# Service difficulty reports: N584NW

A list on [N584NW](https://openairdocs.org/aircraft/N584NW.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 185 reports

- [SDR DALA2026091605167](https://openairdocs.org/sdr/DALA2026091605167.md): Light · inoperative · Sep 7, 2026 · N584NW · Boeing 757351 · Emergency Lighting
  > EMERGENCY LIGHT ON 26D INOP. R & R EMER LIGHT ON 26D PER AMM 33-52. OPS CHK GOOD. OK FOR SVC (9324548)(AIRCRAFT GROUNDED)
- [SDR DALA2026073104428](https://openairdocs.org/sdr/DALA2026073104428.md): Transmission · faulted · Jul 29, 2026 · N584NW · Boeing 757351 · Trailing Edge Flap Control System
  > DE/FCNT- DUE T/E FLAP DISAGREE MESSAGE. REPLACED NUMBER 8 FLAP TRANSMISSION AND DRAINED AND SERVICED ALL OTHER FLAP TRANSMISSIONS.(1727228)(AIRCRAFT GROUNDED)
- [SDR DALA2026072804354](https://openairdocs.org/sdr/DALA2026072804354.md): Warning Message · false activation · Jul 24, 2026 · N584NW · Boeing 757351 · Trailing Flap Position Indicating System
  > DE/FCNT- DUE T/E FLAP DISAGREE MESSAGE. T/S PER FIM. INSPECTED TORQUE LIMITERS. CHECKED ADJUSTMENT OF FLAP TRANSMITTERS. RAN FLAPS THROUGH SEVERAL CYCLES. SYSTEM OPERATES NORMAL.(9207254)(AIRCRAFT GROUNDED)
- [SDR DALA2026072004253](https://openairdocs.org/sdr/DALA2026072004253.md): Test Switch · faulted · Jul 19, 2026 · N584NW · Boeing 757351 · Emergency Lighting
  > EMERGENCY LIGHTS ON & FLICKERING IN THE ARMED POSITION. REPLACED THE EMERGENCY LIGHT TEST SWITCH, S10295 IAW AMM 33-51 AND CHKD GOOD. (LP 9207226 - AIRCRAFT WAS GROUNDED).
- [SDR DALA2026060603411](https://openairdocs.org/sdr/DALA2026060603411.md): Engine · power loss · Jun 6, 2026 · N584NW · Boeing 757351 · Engine (Turbine/Turboprop)
  > ATO- DISCONTINUED TAKEOFF AT 15 KNOTS DUE TO NO ACCEL ON THE RIGHT ENGINE. REPLACED RIGHT ENGINE. (LP 6457816, 1630475 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051303004](https://openairdocs.org/sdr/DALA2026051303004.md): Shim · missing · May 12, 2026 · N584NW · Boeing 757351 · Escape Slide
  > MISSING SHIM FROM RT OFF WING INFLATION LINE FLANGE. INSTALLED NEW SHIM IAW AMM 25-65. (1589489) AIRCRAFT WAS GROUNDED
- [SDR DALA2026032702039](https://openairdocs.org/sdr/DALA2026032702039.md): Skin · cracked · Mar 25, 2026 · N584NW · Boeing 757351 · Fuselage Main, Plate/Skin
  > DTA MONITOR INSPECTION LOG REF ERA 632608-14 FUSELAGE SKIN, BS 890 - 900, S26L - S28L CRACKED AND CORRODED. REF ERA 632608-14. (1511712)
- [SDR DALA2026032702036](https://openairdocs.org/sdr/DALA2026032702036.md): Skin · corroded · Mar 25, 2026 · N584NW · Boeing 757351 · Fuselage Main, Plate/Skin
  > CORROSION BTW FUSELAGE SKIN AND TRAY OF LAVATORY SERVICE DOOR. CORROSION LEVEL 2. AREA BTW FUSELAGE SKIN AND TRAY OF LAVATORY SERVICE DOOR WAS REPAIRED PER ER/A 632678- 14 REV ORIGINAL SECTION I. (1512314)
