Boeing 737-7Q8

Service difficulty reports · 3,961

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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 aircraft_model_key = '7377Q8'
  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 SWAA2024022948056Web · crackedCRACK ON WEB LOC. BS 294.5 BTW RBL 54 TO RBL 60 AND WL 208.1 AT PASSENGER CABIN 2024-77397<[01] REPLACED WEB LOC. BS 294.5 BTW RBL 54 TO RBL 60 AND WL 208.1 AT PASSENGER CABIN. IAW B737-700 SRM 51-10-02 STEP 9 AND DWG 141A8310 REV:B AND DWG 140A9810 REV:- SEE Feb 3, 2024 · N7877H · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2024030447949Rib · crackedCRACK ACCESS PANEL 331B ON RIB LOCATED LE STA 105.29 AT LT HORIZONTAL STABILIZER 2024-77389<[01] REPLACED RIB AND FASTENERS LOCATED LE STA 105.29 AT LT HORIZONTAL STABILIZER I.A.W. B377-700 SRM 51-40-02 AND DRAWING # 186A1001 REV ?A? SEE INDIVIDUAL SING OFF BEFeb 2, 2024 · N7877H · Boeing 7377Q8 · Horizontal Stabilizer, Spar/RibSDR SWAA2024030147542Stringer · crackedCRACK STRINGER 23R LOCATED BS540 FWD CARGO COMPARTMENT 2024-77383 CRACK STRINGER 23R LOCATED BS540 FWD CARGO COMPARTMENT<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 130061901; CAL DUE DATE: 09-JUN-24;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 SFeb 1, 2024 · N7877H · Boeing 7377Q8 · Fuselage Main, Longeron/StringerSDR SWAA2024030147681Access Panel · delaminatedDELAMINATED ACCESS PANEL 193AL BELLY FAIRING FWD EDGE APPROXIMATELY 16 INCHES FROM TOP EDGE AT LOWER FUSELAGE 2024-77386<[01] TOOL USED:CALIPER PN: 500-197-30 SN: A21141912; DUE DATE: 24-DEC-24.;[02] TOOL USED: SCALE P/N:CR5200 S/N:8342514597 DUE DATE:21-FEB-2Feb 1, 2024 · N7877H · Boeing 7377Q8 · Fuselage Main, Plate/SkinSDR SWAA2024030147261Gusset · crackedCRACK GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT 2024-77370<[01] REPLACED GUSSET LOCATED BS500D; STRINGER 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 143A7902; SHEET: 174; REV: -; SEE INDIVIDUAL SIGN-OFF BELOW.Jan 31, 2024 · N7877H · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2024022946840Megaphone · deterioratedDETERIORATED WINDSCREEN LT SIDE THE BATTERIE MEGAPHONE EMERGENCY EQUIPMENT AT AFT GALLEY AREA (8 EA) 2024-77348<[01] REPLACED WINDSCREEN LT SIDE THE BATTERIE MEGAPHONE EMERGENCY EQUIPMENT AT AFT GALLEY AREA (8 EA) IAW B737-700 AMM 25-64-00-900-804;[02] COMPLETJan 31, 2024 · N7877H · Boeing 7377Q8 · Emergency EquipmentSDR SWAA2024022946841Megaphone · deterioratedDETERIORATED WINDSCREEN LT SIDE THE BATTERIE MEGAPHONE EMERGENCY EQUIPMENT AT FWD GALLEY AREA (8 EA) 2024-77349<[01] REPLACED WINDSCREEN LT SIDE THE BATTERIE MEGAPHONE EMERGENCY EQUIPMENT AT FWD GALLEY AREA (8 EA) I.A.W B737-700 AMM 25-64-00-900-804.;[02] TASKJan 31, 2024 · N7877H · Boeing 7377Q8 · Emergency EquipmentSDR SWAA2024030146832Bracket · wornWEAR HARDWARE ON GIRT BAR FLOOR BRACKETS AT FWD ENTRY AND SERVICE DOOR 2024-77334<[01] REPLACED HARDWARE ON GIRT BAR FLOOR BRACKETS AT FWD ENTRY AND SERVICE DOOR IAW AMM:25-66-02-400-801 STEP 3.D.