# Service difficulty reports: N534US, cancelled Nov 3, 2017

A list on [N534US, cancelled Nov 3, 2017](https://openairdocs.org/deregistered/N534US-2017-11-03.md).

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

- [SDR DALA2015083105347](https://openairdocs.org/sdr/DALA2015083105347.md): Power Supply · inoperative · Aug 30, 2015 · N534US · Boeing 757251 · Emergency Lighting
  > EMERGENCY LIGHTING FROM ROWS 16-25 INOPERATIVE. REPLACED THE POWER SUPPLY M9002 IAW CMM 33-50-13.
- [SDR DALA2015062603953](https://openairdocs.org/sdr/DALA2015062603953.md): Wire · damaged · Jun 24, 2015 · N534US · Boeing 757251 · Light System Wiring
  > EMERGENCY TRACK LIGHTING COMING UP AT SEAT ROW 24. SECURED EMERGENCY TRACK LIGHTING AT SEAT ROW 24. FOUND 2 LIGHTS INOPERATIVE. FWD AND PLAC IAW MEL 33-51-03B. NOTIFIED MCC. REPAIRED WIRE SPLICES AT ROW 24 FLOOR LIGHTS. RE-SECURED COVER. OPS CK GOOD. MC
- [SDR DALA2014090504916](https://openairdocs.org/sdr/DALA2014090504916.md): Battery Pack · inoperative · Sep 4, 2014 · N534US · Boeing 757251 · Emergency Lighting
  > DURING WAKEUP, FOUND EMERGENCY LIGHT AT R3 DOOR ON WITH SWITCH IN ARMED POSITION. REPLACED BATTERY PACK ASSY, OPS CHECKED GOOD.
- [SDR DALA2014073104276](https://openairdocs.org/sdr/DALA2014073104276.md): Skin · damaged · Jul 29, 2014 · N534US · Boeing 757251 · Service Doors
  > R4 DOOR SKIN UPPER FWD CORNER DAMAGED BELOW UPPER HINGE GATE. CUTOUT DAMAGE IAW SRM 52-10-01, REPAIR C/W HFEC OF CUTOUT IAW NDT PT. 6 51-00-19 AND BHEC IAW NDT PTG 51-00-16, NO ITEMS WERE NOTED 761595, REPAIRED IAW SRM 52-10-01, REPAIR 07.
- [SDR DALA14019595534](https://openairdocs.org/sdr/DALA14019595534.md): Battery Pack · inoperative · Mar 27, 2014 · N534US · Boeing 757251 · Emergency Lighting
  > EMERGENCY EXIT SIGNS INOPERATIVE. R & R EMERGENCY BATTERY PACK. OPS CHECKED GOOD.
- [SDR DALA12012715534](https://openairdocs.org/sdr/DALA12012715534.md): Charger · inoperative · Nov 15, 2012 · N534US · Boeing 757251 · Emergency Lighting
  > FOUND RT EMERGENCY CEILING EXIT SIGN ABOVE R3 DOOR INOPERATIVE. RELAMPED EXIT SIGN NO HELP. T/S FOUND BATTERY CHARGER TO BE NOT WORKING PROPERLY. R & R BATTERY CHARGER AS REQUIRED IAW AMM 33-50. OPS CHECKED GOOD
- [SDR DALA12009555534](https://openairdocs.org/sdr/DALA12009555534.md): Harness · deteriorated · Oct 6, 2012 · N534US · Boeing 757251 · Escape Slide
  > R4 DOOR EMERGENCY ESCAPE SLIDE HARNESS DETERIORATED AND WILL NOT LATCH. R & R R-4 DOOR EMERGENCY ESCAPE SLIDE HARNESS IAW -A-25-66-01-401-926-A-A.
- [SDR DALA12005335534](https://openairdocs.org/sdr/DALA12005335534.md): Cable · out of tolerance · Aug 10, 2012 · N534US · Boeing 757251 · Passenger/Crew Doors
  > DURING FLIGHT CHECK, MAINTENANCE WAS INSPECTING EMERGENCY POWER ASSIST CABLE TRAVEL. PER AMSD STEP 4C CABLE TRAVEL FAILED. MAINTENANCE LUBED AND CHECKED MOVEMENT PE AMDS 5210-01083-01E. OPERATION OF CABLE CHECKS GOOD AND RII COMPLETED.
