# Service difficulty reports: N603DL, cancelled Aug 21, 2018

A list on [N603DL, cancelled Aug 21, 2018](https://openairdocs.org/deregistered/N603DL-2018-08-21.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 · 56 reports

- [SDR DALA14025830603](https://openairdocs.org/sdr/DALA14025830603.md): Frame · corroded · Apr 24, 2014 · N603DL · Boeing 757232 · Fuselage Main, Frame
  > CORROSION ON TOP OF FUSELAGE FRAME BS 310.5 BETWEEN S23-24L. REPAIRED IAW ERA 514386, REV A.
- [SDR DALA14006890603](https://openairdocs.org/sdr/DALA14006890603.md): Line · ruptured · Feb 1, 2014 · N603DL · Boeing 757232 · Hydraulic System, Main
  > GEAR DISAGREE LIGHT CAME ON DURING GEAR EXTENTION. ACCOMPLISHED QRH 13.9. CREW NEVER HEARD NOSE GEAR DROP OR NOSE GEAR DOORS OPEN, ALTERNATE GEAR EXTENSION PERFORMED. FOUND AFT FLEX LINE FOR LT MLG RETRACT ACTUATOR RUPTURED. INSTALLED NEW LINE IAW AMM 20-1
- [SDR DALA13067300603](https://openairdocs.org/sdr/DALA13067300603.md): Skin · damaged · Dec 6, 2013 · N603DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > DURING INSPECTION, FOUND NUMEROUS BURN MARKS ON LT SKIN FROM RADOME TO NOSE GEAR AFT DOOR BELOW LAP JOINT. ALL BURNISHED MARKS WITHIN SERVICABLE LIMITS IAW SRM 53-00-00. FOUND 2 SOLID RIVETS BURNED BEYOND LIMITS, 3 INCHES ABOVE STRINGER 26L AT STATION 215.25
- [SDR DALA13062280603](https://openairdocs.org/sdr/DALA13062280603.md): Unknown · odor · Nov 16, 2013 · N603DL · Boeing 757232 · Air Distribution System
  > FLIGHT DIVERTED DUE TO A STRONG BURNING ELECTRICAL ODOR FROM THE MID GALLEY. NO VISIBLE SMOKE REPORTED. MAINTENANCE INSPECTED WIRING BEHIND COFFEEMAKERS, OVENS, POWER CONTROL PANELS, AND CEILING LIGHTS WITH NO TROUBLE FOUND. R & R BOTH MID GALLEY COFFEEMAKERS
- [SDR DALA13054260603](https://openairdocs.org/sdr/DALA13054260603.md): Wire Harness · damaged · Oct 20, 2013 · N603DL · Boeing 757232 · Light System Wiring
  > EMERGENCY LIGHT INOPERATIVE. REPLACED SEAT WIRE HARNESS. CHECKED NORMAL.
- [SDR DALA2013082310603](https://openairdocs.org/sdr/DALA2013082310603.md): Girt Bar · dirty · Aug 23, 2013 · N603DL · Boeing 757232 · Emergency Equipment
  > F/A REPORTS L4 DOOR SLIDE WILL NOT DISENGAGE COMPLETELY. CLEANED DEBRIS FROM GIRT BAR AND FLOOR MOUNTED HARDWARE. PERFORMED, AMM 25-66 INSP/CK OPS CHECKS NORMAL. OK FOR SERVICE.
- [SDR DALA1315280603](https://openairdocs.org/sdr/DALA1315280603.md): Snubber · damaged · Jun 11, 2013 · N603DL · Boeing 757232 · Passenger/Crew Doors
  > L4 DOOR VERY HARD TO OPEN. REPLACED ROTARY SNUBBER IAW MM 52-11. INSTALLED SNUBBER IAW MM.
- [SDR DALA1311500603](https://openairdocs.org/sdr/DALA1311500603.md): Frame · corroded · May 1, 2013 · N603DL · Boeing 757232 · Fuselage Main, Frame
  > STA 310.5, CORROSION STR 23 TO 24 LT FRAME TOP LEG. REMOVED DAMAGE 1" X 4.5" UPPER LEG. INSTALL DOUBLER REPAIR IAW ERA 514386-14, REV ORG (TO 514386-14).
