# Service difficulty reports: N680DA, cancelled Jul 14, 2025

A list on [N680DA, cancelled Jul 14, 2025](https://openairdocs.org/deregistered/N680DA-2025-07-14.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 3 · 126 reports

- [SDR DALA2024082108326](https://openairdocs.org/sdr/DALA2024082108326.md): Control Panel · inoperative · Aug 20, 2024 · N680DA · Boeing 757232 · Emergency Lighting
  > SHIP 680 EMER LIGHT GUARD SWITCH INOP. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHTS SWITCH PANEL PER B-757 M/M 33-51. OPS NORMAL. (5907482)
- [SDR DALA2024081408139](https://openairdocs.org/sdr/DALA2024081408139.md): Idg · failed · Aug 13, 2024 · N680DA · Boeing 757232 · AC Generator-Alternator
  > SHIP 0680 -MISC/DE- DUE TO LEFT ELECTRICAL SYSTEM FAULTS. CORRECTIVE ACTION: DEFERRED LEFT ENGINE GENERATOR. (IDG AND HARNESS SUBSEQUENTLY REPLACED)
- [SDR DALA2024080207734](https://openairdocs.org/sdr/DALA2024080207734.md): Wire Harness · arced · Jul 30, 2024 · N680DA · Boeing 757232 · Electrical Power System Wiring
  > SHIP 680 LEFT GEN CONT TRIPS. RESET PER QRH TRIPPED AGAIN. CORRECTIVE ACTION: FOUND IDG HARNESS ARCING AT PYLON CONNECTOR. R/R IDG HARNESS D1092P PER SWPM CH. 20. REMOVED AND REPLACED CONNECTOR D1092J REF. B757 SWPM 20-41-21 AND 20-61-19. REQUIRES OPS CHECK. (
- [SDR DALA2024041704519](https://openairdocs.org/sdr/DALA2024041704519.md): Indicator · malfunctioned · Apr 14, 2024 · N680DA · Boeing 757232 · Emergency Equipment
  > SHIP 680 2R KNUCKLE KNOCKER NOT EXTENDING. CORRECTIVE ACTION: FOUND 2R KNUCKLE KNOCKER BINDING ON DOOR TRIM. ADJUSTED LINING. REF B757 AMM 52-11. CHECKS GOOD. (0294024)
- [SDR DALA2024041504463](https://openairdocs.org/sdr/DALA2024041504463.md): Indicator · none · Apr 11, 2024 · N680DA · Boeing 757232 · Emergency Equipment
  > R2 DOOR KNUCKLE KNOCKER DOES NOT EXTEND. OPERATED ALL CABIN DOORS & 2R 2 TIMES IAW AMM 52-11 ALL FUNCTION PROPERLY.
