# Boeing 767-31K - Type: Aircraft model (FAA registry) - Registry code: 1385192 - Manufacturer (registry): BOEING - Model: 767-31K - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 261 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 3 - Page: https://openairdocs.org/model/boeing-767-31k 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 (3) - [N1373A](https://openairdocs.org/aircraft/N1373A): [Msn 27205 LLC](https://openairdocs.org/faa-owner/MSN%2027205%20LLC), [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase), built 1994, S/N 27205 - [N1487A](https://openairdocs.org/aircraft/N1487A): [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 28865 - [N1489A](https://openairdocs.org/aircraft/N1489A): [Andromeda Leasing I LLC](https://openairdocs.org/faa-owner/ANDROMEDA%20LEASING%20I%20LLC), [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase), built 1994, S/N 27206 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (1,002, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR ABXA20260929441](https://openairdocs.org/sdr/ABXA20260929441), Sep 29, 2026: SWITCH. FAILED. EMER LIGHTS SWITCH DOES NOT CHANGE INTO ARMED WITH SWITCH GUARD DOWN. MTC REMOVED AND REPLACED EMERGENCY LIGHT SWITCH GUARD IAW AMM 33-51-00. OPS CHECK GOOD. A/ - [SDR ABXA20260906396](https://openairdocs.org/sdr/ABXA20260906396), Sep 6, 2026: WARNING MESSAGE. FALSE ACTIVATION. DURING APPROACH MESSAGE "FIRE/ OVHT SYS" ILLUMINATED , MTX PERFORMED AFOLTS TEST IAW B767 AMM 26-10-00. OPS CHECK GOOD. NFF RETURNED A/C TO SERVICE. - [SDR ABXR2026082800015](https://openairdocs.org/sdr/ABXR2026082800015), Aug 28, 2026: SUPPORT. CORRODED. CORROSION ON THE CUTOUT/ SUPPORT STRUCTURE FOR PANEL 195ML, AT THE LEFT UPPER FILLET AREA, AS VIEWED WITH DOOR OPEN. REMOVED CORROSION FROM PNL 195ML'S SUPPORT - [SDR ABXR082800014](https://openairdocs.org/sdr/ABXR082800014), Aug 28, 2026: STIFFENER. CRACKED. STA. 246 FLOORBEAM HAS CRACKED VERTICAL STIFFENER AT LBL 43 IN LEFT TUNNEL OF MEC .REPAIRED VERTICAL STIFFENER AT STA 246 FLOORBEAM LBL 43 IN LEFT TUNNEL OF MEC - [SDR ABXR082800013](https://openairdocs.org/sdr/ABXR082800013), Aug 28, 2026: STIFFENER. CRACKED. STA. 246 FLOORBEAM HAS A CRACKED VERTICAL STIFFENER ON FWD SIDE AT LBL 28 IN LEFT TUNNEL OF MEC . REPAIRED VERTICAL STIFFENER ON FWD SIDE FLOORBEAM OF STA 246 L - [SDR ABXA20260804347](https://openairdocs.org/sdr/ABXA20260804347), Aug 4, 2026: MODULE. DEFECTIVE. AT APPROXIMATELY 300FT AGL THE FLIGHT CREW RECEIVED THE AURAL WARNING, TOO LOW, FLAPS. BOTH THE FO AND PILOT CONFIRMED FLAPS 25 WAS INDICATED. THE PILOT CALLED - [SDR ABXA20260707310](https://openairdocs.org/sdr/ABXA20260707310), Jul 7, 2026: ESCAPE REEL. EXPIRED. DURING INSP/MTC, NR 3 ESCAPE REEL FOUND OUT OF DATE. DEFERRED THE NR 3 ESCAPE REEL IAW MEL 25-61-1-1 C/W MAINTENANCE PROCEDURE 25-61-1 MBCB 07/17/26 PLACARDS IN - [SDR ABXA20260623277](https://openairdocs.org/sdr/ABXA20260623277), Jun 23, 2026: EXTINGUISHER. UNSECURE. PIN TO COCKPIT FIRE EXTINGUISHER