- [SDR DALA12004905534](https://openairdocs.org/sdr/DALA12004905534.md): Mechanism · loose · Aug 5, 2012 · N534US · Boeing 757251 · Passenger/Crew Doors
  > L1 PAX DOOR EMERGENCY OPERATION MECHANISM HAS LOOSE AND MISSING HARDWARE (LOWER OPERATION MECHANISM) ALSO CRANK ASSY BENT, TIGHTENED LOOSE HARDWARE. NSTALLED NEW CRANK AND BUSHING PER CMM 52-11-07. OPS GOOD PER AMM 52-11 RII COMPLETE.
- [SDR DALA1234725534](https://openairdocs.org/sdr/DALA1234725534.md): Duct · damaged · May 29, 2012 · N534US · Boeing 757251 · APU Bleed Air System
  > SMOKE IN THE BACK OF THE AIRCRAFT ACCOMPANIED BY HOT AIR AND WARM FLOOR. CLOSED APU BLEED VALVE HEAT AND DEBRIS BEGAN TO DISSIPATE FOUND APU BLEED DUCT IN AFT CARGO BIN JUST FWD OF PRESSURE BULKHEAD WITH A 3/8 INCH HOLE AT MOUNT CLAMP FWD TO MEL PER 36-11-04.
- [SDR DALA1220355534](https://openairdocs.org/sdr/DALA1220355534.md): Battery Pack · loose · Apr 2, 2012 · N534US · Boeing 757251 · Emergency Lighting
  > DURING LINE CHECK MAINTENANCE FOUND EMERGENCY PATH LIGHTS IN ROW 26-30 INOPERATIVE. MAINTENANCE SECURED LOOSE BATTERY PACK QUICK DISCONNECT. EMERGENCY LIGHTS NOW CHECK OK.
- [SDR DALA1167085534](https://openairdocs.org/sdr/DALA1167085534.md): Connector · disconnected · Dec 4, 2011 · N534US · Boeing 757251 · Light System Wiring
  > DURING LINE CHECK MAINTENANCE FOUND FIRST CLASS EMERGENCY LIGHTS INOP. MAINTENANCE RESEATED CONNECTOR ON BATTERY PACK. LIGHTS NOW CHECK OK. (LP 8490398)
- [SDR DALA1137205534](https://openairdocs.org/sdr/DALA1137205534.md): Boot · blown · May 29, 2011 · N534US · Boeing 757251 · Cabin Pressure Control System
  > AT FL330 GOT CABIN ALT WARNING AND CABIN AUTO INOP CAUTION. DECLARED AN EMERGENCY AND DESCENDED TO 10,000'. CABIN PRESSURE REACHED 11,000'. MASKS DID NOT DEPLOY. FLT RETURNEDTO ATL AND LANDED WITHOUT INCIDENT. REPLACED BLOWN BOOT IN RIGHT ECS BAY, OUTFLO
- [SDR DALA1121595534](https://openairdocs.org/sdr/DALA1121595534.md): Switch · miswired · Mar 22, 2011 · N534US · Boeing 757251 · Light System Wiring
  > DURING A LINE CHECK, MAINTENANCE FOUND THE FLIGHT ATTENDANT EMERGENCY LIGHT TEST SWITCH INOPERATIVE. MAINTENANCE CORRECTED THE SWITCH WIRING. OPERATIONAL CHECK WAS GOOD.
- [SDR DALA1104485534](https://openairdocs.org/sdr/DALA1104485534.md): Channel · corroded · Jan 20, 2011 · N534US · Boeing 757251 · Fuselage Miscellaneous Structure
  > CORROSION ON CABIN COMPARTMENT HAT CHANNEL AFT GALLEY AREA AT STA 1683, BL 0. CORROSION FOUND OUT OF LIMITS IAW REF SRM 53-00-51, FIG.101, DETAIL 6. REMOVED & INSTALLED HAT CHANNEL IAW REF SRM 51-40-02 PARA 4, PAGE 2. COMPLETED.
