# Service difficulty reports: N532US, cancelled Jun 22, 2016

A list on [N532US, cancelled Jun 22, 2016](https://openairdocs.org/deregistered/N532US-2016-06-22.md).

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

- [SDR DALA2015070704148](https://openairdocs.org/sdr/DALA2015070704148.md): Acm · seized · Jul 3, 2015 · N532US · Boeing 757251 · Cabin Cooling System
  > REJECTED TAKEOFF, FOR SMOKE IN THE COCKPIT AND CABIN. MAINTENANCE FOUND LT PACK ACM SEIZED, REPLACED ACM, REHEATER AND LLV. DURING CHECK OUTS FOUND PACK TEMP VALVE BAD. REPLACED SAME. PERFORMED SINGLE PACK, CHECK OPS, CHECKS GOOD.
- [SDR DALA2015060103560](https://openairdocs.org/sdr/DALA2015060103560.md): Light · unsecure · May 23, 2015 · N532US · Boeing 757251 · Emergency Lighting
  > EMERGENCY LIGHT LOOSE AT SEATS 29D TO 32D. SECURED FLOOR TRACK IAW ERA 536365-14. REPLACED LENS WITH NEW LENS. LIGHTING SECURED.
- [SDR DALA2014102505790](https://openairdocs.org/sdr/DALA2014102505790.md): Door Frame · cracked · Oct 24, 2014 · N532US · Boeing 757251 · Fuselage Main, Structure
  > L2 DOOR, UPPER HINGE CUTOUT, FRAME IS CRACKED. R/I DOOR, REPAIRED AND INSPECTED IAW SRM.
- [SDR DALA14015475532](https://openairdocs.org/sdr/DALA14015475532.md): Module · leaking · Mar 9, 2014 · N532US · Boeing 757251 · Hydraulic System, Main
  > LOST LT HYDRAULIC SYSTEM, DECLARED EMERGENCYP AND PERFORMED AN ALTERNATE GEAR EXTENSION IAW QRH. FOUND AND REPLACED LEAKING FLAP/SLAT DEPRESSURIZATION MODULE. ALSO, REPLACED LT ENGINE DRIVEN HYD PUMP DUE TO NO PRESSURE OUTPUT. LEAK AND OPS CK'S OK.
- [SDR DALA13042765532](https://openairdocs.org/sdr/DALA13042765532.md): Controller · failed · Sep 4, 2013 · N532US · Boeing 757251 · Windshield/Door Rain/Ice Removal
  > DUE TO R1 WINDOW SHATTERED. REPLACED WINDOW AND WINDOW HEAT CONTROLLER. OPS CHECKED OK.
- [SDR DALA12009325532](https://openairdocs.org/sdr/DALA12009325532.md): Power Supply · inoperative · Oct 4, 2012 · N532US · Boeing 757251 · Emergency Lighting
  > EMERGENCY FLOOR PATH LIGHTING AT ROW 33FED THRU 40FED INOPERATIVE. INSTALLED SERVICEABLE EMERGENCY LIGHTS POWER SUPPLY IAW AMM 33-51-00. OPS CHECKS NORMALLY. OK FOR SERVICE.
- [SDR DALA12008365532](https://openairdocs.org/sdr/DALA12008365532.md): Bottle · low pressure · Sep 20, 2012 · N532US · Boeing 757251 · Escape Slide
  > R4 DOOR SLIDE INFLATOR BOTTLE PRESSURE GAUGE READS BELOW GREEN BAND. REMOVED AND INSTALLED SERVICABLE ESCAPE SLIDE ASSY IAW 2566-9001-4R. CHECKED GOOD.
- [SDR DALA1159355532](https://openairdocs.org/sdr/DALA1159355532.md): Fuse · blown · Oct 16, 2011 · N532US · Boeing 757251 · Emergency Lighting
  > DURING MAINTENANCE LINE INSPECTION, LEFT AISLE EMERGENCY LIGHT L44 AND L45 WHERE FOUND INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY FUSES PER B757 AMM 33-51-07. SYSTEM OPERATION NORMAL AFTER FUSES WERE REPLACED.
