# Service difficulty reports: N369DL, cancelled Dec 23, 2003

A list on [N369DL, cancelled Dec 23, 2003](https://openairdocs.org/deregistered/N369DL-2003-12-23.md).

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

- [SDR DL73E011337](https://openairdocs.org/sdr/DL73E011337.md): Battery Pack · discharged · Aug 13, 2001 · N369DL · Boeing 7372S3 · Emergency Lighting
  > ON INSPECTION FOUND FWD, MID, AND AFT OVERHEAD EMERGENCY EXIT LIGHTS INOP IN CABIN. REPLACED FWD BATTERY PACK, MID RT BATTERY PACK AND CHARGER ASSY AND AFT BATTERY PACK AND CHARGER ASSY. OPN OF ALL EMERGENCY LIGHTS NOW NORMAL.
- [SDR DL73E011336](https://openairdocs.org/sdr/DL73E011336.md): Battery Pack · discharged · Aug 13, 2001 · N369DL · Boeing 7372S3 · Emergency Lighting
  > ON INSPECTION FOUND OVERWING EMERGENCY EXIT LIGHTS INOP IN CABIN. REPLACED MID LEFT BATTERY PACK PER MM. OPN NORMAL.
- [SDR DL73E011285](https://openairdocs.org/sdr/DL73E011285.md): Battery Pack · discharged · Jul 4, 2001 · N369DL · Boeing 7372S3 · Emergency Lighting
  > ON INSPECTION FOUND EMERGENCY LIGHTS IN CEILING OF CABIN, ALL POSITIONS INOP. BOTH CABIN OVERWING EMERGENCY LIGHTS INOP ALSO. REPLACED FWD, MID AND AFT LEFT BATTERY PACKS PER MM. CKS NORMAL.
- [SDR DL73E010049](https://openairdocs.org/sdr/DL73E010049.md): Flap Track · corroded · Jan 8, 2001 · N369DL · Boeing 7372S3 · Trailing Edge Flaps
  > INSPECTION OF THE INBD FLAP TRACK OF THE OUTBD FLAP ON THE LT WING REVEALED EXTENSIVE PITTING CORROSION. THE FLAP TRACK WAS REMOVED AND DISCARDED. A NEW FLAP TRACK WAS INSTALLED PER ER/A 379729-14AD.
- [SDR DL73E001969](https://openairdocs.org/sdr/DL73E001969.md): Intercostal · cracked · Oct 10, 2000 · N369DL · Boeing 7372S3 · Fuselage Miscellaneous Structure
  > ROUTINE INSPECTIONS OF THE FWD GALLEY DOOR (R1) SURROUND STRUCTURE PER AD 98-22-10, REVEALED A CRACK IN THE LOWER INTERCOSTAL OF THE AFT DOOR FRAME. THE CRACK IS TYPICAL OF BAC S/B 737-53A1108. THE CRACKED INTERCOSTAL WAS REMOVED AND AN IMPROVED VERSION
- [SDR DL73E001331](https://openairdocs.org/sdr/DL73E001331.md): Transmission · seized · Jul 14, 2000 · N369DL · Boeing 7372S3 · Trailing Edge Flap Control System
  > FLAPS LOCKED OUT ON APPROACH TO CAE. CREW DID GO-AROUND. FOUND FLAP TRANSMISSION SEIZED. REPLACED FLAP TRANSMISSION AND JACK SCREW ASSY, CHECKS GOOD.
- [SDR DL73E001071](https://openairdocs.org/sdr/DL73E001071.md): Engine · fod · May 31, 2000 · N369DL · Boeing 7372S3 · Engine (Turbine/Turboprop)
  > ON TAKEOFF, HEARD LOUD BANG. SUSPECT BIRD STRIKES. FOUND NR 2 ENG 1ST STAGE FAN BLADE FOD. REPLACING FAN.
- [SDR DL73E000880](https://openairdocs.org/sdr/DL73E000880.md): Skin · cracked · May 2, 2000 · N369DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > A 2 INCH CRACK WAS FOUND EMANATING FROM UNDER A WING TO BODY FAIRING AT FS 727A+3 AND STRINGER 17L. AN EXISTING REPAIR WAS NEAR THE CRACK. THE PREVIOUS REPAIR WAS REMOVED AND THE NEW CRACK AND EXISTING REPAIR CUTOUT WERE COMBINED INTO A 20 X 11 INCH CUTOUT.
- [SDR DL73E000862](https://openairdocs.org/sdr/DL73E000862.md): Floorbeam · cracked · Apr 28, 2000 · N369DL · Boeing 7372S3 · Fuselage Main, Floor Beam
