N628DL, cancelled Aug 21, 2018

Service difficulty reports · 73

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 = 'N628DL' AND deregistration_id = 'N628DL-2018-08-21'
  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 DALA1122080628Wire · shortedFLIGHT RETURNED TO ATL AFTER CABIN CREW REPORTED SPARKS AND A STRONG ELECTRICAL SMELL COMING FROM AN OVERHEAD LIGHT ASSEMBLY. CABIN LIGHTING WAS TURNED OFF. MAINTENANCE FOUND ROW 20ABC WIRING BURNED. REMOVED BURNED WIRES AND RE-PINNED PLUG IN PSU. RESET CIMar 28, 2011 · N628DL · Boeing 757232 · Light System WiringSDR DALA1108340628Light · defectiveCREW REPORTED AN ELECTRICAL ODOR IN THE AFT CABIN. TURNED OFF UTILITY BUSSES AND RECYCLED PACK BLEEDS PER MCC. ODOR IMPROVED WITH CABIN LIGHTS TURNED OFF. MAINTENANCE FOUND SIDEWALL LIGHTS DIM/FLICKERING AND INSPECTED LIGHT SOCKETS AND BALLASTS WITH NO FIFeb 2, 2011 · N628DL · Boeing 757232 · Passenger Compartment LightingSDR DALA1026610628Socket · inoperativeDURING LAYOVER CHECK FOUND DOOR 3L EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED SOCKET.Oct 9, 2010 · N628DL · Boeing 757232 · Emergency LightingSDR DALA1021040628Wire · damagedDURING LAYOVER CHECK, MX FOUND THE MID LAVATORY AREA EMERGENCY PATH LIGHTS INOPERATIVE. MX REPAIRED THE PATH LIGHT WIRING. OPS CHECK WAS GOOD.Aug 29, 2010 · N628DL · Boeing 757232 · Light System WiringSDR DL757100067Bulb · burned outELECTRICAL ODOR 1L LAV. NO ELECTRICAL ODOR. FOUND HOT PLASTIC ODOR COMING FROM OVERHEAD BULB. REPLACED BULB, CKS OK.Jan 11, 2010 · N628DL · Boeing 757232 · Nose/Tail Landing GearSDR DL757090679Warning System · intermittentON TAKEOFF R2 DOOR HANDLE RAISED UP FROM LOCKED POSITION DOOR WARNING INTERMITTENT IN COCKPIT. R2 DOOR MTC IN PROGRESS.Apr 16, 2009 · N628DL · Boeing 757232 · Door Warning SystemSDR DALA1165610628Gearbox · damagedT/E FLAP TRANSMISSION GEARBOX REPAIRED IAW EA 06-097281-03, ME04.Apr 5, 2009 · N628DL · Boeing 757232 · Trailing Edge Flap Control SystemSDR DL757090007Fan · overheatedGOT AN ELECTRICAL ODOR FOLLOWED BY "EQPT OVHT" MESSAGE. RAN EQUIP OVHT CKLIST AND ODOR DISSIPATED. FOUND NR 1 EQUIP COOL FAN INOP. REPLACED NR 1 EQUIP COOLING FAN. CHECKS GOOD. OK FOR SERVICE. LEAK CHECK GOOD.Jan 2, 2009 · N628DL · Boeing 757232 · Air Distribution FanSDR DALA1165710628Plenum · unknownAIRBORNE AUX POWER AIR INTAKE PLENUM REPLACED IAW ERA 465354-14.Nov 28, 2007 · N628DL · Boeing 757232 · APU Cowling/ContainmentSDR DL757071568Bellmouth · crackedAPU AIR INTAKE PLENUM BELLMOUTH CRACKED. MODIFED BELLMOUTH PER SERVICE BULLETIN 757-49-0011.Nov 28, 2007 · N628DL · Boeing 757232 · APU Core EngineSDR DU4R2006445Fitting · wornNR 2 PYLON FOUND LWR FWD OUTBOARD LUG TO BE 2.008, OVERSIZED SHOULD BE > 2.009. REPAIRED BY FABRICATING AND INSTALLING BUSHING 1.748 ID FROM 15-5 PH IAW DELTA ERA 455545-14AD REV ORIGINAL DATED 5-12-06 APPROVED BY FAA FORM 8100-9.May 16, 2006 · N628DL · Boeing 757232 · Nacelle/Pylon Miscellaneous StructureSDR DU4R2006444Frame · misdrilledNR 2 PYLON INBOARD LOWER CHORD FROM PPS 