JASC 5530

Service difficulty reports · 2,534

Reports filed under 5530 · Vertical Stabilizer, 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 = '5530'
  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 IPXA2021111575994None · noneINSPECTION TYPE:CTHE VERT. STAB. UPR FWD TORQUE BOX PANEL HAS A DISBONDED DENT AT FSS 321.046 ON THE L/H SIDE.REPAIRED PANEL IAW B757 SRM 51-70-07-0G PER SRM 55-30-01-2R-4Nov 7, 2021 · N405UP · Boeing 75724APFSDR IPXA2021110175502Rib · crackedINSPECTION TYPE:SEG3RH VERT STAB RIB #1 CHORD FWD END HAS A CRACK.REPAIRED PER UPS EO B757-5530-82018-A AND VT MAE EA 757-5530-27-A2732 REV -Nov 1, 2021 · N435UP · Boeing 75724APFSDR CALA2021102001925None · noneREF L/P 7147131 DAMAGE TO LHS UPPER SKIN SPAR AND LHS SPAR CHORD C/W STEPS 3-4-5 OF AVO9186. STEP 1 OF AVO 9186 PCW ON L/P 7147131 PERFORMED STEPS 3, 4 AND 5 OF AVO 9186. DAMAGE REMOVED ON SKIN ACCOMPLISHED EXTERNAL INSPECTION OF THE IMPACTED AREA AND 20 ACCOOct 18, 2021 · N76519 · Boeing 737824SDR IPXA2021102675335None · crackedINSPECTION TYPE:3CVERTICAL STABILIZER #4 BANJO FITTING R/H SIDE IS CRACKED.REPAIRED CRACKED VERTICAL STABILIZER #4 BANJO FITTING R/H SIDE IAW VT-SAA EA 011-5530-01-A9386 REV. I/R AND UPS EO MD11-5530-81955-A. (MAJOR) REF FAA FORM 8100-9 BY J. TOM (AR-605565) DOct 13, 2021 · N259UP · Doug MD11FSDR FDEA202109292427Intercostal · crackedEMPENNAGE - LOWER VERTICAL STABILIZER , LEFT HAND REAR CENTER SPAR TO REAR SPAR INTERCOSTAL AT STATION Y = 2164 FOUND CRACKED. EMPENNAGE - LOWER VERTICAL STABILIZER , LEFT HAND REAR CENTER SPAR TO REAR SPAR INTERCOSTAL AT STATION Y = 2164 REPAIR CARRIED OUSep 29, 2021 · N624FE · Doug MD11FSDR SWAA2021110122961Support Angle · crackedCRACK VERTICAL STAB LEADING EDGE SUPPORT ANGLE, BS 1016. REMOVED SUPPORT ANGLE AND PLATE IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON AREA AND NO DAMAGE FOUND. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, AND DWG 176A3101 REV -.Sep 24, 2021 · N420WN · Boeing 7377H4SDR SWAA2021110119231Drag Brace · corrodedCORRODED OTB DRAG BRACE ON VERTICAL STABILIZER. REMOVED THE DRAG BRACE IAW SRM 51-40-02, DRILLED NEW DRAG BRACE IAW SRM 51-40-05. APPLIED PROTECTIVE TREATMENT ON HOLES IAW SRM 51-20-01. INSTALLED THE NEW DRAG BRACE AND FASTENERS IAW SRM 51-40-02, AND DWG 1Sep 19, 2021 · N414WN · Boeing 7377H4SDR SWAA2021110119221Drag Brace · corrodedCORROSION O/B DRAG BRACE AFT LH SIDE ON VERTICAL STABILIZER. MEASURES OF CORROSION ARE L: 0.665 INCH; W: 0.607 INCH; D: 0.045 INCH. REMOVED DRAG BRACE IAW SRM 51-40-02 DUE TO NO FOUND ALLOWABLE DAMAGE LIMITS IN SRM. PERFORMED VISUAL INSPECTION ON ADJACENTSep 18, 2021 · N414WN · Boeing 7377H4SDR SWAA2021110920597None · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT FRON SPAR FITTINGS CORROSION ; / [01] REMOVED BUSHINGS AT VERTICAL STABILIZER CENTER SECTION LEFT FRONT SPAR AS PER B737-700 SOPM 20-50-03; [02] REMOVED CORROSION AT VERTICAL FIN LT FITTING REF B737-7 SSep 16, 2021 · N783SW · Boeing 737*SDR SWAA2021110920604Fitting · corrodedVERTICAL STABILIZER LEFT I/B REAR SPAR FITTINGS CORRODED. REMOVED BUSHINGS AT LEFT VERTICAL STABILIZER I/B REAR SPAR AS PER B737-700 SOPM 20-50-03, AFTER BUSHING REMOVAL, INSPECTED AREA, NO CORROSION FOUND. INSTALLED SERVICEABLE BUSHINGS SOPM 20-50-03 AND Sep 16, 2021 · N783SW · Boeing 7377H4SDR SWAA2021110920600Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT I/B REAR SPAR FITTINGS CORROSION ; / [01] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q006KMKF; [02] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q006KMKFSep 16, 2021 · N783SW · Boeing 737*SDR ASMF202110020None · noneDURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED SEVERAL LIGHTNING STRIKES ON RUDDER SKIN TRAILING EDGE. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION PHASE 1A, LEVEL EXAMINATION AND PHASE 1B AND II, GENERAL VISUAL INSPECTION Sep 10, 2021 · N115AM · Boeing 7379SDR HNAA2021100600478None · noneE879202 - RIGHT HAND VERTICAL STABILIZER SPHERICAL BEARING HOLE IS ENLARGED PAST ORIGINAL DIAMETER NEED TO BE ENLARGED TO FIRST OVERSIZE. .... RIGHT HAND VERTICAL STABILIZER SPHERICAL BEARING HOLE IS ENLARGED TO FIRST OVERSIZE IAW PIEDMONT EO1-55-21-0248.Sep 4, 2021 · N636AE · Emb EMB145LRSDR SWAA2021100512726Drag Brace · corrodedCORROSION FITTING DRAG BRACE LH O/B FWD AT VERTICAL STABILIZER ; 2021-393030 / REPLACED FITTING DRAG BRACE LH O/B FWD AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND EA 21-153-02670 AND REPLACED FITTING DRAG BRACE R/H O/B FWD AT VERTICAL STABILIZERAug 28, 2021 · N7859B · Boeing 7377Q8SDR SWAA2021100512727Drag Brace · corrodedCORROSION FITTING DRAG BRACE RH O/B FWD AT VERTICAL STABILIZER ; 2021-393032 / [01] TOOK MEASURE OF CORROSION ARE : L:0.601 INCH ; W:0.429 INCH ; D:0.041 INCH LOC. ON FITTING DRAG BRACE RH O/B FWD AT VERTICAL STABILIZER ; TOOL USED SOLAR POWER CALIPER P/N:500-Aug 28, 2021 · N7859B · Boeing 7377Q8SDR SWAA2021100512725Drag Brace · corrodedCORROSION FITTING DRAG BRACE LH O/B AFT AT VERTICAL STABILIZER ; 2021-393031 / [01] TOOK MEASURE OF CORROSION ARE : L : 0.378 INCH ; W : 0.195 INCH ; D : 0.078 INCH LOC. ON FITTING DRAG BRACE LH O/B AFT AT VERTICAL STABILIZER ; TOOL USED : SOLAR POWER CALIPER Aug 28, 2021 · N7859B · Boeing 7377Q8SDR SWAA2021101110602None · delaminatedDELAMINATION