# Service difficulty reports: Boeing 767-33A

A list on [Boeing 767-33A](https://openairdocs.org/model/boeing-767-33a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 40 · 1,978 reports

- [SDR ABXR2026060400010](https://openairdocs.org/sdr/ABXR2026060400010.md): Angle · cracked · Jun 4, 2026 · N1997A · Boeing 76733A · Wing, Attach Fittings
  > RIGHT WING L/E #9 SLAT AREA INTERNAL ANGLE CRACKED AT LOWER FWD WEB LOWER ANGLE. LES668. FABRICATED NEW ANGLE IAW B767 SRM 57-41-13 REPAIR 1
- [SDR ABXR2026060400009](https://openairdocs.org/sdr/ABXR2026060400009.md): Frame · corroded · Jun 4, 2026 · N1997A · Boeing 76733A · Fuselage Main, Frame
  > CORROSION AT STA. 1219 RBL22 "J" FRAME FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-511.
- [SDR CNMA2026040004](https://openairdocs.org/sdr/CNMA2026040004.md): Pressure Valve · inoperative · Apr 21, 2026 · N351AX · Boeing 76733A · Pneumatic System
  > L HPSOV EICAS MSG, AND L BLEED LIGHT ILLUMINATED
- [SDR CNMA2026030002](https://openairdocs.org/sdr/CNMA2026030002.md): Altimeter · inoperative · Mar 31, 2026 · N351AX · Boeing 76733A · Altimeter, Barometric/Encoder
  > CA ALTIMETER INOP. FLAGGED OFF AT 25,000 FT.
- [SDR 2026FA0000047](https://openairdocs.org/sdr/2026FA0000047.md): Thrust Reverser · delaminated · Jan 20, 2026 · N407EG · Boeing 76733A · Engine Thrust Reverser
  > DURING AIRCRAFT CARGO CONVERSION AT IAI MAINTENANCE FOUND THE INNER SKIN OF THE ENGINE #1 INBOARD THRUST REVERSER DELAMINATED AT NAC STA 230. THE DAMAGE WAS EVALUATED AND FOUND TO BE BEYOND REPAIR LIMITS. WORK PERFORMED IAW REA NO: MF03036R0233.
- [SDR 2026FA0000046](https://openairdocs.org/sdr/2026FA0000046.md): Frame · cracked · Jan 20, 2026 · N407EG · Boeing 76733A · Fuselage Structure (General)
  > DURING MAINTENANCE INSPECTIONS AT IAI FACILITIES, SHOP FOUND A CRACK IN ENGINE #1 INLET COWL AFT BULKHEAD OUTER FRAME FLANGE, BETWEEN 11 O'CLOCK AND 12 O'CLOCK. WORK PERFORMED IAW REA NO: MF03036R0235.
- [SDR 2026FA0000045](https://openairdocs.org/sdr/2026FA0000045.md): Frame · cracked · Jan 20, 2026 · N407EG · Boeing 76733A · Nacelle/Pylon, Frame/Spar/Rib
  > DURING MAINTENANCE INSPECTIONS AT IAI FACILITIES, SHOP FOUND A CRACK IN ENGINE #2 INLET COWL AFT BULKEAD OUTER FRAME FLANGE, BETWEEN 12 O'CLOCK AND 1 O'CLOCK THE CRACK WAS TRIMMED OUT PER SRM 51-10-02. WORK PERFORMED IAW REA NO MF03036R0229.
- [SDR 2026FA0000044](https://openairdocs.org/sdr/2026FA0000044.md): Angle · gouged · Jan 20, 2026 · N407EG · Boeing 76733A · Nacelle/Pylon, Frame/Spar/Rib
  > DURING INSPECTION OF THE LEFT-HAND CORE COWL OF ENGINE #1 (P/N: 224M4761-513, S/N: 2014001), A GOUGE WAS FOUND ON THE EXISTING FRAME REPAIR ANGLE. WORK PERFORMED IAW REA NO: MF03036R0219.
- [SDR 2026FA0000043](https://openairdocs.org/sdr/2026FA0000043.md): Frame · punctured · Jan 19, 2026 · N407EG · Boeing 76733A · Fuselage Main, Frame
  > DURING MAINTENANCE INSPECTIONS AT IAI, A PUNCTURE WAS FOUND ON THE WEB OF FRAME STA 1417 BETWEEN STR 37R AND 39R. WORK PERFORMED IAW REA NO: MF03036R0237.
