# Service difficulty reports: N902WN A list on [N902WN](https://openairdocs.org/aircraft/N902WN.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 6 · 252 reports - [SDR SWAA2026060809642](https://openairdocs.org/sdr/SWAA2026060809642.md): Cartridge · cracked · Jun 6, 2026 · N902WN · Boeing 7377H4 · Trailing Edge Flaps > LEFT 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. - [SDR SWAA2025102325987](https://openairdocs.org/sdr/SWAA2025102325987.md): Megaphone · damaged · Oct 20, 2025 · N902WN · Boeing 7377H4 · Emergency Equipment > FWD MEGA PHONE HANDLE RETAINING SCREW HOLE STRIPPED OUT.<[01] REMOVED AND REPLACED FWD MEGA PHONE PER MT 725-340-00-01 - [SDR SWAA2025081400262](https://openairdocs.org/sdr/SWAA2025081400262.md): Lens · damaged · Aug 10, 2025 · N902WN · Boeing 7377H4 · Emergency Lighting > AFT LAV B EMERGENCY EXIT LIGHT LENS DAMAGED. REPLACED EMERGENY EXIT LIGHT LENS PER AMM 33-51-01-960-801. - [SDR SWAA2025081892565](https://openairdocs.org/sdr/SWAA2025081892565.md): Support Bracket · cracked · Jul 17, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED 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. - [SDR SWAA2025081592307](https://openairdocs.org/sdr/SWAA2025081592307.md): Stringer · corroded · Jul 17, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CORROSION 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 2 - [SDR SWAA2025081592012](https://openairdocs.org/sdr/SWAA2025081592012.md): Stringer Clip · cracked · Jul 16, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED 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 -. - [SDR SWAA2025081592013](https://openairdocs.org/sdr/SWAA2025081592013.md): Stringer Clip · cracked · Jul 16, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED 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. - [SDR SWAA2025081592014](https://openairdocs.org/sdr/SWAA2025081592014.md): Stringer Clip · cracked · Jul 16, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED 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 -. - [SDR SWAA2025081592017](https://openairdocs.org/sdr/SWAA2025081592017.md): Stringer Clip · cracked · Jul 16, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED 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. - [SDR SWAA2025081592015](https://openairdocs.org/sdr/SWAA2025081592015.md): Stringer Clip · cracked · Jul 16, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED 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 -. - [SDR SWAA2025081592016](https://openairdocs.org/sdr/SWAA2025081592016.md): Stringer Clip · cracked · Jul 16, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED 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 -. - [SDR SWAA2025081591783](https://openairdocs.org/sdr/SWAA2025081591783.md): Stub Frame · cracked · Jul 15, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Frame > CRACK 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 UPPER - [SDR SWAA2025081591789](https://openairdocs.org/sdr/SWAA2025081591789.md): Angle · cracked · Jul 15, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED 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 CO - [SDR SWAA2025081591782](https://openairdocs.org/sdr/SWAA2025081591782.md): Bear Strap · cracked · Jul 15, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Plate/Skin > CRACK 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. - [SDR SWAA2025081491414](https://openairdocs.org/sdr/SWAA2025081491414.md): Sidewall Support · corroded · Jul 15, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION 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 AF - [SDR SWAA2025081491415](https://openairdocs.org/sdr/SWAA2025081491415.md): Sidewall Support · corroded · Jul 15, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION 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 NEW - [SDR SWAA2025081491416](https://openairdocs.org/sdr/SWAA2025081491416.md): Shield · corroded · Jul 15, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION 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 A - [SDR SWAA2025081491417](https://openairdocs.org/sdr/SWAA2025081491417.md): Cargo Track · cracked · Jul 15, 2025 · N902WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > AFT 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. - [SDR SWAA2025081491418](https://openairdocs.org/sdr/SWAA2025081491418.md): Splice Strap · corroded · Jul 15, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION 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. - [SDR SWAA2025081591408](https://openairdocs.org/sdr/SWAA2025081591408.md): Floorbeam · cracked · Jul 14, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CRACKED 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:-. - [SDR SWAA2025081591409](https://openairdocs.org/sdr/SWAA2025081591409.md): Floorbeam · cracked · Jul 14, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CRACKED 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:-. - [SDR SWAA2025081591412](https://openairdocs.org/sdr/SWAA2025081591412.md): Stiffener · cracked · Jul 14, 2025 · N902WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > RIGHT 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. - [SDR SWAA2025081591413](https://openairdocs.org/sdr/SWAA2025081591413.md): Stiffener · cracked · Jul 14, 2025 · N902WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > RIGHT 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. - [SDR SWAA2025081591411](https://openairdocs.org/sdr/SWAA2025081591411.md): Rib · cracked · Jul 14, 2025 · N902WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > LEFT 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. - [SDR SWAA2025081590854](https://openairdocs.org/sdr/SWAA2025081590854.md): Angle · cracked · Jul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED 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-. - [SDR SWAA2025081590952](https://openairdocs.org/sdr/SWAA2025081590952.md): Floorbeam · corroded · Jul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CORROSION 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 AL - [SDR SWAA2025081591054](https://openairdocs.org/sdr/SWAA2025081591054.md): Floorbeam · corroded · Jul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CORROSION 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 PA - [SDR SWAA2025081590956](https://openairdocs.org/sdr/SWAA2025081590956.md): Seat Track · corroded · Jul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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. - [SDR SWAA2025081590963](https://openairdocs.org/sdr/SWAA2025081590963.md): Seat Track · corroded · Jul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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. - [SDR SWAA2025081590964](https://openairdocs.org/sdr/SWAA2025081590964.md): Seat Track · corroded · Jul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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- - [SDR SWAA2025081590960](https://openairdocs.org/sdr/SWAA2025081590960.md): Seat Track · corroded · Jul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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 5 - [SDR SWAA2025081590974](https://openairdocs.org/sdr/SWAA2025081590974.md): Seat Track · corroded · Jul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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 S - [SDR SWAA2025081491050](https://openairdocs.org/sdr/SWAA2025081491050.md): Floor Support · corroded · Jul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION 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. L - [SDR SWAA2025081491053](https://openairdocs.org/sdr/SWAA2025081491053.md): Floor Panel · delaminated · Jul 13, 2025 · N902WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 232RF DELAMINATED. REPLACEMENT FLOOR PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0 ALONG WITH DWG 144A5810 SHEET 124. - [SDR SWAA2025081590853](https://openairdocs.org/sdr/SWAA2025081590853.md): Angle · cracked · Jul 12, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED 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. - [SDR SWAA2025081590605](https://openairdocs.org/sdr/SWAA2025081590605.md): Shear Web · corroded · Jul 11, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION 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:B - [SDR SWAA2025081590606](https://openairdocs.org/sdr/SWAA2025081590606.md): Strap · corroded · Jul 11, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION 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. - [SDR SWAA2025081590609](https://openairdocs.org/sdr/SWAA2025081590609.md): Shear Web · corroded · Jul 11, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION 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. - [SDR SWAA2025081590612](https://openairdocs.org/sdr/SWAA2025081590612.md): Floorbeam · corroded · Jul 11, 2025 · N902WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CORROSION 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 DE - [SDR SWAA2025081490433](https://openairdocs.org/sdr/SWAA2025081490433.md): Floor Panel · delaminated · Jul 11, 2025 · N902WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 241XF DELAMINATED. CABIN FLOOR PANEL 241XF WITH DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1. - [SDR SWAA2025081490434](https://openairdocs.org/sdr/SWAA2025081490434.md): Floor Panel · delaminated · Jul 11, 2025 · N902WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 241ZF DELAMINATED. CABIN FLOOR PANEL 241ZF DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1. - [SDR SWAA2025081490608](https://openairdocs.org/sdr/SWAA2025081490608.md): Support Fitting · corroded · Jul 11, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION 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 2 - [SDR SWAA2025081590303](https://openairdocs.org/sdr/SWAA2025081590303.md): Scuff Plate · cracked · Jul 10, 2025 · N902WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > AED (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 I - [SDR SWAA2025081489866](https://openairdocs.org/sdr/SWAA2025081489866.md): Light · damaged · Jul 10, 2025 · N902WN · Boeing 7377H4 · Emergency Lighting > G-4 EXIT LIGHT IS DAMAGED. REMOVED AND REPLACED G-4 EXIT LIGHT PER AMM 33-51-01-960-802. OPS CHECK TEST GOOD. - [SDR SWAA2025081589592](https://openairdocs.org/sdr/SWAA2025081589592.md): Door · cracked · Jul 9, 2025 · N902WN · Boeing 7377H4 · Landing Gear Doors > LEFT 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. - [SDR SWAA2025081489273](https://openairdocs.org/sdr/SWAA2025081489273.md): Lens · broken · Jul 8, 2025 · N902WN · Boeing 7377H4 · Emergency Lighting > LAV A EXIT LENS IS BROKEN. REMOVED AND REPLACED LAV A EXIT LENS PER AMM 33-51-01-960-802. OPS CHECK TEST GOOD. - [SDR SWAA2024110155088](https://openairdocs.org/sdr/SWAA2024110155088.md): Battery Pack · no test · Oct 31, 2024 · N902WN · Boeing 7377H4 · Emergency Lighting > PASSENGER 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. - [SDR SWAA2024110155089](https://openairdocs.org/sdr/SWAA2024110155089.md): Battery Pack · no test · Oct 31, 2024 · N902WN · Boeing 7377H4 · Emergency Lighting > PASSENGER 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. - [SDR SWAA2024102149323](https://openairdocs.org/sdr/SWAA2024102149323.md): Battery · no test · Oct 16, 2024 · N902WN · Boeing 7377H4 · Emergency Equipment > FA 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. - [SDR SWAA2024101446436](https://openairdocs.org/sdr/SWAA2024101446436.md): Light · inoperative · Oct 8, 2024 · N902WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY EXIT LT AT 13DEF INOP.<[01] RELAMPED EMERGENCY EXIT LIGHT AT 13DEF IAW AMM 31-51-03. Next page: https://openairdocs.org/aircraft/N902WN/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 = 'N902WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N902WN/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.