# Service difficulty reports: N602DL, cancelled May 16, 2017

A list on [N602DL, cancelled May 16, 2017](https://openairdocs.org/deregistered/N602DL-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.

Page 1 of 2 · 56 reports

- [SDR DALA1308500602](https://openairdocs.org/sdr/DALA1308500602.md): Skin · nicked · Apr 5, 2013 · N602DL · Boeing 757232 · Horizontal Stabilizer, Plate/Skin
  > TWO SMALL NICKS RT LOWER L/E HORIZONTAL STABILIZER. CLEANED & FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 55-10-1 TABLE H.
- [SDR DALA1256520602](https://openairdocs.org/sdr/DALA1256520602.md): Skin · damaged · Dec 6, 2012 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE AT APPROXIMATELY BS 408 S3R ON RIVET HEAD IAW SRM 53-00, REPAIR INSTALLATION OK.
- [SDR DALA1256500602](https://openairdocs.org/sdr/DALA1256500602.md): Skin · damaged · Dec 6, 2012 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE AT APPROX LOCATIONS BS 480, 3 INCHES ABOVE STR 4R ON RIVET HEAD. COMPLIED WITH PRI 509608-14, REV 0, STEPS 1-59917734 INSPECTED SAME. ACCOMPLISHED HFEC INSPECTION OF CUTOUT AND BHEC OF EXISTING FASTENER HOLES PRI 509608-14, REV.1 09 DEC 12
- [SDR DALA1256490602](https://openairdocs.org/sdr/DALA1256490602.md): Skin · damaged · Dec 6, 2012 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > HAD LIGHTNING STRIKE AT APPROX LOCATION BS 435, STR 4R ON RIVET HEAD JUST FWD OF SKIN SPLICE. REMOVED FASTENER STEPPED UP HOLE TO REMOVE DAMAGE. COMPLIED WITH HFEC INSPECTION AROUND REMOVED FASTENER AT BS 435 STR 4R. NO DISCREPANCIES NOTED. REPLACED FASTENER
- [SDR DALA1256480602](https://openairdocs.org/sdr/DALA1256480602.md): Skin · damaged · Dec 6, 2012 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > HAD LIGHTNING STRIKE AT APPROX LOCATION BS 408 S3R ON RIVET HEAD. REMOVED FASTENER. REMOVED DAMAGE, COMPLIED WITH HFEC INSPECTION ON FUSELAGE SKIN AROUND CUT OUT AREA AT BS 408 S3R. COMPLIED WITH BHEC INSPECTION ON EXISTING FASTENER HOLES IN S3R. THREE FAST
- [SDR DALA1256470602](https://openairdocs.org/sdr/DALA1256470602.md): Skin · damaged · Dec 6, 2012 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKES ON RIVET HEADS LOCATED AT S4R APPROX BS 356 AND S4R BS 540. REMOVED FASTENERS BS 356. REMOVED FASTENER AT BS 540. COMPLIED WITH HGEC INSPECTION ON FUSELAGE SKIN AROUND REMOVED FASTENERS AT BS 356 S4R AND BS 540 S4R. NO DISCREPANCIES NOTED.
- [SDR DALA1256460602](https://openairdocs.org/sdr/DALA1256460602.md): Skin · damaged · Dec 6, 2012 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > MULTIPLE LIGHTNING STRIKES AT LAP SPLICE AT S4R. LOCATIONS APPROX STA 512, 459 AND 378. CLEANED UP AREA AT BS 378 IAW SRM 53-00-01, FIG 101.849644. CLEANED AREAS AT BS 512-459-449 IAW SRM 53-00. TREATED AND PAINTED IAW PS 900-3-6 NR 3.
- [SDR DALA1256360602](https://openairdocs.org/sdr/DALA1256360602.md): Skin · damaged · Dec 6, 2012 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FOUND LIGHTNING STRIKE DAMAGE AT FS 408 S3R. INSTALLED REPAIR DOUBLER IAW SRM 53-00-01, REPAIR 2.
