# Service difficulty reports: N630DL, cancelled May 16, 2017

A list on [N630DL, cancelled May 16, 2017](https://openairdocs.org/deregistered/N630DL-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 DALA1130440630](https://openairdocs.org/sdr/DALA1130440630.md): Connector · damaged · May 2, 2011 · N630DL · Boeing 757232 · Light System Wiring
  > DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHTS AT SEATS 19 - 22 INOPERATIVE. MAINTENANCE REPAIRED THE CONNECTOR AT SEAT 22. OPERATIONAL CHECK WAS GOOD.
- [SDR DALA1127980630](https://openairdocs.org/sdr/DALA1127980630.md): Connector · damaged · Apr 20, 2011 · N630DL · Boeing 757232 · Emergency Lighting
  > DURING A LAYOVER CHECK, MX FOUND THE EMERGENCY PATHLIGHTS AT SEATS 19DEF THROUGH 22DEF INOPERATIVE. MX REPAIRED A CONNECTOR. OPS CHECK WAS GOOD.
- [SDR DALA1030140630](https://openairdocs.org/sdr/DALA1030140630.md): Light · inoperative · Oct 28, 2010 · N630DL · Boeing 757232 · Emergency Lighting
  > DURING LAYOVER CHECK MAINTENANCE FOUND SEAT 4CD EMERGENCY LIGHT ON THE SIDE PANEL TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND FOLLOW UP CHECK SHOWED LIGHT WAS NOW OPERATIONAL. (2010-D1306) (DL757103000)
- [SDR DL757092025](https://openairdocs.org/sdr/DL757092025.md): Bulb · inoperative · Dec 21, 2009 · N630DL · Boeing 757232 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS INOP AT R2 DOOR. BOTH LT AND RT OVERWING AFT LOCATIONS. AND BOTH L3 AND R3 DOORS AND INTERIOR AT ROW 45. RELAMPED ALL LOCATIONS. LIGHTS CHECK GOOD EL.
- [SDR DL757091010](https://openairdocs.org/sdr/DL757091010.md): Tee Fitting · cracked · Jun 8, 2009 · N630DL · Boeing 757232 · Fuselage Main, Attach Fittings
  > WHILE WORKING EA06-465922-03AD REV B ME-02 OPN0201, FOUND L4 DOOR NR 3 STOP FITTING SUPPORT TEE CRACKED AT RADIUS.
- [SDR DL757090866](https://openairdocs.org/sdr/DL757090866.md): Acoustic Panel · delaminated · May 15, 2009 · N630DL · Boeing 757232 · Engine Cowling System
  > DURING SHOP VISIT, LARGE DELAMINATIONS WERE FOUND ON (PN 314N3011-4)ENGINE INLET ACOUSTIC PANEL, REQUIRING REPLACEMENT OF THE DELAMINATED SKINS. REPAIRED IAW ERA 474813-14.
- [SDR DL757060821](https://openairdocs.org/sdr/DL757060821.md): Controller · malfunctioned · Oct 4, 2006 · N630DL · Boeing 757232 · Cabin Pressure Controller
  > AC DID AN EMERGENCY DECENT DO TO LOSS OF CONTROL OF CABIN IN AUTO.5. NO FAULTS ON CABIN PRESS CONT 1 OR 2. ALL DOOR SEALS GOOD OVER PRESS VLVS NORMAL. REPLACED NR 1 CABIN PRESS CONTROLLER. PRESSURIZED SYS. PRESSURIZATION WAS GOOD DECAY RATE NORMAL
- [SDR DL757060587](https://openairdocs.org/sdr/DL757060587.md): Warning Light · unknown · Jul 15, 2006 · N630DL · Boeing 757232 · Central Warning
  > INTERMITTENT WHEEL WELL FIRE WARNING. PNEUMATIC DUCT REPLACED. FIRE CONTROL CARD REPLACED. ILSN VALVE REPLACED.
- [SDR DL757060571](https://openairdocs.org/sdr/DL757060571.md): Circuit Board · faulty · Jul 10, 2006 · N630DL · Boeing 757232 · Passenger Compartment Lighting
  > FOUND READING LIGHT AT 28B BURNED OUT, HAD SMOKE AND ELECTRICAL SMELL. REPLACED CARD AND SWITCH. CHECKS GOOD. MCO AND PLACARD REMOVED.
