# Service difficulty reports: Boeing 767-238

A list on [Boeing 767-238](https://openairdocs.org/model/boeing-767-238.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 109 reports

- [SDR ABXA20260615260](https://openairdocs.org/sdr/ABXA20260615260.md): Spar · cracked · Jun 15, 2026 · N1499A · Boeing 767238 · Nacelle/Pylon, Frame/Spar/Rib
  > DURING C5 CHECK IN TAMPA WHILE PREPARING TO ACOMPLISH THE SIP MOD ON LT PYLON A CRACK WAS FOUND IN THE AFT MIDSPAR WEB.INBOARD SIDE. MTX REMOVED AND REPLACED NR 1 PYLON MIDSPAR WEB, INBD SIDE IAW ABX-REA-5440-65835-00 AND SRM-51-40-02. AND RETURNED A/C TO SE
- [SDR 2DYA202010105001](https://openairdocs.org/sdr/2DYA202010105001.md): Power Lever · stuck · Jan 6, 2021 · N602KW · Boeing 767238 · Power Lever
  > AT FL39,000 DURING CRUISE, LEFT THRUST LEVER WAS NOT RESPONDING AND EPR WAS STUCK AT 1.00. HAD TO DECENT TO FL36000 TO MAINTAIN AIRSPEED. EGT WAS BEING ERRATIC PRIOR TO THAT + OR MINUS 30 DEGREES. WE WILL FILE A SUPPLEMENTAL REPORT WHEN MORE INFORMATION IS
- [SDR 2DYA202010106001](https://openairdocs.org/sdr/2DYA202010106001.md): Idg · underserviced · Jan 5, 2021 · N602KW · Boeing 767238 · AC Generator-Alternator
  > RIGHT GEN DRIVE EICAS MESSAGE AFTER TAKE-OFF, DRIVE DISC LIGHT CAME ON. CREW CALLED DISPATCH REPORTING RT IDG DRIVE/GEN. OFF EICAS MESSAGE, CREW FOLLOWED FCOM AND DECIDED TO RETURN FIELD (JFK). MOC CALLED JFK MX AND THEY WILL MEET THE AIRCRAFT UPON LANDING.
- [SDR 2DYA20201015001](https://openairdocs.org/sdr/2DYA20201015001.md): Unknown · inoperative · Oct 15, 2020 · N602KW · Boeing 767238 · Emergency Lighting
  > FAA PERFORMED AN INSPECTION ON THE AIRCRAFT 602 FOR A SERIES OF EMERGENCY EXTERIOR LIGHTS. THEY'RE AS FOLLOWS FOR SEATS 13 C-A/HK EMERGENCY EXIT INTEGRATED LIGHTS INOPERABLE. LEFT OVERWING EXTERIOR EMERGENCY LIGHTS C3J INOPERABLE. R-3 AFT EMERGENCY EXTERIOR
- [SDR 2DYA2020082005](https://openairdocs.org/sdr/2DYA2020082005.md): Engine · overtemp · Aug 25, 2020 · N602KW · Boeing 767238 · Engine (Turbine/Turboprop)
  > PASSENGER FLIGHT EN ROUTE FROM GEO TO JFK WAS AT TOP OF DECENT, AT FL380 TIME APPROXIMATE 0027Z. THE LT GENERATOR WENT OFF LINE AND THE APU GENERATOR PICKED UP THE ELECTRICAL LOAD. N1, N2, AND N3 WAS REDUCED WITH COMMAND THROTTLE REDUCED AND EGT BEGAN TO RIS
- [SDR 2DYA20200828005](https://openairdocs.org/sdr/2DYA20200828005.md): Generator · disengaged · Aug 25, 2020 · N602KW · Boeing 767238 · AC Generator-Alternator
  > PASSENGER FLIGHT EN ROUTE FROM GEO TO JFK WAS AT TOP OF DECENT (AT FL380 TIME APPROXIMATE 0027Z). THE LT GENERATOR WENT OFF LINE AND THE APU GENERATOR PICKED UP THE ELECTRICAL LOAD. N1, N2 AND N3 WAS REDUCED WITH COMMANDED THROTTLE REDUCTION AND EGT BEGAN TO
- [SDR 2DYA2020072018002](https://openairdocs.org/sdr/2DYA2020072018002.md): Battery Pack · inoperative · Jul 18, 2020 · N702KW · Boeing 767238 · Emergency Lighting
  > ON VISUAL INSPECTION, THE L2, AND R2 DOOR EMERGENCY LIGHTS WERE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT THE R2 DOOR IAW AMM 33-51-07. OPS CHECKED GOOD IAW AMM 33-51-07.
