# Service difficulty reports: N156DL, cancelled Aug 25, 2023

A list on [N156DL, cancelled Aug 25, 2023](https://openairdocs.org/deregistered/N156DL-2023-08-25.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 4 · 177 reports

- [SDR MK1Y20230503023](https://openairdocs.org/sdr/MK1Y20230503023.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Fuselage Structure (General)
  > STA 139 - ATA 180.5, BELOW WINDOWS R1 AND R1: DURING MAINTANACE INSPECTION AT IAI, SHOP FOUND TWO (2) DOCUMENTED REPAIRS AT THE NOTED LOCATION. FWD REPAIR: LIGHTNING STRIKE REPAIR AT STA 139, BELOW WINDOW R1. AFT REPAIR: A DOUBLER REPAIR ON THE EXTERNAL FUS SK
- [SDR MK1Y20230503022](https://openairdocs.org/sdr/MK1Y20230503022.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Nacelle/Pylon Structure
  > STRUT #2, AFT FAIRNG - TRAILING EDGE, RH AND LH, NAC STA 410 TO 413: DURING MAINTENANCE INSPECTION AT IAI FACILITES, SHOP DISCOVERED UNDOCUMENTED DOBULER REPAIR IN STRUT #2, SKIN PANELS, ON BOTH SIDES.
- [SDR MK1Y20230503021](https://openairdocs.org/sdr/MK1Y20230503021.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Fuselage Structure (General)
  > EXTERNAL FUSELAGE SKIN, STA 661, STR-30R-STR-31R: DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND ONE BULGE ON FUSELAGE SKIN LOCATED AT STA 661, 2-INCH BELOW THE STR 30R. INITIAL DIMENSION OF BULGE IS A=0.57”, Y=0.0278” (A/Y=20). BULGE IS OUT OF LIMITS PER SR
- [SDR MK1Y20230503020](https://openairdocs.org/sdr/MK1Y20230503020.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Fuselage Structure (General)
  > SEC 46 FUSELAGE SKIN, STA 1564.3, 5” ABOVE STR 16L: DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND ONE DENT ON FUSELAGE SKIN LOCATED AT STA 1264.3, 5” ABOVE STR 16L. INITIAL DIMENSION OF DENTED AREA A=0.720”, Y=0.032” (A/Y=22). DENT IS OUT OF LIMITS PER SRM
- [SDR MK1Y20230503019](https://openairdocs.org/sdr/MK1Y20230503019.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Fuselage Structure (General)
  > SECTION 41 – FUSELAGE SKIN – STA 422 BETWEEN STR 31L AND STR 32L: A BULGE OUT OF LIMITS ON THE FUSELAGE SKIN WAS REPAIRED PER SRM 53-00-01 REPAIR 8
- [SDR MK1Y20230503018](https://openairdocs.org/sdr/MK1Y20230503018.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Fuselage Structure (General)
  > SECTION 43 FUSELAGE SKIN STA 669.3 BETWEEN STR 35L AND STR 36L: AN EXISTING BULGE OUT OF LIMITS ON FUSELAGE SKIN WAS REPAIRED PER SRM 53-00-01 REPAIR 8.
- [SDR MK1Y20230503017](https://openairdocs.org/sdr/MK1Y20230503017.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Fuselage Structure (General)
  > SEC 43 FUSELAGE SKIN, STA 600.8 BTWN STR 32L-33L: DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND ONE DENT ON FUSELAGE SKIN LOCATED AT STA 600.8 BETWEEN STR 32L AND STR 33L. INITIAL DIMENSION OF DENTED AREA A=0.680”, Y=0.027” (A/Y=25). DENT IS OUT OF LIMITS P
- [SDR MK1Y202305173016](https://openairdocs.org/sdr/MK1Y202305173016.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Landing Gear System
  > R/H MLG DOOR: MAINTENANCE DISCOVERED A PUNCTURE AT THE INNER SKIN OF R/H MLG DOOR IN A CRITICAL AREA (LESS THAN 10 INCHES FROM THE CENTER HINGE). SHOP REPORTED SEVERAL DAMAGES NEAR THE NOTED PUNCTURE. ALL OTHER DAMAGES WERE REPAIRED PER SRM 52-80 REQUIREMENTS.
