# Service difficulty reports: N126DL, cancelled Jun 21, 2018

A list on [N126DL, cancelled Jun 21, 2018](https://openairdocs.org/deregistered/N126DL-2018-06-21.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 · 94 reports

- [SDR DALA2015111707012](https://openairdocs.org/sdr/DALA2015111707012.md): Wire · pulled · Nov 9, 2015 · N126DL · Boeing 767332 · Light System Wiring
  > EMERGENCY LIGHTS AT SEAT 13AB ARE INOPERATIVE. MAINTENANCE FOUND WIRE PULLED OUT OF PLUG AND REPINNED. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2014102005830](https://openairdocs.org/sdr/DALA2014102005830.md): Wire Harness · damaged · Oct 18, 2014 · N126DL · Boeing 767332 · Light System Wiring
  > EMERGENCY LIGHT INOPERATIVE AT ROW 42 RT SIDE. MAINTENANCE REPLACED THE LIGHTS AND REPAIRED THE WIRING AT SEAT HARNESS CONNECTOR. SYSTEM OPS IS NORMAL.
- [SDR DALA14005650126](https://openairdocs.org/sdr/DALA14005650126.md): Connector · disconnected · Jan 27, 2014 · N126DL · Boeing 767332 · Light System Wiring
  > CABIN EMERGENCY EXIT LIGHTS ARE INOPERATIVE AT LT MID LAVATORY. MAINTENANCE CONNECTED LIGHTS. SYSTEM OPERATION IS NORMAL.
- [SDR DALA13026720126](https://openairdocs.org/sdr/DALA13026720126.md): Skin · worn · May 29, 2013 · N126DL · Boeing 767332 · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON UPPER STRUT SKIN, FWD PANEL, RT & LT SPLICE STRAPS, NAC STA 163.50: REPAIR OF WEAR DAMAGE. ACCOMPLISHED ERA 096790-14, REV A.
- [SDR DALA13026040126](https://openairdocs.org/sdr/DALA13026040126.md): Fairing · delaminated · May 28, 2013 · N126DL · Boeing 767332 · Trailing Edge Flaps
  > RT WING INBD MAIN FLAP L/E OTBD END FAIRING DELAMINATED AS MARKED. FAIRING COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT IAW SRM 57-53-01, REPAIR 1, SRM 51-70-05.
- [SDR DALA13026350126](https://openairdocs.org/sdr/DALA13026350126.md): Frame · cracked · May 27, 2013 · N126DL · Boeing 767332 · Fuselage Main, Frame
  > FRAME CRACKED. REPAIRED IAW ER/A 513104-14AD, REV ORIG.
- [SDR DALA13026340126](https://openairdocs.org/sdr/DALA13026340126.md): Frame · cracked · May 27, 2013 · N126DL · Boeing 767332 · Fuselage Main, Frame
  > BS 859.5 FRAME CRACKED. REPAIR ACCOMPLISHED IAW ER/A 513105-14AD, REV ORIG.
- [SDR DALA13026310126](https://openairdocs.org/sdr/DALA13026310126.md): Fairing · delaminated · May 27, 2013 · N126DL · Boeing 767332 · Wing Main, Frame Structure
  > LEFT WING INBD MAIN FLAP L/E OTBD END FAIRING DELAMINATED. LT WING INBD MAIN FLAP L/E OTBD END FAIRING COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT IAW SRM 57-53-01, REPAIR 1, SRM 51-70-05.
- [SDR DALA13026030126](https://openairdocs.org/sdr/DALA13026030126.md): Floor Panel · damaged · May 27, 2013 · N126DL · Boeing 767332 · Fuselage Floor Panel
  > FWD CARGO BAY FLOOR PANEL 121LT BACKSIDE AFT SKIN FOUND BROKEN AND SURFACE SKIN FOUND DEFORMED AT AFT SECTION. FLOOR PANEL FABRICATED IAW ER/A 513125-14, REV.
- [SDR DALA13026010126](https://openairdocs.org/sdr/DALA13026010126.md): Skin · delaminated · May 27, 2013 · N126DL · Boeing 767332 · Trailing Edge Flaps
  > LT WING T/E FLAP, INBD NOSE SKIN AREA FOUND SEVERAL DELAMINATES LT WING - T/E OTBD FLAP INBD NOSE SKIN AREA COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT IAW SRM 57-53-01 REPAIR 1, SRM 51-70-05.
