N530US, cancelled Dec 30, 2022

Service difficulty reports · 77

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N530US' AND deregistration_id = 'N530US-2022-12-30'
  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 DALA2015082105119Power Supply · inoperativeEMERGENCY LIGHTING INOPERATIVE BETWEEN ROWS 14 AND 23. TROUBLESHOT TO POWER SUPPLY IAW WDM 33-51-13, PP1A, WIP, 262168. REPLACED POWER SUPPLY IAW AMM 33-51-07, OPS CHECKED GOOD IAW AMM.Aug 20, 2015 · N530US · Boeing 757251 · Emergency LightingSDR DALA2015081104912Duct · blownATB, OPERATING ON FLIGHT 2245, PERFORMED AN AIR TURNBACK DUE TO LOSS OF PRESSURIZATION AND CABIN ALTITUDE RISING. STATUS MESSAGES WERE "CABIN AUTO INOPERATIVE, CABIN ALT AUTO" AND "CABIN ALT AUTO 2". MAX CABIN ALTITUDE WAS 11K AND OUTFLOW VALVE INDICATED CLOAug 8, 2015 · N530US · Boeing 757251 · Cabin Pressure Control SystemSDR DALA2015071704456Battery Pack · inoperativeON SERVICE CHECK, FOUND BULLNOSE EMERGENCY LIGHT AT 4AB INOPERATIVE. FOUND NO POWER AT SOCKET, R & R EMERGENCY LIGHT BATTERY PACK, OPS NORMAL, LIGHTS CHECKED OK.Jul 15, 2015 · N530US · Boeing 757251 · Emergency LightingSDR DALA2015071704455Battery Pack · inoperativeON SERVICE CHECK, FOUND BULLNOSE EMERGENCY LT AT 1AB INOPERATIVE. FOUND NO POWER AT SOCKET, R & R EMERGENCY LIGHT BATTERY PACK, OPS NORMAL, LIGHTS CK.Jul 15, 2015 · N530US · Boeing 757251 · Emergency LightingSDR DALA2015060403586Light · unsecureEMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. SECURED LIGHT TRACK 1R.Jun 2, 2015 · N530US · Boeing 757251 · Emergency LightingSDR DALA14013175530Structure · crackedL2 DOOR CRACKED AT FWD DOOR HINGE CUTOUTS. REMOVED L2 DOOR IAW AMDS CARD 5211-9001-2L. INSTALLED SERVICEABLE DOOR IAW AMDS CARD 5211-9001-2L. INSTALLED SLIDE IAW AMS CARD 2566-9001-2L. OK FOR SERVICE.Feb 26, 2014 · N530US · Boeing 757251 · Passenger/Crew DoorsSDR DALA14012755530Cable · inadequateL2 DOOR EMERGENCY POWER ASSIST CABLE TRAVEL INSUFFICIENT. ADJUSTED L2 DOOR POWER ASSIST CABLE TRAVEL. OK FOR SERVICE.Feb 25, 2014 · N530US · Boeing 757251 · Passenger/Crew DoorsSDR DALA13042395530Connector · looseSEAT 4A/B EMERGENCY LIGHT INOPERATIVE AT CURVED EDGE OF STOWAGE BIN CK LIGHT ASSY CHECKED GOOD. RESEATED CONNECTOR ON M731 PWR SUPPLY-NOW OPS CK NML.Aug 31, 2013 · N530US · Boeing 757251 · Light System WiringSDR DALA13040005530Power Supply · inoperativeFWD EMERGENCY EXIT SIGN INOPERATIVE. REPLACED POWER SUPPY M730 IAW AMM 33-51.Aug 18, 2013 · N530US · Boeing 757251 · Emergency LightingSDR DALA13038295530Charger · inoperativeEMERGENCY LIGHT IN OVERHEAD BIN ROW 4 A/B INOPERATIVE. R & R BATTERY CHARGER M731 IAW AMM 33-51 OPS CHECKED GOOD.Aug 6, 2013 · N530US · Boeing 757251 · Emergency LightingSDR DALA13022585530Light · inoperativeBULLNOSE EMERGENCY LIGHT INOPERATIVE AT ROW 4AB. R & R EMERGENCY LIGHT ASSY. OPS CHECKED GOOD.May 15, 2013 · N530US · Boeing 757251 · Emergency LightingSDR DALA13022405530Ground Stud · looseBULLNOSE EMERGENCY LIGHT AT SEAT 18ABC INOPERATIVE. NO POWER TO LIGHT, FUSES GOOD AT POWER SUPPLY. OTHER LIGHT IN CIRCUIT WORKING, SUSPECT POWER SUPPLY. FOUND RING TERMINAL LOOSE ON GROUND STUD GD475-DC. SECURED GROUND STUD. LIGHT NOW OPS NORMAL. REMOMay 5, 2013 · N530US · Boeing 757251 · Light System WiringSDR DALA12014755530Wire · brokenFLOOR EMERGENCY LIGHT (RED) INOPERATIVE AT DOORS. FOUND BROKEN WIRE AT SPLICE. LIGHTS PARTIALLY DISASSEMBLE. REF SWPM 20-30, REPAIRED WIRING AS REQUIRED. OP TEST EMERGENCY LIGHTS OK. REASSEMBLE TRACK.Dec 4, 2012 · N530US · Boeing 757251 · Light System WiringSDR DALA12005605530Bearing · seizedSHIP 5530, MAINTENANCE DISCOVERED DURING THE DOOR 1L EMERGENCY POWER ASSIST MECH CHECK THAT THE TRIGGER BEARING WAS SEIZED. REPLACED BEARING REF AMM 52-11 RII PROCEDURES C/W.Aug 16, 2012 · N530US · Boeing 757251 · Passenger/Crew DoorsSDR DALA1241015530Battery Pack · inoperativeDURING LAYOVER MAINTENANCE, FOUND EMERGENCY LIGHT ABOVE SEAT 4B IN NOSE INOPERATIVE. MAINTENANCE RELAMPED, REPLACED BATTERY PACK, AND CHARGER M731. OPERATION OF LIGHT NOW CHECKS NORMAL.Jul 9, 2012 · N530US · Boeing 757251 · Emergency LightingSDR DALA1234595530Battery Pack · inoperativeFLIGHT ATTENDANT WROTE UP EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. OPERATIONOF LIGHTS CHECK GOOD PER AMM.May 29, 2012 · N530US · Boeing 757251 · Emergency LightingSDR DALA1221985530Power Supply · failedDURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATH LIGHTS IN ROWS 16-22 INOPERATIVE. MAINTENANCE REPLACED BAD POWER SUPPLY IAW AMM 33-51. OPS TESTED OK.Apr 7, 2012 · N530US · Boeing 757251 · Emergency LightingSDR DALA13005655530Skin · damagedLIGHTNING STRIKE FASTENER DAMAGE, BS 310.5 1.5" BELOW S22R REPLACED BLIND FASTENER WITH PERMANENT REPAIR FASTENER REF TO SRM 53-00-01-2R6, CATEGORY A REPAIR.Jul 26, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA13005645530Skin · damagedLIGHTNING FASTENER DAMAGE BS 278 8.5" ABOVE S23R. REPLACED BLIND FASTENER WITH PERMANENT REPAIR FASTENER REF SRM 53-00-01-2R6.Jul 26, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA13005635530Skin · damagedLIGHTNING STRIKE FASTENER DAMAGED BS 297 8.75" BELOW S-23L REPLACED BLIND FASTENER WITH PERMENT REPAIR FASTENER REF TO SRM 53-00-01-2R6, CATEGORY A REPAIR.Jul 26, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA13005625530Skin · damagedLIGHTNING STRIKE FASTENER DAMAGE BS 310.5 1.5" BELOW S24L. REPLACED BLIND FASTENER WITH PERMANENT REPAIR FASTENER REF TO SRM 53-00-01-2R6, CATEGORY A REPAIR.Jul 26, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA13005615530Skin · damagedLIGHTNING STRIKE FASTENER DAMAGE BS 326, S22R. REPLACED BLIND FASTENER WITH PERMENT REPAIR FASTENER REF TO SRM 53-00-01-2R6, CATEGORY A REPAIR.Jul 26, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA13005605530Skin · damagedLIGHTNING STRIKE FASTENER DAMAGE BS 348 S22R. REPLACED BLIND FASTENER WITH PERMANENT REPAIR FASTENER REF TO SRM 53-00-01-2R6, CATEGORY A REPAIR.Jul 26, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1137465530Power Supply · inoperativeEMERGENCY EXIT LIGHT ABOVE DOOR 2R INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY PER AMM 33-51-07.May 30, 2011 · N530US · Boeing 757251 · Emergency LightingSDR DALA2014122306661Skin · damagedDURING MAINTENANCE CHECK, INSPECTION FOUND A LIGHTNING STRIKE ON THE FUSELAGE SKIN AT BS 500 BETWEEN S16-17R. THE DAMAGE WAS BLENDED AND FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101. COMPLIED WITH ERA 488999-14, REV ORIGINAL.Feb 16, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1110945530Skin · dentedLOWER EXTERIOR FUSELAGE IS DENTED FROM STA 1394 TO STA 1400 BETWEEN STR 29L TO 27R. ACCOMPLISHED ER/A 489003-14 REV ORIGINAL THIS REPAIR IS MAJOR AND PERMANENT. REPAIR APPROVAL IS LIMITED TO 12 MONTHS SERVICE ONLY. ADDITIONAL EA IS REQUIRED FOR CONTINUED SERFeb 15, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1110795530Intercostal · crackedINTERCOSTAL CRACKED BETWEEN STA 1420 TO 1440, RBL 10. REMOVED INTERCOSTAL. REMOVED DAMAGED FLANGE AND PERFORMED HFEC ON CUTOUT FLANGE NO NOTED CRACKS, FABRICATED 1EA REPAIR DOUBLER AND 2EA FILLERS FOR INTERCOSTAL TREATED AND PRIMED AND TOP COATED DOUBLER REPAFeb 15, 2011 · N530US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1110965530Skin · dentedDURING M-CHECK AT WHILE ACCOMPLISHING A PERMANENT BETWEEN STA1695 AND STA1705, S-17L AND S-19L, IT WAS NOTED THAT STR 18L WAS DENTED AT STA 1695. DENT IS LOCATED ON THE SKIN ATTACHMENT FLANGE OF STRINGER. ACCOMPLISHED DURING M-CHECK AT SAT, FEB2011. SECTION Feb 14, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1110935530Skin · dentedDURING M-CHECK AT SAT, WHILE ACCOMPLISHING THE PERMANENT REPAIR AT STA 1420, 2 EACH DENTS WERE FOUND ON THE 146N3511-12 SKIN PANEL BETWEEN STA1425 AND STA1430, S-28R AND S-29L. ER/A 488486-14 SECT.I ACCOMPLISHED DURING M-CHECK AT SAT, FEB2011. SECTION II- APPFeb 14, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1110815530Skin · gougedEMPENNAGE EXTERNAL R 2"L AREA OF GOUGE DAMAGE JUST AFT OF HORIZ STAB CUTOUT AND FS 1862.7. ACCOMPLISHED ERA 489457-14 REV ORIG THIS REPAIR WAS CLASSIFIED AS PERMANENT AND MAJOR WITH NO INSP REQUIRED COMPLETED.Feb 14, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1111315530Doubler · damagedDURING M-CHECK OF THE ACFT A DEFERRED ITEM WAS WORKED TO INCORPORATE DL/NWA EA 55-214988 TO INSTALL A PERMANENT REPAIR DOUBLER. DURING INITIAL WORK TO INSTALL EA 55-214988. REPAIR AN UNREPORTED EXISTING SKIN REPAIR WAS FOUND AT BS560-580 S26L-S28L. ER/A 488Feb 13, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1110275530Floorbeam · corrodedFLOORBEAM STA 345, LBL-63 TO RBL-63 HAS