N295WN

Service difficulty reports · 291

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 = 'N295WN' 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 SWAA2023062955205Floor Panel · pulledAFT CABIN FLOOR PANEL 241VF HAS A PULLED THROUGH INSERT HOLE<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW FLOOR PANEL USING BMS4-23 TYPE II LOT 1525675-1 AND BMS5-107 LOT AK2KP8383K-1 RESIN; CURED RESIN WITH A HEAT LAMP USING THERMOMJun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062955231Floor Panel · brokenFWD CABIN FLOOR PANEL 221BF AFT O/B CORNER IS BROKEN (TANG)<[01] IDENTIFIED PANEL 221BF IAW SRM 53-00-50-0I-1 FIGURE 2. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.E.(2).(B) AND WILL BE REPAIRED IAW SRM 53-00-50-2R-6. REMOVED NUMEROUS IJun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062955233Floor Panel · brokenFWD CABIN FLOOR PANEL 221GF FWD O/B CORNER IS BROKEN (TANG)<[01] IDENTIFIED FLOOR PANEL 221GF IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2 <BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR.4 B<BR><BR>DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-1Jun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062955204Floor Panel · pulledAFT CABIN FLOOR PANEL 241VF HAS A PULLED THROUGH INSERT HOLE<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW FLOOR PANEL USING BMS4-23 TYPE II LOT 1525675-1 AND BMS5-107 LOT AK2KP8383K-1 RESIN; CURED RESIN WITH A HEAT LAMP USING THERMOMJun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062954825Stringer · crackedSTRINGER S-24L IS CRACKED AT STA 540.<[01] CRACK FOUND OUT OF LIMITS ON STRINGER S-24L BS 535 SKIN ATTACHMENT FLANGE 100% OF MATERIAL THICKNESS L=0.5' IAW SRM 53-00-03-1A-1;[02] VERIFIED APPLICABILITY OF SRM 53-00-03-2R-1 REP.1. FOR STRINGER S-24L BS 535 SKIN Jun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023062954821Stringer · crackedSTRINGER S-25R IS CRACKED AT STA 540.<[01] REMOVED DAMAGED SECTION OF STRINGER S-25R BS 500D+10' - BS 535 IAW SRM 53-00-03-2R-1 REP.1 PAR 4 A-B AND EA 23-153-01768;[02] PERFORMED A GVI ON REPAIR AREA OF STRINGER S-25R BS 500D+10' - BS 535 AND NOT FOUND ADDITIOJun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023062954823Stringer · crackedSTRINGER S-26L IS CRACKED AT STA 540.<[01] CRACK FOUND OUT OF LIMITS ON STRINGER S-26L BS 535 SKIN ATTACHMENT FLANGE 100% OF MATERIAL THICKNESS L=0.5' IAW SRM 53-00-03-1A-1;[02] VERIFIED APPLICABILITY OF SRM 53-00-03-2R-1 REP.1. FOR STRINGER S-26L BS 535 SKIN Jun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023062954819Stringer · corrodedCORROSION ON STRINGER S-23R FROM STA 520+18 TO STA 540.<[01] CORROSION FOUND OUT OF LIMITS ON STRINGER S-23R BS 535 SKIN ATTACHMENT FLANGE 100% OF MATERIAL THICKNESS LOSS L=1' X W=0.5' IAW SRM 53-00-03-1A-1;[09] RECEIVED PARTS NEW STRINGER SECTION OF STR-23R RJun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023062955285Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 380-400; RBL 10; WL 208 IS CRACKED.<[01] NO ENTRIES FOUND ON SRM FOR PASSENGER CABIN FLOOR SUPPORT BS 380-400; RBL 10; WL 208 PART TO BE REMOVED AND REPLACED PER SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED PASSENGER CABIN FLOOR SUPPJun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062955287Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 380-400; LBL 15; WL 208 IS CRACKED.<[01] NO ENTRIES FOUND ON SRM FOR CRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 15; WL 208 PART TO BE REMOVED AND REPLACED PER SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED CRACKED INTERCOSJun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062955283Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 380-400; RBL 1; WL 208 IS CRACKED.