# Service difficulty reports: N530US, cancelled Dec 30, 2022

A list on [N530US, cancelled Dec 30, 2022](https://openairdocs.org/deregistered/N530US-2022-12-30.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 · 77 reports

- [SDR DALA2015082105119](https://openairdocs.org/sdr/DALA2015082105119.md): Power Supply · inoperative · Aug 20, 2015 · N530US · Boeing 757251 · Emergency Lighting
  > EMERGENCY LIGHTING INOPERATIVE BETWEEN ROWS 14 AND 23. TROUBLESHOT TO POWER SUPPLY IAW WDM 33-51-13, PP1A, WIP, 262168. REPLACED POWER SUPPLY IAW AMM 33-51-07, OPS CHECKED GOOD IAW AMM.
- [SDR DALA2015081104912](https://openairdocs.org/sdr/DALA2015081104912.md): Duct · blown · Aug 8, 2015 · N530US · Boeing 757251 · Cabin Pressure Control System
  > ATB, OPERATING ON FLIGHT 2245, PERFORMED AN AIR TURNBACK DUE TO LOSS OF PRESSURIZATION AND CABIN ALTITUDE RISING. STATUS MESSAGES WERE "CABIN AUTO INOPERATIVE, CABIN ALT AUTO" AND "CABIN ALT AUTO 2". MAX CABIN ALTITUDE WAS 11K AND OUTFLOW VALVE INDICATED CLO
- [SDR DALA2015071704456](https://openairdocs.org/sdr/DALA2015071704456.md): Battery Pack · inoperative · Jul 15, 2015 · N530US · Boeing 757251 · Emergency Lighting
  > ON SERVICE CHECK, FOUND BULLNOSE EMERGENCY LIGHT AT 4AB INOPERATIVE. FOUND NO POWER AT SOCKET, R & R EMERGENCY LIGHT BATTERY PACK, OPS NORMAL, LIGHTS CHECKED OK.
- [SDR DALA2015071704455](https://openairdocs.org/sdr/DALA2015071704455.md): Battery Pack · inoperative · Jul 15, 2015 · N530US · Boeing 757251 · Emergency Lighting
  > ON SERVICE CHECK, FOUND BULLNOSE EMERGENCY LT AT 1AB INOPERATIVE. FOUND NO POWER AT SOCKET, R & R EMERGENCY LIGHT BATTERY PACK, OPS NORMAL, LIGHTS CK.
- [SDR DALA2015060403586](https://openairdocs.org/sdr/DALA2015060403586.md): Light · unsecure · Jun 2, 2015 · N530US · Boeing 757251 · Emergency Lighting
  > EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. SECURED LIGHT TRACK 1R.
- [SDR DALA14013175530](https://openairdocs.org/sdr/DALA14013175530.md): Structure · cracked · Feb 26, 2014 · N530US · Boeing 757251 · Passenger/Crew Doors
  > L2 DOOR CRACKED AT FWD DOOR HINGE CUTOUTS. REMOVED L2 DOOR IAW AMDS CARD 5211-9001-2L. INSTALLED SERVICEABLE DOOR IAW AMDS CARD 5211-9001-2L. INSTALLED SLIDE IAW AMS CARD 2566-9001-2L. OK FOR SERVICE.
- [SDR DALA14012755530](https://openairdocs.org/sdr/DALA14012755530.md): Cable · inadequate · Feb 25, 2014 · N530US · Boeing 757251 · Passenger/Crew Doors
  > L2 DOOR EMERGENCY POWER ASSIST CABLE TRAVEL INSUFFICIENT. ADJUSTED L2 DOOR POWER ASSIST CABLE TRAVEL. OK FOR SERVICE.
- [SDR DALA13042395530](https://openairdocs.org/sdr/DALA13042395530.md): Connector · loose · Aug 31, 2013 · N530US · Boeing 757251 · Light System Wiring
  > SEAT 4A/B EMERGENCY LIGHT INOPERATIVE AT CURVED EDGE OF STOWAGE BIN CK LIGHT ASSY CHECKED GOOD. RESEATED CONNECTOR ON M731 PWR SUPPLY-NOW OPS CK NML.
