# Boeing 757-26D

- Type: Aircraft model (FAA registry)
- Registry code: 1384907
- Manufacturer (registry): BOEING
- Model: 757-26D
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 178
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 8
- Page: https://openairdocs.org/model/boeing-757-26d

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 (8)

- [N312AL](https://openairdocs.org/aircraft/N312AL): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), S/N 24472
- [N473AP](https://openairdocs.org/aircraft/N473AP): [L-3 Communications Advanced Aviation LLC](https://openairdocs.org/faa-owner/L-3%20COMMUNICATIONS%20ADVANCED%20AVIATION%20LLC), [Kalispell, MT](https://openairdocs.org/faa-place/MT/Kalispell), S/N 24473
- [N819DX](https://openairdocs.org/aircraft/N819DX): [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC), [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta), built 2004, S/N 33959
- [N820DX](https://openairdocs.org/aircraft/N820DX): [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC), [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta), built 2004, S/N 33960
- [N821DX](https://openairdocs.org/aircraft/N821DX): [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC), [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta), built 2004, S/N 33961
- [N822DX](https://openairdocs.org/aircraft/N822DX): [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC), [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta), built 2005, S/N 33966
- [N823DX](https://openairdocs.org/aircraft/N823DX): [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC), [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta), built 2005, S/N 33967
- [N900PC](https://openairdocs.org/aircraft/N900PC): [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC), [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta), built 1997, S/N 28446

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (1,057, newest 50)

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

- [SDR DALA2026100605525](https://openairdocs.org/sdr/DALA2026100605525), Oct 2, 2026: CONTROL CARD. FAULTED. DIV TO DTW DUE TO RIGHT DUCT LEAK MESSAGE REQUIRING RIGHT BLEED OFF WITH ICING CONDITIONS ENROUTE. T/S IAW FIM 36-10-00. REPLACED CONTROL CARD M691. REPLACED TS
- [SDR DALA2026081604672](https://openairdocs.org/sdr/DALA2026081604672), Aug 8, 2026: INDICATOR. FOD. R1 DOOR KNUCKLE KNOCKER WILL NOT EXTEND WHEN DOOR IS ARMED. FOUND DEBRIS AROUND KNUCKLE KNOCKER. REMOVED DEBRIS. FUNCTION CHKD ARM/DISARMING OF 1R DOOR. FUNCTIO
- [SDR DALA2026070703948](https://openairdocs.org/sdr/DALA2026070703948), Jul 3, 2026: PUMP. FAULTED. ATO- DISCONTINUED TAKEOFF AT 40 KNOTS DUE TO NO ACCELERATION RIGHT ENGINE. INSPECTED 2.5 BLEED SYSTEM WITH NTF. REPLACED FUEL PUMP, FUEL CONTROL, EEC, AND 14TH 
- [SDR DALA2026060903457](https://openairdocs.org/sdr/DALA2026060903457), Jun 8, 2026: SENSOR. DIRTY. R3 SLIDE LIGHT INOPERATIVE. CLEANED SENSORS & INSPECTED. NO DAMAGE NOTED. CLEANED & LUBRICATED GIRT BAR FITTINGS IAW AMM 25-66. SLIDE LIGHT OPERATES NORMAL. (83
