# Service difficulty reports: N54SW, cancelled Aug 21, 2013

A list on [N54SW, cancelled Aug 21, 2013](https://openairdocs.org/deregistered/N54SW-2013-08-21.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 3 · 103 reports

- [SDR 2002F00919](https://openairdocs.org/sdr/2002F00919.md): Engine · malfunctioned · Aug 7, 2002 · N54SW · Boeing 7372H4 · Engine (Turbine/Turboprop)
  > DURING CLIMB-OUT FROM CLE, NOTED ABNORMAL HIGH OIL TEMP ON NR 1 ENGINE. ACCOMPLISHED PRECAUTIONARY ENGINE SHUTDOWN. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED IN PIT WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE. (M)
- [SDR 2002F00194](https://openairdocs.org/sdr/2002F00194.md): Spar · corroded · Jan 16, 2002 · N54SW · Boeing 7372H4 · Wing Spar
  > FOUND CORROSION ON RIGHT WING UPPER SPAR CHORD ALONG EDGE BETWEEN SPLICE PLATE AND CHORD STATION 663 OUTBOARD OF BBL 70.85 APPROXIMATELY 3.5 INCHES LONG. (M)
- [SDR 2002F00157](https://openairdocs.org/sdr/2002F00157.md): Rib · cracked · Jan 15, 2002 · N54SW · Boeing 7372H4 · Wing, Rib/Bulkhead
  > FOUND LEFT WING STATION 453 HAS A CRACKED RIB AT THE FORWARD VENT STRINGER FORWARD ATTACH BOLT. (M)
- [SDR 2002F00195](https://openairdocs.org/sdr/2002F00195.md): Skin · cracked · Jan 14, 2002 · N54SW · Boeing 7372H4 · Fuselage Main, Plate/Skin
  > AFT CARGO COMPARTMENT DOOR JAMB FORWARD LOWER CORNER EXTERIOR SKIN HAS A ONE INCH CRACK AT FASTENER STATION 794. (M)
- [SDR 2002F00160](https://openairdocs.org/sdr/2002F00160.md): Web · cracked · Jan 14, 2002 · N54SW · Boeing 7372H4 · Horizontal Stabilizer Structure
  > FOUND STATION 1125 W/L 250 SUBWEB UNDER HORIZONTAL STABILIZER SUPPORT FRAME, HAS SIX CRACKS EMANATING FROM THREE LIGHTENING HOLES IN THE SUB WEB. (M)
- [SDR 2002F00196](https://openairdocs.org/sdr/2002F00196.md): Support · cracked · Dec 31, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > LEFT W/W FAIRING SUPPORT PLATE CRACKED AT FS 661. (M)
- [SDR 2002F00118](https://openairdocs.org/sdr/2002F00118.md): Floor Support · corroded · Dec 29, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > AS VIEWED FROM THE E/E COMPT, THERE IS CORROSION ON A MAIN DECK FLOOR SUPPORT AT BS 312 LBL 11R, ON ITS LOWER SIDE AROUND A SCREW HOLE. (M)
- [SDR 2002F00119](https://openairdocs.org/sdr/2002F00119.md): Floorbeam · corroded · Dec 28, 2001 · N54SW · Boeing 7372H4 · Fuselage Main, Floor Beam
  > FORWARD CABIN FLOOR STRUCTURE, FLOORBEAM UPPER CHORD AT BS 294 RBL 10 TO LBL 10 WL 208 HAS CORROSION. (M)
- [SDR 2002F00043](https://openairdocs.org/sdr/2002F00043.md): Support · cracked · Dec 26, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > FOUND STRINGER SUPPORT TIE CRACKED AT FUSELAGE STATION 727B LONGERON 6L. (M)
- [SDR LCQ04](https://openairdocs.org/sdr/LCQ04.md): Stringer · cracked · Dec 20, 2001 · N54SW · Boeing 7372H4 · Fuselage Main, Longeron/Stringer
  > BS 727 STRINGER 18A RIGHT, NOTED CRACK IN THE I/B STRINGER 18A WEB STRAP. CRACK EMANATING FROM HOLE AT BS 725.5 AND PROPAGATING DOWN AND FORWARD (LOOKING AT FASTENERS HOLE FROM INSIDE WHEEL WELL, IT WOULD BE THE 8 O'CLOCK POSITION).
