# Service difficulty reports: N202WN, cancelled Oct 29, 2024 A list on [N202WN, cancelled Oct 29, 2024](https://openairdocs.org/deregistered/N202WN-2024-10-29.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 7 · 314 reports - [SDR SWAA2024072415449](https://openairdocs.org/sdr/SWAA2024072415449.md): Handle · broken · Jul 22, 2024 · N202WN · Boeing 7377H4 · Emergency Equipment > L1 DOOR ASSIST HANDLE BROKEN<[01] SWAPPED BROKEN L1 DOOR ASSIST HANDLE WITH SERVICEABLE HANDLE FROM THE FWD LAV PER AMM 52-11-31. OK TO CONTINUE PER MEL 25-10-01 SP# 1B AUTH# 205343;[02] INSTALLED FWD LAV ASSIST HANDLE PER CMM 25-42-39. - [SDR SWAA2024043080201](https://openairdocs.org/sdr/SWAA2024043080201.md): Fseu · false indication · Apr 27, 2024 · N202WN · Boeing 7377H4 · Leading Edge Slat Position Indicating System > DURING APPROACH/LANDING PROCEDURE NO LEADING-EDGE DEVICE LIGHT ILLUMINATED. LANDED WITH 15' FLAPS EMERGENCY DECLARE.<[01] FOUND MX MSG 27-81277 TASK 834. VERIFIED PINS ON CONNECTOR D728B D2; E2; H2; AND F2. NO DEFECTS NOTED. RAR FSEU PER AMM 27-51-01. OPS CHEC - [SDR SWAA2024041875951](https://openairdocs.org/sdr/SWAA2024041875951.md): Lens · out of adjust · Apr 16, 2024 · N202WN · Boeing 7377H4 · Emergency Lighting > EMER EXIT SIGN ON RIGHT OVERWING EXIT LOWER SIDE DETACHED.<[01] SECURED LENSE ON RIGHT LOWER OVER WING EXIT SIGN ASSEMBLY REF. 33-51-01 - [SDR SWAA2024031159385](https://openairdocs.org/sdr/SWAA2024031159385.md): Sign · broken · Mar 5, 2024 · N202WN · Boeing 7377H4 · Emergency Lighting > AFT ENTRY CEILING EXIT LIGHT SIGN HOUSING IS BROKEN<[01] REMOVED AND REPLACED AFT ENTRY CEILING EMERGENCY EXIT SIGN IAW AMM 33-51-01-960-802-NG. OP CHECK GOOD.;[02] VERIFIED ITEM 1
AUDIT C/W - [SDR SWAA2024031159223](https://openairdocs.org/sdr/SWAA2024031159223.md): Pressure Blkhd · cracked · Mar 4, 2024 · N202WN · Boeing 7377H4 · Fuselage Main, Bulkhead > CRACK INDICATION ON STA 1016 AFT PRESSURE BULKHEAD AT S-23R<[01] REMOVED DAMAGE FROM STA 1016 BULKHEAD WEB WL 244 RBL 0.50 S-23R AND REPAIRED IAW EA 24-153-00607;[02] C/W;[03] C/W
AUDIT C/W - [SDR SWAA2024030858477](https://openairdocs.org/sdr/SWAA2024030858477.md): Pressure Blkhd · cracked · Mar 3, 2024 · N202WN · Boeing 7377H4 · Fuselage Main, Bulkhead > FOUND CRACK INDICATION ON 1016 AFT PRESSURE BULKHEAD AT S-23R. SEE ATTACHED PICTURES. FOUND CRACK INDICATION ON 1016 AFT PRESSURE BULK HEAD AT S-23R. SEE ATTACHED PICTURES. CRACK MEASURES APPROXIMATELY.125.<[01] REPAIRED 1016 AFT PRESSURE BULKHEAD AT S-23R IA - [SDR SWAA2024020247028](https://openairdocs.org/sdr/SWAA2024020247028.md): Girt Bar · out of position · Jan 30, 2024 · N202WN · Boeing 7377H4 · Escape Slide > FWD GALLEY ESCAPE SLIDE GIRT BAR MISALIGNED<[01] INSPECTED ESCAPE SLIDE GIRT BAR AT R1 GALLEY SERVICE DOOR IAW AMM 25-66-01. REPOSITIONED SLIDE TONGUE ON GIRT BAR. GIRT BAR ALIGNMENT IS NORMAL. A/C OK FOR SERVICE. - [SDR SWAA2023092905775](https://openairdocs.org/sdr/SWAA2023092905775.md): Slide · out of adjust · Sep 28, 2023 · N202WN · Boeing 7377H4 · Escape Slide > AFT PASS ENTRY DOOR SLIDE GAUGE NOT VISIBLE.