# Boeing 767-37D

- Type: Aircraft model (FAA registry)
- Registry code: 13852D5
- Manufacturer (registry): BOEING
- Model: 767-37D
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 375
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 1
- Page: https://openairdocs.org/model/boeing-767-37d

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 (1)

- [N1327A](https://openairdocs.org/aircraft/N1327A): [Msn 26328 LLC](https://openairdocs.org/faa-owner/MSN%2026328%20LLC), [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase), built 1996, S/N 26328

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (317, newest 50)

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

- [SDR ABXA20260921415](https://openairdocs.org/sdr/ABXA20260921415), Sep 21, 2026: IDG. FAULTED. DURING ENGINE START AND TAXI, L ENG GEN DRIVE & DISC. CREW RETURNED TO THE GATE (BTB). MTC DEFERRED LT ENGINE IDG IAW MEL 24-00-1-1. MBCB 09/24/26. REF ITEM 2, 
- [SDR ABXA20260816363](https://openairdocs.org/sdr/ABXA20260816363), Aug 16, 2026: SENSE LINE. LOOSE. DURING TAXI RT ENG BLEED OFF AND RT PACK OFF EICAS MESSAGE APPEARED A/C RETURNED TO GATE(BTB) AND MTX GROUNDED ACFT AND FOUND PRVC SENSE LINE LOOSE, RESECURED L
- [SDR ABXA20260814361](https://openairdocs.org/sdr/ABXA20260814361), Aug 14, 2026: START VALVE. MALFUNCTIONED. DURING TAXI OUT ATTEMPTED TO START NR 1 ENGINE, N2 ADVANCED TO 26% BUT VALVE LIGHT ON L STAYED ILLUMINATED ATTEMPTED 2ND TIME, SAME ISSUE, ACFT RETURNED TO GATE
- [SDR ABXA20260808356](https://openairdocs.org/sdr/ABXA20260808356), Aug 8, 2026: A/C PACK. INOPERATIVE. DURING ENGINE START, L PACK INOP. CREW RETURNED TO THE GATE (BTB). MTC RESET L PACK PNUEMATIC SYS IAW AMM 21-00-00 NO DEFECTS NOTED AT THIS TIME L PACK OPERATIO
- [SDR ABXA20260714319](https://openairdocs.org/sdr/ABXA20260714319), Jul 14, 2026: STARTER. INOPERATIVE. DURING TAXI OUT WHILE STARTING RH ENGINE, RH STARTER WAS INOP. A/C RETURNED TO THE GATE (BTB) AND MX GROUNDED A/C. MTX EXERCISED RH START VALVE AND PERFORMED OP
- [SDR ABXA20260611254](https://openairdocs.org/sdr/ABXA20260611254), Jun 11, 2026: CONTROLLER. DEFECTIVE. DURING TAXI, CREW RECEIVED R ENG BLEED OFF R PACK OFF NO R DUCT PRESSURE. CREW RETURNED TO THE GATE (BTB). MTX TROUBLE SHOT AND REMOVED AND REPLACED PRV CONTROL
- [SDR ABXA20260516212](https://openairdocs.org/sdr/ABXA20260516212), May 16, 2026: HINGE ARM. FAILED. DURING CREW PREFLIGHT, LEFT UPPER STORAGE BIN DOOR HINGE ARM FAILED. DEFERRED LEFT OVERHEAD STORAGE BIN SHOCK BIN SHOCK STRUT IAW ABX MEL 25-28-1A. DUE TO OVERH
- [SDR ABXA20260429182](https://openairdocs.org/sdr/ABXA20260429182), Apr 29, 2026: FLAP SYSTEM. FAULTED. DURING DESCENT, LE SLAT DISAGREE LIGHT ILLUMINATED AFTER SELECTING FLAPS 25. CREW EXECUTED A MISSED APPROACH. FOLLOWED QRH PROCEDURES AND LANDED WITH FLAPS 20. 
