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"

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SDR USAA2010070691346Crease Beam · corrodedCLT - C2 - MAJOR REPAIR - CORROSION ON LOWER SURFACE OF CREASE BEAM WEB & T-ANGLE BETWEEN BS 1330 TO BS 1335, S17R, RBL 65. REPLACED CREASE BEAM CHORD BETWEEN BS 1330 TO BS 1335, S17R, RBL 65 IAW B757 DRAWING 146N8322.Jun 28, 2010 · N938UW · Boeing 7572B7 · Fuselage Main, StructureSDR USAA2010070191309Crease Beam · corrodedCLT - C2 - MAJOR REPAIR - CORROSION ON LOWER SURFACE OF CREASE BEAM WEB AT BS 1330, S17R, RBL 65. REPLACED CREASE BEAM WEB AT BS 1330, S17R, RBL 65 IAW BOEING DRAWING 143N8322.Jun 28, 2010 · N938UW · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA201006242139Fitting · misalignedNR 2 PYLON MID BULKHEAD FWD RT BOLT HOLE MEASURES 0.4021 UPON REMOVAL OF EXISTING FASTNER. EO F-5450-7-5005 P2 WORK STEP 1.9 CALLS OUT A MAXIMUM REAM OF 0.3901- 0.3911 AND INSTALLATION OF 1/64 OVER SIZE FASTNER. ACCOMPLISHED EA NR F-5450-131189, CLASSIFIEJun 24, 2010 · N904FD · Boeing 7572B7 · Nacelle/Pylon, Attach FittingsSDR FDEA201006242138Fitting · misalignedEO F-5450-7-5003, PT 3, FIG 8, PANEL 3, STEP 4, STATES TO REMOVED CODE I, 0.0374-0.375 IN FASTENER FROM L/E SUPPORT FITTING AREA, INCOMING FASTENER. REMOVED IS 0.437-0.438 IN DIA ACCOMPLISHED EA F-5450-131188, CLASSIFIED AS MAJOR REPAIR.Jun 24, 2010 · N904FD · Boeing 7572B7 · Nacelle/Pylon, Attach FittingsSDR FDEA201006081868Spar · damagedDURING REMOVAL OF NR2 PYLON OTBD SKIN 1EA NUTPLATE HOLE IN LOWER SPAR IN THE PRECOOLER CUTOUT AREA FOUND ELONGATED COMPLIED WITH EA F-5450-139153 "NACELLES/PYLONS - ELONGATED HOLE IN PYLON LOWER SPAR" DATED 05/21/10. CONSIDERED "MAJOR REPAIR" IAW EA MAJOR REPAJun 8, 2010 · N904FD · Boeing 7572B7 · Nacelle/Pylon, Frame/Spar/RibSDR FDEA201006041829Frame · damagedTV MONITOR SUPPORT BRACKET MOUNT HOLE ON FRAME AT STA 395 STR 2L ELONGATED. REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON ST AEROSPACE MOBILE NR 43269370001 AND EA 757-5332-16-F2660. CLASSIFIED MAJOR REPAIR.Jun 4, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA201006041828Frame · damagedFRAME AT STA 418, BETWEEN STR. 1 AND 2L HAS HOLES THAT WERE DISCOVERED TO BE OUT OF LIMITS WHEN PARTS WERE REMOVED ASSOCIATED WITH THE TV MONITOR BRACKET MOD. REPAIR ACCOMPLISHED PER EA 757-5332-16-F2660, REV A. CLASSIFED MAJOR REPAIR.Jun 4, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA201005281699Splice · damagedBS 700, LBL 45.5, FITTING PN 140N2504U1, IF DRILLED, A VARIETY OF FASTENERS WILL LAND IN RADIUS OF FITTING, ON HORZ. AND VERT FLANGES AT BS 700, LBL 45.5, AN ALTERATION WAD ACCOMPLISHED, DUE TO THE DISCREPANCY EFFECTING THE PTF CONVERSION, ON STAM MOD W/C 1183May 28, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA201005281698Splice · damagedBS 700, LBL 45, AFTER INSTALLING SEAT TRACK ALIGNMENT TOOL, EXISTING FASTENER HOLE IN SEAT TRACK AND FLOORBEAM DO NOT ALIGN. AT BS 700, LBL 45, AN ALTERATION WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON STAM MOD W/C 118350496BZ2R02 ANDMay 28, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA201005271683Floor Support · corrodedFS 1261, STR 17 LT HAS CORROSION ON FLOOR CUSP ANGLE. (NOTE: CREASE BEAM CHORD) REMOVED CORROSION FROM CUSP ANGLE AT LBL-17, LBL 60, STA 1261 IAW SRM 51-10-02. CHECKED LIMITS; ORIG MAT =0.071, MAT LOSS =0.015; FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13 FIG 10May 27, 2010 · N904FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA201005261664Frame · damagedFRAME AT BS 1600, S26L, IS DAMAGED. (IN-PROCESS; AWF FOR REPAIR PARTS) DAMAGED FRAME STA 1600 STR 26L FOUND OUT OF LIMITS IAW SRM 53-00-07 PG-103 FIG. 101 DET. II. ORIG. MAT. .063" MAT. REMAIN .053" MAT. LOSS .010" L=1.0" W=2.0" FABBRICATED & INSTALLED J-SMay 26, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA201005261665Skin · dentedFUSELAGE SKIN DENT, 2EA, AT BS 330, 2" BELOW S22R, ARE OUT OF LIMITS. (IN-PROCESS: REPAIR IS REQUIRED) EVALUATED UPPER DENT IAW SRM 53-00-01, FIG 101,DETAIL 3 AND FOUND TO BE W/I LIMITS ; A=.742",Y=.011",A/Y=67.45. EVALUATED LOWER DENT IAW SRM 53-00-01, FIG 1May 26, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR FDEA201005261663Frame · corrodedFRAME AT BS 1380, S26L-S27L, IS EXFOLIATED. (IN-PROCESS; REMOVING FRAME, AWP 146N8511-34 AND AWE).May 26, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA201005261662Nut Plate · corrodedNR 2 CARGO DOOR LOWER SILL HAS CORRODED NUT PLATES. (IN-PROCESS; REMOVING T-CHORD, AWP)May 26, 2010 · N904FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA201005211602Crease Beam · corrodedINBD CREASEBEAM CHORD CORRODED AT BS 665-755, RBL 58. REMOVED CORROSION ON INBD CHORD, R2 DOOR, BS 665-775, RBL 58, IAW SRM 51-10-02. BLENDED AREA .015", MAX ALLOWED .008"; FOUND OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL 2/6. REMOVED INBD CHORD IAW May 21, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA201005201586Fitting · damagedDWG 657N3160, SH.2, REV. D, FOR AFT PALLET FRAME MOD, SHOWS 4EA. EXISTING FASTENER HOLES TO BE PICKED UP IN THE 657N3161-11 FITTING AT BS 1640. ACFT ACTUALLY HAS 5 EA EXISTING HOLES AT BS 1640, LBL 60, A FRAME REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECMay 20, 2010 · N904FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA201005071482Crease Beam · corrodedR-1 DOOR OTBD CREASEBEAM IS CORRODED AT BS 353-366, RBL 60. R & R NEW CREASEBEAM IAW SRM 51-40-02, 2 BS 353-366, RBL 60. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL 3; BEFORE REWORK: .071", AFTER REWORK: .061", REMOVED; .010". -May 7, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, StructureSDR USAA2010051790978Panel · debondedCLT - C2 - MAJOR REPAIR - NR 19-9755-8-0020 & 5003005 - DISBONDING ON RIGHT VERTICAL TORQUE BOX PANEL. REPAIRED RIGHT VERTICAL TORQUE BOX PANEL IAW B757 SRM 51-70-10 & US AIRWAYS EA 101928.May 5, 2010 · N941UW · Boeing 7572B7 · Vertical Stabilizer, Plate/SkinSDR FDEA201005051464Floorbeam · corrodedMAIN DECK FLOORBEAM