(1)(H) THRU E. AND PERFORMED OPERATIONAL TEST GIRT BAR BRACKETS Jan 30, 2024 · N7877H · Boeing 7377Q8 · Emergency EquipmentSDR SWAA2024022946387Frame · crackedCRACK FRAME STA 312 BETWEEN STR 5LTO STR 6L AT PASSENGER CABIN 2024-77304<[01] PERFORMED PERMANENT REPAIR ON FRAME IAW M-22-153-01244 SEE INDIVIDUAL SIGN OFF BELOW;[02] COMPLETE TASK CERTIFIEDJan 29, 2024 · N7877H · Boeing 7377Q8 · Fuselage Main, FrameSDR SWAA2024022946385Frame · crackedCRACK FRAME STA259.5 AT LEVEL STR 9R AT PASSENGER CABIN 2024-77317<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 200048001; DUE DATE: 01-MAY-24;[02] TOOL USED ULTRASONIC EQUIPMENT P/N 45MG; S/N 130066401 DUE DATE 05-OCT-24 USED ON STEP 9;[Jan 29, 2024 · N7877H · Boeing 7377Q8 · Fuselage Main, FrameSDR SWAA2024022946388Stub Frame · crackedCRACK FRAME STUD LOCATED STA 294.5 AT LEVEL STR 17R AT PASSENGER CABIN 2024-77315<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 200048001; DUE DATE: 01-MAY-24;[02] ON STEP 7; EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 200053402; DUE DATJan 29, 2024 · N7877H · Boeing 7377Q8 · Fuselage Main, FrameSDR SWAA2024022945845Light · brokenBROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2024-77259<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) I.A.W. SOPM 20-50-12;[02] TASK COMPLETEDJan 28, 2024 · N7877H · Boeing 7377Q8 · Emergency LightingSDR SWAA2024020745703Slide · out of adjustCUSTOMER REQUEST: ASD SLIDE HANGS TOO LOW AT GIRT BAR AREA<[01] TUCKED EXCESS GIRT MATERIAL UP IN THE SLIDE COMPARTMENT IAW AMM 25-66-01-400-803 AND MT 725-61-06 STEP 3.I.(2).;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLEJan 28, 2024 · N7864B · Boeing 7377Q8 · Escape SlideSDR SWAA2024020745704Slide · out of adjustCUSTOMER REQUEST: AED SLIDE HANGS TOO LOW AT GIRT BAR AREA<[01] TUCKED EXCESS GIRT MATERIAL UP IN THE SLIDE COMPARTMENT IAW AMM 25-66-01-400-803 AND MT 725-61-06 STEP 3.I.(2).;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLEJan 28, 2024 · N7864B · Boeing 7377Q8 · Escape SlideSDR SWAA2024012945495Slide · partial deployFWD SVC DOOR SLIDE PARTIALLY DEPLOYED<[01] REMOVED AND REPLACED FWD SERVICE SLIDE REF MM 25-66-01.;[02] REMOVED AND REPLACED FWD SERVICE SLIDE REF MT 725-61-06.Jan 27, 2024 · N7863A · Boeing 7377Q8 · Escape SlideSDR SWAA2024030445152Floorbeam · crackedCRACK FLOOR STRUCTURE ANGLE ON BS 540 BTW BL 0 TO RBL 12 AT PASSENGER CABIN 2024-77202<[01] REPLACED ANGLE LOCATED ON FLOOR STRUCTURE ON BS 540 BTW BL 0 TO RBL 12 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-10-02 ITEM 9 ;SRM 51-40-02 AND DWG 143A0060 REV:A SEE IJan 26, 2024 · N7877H · Boeing 7377Q8 · Fuselage Main, Floor BeamSDR