CORROSION. COMPLIED WITH ERA 489011-14 REV ORIGINAL. THIS REPAIR IS MAJOR & PERMANENT WITH NO FURTHER INSPECTIONS REQUIRED. INSPECTION COMPLETED.Feb 12, 2011 · N530US · Boeing 757251 · Fuselage Main, Floor BeamSDR DALA1110255530Floorbeam · corrodedFLOORBEAM, STA 324, BL 0, RBL 63 HAS CORROSION. REMOVED CORROSION FROM FLOOR BEAM STA 324, BL-0. FOUND OUT OF LIMITS. REMOVED WEB FROM RBL 24, STA 324 TO STA 345. FLOORBEAM REPAIRED IAW ERA 488481-14, REV D AND REINSTALLED WEB AT RBL24 STA 324 TO STA 345 IAFeb 12, 2011 · N530US · Boeing 757251 · Fuselage Main, Floor BeamSDR DALA1110265530Crease Beam · corrodedCREASE BEAM ASSY HAS CORROSION STA 1400-1420, RBL 63. COMPLIED WITH ERA 489013-14 REV ORIGINAL. COMPLETED INSPECTION.Feb 11, 2011 · N530US · Boeing 757251 · Fuselage Main, StructureSDR DALA1114565530Skin · gougedDURING M-CHECK AN EXISTING FLUSH REPAIR AT STA 1700-1720, S-17R TO S-20R WAS FOUND WITH GOUGES AND TOOLING MARKS AT THE REPAIR LOCATION. ER/A 488988-14 SECTION I ACCOMPLISHED DURING M-CK FEB 11 AT SAT SECTION II REPAIR APPROVAL IS LIMITED TO 50000 TOTAL CYCLESFeb 10, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1111445530Skin · dentedDURING M-CK AN EXISTING FLUSH SKIN REPAIR WAS FOUND AT STA 1661 TO STA 1681, S-20R TO S-22R. ADDITIONAL DENTS AND TOOLING MARKS WERE ALSO FOUND. ER/A 488989-14AD SECTION I ACCOMPLISHED DURING M-CK AT SAT FEB 2011. SECTION II REPAIR APPROVAL LIMITED TO 42900Feb 10, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1110015530Skin · damagedDURING M-CHECK AT SAT A FLUSH SKIN REPAIR WAS FOUND AT STA 1661 TO STA 1681, S-20R TO S-22R. ADDITIONAL DENTS AND TOOLING MARKS WERE ALSO FOUND AT THE REPAIR LOCATION. ER/A 488989-14 SECTION I ACCOMPLISHED AT SAT M-CK FEB 2011. SECTION II REPAIR APPROVAL Feb 10, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1110235530Skin · damagedFUSELAGE SKIN PANEL, STA 1460, STRINGER 26L DAMAGED. DISCONTINUE REVENUE SERVICE ON OR BEFORE 42,200 TOTAL FLIGHT CYCLES PENDING STAGE III DTA APPROVAL. COMPLIED WITH ERA 488480-14AD REV ORIGINAL. TIME LIMITED REPAIR, REPAIR APPROVAL IS LIMITED TO 42,200 TOTFeb 9, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1110005530Skin · dentedDTA MONITOR INSP, FUSELAGE SKIN PANEL DENTS STA 640 AND STG 15L - 19L. ER/A 488485-14AD WAS APPROVED FOR STAGE I DTA, STATIC STRENGTH, AND IS PENDING STAGE II APPROVAL. THIS APPROVAL IS TEMPORARY FOR ASSOCIATED ER/A 13-488485. THE ER/A 488485-14AD SECTION I Feb 9, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1111325530Doubler · dentedDURING M-CHECK, DENT WAS FOUND AT STA 378, S-14L WITHIN SRM LIMITS EXCEPT ONLY 5.4 INCHES FROM THE L-1 DOOR CUTOUT. DENT WAS CUT OUT AND REPAIRED WITH AN EXTERNAL DOUBLER COMPLIED WITH ERA 488990-14 REV ORIGINAL. THIS IS A TIME LIMITED REPAIR. REPAIR APPRFeb 8, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1108745530Skin · dentedDURING