- [SDR DALA1104445534](https://openairdocs.org/sdr/DALA1104445534.md): Plate · corroded · Jan 20, 2011 · N534US · Boeing 757251 · Cargo/Baggage Doors
  > FWD CARGO LOWER LT DOOR SILL PLATE STRUCTURE HAS SOME HEAVY DEFOLIATION CORROSION. REMOVED FWD CARGO DOOR SILL AND DOOR SILL PLATE REF SRM 51-40-02. LOCATED AND DRILLED REPLACEMENT DOOR SILL AND SILL PLATE REF SRM 51-40-05. INSTALLED REPLACEMENT DOOR SILL AND
- [SDR DALA1104435534](https://openairdocs.org/sdr/DALA1104435534.md): Sill · corroded · Jan 20, 2011 · N534US · Boeing 757251 · Fuselage Miscellaneous Structure
  > CORROSION ON NR4 DOOR SILL RT SIDE SUPPORT FRAME AT BS 1673, RBL 52. REMOVED CORROSION AT NR4 DOOR SILL RT SIDE SUPPORT FRAME IAW REF SRM 51-10-02. FOUND OUT OF LIMITS IAW REF SRM 53-00-51, PAGE 103, FIG 101, DETAIL 6. R & R SUPPORT FRAME IAW SRM 51-40-02.
- [SDR DALA1200685534](https://openairdocs.org/sdr/DALA1200685534.md): Skin · damaged · Jan 18, 2011 · N534US · Boeing 757251 · Cargo/Baggage Doors
  > DURING M CHECK. THE INSPECTION FOUND DAMAGE OUT OF LIMITS EDGE OF SKIN CARGO DOOR. REPAIR WAS ACCOMPLISHED PER ERA 488121-14.
- [SDR DALA1102445534](https://openairdocs.org/sdr/DALA1102445534.md): Box Beam · corroded · Jan 11, 2011 · N534US · Boeing 757251 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT L4 DOOR FLOOR LEVEL AFT BOX BEAM, LBL 54 FROM STA 1661 TO STA 1681. REMOVED CORROSION AT LT DOOR, FLOOR LEVEL AFT BOX BEAM, LBL 54 FROM STA 1661 TO STA 1681 PER REF PS 900-2-4-1- NR 1. FOUND OUT OF LIMITS IAW REF SRM 53-00-51, PAGE 103, F
- [SDR DALA1102415534](https://openairdocs.org/sdr/DALA1102415534.md): Cusp Web · corroded · Jan 11, 2011 · N534US · Boeing 757251 · Fuselage Miscellaneous Structure
  > CORROSION ON NR4 RT DOOR SILL AREA CUSP WEB "J" CHANNEL AT STA 1665. REMOVED CORROSION AT NR4 RT DOOR SILL AT STA 1665. FOUND "U" CHANNEL OUT OF LIMITS, REF SRM 51-10-02, PAGE 12 AND SRM 53-00-51, PAGE 103, FIG 101. R & R "U" CHANNEL AT NR4 RT DOOR SILL AT ST
- [SDR DALA1102405534](https://openairdocs.org/sdr/DALA1102405534.md): Floor Support · corroded · Jan 11, 2011 · N534US · Boeing 757251 · Fuselage Miscellaneous Structure
  > FLOORBEAM CORRODED BETWEEN STA 345 AND 377. REMOVED CORROSION ON 3 EA AREAS FROM STA 345 TO STA 376 ON FLOORBEAM IAW REF SRM 51-10-02, PAGE 12. REMOVED FLOOR BEAM FROM STA 345 TO STA 418 BL 0.0 ON MAIN CABIN REF SRM 51-40-02, PAGE 7. INSTALLED NEW FLOORBEAM
- [SDR DALA1102385534](https://openairdocs.org/sdr/DALA1102385534.md): Intercostal · cracked · Jan 11, 2011 · N534US · Boeing 757251 · Fuselage Miscellaneous Structure
  > 2ND INTERCOSTAL ABOVE L2 DOOR PNUEMATIC DOOR ACTUATOR HAS A CRACK BETWEEN STA 660 TO 680. REMOVED AND INSTALLED NEW INTERCOSTAL ABOVE L-2 DOOR PNUEMATIC DOOR ACTUATOR BETWEEN STA 660 TO 680 REF SRM 51-40-02 PG 2 AND PG7 COMPLETED: A INSPECTED.
- [SDR DALA1102375534](https://openairdocs.org/sdr/DALA1102375534.md): Intercostal · cracked · Jan 11, 2011 · N534US · Boeing 757251 · Fuselage Miscellaneous Structure
  > 2 EA CRACKS AT INTERCOSTAL JUST ABOVE L2 DOOR PNUEMATIC ACTUATOR BETWEEN STA 660 AND 685. REMOVED AND INSTALLED NEW INTERCOSTAL ON L2 DOOR ABOVE PNUEMATIC ACTUATOR BETWEEN STA 660 AND 685 REF SRM 51-40-02 PG 1 AND PG 7.