- [SDR ABXA202604264173](https://openairdocs.org/sdr/ABXA202604264173), Apr 24, 2026: START VALVE. FAULTED. DURING TAXI OUT WHILE STARTING NR 1 ENGINE NO ROTATION ON NR 1, START VALVE STAYED OPEN , A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C AND DEFERRED NR 1 
- [SDR ABXA20260423171](https://openairdocs.org/sdr/ABXA20260423171), Apr 23, 2026: FLAP SYSTEM. WARNING MESSAGE. DURING TAXI, TE FLAP DISAGREE WHEN MOVING TO FLAPS 5 ON THE AFTER START CHECKLIST. CREW RETURNED TO BLOCK (BTB). MTC PERFORMED FIM 27-51 FT 811, RESET BY PASS L
- [SDR ABXA20260331142](https://openairdocs.org/sdr/ABXA20260331142), Mar 31, 2026: ELEC CONNECTOR. FAULTED. PILOT REPORTED CARGO FIRE A 4 AMBER INDICATION. RESET ELECTRICAL CONNECTOR. ON BOX. ERROR CLEARED. OPS CHK GOOD. IAW B767 AMM 26-16-00. THIS CLEARS THE DI. PLAC
- [SDR ABXA20260313107](https://openairdocs.org/sdr/ABXA20260313107), Mar 13, 2026: WARNING MESSAGE. FALSE ACTIVATION. DURING APPROACH INTO MIA, LANDING CONFIG WARNING LIGHT ILLUMINATED AT 3000 FT AGL. FLAPS WERE AT 15 AND GEAR LEVER IN OFF POSITION. CAPTAIN DID A GO AROUND AND 
- [SDR ABXA20260206052](https://openairdocs.org/sdr/ABXA20260206052), Feb 6, 2026: A/C PACK. INOPERATIVE. DURING TAXI OUT AND AFTER START CHECKLIST, L PACK OFF EICAS DISPLAYED QRH PROCEDURE UNSUCCESSFUL. AIRCRAFT RETURNED TO BLOCKS (BTB). TRANSFERED LH PACK TO DI IA
- [SDR ABXA20260116013](https://openairdocs.org/sdr/ABXA20260116013), Jan 16, 2026: FIRE LOOP. FALSE INDICATION. DURING MAINTENANCE INSPECTION, LT ENG OH LP1 EICAS MSG. PLACED ENG OH LP 1 ON DEFERRAL IAW MEL 26-11-2-1 MBCB 01/26/2026 AIRCRAFT ETOPS 120 PLACARD ROTATED. AIR
- [SDR ABXA20251216342](https://openairdocs.org/sdr/ABXA20251216342), Dec 16, 2025: SMOKE DETECTOR. DEFECTIVE. DURING MAINTENANCE INSPECTION, EICAS MSG AFT CARGO DET NR 1 ILLUMINATED. DEFERRED PER MEL 26-16-1-1-1. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR NR 1 PER AM
- [SDR ABXA20250823195](https://openairdocs.org/sdr/ABXA20250823195), Aug 23, 2025: SUPPORT FITTING. CORRODED. DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS. #2 FITTINGS TOTAL WERE FOU
- [SDR ABXA20250823194](https://openairdocs.org/sdr/ABXA20250823194), Aug 23, 2025: SUPPORT FITTING. CORRODED. DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS. #3 FITTINGS TOTAL WERE FOU
- [SDR ABXA20250823193](https://openairdocs.org/sdr/ABXA20250823193), Aug 23, 2025: SUPPORT FITTING. CORRODED. DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS. #4 FITTINGS TOTAL WERE FOU
- [SDR ABXA20250823192](https://openairdocs.org/sdr/ABXA20250823192), Aug 23, 2025: SUPPORT FITTING. CORRODED. DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS. #5 FITTINGS TOTAL WERE FOU