- [SDR DALA13026400126](https://openairdocs.org/sdr/DALA13026400126.md): Skin · damaged · May 25, 2013 · N126DL · Boeing 767332 · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON, LT PANEL NR 447AL SKIN HOLE ELONGATED. NR 2 PYLON LT PANEL 447AL SKIN. REPLACED IAW ER/A 513112-14 REV ORIG SECTION I.
- [SDR DALA13026390126](https://openairdocs.org/sdr/DALA13026390126.md): Skin · damaged · May 25, 2013 · N126DL · Boeing 767332 · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON SKIN PANEL 447AR HAS A HOLE ELONGATED. REPLACED SKIN IAW ER/A 513112-14 REV ORIG.
- [SDR DALA13026380126](https://openairdocs.org/sdr/DALA13026380126.md): Skin · damaged · May 25, 2013 · N126DL · Boeing 767332 · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON SKIN PANEL 437AR HAS SEVERAL SCREW HOLES ELONGATED. SKIN REPLACED IAW ER/A 513112-14 REV ORIG SECTION I.
- [SDR DALA13026370126](https://openairdocs.org/sdr/DALA13026370126.md): Skin · damaged · May 25, 2013 · N126DL · Boeing 767332 · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON SKIN PANEL 437AL HAS SEVERAL SCREW HOLES ELONGATED. SKIN REPLACED IAW ER/A 513112-14, REV ORIG SECTION I.
- [SDR DALA13026360126](https://openairdocs.org/sdr/DALA13026360126.md): Skin · bulged · May 25, 2013 · N126DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN AT BS 1219, S38R FOUND BULGED. REPAIRED IAW SRM 51-10-02, 51-40-02.
- [SDR DALA13026300126](https://openairdocs.org/sdr/DALA13026300126.md): Frame · cracked · May 25, 2013 · N126DL · Boeing 767332 · Fuselage Main, Frame
  > BS 859.5, RBL 89 BELOW WL 200 FRAME TRANSITION RADIUS FOUND CRACK ABOUT 0.8" RUNNING UP. REPAIR ACCOMPLISHED IAW ER/A 513105-14AD REV ORIG SECTION I.
- [SDR DALA13026290126](https://openairdocs.org/sdr/DALA13026290126.md): Frame · cracked · May 25, 2013 · N126DL · Boeing 767332 · Fuselage Main, Frame
  > BS 883.5, RBL 89 BELOW WL 200 FRAME TRANSITION RADIUS FOUND CRACK ABOUT 0.4" RUNNING UP AS MARKED. REPAIR ACCOMPLISHED ER/A 513104-14AD REV ORIG SECTION
- [SDR DALA13025310126](https://openairdocs.org/sdr/DALA13025310126.md): Failsafe · cracked · May 23, 2013 · N126DL · Boeing 767332 · Fuselage Main, Structure
  > BS 955 RT BULKHEAK FITTING FAILSAFE STRAP FOUND CRACKED. REPAIRED IAW IAW ER/A 513102-14AD, REV ORIG.
- [SDR DALA13025300126](https://openairdocs.org/sdr/DALA13025300126.md): Skin · damaged · May 23, 2013 · N126DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN BETWEEN, BS 1461 TO 1502, BETWEEN STR 23-32L DAMAGED. REPAIRED IAW ER/A 513108-14, REV ORIG.
- [SDR DALA13025320126](https://openairdocs.org/sdr/DALA13025320126.md): Skin · corroded · May 21, 2013 · N126DL · Boeing 767332 · Trailing Edge Flaps
  > LT WING INBD MAIN FLAP LOWER SURFACE INBD AFT EDGE PANEL FOUND BULGED. REPAIR ACCOMPLISHED IAW ER/A 513107-14, REV.
- [SDR DALA13027050126](https://openairdocs.org/sdr/DALA13027050126.md): Floorbeam · corroded · May 19, 2013 · N126DL · Boeing 767332 · Fuselage Main, Frame
  > FWD CARGO BAY BS 654 + 44, LBL 20 -44 FLOORBEAM UPPER & LWR SURFACE FOUND CORROSION. FWD CARGO STA654+44 CARGO FLOORBEAM REPLACED AND INSTALLED IAW SRM 51-10-02, 51-40-02, 51-40-05.