- [SDR MK1Y202305173015](https://openairdocs.org/sdr/MK1Y202305173015.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Nacelle/Pylon Structure
  > DURING CONVERSION OF S/N 25354, MAINTENANCE WAS REQUIRED TO REPLACE ENGINE #2 INLET COWL. THE REPLACEMENT INLET COWL P/N 224-2101-563, S/N 0634RV860 PROVIDED BY COSTUMER. THE NOTED INLET COWL WAS INSTALLED ON A/C AND POLISHED. MAINTENANCE REPORTED CORROSION/PI
- [SDR MK1Y20230503014](https://openairdocs.org/sdr/MK1Y20230503014.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Powerplant System
  > DURING MAINTENANCE INSPECTION SHOP FOUND EXISTING LATCH REPAIR DOUBLER ON THE OUTBD CORE COWL ENG #2 B/T NAC STA 267 TO 274.5 AT 6 O’CLOCK, CENTER LATCH. DURING DISASSEMBLE THE EXISTING DOUBLER, SHOP FOUND TWO (2) ELONGATED HOLES, 1 HOLE IN DIA 0.328” AND THE
- [SDR MK1Y202305173013](https://openairdocs.org/sdr/MK1Y202305173013.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Fuselage Structure (General)
  > BT STA 1518-1562, STR 38L-37R: DURING DAMAGED SHEAR TIE P/N 140T2102U585 REMOVAL IN ORDER TO INSTALL NEW SHEAR TIE SHOP MISTAKENLY DOUBLE DRILLED THE TEAR STRAP AND SKIN AT 4EA HOLES. THE ORIGINAL HOLE DIA 0.186”. THE HOLES WERE DRILLED UNTIL THE WHOLE DAMAGE
- [SDR MK1Y202305173006](https://openairdocs.org/sdr/MK1Y202305173006.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Powerplant System
  > ENG #2, INBD SIDE CORE COWL, S/N 0982, P/N 224M4761-513: DURING NAINTENANCE INSPECTION SHOP FOUND SEVERAL LOOSE FASTENERS IN THE EXTERNAL CORE COWL SKIN ON THE INBD SIDE OF ENF #2 BETWEEN NAC STA 303.75 TO 306.75 AT 6 O'CLOCK. AFTER REMOVING THE LOOSE FASTE
- [SDR MK1Y20230503001](https://openairdocs.org/sdr/MK1Y20230503001.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Powerplant System
  > CORE COWL, P/N 224-2302-345, S/N 1198: DURING MAINTENANCE INSPECTION AT IAI FACILITIES. AN UNDOCUMENTED DOUBLER REPAIR LOCATED BETWEEN NAC STA 280 AND 288 AT 10 O'CLOCK. SIZE: 7.4"X4.6". M0566 – A CRACK STRETCHING FROM THE FASTENER TO THE AFT EDGE OF THE EX
- [SDR MK1Y20230503012](https://openairdocs.org/sdr/MK1Y20230503012.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Engine Cowling System
  > OUTB’D FAN COWL ENG #2 S/N 0424 P/N 224-2202-507. DURING MAINTENANCE CHECK AT IAI FACILITIES, SHOP DISCOVERED THE FOLLOWING FINDINGS: DENT IN THE EXTERNAL FAN COWL SKIN, COMMON TO NAC STA 182.5. 59” AWAY FROM THE BOTTOM EDGE OF THE FAN COWL. THE FIBERS ARE D
- [SDR MK1Y20230503011](https://openairdocs.org/sdr/MK1Y20230503011.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Fuselage Structure (General)
  > STA 236.5, LBL 69.25: DURING MAINTENANCE INSPECTION SHOP FOUND FLOOR BEAM AND SHEAR WEB WITH MISSING MATERIAL.