- [SDR DALA2026032702035](https://openairdocs.org/sdr/DALA2026032702035.md): Skin · corroded · Mar 25, 2026 · N584NW · Boeing 757351 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN BTW STA. 890 TO 900 ANS BTW S-28L TO S-27L AT FWD CARGO COMPARTMENT. CORROSION LEVEL 2. CORROSION ON FUSELAGE SKIN BTW STA. 890 TO 900 ANS BTW S-28L TO S-27L AT FWD CARGO COMPARTMENT WAS REPAIRED PER PRI 632608-14 REV 7 AND ERA 632
- [SDR DALA2026032702034](https://openairdocs.org/sdr/DALA2026032702034.md): Skin · mechanic error · Mar 25, 2026 · N584NW · Boeing 757351 · Fuselage Main, Plate/Skin
  > MAINTENANCE ERROR: MISDRILLED HOLE ON OUTER SKIN AND STRAP STA 900 AND BELOW S-26L AT LOWER FUSELAGE. AREA ON OUTER SKIN AND STRAP STA 900 AND BELOW S-26L AT LOWER FUSELAGE. WAS REPAIRED PER PRI 632608-14 REV 7 AND ERA 632608-14 REV ORIGINAL SECTION I. (1511
- [SDR DALA2026032702033](https://openairdocs.org/sdr/DALA2026032702033.md): Skin · mechanic error · Mar 25, 2026 · N584NW · Boeing 757351 · Fuselage Main, Plate/Skin
  > MAINTENANCE ERROR IN REF. TO NRC 00608. ELONGATE HOLES (36 EAS) ALONG TO REPAIR AREA BTW STA. 820 TO 900 AND S-28L TO S25L AT EXTERNAL FUSELAGE SKIN. ELONGATE HOLES (36 EAS) ALONG TO REPAIR AREA BTW STA. 820 TO 900 AND S-28L TO S25L AT EXTERNAL FUSELAGE SKIN
- [SDR DALA2026032702032](https://openairdocs.org/sdr/DALA2026032702032.md): Skin · cracked · Mar 25, 2026 · N584NW · Boeing 757351 · Fuselage Main, Plate/Skin
  > IN REF NRC 00454: AFTER CORROSION WERE REMOVED, CRACK WAS FOUND ON FUSELAGE SKIN BTW STA. 890 TO 900 ANS BTW S-28L TO S-27L AT FWD CARGO COMPARTMENT (AFT BULKHEAD). AREA ON FUSELAGE SKIN BTW STA. 890 TO 900 ANS BTW S-28L TO S-27L AT FWD CARGO COMPARTMENT (AF
- [SDR DALA2026032702031](https://openairdocs.org/sdr/DALA2026032702031.md): Stringer · corroded · Mar 25, 2026 · N584NW · Boeing 757351 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 29R BTW STA 1480 TO STA 1521 AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2. STRINGER 29R BTW STA 1480 TO STA 1521 AT AFT CARGO COMPARTMENT WAS REPLACE PER ERA 568978-14 REV. B SECTION I: PERMANENT REPAIR. (1511796)
- [SDR DALA2026032301936](https://openairdocs.org/sdr/DALA2026032301936.md): Frame · corroded · Mar 21, 2026 · N584NW · Boeing 757351 · Fuselage Main, Frame
  > CORROSION ON FRAME (PREVIOUS REPAIR) BS 1540 AND STR 29R AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2.PREVIOUS REPAIR ON FRAME STA 1540 AND STR 29R AT AFT CARGO COMPARTMENT.WAS REPLACED PER ERA 569126-14AD REV C SECTION I. (1505286)
- [SDR DALA2026032001918](https://openairdocs.org/sdr/DALA2026032001918.md): Floor Support · corroded · Mar 19, 2026 · N584NW · Boeing 757351 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR STRINGERS FROM LBL 16.10 TO RBL 16.10 BTW BS 1460 TO 1521 IN THE AFT CARGO BAY. CORROSION LEVEL 2, PREVIOUS REPAIR AT FLOOR STRINGERS BS 1470, LBL 10.45, LBL 2.90, RBL 7.45, AND BS 1510 LBL 2.90 AND LBL 7.55 WERE REPLACED PER SRM 53-00 -5
