# Service difficulty reports: N367DL, cancelled Apr 16, 2003

A list on [N367DL, cancelled Apr 16, 2003](https://openairdocs.org/deregistered/N367DL-2003-04-16.md).

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

- [SDR DL73E011295](https://openairdocs.org/sdr/DL73E011295.md): Battery · discharged · Aug 6, 2001 · N367DL · Boeing 7372S3 · Emergency Lighting
  > ON INSPECTION FOUND AFT LEFT OVER DOOR EMERGENCY EXIT SIGN INOP. REPLACED BATTERIES PER MM. OPN NORMAL
- [SDR DL73E010864](https://openairdocs.org/sdr/DL73E010864.md): Indicator · failed · May 29, 2001 · N367DL · Boeing 7372S3 · Visual Omnirange (VOR) System
  > NR 1 INST XMFR C/B POPPED ON PRE-DEPARTURE. REPLACED CAPTS RMI DUE TO OFF FLAG IN VIEW.
- [SDR DL73E010557](https://openairdocs.org/sdr/DL73E010557.md): Frame · cracked · Apr 4, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, Frame
  > CRACKS WERE FOUND IN THE FS 178 BULKHEAD LT AND RT SIDE CHORDS. ADDITIONALLY, TWO CRACKS WERE FOUND IN THE CENTER WEB AT LBL 12/WL 218 AND RBL 12/WL 234. THE WEB WAS REPAIRED PER SRM 53-10-11, FIG. 1 AND THE CHORDS WERE REPLACED PER ERA 397408-14AD. THE D
- [SDR DL73E010555](https://openairdocs.org/sdr/DL73E010555.md): Skin · cracked · Apr 4, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > TWO CRACKS WERE FOUND IN THE FUSELAGE SKIN NEAR FS 727B, STR 17 RT AND 727A, STR 18 RT. THE CRACKS WERE CUT OUT AND AN EXTERNAL DOUBLER WAS INSTALLED PER B737-200 SRM 53-30-3, FIG6. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73E010554](https://openairdocs.org/sdr/DL73E010554.md): Skin · cracked · Apr 4, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > A CRACK WAS FOUND IN THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR. THE CRACK WAS COMMON TO THE SKIN, BONDED DOUBLER AND THE BEAR STRAP. THE CRACK WAS CUT OUT AND A DOUBLER / TRIPLER INSTALLED AT HMV.
- [SDR DL73E010518](https://openairdocs.org/sdr/DL73E010518.md): Floorbeam · cracked · Mar 30, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, Floor Beam
  > DURING ACCOMPLISHMENT OF INSPECTION PER S/B 737-57-1210. A CRACK WAS FOUND IN THE PANEL ATTACH HOLE AT FS 660. THE CRACK WAS CUT OUT AND THE AREA REPAIRED BY S/B 737-57-1210.THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73E010499](https://openairdocs.org/sdr/DL73E010499.md): Skin · cracked · Mar 27, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > A CRACK WAS FOUND IN THE FUSELAGE SKIN AT FS 727B AND STR 16L. THE CRACK WAS CUT OUT AND REPAIRED PER SRM 53-30-3. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73E010466](https://openairdocs.org/sdr/DL73E010466.md): Frame · cracked · Mar 22, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, Frame
  > A CRACK WAS FOUND IN THE WEB OF THE FS 795 FRAME BETWEEN STR 23R AND 24R. THE CRACK WAS CUT OUT AND REPAIRED PER SRM 51-40-3, FIGURE 1. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73E001723](https://openairdocs.org/sdr/DL73E001723.md): Support Fitting · corroded · Sep 6, 2000 · N367DL · Boeing 7372S3 · Main Landing Gear Attach Section
  > THE LUG BORE OF THE FS 685 LT MLG SIDE SUPPORT FITTING WAS FOUND WITH CORROSION. THE CORROSION WAS REMOVED BY OVERSIZING THE LUG BORE. AN OVERSIZE BUSHING WAS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 378436-14.