- [SDR ABXA20250823191](https://openairdocs.org/sdr/ABXA20250823191), Aug 23, 2025: SUPPORT FITTING. CORRODED. DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS.# 6 FITTINGS TOTAL WERE FOU
- [SDR ABXA20250823190](https://openairdocs.org/sdr/ABXA20250823190), Aug 23, 2025: SUPPORT FITTING. CORRODED. DURING THE C-6 MAINT VISIT, CORROSION FOUND ON LT HORIZONTAL STAB LOWER BLADE SEAL SUPPORT FITTINGS. NR 7 FITTINGS TOTAL WERE FOUND TO HAVE CORROSION BETWEEN TH
- [SDR ABXA20250823189](https://openairdocs.org/sdr/ABXA20250823189), Aug 23, 2025: SKIN. DAMAGED. DURING THE CURRENT C-6 HEAVY MAINTENANCE CHK, MAINT FOUND AT BS 871.5, RT FWD OVERWING EMERG EXIT DOOR HAD NICK DAMAGE ABOVE WINDOW-PLUG CUTOUT. FASTENERS REMOV
- [SDR ABXA20250823188](https://openairdocs.org/sdr/ABXA20250823188), Aug 23, 2025: PANEL. DAMAGED. DURING THE C-6 MAINTENANCE CHECK, THE NR 2 ENGINE PYLON PANEL ASSEMBLY WAS FOUND TO BE DAMAGED BEYOND REPAIR. MAINTENANCE FABRICATED A NEW PANEL. ACCORDING TO B
- [SDR ABXA20250823187](https://openairdocs.org/sdr/ABXA20250823187), Aug 23, 2025: DOOR FRAME. CORRODED. DURING C6 CHECK AT HACECO INSPECTION FOUND E&E DOOR CUTOUT FWD FRAME WEB STA303 HAS PUNCTURE REMOVED ANGLE SUPPORT RAIL IAW B767 SRM 51-40-02, REMOVED DAMAGE IA
- [SDR ABXA20250410074](https://openairdocs.org/sdr/ABXA20250410074), Apr 11, 2025: TCAS SYSTEM. FAULTED. DURING PUSHBACK GOT TCAS EICAS MSG. A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C, MTX DEFERRED TCAS FOR DEPARTURE IAW MEL ABX-34-45-1A. AND RETURNED A/C TO S
- [SDR ABX2025F00001](https://openairdocs.org/sdr/ABX2025F00001), Apr 6, 2025: AUTOTHROTTLE SYS. WARNING MESSAGE. ON TAXI OUT, AUTO THROTTLE DISC LIGHT & AUTO THROTTLE DISC EICAS MESSAGE ILLUMINATED. A/C RETURNED TO BLOCKS (BTB). DEFERRED AUTO THROTTLE IAW MEL ABX-22-30-1. 
- [SDR ABXA20241012187](https://openairdocs.org/sdr/ABXA20241012187), Oct 12, 2024: ISOLATION VALVE. FAULTED. DURING TAXI R ISLN VALVE LIGHT ON, NO AIR FOR START AC RETURNED TO GATE AND MAITENANCE GROUNDED AC. MTX CYCLED RIGHT ISOLATION VALVE 3 TIMES SUCCESSFULLY PER AM
- [SDR ABXA20240919177](https://openairdocs.org/sdr/ABXA20240919177), Sep 19, 2024: PRESSURE SWITCH. FAULTED. AT ROTATION ON TAKEOFF EICAS MSG C HYD SYS PRESS APPEARED AND AC PERFORMED ATB , AND AFTER LANDING MTX GROUNDED AC AND TROUBLE SHOT TO A CTR HYD PRESSURE SWITCH
- [SDR UIEA2024031700155](https://openairdocs.org/sdr/UIEA2024031700155), Mar 18, 2024: TAPE. DAMAGED. COCKPIT ELT TAPE DAMAGED. PER MCC REGISTERED WITH NOAA PER ENGINEERING DEPARTMENT IAW AMM 25-63-03. DMI 204893 CLOSED.
