JASC 5710

Service difficulty reports · 4,462

Reports filed under 5710 · Wing Main, Frame Structure, 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 jasc_code = '5710'
  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 SWAA2021112446461Spar · crackedCRACK FRONT SPAR ANGLE LOCATED FUEL BOSST PUMP IFSS 120 AREA AT RT WI NG (1 EA) 2021-520664 / TOOL USED DIGITAL CALIPER P/N 500-193-30 S/N 0000291 DUE DATE 16-SEP-22. TOOL USED: POWER PACK P/N PE1068 S/N PE0118/94826 DUE DATE: 23-FEB-22.MULTIMETER P/N FLUKE 87Nov 20, 2021 · N7863A · Boeing 7377Q8SDR SWAA2021112246198Web · crackedLEFT A/C BAY; BS 663; LBL 15.0 TO 19.0; WL 50 TO 67; SEVERAL CRACKS IN BULKHEAD WED SKIN ABOVE EXH. AIR DUCT CUTOUT AROUND ATTACH FASTENERS. BONDED REPAIR PLIES. IAW SRM 51-70-04-2R-10 PAR4D-G REV 74. RESTORED FINISHES IAW SRM 57-10-10-2R-2 REPAIR 2.Nov 18, 2021 · N475WN · Boeing 737*SDR SWAA2021112244533Angle · crackedFOUND CRACK IN L/H A/C BAY STA 663 VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 40 ; / [01] REMOVED STIFFENER ON FWD SIDE OF STA 663 LBL 40 TO FOM IAW SRM 51-40-02-0G-0; [02] REMOVED U-CHANNEL ON FWD SIDE STA 663 LBL 43-65 TO FOM IAW SRM 51-40-02-0G-0; [03] CUT ANDNov 17, 2021 · N475WN · Boeing 737*SDR SWAA2021112244967Attach Angle · crackedFOUND CRACK IN L/H A/C BAY STA 663 VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 40. REMOVED STIFFENER ON FWD SIDE OF STA 663 LBL 40 TO FOM IAW SRM 51-40-02-0G-0. CUT AND REMOVED DAMAGED ATTACH ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5. PERFORMED DVI OF REPAIR AREA &Nov 17, 2021 · N475WN · Boeing 737*SDR FDEA202111122837Support · corrodedR/H WING REAR SPAR SUPPORT-UPPER O/B IDLER, ARB0042-2 IS CORRODED REMOVED AND REPLACED ARB0042-2 SUPPORT PER DAC DWG ARB0042.Nov 12, 2021 · N586FE · Doug MD11FSDR FDEA202111112830None · damagedRH FR47 HOLE 11 HAS THREAD DAMAGE INDICATIONS IN ALL LAYERS. REFER TO EO 6-5710- E0342809 FOR LOCATIONS COMPLIED WITH E.A. 6 - 5710 - T0353473 D P11 "WINGS - BASIC WING STRUCTURE - FR 47 RHS REPAIRED HOLES"Nov 11, 2021 · N662FE · Airbus A300*SDR FDEA202111112829None · damagedRH FR47 HOLE 13 HAS THREAD DAMAGE INDICATIONS IN ALL LAYERS. REFER TO EO 6-5710- E0342809 FOR LOCATIONS COMPLIED WITH E.A. 6 - 5710 - T0353473 D P11 " WINGS - BASIC WING STRUCTURE - FR 47 RHS REPAIRED HOLES"Nov 11, 2021 · N662FE · Airbus A300*SDR FDEA202111112828None · damagedRH FR47 HOLE 10 HAS THREAD DAMAGE INDICATIONS IN ALL LAYERS. REFER TO EO 6-5710- E0342809 FOR LOCATIONS COMPLIED WITH E.A. 6-5710-TO353473 D P11 "WINGS - BASIC WING STRUCTURE - FR47 RHS REPAIRED HOLESNov 11, 2021 · N662FE · Airbus A300*SDR IPXA2021111976120None · corrodedINSPECTION TYPE:C**SUPPLEMENTAL SDR**LH WING LOWER SKIN AT STA 760 TE HAS A 1.30" LONG BY 4.00" WIDE AREA OF INTERGRANULAR CORROSION WHICH WHEN REMOVED HAD .110" OF MATERIAL LOSS MAX ALLOWED IS .40" PER SRM 57-20-01-1A-1 TABLE 2.REPAIR PER RCD INSTRUCTIONS EO Nov 10, 2021 · N452UP · Boeing 75724APFSDR FDEA202111052783Former · unknownAT THE TIME OF AIRCRAFT INSPECTION ON FEDEX EO 1-5100-7-5001 PART1, FOUND 01 EACH EXISTING REPAIR ON PRIMARY STRUCTURE AT LEFT HAND WING FIXED LEADING EDGE INNER COMPARTMENT AT XOS 584.892 WAS NOT DOCUMENTED FOR EVALUATION. EXISTING REPAIR AT LEFT HAND WINNov 5, 2021 · N587FE · Doug MD11FSDR SWAA2021111540840Attach Angle · crackedB.S. 663 BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 8; W.L. 164. ; / [01] TRIMED OUT ATTACH ANGLE AT VAPOR BARRIER BS 663 RBL 15 WL 164 PER SRM 57-10-10-2R-5 STEP 4 B<BR><BR>PERFORMED DETAIL INSPECTION OF THE REPAIR AREA AND UNDERLYING STRUCTURE TO MAKE Nov 4, 2021 · N915WN · Boeing 737*SDR YENA2021111100759Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION AT LH WING, TOP SKIN, LOWER SURFACE OVERHANG RIB 6 TO 8. REF HMV FLIGHTSTAR - VQQ, W/O N653JB-02-01, TASK NO. NR-0080 ; (RESOLVED ON W/O: 1121596 TASKCARD: NR-00010 ) REMOVED CORROSION AT LH WING TOP SKIN LOWER SURFACE OVENov 4, 2021 · N653JB · Airbus A320232SDR YENA2021111100758Skin · corrodedDURING HEAVY MAINTENANCE, LH WING TOP SKIN CORROSION AT TRAILING EDGE, OVERHANG AREA, BTW RIB 5 & RIB 6. REF. HMV FLIGHTSTAR-VQQ, W/O N653JB-02-01, TASK NR-00110 ; (RESOLVED ON W/O: 1121596 TASKCARD: NR-00012 ) REMOVED CORROSION AT LH WING TOP SKIIN, T/E OVERHNov 4, 2021 · N653JB · Airbus A320232SDR YENA2021111100756Wing · corrodedDURING HEAVY MAINTENANCE, CORROSION UPPER RIGHT WING SURFACE, TRAILING EDGE, BTW RIBS 18 AND 19 REF. HMV FLIGHTSTAR-VQQ, W/O# N653JB-02-01, NR # 0012 ; (RESOLVED ON W/O: 1121596 TASKCARD: NR-00013 ) REMOVED CORROSION AT UPPER RH WING SURFACE IAW A320 SRM 51-74Nov 4, 2021 · N653JB · Airbus A320232SDR YENA2021111100755Wing · corrodedDURING HEAVY MAINTENANCE, CORROSION UPPER R/H WING SURFACE, TRAILING EDGE, FWD OF SPOILER NO.5, BTW RIB 19 & 20. REF HMV FLIGHTSTAR-VQQ, W/O 3 N653JB-020-01, NR 3#00120 ; (RESOLVED ON W/O: 1121596 TASKCARD: NR-00014 )REMOVED CORROSION AT UPPER RH WING SURFACE Nov 4, 2021 · N653JB · Airbus A320232SDR YENA2021111100754Spar · corrodedDURING HEAVY MAINTENANCE, CORROSION R/H WING, REAR SPAR, UPPER OVERHANG, LOWER SURFACE, NEAR SUPPORT FITTING #4 SPOILER HINGE, BTW. RIBS 15 AND RIB 17. REF HMV FLIGHTSTAR -VQQ W/O 3 N653JB-02-01, NR # 00126 ; (RESOLVED