- [SDR MK1Y20230503010](https://openairdocs.org/sdr/MK1Y20230503010.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Fuselage Structure (General)
  > FUS. SKIN, SEC 48, BT STA 1809.5 – STA 1824, ABOVE STR 22L: DURING MAINTENANCE INSPECTION SHOP FOUND UNDOCUMENTED REPAIR ON THE EXTERNAL FUS SKIN, P/N 148T3181-7. A REVIEW OF THE PREVIOUS OPERATOR’S RECORDS (DAL) WAS PERFORMED AND NO DOCUMENTATION WAS FOUND. T
- [SDR MK1Y20230503009](https://openairdocs.org/sdr/MK1Y20230503009.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Fuselage Structure (General)
  > SEC 46, STA 1197 – 1197=22, STR 38L -38R: UNDOCUMENTED DOUBLER REPAIR FOUND NEXT TO DOCUMENTED DOUBLER BETWEEN STA 1189 – 1197=14, STR35L – 38L, DOCUMENTED ON ERA 518660-14AD.
- [SDR MK1Y20230503008](https://openairdocs.org/sdr/MK1Y20230503008.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Fuselage Structure (General)
  > DURING MAINTENANCE INSPECTION, SHOP FOUND A LIGHTNING ST88IKE DAMAGE ON SKIN, AT A BUTT JOINT AT THE NOTED AREA. SHOP PERFORMED 0.4"X1.0" SIZE BLEND OUT ON THE DAMAGED AREA. AFTER NDT INSPECTIONS, IT WAS FOUND THAT THE MINIMUM THICKNESS IS 0.54", AND THE NOMIN
- [SDR MK1Y20230503007](https://openairdocs.org/sdr/MK1Y20230503007.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Fuselage Structure (General)
  > TAILCONE OUTER SKIN BTWN STA 1943.5-1952: DURING CONVERSION AT IAI IN TLV, MTX FOUND SEVERAL DAMAGES AND UNDICUMENTED REPAIRS ON OUTER TAILCONE SKIN. THE FOUNDS WERE: -BLEND OUTS; - WELDING REPAIRS; - LIGHTNING STRIKES; - FASTENER REPAIRS. SOME OF THESE FOUNDI
- [SDR MK1Y20230503005](https://openairdocs.org/sdr/MK1Y20230503005.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Fuselage Structure (General)
  > DURING AIRCRAFT CARGO CONVERSION, A 0.186" DIAMETER INITIAL FASTENER HOLE WAS MISTAKENLY DAMAGED IN THE STA 1065 BULKHEAD WEB AND NO. 6 STIFFENER. THE BULKHEAD STRUCTURE IS CLASSIFIED AS PRIMARY STRUCTURE, A PSE, AND FCBS (NOTE 1) PER REF 767-300 SRM 51-00-04,
- [SDR MK1Y20230503004](https://openairdocs.org/sdr/MK1Y20230503004.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Powerplant System
  > DURING MAINTENANCE INSPECTION AT IAI FACILITIES, SHOP DISCOVERED THE FOLLOVING FINDINGS: M0547 – AN UNDOCUMENTED DOUBLER REPAIR LOCATED BETWEEN NAC STA 286.55 AND 288.95 AT 6 O'CLOCK. SIZE: 5.6"X3.6". M0592 – AN UNDOCUMENTED DOUBLER REPAIR LOCATED (TITANIU
- [SDR MK1Y20230503003](https://openairdocs.org/sdr/MK1Y20230503003.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Wing Structure
  > STRUT #2, L/H, NAC STA 285.45 TO 289.95, UNDERWING FAIRING: DURING MAINTENANCE INSPECTION AT IAI FACILITIES, SHOP DISCOVERED UNDOCUMENTED DOUBLER REPAIR.