- [SDR DALA2026060903456](https://openairdocs.org/sdr/DALA2026060903456), Jun 7, 2026: GIRT BAR. FOD. R3 DOOR SLIDE LIGHT NOT ON WHEN DOOR ARMED. DEBRIS FROM GIRT BAR FITTING. OPS CK GOOD PER B757 AMM 25-66. (8316003) AIRCRAFT WAS GROUNDED
- [SDR DALA2026070603929](https://openairdocs.org/sdr/DALA2026070603929), Jun 4, 2026: UNKNOWN. ODOR. FLIGHT DIVERTED TO YEG, DUE TO AN ODOR IN THE AFT GALLEY. NO GO PROCEDURES AND APU & ENG RUNS. UNABLE TO DUPLICATE. ACFT RTS. (8633913) AIRCRAFT WAS GROUNDED
- [SDR DALA2026052803243](https://openairdocs.org/sdr/DALA2026052803243), May 26, 2026: SLIDE. NO TEST. WHILE PERFORMING TEST 2 SQUIB PANEL, EMER ESCAPE FAILED. REF WORKCARD 2560-9901-RT. R & R RT INFLATION SLIDE BOTTLE AS PER AMDS W/C 2565-4646-RH. ALL OPS CHKS N
- [SDR DALA2026060403382](https://openairdocs.org/sdr/DALA2026060403382), May 23, 2026: TRANSMITTER. FAULTY. DUE TO TAKEOFF CONFIG WARNING FLAPS. REPLACED FLAP LEVER POSITION TRANSMITTER AND FLAP PDU POSITION TRANSMITTER. REPLACED TE FLAP POSITION TRANSMITTER AND FLAP 
- [SDR DALA2026052103119](https://openairdocs.org/sdr/DALA2026052103119), May 20, 2026: LIGHT. BROKEN. SEAT MOUNTED ESCAPE LIGHT BROKEN AT 35ABC. REPLACED EMERG LIGHT HOUSING AT 35ABC. OPS OK PER MM-33-51. (8567983) AIRCRAFT WAS GROUNDED
- [SDR DALA2026051503019](https://openairdocs.org/sdr/DALA2026051503019), May 14, 2026: SIGN. UNSECURE. EXIT SIGN BY ROW 33 IS MISSING. INTERIOR. RESECURED EMERGENCY EXIT SIGN PER IAW AMM 33-51. (1593662) AIRCRAFT WAS GROUNDED
- [SDR DALA2026042702639](https://openairdocs.org/sdr/DALA2026042702639), Apr 25, 2026: ACTUATOR. LEAKING. CREW DECLARED EMERGENCY DURING JAX APPROACH DUE TO DECREASING CTR HYD SYS QTY. REPLACED NBR 12 SPOILER ACTUATOR AND RT ENG HYD FILTER MODULE. (8345644) AIRCRAFT
- [SDR DALA2026041502394](https://openairdocs.org/sdr/DALA2026041502394), Apr 14, 2026: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL AND WASTE PANEL ( INNER SURFACE) BTW STA 1680 TO STA 1700 AND S25R TO S28R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 
- [SDR DALA2026041502393](https://openairdocs.org/sdr/DALA2026041502393), Apr 14, 2026: SKIN. CORRODED. AFTER WASTE PANEL REMOVAL CORROSION WAS FOUND ON FUSELAGE SKIN 1680 TO STA 1700 AND S25R TO S28R AT LOWER FUSELAGE. CORROSION LEVEL 2: FUSELAGE SKIN 1680 TO STA
- [SDR DALA2026041502397](https://openairdocs.org/sdr/DALA2026041502397), Apr 13, 2026: FUSE. FAILED. DURING SVC CHECK FOUND DOOR 4R EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. FOUND ONE BAD FUSE ON PWR SUPPLY. REPLACED FUSE PER B757 AMM 20-60. OPS CHK GOOD PER B7
- [SDR DALA2026041502395](https://openairdocs.org/sdr/DALA2026041502395), Apr 13, 2026: SKIN. CORRODED. DTA MONITOR INSPECTION LOG REF ERA 633487-14. FUSELAGE SKIN, AFT LAV SERVICE PANEL CUTOUT, BS 1680 - 1700, S26R - S29R CORRODED. REF ERA 633487-14. (1542619) AI
- [SDR DALA2026041302338](https://openairdocs.org/sdr/DALA2026041302338), Apr 10, 2026: SIGN. DETACHED. EXIT SIGN ABOVE 2L DOOR FELL OFF. RESECURED EMERGENCY EXIT SIGN ABOVE 2L DOOR AS REQUIRED REF B757 AMM 33-51. OPS CKS GOOD. (8541874) AIRCRAFT WAS GROUNDED