ON W/O: 1121596 TASKCARD: NR-00017 ) REMNov 4, 2021 · N653JB · Airbus A320232SDR YENA2021111100753Spoiler · corrodedDURING HEAVY MAINTENANCE, CORROSION UPPER RIGHT WING SURFACE, TRAILING EDGE; FORWARD CTR. OF SPOILER NO.4, RIB 17. REF HMV FLIGHTSTAR-VQQ, W/O# N653JB-02-01, NR #00123; REMOVED CORROSION AT RH WING UPPER T/E SURFACE IAW A320 SRM 51-74-00. REMAINING MATERIAL INov 4, 2021 · N653JB · Airbus A320232SDR YENA2021111100752Spoiler · corrodedDURING HEAVY MAINTENANCE, CORROSION ON UPPER R/H WING SURFACE. 5 LOCATIONS WITHIN 12.00" AREA. TRAILING EDGE, FORWARD OF THE NO. 5 SPOLIER, RIB 19. REF HMV FLIGHTSTAR - VQQ, W/O # N653JB-02-01, NR # 00118 ; (RESOLVED ON W/O: 1121596 TASKCARD: NR-00016 ) REMOVENov 4, 2021 · N653JB · Airbus A320232SDR YENA2021111100751Spar · corrodedDURING HEAVY MAINTENANCE, CORROSION R/H WING, REAR SPAR, UPPER OVERHANG, LOWER SURFACE, NEAR SUPPORT FITTING #4 SPOILER HINGE, BTW. RIBS 15 AND RIB 17. REF HMV FLIGHTSTAR -VQQ W/O 3 N653JB-02-01, NR # 00126 ; (RESOLVED ON W/O: 1121596 TASKCARD: NR-00017 ) REMNov 4, 2021 · N653JB · Airbus A320232SDR SWAA2022010439665Vapor Barrier · crackedSUPPLEMENTAL INFORMATION: RH SIDE STA 663 VAPOR BARRIER HAS A CRACK . ; / [01] STOP DRILL AT THE END CRACK AT VAPOR BARRIER ON STA 663 PER B737 SRM 57-10-10-2R PARAGRAPH 6.B PERFORMED VISUAL INSPECTION AND TAP TEST FOUND CRACK SIZE 12''PER B737 NTM 51-05-01; [Nov 2, 2021 · N770SA · Boeing 737SDR R61A2021112200924Skin · crackedLH WING LOWER SKIN CRACKED 38MM LONG AT FASTENERS OTBD OF RIB 4A AND 12" AFT OF SPAR 2. PERFORMED TEMPORARY REPAIR ON LH WING LOWER SKIN OTBD OF RIB 4A AND 12" AFT OF SPAR 2 BY CUTOUT AND FILLER/DOUBLER REPAIR IN ACCORDANCE WITH, REF ETD2021-170-036608 REV. BNov 2, 2021 · N138HQ · Emb ERJ170200LRSDR SWAA2021111939463Vapor Barrier · crackedLEFT HAND VAPOR BARRIER IS CRACKED AT BS 663; LBL 40 TO 48. ; / [01] REMOVED 1EA PLACARD FROM FWD OB SURFACE (BAC27DHY0286)<BR><BR>IDENTIFIED MATERIAL OF LEFT HAND VAPOR BARRIER IAW SRM 57-10-10-0I-2 FIGURE 1-2; ITEM #4; TABLE 2<BR><BR>DAMAGE IS OUT OF ALLOWABNov 1, 2021 · N968WN · Boeing 737*SDR FDEA202110312699None · cracked#9 SLAT INTERNAL COVE PANEL IS CRACKED @ OSS 574 REMOVED & REPLACED COVE PANEL IAW BAC DWG 114N4003, REV G & BAC DWG 114N4076 REV COct 31, 2021 · N951FD · Boeing 757200SDR FDEA202110312698None · cracked#9 SLAT, INTERNAL COVE PANEL IS CRACKED @ OSS 604 REMOVED & REPLACE COVE PANEL ASSY IAW BAC DWG 114N4003 REV G & BAC DWG 114N4076 REV COct 31, 2021 · N951FD · Boeing 757200SDR SWAA2021112933626Bracket · elongatedLEFT MAIN WHEEL WELL FWD BULKHEAD VAPOR BARRIER UPPER SUPPORT