<[01] NO ENTRIES FOUND ON SRM FOR PASSENGER CABIN FLOOR SUPPORT BS 380-400; RBL 1; WL 208 PART TO BE REMOVED AND REPLACED PER SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED PASSENGER CABIN FLOOR SUPPORJun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062955277Girt Bar · out of adjustFWD ENTRY DOOR FWD GIRT BAR MOUNTING BRACKET INBOARD FASTENER IS LOOSE.<[01] DISCREPANCY TO BE ACCOMPLISHED ON COSTUMER CARD TTG8Q00LDPKH INSTALLATION OF MOPSILL I.A.W SRM 51-40-02-0G-0;[02] VERIFIEDJun 1, 2023 · N295WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2023062955263Stub Frame · crackedPASSENGER CABIN STUB FRAME TO MOPSILL ATTACH ANGLE; OUTBOARD OF MOPSILL; BS 294.5; RBL 65; WL 208 IS CRACKED<[01] AFTER FURTHER INVESTIGATION CRACKED PASSENGER CABIN STUB FRAME TO MOPSILL ATTACH ANGLE; OUTBOARD OF MOPSILL; BS 294.5; RBL 65; WL 208 FOUND CRACK Jun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2023062954829Shield · elongatedFORWARD CARGO BAY AFT SHIELD HAS AN ELONGATED FASTENER HOLE BS495 RBL22 WL 156<[01] ELONGATED HOLE ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1;[03] UPDATE TO CORRECTIVE ACTION STEP 1. ELONGATJun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062955255Bracket · brokenAFT CARGO BAY LAV TANK BULKHEAD LOWER BRACKET IS BROKEN BS867 LBL10 WL166<[01] REMOVED DAMAGED ACB LAV TANK BULKHEAD LOWER BRACKET BS 867; LBL10; WL166 PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED ACB LAV TANK BULKHEAD LOWER BRACKET BS 867; LBL10; WL166 PERJun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062655268Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 312-328; LBL 45; WL 208 IS CRACKED.<Jun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062655262Stub Frame · crackedPASSENGER CABIN STUB FRAME TO MOPSILL ATTACH ANGLE; OUTBOARD OF MOPSILL; BS 294.5; RBL 65; WL 208 IS CRACKED<Jun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2023062655258Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 277-294; RBL 1; WL 208 IS CRACKED.<Jun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062655259Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 277-294; RBL 1; WL 208 IS CRACKED.<[01] VERIFIED APPLICABILITY PER SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1;[02] CRACKED PASSENGER CABIN FLOOR SUPPORT BS 277-294; RBL 1; WL 208 EXCEED ALLOWABLE LIMITS ON SRM 53-10-51-1A-1 ALLOWABLEJun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062655269Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 312-328; LBL 45; WL 208 IS CRACKED.<[01] VERIFIED APPLICABILITY OF SRM 53-10-51-1A-1;[02] CRACKED PASSENGER CABIN FLOOR SUPPORT BS 312-328; LBL 45; WL 208 EXCEED ALLOWABLE LIMITS ON SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1 PAR 4.B Jun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062655297Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 344-360; LBL 3; WL 208 IS CRACKED.<[01] VERIFIED APPLICABILITY OF SRM 53-10-51-1A-1;[02] CRACKED PASSENGER CABIN FLOOR SUPPORT BS 344-360; LBL 3; WL 208 EXCEED ALLOWABLE LIMITS ON SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1 PAR 4.E SRJun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062655296Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 344-360; LBL 3; WL 208 IS CRACKED.<Jun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062655286Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 380-400; LBL 15; WL 208 IS CRACKED.<Jun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062655284Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 380-400; RBL 10; WL 208 IS CRACKED.<Jun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062655282Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 380-400; RBL 1; WL 208 IS CRACKED.