- [SDR UIEA2024031700154](https://openairdocs.org/sdr/UIEA2024031700154), Mar 17, 2024: ELT. UNKNOWN. CAPT REPORTED GALLEY ELT NOT TAPED CORRECTLY(<P>R/R GALLEY PORTABLE ELT IAW AMM 25-63-03 PART EFECTIVITY AIPC 25-63-52-97 ITEM 600. NO FURTHER DEFECTS NOTED. TH
- [SDR UIEA2024031800156](https://openairdocs.org/sdr/UIEA2024031800156), Mar 17, 2024: SIGN. DETACHED. OBSERVED L1 EMERGENCY EXIT SIGN TO BE DISPLACED(<P>RE-SECURED EMERGENCY EXIT SIGN / LIGHT PER AMM 33-51-01. OPS CHCKS GOOD AT THIS TIME.&NBSP;</P>)
- [SDR UIEA2024010500006](https://openairdocs.org/sdr/UIEA2024010500006), Jan 5, 2024: GUARD. UNKNOWN. EMER LIGTHS GUARD SWITCH DOES NOT STAY CLOSED OR SNAPS CLOSED(<P>REMOVED AND REPLACED EMERGENCY LIGHTS GUARD PER AMM 20-11-00 AND 33-51-00-08-01B. OPS CHECKS GO
- [SDR UIEA2023122101009](https://openairdocs.org/sdr/UIEA2023122101009), Dec 19, 2023: FIRST AID KIT. UNKNOWN. FOUND RED TAG MISSING ON FIRST AID KIT(<P>REMOVED AND REPLACED FIRST AID KIT IAW AMM 25-64-03. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023100500863](https://openairdocs.org/sdr/UIEA2023100500863), Oct 11, 2023: UNKNOWN. UNKNOWN. DELAMINATION ON PREVIOUS REPAIR AT RUD STA 106.142 RUDDER TRAILING EDGE RH.(<P>RUDDER TRAILING EDGE RH AT RUD STA 106.142 WAS REPAIRED IAW SRM 55-40-01-2R-1 FIG
- [SDR UIEA2023100500864](https://openairdocs.org/sdr/UIEA2023100500864), Oct 11, 2023: UNKNOWN. UNKNOWN. LIGHTNING STRIKE ON FASTENER HEAD AT STA 212.5 AND BELOW RBL 15, UPPER HALF FUSELAGE EXTERIOR.(<P>LIGHTNING STRIKE ON FASTENER HEAD AT STA 212.5 AND BELOW RBL 1
- [SDR UIEA2023100500865](https://openairdocs.org/sdr/UIEA2023100500865), Oct 11, 2023: UNKNOWN. UNKNOWN. LIGHTNING STRIKE ON FASTENER HEAD AT STA 287 AND 3" BELOW STGR 3 OF UPPER HALF OF FUSELAGE EXTERIOR.(<P>LIGHTNING STRIKE ON FASTENER HEAD AT STA 287 AND 3" BELO
- [SDR UIEA2023100500866](https://openairdocs.org/sdr/UIEA2023100500866), Oct 11, 2023: PCA. UNKNOWN. OUT OF LIMITS FREE PLAY ON OUTBOARD PCA OF RH ELEVATOR.(<P>OUTBOARD PCA OF RH ELEVATOR WAS REPLACED, ADJUSTED AND LEAK CHECK WAS SATISFACTORY IAW AMM 27-31-05-4
- [SDR UIEA2023100500867](https://openairdocs.org/sdr/UIEA2023100500867), Oct 11, 2023: PCA. UNKNOWN. OUT OF LIMITS FREE PLAY ON OUTBOARD PCA OF LH ELEVATOR.(<P>N/R: 00028. OUTBOARD PCA OF LH ELEVATOR. WAS REPLACED, ADJUSTED AND TIGHTENED IAW AMM 27-31-05-424-02
- [SDR UIEA2023100500868](https://openairdocs.org/sdr/UIEA2023100500868), Oct 11, 2023: PCA. UNKNOWN. OUT OF LIMITS FREE PLAY ON MIDDLE PCA OF LH ELEVATOR.(<P>MIDDLE PCA OF LH ELEVATOR WAS REPLACED, ADJUSTED AND TIGHTENED IAW AMM 27-31-05-424-027 &AMP; 27-31-00-
- [SDR UIEA2023100500869](https://openairdocs.org/sdr/UIEA2023100500869), Oct 11, 2023: HOSE. UNKNOWN. FUSELAGE SECTION 43, AREA ABOVE CEILING AT STA 544, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 43, AREA ABOVE CEILING AT STA 544, SMOKE
