# Service difficulty reports: N531US, cancelled Dec 6, 2018

A list on [N531US, cancelled Dec 6, 2018](https://openairdocs.org/deregistered/N531US-2018-12-06.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 2 · 54 reports

- [SDR DALA2014081804601](https://openairdocs.org/sdr/DALA2014081804601.md): Light · loose · Aug 15, 2014 · N531US · Boeing 757251 · Emergency Lighting
  > DURING PREFLIGHT, FOUND 14 FOOT SECTION OF TRIM OF EMERGENCY LIGHTS IN CABIN LOOSE. EMERGENCY WIRES AND LIGHTS HANGING OUT UNDER TRIM RESECURED WIRING AND LIGHTING AS NEEDED IN TRIM IAW AMM 33-51-00. OPS CHECK OK.
- [SDR DALA2014081804600](https://openairdocs.org/sdr/DALA2014081804600.md): Cover · missing · Aug 13, 2014 · N531US · Boeing 757251 · Emergency Lighting
  > EMERGENCY LIGHT ROWS 20D-25D MISSING WIRE COVERING. REPLACED AND ALL CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR DALA2014081004395](https://openairdocs.org/sdr/DALA2014081004395.md): Socket · inoperative · Aug 8, 2014 · N531US · Boeing 757251 · Emergency Lighting
  > FOUND FLOOR EMERGENCY LIGHTING INOPERATIVE ROWS 20-24, R & R TWO LAMP SOCKETS. OPS NORMAL.
- [SDR DALA14027515531](https://openairdocs.org/sdr/DALA14027515531.md): Coffeemaker · failed · Apr 30, 2014 · N531US · Boeing 757251 · Buffet/Galleys
  > FLIGHT DIVERTED, AN ELECTRICAL ODOR REPORTED IN THE AFT CABIN. MAINTENANCE FOUND RT AFT COFFEEMAKER BAD, REPLACED, OPS CHECKED GOOD.
- [SDR DALA14012015531](https://openairdocs.org/sdr/DALA14012015531.md): Power Supply · inoperative · Feb 25, 2014 · N531US · Boeing 757251 · Emergency Lighting
  > FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY IAW AMM 33-51. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR DALA14011525531](https://openairdocs.org/sdr/DALA14011525531.md): Battery Pack · weak · Feb 20, 2014 · N531US · Boeing 757251 · Emergency Lighting
  > AFT EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK IN AFT GALLEY OVERHEAD NEAR FLIGHT & VOICE DATA RECORDERS IAW AMM 33-51. OPS CHECKED GOOD.
- [SDR DALA14011515531](https://openairdocs.org/sdr/DALA14011515531.md): Battery Pack · inoperative · Feb 20, 2014 · N531US · Boeing 757251 · Emergency Lighting
  > SECTION OF TRACK EMERGENCY LIGHTS INOPERATIVE AT MID FWD CABIN. REPLACED BATTERY PACK. OPS NORMAL.
- [SDR DALA13053005531](https://openairdocs.org/sdr/DALA13053005531.md): Fuse · blown · Oct 17, 2013 · N531US · Boeing 757251 · Emergency Lighting
  > EMERGENCY LIGHT IN FIRST CLASS CABIN INOPERATIVE. REPLACED BLOWN FUSE IN POWER PACK IAW AMM 33-51-07, OPS CHECKED OK.
- [SDR DALA13050605531](https://openairdocs.org/sdr/DALA13050605531.md): Light · loose · Oct 4, 2013 · N531US · Boeing 757251 · Emergency Lighting
  > SEAT 22D, EMERGENCY LIGHT LOOSE. REPAIRED EMERGENCY LIGHT.
- [SDR DALA13050595531](https://openairdocs.org/sdr/DALA13050595531.md): Light · damaged · Oct 4, 2013 · N531US · Boeing 757251 · Emergency Lighting
  > EMERGENCY LIGHT DAMAGED. REPAIRED EMERGENCY LIGHT.