- [SDR DALA1209250602](https://openairdocs.org/sdr/DALA1209250602.md): Skin · punctured · Feb 17, 2012 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN PUNCTURED BS 480. REPAIRED PER ERA 500459-14.
- [SDR DALA1202340602](https://openairdocs.org/sdr/DALA1202340602.md): Connector · defective · Jan 15, 2012 · N602DL · Boeing 757232 · Light System Wiring
  > LINE MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT ROW 32 RIGHT. UNDER-SEAT CONNECTOR WAS RE-PINNED, LIGHT OPERATION NORMAL.
- [SDR DALA1164680602](https://openairdocs.org/sdr/DALA1164680602.md): Light · disconnected · Nov 23, 2011 · N602DL · Boeing 757232 · Emergency Lighting
  > DURING LINE CHECK MAINTENANCE EMERGENCY LIGHTS AT STA 670 AND EXIT SIGN DISCONNECTED. MAINTENANCE CONNECTED EMERGENCY LIGHT AND EXIT SIGN. OPERATION OF LIGHTS NOW CHECK OK.
- [SDR DALA1163730602](https://openairdocs.org/sdr/DALA1163730602.md): Door Frame · damaged · Nov 12, 2011 · N602DL · Boeing 757232 · Fuselage Main, Structure
  > ER/A 386365-14AD SECTION II PERMANENT REPAIR OF C1 DOOR STRUCTURE FS 620 AFT EDGE FRAME S-25R. C/W ER/A 386365-14AD REV ORIG ON N/R CARD 005. INSTALLATION OF REPAIR OK.
- [SDR DALA1163830602](https://openairdocs.org/sdr/DALA1163830602.md): Door Frame · damaged · Nov 1, 2011 · N602DL · Boeing 757232 · Cargo/Baggage Doors
  > DURING OPN 5032AD INSPECTION CARGO DOOR FRAMES FOUND SEVERAL OVERSIZED HOLES AND INCORRECT FASTENERS INSTALLED AT C2 CARGO DOOR. REMOVED FASTENERS, PREPARED AREA FOR INSPECTION AS PER ER/A 497284-14AD, AND INSTALLED FASTENERS IN C2 DOOR FRAME.
- [SDR DALA1158850602](https://openairdocs.org/sdr/DALA1158850602.md): Wire · broken · Oct 17, 2011 · N602DL · Boeing 757232 · Light System Wiring
  > DURING A ROUTINE MAINTENANCE VISIT, THE EMERGENCY LIGHT AT SEAT ROW 19 WAS FOUND TO BE INOPERATIVE. FURTHER INSPECTION FOUND WIRE ON SEAT HARNESS BROKEN. WIRE WAS SPLICED PER B757 AMM CHAPTER 20. OPERATION CHECKS GOOD AFTER REPAIR.
- [SDR DALA1154510602](https://openairdocs.org/sdr/DALA1154510602.md): Wire · damaged · Sep 18, 2011 · N602DL · Boeing 757232 · Light System Wiring
  > DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHTS AT SEATS 31D AND 34D INOPERATIVE. MAINTENANCE REPAIRED THE WIRING AT EACH LOCATION. OPERATIONAL CHECK WAS GOOD.
- [SDR DALA1138860602](https://openairdocs.org/sdr/DALA1138860602.md): Unknown · fumes · Jun 8, 2011 · N602DL · Boeing 757232 · Air Distribution System
  > ON DESCENT, FLIGHT ATTENDANTS REPORTED FUMES IN THE AFT GALLEY. THE QRH WAS ACCOMPLISHED. SMELL DISSIPATED. MAINTENANCE CHECKED THE LAVATORIES, GALLEYS, CABIN LIGHTS, AND RECIRCULATION FANS. NO FINDINGS. AIRCRAFT WAS APPROVED FOR SERVICE.
- [SDR DALA1014340602](https://openairdocs.org/sdr/DALA1014340602.md): Skin · bulged · Jun 15, 2010 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > SKIN BULGING FS 1720 S29R. REPAIRED AREA IAW ERA 483346-14 REV A.