- [SDR DALA2026031901892](https://openairdocs.org/sdr/DALA2026031901892.md): Stringer Splice · corroded · Mar 18, 2026 · N584NW · Boeing 757351 · Fuselage Main, Longeron/Stringer
  > AFTER REMOVAL: CORROSION ON SPLICE STA 1440-1460 S29R AND SPLICE STA 1580-1560 S29R ALSO IN THEIR SHIMS (2EAS) IN REF NRC 00382. CORROSION LEVEL 2. SPLICE STA 1440-1460 S29R AND SPLICE STA 1580-1560 S29R WERE REPLACED PER B757-300 SRM 51-40-02-0G PAR. 4
- [SDR DALA2026031801873](https://openairdocs.org/sdr/DALA2026031801873.md): Intercostal · corroded · Mar 18, 2026 · N584NW · Boeing 757351 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL FROM STA. 1520 TO STA 1540 AND STR 29R AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2. INTERCOSTAL FROM STA. 1520 TO STA 1540 AND STR 29R AT AFT CARGO COMPARTMENT.WAS REPLACED PER B757-300 SRM 51-40-02-0G PAR. 7. D. (1499827)
- [SDR DALA2026031701853](https://openairdocs.org/sdr/DALA2026031701853.md): Panel · out of limits · Mar 17, 2026 · N584NW · Boeing 757351 · Fuselage Miscellaneous Structure
  > (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON LH SIDE PANEL FROM STA 1500+6 TO STA 1530 AT AFT CARGO COMPARTMENT, AREA IS OUT WITHIN LIMITS PER B757-300 SRM 53-00-53-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 DETAIL III NOTE C. AND DETAIL IX. (CORROSION LEVEL 2) LH S
- [SDR DALA2026031101720](https://openairdocs.org/sdr/DALA2026031101720.md): Panel · corroded · Mar 11, 2026 · N584NW · Boeing 757351 · Fuselage Miscellaneous Structure
  > SHIP 5804 IN REF TO THE NRC 00370: CORROSION OUT LIMITS (UT) MEASUREMENT THICKNESS WAS ACOMPLISHED ON BELOW SIDE PANEL STA 740-760 LH SIDE PER B757-300 SRM 53-00- 53-1A PROCEDURE 1 ALLOWABLE DAMAGE 1, NOTE C, FIGURE 101, DETAIL IX PER B757 NDT MANUAL PART. 4 5
- [SDR DALA2026030901621](https://openairdocs.org/sdr/DALA2026030901621.md): Frame Angle · corroded · Mar 8, 2026 · N584NW · Boeing 757351 · Fuselage Main, Frame
  > SHIP 5804 IN REF NRC 00382 AFTER REMOVAL: CORROSION ON 2 FRAME CLIPS ON STA 1460 BTW S30 TO S28R AT AFT CARGO COMPARMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00647: CORROSION LEVEL 2.FRAME CLIPS ON STA 1460 BTW S30 TO S28R AT AFT CARGO COMPARMENT WERE REPLACED A
- [SDR DALA2026030901620](https://openairdocs.org/sdr/DALA2026030901620.md): Panel · corroded · Mar 8, 2026 · N584NW · Boeing 757351 · Fuselage Miscellaneous Structure
  > SHIP 5804 CORROSION ON RH SIDE PANEL FROM STA 1310 TO STA 1380 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00289: CORROSION LEVEL 2. RH SIDE PANEL FROM STA 1310 TO STA 1380 AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLED PER B 757-300 SRM 5
- [SDR DALA2026030901618](https://openairdocs.org/sdr/DALA2026030901618.md): Girt Bar · no test · Mar 6, 2026 · N584NW · Boeing 757351 · Emergency Equipment