- [SDR 2DYA20200323002](https://openairdocs.org/sdr/2DYA20200323002.md): Battery Pack · discharged · Mar 12, 2020 · N602KW · Boeing 767238 · Emergency Lighting
  > DURING HEAVY MAINTENANCE CHECK FOUND EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED THE BATTERY PACK PER B767 AMM 33-51-07. PERFORMED OPERATIONAL CHECK. NO DISCREPANCIES FOUND. VERIFIED SATISFACTORY.
- [SDR 2DYA20200323001](https://openairdocs.org/sdr/2DYA20200323001.md): Battery Pack · discharged · Mar 12, 2020 · N602KW · Boeing 767238 · Emergency Lighting
  > DURING HEAVY MAINTENANCE CHECK FOUND EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED THE BATTERY PACK PER B767 AMM 33-51-07. PERFORMED OPERATIONAL CHECK. NO DISCREPANCIES FOUND. VERIFIED SATISFACTORY.
- [SDR 2DYA20200106001](https://openairdocs.org/sdr/2DYA20200106001.md): Battery Pack · failed · Dec 11, 2019 · N602KW · Boeing 767238 · Emergency Lighting
  > EMERGENCY LIGHT FOUND INOP DURING OPS CHECK OF L/H OVERWING SLIDE SYSTEM. REMOVED AND REPLACED L/H OVERWING SLIDE BATTERY PACK IAW B767 AMM 33-51-07. OPS CHECK NORMAL. NOTE: AIRCRAFT WAS IN MAINTENANCE CHECK AT THE TIME THE ISSUE WAS FOUND. FAA PMI HAS BE
- [SDR 2DYA2019040438001](https://openairdocs.org/sdr/2DYA2019040438001.md): Engine · power loss · Mar 8, 2019 · N602KW · Boeing 767238 · Engine (Turbine/Turboprop)
  > ON DESCENT L/H ENGINE LOST PNEUMATIC PRESSURE AFTER THAT ENGINE FAILURE TO ACCELERATE. FOUND FUEL CONTROL APPROACH SOLENOID FAULTY, ACCOMPLISH TEST OF THE PNEUMATIC HIGH PRESSURE CONTROL FOUND OK, ACCOMPLISHED FULL GAS PATH BORESCOPE FOUND NO INTERNAL DAMAGE
- [SDR ABXR2019010800011](https://openairdocs.org/sdr/ABXR2019010800011.md): Structure · cracked · Jan 8, 2019 · N673BF · Boeing 767238 · Fuselage Miscellaneous Structure
  > UPPER CHORD ON FLOOR SUPPORT INTERCOSTAL CRACKED.
- [SDR ABXR2019010800010](https://openairdocs.org/sdr/ABXR2019010800010.md): Attach Angle · corroded · Jan 8, 2019 · N673BF · Boeing 767238 · Wing, Attach Fittings
  > RW LOWER RIB ATTACH ANGLE ON WING TRAILING EDGE IS CORRODED.
- [SDR ABXR2019010800009](https://openairdocs.org/sdr/ABXR2019010800009.md): Structure · corroded · Jan 8, 2019 · N673BF · Boeing 767238 · Wing Miscellaneous Structure
  > LW UPPER CHORD CORRODED AT TRAILING EDGE.
