Boeing 757-2G5

Service difficulty reports · 557

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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 = '7572G5'
  ORDER BY difficulty_date DESC"

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SDR FDEA201204021255Crease Beam · corrodedMAIN CABIN LT SIDE AT BS 860 CREASE BEAM OTBD CHORD WITH CORROSION. REMOVED CORROSION IAW SRM 53-30-13, FOUND OUT OF LIMITS IAW SRM 53-30-13, FIG 101, SHEET 5. R & R CREASEBEAM IAW SRM 53-30-13 AND DWG 143N5520- 27, FROM BS 760-900, LT SIDE. MAJOR REPAIR.Apr 2, 2012 · N962FD · Boeing 7572G5 · Fuselage Floor PanelSDR FDEA201204021252Crease Beam · corrodedLEFT INBD CREASE BEAM CORRODED BS 1315-1320. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-10 FIG 101 SHEETS DETAIL 8. R & R CREASE BEAM IAW SRM 51-40-02 AND DWG 146N8326.Apr 2, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201204021244Frame · gougedBS 1640, FRAME UPPER FLANGE GOUGED AT S27L. R & R FRAME IAW SRM 51-40-02, BS 1640, S26L TO S26R REF DWG 146N1032-1. MAJOR REPAIR CAT A .Apr 2, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, FrameSDR FDEA201204021233Skin · dentedBS 1902 BL 0 HAS TWO DENTS IN SKIN, ONE DENT IS CREASED AND DELAMINATED. REPAIRED SKIN IAW SRM 51-70-10 AND SRM 51-70-01 REPAIR 1. MAJOR REPAIR.Apr 2, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR FDEA201203291193Floorbeam · corrodedFLOORBEAM UPPER TEE BS 324 BL 0- RBL 61 CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TEE TO BE OUT OF LIMITS IAW SRM 53-10-08. R & R TEE IAW SRM 51-40-02, AND DWG 141N2932. MAJOR REPAIR.Mar 29, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201203211204Crease Beam · corrodedRT INBD CREASE BEAM CORRODED STA 1180-1290 REMOVED CORROSION ON CREASE BEAM IAW SRM 51-10-02. CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DETAIL VIII. FABRICATED NEW CREASE BEAM IAW SRM 51-40-05 AND SRM 53-60-13, DETAIL II. TREAMar 21, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201203211206Seat Track · damagedSEAT TRACK AT BS 440 - 630 LBL 25 IS CORRODED, NICKED, GOUGED & HAS SCRATCHES. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW 53-00-52, DETAIL VIII, SHEET 4. R & R SEAT TRACK IAW SRM 51-40-02 AND DWG 143N5090, FROM BS 4Mar 21, 2012 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201203211166Seat Track · gougedLBL 25 SEAT TRACK DIRTY AND GOUGED ON INSIDE AND TOP SURFACES BS 1320-1540. REMOVED NICKS AND GOUGES IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 101 DETAIL XI. R & R SEAT TRACK AT STA 1320-1540 IAW SRM 51-40-02 AND DWG 146N5217.Mar 21, 2012 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201203211155Bonding Strap · corrodedRT WING, WING RIB OTBD, BOND STRAP ATTACH AREA CORRODED, WS 817.27.Mar 21, 2012 · N962FD · Boeing 7572G5 · Wing Main, Frame StructureSDR FDEA201203211140Frame · corrodedCARGO BAY BS 1480, STR 25- 27R, FRAME CORRODED. BLENDED CORROSION AND CHECKED LIMITS IAW SRM 53-00-07, FIG. 101, SHEET 3; ORIGINAL MATERIAL- .063", AFTER BLENDOUT- .050". BLENDOUT IS OUT OF LIMITS. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1030. MAJOR REPMar 21, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, FrameSDR FDEA201203211083Crease Beam · corrodedRT INBD CREASE BEAM ANGLE CORRODED AT BS 1630. