# Service difficulty reports: N138DL, cancelled Jan 9, 2019

A list on [N138DL, cancelled Jan 9, 2019](https://openairdocs.org/deregistered/N138DL-2019-01-09.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 · 78 reports

- [SDR DALA2016011400446](https://openairdocs.org/sdr/DALA2016011400446.md): Wire Harness · disconnected · Jan 13, 2016 · N138DL · Boeing 767332 · Light System Wiring
  > EMERGENCY LIGHTS AT 31FG ARE INOPERATIVE. MAINTENANCE RECONNECTED SEAT HARNESS TO LIGHT FIXTURE. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2015102006352](https://openairdocs.org/sdr/DALA2015102006352.md): Fuse · blown · Oct 16, 2015 · N138DL · Boeing 767332 · Emergency Lighting
  > EMERGENCY LIGHTS FROM ROW 12 TO CENTER LAVS ARE INOPERATIVE ON BOTH SIDES. MAINTENANCE POWER PACK WITH BLOWN FUSE, FOUND SHORT TO GROUND AT SEAT 15 LEFT AND REPINNED PLUG AT SEAT 16 LEFT. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2015102006351](https://openairdocs.org/sdr/DALA2015102006351.md): Connector · damaged · Oct 16, 2015 · N138DL · Boeing 767332 · Light System Wiring
  > EMERGENCY LIGHT AT SEAT 30 RT SIDE ARE INOPERATIVE. MAINTENANCE FOUND PIN PULLED OUT OF PLUG AND REPINNED. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2015080404795](https://openairdocs.org/sdr/DALA2015080404795.md): Receiver · odor · Jul 29, 2015 · N138DL · Boeing 767332 · Automatic Direction Finder (ADF) System
  > PERFORMED AN AIR TURNBACK DUE TO AN ELECTRICAL BURNING ODOR THROUGHOUT THE ACFT. FOUND CIRCUIT BREAKER POSITION F6, LEFT ADF, WAS TRIPPED. VERIFIED THE ADF RECEIVER AS THE CAUSE. REPLACED THE LT ADF RECEIVER IAW AMM 34-57. INSPECTED ACFT CARGO BIN AND E/E
- [SDR DALA2014112606359](https://openairdocs.org/sdr/DALA2014112606359.md): Support Beam · cracked · Nov 25, 2014 · N138DL · Boeing 767332 · Wing Miscellaneous Structure
  > MAIN OTBD SUPPORT BEAM, INBD SIDE AT NR 2 JOINT, 2 EA.3750 SIZE FASTENERS AND 1 FASTENER ON OTBD SIDE AT NR 2 JOINT, SHOW CRACK. C/W ERA 530731-14.
- [SDR DALA2014112606358](https://openairdocs.org/sdr/DALA2014112606358.md): Beam · cracked · Nov 25, 2014 · N138DL · Boeing 767332 · Wing Main, Frame Structure
  > BEAM CRACKED, OTBD SIDE AT LWR FASTENER AFT OF STUD FITTING. CRACKED IN BEAM ONLY. NR 7 FLAP SUPPORT. C/W ERA 530729-14.
- [SDR DALA2014111906251](https://openairdocs.org/sdr/DALA2014111906251.md): Frame · cracked · Nov 18, 2014 · N138DL · Boeing 767332 · Fuselage Main, Frame
  > FRAME CRACKED AT BS 859.5 ON RT SIDE BELOW WL 200. REPAIRED ON WC 5311-01-01195-09.
- [SDR DALA2014062803914](https://openairdocs.org/sdr/DALA2014062803914.md): Oxygen Mask · inoperative · Jun 26, 2014 · N138DL · Boeing 767332 · Passenger Oxygen System
  > DURING AN EMERGENCY DESCENT, DUE TO PRESSURIZATION FAILURE, OXYGEN MASKS AT SEAT 34CDF DID NOT DROP. INSPECTED PSU AND MASK LATCH ASSEMBLY AND VERIFIED DEPLOYMENT DURING MANUAL DEPLOYMENT, AND REPACKED MASKS.
- [SDR DALA13071690138](https://openairdocs.org/sdr/DALA13071690138.md): Bulb · broken · Dec 20, 2013 · N138DL · Boeing 767332 · Emergency Lighting
  > LT SIDE OF FUSELAGE, TWO EMERGENCY EXIT EXTERIOR LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND BROKEN BULB AND DAMAGED HARDWARE AND REPLACED. SYSTEM OPERATION IS NORMAL.
