# Service difficulty reports: N125DL, cancelled Dec 6, 2018

A list on [N125DL, cancelled Dec 6, 2018](https://openairdocs.org/deregistered/N125DL-2018-12-06.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 · 63 reports

- [SDR DALA2016021101130](https://openairdocs.org/sdr/DALA2016021101130.md): Wire · cut · Feb 7, 2016 · N125DL · Boeing 767332 · Light System Wiring
  > EMERGENCY LIGHT ON MID OTBD LAV WALL ARE INOPERATIVE. MAINTENANCE REPAIRED CUT WIRE. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2016021101129](https://openairdocs.org/sdr/DALA2016021101129.md): Wire · cut · Feb 7, 2016 · N125DL · Boeing 767332 · Light System Wiring
  > EMERGENCY LIGHTS ON AFT RT LAV WALL ARE INOPERATIVE. MAINTENANCE FOUND WIRE CUT BELOW CARPET AND REPAIRED. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2015022301796](https://openairdocs.org/sdr/DALA2015022301796.md): Structure · damaged · Feb 22, 2015 · N125DL · Boeing 767332 · Standard Practices/Structures
  > 2 EACH HOLES DAMAGED ON INSIDE OF 1809 FWD CORD, COMMON TO THE SKIN ON LT SIDE BELOW LOWER DAMAGE.
- [SDR DALA2015022301795](https://openairdocs.org/sdr/DALA2015022301795.md): Failsafe · cracked · Feb 22, 2015 · N125DL · Boeing 767332 · Fuselage Main, Structure
  > FUSELAGE, FRAME, STA 859.5, LT SIDE FAIL SAFE INNER CHORD/CRACK REPAIRED IAW ERA 532633-14.
- [SDR DALA2015022001604](https://openairdocs.org/sdr/DALA2015022001604.md): Support Beam · damaged · Feb 19, 2015 · N125DL · Boeing 767332 · Trailing Edge Flaps
  > NR 1 FLAP SUPPORT BEAM 2 EA HOLES DAMAGED ON INBD SIDE, 2ND FROM AFT FASTENERS FWD OF LARGE BUSHING. C/W ERA 5326396-14.
- [SDR DALA2015022001602](https://openairdocs.org/sdr/DALA2015022001602.md): Support Beam · damaged · Feb 19, 2015 · N125DL · Boeing 767332 · Trailing Edge Flaps
  > NR 1 FLAP SUPPORT BEAM: HOLE DAMAGED ON INBD SIDE OF BEAM, AFT UPPER FASTENER OF SIDE BRACE MOUNT FITTING HOLE. C/W ERA 532696-01.
- [SDR DALA2015021901603](https://openairdocs.org/sdr/DALA2015021901603.md): Support Beam · cracked · Feb 18, 2015 · N125DL · Boeing 767332 · Trailing Edge Flaps
  > NR 8 FLAP SUPPORT BEAM "C" FASTENER HOLE INDICATE CRACKED C/W ERA 532817-14.
- [SDR DALA2015021701295](https://openairdocs.org/sdr/DALA2015021701295.md): Support Beam · cracked · Feb 16, 2015 · N125DL · Boeing 767332 · Trailing Edge Flaps
  > NR 7 FLAP SUPPORT BEAM CRACKED. REPAIRED IAW ERA 532683-14.
- [SDR DALA2015021701293](https://openairdocs.org/sdr/DALA2015021701293.md): Beam · cracked · Feb 16, 2015 · N125DL · Boeing 767332 · Fuselage Main, Structure
  > BEAM CRACKED. REPAIRED IAW ERA 532683-14.
- [SDR DALA2015021301288](https://openairdocs.org/sdr/DALA2015021301288.md): Skin · cracked · Feb 12, 2015 · N125DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN IS CRACKED. EMANATING FROM UNDER AFT SCUFF PLATE OF L-1 DOOR AND PROGRESSING DOWN AND AFT. REPAIRED IAW SRM 53-10-01.
- [SDR DALA2015020200977](https://openairdocs.org/sdr/DALA2015020200977.md): Skin · cracked · Feb 1, 2015 · N125DL · Boeing 767332 · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON, OTBD SIDE STRUT ASSY. SKIN AT UPPER AFT CORNER OF 442AL ACCESS DOOR CUTOUT CRACKED. C/W PRI 532568-14.
- [SDR DALA13049610125](https://openairdocs.org/sdr/DALA13049610125.md): Light · inoperative · Sep 29, 2013 · N125DL · Boeing 767332 · Emergency Lighting
  > DURING SERVICE CHECK, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. MX REPLACED THE LIGHT ASSY AND BATTERIES. SYS OPERATION IS NORMAL.