- [SDR DALA2024040904257](https://openairdocs.org/sdr/DALA2024040904257.md): Indicator · stuck · Apr 7, 2024 · N680DA · Boeing 757232 · Emergency Equipment
  > SHIP 680 2R DOOR KNUCKLE KNOCKER STUCK. CORRECTIVE ACTION: KNUCKLE KNOCKER DEPLOYS AND STOWS AS INTENDED. (5372220)
- [SDR DALA2024040203971](https://openairdocs.org/sdr/DALA2024040203971.md): Wire · broken · Mar 28, 2024 · N680DA · Boeing 757232 · Instrument System Wiring
  > SHIP 680 ENTER PANEL BACKLIGHTING FROM STBY INSTRUMENTS TO GEAR HANDLE BEGAN FLICKERING DURING T/O ROLL. FAINT BURNING SMELL ACCOMPANIED THE CONDITION. PANEL LIGHTS TURNED OFF AND SMELL CLEARED QUICKLY. CORRECTIVE ACTION: T/S PER B757 WDM 33-13-12. R/R STBY LI
- [SDR DALA2023122110447](https://openairdocs.org/sdr/DALA2023122110447.md): Unknown · unknown · Dec 19, 2023 · N680DA · Boeing 757232 · Light System Wiring
  > SHIP 0680 EMERGENCY INTERIOR LIGHT ON CEILING PANEL INOPERATIVE AT SEAT 42. CORRECTIVE ACTION: FOUND LOOSE CONNECTION ON LIGHT WIRE. OPS CHK GOOD. (5001860)
- [SDR DALA2023080406336](https://openairdocs.org/sdr/DALA2023080406336.md): Unknown · unknown · Aug 2, 2023 · N680DA · Boeing 757232 · Leading Edge Slat Position Indicating System
  > SHIP 0680 -ATB/DE- AIRCRAFT RETURNED TO ATL AFTER QRH COMPLETION FOR LE SLAT ASYM INDICATION. CORRECTIVE ACTION: C/W OVERWEIGHT LANDING INSP. FOUND SLAT LOSS SWITCH TRIPPED AND RT O/B SLAT LOSS SWITCH CABLE TENSION OUT OF RIG, REPLACED R/H LEADING EDGE SLAT PO
- [SDR DALA2023080106236](https://openairdocs.org/sdr/DALA2023080106236.md): Unknown · unknown · Jul 31, 2023 · N680DA · Boeing 757232 · Leading Edge Slat Position Indicating System
  > SHIP 0680 -MISC/DE- CREW ELECTED DE AFTER QRH COMPLETION FOR LE SLAT ASYM INDICATION. CORRECTIVE ACTION: FOUND R/H O/B SLAT LOSS SWITCH TRIPPED. CABLE AND SLAT LOSS SYSTEM INTACT. FOUND R/H O/B SLAT ROTARY ACTUATOR NBR 20 TORQUE INDICATOR TRIPPED. R/R NBR 20 R
- [SDR DALA2024040804204](https://openairdocs.org/sdr/DALA2024040804204.md): Hinge · misinstalled · Jul 17, 2023 · N680DA · Boeing 757232 · Fuselage, Door Hinge
  > SHIP 680 NO. 2 PASSENGER DOOR FWD FRAME UPPER HINGE CUTOUT SHORT EDGE DISTANCE ON FACTORY SRM REPAIR DOUBLER. CORRECTIVE ACTION: REF ERA 608571-14. (2870814)
- [SDR DALA2023061304849](https://openairdocs.org/sdr/DALA2023061304849.md): Unknown · unknown · Jun 11, 2023 · N680DA · Boeing 757232 · Wing, Plate/Skin
  > SHIP 680 AD - AWR - DAMAGES WERE FOUND ON LH ENG DRAG FTG AND CLAMP-UP HOLES 1-10 AS FOLLOW: HOLE #1 TO #10 CORROSION ON SKIN AND FITTING ALL AROUND, ADDITIONALLY HOLE #7 GOUGE ON FITTING AT 6 CLOCK POSITION, IN REFERENCE TO JOB 068-0001 / CARD. CORRECTIVE ACT
- [SDR DALA2023061204759](https://openairdocs.org/sdr/DALA2023061204759.md): Unknown · unknown · Jun 9, 2023 · N680DA · Boeing 757232 · Leading Edge Devices