- [SDR 2026FA0000042](https://openairdocs.org/sdr/2026FA0000042.md): Ring · worn · Jan 19, 2026 · N407EG · Boeing 76733A · Engine Thrust Reverser
  > DURING MAINTENANCE INSPECTION, WEAR DAMAGE FOUND ON ENGINE NR 1, RIGHT FAN REVERSER, AFT CLOSEOUT RING AT THE LOWER AND UPPER CORNERS.WORK PERFORMED IAW REA NO: MF03036R0222.
- [SDR 2026FA0000041](https://openairdocs.org/sdr/2026FA0000041.md): Frame · corroded · Jan 19, 2026 · N407EG · Boeing 76733A · Fuselage Main, Frame
  > DURING CONVERSION, CORROSION WAS FOUND ON THE FRAME AT STA1480, BETWEEN STR 22L AND STR 24L. WORK PERFORMED IAW- REA NO: MF03036R0202.
- [SDR 2026FA0000039](https://openairdocs.org/sdr/2026FA0000039.md): Frame · damaged · Jan 19, 2026 · N407EG · Boeing 76733A · Fuselage Main, Frame
  > DURING CONVERSION AT IAI FACILITIES, SHOP FOUND DAMAGED FRAME WEB AT STA 478, BETWEEN STR - 27R AND STR - 28R (LARGE CARGO DOOR SURROUND). WORK PERFORMED IAW - REA NO: MF03036R0206.
- [SDR 2026FA0000038](https://openairdocs.org/sdr/2026FA0000038.md): Frame · corroded · Jan 19, 2026 · N407EG · Boeing 76733A · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME STA 1439, OUTER FLANGE, TWO LOCATIONS BETWEEN STR 17L-18L.
- [SDR 2026FA0000037](https://openairdocs.org/sdr/2026FA0000037.md): Channel · cracked · Jan 19, 2026 · N407EG · Boeing 76733A · Engine Exhaust System
  > DURING MAINTENANCE INSPECTIONS AT IAI FACILITIES SHOP FOUND A CRACK ON CHANNEL. DAMAGED AND ENLARGED FASTENER HOLES ON OUTER SKIN FAIRING. WORK PERFORMED IAW REA MF03036R0216.
- [SDR 2026FA0000036](https://openairdocs.org/sdr/2026FA0000036.md): Skin · abnormal · Jan 18, 2026 · N407EG · Boeing 76733A · Fuselage Main, Plate/Skin
  > DUE TO EXISTING EXTERNAL REPAIR IN FUSELAGE SKIN, SHOP CANNOT INSTALL SHEAR TIE, P/N 95292-257 IN ACCORDANCE WITH DWG REQUIREMENTS.
- [SDR 2026FA0000035](https://openairdocs.org/sdr/2026FA0000035.md): Shear Tie · damaged · Jan 18, 2026 · N407EG · Boeing 76733A · Fuselage Internal Mounting Structure
  > SHOP FOUND SIX (6) EXISTING 7/32" DIAMETER FASTNER HOLES DURING SALVAGED SHEAR TIE, P/N BACF3T01G7G16 REMOVAL AT STA 390, BETWEEN STR-20L AND STR-21L. REFER TO FIGURES 1 AND 2 FOR E.M AND FASTENER SPACING.
- [SDR 2026FA0000034](https://openairdocs.org/sdr/2026FA0000034.md): Tear Strap · gouged · Jan 18, 2026 · N407EG · Boeing 76733A · Fuselage Main, Structure
  > DURING INSTALLATION OF P/N 368-53-11-90830-235 SHEAR TIE PER DWG 371-53-11-C3147, VIEWS 1B3 AND 1B12, A GOUGE WAS FOUND ON THE TEAR STRAP AT STA 368, BETWEEN STR 20L AND 21L. THE GOUGE WAS REMOVED, AND THE RESULTING BLEND-OUT DIMENSIONS ARE 1.00" X 0.320". THE
- [SDR 2026FA0000033](https://openairdocs.org/sdr/2026FA0000033.md): Skin · mechanic error · Jan 18, 2026 · N407EG · Boeing 76733A · Fuselage Main, Plate/Skin
  > DURING INSTALLATION OF SHEAR TIE PER DWG 371-53-00-C4157 VIEWS 5C8-1 AND 1B5, THE SHOP MISTAKENLY DAMAGED THE COUNTERSINK OF ONE FASTENER HOLE COMMON TO THE FUSELAGE SKIN AT BS 1241, BETWEEN STR 27R AND 28R.