- [SDR DL757080001](https://openairdocs.org/sdr/DL757080001.md): Nut · worn · Jan 1, 2008 · N602DL · Boeing 757232 · Trailing Edge Flap Control System
  > AT LANDING WHEN FLAPS LEVER PLACED TO 5, GOT TE FLAP DISAGREE CAUTION AND FLAPS LOCKED AT 1. FOUND RT INBD FLAP OUTBD JACKSCREW DISCONNECTED FROM TRANSMISSION AT U JOINT. U JOINT PARTS FOUND IN FAIRING. REPLACED TRANSMISSION, U JOINT PARTS, AND DAMAGED FAIR
- [SDR DU4R2007128](https://openairdocs.org/sdr/DU4R2007128.md): Frame · dented · May 31, 2007 · N602DL · Boeing 757232 · Fuselage Main, Frame
  > FOUND DENT IN UPPER CAP OF AFT PIT MAIN FRAME BS 1400 BETWEEN S-27 AND S-26 LT. REPAIRED BY FABRICATING AND INSTALLING FRAME REPAIR 9 BY 14 FROM 7075-T6.071 IAW DELTA ERA 380490-14MA REV ORIG, DELTA PROCESS STANDARD 900-5-1 NR 4, B757 SRM 51-40-02, PG 2, 7,
- [SDR DU4R2007129](https://openairdocs.org/sdr/DU4R2007129.md): Stringer · corroded · May 29, 2007 · N602DL · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > FOUND S-29L CORRODED IN AFT PIT AT BS 1480. REPAIRED CORRODED STRINGER BY REMOVING AND INSTALLING STRINGER P/N 146N3110-8201 AND SPLICE IAW B757 SRM 53-00-03.
- [SDR DU4R20070123](https://openairdocs.org/sdr/DU4R20070123.md): Skin · damaged · May 29, 2007 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FOUND LIGHTNING STRIKE BS 310 BETWEEN S-8L AND S-9L. REPAIRED BY REMOVING SHEAR TIE, CUT OUT STRIKE AREA, HFEC CUT OUT IAW B757 NTM PT6 51-00-01, 51-00-19 NO RELEVANT INDICATIONS NOTED. TRIMMED OUT AN EXTRA.040” MATERIAL. FABRICATED AND INSTALLED SHEAR TIE
- [SDR DL757070570](https://openairdocs.org/sdr/DL757070570.md): Skin · damaged · May 18, 2007 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > DURING CURRENT HMV, A DENT WAS FOUND ON THE EXTERIOR SKIN PANEL P/N 143N3320-3 JUST ABOVE S-17L AT FS 443. THE SUBJECT DAMAGE WAS OUTSIDE OF THE ALLOWABLE DAMAGE LIMITS OF THE SRM. THE DAMAGE WAS TRIMMED OUT AND AN EXTERNAL REPAIR DOUBLER INSTALLED PER ER/A
- [SDR DU4R2007121](https://openairdocs.org/sdr/DU4R2007121.md): Stringer · corroded · May 17, 2007 · N602DL · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STRINGER AND SKIN AT BS 750 S-23R. REPAIRED BY CUTTING OUT SECTION OF STRINGER. FABRICATED AND INSTALLED STRINGER REPAIR 14 BY 3.5 FROM BAC1498-204 IAW B757 SRM 51-20-01 AND 53-00-03 FIG 201.
- [SDR DU4R2007130](https://openairdocs.org/sdr/DU4R2007130.md): Attach Angle · corroded · May 14, 2007 · N602DL · Boeing 757232 · Fuselage Main, Attach Fittings
  > FOUND CORROSION AFT PIT MAIN FRAME FWD ATTACH ANGLE BS 1680 BETWEEN S-28 - S-29R. REPAIRED CORROSION ON FRAME ATTACH ANGLE BY FABRICATING AND INSTALLING NEW FRAME ATTACH ANGLE FROM 7075-T6.071" CLAD IAW B757 SRM 51-40-02, 51-70-11 AND 51-20-01.