  > SHIP 680 A.A.-A.D. DISBOND (2.000 IN X 2.000 IN) AT ISS 158, UPPER SURFACE LE SLAT 5 TRAILING EDGE WEDGE, LH WING. CORRECTIVE ACTION: SUMMARY OF NRC: 00005 AT ISS 158, UPPER SURFACE LE SLAT 5 TRAILING EDGE WEDGE, LH WING. WAS REPAIRED PER B757-200 SRM. (280856
- [SDR DALA2023061204758](https://openairdocs.org/sdr/DALA2023061204758.md): Unknown · unknown · Jun 9, 2023 · N680DA · Boeing 757232 · Wing Structure
  > SHIP 680 AD - AWR - DAMAGES WERE FOUND ON LH ENG DRAG FTG AND CLAMP-UP COUNTERSINKS 11-18 AS FOLLOW: COUNTERSINK #11 WORN AREAS BETWEEN 3 TO 4 CLOCK POSITION; COUNTERSINK #12 WORN AREAS BETWEEN 10 TO 11 CLOCK POSITION; COUNTERSINK #13 CORROSION BETWEEN 5 TO 11
- [SDR DALA2023061204757](https://openairdocs.org/sdr/DALA2023061204757.md): Unknown · unknown · Jun 9, 2023 · N680DA · Boeing 757232 · Wing Structure
  > SHIP 680 AD - AWR - DAMAGES WERE FOUND ON LH ENG DRAG FTG AND CLAMP-UP COUNTERSINKS 1-10 AS FOLLOW: COUNTERSINK #1 CORROSION BETWEEN 9 TO 12 CLOCK POSITON AND WORN AREAS AT 1 AND 5 CLOCK POSITIONS; COUNTERSINK #2 CORROSION BETWEEN 9 TO 11 CLOCK POSITION; COUNT
- [SDR DALA2023061904953](https://openairdocs.org/sdr/DALA2023061904953.md): Unknown · unknown · Jun 8, 2023 · N680DA · Boeing 757232 · Wing, Plate/Skin
  > SHIP 680 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 609107-14AD CORRECTIVE ACTION: ACCOMPLISH SECTION III REPETITIVE DVI INSPECTIONS PRIOR TO 41,931 TOTAL FLIGHT CYCLES, AND REPETITIVELY EVERY 3,000
- [SDR DALA2023061904951](https://openairdocs.org/sdr/DALA2023061904951.md): Unknown · unknown · Jun 8, 2023 · N680DA · Boeing 757232 · Wing, Plate/Skin
  > SHIP 680 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 609107-14AD. CORRECTIVE ACTION: ACCOMPLISH SECTION VI REPETITIVE UT INSPECTIONS PRIOR TO 43,731 TOTAL FLIGHT CYCLES, AND REPETITIVELY EVERY 4,800
- [SDR DALA2023061904950](https://openairdocs.org/sdr/DALA2023061904950.md): Unknown · unknown · Jun 8, 2023 · N680DA · Boeing 757232 · Wing, Plate/Skin
  > SHIP 680 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 609107-14AD. CORRECTIVE ACTION: ACCOMPLISH SECTION V REPETITIVE BHEC INSPECTIONS (11-18) PRIOR TO 44,931 TOTAL FLIGHT CYCLES, AND REPETITIVELY EVE
- [SDR DALA2023061904949](https://openairdocs.org/sdr/DALA2023061904949.md): Unknown · unknown · Jun 8, 2023 · N680DA · Boeing 757232 · Wing, Plate/Skin
  > SHIP 680 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 609107-14AD. CORRECTIVE ACTION: ACCOMPLISH SECTION IV REPETITIVE BHEC INSPECTIONS (1-10) PRIOR TO 41,931 TOTAL FLIGHT CYCLES, AND REPETITIVELY EVE
- [SDR DALA2023060904706](https://openairdocs.org/sdr/DALA2023060904706.md): Unknown · unknown · Jun 8, 2023 · N680DA · Boeing 757232 · Wing, Plate/Skin
  > SHIP 680 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 609107-14AD. CORRECTIVE ACTION: REF ERA 609107-14AD. (2806394)