- [SDR DALA13061600138](https://openairdocs.org/sdr/DALA13061600138.md): Connector · damaged · Nov 10, 2013 · N138DL · Boeing 767332 · Light System Wiring
  > EMERGENCY LIGHTS AT ROW 14AB IS INOPERATIVE. MAINTENANCE REPAIRED CONNECTOR. SYSTEM OPS NORMAL. (LP 1182487)
- [SDR DALA13061590138](https://openairdocs.org/sdr/DALA13061590138.md): Wire · broken · Nov 9, 2013 · N138DL · Boeing 767332 · Light System Wiring
  > EMERGENY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE. SYSTEM OPERATION IS NORMAL. (LP 1182485)
- [SDR DALA1257210138](https://openairdocs.org/sdr/DALA1257210138.md): Battery Pack · inoperative · Dec 13, 2012 · N138DL · Boeing 767332 · Emergency Lighting
  > EMERGENCY LIGHTS ROW 35 AND AFT ARE INOPERATIVE. MX REPLACED THE BATTERY PACK AND CHARGER. SYS OPERATION IS NORMAL.
- [SDR DALA1247240138](https://openairdocs.org/sdr/DALA1247240138.md): Battery Pack · inoperative · Aug 25, 2012 · N138DL · Boeing 767332 · Emergency Lighting
  > EMERGENCY LIGHTS AT 35A-F TO 46A-F ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER M9010 PER AMM. SYSTEM OPERATION IS NORMAL.
- [SDR DALA1246740138](https://openairdocs.org/sdr/DALA1246740138.md): Charger · inoperative · Aug 19, 2012 · N138DL · Boeing 767332 · Emergency Lighting
  > EMERGENCY LIGHTS FROM ROW 35-47 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND BATTERY CHARGER M9010. SYSTEM OPERATION IS NORMAL.
- [SDR DALA1240800138](https://openairdocs.org/sdr/DALA1240800138.md): Battery Pack · inoperative · Jul 6, 2012 · N138DL · Boeing 767332 · Emergency Lighting
  > FOUND DURING A CHECK EMERGENCY EXIT PATHWAY LIGHTS ROW 35 AFT ARE INOPERATIVE. THE BATTERY PACK REPLACED. SYSTEM OPERATION IS NORMAL.
- [SDR DALA1235470138](https://openairdocs.org/sdr/DALA1235470138.md): Charger · inoperative · Jun 3, 2012 · N138DL · Boeing 767332 · Emergency Lighting
  > EMERGENCY PATCH LIGHTING ROW 35 ON INOPERATIVE. REPLACED BATTERY CHARGER ASSY M9010 PER 767 AMM 33. OPS CHECK NORMAL OK FOR SERVICE.
- [SDR DALA1234140138](https://openairdocs.org/sdr/DALA1234140138.md): Battery Pack · inoperative · May 26, 2012 · N138DL · Boeing 767332 · Emergency Lighting
  > ALL EMERGENCY LIGHT FROM ROW 35 AFT INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51.
- [SDR DALA1156700138](https://openairdocs.org/sdr/DALA1156700138.md): Door · deformed · Oct 4, 2011 · N138DL · Boeing 767332 · Landing Gear Doors
  > RIGHT MLG TRUNNION DOOR LWR EDGE DEFORMED. REPAIRED PER ERA 496335-14.
- [SDR DALA1156690138](https://openairdocs.org/sdr/DALA1156690138.md): Skin · dented · Oct 4, 2011 · N138DL · Boeing 767332 · Trailing Edge Flaps
  > INBOARD AFT FLAP LWR SURFACE DENTED. METAL HOT BOND REPAIR C/W PER B767-300 SRM 57-53-01, REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 201.
- [SDR DALA1156100138](https://openairdocs.org/sdr/DALA1156100138.md): Fitting · damaged · Sep 27, 2011 · N138DL · Boeing 767332 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON MIDSPAR BH FITTING HAS 10 EACH OVERSIZED FASTENERS. REPAIRED PER ERA 496325-14AD REV ORIG.
