# Service difficulty reports: N632DL, cancelled May 16, 2017

A list on [N632DL, cancelled May 16, 2017](https://openairdocs.org/deregistered/N632DL-2017-05-16.md).

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

- [SDR DALA1243550632](https://openairdocs.org/sdr/DALA1243550632.md): Skin · damaged · Jul 30, 2012 · N632DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION AND FOUND 21 LIGHTNING STRIKES ON THE CROWN OF THE AIRCRAFT BETWEEN BS 540 THROUGH 1440. COMPLIED WITH PERMANENT REPAIR INSTRUCTIONS PER ERA 095258-1 REV ORIG ON NRC 1 THROUGH 17.
- [SDR DALA1243450632](https://openairdocs.org/sdr/DALA1243450632.md): Skin · damaged · Jul 27, 2012 · N632DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FOUND ONE LIGHTNING STRIKE AT BS 600 AND ON S4L. REPAIRED PER ERA 5050791-14 REV 0 AND IS A TIME LIMITED REPAIR.
- [SDR DALA1237050632](https://openairdocs.org/sdr/DALA1237050632.md): Power Supply · inoperative · Jun 12, 2012 · N632DL · Boeing 757232 · Emergency Lighting
  > DURING SERVICE CHECK, MAINTENANCE DISCOVERED EMERGENCY LIGHTS ON SEATS 1-6 INOPERATIVE. MAINTENANCE FOUND M9101 POWER SUPPLY INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY, OPS CHECKED GOOD PER AMM 33-51.
- [SDR DALA1100170632](https://openairdocs.org/sdr/DALA1100170632.md): Skin · damaged · Jan 1, 2011 · N632DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > LOG ITEM J614634-001, POSSIBLE RT SIDE ACFT LIGHTENING STRIKE. ACFT INSPECTED IAW AMM 05-51-19. DAMAGE TRANSFERRED TO NR'S 1 THRU 9. DAMAGE ON N/R'S 1-3 AND 5-9 C/W IAW SRM 53-00-01. DAMAGE ON N/R 4 (STA 418 STR 6L) C/W ON ERA 488577-14.
- [SDR DL757100874](https://openairdocs.org/sdr/DL757100874.md): B-Nut · loose · Apr 10, 2010 · N632DL · Boeing 757232 · Hydraulic System, Main
  > AFTER T/O RAISED GEAR, MAIN GEAR DID NOT RETRACT, NOSE GEAR DID. RAN THE GEAR DISAGREE CHECKLIST, THEN GOT A L HYD QTY EICAS MSG. RAN THAT CHECKLIST. LANDED TAXIED OFF RUNWAY AND NOTED RF W/ DECREASE HYD QUANITY. RAN THAT CHECKLIST AND GOT TOWED TO GATE. DID
- [SDR DL757091928](https://openairdocs.org/sdr/DL757091928.md): Anti-Ice Valve · failed · Dec 4, 2009 · N632DL · Boeing 757232 · Engine Anti-Icing System
  > RT ENG ANTI ICE EICAS MESSAGE WITH SWITCH ON, CIRCUIT BREAKER POPPED, RESET BREAKER, POPPED AGAIN INSPECTED WIRES NO DEFECT NOTED SHOOK DOWN HARNESS AT D42322P. UNABLE TO GET C/B TO POP236039ADEL CLAMP ABOVE A/I VALVE DISCONNECTED, 238039, REMOVED WIRE W5600-3
- [SDR DL757091294](https://openairdocs.org/sdr/DL757091294.md): Tee Fitting · cracked · Aug 1, 2009 · N632DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > REPLACED TEE CLIP 146N8748-17 WITH P/N 146N8748U17 FOR DOOR STOP NR 3 AT L4 DOOR STA 1681.8 REPLACED TEE CLIP 146N8748-21 WITH P/N 146N8748U21 FOR DOOR STOP NR 4 AT L4 DOOR STA 1681.8. REPLACED TEE CLIP 146N8748-18 WITH P/N 146N8748U18 FOR DOOR STOP NR 3 AT
- [SDR DL757060774](https://openairdocs.org/sdr/DL757060774.md): Mount · corroded · Sep 22, 2006 · N632DL · Boeing 757232 · Engine Mount Section
  > DURING THE CURRENT HMV3 CHECK, THE NR 2 PYLON P/N 311N3211 -1 FORWARD ENGINE MOUNT FITTING WAS FOUND WITH FRETTING CORROSION ON THE LOWER SURFACE AROUND THE MOUNT HOLES. PERMANENT REPAIR WAS ACCOMPLISHED PER PRODUCTION PERMIT B757-54-25940PA AND ERA 457245-14
- [SDR DL757060773](https://openairdocs.org/sdr/DL757060773.md): Mount · corroded · Sep 22, 2006 · N632DL · Boeing 757232 · Engine Mount Section