<Jun 1, 2023 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062954801Vapor Barrier · debondedR/H VAPOR BARRIER HAS DISBONDED REPAIRS BS663 RBL 35 WL 178<[01] IDENTIFIED R/H VAPOR BARRIER IAW SRM 57-10-10-0I-2 TABLE 2; FIG 2; ITEM 4.<BR><BR>DAMAGE IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PARA 4.D (1).<BR><BR>DAMAGE WILL BE REPAIRED IAW SMay 31, 2023 · N295WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2023053052469Compensator · inoperativeLEFT FUEL IMBALANCE OF 1200 LB AFTER DEPARTING BUR WITH MORE THAN 1000 LB IN CENTER TANK WITH CTR; #1 & #2 FUEL PUMPS. PERFORMED TANK & COMPENSATOR UNIT RESISTANCE & CAPACITANCE CHECK IAW AMM 28-41-21-710-801. FOUND COMPENSATOR CAPACITANCE VALUE OUT OF LIMITMay 26, 2023 · N295WN · Boeing 7377H4 · Fuel Indicating SystemSDR SWAA2023032720603Slide · looseFWD SERVICE DOOR SLIDE BAR RETAINER BRACKET LOOSE<[01] REPLACED RIVET ON FWD SERVICE DOOR SLIDE PER SRM 51-40-02Mar 24, 2023 · N295WN · Boeing 7377H4 · Escape SlideSDR SWAA2023032017395Engine · failedAFTER TAKEOFF LARGE RPM FLUCTUATION NR 2 ENGINE, SPARKS WERE REPORTED BY PASSENGER. NO OVERWEIGHT LANDING. LOUD POPPING SOUNDS FROM NR 2 ENG. REMOVED AND REPLACED NR 2 ENGINE IAW AMM 71-00-02 & MT 771-00-01.Mar 16, 2023 · N295WN · Boeing 7377H4 · Engine (Turbine/Turboprop)SDR SWAA2023021300477Pump · stalledON CLIMB OUT; #2 ENGINE WAS UNRESPONSIVE TO THRUST LEVER MOVEMENT. TOPPED OUT ABOUT 86.4% N1 EGT 40-90 WARMER THEN #1. RAN ENGINE LIMIT SURGE STALL QRH AND RECOVERED NORMAL ENGINE OPERATIONS EGT REMAINS STABLE 40 DEG. WARMER THEN #1.<[01] REMOVED AND REPLACED Feb 7, 2023 · N295WN · Boeing 7377H4 · Engine Fuel/Oil CoolerSDR SWAA2023020698832Valve · faulty#2 ENG COMP STALL<[01] SEE FOUND FAULTS TTG8Q00HMT8Y TTG8Q00HMT1Q TTG8Q00FTQP7 TTG8Q00CYJR7 TTG8Q00HMYNQ TTG8Q00HN801 FOR CORRECTIVE ACTIONS ALSO PERFORMED FIM TASK 71-05 TASK 805 AND AMM 71-00-00-210-801-F00Feb 3, 2023 · N295WN · Boeing 7377H4 · Fuel Controlling SystemSDR SWAA2022040489212Hmu · faultedCLIMBING THROUGH 2;500- LOUD BANG FROM NUMBER 2 ENG FOLLOWED BY FLAMES FROM TAILPIPE- 30 SEC LATER ANOTHER BANG FOLLOWED BY FLAMES AND SPARKS FROM TAILPIPE. RETURNED TO MKE NORMAL LANDING. ALL ENGINE PARAMETERS WHERE NORMAL NO INDICATIONS OF FIRE / [01] R&R?D Mar 29, 2022 · N295WN · Boeing 7377H4 · Fuel Controlling SystemSDR SWAA2022020164877Bulb · inoperativeLH OVERWING EXIT EMERGENCY SIGN HAS ONE LIGHT INOP. ; / [01] RELAMPED LH OVERWING EXIT EMERGENCY SIGN AFT BULB IAW AMM 33-51-01.Jan 28, 2022 · N295WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021072797424Skin · delaminatedR/H OUTBD AFT FLAP HAS DELAM INBD LOWER CORNER. REMOVED AND REPLACED R/H OUT/BD AFT FLAP AS PER AMM 27-51-22.Jul 23, 2021 · N295WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2021080591695Angle · elongatedFORWARD CARGO TRANSITION ANGLE RBL21 HAS NUMEROUS FASTENER HOLES ELONGATED AND DOUBLE DRILLED AT STA494 (MARKED) ; / [01] OVER SIZED THE HOLES TO .216 PER SRM 51-40-05 OK TO INSTALL TRANSITION ANGLE; [02] VERIFIED OVER SIZED THE HOLES TO .216 PER SRM 51-40-05 Jul 7, 2021 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080591696Angle · corrodedFORWARD CARGO TRANSITION ANGLE RBL21 HAS CORROSION AROUND NUMEROUS FASTENER HOLES STA500 TO STA500A (MARKED) ; / [01] REMOVED AND REPLACED TRANSITION ANGLE FROM STA 500-520 PER SRM 51-10-02;51-40-02; [02] VERIFIED INSTALLATIONJul 7, 2021 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080591694Angle · corrodedFORWARD CARGO TRANSITION ANGLE LBL21 HAS CORROSION AROUND FASTENER HOLES STA500+10 TO 500B++10 (MARKED) ; / [01] BLENDED AREAS OF CORROSION AT FWD CARGO TRANSITION ANGLE; STA. 500+10 TO STA.500B+10 LBL 21. REMOVED 0.008; ALLOWED 0.004; BLENDS OUT