- [SDR DALA13043615531](https://openairdocs.org/sdr/DALA13043615531.md): Skin · dented · Sep 4, 2013 · N531US · Boeing 757251 · Fuselage Main, Plate/Skin
  > FOUND FOUR DENTS, LT SIDE FWD OF L4 DOOR BS 1610 18L DENTS OUT OF LIMITS IAW SRM 53-00-01, FIG 101. CUT OUT DAMAGE IAW SRM 53-00-01, FIG 201. PERFORMED HFEC AND BHEC OF REPAIR CUTOUT AND EXISTING FASTENER HOLES IAW SRM 53-00-01, FIG 201, REPAIR 2, NO CRACKS
- [SDR DALA13034585531](https://openairdocs.org/sdr/DALA13034585531.md): Oven · dirty · Jul 12, 2013 · N531US · Boeing 757251 · Buffet/Galleys
  > SMOKING BURNING PLASTIC ODOR. MX INSPECTED CONFIRMED TWO MEAL CARRIER CONTAINERS CONTAINED BURNED PLASTIC RESIDUE-CARRIERS REMOVED FROM ACFT AND RENDERED UNSERVICEABLE. FURTHER INSPECT OF OVENS NOTED NO CONTAMINATION-HEATED OVENS WITH NO DEFECTS.
- [SDR DALA13019925531](https://openairdocs.org/sdr/DALA13019925531.md): Unknown · odor · Apr 26, 2013 · N531US · Boeing 757251 · Air Distribution System
  > ON ARRIVAL THE LOWER EICAS SCREEN BLANKED AND EICAS DISPLAY CAUTION ILLUMINATED. SHORTLY AFTER DETECTED A MILD PUNGENT ODOR IN THE COCKPIT. LANDED AND PERFORMED SMOKE FUME CHECKLIST. ODOR DISSIPATED BUT THEN RETURNED ON TAXI IN, SHUTDOWN UTILITY BUSS SWITC
- [SDR DALA13012465531](https://openairdocs.org/sdr/DALA13012465531.md): Light · missing · Mar 14, 2013 · N531US · Boeing 757251 · Emergency Lighting
  > LIGHT ASSY FOR EMERGENCY PATH AT FLOOR MISSING AT AFT GALLEY REPLACED AFT EMERGENCY PATH LIGHT ASSY IAW BSWP MANUAL OPS CHECK IAW AMM 33-52.
- [SDR DALA13008175531](https://openairdocs.org/sdr/DALA13008175531.md): Inlet · eroded · Oct 9, 2012 · N531US · Boeing 757251 · Turbine Engine Air Inlet Section
  > ON PDC FOUND NR 1 ENG INLET COWL PAINT ERRODED AT EDGE OF COMPOSITE AT 4 O`CLOCK POS. PERFORMED INTERM REPAIR IAW SRM 54-11-01. REPAIRED NR 1 ENGINE COWL PAINT EROSION IAW 900-3-6, NR 36. OK FOR SERVICE.
- [SDR DALA1239125531](https://openairdocs.org/sdr/DALA1239125531.md): Wire · damaged · Jun 26, 2012 · N531US · Boeing 757251 · Light System Wiring
  > DURING SERVICE CHECK, MAINTENNACE FOUND ROWS 33 TO 38 EMERGENCY LIGHTING INOPERATIVE. FOUND ONE WIRE OUT OF TERMINAL JUNCTION. TERMINATED, RELAMPED AFT 3 SEGMENTS. OPS CHECKED GOOD.
- [SDR DALA1146895531](https://openairdocs.org/sdr/DALA1146895531.md): Power Supply · inoperative · Aug 4, 2011 · N531US · Boeing 757251 · Emergency Lighting
  > DURING A LINE CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHT AT ROWS 14-22, AND THE EMERGENCY EXIT LIGHTS AT DOOR 2L & 2R INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. OPERATIONAL CHECK WAS GOOD.