- [SDR DALA1308970603](https://openairdocs.org/sdr/DALA1308970603.md): Structure · cracked · Apr 10, 2013 · N603DL · Boeing 757232 · Cargo/Baggage Doors
  > DAMAGE ON FWD CARGO DOOR LOWER AFT CORNER. REMOVED EDGE CRACK IAW SRM 52-30-01.
- [SDR DALA1256060603](https://openairdocs.org/sdr/DALA1256060603.md): Inlet · damaged · Dec 2, 2012 · N603DL · Boeing 757232 · Turbine Engine Air Inlet Section
  > NR 1 ENGINE INLET COWL RT SIDE 9 OCLOCK POSITION HAS A DENT. DENT OUT OF LIMITS IAW SRM 54-11-01. R & R NR 1 ENGINE INLET COWL IAW AMM 71-11-01.
- [SDR DALA1254480603](https://openairdocs.org/sdr/DALA1254480603.md): Bulb · inoperative · Nov 14, 2012 · N603DL · Boeing 757232 · Emergency Lighting
  > MX DISCOVERED THE L2 DOOR EXIT SIGN HAS MANY BULBS INOPERATIVE. R & R BULBS AT L2 DOOR EXIT SIGN IAW AMM 33-51.
- [SDR DALA1220170603](https://openairdocs.org/sdr/DALA1220170603.md): Charger · inoperative · Mar 29, 2012 · N603DL · Boeing 757232 · Emergency Lighting
  > LINE MAINTENANCE FOUND EMERGENCY PATH LIGHTS INOPERATIVE AT SEATS 1 THRU 6. REPLACED BATTERY CHARGER, OPERATION NORMAL.
- [SDR DALA1162200603](https://openairdocs.org/sdr/DALA1162200603.md): Light · inoperative · Nov 6, 2011 · N603DL · Boeing 757232 · Emergency Lighting
  > SEAT 2D EMERGENCY PROXIMITY LIGHT INOPERATIVE. REPLACED EMERGENCY PROXIMITY LIGHT ASSEMBLY AS PER B757 AMM 33-51. OPS CHECK GOOD.
- [SDR DALA1108190603](https://openairdocs.org/sdr/DALA1108190603.md): Light · inoperative · Feb 1, 2011 · N603DL · Boeing 757232 · Emergency Lighting
  > DURING A LAYOVER CHECK, MAINTENANCE FOUND THE DOOR L2 EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE FUSE AND LAMP. OPERATIONAL CHECK WAS GOOD. (2011-D0139)
- [SDR DALA1108180603](https://openairdocs.org/sdr/DALA1108180603.md): Light · inoperative · Feb 1, 2011 · N603DL · Boeing 757232 · Emergency Lighting
  > DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHTS AT 5D, 27D, AND 37D INOPERATIVE. MAINTENANCE RE-LAMPED ROW 5 AND 27. 37D HAD THE WIRING REPAIRED. OPERATIONAL CHECK WAS GOOD. (2011-D0137)
- [SDR DALA1020420603](https://openairdocs.org/sdr/DALA1020420603.md): Wire · disconnected · Aug 22, 2010 · N603DL · Boeing 757232 · Light System Wiring
  > WHITE EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. HARNESS IS PULLED OUT. SPLICED AND SECURED WIRES UNDER SEAT 25D. OPS CHECK OK.
- [SDR DALA1019850663](https://openairdocs.org/sdr/DALA1019850663.md): Unknown · odor · Aug 10, 2010 · N603DL · Boeing 757232 · Air Distribution System
  > DURING FLIGHT, F/A'S REPORTED A BURNING ODOR IN THE CABIN SO THE ACFT DIVERTED. MX CHECKED ACFT AND CABIN SYSTEMS WITH NO ODOR NOTED AND NO PROBLEMS FOUND. ACFT RETURNED TO SERVICE.
