# Service difficulty reports: N124DE, cancelled May 16, 2018

A list on [N124DE, cancelled May 16, 2018](https://openairdocs.org/deregistered/N124DE-2018-05-16.md).

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

- [SDR DALA2015011200438](https://openairdocs.org/sdr/DALA2015011200438.md): Door Frame · corroded · Jan 11, 2015 · N124DE · Boeing 767332 · Fuselage Main, Structure
  > LEFT FORWARD OVERWING EXIT DOOR FRAME IS CORRODED AT FORWARD LOWER CORNER. REMOVED AND FABRICATED NEW ANGLE.
- [SDR DALA2014091805094](https://openairdocs.org/sdr/DALA2014091805094.md): Skin · damaged · Sep 17, 2014 · N124DE · Boeing 767332 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGED. REPAIRED IAW ERA 528965-14.
- [SDR DALA2014091805093](https://openairdocs.org/sdr/DALA2014091805093.md): Skin · damaged · Sep 17, 2014 · N124DE · Boeing 767332 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGED. REPAIRED IAW ERA 528966-14.
- [SDR DALA2014091805092](https://openairdocs.org/sdr/DALA2014091805092.md): Skin · damaged · Sep 17, 2014 · N124DE · Boeing 767332 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN GROUND DAMAGED. REPAIRED IAW ERA 528964-14.
- [SDR DALA2014091705090](https://openairdocs.org/sdr/DALA2014091705090.md): Stringer · cracked · Sep 16, 2014 · N124DE · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > RT SIDE FUSELAGE STRINGER 30R CRACKED BS 1530-1540. REMOVED STRINGER IAW SRM 53-00-01,. PERFORMED HFEC FOR DAMAGE CONTAINMENT, NO FINDINGS.
- [SDR DALA13028270124](https://openairdocs.org/sdr/DALA13028270124.md): Floorbeam · cracked · Jun 7, 2013 · N124DE · Boeing 767332 · Fuselage Floor Panel
  > CABIN BS 347 FLOORBEAM UPPER TEE FOUND CRACKED AT RBL 2.0 AND RBL 8.0 & LBL 9.0. REPAIRED IAW 514023-14 (LP 0917476).
- [SDR DALA13028260124](https://openairdocs.org/sdr/DALA13028260124.md): Failsafe · cracked · Jun 7, 2013 · N124DE · Boeing 767332 · Fuselage Main, Bulkhead
  > CRACK ON RT BULKHEAD FAIL SAFE STRAP AT BS 955. REPAIRED IAW PRI 514007-14AD, REV 0.
- [SDR DALA13023700124](https://openairdocs.org/sdr/DALA13023700124.md): Stringer · corroded · May 21, 2013 · N124DE · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > FWD CARGO -BS 412-434, STRINGER 38R CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201, REPAIR 2, REV 92.00.
- [SDR DALA13023690124](https://openairdocs.org/sdr/DALA13023690124.md): Stringer · corroded · May 21, 2013 · N124DE · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > FWD CARGO BS 412-434, STRINGER 36R CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201, REPAIR 2, REV 92.00.
- [SDR DALA13023680124](https://openairdocs.org/sdr/DALA13023680124.md): Stringer · corroded · May 21, 2013 · N124DE · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > FWD CARGO BS 412-434, STRINGER 34R CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201, REPAIR 2, REV 92.00.
- [SDR DALA13023670124](https://openairdocs.org/sdr/DALA13023670124.md): Stringer · corroded · May 21, 2013 · N124DE · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > FWD CARGO BS 412-434 STRINGER 27R CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-03 FIG 201, REPAIR 2, REV 92.00.
- [SDR DALA13023660124](https://openairdocs.org/sdr/DALA13023660124.md): Stringer · corroded · May 21, 2013 · N124DE · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > FWD CARGO BS 412-434 STRINGER 39R CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201, REPAIR 2, REV 92.00.
- [SDR DALA13023650124](https://openairdocs.org/sdr/DALA13023650124.md): Stringer · corroded · May 21, 2013 · N124DE · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > FWD CARGO BS 412-434, STRINGER 35R CORRODED, REPAIR CARRIED OUT IAW SRM 53-00-03 FIG 201, REPAIR 2, REV 92.00.