- [SDR DALA13040005530](https://openairdocs.org/sdr/DALA13040005530.md): Power Supply · inoperative · Aug 18, 2013 · N530US · Boeing 757251 · Emergency Lighting
  > FWD EMERGENCY EXIT SIGN INOPERATIVE. REPLACED POWER SUPPY M730 IAW AMM 33-51.
- [SDR DALA13038295530](https://openairdocs.org/sdr/DALA13038295530.md): Charger · inoperative · Aug 6, 2013 · N530US · Boeing 757251 · Emergency Lighting
  > EMERGENCY LIGHT IN OVERHEAD BIN ROW 4 A/B INOPERATIVE. R & R BATTERY CHARGER M731 IAW AMM 33-51 OPS CHECKED GOOD.
- [SDR DALA13022585530](https://openairdocs.org/sdr/DALA13022585530.md): Light · inoperative · May 15, 2013 · N530US · Boeing 757251 · Emergency Lighting
  > BULLNOSE EMERGENCY LIGHT INOPERATIVE AT ROW 4AB. R & R EMERGENCY LIGHT ASSY. OPS CHECKED GOOD.
- [SDR DALA13022405530](https://openairdocs.org/sdr/DALA13022405530.md): Ground Stud · loose · May 5, 2013 · N530US · Boeing 757251 · Light System Wiring
  > BULLNOSE EMERGENCY LIGHT AT SEAT 18ABC INOPERATIVE. NO POWER TO LIGHT, FUSES GOOD AT POWER SUPPLY. OTHER LIGHT IN CIRCUIT WORKING, SUSPECT POWER SUPPLY. FOUND RING TERMINAL LOOSE ON GROUND STUD GD475-DC. SECURED GROUND STUD. LIGHT NOW OPS NORMAL. REMO
- [SDR DALA12014755530](https://openairdocs.org/sdr/DALA12014755530.md): Wire · broken · Dec 4, 2012 · N530US · Boeing 757251 · Light System Wiring
  > FLOOR EMERGENCY LIGHT (RED) INOPERATIVE AT DOORS. FOUND BROKEN WIRE AT SPLICE. LIGHTS PARTIALLY DISASSEMBLE. REF SWPM 20-30, REPAIRED WIRING AS REQUIRED. OP TEST EMERGENCY LIGHTS OK. REASSEMBLE TRACK.
- [SDR DALA12005605530](https://openairdocs.org/sdr/DALA12005605530.md): Bearing · seized · Aug 16, 2012 · N530US · Boeing 757251 · Passenger/Crew Doors
  > SHIP 5530, MAINTENANCE DISCOVERED DURING THE DOOR 1L EMERGENCY POWER ASSIST MECH CHECK THAT THE TRIGGER BEARING WAS SEIZED. REPLACED BEARING REF AMM 52-11 RII PROCEDURES C/W.
- [SDR DALA1241015530](https://openairdocs.org/sdr/DALA1241015530.md): Battery Pack · inoperative · Jul 9, 2012 · N530US · Boeing 757251 · Emergency Lighting
  > DURING LAYOVER MAINTENANCE, FOUND EMERGENCY LIGHT ABOVE SEAT 4B IN NOSE INOPERATIVE. MAINTENANCE RELAMPED, REPLACED BATTERY PACK, AND CHARGER M731. OPERATION OF LIGHT NOW CHECKS NORMAL.
- [SDR DALA1234595530](https://openairdocs.org/sdr/DALA1234595530.md): Battery Pack · inoperative · May 29, 2012 · N530US · Boeing 757251 · Emergency Lighting
  > FLIGHT ATTENDANT WROTE UP EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. OPERATIONOF LIGHTS CHECK GOOD PER AMM.
- [SDR DALA1221985530](https://openairdocs.org/sdr/DALA1221985530.md): Power Supply · failed · Apr 7, 2012 · N530US · Boeing 757251 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATH LIGHTS IN ROWS 16-22 INOPERATIVE. MAINTENANCE REPLACED BAD POWER SUPPLY IAW AMM 33-51. OPS TESTED OK.
