAB STA 120.30 AND 34 INCHES FROM FRONT EDGE LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB IAW SRM 51-40-02, AND SRM 55-10-09-2R-4, REPAIR 4, FIG 202, DETAIL A.
- [SDR SWAA2025102214155](https://openairdocs.org/sdr/SWAA2025102214155.md): Rib · cracked · Sep 13, 2025 · N7861J · Boeing 73779P · Horizontal Stabilizer, Spar/Rib
  > CRACKED INSPAR RIB LOCATED STAB STA 120.30 AND 27 INCHES FROM FRONT EDGE LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB IAW SRM 51-40-02, AND SRM 55-10-09-2R-4, REPAIR 4 FIG 202, DETAIL A.
- [SDR SWAA2025102214156](https://openairdocs.org/sdr/SWAA2025102214156.md): Rib · cracked · Sep 13, 2025 · N7861J · Boeing 73779P · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 19 INCHES FROM FRONT EDGE LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB IAW SRM 51-40-02, AND SRM 55-10-09-2R-4, REPAIR 4, FIG 202, DETAIL A.
- [SDR SWAA2025102314094](https://openairdocs.org/sdr/SWAA2025102314094.md): Rib · cracked · Sep 12, 2025 · N7861J · Boeing 73779P · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 27 INCHES FROM FRONT EDGE LT HORIZONTAL STAB.
- [SDR SWAA2025102314093](https://openairdocs.org/sdr/SWAA2025102314093.md): Rib · cracked · Sep 12, 2025 · N7861J · Boeing 73779P · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB LOCATED STAB STA120.30 AND 19 INCHES FROM FRONT EDGE LT HORIZONTAL STAB.
- [SDR SWAA2025102214153](https://openairdocs.org/sdr/SWAA2025102214153.md): Rib · cracked · Sep 12, 2025 · N7861J · Boeing 73779P · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB LOCATED STAB STA 129.50 AND 34 INCH FROM FRONT EDGE AT RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB IAW SRM 55-10-09-2R-5, REPAIR 5, FIG 204, DETAIL A.
- [SDR SWAA2025102313442](https://openairdocs.org/sdr/SWAA2025102313442.md): Angle · cracked · Sep 11, 2025 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK ANGLE FLOOR STRUCTURE LOCATED BS 695 AND RBL 24.75 AT PASSENGER CABIN. REPLACED ANGLE ON FLOOR STRUCTURE LOCATED BS 695 AND RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DWG: 273A9110 SHEET: 6 REV: A.
- [SDR SWAA2025102313443](https://openairdocs.org/sdr/SWAA2025102313443.md): Stiffener · cracked · Sep 11, 2025 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK STIFFENER ASSY FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL 0 AND RBL 24.75 PASSENGER CABIN. REPLACED STIFFENER ASSY FLOOR STRUCTURE AND FASTENERS LOCATED BS 540 BETWEEN BL 0 AND RBL 24.75 PASSENGER CABIN IAW B737-700 SRM-51-10-02 ITEM 9 AND B737-700 SRM 5
- [SDR SWAA2025102313453](https://openairdocs.org/sdr/SWAA2025102313453.md): Beam · cracked · Sep 11, 2025 · N7861J · Boeing 73779P · Service Doors
  > CRACK INDICATION ON RADIUS OF FORWARD SERVICE DOOR 141A6536-14 BEAM #4.LENGTH OF CRACK: 0.625 IN. EO 5241-C-14093 OR 5241-C-14344 WILL BE ADDED TO REPAIR ORDER FOR REPAIR. REPLACED TRACE BEAM NR 4 BTW BS 299.10 AND 328.87, FWD SERVICE DOOR IAW SRM 51-10-02 P
- [SDR SWAA2025102213441](https://openairdocs.org/sdr/SWAA2025102213441.md): Angle · cracked · Sep 11, 2025 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACKED ANGLE LOCATED BS 695 BL0 AFT SIDE. REPLACED ANGLE IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2025102213444](https://openairdocs.org/sdr/SWAA2025102213444.md): Angle · cracked · Sep 11, 2025 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACKED ANGLE LOCATED BS 695 AND BL0 FWD SIDE. REPLACED ANGLE IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2025071691040](https://openairdocs.org/sdr/SWAA2025071691040.md): Light · inoperative · Jul 14, 2025 · N7861J · Boeing 73779P · Emergency Lighting
  > SEAT ROW 6ABC EMERGENCY LIGHT OUT. RELAMPED SEAT ROW 6ABC EMERGENCY AREA LIGHT. OPS CHECK GOOD PER AMM 33-51-03.
