# Service difficulty reports: N137DL, cancelled Jul 12, 2018

A list on [N137DL, cancelled Jul 12, 2018](https://openairdocs.org/deregistered/N137DL-2018-07-12.md).

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

- [SDR DALA2017042703426](https://openairdocs.org/sdr/DALA2017042703426.md): Skin · corroded · May 24, 2015 · N137DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > ON WALK AROUND FOUND CORRODED HOLE IN FUSELAGE 1" X 1" ON LT FWD SIDE OF SECTION FS 456.0. REPAIRED DOUBLER.
- [SDR DALA13064380137](https://openairdocs.org/sdr/DALA13064380137.md): Wire Harness · pinched · Nov 22, 2013 · N137DL · Boeing 767332 · Electrical Power System Wiring
  > F/A REPORTED AFTER LANDING "SPARKS" CAME OUT OF FWD BULKHEAD AT SEATS 1E, F AND THEN THE IFES FOR E & F ROWS WENT BLANK. MAINTENACE INSPECTED MONITORS & SEAT BOX AT 1E&F. NO DAMAGE NOTED. NO ODOR OF FIRE AROUND 1E&F. FOUND POWER HARNESS PINCHED UNDER SEAT 1
- [SDR DALA1229380137](https://openairdocs.org/sdr/DALA1229380137.md): Nut · loose · May 5, 2012 · N137DL · Boeing 767332 · Leading Edge Devices
  > FOUND NR 1 SLAT INBD SLAT TRACK DOWN STOP NUT LOOSE. C/W EA 01-469704-03AD OPN 2201, NO DEFECTS NOTED. REPLACED DOWNSTOP ATTACH BOLT NUT IAW B767 AMM 27-81-34-404-014 STEP D (3)(D)1-3.
- [SDR DALA1129750137](https://openairdocs.org/sdr/DALA1129750137.md): Frame · cracked · Apr 2, 2011 · N137DL · Boeing 767332 · Fuselage Main, Frame
  > CABIN: STA 903.5 FRAME INNER CHORD FOUND CRACKED TRANSITION RADIUS AT RBL 90. STA 903.5 FRAME CRACKED INNER CHORD REPAIRED IAW ER/A 490891-14AD REV ORIGINAL.
- [SDR DALA1129740137](https://openairdocs.org/sdr/DALA1129740137.md): Frame · punctured · Mar 31, 2011 · N137DL · Boeing 767332 · Fuselage Main, Frame
  > AFT CARGO: STA 1351 BETWEEN STR 26R AND 27R FRAME WEB FOUND PUNCTURE (DENT 0.7" WITH 0.4" CRACKED). STA 1351 BETWEEN STR 26R AND 27R FRAME WEB PUNTURED AREA TRIMMED-OUT AND REPAIRED IAW ER/A 490897-14 REV ORIGINAL.
- [SDR DALA1129080137](https://openairdocs.org/sdr/DALA1129080137.md): Floorbeam · corroded · Mar 29, 2011 · N137DL · Boeing 767332 · Fuselage Main, Floor Beam
  > AFT CARGO FLOORBEAM AT STA 1197, INNER CHORD FOUND CORRODED AT LBL 13.0 AND LBL 42.0. AFT CARGO FLOORBEAM AT STA 1197 INNER CHORD TRIMMED BETWEEN BL 0 TO LBL 44 AND REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 4, OTIS.
- [SDR DALA1129070137](https://openairdocs.org/sdr/DALA1129070137.md): Floorbeam · corroded · Mar 27, 2011 · N137DL · Boeing 767332 · Fuselage Main, Floor Beam
  > CABIN: STA 325, RBL 26.0, FLOORBEAM UPPER HORIZ FLANGE FOUND CORRODED. STA 325 FLOORBEAM UPPER HORIZ CORRODED FLANGE TRIMMED BET RBL 12.0 TO RBL 45.5 AND REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201, OTIS.
