N902WN

Service difficulty reports · 252

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 = 'N902WN' 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 SWAA2026060809642Cartridge · crackedLEFT WING OTBD AFT FLAP INBD PROGRAM ROLLER CARTRIDGE ASSY; HAS A HFEC CRACK INDICATION ON THE LOWER AFT SURFACE. R & R LT WING OTBD FLAP IAW AMM 27-51-21, INSPECTED IAW AMM 27-51-22-601-NG.Jun 6, 2026 · N902WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2025102325987Megaphone · damagedFWD MEGA PHONE HANDLE RETAINING SCREW HOLE STRIPPED OUT.<[01] REMOVED AND REPLACED FWD MEGA PHONE PER MT 725-340-00-01Oct 20, 2025 · N902WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2025081400262Lens · damagedAFT LAV B EMERGENCY EXIT LIGHT LENS DAMAGED. REPLACED EMERGENY EXIT LIGHT LENS PER AMM 33-51-01-960-801.Aug 10, 2025 · N902WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025081892565Support Bracket · crackedCRACKED LOWER O/B PULLEY BRACKET SUPPORT BS 692 LBL 25 WL 203. REMOVED. FABRICATED, AND INSTALLED LOWER O/B PULLEY BRACKET SUPPORT BS 692 LBL 25 WL 203 IAW SRM 51-40-02-0G-0; 51-10-02-0G-0 AND BOEING DWG 273A9110 REV:A; 273A9112 REV H.Jul 17, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025081592307Stringer · corrodedCORROSION ON STRINGER; S-28L END SPLICE IN BILGE AREA AFT OF E/E COMPARTMENT DOOR CUTOUT BS350+8 LBL10 WL140.<[01] REMOVED 2 FASTENERS ON REPORTED CORROSION AREA CLEAN AREA; REMOVED PROTECTIVE TREATMENT AND NOT CORROSION FOUND;[02] CORRECTION ITEM 1: REMOVED 2Jul 17, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2025081592012Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727C S-6L. REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727C S-6L IAW SRM 51-40-02-0G-0 AND DWG 146A1103 SHEET 11 REV - .Jul 16, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2025081592013Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727E S-6L. REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727E S-6L IAW SRM 51-40-02-0G-0 AND DWG 146A1112 SHEET 1 REV C.Jul 16, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2025081592014Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727D S-6R. REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727D S-6R IAW SRM 51-40-02-0G-0 AND DWG 146A1111 SHEET 11 REV -.Jul 16, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2025081592017Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727E S-7R. REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727E S-7R IAW SRM 51-40-02-0G-0 AND DWG 146A1112 SHEET 1 REV C .Jul 16, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2025081592015Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS 727C S-5R. REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727C S-5R IAW SRM 51-40-02-0G-0 AND DWG 146A1103 SHEET 11 REV - .Jul 16, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2025081592016Stringer Clip · crackedCRACKED STRINGER CLIP AT PAX CABIN BS 727B S5R. REMOVED AND REPLACED STR CLIP AT PAX CABIN BS 727B S5R IAW SRM 51-40-02-0G-0 AND DWG 146A1102 SHEET 15 REV -.Jul 16, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2025081591783Stub Frame · crackedCRACK FOUND ON R1 STUB FRAME AT BS 291.5+7.5; .15' ABOVE SEAL DEPRESSOR; .6' LENGTH (MARKED)<[01] TASK CARD COMPLETED; SUMMARY STATEMENT; NO ALLOWABLE LIMITS FOUND ON SRM THEREFORE PART TO BE REMOVE AND REPLACE I.A.W SRM 51-10-02-0G-0 PAR.9.C REMOVED FSD UPPERJul 15, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2025081591789Angle · crackedCRACKED ANGLE BS 294.5 RBL 60 WL 208 COMMON TO I/B CHORD UPPER SIDE OF CREASE BEAM WEB.