# Service difficulty reports: N628DL, cancelled Aug 21, 2018

A list on [N628DL, cancelled Aug 21, 2018](https://openairdocs.org/deregistered/N628DL-2018-08-21.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 73 reports

- [SDR DALA1122080628](https://openairdocs.org/sdr/DALA1122080628.md): Wire · shorted · Mar 28, 2011 · N628DL · Boeing 757232 · Light System Wiring
  > FLIGHT 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 CI
- [SDR DALA1108340628](https://openairdocs.org/sdr/DALA1108340628.md): Light · defective · Feb 2, 2011 · N628DL · Boeing 757232 · Passenger Compartment Lighting
  > CREW 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 FI
- [SDR DALA1026610628](https://openairdocs.org/sdr/DALA1026610628.md): Socket · inoperative · Oct 9, 2010 · N628DL · Boeing 757232 · Emergency Lighting
  > DURING LAYOVER CHECK FOUND DOOR 3L EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED SOCKET.
- [SDR DALA1021040628](https://openairdocs.org/sdr/DALA1021040628.md): Wire · damaged · Aug 29, 2010 · N628DL · Boeing 757232 · Light System Wiring
  > DURING LAYOVER CHECK, MX FOUND THE MID LAVATORY AREA EMERGENCY PATH LIGHTS INOPERATIVE. MX REPAIRED THE PATH LIGHT WIRING. OPS CHECK WAS GOOD.
- [SDR DL757100067](https://openairdocs.org/sdr/DL757100067.md): Bulb · burned out · Jan 11, 2010 · N628DL · Boeing 757232 · Nose/Tail Landing Gear
  > ELECTRICAL ODOR 1L LAV. NO ELECTRICAL ODOR. FOUND HOT PLASTIC ODOR COMING FROM OVERHEAD BULB. REPLACED BULB, CKS OK.
- [SDR DL757090679](https://openairdocs.org/sdr/DL757090679.md): Warning System · intermittent · Apr 16, 2009 · N628DL · Boeing 757232 · Door Warning System
  > ON TAKEOFF R2 DOOR HANDLE RAISED UP FROM LOCKED POSITION DOOR WARNING INTERMITTENT IN COCKPIT. R2 DOOR MTC IN PROGRESS.
- [SDR DALA1165610628](https://openairdocs.org/sdr/DALA1165610628.md): Gearbox · damaged · Apr 5, 2009 · N628DL · Boeing 757232 · Trailing Edge Flap Control System
  > T/E FLAP TRANSMISSION GEARBOX REPAIRED IAW EA 06-097281-03, ME04.
- [SDR DL757090007](https://openairdocs.org/sdr/DL757090007.md): Fan · overheated · Jan 2, 2009 · N628DL · Boeing 757232 · Air Distribution Fan
  > GOT 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.
- [SDR DALA1165710628](https://openairdocs.org/sdr/DALA1165710628.md): Plenum · unknown · Nov 28, 2007 · N628DL · Boeing 757232 · APU Cowling/Containment
  > AIRBORNE AUX POWER AIR INTAKE PLENUM REPLACED IAW ERA 465354-14.
- [SDR DL757071568](https://openairdocs.org/sdr/DL757071568.md): Bellmouth · cracked · Nov 28, 2007 · N628DL · Boeing 757232 · APU Core Engine
  > APU AIR INTAKE PLENUM BELLMOUTH CRACKED. MODIFED BELLMOUTH PER SERVICE BULLETIN 757-49-0011.
- [SDR DU4R2006445](https://openairdocs.org/sdr/DU4R2006445.md): Fitting · worn · May 16, 2006 · N628DL · Boeing 757232 · Nacelle/Pylon Miscellaneous Structure
  > NR 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.
- [SDR DU4R2006444](https://openairdocs.org/sdr/DU4R2006444.md): Frame · misdrilled · May 16, 2006 · N628DL · Boeing 757232 · Nacelle/Pylon, Frame/Spar/Rib
  > NR 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 RE
- [SDR DU4R2006426](https://openairdocs.org/sdr/DU4R2006426.md): Tripler · corroded · May 11, 2006 · N628DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > CORROSION 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.
- [SDR DU4R2006443](https://openairdocs.org/sdr/DU4R2006443.md): Attach Angle · corroded · May 10, 2006 · N628DL · Boeing 757232 · Fuselage Main, Attach Fittings
  > CORROSION 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.
- [SDR DU4R2006442](https://openairdocs.org/sdr/DU4R2006442.md): Intercostal · corroded · May 10, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION 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.
- [SDR DU4R2006440](https://openairdocs.org/sdr/DU4R2006440.md): Shear Tie · corroded · May 6, 2006 · N628DL · Boeing 757232 · Fuselage Internal Mounting Structure
  > CORROSION 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.
- [SDR DU4R2006435](https://openairdocs.org/sdr/DU4R2006435.md): Shear Tie · corroded · May 5, 2006 · N628DL · Boeing 757232 · Fuselage Internal Mounting Structure
  > CORROSION 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 53-00
- [SDR DU4R2006434](https://openairdocs.org/sdr/DU4R2006434.md): Intercostal · corroded · May 5, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION 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.
- [SDR DU4R2006433](https://openairdocs.org/sdr/DU4R2006433.md): Panel · corroded · May 5, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION 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.
- [SDR DU4R2006427](https://openairdocs.org/sdr/DU4R2006427.md): Angle · corroded · May 5, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION 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-T6.063
- [SDR DU4R2006437](https://openairdocs.org/sdr/DU4R2006437.md): Intercostal · corroded · May 4, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION 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.
- [SDR DU4R2006431](https://openairdocs.org/sdr/DU4R2006431.md): Transition Panel · corroded · May 3, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > LEFT 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.
- [SDR DU4R2006436](https://openairdocs.org/sdr/DU4R2006436.md): Transition Panel · corroded · May 1, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION 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.