- [SDR DALA13023490124](https://openairdocs.org/sdr/DALA13023490124.md): Frame · cracked · May 20, 2013 · N124DE · Boeing 767332 · Fuselage Main, Frame
  > DURING HFEC INSPECTION ON BS 1809, BULKHEAD LT FORWARD OUTER FRAME S6-7L FOUND CRACKED. REPAIRED FRAME.
- [SDR DALA13028310124](https://openairdocs.org/sdr/DALA13028310124.md): Structure · corroded · May 8, 2013 · N124DE · Boeing 767332 · Fuselage Main, Structure
  > WING CENTER SECTION UPPER SURFACE BETWEEN BS 857 AND 859, LBL 88. REWORKED IAW PRI 514634-14, REV 0, REV 1, REV 2, REV 3 AND REV 4.
- [SDR DALA13028300124](https://openairdocs.org/sdr/DALA13028300124.md): Structure · corroded · May 8, 2013 · N124DE · Boeing 767332 · Fuselage Main, Structure
  > WING CENTER SECTION UPPER SURFACE AT BS 927, LBL 90. REPAIR CARRIED OUT IAW- PRI 514016-14, REV 0, REV 1, REV 2, REV 3, REV 4, REV 5 AND REV 6. AND COMPLIED WITH ER/A 514016-14, REV ORIGINAL.
- [SDR DALA2015082707893](https://openairdocs.org/sdr/DALA2015082707893.md): Skin · cracked · Aug 14, 2012 · N124DE · Boeing 767332 · Fuselage Main, Plate/Skin
  > CRACK AT BS 687, STRINGER 36R AT CARRY THOUGH HOLE, RT AIRFONE BLANKING PLATE, 1/8TH INCH CRACK.
- [SDR DALA1245820124](https://openairdocs.org/sdr/DALA1245820124.md): Skin · cracked · Aug 14, 2012 · N124DE · Boeing 767332 · Fuselage Main, Plate/Skin
  > SKIN CRACKED ONE EIGTH INCH CRACK RT AIRFONE BLANKING PLATE INST STA 687 STR 36R AT CARRY THRU HOLE LOC MARKED REF ERA 389647-14 REV A. REPAIRED PER SRM B767-300 53-00-01 REPAIR 12.
- [SDR DALA1102330124](https://openairdocs.org/sdr/DALA1102330124.md): Skin · delaminated · Jan 11, 2011 · N124DE · Boeing 767332 · Trailing Edge Flaps
  > RT WING OTBD FLAP LWR SURFACE MID INSPAR PANEL SKIN DELAMINATED AT APPROX 66"FROM INBD AND 24" FRM BOTTOM; CA: REPAIR DOUBLER AND FILLER FABRICATED IAW SRM 57-53-01 OTIS. REPAIR PARTS BONDED IAW SRM 51-70-10 OTIS. DECAL INSTALLED ADJ TO REPAIR IAW PS 900-5-
- [SDR DALA1102320124](https://openairdocs.org/sdr/DALA1102320124.md): Wedge · delaminated · Jan 11, 2011 · N124DE · Boeing 767332 · Leading Edge Devices
  > LT WING L/E NR2 SLAT WEDGE UPPER SURFACE FOUND DELAMINATED; CA: LT WING L/E NR2 SLAT WEDGE UPPER SURFACE, REPAIR FILLER AND DOUBLER FABRICATED IAW 51-70-10 OTIS. DECAL INSTALLED ADJ TO REPAIR IAW DELTA PS 900-5-1, NR 4.
- [SDR DALA1102060124](https://openairdocs.org/sdr/DALA1102060124.md): Skin · dented · Jan 10, 2011 · N124DE · Boeing 767332 · Vertical Stabilizer, Plate/Skin
  > LT V-STAB EXTERIOR AROUND FS STA 270.784 FOUND DENT DURING HMV INSP AT SIN; C/A-DENTED SURFACE TRIMMED OFF. REPAIR PART FABRICATED IAW SRM 51-70-01, FIG 201, OT IS REPAIR PARTS BONDS IAW SRM 51-71-10.