- [SDR DL73E001722](https://openairdocs.org/sdr/DL73E001722.md): Beam · tool damage · Sep 6, 2000 · N367DL · Boeing 7372S3 · Wing Spar
  > THE AFT TRUNNION BORE OF THE LT WING MLG SUPPORT BEAM SUFFERED TOOLING DAMAGE IN THE HOLE BORE. THE BORE WAS OVERSIZED TO REMOVE THE TOOLING DAMAGE, ROTO PEENED, AND AN OVERSIZE BUSHGING INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 378444-14.
- [SDR DL73E001670](https://openairdocs.org/sdr/DL73E001670.md): Link · corroded · Aug 23, 2000 · N367DL · Boeing 7372S3 · Landing Gear Retraction/Extension System
  > MLG TRUNNION LINK PITTED AND RUSTY RUST COMING OUT OF MATING SURFACES OF TRUNNION LINK ASSY AND TRUNNION PIN I/B OF MLG ACTUATOR. RIGHT MLG TRUNNION LINK PITTED/CORRODED ON I/B AND O/B FACES. RT MLG UPPER STRUT TRUNNION LUG CORROSION. RT MLG UPPER STRUT CYL
- [SDR DL73E001623](https://openairdocs.org/sdr/DL73E001623.md): Pcu · malfunctioned · Aug 19, 2000 · N367DL · Boeing 7372S3 · Rudder Control System
  > NOTICED A SHARP ABRUPT YAW INPUT SHORTLY AFTER NOSE WHEEL LIFT OFF. NO ABNORMAL WINDS OR AIRCRAFT WAKE EXISTING. YAW WAS SIGNIFICIANT, NO INPUTS NOTED IN RUDDER PEDALS BY PILOT FLYING. CHECKED YAW DAMP FOR FAULTS, NONE. REPLACED RUDDER PCU PER M/M RII. C
- [SDR DL73E001600](https://openairdocs.org/sdr/DL73E001600.md): Actuator · malfunctioned · Aug 19, 2000 · N367DL · Boeing 7372S3 · Rudder Actuator
  > NOTICED A SHARP ABRUPT YAW INPUT SHORTLY AFTER NOSE WHEEL LIFTOFF. NO ABNORMAL WINDS OR AIRCRAFT WAKE EXISTING. YAW WAS SIGNIFICANT NO INPUTS NOTED IN RUDDER PEDALS BY PILOT FLYING. REPLACING RUDDER PACK.
- [SDR DL73E991786](https://openairdocs.org/sdr/DL73E991786.md): Light · inop · Aug 10, 1999 · N367DL · Boeing 7372S3 · Emergency Lighting
  > EMERGENCY LTS INOP LT AND RT FWD ENTRY DOOR ON OUTSIDE OF AIRCRAFT REF WDM 33-51-01. REPLACED M571. OPS NORMAL.
- [SDR DL73E991322](https://openairdocs.org/sdr/DL73E991322.md): Skin · cracked · Jun 11, 1999 · N367DL · Boeing 7372S3 · Service Doors
  > DURING THE INSP OF THE R1 DOOR UPPER CORNERS SEVERAL CRACKS WERE FOUND IN THE SKIN ASSY AND BEARSTRAP. REPAIRED PER ERA 367544-14, REV A.
- [SDR DL73E990846](https://openairdocs.org/sdr/DL73E990846.md): Connector · loose · Apr 16, 1999 · N367DL · Boeing 7372S3 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ALONG AISLE AND LOWER DOORS COME ON AND GO OFF ON THEIR OWN. FOUND WIRE LOOSE ON AFT FLT ATTENDANT PANEL EMERGENCY SWITCH. TIGHTENED CONNECTOR ON SWITCH. LIGHTS OPS CHK NML.
- [SDR DL73E990133](https://openairdocs.org/sdr/DL73E990133.md): Battery · discharged · Jan 21, 1999 · N367DL · Boeing 7372S3 · Emergency Lighting
  > EMERGENCY EXIT LIGHT BATTERIES DEAD DUE TO GND POWER LOSS. REPLACED EMERGENCY EXIT BATTERIES AND BASE ASSY.