- [SDR DALA1156090138](https://openairdocs.org/sdr/DALA1156090138.md): Fitting · damaged · Sep 27, 2011 · N138DL · Boeing 767332 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON MIDSPAR BH FITTING HAS 10 EACH OVERSIZED FASTENERS. REPAIRED PER ERA 496325-14AD REV ORIG.
- [SDR DALA1156080138](https://openairdocs.org/sdr/DALA1156080138.md): Fitting · misrepaired · Sep 27, 2011 · N138DL · Boeing 767332 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON UPPER PITCH LOAD FITTING "T" CLIP HAS HOLE WITH SHORT EDGE DISTANCE. C/W REPAIR PER ERA 496333-14AD REV ORIG.
- [SDR DALA1156070138](https://openairdocs.org/sdr/DALA1156070138.md): Fitting · misrepaired · Sep 27, 2011 · N138DL · Boeing 767332 · Nacelle/Pylon Miscellaneous Structure
  > LT UPPER PITCH LOAD FITTING "T" CLIP HAS SHORT EDGE DISTANCE AT FASTENER HOLE FOR NR 1 PYLON. REPAIR PER ERA 496333-14AD.
- [SDR DALA1155580138](https://openairdocs.org/sdr/DALA1155580138.md): Panel · debonded · Sep 27, 2011 · N138DL · Boeing 767332 · Trailing Edge Flaps
  > RT WING O/B FLAP UPPER PANEL 666KT IS DISBONDED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 201.
- [SDR DALA1156110138](https://openairdocs.org/sdr/DALA1156110138.md): Frame · corroded · Sep 26, 2011 · N138DL · Boeing 767332 · Fuselage Main, Frame
  > FWD C/C FS 654+121 LBL 38 FRAME UPPER CHORD IS CORRODED BEYOND LIMITS. CHORD REPLACED PER B767-300 SRM 51-10-02 AND INSTALLED PER B767-300 SRM 51-40-02.
- [SDR DALA1155570138](https://openairdocs.org/sdr/DALA1155570138.md): Wedge · dented · Sep 26, 2011 · N138DL · Boeing 767332 · Trailing Edge Flaps
  > RT WING I/B T/E AFT FLAP T/E WEDGE IS DENTED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 201.
- [SDR DALA1155560138](https://openairdocs.org/sdr/DALA1155560138.md): Fairing · delaminated · Sep 26, 2011 · N138DL · Boeing 767332 · Trailing Edge Flaps
  > LT WING I/B MAIN FLAP O/B L/E FAIRING IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 PAR 5A (1).
- [SDR DALA1155550138](https://openairdocs.org/sdr/DALA1155550138.md): Flap · delaminated · Sep 26, 2011 · N138DL · Boeing 767332 · Trailing Edge Flaps
  > LT WING O/B FLAP L/E AREA IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND 51-70-05 PAR 5A (1).
- [SDR DALA1155540138](https://openairdocs.org/sdr/DALA1155540138.md): Frame · corroded · Sep 26, 2011 · N138DL · Boeing 767332 · Fuselage Main, Frame
  > FWD C/C FS 654+121 LBL 38 FRAME UPPER CHORD IS CORRODED BEYOND LIMITS.
- [SDR DALA1155340138](https://openairdocs.org/sdr/DALA1155340138.md): Spar · misrepaired · Sep 26, 2011 · N138DL · Boeing 767332 · Nacelle/Pylon, Frame/Spar/Rib
  > NR 2 PYLON FWD UPPER SPAR WEB FASTENER PATTERN DOES NOT MATCH SB 767-54-0090 REV 2 FIG 10. SPAR WEB REPAIRED PER ERA 496330-14 REV ORIG.
- [SDR DALA1155330138](https://openairdocs.org/sdr/DALA1155330138.md): Spar · misrepaired · Sep 26, 2011 · N138DL · Boeing 767332 · Nacelle/Pylon, Frame/Spar/Rib
  > NR 1 PYLON FWD UPPER SPAR WEB FASTENER PATTERN DOES NOT MATCH SB 767-54-0090 REV 2 FIG 10. SPAR WEB REPAIRED PER ERA 496329-14 REV ORIG.