- [SDR DL76S071392](https://openairdocs.org/sdr/DL76S071392.md): Indicator · malfunctioned · Oct 27, 2007 · N124DE · Boeing 767332 · Airspeed/Mach Indicator
  > AFTER TO, F/O AIRSPEED INDICATOR BECAME UNREADABLE AND ROSE STEADILY TO 400 KTS. NO FLAGS OR OTHER INDICATIONS, OTHER THAN OVERSPEED WARNING. ACTUAL AIRSPEED ON CAPTS IND NORMAL. FOUND QUICK DISCONNECT DAMAGED ON PITOT PRESS ON RT ADC. REPLACED SAME. LEAK
- [SDR DL76S071386](https://openairdocs.org/sdr/DL76S071386.md): Trunnion · corroded · Oct 24, 2007 · N124DE · Boeing 767332 · Fuselage, Landing Gear Attach Fittings
  > LT AND RT NOSE LANDING GEAR TRUNNION FITTINGS CORRODED IN THE INNER DIAMETER. CORROSION CLEANED UP AND OVERSIZED BUSHINGS WERE INSTALLED.
- [SDR DL76S071046](https://openairdocs.org/sdr/DL76S071046.md): Mec · malfunctioned · Aug 8, 2007 · N124DE · Boeing 767332 · Fuel Controlling System
  > RTO DUE TO RT ENGINE WOULD NOT MAKE TAKEOFF POWER. REPLACED RT ENGINE MEC. AFTER RUNUP ENGINE MAKES TAKEOFF POWER.
- [SDR DL76S070504](https://openairdocs.org/sdr/DL76S070504.md): Charger · missing · May 9, 2007 · N124DE · Boeing 767332 · Emergency Lighting
  > EMERGENCY LIGHT EXIT SIGN INOP AT L1 AND R1 DOOR. INSTALLED NEW BATTERY AND CHARGER TRA, FOUND TRAY AND BATTERY PACK ASSY MISSING AT L1 POSITION.
- [SDR DL76S060797](https://openairdocs.org/sdr/DL76S060797.md): Floorbeam · corroded · Sep 28, 2006 · N124DE · Boeing 767332 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM UPPER CHORD STA 287 CORRODED AT RBL 51 TO RBL 62 AND ALSO EXISTING SPLICE PLATE CORRODED AT RBL 10 TO RBL 15. REPAIRED PER SRM 53-00-51D FIGURE 201, AMM 32-41-00.
- [SDR DL76S060796](https://openairdocs.org/sdr/DL76S060796.md): Floorbeam · cracked · Sep 28, 2006 · N124DE · Boeing 767332 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM AT STA 325 LBL 32 UPPER STRUCTURE BENT AND CRACKED IN RADIUS AS MARKED. REPAIRED PER SRM 53-00-51D FIGURE 201.
- [SDR DL76S060793](https://openairdocs.org/sdr/DL76S060793.md): Fitting · fatigued · Sep 28, 2006 · N124DE · Boeing 767332 · Nacelle/Pylon, Attach Fittings
  > DURING REWORK OF THE FORWARD UPPER SPAR FITTING PER SIP EO, CRACKING INDICATIONS WERE FOUND AT AFT OUTBOARD FASTENER LOCATIONS COMMON TO MIDSTRUT BULKHEAD FITTING ON EACH PYLON. HOLES WERE OVERSIZED AND BUSHED BACK TO DIAMETER.
- [SDR DL76S060792](https://openairdocs.org/sdr/DL76S060792.md): Fitting · fatigued · Sep 28, 2006 · N124DE · Boeing 767332 · Engine Mount Section
  > CRACK INDICATIONS WERE FOUND AT THE FORWARD OUTBOARD BOLT HOLE LOCATION OF THE AFT PITCH LOAD FITTING, NR 1 PYLON. CRACK IS IN LOWER WING SKIN ALSO, AND REQUIRED SUBJECT HOLE TO BE OVERSIZED AND BUSHED BACK TO DIAMETER.
- [SDR DL76S060791](https://openairdocs.org/sdr/DL76S060791.md): Frame · cracked · Sep 28, 2006 · N124DE · Boeing 767332 · Fuselage Main, Frame
  > FUSELAGE STATION 903.5 FRAME INNER CHORD FOUND CRACKED. ON BOTH LT AND RT AT TRANSITION BETWEEN CHORD FLANGES. AREA TRIMMED AND REPAIR INSTALLED.