- [SDR DALA1146885531](https://openairdocs.org/sdr/DALA1146885531.md): Battery Pack · discharged · Aug 4, 2011 · N531US · Boeing 757251 · Emergency Lighting
  > DURING A LINE CHECK, MAINTENANCE FOUND THE CENTER AND RIGHT DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK WAS GOOD.
- [SDR DALA1133005531](https://openairdocs.org/sdr/DALA1133005531.md): Gate · corroded · May 9, 2011 · N531US · Boeing 757251 · Service Doors
  > R2 DOOR LWR GATE HAS CORROSION ON LWR EDGE. REMOVED AND REPLACED LOWER GATE IAW 757 M/M 52-11-38 AND DOOR SEAL IAW 757 M/M 52-09-01. RIG AND ADJUSTMENT GOOD IAW 757 M/M 52-11-00. BLENDED IAW SRM 52-10-07. DETAIL V AND VII FIG 101 SHEET 4 AND 7 OUT OF LIMIT
- [SDR DALA1131955531](https://openairdocs.org/sdr/DALA1131955531.md): Floorbeam · corroded · May 8, 2011 · N531US · Boeing 757251 · Fuselage Main, Floor Beam
  > FLOORBEAM AT STA 324 RBL 43-61 UPPER SURFACE HAS CORROSION. REMOVED CORROSION OUT OF LIMITS PER SRM 53-00-51. REMOVED TEE CHORD SRM 51-40-02. FABRICTED NEW TEE CHORD AND REP SPLICES ON STAM TRAVELER, FABRICATED REPAIR STRAPS PER ER/A 491292-14. DRILLED TEE
- [SDR DALA1131945531](https://openairdocs.org/sdr/DALA1131945531.md): Stringer · corroded · May 6, 2011 · N531US · Boeing 757251 · Fuselage Main, Longeron/Stringer
  > FWD PIT STRINGER S24L, 6 INCH FWD OF FRAME STA 760 IS CORRODED. CHECKED LIMITS, L=4.0" W=1.0"D=0.040" ORIG MAT 0.080 INCH OUT OF LIMITS IAW SRM 53-30-03 FIG 101 DET.II. FABRICATED STRINGER ON T11/879142, FABRICATED STRINGER SPLICE ON T11/879141 IAW SRM 53-00
- [SDR DALA1131935531](https://openairdocs.org/sdr/DALA1131935531.md): Gate · corroded · May 6, 2011 · N531US · Boeing 757251 · Service Doors
  > R4 DOOR LWR GATE HAS CORROSION ON FWD AND AFT CORNER. BLENDED FWD AND AFT LOWER CORNER OF R-4 IAW SRM 51-10-02 DIMENSIONS OF DAMAGE FWD EDGE L=.805 W=.260 D=.105 AFT EDGE L=.895, W=.235, D=.120 OUT OF LIMITS IAW SRM 51-10-02 FIG 10, DETAIL VII. REMOVED AND R
- [SDR DALA1131225531](https://openairdocs.org/sdr/DALA1131225531.md): Floorbeam · corroded · May 3, 2011 · N531US · Boeing 757251 · Fuselage Main, Floor Beam
  > DURING HMV CHECK AT BFM, INSPECTION FOUND CORROSION LOCATED ON THE UPPER SURFACE OF BS 324 FLOORBEAM UPPER CAP ER/A 491292-14 SECTION I-ACCOMPLISHED DURING MCK AT BFM, MAY2011 ER/A SECTION II-PENDING FOR DTA RESULT WITHIN 24 MONTHS (730 DAYS) FROM 28-APR-2011.