128 TO PPS 138 HAS 8 EACH DRILL MARKS BESIDE FASTENER HOLES. REPAIRED FASTENER HOLES BY FABRICATING AND INSTALLING FREEZE PLUGS 1 EACH .391 X .225 INCH AND 2 EACH .405 X .225 INCH FROM 15-5 PH IAW DELTA ERA 455398-14 REMay 16, 2006 · N628DL · Boeing 757232 · Nacelle/Pylon, Frame/Spar/RibSDR DU4R2006426Tripler · corrodedCORROSION ON FUSELAGE SKIN TRIPLER BS 1466 TO 1478 WL 138.5 BL 0. REMOVED TRIPLER, FABRICATED AND INSTALLED REPAIR TRIPLER 23 X 12.5 INCHES FROM 2024-T3 .063 IAW B757 SRM 51-40-02, 51-20-01 AND 51-41-00352-013.May 11, 2006 · N628DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DU4R2006443Attach Angle · corrodedCORROSION ON INTERCOSTAL ATTACH ANGLE IN AFT PIT BS 1320 RBL 6. FABRICATED AND INSTALLED INTERCOSTAL ATTACH ANGLE 6.75 X 1.25 X 1.25 INCHES FROM 7075-T6 .063 IAW DELTA B757 SRM 51-30-01, 51-20-01, 51-10-2, 51-40-02 AND 51-00-00D.May 10, 2006 · N628DL · Boeing 757232 · Fuselage Main, Attach FittingsSDR DU4R2006442Intercostal · corrodedCORROSION ON INTERCOSTAL LWR LEG IN AFT PIT BS 1480 - 1500 LBL 24. REMOVED INTERCOSTAL, FABRICATED AND INSTALLED INTERCOSTAL ANGLE 16.25 X 2.25 INCHES FROM 7075-T6 .050 IAW DELTA B757 SRM 51-40-02, 53-60-04, 51-70-11, 51-70-01.May 10, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006440Shear Tie · corrodedCORROSION ON BS 1400 FRAME SHEAR TIE S-26R. REMOVED SHEAR TIE, FABRICATED AND INSTALLED SHEAR TIE 6.25 X 2.0 INCHES FROM L-ANGLE EXTRUSION 7075-T6 .100" IAW B757 SRM 51-20-01 AND 51-40-02.May 6, 2006 · N628DL · Boeing 757232 · Fuselage Internal Mounting StructureSDR DU4R2006435Shear Tie · corrodedCORROSION AFT PIT ON FRAME AND FRAME SHEAR TIE BS 1500 S-29L TO S-27L. REMOVED CORROSION ON FRAME, FOUND TO BE WITHIN LIMITS. REMOVED CORRODED SHEAR TIES, FABRICATED AND INSTALLED 2 EACH SHEAR TIES 5.25 X .75 X .75 INCHES FROM 7075-T6 .040 IAW B757 SRM 53-00May 5, 2006 · N628DL · Boeing 757232 · Fuselage Internal Mounting StructureSDR DU4R2006434Intercostal · corrodedCORROSION NOTED ON AFT PIT FLOOR STRUCTURE INTERCOSTAL WEB BS 1460 - 1480 RT. REMOVED CORRODED INTERCOSTAL. FABRICATED AND INSTALLED INTERCOSTAL 19.375 X 7.5 INCHS FROM 7075-T6 .040 IAW B757 SRM 53-60-04 AND 51-40-02.May 5, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006433Panel · corrodedCORROSION NOTED ON AFT PIT PANEL BS 1440 - 1530 RT. REMOVED CORRODED PANEL AND INSTALLED P/N 146N5391-30 IAW B757 SRM 51-10-01 AND 51-40-02.May 5, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006427Angle · corrodedCORROSION ON TRANSITION ANGLE, FROM BS 1310 TO 1380 RT SIDE (ENTIRE LENGTH). REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR DOUBLER 40.75 INCHES FROM 2024-T3. 