- [SDR DU4R2006528](https://openairdocs.org/sdr/DU4R2006528.md): Frame · corroded · Jun 27, 2006 · N630DL · Boeing 757200 · Fuselage Main, Frame
  > CORROSION LEFT LOWER WING TO BODY FAIRING STRUCTURE BS 1037 BL 7 TO BL 30L. REMOVED CORRODED SECTION BL 7L TO BL 29L BS 1037. FABRICATED AND INSTALLED REPAIR PLATES 11-5/8" X 1-1/8" FROM 7075-T6.063, 11-5/8" X 1-1/8" FROM 7075-T6.050 AND EXTRUSION 21-3/4"
- [SDR DU4R2006530](https://openairdocs.org/sdr/DU4R2006530.md): Fitting · corroded · Jun 25, 2006 · N630DL · Boeing 757200 · Fuselage Main, Attach Fittings
  > TWO CHORD FITTINGS CORRODED IN CABIN FRAME BS 1720, RBL 56 S-17R. REMOVED AND REPLACED 2 EA CHORD FITTINGS P/N 146N8722-16 AND 146N8726U2 IAW B757 SRM 51-10-2, 51-40-02, 51-20-01, 53-80-08 FIG 101 AND BOEING DWG 146N8722.
- [SDR DU4R2006529](https://openairdocs.org/sdr/DU4R2006529.md): Fitting · corroded · Jun 25, 2006 · N630DL · Boeing 757200 · Fuselage Main, Bulkhead
  > TWO CORRODED AND ELONGATED HOLES IN TEE CHORD AT AFT PRESSURE BULKHEAD P/N 146N8726U2 AND 146N8722-16 BS 1720 RBL 57. OVERSIZED 2 EA HOLES AND INSTALLED FREEZE PLUGS IN UPPER HOLE AND INSTALLED OVERSIZED BOLT IN LOWER HOLE, INSTALLED NEW TEE FITTING IAW B757
- [SDR DU4R2006501](https://openairdocs.org/sdr/DU4R2006501.md): Transition Panel · corroded · Jun 23, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > S/O 292018 NR 23829 CORROSION AFT PIT RT TRANSITION PANEL 1460 - 1530. REMOVED CORRODED PANEL. DRILLED ATTACHMENT HOLES AND INSTALLED NEW PANEL P/N 146N5391-51 IAW B757 SRM 51-40-2.
- [SDR DU4R2006498](https://openairdocs.org/sdr/DU4R2006498.md): Transition Panel · corroded · Jun 21, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT PIT TRANSITION PANEL BS 1310 - 1380 RT. FABRICATED AND INSTALLED TRANSITION PANEL SPLICE 10 X 10 INCHES FROM 7075-T6.071" IAW SRM 53-60-53D.
- [SDR DU4R2006506](https://openairdocs.org/sdr/DU4R2006506.md): Floor Support · corroded · Jun 20, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > S/O 291018 NR 23848 CORROSION AROUND FASTENER HOLES ON FLOOR SUPPORT AFT PIT BS 1490 TO 1520, RBL 3. FABRICATED AND INSTALLED REPAIR CHANNEL 211/2 INCHES FROM BAC1510-1087 AND L-ANGLE 5-1/2 INCHES FROM 7075-T6.080 B757 SRM 53-60-53 FIG 206.
- [SDR DU4R2006505](https://openairdocs.org/sdr/DU4R2006505.md): Floor Support · corroded · Jun 20, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > S/O 291018 NR 23847 CORROSION AROUND FASTENER HOLES ON FLOOR SUPPORT AFT PIT BS 1500 TO 1523, LBL 3. FABRICATED AND INSTALLED REPAIR CHANNEL 31 INCHES FROM BAC1510-1087 AND L-ANGLE 6 INCHES FROM 7075-T6.080 B757 SRM 53-60-53 FIG 206.
- [SDR DU4R2006504](https://openairdocs.org/sdr/DU4R2006504.md): Floor Support · corroded · Jun 20, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > S/O 291018 NR 23846 CORROSION AROUND FASTENER HOLES ON FLOOR SUPPORT AFT PIT BS 1500 TO 1520, LBL 7. FABRICATED AND INSTALLED REPAIR CHANNEL 19 INCHES FROM BAC1510-1087 AND L-ANGLE 5 INCHES FROM AND10136-2001 IAW B757 SRM SRM 53-60-53 FIG 206.