- [SDR DALA13027370125](https://openairdocs.org/sdr/DALA13027370125.md): Wire · damaged · May 24, 2013 · N125DL · Boeing 767332 · Emergency Lighting
  > SEAT 25 A/B RED AISLE EMERGENCY LIGHTS ARE INOPERATIVE. MX REPAIRED WIRES. SYS OPERATION IS NORMAL.
- [SDR DALA13018630125](https://openairdocs.org/sdr/DALA13018630125.md): Connector · damaged · Apr 23, 2013 · N125DL · Boeing 767332 · Light System Wiring
  > EMERGENCY PATH LIGHTS AT ROW 41GF ARE INOPERATIVE. MX SECURED PATH LIGHT PLUG SYS OPERATION IS NORMAL.
- [SDR DALA1303660125](https://openairdocs.org/sdr/DALA1303660125.md): Fitting · damaged · Feb 8, 2013 · N125DL · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > WHILE ACCOMPLISHING EA 01-499898-03 AD NEW LONGERON FITTING, WAS FOUND WITH SHORT EDGE MARGIN ON INBD FLANGE SIDE OF FITTING FASTENER HOLES. NEW REPLACEMENT LONGERON FITTING (PN 1114020-8) FABRICATED AND INSTALLED IAW PR1 509717-14 REV 0. DATED 19JAN13. REF
- [SDR DALA1303700125](https://openairdocs.org/sdr/DALA1303700125.md): Washer · migrated · Jan 11, 2013 · N125DL · Boeing 767332 · Wing, Attach Fittings
  > WHILE ACCOMPLISHMENT OF EA 01-499890-03AD ME12 WORK CARD STEP 30, FOUND TENSION BOLT'S SELF AUGMENT WASHER RIDING ON RADIUS OF INTERNAL BATHTUB FITTING. INSTALLATION OF NEW REPLACEMENT LONGERON FITTING TENSION BOLTS CARRIED OUT IAW PRI 509717-14, REV 1, REF
- [SDR DALA1303850125](https://openairdocs.org/sdr/DALA1303850125.md): Web · misrepaired · Jan 10, 2013 · N125DL · Boeing 767332 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON LT UPPER WEB FOUND EXISTING REPAIR IAW ERA 267062-14 NOT IAW SRM AND UPON NDT INSPECTION FOUND CRACK AT ANTI-ICE DUCT CUT-OUT ON WEB. NR 1 PYLON UPPER SPAR WEB CRACKED AREA REPAIRED IAW PRI 510604-14, REV O AND REV 1. (ERA 267062-14)
- [SDR DALA1303380125](https://openairdocs.org/sdr/DALA1303380125.md): Floorbeam · corroded · Jan 4, 2013 · N125DL · Boeing 767332 · Fuselage Main, Floor Beam
  > BS 325, FLOORBEAM UPPER TEE AT RBL25 FOUND CORRODED. EXISTING T-CHORD REPAIR FROM RBL8 TO RBL93. AREA PREVIOUSLY REPAIR IAW SRM 53-00-51, FIG 201, REPAIR 1. EXISTING CORRODED REPAIR UPPER T CHORD, REMOVED AND FABRICATED NEW UPPER T-CHORD INSTALLED IAW SRM
- [SDR DALA1303820125](https://openairdocs.org/sdr/DALA1303820125.md): Skin · misrepaired · Jan 2, 2013 · N125DL · Boeing 767332 · Nacelle/Pylon, Plate/Skin
  > HMV2, DURING ACCOMPLISHMENT OF EA 01-487658, REV A MEO1. FOUND NR 1 PYLON NS 150-180 RT SIDE ACCESS DOOR CUT OUT EXISTING REPAIR NOT IAW THE SRM EXISTING REPAIR DOUBLER AT NR 1 PYLON NACELLE STRUT SKIN ASSY RT SIDE ACCESS DOOR CUT OUT EXTERIOR. REMOVED AND NE
- [SDR DALA1303680125](https://openairdocs.org/sdr/DALA1303680125.md): Support · cracked · Dec 17, 2012 · N125DL · Boeing 767332 · Fuselage Miscellaneous Structure
  > FWD CARGO BETWEEN BS 654 AND 742 LT SIDEWALL UPPER SUPPORT. (STABILIZATION ANGLE) FOUND DAMAGED. FWD CARGO LT SIDE STABILIZATION ANGLE, PN, 143T5401-82 DAMAGED PORTION CUT AND REMOVED BET STA 654-113 TO STA 736 AND REPAIRED IAW PRI ER/A 510619-14, REV O
- [SDR DALA1303690125](https://openairdocs.org/sdr/DALA1303690125.md): Support · cracked · Dec 16, 2012 · N125DL · Boeing 767332 · Fuselage Miscellaneous Structure
  > AFT CARGO BS 1105-1280 LT UPPER SUPPORT FOUND DAMAGED. AFT CARGO LT SIDE STABILIZATION ANGLE, DAMAGED PORTION CUT AND REMOVED AND REPAIRED IAW PRI ER/A 510625-14, REV O AND REV I.