- [SDR 2026FA0000032](https://openairdocs.org/sdr/2026FA0000032.md): Frame · mechanic error · Jan 18, 2026 · N407EG · Boeing 76733A · Fuselage Main, Frame
  > DURING CNV WORK SHOP CAUSED DAMAGE TO THE FRAME EDGE AT SPLICE AREA, OUTER FLANGE.
- [SDR 2026FA0000031](https://openairdocs.org/sdr/2026FA0000031.md): Doubler · corroded · Jan 18, 2026 · N407EG · Boeing 76733A · Fuselage Main, Plate/Skin
  > DURING INSTALLATION OF DOUBLER PER DWG 371-53-11-C3164, CORROSION WAS DETECTED ON THE OUTER FLANGE OF FRAME BS 390 BETWEEN STR 19R AND 20R.
- [SDR 2026FA0000025](https://openairdocs.org/sdr/2026FA0000025.md): Bracket · misinstalled · Jan 15, 2026 · N407EG · Boeing 76733A · Fuselage Main, Floor Beam
  > ACCORDING TO INSTALLATION 371-53-00-C4178-003 SHOP REQ TO REMOVE AND REPLACE TWO EXISTING BRACKETS.HOWEVER INSTALLATION OF FITTINGS WILL RESULT IN SHORT EDGE MARGIN.BRACKETS ARE DIFFRENT THAN WHAT ITS SHOULD BE PER DWG 145T8722. IN ADDITION THE FOUR FASTNER
- [SDR NACA2025101000006](https://openairdocs.org/sdr/NACA2025101000006.md): Igniter · worn · Oct 10, 2025 · N567NC · Boeing 76733A · Spark Plug/Igniter
  > NR 2 ENGINE UPPER IGNITER PLUG WORN BEYOND LIMITS. REMOVED AND REPLACED NR 2 UPPER IGNITER PLUG IAW AMM 74-21-02-004-001-N00 AND AMM 74-21-01-404-014-N00. OPS CHECK GOOD.
- [SDR NACA2025101000005](https://openairdocs.org/sdr/NACA2025101000005.md): Igniter · worn · Oct 10, 2025 · N567NC · Boeing 76733A · Spark Plug/Igniter
  > NR 2 ENG LOWER IGNITER PLUG WORN BEYOND LIMITS. REMOVED AND REPLACED NR 2 LOWER IGNITER PLUG IAW AMM 74-21-02-004-001-N00 AND AMM 74-21-01-404-014-N00. OPS CHECK GOOD.
- [SDR NACA2025101000004](https://openairdocs.org/sdr/NACA2025101000004.md): Cable · cracked · Oct 10, 2025 · N567NC · Boeing 76733A · Ignition System Wiring
  > NR 2 ENG LOWER IGNITION EXCITER CABLE BUSHING UNDER CERAMIC SLEEVE CRACKED. DOT 048200. REMOVED AND REPLACED NR 2 ENG LOWER IGNITION EXCITER CABLE IAW B767 AMM 74-21-01-004-001-N00. TEST OK. PO # GYR10300795. TW ID T100360-1 D/D 8/12/26. MECH: ALD025 10/06/
- [SDR NACA2025101000003](https://openairdocs.org/sdr/NACA2025101000003.md): Circuit Card · faulted · Oct 10, 2025 · N567NC · Boeing 76733A · Fire Detection
  > LEFT ENGINE FAILED AUTOMATIC FIRE / OVERHEAT LOGIC /TEST SYSTEM (AFOLTS) SYSTEM CHECK. CARDS WERE REPLACED WITH PN S332T301-181 SN 940, 699, 8823 AND 6780
- [SDR NACA2025101000002](https://openairdocs.org/sdr/NACA2025101000002.md): Valve · cracked · Oct 10, 2025 · N567NC · Boeing 76733A · Turbine Engine Air Inlet Section
  > IP VALVE ON #1 ENGINE HAS SIGNS OF CRACKING AND CORROSION ON FUSELAGE. INSTALLED SERVICEABLE IP VALVE ON # 1 ENG IAW AMM 36-11-06-404-033-002. NO LEAK NOTED.