- [SDR MK1Y20230503002](https://openairdocs.org/sdr/MK1Y20230503002.md): Unknown · unknown · May 3, 2023 · N156DL · Boeing 7673P6 · Fuselage Structure (General)
  > FUSELAGE SKIN REPAIR, BETWEEN STA 157 AND STA 162, ABOVE STR-21L: DURING MAINTENANCE CHECK, IAI SHOP DISCOVERED AN EXISTING REPAIR IN FUSELAGE SKIN LOCATED AT THE NOTED AREA. THE FLUSH REPAIR IS LOCATED IN THE EXTRA CRITICAL AREA, FWD TO THE PITOT STATIC PROBE
- [SDR DALA2020070762549](https://openairdocs.org/sdr/DALA2020070762549.md): Battery Pack · inoperative · Jul 4, 2020 · N156DL · Boeing 7673P6 · Emergency Lighting
  > EMERGENCY EXIT LIGHT OVER WING LEFT SIDE IS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2020070762548](https://openairdocs.org/sdr/DALA2020070762548.md): Battery Pack · inoperative · Jul 4, 2020 · N156DL · Boeing 7673P6 · Emergency Lighting
  > EMERGENCY EXIT LIGHT SIGN AT P12 INOPERATIVE. REPLACED BATTERY. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2020051902410](https://openairdocs.org/sdr/DALA2020051902410.md): Warning System · false activation · May 13, 2020 · N156DL · Boeing 7673P6 · Autopilot System
  > SHIP 1506 - ATO - ON T/O ROLL, LT YAW DAMP MESSAGE & OVERHEAD LIGHT ILLUMINATED. CORRECTIVE ACTION: INITIALLY APPLIED MEL 22-21-01. DURING RON, PERFORMED SYSTEM BITE & MCDP TESTS 30 & 40. OPERATIONAL CHECK OK. LP 7043212
- [SDR DALA2020040602180](https://openairdocs.org/sdr/DALA2020040602180.md): Battery Pack · discharged · Apr 4, 2020 · N156DL · Boeing 7673P6 · Emergency Lighting
  > DURING SERVICE CHECK FOUND BACK CEILING EMERGENCY LIGHTS OUT EXTENDING FROM ROW 35A INTO AFT GALLEY. REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2020020300825](https://openairdocs.org/sdr/DALA2020020300825.md): Battery Pack · inoperative · Feb 3, 2020 · N156DL · Boeing 7673P6 · Emergency Lighting
  > EMERGENCY EXIT SIGN AFT CEILING ARE INOPERATIVE. REPLACED BATTERY M739. SYSTEM OPERATION IS NORMAL.
- [SDR DALA202002030826](https://openairdocs.org/sdr/DALA202002030826.md): Battery Pack · inoperative · Jan 29, 2020 · N156DL · Boeing 7673P6 · Emergency Lighting
  > EMERGENCY LIGHTS AT 34-40AB ON CEILING ARE INOPERATIVE. REPLACED BATTERY AT M739. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2019112506897](https://openairdocs.org/sdr/DALA2019112506897.md): Charger · inoperative · Nov 23, 2019 · N156DL · Boeing 7673P6 · Emergency Lighting
  > DURING SERVICE CHECK FOUND AFT 3 LEFT EXTERNAL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2019111046511](https://openairdocs.org/sdr/DALA2019111046511.md): Connector · disconnected · Nov 4, 2019 · N156DL · Boeing 7673P6 · Light System Wiring
  > EMERGENCY FLOOR PATH LGITHS ARE INOPERATIVE AT SEAT 39B. RECONNECTED LIGHT ASSEMBLY.