- [SDR DALA1036775534](https://openairdocs.org/sdr/DALA1036775534.md): Floor Support · cracked · Dec 28, 2010 · N534US · Boeing 757251 · Fuselage Miscellaneous Structure
  > DURING M-CHECK, FOUND FWD CARGO BETWEEN STA 680 AND STA 660, 36" LT OF CTR THE FLOOR SUPPORT IS CRACKED. REMOVED FLOOR SUPPORT AND INTERCOSTAL WEB CRACKED. FABRICATED REPLACEMENT INTERCOSTAL WEB LOCATED AND DRILLED NEW INTERCOSTAL WEB. NDT VERIFIED FLOOR SU
- [SDR DALA1036715534](https://openairdocs.org/sdr/DALA1036715534.md): Floor Support · corroded · Dec 28, 2010 · N534US · Boeing 757251 · Fuselage Miscellaneous Structure
  > DURING M-CHECK, FOUND RT DOOR SILL AT STA 365.25, FLOOR SUPPORT HAS SURFACE CORROSION OTBD OF RBL 53. R & R FLOOR SUPPORT FROM STA 348 TO 365.25 AT RBL 53 IAW REF SRM 51-40-02.
- [SDR DALA1101905534](https://openairdocs.org/sdr/DALA1101905534.md): Intercostal · cracked · Dec 3, 2010 · N534US · Boeing 757251 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACK AT NR2 R DOOR JUST ABOVE PNEUMATIC ACTUATOR BETWEEN STA 660 AND 685. R & R INTERCOSTAL AT NR2 R DOOR BETWEEN STA 660 AND STA 685, REF SRM 51-40-02, PG 2, 7.
- [SDR DALA1101915534](https://openairdocs.org/sdr/DALA1101915534.md): Floorbeam · corroded · Nov 23, 2010 · N534US · Boeing 757251 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED AT STA 365 FROM BL 0.0, TO RBL 64. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM B757-20053-00-51, FIG 101. GAINED ACCESS TO REPAIR AREA, CUT OUT DAMAGE "T" ANGLE. FABRICATED & INSTALLED REPLACEMENT "T" ANGLE, 2 EA REPAIR ANGLES AND
- [SDR DALA1102935534](https://openairdocs.org/sdr/DALA1102935534.md): Skin · cracked · Jul 18, 2008 · N534US · Boeing 757251 · Nacelle/Pylon, Plate/Skin
  > EA 55-212961 SECTION I ISSUED FOR NR2 PYLON, RT SIDE SKIN CRACK AT NAC STA 132. FOLLOW ON ACTION IS REQUIRED. COMPLIED WITH ER/A 488115-14 REV ORIGINAL PERMENANT REPAIR ACCOMPLISHED COMPLETED.
- [SDR NWAA073645534](https://openairdocs.org/sdr/NWAA073645534.md): Battery Pack · inoperative · Nov 2, 2007 · N534US · Boeing 757251 · Emergency Lighting
  > DURING OVERNIGHT LINE CHECK, FOUND ESCAPE PATH LIGHTS ON FLOOR INOP BETWEEN ROWS 23 THRU 32. MAINTENANCE REMOVED AND REPLACED 2 BATTERY PACKS AND A TEST SWITCH AT THE FORWARD FLIGHT ATTENDANT PANEL. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVI
- [SDR 0601665534](https://openairdocs.org/sdr/0601665534.md): Acm · seized · Jul 22, 2006 · N534US · Boeing 757251 · Cabin Cooling System
  > DURING CLIMB BOTH PILOTS SMELLED ELECTRICAL SMOKE, THEY IMMEDIATELY DONNED OXYGEN MASKS. THERE WAS NO SMOKE IN THE COCKPIT. FLIGHT ATTENDANTS REPORTED SOME WHITE SMOKE IN THE CABIN. THE EVENT LASTED ABOUT TWO MINUTES. THE FLIGHT CONTINUED AND LANDED WITHOUT IN
- [SDR 0401065534](https://openairdocs.org/sdr/0401065534.md): Seat Track · corroded · Jun 24, 2004 · N534US · Boeing 757251 · Fuselage, Seat/Cargo Attach Fittings
  > DURING (H) CHECK FOUND CORROSION ON SEAT TRACK AT BS 1640 LBL 46. REPAIRED IAW EA 55-199278.