- [SDR NACA2025101000001](https://openairdocs.org/sdr/NACA2025101000001.md): Vane · broken · Oct 10, 2025 · N567NC · Boeing 76733A · Turbine Engine Air Inlet Section
  > ONE EA FAN EXIT VANE OF THE NR 2 ENGINE HAS A BROKEN PLATFORM AT THE INNER BASE OF PART. PERFORMED EVALUATION IF 1 EACH FAN EXIT VALVE OF #2 ENG BROKEN PLATFORM NO ADITIONAL DEFECTS NOTED. REPAIRED FAN EXIT VALVE IAW 72-33-02-308-003-N00.
- [SDR NACA2025100400002](https://openairdocs.org/sdr/NACA2025100400002.md): Screen · damaged · Oct 4, 2025 · N567NC · Boeing 76733A · Engine Bleed Air System
  > NR 1 FAN EXIT CASE BLEED AIR DUCT, BLEED SCREENS 8 EA FROM UPPER DUCTS ARE BROKEN / MISSING. REMOVE AND REPLACE 6 EA SCREENS ON #1 ENG ESN 724378 IAW AMM 72-00-00-416-342-N00 REMAINING 2 EA UPPER SCREENS FOUND TO BE IN SERVICEABLE CONDITION IAW AMM TASK 75-3
- [SDR NACA2025100400001](https://openairdocs.org/sdr/NACA2025100400001.md): Sense Line · chafed · Oct 4, 2025 · N567NC · Boeing 76733A · Engine Indicating System
  > STATIC PRESSURE SENSE LINE TUBE CHAFED ON #2 ENG. INBD FAN COWL. REMOVED AND REPLACED STATIC PRESSURE SENSE LINE TUBE ON #2 ENG INBD FAN COWL. LEAK TEST AND STATIC TEST GOOD IAW B767 AMM 71-00-02-844-002-N00 STEP 2 AMM 71-00-02-844-077-N00 STEP 7 AMM 71-00-
- [SDR NACA2025093000008](https://openairdocs.org/sdr/NACA2025093000008.md): Seal · deteriorated · Sep 30, 2025 · N567NC · Boeing 76733A · Turbine Engine Oil System
  > NR 2 ENGINE SEAL ATTACHED TO OIL DRAIN COLLECTOR IS DAMAGED & DETERIORATING. REMOVED & REPLACED NR 2 ENG SEAL ATTACHED TO OIL DRAIN COLLECTOR IAW AMM 51-31-01-302-001 AND 51-31-01-392-013.
- [SDR NACA2025093000007](https://openairdocs.org/sdr/NACA2025093000007.md): Exciter · damaged · Sep 30, 2025 · N567NC · Boeing 76733A · Exciter
  > NR 1 ENG TOP IGNITION EXCITER INSIDE OUTPUT RECEPTACLE WELL HAS DAMAGE / SIGNS OF ARCING ON THE CONTACT BUTTON. REMOVED AND REPLACED #1 ENG TOP IGNITION EXCITER IAW B767 AMM 74-11-01-004-001-N00 AND AMM 74-11-01-404-019 STEP 3.
- [SDR NACA2025093000006](https://openairdocs.org/sdr/NACA2025093000006.md): Igniter · worn · Sep 30, 2025 · N567NC · Boeing 76733A · Spark Plug/Igniter
  > NR 1 ENG. SYS. 1 TOP IGNITION EXCITER PLUG IS WORN BEYOND LIMITS. IGNITER PLUG REPLACED IAW AMM 74-21-02-404-014-N00.
- [SDR NACA2025093000005](https://openairdocs.org/sdr/NACA2025093000005.md): Sealant · missing · Sep 30, 2025 · N567NC · Boeing 76733A · Engine (Turbine/Turboprop)
  > 10 O'CLOCK (FWD LOOKING) FAN EXIT STRUT LOWER SURFACE MISSING SEALANT ON NR 2 ENGINE. APPLIED SEALANT ON FAN EXIT STRUT LOWER SURFACE #2 ENG AT 10 O'CLOCK PER B767 AMM 73-3405 TASK 72-34-05-404-005-N00 PAR D (3) (E).
