Boeing 757-2B7

Service difficulty reports · 3,730

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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 aircraft_model_key = '7572B7'
  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 FDEA200910223645Skin · damagedAPU COMPARTMENT INTERNAL SKIN HAS UNIDENTIFIED HOLE ABOUT 3/8", BETWEEN FS 1918.9 & 1941, AT 1 (ONE) O'CLOCK POSITION. REMOVED APU COMP. SKIN FROM STA. 1918.9 TO 1941 TO FOM IAW SRM 51-40-02, REPAIR SKIN IAW SRM 51-70-10 AND REINSTALLED IAW SRM 51-40-02 ANOct 22, 2009 · N907FD · Boeing 7572B7 · APU Cowling/ContainmentSDR FDEA200910203619Crease Beam · corrodedSTA 1277- 1287 LT CREASE BEAM CORRODED. REMOVED CREASE BEAM IAW SRM 51-40-02, FABRICATED NEW BEAM FROM MAT BAC1515-5537075T6511, IAW SRM 51-30-01, INSTALLED CREASE BEAM STA 1180-1290, LBL 60, IAW SRM 51-40-02, MAJOR REPAIR.Oct 20, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA200910203618Floorbeam · corrodedBS 700 FLOORBEAM UPPER CAP CORRODED B/T LBL 45- LBL TO AT FS 700 B/T B/L 36.5 TO B/L 70 LT A FLOORBEAM REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE WC 118350502BZ2R02, AND EA 757-5335-16-F2279, REV B, DATED 10/06/2009. THIS Oct 20, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA200910203615Floor Support · corrodedMAIN DECK FLOOR SUPPORT STA 680-740 AND RBL 65 HAS SEVERAL AREAS OF CORROSION REMOVED CORRISION INBD CHORD STA 680-740, RBL 65 IAW SRM 53-30-13. MAT THICKNESS .190", MAT REMOVED .100", MAT REMAINING .090". FOUND OUT OF LIMITS IAW SRM 53-30-13, PG 102, FIG 10Oct 20, 2009 · N907FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA200910143573Floor Support · corrodedMAIN CABIN, STA 345-365, APROX BL0 FLOOR SUPPORT HAS CORROSION. BLENDED AREA IAW SRM 51-10-02 DAMAGE L=1" X W=1" X D .010 FOUND TO BE OUT OF LIMITS IAE SRM 52-00-51 DETAIL 2, REMOVED FLOOR SUPPORT BETWEEN STA 345-365 AND FABRICATED 2 EA SUPPORT BRACKETS OOct 14, 2009 · N907FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA200910143557Unknown · power lossWHEN SELECTING ACFT PWR (APU) ON THE GND, THE PWR SHIFT REJECTED THE APU PWR, THE APU FAULTED AND SHUTDOWN. QRH PROCEDURE FOLLOWED AND APU RESTARTED SUCCESSFULLY AND THE AC ACCEPTED THE APU PWR. AFTER TAKEOFF THEN BEGAN TO EXPERIENCE NUMEROUS ELECTRICAL ANOct 14, 2009 · N903FD · Boeing 7572B7 · AC Generation SystemSDR FDEA200910093530Floorbeam · misrepairedEXISTING FLOORBEAM UPPER CHORD REPAIR AT STA 740, LBL 58 WILL INTERFERE WITH INSTALLATION OF SECTION 43 SEAT TRACK NR 657N3332-2. REPAIR AT STA 740, LBL 58 WAS ACCOMPLSHED EFFECTING PTF CONVERSION ON MAE-MOD W/C 118350502BZR02 AND MAE EA 757-5365-16-F2265 REVOct 9, 2009 · N908FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA200910093529Attach Angle · failedEXISTING DUCT AND ALL ATTACHING ANGLES, CLIPS AND SSEMBLIES INTERFERE WITH INSTALLAATION OF E 7 RACK AT STA 