  > SHIP 5804 A.D. A.A. 2561-01257-01B STEP 16: DURING GIRT BAR OPERATIONAL CHECK. CHAFING WAS FOUND BTW FWD FLOOR FITTING AND FWD GIRT BAR SLIDER AT R1 DOOR GIRT BAR. CORRECTIVE ACTION: SUMMARY OF NRC 00656: GIRT BAR ADJUSTMENT WAS PERFORMED PER B757 -300 AMM 52
- [SDR DALA2026030901613](https://openairdocs.org/sdr/DALA2026030901613.md): Support · corroded · Mar 4, 2026 · N584NW · Boeing 757351 · Fuselage Miscellaneous Structure
  > SHIP 5804 CORROSION ON LOWER SILL SETTLEMENT AREA OF THRESHOLD (UPPER/LOWER FACE) BTW STA 1360 TO STA 1460 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00217: CORROSION LEVEL 2. LOWER SILL SETTLEMENT AREA OF THRESHOLD (UPPER/LOWER FACE) BTW STA
- [SDR DALA2026030901612](https://openairdocs.org/sdr/DALA2026030901612.md): Strap · cracked · Mar 4, 2026 · N584NW · Boeing 757351 · Fuselage Miscellaneous Structure
  > SHIP 5804 CRACK ON STABILIZATION STRAP BTW STA 1640 AND LBL 24 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00336: STABILIZATION STRAP BTW STA 1640 AND LBL 24 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B 757-300 SRM 53-00- 51-2R PROCEDURE REPAIR
- [SDR DALA2026030301470](https://openairdocs.org/sdr/DALA2026030301470.md): Floor Support · out of limits · Mar 2, 2026 · N584NW · Boeing 757351 · Fuselage Miscellaneous Structure
  > SHIP 5804, IN REF NRC 00600:UT MEASUREMENT THICKNESS WAS ACCOMPLISHED ON CABIN FLOOR SUPPORT (W3 AREA) BTWN BS 1250 - 1280, RBL 64 IN THE PAX CABIN. AREA IS OUT LIMITS IAW SRM 53-60-13-1A- 1 ALLOWABLE DAMAGE 1, FIG 101 DETAIL III, & NDT MANUAL PART. 4 51-00-1
- [SDR DALA2026030201410](https://openairdocs.org/sdr/DALA2026030201410.md): Seat Track · corroded · Mar 1, 2026 · N584NW · Boeing 757351 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE BTW STA 1600- 1640 RBL22 AND RBL44 AT PASSENGER CABIN (W4).: CORROSION LEVEL 2. SEAT TRACK FLANGE BTW STA 1600-1640 RBL22 AND RBL44 AT PASSENGER CABIN WERE REPLACED AND INSTALLED PER DWG 146N5126 REV: - AND B757-300 SRM 51-40-02
- [SDR DALA2026022701392](https://openairdocs.org/sdr/DALA2026022701392.md): Girt Bar · faulted · Feb 27, 2026 · N584NW · Boeing 757351 · Passenger/Crew Doors
  > SHIP 5804 A.A 2561-01257-01A. STEP 14. M NIMUM ENGAGEMENT BELOW 0.37 INCH AT AFT SLIDER ON GIRT BAR OF L1 DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00004:L1 GIRT BAR WAS REPLACED PER B757-300 AMM 25-66-10 WAS VERIFIED PER B757-300 IPC 25-66-05 ALSO PROCEDURES BE
- [SDR DALA2026022701391](https://openairdocs.org/sdr/DALA2026022701391.md): Seat Track · corroded · Feb 26, 2026 · N584NW · Boeing 757351 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 5804 CORROSION ON SEAT TRACK FLANGE BTW STA 1620- 1640 LBL22 AND LBL44 AT PASSENGER CABIN (W4). CORRECTIVE ACTION: SUMMARY OF NRC 00420: CORROSION LEVEL 2. SEAT TRACK BTW STA 1620 -1640 LBL22 AND LBL44 AT PASSENGER CABIN WERE REPLACED AND INSTALLED PER DW