- [SDR DALA1130495531](https://openairdocs.org/sdr/DALA1130495531.md): Seat Track · gouged · May 1, 2011 · N531US · Boeing 757251 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK INST ON N/R 240/4, FOUND 1EA GOUGED AT FLOOR BEAM STA 1100 UPPER CHORD LOWER SURFACE LBL 46. REMOVED DAMAGE AND FOUND OUT OF LIMITS. REMOVED SEAT TRACK, CUSP WEBS AND CREASE BEAM, BATH TUB FITTINGS TO FOM IAW SRM 51-40-02. FAB FLOORBEAM DWG 1444
- [SDR DALA1130235531](https://openairdocs.org/sdr/DALA1130235531.md): Skin · chafed · Apr 30, 2011 · N531US · Boeing 757251 · Leading Edge Devices
  > NR 8 SLAT T/E LWR SKIN CHAFED. REMOVED DAMAGED SKIN, REMOVED CORE, FABRICATED REPAIR PARTS AND BONDED IAW SRM 57-43-01, FIG 1 & 51-70-10, FIG 202 SHT NR 8 REPAIR NR4 R & R SLAT IAW MM 27-81-02. OPS CHECK ON NR 22, ZONE 520. PAINTED IAW MM 51-24-13. EXT. DOU
- [SDR DALA1129565531](https://openairdocs.org/sdr/DALA1129565531.md): Intercostal · corroded · Apr 27, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous Structure
  > FLOORBEAM VERTICAL INTERCOSTAL BET STA 345-365, RBL 47 HAS CORROSION AS MARKED. BLENDED AREA & REMOVED CORR IAW SRM 51-10-02. OUT OF LIMITS IAW SRM 53-00-51, FIG 101, SHEET 3. REMOVED FLOOR SUPPORT BEAM VERTICAL INTERCOSTAL IAW SRM 51-40-02 & 3 EA ANGLES FABR
- [SDR DALA1129555531](https://openairdocs.org/sdr/DALA1129555531.md): Intercostal · corroded · Apr 27, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous Structure
  > RT DOOR ENTRANCE VERTICAL INTERCOSTAL AT STA 345-365 UPPER & LWR SURFACE HAS CORROSION SEVERAL PLACES AROUND HOLES, AS MARKED. REMOVED CORROSION IAW SRM 51-10-01 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. REMOVED DOOR ENTRANCE (RT) VERTICAL INTERCOSTAL IAW
- [SDR DALA1129545531](https://openairdocs.org/sdr/DALA1129545531.md): Floor Support · corroded · Apr 27, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous Structure
  > PAX CABIN FLOOR SUPPORT BEAM BL "O" BTW STA 1640 AND STA 1660 HAS CORROSION. REMOVED CORROSION IAW SRM 53-00-51 OUT OF LIMITS. REMOVED SUPPORT IAW SRM 51-40-02, FABRICATED NEW SUPPORT ON STAM TRAVELER T11/878285 LOCATED, DRILLED IAW SRM 51-40-05 AND TREATED
- [SDR DALA1129535531](https://openairdocs.org/sdr/DALA1129535531.md): Floorbeam · corroded · Apr 27, 2011 · N531US · Boeing 757251 · Fuselage Main, Floor Beam
  > FLOORBEAM UPPER & LWR SURFACE AT STA 345, RBL 2, RBL 50 HAS CORROSION SEVERAL PLACES AS MARKED. BLENDED CORRODED IAW SRM 53-00-51 OUT OF LIMITS CUT FLOORBEAM TOP CAP AT STA 345 IAW SRM 53-00-51, FIG 201, FABRICATED REPAIR PARTS LOCATED & DRILLED REPAIR IAW
- [SDR DALA1129525531](https://openairdocs.org/sdr/DALA1129525531.md): Floorbeam · corroded · Apr 27, 2011 · N531US · Boeing 757251 · Fuselage Main, Floor Beam