080", 13 X 6.5 INCHES FROM 7075-T6 .071" AND 33.5 X 1 INCHES AND 7 X 1 INCHES FROM 7075-T6 .063May 5, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006437Intercostal · corrodedCORROSION AFT PIT INTERCOSTAL BS 1540 - BS 1560 LT. FABRICATED AND INSTALLED INTERCOSTAL 19.50 X 3.75 INCHES FROM 7075-T6 .032" IAW BOEING DWG 146N5461-15 AND 51-40-02.May 4, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006431Transition Panel · corrodedLEFT TRANSITION PANEL BS 1410 - 1530 CORRODED BA 1410 TO BS 1530 LT. REMOVED CORRODED PANEL. INSTALLED FABRICATED AND INSTALLED REPLACEMENT WEB 20.875 X 2.75 INCHES FROM 7075-T6 .032 IAW B757 SRM 53-00-04 DETAIL 11 FIG 101, 51-40-02, 51-20-01 AND 51-10-02.May 3, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006436Transition Panel · corrodedCORROSION AFT PIT ON RT TRANSITION PANEL BETWEEN BS 1530 TO 1640. FABRICATED AND INSTALLED TRANSITION PANEL REPAIRS 63 X 1.5 INCHES FROM 2024-T3 .063 AND 64 X 3 INCHES FROM 7075-T6 .071 IAW B757 SRM 51-10-01 AND 53-88-01-801.May 1, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006430Transition Panel · corrodedCORROSION AFT PIT ON LT TRANSITION PANEL NUMEROUS AREAS FROM BS 1530 TO 1640. REMOVED CORRODED TRANSITION PANEL AND INSTALLED NEW PANEL P/N 146N5431-41 IAW B757 SRM 51-40-08 AND 51-40-02.May 1, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006432Door Frame · corrodedCORROSION LT AC BAY DOOR HINGE FRAME FROM BS 900 TO 1040. FABRICATED AND INSTALLED REPLACEMENT BEAM 38 X 1.625 X 2.875 X 1.5 INCHES FROM BAC1505-10047 IAW B757 SRM 51-20-01 AND 51-40-02.May 1, 2006 · N628DL · Boeing 757232 · Fuselage Main, StructureSDR DU4R2006428Floor Support · corrodedCORROSION ON FLOOR SUPPORT STRUCTURE UPPER WEB FROM BS 1320 - 1340 ABOVE S-30, RBL 9. REMOVED CORRODED WEB. FABRICATED AND INSTALLED REPLACEMENT WEB 20.875 X 2.75 INCHES FROM 7075-T6 .032 IAW B757 SRM 53-00-04 DETAIL 11 FIG 101, 51-40-02, 51-20-01 AND 53-60-May 1, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DL757060356Spar · damagedTHE NR 2 PYLON INBOARD MID SPAR CHORD HAS 3 ELONGATED HOLES. HOLES WERE OVERSIZED TO CLEAN UP THE DAMAGE AND BUSHED TO ORIGINAL SIZE AND LOCATION.May 1, 2006 · N628DL · Boeing 757232 · Nacelle/Pylon, Frame/Spar/RibSDR DU4R2006429Web · corrodedCORROSION ON AFT PIT FLOOR STRUCTURE WEB FROM BS 1320 - 1340 LT LBL 9. REMOVED CORRODED WEB. FABRICATED AND INSTALLED REPLACEMENT WEB 20.875 X 2.75 INCHES FROM 7075-T6 .032 IAW B757 SRM 53-00-04 DETAIL 11 FIG 101, 51-40-02, 51-20-01 AND 51-10-02.Apr 30, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006424Floorbeam · corrodedFOUND CORROSION, AFT PIT, ON FLOOR SUPPORT ANGLE LWR SIDE BS 1510 LBL 7. FABRICATED AND INSTALLED REPAIR ANGLE 10 X .75 X .75 INCH FROM 7075-T6 .080 IAW B757 SRM 53-60-53 PG 221 & 222.Apr 28, 2006 · N628DL · Boeing 757232 · Fuselage Main, Floor BeamSDR DU4R2006423Floorbeam · corrodedFOUND CORROSION AFT PIT ON FLOOR SUPPORT ANGLE LWR SIDE BS 1510, LBL 3. FABRICATED AND INSTALLED REPAIR ANGLE 10 INCHES LONG FROM 7075-T6 .080 IAW B757 SRM 53-60-53 PG 221 AND 222.Apr 28, 2006 · N628DL · Boeing 757232 · Fuselage Main, Floor BeamSDR DU4R2006422Floorbeam · corrodedFOUND CORROSION AFT PIT ON FLOOR SUPPORT ANGLE LWR SIDE BS 1510, RBL 7. FABRICATED AND INSTALLED REPAIR ANGLE 8.75 INCHES LONG FROM 7075-T6 .080 IAW B757 SRM 53-60-53 PG 221 AND 222.Apr 28, 2006 · N628DL · Boeing 757232 · Fuselage Main, Floor