- [SDR DALA2026022601370](https://openairdocs.org/sdr/DALA2026022601370.md): Floor Support · corroded · Feb 25, 2026 · N584NW · Boeing 757351 · Fuselage Miscellaneous Structure
  > SHIP 5804 IN REF NRC 00458 AFTER REMOVAL CORROSION, (UT) THICKNESS MEASUREMENT INSPECTION WAS ACCOMPLISHED ON FLOOR SUPPORTS BTW STA 1007 TO 1040 LBL 64 ALSO BTW STA 1005 TO 1040 RBL 64, THEREFORE AREAS ARE OUT OF LIMIST PER B757-300 SRM 53-40-13-1A PROCEDURE
- [SDR DALA2026022601369](https://openairdocs.org/sdr/DALA2026022601369.md): Seat Track · corroded · Feb 25, 2026 · N584NW · Boeing 757351 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 5804 IN REF NRC 00173: CORROSION OUT OF LIMITS: (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON INBD/OUTBD PASSENGER RH SEAT CROWN BTW STA 365 TO STA 418. THEREFORE, IT IS OUT LIMITS PER B757-300 SRM 53-00-52-1A-1 PROCEDURE 1, ALLOWABLE DAMAGE 1, NOTE 1, D
- [SDR DALA2026021901208](https://openairdocs.org/sdr/DALA2026021901208.md): Box Beam · corroded · Feb 18, 2026 · N584NW · Boeing 757351 · Fuselage Main, Structure
  > CORROSION ON BOX BEAM BTW BS 700 - 720, LBL 62 APPROX ON SETTLEMENT FLOOR PANELS UPPER/LOWER AREA AT PASSENGER CABIN. GUTTER SUPPORT WAS FABRICATED IAW DWG 143N5410 REV A. AND GUTTER SUPPORT BTW BS 700 - 720, LBL 60 APROX AT PASSENGER WAS INSTALLED IAW SRM
- [SDR DALA2026021801142](https://openairdocs.org/sdr/DALA2026021801142.md): Floor Support · corroded · Feb 17, 2026 · N584NW · Boeing 757351 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS, IN REF TO NRC 00453: CORROSION ON LOWER SILL LH SIDE UPPER SURFACE STA 732 AT FLOOR STRUCTURE LEVEL IS OUT OF LIMITS PER B757-300 SRM 53-30-15-1A PROCEDURE 1 AD 1. FIG. 101 DETAIL VI SECTION B-B. NEW LOWER SILL LH UPPER SURFACE STA 6
- [SDR DALA2026021801141](https://openairdocs.org/sdr/DALA2026021801141.md): Box Beam · corroded · Feb 17, 2026 · N584NW · Boeing 757351 · Fuselage Main, Structure
  > CORROSION OUT OF LIMITS. IN REF NRC 423: CORROSION ON BOX BEAM BTW STA 1660-1680 AND LBL 55 AT PASSENGER CABIN IS OUT OF LIMITS PER B757-300 SRM 53-00-51-1A PROCEDURE 1 AD 1. FIG. 101 DETAIL VI SECTION B-B. NEW BOX BEAM WAS REPLACED ON BTW STA 1660- 1680 AND
- [SDR DALA2026021801140](https://openairdocs.org/sdr/DALA2026021801140.md): Fitting · corroded · Feb 17, 2026 · N584NW · Boeing 757351 · Emergency Equipment
  > CORROSION ON CENTER FITTING ON GIRT BAR OF L2, R4 AND L4 DOORS. CENTERS FITTING ON GIRT BAR OF L2, R4 AND L4 DOORS P/N: 416N2113-2 (3EAS) WERE REPLACED PER B757-300 AMM. (1455183)
- [SDR DALA2026021201017](https://openairdocs.org/sdr/DALA2026021201017.md): Snubber · out of limits · Feb 11, 2026 · N584NW · Boeing 757351 · Passenger/Crew Doors
  > COMPRESSOR INDICATOR EXTENSION OUT OF LIMITS AT ROTARY SNUBBER OF R4 DOOR. THE R4 DOOR WAS REMOVED & INSTALLED IAW AMM 52-11-01, ROTARY SNUBBER WAS REPLACED IAW AMM 52-11-09. AND AMM 52-11-10. (1446927)