- [SDR UIEA2023100500870](https://openairdocs.org/sdr/UIEA2023100500870), Oct 11, 2023: O-RING. UNKNOWN. RH WING OVERWING PORT FUEL LEAK(<P>RH WING OVERWING PORT O-RINGS WERE REPLACED IAW AMM TASK 28-11-04-404-019 REV 140 DATE 22 AUG 23. LEAK TEST WAS PERFORMED, NO
- [SDR UIEA2023100500871](https://openairdocs.org/sdr/UIEA2023100500871), Oct 11, 2023: HOSE. UNKNOWN. FUSELAGE SECTION 43, AREA ABOVE CEILING AT STA 610, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 43, AREA ABOVE CEILING AT STA 610, SMOKE
- [SDR UIEA2023100500872](https://openairdocs.org/sdr/UIEA2023100500872), Oct 11, 2023: HOSE. UNKNOWN. FUSELAGE SECTION 43, AREA ABOVE CEILING BTW STA 654+66 AND STA 654+88, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 43, AREA ABOVE CEILIN
- [SDR UIEA2023100500873](https://openairdocs.org/sdr/UIEA2023100500873), Oct 11, 2023: HOSE. UNKNOWN. FUSELAGE SECTION 46, AREA ABOVE CEILING BTW STA 1307 AND STA 1329, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 46, AREA ABOVE CEILING BT
- [SDR UIEA2023100500874](https://openairdocs.org/sdr/UIEA2023100500874), Oct 11, 2023: HOSE. UNKNOWN. FUSELAGE SECTION 46, AREA ABOVE CEILING BTW STA 1461 AND STA 1480, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 46, AREA ABOVE CEILING BT
- [SDR UIEA2023100500875](https://openairdocs.org/sdr/UIEA2023100500875), Oct 11, 2023: HOSE. UNKNOWN. FUSELAGE SECTION 46, AREA ABOVE CEILING AT STA 1395, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 46, AREA ABOVE CEILING AT STA 1395, SMO
- [SDR UIEA2023100500876](https://openairdocs.org/sdr/UIEA2023100500876), Oct 11, 2023: COMPUTER. UNKNOWN. STABILIZER TORSION BOX. INTERNAL STRUCTURE, ELEVATOR FUEL COMPUTER BETWEEN STA 1702 AND STA 1725.5. WITH SEVERAL LINES WITH HYD LEAK.(<P>ELEVATOR FEEL COMPUTER 
- [SDR UIEA2023100500877](https://openairdocs.org/sdr/UIEA2023100500877), Oct 11, 2023: ACTUATOR. UNKNOWN. STABILIZER TORSION BOX. INTERNAL STRUCTURE BETWEEN STA 1809.5 AND STA 1832, FEEL ACTUATOR WITH EVIDENCE LEAK.(<P>THE FEEL ACTUATOR WAS REPLACED, WAS TIGHTENED A
- [SDR UIEA2023100600878](https://openairdocs.org/sdr/UIEA2023100600878), Oct 11, 2023: UNKNOWN. UNKNOWN. FUEL LEAK ON REAR SPAR SPLICE FITTING AND BBR 97.42 AT CENTER TANK.(<P>FUEL LEAK ON REAR SPAR SPLICE FITTING AND BBR 97.42 AT CENTER TANK WAS REPAIRED AND THE T
- [SDR UIEA2023100600879](https://openairdocs.org/sdr/UIEA2023100600879), Oct 11, 2023: ANGLE. UNKNOWN. BULK CARGO COMPARTMENT, FLOOR LEVEL. LH SIDE ANGLE WITH CORROSION AT B.STA 1417 LBL41.(<P>&NBSP;</P> / <P>BULK CARGO COMPARTMENT, FLOOR LEVEL. LH SIDE ANGLE, AT

All 317: https://openairdocs.org/model/boeing-767-37d/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.