BRACKET HOLE ELONGATED JUST O/B OF LBL 40.87 ; / [01] PERFORMED HFEC ROTO ON OPEN FASTENER HOLES ON UPPER SUPPORT BRACKET AT BS 663.75 LBL 40.85 (LEFT MAIN WHEEL WELL FWD BULKHEAD) EXCEPT ELONGATED Oct 26, 2021 · N777QC · Boeing 7377H4SDR FDEA202110252610None · noneCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "I" HOLE FOUND CRACK SIGNAL COMPLIED WITH EO 6-5710-E0342809 B P2 STEP 5.D-5.E. TITLE: WINGS - CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM Oct 25, 2021 · N661FE · Airbus A300*SDR FDEA202110252609None · noneCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "I" HOLE FOUND CRACK SIGNAL COMPLIED WITH EO 6-5710-E0342809 B P1 STEP 5.D-5.E. TITLE: WINGS - CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM Oct 25, 2021 · N661FE · Airbus A300*SDR R61A2021102500825Doubler · crackedWHILE THE AC WAS ON HEAVY VISIT MAINTENANCE FOUND L/H WING LOWER SKIN CRACKED AROUND FASTENER 3.500" OTBD OF RIB 4A AND 3.250" AFT OF SPAR 2. REPAIRED L/H WING LOWER SKIN DOUBLER AND INTERNAL SPLICE AROUND FASTENER 3.500" OTBD OF RIB 4A AND 3.250" AFT OF SPAOct 25, 2021 · N137HQ · Emb ERJ170200LRSDR FDEA202110172555Former · crackedRIGHT HAND WING FIXED LEADING EDGE COMPARTMENT SUPPORT FORMER FOUND CRACKED AT STATION XOS 1025. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT CRACKED FORMER AT STATION XOS 1025 REMOVED AND REPLACED AS PER SRM 51-31-01-OG . FORMER FABRICATED AS PER DOUGOct 17, 2021 · N522FE · Doug MD11FSDR SWAA2021102031312Vapor Barrier · crackedR/H WHEEL WELL VAPOR BARRIER HAS A CRACK EXTENDING O/B + DOWN FROM RBL 45.64 3.5 INCHES LONG + 7.5 INCHES FROM BOTTOMACCOMPLISHED SEAL REPAIR IAW SRM 57-10-10-1A-2REPETITIVE ACTION REQUIREDMAKE SURE TAPE IS IN SATISFACTORY CONDITION AT EACH 600 FLIGHT CYCLES IOct 16, 2021 · N8326F · Boeing 7378H4SDR SWAA2021102031313Vapor Barrier · crackedR/H WHEEL WELL VAPOR BARRIER HAS A CRACK EXTENDING I/B + UP FROM RBL 45.64 1.0 INCH LONG + 16.0 INCHES FROM BOTTOMACCOMPLISHED INTERIM SEAL IAW SRM 57-10-10-1A-2REPETITIVE ACTION REQUIREDMAKE SURE TAPE IS IN SATISFACTORY CONDITION AT EACH 600 FLIGHT CYCLES INTOct 16, 2021 · N8326F · Boeing 7378H4SDR CALA2021101801909None · crackedCRACK FOUND ON CENTER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN RBL 40 TO RBL 45.64 (BETWEEN WL 200.6 AND 192.0) CRACK LENGTH : 0787" STA 663. (REF AAR NR 9635556) ACCOMPLISHED REPAIR AT CENTER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN RBL 40 TO RBL 45.6Oct 16, 2021 · N33262 · Boeing 737824SDR CALA2021101801899Bulkhead · crackedCRACK FOUND ON CENTER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN LBL 40.00 & LBL 45.64 ( BETWEEN WL 200.6 & 192.0 ) CRACK LENGTH : 1.575" REF. AAR N/R: 9635555 REMOVED DAMAGED AREA . FABRICATED NEW FILLER AND DOUBLERS. INSPECTED BY: V915555 INSTALLED NEW FILOct 15, 2021 · N33262 · Boeing 737824SDR SWAA2021101829129Bracket · crackedSUPPLEMENTAL INFORMATION: LEFT MAIN WHEEL WELL BRACKET CRACKED STA 663 ABOVE # 1 AFT BOOST PUMP ; / [01] REMOVED AND REPLACED BRACKET PER SRM 51-40-02Oct 12, 2021 · N477WN · Boeing 737SDR SWAA000029224None · crackedSUPPLEMENTAL INFORMATION: MAIN CABIN CENTER WING FLOOR SUPPORT BREAK CRACKED @ LBL-1 STA 540 MKD DOT ; / [01] REMOVED MAIN CABIN CENTER WING FLOOR SUPPORT BRACKET LBL-1 STA 540. IAW B 737-7 SRM 51-40-02.; [02] LOCATED AND DRILLED NEW FLOOR SUPPORT . IAW B 737-Oct 12, 2021 · N777QC · Boeing 737SDR SWAA2021112929225None · crackedMAIN CABIN CENTER WING FLOOR SUPPORT BREAK CRACKED @ FASTENER TAIL RBL-1 ; STA 540 MKD DOT ; / [01] REMOVED MAIN CABIN CENTER WING FLOOR SUPPORT BRACKET RBL-1 STA 540. IAW B 737-7 SRM 51-40-02.; [02] LOCATED AND DRILLED NEW FLOOR SUPPORT. IAW B 737-7 SRM 51-40Oct 12, 2021 · N777QC · Boeing 7377H4SDR SWAA2021111828877None · crackedLOWER FUSELAGE CENTER WING L/H AIR CONDITIONING EXHAUST AIR EXIT SEAL RETAINER CRACKED @ INB. SIDE ;STA 663.75 MKD DOT ; / [01] REMOVED PREVIOUS REPAIR FOR ACCESS AT LOWER FUSELAGE CENTER WING L/H AIR CONDITIONING EXHAUST. PER SRM 51-40-02-0G-0; [02] REMOVED SOct 8, 2021 · N786SW · Boeing 737*SDR SWAA2021101227976Vapor Barrier · crackedFOUND 14' DIAGONAL CRACK IN VAPOR BARRIER LEFT W/W; FWD SPAR. ; FOUND 14' DIAGONAL CRACK IN VAPOR BARRIER LEFT WW; FWD SPAR. LBL 33.5; 4.5 DOWN FROM UPPER WEB TO LBL38..5 AND 5.25' UP FROM BOTTOM. / [01] PERFORMED SRM 57-10-10-1A-2 PARAGRAPH 2(C)(4)(A) STOP DROct 8, 2021 · N7748A · Boeing 7377BDSDR SWAA2021112927451Web · crackedSUPPLEMENTAL INFORMATION: CTR. WING REAR SPAR STA. 663; BWL 160;R/H LWR. GFRP WEB IS CRACKED BETWEEN RBL25.00 & RBL31.83. / FOUND PERMANENT METAL REPAIR AT FWD. FACE OF CTR. WING REAR SPER STA. 663 BWL 160 - 168R/H LWR. GFRP WEBRBL 25 & RBL 31.83. APPLIED SEALOct 6, 2021 · N777QC · Boeing 737SDR SWAA2021112927450Web · crackedCTR. WING REAR SPAR STA. 663; BWL 160;L/H LWR. GFRP WEB IS CRACKED BETWEEN LBL45.64 & LBL54.21. ; / [01] PREPARED PANEL (VAPOR BARRIER) FOR DRY PROCESS AS PER BOEING 737 SRM 51-70-04-2R-10; [02] VERIFIED STEP 1; [03] ACOMPLISHED DRY PROCESS (24 HRS) ON VAPOR BOct 6, 2021 · N777QC · Boeing 7377H4SDR R61A2021110100844Skin · crackedL/H WING LOWER SKIN CRACKED 16MM LONG AT FASTENER OTBD OF RIB 4A AND AFT OF SPAR 2 (HFEC VERIFIED). PERFORMED TEMPORARY REPAIR BY CUTOUT AND