1640-1681 STR. 26L-28L. AT STA. 1640 -1681 STR. 26L-28L- ASSEMBLIES WERE RELOCATED AND ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION Oct 9, 2009 · N908FD · Boeing 7572B7 · Fuselage Main, Attach FittingsSDR FDEA200910093528Floorbeam · noneEXISTING FLOORBEAM REPAIR INTERFERES WITH INSTALLATION OF DWG FASTENERS, AT F STA 740, RBL 58 AT STA 740, RBL 58 FLOORBEAM REPAIR ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MAE W/C 118350441BZR03, AND MAE EA 757-5335-16-F2266 REV B, DATED Oct 9, 2009 · N908FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA200910093527Frame · corrodedBULK CARGO COM, STA 1500 BETWEEN STR 28L-29L, WL 138 FRAME CORRODED AND HAVE MISSING SHEAR TIE. FRAME FOUND OUT OF LIMITS IAW SRM 53-60-07 FIG 101 DET 1, REMOVED 2 EA, INTERCOSTAL AND REINSTALLED IAW SRM 51-40-02. REMOVED AND REPLACED FRAME ASSY STA 1500 BETOct 9, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA200910083500Crease Beam · misalignedDURING INSTALLATION OF INNER CREASE BEAM CHORD AT STA 640, 2 EA EXISTING HOLES WERE FOUND THAT CANNOT BE PICKED UP. COMPLIED WITH EA 757-5331-16-F2284 AT STA 640, LBL 58, ON MAE WORK CARD 118350403BZ2R01. THIS NON ROUTINE IS FOR TRACKING PURPOSES ONLY. (MAJOOct 8, 2009 · N908FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA200910083513Skin · dentedNR 2 PYLON PNL 443 BR LAND SKIN DENTED COMPLIED WITH EA F-5450-131126 DATED 10/07/09, PYLON NR 2 ENG STRUT SIDE SKIN DAMAGE REPAIR , THIS A MAJOR "A " REPAIR NO FOLLOW-UP INSP REQUIRED.Oct 8, 2009 · N907FD · Boeing 7572B7 · Nacelle/Pylon, Plate/SkinSDR FDEA200910083511Crease Beam · corrodedLBL 62 FLOORBOARD SUPPORT FS, 395-377 CORRODED REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MAT .050 MAT LOSS IS .050 FOUND TO BE OUT OF LIMITS IAW SRM 53-0051 FIG 101 DETAIL 2 RMOVED CREASE BEAM IAW SRM 51-40-02. FABED NEW ON TRAVELER NR T9/ 804601 IAW SRMOct 8, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA200910083510Floorbeam · corrodedSTA 740 RBL 60 UPPER CAP CORRODED (FLOORBEAM ). AT BS 740 B/T RBL 30 TO RBL 63 , FLOORBEAM REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MAE. W/C 118350441BZR03, AND MAE EA NR 757-5335-16-F2280 REV B DATED 09/11/2009, NON-ROUTINE IOct 8, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA200910073497Shear Tie · corrodedBULK CARGO COMP STA 1520 BETWEEN STR 27R AND 28R, WL 138, FRAME SHEAR TIE HAS BARE METAL AND SURFACE CORROSION. REMOVED SHEAR TIE, FABRICATED NEW SHEAR TIE AND INSTALLED IAW SRM 51-40-02, THIS IS A MAJOR "A" REPAIR NO FOLLOW-UP INSPECTIONS REQUIRED.Oct 7, 2009 · N907FD · Boeing 7572B7 · Fuselage Internal Mounting StructureSDR FDEA200910063487Seat Track · corrodedMAIN DECK AT STA 700 TO 740 LBL 45 SEAT TRACK CORRODED. REMOVED CORROSION AT STA 700 TO 740 LBL 45.50 IAW SRM 51-10-2. FOUND OUT OF LIMIT IAW SRM 53-00-52 DETAIL I, REMOVED SEAT TRACK AND FABED A