<[01] REMOVED AND REPLACED ANGLE AT BS 294.5 RBL 60; WL 208 COMMON TO I/B CHORD UPPER SIDE OF CREASE BEAM WEB IAW SRM 51-40-02-0G-0 AND DWG 141A8310 ; REV:D;[02] VERIFIED COJul 15, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025081591782Bear Strap · crackedCRACK FOUND ON R1 BEAR STRAP AT BS 291.5+4; WL 265.6; .6' IN LENGTH (MARKED)<[01] REPAIRED BY 737 SRM 53-10-01-2R-6 AND EA M-25-153-01539 CCN TTG8Q013R942;[02] ALL STEPS COMPLETED.;[03] ALL STEPS COMPLETED.Jul 15, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2025081491414Sidewall Support · corrodedCORROSION AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B+10 TO 787+14, LBL 22, WL 156. CORROSION ON AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT, FOUND TO BE OUT OF LIMITS. REMOVED, REPLACED AND INSTALLED A NEW AFJul 15, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025081491415Sidewall Support · corrodedCORROSION AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B+10 TO 767, RBL 22, WL 156. CORROSION ON AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT. FOUND TO BE OUT OF LIMITS. REMOVED, REPLACED, AND INSTALLED A NEWJul 15, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025081491416Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS 767+3 TO 794, RBL 22, WL 156. CORROSION ON AFT CARGO BAY FWD SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. REMOVED, REPLACED, AND INSTALLED A NEW AJul 15, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025081491417Cargo Track · crackedAFT CARGO BAY CARGO TRACK IS CRACKED, BS 727E AND 747, RBL 13, WL 156. CRACK FOUND TO BE OUT OF LIMITS. REMOVED, AND REPLACED CARGO TRACK IAW EA 25-153-01951, AND 53-00-53-2R-3.Jul 15, 2025 · N902WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025081491418Splice Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE, BS 727D+5, LBL 3 - RBL 12, WL 156. RECEIVED A NEW STRAP, APPLIED WHITE ENAMEL IAW ACO 5360-E-16462, AND NEW STRAP WILL BE INSTALLED ON CUSTOMER CARD TTG8Q0132YHR.Jul 15, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025081591408Floorbeam · crackedCRACKED BREAKER PANEL AT BS 540 RBL 0 - RBL 25 WL 208. REPLACED NEW BREAKER PANEL AT BS 540 RBL 0 - RBL 25 WL 208 IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND BOEING DWG 143A0060 REV:-.Jul 14, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2025081591409Floorbeam · crackedCRACKED BREAKER PANEL AT BS 540 LBL 0 - LBL 25 WL 208. REPLACED NEW BREAKER PANEL AT BS 540 LBL 0 - LBL 25 WL 208 IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND BOEING DWG 143A0060 REV:-.Jul 14, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2025081591412Stiffener · crackedRIGHT HORIZONTAL STAB INSPAR AT RIB NR 1, HSS 92.70. FOUND STIFFENER NR 1 CRACKED AT LOWER END. REPAIRED RT HORIZONTAL STAB INSPAR AT RIB NR 1 VERTICAL STIFFENER NR 1 IAW SRM 55-10-09-2R-4.Jul 14, 2025 · N902WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2025081591413Stiffener · crackedRIGHT HORIZONTAL STAB INSPAR AT RIB NR 4, HSS 120.30, FOUND STIFFENER NR 4 CRACKED AT LOWER END. REPAIRED RT HORIZONTAL STAB INSPAR RIB NR 4, STIFFENER NR 4 IAW SRM 55-10-09-2R-4.Jul 14, 2025 · N902WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2025081591411Rib · crackedLEFT HORIZONTAL STAB INSPAR AT RIB NR 4, HSS 120.30, FOUND STIFFENER NR 3 CRACKED AT LOWER END. REPAIRED LT HORIZONTAL STAB INSPAR RIB NR 4 AT STIFFENER NR 3 IAW SRM 55-10-09-2R-4.Jul 14, 2025 · N902WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2025081590854Angle · crackedCRACKED ANGLE AT BS 380 - 400, LBL 11, WL 208. REMOVED, REPLACED, AND INSTALLED A NEW ANGLE IAW SRM 51-40-02 AND DWG 143A5400, SH 105, REV-.Jul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025081590952Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 328 RBL 