Boeing 737-7CT

Service difficulty reports · 2,412

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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 = '7377CT'
  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 SWAA2025120136615Scuff Plate · crackedFWD SERVICE DOOR SCUFF PLATE IS CRACKED AT AFT LOWER CORNER. REMOVE AND REPLACED FWD SERVICE DOOR SCUFF PLATE IS CRACKED AT AFT LOWER CORNER IAW AMM 53-11-01-420-801, REJECT; FWD SERVICE DOOR FWD LOWER CORNER CUTOUT LEAK CHECK FAILED. IT HAS A HISSING SOUNNov 18, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025120132998Floorbeam · crackedDURING OK TO CLOSE, FOUND THE FLOORBEAM CRACKED AT BS 540, RBL 1 - 25. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, AND DWG 143A0060, REV B;Nov 7, 2025 · N7881A · Boeing 7377CT · Fuselage Main, Floor BeamSDR SWAA2025120130518Plate · crackedRIGHT WING T/E WIGGLE PLATE COMMON TO PANEL 651EB ON THE I/B SIDE IS CRACKED. REMOVED AND REPLACED THE RT WING T/E WIGGLE PLATE COMMON TO PANEL 651EB ON THE INBD SIDE IAW SRM 51-40-02, AND DWG 115A2781, REV B.Oct 31, 2025 · N7881A · Boeing 7377CT · Wing Main, Frame StructureSDR SWAA2025120130385Bulkhead · crackedBS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 45, WL 173. THE COMPOSITE BULKHEAD WAS REPAIRED IAW SRM 51-70-04-2R-10.Oct 30, 2025 · N7881A · Boeing 7377CT · Fuselage Main, BulkheadSDR SWAA2025120129664Rib · crackedRIGHT HORIZONTAL STABILIZER NR 6 INSPAR RIB AT STABILIZER STATION 138.70; 3RD VERTICAL STIFFENER IS CRACKED. PERFORMED REPAIR AT HORIZONTAL STABILIZER NO 6 INSPAR RIB STABILIZER STATION 138.70 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4, REPAIR 4.Oct 28, 2025 · N7881A · Boeing 7377CT · Horizontal Stabilizer, Spar/RibSDR SWAA2025120129201Frame · crackedCRACKED FRAME BS 312 LBL 33 WL 282 ABOVE FWD ENTRY DOOR UPPER SILL WEB. REPAIRED IAW SRM 22-153-01244.Oct 27, 2025 · N7881A · Boeing 7377CT · Fuselage Main, FrameSDR SWAA2025120129202Stringer · crackedCRACKED STRINGER 7L, BS 296, LBL 41, WL 274. THE DAMAGE WAS REPAIRED IAW SRM 53-00-03-2R-1, REPAIR 1, AND EA 25-153-02976 WITH AN INSPECTION PROGRAM DEFINED IN 25-153-02976-INSP. HFEC INSPECTED AREA IAW NDTM PART 6, 51-00-00, PROCEDURE 23. CRACK NOTED. NO Oct 27, 2025 · N7881A · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2025120128469Girt Bar · looseAFT ENTRY DOOR SLIDE GIRT BAR BRACKET LOOSE. REMOVED AND REPLACED FASTENER AFT ENTRY DOOR SLIDE GIRT BAR BRACKET IAW SRM 51-40-02-0G-0.Oct 25, 2025 · N7881A · Boeing 7377CT · Emergency EquipmentSDR SWAA2025120128621Skin · crackedRIGHT WING NR 8 SLAT NOSE SKIN AT ACTUATOR RIB HAS POSSIBLE CRACK. CLEANED RIGHT WING NR 8 SLAT NOSE SKIN AT ACTUATOR IAW SOPM 20-30-03. REPAIRED SLAT IAW SRM 57-42-01-2R-8, REPAIR 8, ALTERNATIVE 1, FIG 202.Oct 25, 2025 · N7881A · Boeing 7377CT · Leading Edge DevicesSDR SWAA2025120128055Floor Panel · delaminatedFWD FLOOR PANEL 221EF UPPER SURFACE DELAMINATED. THE FWD FLOOR PANEL 221EF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9.A.1,Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025120127810Floor Panel · pulledAFT FLOOR PANEL 242RF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025120128041Floor Support · corrodedCORRODED FLOOR SUPPORT, BS 304, LBL 11, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 141A5600, REV N.Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025120128224Floorbeam · corrodedCORRODED FLOORBEAM, BS 986, LBL 38-45, WL 208. REMOVED AND REPLACED THE FILLER IAW EXISTING REPAIR SRM 53-70-51-2R-6, ALT 4.Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Main, Floor BeamSDR SWAA2025120128225Floorbeam · corrodedCORRODED FLOORBEAM, BS 986, RBL 38-45, WL 208. INSTALLED A REPAIR IAW SRM 53-70-51-2R-6, ALTERNATIVE 3, FIG 204, SHEET 1.Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Main, Floor BeamSDR SWAA2025120128049Floor Support · crackedCRACKED INTERCOSTAL, BS 315, RBL 30, WL 208. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, AND DWG 141A5400, REV -.Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025120127802Floor Panel · pulledAFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241UF WITH UPPER SKIN AREAS OF PULLED STRANDS, REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025120127808Floor Panel · pulledAFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241ADF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025120127809Floor Panel · pulledAFT FLOOR PANEL 241AEF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241AEF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025120127814Floor Panel · pulledAFT FLOOR PANEL 242UF FWD O/B CORNER IS CRACKED. AFT FLOOR PANEL 242UF WITH FWD O/B CORNER CRACKED WAS REPAIRED PER SRM 53-00-50-2R-1.Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025120127815Floor Panel · pulledAFT FLOOR PANEL 242WF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF DAMAGE. REPLACED AFT FLOOR PANEL 242WF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-26 ITEM 195.Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025120127816Floor Panel · damagedFLOOR PANEL 242XF IS SOFT IN THE MIDDLE OF PANEL.<[01] FLOOR PANEL 242XF WITH SOFT AREA IN THE MIDDLE OF PANEL WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1.Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025120127302Former · crackedWING TO BODY FAIRING FORMER CRACKED, BS 500D BETWEEN S19 & 20L. REMOVED AND REPLACED THE WING TO BODY FAIRING SUPPORT IAW SRM 51-40-02, AND DWG 116A3010, REV-.Oct 23, 2025 · N7881A · Boeing 7377CT · Aerodynamic FairingsSDR SWAA2025120127305Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS 727D+6, RBL 11.5, WL 156. EVALUATED CORROSION OF FLOOR STRAP. FOUND TO BE OUT OF LIMITS, RECEIVED NEW STRAP AND APPLIED WHITE ENAMEL ALL IAW SRM 51-10-02, AMM 51-21-73-370-804, AND ACO 5360Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025120127295Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS 767+3 - 794, RBL 22, WL 156. FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN IN THE SRM. REMOVED, REPLACED, AND INSTALLED A NEW SHIELD IAW SRM 51-10-02, SRM 51-40-05-0G-0, SOct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025120127291Support Plate · corrodedCORROSION AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES, BS 727B - 767, LBL 22, WL 156. CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT OF LIMITS. REMOVED, REPLACED, AND INSTALLED A NOct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025120127290Sidewall Support · corrodedCORROSION AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES, BS 727B - 767, RBL 22, WL 156. CORROSION ON AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT OF LIMITS. REMOVED, REPLACED, AND INSTALLED Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025120126957Attach Angle · crackedBS 663, LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT LBL 45, WL 165. REMOVED, REPLACED, AND INSTALLED A NEW ATTACH ANGLE IAW SRM 51-40-02-0G-0, AND DWG 111A1000, REV A.Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Main, Attach FittingsSDR SWAA2025120127299Web · corrodedCORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS 794 - 847, RBL 26, WL 156. REMOVED AND REPLACED THE THRESHOLD WEB IAW SRM 51-40-02, AND DWG:146A8340 REV-.Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025120127296Scuff Plate · crackedFORWARD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. WELDED THE CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, STEP 4.B.(4).Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025120127297Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. WELDED THE CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, STEP 4.B.(4).Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025120126946Doubler · crackedEGPR SURROUND DOUBLER CRACKED BS 233, WL 175+8, ABOVE S24R. TRIMMED DAMAGED AREA; FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-15-2R-4, REPAIR 4, PARG 4 (B-M).Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Main, Plate/SkinSDR SWAA2025120127298Attach Angle · corrodedCORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS 767 TO 787, RBL 21, WL 156. CORROSION ON AFT CARGO BAY ATTACH ANGLE UNDER SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. REMOVED, REPLACED, ANDOct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Main, Attach FittingsSDR SWAA2025120126776Switch · brokenAFT ATTENDANCE PANEL EMERGENCY LIGHT SWITCH IS BROKEN. REMOVED AND REPLACED AFT ATTENDANT PANEL EMERGENCY LIGHT SWITCH COVER IAW SWPM 20-84-14..Oct 21, 2025 · N7881A · Boeing 7377CT · Emergency LightingSDR SWAA2025120126766Panel · delaminatedPANEL 194CL DELAMINATED ON OUTER SURFACE. PANEL 194CL REPAIRED IAW SRM 51-70-05-2R-2.Oct 21, 2025 · N7881A · Boeing 7377CT · Aerodynamic FairingsSDR SWAA2025100319191Fuel Sys · leakingSUSPECTED FUEL LEAK FROM NO.1 ENGINE SIDE. NEEDED TO CROSSFEED TWICE DUE TO 400 LB. IMBALANCE. NOTED FUEL FLOW NR 1 SIDE HIGHER THAN NR 2 SIDE BY AS MUCH AS 200 LBS PER HOUR AT CRUISE. POSSIBLE FLUID ON FLAP ON NR 1 SIDE. FUEL BURN STL-BWI 400 LBS GREATER BETWSep 29, 2025 · N7825A · Boeing 7377CT · Fuel StorageSDR SWAA2025092918272Lamp · inoperativeEMERGENCY EXIT LIGHT ON AFT LAV HAS AN INOPERATIVE SEGMENT. REPLACED THE LAMPS EMERGENCY EXIT LIGHT ON AFT LAV AND PERFORMED GOOD TEST IAW AMM 33-51-01-960-801.Sep 26, 2025 · N7831B · Boeing 7377CT · Emergency LightingSDR SWAA2025092917862Light · inoperativeLEFT SLIDE/OVERWING LIGHT (LOWER) LIGHT IS INOPERATIVE. REMOVED AND REPLACED AND PERFORMED GOOD TEST OF LEFT SLIDE/OVERWING LIGHT (LOWER) IAW AMM 33-51-04-960-801.Sep 24, 2025 · N7831B · Boeing 7377CT · Emergency LightingSDR SWAA2025092918136Oil System · low#2 ENG. OIL SERVICED TO FULL IN BNA. DROPPED BELOW 50% DURING FIRST HOUR OF FLIGHT; THEN TO 0% & OIL PRESSURE WENT TO 0 PSI DURING DECENT INTO ORF. MANUALLY SHUT DOWN #2 ENGINE.REMOVED AND REPLACED #2 ENGINE ASSEMBLY AS PER MT 771-00-01; REFERENCE WO #10734405Sep 24, 2025 · N7821L · Boeing 7377CT · Turbine Engine Oil SystemSDR SWAA2025092417721Bypass Switch · faultedNR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. DID NOT EXTINGUISH WITH THRUST LEVER RETARDED TO CLOSED. INSPECTED NR 2 ENG OIL FILTER & FOUND NO PRESCENCE OF CONTAMINANTS; R & R OIL FILTER IAW AMM 79-21-06. LEAK CHECKED GOOD. OK TO CONTINUE PER Sep 23, 2025 · N7821L · Boeing 7377CT · Engine Oil System (Airframe Furnished)SDR SWAA2025092417735Filter · contaminatedNUMBER 2 ENG OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. DID NOT EXTINGUISH WITH THRUST LEVER RETARDED TO CLOSED. INSPECTED NR 2 ENG OIL FILTER & FOUND NO PRESCENCE OF CONTAMINANTS. R & R OIL FILTER IAW AMM 79-21-06. LEAK CHECKED GOOD.Sep 23, 2025 · N7821L · Boeing 7377CT · Turbine Engine Oil SystemSDR SWAA2025092916642Lens · brokenSIDEWALL PANEL 231YHW EMERGENCY EXIT LIGHT LENS ASSY IS BROKEN. REMOVED AND REPLACED AND PERFORMED GOOD TEST OF SIDEWALL PANEL 231YHW EMERGENCY EXIT LIGHT LENS ASSY IAW AMM 33-51-01-960-802.Sep 20, 2025 · N7831B · Boeing 7377CT · Emergency LightingSDR SWAA2025092912193Panel · delaminatedPANEL 194CR HAS AREA OF DELAMINATION ON OUTER SURFACE. PANEL 194CR WAS REPAIRED IAW SRM 51-70-05-2R-2.Sep 6, 2025 · N7831B · Boeing 7377CT · Aerodynamic FairingsSDR SWAA2025092912110Attach Angle · crackedRIGHT WING T/E FIXED PANEL MID ATTACH ANGLE CRACKED. R & R RT WING T/E FIXED PANEL MID ATTACH ANGLE IAW SRM 51-40-02, AIPC 57-50-00-25, AND AMM 20-50-11-910-801.Sep 6, 2025 · N7831B · Boeing 7377CT · Wing, Attach FittingsSDR SWAA2025092912108Attach Fitting · crackedRIGHT WING T/E FIXED PANEL SUPPORT BEAM, ATTACHMENT FITTING CRACKED, JUST INBD OF DEFLECTION CONTROL RIB. R & R ATTACH FITTING IAW 51-4002-0G-0.Sep 6, 2025 · N7831B · Boeing 7377CT · Wing, Attach FittingsSDR SWAA2025092911482Handle · looseFWD ENTRY DOOR AFT CUTOUT LINER ASSIST HANDLE IS LOOSE. SECURED FWD ENTRY DOOR AFT CUTOUT LINER ASSIST HANDLE PER AMM 25-21-31-420-802 STEP 3. B. (6).Sep 5, 2025 · N7831B · Boeing 7377CT · Passenger/Crew DoorsSDR SWAA2025092911866Pressure Deck · crackedCRACK NOTED ON RH HORIZONTAL PRESSURE DECK WEB BS 663+1.5 WL 202.5; RBL 40.5; L: 0.3'. REMOVED DAMAGE BS 663- BS674 RBL 38- RBL60; FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS ON BS663-BS674 RBL30-RBL60 WL 203 I.A.W SRM 53-40-51-2R-2 REPAIR 2.Sep 5, 2025 · N7831B · Boeing 7377CT · Fuselage Main, StructureSDR SWAA2025100212739Fairing · temp repairPREVIOUS TEMP REPAIR NOTED ON FAIRING 193CR. TEMP REPAIR REMOVED AND REPLACED WITH A PERMANENT REPAIR IAW SRM 51-70-05-2R-2.Sep 4, 2025 · N7831B · Boeing 7377CT · Aerodynamic FairingsSDR SWAA2025080697686Handle · brokenFWD SERVICE DOOR BULKHEAD ASSISST HANDLE BROKEN. TIGHTENED ASSISST HANDLE PER CMM 25-21-71.Aug 2, 2025 · N569WN · Boeing 7377CT · Service DoorsSDR SWAA2025072895258Slide · out of positionAFT ENTRY DOOR SLIDE PARTIALLY PULLED OUT<[01] REPOSITIONED AFT ENTRY DOOR SLIDE PER AMM 25-66-01 AND MT 725-61-06 WITH NO DEFECTS NOTED. AC OK FOR SERVICEJul 24, 2025 · N569WN · Boeing 7377CT · Escape SlideSDR SWAA2025062383727Cabin Air Sys · odorFORWARD FLIGHT ATTENDANTS REPORTED A EXHAUST SMELL ON A CLIMBOUT. NO ABNORMAL SMELLS OR INDICATION ON THE COCKPIT OR AFT SECTION OF THE AIRPLANE <[01]. C/W CONDITIONAL INSPECTION PER MM 05-51-56. R&R BOTH PACKS COALESCER BAGS PER MM 21-51-05. R&R RECIRCULATJun 19, 2025 · N7828A · Boeing 7377CT · Air Distribution System
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