- [SDR DALA13025290126](https://openairdocs.org/sdr/DALA13025290126.md): Structure · damaged · May 19, 2013 · N126DL · Boeing 767332 · Fuselage Main, Structure
  > AFT CARGO BAY BS 1241 RBL 8, ANCHOR NUT HOLE ELONGATED. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 4.
- [SDR DALA13025280126](https://openairdocs.org/sdr/DALA13025280126.md): Floorbeam · damaged · May 19, 2013 · N126DL · Boeing 767332 · Fuselage Main, Floor Beam
  > FWD CARGO COMPT BS 434, LBL 20-30, FLOORBEAM ANCHOR NUTS DAMAGED. FLOORBEAM REPAIRED IAW SRM 53-00-07, REPAIR 4.
- [SDR DALA13025270126](https://openairdocs.org/sdr/DALA13025270126.md): Structure · damaged · May 19, 2013 · N126DL · Boeing 767332 · Fuselage Main, Structure
  > FWD CARGO COMPT BS 654+22, RBL 35 ANCHOR NUT HOLE FOUND ELONGATED. MX REPAIRED IAW SRM 53-00-07, REPAIR 4, FIG 201.
- [SDR DALA13027040126](https://openairdocs.org/sdr/DALA13027040126.md): Shear Tie · corroded · May 18, 2013 · N126DL · Boeing 767332 · Fuselage Internal Mounting Structure
  > AFT CARGO COMPT, BELOW FLOOR SHEAR TIE FOUND CORROSION AT BS 1197+22, STR 38-39L. AFT CARGO STA 1197+22 BETWEEN STR 38L TO 39L SHEAR TIE CORROSION AND REMOVED IAW SRM 51-10-02, 51-20-01. BLENDED DEPTH OUT OF LIMITS SHEAR TIE REPLACED AND INSTALLED IAW SRM 51
- [SDR DALA13025410126](https://openairdocs.org/sdr/DALA13025410126.md): Structure · corroded · May 18, 2013 · N126DL · Boeing 767332 · Fuselage Main, Structure
  > AFT CARGO BELOW FLOOR SHEAR TIE FOUND CORROSION AT BS 1197+66, S38-39R. MX REPLACED AS SRM 51-10-02, 51-40-05, 51-40-02.
- [SDR DALA13025400126](https://openairdocs.org/sdr/DALA13025400126.md): Shear Tie · corroded · May 18, 2013 · N126DL · Boeing 767332 · Fuselage Internal Mounting Structure
  > AFT CARGO BAY BELOW FLOOR SHEAR TIE FOUND CORROSION AT BS 1197+132, STR 38R - 39R. MX REPLACED SHEAR TIE IAW SRM 51-10-02, 51-40-05, 51-40-02.
- [SDR DALA13025390126](https://openairdocs.org/sdr/DALA13025390126.md): Shear Tie · corroded · May 18, 2013 · N126DL · Boeing 767332 · Fuselage Internal Mounting Structure
  > BS 1219, BETWEEN S39L AND S39R SHEAR TIE CORRODED. (CP 53-156-01I) MX REPLACED AND INSTALLED SRM 51-40-02, SHEAR TIE.
- [SDR DALA13023500126](https://openairdocs.org/sdr/DALA13023500126.md): Floorbeam · corroded · May 18, 2013 · N126DL · Boeing 767332 · Fuselage Main, Floor Beam
  > FLOORBEAM BS 325, RBL 28 -55, FOUND CORRODED, FLOORBEAM REPAIRED.
- [SDR DALA13025530126](https://openairdocs.org/sdr/DALA13025530126.md): Unknown · corroded · May 17, 2013 · N126DL · Boeing 767332 · Fuselage Structure (General)
  > FWD CARGO BAY BS 775, S35L FOUND CORRODED. MAINTENANCE REPLACED IAW SRM 53-00-03, REPAIR 2, FIG 201.
- [SDR DALA13025520126](https://openairdocs.org/sdr/DALA13025520126.md): Support Beam · corroded · May 17, 2013 · N126DL · Boeing 767332 · Fuselage Miscellaneous Structure
  > CARGO BAY BS 1461-1480 S24-25L FRAME SUPPORT BEAM CORRODED. MX REPLACED AND INSTALLED IAW SRM 51-40-02.