OF LIMITS ALLJul 7, 2021 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080591698Angle · corrodedFORWARD CARGO TRANSITION ANGLE LBL21 HAS CORROSION NUMEROUS FASTENER HOLES STA500B+10 TO 500D (MARKED) ; / [01] BLENDED AREAS OF CORROSION ON FWD CARGO TRANSITION ANGLE STA. 500B+10 TO STA.500D; REMOVED 0.005; ALLOWED 0.004; BLENDS OUT OF LIMITS ALL IAW SRM 53Jul 7, 2021 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080591705Angle · corrodedAFT CARGO LEFT SIDE TRANSITION ANGLE HAS CORROSION F.S. 727D TO 807. ; / [01] BLENDED/REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED DAMAGED TRANSITION ANGLE. ORIGINAL THICKNESS = .040'. REMAINING THJul 7, 2021 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080591702Angle · corrodedAFT CARGO RIGHT SIDE TRANSITION ANGLE HAS CORROSION F.S. 727D TO 767. ; / [01] BLENDED/REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED DAMAGED TRANSITION ANGLE. ORIGINAL THICKNESS = .040'. REMAINING TJul 7, 2021 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080591699Angle · corrodedAFT CARGO RIGHT SIDE TRANSITION ANGLE HAS CORROSION F.S.727A TO 727B. ; / [01] BLENDED/REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED DAMAGED TRANSITION ANGLE. ORIGINAL THICKNESS = .040'. REMAINING TJul 7, 2021 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080591697Angle · corrodedAFT CARGO RIGHT SIDE TRANSITION ANGLE HAS CORROSION FORWARD OF CARGO DOOR CUTOUT AT BS 767 TO 787. BLENDED/REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED DAMAGED TRANSITION ANGLE. DRILLED UP REPLAJul 7, 2021 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080591704Angle · corrodedAFT CARGO LEFT SIDE TRANSITION ANGLE HAS CORROSION BS 727 TO 727D. BLENDED/REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED DAMAGED TRANSITION ANGLE. REMOVED AND REPLACED THE TRANSITION ANGLE IAW SRMJul 7, 2021 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080591262Floor Panel · damagedFLOOR PANEL 241AF HAS AREAS OF DAMAGE TO UPPER SURFACE. REMOVED AND REPLACED FLOOR PANEL 241AF PER AMM 53-21-00.Jul 6, 2021 · N295WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080591263Floor Panel · damagedFLOOR PANEL 241BF HAS AREAS OF DAMAGE TO UPPER SURFACE. ; REMOVED AND REPLACED 241BF PER AMM 53-21-00.Jul 6, 2021 · N295WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080591265Floor Panel · damagedFLOOR PANEL 242AF HAS AREAS OF DAMAGE TO UPPER SURFACE. REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.Jul 6, 2021 · N295WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080591266Floor Panel · damagedFLOOR PANEL 242BF HAS AREAS OF DAMAGE TO UPPER SURFACE. ; / [01] R&R'D FLOOR PANEL PER MM 53-21-00 R&R FLOOR PANEL PER MM 53-21-00.Jul 6, 2021 · N295WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080990181Fitting · damaged#1 ENGINE AFT O/B PYLON FITTING HAS DAMAGE FROM MAKING CONTACT WITH AFT UPPER METAL FIRE SEAL ON O/B T/R.(MARKED) ; / [01] REMOVED DAMAGE ON #1 ENGINE AFT O/B GSE BOOTSTRAP FITTING.MEASURING 1INCH DOWN FROM TOP OF STRUT BOX TO FORWARD O/B FLANGE EDGE OF FITTINJul 3, 2021 · N295WN · Boeing 7377H4 · Nacelle/Pylon, Attach FittingsSDR SWAA2021080990173Skin · chafedRIGHT HAND WING INBOARD GROUND SPOILER #7 O/B LEADING EDGE LOWER SURFACE IS CHAFED.(MARKED) ; / [01] #7 GROUND SPOILER TO BE REPLACED ON CARD# TTG8Q005NZHO.; [02] CARD # SHOULD BE TTG8Q005NZH0; [03] C/W; [04] VERIFIED.Jul 2, 2021 · N295WN · Boeing 7377H4 · SpoilersSDR SWAA2021080990164Angle · bentLEFT WING PNL 551FB FWD ATTACH ANGLE IS BENT. ; / [01] REMOVED AND REPLACED FWD ATTACH ANGLE ON PANEL 551FB PER SRM 51-40-02Jul 2, 2021 · N295WN · Boeing 7377H4 · Wing Miscellaneous Structure
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