NEAR LAV DISCOVERED ON FLOOR BY MTC. REATTACHED PIN TO FIRE EXTINGUISHER HANDLE USING BREAKAWAY WIRE. PLACARDS INSTALLED. ACFT - [SDR ABXA20260622274](https://openairdocs.org/sdr/ABXA20260622274), Jun 22, 2026: WARNING MESSAGE. ILLUMINATED. AFTER PUSHBACK, DURING TAXI, LT REV ISLN VALVE. RETURNED TO GATE (BTB). PLACED LEFT T/R ON DI PER MEL 78-31-1 MBCB 07/02/2026 PLACARD INSTALLED A/C DOWNGRADED T - [SDR ABXA20260619271](https://openairdocs.org/sdr/ABXA20260619271), Jun 19, 2026: FIRE LOOP. FAULTED. LT ENG FIRE LP 1, STATUS MESSAGE IN FLIGHT ACFT LANDED NO PROBLEMS, MTX GROUNDED ACFT AND DEFERRED LP 1 LOOP IAW MEL ABX-26-11-1-1 AND RETURNED A/C TO SERVICE. - [SDR ABXA20260616263](https://openairdocs.org/sdr/ABXA20260616263), Jun 16, 2026: EXTINGUISHER. DAMAGED. DURING CREW PREFLIGHT, CREW SAID THE RT PORTABLE FIRE EXTINGUISHER BY LAV MOUNTED ON GROUND HAD A CROOKED PRESSURE GAUGE AND WAS WORRIED IT COULD RUPTURE IN FLI - [SDR ABXA20260427178](https://openairdocs.org/sdr/ABXA20260427178), Apr 27, 2026: ACTUATOR. MALFUNCTIONED. RUDDER RATIO EICAS MESSAGE ON TAXI OUT. REMOVED AND REPLACED RUDDER RATIO CHANGER ACTUATOR IAW B767 AMM 27-21-15 LEAK CHECK GOOD, OPS CHECK GOOD.RAN BOTH ENGINE - [SDR ABXA20260424172](https://openairdocs.org/sdr/ABXA20260424172), Apr 24, 2026: EEC. FAULTED. DURING TAXI, ON ENGINE START BOTH EEC TO ALT W/ L & R ENG EEC MODE EICAS MESSAGES. CREW RETURNED TO THE GATES (BTB). MTC DEFERRED IAW MEL 73-21-1-3 NO MX ACTION - [SDR ABXA20260422170](https://openairdocs.org/sdr/ABXA20260422170), Apr 22, 2026: PITOT TUBE. DEFECTIVE. AFTER ENGINE START AND TAXI OUT, CAPT PITOT ANNUNCIATOR AND EICAS MESSAGE. CREW RETURNED TO BLOCKS (BTB). MAINTENANCE REMOVED AND REPLACED CAPT PITOT IAW B767 A - [SDR 2026F00020](https://openairdocs.org/sdr/2026F00020), Mar 3, 2026: SKIN. CRACKED. EXTERIOR FUSELAGE SKIN ONLY IS CRACKED AT ONE FASTENER HOLE LOCATED L1 DOOR CUT OUT AFT CORNER STA 335 JUST ABOVE STR 20L(VERIFIED WITH HFEC).REPAIRED EXTERIOR - [SDR ABXA20260221074](https://openairdocs.org/sdr/ABXA20260221074), Feb 21, 2026: RELAY. FAULTED. L AUX PITOT EICAS MSG DURING TAXI OUT, AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX . REMOVED AND REPLACED L AUX PITOT IAW B767 AMM 34-11-01 OPS AND LEAK - [SDR ABXA20251122306](https://openairdocs.org/sdr/ABXA20251122306), Nov 22, 2025: SENSOR. FAULTED. RIGHT ENGINE CONTROL EICAS MESSAGE AFTER PUSHBACK FROM GATE AFTER ENGINE START, ACFT RETURNED TO GATE (BTB), AND MTX GROUNDED ACFT, MTX TROUBLESHOT & PERFORMED - [SDR ABXA20250419082](https://openairdocs.org/sdr/ABXA20250419082), Apr 19, 2025: INDICATOR. UNRELIABLE. DURING CLIMB, AIRSPEED UNRELIABLE / STUCK AT 270 KTS INDICATION OF OVERSPEED WITH FLAPS & GEAR UP AT 270 KTS. EMERGENCY DECLARED, AIR TURN BACK. (ATB) . MAINTEN - [SDR UIEA2025031900344](https://openairdocs.org/sdr/UIEA2025031900344), Mar 15, 2025: FITTING. CORRODED. HORIZONTAL STABILIZER PIVOT FITTING RH UPPER ATTACHMENTS, TWO HOLES WITH CORROSION. SEE NDT INSPECTION REPORT.(