- [SDR DALA2019110106344](https://openairdocs.org/sdr/DALA2019110106344.md): Battery Pack · inoperative · Oct 31, 2019 · N156DL · Boeing 7673P6 · Emergency Lighting
  > FOUND EXTERIOR EMERGENCY LIGHT LEFT SIDE L396 AND L645 NOT ILLUMINATING DURING TEST. REPLACED BATTERY PACK ON M738. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2019102196016](https://openairdocs.org/sdr/DALA2019102196016.md): Skin · cracked · Oct 18, 2019 · N156DL · Boeing 7673P6 · Nacelle/Pylon, Plate/Skin
  > #1 PYLON OB SIDE STRUT SKIN HAS 2" CRACK ABOVE 432AL. VERIFIED WITH HFEC SCAN TAG # 6741, CREATE EWO FOR REPAIR. REPAIRED #1 PYLON OB STRUT SKIN IAW ERA 581953-14 REV O. JOB COMPLETE. (LP1321034)
- [SDR DALA2019101765940](https://openairdocs.org/sdr/DALA2019101765940.md): Skin · cracked · Oct 15, 2019 · N156DL · Boeing 7673P6 · Nacelle/Pylon, Plate/Skin
  > NUMBER 1 PYLON PANEL 436CR HAS HOLE ELONGATED, CRACKED ON INNER SKIN AND SPRING SEAL WORN (M) MOORE 350206 09/09/19 (ON REPAIR RACK). REPAIRED PYLON PANEL 436CR I/A/W ERA 581311-14 REV O. (LP1316822)
- [SDR DALA2019101405892](https://openairdocs.org/sdr/DALA2019101405892.md): Panel · corroded · Oct 11, 2019 · N156DL · Boeing 7673P6 · Fuselage Miscellaneous Structure
  > ALC BILGE PNL STA 1153-1175 LBL20-RBL20 CORROSION AT NUMEROUS PLACES. REPAIR BILGE PNAL IAW ERA 581853-14 REV O.
- [SDR DALA2019101105845](https://openairdocs.org/sdr/DALA2019101105845.md): Skin · bent · Oct 10, 2019 · N156DL · Boeing 7673P6 · Nacelle/Pylon, Plate/Skin
  > NO. 2 ENG OUTBD CORE COWL 1ST LATCH HAS BENT SKIN ABOVE LATCH. MARKED. NO. 2 ENG OOUBOARD CORE COWL 1ST LATCH SKIN BENT ABOVE LATCH HAS BEEN REPAIRED PER ER/A 581524-14 REV-0 JOB COMPLETE (LP1309495)
- [SDR DALA2019101115844](https://openairdocs.org/sdr/DALA2019101115844.md): Skin · corroded · Oct 9, 2019 · N156DL · Boeing 7673P6 · Fuselage Main, Plate/Skin
  > SKIN BENEATH STUB BEAM AT RT FUSELAGE, BS 883.5 WAS CORRODED RBL 90. REPAIRED THE SKIN IAW ERA 581549-14, REV 0.
- [SDR DALA2019101115843](https://openairdocs.org/sdr/DALA2019101115843.md): Skin · corroded · Oct 9, 2019 · N156DL · Boeing 7673P6 · Wing, Rib/Bulkhead
  > HORIZONTAL STAB CENTER BOX UPPER SURFACE SKIN CORRODED, STRINGER 3, BL 0. REPAIRED THE UPPER SKIN IAW ERA 581523-14, REV 0.
- [SDR DALA2019100905791](https://openairdocs.org/sdr/DALA2019100905791.md): Floorbeam · corroded · Oct 8, 2019 · N156DL · Boeing 7673P6 · Fuselage Main, Floor Beam
  > CORROSION STA 287 FLOOR BEAM RBL 75 (APPROX.) UPPER SURFACE. REMOVED, LOCATED, DRILLED, DEBURD AND INSTALL NEW T-CAP AT STA 287 RBL75, ALODINE, PRIMED AND TOP COAT IAW B767-300 SRM 53-00- 51 FIG 201 REPAIR 1, SRM 51-40-02 AND SRM 51-20-01 JOB COMPLETE. (LP1305
- [SDR DALA2019100405705](https://openairdocs.org/sdr/DALA2019100405705.md): Shear Tie · corroded · Oct 4, 2019 · N156DL · Boeing 7673P6 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON THE SHEAR TIE AT BS 1197+110, BETWEEN STRINGERS 35L AND STR 36L. FOUND TO BE OUT OF LIMITS. REPLACED THE SHEAR TIE.