  > PAX CABIN FLOOR STA 1640, RBL 29" HAS CORROSION. BLENDED CORRODED OUT OF LIMITS. REMOVED DAMAGE SECTION OF BEAM IAW SRM 53-00-51, FIG 201, FAB. REPAIR PARTS, CHORD LOC. & DRILLED IAW SRM 51-40-05, TREATED & PRIMED AND PAINTED IAW SRM 51-20-01. INSTALLED REPA
- [SDR DALA1129515531](https://openairdocs.org/sdr/DALA1129515531.md): Floor Support · corroded · Apr 27, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous Structure
  > PAX CABIN FLOOR STA 1660, RBL 48" HAS CORROSION REMOVED CORROSION IAW SRM 53-00-51 L=2.9 W=1.95, D=.020 MAT..125 OUT OF LIMITS. DETAIL III, CUT OUT DAMAGED AREA IAW SRM 53-00-51, REPAIR 5, FABRICATED NEW PART LOC & DRILLED TEE IAW SRM 53-00-51 INSTALLED TEE
- [SDR DALA1129505531](https://openairdocs.org/sdr/DALA1129505531.md): Floorbeam · corroded · Apr 27, 2011 · N531US · Boeing 757251 · Fuselage Main, Floor Beam
  > FLOORBEAM AT STA 377.7, LBL 60 TO RBL 6 UPPER & LOWER SURFACE HAS CORROSION SEVERAL PLACES AS MARKED. REMOVED CORROSION, OUT OF LIMITS, REMOVED TOP CAP OF FLOORBEAM FROM STA 377, LBL 5- RBL 60 IAW SRM 53-00-51, FIG 201, SH 1 FABRICATED REPAIR PARTS IAW SRM 5
- [SDR DALA1129465531](https://openairdocs.org/sdr/DALA1129465531.md): Sill · corroded · Apr 27, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT, NR 3 LT EMERGENCY EXIT LOWER SILL AT STA 1347 AROUND FASTENER HOLE CORRODED BLENDED AREA IAW SRM 51-10-02 OUT OF LIMITS IAW SRM 53-60-15, FIG 101 DETAIL VI. R & R WITH NEW CHORD IAW SRM 51-40-02.
- [SDR DALA1128875531](https://openairdocs.org/sdr/DALA1128875531.md): Sill · corroded · Apr 26, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT NR 3 RT EMERGENCY EXIT LOWER SILL AT ST6A 1343 CORRODED AROUND NUT PLATE. R & R CREASE BEAM AT NR 3 RT EMERGENCY EXIT STA 1343 IAW SRM 51-40-02. DAMAGE DIM; L=3.40 W=1.10 D=.046 ORIG THICKNESS.100 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15, FI
- [SDR DALA1128685531](https://openairdocs.org/sdr/DALA1128685531.md): Floor Panel · damaged · Apr 25, 2011 · N531US · Boeing 757251 · Fuselage Floor Panel
  > PAX CABIN FLOOR, STA 1660, RBL 10" HAS TOOL MARKED. BLENDED IAW SRM 53-00-51, ORIG.125, L=5.0, W=2.0, D=.017 OUT OF LIMITS. REMOVED DAMAGE AREA IAW SRM 53-00-51, FABRICATED PARTS, TREATED, PRIMED AND TOPCOATED IAW SRM 51-20-01 & AMM 51-20-10. INSTALLED REP
- [SDR DALA1128675531](https://openairdocs.org/sdr/DALA1128675531.md): Intercostal · corroded · Apr 25, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous Structure
  > FLOORBEAM VERTICAL INTERCOSTAL BETWEEN STA 345-365 RBL 26 HAS CORROSION. REMOVED FLOORBEAM VERTICAL FABRICATED NEW FLOORBEAM VERTICAL IAW TRAVELER T11/878541 PER DWG 141N5160. INSTALLED FLOORBEAM VERTICAL IAW SRM 51-40-02 (DUE TO CRACK).