TWO HOLES WITH CORROSION AT HORIZONTAL STABILI - [SDR UIEA2025031900343](https://openairdocs.org/sdr/UIEA2025031900343), Mar 15, 2025: SKIN. PUNCTURED. PUNCTURE DAMAGE TO UPPER SPOILER SKIN 6, REPAIR AS REQUIRED.(

UPPER SPOILER SKIN 6 WAS REPAIRED I.A.W B767 SRM 57-70-01-2R-1 AND SRM 51-70-04-0G-0 PAR 5 B AND - [SDR UIEA2025031900342](https://openairdocs.org/sdr/UIEA2025031900342), Mar 15, 2025: SUPPORT. CORRODED. LH WING INBOARD FLAP TRACK #3 SUPPORT AFT ATTACHMENT HOLES, BORE WITH CORROSION (4EA).(

LH WING INBOARD FLAP TRACK #3 SUPPORT AFT ATTACHMENT HOLES WERE REPAIR - [SDR UIEA2025031900341](https://openairdocs.org/sdr/UIEA2025031900341), Mar 15, 2025: FITTING. CORRODED. HORIZONTAL STABILIZER PIVOT FITTING RH LOWER ATTACHMENTS, HOLE WITH CORROSION. SEE NDT INSPECTION REPORT.(

HOLE WITH CORROSION AT HORIZONTAL STABILIZER PIVOT - [SDR UIEA2025031900340](https://openairdocs.org/sdr/UIEA2025031900340), Mar 15, 2025: PACKING. LEAKING. RH WING, PDU SLATS, HYDRAULIC MOTOR WITH EVIDENCE OF HYD LEAK.(

RH WING PDU HYD MOTOR PACKING WAS REPLACED AND LINES WERE TIGHTEN I.A.W AMM 27-81-11-424-029 R - [SDR UIEA2025031900339](https://openairdocs.org/sdr/UIEA2025031900339), Mar 15, 2025: BUSHING. CORRODED. HORIZONTAL STAB, RH PIVOT PIN, SLEEVE WITH CORROSION.(

HORIZONTAL STAB RH PIVOT PIN SLEEVE WAS REPLACED WITH NR00439 IAW SRM 51-10-02-0G-0 REV 12 - [SDR UIEA2025031900338](https://openairdocs.org/sdr/UIEA2025031900338), Mar 15, 2025: LONGERON. CORRODED. AFT CARGO COMPARTMENT, BTW STA 1065 AND 1087, STRG 23L AND 24L, LONGERON WITH CORROSION, L=4" W=1.580".(

AFT CARGO COMPARTMENT, BTW STA 1065 AND 1087, STRG 23 - [SDR UIEA2025031900337](https://openairdocs.org/sdr/UIEA2025031900337), Mar 15, 2025: SUPPORT. CORRODED. RIGHT WING TRAILING EDGE OUTBOARD FLAP SUPPORT #7, SUPPORT ACTUATOR HOLE WITH CRACK INDICATION AT 6 O´CLOCK APPROX.(

RIGHT WING TRAILING EDGE OUTBOARD FLAP S - [SDR UIEA2025031940336](https://openairdocs.org/sdr/UIEA2025031940336), Mar 15, 2025: SUPPORT. CORRODED. RIGHT WING TRAILING EDGE OUTBOARD FLAP SUPPORT #8, SUPPORT ACTUATOR HOLE WITH CORROSION INDICATION.(

RIGHT WING TRAILING EDGE OUT BOARD FLAP SUPPORT #8, SUPPO - [SDR UIEA2025031200280](https://openairdocs.org/sdr/UIEA2025031200280), Mar 15, 2025: SKIN. DAMAGED. DURING THE REMOVAL OF SLAT #6 FOR REPAIR (NR 00005), HIDDEN DAMAGE WAS FOUND ON LH WING FIXED LEADING EDGE AT RIB LES 351.10, WITH EXCESSIVE WEAR AND HOLE.(

O - [SDR UIEA2025031200279](https://openairdocs.org/sdr/UIEA2025031200279), Mar 15, 2025: CASE. CORRODED. ENG 2, FAN CASE, AT 6' O CLOCK, UNDER STRUT AREA, BASE WITH CORROSION L=2.100" W=1"(

ENG 2, FAN CASE, AT 6' O CLOCK, UNDER STRUT AREA, BASE, CORROSION LEVEL 1 - [SDR UIEA2025031200278](https://openairdocs.org/sdr/UIEA2025031200278), Mar 15, 2025: CASE. CORRODED. ENG 1, AFT FAN CASE, AT 5 TO 6 O'CLOCK APROX, WITH SEVERAL POINTS OF CORROSION (3EA).(