  > DURING THE CURRENT HMV3 CHECK, THE NR 1 PYLON P/N 311N3211-1 FORWARD ENGINE MOUNT FITTING WAS FOUND WITH FRETTING CORROSION ON THE LOWER SURFACE AROUND THE MOUNT HOLES. ACCOMPLISHED PERMANENT REPAIR PER PRODUCTION PERMIT B757-54-25939PA REF ERA 457244-14.
- [SDR DL757060772](https://openairdocs.org/sdr/DL757060772.md): Mount · corroded · Sep 22, 2006 · N632DL · Boeing 757232 · Engine Mount Section
  > NR 2 ENGINE FORWARD LOWER MOUNT FITTING HAD PITTING, REMOVED BY BLENDING. ACCOMPLISHED PERMANENT REPAIR PER PRODUCTION PERMIT B757-71-25751 REF ERA 457048-14.
- [SDR DL757060771](https://openairdocs.org/sdr/DL757060771.md): Mount · corroded · Sep 22, 2006 · N632DL · Boeing 757232 · Engine Mount Section
  > NR 1 ENGINE FORWARD LOWER MOUNT ON PYLON WAS BLENDED TO A DEPTH OF.003 INCHES TO REMOVE DAMAGE. ACCOMPLISHED PERMANENT REPAIR PER ACTS PRODUCTION PERMIT B757-71-25751. REFERENCE ERA 457046-14.
- [SDR DL757060766](https://openairdocs.org/sdr/DL757060766.md): Fitting · damaged · Sep 21, 2006 · N632DL · Boeing 757232 · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON STRUT FITTINGS HAVE ELONGATED HOLES. ACCOMPLISHED PERMANENT REPAIR PER ACTS PRODUCTION PERMIT B757-54-25720. REFERENCE ERA 456938-14.
- [SDR DL757060751](https://openairdocs.org/sdr/DL757060751.md): Skin · cracked · Sep 15, 2006 · N632DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > THE L1 DOOR OPENING, UPPER FORWARD CORNER, HAS A CRACK IN THE FUSELAGE SKIN. THE CRACKED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.
- [SDR DL757060762](https://openairdocs.org/sdr/DL757060762.md): Fitting · oversized · Sep 13, 2006 · N632DL · Boeing 757232 · Nacelle/Pylon, Attach Fittings
  > NR 2 PYLON UPPER LINK WING FITTING WAS FOUND WITH AN INNER LUG DIA. GREATER THAN ALLOWED. THE HOLE WAS OVERSIZED AND INSPECTED. AN OVERSIZED BUSHING WAS INSTALLED. REF AD 2003-18-05
- [SDR DL757060744](https://openairdocs.org/sdr/DL757060744.md): Fitting · misrepaired · Sep 12, 2006 · N632DL · Boeing 757232 · Nacelle/Pylon, Main Frame
  > THE NR 1 PYLON INBOARD MID SPAR FITTING WAS INCORRECTLY OVERSIZED. THE HOLE WAS OVERSIZED TO THE NEXT SIZE FASTENER AND A LARGER FASTENER WAS INSTALLED REF 2003-18-05.
- [SDR DL757060322](https://openairdocs.org/sdr/DL757060322.md): Window · cracked · Apr 24, 2006 · N632DL · Boeing 757232 · Flight Compartment Windows
  > DURING FLIGHT, R-1 WINDOW BEGAN TO ARC AND DELAMINATE. FOLLOW POM PROCEDURES AND TURNED OFF WINDOW HEAT. R-1 WINDOW THEN SPIDER WEB CRACKED. REPLACED R-1 WINDOW, OPS CHECK GOOD.
- [SDR DL757060148](https://openairdocs.org/sdr/DL757060148.md): Circuit Breaker · faulty · Feb 20, 2006 · N632DL · Boeing 757232 · Emergency Lighting
  > EMERGENCY LIGHTS ALONG MAIN AISLE FLOOR ILLUMINATED WITH COCKPIT SW IN ARMED POS AND FLT ATTENDANT PANEL SW IN NORMAL POS. REPLACED C/B TO CHARGER.
- [SDR DL757050222](https://openairdocs.org/sdr/DL757050222.md): Annunciator · shorted · Apr 16, 2005 · N632DL · Boeing 757232 · Flight Compartment Lighting
  > ENTRY DOOR LIGHT ON OVERHEAD INDICATOR PANEL SHORTING OUT AND TRIPPING R IND LIGHT C/B. REMOVED AND REPLACED OVERHEAD IND LIGHT PANEL PER MM, CHECKS OK.
- [SDR DL757040592](https://openairdocs.org/sdr/DL757040592.md): Pin · cracked · Jun 23, 2004 · N632DL · Boeing 757232 · Nacelle/Pylon, Main Frame
  > CRACKS WERE NOTED IN THE FUSE PINS ON THE NR 1 PYLON DIAGONAL BRACE. COMPLIED WITH ERA 091408-14AD.
- [SDR DL757030257](https://openairdocs.org/sdr/DL757030257.md): Actuator · unserviceable · Mar 17, 2003 · N632DL · Boeing 757232 · Drag Control System
  > UNCOMMANDED ROLL TO THE RIGHT. SPOILER MESSAGE DISPLAYED. REPLACED NR 12 SPOILER PCA. ADJUSTED AND TEST PER AMM.