FOUND ON REPAIR AREA UPPER AND LOWER ON ACCESS PANEL 322B LEADING EDGE. REMOVED REPAIR PLIES AND PREPARED REPAIR AREA IAW SRM 51-70-04-2R-10, REPAIR 10, PARAGRAPH 4. B; C. INSTALLED A NEW REPAIR IAW SRM 51-70-04-2R-10, REPAIR 10, PARAGRAPH 4. CAug 25, 2021 · N415WN · Boeing 7377H4SDR SWAA2021091312126Retainer · crackedVERTICAL STAB PANEL 324AL RETAINER CRACKED ; / [01] REMOVED AND REPLACED VERTICAL STAB PANEL 324AL RETAINER IAW SRM 51-40-02-0G-0 STEP 4 AND DRAWING 172A6123; [02] VERIFIED REMOVED AND REPLACED VERTICAL STAB PANEL 324AL RETAINER IAW SRM 51-40-02-0G-0 STEP 4 ANAug 25, 2021 · N966WN · Boeing 7377H4SDR DALA2021082404988Bearing · corrodedSHIP 3170 - CORROSION BEARING HINGE ARM 5 ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPLACED HINGE FITTING #5 AND FASTENERS LOC. ON VERTICAL STABILIZER AS PER SRM 55-36.(1917794)Aug 19, 2021 · N370NB · Airbus A319114SDR DALA2021082404987Hinge Fitting · corrodedSHIP 3170 - CORROSION ON BORE OF HINGE #1 OF VERTICAL STABILIZER. CORRECTIVE ACTION: REPLACED HINGE FITTING #1 AND FASTENERS LOC. ON VERTICAL STABILIZER AS PER A319 SRM 55-36.(1917792)Aug 19, 2021 · N370NB · Airbus A319114SDR V0XD2021819001Drag Angle · crackedVERTICAL STABILIZER L/H AFT DRAG ANGLE IS CRACKED. CORRECTIVE ACTION: REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW BOMBARDIER REO 670-55-31-018 REV. A DATED 2016-11-10, AND REO 53-31-063 REV. -- DATED 2021-08-18.Aug 19, 2021 · N249LR · Cndair CL6002D24SDR FDEA202108152424Doubler · wornAFT FUSELAGE; 311AB DOOR LAND WORN THRU SKIN @ LH AFT LATCH CONTACT POINT. DOT #11 REPAIRED PER EA 8-5330-T0364309.Aug 15, 2021 · N307FE · Doug MD1030FSDR SWAA2021091606984Fitting · corrodedVERTICAL STAB REAR SPAR RIGHT AFT O/B FITTING HAS FWD OB DRAG ANGLE WITH CORROSION IN BOLT HOLE. 8-71 ; / [01] REMOVED AT VERTICAL STABILIZER REAR SPAR RIGHT SIDE THE FWD OUTBOARD FITTING IN IAW SRM 51-40-02-0G-0; [02] PERFORMED ROTO INSP ON ALL OPEN HOLES AT Aug 12, 2021 · N413WN · Boeing 7377H4SDR SWAA2021081605677Skate Angle · chafedLEFT SIDE OF VERTICAL FIN FWD END OF LONG SKATE ANGLE IS CHAFED ON TOP OF FUSELAGE. SKATE ANGLE DAMAGED OUT OF LIMITS. VERIFIED : SKATE ANGLE DAMAGED OUT OF LIMITS. REMOVED L/H AFT SKATE ANGLE DRILLED AND COUNTERSUNK NEW L/H LONG AFT SKATE ANGLE IAW SRM 51-40Aug 11, 2021 · N292WN · Boeing 7377H4SDR REXA2021090900706Drag Angle · crackedL/H VERTICAL STABILIZER AFT DRAG ANGLE IS CRACKED. REMOVED LH AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01 AND 51-42-22-001-001-A01. LOCATED, DRILLED AND INSTALLED LH AFT DRAG ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-13-0Aug 10, 2021 · N348PQ · Cndair CL6002D24SDR