NEW SEAT TRACK USING MAT PN BAC1520-792 BATCH NR 0001544831 IAWOct 6, 2009 · N908FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910063489Skin · dentedLT WING, OTBD FLAP, L/E, BEHIND NR 4 SPOILER, IS CREASED. CHECKED LIMITS OF DENT/CREASE AND FOUND OUT OF LIMITS IAW SRM 57-53-01; A=1.0", W=.044", A/Y=22.7. ACCOMPLISHED DOUBLER REPAIR ON LT WING, OTBD FLAP, L/E, BEHIND NR 4 SPOILER, IAW SRM 57-53-01, REPAIROct 6, 2009 · N907FD · Boeing 7572B7 · Trailing Edge FlapsSDR FDEA200910063488Panel · crackedLT WING NR 1 SLAT, INBD NOSE COVE PANEL HAS A 1" CRACK DIRECTLY FWD OF THE INBD DRIVE TRACK. REMOVED NR 1 SLAT SEAL RETAINER FOR REPAIR ACCESS. REMOVED CRACKED COVE PANEL IAW SRM 51-40-02. FABRICATED NEW COVE PANEL IAW MAT ID SHT7075-T6, .050" THICK, BATCH NOct 6, 2009 · N907FD · Boeing 7572B7 · Leading Edge DevicesSDR USAA20091008BB143Wire · brokenLAS - SLIDE RAMP LIGHTS DOORS L3/R3 WILL NOT TEST USING NLG TEST PANEL (LIGHTS DO TEST OK FROM FLIGHT DECK TEST PANEL). REPAIRED BROKEN WIRE AT PIN D OF D40488P.Oct 5, 2009 · N937UW · Boeing 7572B7 · Light System WiringSDR FDEA200910033464Circuit Board · failedAPU FAULTED, RAN QRH CHECKLIST. APU FAULT LIGHT REMAINED ON. SINCE SINGLE GEN OPS RETURNED TO ICT. CREW REPORTED THAT APU DID AUTO SHUTDOWN AND IAW CHECKLIST THEY WERE NOT DIRECTED TO TAKE SWITCH TO OFF. THEY TRIED TO RESTART WITH NO LUCK. WHEN ACFT ARRIVOct 3, 2009 · N903FD · Boeing 7572B7 · APU System WiringSDR FDEA200910023461Strap · corrodedTHE APU AIR INLET DOOR ASSY FWD MOUNTING LAND ON EMPANAGE IS CORRODED. REMOVED DAMAGED SUPPORT IAW SRM 51-40-02, REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS ORIG MAT .100, BLENDED 2 EA AREAS 1.0" X 2.0" X .060" OUT OF LIMITS IAW SRM 53-80-05 FIG 101 DETOct 2, 2009 · N907FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA200909303447Skin · corrodedTHE AFT CARGO DOOR CUT OUT FWD JAMB LOWER SECTION, HAS 2EA AREAS OF CORROSION ADJACENT TO THE LOWER STOP FITTING. REMOVED DAMAGED PART, FABRICATED REPAIR PLATE 2024T3.090C, SHIM 2024T3.100C, INSTALLED REPAIR PARTS IAW SRM 51-00-02. STA 1380, STRG- 22-27R. Sep 30, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR FDEA200909303436Seat Track · mislocatedMCD STA 1540-1640 LBL 45 FOUND INCOMING SEAT TRACK NOT "JIGGING" ON TOOLING (MISLOCATED) REMOVED SEAT TRACK IAW SRM 51-40-02 , FAB NEW SEAT TRACK FROM BAC 1520-792 BATCH 0001541897, LOCATED AND DRILLED IAW SRM 51-40-02 TRATED AND PRIMED IAW SRM 51-21- 01 ISep 30, 2009 · N907FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909303435Seat Track · misalignedMCD STA 1540-1640 LBL 24 FOUND INCOMING SEAT TRACK NOT "JIGGING" ON TOOLING. REMOVED SEAT TRACK STA 1540-1640 LBL 24 FAB NEW SEAT TRACK FROM BAC 1520-792 BATCH NR 0001514831 TREATED AND PRIMED NEW SEAT TRACK IAW SRM 51-20-01 INSTALLED NEW SEAT TRACK IAW SRM Sep 30, 2009 · N907FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909283412Web · crackedFWD CARGO COMPT, BILGE AREA, STA. 680 - 700, RBL 3, WL 148.5, WEB INTERCOSTAL LWR LEG HAVE CORROSION. DOT NR 102-026. NOTE: AFTER REMOVAL FOUND TO BE CRACKED AT 3 FASTENER HOLES. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53Sep 28, 2009 · N907FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA200909283413Intercostal · damagedFWD CARGO COMPT, INTERCOSTAL WEB BTW FS 820 AND 839, S-26R UPPER EDGE DAMAGED AT FASTENER HOLE, DAMAGE CLEANUP IS OUT OF LIMITS IAW SRM 53-00-04, DETAIL I, FIG 101. NOTE: DAMAGE CLEANUP WAS EXISTING. REMOVED TRANSITION PANEL IAW SRM 51-40-02 FOR ACCESS FROM Sep 28, 2009 · N907FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA200909253385Frame · dentedFWD CARGO COMPT, BILGE AREA, STA 720, BL-0, WL 154, TOP OF FRAME HAS SMALL DENT AND SMALL CHAFE MARK ON TOP SURFACE. DOT NR102-013. TRIMMED OUT DAMAGED AREA IAW SRM 53-00-07, FIG 201; PERFORMED HFEC IAW NTM 51-00- 19, PT 6 ON INITIAL FASTENER HOLES COMMON TOSep 25, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA200909243378Seat Track · corrodedSEAT TRACK F,S 1540- 1640, RBL 48. REMOVED SEAT TRACK AT FS. 1540-1640 RBL 48, FABRICATED AND INSTALLED IAW SRM 51-40-02, THIS IS A MAJOR "A" REPAIR NO FOLLOW-UP INSP REQUIRED.Sep 24, 2009 · N907FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909233376Support · corrodedSTA 365 - 418 RBL 24 SEAT TRACK SUPPORT CORRODED. REMOVED CORROSION. REMOVED .030 INCHES MATERIAL FROM .080 INCHES ORIGINAL OUT OF LIMITS IAW SRM 53-00-52. REMOVED SUPPORT AT RBL 24 STA 365-418. RECEIVED NEW SUPPORT IAW TRAVELER NR T9/803243 IAW SRM 53-10Sep 23, 2009 · N907FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA200909223356None · noneACFT DOES NOT MATCH DWG 657N3160 FIG E, SHT 2 , REV D AT STA 1640, LBL 60 -62. DWG SHOWS 4 EA EXISTING FASTENERS BUT THE ACFT HAS 5 EA AT STA 1640; LBL 60 - 62. REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFECTING THE PTF CONVERSION, ON MAE MOD W/C 118350399Sep 22, 2009 · N908FD · Boeing 7572B7 · Standard Practices/StructuresSDR FDEA200909223354None · noneACFT DOES NOT MATCH DWG NR 657N3160 FIG. E , SHT 2, REV D AT STA 1640, RBL 60 - 62. DWG SHOWS 4 EA EXISTING FASTENERS, BUT THE ACFT HAS 5 EA AT STA: 1640; RBL 60 - 62 WAS REPAIRED IAW EA 757-5362-16-F2251, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MASep 22, 2009 · N908FD · Boeing 7572B7 · Standard Practices/StructuresSDR FDEA200909223353Structure · unknownUPPER CORD AT BL-0;900 -1080 HAS AN EXISTING FASTENER BREAKING OUT ON EDGE OF CHORD AT STA 925. IF THIS HOLE IS PICKED-UP IN THE NEW CHORD PN 111N5207-10 WE WILL DUPLICATE THE PROBLEM. AT STA 925, BL-0 , EA 757-5345-16-F2226, WAS COMPLIED WITH AND ACCOMPLISSep 22, 2009 · N908FD · Boeing 7572B7 · Standard Practices/StructuresSDR FDEA200909223348Gcu · damagedON CLIMBOUT ELECTRICAL