- [SDR ABXR2019010800008](https://openairdocs.org/sdr/ABXR2019010800008.md): Panel Support · corroded · Jan 8, 2019 · N673BF · Boeing 767238 · Wing Miscellaneous Structure
  > LW TRAILING EDGE PANEL SUPPORT CORRODED.
- [SDR ABXR2019010800007](https://openairdocs.org/sdr/ABXR2019010800007.md): Skin Panel · corroded · Jan 8, 2019 · N673BF · Boeing 767238 · Wing, Plate/Skin
  > LW UPPER SKIN CORRODED.
- [SDR ABXR2019010800006](https://openairdocs.org/sdr/ABXR2019010800006.md): Skin Panel · corroded · Jan 8, 2019 · N673BF · Boeing 767238 · Wing, Plate/Skin
  > LW UPPER SKIN PANEL CORRODED.
- [SDR ABXR2019010800005](https://openairdocs.org/sdr/ABXR2019010800005.md): Longeron Splice · corroded · Jan 8, 2019 · N673BF · Boeing 767238 · Fuselage Main, Longeron/Stringer
  > FUSELAGE EXTERNAL LONGERON SPLICE FITTING CORRODED.
- [SDR ABXR2019010800004](https://openairdocs.org/sdr/ABXR2019010800004.md): Skin Panel · corroded · Jan 8, 2019 · N673BF · Boeing 767238 · Wing, Plate/Skin
  > LW UPPER SKIN PANEL CORRODED.
- [SDR ABXR2019010800003](https://openairdocs.org/sdr/ABXR2019010800003.md): Rib · corroded · Jan 8, 2019 · N673BF · Boeing 767238 · Wing, Rib/Bulkhead
  > LW AIRLOAD RIB CORRODED.
- [SDR ABXR2019010800002](https://openairdocs.org/sdr/ABXR2019010800002.md): Skin Panel · corroded · Jan 8, 2019 · N673BF · Boeing 767238 · Wing, Plate/Skin
  > RW SKIN CORRODED AT OVERWING FILL PORT.
- [SDR ABXR2019010800001](https://openairdocs.org/sdr/ABXR2019010800001.md): Skin Panel · corroded · Jan 8, 2019 · N673BF · Boeing 767238 · Wing, Plate/Skin
  > LW SKIN CORRODED AT OVERWING FILL PORT.
- [SDR 2DYA2018012134001](https://openairdocs.org/sdr/2DYA2018012134001.md): Lamp · inoperative · Nov 14, 2018 · N602KW · Boeing 767238 · Emergency Lighting
  > 1 SMALL EMERG EXIT LIGHT AFT OF CARGO DOOR, EXTERIOR INOP. RELAMPED SMALL EMERGENCY LIGHT AFT OF REAR CARGO DOOR IAW AMM 33-31-06. OPS CHECK OK
- [SDR 2DYA2018121300001](https://openairdocs.org/sdr/2DYA2018121300001.md): Compressor · stalled · Sep 11, 2018 · N602KW · Boeing 767238 · Turbine Engine Compressor Section
  > AT TOP OF DECENT LH ENGINE COMPRESSOR STALLED 4 TIMES. OIL PRESSURE DROPPED TO 13 PSI NO TEMPERATURE EXCEEDANCE SHUT DOWN PER QRH. SERVICED # 1 ENG OIL IAW B767 AMM 12-13-01. PERFORMED LEAK DETECTION IAW B767 AMM 79-00-00. NO LEAK NOTED. PERFORMED # 1 ENG IDLE
- [SDR ABXR2016032500001](https://openairdocs.org/sdr/ABXR2016032500001.md): Structure · corroded · Mar 25, 2016 · N2767 · Boeing 767238 · Fuselage Main, Structure
  > NOSE WHEEL WELL CHORD CORRODED AT FS 287, BUTTLINE ZERO.