- [SDR DALA13005655530](https://openairdocs.org/sdr/DALA13005655530.md): Skin · damaged · Jul 26, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE FASTENER DAMAGE, BS 310.5 1.5" BELOW S22R REPLACED BLIND FASTENER WITH PERMANENT REPAIR FASTENER REF TO SRM 53-00-01-2R6, CATEGORY A REPAIR.
- [SDR DALA13005645530](https://openairdocs.org/sdr/DALA13005645530.md): Skin · damaged · Jul 26, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > LIGHTNING FASTENER DAMAGE BS 278 8.5" ABOVE S23R. REPLACED BLIND FASTENER WITH PERMANENT REPAIR FASTENER REF SRM 53-00-01-2R6.
- [SDR DALA13005635530](https://openairdocs.org/sdr/DALA13005635530.md): Skin · damaged · Jul 26, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE FASTENER DAMAGED BS 297 8.75" BELOW S-23L REPLACED BLIND FASTENER WITH PERMENT REPAIR FASTENER REF TO SRM 53-00-01-2R6, CATEGORY A REPAIR.
- [SDR DALA13005625530](https://openairdocs.org/sdr/DALA13005625530.md): Skin · damaged · Jul 26, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE FASTENER DAMAGE BS 310.5 1.5" BELOW S24L. REPLACED BLIND FASTENER WITH PERMANENT REPAIR FASTENER REF TO SRM 53-00-01-2R6, CATEGORY A REPAIR.
- [SDR DALA13005615530](https://openairdocs.org/sdr/DALA13005615530.md): Skin · damaged · Jul 26, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE FASTENER DAMAGE BS 326, S22R. REPLACED BLIND FASTENER WITH PERMENT REPAIR FASTENER REF TO SRM 53-00-01-2R6, CATEGORY A REPAIR.
- [SDR DALA13005605530](https://openairdocs.org/sdr/DALA13005605530.md): Skin · damaged · Jul 26, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE FASTENER DAMAGE BS 348 S22R. REPLACED BLIND FASTENER WITH PERMANENT REPAIR FASTENER REF TO SRM 53-00-01-2R6, CATEGORY A REPAIR.
- [SDR DALA1137465530](https://openairdocs.org/sdr/DALA1137465530.md): Power Supply · inoperative · May 30, 2011 · N530US · Boeing 757251 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ABOVE DOOR 2R INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY PER AMM 33-51-07.
- [SDR DALA2014122306661](https://openairdocs.org/sdr/DALA2014122306661.md): Skin · damaged · Feb 16, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING MAINTENANCE CHECK, INSPECTION FOUND A LIGHTNING STRIKE ON THE FUSELAGE SKIN AT BS 500 BETWEEN S16-17R. THE DAMAGE WAS BLENDED AND FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101. COMPLIED WITH ERA 488999-14, REV ORIGINAL.
- [SDR DALA1110945530](https://openairdocs.org/sdr/DALA1110945530.md): Skin · dented · Feb 15, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > LOWER EXTERIOR FUSELAGE IS DENTED FROM STA 1394 TO STA 1400 BETWEEN STR 29L TO 27R. ACCOMPLISHED ER/A 489003-14 REV ORIGINAL THIS REPAIR IS MAJOR AND PERMANENT. REPAIR APPROVAL IS LIMITED TO 12 MONTHS SERVICE ONLY. ADDITIONAL EA IS REQUIRED FOR CONTINUED SER