SWAA2024030445153Floorbeam · crackedCRACK ANGLE FLOOR STRUCTURE ON BS 540 BTW BL 0 TO LBL 12 AT PASSENGER CABIN 2024-77211<[01] REPLACED ANGLE LOCATED ON FLOOR STRUCTURE ON BS 540 BTW BL 0 TO LBL 12 AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 ITEM 9;SRM 51-40-02 AND DWG 143A0060 REV:A SEE INDJan 26, 2024 · N7877H · Boeing 7377Q8 · Fuselage Main, Floor BeamSDR SWAA2024022945292Scuff Plate · crackedCRACK ON AFT CORNER SCUFF PLATE ON FWD CARGO COMPARTMENT DOOR CUTOUT. REPAIRED AFT CORNER SCUFF PLATE ON FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.Jan 26, 2024 · N7877H · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2024020844415Bracket · crackedL/H HORIZONTAL STAB RIB TO FRONT SPAR WEB TEE CHORD ATTACH BRACKET CRACKED AT STA 129.5<[01] REMOVED AND REPLACED L/H HORIZONTAL STAB RIB TO FRONT SPAR WEB TEE CHORD ATTACH BRACKET STA 129.5 PER SRM 51-40-02; SRM 51-40-05; DWG# 182A5305; DWG# 182A2401 REV F; AJan 25, 2024 · N7864B · Boeing 7377Q8 · Horizontal Stabilizer StructureSDR SWAA2024030144218Handle · brokenBROKEN LINING HANDLE AFT ENTRY DOOR AT AFT GALLEY AREA (1 EA) 2024-77079<[01] REPLACED LINING HANDLE AFT ENTRY DOOR AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 25-21-25-420-801 STEP 3.C.(5).;[02] REPLACED LINING HANDLE AFT ENTRY DOOR AT AFT GALLEY AREA (1 EA)Jan 24, 2024 · N7877H · Boeing 7377Q8 · Passenger/Crew DoorsSDR SWAA2024030144219Light · inoperativeINOP LAMPS ASSY GALLEY 4 EMERGENCY EXIT AFT GALLEY AREA (1EA) 2024-77077<[01] REPLACED LAMPS ASSY GALLEY 4 EMERGENCY EXIT AFT GALLEY AREA (1EA) IAW B737-700 AMM 33-51-01-960-802;[02] CERTIFIED WORK PERFORMEDJan 24, 2024 · N7877H · Boeing 7377Q8 · Emergency LightingSDR SWAA2024020844414Rib · crackedL/H HORIZONTAL STAB RIB AT STA 129.5 WEB AT FWD UPPER CORNER IS CRACKED<[01] REPAIRED L/H HORIZONTAL STABILIZER RIB AT STA 129.5 WEB AT FWD UPPER CORNER IAW EA NO: 24-155-00236 REV A.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.;[03] THE DAMAGE WASJan 24, 2024 · N7864B · Boeing 7377Q8 · Horizontal Stabilizer, Spar/RibSDR SWAA2024020844319Lens · brokenEMERGENCY EXIT LIGHT LENS COVER ATTACH SCREW BROKEN CABIN SIDEWALL JUST FWD OF R/H OVER WING EXIT DOOR CUTOUT.<[01] REMOVED AND REPLACED R/H EXIT SIGN JUST FWD OF OVERWING EXIT DOOR COUT OUT IAW AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION #1;[03] COMJan 24, 2024 · N7864B · Boeing 7377Q8 · Emergency LightingSDR SWAA2024012544411Handle · brokenAFT SERVICE DOOR ASSIT HANDLE BROKEN SWAPPED AFT LAV DOOR ASSIST HANDLE WITH AFT SERVICE DOOR ASSIST HANDLE PER AMM 52-41-31. AFT LAV DOOR ASSIST HANDLE IS INOP. OK TO CONTINUE PER MEL 25-10-01 SP1B.