DOUBLER INSTALLATION ON L/H WING LOWER SKIN OTBD OF RIB 4A IN ACCORDANCE WITH, REF ETD2021-170-033505Oct 6, 2021 · N120HQ · Emb ERJ170200LRSDR SWAA2021111626860Web · crackedCRACK FOUND AT EXTERNAL WHEEL WELL WEB LOCATED AT RT SIDE STA 663 BETWEEN RBL 31.83 & RBL 40.00. CRACK LENGTH : 0.512'. / [01] INSTALLED EWIS PROTECTION AT EXTERNAL WHEEL WEB AT R/H SIDE STA 663 BETWEEN RBL 31.83 AND RBL 40.00 IN REFERENCE B-737 AMM20-60-07-91Oct 5, 2021 · N774SW · Boeing 737*SDR FDEA202110012445Support Angle · corrodedUPON REMOVAL OF LH WING, TRIALING EDGE, UPPER SKIN PANEL, DISCOVERED THE FORWARD LAND AT REAR SPAR HAD CORROSION. STARTED REMOVAL OF CORROSION AT T/E OF LEFT WING UPPER SKIN PANEL, BETWEEN WS 150-180 & WS 194.5 IAW SRM 57-20-01-1A. FOUND CORROSION EXTENDOct 1, 2021 · N958FD · Boeing 757236SDR IPXA2021102375250Washer · crackedINSPECTION TYPE:A300ROTO PROBE OF RH FR40 CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND DAMAGE IN MIDDLE HOLE.INSTALL WASHER 2 PER EA# A300-5710-81939-A , INSTALL ONLY.Sep 29, 2021 · N146UP · Airbus A300F4622RSDR IPXA2021102375249Washer · crackedINSPECTION TYPE:A300ROTO PROBE OF RH FR 40 CENETER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND DAMAGE IN MIDDLE HOLE.INSTALL WASHER 1 PER EA# A300-5710-81939-A , INSTALL ONLY.Sep 29, 2021 · N146UP · Airbus A300F4622RSDR IPXA2021102375248Bushing · crackedINSPECTION TYPE:A300ROTO PROBE OF RH FR 40 CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND DAMAGE IM MIDDLE HOLE.INSTALL BUSHING PER EA# A300-5710-81939-A, INSTALL ONLY.Sep 29, 2021 · N146UP · Airbus A300F4622RSDR IPXA2021102375247Bushing · crackedINSPECTION TYPE:A300ROTO PROBE OF RH FR 40 CENETER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND DAMAGE IN MIDDLE HOLE.INSTALL BUSHING PER EA3 A300-5710-81939-A,INSTALL ONLY.Sep 29, 2021 · N146UP · Airbus A300F4622RSDR IPXA2021102375246Bushing · crackedINSPECTION TYPE:A300ROTO PROBE OF RH FR 40 CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND DAMAGE IN MIDDLE HOLE.INSTALL BUSHING PER EO# A300-5710-81939-A,INSTALL ONLY.Sep 29, 2021 · N146UP · Airbus A300F4622RSDR SIMA20210928006Spar · crackedR/H WING OUTBD TIP SPAR 1 CRACKED (MARKED) (MAJOR REPAIR)-C/A-COMPLETE:RAR RH WING OUTBD TIP SPAR 1 IAW EMB-175 SRM 51-40-08, AND ERS-EJ-5700-1354. SEE WIPS AND TASK FOR DETAILS.Sep 28, 2021 · N221NN · Emb ERJ170200LRSDR SWAA2021102723735Bulkhead · crackedBS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 36, WL 154. REPAIRED IAW SRM 51-70-04-2R-10 PARA 4 STEPS C ; D & E.Sep 28, 2021 · N263WN · Boeing 7377H4
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