- [SDR DL757101231](https://openairdocs.org/sdr/DL757101231.md): Battery Pack · inoperative · May 12, 2010 · N603DL · Boeing 757232 · Emergency Lighting
  > DURING LAYOVER CHECK, MX FOUND EMERGENCY PATH LIGHTS VERY DIM AT ROWS 19-27. MX REPLACED THE BATTERY PACK. OPS CHECK WAS GOOD.
- [SDR DL757101010](https://openairdocs.org/sdr/DL757101010.md): Light · inoperative · Apr 22, 2010 · N603DL · Boeing 757232 · Emergency Lighting
  > DURING LAYOVER CHECK, MAINTENANCE FOUND EMERGENCY PATH LIGHT AT SEAT 5C INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD.
- [SDR DL757100526](https://openairdocs.org/sdr/DL757100526.md): Wire · damaged · Feb 24, 2010 · N603DL · Boeing 757232 · Light System Wiring
  > ON A CHECK FOUND EMERGENCY PATH SEAT LIGHTS INOP AT ROWS 25, 26, 27, 30, 31, 39, 43-45. REPAIRED WIRING AT AFFECTED SEATS OPS CK OK.
- [SDR DL757100505](https://openairdocs.org/sdr/DL757100505.md): Wire · damaged · Feb 24, 2010 · N603DL · Boeing 757232 · Light System Wiring
  > DURING SERVICE CHECK AD 2 FOUND EMERGENCY PATH SEAT LIGHTS INOP AT ROWS 25, 26, 27, 30, 31, 39, 43-45. REPAIR WIRING AT AFFECTED SEATS, OPS CK OK.
- [SDR DL757091606](https://openairdocs.org/sdr/DL757091606.md): Spar · corroded · Oct 9, 2009 · N603DL · Boeing 757232 · Horizontal Stabilizer, Spar/Rib
  > DURING PSV CHECK, MAINTENANCE FOUND THE RT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD CORRODED WHERE THE UPPER T/E PANEL ATTACHES. THE CHORD WAS REPAIRED PER ERA 476883-14.
- [SDR DL757091605](https://openairdocs.org/sdr/DL757091605.md): Rib · corroded · Oct 9, 2009 · N603DL · Boeing 757232 · Horizontal Stabilizer, Spar/Rib
  > DURING PSV MAINTENANCE FOUND CORROSION ON THE RT HORIZONTAL STABILIZER RIB 11 UPPER SURFACE. CORROSION EXCEEDED SRM LIMITS. ACCOMPLISHED REPAIR PER ERA 477049-14.
- [SDR DL757091585](https://openairdocs.org/sdr/DL757091585.md): Butt Joint · corroded · Aug 31, 2009 · N603DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > DURING PSV 23 THE RT FUSELAGE SPLICE PLATE AT STATION 900 WAS FOUND TO HAVE CORROSION. THE BAC P/N IS A 144N3310-8402. CORROSION WAS VISIBLE AT THE STATION 900 SKIN BUTT SPLICE AT STRINGER 13R TO 15R. THE SPLICE PLATE WAS REPLACED AND AIRCRAFT RETURNED TO S
- [SDR DL757090175](https://openairdocs.org/sdr/DL757090175.md): Actuator · worn · Feb 6, 2009 · N603DL · Boeing 757232 · Engine Thrust Reverser
  > RIGHT THROTTLE THRUST LEVER STOPPED HARD AND WOULD NOT GET TO TAKEOFF POWER. FOUND RIGHT THROTTLE PHYSICALLY STUCK AS IF HITTING A STOP INSP THROTTLE QUADRANT AREA ABOVE AND BELOW THROTTLES NO BINDING AREAS NOTED FREED THROTTLE WITH LIGHT FORCE PERFORMED MCDP
- [SDR DL757080291](https://openairdocs.org/sdr/DL757080291.md): Skin · misrepaired · Feb 26, 2008 · N603DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > DURING HMV AT SAA, THE FUSELAGE SKIN AT STA 628 AND S-25L WAS FOUND WITH AN EXISTING REPAIR THAT DID NOT MEET SRM REQUIREMENTS. THE REPAIR DOUBLER WAS REMOVED AND A BOEING DESIGNED REPAIR WAS INSTALLED.