- [SDR DU4R2006500](https://openairdocs.org/sdr/DU4R2006500.md): Transition Panel · corroded · Jun 18, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION ON RT TRANSITION PANEL IN AFT PIT BS 1530 TO BS 1640. ROUTED OUT CORRODED AREAS IAW B757 MM 53-88-01-801. FABRICATED AND INSTALLED 2 EACH REPAIR DOUBLERS 9.0 X 7.25 AND 6 X 3.0 INCHES FROM 2024-T3.071" IAW B757 SRM 53-88-01-801.
- [SDR DU4R2006509](https://openairdocs.org/sdr/DU4R2006509.md): Seat Track · corroded · Jun 16, 2006 · N630DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > S/O 291018 NR 23985 CORROSION ON CABIN SEAT TRACK AT OUTBD SIDE FLOOR PANEL ATTACH FLANGE BS 1117 RBL 47. FABRICATED AND INSTALLED SEAT TRACK REPAIR 106 X 3-1/2 FROM BAC1520-792 IAW B757 SRM 51-40-02.
- [SDR DU4R2006503](https://openairdocs.org/sdr/DU4R2006503.md): Angle · corroded · Jun 15, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > S/O 291018 NR 23842 CORROSION IN AFT PIT BS 1470 TO 1475, RBL 12 AROUND NUTPLATE HOLES, ANGLE. REMOVED CORRODED ANGLE. DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED NEW ANGLE IAW B757 SRM SRM 51-40-02, 51-00-53 AND 51-20-01.
- [SDR DU4R2006502](https://openairdocs.org/sdr/DU4R2006502.md): Intercostal · corroded · Jun 15, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > S/O 291018 NR 23839 CORROSION IN AFT PIT BS 1478 INTERCOSTAL WEB RBL-11. FABRICATED AND INSTALLED INTERCOSTAL WEB 20.5" X 8.5" FROM 7075-T6.040 IAW B757 SRM 51-40-02, 53-60-04 FIG. 101.
- [SDR DU4R2006510](https://openairdocs.org/sdr/DU4R2006510.md): Fitting · corroded · Jun 14, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > S/O 291018 NR 24021 CORROSION ON CABIN CREASE BEAM UPPER FITTING AT BS 1720 BULKHEAD. REMOVED AND REPLACED FITTING P/N 146N8726U2 IAW B757 SRM 51-40-02.
- [SDR DU4R2006499](https://openairdocs.org/sdr/DU4R2006499.md): Strap · chafed · Jun 14, 2006 · N630DL · Boeing 757232 · Fuselage Main, Frame
  > CABIN FRAME STA 1640 S-10R CHORD/STRAP CHAFED. FABRICATED AND INSTALLED REPAIR STRAP FROM 7075-T6 IAW BOEING DWG 146N8738 REV V DATED 2-12-02 IAW B757 SRM 51-40-2.
- [SDR DU4R2006490](https://openairdocs.org/sdr/DU4R2006490.md): Transition Panel · corroded · Jun 13, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION FWD PIT LT TRANSITION PANEL BS 510 - 644. INSTALLED NEW TRANSITION PANEL P/N 143N366Y83 IAW B757 SRM 53-30-53 FIG 1, 53-00-53 FIG 101, 51-40-05 FIG 2, 3, 4 AND 51-40-02 PG 2 & 3.
- [SDR DU4R2006496](https://openairdocs.org/sdr/DU4R2006496.md): Shim · corroded · Jun 12, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION AT CABIN FLOOR SUPPORT BS 1676 BL 0. REMOVED CORROSION. SHIM OUT OF LIMITS. FABRICATED AND INSTALLED SHIM 2 X 15.75 INCHES FROM 7075-T6.125" IAW B757 SRM 51-30-01, 51-20-01 AND 51-40-02.
- [SDR DU4R2006489](https://openairdocs.org/sdr/DU4R2006489.md): Skin · corroded · Jun 12, 2006 · N630DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > CORROSION LOWER FUSELAGE EXT SKIN AROUND FWD FASTENER HOLES OF PANEL 191AL BL 0 - LBL 17. FABRICATED AND INSTALLED REPAIR DOUBLER 10.4 X 8.3 INCHES FROM 20-24-T3.100 IAW B757 SRM 53-00-01 FIG 201 REPAIR 3 AND 51-20-01.