REXA2021090900705Drag Angle · cracked"R/H VERTICAL STABILIZER AFT DRAG ANGLE IS CRACKED. REMOVED R/H AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01 AND 51-42-22-001-001-A01. LOCATED, DRILLED AND INSTALLED RH AFT DRAG ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-1Aug 10, 2021 · N348PQ · Cndair CL6002D24SDR SWAA2021080903274Angle · crackedCRACK ANGLE LOCATED INTERNAL AREA BS 1016 AT VERTICAL STABILIZER. REMOVED ANGLES & PLATES. LOC LEADING EDGE AT LEVEL BS 1016 AT VERTICAL STAB IAW SRM 51-40-02 & PERFORMED VISUAL INSPECTION ON AREA AND FOUND NO MORE DAMAGE. CRACK IS NOT ALLOWED ON SUPPORT ANAug 3, 2021 · N410WN · Boeing 7377H4SDR SWAA2021082300599Attach Bracket · corroded***CORROSION*** DORSAL FIN 321A AFT LT ATTACH BRACKET HAS CORROSION IN THE BOLT HOLE ; / [01] REMOVED LIGHT CORROSION AT DORSAL FIN 321AAFT LT ATTACH BRACKET IAW B737 AMZM 51 21 31 350 801; [02] VERIFIED STEP #1:OK TO TREAT AND PRIME; [03] TREATED AND PRIMED AJul 30, 2021 · N902WN · Boeing 7377H4SDR IPXA2021081072615Fastener · shearedINSPECTION TYPE:2CVERTICAL STABILIZER AFT SPAR #4 BANJO FITTING L/H AFT CARRY THROUGH CAP HAS 1EA SHEARED FASTENER.REPAIRED VERTICAL STABILIZER AFT SPAR #4 BANJO FITTING L/H AFT CARRY THROUGH CAP SHEARED FASTENER IAW UPS EO MD11-5530-46641-A APPENDIX B & D. (MJul 22, 2021 · N273UP · Doug MD11FSDR SWAA2021080396491Skate Angle · chafedCHAFE DAMAGE ON R/H VERTICAL STAB TO FUSELAGE FWD SKATE BS1006-1016 ; / [01] REMOVED R/H SKATE ANGLE IAW SRM 51-40-02; [02] LOCATED; DRILLED AND COUNTERSINK NEW L/H SKATE ANGLE P/N 147A32OOU12 IAW SRM 51-40-05;SRM 51-40-08 AND DWG 147A0030 REV. 0; [03] NO ALLOJul 19, 2021 · N962WN · Boeing 7377H4SDR SWAA2021080396493Skate Angle · chafedCHAFE DAMAGE ON L/H VERTICAL STAB TO FUSELAGE FWD SKATE BS1006-1016 ; / [01] REMOVED L/H SKATE ANGLE IAW SRM 51-40-02; [02] LOCATED; DRILLED AND COUNTERSINK NEW L/H SKATE ANGLE P/N 147A32OOU11 IAW SRM 51-40-05;SRM 51-40-08 AND DWG 147A0030 REV. 0; [03] NO ALLOJul 19, 2021 · N962WN · Boeing 7377H4SDR SWAA2021080394625Skate Angle · chafedCHAFE DAMAGE ON THE R/H VERTICAL STAB TO FUSELAGE SKATE ANGLES / [01] REMOVED R/H SKATE ANGLES IAW SRM 51-40-02; [02] LOCATED; DRILLED AND COUNTERSINK NEW L/H SKATE ANGLE P/N 148A8310U4 PO#823628 /1 IAW SRM 51-40-05;SRM 51-40-08 AND DWG 148A8300 REV.A; [03] NOJul 13, 2021 · N962WN · Boeing 7377H4SDR SWAA2021080394626Skate Angle · corrodedCHAFE DAMAGE ON THE L/H VERTICAL STAB TO FUSELAGE SKATE ANGLES / [01] REMOVED LH SKATE ANGLES PER SRM 51-40-02.; [02] LOCATED; DRILLED AND COUNTERSINK NEW L/H SKATE ANGLE P/N 148A8310U3 PO#829514 /1 IAW SRM 51-40-05;SRM 51-40-08 AND DWG 148A8300 REV.A; [03] NOJul 