<[01] REMOVED; REPOSITIONED; AND REINSTALLED L2 DOOR SLIDE IAW MT 725-61-06. - [SDR SWAA2023081487935](https://openairdocs.org/sdr/SWAA2023081487935.md): Unknown · unknown · Aug 9, 2023 · N202WN · Boeing 7377H4 · Trailing Edge Flap Control System > RT FLAP SPLIT ON FINAL @ FLAPS 30 DEG. FLAP WOULD NOT RETRACT AFTER LANDING<[01] PREFORM FIM TASK 27-51 TASK 813 FOUND FAULT 27-52259 OPS CHECK OK OF SYSTEM NO FAULTS NOTED AT THIS TIME - [SDR SWAA2023052250093](https://openairdocs.org/sdr/SWAA2023052250093.md): Flap · cracked · May 19, 2023 · N202WN · Boeing 7377H4 · Trailing Edge Flap Control System > LH IB AFT FLAP DENT/CRACK LH IB AFT FLAP DENT/CRACK LOWER SKIN<[01] APPLIED PERMANENT REPAIR PER SRM 57-53-01-2R-4 AND SRM 51-70-10. - [SDR SWAA2023030712119](https://openairdocs.org/sdr/SWAA2023030712119.md): Lens · missing · Mar 3, 2023 · N202WN · Boeing 7377H4 · Emergency Lighting > THE MID LEVEL EMERGENCY EXIT LIGHT LENS IS MISSING AT THE RIGHT OVERWING EMERGENCY EXIT<[01] INSTALLED LENS REF AMM 33-51-01 - [SDR SWAA2022081842869](https://openairdocs.org/sdr/SWAA2022081842869.md): Girt Bar · loose · Aug 18, 2022 · N202WN · Boeing 7377H4 · Emergency Equipment > FED AFT GRIT BAR FITTING IS LOOSE. / [01] TIGHTENED FED AFT GIRT BAR FITTING PER AMM 25-66-02-400-801 PARA: 3.D.(1)(G) - (J);[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] VERIFIED MEASUREMENTS TABLE.;[04] CERTIFY - [SDR SWAA2022081842770](https://openairdocs.org/sdr/SWAA2022081842770.md): Battery Pack · inoperative · Aug 17, 2022 · N202WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHTS ON BIN BULLNOSE INOP AT SEATS 9CBA AND 11CBA. REPLACED EMERGENCY LIGHTS BATTERY PACK M1670 AND PERFORMED GOOD TEST PER AMM 33-51-06-960-805. - [SDR SWAA2022081842769](https://openairdocs.org/sdr/SWAA2022081842769.md): Light · inoperative · Aug 17, 2022 · N202WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHT BULBS BURNED OUT AT R OWE EXIT SIGNS. REPLACED LAMPS AND PERFORMED GOOD FUNCTIONAL TEST OF EMERGENCY LIGHT RT OWE EXIT SIGNS IAW AMM 33-51-01-960-801. - [SDR SWAA2022081832070](https://openairdocs.org/sdr/SWAA2022081832070.md): Baffle · cracked · Jul 22, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Plate/Skin > FWD CARGO BAY BAFFLE CRACKED BS 500 - BS 500A LBL 25 / [01] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS;[02] FWD CARGO BAY BAFFLE FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2; STEP 4C;[03] REMOVED FWD CARGO BAY BAFFLE FROM BS 500 TO BS 500A; LBL 25 IAW SRM 51-40-0 - [SDR SWAA2022081832069](https://openairdocs.org/sdr/SWAA2022081832069.md): Baffle · cracked · Jul 22, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Plate/Skin > FWD CARGO BAY BAFFLE CRACKED BS 500B - BS 500C LBL 25 / [01] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS; CRACK FOUND OUT OF LIMITS;[02] REMOVED FWD CARGO BAY BAFFLE