- [SDR 2PSA2015121201](https://openairdocs.org/sdr/2PSA2015121201.md): Seal · leaking · Dec 8, 2015 · N673BF · Boeing 767238 · Turbine Engine Oil System
  > TAKEOFF & 0:30 CREW OBSERVED LT ENG OIL QTY DECREASING ABNORMALLY. ENG WAS SHUT DOWN & ACFT RETURNED. DISCOVERED A FAILED FACE SEAL AT THE FUEL PUMP DRIVE PAD ON THE ACCESSORY GEAR BOX. A GVI OF THE SEAL WAS COMPLIED WITH PRIOR TO THE PUMP INSTALLATION THE
- [SDR ABXR201511172](https://openairdocs.org/sdr/ABXR201511172.md): Linkage · worn · Nov 17, 2015 · N673BF · Boeing 767238 · Wing, Control Surface Attach Fittings
  > FOUND LOOSE BUSHINGS IN FLAP SUPPORT LINKAGE 9 - 10 BEAM. BUSHINGS WERE REMOVED, HOLES IN LINKAGE OVERSIZED & OVERSIZED BUSHINGS WERE INSTALLED.
- [SDR ABXR201511171](https://openairdocs.org/sdr/ABXR201511171.md): Support · gouged · Nov 17, 2015 · N673BF · Boeing 767238 · Wing, Control Surface Attach Fittings
  > DEFECTS BEYOND SRM LIMITS FOUND IN FLAP SUPPORT HOLES FOR FLAP SUPPORTS 1, 7 & 8 WHILE ACCOMPLISHING SB 767-57A0131. HOLES WERE OVERSIZED, OVERSIZE BOLTS INSTALLED.
- [SDR ABXR2013101600003](https://openairdocs.org/sdr/ABXR2013101600003.md): Shaft · broken · Oct 16, 2013 · N673BF · Boeing 767238 · Escape Slide
  > DURING A-CHECK, OVERWING ESCAPE SLIDE FAILED TO OPEN WHILE PERFORMING OPS CHECK. FOUND BROKEN SHAFT ON INTEGRATER. REPLACED INTEGRATER. OPS CHECKED GOOD.
- [SDR ABXR2013041900002](https://openairdocs.org/sdr/ABXR2013041900002.md): Door Frame · corroded · Apr 19, 2013 · N673BF · Boeing 767238 · Fuselage Main, Structure
  > DURING 'A' CHECK FOUND AFT LOWER CARGO DOOR JAMB AFT LOWER CORNER CORRODED. REPAIRED IAW AMES REA 47048REA02.
- [SDR ABXR2012110800069](https://openairdocs.org/sdr/ABXR2012110800069.md): Skin · dented · Nov 8, 2012 · N673BF · Boeing 767238 · Fuselage Main, Plate/Skin
  > DURING A ROUTINE SCHEDULED C2 CHECK INSPECTION, A DENT WAS DISCOVERED AT BS 1619, BETWEEN S-33R AND S-32R. FOUND DENT TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. REPAIRED DENT IAW SRM 53-00-01, REPAIR 14, FIG 201.
- [SDR ABXR2012110800068](https://openairdocs.org/sdr/ABXR2012110800068.md): Bulkhead · dented · Nov 8, 2012 · N673BF · Boeing 767238 · Fuselage Main, Bulkhead
  > DURING A ROUTINE SCHEDULED C2 INSPECTION, DISCOVERED AFT PRESSURE BULKHEAD BS 1582 AFT SIDE HAS A DENT INBD OF RADIAL STRAP 17 BETWEEN TEAR STRAP 4 & TEAR STRAP 5. CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-80-08, FIG 201, REPAIR 2.