STA 1681.8, LBL39 UPPER CHORD HAS CORROSION AROUND NUT PLATE. REMOVED CORROSION FROM F/B STA 1681 IAW SRM 51-10-02. BLENDED AREA L=4.0" W=1.0, D=.019, ORIG MAT 156 REMAINING 137 OUT OF LIMITS IAW SRM 53-99-51, FIG 101, DET III. REPAIREMay 5, 2010 · N925FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA201005041440Support · damagedTV MONITOR SUPPORT BRACKET MOUNT HOLE DISTANCE FROM ANOTHER HOLE IS OUT OF LIMITS ON FRAME AT STA 1120 BETWEEN STR 4R, AND STR 3R. REMOVED DAMAGED SECTION, STA 1120, STR. 3R-4R, IAW SRM 53-00-07, REPAIR 3. RECEIVED REPAIR PART FROM FAB SHOP ON T10/830330, BATMay 4, 2010 · N904FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA201005041438Support Bracket · damagedTV MONITOR SUPPORT BRACKET MOUNT HOLE ON FRAME IS WITHOUT PROPER PITCH AT BS 1100, BETWEEN STR 3-R AND 4R. REMOVED DAMAGED SECTION OF FRAME. LOCATED AND DRILLED FRAME AND REPAIR DOUBLERS IAW SRM 53-00-07. TREATED AND PRIMED FRAME AND DOUBLERS IAW SRM 51-21-01May 4, 2010 · N904FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA201004291400Frame · damagedBS 395 FRAME, BETWEEN S1/ 2L, HAS MULTIPLE HOLES THAT ARE NOT WITHIN PITCH LIMITS.Apr 29, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA201004291399Frame · damagedBS 1100, FRAME, S3R/ 4R, HAS MULTIPLE HOLES THAT ARE NOT WITHIN PITCH LIMITS.Apr 29, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA201004291398Frame · damagedBS 1120 FRAME, BETWEEN S3R/ 4R, HAS MULTIPLE HOLES THAT ARE NOT WITHIN PITCH LIMITS.Apr 29, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA201004161208Seat Track · corrodedSEAT TRACK CORRODED AND GOUGED AT BS 640-780, RBL 45.5, IN SEVERAL PLACES. R & R DAMAGED SEAT TRACK AT RBL 45.5, BS 640-780, IAW SRM 53-00-52, AND SRM 51-40-02. CORROSION AND GOUGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL 7, PAGE 101-104; L=100",WApr 16, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201004161207Seat Track · corrodedMCD SEAT TRACK CROWN CORRODED AT BS 1640, LBL 24. R & R SEAT TRACK BETWEEN BS 1540-1640, LBL 24.50, IAW SRM 53-00- 52 / 51-40-02. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL 1, PAGE 102. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.Apr 16, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201004161206Seat Track · gougedSEAT TRACK GOUGED AND WORN AT BS 780-879, LBL 24. CLEANED AND CHECKED LIMITS ON SEAT TRACK AT BS 780-879, LBL 24; THE GOUGE AND WORN AREA EXCEEDS .260" MINIMUM FOR ACCEPTABLE WEAR AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. R & R- SEAT TRACK AT BApr 16, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201004161205Floorbeam · damagedTHE 144N8007-64 CHORD, LWR FLANGE, AT BS 1160, RBL 8-LBL 8, WILL HAVE SHORT E.D. CONDITION ON 14 EA .250" HOLE LOCATIONS. AT BS 1160, RBL8 - LBL 8, A T-CHORD REPLACEMENT WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING PTF CONVERSION, ON MAE MOD W/C 118350451CApr 16, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA201004161204Seat Track · mislocatedFRAME STA 