N7862A

Service difficulty reports · 236

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N7862A' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWAA2025110531910Coalescer Bag · odorON TAXI IN, STARTED APU, TURNED ON APU AIR. SMELLED SMOKE, TURNED OFF APU AIR AND APU. TURNED OFF RECIRCULATION FAN ODOR CLEARED. SMOKE ODOR IN ENTIRE CABIN, FWD AND AFT. C/W INSPECTION 05-51-56-0200-801 COULD NOT DUPLICATE. REPLACED COALESCER BAGS NR 1 & Nov 4, 2025 · N7862A · Boeing 73779P · Humidity Control SystemSDR SWAA2025110327051Lamp · not seatedLEFT EMERGENCY EXIT HATCH OVERHEAD LIGHT INOPERATIVE. ON INVESTIGATION FOUND LT EMERGENCY EXIT HATCH OVERHEAD LAMP INCORRECTLY SEATED, SEATED CORRECTLY AND PERFORMED GOOD LAMP TEST IAW AMM 33-21-00-960-801.Oct 22, 2025 · N7862A · Boeing 73779P · Emergency LightingSDR SWAA2025110327053Connector · disconnectedSEVERAL RT & LT OVERHEAD STOWAGE BULLNOSE EMERGENCY EXIT LIGHTS INOPERATIVE. RECONNECTED CONNECTOR D13018 TO EMERGENCY LIGHT POWER SUPPLY M2335 IAW AMM 33-51-06-960-806 AND PERFORMED SATISFACTORY OPS TEST IAW AMM 33-51-00-710-801.Oct 22, 2025 · N7862A · Boeing 73779P · Light System WiringSDR SWAA2025110323750Glowstrip · damagedMULTIPLE PHOTOLUMINESCENT STRIPS FOUND DAMAGED. REPLACED AND INSTALLED NEW PHOTOLUMINESCENTS STRIPS KIT IAW DWG 33500007, REV 2.Oct 12, 2025 · N7862A · Boeing 73779P · Emergency EquipmentSDR SWAA2025103022363Rib · crackedFOUND CRACK LOCATED AT RT HORIZONTAL STAB NR 4 RIB STAB STA 120.30 NR 1 VERTICAL STIFFENER. REPAIRED IAW SRM 55-10-09-2R-4.Oct 8, 2025 · N7862A · Boeing 73779P · Horizontal Stabilizer, Spar/RibSDR SWAA2025103022364Rib · crackedFOUND CRACK LOCATED AT RT HORIZONTAL STAB NR 4 RIB STAB STA 120.30 NR 4 VERTICAL STIFFENER. REPAIRED IAW SRM 55-10-09-2R-5.Oct 8, 2025 · N7862A · Boeing 73779P · Horizontal Stabilizer, Spar/RibSDR SWAA2025103022362Rib · crackedFOUND CRACKS LOCATED AT RT HORIZONTAL STAB NR 4 RIB HSS 120.30, FRONT SPAR ATTACH STIFFENER. REMOVED AND REPLACED RT HORIZONTAL STAB RIB FRONT STIFFENER IAW SRM 51-40-02-0G-0 AND DWG 142A2401 REV:F.Oct 8, 2025 · N7862A · Boeing 73779P · Horizontal Stabilizer, Spar/RibSDR SWAA2025110421441Angle · deformedDEFORMED ANGLE RBL20.6 STA1096 WL 249.61 HORIZONTAL BEAM LOWER. RII ITEMS COMPLIED WITH ON 25-153-02689-WIP1-WIP4. NO RII REQUIREMENTS ON 25-153-01768-WIP1. REMOVED AND REPLACE ANGLE IAW EA 25-153-02689.Oct 4, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2025110421439Stiffener · deformedDEFORMED STIFFENER BS 1096, RBL 10 - 30.6, WL 249.61 HORIZONTAL BEAM LOWER. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-02-0G-0 AND EA 25-153-02689, FIGURE 3, SHEET 1.Oct 4, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2025110321440Stiffener · deformedDEFORMED STIFFENER BS 1088, RBL 15 TO RBL 29, WL 249.61. HORIZONTAL BEAM LOWER. REFER TO FAULT TTG8Q015D0QP WHERE EA 25-153-02689 WAS ADDED AS A SUBTASK..Oct 4, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2025110321438Angle · deformedDEFORMED ANGLE, RBL 20.6, BS 1088 - 1096, WL 249.61, HORIZONTAL BEAM LOWER. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, AND EA 25-153-02689, FIGURE 3, SHEET 1.Oct 4, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2025103018362Intercostal · corrodedCORROSION ON AFT CARGO BAY INTERCOSTAL AT BS 767 TO 787 RBL 6 WL 150. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G, AND DWG 146A8130, REV B.Sep 26, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2025103018363Intercostal · corrodedCORROSION ON AFT CARGO BAY INTERCOSTAL AT BS 787 TO 807 RBL 6 WL 150. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G AND DWG 146A8130, REV B.Sep 26, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2025110318359Web · corrodedCORROSION ON AFT CARGO BAY SUB WEB THRESHOLD AT BS 794 - 847, RBL 25, WL 155. REMOVED AND REPLACED ACB SUB THRESOLD WEB IAW SRM 51-40-02 AND DWG 146A8120 REV: E.Sep 25, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2025103018360Intercostal · corrodedCORROSION ON AFT CARGO BAY INTERCOSTAL AT BS 767 - 807, RBL 6, WL 150. OPENSep 25, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2025103018356Sidewall Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 727C - 787, LBL 21, WL 155. REMOVED & REPLACED THE FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0 & DWG 146A7500, REV B.Sep 25, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2025103018361Sidewall Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 727C - 787, RBL 21, WL155. REMOVED & REPLACED FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02, & DWG 146A7500 ID: 0085 REV A.Sep 25, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2025110417169Seat Track · corrodedCORROSION ON SEAT TRACK, LBL 45, BS 480+18, 500A+9, 500D+10. THIS FAULT WILL BE RESOLVED IN FAULT TTG8Q015AMZ5; DUE REPLACEMENT OF SEAT TRACK.Sep 22, 2025 · N7862A · Boeing 73779P · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025110317055Shield · corrodedCORROSION ON AFT SHIELD BS 500-500A, S27R WL 156. REMOVED AND REPLACED FCB AFT SHIELD IAW SRM 51-40-02-0G-0 AND DWG 143A0080 REV -.Sep 22, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2025110317053Door Frame · crackedPASSENGER CABIN FWD ENTRY DOOR STOP FITTING WEB CRACKED BS295 S-16L. REMOVED AND REPLACED PASSENGER CABIN FWD ENTRY DOOR STOP FITTING INTERCOSTAL S16L IAW SRM 51-40-02 AND DWG 141A8180 REV: C.Sep 22, 2025 · N7862A · Boeing 73779P · Fuselage Main, StructureSDR SWAA2025103017185Stringer Clip · crackedCRACKED STRINGER CLIP, BS 727A, S7R. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1102, REV E.Sep 22, 2025 · N7862A · Boeing 73779P · Fuselage Main, Attach FittingsSDR SWAA2025103017186Stringer Clip · crackedCRACKED STRINGER CLIP AT BS 727B, S7R. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1102 REV D.Sep 22, 2025 · N7862A · Boeing 73779P · Fuselage Main, Attach FittingsSDR SWAA2025103016913Rib · crackedDURING INSPECTION FOUND CRACK AT NR 4 RIB STA 120.30 STIFFENER NR 2. REPAIRED IAW SRM 55-10-09-2R-5.Sep 21, 2025 · N7862A · Boeing 73779P · Horizontal Stabilizer, Spar/RibSDR SWAA2025110316500Scuff Plate · crackedAFT CARGO DOOR FWD CORNER SCUFF PLATE IS CRACKED. RECEIVED NEW AFT CARGO DOOR FWD CORNER SCUFF PLATE ITEM 146A8341-07. IT