- [SDR DU4R2007124](https://openairdocs.org/sdr/DU4R2007124.md): Stringer · corroded · May 14, 2007 · N602DL · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 29R AT BS 1681 CORRODED. REPAIRED CORROSION ON STRINGER S-29R AT BS 1681 BY CUTTING OUT AND REMOVING CORRODED SECTION OF STRINGER BS 1670 TO BS 1720 IAW B757 SRM 53-00-53 AND 51-40-02. FABRICATED AND INSTALLED STRINGER SECTION 50 BY 3 REPAIR F
- [SDR DU4R2007122](https://openairdocs.org/sdr/DU4R2007122.md): Skin · dented · May 8, 2007 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FOUND DENT BELOW STR 17L, BS 440. REPAIRED BY CUTTING OUT DENTED SECTION OF SKIN, HFEC CUT OUT IAW B757 NTM PT6, 51-00-01, NO RELEVANT INDICATIONS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER 15-1/4 BY 13-1/2 FROM 2024-T3.063 IAW B757 SRM 53-00-01 FIG 201
- [SDR DL757070059](https://openairdocs.org/sdr/DL757070059.md): Light · broken · Jan 26, 2007 · N602DL · Boeing 757232 · Exterior Lighting
  > ON ARRIVAL TO GATE, FOUND LOWER ANTI COLLISION BEACON LIGHT LENS BROKEN. REPLACED LIGHT ASSY.
- [SDR DL757040801](https://openairdocs.org/sdr/DL757040801.md): Wire · damaged · Aug 23, 2004 · N602DL · Boeing 757232 · Electrical Power System Wiring
  > CIRCUIT BREAKER C-23 ON P-64 PANEL POPPED IN FLIGHT. BREAKER IS FOR TRANSFORMER RECTIFIER UNIT. REPAIRED DAMAGED WIRING OVER DRIP PAN IN E/E.
- [SDR DL757040230](https://openairdocs.org/sdr/DL757040230.md): Skin · cracked · Mar 10, 2004 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > THE UPPER FWD CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A 2 INCH CRACK IN THE SKIN AND UNDERLYING BEARSTRAP. THE CRACK WAS REMOVED WITH A CUTOUT THROUGH ALL LAYERS OF THE SKIN ASSEMBLY. THE AREA WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/
- [SDR DL757040120](https://openairdocs.org/sdr/DL757040120.md): Power Supply · inoperative · Jan 31, 2004 · N602DL · Boeing 757232 · Emergency Lighting
  > F/C SEATS EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY.
- [SDR DL757031000](https://openairdocs.org/sdr/DL757031000.md): Line · damaged · Nov 11, 2003 · N602DL · Boeing 757232 · Hydraulic System, Main
  > RIGHT HYD QTY LOSS. FOUND PRESSURE LINE IN RT PYLON DAMAGED. REPLACED SAME.
- [SDR DL757030410](https://openairdocs.org/sdr/DL757030410.md): Clamp · loose · May 2, 2003 · N602DL · Boeing 757232 · Cabin Cooling System
  > LT DUCT LEAK. EICAS MSG. WITH CORRESPONDING DUCT LEAK LT ON AIR CONDITIONING PANEL. FOUND PNEUMATIC DUCT LT WING LEAKING. RESECURED. NO FURTHER LEAKS NOTED
- [SDR DL757020005](https://openairdocs.org/sdr/DL757020005.md): Skin · punctured · Dec 31, 2001 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / FS 590-620 / STRG. 15L-18L: PUNCTURE REPAIR THE FUSELAGE SKIN WAS PUNCTURED BY GROUND EQUIPMENT AT FS 610 AND STRINGER 16L. THE DAMAGE WAS ADJACENT TO 2 EXISTING SKIN REPAIR
- [SDR DL757011766](https://openairdocs.org/sdr/DL757011766.md): Spar · damaged · Nov 5, 2001 · N602DL · Boeing 757232 · Leading Edge Devices
  > NR 9 SLAT NOSE BEAM SPAR WAS FOUND WITH SEVERAL DAMAGED FASTENER HOLES. REPAIR PER ER/A 410486-14.