- [SDR DALA2023060904702](https://openairdocs.org/sdr/DALA2023060904702.md): Unknown · unknown · Jun 7, 2023 · N680DA · Boeing 757232 · Leading Edge Devices
  > SHIP 680 A.A.-A.D. DISBOND (2.250 IN X 1.500 IN) AT OSS 523 UPPER SURFACE LE SLAT 8 TRAILING EDGE WEDGE, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00007: UPPER SURFACE LE SLAT 8 TRAILING EDGE WEDGE, RH WING AT OSS 523. WAS REPAIRED PER B757-200 AMM 51-21- 14
- [SDR DALA2023060704658](https://openairdocs.org/sdr/DALA2023060704658.md): Unknown · unknown · Jun 4, 2023 · N680DA · Boeing 757232 · Wing, Plate/Skin
  > SHIP 680 A.A/A.D. NICK ON COUNTERSINK AT HOLE 5 BTW 4-7 HRS AND BTW 11-1 HRS. RH ENG DRAG FTG CLAMP-UP RH WING (REF. CARD). CORRECTIVE ACTION: SUMMARY OF NRC 00235: COUNTERSINK AT HOLE 5 BTW 4-7 HRS AND BTW 11-1 HRS. RH ENG DRAG FTG CLAMP-UP RH WING WAS REPAI
- [SDR DALA2023060704657](https://openairdocs.org/sdr/DALA2023060704657.md): Unknown · unknown · Jun 4, 2023 · N680DA · Boeing 757232 · Wing Structure
  > SHIP 680 A.A/A.D.DAMAGES WERE FOUND AS FOLLOWS: NICK ON COUNTERSINK AT HOLE 14 BTW 4-6 HRS AND BTW 10-12 HRS, HOLE 18 6 HRS AND 2 HRS. RH ENG DRAG FTG CLAMP-UP RH WING (REF. CARD). CORRECTIVE ACTION: SUMMARY OF NRC 00237: NICK ON COUNTERSINK AT HOLE 14 BTW 4-6
- [SDR DALA2023060704656](https://openairdocs.org/sdr/DALA2023060704656.md): Unknown · unknown · Jun 4, 2023 · N680DA · Boeing 757232 · Wing Structure
  > SHIP 680 A.A/A.D. DAMAGES WERE FOUND AS FOLLOWS: CORROSION ON HOLE 5 FITTING BTW 6-8 HRS, HOLE 3 SKIN BTW 9-12 HRS, HOLE 8 SKIN/ FITTING BTW 3-5 HRS, HOLE 6 SKIN BTW 5-6 HRS ALSO GOUGES ON HOLE 4 SKIN 6 HRS, HOLE 2 SKIN 5 HRS, HOLE 10 FITTING BTW 6-7 HRS, HOLE
- [SDR DALA2023060604617](https://openairdocs.org/sdr/DALA2023060604617.md): Unknown · unknown · Jun 2, 2023 · N680DA · Boeing 757232 · Wing, Plate/Skin
  > SHIP 680 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 609153-14AD. CORRECTIVE ACTION: REF ERA 609153-14AD. (2796803)
- [SDR DALA2023060504508](https://openairdocs.org/sdr/DALA2023060504508.md): Unknown · unknown · May 31, 2023 · N680DA · Boeing 757232 · Wing Structure
  > SHIP 680 A.A.-A.D. DISBOND (1.500 IN X 1.500 IN) ON PREVIOUS REPAIR AT OSS 469, UPPER SURFACE LE SLAT 8 TRAILING EDGE WEDGE, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00006: UPPER SURFACE (OSS 469) SLAT 8 TRAILING EDGE WEDGE RH WING WAS REPAIRED PER B757-200
- [SDR DALA2023051904010](https://openairdocs.org/sdr/DALA2023051904010.md): Unknown · unknown · May 17, 2023 · N680DA · Boeing 757232 · Fuselage Structure (General)
  > SHIP 680 AMOC, ER/A 608829-14AD - SECTION I REPAIR IS COMMON TO SSI INSPECTION AREA SSI 53-60-24. REF ERA 608829-14AD. (2771971)
- [SDR DALA2022120707867](https://openairdocs.org/sdr/DALA2022120707867.md): None · none · Jul 18, 2022 · N680DA · Boeing 757232 · Standard Practices/Structures
  > DTA MONITOR INSPECTION LOG IAW ERA 494839-14 REV. C. ERA 494839-14 REV C.