- [SDR DL76S060790](https://openairdocs.org/sdr/DL76S060790.md): Rib · corroded · Sep 28, 2006 · N124DE · Boeing 767332 · Wing, Rib/Bulkhead
  > RT WING RIB NR 8, LOWER OUTBOARD HOLE WAS FOUND WITH CORROSION PITTING. DAMAGE WAS REMOVED BY OVERSIZED HOLE, BUSHING INSTALLATION.
- [SDR DL76S060695](https://openairdocs.org/sdr/DL76S060695.md): Linkage · misinstalled · Aug 23, 2006 · N124DE · Boeing 767332 · Escape Slide
  > DURING INSPECTION OF THE LT OFF WING ESCAPE SLIDE PER JIC 6075 THE TECHNICIAN FOUND THAT THE INTEGRATOR LOCK HANDLE HAD TO BE FORCED INTO THE SAFETY POSITION. UPON FURTHER INVESTIGATION IT WAS DETERMINED THAT SLIDE DOOR OPENING ACTUATOR LINKAGE LEVER WAS INSTA
- [SDR DL76S060467](https://openairdocs.org/sdr/DL76S060467.md): Skin · lightning strike · May 23, 2006 · N124DE · Boeing 767332 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN WAS STRUCK BY LIGHTNING BETWEEN BS 257 AND 277 BELOW S-11L. THE DAMAGED SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED.
- [SDR DL76S060140](https://openairdocs.org/sdr/DL76S060140.md): Bolt · missing · Feb 15, 2006 · N124DE · Boeing 767332 · Leading Edge Slat Actuator
  > NR 2 SLAT I/B ACTUATOR COVER DAMAGED. REINSTALLED MISSING HARDWARE, RAN SLATS, ALL OK.
- [SDR DL76S030503](https://openairdocs.org/sdr/DL76S030503.md): Skin · cracked · Jun 2, 2003 · N124DE · Boeing 767332 · Fuselage Main, Plate/Skin
  > MECHANIC FOUND 2 INCH CRACK IN FUSELAGE SKIN RT SIDE STA 1654.5 STR 3R. ALSO, FOUND STRINGER 3R AND 3L CRACKED AT SAME LOCATION. REPAIRED CRACK.
- [SDR DL76S020842](https://openairdocs.org/sdr/DL76S020842.md): Skin · dented · Jul 18, 2002 · N124DE · Boeing 767332 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / FS 287-303 / STRG. 37R: DENT REPAIR THE FUSELAGE SKIN WAS DENTED AT THE STRINGER 37R SKIN LAP JOINT BETWEEN FS 287 & 303. THE LAPJOINT WAS CUTOUT IN THE AREA TO REMOVE T
- [SDR DL76S020565](https://openairdocs.org/sdr/DL76S020565.md): Power Supply · discharged · May 17, 2002 · N124DE · Boeing 767332 · Emergency Lighting
  > OVERHEAD AISLE LIGHTS FIRST CLASS LEFT SIDE INOP. REPLACED BATTERY PACK AND RACK.
- [SDR DL76S020406](https://openairdocs.org/sdr/DL76S020406.md): Skin · cracked · Apr 4, 2002 · N124DE · Boeing 767332 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING THE FS 1809.5 BULKHEAD OUTER CHORD MOD PER BAC S/B 767-53-0078 AND AD 2001-09-13, A CRACK WAS FOUND IN THE SKIN COMMON TO A FASTENER HOLE FOR THE OUTER CHORD ON THE LT SIDE. THE HOLE WAS OVERSIZED IN THE SKIN ASSY ONLY AND A BUSHING INSTAL
- [SDR DL76S011920](https://openairdocs.org/sdr/DL76S011920.md): Battery Pack · discharged · Dec 10, 2001 · N124DE · Boeing 767332 · Emergency Lighting
  > LEFT FORWARD OVERHEAD EMERGENCY LIGHTS INOP IN CABIN. REMOVED AND REPLACED BATTERY PACK FOR LEFT FORWARD OVERHEAD EMERGENCY LIGHTS, CHECKS GOOD.
- [SDR DL76S011516](https://openairdocs.org/sdr/DL76S011516.md): Engine · unserviceable · Sep 10, 2001 · N124DE · Boeing 767332 · Engine (Turbine/Turboprop)
  > ON CLIMB OUT RIGHT ENGINE STALLED. ACCOMPLISHED POM "ENGINE SURGE OR STALL" PROCEDURE. THROTTLE REDUCED TO IDLE. ENGINE SHUT DOWN AFTER LANDING. EGT MAX 895 FOR 1.4 SECONDS. FOUND METAL IN EXHAUST. REPLACED ENGINE.