FROM BS 500B TO BS 500C; LBL 25 IAW 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW FWD CARGO BAY BA - [SDR SWAA2022081832068](https://openairdocs.org/sdr/SWAA2022081832068.md): Baffle · cracked · Jul 22, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Plate/Skin > FWD CARGO BAY BAFFLE CRACKED BS 400 - BS 420 LBL 25 / [01] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS; CRACK FOUND OUT LIMITS;[02] REMOVED FWD CARGO BAY BAFFLE FROM BS 400 TO BS 420; LBL 25 IAW SRM 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW FWD CARGO BAY BAFFL - [SDR SWAA2022080329735](https://openairdocs.org/sdr/SWAA2022080329735.md): Light · broken · Jul 15, 2022 · N202WN · Boeing 7377H4 · Emergency Lighting > SIDEWALL PANEL 232YHW EMERGENCY EXIT LIGHT LENS COVER IS BROKEN / [01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS COVER ON SIDEWALL PANEL 232YHW IAW AMM 33-51-01-960-801 STEPS 2. C. (1)(A) AND (4);[02] VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2022081928559](https://openairdocs.org/sdr/SWAA2022081928559.md): Frame Splice · corroded · Jul 13, 2022 · N202WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON PASSENGER CABIN FRAME SPLICE AT BS 277 BL 0 STRINGER 1.(MARKED) / [01] NOT ALLOWABLE LIMITS FOUND ON SRM FOR BS277 FRAME SPLICE;SRM 51-10-02-0G-0 PAR. 9.C REPLACEMENT OF THE PART IS APPLICABLE;[02] REMOVED BS277 FRAME SPLICE LBL3-RBL3 WL287 I.A.W - [SDR SWAA2022081828562](https://openairdocs.org/sdr/SWAA2022081828562.md): Web · cracked · Jul 13, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Frame > CRACK ON PASSENGER CABIN FWD ENTRY DOOR FWD WEB AT BS 294+1 L/H STRINGER 16.(MARKED) / [01] CLEANED PASSENGER CABIN FWD ENTRY DOOR FWD WEB AT BS 294+1 L/H
STRINGER 16.;[02] VERIFIED WORK PERFORMED;[03] NDT HFEC SURFACE INSPECTED AREA PER 737 NDTM PART 6 51- - [SDR SWAA2022081828561](https://openairdocs.org/sdr/SWAA2022081828561.md): Stringer Clip · cracked · Jul 13, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Frame > CRACK ON PASSENGER CABIN FWD ENTRY DOOR CLIP AT BS 294 L/H STRINGER 13.(MARKED) / [01] REMOVED CRACKED CLIP AT BS 294 STR 13 L/H IAW SRM 51-40-02-0G-0;[02] UPDATED MEASUREMENT TABLE;[03] FABRICATED NEW CLIP FROM BAC1489-360 LOT# 1464682-1.050' IAW DWG PL 141A - [SDR SWAA2022081828560](https://openairdocs.org/sdr/SWAA2022081828560.md): Stringer Clip · cracked · Jul 13, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Frame > CRACK ON PASSENGER CABIN STRINGER CLIP AT BS 277 R/H STRINGER 10.(MARKED) / [01] CLEANED PASSENGER CABIN STRINGER CLIP AT BS 277 R/H STRINGER 10.;[02] VERIFIED WORK PERFORMED;[03] NDT HFEC SURFACE INSPECTED AREA PER 737 NDTM PART 6 51-00-00 PROC 23; LARGE SEVE - [SDR SWAA2022081828557](https://openairdocs.org/sdr/SWAA2022081828557.md): Floor Panel · frayed · Jul 13, 2022 · N202WN · Boeing 7377H4 · Fuselage Floor Panel > AFT FLOOR PANEL 242VF UPPER SKIN FRAYED AT SEVERAL PLACES / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 6 TABLE 6.
FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.
DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1.
R - [SDR SWAA2022081828555](https://openairdocs.org/sdr/SWAA2022081828555.md): Floor Panel · frayed · Jul 13, 2022 · N202WN · Boeing 7377H4 · Fuselage Floor Panel > AFT FLOOR PANEL 241ADF UPPER SKIN FRAYED AT SEVERAL PLACES / [01] IDENTIFIED AFT FLOOR PANEL 241ADF IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F. DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-1.< - [SDR SWAA2022081928206](https://openairdocs.org/sdr/SWAA2022081928206.md): Seal Depressor · cracked · Jul 12, 2022 · N202WN · Boeing 7377H4 · Service Doors > FSD UPPER HINGE CUTOUT UPPER REVEAL IS CRACKED. / [01] LOCATED AND DRILLED NEW SEAL DEPRESSOR P/N 141A8372U1 LOT# 1485850-1 I.A.W. B737-700 SRM 51-40-05-0G-0 FIGURE 2 AND FIGURE 3 TABLE A. OK TO INSTALL NEW SEAL DEPRESSOR FORWARD SERVICE DOOR CUTOUT.;[02] VERI - [SDR SWAA2022081927414](https://openairdocs.org/sdr/SWAA2022081927414.md): Support Angle · corroded · Jul 9, 2022 · N202WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON THRESHOLD SUPPORT ANGLE AT FWD PASSENGER CABIN BS318 TO 338 LBL59. MARKED / [01] UPDATED MEASUREMENT TABLE;[02] REMOVED CORROSION ON THRESHOLD SUPPORT ANGLE AT FWD CABIN BS318 TO 338 LBL59 IN A 1X1.5X.010' AREA IAW SRM 51-10-02-0G-0. ORIGINAL THIC - [SDR SWAA2022081927406](https://openairdocs.org/sdr/SWAA2022081927406.md): Support Fitting · corroded · Jul 9, 2022 · N202WN · Boeing 7377H4 · Escape Slide > CORROSION ON FED GIRT BAR LATCH SUPPORT FITTING BS312 LBL9. MARKED. / [01] PITTING CORROSION EXCEEDS 50% OF MACHINED THICKNESS ON UPPER SURFACE OF FITTING. SRM DOES NOT HAVE ALLOWABLE DAMAGE LIMITS FOR GIRT BAR LATCH FITTINGS. R&R IAW SRM 51-10-02-0G-0 STEP 9. - [SDR SWAA2022081927415](https://openairdocs.org/sdr/SWAA2022081927415.md): Fitting · corroded · Jul 9, 2022 · N202WN · Boeing 7377H4 · Emergency Equipment > CORROSION ON FED GIRT BAR LATCH SUPPORT FITTING BS344 LBL14. MARKED. / [01] PITTING CORROSION EXCEEDS 50% OF MACHINED THICKNESS ON UPPER SURFACE OF FITTING. SRM DOES NOT HAVE ALLOWABLE DAMAGE LIMITS FOR GIRT BAR LATCH FITTINGS. R&R IAW SRM 51-10-02-0G-0 STEP 9 - [SDR SWAA2022081927416](https://openairdocs.org/sdr/SWAA2022081927416.md): Floor Support · corroded · Jul 9, 2022 · N202WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON FLOOR SUPPORT AT FWD CABIN BS330 LBL11. MARKED. / [01] UPDATED MEASUREMENTS LIST.;[02] DAMAGE EVALUATION; ORIGINAL THICKNESS.080.