- [SDR DALA2020031001764](https://openairdocs.org/sdr/DALA2020031001764.md): Fitting · obstructed · Mar 6, 2020 · N680DA · Boeing 757232 · Passenger/Crew Doors
  > (AIRCRAFT 680, L/P 7219792) GUST LOCK ON 2L DOOR WILL NOT ENGAGE. CORRECTIVE ACTION: CLEARED DEBRIS FROM L2 DOOR FITTING AND LUBED HOLD OPEN LOCK COLLAR AND OPS CK OK PER B757-AMM-52-11.
- [SDR DALA2019100985799](https://openairdocs.org/sdr/DALA2019100985799.md): Stop Fitting · missing · Oct 7, 2019 · N680DA · Boeing 757232 · Passenger/Crew Doors
  > DURING A-CHK FOUND 1 DOOR STOP FITTING MISSING ON L2 AND R2 DOORS. INSTALLED DOOR STOP FITTINGS IAW AMM 52-11-00.
- [SDR DALA201902153108](https://openairdocs.org/sdr/DALA201902153108.md): Indicator · sticking · Feb 12, 2019 · N680DA · Boeing 757232 · Emergency Equipment
  > SHIP 680 KNUCKLE-KNOCKER ON AFT LEFT DOOR STICKS. IT POPPED OUT AS ARMED ON TAXI VICE WHEN ARMED. CORRECTIVE ACTION: OPERATED SEVERAL TIMES. KNOCKER OPS CHK NML. (5601926)
- [SDR DALA2023052604208](https://openairdocs.org/sdr/DALA2023052604208.md): None · none · Dec 17, 2018 · N680DA · Boeing 757232 · Fuselage Structure (General)
  > SHIP 680 ERA 571509-14 REVISION A REQUIRES THE FOLLOW-ON SECTION II ONE TIME INPECTION AT THE NEXT C-CHECK. CORRECTIVE ACTION: REF ERA 571509-14. (0868168)
- [SDR DALA2018121207155](https://openairdocs.org/sdr/DALA2018121207155.md): Wire · detached · Dec 3, 2018 · N680DA · Boeing 757232 · Water/Waste System Wiring
  > (AIRCRAFT 680, L/P 5189820) ON SVC FOUND WHEN YOU TOUCH LAV K FAUCET AND DOOR YOU GET SHOCKED. RECONNECTED WIRES 8-MM1-004, 8-MM1-044, AND 6-RR1-050 TO GROUND STUD 6. RECONNECTED WIRE 8-MM1-012 TO GROUND STUD 7 PER ZODIAC CMM 25-40-40.
- [SDR DALA2018112956888](https://openairdocs.org/sdr/DALA2018112956888.md): Light · missing · Nov 25, 2018 · N680DA · Boeing 757232 · Emergency Lighting
  > (AIRCRAFT 680, L/P 5155698) DURING SERVICE CHECK FOUND SEAT MOUNTED EMERGENCY LIGHT MISSING AT SEAT 43D. REPLACED SEAT MOUNTED LIGHT AND SHROUD AT ROW 43D PER CMM 1041631.
- [SDR DALA2018092105696](https://openairdocs.org/sdr/DALA2018092105696.md): Strap · broken · Sep 20, 2018 · N680DA · Boeing 757232 · Escape Slide
  > BROKEN STRAPS ON BOTH UPPER SECURITY PINS OF THE R4 DOOR SLIDE, CARD 2040-0057 (PTAS). EVACUATION SLIDE ASSY 4R WAS REMOVED PER 2040-0057-4R, AND WAS REPLACED FOR A SERVICEABLE PART PER AMDS 2040-0057-4R.