ENG 1, AFT FAN CASE, AT 5 TO 6 O'CLOCK APROX, CORROSIONS LEVEL 1 WAS RE - [SDR UIEA2025031900255](https://openairdocs.org/sdr/UIEA2025031900255), Mar 15, 2025: SKIN. DENTED. LH WING INBOARD TRAILING EDGE FLAP, LOWER AREA UPPER SKIN WITH SEVERAL DENTS.(

ONE DENT WAS REPAIRED IAW SRM 57-53-01-2R-1 PAG.1-7 FIG. 201 SHEET 4 AND SRM 51 - [SDR UIEA2025031900254](https://openairdocs.org/sdr/UIEA2025031900254), Mar 15, 2025: SKIN. PUNCTURED. RH OUTBOARD ELEVATOR, LOWER AND UPPER SKIN WITH A PUNCTURE BTW ELEV STA 200 AND 176, AT 2" FROM TRAILING EDGE.(

RH OUTBOARD ELEVATOR, LOWER AND UPPER SKIN WAS - [SDR UIEA2025031900253](https://openairdocs.org/sdr/UIEA2025031900253), Mar 15, 2025: BEAM. CORRODED. AFT CARGO DOOR, BEAM INNER CHORD, BTW STA 1285 AND STA 1329 STRG 23 WITH CORROSION AROUND FASTENER HOLES (L= 1.250" W=1 ").(

REPAIRED IN ACCORDANCE WITH TRE67 - [SDR UIEA2025031000252](https://openairdocs.org/sdr/UIEA2025031000252), Mar 15, 2025: SKIN. DENTED. LEFT WING, SLAT 6 INBOARD FACE WITH DENT APRX 10€Œ OF OUTBOARD EDGE.(

LEFT WING, SLAT 6 INBOARD FACE WITH DENT APRX 10€Œ OF OUTBOARD EDGE WAS REPAIRED IAW S - [SDR UIEA2025031000251](https://openairdocs.org/sdr/UIEA2025031000251), Mar 15, 2025: SUPPORT. CORRODED. RIGHT WING TRAILING EDGE INBOARD FLAP #5 SUPPORT MECHANISM 6-6 OUTER PIN WITH SEVERAL CORROSION IN THE INNER BORE.(

RIGHT WING TRAILING EDGE INBOARD FLAP #5 S - [SDR UIEA2025031900250](https://openairdocs.org/sdr/UIEA2025031900250), Mar 15, 2025: SKIN. CORRODED. CORROSION ON THE UPPER SKIN OF THE HORIZONTAL STABILIZER CENTER SECTION, RH SIDE.(

THE UPPER SKIN OF THE HORIZONTAL STABILIZER CENTER SECTION, RH SIDE MWAS RE - [SDR UIEA2025031900247](https://openairdocs.org/sdr/UIEA2025031900247), Mar 15, 2025: SKIN. DENTED. SLAT #5, LEADING EDGE EXTERNAL SKIN, LOWER INBOARD EDGE WITH A DENT.(

SLAT #5, LEADING EDGE EXTERNAL SKIN, LOWER INBOARD EDGE DAMAGE WAS REPAIRED IAW. TRE6757 - [SDR UIEA2025031900246](https://openairdocs.org/sdr/UIEA2025031900246), Mar 15, 2025: SKIN. CORRODED. FUSELAGE SECTION 48, APU INTAKE DOOR CUTOUT, UPPER STRIP BROKEN AND WITH CORROSION.(

FUSELAGE SECTION 48, APU INTAKE DOOR CUTOUT, UPPER STRIP WAS REPLACED IAW - [SDR UIEA2025031900244](https://openairdocs.org/sdr/UIEA2025031900244), Mar 15, 2025: SKIN. DAMAGED. RH WING, FIXED LEADING EDGE, BETWEEN WS 538.2 AND WS 564.2 (SLAT # 9, INBOARD MAIN TRACK, CUT OUT) WITH EDGE BROKEN.(

RH WING, FIXED LEADING EDGE, BETWEEN WS - [SDR UIEA2025031900243](https://openairdocs.org/sdr/UIEA2025031900243), Mar 15, 2025: SPACER. CORRODED. HORIZONTAL STABILIZER RH PIVOT PIN, OUTER SPACER WITH CORROSION.(

