JASC 5100

Service difficulty reports · 4,244

Reports filed under 5100 · Standard Practices/Structures, 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 = '5100'
  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 CALA2022092602509None · noneRIGHT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7003} - PANEL 611CB FOIL TAPE MISSING AND DELAMINATED IN VARIOUS LOCATIONS. DAMAGE WITHIN LIMITS AS PER SRM-51-70-14-1A PARA 6. PERFORMED PERMANENT REPAIR AS PER SRM-51-70-14-2R-3 PARA 6 A- J COMPLIEDSep 26, 2022 · N787UA · Boeing 777SDR CALA2022092602508None · noneRIGHT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7003} - PANEL 611PB DISBONDED FOIL TAPE ALONG EDGE. DAMAGE WITHIN LIMITS AS PER SRM-51-70-14-1A PARA 6. PERFORMED PERMANENT REPAIR AS PER SRM-51-70-14-2R-3 PARA 6 A- J COMPLIED WITH INSPECTION REQUIRESep 26, 2022 · N787UA · Boeing 777SDR CALA2022092602507None · noneRIGHT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7003} - PANEL 611 FB HAS DISBONDED FOIL TAPE ALONG EDGES. DAMAGE WITHIN LIMITS. PERFORMED PERMANENT REPAIR AS PER SRM-51-70-14-2R-3 PARA 6 A- J COMPLIED WITH INSPECTION REQUIREMENTS FOR PERMANENT REPASep 26, 2022 · N787UA · Boeing 777SDR CALA2022092602506Panel · tornLEFT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7002} - LFT WING FIXED LEADING EDGE PANEL 116W2502 ABOVE ISS 281 TORN. DAMAGE WITHIN LIMITS AS PER SRM-51-70-14-1A PARA 6. PERFORMED PERMANENT REPAIR AS PER SRM-51-70-14-2R-3 PARA 6 A- J ON LEFT WING ISep 26, 2022 · N787UA · Boeing 777SDR FDEA202209242717None · noneAGING AIRCRAFT ASSESSMENT:EXISTING DOUBLER REPAIR FOUND ON RH WING #1 SPOILER UPR SKIN I/B EDGE MID SECTION. REMOVED THE UNDOCUMENTED EXISTING DOUBLER REPAIR ON RH #1 SPOILER UPR SKIN I/B EDGE AERA AND PERFORMED NEW REPAIR WITH PRE-CURED CFRP DOUBLER I.A.WSep 24, 2022 · N650FE · Airbus A300F4605RSDR FDEA202209242716None · noneAGING AIRCRAFT ASSESSMENT:EXISTING DOUBLER REPAIR FOUND ON RH WING #1 SPOILER UPR SKIN O/B EDGE MID SECTION. REMOVED THE UNDOCUMENTED EXISTING DOUBLER REPAIR ON RH #1 SPOILER UPR SKIN O/B EDGE AERA AND PERFORMED NEW REPAIR WITH PRE-CURED CFRP DOUBLER I.A.WSep 24, 2022 · N650FE · Airbus A300F4605RSDR K11A2022092400166None · noneMASTER CAUTION ENGINE LIGHT ON TAKEOFF ROLL, NUMBER 2 ENGINE BIRD STRIKE, ENGINE NORMAL PARAMETERS. PERFORMED CONDITIONAL INSPECTION IAW B737 AMM 05-51-18 AND 71-00-00. NO DEFECTS NOTED, NO FURTHER ACTION IS REQUIRED AT THIS TIMESep 24, 2022 · N318FL · Boeing 7378SDR IPXA2022100686899None · noneINSPECTION TYPE:SEG3DURING INSPECTION PER EO B757-5310-73926-A FOUND AN EXISTING REPAIR AT STA 1320 