- [SDR 0401075534](https://openairdocs.org/sdr/0401075534.md): Floorbeam · cracked · Jun 24, 2004 · N534US · Boeing 757251 · Fuselage Main, Floor Beam
  > DURING (H) CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 45. REPAIRED IAW EA 55-199754.
- [SDR 0401175534](https://openairdocs.org/sdr/0401175534.md): Floorbeam · corroded · Jun 17, 2004 · N534US · Boeing 757251 · Fuselage Main, Floor Beam
  > DURING H-CHECK FOUND CORROSION ON FLOORBEAM AT BS 365 RBL 25. REPAIRED IAW EA 55-198961.
- [SDR 0202805534](https://openairdocs.org/sdr/0202805534.md): Power Supply · defective · Aug 30, 2002 · N534US · Boeing 757251 · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST, MID CABIN AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD.
- [SDR 0103475534](https://openairdocs.org/sdr/0103475534.md): Smoke · detected · Oct 1, 2001 · N534US · Boeing 757251 · Air Distribution System
  > DURING CRUISE AT 41,000 FT, A BURNING SMELL WAS NOTICED IN THE FLIGHT DECK. LEAD FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. SMOKE IN THE AIRCRAFT DISSIPATED AFTER SMOKE CHECK LIST WAS COMPLIED WITH BUT RETURNED DURING APPROACH. MAINTENANCE CHECKED OPERAT
- [SDR 0101375534](https://openairdocs.org/sdr/0101375534.md): Fire Detector · malfunctioned · Apr 13, 2001 · N534US · Boeing 757251 · Fire Detection
  > ON ENGINE START, THE LEFT ENGINE FIRE WARNING OCCURRED. WARNINGS STOPPED AFTER FIRE SWITCH WAS PULLED AND ONE BOTTLE DISCHARGED. MAINTENANCE CHECKED ENGINE, DUCTING, AND FUEL AND OIL LINES FOR EVIDENCE OF FIRE WITH NONE FOUND. REPLACED THE NR 1, 2, 3, AND 4
- [SDR 9809875534](https://openairdocs.org/sdr/9809875534.md): Engine · failed · Aug 9, 1998 · N534US · Boeing 757251 · Engine (Turbine/Turboprop)
  > DURING FINAL APPROACH AT 1000 FEET, NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL AND FLAMED OUT. AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED. MAINTENANCE FOUND TRACE OF METAL IN THE TAILPIPE AND REPLACED THE ENGINE.
- [SDR 9620425534](https://openairdocs.org/sdr/9620425534.md): Floorbeam · corroded · Sep 16, 1996 · N534US · Boeing 757251 · Fuselage Main, Floor Beam
  > DURING PERIODIC CHECK, FOUND CORROSION ON THE BS 1640 FLOORBEAM UPPER CHORD FROM LBL 6 TO RBL 60. REPAIRED CHORD (P/N 146N5089) PER EA 55-106273.
- [SDR 9504955534](https://openairdocs.org/sdr/9504955534.md): Floor Support · corroded · Mar 25, 1995 · N534US · Boeing 757251 · Fuselage Miscellaneous Structure
  > DURING PERIODIC CHECK, THE AFT CARGO FLOOR SUPPORT STRINGERS WERE FOUND CORRODED AROUND NUTPLATES BETWEEN FS 1445 AND 1500, LBL 11 AND RBL 3. REMOVED CORROSION AND INSTALLED REPAIR PER NWA EA 55-97818.
- [SDR 9505035534](https://openairdocs.org/sdr/9505035534.md): Skin · damaged · Mar 24, 1995 · N534US · Boeing 757251 · Spoilers
  > DURING PERIODIC CHECK, THE NR 1, NR 2, NR 10, NR 11, AND NR 12 SPOILER UPPER SKIN PANELS WERE FOUND WITH NUMEROUS AREAS OF DAMAGE AND DELAMINATION (2 INCH DIAMETER TYPICAL). INSTALLED REPAIRS PER SRM 57-70-01, FIG. 201 AND NWA EA 55-97817.

## 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 = 'N534US' AND deregistration_id = 'N534US-2017-11-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N534US-2017-11-03/reports

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