- [SDR DALA1303870125](https://openairdocs.org/sdr/DALA1303870125.md): Stringer · corroded · Dec 15, 2012 · N125DL · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BS 1313, STR 35L FOUND CORRODED. STRINGER REPAIRED IAW ER/A 510073-14, REV ORIG.
- [SDR DALA1303860125](https://openairdocs.org/sdr/DALA1303860125.md): Skin · corroded · Dec 15, 2012 · N125DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > AFT CARGO BS 1200-1219 STRINGER 36R CAP JOINT SKIN CORROSION. REPAIRED IAW ER/A 509718-14, REV 0.
- [SDR DALA1303840125](https://openairdocs.org/sdr/DALA1303840125.md): Floorbeam · corroded · Dec 13, 2012 · N125DL · Boeing 767332 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM UPPER TEE AT BS 347, RBL 25 TO 31 FOUND CORRODED. FLOORBEAM SECTION REMOVED AND NEW FABRICATED REPAIR FLOORBEAM SECTION INSTALLED IAW ER/A 458406-14, REV ORIG.
- [SDR DALA1303390125](https://openairdocs.org/sdr/DALA1303390125.md): Floorbeam · corroded · Dec 13, 2012 · N125DL · Boeing 767332 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM UPPER TEE AT BS 347 BET RBL 25 TO RBL 31. FOUND CORROSION. AREA OF FLOORBEAM IS PREVIOUSLY SECTIONAL CUT-OUT AT RBL3102 AND LBL 3102 AND REPAIRED IAW ER/A 458406-14 (REF: ACTS PP NO B767-53-27165). EXISTING REPAIRED CORRODED FLOORBEAM SECTIO
- [SDR DALA1204970125](https://openairdocs.org/sdr/DALA1204970125.md): Battery Pack · discharged · Jan 27, 2012 · N125DL · Boeing 767332 · Emergency Lighting
  > EMERGENCY EXIT LIGHT AFT R3 ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.
- [SDR DALA1256700125](https://openairdocs.org/sdr/DALA1256700125.md): Failsafe · cracked · Jul 26, 2011 · N125DL · Boeing 767332 · Fuselage Main, Structure
  > A CRACK WAS FOUND DURING INSPECTION OF THE FAILSAFE FITTING IN THE RT AND LT MAIN LANDING GEAR WHEEL WELL. REPAIR IAW 479305-14.
- [SDR DALA1112880125](https://openairdocs.org/sdr/DALA1112880125.md): Wire · broken · Feb 22, 2011 · N125DL · Boeing 767332 · Light System Wiring
  > EMERGENCY LIGHTS RED ON LAVATORY L2 ARE INOPERATIVE. MAINTENANCE FOUND WIRE BROKEN AT FLOOR LEVEL AND REPAIRED. SYSTEM OPERATION IS NORMAL.
- [SDR DALA1012540125](https://openairdocs.org/sdr/DALA1012540125.md): Light · inoperative · Jun 6, 2010 · N125DL · Boeing 767332 · Emergency Lighting
  > PASSENGER SEAT 05C EMERGENCY LIGHTING FLOOR LIGHTS INOP. RESET SYS. OPS CK OK.
