# Boeing 767-33A

- Type: Aircraft model (FAA registry)
- Registry code: 1385209
- Manufacturer (registry): BOEING
- Model: 767-33A
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 330
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 4
- Page: https://openairdocs.org/model/boeing-767-33a

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

None matched.

## Registered aircraft (4)

- [N1439A](https://openairdocs.org/aircraft/N1439A): [Andromeda Leasing I LLC](https://openairdocs.org/faa-owner/ANDROMEDA%20LEASING%20I%20LLC), [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase), built 1997, S/N 28495
- [N1997A](https://openairdocs.org/aircraft/N1997A): [Andromeda Leasing II LLC](https://openairdocs.org/faa-owner/ANDROMEDA%20LEASING%20II%20LLC), [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase), built 1994, S/N 27310
- [N351AX](https://openairdocs.org/aircraft/N351AX): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1995, S/N 27908
- [N378AX](https://openairdocs.org/aircraft/N378AX): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1996, S/N 28147

## NTSB investigations (3)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA26MA352](https://openairdocs.org/ntsb/DCA26MA352), Sep 6, 2026: Boeing 767 (N1997A), Miami, FL, substantial damage, 5 fatal, investigation ongoing
- [NTSB DCA19WA202](https://openairdocs.org/ntsb/DCA19WA202), Aug 15, 2019: Boeing 767 (N378AX), Shannon, Ireland, incident, minor damage
- [NTSB DCA17WA073](https://openairdocs.org/ntsb/DCA17WA073), Feb 28, 2017: Boeing 767 33A (N351AX), Azraq, Jordan, substantial damage

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20240316006459I](https://openairdocs.org/incident/20240316006459I), Mar 16, 2024: Boeing 767-33A (N378AX), Tulsa, OK, Minor damage. During approach, the pilots experienced increased effort applying right aileron after they turned off the autopilot. They landed the plane without further…
- [Incident 20150501005879I](https://openairdocs.org/incident/20150501005879I), May 1, 2015: Boeing 767-33A (N583HA), Kahului, HI, No damage. (1) The reason for the evacuation: A. air cycle machine malfunction, which introduced smoke/haze into the cabin. (2) Who initiated the evacuation: A. the pilot…