- [SDR DALA2018092105693](https://openairdocs.org/sdr/DALA2018092105693.md): Stringer Splice · corroded · Sep 20, 2018 · N680DA · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER SPLICE FROM STA 1400 TO 1420 S-28L AT AFT CARGO COMPARTMENT PER TASK NR CP53-153-01I 2020-2379 (C2). LEVEL CORROSION 2, STR 29L BTW STA 1400 TO STA 1420 WAS REPAIRED PER INSTRUCTIONS CONTAINED IN ER/A 571509-14 REV ORIGINAL.
- [SDR DALA2018092005677](https://openairdocs.org/sdr/DALA2018092005677.md): Beam · corroded · Sep 17, 2018 · N680DA · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION ON BEAM RBL 16, LBL 16, RBL 2 AND LBL 2 ALSO ON STRINGER RBL 10, LBL 10, RBL7 AND LBL 7 FROM STA 1300 TO 1350 AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2 BEAM RBL 16, LBL 16, RBL 2 AND LBL 2 ALSO ON STRINGER RBL 10, LBL 10, RBL7 AND LBL 7 FROM STA 13
- [SDR DALA2018091805649](https://openairdocs.org/sdr/DALA2018091805649.md): Stringer · corroded · Sep 17, 2018 · N680DA · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER S-29R BTW STA 1460 TO 1480 AT AFT CARGO COMPARTMENT PER TASK NR CP53-153-01, 2020-2379. REPAIR ON STRINGER S-29R BTW STA 1460 TO 1480 AT AFT CARGO COMPARTMENT WAS ACCOMPLISHED WITH ER/A 571426-14 REV A.
- [SDR DALA2018091705618](https://openairdocs.org/sdr/DALA2018091705618.md): Stringer · corroded · Sep 17, 2018 · N680DA · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > CORROSION ON RT STRINGERS RBL 2.90, 7.55 AND 10.45 FROM STA 1500 TO 1520 AT AFT CARGO COMPARTMENT CP53-153-01I (C2). CORROSION LEVEL 2. CORROSION ON STGR RBL 2.90 WAS REPAIRED PER SRM 53-00-53 REPAIR 1 FIG 201. CORROSION ON STGR RBL 7.55 AND 10.45 WAS FOUND AT
- [SDR DALA2018092005676](https://openairdocs.org/sdr/DALA2018092005676.md): Access Panel · cracked · Sep 16, 2018 · N680DA · Boeing 757232 · Leading Edge Devices
  > CRACKED LOWER SKIN, AT SLAT PANEL N?10, STA OSS 809, RT WING (AD). ACCESS PANEL WAS REPAIRED PER ER/A 366767-14MA REV C.
- [SDR DALA2018091805648](https://openairdocs.org/sdr/DALA2018091805648.md): Support · corroded · Sep 15, 2018 · N680DA · Boeing 757232 · Trailing Edge Flaps
  > CORROSION ON AFT FAIRING FLAP SUPPORT STA WS 315 AT RT WING INBD MAIN FLAP. LEVEL CORROSION 2, SUPPORT ON FAIRING FLAP WAS REPLACED WHERE ORIG THICKNESS 0.266" REMAINING THICKNESS 0.252" PER SRM 51-40-02 PAR 9 AND B DRAWING 113N2383 REV D.
- [SDR DALA2018091705619](https://openairdocs.org/sdr/DALA2018091705619.md): Stringer · corroded · Sep 15, 2018 · N680DA · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LT STRINGERS LBL2.90 AND LBL10.45 FROM STA 1500 TO 1520 AT AFT CARGO COMPARTMENT. REPAIRED PER SRM 53-00-53 REP 1.
- [SDR DALA2018091805647](https://openairdocs.org/sdr/DALA2018091805647.md): Ballscrew · corroded · Sep 11, 2018 · N680DA · Boeing 757232 · Trailing Edge Flap Actuator
  > CORROSION ON BALLSCREW NUT IN INBD FLAP OUTBD BALLSCREW AT RT WING. R&R OUTBOARD BALLSCREW OF INBOARD FLAP AT RT WING. TEST OK.