- [SDR SWAA2025052775456](https://openairdocs.org/sdr/SWAA2025052775456.md): Unknown · odor · May 26, 2025 · N7861J · Boeing 73779P · Air Distribution System
  > F/A REPORTS SMELL OF SMOKE IN THE AFT CABIN<[01] C/W SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW AMM 05-51-56 AND FIM 21-00 TASK 806. NO DEFECTS NOTED AT THIS TIME. AIRCRAFT OK FOR SERVICE.
- [SDR SWAA2025052071311](https://openairdocs.org/sdr/SWAA2025052071311.md): Lock · out of adjust · May 15, 2025 · N7861J · Boeing 73779P · Passenger Compartment Equipment
  > PASSENGER CABIN SEAT EXIT ROW 11C IS RECLINING.<[01] ADJUSTED HYDRO-LOCK PER AMM 25-22-00;[02] INSPECTED C/A 1. ROBERT FRENZEL (TECHNICIAN); ADJUSTED HYDRO-LOCK PER AMM 25-22-00
- [SDR SWAA2025012489208](https://openairdocs.org/sdr/SWAA2025012489208.md): Compressor · stalled · Jan 23, 2025 · N7861J · Boeing 73779P · Turbine Engine Compressor Section
  > ON CLIMB OUT THROUGH 9000 FEET; AIRCRAFT SHUDDERED AND ENGINE #1 N1 BEGAN CYCLING THROUGH 80% AND 90% N1. ENGINE REDUCED TO 50% N1 AND ENGINE INDICATIONS WERE NORMAL AT 50% N1 AND BELOW FOR REMAINDER OF FLIGHT<[01] ACCOMPLISHED BORESCOPE INSPECTION OF #1 ENGIN
- [SDR SWAA2024111157548](https://openairdocs.org/sdr/SWAA2024111157548.md): Cover · misinstalled · Nov 7, 2024 · N7861J · Boeing 73779P · Emergency Lighting
  > AFT SERVICE DOOR HAS THE INCORRECT DIRECTION EMERGENCY LENS COVER.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-960-802-NG (EXIT SIGN - LIGHT ASSEMBLY REPLACEMENT - PERMANENT)]
- [SDR SWAA2024081526100](https://openairdocs.org/sdr/SWAA2024081526100.md): Balance Weight · corroded · Aug 15, 2024 · N7861J · Boeing 73779P · Rudder Structure
  > RUDDER BALANCE WEIGHT HAS EVIDENCE OF CORROSION<[01] R AND R RUDDER BALANCE WEIGHT PER EA 24-155-02244
- [SDR SWAA2024032667236](https://openairdocs.org/sdr/SWAA2024032667236.md): Doubler · cracked · Mar 24, 2024 · N7861J · Boeing 73779P · Fuselage Main, Structure
  > GROUND POWER DOOR CUTOUT DOUBLER AFT EDGE FOUND CRACK<[01] PERFORMED HFEC OF THE CUTOUT REF 737 NDT MANUAL PART 6 51-00-00 PROCEDURE 23. NO DEFECTS NOTED AT THIS TIME.;[02] TRIMMED GROUND POWER DOOR SURROUND DOUBLER AS REQUIRED PER SRM 53-10-15-2R-4 ZONE 1;[03
- [SDR SWAA2024031964420](https://openairdocs.org/sdr/SWAA2024031964420.md): Extinguisher · leaking · Mar 16, 2024 · N7861J · Boeing 73779P · Fire Bottle, Portable
  > COCKPIT FIRE EXTINGUISHER HAS A SLOW LEAK.<[01] REPLACED COCKPIT FIRE EXTINGUISHER PER AMM 26-26-01.