- [SDR DL76S100244](https://openairdocs.org/sdr/DL76S100244.md): Failsafe · cracked · Dec 14, 2009 · N125DL · Boeing 767332 · Fuselage Main, Structure
  > INSPECTIONS SI 01-086393-12AD FOUND CORROSION IN THE RT AND LT FAILSAFE STRAPS WHICH REQUIRED TRIMMING IAW SB INSTRUCTIONS UPON REMOVAL OF THE CUT SECTIONS CORROSIONS WAS NOTED ON THE FUSALAGE SKIN COMMON TO THE AREA TRIMMED OUT. PLEASE NOTE THAT THE DEPTH WAS
- [SDR DL76S100243](https://openairdocs.org/sdr/DL76S100243.md): Failsafe · cracked · Dec 14, 2009 · N125DL · Boeing 767332 · Fuselage Main, Structure
  > AT PSV INSPECTIONS PRE SI 01-086393-12AD FOUND THE FAILSAFE CRACKED BOTH LT AND RT SIDES AND REQUIRED TRIMMING IAW SB 767-53-0100 REV 1. UPON REMOVAL OF THE CUT SECTIONS CORROSION WAS NOTED ON THE FUSALAGE SKIN COMMON TO THE AREA TRIMMED NOTE THAT THE 2 LOWER
- [SDR DL76S100242](https://openairdocs.org/sdr/DL76S100242.md): Fitting · corroded · Dec 14, 2009 · N125DL · Boeing 767332 · Fuselage Main, Attach Fittings
  > WHILE ACCOMPLISHING INSPECTIONS OF THE FS 955 REAR SPAR BULKHEAD AND FAILSAFE STRAPS FOR CORROSION AND FATIGUE CRACKS IAW DAL SI01-086393-12AD CORROSION WAS FOUND ON THE RT SIDE BRACE FITTING AND FAILSAFE STRAPS BOTH SIDE BRACE AND FAILSAFE WERE REPLACED ON TH
- [SDR DL76S071641](https://openairdocs.org/sdr/DL76S071641.md): Skin · damaged · Dec 20, 2007 · N125DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > MINOR SKIN BLENDS AT FS 1219-1270 ALONG S-21R TO S-26R.
- [SDR DL76S071639](https://openairdocs.org/sdr/DL76S071639.md): Skin · damaged · Dec 18, 2007 · N125DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > MINOR SKIN BLENDS AT FS 1438 TO 1540, ALONG S-19L TO S-26L. REPAIRED PER ER/A 459229-14ADREVA.
- [SDR DL76S071631](https://openairdocs.org/sdr/DL76S071631.md): Skin · damaged · Dec 18, 2007 · N125DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > SKIN BLENDS FS 1444 AND S-39R, AND FS 1448 AND S-38L. REPAIRED PER ER/A 459236-14 REV A.
- [SDR DL76S071621](https://openairdocs.org/sdr/DL76S071621.md): Skin · damaged · Dec 3, 2007 · N125DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BLENDS, FS 1285, AND STR 36R. REPAIRED PER ER/A 459263-14 REV A.
- [SDR DL76S071600](https://openairdocs.org/sdr/DL76S071600.md): Skin · damaged · Nov 28, 2007 · N125DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BLENDS AT FS 1286.5 AND 32L DUE TO GROUND DAMAGE PER ER/A 459209-14 REV A.
- [SDR DL76S070818](https://openairdocs.org/sdr/DL76S070818.md): Fitting · corroded · Jun 24, 2007 · N125DL · Boeing 767332 · Fuselage Main, Attach Fittings
  > RT NLG TRUNNION BORE CORRODED AND TOOLING DAMAGE FOUND ON WEB. BORE OVERSIZED AND AN OVERSIZED BUSHING INSTALLED. TOOLING DAMAGE OVERSIZED AND A BUSHING INSTALLED.
- [SDR DL76S070211](https://openairdocs.org/sdr/DL76S070211.md): Starter · inoperative · Mar 16, 2007 · N125DL · Boeing 767332 · APU Start/Ignition System
  > STRONG SMELL NOTICED BOTH INSIDE AND OUTSIDE AIRCRAFT SMELL STARTED AFTER POWER TRANSFER TO APU AND PACKS WERE TURNED ON. GROUND PERSONNEL ALSO REPORTED STRONG SMELL AND REPORTED SMOKE COMING OUT OF AN APU VENT. INSP APU AREA FOUND STARTER MOTOR W/STRONG BUR
- [SDR DL76S061058](https://openairdocs.org/sdr/DL76S061058.md): Skin · lightning strike · Dec 23, 2006 · N125DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > AT HMV, LIGHTNING STRIKES WERE FOUND JUST AFT OF FS 347 AND ABOVE S33R AND REPAIRED PER SRM 53-00-01, FIGURE 201, REPAIR 14. THIS REPAIR IS LOCATED JUST ABOVE AND AFT OF A REPAIR INSTALLED PER ERA 387247-14. THE REPAIRS ARE LOCATED 13" APART. ERA 459155-14
- [SDR DL76S061057](https://openairdocs.org/sdr/DL76S061057.md): Skin · nicked · Dec 22, 2006 · N125DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > AT HMV, TWO NICKS WERE NOTED IN THE FUSELAGE SKIN AT FS 654 +4-+9 BETWEEN STR 35L AND 36L. THE RESULTING BLENDS EXCEEDED THE SRM ALLOWABLE DAMAGE REQUIREMENTS. ERA 459156-14 WAS ISSUED TO REPAIR THE DAMAGE.
