Boeing 757-2Q8

Service difficulty reports · 2,798

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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 = '7572Q8'
  ORDER BY difficulty_date DESC"

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SDR FDEA201108023101Skin · misrepairedSKIN AT BS 1380-1400, S-23L-S-25L MISREPAIRED. REMOVED AND REPLACED DOUBLER PER SRM 51-40-02 AND SRM 53-00-01, REPAIR 16. FABRICATED DOUBLER PER SRM 53-00-01, TABLE 1 AND 2, FIG. 201, P. 203. MAJOR REPAIRAug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201108023156Skin · misrepairedSKIN REPAIR AT 1394-1420 S-20L-S-22L IST NOT IN COMPLIANCE WITH SRM. REMOVED & REPLACED DOUBLER AS PER SRM 51-40-02 / 53-00-01. FABRICATED DOUBLER AS PER SRM 53-00-01 TABLE I & III FIG 201 P. 203 . CATEGORY B MAJOR REPAIR.Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201108023192Frame · corrodedFRAME AT STA 1645 (FWD OF L-4 DOOR) HAS CORROSION ON LOWER END WL 210 INBD FLANGE LT SIDE LBL 55.Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201108023182Frame · corrodedFRAME AT BS 1645, LOWER END HAS CORROSION AT WL 210 INBD FLANGE RBL 55.Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201108023107Skin · misrepairedREPAIR AT STA 17800-1720, S-23L-S-25L DOES NOT MEET SRM REQUIREMENTS. REMOVED &REPLACED DOUBLER STA. 1700-1720 S-23L-25L AS PER SRM 51-40-02/ 53-00-01, REPAIR 16, FABRICATED DOUBLER AS PER SRM 53-00-01 FIG 201 TABLE I & III PG 203. CATEGORY B REPAIR 16, Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201108023097Skin · misrepairedFUSELAGE SKIN REPAIR AT BS 365, S21-22L, IS NOT IN COMPLIANCE WITH SRM. REMOVED EXISTING SKIN REPAIR DOUBLER AT STA 365 S-21L-22L IAW SRM 51-40-02. FABRICATE NEW REPAIR DOUBLER AND REINSTALLED WITH FILLER AND CONICAL WASHER IAW SRM 53-00-01 AND 51-40-02. Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201108023092Skin · misrepairedREPAIR AT STA 1500-1570, S-21L-S-22L DOES NOT MEET SKIN REPAIR 757SF SRM REQUIREMENTS. REMOVED AND REPLACED DOUBLER, BS 1511-1522, S22L - S23L, AS PER SRM 51-40-02, 53-00-01, REPAIR 16. FABRICATED DOUBLER, AS PER SRM 53-00-01, TABLE 1, FIG. 201, P.203, RAug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201108023075Floorbeam · misrepairedFLOORBEAM STA 1300 HAS IN COMING REPAIR THAT DOES NOT COMPLY WITH SRM, EA OR ANY DOCUMENT. REMOVED REPAIR, FABRICATED REPAIR ANGLES, STRAP, AND FILLER. LOCATED AND DRILLED NEW PARTS, TREATED ALODINED, PRIMED AND INSTALLED REPAIR PARTS AT FLOORBEAM UPPER CAug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201108023105Skin · misrepairedSKIN, BS 1560-1585, S26-29R MISREPAIRED. FABRICATED DOUBLER IAW EA F-5330-147736 AND INSTALLED NEW DOUBLER IAW SRM 51-40-02 AND EA 5330-147736.Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201108023074Beam · gougedNR 1 CARGO DOOR LOWER EDGE BEAM HAS SEVERAL DENTS AND GOUGES. REPLACED EDGE BEAM IAW SRM 51-40-02, CHECKED LIMITS ON EDGE BEAM ORIGINAL MATERIAL .050 MAT LOSS .025 REMAINING .025 FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02 FIG 101 DETAIL III PAGE 105.Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201108013057Gate · corrodedR-4 DOOR LOWER GATE CORRODED AT SEAL RETAINER ATTACHMENT POINT. REMOVED AND REPLACED R-4 DOOR LOWER GATE ASSY IAW AMM 52-11-38-4, NO RIG REQUIRED, NO RIG DISTURBED. MAJOR REPAIR.Aug 1, 2011 · N996FD · Boeing 7572Q8 · Passenger/Crew DoorsSDR FDEA201107293026Gate · corrodedL-4 DOOR LOWER GATE CORRODED AT SEAL RETAINER ATTACHMENT POINT. REMOVED AND REPLACED L-4 DOOR LOWER GATE ASSY IAW AMM 52-11-38-4. NO ADJUSTMENT REQUIRED.MAJOR REPAIR.Jul 29, 2011 · N996FD · Boeing 7572Q8 · Passenger/Crew DoorsSDR FDEA201107293025Gate · corrodedR2 DOOR LOWER GATE CORRODED AT LOWER EDGE.Jul 29, 2011 · N996FD · Boeing 7572Q8 · Passenger/Crew DoorsSDR FDEA201107283010Crease Beam · corrodedMAIN DECK LT CREASE BEAM EXFOLIATED AT STA 680. FOUND CREASE BEAM TO BE OUT OF LIMITS IAW SRM 53-30-15 DETAIL III FIG 101 REMOVED AND INSTALLED NEW CREASE BEAM PN/143N8328053 FROM 640 TO 760 LEFT HAND SIDE IAW SRM 51-40-02 MAX MATERIAL LOSS 0.041 MAX ALLOWAJul 28, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, StructureSDR FDEA201107232922Skin · crackedRT APU DOOR AFT EDGE HAS CRACK IN SKIN ON EDGE. CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 52-40-02, DET VI, FIG 101. REMOVED DAMAGE AREA IAW SRM 51-10-02. FABED DOUBLER IAW SRM 52-40-01, BATCH NR 2061447, PN 2024-T3. LOCATED & DRILLED DOUBLER IAW SRMJul 23, 2011 · N996FD · Boeing 7572Q8 · Auxiliary Power Unit (APU) DoorsSDR FDEA201107232919Frame · damagedUPPER LOBE STRUCTURE FRAME HAS DOUBLED DRILLED HOLE AT STA 800 BET. STR 2L & STR 3L. FOUND TO BE OUT OF LIMITS IAW SRM-51-40-06, BETWEEN STR 2L-3L, CUT OUT DAMAGED FRAME AND INSTALLED SPLICES AND FRAME IAW SRM-53-00-07, REPAIR 3. MAJOR REPAIR "CAT B"Jul 23, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201107212881Door Frame · gougedL2 DOOR CUTOUT FWD FRAME AT STA 690 HAS 2 GOUGES BETWEEN S15R AND S17R. OUT OF LIMITS STRAP & FRAME, REMOVED STRAP & FRAME REMOVED ANGLES & DOOR LOCK, DOOR STOP FITTING IAW SRM 51-40-02, LOCATED DRILLED NEW FRAME & STRAP & ANGLE, DOOR LOCK, DOOR STOP FITTINJul 21, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, StructureSDR FDEA201107202859Door Frame · gougedAFT CARGO DOOR MID LOWER FRAME SECTION HAS SEVERAL GOUGES. EVALUATED GOUGE AFT CARGO DOOR MID LOWER FRAME, FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02, FIG 101, DETAIL IV. R & R IAW SRM 51-40-02 AND DWG NR 146N6621, MAJOR REPAIR.Jul 20, 2011 · N995FD · Boeing 7572Q8 · Cargo/Baggage DoorsSDR FDEA201107192808Seat Track · damagedMAIN DECK SEAT TRACK AT LBL 25 HAS BROKEN OFF LUGS AT STA 454. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL I, REMOVED SEAT TRACK STA 440- 470 LBL 25 IAW SRM 53-40-02, FABRICATED REPAIR ANGLES IAW SRM 53-00-52 FIG 201. LOCATED AND DRILLED REPJul 19, 2011 · N996FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107132682Floorbeam · corrodedFLOORBEAM TEE BETWEEN RBL 41-62 BS 324 CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-08. ORIGINAL MATERIAL .0125 AFTER REWORK .110. R & R TEE IAW SRM 51-40-01. MAJOR REPAIR.Jul 13, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201107132686Seat Track · gougedGOUGE SEAT TRACK BETWEEN STA 1200-1220 LT SIDE OF CABIN INBD TRACK FOUND SEAT TRACK AT STA 1200-1220, LBL 24 OUT OF LIMITS IAW SRM 53-00-52 FIG 101, DETAIL I. FABRICATED NEW SEAT TRACK WITH PN BAC1520-792. REMOVED AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02Jul 13, 2011 · N996FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107132677Seat Track · gougedSEAT TRACK BETWEEN STA 418 AND 440 GOUGED MAIN CABIN RBL24. R & R SEAT TRACK IAW SRM-53-00-52, DETAIL I, FIG 101 FOUND TO BE OUT OF LIMITS L=2.8 W=1.3 D=0.025 IAW SRM-5300-52, DETAIL I, FIG 101.Jul 13, 2011 · N996FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107122666Seat Track · gougedMAIN DECK SEAT TRACK LBL 45 HAS GOUGED LUG BETWEEN BS 418-440. BLENDED GOUGE, FOUND TO BE OUT OF LIMITS IAW-SRM-53-00-52, FIG 101, DETAIL 1. R & R SEAT TRACK IAW-SRM-51-40-025.Jul 12, 2011 · N996FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107122665Frame · gougedAFT PIT FRAME 1340 LT DEEP GOUGE IN FRAME BETWEEN STRINGERS L25-26L. REMOVED GOUGE IAW SRM 51-10-02. ORIGINGAL MATERIAL .071 REMAINING .050 FOUND OUT OF LIMITS IAW SRM 53-00-07, FIG 101, ALLOWABLE DAMAGE 2. R & R FRAME IAW SRM 51-40-02. MAJOR REPAIR.Jul 12, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201107122663Frame Splice · gougedAFT CARGO BAY FRAME, BS 1340 SPLICE. DEEP GOUGE BETWEEN STRINGERS 23L AND 24L. REMOVED GOUGE IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-07, FIG 101. R & R SPLICE IAW SRM 51-40-02. MAJOR REPAIR.Jul 12, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, FrameSDR DALA1142496803Floorbeam · corrodedFUSELAGE STATION 1640 FLOORBEAM CORRODED MULTIPLE AREAS PSV 11 NR CARDS 44, 216, 217, 218.Jul 5, 2011 · N704X · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR DALA1142266803Floorbeam · corrodedFUSELAGE STATION 365 FLOORBEAM CORROSION APPROX B/L 0 THROUGH THE R1 DOOR.Jul 4, 2011 · N704X · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201107012528Floorbeam · corrodedSTA 345, FLOORBEAM, RBL 60 CORRODED AND PREVIOUS BLEND ON UPPER FLANGE. REMOVED DAMAGED AREA FROM UPPER FRAME STA 345 RBL 52- RBL 70 IAW SRM 51-10-02 AND SRM 53-00-51 FIG 201. DRILLED AND LOCATED HOLES FOR REPAIR IAW SRM 51-40-05. DRILLED AND LOCATED REPAIJul 1, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201106262429Ring · dislodgedL1 DOOR HAS STRAP AND D-RING HANGING DOWN OUT OF DOOR PACKAGE. RELEASED FOR SERVICE IAW MEL: 52-11-01-A CATEGORY: B EXPIRATION: 29JUN11 "MEL 52-11-01-A: L1 DOOR SLIDE- INOP (IDENTIFY INOP OR MISSING)." FOUND D-RING TO INTERFEAR WITH ARMING GIRT BAR, REPOSTIOJun 26, 2011 · N993FD · Boeing 7572Q8 · Escape SlideSDR FDEA201106242411Frame · gougedAFT PIT FRAME RT STA 1320 BETWEEN STR 25R AND STR 27R, GOUGED. REMOVED GOUGE IAW SRM 51-10-02 ORIG MAT .071 REMAINING = .061, OUT OF LIMITS IAW SRM 53-00-07, FIG 101 DETAIL I A. D.2. R & R FRAME AT STA 1320 STR'S 25L- 25R IAW SRM 51-40-02. MAJOR REPAIR.Jun 24, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201106232402Skin · dentedRT WING NR 6 SLAT HAS NUMEROUS DENTS ALONG NOSE SKIN.Jun 23, 2011 · N996FD · Boeing 7572Q8 · Leading Edge DevicesSDR FDEA201106222388Frame · corrodedAFT PIT 1460 FRAME, NUMEROUS AREAS ON FRAME CORRODED, TOTAL OF NINE AREAS. REMOVED CORROSION IAW SRM SRM 53-00-07 FIG 101 ORIGINAL THICKNESS .067" AFTER CORROSION REMOVED .055" FOUND OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL V. REMOVED AND REPLACED FRJun 22, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, FrameSDR DALA1142166803Floorbeam · corrodedCORROSION DAMAGE WAS FOUND TO THE UPPER CHORD OF THE STA 324 FLOORBEAM FROM RBL 33 TO THE O/B END. THE SUBJECT CHORD WILL BE REMOVED AND A NEW SECTION WILL BE SPLICED IN. THE SUBJECT CHORD IS MADE FROM 7075-T6511 ALUMINUM EXTRUSION PER AND 10136-2409.Jun 17, 2011 · N704X · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201106152275Floor Support · corrodedMAIN CABIN FLOOR SUPPORT, LBL 45 HAS CORROSION AT STA 377.7.Jun 15, 2011 · N996FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201106152274Floorbeam · corrodedSTA 377, RBL 4 TO RBL 12 FLOORBEAM CORRODED MAIN CABIN. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW SRM-53-00-51, FIG 101, DETAIL III ORIGINAL. MATERIAL .125 REMOVED .016, REMAINING MATERIAL .109. R & R FLOORBEAM IAW SRM 51-40-02. MAJOR REPAIR.Jun 15, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201106152273Floorbeam · corrodedSTA 395, RBL 54 FLOORBEAM CORRODED MAIN CABIN. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. REMOVED FLOORBEAM IAW SRM 51-40-02. DRILLED AND LOCATED NEW FLOORBEAM IAW SRM 53-10-51 DETAIL II AND SRM 51-40-05.Jun 15, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201106152272Floorbeam · corrodedSTA 365, BL 0 TO RBL 17 CORROSION ON FLOORBEAM MAIN CABIN. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MATERIAL .125 MATERIAL REMOVED .015 REMAINING MAT .110. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. REMOVED FLOORBEAM IAW SRM 51-40Jun 15, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR DALA1139736802Floorbeam · corrodedDURING PSV IN ATL, MAINT NOTED CORROSION TO THE UPPER CAP OF THE FLOORBEAM AT STA 1640. SUBJECT CAP WILL BE CUT FROM LBL 13 TO THE RT END. A REPLACEMENT CAP WILL BE SPLICED INTO THE WEB AND THE REMAINING UNDAMAGED SECTION. SUBJECT CAP IS 7075-T6511, EXTRUSJun 14, 2011 · N703TW · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR DALA1137736802Bulkhead · corrodedSTA 324 BULKHEAD UPPER CHORD CORRODED. REPAIR C/W PER ERA 492992-14 - RBL 33 TO RT END OF PART.Jun 6, 2011 · N703TW · Boeing 7572Q8 · Fuselage Main, BulkheadSDR DALA1137726802Floorbeam · corrodedTRANSVERSE FLOORBEAM STA 365 LBL 9.5 RBL 70.5 - UPPER CAP CORRODED. REPAIR COMPLETED PER ERA492888-14 REV ORIG.Jun 6, 2011 · N703TW · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR DALA1138276809Battery Pack · dischargedDURING A LIGHTING TEST, MAINTENANCE FOUND THE DOOR 1L EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER. OPERATIONAL CHECK WAS GOOD.Jun 3, 2011 · N713TW · Boeing 7572Q8 · Emergency LightingSDR DALA1137296801Floorbeam · corrodedSTA 377 FLOORBEAM UPPER FLANGE CORROSION DAMAGE-BL0 - LBL 23. REPAIR COMPLETED PER ERA 492668-14 REV A.Jun 1, 2011 · N702TW · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201105201905Slide · malfunctionedL1 CREW ENTRY DOOR SLIDE LIGHT WAS DIFFICULT TO ARM. OPS CHECKED L1 DOOR SLIDE ESCAPE SYSTEM REF MM 25-66-00-5-0. OPS CHECK GOOD, ACFT OK FOR SERVICE.May 20, 2011 · N993FD · Boeing 7572Q8 · Escape SlideSDR DALA1137396801Floorbeam · corrodedCABIN FLOORBEAM STA 1640 T-CAP CORROSION. REPAIRED PER ERA 493066-14 REV ORIG.May 18, 2011 · N702TW · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201101310427Stringer · corrodedREWORK OF NR N00451: FWD CARGO PIT STA 770, S-27L, WL 138 CORRODED REQUIRES REWORK DUE TO INCORRECT SRM REF USED REWORKED REPAIR SPLICE AT STA 770 S-27L . INSTALLED SPLICES IAW SRM 53-00-03 REPAIR 3 CAT "A" MAJOR REPAIR.Jan 31, 2011 · N993FD · Boeing 7572Q8 · Fuselage Main, Longeron/StringerSDR FDEA201101310428Skin · misrepairedPREVIOUS OPERATOR INSTALLED REPAIR EVALUATED IAW INCORRECT SRM REF. COMPLIED WITH EA F-5330-146251. FUSELAGE PLATES AND SKINS EO F-5100-7-5001 PART 1-EXISTING REPAIR TRACKING (DTA REQUIRED). MAJOR REPAIR.Jan 31, 2011 · N993FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201101310425Stringer · corrodedCORROSION ON S-26L BETWEEN STA 760-780 INSIDE FWD CARGO COMPARTMENT REQUIRES REWORK DUE TO INCORRECT SRM REF USED. REWORKED REPAIR SPICE AT STA 760-780 ON S-26L. RECEIVED NEW FILLER AND SPLICES ON T11/867864 AND T11/868216. INSTALLED NEW FILLER AND SPLICES IJan 31, 2011 · N993FD · Boeing 7572Q8 · Fuselage Main, Longeron/StringerSDR FDEA201101250349Skin · dentedDENT ON FUSELAGE SKIN STA 580-600 BETWEEN S-27L TO S-28L. DENT AT STA 580-600 BETWEEN S-27L TO S28L FOUND OUT OF LIMITS DUE TO PROXIMITY TO FRAME IAW SRM 53-00-01, FIG 101 DETAIL III. REPAIRED SKIN IAW SRM 53-00-01, PG 201, FIG 201, REPAIR 16. CATEGORY "B" Jan 25, 2011 · N993FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201101250348Skin · dentedDENT ON FUSELAGE SKIN, STA 333.45 BETWEEN S-21L TO S-22L REQUIRES REWORK DUE TO INCORRECT SRM REF USED. DENT ON FUSELAGE SKIN STA 333.45 BETWEEN S-21L TO S-22L FOUND OUT OF LIMITS DUE TO PROXIMITY TO FRAME IAW SRM 53-00-01, FIG 101, DETAIL III. REPAIRED SKJan 25, 2011 · N993FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201101250350Skin · dentedREWORK OF NR N00182: EXTERNAL FUSELAGE SKIN FOUND DENT AT STA 1120-1139, S-8R DENT AT STA 1120-1139, S-8R FOUND OUT OF LIMITS DUE TO PROXIMITY TO STRINGER IAW SRM 53-00-01, FIG 101 DETAIL II. REPAIRED AREA IAW SRM 53-00-01, FIG 201, PG 204, TABLE 1 REPAIR Jan 25, 2011 · N993FD · Boeing 7572Q8 · Fuselage Main, Plate/Skin
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