- [SDR DALA1156805532](https://openairdocs.org/sdr/DALA1156805532.md): Flange · leaking · Oct 1, 2011 · N532US · Boeing 757251 · Fuel Storage
  > DURING APPROACH PASSING 1200 FEET A STRONG SMELL OF JET FUEL BECAME APPARENT. LASTED STRONG ENOUGH THRU TOUCHDOWN AND DISSIPATED BY TAXI SPEED. FLIGHT CREW FILLED OUT AIRCRAFT FUME QUESTIONNAIRE. ONCE ON GROUND MAINTENANCE FOUND FUEL LEAK IN THE LEFT ECS BA
- [SDR DALA1106625532](https://openairdocs.org/sdr/DALA1106625532.md): Gate · corroded · Jan 20, 2011 · N532US · Boeing 757251 · Passenger/Crew Doors
  > (MZAR) R-4 DOOR LOWER GATE CORRODED. REMOVED R4 DOOR LOWER GATE & REPLACED WITH NEW ONE, MATERIAL R & R LOWER SEAL & REMOVED & REINSTALLED 3EA ATTACH FITTINGS IAW SRM 52-11-38. PERFORMED & TESTED GIRT BAR MECHANISM IAW AMM 52-11-25 & FOUND GOOD. REQUIRED INS
- [SDR DALA1102705532](https://openairdocs.org/sdr/DALA1102705532.md): Skin · damaged · Jan 12, 2011 · N532US · Boeing 757251 · Fuselage Main, Plate/Skin
  > ERA 487447-14, SECTION I, ISSUED FOR FUSELAGE SKIN REPAIR AT BS 500, S-27R. SECTION I ACCOMPLISHED DURING M-CHECK. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH SECTION II INSP WITHIN 24 MONTHS FROM 10JAN11.
- [SDR DALA1034535532](https://openairdocs.org/sdr/DALA1034535532.md): Support · corroded · Dec 1, 2010 · N532US · Boeing 757251 · Fuselage Miscellaneous Structure
  > DURING M-CHECK, FOUND LOWER FUSELAGE FAIRING SUPPORT AT STA 900 BETWEEN STR 26L TO STR 26R AND 6 O`CLOCK HAS CORROSION. BLENDED-OUT CORRODED AREAS IAW SRM 51-10-01, DIMENSIONS OF BLENDED-OUT AREAS WHICH WERE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-71 FIG 101.
- [SDR DALA1034525532](https://openairdocs.org/sdr/DALA1034525532.md): Floorbeam · corroded · Dec 1, 2010 · N532US · Boeing 757251 · Fuselage Main, Floor Beam
  > DURING M-CHECK FOUND FLOORBEAM AT STA 345, BET BL 0 TO RBL 60 UPPER CHORD HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL IV. R & R UPPER CHORD IAW SRM 53-00-51, REPAIR 3 AND SRM 51-40-05. FABRI
- [SDR DALA1033385532](https://openairdocs.org/sdr/DALA1033385532.md): Sill · corroded · Nov 23, 2010 · N532US · Boeing 757251 · Fuselage Miscellaneous Structure
  > DURING M-CHECK FOUND FT AFT CABIN 4L DOOR SILL HAS CORROSION BS 1640-1681 LBL54" TOP SURFACE & LWR SURFACE AT BS 1640. CLEANED OUT CORRODED AREA IAW SRM 51-10-02, DIMENSIONS L=2.6 W=2.0 D=.0205 IAW SRM 53-60-15 OUT OF LIMITS, REMOVED DOOR SILL IAW SRM 51-40-0
- [SDR DALA1033425532](https://openairdocs.org/sdr/DALA1033425532.md): Floorbeam · corroded · Nov 22, 2010 · N532US · Boeing 757251 · Fuselage Main, Floor Beam
  > DURING M-CHECK, FOUND AFT CABIN FLOORBEAM BS 1640 BBL "0" TO RBL 54" CORRODED AT UPPER SKIN & LOWER SKIN SURFACE AROUND FASTENER HOLE. BLENDED OUT AREAS BEAM 1640 BBL 0 TO RBL 54 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-40-51, FIG 101, SHEET 1 AND SHEET 3, DE
- [SDR DALA1033415532](https://openairdocs.org/sdr/DALA1033415532.md): Floorbeam · corroded · Nov 22, 2010 · N532US · Boeing 757251 · Fuselage Main, Floor Beam
  > DURING M-CHECK FOUND AFT CABIN FLOORBEAM CORRODED AT BS 1640 LBL 54 00-51 FIG 101. REMOVED STIFFENERS AND UPPER CHORD IAW SRM 51-40 02. RECEIVED EXTRUSION IAW SRP B757-A-53-01-07-801-863A-A AND SRM 53-00-51 FIG 201 PARTS SRM 53-00-51. LOCATED AND DRILLED ALL
- [SDR DALA1033405532](https://openairdocs.org/sdr/DALA1033405532.md): Support · corroded · Nov 22, 2010 · N532US · Boeing 757251 · Fuselage, Seat/Cargo Attach Fittings