- [SDR DALA1110795530](https://openairdocs.org/sdr/DALA1110795530.md): Intercostal · cracked · Feb 15, 2011 · N530US · Boeing 757251 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED BETWEEN STA 1420 TO 1440, RBL 10. REMOVED INTERCOSTAL. REMOVED DAMAGED FLANGE AND PERFORMED HFEC ON CUTOUT FLANGE NO NOTED CRACKS, FABRICATED 1EA REPAIR DOUBLER AND 2EA FILLERS FOR INTERCOSTAL TREATED AND PRIMED AND TOP COATED DOUBLER REPA
- [SDR DALA1110965530](https://openairdocs.org/sdr/DALA1110965530.md): Skin · dented · Feb 14, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING M-CHECK AT WHILE ACCOMPLISHING A PERMANENT BETWEEN STA1695 AND STA1705, S-17L AND S-19L, IT WAS NOTED THAT STR 18L WAS DENTED AT STA 1695. DENT IS LOCATED ON THE SKIN ATTACHMENT FLANGE OF STRINGER. ACCOMPLISHED DURING M-CHECK AT SAT, FEB2011. SECTION
- [SDR DALA1110935530](https://openairdocs.org/sdr/DALA1110935530.md): Skin · dented · Feb 14, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING M-CHECK AT SAT, WHILE ACCOMPLISHING THE PERMANENT REPAIR AT STA 1420, 2 EACH DENTS WERE FOUND ON THE 146N3511-12 SKIN PANEL BETWEEN STA1425 AND STA1430, S-28R AND S-29L. ER/A 488486-14 SECT.I ACCOMPLISHED DURING M-CHECK AT SAT, FEB2011. SECTION II- APP
- [SDR DALA1110815530](https://openairdocs.org/sdr/DALA1110815530.md): Skin · gouged · Feb 14, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > EMPENNAGE EXTERNAL R 2"L AREA OF GOUGE DAMAGE JUST AFT OF HORIZ STAB CUTOUT AND FS 1862.7. ACCOMPLISHED ERA 489457-14 REV ORIG THIS REPAIR WAS CLASSIFIED AS PERMANENT AND MAJOR WITH NO INSP REQUIRED COMPLETED.
- [SDR DALA1111315530](https://openairdocs.org/sdr/DALA1111315530.md): Doubler · damaged · Feb 13, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING M-CHECK OF THE ACFT A DEFERRED ITEM WAS WORKED TO INCORPORATE DL/NWA EA 55-214988 TO INSTALL A PERMANENT REPAIR DOUBLER. DURING INITIAL WORK TO INSTALL EA 55-214988. REPAIR AN UNREPORTED EXISTING SKIN REPAIR WAS FOUND AT BS560-580 S26L-S28L. ER/A 488
- [SDR DALA1110275530](https://openairdocs.org/sdr/DALA1110275530.md): Floorbeam · corroded · Feb 12, 2011 · N530US · Boeing 757251 · Fuselage Main, Floor Beam
  > FLOORBEAM STA 345, LBL-63 TO RBL-63 HAS CORROSION. COMPLIED WITH ERA 489011-14 REV ORIGINAL. THIS REPAIR IS MAJOR & PERMANENT WITH NO FURTHER INSPECTIONS REQUIRED. INSPECTION COMPLETED.
- [SDR DALA1110255530](https://openairdocs.org/sdr/DALA1110255530.md): Floorbeam · corroded · Feb 12, 2011 · N530US · Boeing 757251 · Fuselage Main, Floor Beam
  > FLOORBEAM, STA 324, BL 0, RBL 63 HAS CORROSION. REMOVED CORROSION FROM FLOOR BEAM STA 324, BL-0. FOUND OUT OF LIMITS. REMOVED WEB FROM RBL 24, STA 324 TO STA 345. FLOORBEAM REPAIRED IAW ERA 488481-14, REV D AND REINSTALLED WEB AT RBL24 STA 324 TO STA 345 IA
- [SDR DALA1110265530](https://openairdocs.org/sdr/DALA1110265530.md): Crease Beam · corroded · Feb 11, 2011 · N530US · Boeing 757251 · Fuselage Main, Structure
  > CREASE BEAM ASSY HAS CORROSION STA 1400-1420, RBL 63. COMPLIED WITH ERA 489013-14 REV ORIGINAL. COMPLETED INSPECTION.