CORROSION MATERIAL LOSS MEASURES (.022) FOUND TO BE OUT OF LIMITS AS PER SRM 53-10-04-0I-1.;[03] UPDATING TO ADD - [SDR SWAA2022081927419](https://openairdocs.org/sdr/SWAA2022081927419.md): Support Angle · corroded · Jul 9, 2022 · N202WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON FSD THRESHOLD SUPPORT ANGLE BS305 - BS323 RBL57. MARKED. / [01] FOUND SRM 53-10-15-1A-2 IS APPLICABLE FOR CORROSION REMOVAL AT BS 305-323 RBL 57 WL 209;[02] REMOVED CORROSION IN MULTIPLE AREAS ON FSD THRESHOLD SUPPORT ANGLE AT BS 305-323; RBL 57. - [SDR SWAA2022081727409](https://openairdocs.org/sdr/SWAA2022081727409.md): Intercostal · cracked · Jul 9, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Structure > CRACKED INTERCOSTAL AT FWD CABIN BS349 BL0 WL208. / [01] LOCATED AND MATCH DRILLED NEW INTERCOSTAL AT FWD CABIN BS349 BL0 WL208 IAW SRM 51-40-05 AND BOEING DWG 141A5400;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION 1;[04] INSTALLED INTERCOSTAL IAW SRM 51-4-02 - [SDR SWAA2022081727410](https://openairdocs.org/sdr/SWAA2022081727410.md): Intercostal · cracked · Jul 9, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Structure > CRACKED INTERCOSTAL AT FWD CABIN BS353 RBL11 WL208. / [01] UPDATED STEP 1 AND VERIFIED APPLICABILITY PER SRM 53-00-04-1A-1 AND BOEING DWG 141A5400

LOCATED AND MATCH DRILLED NEW INTERCOSTAL AT FWD CABIN BS349 RBL11 WL208 IAW SRM 51-40-05 AND BOEING DWG 1 - [SDR SWAA2022081727420](https://openairdocs.org/sdr/SWAA2022081727420.md): Intercostal · cracked · Jul 9, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Structure > CRACKED INTERCOSTAL AT FWD CABIN BS294+6 RBL31. MARKED. / [01] REMOVED HI-LOCKS FROM INTERCOSTAL AT FWD CABIN BS 294+6 RBL 31
IAW SRM 51-40-02-0G-0.;[02] VERIFIED APPLICABILITY PER SRM 53-00-04-1A-1 AND BOEING DWG 141A5400
REPAIR PER REPLACEMENT PER SRM - [SDR SWAA2022080327411](https://openairdocs.org/sdr/SWAA2022080327411.md): Channel · cracked · Jul 9, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Structure > CRACKED FWD ENTRY DOOR MOP SILL BS303 LBL55 WL208. MARKED. / [01] FED MOPSILL AT B.S 303 LBL55 WL208 IS CRACKED ON VERTICAL FLANGE. OUT OF LIMITS IAW SRM 53-10-15-1A-1. STARTED FASTENER REMOVAL IAW SRM 51-40-02-0G-0.;[02] UPDATED MEASUREMENT TABLE;[03] REMOVED - [SDR SWAA2022080327417](https://openairdocs.org/sdr/SWAA2022080327417.md): Intercostal · cracked · Jul 9, 2022 · N202WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED INTERCOSTAL AT FWD CABIN BS284 BL0 WL208. MARKED. / [01] UPDATED MEASUREMENTS. CRACKED INTERCOSTAL FOUND TO BE OUT OF LIMITS AND WILL BE REPLACEMENT OF THE PART IAW SRM 51-10-02 STEP 9. REMOVED CRACKED INTERCOSTAL AT BS284 BL0 WL208 IAW SRM 51-40-02. R - [SDR SWAA2022080327408](https://openairdocs.org/sdr/SWAA2022080327408.md): Intercostal · cracked · Jul 9, 2022 · N202WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED INTERCOSTAL AT FWD CABIN BS353 LBL11 WL208. / [01] VERIFIED APPLICABILITY PER SRM 53-00-04-1A-1 AND BOEING DWG 141A5400