- [SDR DU4R2006492](https://openairdocs.org/sdr/DU4R2006492.md): Skin · corroded · Jun 10, 2006 · N630DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > CORROSION FWD CARGO FUSELAGE INTERNAL SKIN SURFACE B/O 0 BS 660. FABRICATED AND INSTALLED FUSELAGE SKIN REPAIR 8.3 X 7.75 INCHES FROM 2024-T3.063 IAW B757 SRM 53-30-01 FIG 1, 53-00-01 FIG 101 AND 51-20-01 PG 7.
- [SDR DU4R2006497](https://openairdocs.org/sdr/DU4R2006497.md): Support Angle · corroded · Jun 8, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION ON CABIN L-4 DOOR SILL SUPPORT ANGLE BS 1681.8. REMOVED DOOR SILL SUPPORT ANGLE. FABRICATED AND INSTALLED ANGLE REPAIR 5 X 1 X 1 INCH FROM 7075-T6.063 IAW B757 SRM 51-10-03.
- [SDR DU4R2006495](https://openairdocs.org/sdr/DU4R2006495.md): Transition Panel · corroded · Jun 7, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT PIT LT TRANSITION PANEL BS 1200 TO 1310. REMOVED CORRODED TRANSITION. DRILLED FASTENER HOLES AND INSTALLED P/N 146N539U171 AND INSTALLED NUT PLATES IAW B757 SRM 51-10-01 AND 51-40-02.
- [SDR DU4R2006494](https://openairdocs.org/sdr/DU4R2006494.md): Shear Plate · corroded · Jun 7, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION AT CABIN SUB-FLOOR B/O 0 TO RBL 50 BS 1716 (MAIN DECK FLOOR) SHEAR DECK PLATE RBL 25 CORRODED. REMOVED CORROSION RBL 28 TO RBL 50 WITHIN LIMITS. FABRICATED AND INSTALLED EXTERNAL DOUBLER 9 X 5.5 INCHES FROM 2024-T3.063 IAW B757 SRM 53-60-51 FIG 20
- [SDR DU4R2006493](https://openairdocs.org/sdr/DU4R2006493.md): Skin · corroded · Jun 7, 2006 · N630DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > CORROSION FWD CARGO PIT IN BILGE AT BS 850 B/O 0 WL 148.5 ON UPPER SURFACE OF THE LOWER SKIN. FABRICATED AND INSTALLED EXTERNAL DOUBLER 10.5 X 8.5 INCHES FROM 2024-T3.125 IAW B757 SRM 53-30-01 FIG 201 AND 51-20-01.
- [SDR DU4R2006507](https://openairdocs.org/sdr/DU4R2006507.md): Crease Beam · corroded · Jun 6, 2006 · N630DL · Boeing 757232 · Fuselage Main, Structure
  > S/O 291018 NR 23878 CORROSION ON CABIN CREASE BEAM BS 660 TO 760 LT. REMOVED AND REPLACED L/H BS 660 - 760 CABIN CREASE BEAM P/N 143N8328U53 IAW B757 SRM 51-40-02.
- [SDR DU4R2006491](https://openairdocs.org/sdr/DU4R2006491.md): Transition Panel · corroded · Jun 4, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CORROSION FWD PIT RT TRANSITION PANEL BS 560 - 644. INSTALLED NEW TRANSITION PANEL P/N 143N366U126 IAW B757 SRM 53-30-53 FIG 1, 53-00-53 FIG 101, 51-40-05 FIG 2, 3, 4 AND 51-40-02 PG 2 & 3.
- [SDR DL757040316](https://openairdocs.org/sdr/DL757040316.md): Engine · failed · Apr 8, 2004 · N630DL · Boeing 757232 · Engine (Turbine/Turboprop)
  > ENGINE FAILURE ON LEFT ENGINE WITH T/O POWER SET, BOTH FIRE BOTTLES DISCHARGED INTO ENGINE MAX EGT 762 DEG FOR 3.06 MINUTES. REPLACED ENGINE.
- [SDR DL757040317](https://openairdocs.org/sdr/DL757040317.md): Skin · dented · Apr 5, 2004 · N630DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND DENTED BETWEEN STRINGERS 18L & 19L, JUST FWD OF THE FS 1618 SKIN BUTT SPLICE. THE DENTED AREA WAS REMOVED WITH A CUT OUT AND REPAIRED WITH TWO ALUMINUM REPAIR DOUBLERS. THE REPAIR WAS ACCOMPLISHED PER ER/A 089586-14, REV A.