- [SDR DALA2018091305587](https://openairdocs.org/sdr/DALA2018091305587.md): Plate · cracked · Sep 11, 2018 · N680DA · Boeing 757232 · Fuselage Miscellaneous Structure
  > CRACK ON RT SIDE PLATE STA 658 RBL 26 AT FWD CARGO COMPARTMENT. SIDE PANEL RT ON FWD CARGO COMPARTMENT WAS REPLACED PER. SRM 51-40-02 PAR A AND 7 AND SRM 53-00-53 REPAIR 2.
- [SDR DALA2018091105549](https://openairdocs.org/sdr/DALA2018091105549.md): Stringer · corroded · Sep 9, 2018 · N680DA · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > LEVEL CORROSION II. CORROSION ON STRINGERS FROM STA 1460 TO 1480 RBL-16, RBL-11, RBL-7 AND LBL-16. LEVEL CORROSION 2 STRINGERS FROM STA 1460 TO 1480 RBL-16, RBL-11, RBL-7 AND LBL-16 WERE REPAIRED PER SRM 53-60-53 FIG 1.
- [SDR DALA2018091005522](https://openairdocs.org/sdr/DALA2018091005522.md): Panel · corroded · Sep 8, 2018 · N680DA · Boeing 757232 · Fuselage Miscellaneous Structure
  > LEVEL CORROSION II. CORROSION ON RT SIDE PANEL FROM STA 1375 TO 1380 AT AFT CARGO COMPARTMENT. RT SIDE PANEL FROM STA 1375 TO 1380 AT AFT CARGO COMPARTMENT WAS REPLACED PER SRM 51-40-02 PAR 4 AND 7.
- [SDR DALA2018091005521](https://openairdocs.org/sdr/DALA2018091005521.md): Beam · cracked · Sep 8, 2018 · N680DA · Boeing 757232 · Fuselage Main, Structure
  > CRACKED BEAM STA 1070 AND RBL 60 AT RT WHEEL WELL AREA (FYT). REPAIRED PER ER/A 571403-14 REV ORIGINAL.
- [SDR DALA2018091005518](https://openairdocs.org/sdr/DALA2018091005518.md): Floor Support · corroded · Sep 7, 2018 · N680DA · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT STA 1200 FROM PROJECTION S-23L TO S-27L ALSO S-23R TO S-27R AT AFT CARGO COMPARTMENT (C2). LEVEL CORROSION 2. SUPPORTS WERE REPLACED PER DRAWING 453N1602 REV AT.
- [SDR DALA2018090705486](https://openairdocs.org/sdr/DALA2018090705486.md): Floorbeam · corroded · Sep 6, 2018 · N680DA · Boeing 757232 · Fuselage Main, Floor Beam
  > INITIAL INSPECTION. CORROSION ON FLOORBEAM UPPER CHORD LWR SURFACE STA 345 LBL 63 AT PAX CABIN FLOOR STRUCTURE. DAMAGE ON BEAM STA 345 LBL 63 LWR SECTION WAS REPAIRED PER ER/A 571242-14 REV ORIGINAL.
- [SDR DALA2018090605455](https://openairdocs.org/sdr/DALA2018090605455.md): Shear Tie · corroded · Sep 5, 2018 · N680DA · Boeing 757232 · Fuselage Internal Mounting Structure
  > CORROSION ON INTERCOSTAL OF STA 1380 AND S27R AT AFT CARGO COMPARTMENT. (LEVEL CORROSION 2) ANGLE (SHEAR TIE) WAS REPLACED PER DWG 146N5421 REV B AND SRM 51-40-02.

Next page: https://openairdocs.org/deregistered/N680DA-2025-07-14/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 = 'N680DA' AND deregistration_id = 'N680DA-2025-07-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N680DA-2025-07-14/reports

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