  > REMOVED CORROSION FROM SEAT TRACK SUPPORT IAW SRM 51-10-02 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101. REMOVED SEAT TRACK SUPPORT IAW SRM 51-40-02, RBL 45 STA 365-418. FABRICATED NEW SEAT TRACK TREATED, PRIMED APPLIED TOPCOAT, LOCATED AND DRILLED IAW
- [SDR DALA1033395532](https://openairdocs.org/sdr/DALA1033395532.md): Support Angle · corroded · Nov 22, 2010 · N532US · Boeing 757251 · Fuselage Miscellaneous Structure
  > DURING M-CHECK FOUND THRESHOLD PLATE SUPPORT ANGLE 2 EA AT BS 1640 & 1681 LBL 54 INCHES HAS CORROSION. REMOVED PLATE SUPPORT ANGLE IAW SRM 51-40-02, FABRICATED PLATE SUPPORT ANGLE AND PLATED ANGLE SUPPORT 1 EA LOCATED AND DRILLED IAW SRM 51-40-05. TREATED AN
- [SDR DALA1033805532](https://openairdocs.org/sdr/DALA1033805532.md): Sill · corroded · Nov 21, 2010 · N532US · Boeing 757251 · Fuselage Miscellaneous Structure
  > DURING M-CHECK FOUND L4 DOOR LOWER SILL WEB CORRODED AT STA 1640. REMOVED L-4 DOOR SILL WEB AND 5 (EACH) STIFFENERS IAW SRM 51-40-02. FABRICATED NEW L-4 DOOR SILL WEB IAW SRM 51-40-05. TREATED, PRIMED, AND APPLIED TOPCOAT IAW SRM 51-20-01 AND AMM 51-21-10.
- [SDR DALA1034675532](https://openairdocs.org/sdr/DALA1034675532.md): Web · punctured · Nov 20, 2010 · N532US · Boeing 757251 · APU Cowling/Containment
  > DURING M-CHECK, FOUND APU COMPARTMENT UPPER SURFACE SKIN AT STA 1914 AND 17" LT FROM CTR WAS PUNCTURED. REMOVED DAMAGED SKIN, FABRICATED REPAIR DOUBLER. ALL WORK PERFORMED IAW SRM 51-70-10.
- [SDR DALA1032975532](https://openairdocs.org/sdr/DALA1032975532.md): Skin · dented · Nov 18, 2010 · N532US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING M-CHECK FOUND APU COMPT EXTERNAL SKIN DENTED BETWEEN STA 1896.20 & STA 1918.9, BL 25.0. CHECKED DENT LIMITS, SANDED DAMAGED AREA, POTTED DENT, FABRICATED REPAIR DOUBLER, BONDED REPAIR DOUBLER,CLEANED AREA APPLIED SEALANT AROUND DOUBLER AND PRIMED.ALL WO
- [SDR DALA1033795532](https://openairdocs.org/sdr/DALA1033795532.md): Sill · corroded · Nov 17, 2010 · N532US · Boeing 757251 · Fuselage Miscellaneous Structure
  > DURING M-CHECK FOUND AFT CBN 4R SILL HAS CORROSION BS 1640-1681 RBL 54 BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15 BS 1640 TO 1660. REMOVED 2 EA SUPPORTS IAW SRM 51-40-02. FABRICATED 2 EA SUPPORTS TREATED, PRIMED & PAINTED DOOR SILLS IAW
- [SDR DALA1032725532](https://openairdocs.org/sdr/DALA1032725532.md): Support · corroded · Nov 17, 2010 · N532US · Boeing 757251 · Fuselage, Seat/Cargo Attach Fittings
  > DURING “M” CHECK FOUND SEAT TRACK SUPPORT BET STA 365 & 377 RBL 24 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101, FABRICATED NEW SEAT TRACK SUPPORT IAW TRAVELLER T10/859329 P/N DA-141N5131-4-20.TREATED AND
- [SDR DALA1032595532](https://openairdocs.org/sdr/DALA1032595532.md): Floorbeam · corroded · Nov 16, 2010 · N532US · Boeing 757251 · Fuselage Main, Floor Beam
  > DURING M-CHECK, FOUND FLOORBEAM STA 365 UPPER CORD FROM BL0 TO RBL 60 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02 DIM. L=44" W=2" D=.065" ORIG MAT.130" FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51, REMOVED FLOORBEAM REPAIR IAW SRM 51-40-02 FABRICATED NEW
- [SDR DALA1031235532](https://openairdocs.org/sdr/DALA1031235532.md): Support · corroded · Nov 14, 2010 · N532US · Boeing 757251 · Fuselage, Seat/Cargo Attach Fittings
  > DURING L-CHECK FOUND CORROSION ON SEAT TRACK SUPPORT AT BS 324 TO BS 418 RBL 0. REPAIRED PER SRM 51-40-05, SRM 51-21-02, SRM 51-120-01.