1420-1620, LBL 58.22, UNABLE TO LOCATE SEAT TRACK PN 657N3332-10. EXISTING SEAT TRACK BETWEEN BS 1540-1620, LBL 24.75 AND 45.50, MISLOCATED. SEAT TRACK AT BS 1420-1620, LBL 58.22, WAS REPLACED IAW MAE EA 757-5365-16-F2600, DATED 04/08/2010, REV AApr 16, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA20100416BB025Clamp · loosePHL FLT 1528 - EN ROUTE CLT TO PHL. DURING CLIMB, THE FLIGHT DECK CREW COMPLAINED OF EXCESS NOISE IN THE COCKPIT. THE LEFT PACK WAS TURNED OFF. THEN THE AIRCRAFT INDICATED EXCESS CABIN ALTITUDE. THE FLIGHT WENT TO 13,000 FEET AND DECLARED AN EMERGENCY WITHApr 15, 2010 · N206UW · Boeing 7572B7 · Air Distribution SystemSDR USAA2010051990993Crease Beam · corrodedCLT - C2 - MAJOR REPAIR - CORROSION ON LEFT CREASE BEAM INNER CHORD BETWEEN BS 670 & BS 686, S17L. REPLACED LEFT CREASE BEAM INNER CHORD BETWEEN BS 670 & BS 755, S17L IAW B757 SRM 51-10-02 & BOEING DRAWING 143N8322.Apr 13, 2010 · N941UW · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA201004051052Skin · dentedEXTERNAL FUSELAGE SKIN AT STA 1700-1720 S-20R TO S-21R HAS 1EA OUTWARD DENT. DENT FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101 DETAIL I. REPAIRED DENT AT STA 1700-1720 S-20R TO S-21R IAW SRM 53-00-01 FIG 201, REPAIR 7. SUPPLEMENTAL INSP THRESHOLD OF 24,000Apr 5, 2010 · N909FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR USAA2010040890736Panel · warpedCLT - C2 - MAJOR REPAIR - NR 5 SPOILER PANEL IS WARPED. REPLACED NR 5 SPOILER IAW JOB CARD 19L55027003.Apr 3, 2010 · N206UW · Boeing 7572B7 · SpoilersSDR USAA2010040890735Seat Track · brokenCLT - C2 - MAJOR REPAIR - CABIN SEAT TRACK DAMAGED BETWEEN BS 850 TO BS 882, RBL 45. REPAIRED CABIN SEAT TRACK BETWEEN BS 850 TO BS 882, RBL 45 IAW B757 SRM 53-00-25 REPAIR 3 & EA 101868.Mar 30, 2010 · N206UW · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA20100331BB023Charger · inoperativePHL - THE EXTERNAL EMERGENCY LIGHT AT DOOR L4 WAS INOPERATIVE. CLEANED THE TERMINAL AT LIGHT ASSEMBLY AT DOOR L4. ALSO, REMOVED AND REPLACED THE BATTERY PACK AND CHARGER.Mar 29, 2010 · N939UW · Boeing 7572B7 · Emergency LightingSDR FDEA201003251004Seat Track · gougedSEAT TRACK GOUGED AND WORN AT STA 879 TO 900 RBL 45 BLENDED AERA , CHECKED LIMITS, FOUND OUT IAW SRM 53-00-52 FIG 101 DETAIL 1, ORIG MAT 225 , AFTER REWORK .203, EXCEEDS MAX MAT LOSS OF .004 , REMOVED SEAT TRACK CROWN STA 879 TO 900 RBL 45 IAW SRM 51-40-02, Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003251003Seat Track · gougedSEAT TRACK GOUGED AND WORN AT STA 879TO 900 RBL24 BLENDED AREA, CHECK LIMITS FOUND OUT IAW SRM 53-00-52 FIG 101 DETAIL 1, ORIG MAT .225 AFTER REWORK .213 MAT LOSS OF .12 EXCEEDS MAX MAT WEAR OF .004 . REMOVED SEAT TRACK CROWN STA 879 - 900 RBL 24 IAW SRM 51-Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003251001Frame · gougedFUSELAGE FRAME AT BS 1280, S10R-S11R, FLANGE IS GOUGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL 2, P.103. REMOVED AND INSTALLED NEW FRAME SECTION, AND 2EA. CHANNELS, AT BS 1280, S10R