<[01] SWAPPED AFT LAV DOOR ASSIST HANDLE WITH AFT SERVICE DOOJan 24, 2024 · N7851A · Boeing 7377Q8 · Emergency EquipmentSDR SWAA2024011741498Overheat Sensor · faultedDURING DESCENT RIGHT WING TO BODY OVERHEAT ILLUMINATED RAN QRH PROCEDURE. LIGHT EXTINGUISHED<[01] R/R M1763 & M1764 FWD AND AFT WING TO BODY STRUT ELEMENTS PER AMM 26-18-02. OPS CHECK OK.Jan 15, 2024 · N7863A · Boeing 7377Q8 · Overheat DetectionSDR SWAA2024020838222Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION IN WELL OF CROWN AT BS 706+5; 727+15; RBL 45; WL 208<[01] UPDATED MEASUREMENT TABLE;[02] UPDATE STEP 2;[03] UPDATED STEP 3;[04] UPDATED STEP 3;[05] REMOVED CORROSION AND APPLIED FINISH TO REWORKED AREAS. ALL BLENDS FOUND TO BE WIJan 8, 2024 · N7864B · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024020838223Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION ON TOP OF CROWN AT BS 639+23; RBL 45; WL 208<[01] UPDATED STEP 1 AND STEP 2;[02] VERIFIED STEP 1 AND 2.;[03] UPDATED STEP 3;[04] UPDATED STEP 4;[05] REMOVED CORROSION AND APPLIED FINISH TO REWORKED AREAS. ALL BLENDS FOUND TO BE WJan 8, 2024 · N7864B · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024020838235Attach Angle · crackedMID CABIN; WING CENTER SECTION; CABLE INTERCOSTAL O/B ATTACH ANGLE IS CRACKED AT BS 685+8; RBL 24; WL 203 (MARKED)<[01] REMOVED AND REPLACED ANGLE LOCATED ON MID CABIN; WING CENTER SECTION; AT BS 685+8; RBL 24; WL 203 PART RECEIVED CUSTOMER RO NO: 955232-SWA LJan 8, 2024 · N7864B · Boeing 7377Q8 · Fuselage Main, Attach FittingsSDR SWAA2024020838232Support Angle · crackedRIGHT WING: UPPER T/E SUPPORT ANGLE CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT ABOVE #2 PYLON AFT TIP<[01] REMOVED UPPER T/E SUPPORT ANGLE AT TRANSVERSE WEB ABOVE #2 PYLON AFT TIP AND INSTALLED NEW SUPPORT ANGLE P/N 115A2982-10; PO # 934058/1; IAW SRM 51-40-Jan 8, 2024 · N7864B · Boeing 7377Q8 · Wing Miscellaneous StructureSDR SWAA2024020838233Support Angle · crackedRIGHT WING: T/E COVE SEAL SUPPORT ANGLE CRACKED ABOVE #2 PYLON AFT TIP<[01] REMOVED ANGLE AND INSTALLED NEW T/E COVE SEAL SUPPORT ANGLE P/N 115A2953-2; PO # 956288/1 ABOVE # 2 PYLON AFT TIP IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMEJan 8, 2024 · N7864B · Boeing 7377Q8 · Wing Miscellaneous StructureSDR SWAA2024020839134Threshold · corrodedACB CENTER THRESHOLD IS CORRODED AT BS 787+12 - 827+8; RBL 24-29; WL 157<[01] CORRECTION: UPDATED PART NUMBER ON MEASUREMENT TABLE;[02] REMOVED AND REPLACED ACB SUB-THRESHOLD WEB IAW SRM 51-40-02-0G-0Jan 8, 2024 · N7864B · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2024020838231Stringer · crackedSTR 26L IS CRACKED AT AFT FASTENER IN AREA AFT OF FCB; BS 520+19<[01] TASK COMPLETE:<BR>REMOVED PANEL IAW AMM 53-51-21. INSTALLED REPAIR PARTS IAW SRM 53-00-03-2R-1. INSTALLED PANEL 191CL IAW AMM 53-51-21-400-803;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMEJan 8, 2024 · N7864B · Boeing 7377Q8 · Fuselage Main, Longeron/StringerSDR SWAA2024020838229Stringer · crackedSTR 26R IS CRACKED AT AFT FASTENER IN AREA AFT OF FCB; BS 520+19<[01] REMOVED DAMAGED AREA OF STRINGER AND INSTALLED REPAIR PARTS ON STRINGER 26 R/H BETWEEN BS 500D+6' TO BS 539 AT FCB PER SRM 53-00-03-2R-1 REPAIR 1;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASURJan 8, 2024 · N7864B · Boeing 7377Q8 · Fuselage Main, Longeron/StringerSDR SWAA2024020738234Stiffener · crackedLH HORIZONTAL STAB RIB #5; STAB STA 129.5; 3RD VERTICAL STIFFENER CRACKED.