- [SDR DALA1129060137](https://openairdocs.org/sdr/DALA1129060137.md): Floorbeam · corroded · Mar 27, 2011 · N137DL · Boeing 767332 · Fuselage Main, Floor Beam
  > CABIN AT STA 287, RBL 60.75 FLOORBEAM UPPER HORIZ FLANGE FOUND CORRODED. CORROSION FOUND ON EXISTING REPAIRED TEE:EXISTING REPAIRED TEE WITH CORROSION REMOVED AND NEW TEE FABRICATED AND INSTALLED IAW SRM 53-00-51, FIG 201, REPAIR 1 OTIS. AREA REPAIRED IAW S
- [SDR DALA1129050137](https://openairdocs.org/sdr/DALA1129050137.md): Failsafe · cracked · Mar 21, 2011 · N137DL · Boeing 767332 · Fuselage Main, Bulkhead
  > DURING ACCOMPLISHMENT INSP IAW DAL OPN 8701AD FOUND BS 955 REAR SPAR BULKHEAD LT SIDE FAIL SAFE STRAP, PN 145T2524-23, FOUND CRACKED. REAR SPAR BULKHEAD LT SIDE CRACKED FAIL SAFE STRAP REPAIRED IAW ER/A490874-14AD, REV ORIGINAL.
- [SDR DALA1107880137](https://openairdocs.org/sdr/DALA1107880137.md): Charger · inoperative · Jan 28, 2011 · N137DL · Boeing 767332 · Emergency Lighting
  > FOUND AT A CHECK EMERGENCY LIGHTS AFT ARE INOPERATIVE. MX REPLACED THE BATTERY CHARGER. SYS OPERATION IS NORMAL.
- [SDR DALA1030510137](https://openairdocs.org/sdr/DALA1030510137.md): Charger · inoperative · Nov 1, 2010 · N137DL · Boeing 767332 · Emergency Lighting
  > EMERGENCY LIGHTS ROWS 34 - 43 INOP. REPLACED BATTERY CHARGER PER AMM 33-50-00. OPS CHECK GOOD. (DL76S103008)
- [SDR DALA1102790137](https://openairdocs.org/sdr/DALA1102790137.md): Skin · damaged · Jan 15, 2010 · N137DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > FUSELAGE STA 522, S-11L, SKIN AND TEAR STRIP DAMAGE REPAIRED IAW ERA 479184-14.
- [SDR DL76S081242](https://openairdocs.org/sdr/DL76S081242.md): Line · leaking · Sep 27, 2008 · N137DL · Boeing 767332 · Crew Oxygen System
  > CREW OXYGEN PRESSURE DROPPED TO 10 PSI. FOUND BAD O2 LINE BEHIND F/O OXYGEN MASK CONTAINER. REPLACED LINE AND CREW O2 BOTTLE. LEAK CHECK GOOD.
- [SDR DALA1103290137](https://openairdocs.org/sdr/DALA1103290137.md): Link · damaged · Feb 21, 2008 · N137DL · Boeing 767332 · Trailing Edge Flap Control System
  > T/E FLAP 3-10 LINKS REPAIRED IAW EA 01-076248-12, ME07, ME08, ME09, ME10, ME11, ME12.
- [SDR DL76S080149](https://openairdocs.org/sdr/DL76S080149.md): Wire · damaged · Jan 1, 2008 · N137DL · Boeing 767332 · Light System Wiring
  > EMERGENCY LIGHT INOP AT SEAT 14F AND 10F. REPAIRED WIRES, OPS CK OK.
- [SDR DL76S071590](https://openairdocs.org/sdr/DL76S071590.md): Engine · failed · Dec 5, 2007 · N137DL · Boeing 767332 · Engine (Turbine/Turboprop)
  > ADVANCED THROTTLES ON T/O AND GOT A LOUD POP FROM RT ENGINE REMOVED AND REPLACED NR 2 ENG IAW TRANS 1T145.
- [SDR DL76S060946](https://openairdocs.org/sdr/DL76S060946.md): Skin · gouged · Nov 8, 2006 · N137DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT AND GOUGE AT S38R AT FS 368. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.
- [SDR DALA1102780137](https://openairdocs.org/sdr/DALA1102780137.md): Bulkhead · unknown · Oct 19, 2006 · N137DL · Boeing 767332 · Fuselage Main, Bulkhead
  > FUSELAGE NLG WHEEL WELL AFT BULKHEAD STA 287, LBL 25 CHORD, WL 173. REPAIRED IAW ERA 458240-14AD.
- [SDR DL76S050794](https://openairdocs.org/sdr/DL76S050794.md): Packing · leaking · Dec 16, 2005 · N137DL · Boeing 767332 · Turbine Engine Oil System
  > RIGHT ENGINE LOST OIL QTY IN FLIGHT. REPLACED STARTER SHAFT PACKING.