- [SDR DALA2026041302337](https://openairdocs.org/sdr/DALA2026041302337), Apr 10, 2026: PAN. DAMAGED. SECTION I REPAIR TO AFT LAVATORY SERVICE PANEL PAN REQUIRES PART REPLACEMENT PER SECTION II OF ERA 633530-14. (FUSELAGE / ACCESS COVERS / AFT LAV SERVICE PANEL 
- [SDR DALA2026040902275](https://openairdocs.org/sdr/DALA2026040902275), Apr 8, 2026: RESERVOIR. LOW PRESSURE. IN REFERENCE TO AMDS 2040-0191-4L: DURING THE INSTALLATION, LOW PRESSURE ON EMERGENCY POWER RESERVOIR AT 4L DOOR WAS FOUND. EMERGENCY POWER RESERVOIR ASSY WAS R
- [SDR DALA2026040602194](https://openairdocs.org/sdr/DALA2026040602194), Apr 2, 2026: SPRING. FAULTED. AD. A.A. IN REF AMDS 2560-01492-0101 STEP 2: ENGAGEMENT DIMENSION LESS THAN 0.37 INCH ON FWD GIRT BAR SLIDER AT L2 DOOR. SPRINGS ON GIRT BAR SLIDER DOOR 2L WERE
- [SDR DALA2026022301284](https://openairdocs.org/sdr/DALA2026022301284), Feb 21, 2026: RESERVOIR. LOW PRESSURE. DOOR 4R EMERGENCY ASSIST RESERVOIR HAD LOW PRESSURE. R & R DOOR R4 EMERGENCY ASSIST RESERVOIR IAW AMM 52-11. (8862602)
- [SDR DALA2026021901212](https://openairdocs.org/sdr/DALA2026021901212), Feb 18, 2026: RESERVOIR. FAULTED. NEED A LOT FORCE TO CLOSE R1 DOOR. EMERGENCY POWER RESERVOIR AT R1 DOOR WAS REMOVED AND SERVICEABLE EMERGENCY POWER RESERVOIR WAS INSTALLED IAW AMM 52-11-30, LO
- [SDR DALA2026021801144](https://openairdocs.org/sdr/DALA2026021801144), Feb 15, 2026: BATTERY PACK. INOPERATIVE. DURING S/C FOUND EMERGENCY LIGHTS INOP. ABOVE LEFT AFT EMERG.EXIT DOOR AND AFT SERVICE DOOR. LIGHTS M11082, M737,M736. REPLACED BATTERY M11082 AND BATTERY M737.
- [SDR DALA2026021701082](https://openairdocs.org/sdr/DALA2026021701082), Feb 14, 2026: SIGN. DAMAGED. EMERGENCY EXIT SIGN AT L2 DOOR DAMAGED. REPLACED EMERGENCY EXIT SIGN IAW AMM 33-51. (8510603)
- [SDR DALA2026021100999](https://openairdocs.org/sdr/DALA2026021100999), Feb 8, 2026: SNUBBER. OUT OF TOLERANCE. IN REFERENCE TO THE AMDS 2040-0191-1R STEP 7, OUT OF TOLERANCE LENGTH TO THE PIN EXTENSION ON ROTARY SNUBBER FLUID LEVEL L1 DOOR. R & R ROTARY SNUBBER IAW AMM 5
- [SDR DALA2026020600870](https://openairdocs.org/sdr/DALA2026020600870), Feb 5, 2026: POWER SUPPLY. NO TEST. DURING SERVICE CHECK FOUND EMERGENCY LIGHTS INOP FROM SEAT 4DC-MID CABIN LAV. RT OVERWING EXIT SIGNS INOP (SEATROW 26-27DEF ). SEAT 32DEF OVERHEAD EMER LITES 36
- [SDR DALA2026020600868](https://openairdocs.org/sdr/DALA2026020600868), Feb 2, 2026: SNUBBER. OUT OF TOLERANCE. IN REFERENCE TO THE AMDS 2040-0191-1R STEP 7: OUT OF TOLERANCE LENGTH TO THE PIN EXTENSION ON ROTARY SNUBBER FLUID LEVEL R1 DOOR. SUMMARY OF NRC 00105:ROTARY SN
- [SDR DALA2026020200787](https://openairdocs.org/sdr/DALA2026020200787), Feb 2, 2026: FRAME. NO DISCREPANCY. EXISTING FRAME SEGMENT REPAIR WAS FOUND AT BS 1640, BTWN S9 - 19L. TASK CARD 5311-01258-01A, NO CORRECTIVE ACTIONS IS REQUIRED IAW ENGINEERING REPAIR AUTHORIZAT