- [SDR DL757080287](https://openairdocs.org/sdr/DL757080287.md): Skin · damaged · Feb 24, 2008 · N603DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > TOOLING MARKS WERE FOUND AT THE AIRPHONE ANTENNA SKIN AT FS 1515 BETWEEN S-28R AND S-29R. THE ANTENNA IS NO LONGER IN USE. BECAUSE THE ANTENNA HAD BEEN SUBJECT TO AN STC, THE ANTENNA WAS REMOVED, AND THE FASTENER PATTERN CUTOUT. AN EXTERNAL REPAIR DOUBLER
- [SDR DL757080258](https://openairdocs.org/sdr/DL757080258.md): Skin · damaged · Feb 21, 2008 · N603DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > DURING HMV AT SAA, A CREASE WAS FOUND IN THE FUSELAGE SKIN AT STA 1420, S-28R. THE CREASE EXCEEDED THE ALLOWABLE SRM LIMIT. A REPAIR WAS ACCOMPLISHED PER BOEING INSTRUCTIONS. STARTING AT 12,000 CYCLES AFTER REPAIR INSTALLATION AND EVERY 12,000 CYCLES THEREA
- [SDR DL757071620](https://openairdocs.org/sdr/DL757071620.md): Skin · corroded · Dec 14, 2007 · N603DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FUSELAGE/SKIN/FS 880/STRG 28L-28R:CORROSION REPAIR. THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION AT FS 880 BETWEEN STRINGERS 28L AND 28R. THE CORROSION WAS ADJACENT TO AN AIR CONDITIONING DUCT CUTOUT. THE DAMAGE WAS REMOVED WITH A CUTOUT TO THE SK
- [SDR DL757070560](https://openairdocs.org/sdr/DL757070560.md): Bulkhead · gouged · Feb 26, 2007 · N603DL · Boeing 757232 · Fuselage Main, Bulkhead
  > THE AFT FUSELAGE PRESSURE BULKHEAD WAS DAMAGED DURING A TAIL STRIKE. THE BULKHEAD CHORDS WERE CUT OUT AND A NEW SECTION WAS FABRICATED AND SPLICED IN. REF ER/A'S 460538-14 AND 460643-14 FOR SAME DAMAGE.
- [SDR DL757060676](https://openairdocs.org/sdr/DL757060676.md): Amplifier · malfunctioned · Aug 23, 2006 · N603DL · Boeing 757232 · Entertainment System
  > P/A MAKING BUZZING SOUND WITH POSSIBLE ELECTRICAL SMELL NEAR MID LAVS. REPLACED P/A AMP AND IFE CONTROLLER CHECKS OK.
- [SDR DL757060200](https://openairdocs.org/sdr/DL757060200.md): Linkage · lack of lube · Mar 17, 2006 · N603DL · Boeing 757232 · Landing Gear Door Retract Section
  > ON TAKEOFF GEAR DOOR LIGHT ILLUMINATED. AIRCRAFT PERFORMED AIR RETURN. FOUND FOLLOW UP LINKAGE FOR MANUAL RELEASE OF NOSE GEAR DOORS STICKING. CLEANED AND LUBED SAME. CYCLED DOORS MANUALLY SEVERAL TIMES. JACKED NOSE GEAR AND PERFORMED NOSE GEAR EXTENTION/
- [SDR DL757060138](https://openairdocs.org/sdr/DL757060138.md): Slide · out of position · Feb 18, 2006 · N603DL · Boeing 757232 · Escape Slide
  > L1 ESCAPE SLIDE FELL OUT WHEN DOOR WAS OPENED. REPLACED L1 DOOR SLIDE PER M/M. SAFETY PIN REMOVED AND STOWED.