- [SDR DALA1114565530](https://openairdocs.org/sdr/DALA1114565530.md): Skin · gouged · Feb 10, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING M-CHECK AN EXISTING FLUSH REPAIR AT STA 1700-1720, S-17R TO S-20R WAS FOUND WITH GOUGES AND TOOLING MARKS AT THE REPAIR LOCATION. ER/A 488988-14 SECTION I ACCOMPLISHED DURING M-CK FEB 11 AT SAT SECTION II REPAIR APPROVAL IS LIMITED TO 50000 TOTAL CYCLES
- [SDR DALA1111445530](https://openairdocs.org/sdr/DALA1111445530.md): Skin · dented · Feb 10, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING M-CK AN EXISTING FLUSH SKIN REPAIR WAS FOUND AT STA 1661 TO STA 1681, S-20R TO S-22R. ADDITIONAL DENTS AND TOOLING MARKS WERE ALSO FOUND. ER/A 488989-14AD SECTION I ACCOMPLISHED DURING M-CK AT SAT FEB 2011. SECTION II REPAIR APPROVAL LIMITED TO 42900
- [SDR DALA1110015530](https://openairdocs.org/sdr/DALA1110015530.md): Skin · damaged · Feb 10, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING M-CHECK AT SAT A FLUSH SKIN REPAIR WAS FOUND AT STA 1661 TO STA 1681, S-20R TO S-22R. ADDITIONAL DENTS AND TOOLING MARKS WERE ALSO FOUND AT THE REPAIR LOCATION. ER/A 488989-14 SECTION I ACCOMPLISHED AT SAT M-CK FEB 2011. SECTION II REPAIR APPROVAL
- [SDR DALA1110235530](https://openairdocs.org/sdr/DALA1110235530.md): Skin · damaged · Feb 9, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN PANEL, STA 1460, STRINGER 26L DAMAGED. DISCONTINUE REVENUE SERVICE ON OR BEFORE 42,200 TOTAL FLIGHT CYCLES PENDING STAGE III DTA APPROVAL. COMPLIED WITH ERA 488480-14AD REV ORIGINAL. TIME LIMITED REPAIR, REPAIR APPROVAL IS LIMITED TO 42,200 TOT
- [SDR DALA1110005530](https://openairdocs.org/sdr/DALA1110005530.md): Skin · dented · Feb 9, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DTA MONITOR INSP, FUSELAGE SKIN PANEL DENTS STA 640 AND STG 15L - 19L. ER/A 488485-14AD WAS APPROVED FOR STAGE I DTA, STATIC STRENGTH, AND IS PENDING STAGE II APPROVAL. THIS APPROVAL IS TEMPORARY FOR ASSOCIATED ER/A 13-488485. THE ER/A 488485-14AD SECTION I
- [SDR DALA1111325530](https://openairdocs.org/sdr/DALA1111325530.md): Doubler · dented · Feb 8, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING M-CHECK, DENT WAS FOUND AT STA 378, S-14L WITHIN SRM LIMITS EXCEPT ONLY 5.4 INCHES FROM THE L-1 DOOR CUTOUT. DENT WAS CUT OUT AND REPAIRED WITH AN EXTERNAL DOUBLER COMPLIED WITH ERA 488990-14 REV ORIGINAL. THIS IS A TIME LIMITED REPAIR. REPAIR APPR
- [SDR DALA1108745530](https://openairdocs.org/sdr/DALA1108745530.md): Skin · dented · Feb 4, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING M-CHECK, A DENT WAS FOUND ON THE FUSELAGE SKIN BETWEEN STA 1500 AND STA 1520 AND S-19L AND S-20L. THE DENT MEASURES 8.0" L X 3.50" W X 0.041" DEEP DENT IS LOCATED NEAR TO THE LAP SPLICE AT S-20L. ER/A SECTION, REPAIR APPROVAL IS LIMITED TO 50,000 TOTA
- [SDR DALA1108735530](https://openairdocs.org/sdr/DALA1108735530.md): Skin · damaged · Feb 4, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > DURING MAINTENANCE CHECK INSPECTION FOUND A LIGHTNING STRIKE ON THE FUSELAGE SKIN AT STA 500 BETWEEN S-16R AND S-17R. THE DAMAGE BLENDED AND FOUND OUT OF LIMITS PER B757-200 SRM 53-00-01, FIG 101 ER/A SECTION I REPAIR APPROVAL IS LIMITED TO 38,633 TOTAL AIRFR
- [SDR DALA1108325530](https://openairdocs.org/sdr/DALA1108325530.md): Skin · dented · Feb 3, 2011 · N530US · Boeing 757251 · Fuselage Main, Plate/Skin
  > FUSELAGE DENT WAS FOUND AT STA 500, S-27R. THE DENT WAS REMOVED BY TRIMMING THE SKIN. REPAIR WAS COMPLETED PER SRM 53-00-01 REPAIR 2 EXCEPT THE REPAIR DOUBLER WAS 0.063" THICK. ER/A SECTION I REPAIR IS APPROVED FOR 12 MONTHS (365 DAYS) ONLY. ADDITIONAL ER/
- [SDR DALA1106675530](https://openairdocs.org/sdr/DALA1106675530.md): Box Beam · corroded · Jan 27, 2011 · N530US · Boeing 757251 · Fuselage Miscellaneous Structure
  > BOX BEAM HAS CORROSION STA 1640-1660, RBL-60. R & R BOX BEAM AT STA FS, STA 1640-1660 RBL-60 IAW SRM 51-40-02, PAGE 1-10.