- [SDR DALA13025380126](https://openairdocs.org/sdr/DALA13025380126.md): Seat Track · corroded · May 17, 2013 · N126DL · Boeing 767332 · Fuselage, Seat/Cargo Attach Fittings
  > BS 346-350 LBL 88, SEAT TRACK FLANGE FOUND CORRODED. MX REPLACED SRM 51-10-02 & FASTENERS INSTALLED IAW SRM 51-40-02.
- [SDR DALA13025510126](https://openairdocs.org/sdr/DALA13025510126.md): Shear Tie · corroded · May 16, 2013 · N126DL · Boeing 767332 · Fuselage Internal Mounting Structure
  > AFT CARGO BAY SHEAR TIE FOUND CORRODED AT BS 1395, S36-37R. REPLACED IAW SRM 51-10-02, 51-40-05, 51-40-02.
- [SDR DALA13025500126](https://openairdocs.org/sdr/DALA13025500126.md): Shear Tie · corroded · May 16, 2013 · N126DL · Boeing 767332 · Fuselage Internal Mounting Structure
  > AFT CARGO BAY SHEAR TIE FOUND CORROSION AT BS 1395, STR 38-39R. REPLACED IAW SRM 51-10-02 & FASTENERS INSTALLED IAW SRM 51-40-02.
- [SDR DALA13025490126](https://openairdocs.org/sdr/DALA13025490126.md): Shear Tie · corroded · May 16, 2013 · N126DL · Boeing 767332 · Fuselage Internal Mounting Structure
  > CARGO BAY BELOW FLOOR, SHEAR TIE FOUND CORROSION AT BS 1417, S36-37R. REPLACED SRM 51-10-02 & FASTENERS INSTALLED IAW SRM 51-40-02.
- [SDR DALA13025480126](https://openairdocs.org/sdr/DALA13025480126.md): Shear Tie · corroded · May 16, 2013 · N126DL · Boeing 767332 · Fuselage Internal Mounting Structure
  > CARGO BAY BELOW FLOOR, SHEAR TIE FOUND CORROSION AT BS 1417, STR 35-36R. REPLACED SRM 51-10-02 & FASTENERS INSTALLED IAW SRM 51-40-02.
- [SDR DALA13025470126](https://openairdocs.org/sdr/DALA13025470126.md): Stringer · corroded · May 16, 2013 · N126DL · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > FWD CARGO BS 412-434, STRINGER 34R, FOUND CORRODED. REPAIRED IAW SRM 53-00-03, REPAIR 2, FIG 201.
- [SDR DALA13025460126](https://openairdocs.org/sdr/DALA13025460126.md): Structure · corroded · May 16, 2013 · N126DL · Boeing 767332 · Fuselage Main, Structure
  > BULK CARGO, BELOW FLOOR SHEAR TIE FOUND CORROSION AT STA 1417, S37-38R. REPLACED IAW SRM 51-40-05, 51-10-02, 51-40-02.
- [SDR DALA13025450126](https://openairdocs.org/sdr/DALA13025450126.md): Structure · corroded · May 16, 2013 · N126DL · Boeing 767332 · Fuselage Main, Structure
  > BULK CARGO, BELOW FLOOR SHEAR TIE FOUND CORROSION AT BS 1439, S37-38R, REPLACED IAW SRM 51-40-02.
- [SDR DALA13025370126](https://openairdocs.org/sdr/DALA13025370126.md): Shear Tie · damaged · May 16, 2013 · N126DL · Boeing 767332 · Fuselage Internal Mounting Structure
  > BULK CARGO BAY BELOW FLOOR SHEAR TIE FOUND CORROSION AT BS 1439, STR 36R-37R. DAMAGED SHEAR TIE REPLACED IAW SRM 51-10-02 & FASTENERS INSTALLED IAW SRM 51-40-02.
- [SDR DALA13025440126](https://openairdocs.org/sdr/DALA13025440126.md): Structure · corroded · May 15, 2013 · N126DL · Boeing 767332 · Fuselage Main, Structure
  > AFT CARGO, BELOW FLOOR SHEAR TIE FWD ATT PLATE FOUND CORROSION AT BS 1197+100, S39L-39R. REPLACED IAW SRM 51-10-02, 51-40-02.