- [SDR DL76S061056](https://openairdocs.org/sdr/DL76S061056.md): Skin · nicked · Dec 22, 2006 · N125DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > AT HMV, SIX NICKS TO THE FUSELAGE SKIN WERE FOUND AND BLENDED PER SRM. THE RESULTING BLENDS EXCEEDED SRM ALLOWABLE LIMITS. ERA 459158-14 ACCOMPLISHED REPAIR.
- [SDR DL76S061055](https://openairdocs.org/sdr/DL76S061055.md): Skin Panel · corroded · Dec 22, 2006 · N125DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > CORROSION WAS FOUND AT FS 1585 AND STR 38R-39R, 148T3251-4 SKIN PANEL. THE CORROSION WAS FOUND AT HMV AND WAS REPAIRED PER ERA 458836-14.
- [SDR DL76S061054](https://openairdocs.org/sdr/DL76S061054.md): Floorbeam · cracked · Dec 22, 2006 · N125DL · Boeing 767332 · Fuselage Main, Floor Beam
  > FIVE CRACKS WERE FOUND IN THE FS 347 FLOORBEAM UPPER CAP. THREE OF THE CRACKS EXTENDED INTO THE WEB. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 458406-14.
- [SDR DL76S061053](https://openairdocs.org/sdr/DL76S061053.md): Skin · damaged · Dec 22, 2006 · N125DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > DAMAGE WAS DISCOVERED IN THE FUSELAGE SKIN AT FS 654 +22 TO +66 AND STR 3R - 4R THAT RESULTED IN TWO SRM REPAIRS 4.875" APART. A DTA WAS ACCOMPLISHED AND THE INSPECTION REQUIREMENTS WERE IMPLEMENTED PER ERA 459157-14.
- [SDR DL76S061050](https://openairdocs.org/sdr/DL76S061050.md): Frame · cracked · Dec 21, 2006 · N125DL · Boeing 767332 · Fuselage Main, Frame
  > A CRACK WAS FOUND IN THE INNER CHORD OF THE STA 883.5 FRAME AT WL 190 ON THE RT SIDE. THE CRACK WAS TRIMMED OUT AND A REPAIR ANGLE WAS INSTALLED.
- [SDR DL76S061049](https://openairdocs.org/sdr/DL76S061049.md): Frame · cracked · Dec 21, 2006 · N125DL · Boeing 767332 · Fuselage Main, Frame
  > A CRACK WAS FOUND ON THE INNER CHORD OF THE STA 903.5 FRAME. THE CRACK WAS TRIMMED OUT AND A REPAIR ANGLE WAS INSTALLED.
- [SDR DL76S060990](https://openairdocs.org/sdr/DL76S060990.md): Web · cracked · Nov 16, 2006 · N125DL · Boeing 767332 · Nacelle/Pylon, Main Frame
  > THE NR 1 STRUT MIDSPAR WEB WAS FOUND CRACKED. THE CRACKED WEB REINFORCED WITH A DOUBLER.
- [SDR DL76S040343](https://openairdocs.org/sdr/DL76S040343.md): Switch · overheated · Apr 15, 2004 · N125DL · Boeing 767332 · Independent Position Determining System
  > ON DESCENT STARTED TO DETECTED A SLIGHT BURNING ODOR, ELECTRICAL ODOR. CREW DECLARED AN EMERGENCY. FOUND GPWS MODULE OVERHEATED. REMOVED MODULE AND FORWARDED TO MCO AND PLACARD.
- [SDR DL76S010370](https://openairdocs.org/sdr/DL76S010370.md): Skin · tool damage · Mar 2, 2001 · N125DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF A SRM SKIN REPAIR, TOOLING DAMAGE OCCURRED TO STR 39L. THIS DOCUMENT PROVIDES A REPAIR OF BOTH THE STRINGER AND SKIN. THE DAMAGE IS LOCATED AT STA 355. CORRECTIVE ACTION: ER/A 397313-14

Next page: https://openairdocs.org/deregistered/N125DL-2018-12-06/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 = 'N125DL' AND deregistration_id = 'N125DL-2018-12-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N125DL-2018-12-06/reports

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