SYSTEM STARTED TO "FADE" IN AND OUT. SEEMED TO BE THE LT SIDE ELECTRICAL, AUTOPILOTS AND AUTO THROTTLES BECAME INTERMITTENT. WHEN A/P WOULD BE WORKING IT HAD A PRONOUNCED BUMP IN PITCH LIKE AIR IN HYD SYS. CAPT'S FMC TIMED OUT AND WSep 22, 2009 · N903FD · Boeing 7572B7 · AC Generation SystemSDR FDEA200909223352Seat Track · corrodedSEAT TRACK, 24 L, FST. 1540-1640 L CORRODED. REMOVED SEAT TRACK, FABRICATED NEW PART AND INSTALLED IAW SRM 51-40-02, THIS IS A MAJOR "A" REPAIR WITH NO FOLOW-UP INSPECTION REQUIRED.Sep 22, 2009 · N907FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909223351Seat Track · corrodedSEAT TRACK 24R, FST. 1540- 1640 R, IS CORRODED. REMOVED SEAT TRACK, FABRICATED NEW PART AND INSTALLED IAW SRM 51-40-02, THIS IS A MAJOR "A" REPAIR NO FOLLOW-UP INSP REQUIRED.Sep 22, 2009 · N907FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909213344Seat Track · unknownSEAT TRACK 657N3318-7 AT LBL 24.5, STA 1280 - 1320 CAN NOT BE LOCATED AND DRILLED DUE TO ACFT CONFIGURATION NOT MATCHING UP TO DWG AT STA 1280 LBL 24, PREVIOUSLY INSTALLED REPAIR CONFLICTED WITH ACCOMPLISHMENT OF PTF CONVERSION. NEW REPAIR WAS ACCOMPLISHED ATSep 21, 2009 · N908FD · Boeing 7572B7 · Standard Practices/StructuresSDR FDEA200909213343Floorbeam · noneBS 377, LBL 58, FLOORBEAM HAS EXISTING REPAIR THAT INTERFERES WITH INSTALLATION OF RCB, ON MOD W/C 118350472RCBR08 AND W/C 118350431AZ2R03. REMOVED PREVIOUS REPAIR AND CUT OUT DAMAGED AREA AT BS 377, LBL70-RBL 34, IAW SRM 53-00-51, FIG 201, REPAIR NR 3. FABRISep 21, 2009 · N907FD · Boeing 7572B7 · Standard Practices/StructuresSDR FDEA200909213342Floorbeam · corrodedMAIN DECK FLOORBEAM AT BS 377, LBL 3-20, UPPER CHORD HAS AREAS OF CORROSION. REMOVED CORROSION AT BS 377, LBL 3-20, IAW SRM 53-00-51. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3; ORIGINAL MATL- .125 INCH, AFTER REWORK- .090 INCH. REPAIR ACCSep 21, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR USAA20090922BB137Battery · dischargedPHL - "A" FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT INOPERATIVE. REPLACED BATTERY.Sep 20, 2009 · N200UU · Boeing 7572B7 · Emergency EquipmentSDR FDEA200909183327Seat Track · crackedEXITING SEAT TRACK AT STA 1540-1640 HAS A 1.0 INCH CRACK AT STA 1640 ON INB OF SEAT TRACK AND CROWN AT RBL 45. REMOVED SEAT TRACK STA 1540-1640 BL 45, FABRICATED NEW SEAT TRACK FROM BAC 1520- 792 BATCH NR 00015411987, LOCATED AND DRILLED HOLES, TREATED, PRISep 18, 2009 · N908FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909173326Control Panel · failedON CLIMB OUT ICT, CTR A/P FAILED. (HEAVY PITCH PULLS) RETURNED TO ICT C/W QRH. ORIGINAL PLAN DATE WAS ENTERED. RELEASED FOR SERVICE IAW MEL: 22-10-01-C CATEGORY: B EXPIRATION: 20SEP09 "MEL 22-10-01-C: ALL AUTOPILOTS INOP. - ACFT NOT C ATII - NO RVSM OSep 17, 2009 · N903FD · Boeing 7572B7 · Autopilot SystemSDR