WILL BE INSTALL ON TASK CARD TTG8Q0157507.Sep 20, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2025110316512Fitting · crackedCRACKED FITTING, BS 559+8, LBL 6, WL 148.5. RECEIVED NEW FITTING. REMOVED AND REPLACED THE FITTING IAW SRM 51-40-02-0G-0, AND AIPC 53-12-11-25 FIG 2.Sep 20, 2025 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2025110316718Floorbeam · crackedCRACKED FLOORBEAM, BS 540, LBL 2, WL 208. REMOVED AND INSTALLED A NEW FLOORBEAM IAW SRM 51-40-02 AND DWG 143A0060.Sep 20, 2025 · N7862A · Boeing 73779P · Fuselage Main, Floor BeamSDR SWAA2025110316719Floorbeam · crackedCRACKED FLOORBEAM BS 540, RBL 2, WL 208. REMOVED AND REINSTALLED THE FLOORBEAM IAW SRM 51-40-02 AND DWG 143A0060.Sep 20, 2025 · N7862A · Boeing 73779P · Fuselage Main, Floor BeamSDR SWAA2025103016496Stringer Clip · no discrepancyFUSELAGE STRINGER CLIP BS 706, S10L CRACKED. HFEC INSPECTED AREA IAW NDTM PART 6, 51-00-00, PROCEDURE 23. NO CRACKS NOTED.Sep 19, 2025 · N7862A · Boeing 73779P · Fuselage Main, Attach FittingsSDR SWAA2025103016497Stringer Clip · no discrepancyFUSELAGE STRINGER CLIP BS 727A S15L CRACKED. HFEC INSPECTED AREA IAW NDTM PART 6; 51-00-00, PROCEDURE 23. NO CRACKS NOTED.Sep 19, 2025 · N7862A · Boeing 73779P · Fuselage Main, Attach FittingsSDR SWAA2025110316163Pressure Deck · crackedCRACK NOTED ON LEFT HORIZONTAL PRESSURE DECK WEB BS 673, LBL 32, WL 202.5. L: 0.4. REPAIRED THE PRESSURE DECK AND REMOVED & REPLACED ALL SHORT AND HIGH FASTENERS AND INSTALLED MISSING COLLARS AT THE REPAIR AREA AS A CORRECTION FOR STEP 10, ITEM 1 IAW SRM 53-Sep 18, 2025 · N7862A · Boeing 73779P · Fuselage Main, StructureSDR SWAA2025103015048Floor Panel · pulledFLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2025103015049Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2025103015050Floor Panel · pulledFLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2025103015052Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 241BF REPLACED WITH A NEW FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2025103015054Floor Panel · pulledFLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2025103015057Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2025103015056Floor Panel · pulledFLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2025103015058Floor Panel · pulledFLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED A NEW FLOOR PANEL IAW DWG 144A5810 0123.Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2025103015051Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF NEW 241AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0-A00938.Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2025103015047Floor Panel · pulledFLOOR PANEL 232RF UPPER SKIN HAS AREAS OF PULLED STRANDS FABRICATION OF NEW FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0-A00938.Sep 16, 2025 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2025110415045Skin · no discrepancySUSPECT CRACK RT WING NR 5 SLAT LEADING EDGE AT ACTUATOR ATTACH FITTING, SLAT STATION 85.19. HFEC INSPECTED RT WING #5 SLAT LEADING EDGE AT ACTUATOR ATTACH FITTING SLAT STATION 85.19 IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS NOTED.Sep 15, 2025 · N7862A · Boeing 73779P · Leading Edge DevicesSDR SWAA2025110415026Inlet · pulledPULLED THROUGH FASTENERS 2 O' CLOCK POSITION ON RIGHT INLET COWL OUTER LIP SKIN. REMOVED AND REPLACED RT INLET COWL OUTER LIP SKIN IAW SRM 54-10-01-1A-2 AND SRM 51-40-02. ACCOMPLISHED NDI INSPECTION IAW NDTM PART 6; 51-00-00. REMOVED AND REPLACED NR 2 ENGISep 15, 2025 · N7862A · Boeing 73779P · Nacelle/Pylon, Main FrameSDR SWAA2025040720513Door · warning lightCLIMBING OUT GOT AFT ENTRY DOOR LT; RAN QRH HANDLE HAD MOVED; LT WENT OUT; DOOR LT CAME BACK ON A 2ND TIME ON FINAL; AT DIVERT CITY OF KLIT.<[01] REMOVED DEBRIS FROM AFT ENTRY DOOR EXTERIOR HANDLE RECESS & ACCOMPLISHED OPEN/CLOSE WITH THE INTERIOR & EXTERIORDOApr 1, 2025 · N7862A · Boeing 73779P · Door Warning SystemSDR SWAA2025010783480Battery Pack · no testALL LIGHT RELATED TO BATTERY PACK M2335 FAIL TEST. REPLACED EMERGENCY BATTERY PACK. PERFORMED GOOD TEST PER AMM 33-51-06-960-805.Jan 6, 2025 · N7862A · Boeing 73779P · Emergency LightingSDR SWAA2025010783482Lamp · failedLEFT AND RIGHT OVERWING ESCAPE GROUND ILLUMINATION FAIL EMERGENCY LIGHT TEST (L548) (L547)<[01] REPLACED LAMP TO LEFT AND RIGHT OVERWING ESCAPE (L548) AND (L547) PER AMM 33-51-04-960-801. GOOD TEST.;[02] VERIFIED CORRECTIVE ACTION STEP 1.Jan 6, 2025 · N7862A · Boeing 73779P · Emergency LightingSDR SWAA2025010783481Lamp · inoperativeEMERGENCY LIGHT AFT ESCAPE SLIDE LIGHT (L732) OUTSIDE SERVICE DOOR LH SIDE INOP<[01] REPLACED LAMP TO EMERGENCY LIGHT AFT ESCAPE SLIDE LIGHT (L732) OUTSIDE SERVICE DOOR LH SIDE PER AMM 33-51-04-960-801. GOOD TEST.;[02] VERIFIED CORRECTIVE ACTION STEP 1.Jan 6, 2025 · N7862A · Boeing 73779P · Emergency LightingSDR SWAA2025010681802Intercostal · crackedINTERNAL DAMAGE BETWEEN STA 927 AND 947 STR 21 L/H INTERCOSTAL CRACKED.<[01] PART TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9.<BR><BR>REMOVED DAMAGED INTERCOSTAL AT STA 927 - 947; STR- 21L/H PER SRM 51-40-02.;[02] FABRICATED; LOCATED AND DRDec 30, 2024 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2024123080862Intercostal · crackedINTERNAL DAMAGE BETWEEN STA 927 AND 947 STR 21 LH INTERCOSTAL IS CRACK.<[01] PREFORMED SURFACE CRACK NDT PER PART 6 51-00-00 PRO 23;[02] PERFORMED EA 24-153-03554'. ADD A REFERENCE TO THE FAULT TTG8Q00XT976.;[03] VERIFIED PERFORMED EA 24-153-03554'. ADD A REFEDec 26, 2024 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2024123080858Skin · crackedINTERNAL DAMAGE AT STA 927 STR 21 LH CRACK. PREFORMED SURFACE CRACK NDT PER PART 6 51-00-00 PRO 23. PERFORMED EA 24-153-03554'. ADD A REFERENCE TO THE FAULT TTG8Q00XT976.Dec 26, 2024 · N7862A · Boeing 73779P · Fuselage Main, Plate/SkinSDR SWAA2024102852533Seal · crackedLEFT HORIZONTAL STABILIZER UPPER STAB TO BODY SLIDING SEAL IS CRACKED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-401 CONFIG 1-NG (STABILIZER TO BODY FRONT SPAR SLIDING SEAL - REMOVAL/INSTALLATION - PERMANENT)]Oct 24, 2024 · N7862A · Boeing 73779P · Horizontal Stabilizer Miscellaneous Structure
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