HORIZONTALSTABILIZER RH PIVOT PIN, OUTER SPACER WAS REPLACED I.A.W AMM 55-17-51-404-013 REV - [SDR UIEA2025031900241](https://openairdocs.org/sdr/UIEA2025031900241), Mar 15, 2025: STRINGER. BROKEN. BULK CARGO COMPARTMENT, BTW STA 1480 AND STA 1502, STRINGER 30L BROKEN.(

BULK CARGO COMPARTMENT, BTW STA 1480 AND STA 1502, STRINGER 30L WAS REPAIRED IAW. TRE - [SDR UIEA2025030800240](https://openairdocs.org/sdr/UIEA2025030800240), Mar 15, 2025: CONTROL MODULE. LEAKING. HORIZONTAL STABILIZER WITH EVIDENCE OF HYDRAULIC LEAKAGE STAB TRIM CONTROL MODULE RH.(

LEAKAGE CHECK IN STAB TRIM CONTROL MODULE RH WAS PERFORMED IAW AMM 29-1 - [SDR UIEA2025031900237](https://openairdocs.org/sdr/UIEA2025031900237), Mar 15, 2025: DOOR FRAME. CORRODED. AFT CARGO COMPARTMENT, CUT OUT LOWER DOOR, BETWEEN STA 1263 AND STA 1285, FRAME WITH CORROSION, L=2", W=1.5".(

AFT CARGO COMPARTMENT, CUT OUT LOWER DOOR, BETW - [SDR UIEA2025031900235](https://openairdocs.org/sdr/UIEA2025031900235), Mar 15, 2025: LENS. BROKEN. SWITCH "MAIN DECK CARGO", LENS BROKEN.(

MAIN DECK CARGO LIGHTS SWITCH LENS WAS REPLACED IAW AMM 33-34-00-900-801 REV 144 22DEC24 MAIN DECK CAR GO LIGHTS SWITC - [SDR UIEA2025031900234](https://openairdocs.org/sdr/UIEA2025031900234), Mar 15, 2025: SKIN. GOUGED. ENG 1, LH SIDE, SKIN ON AFT TORQUE BOX WITH A GOUGE.(

ENG 1, LH SIDE, SKIN ON AFT TORQUE BOX DAMAGE WAS REPAIRED IAW TRE6754205 ISSUED DATE 01MAR25. RDR NUMBE - [SDR UIEA2025031980233](https://openairdocs.org/sdr/UIEA2025031980233), Mar 15, 2025: BRACKET. CORRODED. CORROSION ON PROXIMITY SENSORS BASE SUPPORT (S234, S235) AT FWD BULKHEAD OF NLG WHEEL WELL. (L= 1 IN, W= 2 IN).(

PROXIMITY SENSORS BASE SUPPORT (S234, S235) A - [SDR UIEA2025030800232](https://openairdocs.org/sdr/UIEA2025030800232), Mar 15, 2025: ELEC CONNECTOR. CORRODED. CORROSION ON UPPER CONNECTOR OF PROXIMITY SENSOR S234 AT FWD BULKHEAD OF NLG WHEEL WELL.(

CONNECTOR S234 WAS REPLACED IAW SWPM 20-61-00 REV 88, TEST SATISFACT - [SDR UIEA2025030800230](https://openairdocs.org/sdr/UIEA2025030800230), Mar 15, 2025: LAMP. INOPERATIVE. REF DMI 225254 PARKING BRAKE LIGHT INOP, PARKING BRAKE LIGHTS, PARK BRAKE LIGHT 300 ANTISKID LIGHT VERIFIED OPERATIVE.(

PARK BRAKE LIGHT 300 ANTISKID LIGHT VE - [SDR UIEA2025031980228](https://openairdocs.org/sdr/UIEA2025031980228), Mar 15, 2025: SKIN. DENTED. LEFT WING, OUTBOARD SLAT #1 IN REAR SKIN WITH DENT.(

LEFT WING, SLAT 1 T/E WEDGE, LOWER SURFACE WAS REPAIRED IAW SRM 57- 43-02-2R-1 FIG.201 PAG.2-3 AND SRM 51 - [SDR UIEA2025031960223](https://openairdocs.org/sdr/UIEA2025031960223), Mar 15, 2025: SUPPORT. CRACKED. LEFT WING TRAILING EDGE INBOARD FLAP 4 SUPPORT MECHANISM 6-6 OUTER PIN WITH CRACK INDICATION.(

THE 6-6 OUTER PIN OF THE LH WING INB FLAP SUPPORT #4 WAS REPLAC All 1,002: https://openairdocs.org/model/boeing-767-31k/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.