M-CHECK, A DENT WAS FOUND ON THE FUSELAGE SKIN BETWEEN STA 1500 AND STA 1520 AND S-19L AND S-20L. THE DENT MEASURES 8.0" L X 3.50" W X 0.041" DEEP DENT IS LOCATED NEAR TO THE LAP SPLICE AT S-20L. ER/A SECTION, REPAIR APPROVAL IS LIMITED TO 50,000 TOTAFeb 4, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1108735530Skin · damagedDURING MAINTENANCE CHECK INSPECTION FOUND A LIGHTNING STRIKE ON THE FUSELAGE SKIN AT STA 500 BETWEEN S-16R AND S-17R. THE DAMAGE BLENDED AND FOUND OUT OF LIMITS PER B757-200 SRM 53-00-01, FIG 101 ER/A SECTION I REPAIR APPROVAL IS LIMITED TO 38,633 TOTAL AIRFRFeb 4, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1108325530Skin · dentedFUSELAGE DENT WAS FOUND AT STA 500, S-27R. THE DENT WAS REMOVED BY TRIMMING THE SKIN. REPAIR WAS COMPLETED PER SRM 53-00-01 REPAIR 2 EXCEPT THE REPAIR DOUBLER WAS 0.063" THICK. ER/A SECTION I REPAIR IS APPROVED FOR 12 MONTHS (365 DAYS) ONLY. ADDITIONAL ER/Feb 3, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1106675530Box Beam · corrodedBOX BEAM HAS CORROSION STA 1640-1660, RBL-60. R & R BOX BEAM AT STA FS, STA 1640-1660 RBL-60 IAW SRM 51-40-02, PAGE 1-10.Jan 27, 2011 · N530US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1106655530Support Angle · corrodedCREASE BEAM TO FLOOR TRANSITION ANGLE HAS CORROSION STA 660-760 RBL-60. R & R CHORD ZEE ANGLE FROM MAIN CABIN STA 660-760, RBL 60 IAW SRM 51-40-02.Jan 27, 2011 · N530US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1106645530Box Beam · corrodedBOX BEAM HAS CORROSION STA 1660-1680 AT BL-0. R & R BOX BEAM AT FS STA 1660-1680, BL-0 IAW SRM 51-40-02, PAGE 1-10.Jan 27, 2011 · N530US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1106635530Box Beam · corrodedBOX BEAM HAS CORROSION STA1660-1680, RBL-60. R & R BOXBEAM AT FS STA 1660-1680, RBL-60 IAW SRM 51-40-02.Jan 27, 2011 · N530US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1106425530Box Beam · corrodedBOX BEAM HAS CORROSION STA 1640-1660, LBL-60 BLENDED. CORROSION FROM BOX BEAM STA 1640-1660, LBL-60 OUT OF LIMITS IAW SRM 53-00-51. R & R BOX BEAM STA 1640-1660, LBL-60 IAW SRM 51-40-02, COMPLETED.Jan 26, 2011 · N530US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1106405530Box Beam · corrodedBOX BEAM HAS CORROSION STA 1660-1680, LBL-60. REMOVED CORROSION BOX BEAM STA 1660-1680, LBL-60 OUT OF LIMITS IAW SRM 53-00-51, PG:103. R & R BOX BEAM IAW SRM 51-40-02, COMPLETED.Jan 26, 2011 · N530US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1106145530Floorbeam · corrodedFLOORBEAM HAS CORROSION STA 1640, BL-0, RBL-55. REMOVED CORROSION ON FLOORBEAM AT FS STA 1640, BL-0 TO RBL-55, NO CORROSION FOUND. REMOVED CORROSION AT BS 1640 RBL-63. FOUND CORROSION AND DOUBLE HOLES OUT OF LIMITS IAW SRM. REMOVED FLOOR BEAM BS 1640 FROM Jan 25, 2011 · N530US · Boeing 757251 · Fuselage Main, Floor Beam
Back to N530US, cancelled Dec 30, 2022