- [SDR DL76S040471](https://openairdocs.org/sdr/DL76S040471.md): Wire · shorted · May 27, 2004 · N137DL · Boeing 767332 · Light System Wiring
  > RED EMERGENCY LIGHTS AT 25AB INOP. FOUND WIRING SHORTED AT PAX SEAT 25AB BETWEEN LWR SIDEWALL PANEL AND SEAT TRACK. REPLACED BLOWN FUSES IN M9009 AND M9010 ESCAPE PATH PWR SUPPLIES. REINSTALLED ALL LWR KICK PNLS. EMERGENCY LIGHTS ESCAPE PATH SYS OP CHECKS
- [SDR DL76S021404](https://openairdocs.org/sdr/DL76S021404.md): Controller · malfunctioned · Dec 3, 2002 · N137DL · Boeing 767332 · Trailing Edge Flap Control System
  > ON APPROACH IN ATL, FLAPS WOULD NOT EXTEND PAST 25 WITH 30 SELECTED. FLAPS WOULD NOT RETRACT ON GO AROUND. LANDED WITH FLAPS AT 20 PER NON-NORMAL PROCEDURE. BITE OF FSEU PER FIM HAD NO FAULTS, RAN AND INSPECTED FLAPS SEVERAL CYCLES WITH NO STATUS MESSAGES O
- [SDR DL76S021130](https://openairdocs.org/sdr/DL76S021130.md): Spar · cracked · Sep 23, 2002 · N137DL · Boeing 767332 · Nacelle/Pylon, Frame/Spar/Rib
  > PYLON NR 1 ENGINE FWD UPPER SPAR WEB CRACKED, REPAIRED THE FWD UPPER SPAR WEB. THE CUTOUT SIZE WAS ENLARGER TO REMOVE THE CRACK AND EXISING NUTPLATE LOCATIONS AT THE CUTOUT CORNERS. THE AREA WAS MODIFIED PER THE REQUIREMENTS OF BAC S/B 767-54-0090 AND DOCUM
- [SDR DL76S020556](https://openairdocs.org/sdr/DL76S020556.md): Cable · shorted · May 16, 2002 · N137DL · Boeing 767332 · Electrical Power System
  > APU GENERATOR FEEDER CABLE SHORTED ABOVE WATER TANK @STA 16 00. ARCHING AND SOME HEAT DAMAGE TO AREA. CA RPLD FEEDER CABLE AND PERFORMED C/W EO 1-74974-3 REV B / FEEDER CABLE MODIFICATION. REPAIRED DAMAGED FEEDER CABLE STANDOFF BRACKET AT
- [SDR DL76S020434](https://openairdocs.org/sdr/DL76S020434.md): Flap · malfunctioned · Apr 13, 2002 · N137DL · Boeing 767332 · Trailing Edge Flap Control System
  > ON APPROACH TRAILING EDGE FLAP DISAGREE EICAS WITH T/E FLAP. SHUT DOWN STATUS MSG LANDED WITH FLAPS AT 23 DEG. T/S PER FIM 27-51-00 FIG 114B. SYS TEST NORMAL. MSG CLEARED, NO FAULTS.
- [SDR DL76S011947](https://openairdocs.org/sdr/DL76S011947.md): Floorbeam · cracked · Dec 15, 2001 · N137DL · Boeing 767332 · Fuselage Main, Floor Beam
  > THE WEB AND LOCAL REINFORCING DOUBLER OF THE LBL 24 LONGITUDINAL FLOORBEAM WAS FOUND CRACKED NEAR AT FS 680. THE CRACKED REINFORCING DOUBLER WAS REMOVED AND WEB CRACK TRIMMED OUT. A NEW REINFORCING DOUBLER WAS INSTALLED AND AN ALUMINUM REPAIR DOUBLER. THE UP
- [SDR DL76S011695](https://openairdocs.org/sdr/DL76S011695.md): Socket · defective · Oct 20, 2001 · N137DL · Boeing 767332 · Emergency Lighting
  > SLIDE EMERGENCY LIGHT INOP LEFT AFT CABIN DOOR EXTERIOR. REPLACED POWER SUPPLY, NO HELP. REPLACED SOCKET ASSY, OPS CHECKS OK.
- [SDR DL76S000355](https://openairdocs.org/sdr/DL76S000355.md): Light · inoperative · Feb 21, 2000 · N137DL · Boeing 767332 · Emergency Lighting
  > EMERGENCY SEAT TRACK LIGHTS INOP MID AFT LEFT AND AFT RIGHT SECTIONS. REPLACED POWER SUPPLY.