13, 2021 · N962WN · Boeing 7377H4SDR REXA2021071300497Drag Angle · crackedVERT. STAB LH AFT DRAG ANGLE CRACKED. REPAIRED VERTICAL STAB LH AFT DRAG ANGLE IAW CRJ900 SRM 55-31-00-201-001-A01.Jul 10, 2021 · N341PQ · Cndair CL6002D24SDR REXA2021071300496Drag Angle · crackedVERT. STAB RH AFT DRAG ANGLE CRACKED. REPAIRED VERTICAL STAB RH AFT DRAG ANGLE IAW SRM 55-31-00-201-001-A01.Jul 10, 2021 · N341PQ · Cndair CL6002D24SDR SWAA2021081992456Seal · crackedA22-78; VERTICAL STAB STA 1018; LBL & RBL10'; JUST ABOVE FWD SPAR ATTACH LUGS; WEB STIFFNER CRACKED @ LEFT & RIGHT SIDES @ STRAIN RELIEF CUTOUTS; MRK'D. ; / [01] REMOVED EXPANSION JOINT ASSY. IAW SRM 51-40-02-0G-0; [02] VERIFIED NEW SPRING SEAL AS P/N 176A3101Jul 7, 2021 · N941WN · Boeing 7377H4SDR SWAA2021073091642Spring · crackedVERTICAL STAB FIXED L/E SPRING P/N 176A3101-26 R/H SIDE HAS CRACK AT RADIUS DOT A-21-11 ; / [01] REMOVED CRACKED FIXED L/E -26 SPRING IAW SRM 51-40-02-0G.; [02] RECEIVED NEW PART P/N 176A3101U26; A-TAG AK7947; LOCATED AND DRILLED ALL HOLES TO SIZE AND DEBURREDJul 6, 2021 · N287WN · Boeing 7377H4SDR SIMA20210706002Stiffener · crackedVERTICAL STAB L/H SKIN TRAILING EDGE STIFFENER HAS CRACK AT MID SECTION (MAJOR REPIAR)-C/A-REPAIRED RH ENGINE YOKE FWD LOWERLINK IAW ERS-EM-54MR-698. VERTICAL STAB L/H SKIN TRAILING EDGE STIFFENER HAS CRACK AT MID SECTION (MAJOR REPIAR)-C/A-REPAIRED RH ENGINE Jul 6, 2021 · N925AE · Emb EMB145LRSDR SWAA2021080990310Support Angle · crackedDORSAL FIN TERMINATION FITTINGS LOWER SECTION; SUPPORT ANGLE CRACKED 2EA PLACES BS 1016 RBL-11.5 AND LBL-11.5 MAD 126-20. ; / [01] PERFORMED HFEC INSP. ON SUSPECTED CRACK IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. CRACK CONFIRMED <BR>TOOL: NORTEC 600 B/C:166Jul 1, 2021 · N561WN · Boeing 73773VSDR SWAA2021081188872Skate Angle · chafedRT VERTICAL FIN TO BODY SKATE ANGLE CHAFED BS 1016-1122 / [01] NO ALLOWABLE DAMAGE FOUNDED ON SRM REPLACED PART FOR REPAIR IAW SRM 51-10-02-0G-0; [02] REMOVED R/H SKATE ANGLE AT BS1016 TO BS1132 IAW SRM 51-10-02; [03] VERIFIED; [04] UPDATED MEASUREMENTS; [05] Jun 29, 2021 · N750SA · Boeing 7377H4SDR SWAA2021081188873Skate Angle · chafedRT VERTICAL FIN TO BODY SKATE ANGLE CHAFED BS 1013-1017 / [01] NO ALLOWABLE DAMAGE FOUNDED ON SRM REPLACED PART FOR REPAIR IAW SRM 51-10-02-0G-0; [02] REMOVED R/H SKATE ANGLE AT BS1006 TO BS1016 IAW SRM 51-40-02; [03] VERIFIED; [04] UPDATED MEASUREMENTS; [05] Jun 29, 2021 · N750SA · Boeing 7377H4SDR SWAA2021081188870Skate Angle · chafedLT VERTICAL FIN TO BODY SKATE ANGLE CHAFED BS 1016-1122 / [01] NO ALLOWABLE DAMAGE FOUNDED ON SRM REPLACED PART FOR REPAIR IAW SRM 51-10-02-0G-0; [02] REMOVED