TO S11R IAW SRM 51-40-02 / 53-00-07, FIG 202, P.201-206Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA201003250999Seat Track · damagedSEAT TRACK AT BS 575, RBL 24, HAS BROKEN FLANGE. BLENDED AREA IAW SRM 51-10-02. SEAT TRACK DAMAGE AT BS 575, RBL 24 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 2 AND 3; L=6",W=1.3",D=.100". R & R SEAT TRACK AT BS 440-640, RBL 24.75, IAW SRM 5Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003250998Seat Track · gougedSEAT TRACK AT BS 640-780, RBL 24, IS GOUGED.Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003250997Seat Track · gougedSEAT TRACK AT BS 780-879, RBL 24, IS BROKEN AND GOUGED. R & R SEAT TRACK, PN 1520-792, FROM BS 780-879, RBL 24.75, PER SRM 53-00-52, AND SRM 51-40-02. DAMAGE TO SEAT TRACK OUT OF LIMITS IAW SRM 53-00-52, DETAIL 1. MAJOR REPAIR.Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003250996Seat Track · gougedSEAT TRACK AT BS 780-870, RBL 45, IS GOUGED AND WORN. R & R SEAT TRACK, PN BAC 1520-792, 7178-T6, FROM BS 780-879, RBL 45.50, PER SRM 53-00-52 AND 51-40-02. GOUGE/ WEAR FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL 1. MAJOR REPAIR.Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003250995Crease Beam · corrodedR1 DOOR CREASE BEAM IS CORRODED AT BS 350, RBL 58.Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA201003250994Sill · corrodedL3 DOOR LOWER SILL IS CORRODED.Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA201003190934None · noneBS1640 FLOORBEAM PREVIOUS REPAIR INTERFERES WITH PTF CONVERSION. (IN-PROCESS).Mar 19, 2010 · N904FD · Boeing 7572B7 · Standard Practices/StructuresSDR FDEA201003190933Floorbeam · corrodedAT STA 1661 LBL 57 FLOORBEAM UPPER CHORD, UPPER SURFACE CORRODED.Mar 19, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR USAA2010031690593Skin · delaminatedDELAMINATION ON NR 5 SLAT. REPLACED NR 5 SLAT IAW JOB CARD 19C51227001 & PERFORMED RIGGING PER AMM 27-61-00. REPAIR COMPLETED.Mar 16, 2010 · N935UW · Boeing 7572B7 · Leading Edge DevicesSDR USAA20100311BB016Battery Pack · dischargedPHL - THE EMERGENCY LIGHTS BY DOOR R1, L1, COCKPIT AND THE RIGHT SIDE OF FIRST CLASS WERE INOPERATIVE. REMOVED AND REPLACED THE FORWARD BATTERY PACK.Mar 11, 2010 · N937UW · Boeing 7572B7 · Emergency LightingSDR FDEA201003100876Floorbeam · corrodedSTA 365 RBL 0-18 HAS EXISTING REPAIR THAT INTERFERS WITH MOD CARD 1183650461AZ2R05 INSTALL, ALSO FOUND CORRODED OUT OF LIMITS LBL 58. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3; ORIGINAL THICKNESS=.125' / AFTER REWORK=.092Mar 10, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA201003100874Floorbeam · corrodedFLOORBEAM HAS CORROSION AT STA 345 LBL 12 TO 17. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. FIG 101, DET III. FABRICATED UPPER T-CHORD MAT BAC 1505-100880, REPAIR ANGLES MAE TRAV NR T10/824058, AND REPAIR STRAPS MAE TRAV NR T10/8240Mar 10, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, Floor Beam
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