- [SDR DL76S992685](https://openairdocs.org/sdr/DL76S992685.md): Lamp · failed · Dec 9, 1999 · N137DL · Boeing 767332 · Door Warning System
  > LEFT AFT DOOR ARMED LIGHT ON LT FWD ATTND PANEL FAILED TO TEST. RELAMPED, OPS CKS GOOD.
- [SDR DL76S990785](https://openairdocs.org/sdr/DL76S990785.md): Fitting · leaking · Apr 10, 1999 · N137DL · Boeing 767332 · Engine Fuel Distribution
  > AT TOP OF DESCENT, NR 1 ENGINE ROLLED BACK AND OIL PRESSURE STARTED TO DECAY WITH N1 AND N2 STILL INDICATING DOUBLE DIGITS. REPLACED T-BONE FITTING AT 10 O'CLOCK POSITION.
- [SDR DL76S981380](https://openairdocs.org/sdr/DL76S981380.md): Skin · gouged · Jul 1, 1998 · N137DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > FUSELAGE/SKIN, BULK CARGO DOOR SURROUND FS 146. REPAIR FOR EDGED GOUGES. THE FUSELAGE SKIN AND UNDERLYING BEAR STRAP AT THE FWD EDGE OF THE BULK CARGO DOOR OPENING WAS DAMAGED BY GROUND EQUIP. THE DAMAGED AREAS WERE TRIMMED OUT FROM THE EDGE AND REPAIRED WI
- [SDR DL76S981053](https://openairdocs.org/sdr/DL76S981053.md): Skin · delaminated · May 18, 1998 · N137DL · Boeing 767332 · Leading Edge Devices
  > NR 1 L/E SLAT T/E WEDGE WAS FOUND TO HAVE THE UPPERR SKIN DAMAGED AT A LOCATIONS WHICH IS APPROX 24 INCHES FROM THE OUTBD EDGE AND RUNS APPROX 2 INCHES FWD FROM THE AFT EDGE. REPAIRED PER ERA 364811-14AD.
- [SDR DL76S962294](https://openairdocs.org/sdr/DL76S962294.md): Mount · loose · Oct 10, 1996 · N137DL · Boeing 767332 · Engine Mount Section
  > DURING LETTER CHECK NR 34 WRITTEN, GAP BETWEEN FWD ENG MOUNT AND AND PYLON. REMOVED ENG PER 1T147, INSPECTED ON NR 34 AND NO DAMAGE FOUND TO MOUNTS. REPLACED ALL MOUNT NUTS, REINSTALLED SAME ENG.
- [SDR DL76S950548](https://openairdocs.org/sdr/DL76S950548.md): Skin · lightning strike · Feb 7, 1995 · N137DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > DURING LETTER CHECK INSP, FOUND 10 LIGHTNING STRIKES ON A/C BELLY (STARTING JUST AFT OF NOSE GEAR TO SECOND BODY DRAIN AFT OF E AND E COMPT AT 6 O'CLOCK POS) FUSELAGE SKIN BLENDED DAMAGE PER SRM 53-00-01, DYE CHECK OK. TREATED AREAS W/ALODINE.
- [SDR DL76S950547](https://openairdocs.org/sdr/DL76S950547.md): Skin · lightning strike · Feb 7, 1995 · N137DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > FOUND DURING LETTER CHECK INSP, LIGHTNING STRIKE FOREWARD OF RIGHT LOWER PITOT TUBE ON FUSE SKIN BLENDED DAMAGE PER SRM 53-00-01 DYE CHK OK, TREATED AREA AND REPAINTED.
- [SDR DL76S950546](https://openairdocs.org/sdr/DL76S950546.md): Aileron · lightning strike · Feb 7, 1995 · N137DL · Boeing 767332 · Ailerons
  > DURING LETTER CHECK INSP, FOUND L/WING ODBD AILERON EVIDENCE OF LIGHTNING STRIKE INSTALLED PERMANENT REPAIR AS PER SRM 57-60-02 FIG 201, BALANCE NOT CHANGED REF 51-60-01, PAINTED REPAIR ON LEFT AILERON.

## 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 = 'N137DL' AND deregistration_id = 'N137DL-2018-07-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N137DL-2018-07-12/reports

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