- [SDR DL76S010388](https://openairdocs.org/sdr/DL76S010388.md): Probe · malfunctioned · Mar 10, 2001 · N124DE · Boeing 767332 · Flight Environment Data
  > RTB FOR INSP. DUE TO SMOKE COMING FROM LT NOSE AREA OVER RADOME. J/C VISUAL INSPECTION OF NLG AREA, FWD AND MAIN E/E COMPARTMENTS. ALSO VISUALLY INSPECTED OF LT / RT ACM AREAS AND RADAR ANTENNA AREA. NO ANOMALIES NOTED-ALL HYD QTYS NORMAL, NO HYD LEAKS FOUN
- [SDR DL76S010170](https://openairdocs.org/sdr/DL76S010170.md): Frame · corroded · Jan 26, 2001 · N124DE · Boeing 767332 · Fuselage Main, Frame
  > CORROSION WAS FOUND ON THE FWD FRAME AT THE CUTOUT FOR THE FWD LT PASSENGER DOOR. THE CORROSION WAS LOCATED ON THE AFT SURFACE OF THE FRAME WEB SURROUNDING THE GIRT BAR HOLE (JUST ABOVE CABIN FLOOR LEVEL). REPAIRED DAMAGE PER ER/A 396699-14.
- [SDR DL76S010171](https://openairdocs.org/sdr/DL76S010171.md): Skin · dented · Jan 25, 2001 · N124DE · Boeing 767332 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN WAS DENTED DUE TO NOSE TIRE BLOWOUT. THE DENTS WERE APPROVED FOR INTERIM SERVICE PER ER/A 269377-14. THE DAMAGE WAS PERMANENTLY REPAIRED PER ER/A 269377-14 AT OVERHAUL MTC VISIT. REPAIRED DAMAGE PER ER/A 269377-14.
- [SDR DL76S992442](https://openairdocs.org/sdr/DL76S992442.md): Light · inop · Nov 4, 1999 · N124DE · Boeing 767332 · Emergency Lighting
  > FOUR AISLE EMERGENCY LIGHTS INOP AFT RIGHT SIDE. REPLACED POWER SUPPLY, SYSTEM CHECKS NORMAL.
- [SDR DL76S990692](https://openairdocs.org/sdr/DL76S990692.md): Mask · fell · Mar 29, 1999 · N124DE · Boeing 767332 · Passenger Oxygen System
  > THE O2 MASK ZONE C HANGING DOWN. REINSTALLED MASK AND SECURED PANEL.
- [SDR DL76S981698](https://openairdocs.org/sdr/DL76S981698.md): Skin · corroded · Aug 12, 1998 · N124DE · Boeing 767332 · Wing, Plate/Skin
  > CORROSION WAS FOUND ON THE WING CENTER SECTION. DAMAGE LOCATED ON AFT SKIN PANEL, FWD EDGE ON THE LT OUTBD END. REPAIRED PER ERA 331990-14.
- [SDR DL76S981265](https://openairdocs.org/sdr/DL76S981265.md): Power Supply · inoperative · Jun 15, 1998 · N124DE · Boeing 767332 · Emergency Lighting
  > ON L/O, FOUND ZONE EMERGENCY TRACK LIGHTS INOP BOTH AISLES. REPLACED PWR SUPPLY M9010. LIGHTS OPS NML.
- [SDR DL76S971347](https://openairdocs.org/sdr/DL76S971347.md): Skin · delaminated · Jul 1, 1997 · N124DE · Boeing 767332 · Leading Edge Devices
  > THE NR 9 LE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE A 3.5 DIAMETER SECTION OF THE UPPER SKIN DELAMINATED. THE DAMAGE IS LOCATED IN THE CENTER OF THE SLAT WEDGE FWD/ AFT AND INB'D/OUTB'D. THE DAMAGED SECTION WAS REPAIRED PER B767 SRM 57-43-02, FIGURE 201.

## 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 = 'N124DE' AND deregistration_id = 'N124DE-2018-05-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N124DE-2018-05-16/reports

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