S26R-S25RACCOMPLISHED PER EO B757-5310-84517-A AND VT MAE EA 757-5360-27-A3044 REV-Sep 23, 2022 · N446UP · Boeing 75724APFSDR IPXA2022100486840None · noneINSPECTION TYPE:SEG3DURING INSPECTION PER EO B757-5310-73926-A FOUND AN EXISTING REPAIR AT STA 1280 S26R-S25RACCOMPLISHED ALTERNATE INSPECTION PER UPS EO B757-5310-33992-C AND VT MAE EA 757-5360-27-A3043 REV-Sep 23, 2022 · N446UP · Boeing 75724APFSDR CALA2022092302488None · nonePANAL 511AB NEEDS ALUMINUM FOIL TAPE REPAIR IAW AMM TASK 51-27-01-340-801 IN COMPLIANCE WITH SRM 51-70-14-2R AND RII CLEAR TO INSTALL REPAIR IN COMPLIANCE WITH REF SRM 51-70-14-2R-3 AND RII. CLEAR REPAIR TO INSTALL PANAL 511AB TAPE AND ADHESIVE REMOVED IN REF.Sep 23, 2022 · N784UA · Boeing 777SDR CALA2022092302486None · nonePANAL 511MB NEEDS ALUMINUM FOIL TAPE REPAIR IAW AMM TASK 51-27-01-340-801 IN COMPLIANCE WITH SRM 51-70-14-2R AND RII CLEAR TO INSTALL ACP RII INSPECTION OF REPAIR AND EDGE SEAL OK TO INSTALL PANEL REPAIR PANEL TAPE AND ADHESIVE REMOVED IN REFERENCE WITH SRM ASep 23, 2022 · N784UA · Boeing 777SDR CALA2022092302485None · nonePANAL 511LB NEEDS ALUMINUM FOIL TAPE REPAIR IAW AMM TASK 51-27-01-340-801 IN COMPLIANCE WITH SRM 51-70-14-2R AND RII CLEAR TO INSTALL ACP RII INSPECTION OF REPAIR AND EDGE SEAL OK TO INSTALL PANEL REPAIR REMOVED OLD TAPE AND CLEANED PANEL. AWAITING INSPECTIONSep 23, 2022 · N784UA · Boeing 777SDR CALA2022092302484None · nonePANAL 511NB NEEDS ALUMINUM FOIL TAPE REPAIR IAW AMM TASK 51-27-01-340-801 IN COMPLIANCE WITH SRM 51-70-14-2R AND RII CLEAR TO INSTALL ACP RII INSPECTION OF REPAIR AND EDGE SEAL OK TO INSTALL PANEL REPAIR PANEL TAPE AND ADHESIVE REMOVED IN REFERENCE WITH SRM ASep 23, 2022 · N784UA · Boeing 777SDR CALA2022092302483None · nonePANAL 511EB NEEDS ALUMINUM FOIL TAPE REPAIR IAW AMM TASK 51-27-01-340-801 IN COMPLIANCE WITH SRM 51-70-14-2R AND RII CLEAR TO INSTALL ACP RII INSPECTION OF REPAIR AND EDGE SEAL OK TO INSTALL PANEL REPAIR PANAL TAPE AND ADHESIVE REMOVED IN REFERENCE WITH SRM PSep 23, 2022 · N784UA · Boeing 777SDR CALA2022092302481None · noneLEFT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7002} - PANEL 511 DB CONDUCTIVITY TAPE NEEDS REPAIR CLEARED TO APPLY CONDUCTIVE TAPE REPAIR. ACCOMPLISHED INSPECTION OF TAP APPLICATIO IAW SRM 51-70-14-2R-3 PARA 6 REMOVED DAMAGED ALUMINIUM FOIL TAPE OSep 23, 2022 · N228UA · Boeing 777SDR CALA2022092302480None · noneLEFT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7002} - PANEL 511 FB CONDUCTIVITY TAPE NEEDS TO BE REPAIR CLEARED TO APPLY CONDUCTIVE REPAIR TAPE REPAIR IS A MAJOR REPAIR REMOVED DAMAGED ALUMINUM FOIL TAPE ON