LOCATED AND MATCH DRILLED NEW INTERCOSTAL AT FWD CABIN BS349 LBL11 WL208 IAW SRM 51-40-05 AND BOEING DWG 141A5400;[02] VERIFI - [SDR SWAA2022082227173](https://openairdocs.org/sdr/SWAA2022082227173.md): Floor Support · corroded · Jul 8, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CORROSION ON FLOOR BEAM AT AFT WET AREA BS986 RBL36 - RBL43. MARKED. / [01] VERIFIED APPLICABILITY PER SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1;[02] REMOVED DAMAGE ON BS986 FLOOR BEAM UPPER CHORD FLANGE RBL36-RBL43 WL208 7'X1' AND FOUND TO BE OUT LIMIT AT NUT PLAT - [SDR SWAA2022081927281](https://openairdocs.org/sdr/SWAA2022081927281.md): Bear Strap · cracked · Jul 8, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > PASSENGER CABIN FSD CUTOUT BARE STRAP CRACKED BS299; 3' BELOW FWD UPPER DOOR STOP FITTING. MARKED. / LOCATED & DRILLED NEW UPPER STUB FRAME P/N 141A8370U13 LOT# 1497302-1 P.O. CERT# 875637 I.A.W B737-700 SRM 51-40-05-0G-0 FIGURE 2 & FIGURE 3 TABLE A. OK TO INS - [SDR SWAA2022081927166](https://openairdocs.org/sdr/SWAA2022081927166.md): Web · corroded · Jul 8, 2022 · N202WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON 1016 WEB AT AFT WET AREA BS1016 RBL6. MARKED. / [01] BEGAN REMOVING FASTENERS COMMON TO WEB BS1016-BS1031 BL0-RBL37 IAW SRM 51-40-02.;[02] NO ALLOWABLE LIMITS FOUND ON SRM FOR BS1016 SHEAR WEB;REMOVED AND REPLACED OF THE PART IS APPLICABLE I.A.W - [SDR SWAA2022081927168](https://openairdocs.org/sdr/SWAA2022081927168.md): Tension Tie · corroded · Jul 8, 2022 · N202WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON TENSION STRAP AT AFT WET AREA BS1016 RBL3. MARKED. / [01] NOT LIMITS FOUND ON MANUAL; PART TO BE REPLACED IAW SRM 51-10-02 PART REPLACEMENT; REMOVED DAMAGED STRAP; LOCATED AND DRILLED NEW STRAP P/N 147A5744U1 IAW SRM 51-40-02-0G-0 AND 51-40-05-0G- - [SDR SWAA2022081927169](https://openairdocs.org/sdr/SWAA2022081927169.md): Tension Tie · corroded · Jul 8, 2022 · N202WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON TENSION STRAP AT AFT WET AREA BS1016 - BS1028 LBL3. MARKED. / [01] NOT LIMITS FOUND ON MANUAL; PART TO BE REPLACED IAW SRM 51-10-02 PART REPLACEMENT; REMOVED DAMAGED STRAP; LOCATED AND DRILLED NEW STRAP P/N 147A5620U3 IAW SRM 51-40-02-0G-0 AND 51- - [SDR SWAA2022081927170](https://openairdocs.org/sdr/SWAA2022081927170.md): Web · corroded · Jul 8, 2022 · N202WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON WEB AT AFT WET AREA BS1028 LBL4 TO LBL19. MARKED. / [01] NO ALLOWABLE LIMITS FOUND ON SRM FOR BS1028 LBL4-LBL19 SHEAR WEB;REMOVED AND REPLACED OF THE PART IS APPLICABLE I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED BS1016
L/H SHEAR WEB I.A.W SR - [SDR SWAA2022081927171](https://openairdocs.org/sdr/SWAA2022081927171.md): Web · corroded · Jul 8, 2022 · N202WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON WEB AT AFT WET AREA BS1016 LBL11; LBL34. MARKED. / [01] NO ALLOWABLE LIMITS FOUND ON SRM FOR BS1016 L/H SHEAR WEB;REMOVED AND REPLACED OF THE PART IS APPLICABLE I.A.W SRM 51-10-02-0G-0 PAR 9.C ALL REMOVAL AND REPLACED TO BE ACCOMPLSHED ON COSTUME - [SDR SWAA2022081927172](https://openairdocs.org/sdr/SWAA2022081927172.md): Floorbeam · corroded · Jul 8, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CORROSION ON FLOORBEAM AT AFT WET AREA