- [SDR DL757020456](https://openairdocs.org/sdr/DL757020456.md): Bottle · inoperative · Apr 19, 2002 · N632DL · Boeing 757232 · Escape Slide
  > EMERGENCY ESCAPE TEST 2 BOTTLE PRESSURE INOP ON RIGHT SIDE. REPLACED BOTTLE ASSY PER M/M, TESTS GOOD.
- [SDR DL757020369](https://openairdocs.org/sdr/DL757020369.md): Switch · faulty · Mar 25, 2002 · N632DL · Boeing 757232 · Cargo Compartment Lighting
  > ON L/O CHECK, AFT CARGO LIGHT SWITCH CAUGHT ON FIRE. REPLACED SWITCH.
- [SDR DL757011048](https://openairdocs.org/sdr/DL757011048.md): Oven · malfunctioned · Jun 23, 2001 · N632DL · Boeing 757232 · Buffet/Galleys
  > F/C AFT OVEN WORKING INTERMITTENTLY, MAY HAVE SEEN SPARKS ABOVE BUN WARMER. OVEN APPEARS TO OPERATE NORMAL AT GATE. FOR PRECAUTION C/B PULLED AND COLLARED. OVEN FWD TO MCO AND PLACARD.
- [SDR DL757001493](https://openairdocs.org/sdr/DL757001493.md): Skin · dented · Aug 7, 2000 · N632DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AND UNDERLYING BEARSTRAP WERE FOUND DENTED AND GOUGED JUST FWD OF THE LOWER AFT CORNER OF THE C2 DOOR. THE DAMAGE WAS REMOVED WITH A 6 X 1 INCH CUTOUT IN THE SKIN AND BEARSTRAP. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND
- [SDR DL757001494](https://openairdocs.org/sdr/DL757001494.md): Skin · lightning strike · Aug 4, 2000 · N632DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH SEVERAL LIGHTNING STRIKE AREAS BETWEEN FS 440 & 460 AND BETWEEN STRINGERS 18R. THE LIGHTNING STRIKES WERE REMOVED WITH 3 SMALL CUTOUTS IN THE SKIN. THE CUTOUTS WERE REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER INSTA
- [SDR DL757992538](https://openairdocs.org/sdr/DL757992538.md): cable frayed · Nov 15, 1999 · N632DL · Boeing 757232 · Stabilizer Control System
  > STAB TRIM LEVERS MOVE WHEN SPEEDBRAKE IS DEPLOYED APPEARS THAT THE LEFT STAB TRIM LEVER BINDS ACTS AS IF THE SPRING IS BROKEN. FOUND STAB TRIM CABLE STB1/STB2 MISROUTED AROUND SPOILER, NO BRAKE CLUTCH ASSY BENEATH STAB TRIM HANDLES CABLE FRAYED. CABLES REPLA
- [SDR DL757960836](https://openairdocs.org/sdr/DL757960836.md): Light · inoperative · Apr 10, 1996 · N632DL · Boeing 757232 · Emergency Lighting
  > FWD RIGHT OVERWING EMERGENCY EXIT TRACK LIGHT SIGN INOP. REPLACED LIGHT ASSY, OPN OK.
- [SDR DL757960449](https://openairdocs.org/sdr/DL757960449.md): Skin · delaminated · Feb 15, 1996 · N632DL · Boeing 757232 · Leading Edge Devices
  > DURING SHOP INSPECTION FOR NR 2 L/E SLAT, FOUND T/E WEDGE DELAMINATED. REPAIRED PER SRM 57-43-02.
- [SDR DL757952988](https://openairdocs.org/sdr/DL757952988.md): Press Controller · malfunctioned · Jul 6, 1995 · N632DL · Boeing 757232 · Cabin Pressure Controller
  > LOG ITEM-CABIN PRESS EICAS MSG RED AND CABIN WARN SOUNDED AT FL 330. EMERG DESCENT ACCOMPLISHED. MANUAL CONT WORKS OK. STATUS MSG CABIN ALT AUTO 1 AND CABIN ALT AUTO 2 CAME ON IN FLT. CORRECTIVE ACTION-NR 1 CONTROLLER FAULTS CONTROLLER AND LOW INFLOW. NR
- [SDR DL757951037](https://openairdocs.org/sdr/DL757951037.md): Actuator · faulty · Mar 8, 1995 · N632DL · Boeing 757232 · Compressor Bleed Control
  > DURING CRUISE, HAD SVA FAILSAFE MSG, NR 2 ENGINE FLAMED-OUT. LANDED RDU. RAN ENGINE PER PFHB TEST 14 SVA, TEST NORMAL. FERRIED AC TO ATL. REPLACED STATOR VANE ACTUATOR, RETURNED TO SERVICE.

## 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 = 'N632DL' AND deregistration_id = 'N632DL-2017-05-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N632DL-2017-05-16/reports

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