BeamSDR DUR42006417Skin · dentedFOUND CREASE 28" AFT OF L-4 DOOR AT SILL LEVEL. CUT OUT CREASED AREA IAW B757 SRM 53-00-01 FIG 201. HFEC FOR CRACKS IAW D6-34N301-6-51-00P6. FABRICATED AND INSTALLED REPAIR DOUBLER X 4.75" FROM 2024-T3 0.090" IAW B757 SRM 53-00-01 FIG 201 REPAIR 3.Apr 27, 2006 · N628DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DUR42006416Frame · dentedFOUND FRAME DENTED AT S-25L IN AFT PIT BS 1480. CUT OUT DENTED AREA IAW B757 SRM 51-70-11. FABRICATED AND INSTALLED FORMED SECTION REPAIR 210.50" BY 4.75" FROM 7075-0 .050" HEAT TREATED TO TPS-1002 IAW B757 SRM 51-20-01 AND 51-70-11.Apr 27, 2006 · N628DL · Boeing 757232 · Fuselage Main, FrameSDR DUR42006413Floor Support · corrodedFOUND CORROSION AROUND NUTPLATES ON FLOOR SUPPORT RBL NR 10, NR 45 SEVERAL AREAS FROM BS 1400 TO BS 1440. FABRICATED AND INSTALLED REPAIR SUPPORT 102-1/8" FROM BAC1517-2226 IAW B757 SRM 53-00-53 AND 53-87-01-801.Apr 26, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006403Panel · corrodedFOUND CORROSION ON RT TRANSITION STRIP BETWEEN BS 645 AND 765 (FWD CARGO). FABRICATED AND INSTALLED REPAIR DOUBLER 6-1/4" BY 2.5" BY 1-1/4" BY 3/4" FROM 7075 T6 .071 AND FILLER 2.5" BY 2.8" BY 1/4" FROM 7075-T6 .063" IAW B757 AMM 53-88-01-801.Apr 26, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006401Floor Support · corrodedFOUND CORROSION ON FLOOR SUPPORT AT BS 1340 LBL 16 ABOVE S-29L (AFT PIT). FABRICATED AND INSTALLED DOUBLER REPAIR 5-3/4" FROM 301 .032 HD AND REPAIR SUPPORT 17" FROM BAC1517-2226 7075-T65 IAW B757 SRM 51-20-01 AND B757 MM 53-87-01-801.Apr 26, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006408Skin · puncturedFOUND PUNCTURED HOLE IN EXTERNAL FUSELAGE SKIN BS 1927 LBL 5.5, ABOVE APU. CUT OUT AND REMOVED PUNCTURED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER 4.25" IN DIAMETER FROM 2024-T3 .020 IAW B757 SRM 53-80-01, 51-70-10 FIG 203.Apr 25, 2006 · N628DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DU4R2006402Frame · corrodedFOUND CORROSION ON FRAME ANGLE BS 1360 BETWEEN S-27L AND S-25L (AFT PIT). FABRICATED AND INSTALLED CHANNEL REPAIR 31" BY 3" FROM 2024-T3 .050" IAW B757 SRM 51-20-01, 51-40-02 AND BOEING DRAWING 453N1801.Apr 25, 2006 · N628DL · Boeing 757232 · Fuselage Main, FrameSDR DU4R2006438Intercostal · corrodedCORROSION ON FLOOR STRUCTURE AT L4 DOOR BETWEEN BS 1640 TO 1681. FABRICATED AND INSTALLED 2 EACH INTERCOSTAL WEBS 21.75 X 3.5 X 1.8 INCHES FROM 7075-T6 .071" IAW B757 SRM 51-30-01, 51-40-05 AND 51-40-02.Apr 24, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006411Cusp Web · corrodedFOUND CORROSION AT CABIN FLOOR STRUCTURE RBL 65 BS 996. FABRICATED AND INSTALLED REPAIR STIFFENER 3-3/4" BY 3-7/8" FROM 7075-T6 .090" IAW B757 SRM 53-40-13, 51-40-02 PG, 6, 7, AND 51-20-01.Apr 24, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006410Intercostal · corrodedFOUND CORROSION IN AFT PIT ON FRAME UPPER ANGLE BS 1560, S-26R TO S-23R (UPPER SURFACE). CUT OUT CORRODED "C" CHANNEL. FABRICATED AND INSTALLED REPAIR "C" CHANNEL 34" BY 1.25" FROM 2024-T4 .050" IAW B757 SRM 51-30-1, 51-20-01 AND 51-40-02.Apr 24, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006407Floor Support · corrodedFOUND CORROSION ON FLOOR STRUCTURE AT R-4 DOOR BETWEEN BS 1640 AND BS 1681. REMOVED CORRODED FLOOR SUPPORT. FABRICATED AND INSTALLED FORMED SECTION REPAIRS 3.5" BY 2.25" BY 1" AND 3-9/16" BY 1-5/8" BY 11/16" FROM 7075-T6 .080" AND 1-3/4" BY 5/8" AND 1-3/8" BApr 24, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006404Intercostal · corrodedFOUND CORROSION ON WEB AT FWD END AT SKIN BELOW FLOOR SUPPORT RBL 2.90 FROM BS 1400 TO 1420 (AFT CARGO). REMOVED CORRODED INTERCOSTAL. FABRICATED AND INSTALLED REPAIR INTERCOSTAL 19-3/8" FROM 7075-T6 .040" FROM B757 SRM 51-10-02, 51-20-01 AND 51-40-02.Apr 24, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006400Panel · corrodedFOUND CORROSION ON NUMEROUS AREAS OF TRANSITION ANGLE FROM BS 1200 TO 1310 RT. DRILLED AND INSTALLED NEW TRANSITION PANEL IAW B757 SRM 53-00-53 FIG 101.Apr 24, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006425Frame · corrodedFOUND CORROSION, AFT PIT, ON ATTACH ANGLE FOR FLOOR AND SIDEWALL PANELS (ALSO MISDRILLED HOLES, LOOSE FASTENERS) BS 1640 S-22R TO S-22L. FABRICATED AND INSTALLED REPAIR ATTACH ANGLE 3.5 X 1.5 INCH AND 2 EA ATTACH ANGLES 1.5 X 2.5 INCH FROM 2024-T3 .050 IAW B7Apr 21, 2006 · N628DL · Boeing 757232 · Fuselage Main, FrameSDR DUR42006415Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM BETWEEN R-1 AND L-1 DOORS BS 345. FABRICATED AND INSTALLED REPLACEMENT UPPER CAP 11 FEET BY 2" FROM BAC1505-100617 7075-T73 IAW B757 SRM 53-10-51 PG 217.Apr 19, 2006 · N628DL · Boeing 757232 · Fuselage Main, Floor BeamSDR DUR42006414Intercostal · corrodedFOUND CORROSION IN AFT PIT ON WEB BS 1600 TO 1620 INBD OF S-28L. FABRICATED AND INSTALLED INTERCOSTAL 19-5/8" BY 7-1/2" FROM 7075-T6 .040 IAW B757 SRM 51-20-01 AND 51-40-02.Apr 19, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006409Floorbeam · corrodedFOUND CORROSION ON FLOOR FRAME UPPER SURFACE, BS 700 INBD OF L2 DOOR AND UNDER CENTER FLOOR PANEL. CUT OUT CORRODED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER 14-1/2" BY 1-1/4" FROM 2075-T6 .063 AND 13" BY 1" BY 1/2" FROM 7075-T6 .080 IAW B757 SRM 53-00-5Apr 19, 2006 · N628DL · Boeing 757232 · Fuselage Main, Floor BeamSDR DU4R2006439Seat Track · corrodedCORROSION ON LEFT O/B SEAT TRACK BS 1027. FABRICATED AND INSTALLED SEAT TRACK BS 898 TO BS 1075 177 INCHES FROM BAC1520-541 IAW B757 SRM 51-40-02 AND 53-00-52.Apr 17, 2006 · N628DL · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR DU4R2006418Floorbeam · corrodedFOUND CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 720 INBD OF L2 DOOR AND UNDER CENTER FLOOR PANEL. FABRICATED AND INSTALLED FLOORBEAM REPAIR 12.25" BY 1.75" BY .9" FROM 7075-T6 .080" AND 15.25" BY 1.8" BY 1" FROM 7075-T6 .063" IAW B757 SRM 53-30-51D FIG 20Apr 17, 2006 · N628DL · Boeing 757232 · Fuselage Main, Floor Beam
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