- [SDR DALA2026012800648](https://openairdocs.org/sdr/DALA2026012800648), Jan 27, 2026: SENSOR. DIRTY. L2 DOOR SLIDE LIGHT DID NOT EXTINGUISH WHEN DISARMED. CLEANED SENSORS & TARGETS, OPS CHECKED IAW AMM 52-11. NO ISSUES NOTED. (7654634)
- [SDR DALA2026012700632](https://openairdocs.org/sdr/DALA2026012700632), Jan 26, 2026: SKIN. DEBONDED. SKIN IS DEBONDED ON INNER SKIN, DAMAGE ALSO TO OUTER SKIN. REMOVED THE DAMAGED ON THE INNER SKIN, CORE & PREVIOUS EXTERNAL SKIN REPAIR AT LOWER PANEL.. PREPPED 
- [SDR DALA2026012100469](https://openairdocs.org/sdr/DALA2026012100469), Jan 19, 2026: INDICATOR. FAULTED. L2 KNUCKLE KNOCKER DID NOT EXTEND, ESCAPE SLIDE ARMED CONDITION INDICATORS. ADJUSTED 2L DOOR KNUCKLE KNOCKER, OPS CKS NORM WITH DOOR ARMED. DIS-ARMED DOOR. (140
- [SDR DALA2026012100468](https://openairdocs.org/sdr/DALA2026012100468), Jan 19, 2026: INDICATOR. FAULTED. L1 DOOR KNUCKLE KNOCKER DID NOT EXTEND, ESCAPE SLIDE ARMED CONDITION INDICATORS. ADJUSTED THE KNUCKLE KNOCKER, OPS CKS NORM WITH DOOR ARMED. DIS-ARMED DOOR. (14
- [SDR DALA2026012000419](https://openairdocs.org/sdr/DALA2026012000419), Jan 19, 2026: SKIN. SCRATCHED. IN REF AMDS 5720-01100-04A STEP 18 , SCRATCH ON FASTENER HOLE NO.7 ON SKIN AND FITTING AT 5 O'CLOCK POSITION AT LT WING. REASON FOR RE-WRITE: AFTER FINAL INSTAL
- [SDR DALA2026012000418](https://openairdocs.org/sdr/DALA2026012000418), Jan 19, 2026: SKIN. SCRATCHED. IN REF AMDS 5720-01100-04A STEP 18, SCRATCH ON FASTENER HOLE NR 7 ON SKIN AND FITTING AT 5 O'CLOCK POSITION AT LT WING. SCRATCH ON FASTENER HOLE NR 7 ON SKIN & 
- [SDR DALA2026012000423](https://openairdocs.org/sdr/DALA2026012000423), Jan 18, 2026: COVER. MISINSTALLED. HARD TO OPERATE (DISARMED- ARMED AT HALF WAY) R2 DOOR SLIDE ACTIVATION HANDLE. GIRT BAR PROXIMITY SWITCH (S10220 AND S10221) COVERS WERE INSTALLED CORRECTLY PER
- [SDR DALA2026012000421](https://openairdocs.org/sdr/DALA2026012000421), Jan 18, 2026: SKIN. DENTED. FUSELAGE DENT BETWEEN BS 620 - 640, STRINGERS 15L-17L. REMOVED SKIN SECTION WHERE DAMAGE WAS LOCATED IAW SRM 53-30 -01-2R-2. PERFORMED HFEC OF CUTOUT & BHEC OF 
- [SDR DALA2026012000417](https://openairdocs.org/sdr/DALA2026012000417), Jan 18, 2026: FRAME. CORRODED. CORROSION ON FRAME BS 1540 BTW S28 & 29R IN AFT CARGO BAY. FRAME BS 1540 BTW S28 & 29R IN AFT CARGO BAY WAS REPAIRED IAW PRI 631344-14, REV 0, AND ER/A 631344-1
- [SDR DALA2026012000425](https://openairdocs.org/sdr/DALA2026012000425), Jan 17, 2026: FRAME. DAMAGED. DTE, ERA 631344-14, AFT CARGO COMPARTMENT FRAME BS 1540, BTW S28R & S29R CORRODED, MONITOR INSPECTION LOG REPAIR TO FUSELAGE FRAME AT BS 1540 BETWEEN STRINGERS 
- [SDR DALA2026011600385](https://openairdocs.org/sdr/DALA2026011600385), Jan 16, 2026: SKIN. NOT REPORTED. ERA 536961-14, MONITOR INSPECTION LOG REPAIR TO C1 DOOR CUTOUT, LOWER FWD CORNER. REF ERA 536961-14AD. (1404006)
- [SDR DALA2026011500349](https://openairdocs.org/sdr/DALA2026011500349), Jan 13, 2026: TRUNNION. CORRODED. COMPLIED WITH PRI 631159-14 REV 0,1,2,3 AND 4 RT WING / MLG FWD TRUNNION SUPPORT FITTING / LOWER BORE CORROSION TO REPLACE FITTING. REPLACED FITTING PER ERA 631