- [SDR DALA1156130138](https://openairdocs.org/sdr/DALA1156130138.md): Floorbeam · corroded · Sep 22, 2011 · N138DL · Boeing 767332 · Fuselage Main, Floor Beam
  > FS 1219 FLOOR FRAME UPPER CHORD IS CORRODED AT LBL 22.5 BEYOND SRM LIMITS. FLOORBEAM UPPER CHORD REPLACED IAW B767-300 SRM 51-10-02 AND INSTALLED IAW B767-300 SRM 51-40-02.
- [SDR DALA1156120138](https://openairdocs.org/sdr/DALA1156120138.md): Floorbeam · corroded · Sep 22, 2011 · N138DL · Boeing 767332 · Fuselage Main, Floor Beam
  > FS 1197+66 FLOOR FRAME UPPER SURFACE CORRODED AT RBL 42 BEYOND LIMITS OF SRM. FLOORBEAM UPPER CHORD REPLACED PER B767-300 N SRM 51-10-02 AND INSTALLED PER B767-300 SRM 51-40-02.
- [SDR DALA1154960138](https://openairdocs.org/sdr/DALA1154960138.md): Floorbeam · corroded · Sep 22, 2011 · N138DL · Boeing 767332 · Fuselage Main, Floor Beam
  > FS 1219 FLOOR FRAME UPPER CHORD IS CORRODED AT BL L22.5 BEYOND SRM LIMITS.
- [SDR DALA1154950138](https://openairdocs.org/sdr/DALA1154950138.md): Floorbeam · corroded · Sep 22, 2011 · N138DL · Boeing 767332 · Fuselage Main, Floor Beam
  > FS 1197 +66 FLOOR FRAME UPPER SURFACE IS CORRODED AT RBL 42 BEYOND LIMITS OF SRM.
- [SDR DALA1157520138](https://openairdocs.org/sdr/DALA1157520138.md): Frame · cracked · Sep 12, 2011 · N138DL · Boeing 767332 · Fuselage Main, Frame
  > CABIN RT STA 883 BETWEEN STR 20R AND STR 21R FRAME INNER CHORD CRACK. REPAIR ACCOMPLISHED AS PER ERA 491126-14AD REV 0.
- [SDR DALA1139990138](https://openairdocs.org/sdr/DALA1139990138.md): Relay · malfunctioned · Jun 17, 2011 · N138DL · Boeing 767332 · Passenger Compartment Lighting
  > THE FLIGHT CREW REPORTED THAT SPARKS AND SMOKE WERE COMING FROM THE 2R SLIDE LIGHT. MAINTENANCE REMOVED AND REPLACED THE RELAY BEHIND THE 2R FLIGHT ATTENDANT LIGHTING CONTROL PANEL. ALL CHECKS WELL PER AMM.
- [SDR DALA1140780138](https://openairdocs.org/sdr/DALA1140780138.md): Stringer · damaged · Apr 12, 2011 · N138DL · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER LBL & RBL 85.9, FS 966. REPAIRED IAW ERA 481423-14.
- [SDR DALA1140770138](https://openairdocs.org/sdr/DALA1140770138.md): Skin · damaged · Jan 26, 2011 · N138DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN STA 140-152, STR 24R-27R LIGHTNING DAMAGE. REPAIRED IAW ERA 479493-14.
- [SDR DL76S100931](https://openairdocs.org/sdr/DL76S100931.md): Failsafe · corroded · Apr 7, 2010 · N138DL · Boeing 767332 · Fuselage Main, Structure
  > A CRACK INDICATION WAS FOUND ON THE RT FAIL SAFE STRAP REF ERA 481422-14AD.
- [SDR DL76S100930](https://openairdocs.org/sdr/DL76S100930.md): Failsafe · corroded · Apr 7, 2010 · N138DL · Boeing 767332 · Fuselage Main, Structure
  > A CRACK INDICATION WAS FOUND AT LWR BOLT HOLE FAIL SAFE STRAP INSP REF ERA 481421-14AD.
- [SDR DL76S091966](https://openairdocs.org/sdr/DL76S091966.md): Slide · open · Dec 12, 2009 · N138DL · Boeing 767332 · Escape Slide
  > R1 DOOR SLIDE WOULD NOT ARM AT DEPARTURE TIME. FOUND SLIDE PACK PARTIALLY OPEN. REPLD R1 SLIDE PACK IAW AMM. OPS CKS NML.