- [SDR DALA1031225532](https://openairdocs.org/sdr/DALA1031225532.md): Skin · damaged · Nov 10, 2010 · N532US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING M-CHECK SCRIBE LINE DAMAGE FOUND AT S-14R LAP SPLICE FROM BS 1598.75 TO BS 1605.812, WITH (D MIN)=.156" AND (D MAX)=.313"N/R 200/10. SCRIBE LINE DAMAGE FOUND AT S-14R LAP SPLICE FROM BS 1598.750TO BS 1605.812, WITH (D MIN)=.156" AND (D MAX)=.313". THE
- [SDR DALA1030985532](https://openairdocs.org/sdr/DALA1030985532.md): Skin · damaged · Nov 10, 2010 · N532US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING M-CHECK SCRIBE LINE DAMAGE FOUND AT S-14R LAP SPLICE FROM BS 1598.75TO BS 1605.812, WITH (D MIN)=.156" AND (D MAX)=.313" N/R 200/10. DFRD BY BROWN III (D_MIN)=.156" AND (D_MAX)=.313".FOLLOWING NDT INSP TO DETECT CRACKS WERE ACCOMPLISHED: LOCAL SURFACE H
- [SDR DALA1030975532](https://openairdocs.org/sdr/DALA1030975532.md): Skin · damaged · Nov 10, 2010 · N532US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING M-CHECK SCRIBE LINE DAMAGE FOUND AT S-20R LAP SPLICE FROM BS 1452.062 TO BS 1453.687, WITH (D MIN) =.031" AND (D MAX) =.219" N/R 100/12. TASK ELAPSE TIME HRS: 0000.0 RII: N SCRIBE LINE DAMAGE FOUND AT S-20R LAPSPLICE FROM BS 1452.062TO BS 1453.687, WITH
- [SDR DALA1030965532](https://openairdocs.org/sdr/DALA1030965532.md): Floorbeam · corroded · Nov 9, 2010 · N532US · Boeing 757251 · Fuselage Main, Floor Beam
  > DURING M-CHECK FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 377 LBL 60. REPAIRED PER SRM 53-00-51 FIGURE 201, SRM 51-40-05, SRM 51-20-01 & SRM 51-40-02.
- [SDR NWAA081845532](https://openairdocs.org/sdr/NWAA081845532.md): Skin · cracked · Apr 19, 2008 · N532US · Boeing 757251 · Nacelle/Pylon, Plate/Skin
  > DURING "M" CHECK, FOUND CRACK IN NR 2 PYLON SKIN AT NAC STA 132 RT. REPAIRED PER EA 56-212921.
- [SDR 0601875532](https://openairdocs.org/sdr/0601875532.md): Oven · smoke · Aug 26, 2006 · N532US · Boeing 757251 · Buffet/Galleys
  > THE FIRST CLASS (G-1) OVEN BEGAN TO RELEASE SMOKE AFTER BEING TURNED ON. AN ELECTRICAL SMELL WAS NOTICED IN THE COCKPIT AND BY PASSENGERS. THE SMELL DISSIPATED WHEN THE OVEN WAS TURNED OFF. MAINTENANCE INSPECTED THE AREA AND FOUND NO EVIDENCE OF FIRE OR SMOKE
- [SDR 0400615532](https://openairdocs.org/sdr/0400615532.md): Floorbeam · cracked · Apr 28, 2004 · N532US · Boeing 757251 · Fuselage Main, Floor Beam
  > DURING "H" CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 25. REPAIRED PER EA 55-198777.