- [SDR ABXR2012110800067](https://openairdocs.org/sdr/ABXR2012110800067.md): Strap · damaged · Nov 8, 2012 · N673BF · Boeing 767238 · Trailing Edge Flaps
  > DURING A ROUTINE SCHEDULED C2 INSPECTION, NR 1 FLAP SUPPORT FITTING OTBD STRAP UPPER COUNTERSUNK FASTENER, COUNTERSINK DAMAGED. THE OTBD SIDE HAS A THICKNESS OF 0.865. THE DAMAGE WAS REMOVED AND THE COUNTERSINK FASTENER HAD A MAXIMUM WIDTH OF 0.635 AND DEPTH O
- [SDR ABXR2012110800066](https://openairdocs.org/sdr/ABXR2012110800066.md): Bulkhead · dented · Nov 8, 2012 · N673BF · Boeing 767238 · Fuselage Main, Bulkhead
  > DURING A ROUTINE SCHEDULED C2 INSPECTION,FOUND AFT PRESSURE BULKHEAD BS 1582 AFT SIDE DENT INBD OF RADIAL STIFFENER 16, ABOVE TEAR STRAP 3. CUT OUT DENT DAMAGE IN WEB AND LAYED OUT AND INSTALLED REPAIR REF SRM 53-80-03, AND EXTENDED FASTENER ROWS PAST RADIAL
- [SDR ABXR2012110800065](https://openairdocs.org/sdr/ABXR2012110800065.md): Skin · cracked · Nov 8, 2012 · N673BF · Boeing 767238 · Fuselage Main, Plate/Skin
  > DURING A ROUTINE C2 INSPECTION, FOUND CRACKS EMINATING FROM FASTENERS AT BS 1654.5 BETWEEN STR 3 RT AND STR 7 RT. FOUR CRACKS, THE LONGEST MEASURING.5". REPAIRED USING 0.032, 0.040, 0.063 7075 T6 REF SRM 53-80-01, FIG 201, REPAIR 4.
- [SDR ABXR2012110800064](https://openairdocs.org/sdr/ABXR2012110800064.md): Skin · cracked · Nov 8, 2012 · N673BF · Boeing 767238 · Fuselage Main, Plate/Skin
  > DURING A ROUTINE SCHEDULED C2 INSPECTION, STA 1654 HAS 3 FUSELAGE SKIN CRACKS, ADJACENT TO S3 LENGTH 1.125, 2 BETWEEN S4 & S5 LENGTHS.175 AND.075. REPAIRED USING 0.032, 0.040, 0.063 7075 T6 REF SRM 53-80-01, FIG 201, REPAIR 4.
- [SDR I5EA2012071101](https://openairdocs.org/sdr/I5EA2012071101.md): Housing · cracked · Jul 11, 2012 · N250MY · Boeing 767238 · Fuel Control/Turbine Engines
  > LEAKING FUEL AFTER START.
- [SDR I5EA20110511](https://openairdocs.org/sdr/I5EA20110511.md): Battery Pack · defective · May 10, 2011 · N250MY · Boeing 767238 · Emergency Lighting
  > EMERGENCY LIGHTING BATTERY PACK NOT HOLDING CHARGE.
- [SDR I5EA20110510](https://openairdocs.org/sdr/I5EA20110510.md): Battery Pack · defective · May 10, 2011 · N250MY · Boeing 767238 · Emergency Lighting
  > EMERGENCY LIGHTING BATTERY PACK NOT HOLDING CHARGE.
- [SDR I5EA20110509](https://openairdocs.org/sdr/I5EA20110509.md): Battery Pack · defective · May 10, 2011 · N250MY · Boeing 767238 · Emergency Lighting
  > EMERGENCY LIGHTING BATTERY PACK NOT HOLDING CHARGE.
- [SDR I5EA20110508](https://openairdocs.org/sdr/I5EA20110508.md): Battery Pack · defective · May 10, 2011 · N250MY · Boeing 767238 · Emergency Lighting
  > EMERGENCY LIGHTING BATTERY PACK NOT HOLDING CHARGE.
- [SDR I5EA20110507](https://openairdocs.org/sdr/I5EA20110507.md): Battery Pack · defective · May 10, 2011 · N250MY · Boeing 767238 · Emergency Lighting
  > EMERGENCY LIGHTING BATTERY PACK NOT HOLDING CHARGE.
- [SDR I5EA20110506](https://openairdocs.org/sdr/I5EA20110506.md): Battery Pack · defective · May 10, 2011 · N250MY · Boeing 767238 · Emergency Lighting
  > EMERGENCY LIGHTING BATTERY PACK NOT HOLDING CHARGE.