- [SDR DALA1140760138](https://openairdocs.org/sdr/DALA1140760138.md): Door · damaged · Nov 4, 2009 · N138DL · Boeing 767332 · Cargo/Baggage Doors
  > AFT CARGO DOOR LOWER AFT CORNER DAMAGE. REPAIRED IAW ERA 477986-14.
- [SDR DL76S091635](https://openairdocs.org/sdr/DL76S091635.md): Module · missing · Oct 14, 2009 · N138DL · Boeing 767332 · Passenger Oxygen System
  > DURING EA 01-477420-12 AD REV ORIG MEO1 FOUND ENTIRE O2/MASK MODULE MISSING OVER SEAT 12AB. INST O2 MASK/GEN MODULE ASSY AT 12AB
- [SDR DL76S091021](https://openairdocs.org/sdr/DL76S091021.md): Circuit Card · inoperative · Jun 11, 2009 · N138DL · Boeing 767332 · Flight Control System Wiring
  > ON TAKEOFF ROLL EXACTLY THE SAME THING HAPPENED AS PREVIOUS WRITE-UP. BRAKE TEMP NEVER ABOVE 2. PERFORMED FIM AND MM TESTS OF STAB TRIM INDICATION SYSTEM. FOUND CENTER FSPM CARD WOULD NOT TEST. REPLACED CTR FSPM CARD. STAB RATE ISOLATES L AND C POSI
- [SDR DL76S091018](https://openairdocs.org/sdr/DL76S091018.md): Sensor · malfunctioned · Jun 11, 2009 · N138DL · Boeing 767332 · Stabilizer Control System
  > UNSCHEDULED STAB TRIM DURING TAKEOFF AT APPROX 75 KTS. RTO, TS PER FIM 27-09-00 FIG 106A. CHECKED SAMS CHECKED FSPMS ALL CHK NORM. PERFORMED STAB TRIM CHKS FROM YOKE AND PEDESTAL PER FIM. ALL NORM. INSPECTED STAB POS XMITTER CABLES ALL PULLEYS AND CABLES
- [SDR DL76S091017](https://openairdocs.org/sdr/DL76S091017.md): Sensor · malfunctioned · Jun 11, 2009 · N138DL · Boeing 767332 · Stabilizer Control System
  > REJECTED TAKEOFF FOR UNSCHEDULED TRIM EICAS MSG. PERFORMED FIM AND MM TESTS OF STAB TRIM INDICATION SYSTEM. FOUND CENTER FSPM CARD WOULD NOT TEST. REPLACED CTR FSPM CA STAB RATE ISOLATES L AND C POSITION SENSORS. REPLACED R STA TRIM POSITION SENSOR. ALL P
- [SDR DL76S080838](https://openairdocs.org/sdr/DL76S080838.md): Trim System · malfunctioned · Jun 7, 2008 · N138DL · Boeing 767332 · Stabilizer Control System
  > UNSCHEDULED STAB TRIM 3X DURING T/O ROLL. RTO AND RTN GATE. NO HIST, T/S PER FIM 27-09-00 FIG 106A. SAMS AND FSPM BITE CHK GOOD. RAN STAB FROM BOTH COLUMNS AND CTR PEDESTAL FULL TRAVEL NO EICAS MSGS. ALL CHKS OK. A/C OK FOR SERVICE.
- [SDR DALA1140800138](https://openairdocs.org/sdr/DALA1140800138.md): Link · damaged · Apr 3, 2008 · N138DL · Boeing 767332 · Trailing Edge Flap Control System
  > TRAILING EDGE FLAP 3-10 LINKS. REPAIRED IAW EA 01-076248-12, ME07, ME08, ME09, ME10, ME11, ME12.
- [SDR DL76S080046](https://openairdocs.org/sdr/DL76S080046.md): Skin · damaged · Jan 9, 2008 · N138DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH LIGHTNING STRIKE DAMAGE AT STA 196.5 BETWEEN S-21L AND S-24L. THE DAMAGED SKIN WAS CUTOUT AND A REPAIR DOUBLER WAS INSTALLED.

Next page: https://openairdocs.org/deregistered/N138DL-2019-01-09/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 = 'N138DL' AND deregistration_id = 'N138DL-2019-01-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N138DL-2019-01-09/reports

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