## Service difficulty reports (1,978, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR ABXR2026060400010](https://openairdocs.org/sdr/ABXR2026060400010), Jun 4, 2026: ANGLE. CRACKED. 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), Jun 4, 2026: FRAME. CORRODED. 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), Apr 21, 2026: PRESSURE VALVE. INOPERATIVE. L HPSOV EICAS MSG, AND L BLEED LIGHT ILLUMINATED
- [SDR CNMA2026030002](https://openairdocs.org/sdr/CNMA2026030002), Mar 31, 2026: ALTIMETER. INOPERATIVE. CA ALTIMETER INOP. FLAGGED OFF AT 25,000 FT.
- [SDR 2026FA0000047](https://openairdocs.org/sdr/2026FA0000047), Jan 20, 2026: THRUST REVERSER. DELAMINATED. 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 EVA
- [SDR 2026FA0000046](https://openairdocs.org/sdr/2026FA0000046), Jan 20, 2026: FRAME. CRACKED. 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.
- [SDR 2026FA0000045](https://openairdocs.org/sdr/2026FA0000045), Jan 20, 2026: FRAME. CRACKED. 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 TH
- [SDR 2026FA0000044](https://openairdocs.org/sdr/2026FA0000044), Jan 20, 2026: ANGLE. GOUGED. 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 PERFORME
- [SDR 2026FA0000043](https://openairdocs.org/sdr/2026FA0000043), Jan 19, 2026: FRAME. PUNCTURED. 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), Jan 19, 2026: RING. WORN. 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:
- [SDR 2026FA0000041](https://openairdocs.org/sdr/2026FA0000041), Jan 19, 2026: FRAME. CORRODED. 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), Jan 19, 2026: FRAME. DAMAGED. 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 - 
- [SDR 2026FA0000038](https://openairdocs.org/sdr/2026FA0000038), Jan 19, 2026: FRAME. CORRODED. CORROSION FOUND ON FRAME STA 1439, OUTER FLANGE, TWO LOCATIONS BETWEEN STR 17L-18L.
- [SDR 2026FA0000037](https://openairdocs.org/sdr/2026FA0000037), Jan 19, 2026: CHANNEL. CRACKED. DURING MAINTENANCE INSPECTIONS AT IAI FACILITIES SHOP FOUND A CRACK ON CHANNEL. DAMAGED AND ENLARGED FASTENER HOLES ON OUTER SKIN FAIRING. WORK PERFORMED IAW RE
- [SDR 2026FA0000036](https://openairdocs.org/sdr/2026FA0000036), Jan 18, 2026: SKIN. ABNORMAL. 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), Jan 18, 2026: SHEAR TIE. DAMAGED. 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 
- [SDR 2026FA0000034](https://openairdocs.org/sdr/2026FA0000034), Jan 18, 2026: TEAR STRAP. GOUGED. 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 ST
- [SDR 2026FA0000033](https://openairdocs.org/sdr/2026FA0000033), Jan 18, 2026: SKIN. MECHANIC ERROR. 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 FUS
- [SDR 2026FA0000032](https://openairdocs.org/sdr/2026FA0000032), Jan 18, 2026: FRAME. MECHANIC ERROR. DURING CNV WORK SHOP CAUSED DAMAGE TO THE FRAME EDGE AT SPLICE AREA, OUTER FLANGE.
- [SDR 2026FA0000031](https://openairdocs.org/sdr/2026FA0000031), Jan 18, 2026: DOUBLER. CORRODED. 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), Jan 15, 2026: BRACKET. MISINSTALLED. 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 MA
- [SDR NACA2025101000006](https://openairdocs.org/sdr/NACA2025101000006), Oct 10, 2025: IGNITER. WORN. 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 C
- [SDR NACA2025101000005](https://openairdocs.org/sdr/NACA2025101000005), Oct 10, 2025: IGNITER. WORN. 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 CHEC
- [SDR NACA2025101000004](https://openairdocs.org/sdr/NACA2025101000004), Oct 10, 2025: CABLE. CRACKED. 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 
- [SDR NACA2025101000003](https://openairdocs.org/sdr/NACA2025101000003), Oct 10, 2025: CIRCUIT CARD. FAULTED. 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), Oct 10, 2025: VALVE. CRACKED. 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), Oct 10, 2025: VANE. BROKEN. 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
- [SDR NACA2025100400002](https://openairdocs.org/sdr/NACA2025100400002), Oct 4, 2025: SCREEN. DAMAGED. 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-
- [SDR NACA2025100400001](https://openairdocs.org/sdr/NACA2025100400001), Oct 4, 2025: SENSE LINE. CHAFED. 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 STA
- [SDR NACA2025093000008](https://openairdocs.org/sdr/NACA2025093000008), Sep 30, 2025: SEAL. DETERIORATED. 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 51-31-01-3
- [SDR NACA2025093000007](https://openairdocs.org/sdr/NACA2025093000007), Sep 30, 2025: EXCITER. DAMAGED. 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
- [SDR NACA2025093000006](https://openairdocs.org/sdr/NACA2025093000006), Sep 30, 2025: IGNITER. WORN. 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), Sep 30, 2025: SEALANT. MISSING. 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 B
- [SDR NACA2025093000004](https://openairdocs.org/sdr/NACA2025093000004), Sep 30, 2025: LINER. MISINSTALLED. 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 B
- [SDR NACA2025093000003](https://openairdocs.org/sdr/NACA2025093000003), Sep 30, 2025: CONTROL UNIT. FAULTED. 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), Sep 30, 2025: CLAMP. MISINSTALLED. 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 20-10-1
- [SDR NACA2025093000001](https://openairdocs.org/sdr/NACA2025093000001), Sep 30, 2025: OIL TUBE. UNSECURE. 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 213/20-11-00-99
- [SDR NACA2025092600002](https://openairdocs.org/sdr/NACA2025092600002), Sep 26, 2025: SEALANT. MISSING. 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) FAIR
- [SDR NACA2025092600001](https://openairdocs.org/sdr/NACA2025092600001), Sep 26, 2025: CLAMP. UNSECURE. 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-
- [SDR NACA2025092300001](https://openairdocs.org/sdr/NACA2025092300001), Sep 23, 2025: IGNITER. WORN. 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), Sep 18, 2025: POWER SUPPLY. INOPERATIVE. FOUND INTERIOR EMERGENCY LIGHTS RIGHT CEILING, DOOR EXIT SIGN AND DOOR THRESHOLD LIGHT INOPERATIVE DURING EMERGENCY LIGHT TEST. PLACED ON DEFERRAL 66237. MINIMU
- [SDR IXXA20250908001](https://openairdocs.org/sdr/IXXA20250908001), Sep 8, 2025: TUBE. DENTED. 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". 
- [SDR IXX2025F00019](https://openairdocs.org/sdr/IXX2025F00019), Sep 8, 2025: BEAM. CORRODED. FLC DOOR CUTOUT LWR SILL BEAM EXFOLIATED STA622
- [SDR IXXA2025090300018](https://openairdocs.org/sdr/IXXA2025090300018), Sep 3, 2025: TUBE. DENTED. 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), Aug 31, 2025: SKIN. CORRODED. RIGHT WING TOP EXTERNAL SKIN CORRODED AT SKIN SPICE AT WING STA 383.5-395
- [SDR IXX2025F00016](https://openairdocs.org/sdr/IXX2025F00016), Aug 31, 2025: SKIN. DELAMINATED. VERTICAL STAB PANEL LEFT SIDE DELAMINATED
- [SDR 21GA202509030017](https://openairdocs.org/sdr/21GA202509030017), Aug 29, 2025: CONTROLLER. FAULTED. ON APPROACH, RECEIVED WHEEL WELL FIRE EICAS MESSAGE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. INSPECTED AND FOUND NO EVIDENCE OF FIRE. REPLACED DETECTION
- [SDR NACA2025082000002](https://openairdocs.org/sdr/NACA2025082000002), Aug 20, 2025: ELEC CONNECTOR. DAMAGED. 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
- [SDR NACA2025082000001](https://openairdocs.org/sdr/NACA2025082000001), Aug 20, 2025: PRESSURE SWITCH. FAILED. 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 
- [SDR NACA2025081700001](https://openairdocs.org/sdr/NACA2025081700001), Aug 17, 2025: COOLER. FAILED. 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 LE

All 1,978: https://openairdocs.org/model/boeing-767-33a/reports.md

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