BS986 LBL34 - LBL43. MARKED. / [01] VERIFIED APPLICABILITY PER SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1;[02] REMOVED DAMAGE ON BS986 FLOOR BEAM UPPER CHORD FLANGE LBL34-LBL43 WL208 9'X1' AND FOUND TO BE OUT LIMIT AT NUT PLATE - [SDR SWAA2022081827282](https://openairdocs.org/sdr/SWAA2022081827282.md): Frame · cracked · Jul 8, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Frame > FWD PASSENGER CABIN CRACKED FRAME AT BS312 11' BELOW S-4L WL283. MARKED. / [01] REMOVED DAMAGE ON FRAME AT BS312; 11' BELOW S-4L WL283 IAW SRM 51-10-02.;[02] REMOVED DAMAGE ON FRAME AT BS312; 11' BELOW S-4L WL283 IN AN AREA OF 1' X.2' IAW SRM 51-10-02.;[03] R - [SDR SWAA2022081827176](https://openairdocs.org/sdr/SWAA2022081827176.md): Frame · cracked · Jul 8, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Frame > CRACKED FRAME AT AFT PASSENGER CABIN S-8L BS927. MARKED. / [01] REMOVED FRAME TO BIN RAIL ATTACH ANGLE BS 927; STR 8L FOR ACCESS IAW SRM 51-40-02-0G-0. NO VISUAL SIGN OF CRACK ON FRAME;[02] VERIFIED CORRECTIVE ACTION #1;[03] REQUEST NDI FOR CRACK FREE CONDITIO - [SDR SWAA2022080327283](https://openairdocs.org/sdr/SWAA2022080327283.md): Bracket · loose · Jul 8, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Structure > LOOSE FASTENERS CHAFING ON INTERCOSTAL AT FWD PASSENGER CABIN BS277 3' OB OF S-2R WL282. / [01] GAINED ACCESS BY REMOVING COCKPIT DOOR POST PER SRM 51-40-02;[02] REMOVED CHAFFED BRACKET AT BS 277;3' OUTBD OF STR 2R; WL 282 IAW SRM 51-40-02;[03] LOCATED NEW BR - [SDR SWAA2022081926591](https://openairdocs.org/sdr/SWAA2022081926591.md): Pressure Deck · cracked · Jul 7, 2022 · N202WN · Boeing 7377H4 · Fuselage Main, Frame > HORIZONTAL PRESSURE DECK CRACKED AT BS 664.5; LBL 30.5 AND 32; WL 202.5. (CRACKS CIRCLED IN RED) / CUTED AND REMOVED THE DAMAGE PART OF THE WEB PER SRM 53-40-51-2R-2. PAR. 4 A;B;C (1)(2)(3).HFEC INSPECTED CUTOUT AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.< - [SDR SWAA2022081826586](https://openairdocs.org/sdr/SWAA2022081826586.md): Floor Panel · damaged · Jul 7, 2022 · N202WN · Boeing 7377H4 · Fuselage Floor Panel > FWD FLOOR PANEL 222DF HAS A RIPPED OUT INSERT ALONG THE O/B EDGE. (MARKED) / [01] IDENTIFIED FWD PANEL 222DF IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW 53-00-50-1A-1 PARA 4.F.
DAMAGE WILL BE REPAIRED IAW SRM 53-0 - [SDR SWAA2022081826585](https://openairdocs.org/sdr/SWAA2022081826585.md): Floor Panel · pulled · Jul 7, 2022 · N202WN · Boeing 7377H4 · Fuselage Floor Panel > FWD FLOOR PANEL 222BF UPPER SURFACE HAS AREAS OF PULLED STRANDS. / REMOVED ALL INSERTS TO FACILITATE REPAIR IAW SRM 53-00-50-2R-1 PARA 3B
REMOVED PREVIOUS REPAIR AND ALL DAMAGE NOTED AND CLEANED REPAIR AREAS IAW SRM 53-00-50-2R-1 PARA 3C-F;[02] VALIDATED AP Next page: https://openairdocs.org/deregistered/N202WN-2024-10-29/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 = 'N202WN' AND deregistration_id = 'N202WN-2024-10-29' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N202WN-2024-10-29/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, except the copies of manufacturers’ service documents, which belong to their rights holders.