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DETAIL VIII. FABRICATED, ALODINED, PRIMED IAW SRM 51-20-01 AND INSTALLED IAW SRM 51-40-02, AND DWG 146NMar 21, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201203211065Beam · corrodedAFT BULKHEAD BS 1720, FWD FACE HORIZONTAL BEAM CORRODED BETWEEN RBL 26.70 - 45.70. FOUND OUT OF LIMITS IAW SRM 53-80-08, DETAIL IX. REMOVED DAMAGED HORIZONTAL BEAM IAW SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-40-02 AND 51-40-05 AND DWG 148N2332.Mar 21, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, BulkheadSDR FDEA201203211054Shear Tie · crackedSHEAR TIE IS CRACKED AT FRAME BS 1300 BETWEEN S20L AND S21L. FABRICATED AND LOCATED AND DRILLED NEW SHEAR TIE IAW SRM 51-53-01. CRACK LENGTH 1.5". INSTALLED NEW SHEAR TIE, IAW SRM 51-40-02 AND DWG 140N2006. MAJOR REPAIR.Mar 21, 2012 · N962FD · Boeing 7572G5 · Fuselage Internal Mounting StructureSDR FDEA201203211051Skin · corrodedSKIN, BS 1885.2 S17R, CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-80-01. REPAIRED SKIN IAW SRM 51-70-10, REPAIR NR 4, MAJOR REPAIR.Mar 21, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR FDEA201203211049Bulkhead · corrodedNR 2 PYLON, PP STA 174.3 BULKHEAD, CORRODED. REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS AND FOUND OUT OF LIMITS IAW SRM 54-50-02, PAGE 105, DETAIL IV, FIG. 101. CAT "A", MAJOR REPAIR.Mar 21, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Bulkhead/FirewallSDR FDEA201203211048Bulkhead · gougedNR 2 PYLON BULKHEAD PP STA 174.3, RT HALF, GOUGED FWD AND AFT SIDE AT UPPER BOLT.Mar 21, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Bulkhead/FirewallSDR FDEA201203211047Bulkhead · corrodedLEFT PYLON MID BULKHEAD FWD FACE WITH CORROSION. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 54-50-02, PAGE 105, FIG 101, DETAIL IV. CAT "A" MAJOR REPAIR.Mar 21, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Bulkhead/FirewallSDR FDEA201203211046Fastener · damagedLEFT PYLON, RT SIDE ACCESS THRU PANEL NR 433LR MID BULKHEAD UPPER SIDE WITH DAMAGED FASTENER. BLENDED IAW EA F-5450-159926.Mar 21, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon Miscellaneous StructureSDR FDEA201203160982Seat Track · gougedLBL 45, SEAT TRACK DIRTY AND GOUGED ON INSIDE AND TOP SURFACES BS 1320-1540. REMOVED DAMAGE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, PAGE 102 AND 103, FIG 101, DETAIL 1. R & R SEAT TRACK IAW SRM 51-40-02 AND DWG 146N5134. MAJOR REPAIMar 16, 2012 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201203160981Seat Track · corrodedLBL 25, SEAT TRACK CORRODED BS 1610-1640. FOUND OUT OF LIMITS IAW SRM 53-00-52, PAGE 104, FIG 101, DETAIL 7. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-60-52, AND DWG 146N5217. MAJOR REPAIR.Mar 16, 2012 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR CA120316007Bearing · worn(CAN) DURING A LIGHTNING STRIKE INSPECTION, WHERE THE EXIT POINT WAS ON THE LT ELEVATOR, THE ELEVATOR PCA WERE INSPECTED AS REQUIRED. THE LT ELEVATOR CENTER PCA LINK ASSY BEARING WAS FOUND TO BE VERY LOOSE AND WORN, UNRELATED TO THE LIGHTNING STRIKE. THE BEARMar 15, 2012 · Boeing 7572G5 · Elevator Tab Control SystemSDR FDEA201203150955Floorbeam · corrodedBS 1360, FLOORBEAM LOWER FLANGE BOTTOM SURFACE CORRODED AT FASTENER HOLES LBL 45 TO RBL 45. R & R FLOORBEAM, AT BS 1360, IAW SRM 51-40-02 AND DWG 146N5009. REMOVED DAMAGE AT BS 1360, LBL 2, 40, 45, AND RBL 20, IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SMar 15, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201203140939Crease Beam · corrodedMAIN CABIN LEFT BS 395 - 377, S17L CREASE BEAM CORRODED.Mar 14, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201203140946Skin · corrodedLT PYLON ACCESS THRU PANEL 433AL HAS CORROSION IN BETWEEN CUT-OUT AND SKIN. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMIT OF REMOVAL, REMOVED .017, ORIGINAL .090, REMAINING .063, OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL V. LOCATED, DRILLED ANMar 14, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201203140945Skin · corrodedLEFT PYLON CORROSION ON PANEL 433GR CUT-OUT. REMOVED CORROSION IAW SRM 51-10-02. MATERIAL LOSS OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL 5. INSTALLED NEW FWD RT SKIN IAW SRM 51-40-02 AND BAC DWG 311N5002. MAJOR REPAIRMar 14, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201203140944Skin · corrodedNR 2 PYLON LT DOOR 443GL CUT-OUT HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01, PG 103, FIG 101. REMOVED INBD FWD SKIN IAW SRM 51-40-02. LOCATED,DRILLED AND COUNTERSUNK NEW SKIN IAW SRM 51-40-02 AND DWG 311N5002. INSTALLEDMar 14, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201203140943Skin · corrodedNR 2 PYLON RT PANEL 443 AR CUT OUT HAS CORROSION SPOTS.Mar 14, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201203140940Floorbeam · damagedBS 1540 FLOORBEAM UPPER SURFACE SCRATCHED AND GOUGED BL 0- LBL 60. REMOVED DAMAGE IAW-SRM-51-10-02. CHECKED LIMITS ORIG MAT= .125" AFTER REWORK=.090" FOUND TO BE OUT OF LIMITS IAW-SRM-53-00-51, FIG 101, DETAIL II AND III. REMOVED AND REINSTALLED SHEAR WEBSMar 14, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201203130928Skin · corrodedLEFT PYLON, LT SIDE THRU ACCESS PANEL, NR 433BL, CORROSION ON INTERNAL SKIN. REMOVED CORROSION IAW SRM 51-10-02. MATERIAL LOSS .023, ORIGINAL .090, REMAINING .067, OUT OF LIMITS OF SRM 54-50-01, FIG 101, DETAIL V. LOCATED, DRILLED AND COUNTERSUNK NEW SKINMar 13, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201203130927Skin · corrodedNR 2 PYLON LT SKIN HAS CORROSION SPOTS ON P-STA 128-136. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL V. INSTALLED NEW SKIN IAW SRM 51-40-02 AND DWG 311N5002. MAJOR REPAIR.Mar 13, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201203130914Frame · corrodedAFT CARGO BAY, STA 1380 STR 29L-29R, FRAME LOWER CHORD CORRODED. REMOVED CORROSION ORIG MAT .090 AFTER REWORK MAT WAS .061 WITH MATERIAL LOSS OF .029 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL 2. INSTALLED FAILSAFE AND TWO VERTICAL SUPPORTS Mar 13, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, FrameSDR FDEA201203120899Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER TEE CORRODED, BL 0 - RBL 11, BS 377. REPAIRED IAW SRM 51-40-02 AND SRM 53-00-51, AND INSTALLED UPPER TEE AND REPAIR IAW SRM 53-00-51. REPAIR 3, FIG 101. MAJOR REPAIR.Mar 12, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201203120896Seat Track · corrodedMAIN CABIN SEAT TRACK RBL 44 BS 1320-1340 CORRODED.Mar 12, 2012 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201203120898Seat Track · gougedSEAT TRACK GOUGED, RBL 45.5, BS 408.Mar 12, 2012 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201203120897Seat Track · corrodedSEAT TRACK FLANGE CORRODED, BS 365-377, RBL 45.5. BLENDED CORROSION IAW SRM 51-10-02. ORIG MATERIAL THICKNESS WAS .090 AFTER REWORK .070 TOTAL MATERIAL LOSS WAS .020. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101 DETAIL VIII. FABRICATED NEW SEAT TRACMar 12, 2012 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201203100870Frame · corrodedAFT CARGO BAY BS 1260, STR30 FRAME CORRODED.Mar 10, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, FrameSDR FDEA201203100869Frame · corrodedAFT CARGO BAY STRINGERS 28-29R, FRAME CORRODED.Mar 10, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, FrameSDR FDEA201203100876Crease Beam · corrodedMAIN CABIN LT SIDE BETWEEN BS333.45 TO BS310.5 CREASE BEAM CORRODED. REMOVED CORROSION IAW SRM 51-10-02, MAT LOSS .002, ORIG MAT .071, AFTER BLEND .069, FOUND TO BE WITHIN LIMITS IAW SRM 53-30-13, FIG.101, PAGE 105.Mar 10, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201203100875Crease Beam · corrodedMAIN CABIN LT SIDE BS 418-395 CREASE BEAM CORRODED.Mar 10, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201203100874Skin · corrodedNR 2 PYLON RT INTERNAL SKIN, PP STA144-153, CORRODED. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS AND FOUND OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL IV. REMOVED AND INSTALLED NEW RT SIDE SKIN IAW SRM 51-40-02 AND DWG 311N5002.Mar 10, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201203090853Web · corrodedSHEAR DECK BS 1680-1720, BL 0 - RBL 60 HAS NUMEROUS AREAS OF CORROSION.Mar 9, 2012 · N962FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201203090846Floorbeam · corrodedCABIN FLOORBEAM BS 365.25, BL 0 - RBL 61, UPPER TEE CORRODED. REMOVED CORROSION, ORIGINAL MATERIAL .125", REMOVED .090", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, SHEET 4, DETAIL 3. REPAIRED FLOORBEAM AT BS 365.25, BL 0 - RBL 61, IAW SRM 53-00Mar 9, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201203090859Web · corrodedSHEAR DECK UPPER SURFACE BS 1680-1720, BL 0 - LBL 60 HAS NUMEROUS AREAS OF CORROSION. MINOR REPAIR.Mar 9, 2012 · N962FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201203090860Floorbeam · corrodedMAIN CABIN FLOORBEAM BS 1280, RBL 41 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, PG 104, DETAIL IV. FABRICATED NEW FOORBEAM, IAW SRM 53-60-51, PG 5, FIG 1, DETAIL II, SRM 51-40-02, DWG 146N5005. INSTALLMar 9, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201203090855Floorbeam · corrodedMAIN CABIN FLOORBEAM, BS 1320 BETWEEN LBL 25 AND RBL 25 HAS CORROSION. REMOVED DAMAGE IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-51, PAGE 104, DETAILS III AND IV. REMOVED FLOORBEAM IAW SRM 51-40-02. FABRICATED NEW FLOORBEAM IAW SRM 53-60-51, PAGE 2Mar 9, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201203080826Floorbeam · corrodedBS 1640 FLOORBEAM UPPER SURFACE CORRODED FROM LBL 60 TO RBL 60. REMOVED DAMAGE PER SRM 51-10-02, FOUND OUT OF LIMITS PER SRM 53-00-51, FIG. 1, DETAIL IV, PAGE 104. REPLACED FLOORBEAM PER SRM 53-60-51, PAGE 5, FIG. 1, DETAIL II, SRM 51-40- 02, AND BOEING DRMar 8, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201112085216Lock · brokenDOOR HOLD OPEN LOCK LEVER ASSY IS BROKEN/DISASSEMBLED IN DOOR HINGE. PREVENTING DOOR FROM LATCHING. INSTALLED LOCK COLLAR AT L1 DOOR. OPS CHECKED GOOD IAW AMM 52-11-08-4, AND MM 52-11-08.Dec 8, 2011 · N943FD · Boeing 7572G5 · Passenger/Crew DoorsSDR FDEA201112085215Latch · brokenDOOR OUTSIDE BUTTERFLY HANDLE HOLD DOWN LATCH ASSY BROKEN. BUTTERFLY LOCKDOWN LATCH SPRING BROKEN. INSTALLED SPRING ON L1 DOOR OUTSIDE BUTTERFLY HANDLE. REF ABOVE ENTRY FOR RII ACTION REQUIRED. FINAL CLOSED.Dec 8, 2011 · N943FD · Boeing 7572G5 · Passenger/Crew DoorsSDR FDEA201109214009Cam · out of adjustCAPTAIN`S SLIDING WINDOW DOES NOT STAY CLOSED WHEN CRANK HANDLE IS RELEASED. WINDOW CRANK MOVES TOWARDS OPEN AND OVER CENTER INDICATOR MOVES TOWARD OPEN. CAPT'S SLIDING WINDOW FOUND UPPER CAM BLOCK, AND WINDOW OPERATING CLUTCH OUT OF ADJUSTMENT. ADJUSTED ANSep 21, 2011 · N943FD · Boeing 7572G5 · Flight Compartment WindowsSDR FDEA201109143886Battery Pack · failedEMERGENCY EXIT LIGHTS WILL NOT TEST. R & R L1 EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-51-07-2. OPS CHECKED NORMAL.Sep 14, 2011 · N943FD · Boeing 7572G5 · Emergency Lighting
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