  > THE RBL 45.5 FLOOR LONGITUDINAL FLOORBEAM OVER THE MLG WHEEL WELL WAS FOUND WITH A 12 INCH CRACK IN THE BEAM WEB BETWEEN FS 633 & 645. THE CRACKED SECTION OF WEB WAS CUT AND REMOVED. A NEW SECTION OF WEB WAS SPLICED IN WITH TWO ALUMINUM SPLICE DOUBLERS
- [SDR DL73E992535](https://openairdocs.org/sdr/DL73E992535.md): damaged · Nov 16, 1999 · N369DL · Boeing 7372S3 · Flight Control System
  > RT WING OUTBOARD FLAP JACKSCREW DAMAGED. REPLACED NR 8 JACKSCREW TRANSMISSION ASSY.
- [SDR DL73E991724](https://openairdocs.org/sdr/DL73E991724.md): Radar Tr Unit · inop · Aug 1, 1999 · N369DL · Boeing 7372S3 · Weather Radar System
  > WX RADAR ANT FLASHING ON SCREEN. NO RADAR AVAILABLE. REPLACED WX RARAR TRANSCEIVER.
- [SDR DL73E990287](https://openairdocs.org/sdr/DL73E990287.md): Generator · failed · Feb 13, 1999 · N369DL · Boeing 7372S3 · AC Generator-Alternator
  > NR 1 ENG GEN FAILED SHORTLY AFTER T/O. THERE WAS NO INDICATION ON THE OVERHEAD ELECT PANEL THAT THE GENERATOR HAD FAILED. REPLACED GCU.
- [SDR DL73E982420](https://openairdocs.org/sdr/DL73E982420.md): Battery Pack · discharged · Nov 23, 1998 · N369DL · Boeing 7372S3 · Emergency Lighting
  > ONE SECTION OF EMERGENCY LIGHTS REMAINED ON DURING FLT. REPLACED EMERG BATTERY PACK, OPS CK OK.
- [SDR DL73E982303](https://openairdocs.org/sdr/DL73E982303.md): Skin · cracked · Nov 4, 1998 · N369DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN, DOUBLER AND BEAR STRAP WERE FOUND WITH A 1 INCH TYPICAL CRACK IN THE LOWER FWD CORNER OF THE R2 DOOR CUTOUT. THE CRACK WAS REPAIRED PER B737 SRM 53-30-3, FIG 24 EXCEPT BLIND FASTENERS WERE AUTHORIZED ON A TIME-LIMITED BASIS. THE REPAIR WAS
- [SDR DL73E981948](https://openairdocs.org/sdr/DL73E981948.md): Circuit Breaker · tripped · Sep 20, 1998 · N369DL · Boeing 7372S3 · Landing Gear Retraction/Extension System
  > AIR TURNBACK DUE TO LANDING GEAR LEVER WOULDN'T MOVE TO UP POS ON T/O. ABNORMAL PROCEDURES RUN TO RAISE LANDING GEAR. LAND GEAR EXT NORMAL ON RETURN. RESET LEVER LATCH C/B. CYCLED LAND GEAR LEVER, ALL IND NORMAL. REPLACED LEVER LATCH C/B. CYCLED L/G LEVER
- [SDR DL73E980955](https://openairdocs.org/sdr/DL73E980955.md): Skin · punctured · Apr 30, 1998 · N369DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > A 1.5 X 1.5 PUNCTURE WAS FOUND IN THE FUSELAGE SKIN JUST AFT OF STA 460 BELOW THE STRINGER 25R SKIN LAP SPLICE. THE PUNCTURE WAS TRIMMED TO A SMOOTH CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND AN ADDITIONAL DOUBLER TO OVERLAP THE SKIN LAP SPLICE
- [SDR DL73E980935](https://openairdocs.org/sdr/DL73E980935.md): Bolt · loose · Apr 29, 1998 · N369DL · Boeing 7372S3 · Trailing Edge Flaps
  > DURING AD MANDATED INSPECTION, THE OUTBD BOLT ON THE NR 3 FLAP OUTBD TRACK AFT ATTACH FITTING WAS FOUND LOOSE. THE CONDITION WAS CORRECTED BY INSTALLING THE TRACK MODIFICATION PER BAC S/B 737-57A1130. THE MODIFICATION WAS DOCUMENTED PER ER/A 364643-14AD.
- [SDR DL73E980720](https://openairdocs.org/sdr/DL73E980720.md): Anti-Ice · odor · Apr 2, 1998 · N369DL · Boeing 7372S3 · Engine Anti-Icing System
  > AT 25,000, AN ELECTRICAL SMELL WAS NOTED IN ENTIRE AIRCRAFT WHEN ENGINE ANTI-ICE WAS TURNED ON. SMELL WENT AWAY WHEN ENGINE ANTI-ICE TURNED OFF. RAN ENGINES AND PACKS, INSPECTED FOR SOURCE, NO TROUBLE FOUND.