- [SDR DL757010907](https://openairdocs.org/sdr/DL757010907.md): Door Frame · corroded · Jun 1, 2001 · N602DL · Boeing 757232 · Fuselage Main, Structure
  > THE LOWER DOOR SILL CHORD OF THE C2 DOOR CUTOUT WAS CORRODED AND REQUIRED REPLACEMENT. TO ALLOW REMOVAL AND INSTALLATION OF A NEW CHORD, THE OUTER CHORD OF THE FS 1440 DOOR OPENING FRAME WAS CUT NEAR STRINGER 27R AND THE LOWER SECTION REMOVED. A NEW SECTION
- [SDR DL757010906](https://openairdocs.org/sdr/DL757010906.md): Skin · damaged · Jun 1, 2001 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND CREASED JUST FWD OF THE E&E COMPARTMENT DOOR CUTOUT AT RBL 2.3 BETWEEN FS 223 & 239. THE DAMAGE WAS CUTOUT OF THE SKIN AND REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 380763-14, REV A.
- [SDR DL757010774](https://openairdocs.org/sdr/DL757010774.md): Floorbeam · corroded · May 14, 2001 · N602DL · Boeing 757232 · Fuselage Main, Floor Beam
  > THE UPPER CAP OF THE FS 1681 PASSENGER FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION ALONG ITS LENGTH. THE UPPER CAP WAS TRIMMED OFF ALONG THE ENTIRE BEAM LENGTH TO REMOVE ALL CORROSION. A NEW UPPER CAP WAS FABRICATED FROM AN ALUMINUM EXTRUSION AND INST
- [SDR DL757010773](https://openairdocs.org/sdr/DL757010773.md): Skin · gouged · May 14, 2001 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN BETWEEN FS 590-660 AND BETWEEN STRINGES 16L & 18L WAS FOUND WITH SEVERAL DENTS AND GOUGES. THE DAMAGES WERE REMOVED WITH THREE SEPARATE CUTOUTS. EACH CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER E
- [SDR DL757010766](https://openairdocs.org/sdr/DL757010766.md): Skin · cracked · May 11, 2001 · N602DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING A SKIN REINFORCEMENT MODIFICATION TO THE LOWER AFT VHF ANTENNA CUTOUT, AN EXISTING REPAIR DOUBLER WAS FOUND. THE EXISTING REPAIR WAS REMOVED AND THE CUTOUT AREA INCREASED TO 18 X 5.25 INCHES. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMI
- [SDR DL757010765](https://openairdocs.org/sdr/DL757010765.md): Door Frame · corroded · May 11, 2001 · N602DL · Boeing 757232 · Fuselage Main, Structure
  > THE C1 DOOR OPENING LOWER SILL WAS FOUND BADLY CORRODED AND REQUIRES REPLACEMENT BETWEEN STRINGERS 25R & 26R. THE LOWER SECTIONS WERE TEMPORARILY REMOVED TO ALLOW INSTALLATION OF A NEW SILL CHORD. THE CHORD WAS SPLICED BACK WITH TWO ALUMINUM ANGLES AND
- [SDR DL757010236](https://openairdocs.org/sdr/DL757010236.md): Engine · malfunctioned · Feb 9, 2001 · N602DL · Boeing 757232 · Engine (Turbine/Turboprop)
  > AT 41000 FT LEFT OIL QTY DROPPED TO 0 WITH INCREASING OIL TEMP. OIL TEMP REACH YELLOW BAND, MAX TEMP 171.ENG WAS OPERATED AT IDLE AND DESCENDED TO 29000. OIL QTY AND TEMP RETURNED TO NORMAL AT 41000 FT. SCAVANGE PUMP PRES WAS 2 PSI. REPLACED GEARBOX SCAVAN
- [SDR DL757000206](https://openairdocs.org/sdr/DL757000206.md): Actuator · malfunctioned · Jan 27, 2000 · N602DL · Boeing 757232 · Leading Edge Slat Actuator
  > L/E SLAT DISAGREE LIGHT ILLUMINATED ON TAKEOFF. PERFORMED PROC PER POM. LIGHT REMAINED ILLUMINATED. FLAPS INDICATED A LITTLE LESS THAN 1 DEG. REPLACED NR 6 I/B AND O/B SLAT ACTUATORS.