- [SDR NACA2025093000004](https://openairdocs.org/sdr/NACA2025093000004.md): Liner · misinstalled · Sep 30, 2025 · N567NC · Boeing 76733A · Engine (Turbine/Turboprop)
  > 6 TO 7 O'CLOCK (LOOKING FWD) FAN EXIT LINER NOT PROPERLY FAIRED ON #2 ENGINE. REPAIRED FAIRED FAN EXIT LINER ON #2 ENGINE AT 6 TO 7 O'CLOCK POSITION, REPLACED BROKEN SUPPORT BRACKETS FOR LINER REF MAN-PW4ENG-109 PG 18 AND SRM 51-40-02 STEP 4 (B).
- [SDR NACA2025093000003](https://openairdocs.org/sdr/NACA2025093000003.md): Control Unit · faulted · Sep 30, 2025 · N567NC · Boeing 76733A · DC Generating System
  > BUSS POWER CONTROL UNIT HAS A FAULT MESSAGE IDG / OIL OUT. PERFORMED BPCU BITE PROCEDURE PER B-767 FIM 24-30 FAULT TREE 801. BITE PROCEDURE OK.
- [SDR NACA202510229002](https://openairdocs.org/sdr/NACA202510229002.md): Clamp · misinstalled · Sep 30, 2025 · N567NC · Boeing 76733A · Nacelle/Pylon Structure
  > NR 2 ENGINE IDG WIRING HARNESS CLAMPS NOT PROPERLY INSTALLED PERFORMED PROPERLY INSTALLATION OF THE CLAMPS IN THE IDG WIRE HARNESS AT #2 ENGINE IAW SWPM 20-10-12 STEP Y PG 148.
- [SDR NACA2025093000001](https://openairdocs.org/sdr/NACA2025093000001.md): Oil Tube · unsecure · Sep 30, 2025 · N567NC · Boeing 76733A · Turbine Engine Oil System
  > BROKEN CLAMP ON OIL TUBE FWD OF OIL TANK ON #1 ENGINE. INSTALLED NEW CLAMP ON FIRE EXT. TUBE FWD OF OIL TANK ON #1 ENGINE PER AMM 20-11-00 TABLE 213/20-11-00-993-830
- [SDR NACA2025092600002](https://openairdocs.org/sdr/NACA2025092600002.md): Sealant · missing · Sep 26, 2025 · N567NC · Boeing 76733A · Engine (Turbine/Turboprop)
  > SEVERAL FAN EXIT (INNER FRONT) FAIRINGS SEGEMENTS MISSING SEALANT AROUND COMPRESSOR SECTION CASE ON NR 2 ENG. APPLIED RTV SEALANT TO FAN EXIT (INNER FRONT) FAIRING SEGMENTS IAW B767-300 REF. AMM 72-34-03.
- [SDR NACA2025092600001](https://openairdocs.org/sdr/NACA2025092600001.md): Clamp · unsecure · Sep 26, 2025 · N567NC · Boeing 76733A · Nacelle/Pylon Structure
  > NR 2 ENGINE IDG WIRING HARNESS CLAMPS NOT PROPERLY INSTALLED. PERFORMED PROPERLY INSTALLATION OF THE CLAMPS IN THE IDG WIRE HARNESS AT #2 ENGINE IAW SWPM 20-10-12 STEP Y PG 148.
- [SDR NACA2025092300001](https://openairdocs.org/sdr/NACA2025092300001.md): Igniter · worn · Sep 23, 2025 · N567NC · Boeing 76733A · Spark Plug/Igniter
  > NR 1 ENG IGNITOR PLUG FOR SYSTEM 2 (BOTTOM PLUG) IS WORN BEYOND LIMITS. IGNITER PLUG REPLACED IAW AMM 74-21-02-404-014-N00.