- [SDR DL73E971682](https://openairdocs.org/sdr/DL73E971682.md): Skin · cut · Aug 22, 1997 · N369DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING THE REPLACEMENT OF STA 727 FRAME CHORD PER E.O. 3-68646-3AD, THE FUSELAGE SKIN BETWEEN ST 727 BULKHEAD AND STA 727+10 WAS CUT IN ORDER TO PROVIDE ACCESS FOR THE CHORD REPLACEMENT. WHEN CUTTING THE SKIN, MX ALSO CUT THE INTERNAL BONDED WAFF
- [SDR DL73E971681](https://openairdocs.org/sdr/DL73E971681.md): Frame · cracked · Aug 22, 1997 · N369DL · Boeing 7372S3 · Fuselage Main, Frame
  > THE FS 727 BULKHEAD O/B CHORD AT STR 18A WAS FOUND CRACKED AND IS BEING REPLACED PER BACO DWG 65C33722, AS REQUIRED BY DAL EO 3-68646-3AD, WHICH ACCOMPLISHES S/B 737-53-1088. BETWEEN STR S-24 AND S-27, BACB30FP* FASTENERS, SAME SIZE AS REQUIRED BY BP, WERE IN
- [SDR DL73E971680](https://openairdocs.org/sdr/DL73E971680.md): Frame · cracked · Aug 22, 1997 · N369DL · Boeing 7372S3 · Fuselage Main, Frame
  > WHILE ACCOMP INSPECTIONS REQUIRED BY AD 95-12-17, A TYPICAL CRACK WAS FOUND IN THE BS 727 FRAME, OUTBOARD CHORD AT STR 18A, LHS. THE CHORD WILL BE REPLACED PER S/B 737-53-1088 AND A PREVENTATIVE MODIFICATION WILL BE ACCOMP PER S/B 737-53A1166. THE S/B REQUIR
- [SDR DL73E970856](https://openairdocs.org/sdr/DL73E970856.md): Light · inop · May 5, 1997 · N369DL · Boeing 7372S3 · Emergency Lighting
  > ON L/O, FOUND EMERGENCY EXIT LIGHT ABOVE 2L DOOR INOP. REPLACED LIGHT ASSEMBLY.
- [SDR DL73E961648](https://openairdocs.org/sdr/DL73E961648.md): Bolt · worn threads · Jun 23, 1996 · N369DL · Boeing 7372S3 · Trailing Edge Flaps
  > WHILE ACCOMPLISHING TORQUE CHECK OF CENTER ATTACH BOLT OF NR 2 FLAP O/B TRACK ATTACH FITTING, THE CENTER BOLT WAS FOUND TO HAVE DAMAGED THREADS. IN ACCORDANCE WITH SB 737-57A1130, THE PREVENTATIVE MOD WILL BE INSTALLED. ADDITIONALLY, THE FLAP TRACK BUSHING W
- [SDR DL73E960901](https://openairdocs.org/sdr/DL73E960901.md): Light · malfunctioned · Apr 17, 1996 · N369DL · Boeing 7372S3 · Emergency Lighting
  > FORWARD ENTRY DOOR EMERGENCY LIGHT COMES ON WHEN SWITCH NOT ARMED AND AIRCRAFT POWER OFF. REPLACED LIGHT ASSEMBLY (P/N 10-0067-7).
- [SDR DL73E960325](https://openairdocs.org/sdr/DL73E960325.md): Battery · discharged · Feb 10, 1996 · N369DL · Boeing 7372S3 · Emergency Lighting
  > ON PREFLIGHT, EMERGENCY EXIT LIGHT AT FWD SERVICE DOOR INOP. REPLACED BATTERIES, BULBS AND SECURED WIRE TERMINAL, OPERATION NORMAL.
- [SDR DL73E960272](https://openairdocs.org/sdr/DL73E960272.md): Floorbeam · cracked · Feb 2, 1996 · N369DL · Boeing 7372S3 · Fuselage Main, Floor Beam
  > DURING INSPECTION, THE LONGITUDINAL FLOORBEAM AT APPROXIMATELY STA 675 AND RBL 45 WAS FOUND WITH A 2.5 INCH CRACK IN THE LOWER CHORD. DAMAGE REMOVAL RESULTED IN TRIMMING OUT THE LOWER HORIZONTAL FLANGE OF THE CHORD IN ACCORDANCE WITH FORM 8110-3, DATED 2-2-96

## 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 = 'N369DL' AND deregistration_id = 'N369DL-2003-12-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N369DL-2003-12-23/reports

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