- [SDR DL757021151](https://openairdocs.org/sdr/DL757021151.md): Coffeemaker · shorted · Sep 29, 2002 · N630DL · Boeing 757232 · Buffet/Galleys
  > A/C 630 ON FLT 1107 HAD ATB TO SAV DUE TO F/C GALLEY COFFEE MAKER HAD AN ELECTRICAL SHORT AND CAUSED HAZE/SMELL IN FWD GALLEY/CABIN AREAS. CREW REPORTED NO SMOKE IN COCKPIT. RETURNED TO SAV WITHOUT INCIDENT. FOUND FWD COFFEE MAKER BAD REPLACED COFFEE MAKER
- [SDR DL757020071](https://openairdocs.org/sdr/DL757020071.md): Wire · damaged · Jan 20, 2002 · N630DL · Boeing 757232 · Hydraulic Power System Wiring
  > LEFT ENGINE HYD MESSAGE AND OVERHEAD LIGHT CAME ON PRIOR TO T/O. REPAIRED SHIELDED WIRE 18 INCHES FROM CANNON PLUG IN LEFT ENGINE PYLON. INDICATION NOW NORMAL.
- [SDR DL757011928](https://openairdocs.org/sdr/DL757011928.md): Line · failed · Dec 11, 2001 · N630DL · Boeing 757232 · Hydraulic System, Main
  > CENTER HYDRAULIC SYST QUANTITY LOSS WITH 'C HYD QTY' EICAS MSG. REPLACED FLEX LINE AT CENTER HYD BAY. LEAK CHECKS GOODSERVICED SYSTEM TO FULL.
- [SDR DL757001102](https://openairdocs.org/sdr/DL757001102.md): Keelbeam · corroded · Jun 6, 2000 · N630DL · Boeing 757232 · Fuselage Main, Floor Beam
  > THE STRINGER 29R KEEL CHORD WAS FOUND BADLY CORRODED AT FS 1405. THE CHORD WAS CUT AT FS 1390 AND THE AFT SECTION OF CHORD REMOVED TO ELIMINATE THE CORROSION. A NEW SECTION OF CHORD WAS SPLICED IN AT FS 1390 WITH STEEL REPAIR CHANNELS INSTALLED PER ER/A 37
- [SDR DL757001100](https://openairdocs.org/sdr/DL757001100.md): Skin · lightning strike · Jun 6, 2000 · N630DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE CROWN SKIN BETWEEN FS 514 & 520 WAS DAMAGED IN TWO SPOTS BY LIGHTNING. THE DAMAGE WAS REMOVED WITH A 3.5 X 2.9 CUTOUT AND A 1.1 X 1.9 CUTOUT. BOTH CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 377377-14, REV
- [SDR DL757990055](https://openairdocs.org/sdr/DL757990055.md): Fire Light · contaminated · Jan 10, 1999 · N630DL · Boeing 757232 · Fire Detection
  > AT FLIGHT LEVEL 350 EXPERIENCED MODERATE UNEXPECTED TURBULANCE, BOTTLED WATER SPILLED ON CENTER CONSOLE. DURING DESCENT TO FL 260 AFT CARGO FIRE LIGHT ILLUMINATED. NO OTHER INDICATIONS. HOWEVER, IAW POM NR 1 BOTTLE WAS DISCHARGED AND PACK SHUT DOWN. LIGHT
- [SDR DL757961871](https://openairdocs.org/sdr/DL757961871.md): Battery Pack · discharged · Aug 11, 1996 · N630DL · Boeing 757232 · Emergency Lighting
  > ON L/O, FOUND 1ST CLASS EMERGENCY PATH LIGHTS INOP. REPLACED BATT PACK, CHECKS GOOD.
- [SDR DL757954061](https://openairdocs.org/sdr/DL757954061.md): Bulb · failed · Oct 19, 1995 · N630DL · Boeing 757232 · Emergency Lighting
  > R2 EMERGENCY ESCAPE LIGHT IS INOP. RELAMPED, OPS CKS GOOD.

## 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 = 'N630DL' AND deregistration_id = 'N630DL-2017-05-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N630DL-2017-05-16/reports

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