- [SDR DALA2019100405704](https://openairdocs.org/sdr/DALA2019100405704.md): Shear Tie · corroded · Oct 4, 2019 · N156DL · Boeing 7673P6 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON THE SHEAR TIE AT BS 1219, STRINGERS 34L-33L. REPLACED THE SHEAR TIE.
- [SDR DALA2019100405703](https://openairdocs.org/sdr/DALA2019100405703.md): Shear Tie · corroded · Oct 4, 2019 · N156DL · Boeing 7673P6 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON THE SHEAR TIE AT BS 1219, STRINGERS 35L-34L. REPLACED THE SHEAR TIE.
- [SDR DALA2019100735755](https://openairdocs.org/sdr/DALA2019100735755.md): Shear Tie · corroded · Oct 3, 2019 · N156DL · Boeing 7673P6 · Fuselage Internal Mounting Structure
  > ALC SHEAR TIE AT STA. 1285, BTW STR. 37L AND STR. 38L IS FOUND TO BE OUT OF LIMITS AND REQUIRES REPLACEMENT. REMOVED, FABRICATED, AND INSTALLED NEW SHEAR TIE AT STA 1285 STR 37L TI 38L AS NEEDED I.A.W B767-300 SRM 51-40-02 PARA 4 AND 7 AND BOEING DWG 140T2102.
- [SDR DALA2019100405702](https://openairdocs.org/sdr/DALA2019100405702.md): Shear Tie · corroded · Oct 3, 2019 · N156DL · Boeing 7673P6 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON THE SHEAR TIE AT BS 1197+66, STRINGERS 38R-37R. REPLACED THE SHEAR TIE.
- [SDR DALA2019100405701](https://openairdocs.org/sdr/DALA2019100405701.md): Shear Tie · corroded · Oct 3, 2019 · N156DL · Boeing 7673P6 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON THE SHEAR TIE AT BS 1263, BETWEEN STRINGERS 38L AND 39L, FOUND OUT OF LIMITS. REPLACED THE SHEAR TIE.
- [SDR DALA2019100405700](https://openairdocs.org/sdr/DALA2019100405700.md): Shear Tie · corroded · Oct 3, 2019 · N156DL · Boeing 7673P6 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON THE SHEAR TIE AT BS 1197+88, BETWEEN STRINGERS 36R AND 37R, FOUND OUT OF LIMITS. REPLACED THE SHEAR TIE.
- [SDR DALA2019100405699](https://openairdocs.org/sdr/DALA2019100405699.md): Shear Tie · corroded · Oct 3, 2019 · N156DL · Boeing 7673P6 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON THE SHEAR TIE AT BS 1219, BETWEEN STRINGERS 39L AND 39R, FOUND TO BE OUT OF LIMITS. REPLACED THE SHEAR TIE.
- [SDR DALA2019100405698](https://openairdocs.org/sdr/DALA2019100405698.md): Shear Tie · corroded · Oct 3, 2019 · N156DL · Boeing 7673P6 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON THE SHEAR TIE AT BS 1197, STRINGERS 38L-39L. REPLACED THE SHEAR TIE.
- [SDR DALA2019100405697](https://openairdocs.org/sdr/DALA2019100405697.md): Shear Tie · corroded · Oct 3, 2019 · N156DL · Boeing 7673P6 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON THE SHEAR TIE AT BS 1197+66, STRINGERS 36R-35R CORRODED. REPLACED SHEAR TIE.
- [SDR DALA2019100405696](https://openairdocs.org/sdr/DALA2019100405696.md): Shear Tie · corroded · Oct 3, 2019 · N156DL · Boeing 7673P6 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON THE SHEAR TIE AT BS 1197+88 BETWEEN STRINGERS 35R AND 36R, FOUND OUT OF LIMITS. REPLACED THE SHEAR TIE.

Next page: https://openairdocs.org/deregistered/N156DL-2023-08-25/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 = 'N156DL' AND deregistration_id = 'N156DL-2023-08-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N156DL-2023-08-25/reports

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