- [SDR DALA2026011300325](https://openairdocs.org/sdr/DALA2026011300325), Jan 12, 2026: ATTACH FITTING. CORRODED. SHIP 6820 LT MLG O/B ATTACH POINT FOR REACTION LINK HAS CORROSION ON UPPER AND LOWER SURFACE ALONG THE SLEEVE. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL 
- [SDR DALA2026012800647](https://openairdocs.org/sdr/DALA2026012800647), Jan 10, 2026: TRUNNION. CORRODED. STAGE 3 TRACKING FOR ER/A 631159-14. RT WING MLG FWD TRUNNION SUPPORT FITTING, LOWER BORE CORRODED AND FITTING REPLACEMENT. REF ERA 631159-14AD. (1395608)
- [SDR DALA2026083104905](https://openairdocs.org/sdr/DALA2026083104905), Jan 9, 2026: SLEEVE. CORRODED. CORROSION ALONG THE BEVELED PART OF THE BEARING SLEEVE. FITTING REPLACED ON NR 18. (1393346)(AIRCRAFT GROUNDED)
- [SDR DALA2026011200292](https://openairdocs.org/sdr/DALA2026011200292), Jan 9, 2026: SKIN. DEBONDED. DEBOND WAS FOUND OF: 3.500 IN X 1.000 IN LENGTH/ WIDTH ON UPPER SURFACE AT TRAILING EDGE WEDGE SLAT #2. OSS: 706 LH WING. DISBOND OF: 3.500 IN X 1.000 IN LENGTH
- [SDR DALA2026010800161](https://openairdocs.org/sdr/DALA2026010800161), Jan 7, 2026: GIRT BAR. FAULTED. ENGAGEMENT LESS THAN 0.37 IN BTW GIRT BAR SLIDER AND FWD FLOOR FITTING AT L4 DOOR IN PAX CABIN. GIRT BAR WAS REPLACED PER AMDS 2561-01257- 01E AND PER B757-200 
- [SDR DALA2026010600110](https://openairdocs.org/sdr/DALA2026010600110), Dec 29, 2025: SNUBBER. OUT OF TOLERANCE. OUT OF LIMITS EXTENSION PIN ON SNUBBER AT R1 DOOR. R1 SNUBBER WAS REPLECED PER SERVICIABLE R1 SNUBBER PER B757-200 AMM 52-11-10 AND DOOR R1 WAS REMOVED/INSTALLE
- [SDR DALA2026010500062](https://openairdocs.org/sdr/DALA2026010500062), Dec 29, 2025: SNUBBER. OUT OF TOLERANCE. OUT OF LIMITS EXTENSION PIN ON SNUBBER AT L2 DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00134, THE L2 SNUBBER WAS REMOVED AND REPLACED PER B757-200 AMM 52-11.
- [SDR DALA2025123009523](https://openairdocs.org/sdr/DALA2025123009523), Dec 29, 2025: FUEL CONTROL. FAULTED. ATB/DE, LEFT ENGINE COMPRESSOR STALL DURING CLIMB. PULLED THROTTLES BACK AND ENGINE WAS STABLE. BORESCOPE COMPLETED WITH NO FINDINGS, REPLACED FCU.
- [SDR DALA2025123009519](https://openairdocs.org/sdr/DALA2025123009519), Dec 27, 2025: UNKNOWN. ODOR. FA REPORTED SMELLING BURN RUBBER OR TAR SMELL COMING FROM AROUND THE 4R DOOR. DEFERRING PER MEL 21-45-03. R/R 4R DOOR HEATER REF AMM 21-45. OPS/LEAK CHK GOOD. (
- [SDR DALA2025123009517](https://openairdocs.org/sdr/DALA2025123009517), Dec 24, 2025: SNUBBER. OUT OF TOLERANCE. OUT OF LIMITS EXTENSI N PIN ON SNUBBER AT L4 DOOR. 4L DOOR ROTARY SNNUBER WAS REPLACED BY SERVICIABLE SNUBBER PER AMM 52- 11-10 ALSO SAME 4L DOOR WAS REMOVED/IN
- [SDR DALA2025122209322](https://openairdocs.org/sdr/DALA2025122209322), Dec 20, 2025: REPAIR. NOT REPORTED. IN REFERENCE TO AMDS 5311-01227-02B STEP 2 , EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA AT STA 1360 STR 26RH. CORRECTIVE ACTION: SUMMARY OF NRC 00054: REP

All 1,057: https://openairdocs.org/model/boeing-757-26d/reports.md

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