- [SDR DALA13025430126](https://openairdocs.org/sdr/DALA13025430126.md): Structure · corroded · May 15, 2013 · N126DL · Boeing 767332 · Fuselage Main, Structure
  > AFT CARGO BELOW FLOOR SHEAR TIE FOUND CORROSION AT BS 1285, S39L-39R. REPLACED IAW SRM 51-10-02, 51-40-02.
- [SDR DALA13025420126](https://openairdocs.org/sdr/DALA13025420126.md): Floor Panel · corroded · May 13, 2013 · N126DL · Boeing 767332 · Fuselage Floor Panel
  > FLOOR PANEL FOUND CORRODED AT BS 1462-1480, LBL 90-96. CRACKED FLOOR PANEL REPLACED IAW SRM 51-10-02 & SRM 51-40-02.
- [SDR DALA13025360126](https://openairdocs.org/sdr/DALA13025360126.md): Stiffener · corroded · May 13, 2013 · N126DL · Boeing 767332 · Fuselage Miscellaneous Structure
  > BS 1480 LT OTBD CORRODED. FLOOR WEB SUPPORT STIFFENER REPLACED IAW SRM 51-10-02 & FASTENERS INSTALLED IAW SRM 51-40-02.
- [SDR DALA13025350126](https://openairdocs.org/sdr/DALA13025350126.md): Floorbeam · corroded · May 10, 2013 · N126DL · Boeing 767332 · Fuselage Main, Floor Beam
  > BS 303, LBL 22-55, FLOORBEAM FOUND CORROSION REPAIRED IAW SRM 53-00-51, REPAIR 4, FIG 201.
- [SDR DL76S091252](https://openairdocs.org/sdr/DL76S091252.md): Engine · coked · Jul 21, 2009 · N126DL · Boeing 767332 · Engine (Turbine/Turboprop)
  > WHILE WORKING MCO ON LT ENGINE OVERHEAT DETECTION SYSTEM LOOP 2 OBSERVED SEVERE COKING ON UPPER ENGINE CASE AND HEAT DAMAGE TO PYLON INSULATION AND ELECTRICAL CONNECTORS AT J BOX. INSULATION AND ELECTRICAL CONNECTORS ON PYLON REPLACED. ENGINE SENT TO SHOP FO
- [SDR DL76S081692](https://openairdocs.org/sdr/DL76S081692.md): Strut · unknown · Dec 3, 2008 · N126DL · Boeing 767332 · Main Landing Gear Strut/Axle/Truck
  > MLG SHOCK STRUT CYLINDER REPAIR IAW ERA 01-471561-14 REV A C/W ERA 01-471561-14.
- [SDR DL76S080359](https://openairdocs.org/sdr/DL76S080359.md): Attach Fitting · corroded · Mar 13, 2008 · N126DL · Boeing 767332 · Fuselage, Landing Gear Attach Fittings
  > NLG W/W LT AND RT NLG TRUNNION ATTACH FITTINGS. CORROSION IN FITTING BORES AND TOOLING DAMAGED FASTENER HOLES. OVERSIZED BORES AND INSTALLED NEW ENLARGED BUSHINGS.
- [SDR DL76S080297](https://openairdocs.org/sdr/DL76S080297.md): Elbow · cracked · Feb 29, 2008 · N126DL · Boeing 767332 · Engine Cooling System
  > L ENG FIRE LP1 STATUS MESSAGE ABOUT 15 MINUTES INTO FLIGHT FOLLOWED BY ILLUMINATION OF L ENGINE FIRE WARNING LIGHTS. ENGINE SHUTDOWN IN ACCORDANCE WITH QRH. NOTE, FIRE SWITCH WAS PULLED, HOWEVER, FIRE BOTTLE WERE NOT DISCHARGED. FOUND NR 1 ENG LT HIGH PRESS
- [SDR DL76S080162](https://openairdocs.org/sdr/DL76S080162.md): Skin · damaged · Feb 5, 2008 · N126DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > FOUND SKIN BLENDS AT FS 536 - FS 625, AND S-27R TO S-33R.

Next page: https://openairdocs.org/deregistered/N126DL-2018-06-21/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 = 'N126DL' AND deregistration_id = 'N126DL-2018-06-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N126DL-2018-06-21/reports

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