- [SDR I5EA20110503C](https://openairdocs.org/sdr/I5EA20110503C.md): Structure · cracked · May 10, 2011 · N250MY · Boeing 767238 · Leading Edge Devices
  > NR 1 I/B, NR 2 O/B AND NR 12 I/B LEADING EDGE SLAT ACTUATOR POSITIONS HAVE CRACKED/TORN STRUCTURE AT WING LOWER SURFACE SPLICE PLATE.
- [SDR I5EA20110503B](https://openairdocs.org/sdr/I5EA20110503B.md): Slat · cracked · May 10, 2011 · N250MY · Boeing 767238 · Leading Edge Devices
  > NR 1 I/B, NR 2 O/B AND NR 12 I/B LEADING EDGE SLAT ACTUATOR POSITIONS HAVE CRACKED/TORN STRUCTURE AT WING LOWER SURFACE SPLICE PLATE.
- [SDR I5EA20110503](https://openairdocs.org/sdr/I5EA20110503.md): Slat · cracked · May 10, 2011 · N250MY · Boeing 767238 · Leading Edge Devices
  > NR 1 I/B, NR 2 O/B AND NR 12 I/B LEADING EDGE SLAT ACTUATOR POSITIONS HAVE CRACKED/TORN STRUCTURE AT WING LOWER SURFACE SPLICE PLATE.
- [SDR I5EA20110502](https://openairdocs.org/sdr/I5EA20110502.md): Structure · corroded · May 10, 2011 · N250MY · Boeing 767238 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT CARGO DOOR BEARSTRAPS AFT CARGO PIT AT THE CARGO HANDLING LOADER CONTROL PANEL CUTOUT (BOX) LOWER LATCH. (OUTSIDE CONTROL)
- [SDR 2PSASDR7671010](https://openairdocs.org/sdr/2PSASDR7671010.md): O-Ring · failed · Oct 10, 2010 · N673BF · Boeing 767238 · Turbine Engine Oil System
  > DURING CRUISE FLIGHT, AT APPROX 3:22 AFTER TAKEOFF, OBSERVED NR2 ENGINE OIL QTY STARTED TO SHOW A POSSIBLE LOSS OF OIL AT A RATE OF 1 QT EVERY 3 MINUTES. WHEN QTY REACHED 3 QTS, ENGINE BROUGHT BACK TO IDLE & SHUTDOWN INITIATED. ACFT LANDED WITH A TOTAL FLIGH
- [SDR 7A7B20090610001](https://openairdocs.org/sdr/7A7B20090610001.md): Stiffener · corroded · Jun 10, 2009 · N673BF · Boeing 767238 · Fuselage Miscellaneous Structure
  > DURING THE PROCESS OF GAINING ACCESS TO THE FAIL-SAFE STRAP TRIM OUT AREA, IT WAS DETERMINED THAT THE INSTRUCTION IAW REV 1 OF THE SB WAS INSUFFICIENT TO REMOVE THE T-FITTINGS. MFG WAS CONTACTED VIA FIRST RESPONSE ON 6/9/09 AND THE SB ENGINEERING GROUP RESPON
- [SDR 2PSASDR7670902](https://openairdocs.org/sdr/2PSASDR7670902.md): Skin · cracked · Jun 3, 2009 · N673BF · Boeing 767238 · Fuselage Main, Plate/Skin
  > DURING REMOVAL OF THE RT LWR AFT BODY FAIRING, ZONE 198, A CRACK WAS DISCOVERED IN THE FUSELAGE SKIN BETWEEN BS 1197 AND 1199,.5 INCH ABOVE STRINGER S-32R. THE CRACK IS APPROXIMATELY 1.625 INCHES IN LENGTH AND RUNS PARALLEL TO THE STRINGER. THE CRACK IS A R

Next page: https://openairdocs.org/model/boeing-767-238/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 aircraft_model_key = '767238'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-767-238/reports

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