L/H SKATE ANGLE AT BS1016 TO BS1122 IAW SRM 51-40-02; [03] VERIFIED; [04] UPDATED MEASUREMENTS; [05] Jun 29, 2021 · N750SA · Boeing 7377H4SDR SWAA2021081188871Skate Angle · chafedLT VERTICAL FIN TO BODY SKATE ANGLE CHAFED BS 1014-1016 / [01] NO ALLOWABLE DAMAGE FOUNDED ON SRM REPLACED PART FOR REPAIR IAW SRM 51-10-02-0G-0M; [02] REMOVED L/H SKATE ANGLE AT BS1006 TO BS 1016 IAW SRM 51-40-02; [03] NO ALLOWABLE DAMAGE FOUNDED ON SRM REPLAJun 29, 2021 · N750SA · Boeing 7377H4SDR DALA2021062903566Hinge Fitting · corrodedSHIP 3161 - FOUND CORROSION ON HINGE ARM 1 OF BORE AFTER BEARING REMOVAL. CORRECTIVE ACTION: REPLACED HINGE FITTING #1 LOC ON VERTICAL STABILIZER AS PER SRM 55-36. (1853146)Jun 25, 2021 · N361NB · Airbus A319114SDR SWAA2021080487827Fitting · corrodedCORROSION ** AT VERTICAL STABILIZER REAR SPAR L/H AFT O/B HINGE FITTING AFT CLEVIS INTERNAL ; / [01] REMOVED FITTING AT VERTICAL STAB REAR SPAR L/H AFT O/B HINGE FITTING AFT CLOVIS INTERNAL IN IAW SRM 51-40-02-0G-0; [02] VERIFIED 1.; [03] PARTIALLY: STARTED DRJun 24, 2021 · N417WN · Boeing 7377H4SDR IPXA2021070171183Support Channel · crackedINSPECTION TYPE:2CVERTICAL STAB TO FUSELAGE SUPPORT CHANNEL AT YID 310.35 IS CRACKED.REMOVED AND REPLACED CRACKED VERTICAL STAB TO FUSELAGE SUPPORT CHANNEL AT YID 310.35 IAW SRM 51-35-01. (MINOR)Jun 22, 2021 · N296UP · Doug MD11FSDR SWAA2021072885931Support Web · crackedCRACK LEADING EDGE SUPPORT WEB LOCATED AT BS 1016 AT LEVEL S-2R AND 2L AT VERTICAL STABILIZER ; 2021-287875 / [01] REPLACED LEADING EDGE SUPPORT WEB LOCATED AT BS 1016 AT LEVEL S-2R AND 2L AT VERTICAL STABILIZER IAW B737-700 SRM51-10-2 TEM 9; SRM 51-40-02 AND Jun 18, 2021 · N7827A · Boeing 73779PSDR SWIA202161357None · cracked*RH VERTICAL STAB/FUSE DRAG ANGLE (AFT SECTION) HAS POSSIBLE CRACK (C-CHECK RO 9/27/2021) REPAIRED RH VERTICAL STAB/FUSE AFT DRAG ANGLE, REF CRJ 700 SRM 55-31-00-201-001-A01, COMPLIED WITH TASK CARD 51-900-1002-SKYJun 10, 2021 · N708EV · Cndair CL6002C10SDR FDEA202106091623Nut Plate · damagedNUMEROUS NUT PLATES DAMAGED INSIDE ZONE 316 R/H UPPER SIDE. AFTER FURTHER INSPECTION CORROSION WAS FOUND AND DETERMINED OUT OF LIMITS. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-20-00 #24 AND EA NO. 8-5330-T0362493. REPLACED NUT-PLATES IAW SRM 51-31-01Jun 9, 2021 · N306FE · Doug MD1030FSDR IPXA2021060470168Panel · delaminatedINSPECTION TYPE:SEGR/H LWR FWD TORQUE BOX PANEL HAS A SMALL DELAMINATION MARKED IN RED BELOW FSS 195.390REPAIRED PANEL IAW B757 SRM 51-70-07-OG 250 DEG F CURE PER SRM 57-20-09-2R PER SRM 55-30-01-2R-5Jun 4, 2021 · N475UP · Boeing 75724APF
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