- [SDR DALA2026021101003](https://openairdocs.org/sdr/DALA2026021101003.md): Girt Bar · faulted · Feb 10, 2026 · N584NW · Boeing 757351 · Emergency Equipment
  > A.A 2561-01257-01B. STEP 13. AFT LEAF SPRING DOES NOT RETAIN THE SLIDER AND RIDES BELOW THE SPRING ON GIRT BAR OF R1 DOOR. THE GIRT BAR WAS REMOVED IAW AMM 25-66-10, ALSO REPLACED BY A MODIFIED GIRT BAR AND VERIFIED IAW IPC 25-66-05-05. (1445287)
- [SDR DALA2026030501542](https://openairdocs.org/sdr/DALA2026030501542.md): Splice · damaged · Jan 24, 2026 · N584NW · Boeing 757351 · Door Warning System
  > LEFT CTR ENTRY DOOR EICAS MESSAGE POSTED IMMEDIATELY AFTER LANDING. LANDING WAS NOT FIRM AT ALL. SPLICE (SP142) OF SENSOR (S10095) WAS REPAIRED IAW SWPM 20-10-13. PROXIMITY SWITCH ELECTRONICS UNIT BITE WAS PERFORMED IAW FIM 32-09-03-815-812. SATISFACTORY FS
- [SDR DALA2026011200296](https://openairdocs.org/sdr/DALA2026011200296.md): Oil System · leaking · Jan 11, 2026 · N584NW · Boeing 757351 · APU Oil System
  > SMKE/FUME- ON TAXI OUT CREW REPORTED FLIGHT DECK FILLED WITH NOTICEABLE HAZE AND SMOKE. FOUND APU OIL LEAK AT GEN SEAL AND OIL QTY XMTR. REPLACED GEN AND XMTR SEAL. INSPECTED APU BLEED DUCT AND PACK HEAT EXCHANGERS FOR CONTAMINATION, NONE FOUND. CHECKED CABIN
- [SDR DALA2026010600109](https://openairdocs.org/sdr/DALA2026010600109.md): Indicator · inoperative · Jan 4, 2026 · N584NW · Boeing 757351 · Emergency Equipment
  > L4 KNUCKLE KNOCKER WON'T EXTEND WHEN SLIDE ARMED. REMOVED DEBRIS FROM AROUND KNUCKLE KNOCKER. OPS OK. (8143184)
- [SDR DALA2025122909478](https://openairdocs.org/sdr/DALA2025122909478.md): Sensor · out of adjust · Dec 24, 2025 · N584NW · Boeing 757351 · Door Warning System
  > LEFT CENTER ENTRY DOOR EICAS MESSAGE ON LANDING. FOUND JAM NUT LOOSE AND 1 OF 3 MOUNTING BOLTS LOOSE. ADJUSTED CLEARANCE BETWEEN TARGET AND SENSOR PER AMM 52-71, TIGHTENED JAM NUT AND MOUNTING BOLT. OPS CHECK GOOD AT THIS TIME. (8143126)
- [SDR DALA2025122209329](https://openairdocs.org/sdr/DALA2025122209329.md): Proximity Sensor · faulted · Dec 19, 2025 · N584NW · Boeing 757351 · Door Warning System
  > FLT CREW REPORTED ON LANDING, LEFT CTR DOOR (L2) EICAS MSG. R & R L2 CABIN DOOR PROX SENSOR IAW AMM 52-71. OPS NORMAL. GOOD INDICATIONS MSG DOES NOT SHOW WHEN DOOR IS CLOSED. (6582997)
- [SDR DALA2025121609173](https://openairdocs.org/sdr/DALA2025121609173.md): Sensor · out of adjust · Dec 14, 2025 · N584NW · Boeing 757351 · Door Warning System
  > LEFT CENTER ENTRY DOOR EICAS ON LANDING. WENT OUT ON TAXI IN. ADJUSTED LT CENTER ENTRY DOOR SENSOR IAW AMM 52-71. OPS CHKD NORMAL. (6582950)
- [SDR DALA2025121009032](https://openairdocs.org/sdr/DALA2025121009032.md): Switch · lack of lube · Dec 9, 2025 · N584NW · Boeing 757351 · Door Warning System
  > ON LANDING ROLL L ENTRY DOOR OPEN ON EICAS. CLEANED AND LUBED DOOR SWITCH. PERFORMED OPS CHECK OF DOOR INDICATION SYSTEM. OPS CHECK NORMAL. (6582931)