- [SDR DALA1128195531](https://openairdocs.org/sdr/DALA1128195531.md): Seat Track · corroded · Apr 24, 2011 · N531US · Boeing 757251 · Fuselage, Seat/Cargo Attach Fittings
  > LT INBD SEAT TRACK CROWN, STA 1110 CORRODED OUT OF LIMITS. REMOVED SEAT TRACK IAW SRM 51-40-02 FABRICATED ON STAM TRAVELER T11/878418, MAT BAC 1520-792, BATCH 001704665 IAW SRM 53-00-52. LOCATED & DRILLED IAW SRM 51-40-05. TREATED & PRIMED IAW SRM 51-20-01.
- [SDR DALA1128175531](https://openairdocs.org/sdr/DALA1128175531.md): Floor Support · corroded · Apr 24, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous Structure
  > FLOORBEAM VERTICAL INTERCOSTAL STA 324-345, RBL 41 UPPER & LOWER SURFACE HAS CORROSION SEVERAL PLACES. REMOVED CORROSION FROM AREA IAW SRM 51-10-02, BLENDED AREA L=2.0, W=2.0 D=.010 ORIG MAT THICKNESS.038 OUT OF LIMITS AT.021 IAW SRM 53-00-51. REMOVED INTE
- [SDR DALA1128155531](https://openairdocs.org/sdr/DALA1128155531.md): Floorbeam · damaged · Apr 21, 2011 · N531US · Boeing 757251 · Fuselage Main, Floor Beam
  > FLOORBEAM, STA 377.7 REWORKED, 2 EA SUPPORT ANGLES, BL0 NEED TO BE FABRICATED TO FACILITATE REPAIR. FABRICATED ANGLES 2EA ON STAM TRAVELER T11/879680 DWG 141N5 130, BATCH3, 001848807 MAT 7075-063. FABRICATED 2 EA FILLER MAT 7075-T6.071 IAW SRM 51-10-02. I
- [SDR DALA1128185531](https://openairdocs.org/sdr/DALA1128185531.md): Seat Track · corroded · Apr 20, 2011 · N531US · Boeing 757251 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK UPPER SURFACE AT STA. 377.7, LBL 25 FWD HAS CORROSION. BLENDED SEAT TRACK & CHECKED LIMITS L=2.50 W=1.00D=0.120 OUT OF LIMITS IAW SRM 53-00-52, FIG 101. R & R SEAT TRACK IAW SRM 51-40-02. FABED SEAT TRACK ON STAM TRAVELER T11/878419, PN BA
- [SDR DALA1128165531](https://openairdocs.org/sdr/DALA1128165531.md): Intercostal · corroded · Apr 20, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous Structure
  > RTB DOOR ENTRANCE VERTICAL INTERCOSTAL BETWEEN STA 62, UPPER & LOWER SURFACE & AROUND NUTPLATES HAS CORROSION SEVERAL PLACES AS MARKED. R & R SUPPORT IAW SRM 51-40-02. FAB NEW SUPPORT ON STAM TRAVELER T11/878290 IAW DWG 141N5170. RETAIN FOR RECORDS.