- [SDR DU4R2006430](https://openairdocs.org/sdr/DU4R2006430.md): Transition Panel · corroded · May 1, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION 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.
- [SDR DU4R2006432](https://openairdocs.org/sdr/DU4R2006432.md): Door Frame · corroded · May 1, 2006 · N628DL · Boeing 757232 · Fuselage Main, Structure
  > CORROSION 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.
- [SDR DU4R2006428](https://openairdocs.org/sdr/DU4R2006428.md): Floor Support · corroded · May 1, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION 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-
- [SDR DL757060356](https://openairdocs.org/sdr/DL757060356.md): Spar · damaged · May 1, 2006 · N628DL · Boeing 757232 · Nacelle/Pylon, Frame/Spar/Rib
  > THE 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.
- [SDR DU4R2006429](https://openairdocs.org/sdr/DU4R2006429.md): Web · corroded · Apr 30, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION 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.
- [SDR DU4R2006424](https://openairdocs.org/sdr/DU4R2006424.md): Floorbeam · corroded · Apr 28, 2006 · N628DL · Boeing 757232 · Fuselage Main, Floor Beam
  > FOUND 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.
- [SDR DU4R2006423](https://openairdocs.org/sdr/DU4R2006423.md): Floorbeam · corroded · Apr 28, 2006 · N628DL · Boeing 757232 · Fuselage Main, Floor Beam
  > FOUND 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.
- [SDR DU4R2006422](https://openairdocs.org/sdr/DU4R2006422.md): Floorbeam · corroded · Apr 28, 2006 · N628DL · Boeing 757232 · Fuselage Main, Floor Beam
  > FOUND 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.
- [SDR DUR42006417](https://openairdocs.org/sdr/DUR42006417.md): Skin · dented · Apr 27, 2006 · N628DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FOUND 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.
- [SDR DUR42006416](https://openairdocs.org/sdr/DUR42006416.md): Frame · dented · Apr 27, 2006 · N628DL · Boeing 757232 · Fuselage Main, Frame
  > FOUND 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.
- [SDR DUR42006413](https://openairdocs.org/sdr/DUR42006413.md): Floor Support · corroded · Apr 26, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR DU4R2006403](https://openairdocs.org/sdr/DU4R2006403.md): Panel · corroded · Apr 26, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR DU4R2006401](https://openairdocs.org/sdr/DU4R2006401.md): Floor Support · corroded · Apr 26, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR DU4R2006408](https://openairdocs.org/sdr/DU4R2006408.md): Skin · punctured · Apr 25, 2006 · N628DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FOUND 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.
- [SDR DU4R2006402](https://openairdocs.org/sdr/DU4R2006402.md): Frame · corroded · Apr 25, 2006 · N628DL · Boeing 757232 · Fuselage Main, Frame
  > FOUND 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.
- [SDR DU4R2006438](https://openairdocs.org/sdr/DU4R2006438.md): Intercostal · corroded · Apr 24, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION 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.
- [SDR DU4R2006411](https://openairdocs.org/sdr/DU4R2006411.md): Cusp Web · corroded · Apr 24, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR DU4R2006410](https://openairdocs.org/sdr/DU4R2006410.md): Intercostal · corroded · Apr 24, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR DU4R2006407](https://openairdocs.org/sdr/DU4R2006407.md): Floor Support · corroded · Apr 24, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > FOUND 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" B
- [SDR DU4R2006404](https://openairdocs.org/sdr/DU4R2006404.md): Intercostal · corroded · Apr 24, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR DU4R2006400](https://openairdocs.org/sdr/DU4R2006400.md): Panel · corroded · Apr 24, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR DU4R2006425](https://openairdocs.org/sdr/DU4R2006425.md): Frame · corroded · Apr 21, 2006 · N628DL · Boeing 757232 · Fuselage Main, Frame
  > FOUND 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 B7
- [SDR DUR42006415](https://openairdocs.org/sdr/DUR42006415.md): Floorbeam · corroded · Apr 19, 2006 · N628DL · Boeing 757232 · Fuselage Main, Floor Beam
  > FOUND 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.
- [SDR DUR42006414](https://openairdocs.org/sdr/DUR42006414.md): Intercostal · corroded · Apr 19, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR DU4R2006409](https://openairdocs.org/sdr/DU4R2006409.md): Floorbeam · corroded · Apr 19, 2006 · N628DL · Boeing 757232 · Fuselage Main, Floor Beam
  > FOUND 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 53-00-5
- [SDR DU4R2006439](https://openairdocs.org/sdr/DU4R2006439.md): Seat Track · corroded · Apr 17, 2006 · N628DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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.
- [SDR DU4R2006418](https://openairdocs.org/sdr/DU4R2006418.md): Floorbeam · corroded · Apr 17, 2006 · N628DL · Boeing 757232 · Fuselage Main, Floor Beam
  > FOUND 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 20

Next page: https://openairdocs.org/deregistered/N628DL-2018-08-21/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N628DL-2018-08-21/reports

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