- [SDR IXXA20250918053](https://openairdocs.org/sdr/IXXA20250918053.md): Power Supply · inoperative · Sep 18, 2025 · N1439A · Boeing 76733A · Emergency Lighting
  > FOUND INTERIOR EMERGENCY LIGHTS RIGHT CEILING, DOOR EXIT SIGN AND DOOR THRESHOLD LIGHT INOPERATIVE DURING EMERGENCY LIGHT TEST. PLACED ON DEFERRAL 66237. MINIMUM EQUIPMENT LIST ATI-33-51-01-01 CATEGORY D. TROUBLESHOT IN ACCORDANCE WITH B767 IAI WIRING DIAGRAM
- [SDR IXXA20250908001](https://openairdocs.org/sdr/IXXA20250908001.md): Tube · dented · Sep 8, 2025 · N1439A · Boeing 76733A · Aircraft Fuel Distribution System
  > A DENT WAS FOUND DURING C-CHECK MAINTENANCE VISIT LOCATED INSIDE 532BB BETWEEN LOWER STRINGER L-6 AND L-7. THE DENT WAS MEASURED AS L=0.400" W=0.700" D=0.129". DENT TO BE RE INSPECTED AT NEXT C-CHECK TO BE CONSIDERED PERMANENT
- [SDR IXX2025F00019](https://openairdocs.org/sdr/IXX2025F00019.md): Beam · corroded · Sep 8, 2025 · N1439A · Boeing 76733A · Fuselage Main, Structure
  > FLC DOOR CUTOUT LWR SILL BEAM EXFOLIATED STA622
- [SDR IXXA2025090300018](https://openairdocs.org/sdr/IXXA2025090300018.md): Tube · dented · Sep 3, 2025 · N1439A · Boeing 76733A · Aircraft Fuel Distribution System
  > LEFT WING FUEL DISTRIBUTION TUBE HAS A DENT, LOCATED INSIDE 532BB BETWEEN LOWER STRINGER L-6 AND L-7
- [SDR IXXA20250831002](https://openairdocs.org/sdr/IXXA20250831002.md): Skin · corroded · Aug 31, 2025 · N1439A · Boeing 76733A · Wing, Plate/Skin
  > RIGHT WING TOP EXTERNAL SKIN CORRODED AT SKIN SPICE AT WING STA 383.5-395
- [SDR IXX2025F00016](https://openairdocs.org/sdr/IXX2025F00016.md): Skin · delaminated · Aug 31, 2025 · N1439A · Boeing 76733A · Vertical Stabilizer, Plate/Skin
  > VERTICAL STAB PANEL LEFT SIDE DELAMINATED
- [SDR 21GA202509030017](https://openairdocs.org/sdr/21GA202509030017.md): Controller · faulted · Aug 29, 2025 · N1997A · Boeing 76733A · Fire Detection
  > ON APPROACH, RECEIVED WHEEL WELL FIRE EICAS MESSAGE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. INSPECTED AND FOUND NO EVIDENCE OF FIRE. REPLACED DETECTION CONTROL CARD.
- [SDR NACA2025082000002](https://openairdocs.org/sdr/NACA2025082000002.md): Elec Connector · damaged · Aug 20, 2025 · N567NC · Boeing 76733A · Fuel System Wiring
  > DURING TROUBLESHOOTING FOUND LEFT FWD FBP CONNECTOR D1550 PIN #6 WILL NOT SECURE. REPLACED FUEL PUMP CONNECTOR D1550 PER SWPM 20-61-00 OPS CHECK GOOD PER AMM 28-42-01
- [SDR NACA2025082000001](https://openairdocs.org/sdr/NACA2025082000001.md): Pressure Switch · failed · Aug 20, 2025 · N567NC · Boeing 76733A · Fuel Boost Pump
  > AFTER LEFT ENGINE START L FWD BOOST PUMP PRESSURE LIGHT ILLUMINATED AND ASSOCIATED EICAS MESSAGE. REPLACED LEFT FWD PUMP PRESSURE SWITCH OPS CHECK GOOD PER AMM 28-42-01 PART IS UNKNOWN TO TRAX.
- [SDR NACA2025081700001](https://openairdocs.org/sdr/NACA2025081700001.md): Cooler · failed · Aug 17, 2025 · N567NC · Boeing 76733A · Turbine Engine Oil System
  > RIGHT ENGINE OIL QTY DROPPED FROM 17 UNITS TO 12 DURING FLIGHT. SUSPECT OIL LEAK STILL PRESENT. FOUND OIL PUDDLING AT 6 OCLOCK OF ENGINE WITH EVIDENCE OF OIL LEAKAGE ON THE LH SIDE OF ENGINE CORE EMANATING FROM AIR/OIL COOLER. REMOVED AND REPLACED #2 ENGINE AI

Next page: https://openairdocs.org/model/boeing-767-33a/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 = '76733A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-767-33a/reports

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