- [SDR 0201345532](https://openairdocs.org/sdr/0201345532.md): Warning System · false activation · Apr 18, 2002 · N532US · Boeing 757251 · Landing Gear Position and Warning
  > AFTER TAKEOFF WHEN RETRACTING GEAR, CREW RECEIVED LEFT MAIN GEAR DISAGREE AND GEAR DOOR MESSAGE. CREW CYCLED GEAR AND SAME INDICATION REMAINED. FLIGHT RETURNED TO DTW AND COMPLETED AN UNEVENTFUL LANDING. DTW MAINTENANCE PERFORMED OPERATIONAL CHECK PER MM AN
- [SDR 0100585532](https://openairdocs.org/sdr/0100585532.md): Slide · failed · Feb 13, 2001 · N532US · Boeing 757251 · Escape Slide
  > DURING SLIDE SHOP TEST, INFLATABLE SUB ASSEMBLY RUPTURED DURING FLAT FIRE PROCEDURE AT NORMAL OPERATING PRESSURE. INFLATABLE SEAMS FAILED AT UPPER TUBE LEFT AND RIGHT. NEW INFLATABLE SUB ASSEMBLY WAS INSTALLED.
- [SDR 9710865532](https://openairdocs.org/sdr/9710865532.md): Engine · failed · Jun 5, 1997 · N532US · Boeing 757251 · Engine (Turbine/Turboprop)
  > DURING CRUISE FLIGHT, NR 1 ENGINE OIL PRESSURE AND QUANTITY DETERIORATED. AIRCRAFT DIVERTED TO GEG AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED ENGINE FOR OIL LEAKS, NONE FOUND. AIRCRAFT MAINTENANCE FERRIED TO SEA AND REPLACED NR 1 ENGINE.
- [SDR 9709925532](https://openairdocs.org/sdr/9709925532.md): Battery Pack · discharged · May 15, 1997 · N532US · Boeing 757251 · Emergency Lighting
  > DURING PREFLIGHT, FOUND RIGHT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND CHARGER, OPERATIONAL CHECK OK.
- [SDR 9604095532](https://openairdocs.org/sdr/9604095532.md): Oven · dirty · Feb 18, 1996 · N532US · Boeing 757251 · Buffet/Galleys
  > DURING CLIMB WHILE PREPARING MEALS, FLIGHT ATTENDANT REPORTED SMOKE COMING FROM AFT GALLEY LT OVEN. FIRE BOTTLE WAS USED TO EXTINGUISH SMOKE. DECLARED AN EMERGENCY, RETURNED TO DTW, LANDING WAS UNEVENTFUL. UPON AIRCRAFT COMING TO A STOP ON TAXIWAY, CREW INI
- [SDR 9504155532](https://openairdocs.org/sdr/9504155532.md): Skin · damaged · Mar 13, 1995 · N532US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING PERIODIC CHECK, THE FUSELAGE BELLY SKIN BETWEEN FS 660 - 670 AROUND STRINGER 27R WAS FOUND WITH TYPICAL NICK AND GOUGE DAMAGE CAUSED BY CARGO NETS. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 AND NWA EA 55-93840.
- [SDR 9504175532](https://openairdocs.org/sdr/9504175532.md): Skin · damaged · Feb 14, 1995 · N532US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING PERIODIC CHECK, THE FUSELAGE BELLY SKIN BETWEEN FS 1355 - 1410, STR 24L - 26L WAS FOUND WITH NICKS AND GOUGES CAUSED BY CARGO NETS. REMOVED DAMAGED SKIN AND INSTALLED REPAIR PER SRM 53-00-01, FIG 205 AND NWA EA 55-93836.
- [SDR 9504165532](https://openairdocs.org/sdr/9504165532.md): Skin · damaged · Feb 10, 1995 · N532US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING PERIODIC CHECK, NUMEROUS NICKS AND SCRATCHES WERE FOUND ON THE FUSELAGE BELLY SKIN BETWEEN FS 1340 - 1360, STR 26R. DAMAGE WAS CAUSED BY CARGO NETS. INSTALLED REPAIR DOUBLER PER SRM 53-00-01, FIG 204 AND NWA EA 55-93835.

## 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 = 'N532US' AND deregistration_id = 'N532US-2016-06-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N532US-2016-06-22/reports

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