FDEA200909173322Seat Track · noneSEAT TRACK 657N3318-7 AT LBL 45.5, STA 1280 - 1320 CAN NOT BE LOCATED AND DRILLED DUE TO ACFT CONFIGURATION NOT MATCHING UP TO DWG AT STA 1280 - 1320, SEAT TRACK REPAIR WAS ACCOMPLISHED, DUE TO WRONG CONFIGURATION EFFECTING THE PTF CONVERTION, ON MAE W/C NRSep 17, 2009 · N908FD · Boeing 7572B7 · Standard Practices/StructuresSDR FDEA200909173321Skin · damagedAPPROX STA 437, BETWEEN STR'S 17 AND 18 LT 1 EA EXISTING FASTENER HOLE IN ACFT SKIN IS AT A 0.256 DIA AT STA 437, BETWEEN STR'S 17 AND 18 LT, A REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE P TO F CONVERSION, ON MAE WC NR 118250073ASSR03, AND MAE Sep 17, 2009 · N908FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR FDEA200909173320Intercostal · crackedINTERCOSTAL CRACKED. NEW INTERCOSTAL FABRICATED ON TRAVELER NR T9/800306. (MAJOR REPAIR)Sep 17, 2009 · N908FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA200909163309Floorbeam · corrodedSTA 365 FLOORBEAM RBL 10 CORRODED UPPER SURFACE. REMOVED CORROSION IAW SRM 53-00-51. ORIGINAL MATERIAL .125 MATERIAL REMOVED .025. AFTER REPAIR .100 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. REMOVED DAMAGED AREA AND PREVIOUS RSep 16, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA200909163307Skin · dentedLWR EXT FUSE STA 645 ABOVE STR 18R SKIN DENTED. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-01 FIG.1. REMOVED DAMAGED SKIN AT STA 645; STR 18R IAW SRM 53-00-01, FIG 201, TABLE 1. PERFORMED HFEC IAW NTM 51-00-19 PT 6 ON CUT OUT AREA. NO CRACK INDICATION NOTED. Sep 16, 2009 · N908FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR USAA2009092292587Intercostal · corrodedMCN - B12 - MAJOR REPAIR - CORROSION ON INTERCOSTAL BETWEEN BS 1400 TO BS 1420, S29R. REPLACED INTERCOSTAL BETWEEN BS 1400 TO BS 1420, S29R IAW B757 SRM 51-40-05 & BOEING DRAWING 140N5425.Sep 9, 2009 · N927UW · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR USAA2009092292586Strap · corrodedMCN - B12 - MAJOR REPAIR - CORROSION ON STRAP AT BS 1400 BETWEEN S27L TO S28R. REPLACED STRAP AT BS 1400 BETWEEN S27L TO S28R IAW B757 SRM 51-40-02 & BOEING DRAWING 146N3810.Sep 8, 2009 · N927UW · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR USAA2009091692554Shear Tie · corrodedMCN - B12 - MAJOR REPAIR - CORROSION ON SHEAR TIE AT BS 1400 BETWEEN S28R TO S29R. REPLACED SHEAR TIE AT BS 1400 BETWEEN S28R TO S29R IAW B757 SRM 51-30-01 & BOEING DRAWING 146N1602.Sep 8, 2009 · N927UW · Boeing 7572B7 · Fuselage Internal Mounting StructureSDR USAA2009091692553Shear Tie · corrodedMCN - B12 - MAJOR REPAIR - CORROSION ON SHEAR TIE AT BS 1400 BETWEEN S30R TO S29R. REPLACED SHEAR TIE AT BS 1400 BETWEEN S30R TO S29R IAW B757 SRM 51-30-01 & BOEING DRAWING 146N1603.Sep 8, 2009 · N927UW · Boeing 7572B7 · Fuselage Internal Mounting Structure
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