- [SDR DL73E982302](https://openairdocs.org/sdr/DL73E982302.md): Skin · cracked · Nov 6, 1998 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH A 1.875 INCH CRACK BELOW THE L1 DOOR AT APPROX FS 335. THE CRACK IS TYPICAL OF BAC S/B 737-53-1083. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN INTERIM DOUBLER REPAIR PER THE S/B. THE REPAIR WILL BE REPLACED WITH A PERMA
- [SDR DL73E982128](https://openairdocs.org/sdr/DL73E982128.md): Floorbeam · cracked · Oct 12, 1998 · N367DL · Boeing 7372S3 · Fuselage Main, Floor Beam
  > THE UPPER CAP OF THE RBL 24.82 OVERWING PASSENGER FLOORBEAM WAS FOUND WITH A.5 INCH CRACK EMANATING FROM A CUTOUT FOR A SEAT TRACK ATTACH POINT. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER AND TRIPLER PER ER/A 365847-14, REV B.
- [SDR DL73E982127](https://openairdocs.org/sdr/DL73E982127.md): Skin · cracked · Oct 12, 1998 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > THE UPPER HINGE CUTOUT OF THE L1 DOOR OPENING WAS FOUND WITH A TYPICAL CRACK IN THE SKIN AND BONDED DOUBLER. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER THE B737 SRM 53-30-3 FIG 21. THE REPAIR WAS DOCUMENTED PER ER/A 365839-14, R
- [SDR DL73E981894](https://openairdocs.org/sdr/DL73E981894.md): Audio Acc Unit · failed · Sep 12, 1998 · N367DL · Boeing 7372S3 · Audio Integrating System
  > COMM RADIO FAILURE IN FLIGHT OCCURED 5 MIN AFTER T/O. RADIOS RESTORED AFTER APU STARTED AND TRANSFERED NR 2 BUS TO APU. RAN ENGS ALL COMRADIOS CK GOOD. INSPECTED STATIC WICKS AND ANTS. ALL OK. REPLACED AUDIO ACC UNIT. ALL RADIO FUNCTIONS NORMAL.
- [SDR DL73E981449](https://openairdocs.org/sdr/DL73E981449.md): Clip · cracked · Jul 9, 1998 · N367DL · Boeing 7372S3 · Fuselage Miscellaneous Structure
  > A SKIN AND STRINGER REPAIR WERE ACCOMPLISHED AT FS 597 STR 2L. THE FRAME-TO-STRINGER CLIP INSPECTION REQUIRED PER BAC S/B 737-53-1085 (AD 93-08-04) WAS ACCOMPLISHED AT THIS LOCATION AND RESULTED IN FINDING A CRACKED CLIP. A NEW CLIP HAD TO BE MODIFIED TO ALL
- [SDR DL73E981447](https://openairdocs.org/sdr/DL73E981447.md): Clips · cracked · Jul 8, 1998 · N367DL · Boeing 7372S3 · Fuselage Miscellaneous Structure
  > WHILE ACCOMPLISHING REPLACEMENT OF CRACKED FRAME-TO-STRINGER CLIPS PER BAC S/B 737-53-1085 (AD 93-08-04), MTC. WAS UNABLETO INSTALL THE REQUIRED RIVETS. THE RIVETS WERE SUBSTITUTED WITH STEEL HI-LOKS PER ER/A 365196-14AD, REV A.