- [SDR DALA1126435531](https://openairdocs.org/sdr/DALA1126435531.md): Intercostal · corroded · Apr 16, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous Structure
  > FLOORBEAM VERTICAL, INTERCOSTAL AT STA 395 RBL 19.5 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-01 OUT OF LIMITS IAW SRM 53-00-51 ORIG MAT..040. NEW PART FABBED ON STAM TRAVELER T11/878529 MAT BAC-1508-238/70 75-T-65H, BATCH 3 0001962671. LOCATED & DR
- [SDR DALA1126425531](https://openairdocs.org/sdr/DALA1126425531.md): Sill · corroded · Apr 16, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT AT STA 1420 UPPER FRAME ADJACENT TO DOOR SILL CHANNEL SUPPORT HAS CORROSION. REMOVED SHEAR CLIP IAW SRM 51-40-02, REMOVED CORR ORIG.040, REMOVED.020,.020 REMAINING OUT OF LIMITS IAW SRM 53-00-53, FABBED NEW SHEAR CLIP ON TRAVELER T11/878861
- [SDR DALA1126415531](https://openairdocs.org/sdr/DALA1126415531.md): Intercostal · corroded · Apr 16, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous Structure
  > FLOORBEAM VERTICAL INTERCOSTAL AT STA 365-377 RBL 44 UPPER SURFACE HAS CORROSION AT MARKED. FOUND OUT OF LIMITS IAW SRM 53-00-51 FIG 101 ORIGINAL MAT'L.053 LOSS MAT'L.014, REMAINING MAT'L.039, REMOVED BEAM & ANGLES. RECEIVED PART (BEAM) DA-141N5185-24 ON
- [SDR DALA1126405531](https://openairdocs.org/sdr/DALA1126405531.md): Vertical Support · corroded · Apr 15, 2011 · N531US · Boeing 757251 · Cargo/Baggage Doors
  > AFT CARGO DOOR LOWER INNER STRUCTURE NR 2 FROM FWD VERT SUPPORT BRACKET INR & OUTER SKIN CORRODED. REMOVED BRACKET IAW SRM 51-40-02, REMOVED CORR IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02 FIG 101. FABBED PART IAW TRAVELER T11/878611 DWG 14
- [SDR DALA1125525531](https://openairdocs.org/sdr/DALA1125525531.md): Floor Support · corroded · Apr 12, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE AT STA 433-LBL 63 UPPER SURFACE HAS CORROSION, AS MARKED. REMOVED SUPPORT ANGLE IAW SRM 51-40-02. FABRICATED SUPPORT ANGLE ON STAM TRAVELER T11/878440. LOCATED AND DRILLED SUPPORT ANGLE IAW SRM 51-490-08. TREATED, PRIMED AND TOP COATED SU
- [SDR DALA1125405531](https://openairdocs.org/sdr/DALA1125405531.md): Plate · corroded · Apr 11, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT METAL PLATE AT STA 365 RBL 26.5 UPPER SURFACE HAS CORROSION, AS MARKED. REMOVED CORROSION IAW SRM 51-10-02.CHECKED LIMITS: L=4.0 W=4.0 D=0.012. ORIGINAL OUT OF LIMITS IAW SRM 53-00-51. REMOVED METAL PLATE IAW SRM 51-40-0 2. FABBED NEW
- [SDR DALA1127675531](https://openairdocs.org/sdr/DALA1127675531.md): Skate Angle · damaged · Oct 11, 2010 · N531US · Boeing 757251 · Nacelle/Pylon, Main Frame
  > IAW ERA 486416-14, SECTION II REPEAT CHECK AND SECTION III PERMANENT REPAIR IS REQUIRED ON THE NR1 PYLON INBD SKATE ANGLE ACCOMPLISH SECTION II. R & R RIVET IAW SECTION III. PERMANENT REPAIR. REQUEST THIS LOG PAGE BE CLOSED & MONITOR REMOVED. SIGNED, MONI
- [SDR DALA1010005531](https://openairdocs.org/sdr/DALA1010005531.md): Skin · damaged · May 14, 2010 · N531US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING LINE CHECK FOUND DAMAGE TO FUSELAGE SKIN AT BS 1475 S10L. REPAIRED IAW SRM 53-00-01, FIGURE 201 AND ERA 482513-14.
- [SDR NWAA073325531](https://openairdocs.org/sdr/NWAA073325531.md): Controller · malfunctioned · Sep 30, 2007 · N531US · Boeing 757251 · Cabin Temperature Controller
  > DURING CLIMB-OUT FROM DTW, CABIN AND FLIGHT DECK BECAME VERY HOT. COM PROCEDURE TO ALLEVIATE HEAT COMING FROM PACK WAS INEFFECTIVE. EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO DTW FOR A UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED 2 TEMP SENSORS

Next page: https://openairdocs.org/deregistered/N531US-2018-12-06/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 = 'N531US' AND deregistration_id = 'N531US-2018-12-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N531US-2018-12-06/reports

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