PANEL 511 FB. REQUIRES INSPECTION PRIOR Sep 23, 2022 · N228UA · Boeing 777SDR CALA2022092302479None · noneLEFT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7002} - PANEL 511 NB CONDUCTIVITY TAPE NEEDS TO BE REPAIR. REPAIR IS A MAJOR REPAIR CLEARED TO APPLY CONDUCTIVE TAPE REPAIR REMOVED DAMAGED TAPE. CLEANED PANEL. REF SRM 51-70-14-2R-3. APPLLIED CONDUCTISep 23, 2022 · N228UA · Boeing 777SDR CALA2022092302478None · noneLEFT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7002} - PANEL 511 JB CONDUCTIVITY TAPE NEEDS TO BE REPAIR. REPAIR IS A MAJOR REPAIR CLEAR TO INSTALL TAPE AND SEAL. REMOVED AND CLEANED ADHESIVE IN PANEL 511JB, REQUIRES RII INSPECTION PRIOR TO PERMANESep 23, 2022 · N228UA · Boeing 777SDR CALA2022092302477None · noneLEFT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7002} - PANEL 511 GB CONDUCTIVITY TAPE NEEDS TO BE REPAIR REPAIR IS A MAJOR REPAIR CLEARED TO INSTALL TAPE IAW SRM 51-70-14 2R3. ACCOMPLISHED INSPECTION OF REPAIR APPLICATION IAW SRM 51-70-14-2R-3. CLESep 23, 2022 · N228UA · Boeing 777SDR CALA2022092302476None · noneLEFT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7002} - PANEL 511 EB CONDUCTIVITY TAPE NEEDS TO BE REPAIR. REPAIR IS A MAJOR REPAIR CLEARED TO APPLY CONDUCTIVE TAPE REPAIR ACCOMPLISHED INSPECTION OF TAP APPLICATION IAW SRM 51-70-14-2R-3 .STEP 6 REMOSep 23, 2022 · N228UA · Boeing 777SDR CALA2022092302474None · noneLEFT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7002} - PANEL 511 HB CONDUCTIVITY TAPE NEEDS TO BE REPAIR. CLEARED TO APPLY CONDUCTIVE REPAIR TAPE INSPECTED TAPE AND SEALANT APPLICATION IAW SRM 51-70-14 2R3. CLEAR TO INSTALL. REPAIR IS A MAJOR REPAISep 23, 2022 · N228UA · Boeing 777SDR CALA2022092302451None · corrodedFWD CABIN, FR16, Y765/Y254, AREA WITH CORROSION AND SCRATCHES. REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW A-319 SRM 51-42-11/0 01. RECEIVED NEW FLOOR SUPPORT P/N = 5311282600200 B/N = 0003993 146 WORK ACCOMPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 37Sep 23, 2022 · N841UA · Airbus A300*SDR CALA2022092302473None · noneRII INSPECTION REQUIRED RII INSPECTION REQUIRED REF LP 9585915 AND LP 9579571 PANEL 511QB WAS INSTALLED AFTER REPAIR WITHOUT INSPECTION. REPAIR WAS A MAJOR REPAIR AND REQUIRES INSPECTION RII. CLEARED TO INSTALL REPAIR IAW SRM 51-70-14-2R-3 STEP 6 . REMOVED DAMSep 23, 2022 · N228UA · Boeing 777SDR CALA2022092302471None · noneLEFT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7002} - PANEL 511 KB CONDICTIVITY TAPE NEEDS TO REPAIR REPAIR IS A MAJOR REPAIR CLEARED TO APPLY NEW CONDUCTIVE TAPE INSPECTED TAPE AND SEALANT