- [SDR DALA1106655530](https://openairdocs.org/sdr/DALA1106655530.md): Support Angle · corroded · Jan 27, 2011 · N530US · Boeing 757251 · Fuselage Miscellaneous Structure
  > CREASE BEAM TO FLOOR TRANSITION ANGLE HAS CORROSION STA 660-760 RBL-60. R & R CHORD ZEE ANGLE FROM MAIN CABIN STA 660-760, RBL 60 IAW SRM 51-40-02.
- [SDR DALA1106645530](https://openairdocs.org/sdr/DALA1106645530.md): Box Beam · corroded · Jan 27, 2011 · N530US · Boeing 757251 · Fuselage Miscellaneous Structure
  > BOX BEAM HAS CORROSION STA 1660-1680 AT BL-0. R & R BOX BEAM AT FS STA 1660-1680, BL-0 IAW SRM 51-40-02, PAGE 1-10.
- [SDR DALA1106635530](https://openairdocs.org/sdr/DALA1106635530.md): Box Beam · corroded · Jan 27, 2011 · N530US · Boeing 757251 · Fuselage Miscellaneous Structure
  > BOX BEAM HAS CORROSION STA1660-1680, RBL-60. R & R BOXBEAM AT FS STA 1660-1680, RBL-60 IAW SRM 51-40-02.
- [SDR DALA1106425530](https://openairdocs.org/sdr/DALA1106425530.md): Box Beam · corroded · Jan 26, 2011 · N530US · Boeing 757251 · Fuselage Miscellaneous Structure
  > BOX BEAM HAS CORROSION STA 1640-1660, LBL-60 BLENDED. CORROSION FROM BOX BEAM STA 1640-1660, LBL-60 OUT OF LIMITS IAW SRM 53-00-51. R & R BOX BEAM STA 1640-1660, LBL-60 IAW SRM 51-40-02, COMPLETED.
- [SDR DALA1106405530](https://openairdocs.org/sdr/DALA1106405530.md): Box Beam · corroded · Jan 26, 2011 · N530US · Boeing 757251 · Fuselage Miscellaneous Structure
  > BOX BEAM HAS CORROSION STA 1660-1680, LBL-60. REMOVED CORROSION BOX BEAM STA 1660-1680, LBL-60 OUT OF LIMITS IAW SRM 53-00-51, PG:103. R & R BOX BEAM IAW SRM 51-40-02, COMPLETED.
- [SDR DALA1106145530](https://openairdocs.org/sdr/DALA1106145530.md): Floorbeam · corroded · Jan 25, 2011 · N530US · Boeing 757251 · Fuselage Main, Floor Beam
  > FLOORBEAM HAS CORROSION STA 1640, BL-0, RBL-55. REMOVED CORROSION ON FLOORBEAM AT FS STA 1640, BL-0 TO RBL-55, NO CORROSION FOUND. REMOVED CORROSION AT BS 1640 RBL-63. FOUND CORROSION AND DOUBLE HOLES OUT OF LIMITS IAW SRM. REMOVED FLOOR BEAM BS 1640 FROM

Next page: https://openairdocs.org/deregistered/N530US-2022-12-30/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 = 'N530US' AND deregistration_id = 'N530US-2022-12-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N530US-2022-12-30/reports

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