<[01] NDT HFEC INSPECTED SURFACE PER 737 NDTM PART 6; 51-00-00; PROC 23; CRACK NOTED; 3RD VERTICAL STIFFENER; LOWER END.<BR>EQUIP ID IS000680 DUE 05/24;[02] REPAIRED L/H HORIZONTAL STAB Jan 8, 2024 · N7864B · Boeing 7377Q8 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024011138879Retainer · out of adjustFWD ENTRY DOOR GIRT BAR RETAINER CLIP MISSING RETAINER PIN<[01] REPLACED FWD ENTRY DOOR GIRT BAR REF AMM 25-66-01Jan 8, 2024 · N7874B · Boeing 7377Q8 · Emergency EquipmentSDR SWAA2024020838212Rib · crackedR/H HORIZONTAL STAB REMOVABLE L/E 341B RIB #4 IS CRACKED<[01] REMOVED RIB #4 AND INSTALLED NEW R/H HORIZONTAL STAB REMOVABLE L/E 341B RIB #4 IAW SRM 51-40-02-0G-0 AND DWG. 186A1001.;[02] VERIFIED CORRECTION ACTION 1 AND MEASUREMENT TABLEJan 7, 2024 · N7864B · Boeing 7377Q8 · Horizontal Stabilizer, Spar/RibSDR SWAA2024020838211Rib · crackedR/H HORIZONTAL STAB REMOVABLE L/E 341B RIB #5 IS CRACKED<[01] REMEVED RIB #5 AND INSTALLED NEW R/H HORIZONTAL STAB REMOVABLE L/E 341B RIB # 5 P/N 186A1305-2; IAW SRM 51-40-02-0G-0 AND DWG. 186A1001.;[02] CUSTOMER CARD COMPLETEJan 7, 2024 · N7864B · Boeing 7377Q8 · Horizontal Stabilizer, Spar/RibSDR SWAA2024020838210Bearing · out of limitsDURING ACCOMPLISHMENT OF CUSTOMER CARD 5510-I-16685-NG; INSP- STABILIZERS- HORIZONTAL STABILIZER SPHERICAL BEARING. FOUND DIMENSION H TO BE .09275' AND OUT OF LIMITS.<[01] COMPLETED STEPS 5 AND 6.;[02] COMPLETED STEPS 8 AND 10;[03] COMPLETED STEP 11;[04] UPDATJan 7, 2024 · N7864B · Boeing 7377Q8 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024020838201Pressure Deck · crackedCRACK; HORIZONTAL PRESSURE DECK WEB; BS 663 + 2; RBL 40<[01] NDT HFEC SURFACE INSPECTED AREA IAW 737 NDTM PART 6 51-00-00 PROC 23; .400 INCH CRACK NOTED; MARKED ENDS AND DIRECTION.<BR>EQUIP USED: NORTEC 600 IS0000680 DUE 05/24;[02] UPDATED MEASUREMENT TABLE.;[Jan 6, 2024 · N7864B · Boeing 7377Q8 · Fuselage Main, StructureSDR SWAA2024020838198Scuff Plate · crackedAFT CARGO BAY AFT SCUFF PLATE CRACKED<[01] UPDATED MEASUREMENT TABLE;[02] ACB SCUFF PLATES WILL BE INSTALLED ON CUST CARD # TTG8Q00QPWHV;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLEJan 6, 2024 · N7864B · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2024020838203Scuff Plate · crackedAFT CARGO BAY FWD SCUFF PLATE CRACKED<[01] UPDATED MEASUREMENT TABLE;[02] ACB SCUFF PLATES WILL BE INSTALLED ON CUST CARD # TTG8Q00QPWHV;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLEJan 6, 2024 · N7864B · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2024020838193Floor Panel · pulledFLOOR PANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW PASSENGER CABIN FLOOR PANEL 241CF FROM BMS4-17 TYPE 6 LOT#1534398-1; INSERTS INSTALLED USING BMS5-107 LOT#AK3BA2380A/A; CURED INSERTS USING HEAT LAMPS ANDJan 6, 2024 · N7864B · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2024020838195Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW PASSENGER CABIN FLOOR PANEL 241AF FROM BMS4-17 TYPE 6 LOT#1534398-1; INSERTS INSTALLED USING BMS5-107 LOT#AK3BA2380A/A; CURED INSERTS USING HEAT Jan 6, 2024 · N7864B · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2024020838189Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL USING BMS 4-23 TY 2 LOT#1545419-1; RESIN BMS 5-107 LOT#AK3BA2380A/A; THERMOMETER ID:ATJan 6, 2024 · N7864B · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2024010837836Cover · missingF/A REPORTS R/H O/W EXIT EMERGENCY EXIT LIGHT COVER MISSING<[01] REPLACED MISSING LENS PER AMM 33-51-03Jan 4, 2024 · N7865A · Boeing 7377Q8 · Emergency LightingSDR SWAA2024010437684Door Frame · crackedEXTERNAL LOWER POWER DOOR CUTOUT DOOR CRACKED<[01] REMOVED DAMAGED AREA ON EXTERNAL LOWER POWER DOOR CUTOUT IAW SRM 53-10-15-2R-4;[02] ACCOMPLISHED HFEC OF CUT OUT PER NDT PART 6; 51-00-00 PROCEDURE 23. NO DEFECTS FOUND.;[03] FABRICATED AND INSTALLED REPAIR TOJan 4, 2024 · N7819A · Boeing 7377Q8 · Fuselage Main, StructureSDR SWAA2024010236099Lock · looseSEAT 11 E RECLINES -SHOULD NOT RECLINE DUE TO EXIT ROW ON 12 REQUIRES NEW HYDRLOCK SEAT SHOULD BE SECURED IN UPRIGHT POSITION AFTER INSTALLATION.<[01] OK TO CONTINUE PER MEL 25-6-02 SP1 B AUTHORIZATION # 172847;[02] REMOVED AND REPLACED SEAT 11E HYDROLOK ASSY;Dec 29, 2023 · N7851A · Boeing 7377Q8 · Passenger Compartment EquipmentSDR SWAA2024010335622Actuator · faultyAUTOPILOT WOULD NOT ENGAGE; STAB OUT OF TRIM LIGHT ILLUMINATED MOMENTARILY. PLANE NOSED OVER SLIGHTLY; AUTOPILOT CONTINUED TO DISENGAGE AND WOULD NOT REMAIN ENGAGED. FLIGHT CONTROLS WERE LESS RESPONSIVE IN ROLL THAN USUAL. AUTOPILOT IS FAULTING THE LVDT ON THEDec 27, 2023 · N7851A · Boeing 7377Q8 · Autopilot SystemSDR SWAA2023122634743Light · inoperativeSTARBOARD OVERAWING EXIT ROW LIGHT BURNT OUT.<[01] RE-LAMP L/H OVERWING EXIT ROW LIGHT REF AMM 33-51-04.Dec 21, 2023 · N7867A · Boeing 7377Q8 · Emergency LightingSDR SWAA2024010432086Floor Panel · debondedFLOOR PANEL 242AF UPPER SKIN HAS AN AREA OF DISBOND NEAR CENTER OF PANEL. (MARKED)<[01] FLOOR PANEL 242AF WITH DISBOND IN UPPER SKIN WAS REPLACED BY FABRICATING NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG NO. 144A5810 ID:0037;[02] VERIFIED CORRECTIVE ACTION ITEM 1Dec 15, 2023 · N7866A · Boeing 7377Q8 · Fuselage Floor Panel
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