APPLICATION IAW SRM 51-70-14 2R3. CLEARED TO INSTALL REPASep 23, 2022 · N228UA · Boeing 777SDR CALA2022092302470None · noneLEFT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7002} - PANEL 511 CB CONDUCTIVITY TAPE NEEDS TO BE REPAIR. CLEARED TO APPLY CONDUCTIVE TAPE REPAIR ACCOMPLISHED REPAIR INSPECTION IAW SRM 51-70-14-2R-3 STEP 6. CLEARED TO INSTALL . REPAIR IS A MAJOR RESep 23, 2022 · N228UA · Boeing 777SDR CALA2022092302469None · noneLEFT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7002} - PAMEL 511 MB CUNDUCTIVITY TAPE NEEDS TO BE REPAIR REPAIR IS A MAJOR REPAIR CLEARED TO APPLY CONDUCTIVE TAPE REPAIR IAW SRN 51-70-14-2R-3 STEP 6 CLEANED ADHESIVE FROM EFFECTED AREA ON PANEL 511MSep 23, 2022 · N228UA · Boeing 777SDR CALA2022092302468None · noneLEFT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7002} - PANEL 511 LB CONDUCTIVITY TAPE NEEDS TO BE REPAIR REPAIR IS A MAJOR REPAIR CLEARED TO APPLY CONDUTIVE REPAIR TAPE INSPECTED TAPE REPAIR AND SEALANT APPLICATION IAW SRM 51-70-14 2R3. CLEAR TO INSep 23, 2022 · N228UA · Boeing 777SDR 2023FA0000356Unknown · unknownAIRCRAFT HAD BEEN PERFORMING MANEUVERS FOR 30 MINUTES. UPON APPROACH TO THE RUNWAY AT LOW ALTITUDE THE ENGINE BEGAN TO SPUTTER AND QUICKLY SHUT DOWN. PILOT MADE AN EMERGENCY LANDING ON A HIGHWAY. I HAVE DETERMINED THE CAUSE TO BE EXCESSIVE HEATING OF THE FUEL Sep 22, 2022 · N495TC · Gulstm 114TCSDR FDEA202209222741None · noneCTR CARGO COMPT - FRAME AT STA 1661 L48R REQUIRED TO BE SPLIT FOR ACCESS TO LONGERON REPAIR.(REF. N649) SPLIT AND SPLICED FRAME AT STA 1661 BETWEEN L48R & L47R REF MD-11 SRM 53-00-07-2R, REAPIR #4 AND EA# 1-5350-T0370855 TITLE: FUSELAGE -AFT INTERMEDIATE SSep 22, 2022 · N591FE · Doug MD11FSDR CALA2022091902414Beam · corrodedAFT CABIN, FR68/FR70, Y1160, BEAM CORRODED. EVALUATED BEAM LONGITUDUAL CORROSION AND FOUND OUT OF LIMITS I.A WORK ACCOMPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 373 .W SRM 51.74-11; REMOVED AND REPLACED BEAM-LONGITUDUAL AND HARD 10 POINT AT AFT CABIN Sep 19, 2022 · N841UA · Airbus A300*SDR CALA2022091902407Beam · corrodedAFT CABIN, FR68/FR70, Y1160, BEAM CORRODED. EVALUATED BEAM LONGITUDUAL CORROSION AND FOUND OUT OF LIMITS I.A WORK ACCOMPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 373 .W SRM 51.74-11; REMOVED AND REPLACED BEAM-LONGITUDUAL AND HARD 10 POINT AT AFT CABIN Sep 18, 2022 · N841UA · Airbus A300*SDR FDEA202209172350None · noneAGING AIRCRAFT ASSESSMENT : EXISTING UPR FLANGE REPAIR FOUND ON FWD CARGO COMPARTMENT FLOOR CROSSBEAM AT FR 35, BTW Y140~Y805. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF ESep 17, 2022 · N742FD · Airbus A300*SDR IPXA2022091786342Longeron · corrodedINSPECTION TYPE:3CAFT CARGO LOWER BILGE LONGERON 52 STA 1946 TO STA 1957 IS CRACKEDREMOVED AND REPLACED AFT CARGO LOWER BILGE LONGERON 52 FROM STA 1946 TO STA 1964 PER MD11 SRM 51-31-01 AND DWG# AGA3092, DWG AGA7416.Sep 17, 2022 · N293UP · Boeing 737SDR CALA2022091902405Frame · crackedRH FWD OVER WING DOOR INTERNAL FRAME IS CRACKED ON HAECO LCQ REF 9290377/40377 SPEC A3NB-52-4-6031. NR GENERATED BY V892442 REMOVED AND REPLACED CRACKED INTERNAL FRAME ON RH FWD OVERWING DOOR.Sep 16, 2022 · N417UA · Airbus A300*SDR F3LA2022101100133Frame · mechanic errorFRAME 69, S23L HAS DOUBLE DRILLED HOLES. REMOVED AND REPLACED FRAME 69 BETWEEN STRINGER 15 TO STRINGER 29 IAW SRM 51-42-11Sep 15, 2022 · N207FR · Airbus A320214SDR CALA2022091402346None · corroded(A3NB) AFT CABIN, LEFT PAX DOOR SILL, FR68, AREA CORRODED. DOT 8 8-037. REMOVED CORROSION IAW SRM 51-74-00-01. AREA FOUND TO BE OUT OF L IMITS IAW SRM 53-41-14-283-002. REPAIRED AREA IAW SRM 53-41-14-3 00-001 WORK ACCOMPLISHED AT ST ENGINEERING OF MOBILE AT BFSep 14, 2022 · N841UA · Airbus A300*SDR FDEA202209132342None · noneAGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON AFT CARGO COMPARTMENT FLOOR CROSSBEAM AT FR 58, BTW Y805~Y1470. COMPLIED WITH ATTACH MENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE:A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMR)TRK,INSPECTION OF EXISTISep 13, 2022 · N742FD · Airbus A300*SDR FDEA202209132341None · noneAGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON AFT CARGO COMPARTMENT FLOOR CROSSBEAM AT FR 59, BTW Y805~Y1470. COMPLIED WITH ATTACH MENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE:A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMR)TRK,INSPECTION OF EXISTISep 13, 2022 · N742FD · Airbus A300*SDR CALA2022091402355Beam · corroded(A3NB-53-3-6187) AFT CABIN, FR68/FR70, Y-464.8 BEAM CORRODED. DO T 88-043 CORROSION AT BEAM - LONGITUDINAL AND FOUND OUT OF LIMITS I.A.W S WORK ACCOMPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 373 RM 51-74-11, REMOVED AND REPLACED BEAM LONGLONGITUDINAL Sep 12, 2022 · N841UA · Airbus A300*SDR CALA2022091402354Beam · corroded(A3NB-53-36102) FWD CABIN, FR20, BEAM NEXT TO Y-254 CORRODED, DO T 88-035 REPLACED FLOOR BEAM AT Y-189 BETWEEN FR20 TO FR24 I.A.W A319 SRM 51-42-11 WORK ACCOMPLSHED AT ST ENGINEERING OF MOBILE AT BFM ON N/R# 37300Sep 12, 2022 · N841UA · Airbus A300*SDR IPXA2022091286157None · noneINSPECTION TYPE:SEG3DURING ACCOMPLISHMENT OF EO B757-5310-73926-A FOUND AN EXISTING FRAME REPAIR AT STA 1240 R/HACCOMPLISHED