- [SDR SWAA2024011540601](https://openairdocs.org/sdr/SWAA2024011540601.md): Transmitter · faulty · Jan 13, 2024 · N7861J · Boeing 73779P · Trailing Edge Flap Control System
  > ON FINAL AFTER SELECTING FLAPS 10 FROM FLAPS 5 FLAPS SPLIT-LEFT INDICATED 6 RIGHT =8 LANDED FLAPS 5 POSITION-AFTER LANDING FLAPS INDICATED 5;PSEU LIGHT AFTER LANDING 27-52261<[01] REMOVED AND REPLACED R/H FLAP POSITION TRANSMITTER PER AMM 27-58-01 OPS CHECK GO
- [SDR SWAA2023092603524](https://openairdocs.org/sdr/SWAA2023092603524.md): Light · inoperative · Sep 25, 2023 · N7861J · Boeing 73779P · Emergency Lighting
  > EMERGENCY EXIT LIGHT ON L/H OWE FWD OF WINDOW LIGHT INOP<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY EXIT LIGHT ON FWD SIDE OF L/H OWE WINDOW LIGHT IAW AMM 33-51-03-960-801.;[02] JOB COMPLETE.
- [SDR SWAA2023092603526](https://openairdocs.org/sdr/SWAA2023092603526.md): Light · inoperative · Sep 25, 2023 · N7861J · Boeing 73779P · Emergency Lighting
  > BULLNOSE EMERGENCY EXIT LIGHT INOP AT SEAT ROW 4ABC<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF BULLNOSE EMERGENCY EXIT LIGHT AT SEAT ROW 4ABC IAW AMM 33-51-03-960-801.;[02] JOB COMPLETE.
- [SDR SWAA2023092603525](https://openairdocs.org/sdr/SWAA2023092603525.md): Light · inoperative · Sep 25, 2023 · N7861J · Boeing 73779P · Emergency Lighting
  > EMERGENCY EXIT LIGHT IN BETWEEN FWD RECESSED CEILING LIGHTS INOP<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF FWD RECESSED CEILING EMERGENCY EXIT LIGHT IAW AMM 33-51-03-960-801.;[02] JOB COMPLETE.
- [SDR SWAA2023092603523](https://openairdocs.org/sdr/SWAA2023092603523.md): Light · inoperative · Sep 24, 2023 · N7861J · Boeing 73779P · Emergency Lighting
  > EMERGENCY EXIT AREA LIGHT AT SEAT ROW 16FED IS INOP<[01] REMOVED AND REPLACED AREA LIGHT LAMP AT SEAT ROW 16FED OPS CHECK GOOD IAW AMM 33-51-03-960-801.;[02] VERIFIED CORRECTIVE ACTION STEP 1. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
- [SDR SWAA2023092603382](https://openairdocs.org/sdr/SWAA2023092603382.md): Light · broken · Sep 22, 2023 · N7861J · Boeing 73779P · Emergency Lighting
  > LWH OVERWING EXIT LIGHT FWD OF DOOR CUTOUT IS BROKEN.<[01] REPLACED LWH OVERWING EXIT LIGHT FWD OF DOOR AND GOOD OPERATIONAL TEST PER AMM 33-51-01-960-802.;[02] VERIFIED
- [SDR SWAA2023092699962](https://openairdocs.org/sdr/SWAA2023092699962.md): Panel · cracked · Sep 13, 2023 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACKED BREAK PANEL STA 540; RBL 1; WL 208.<[01] UPDATED TABLE;[02] COMPLETED STEPS 1-2; OK TO INSTALL STEP 3.;[03] REMOVED & INSTALLED NEW BREAK PANEL AT BS 540 RBL 1 WL 208 PER SRM 5140-02-0G-0 AND SRM 51-40-05-0G-0 AND BOEING DWG 143A5240
- [SDR SWAA2023092699961](https://openairdocs.org/sdr/SWAA2023092699961.md): Panel · cracked · Sep 13, 2023 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACKED BREAK PANEL STA 540; LBL 1; WL 208.<[01] COMPLETED STEPS 1-2; OK TO INSTALL STEP 3.;[02] REMOVED AND REPLACED BREAK PANEL AT BS 540 LBL 1 WL 208 PER SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-00 AND DWG # 143A5240
- [SDR SWAA2023092899197](https://openairdocs.org/sdr/SWAA2023092899197.md): Scuff Plate · cracked · Sep 11, 2023 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] REPAIRED THE CORNER SCUFF PLATE PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(4) AND BAC 5975 APPLIED A CHEMICAL CONVERSION COATING TO BARE ALUMINUM SURFACES PER SOPM 20-43-03; TYPE 2; CLASS A OR C AND SRM 53-60

Next page: https://openairdocs.org/aircraft/N7861J/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 = 'N7861J' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7861J/reports

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