- [SDR DL757040468](https://openairdocs.org/sdr/DL757040468.md): Skin · cracked · May 24, 2004 · N603DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN ASSY L1 DOOR CUTOUT UPPER FWD CORNER: CRACK REPAIR, INSPECTION OF THE FUSELAGE SKIN AT THE UPPER FWD CORNER OF THE L1 DOOR CUTOUT REVEALED A CRACK. THE CRACK IS TYPICAL OF AD 2004-09-32. THE CRACK WAS CUTOUT OF THE SKIN AND UNDERLYING BEARS
- [SDR DL757031063](https://openairdocs.org/sdr/DL757031063.md): Switch · faulty · Nov 29, 2003 · N603DL · Boeing 757232 · Fixed Inner Doors
  > CENTER LAV DOOR LATCH HOT AND EMITTING SMOKEY O-ZONE SMELL. REPLACED DOOR LATCH SWITCH.
- [SDR DL757020105](https://openairdocs.org/sdr/DL757020105.md): Skin · dented · Jan 25, 2002 · N603DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / FS 1630 / STRG. 24R-26R: GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS DENTED AND GOUGED AT FS 1630 BETWEEN STRINGERS 24R & 26R. THE DAMGE WAS REMOVED WITH A 7" X 2" CUTOUT AND A 5" X 2"
- [SDR DL757020104](https://openairdocs.org/sdr/DL757020104.md): Skin · cracked · Jan 25, 2002 · N603DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / FS 1701 / STRG. 29L: CRACKED HOLE REPAIR A SMALL CRACK WAS FOUND AT FASTENER HOLE DUE TO IMPROPER FASTENER INSTALLATION AT FS 1701 AND STRINGER 29L. THE CRACK WAS REMOVED WI
- [SDR DL757020088](https://openairdocs.org/sdr/DL757020088.md): Door Frame · corroded · Jan 23, 2002 · N603DL · Boeing 757232 · Fuselage Main, Structure
  > OUTER CHORD AND WEB SPLICE; LOWER SILL CHORD SUBSTITUTION THE LOWER SILL OF THE C2 DOOR OPENING WAS FOUND WITH SEVERAL AREAS OF CORROSION. THE OUTER CHORD AND WEB OF THE FS 1440 OPENING FRAME WERE CUT AND THE LOWER SECTION REMOVED TO ALLOW REPLACEMENT OF THE
- [SDR DL757020086](https://openairdocs.org/sdr/DL757020086.md): Skin · gouged · Jan 23, 2002 · N603DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / FS 1701 / STRG. 20L / SKIN LAP JOINT: GOUGE CUTOUT REPAIR THE LOWER SKIN OF THE STRINGER 20L SKIN LAP JOINT WAS GOUGED BY TOOLING AT FS 1701. THE DAMAGED AREA OF SKIN WAS TRIMMED OUT. TH
- [SDR DL757020079](https://openairdocs.org/sdr/DL757020079.md): Trunnion · corroded · Jan 22, 2002 · N603DL · Boeing 757232 · Main Landing Gear Attach Section
  > INSPECTION OF THE MLG FUSE PINS AND ADJACENT LUG BORES PER AD 2000-07-13, REVEALED CORROSION IN THE FUSE PIN LUG BORES OF THE LT MLG FWD TRUNNION BEARING SUPPORT FITTING ASSEMBLY. CLEANUP OF THE CORROSION RENDERED THE FITTING UNACCEPTABLE FOR FURTHER SERVICE.
- [SDR DL757020037](https://openairdocs.org/sdr/DL757020037.md): Skin · dented · Jan 11, 2002 · N603DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / FS 1620-1720 / STRG. 14A-20L: SKIN REPLACEMENT THE FUSELAGE SKIN WAS FOUND WITH NUMEROUS DENTS AND GOUGES NEAR THE L4 DOOR OPENING. THE SKIN PANEL WAS REMOVED TO ELIMINATE ALL OF THE
- [SDR DL757020028](https://openairdocs.org/sdr/DL757020028.md): Skin · gouged · Jan 9, 2002 · N603DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / FS 1610 / STRG. 26L: DENT & GOUGE REPAIR THE FUSELAGE SKIN WAS DENTED AND GOUGED BY TOOLING AT FS 1610 JUST ABOVE THE STRINGER 26L SKIN LAP JOINT. THE DAMAGE WAS REMOVED W
- [SDR DL757020027](https://openairdocs.org/sdr/DL757020027.md): Floorbeam · corroded · Jan 9, 2002 · N603DL · Boeing 757232 · Fuselage Main, Floor Beam
  > THE UPPER CAP OF THE FS 1681 PASSENGER FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION. TO REMOVE THE DAMAGE, THE ENTIRE UPPER CAP WAS TRIMMED OFF. A NEW CAP WAS FABRICATED FROM ALUMINUM EXTRUSION AND INSTALLED PER ER/A 382227-14, REV A.