- [SDR DL757992144](https://openairdocs.org/sdr/DL757992144.md): Retract Mech · malfunctioned · Sep 25, 1999 · N602DL · Boeing 757232 · Landing Gear Door Retract Section
  > ON GEAR RETRACTION HAD DOOR DISAGREE AND DOOR LIGHT REMAINED ON ACCOMPANIED BY WIND NOISE. ALSO HAD EICAS MESSAGE.
- [SDR DL757991652](https://openairdocs.org/sdr/DL757991652.md): Contl Module · failed · Jul 23, 1999 · N602DL · Boeing 757232 · Landing Gear Retraction/Extension System
  > GEAR FAILED TO RETRACT, GEAR HANDLE RAISED TO OFF POSITION AND WOULD NOT MOVE FURTHER. GEAR LIGHT AND GEAR DISAGREE MSG ILLUMINATED. FOLLWED POM PROCEDURE. RETURNED TO JFK. ON LANDING AIRCRAFT PULLED TO RIGHT. FOUND NR 3 BRAKE DRAGING REPLACED SAME. HAD
- [SDR DL757991403](https://openairdocs.org/sdr/DL757991403.md): Eec · failed · Jun 20, 1999 · N602DL · Boeing 757232 · Fuel Control/Turbine Engines
  > ON DESCENT RT ENGINE ROLLED BACK TO IDLE AND STABILIZED, THEN ENGINE ROLLED BELOW IDG ONLINE SPEED. CREW ELECTED TO SHUTDOWN ENGINE. RT ENG PRI CONTROL STATUS MSG ON AND THE EPCS MESSAGE EEC P/EEC 275-16 275-19 PRESENT.
- [SDR DL757982364](https://openairdocs.org/sdr/DL757982364.md): Battery Pack · discharged · Nov 14, 1998 · N602DL · Boeing 757232 · Emergency Lighting
  > EMERGENCY LIGHT IN FIRST CLASS (SIDES OF SEATS) DO NOT ILLUMINATE. REPLACED BATTERY MODULE BASE.
- [SDR DL757981203](https://openairdocs.org/sdr/DL757981203.md): Wire · failed · Jun 7, 1998 · N602DL · Boeing 757232 · Landing Gear System Wiring
  > STRONG SMELL/FUMES LIKE ELECTRIC INSULATION BURNING DETECTED DURING APPROACH IN COCKPIT AND BY FLT ATTENDANT IN FWD GALLEY. REPLACED NOSE GEAR GREEN LIGHT IN COCKPIT AND REPAIRED ASSOCIATED WIRING.
- [SDR DL757970985](https://openairdocs.org/sdr/DL757970985.md): Bulb · failed · May 22, 1997 · N602DL · Boeing 757232 · Emergency Lighting
  > RT FWD OVERWING EMERG EXT LT INOP. RELAMPE, OPN NORMAL.
- [SDR DL757970830](https://openairdocs.org/sdr/DL757970830.md): Light · inoperative · May 3, 1997 · N602DL · Boeing 757232 · Emergency Lighting
  > THE 4L DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED AND REPLACED POWER SUPPLY, BOTH NO HELP. NEEDS NEW LIGHT ASSY. PLACED ON MAINTENANCE CARRY OVER.
- [SDR DL757970829](https://openairdocs.org/sdr/DL757970829.md): Bulb · failed · May 3, 1997 · N602DL · Boeing 757232 · Emergency Lighting
  > RIGHT OVERWING ESCAPE PATH LIGHT FORWARD POSITION INOP. RELAMPED, OP CK GOOD.

Next page: https://openairdocs.org/deregistered/N602DL-2017-05-16/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 = 'N602DL' AND deregistration_id = 'N602DL-2017-05-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N602DL-2017-05-16/reports

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