25 WL 208<[01] NO ALLOWABLE DAMAGE PERMITTED UNDER SEAT TRACK ATTACHMENT PER SRM 737-700 SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1 PAR.1.B(2) ON BS328 FLOOR BEAM; THEREFORE DAMAGE TO BE REPAIRED PER SRM 53-10-51-2R-7 REPAIR 7 ALJul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2025081591054Floorbeam · corrodedCORROSION ON FASTENER HOLE ON FLOORBEAM AT BS 986 LBL 44 WL 208. EVALUATED CORROSION ON FASTENER HOLE ON FLOOR BEAM AT BS 986 LBL 44 WL 208. BLEND WAS .3'X.3'X.049'. DEPTH GAUGE ID ATS3189 DUE 12/2025. BLEND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1 PAJul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2025081590956Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK ON TOP/CROWN AND IN WELL AT BS 480 - 520 LBL 25 WL 208. SEAT TRACK TO BE REPLACED ON TTG8Q013Q2ZW.Jul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025081590963Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK ON TOP/CROWN AND IN WELL AT BS 480 - 520 LBL 45 WL 208. SEAT TRACK WILL BE REPLACED ON TTG8Q013Q302.Jul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025081590964Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK ON TOP/CROWN AND IN WELL AT BS 540 - 727B LBL 25 WL 208. AREA BLENDED IS L=5'' BY W=.5'' BY D=.024''. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1. REMOVED SEAT TRACK BS 540-727B LBL 25 WL 208 IAW SRM 51-40-02-0G-Jul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025081590960Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK ON TOP/CROWN AND IN WELL AT BS 540 - 727B LBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK SECTION BS 540 - 727B LBL 45 DUE TO FOUND OUT LIMITS AT BS 706 LBL 45 WL 208 AREA BLENDED IS L=5'' BY W=.5'' BY D=.025'' IAW SRM 5Jul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025081590974Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK ON TOP/CROWN AND IN WELL AT BS 540 - 727B RBL 25 WL 208. REMOVED CORROSION ON TOP OF PAX CABIN SEAT TRACK AT BS 540-0727B RBL 25 WL 208. IAW SRM 51-10-02-0G-0. AREA BLENDED IS L=5'' BY W=1'' BY D=.009''.IN LIMITS PER SJul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025081491050Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT BS 951, RBL 35, WL 208. EVALUATED CORROSION ON FLOOR SUPPORT AT BS 951 RBL 35 WL 208. BLEND WAS 4'X.6'X.008'. FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM. REMOVED FLOOR SUPPORT AT BS 951 RBL 35 WL 208 IAW SRM 51-40-02. LJul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025081491053Floor Panel · delaminatedCABIN FLOOR PANEL 232RF DELAMINATED. REPLACEMENT FLOOR PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0 ALONG WITH DWG 144A5810 SHEET 124.Jul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025081590853Angle · crackedCRACKED ANGLE AT BS 380 - 400 RBL 11 WL 208<[01] REMOVED; REPLACED; AND INSTALLED A NEW ANGLE AT BS 380-400; RBL11; WL 208 IAW SRM 51-40-02 AND BOEING DWG 143A5400 SH 105 REV:-;[02] STEP 1 COMPLETED.Jul 12, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025081590605Shear Web · corrodedCORROSION ON L/H SHEAR WEB AT BS 1026 LBL 22 WL 208<[01] SHEAR WEB FOUND TO BE OUT LIMITS; PART REMOVED AND REPLACED SHEAR WEB AT BS 1016 TO BS 1033 LBL0 TO LBL39 WL 208 PER I.A.W SRM 51-10-02-0G-0 PAR 9.C; SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 REV:BJul 11, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025081590606Strap · corrodedCORROSION ON STRAP AT BS 1016 LBL 3 WL 208<[01] STRAP FOUND TO BE OUT LIMITS; PART REMOVED AND REPLACED AT BS 1016 TO BS 1029 LBL3 TO LBL39 WL 208 PER I.A.W SRM 51-10-02-0G-0 PAR 9.C; SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 REV:B.Jul 11, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025081590609Shear Web · corrodedCORROSION ON STRAP ON R/H SHEAR WEB AT BS 1028.5 RBL 18 WL 208. STRAP FOUND TO BE OUT LIMITS; PART REMOVED AND REPLACED BS 1016-BS1029 RBL18 WL 208 PER I.A.W SRM 51-10-02-0G-0 PAR 9.C; SRM 51-40-02-0G-0 AND BOEING DWG 147A5730 REV:C.Jul 11, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025081590612Floorbeam · corrodedCORROSION AROUND NUT PLATE HOLE FASTENER AT BS 986 RBL 43 WL 208. EVALUATED CORROSION AROUND NUT PLATE HOLE FASTENER AT BS 986 RBL 43 WL 208. BLEND WAS 1'X.3'X.040'. BLEND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1 PARAGRAPH 4. H. (2) (B) FIGURE 103 DEJul 11, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2025081490433Floor Panel · delaminatedCABIN FLOOR PANEL 241XF DELAMINATED. CABIN FLOOR PANEL 241XF WITH DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.Jul 11, 2025 · N902WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025081490434Floor Panel · delaminatedCABIN FLOOR PANEL 241ZF DELAMINATED. CABIN FLOOR PANEL 241ZF DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.Jul 11, 2025 · N902WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025081490608Support Fitting · corrodedCORROSION ON AFT LAV MOUNT SUPPORT FITTING ON STRUCTURE AT BS 1021, LBL 1, WL 208. REMOVED AFT LAV MOUNT SUPPORT FITTING ON STRUCTURE AT BS 1021 LBL 1 WL 208 IAW SRM 51-40-02-0G-0.;[02] REMOVED AND REPLACED AFT LAV MOUNT SUPPORT FITTING AT BS 1021 LBL 1 WL 2Jul 11, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025081590303Scuff Plate · crackedAED (L2) SCUFF PLATE REQUIRES REPLACEMENT<[01] UPDATED TABLE MEASUREMENT;[02] REPLACED DAMAGE SCUFF PLATE DUE TO NO LIMITS FOUND ALL I.A.W SRM 51-10-02-0G-0 PAR 9.C AND AIPC 53-13-00-13; SCUFF PLATE TO BE INSTALLED ON CCN TTG8Q0029YBF STEP 18;[03] ADDED PART IJul 10, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025081489866Light · damagedG-4 EXIT LIGHT IS DAMAGED. REMOVED AND REPLACED G-4 EXIT LIGHT PER AMM 33-51-01-960-802. OPS CHECK TEST GOOD.Jul 10, 2025 · N902WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025081589592Door · crackedLEFT MAIN GEAR CENTER DOOR IS CRACKED, JUST FWD OF FWD HINGE ATTACH POINT. REMOVED AND REINSTALLED LT MLG CENTER DOOR IAW AMM 32-13-11.Jul 9, 2025 · N902WN · Boeing 7377H4 · Landing Gear DoorsSDR SWAA2025081489273Lens · brokenLAV A EXIT LENS IS BROKEN. REMOVED AND REPLACED LAV A EXIT LENS PER AMM 33-51-01-960-802. OPS CHECK TEST GOOD.Jul 8, 2025 · N902WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024110155088Battery Pack · no testPASSENGER CABIN; FWD EMERGENCY EXIT LT BATTERY PACK M1674 FAILED CAPACITY TEST/CHECK.<[01] R&R PASSENGER CABIN FWD EMERGENCY EXIT LT BATTERY PACK M1674 IAW AMM 33-51-06.Oct 31, 2024 · N902WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024110155089Battery Pack · no testPASSENGER CABIN; FWD EMERGENCY EXIT LT BATTERY PACK M1675 FAILED CAPACITY TEST/CHECK.<[01] R&R PASSENGER CABIN; FWD EMERGENCY EXIT LT BATTERY PACK M1675 IAW AMM 33-51-06.;[02] R&R PASSENGER CABIN; FWD EMERGENCY EXIT LT BATTERY PACK M1675 IAW AMM 33-51-06.Oct 31, 2024 · N902WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024102149323Battery · no testFA REPORTS AFT GAL FLASH LIGHT NOT TESTING<[01] OK TO CONTINUE PER MEL 25-12-01 SP1B AUTHORIZATION# 219007;[02] REMOVED AND REPLACED AFT GALLEY EMERGENCY FLASHLIGHT BATTERY IAW CMM 25-60-02.Oct 16, 2024 · N902WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2024101446436Light · inoperativeEMERGENCY EXIT LT AT 13DEF INOP.<[01] RELAMPED EMERGENCY EXIT LIGHT AT 13DEF IAW AMM 31-51-03.Oct 8, 2024 · N902WN · Boeing 7377H4 · Emergency Lighting
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