REPAIR PER EA 757-5360-27-A3012 REV-Sep 12, 2022 · N441UP · Boeing 75724APFSDR FDEA202209112284None · noneEXISTING REPAIR AT LOWER FUSELAGE SKIN RIGHT HAND SIDE STATION 1191 BETWEEN LONGERON 46 RIGHT TO LONGERON 47 RIGHT REQUIRES REPLACEMENT (REFER M MOD NUMBER : SRM000078194N90 & WRI 53102005) LOWER FUSELAGE SKIN RIGHT HAND SIDE STATION 1191 BETWEEN LONGEROSep 11, 2022 · N616FE · Doug MD11FSDR CALA2022091202337Door Sill · corroded(A3NB) AFT CABIN, LEFT PAX DOOR SILL, FR68, AREA CORRODED. DOT 8 8-037.Sep 11, 2022 · N841UA · Airbus A300*SDR CALA2022090702304Seat Track · corroded(A3NB-53-3-6187) AFT CABIN, FR67/FR69, Y-1292, SEAT TRACK CORROD ED. DOT 88-041() REMOVED AND REPLACED FLOOR BEAMS FR66 TO FR69 RH -Y1292 IAW SRM 51-21-11 AND APPLIED TOP COAT IAW SRM 51-23-11. EMP# V936136 WOR 51-42-11, RECEIVED 2EA FLOOR BEAM BN: 0003916252 Sep 6, 2022 · N841UA · Airbus A300*SDR VNAA2022090399914Fitting · corrodedL/H JACK FITTING WEB IS CORRODED/CRACKED. REMOVED AND REPLACED NOSE JACK FITTING AND LH + RH INTERCOSTALS IAW CRJ-700 SRM 51--42-06-001-001-A01 AND 51-42-21-001-001-A01Sep 3, 2022 · N531EG · Bombdr CL6002D15SDR VNAA2022090399912Skin · damagedLEFT HAND SIDE EXTERNAL FUSELAGE AT APPROX FS360.00 JUST FWD OF THE EXTERNAL EMERGENCY LIGHT AND AFT OF PAX DOOR HAS LIGHT SCRATCHES VISIBLE. L/H SIDE EXTERNAL FUSELAGE AT APPROX. F.S360.00 JUST FWD OF THE EXTERNAL EMERGENCY LIGHT AND AFT OF PAX DOOR LIGHT SSep 3, 2022 · N531EG · Bombdr CL6002D15SDR VNAA2022090399911Frame · corrodedFRAME CORRODED AT FS 969.00 BETWEEN STGR 25L AND 26R. REPAIRED CORROSION FRAME 969.00 STGR 25L - 26R IAW EA 22-C7-53-0968 REV IR DATED 08/09/2022. DTE TO BE ACCOMPLISHED WITHIN 12 MONTHS OF THE RETURN TO SERVICE DATE FOR THE SECTION III REPAIR IN ACCORDANCE WSep 3, 2022 · N531EG · Bombdr CL6002D15SDR VNAA2022090399910Joint · corrodedFS 280.00 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STGR 24L AND 23R. REPAIRED IAW OLIVER-WYMAN EA # 22-C7-53-0967 REV IR DATED 8/2/2022Sep 3, 2022 · N534EG · Bombdr CL6002D15SDR VNAA202209039999Intercostal · corrodedAVI BAY DOOR INTERCOSTAL IS CORRODED BETWEEN STGR 27 TO 26R. INSTALLED NEW INTERCOSTAL AT STGR 27 - 26R FWD ON AVI BAY DOOR IAW CRJ700 SRM 51--42-06-001-001-A01Sep 3, 2022 · N531EG · Bombdr CL6002D15SDR VNAA202209039998Intercostal · corrodedL/H AVI DOOR INTERCOSTAL BETWEEN STGR 27 TO STGR 26L IS CORRODED. REMOVED AND INSTALLED NEW INTERCOSTAL AT LH AVI DOOR BETWEEN STGR 27 AND STGR 26L IAW CRJ700 SRM 51-42–06-001-001-A01 AND SRM 51-42-21-001-001-A01Sep 3, 2022 · N531EG · Bombdr CL6002D15
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