- [SDR DL73E980037](https://openairdocs.org/sdr/DL73E980037.md): Skin · cracked · Jan 6, 1998 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > FUSELAGE/SKIN, FS 727A-727B, S-16R-17R, REPAIRED FOR SKIN CRACKS. THE FUSELAGE SKIN BETWEEN FS 727A AND 727B AND BETWEEN STRINGER 16R AND 17R WAS FOUND WITH A 3.25 LONG CRACK AND A 2.25 LONG CRACK. THE CRACKS WERE CUT OUT AND A REPAIR DOUBLER WAS INSTALLED P
- [SDR DL73E970290](https://openairdocs.org/sdr/DL73E970290.md): Intercostal · cracked · Feb 12, 1997 · N367DL · Boeing 7372S3 · Fuselage Miscellaneous Structure
  > THE R-1 DOOR FRAME INTERCOSTALS AT STR 8A,10A, 11A WERE FOUND CRACKED IN THE TYPICAL MANNER SHOWN IN S/B 737-53A1108, REV 5. THIS ER/A ACCOMPLISHED A REPAIR AT THIS LOCATION WITH THE LISTED S/B AND AD 88-03-03. REPETITIVE INSPECTIONS PER EO 3-55852-12AD MUS
- [SDR DL73E970200](https://openairdocs.org/sdr/DL73E970200.md): Uplock Sensor · malfunctioned · Feb 1, 1997 · N367DL · Boeing 7372S3 · Landing Gear Position and Warning
  > LEFT GEAR RED ON RETRACTION. RETURNED TO CVG. CORRECTIVE ACTION NECESSARY TO DO GEAR SWING. CHECKING UPLOCK. REPLACED UPLOCK SENSOR. CHECKS OK.
- [SDR DL73E962787](https://openairdocs.org/sdr/DL73E962787.md): Pwr Supply · inoperative · Dec 30, 1996 · N367DL · Boeing 7372S3 · Emergency Lighting
  > BOTH LT AND RT LOWER EMERG DOOR EXIT IDENTIFIERS INOP. REPLACED EMERG LIGHT PWR SUPPLY PACK M9027, OPS GOOD PER MM.
- [SDR DL73E962403](https://openairdocs.org/sdr/DL73E962403.md): Transmitter · inoperative · Oct 28, 1996 · N367DL · Boeing 7372S3 · Trailing Flap Position Indicating System
  > FLAPS FAILED TO EXTEND. REPLACED LT FLAP POS TRANSMITTER AND INDICATOR, OPER CK OK.
- [SDR DL73E954745](https://openairdocs.org/sdr/DL73E954745.md): Rib · cracked · Dec 21, 1995 · N367DL · Boeing 7372S3 · Cargo/Baggage Doors
  > DURING SHOP INSPECTION, C-2 CARGO DOOR WAS FOUND WITH CRACKS TO A RIB AND SUPPORT ANGLE AT ACCESS HOLE NR 23. ACCOMPLISHED REPAIRS PER ERA 271679-14AD AND SRM 52-30-2.
- [SDR DL73E954496](https://openairdocs.org/sdr/DL73E954496.md): Frame · cracked · Sep 22, 1995 · N367DL · Boeing 7372S3 · Cargo/Baggage Doors
  > AIRWORTHINESS DIRECTIVE 90-06-02, DOOR AFT CARGO, LOWER AFT CORNER, FRAME AND BEAM REPAIR. DURING ROUTINE OVERHAUL, THE LOWER AFT CORNER OF THE AFT CARGO DOOR WAS FOUND DAMAGED. THE FRAME WAS CRACKED AXIALLY ALONG THE RADIUS APPROX 20 INCHES. THE LOWER BEAM
- [SDR DL73E952649](https://openairdocs.org/sdr/DL73E952649.md): Skin · cracked · Jun 7, 1995 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > DURING INSPECTION, THE FUSELAGE SKIN AT STA 303.9 BETWEEN STR 10 AND STR 14 WAS CRACKED AT THE LOWER FORWARD CORNER OF THE FORWARD ENTRY DOORWAY (L-1) LOWER HINGE CUTOUT. THE CRACK MEASURED APPROX 1.8 LONG. FAA FORM 8110-3 DATED 6/7/95, THE DAMAGE WAS CUT OU

## 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 = 'N367DL' AND deregistration_id = 'N367DL-2003-04-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N367DL-2003-04-16/reports

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