- [SDR DALA2025120208808](https://openairdocs.org/sdr/DALA2025120208808.md): Indicator · fod · Nov 29, 2025 · N584NW · Boeing 757351 · Emergency Equipment
  > L4 & R4 DOORS NOT SHOWING DOOR KNOCKERS WHEN ARMING DOORS. REMOVED TRIM DEBRIS OBSTRUCTING DOOR KNOCKERS. BOTH L4 & R4 DOORS OPERATE AND ARM CORRECTLY IAW AMM 52-11. (8143696)
- [SDR DALA2025112408536](https://openairdocs.org/sdr/DALA2025112408536.md): Elec Connector · damaged · Nov 21, 2025 · N584NW · Boeing 757351 · Light System Wiring
  > WHILE WORKING W/C 3351-7001 FOUND NBR 4 DOOR LT & RT EXTERIOR PLUS AFT HATCH LT/RT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. RELAMPED NR 4 DOOR LT & RT EXTERIOR EMERGENCY LIGHTS. REPLACED NLG EMERGENCY LIGHTS TEST SWITCH S10035. RE-PINNED PINS: C, C-, G- ON PLU
- [SDR DALA2025111708384](https://openairdocs.org/sdr/DALA2025111708384.md): Battery · inoperative · Nov 14, 2025 · N584NW · Boeing 757351 · Emergency Lighting
  > SHIP 5804 MULTIPLE EMERGENCY LIGHTS NOT WORKING IN FWD CABIN. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY BATTERY AND CHARGER PER B757 AMM 33-51. OPS CHK GOOD. (8143628)
- [SDR DALA2025101407515](https://openairdocs.org/sdr/DALA2025101407515.md): Power Supply · faulted · Oct 12, 2025 · N584NW · Boeing 757351 · Emergency Lighting
  > ROW 27-38 SEAT MOUNTED EMERGENCY LIGHTS INOP. SLAVED IN BATTERY AND CHARGER IN LOCATIONS M114881 AND M11082 REF B757 AMM 33-51, REF B757 WDM 33-51-21 REPAIRED WIRE AT SEAT 38 DEF PER SWPM CH 20. RPLCD EMERG LT PWR SUPPLY M11487 REF AMM 33-51. ALL SEAT MOUNTED
- [SDR DALA2025101007437](https://openairdocs.org/sdr/DALA2025101007437.md): Cover · loose · Oct 8, 2025 · N584NW · Boeing 757351 · Emergency Lighting
  > EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:609, UPSIDE DOWN. REMOVED EXIT SIGN AT DOOR 3L AND REINSTALLED RIGHT SIDE UP. (1240886)
- [SDR DALA2025091406749](https://openairdocs.org/sdr/DALA2025091406749.md): Battery Pack · inoperative · Sep 13, 2025 · N584NW · Boeing 757351 · Emergency Lighting
  > AIRCRAFT 5804, DURING SERVICE CHECK, FOUND R2 DOOR EXIT SIGN AND SEAT 14 THROUGH 20 EMERGENCY PATH LIGHT OUT. CORRECTIVE ACTION: REPLACED M11612 POWER SUPPLY BATTERY PACK AND CHECKED NORMAL PER B757 AMM 33-51. (LP 7855458)
- [SDR DALA2025061304491](https://openairdocs.org/sdr/DALA2025061304491.md): Compressor · damaged · Jun 13, 2025 · N584NW · Boeing 757351 · Turbine Engine Compressor Section
  > SHIP 5804 -DIV/DE- DIVERSION TO BNA DUE TO LEFT ENGINE STALL. CORRECTIVE ACTION: PERFORMED BSI, FOUND COMPRESSOR DAMAGE REPLACED LEFT ENGINE.

Next page: https://openairdocs.org/aircraft/N584NW/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 n_number = 'N584NW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N584NW/reports

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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.