- [SDR DL757011466](https://openairdocs.org/sdr/DL757011466.md): Brake · damaged · Sep 2, 2001 · N603DL · Boeing 757232 · Brake
  > NR FIVE BRAKE TWISTED AND PADS COMING APART, REPLACED BRAKE.
- [SDR DL757010545](https://openairdocs.org/sdr/DL757010545.md): Battery Pack · inoperative · Apr 1, 2001 · N603DL · Boeing 757232 · Emergency Lighting
  > FOUND ON LO FC EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK OPS NORMAL
- [SDR DL757010199](https://openairdocs.org/sdr/DL757010199.md): Acm · worn · Feb 4, 2001 · N603DL · Boeing 757232 · Cabin Pressure Control System
  > A/C WILL NOT MAINTAIN HIGHER THAN 7.2 PSID UNTIL RT RECIRC FAN TURNED OFF. WITH RT RECIRC FAN OFF PRESSURIZATION AND TEMP CONTROL WERE NORMAL. AT FL 390 RT PACK OFF LIGHT CAME ON, LATER RT ENG BLEED OFF LIGHT ON. COULD NOT RECOVER RT PK UNTIL ON GROUND AT L
- [SDR DL757002188](https://openairdocs.org/sdr/DL757002188.md): Torque Tube · failed · Nov 7, 2000 · N603DL · Boeing 757232 · Trailing Edge Flap Control System
  > DURING LANDING WHEN FLAP LEVER MOVED FROM 15 TO 20 EICAS MSG FLAP ASYM AND TRAILING EDGE LIGHT ILLUM THE LEFT FLAP REMAINED AT 15 RIGHT FLAP STOPPED. LEFT INBOARD OUTBOARD TORQUE TUBE REMOVED AND REPLACED.
- [SDR DL757982187](https://openairdocs.org/sdr/DL757982187.md): Transmitter · failed · Oct 22, 1998 · N603DL · Boeing 757232 · Trailing Flap Position Indicating System
  > T/E FLAP ASSY LIGHT CAME ON AFTER T/O WHEN RAISING FLAPS FROM 10-15 DEG. FLAP NEEDLES SPLIT AND STOPPED. REPLACED T/E FLAP TRANSMITTER.
- [SDR DL757980448](https://openairdocs.org/sdr/DL757980448.md): Skin · dented · Feb 20, 1998 · N603DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN BETWEEN FS 1627 AND 1639 AND BETWEEN STR 28L AND 29L WAS DENTED AND GOUGED DUE TO GROUND DAMAGE. THE DAMAGED AREA WAS CUT OUT AND A SKIN DOUBLER WAS INSTALLED PERER/A 364038-14, REV B.
- [SDR DL757980447](https://openairdocs.org/sdr/DL757980447.md): Skin · dented · Feb 20, 1998 · N603DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN HAD NUMEROUS GOUGES, DENTS AND SCRATCHED BETWEEN FS 1550 AND 1621 AND BETWEEN STRINGERS 26L AND 26R. THE DAMAGED SECTION OF SKIN WAS REMOVED AND A NEW SECTION WAS SPLICED IN PER ER/A 364044-14, REV B.

Next page: https://openairdocs.org/deregistered/N603DL-2018-08-21/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 = 'N603DL' AND deregistration_id = 'N603DL-2018-08-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N603DL-2018-08-21/reports

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