- [SDR 2002F00159](https://openairdocs.org/sdr/2002F00159.md): Shear Tie · cracked · Dec 19, 2001 · N54SW · Boeing 7372H4 · Fuselage Main, Structure
  > FOUND SHEAR TIE IS CRACKED AT STATION 787 STRINGER 6R. (M)
- [SDR 2002F00156](https://openairdocs.org/sdr/2002F00156.md): Shear Tie · cracked · Dec 19, 2001 · N54SW · Boeing 7372H4 · Fuselage Main, Structure
  > SHEAR TIE IS CRACKED AT STATION 727A STRINGER 3R, 4R AND 5R. (M)
- [SDR 2002F00128](https://openairdocs.org/sdr/2002F00128.md): Stringer · cracked · Dec 19, 2001 · N54SW · Boeing 7372H4 · Fuselage Main, Longeron/Stringer
  > FOUND BS 727 STRINGER 18A LEFT VERTICAL OUTER CHORD IS CRACKED FROM THE FORWARD HOLE BS 727.5 AND PROPAGATES AFT APPROXIMATELY.25 INCH IN LENGTH. (M)
- [SDR 2002F00127](https://openairdocs.org/sdr/2002F00127.md): Floorbeam · corroded · Dec 19, 2001 · N54SW · Boeing 7372H4 · Fuselage Main, Floor Beam
  > FOUND CORROSION AROUND FLOORBEAM FASTENER HOLES AT STATION 344 LBL 10 AND STATION 360 RBL 1. (M)
- [SDR 2002F00126](https://openairdocs.org/sdr/2002F00126.md): Angle · corroded · Dec 19, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > FOUND R2 DOOR THRESHOLD AREA HAS CORROSION ON SUPPORT ANGLES BS 950 THROUGH 1006 RBL 52. (M)
- [SDR 2002F00125](https://openairdocs.org/sdr/2002F00125.md): Tie Clip · cracked · Dec 19, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > FOUND STRINGER TIE CLIPS CRACKED AT STATION 727B, STRINGER 3R, 4R, 5R AND 6R. (M)
- [SDR 2002F00124](https://openairdocs.org/sdr/2002F00124.md): Shear Tie · cracked · Dec 19, 2001 · N54SW · Boeing 7372H4 · Fuselage Main, Structure
  > FOUND SHEAR TIE CLIP IS CRACKED AT STATION 616 STRINGER 5R. (M)
- [SDR 2002F00123](https://openairdocs.org/sdr/2002F00123.md): Clip · cracked · Dec 19, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > LEFT CABIN STATION 747 STRINGER 4 AND STRINGER 7 HAS ATTACH CLIPS CRACKED. (M)
- [SDR 2002F00122](https://openairdocs.org/sdr/2002F00122.md): Tie Clip · cracked · Dec 19, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > FOUND CRACK IN U-CHANNEL TIE CLIP AT STRINGER 4L FLIGHT STATION 625. (M)
- [SDR 2002F00121](https://openairdocs.org/sdr/2002F00121.md): Clip · cracked · Dec 19, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > LEFT CABIN STATION 827 STRINGER 6L HAS ATTACH CLIP CRACKED. (M)
- [SDR 2002F00120](https://openairdocs.org/sdr/2002F00120.md): Stringer · cracked · Dec 19, 2001 · N54SW · Boeing 7372H4 · Fuselage Main, Longeron/Stringer
  > FOUND BS 727 STRINGER 18A RIGHT, CRACK IN INBOARD STRINGER 18A WEB STRAP. CRACK EMANATING FROM HOLE AT BS 725.5 AND PROPAGATING DOWN AND FORWARD. (M)
- [SDR 2002F00130](https://openairdocs.org/sdr/2002F00130.md): Bulkhead · cracked · Dec 18, 2001 · N54SW · Boeing 7372H4 · Fuselage Main, Frame
  > ON INSPECTION OF BS 178 BULKHEAD, NOTED CRACK FROM AFT SIDE ON PILOT SIDE INSPECTED SIDE CHORD AREA ABOVE W/L 207. TWO INCH CRACK DOWN RADIUS OF SIDE CHORD. (M)
- [SDR 2002F00129](https://openairdocs.org/sdr/2002F00129.md): Attach Angle · cracked · Dec 18, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > FOUND LEFT FORWARD PIT FUSELAGE STATION 380 LBL 51 FRAME ATTACH ANGLE CRACKED. (M)
- [SDR 150070003](https://openairdocs.org/sdr/150070003.md): Bulkhead · cracked · Dec 18, 2001 · N54SW · Boeing 7372H4 · Fuselage Main, Bulkhead
  > ON INSPECTION OF THE 178 BULKHEAD NOTED CRACK FROM AFT SIDE ON PILOTS SIDE. (INSPECTED SIDE CHORD AREA ABOVE WL 207). NOTED APPROX 2 INCHES CRACK DOWN RADIUS OF SIDE CHORD.
- [SDR 2002F00164](https://openairdocs.org/sdr/2002F00164.md): Seat Track · corroded · Dec 17, 2001 · N54SW · Boeing 7372H4 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND SEAT TRACK AT STATION 400 LBL 43.5 CORRODED. (M)
- [SDR 2002F00163](https://openairdocs.org/sdr/2002F00163.md): Web · cracked · Dec 17, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > FOUND FORWARD PIT BS 460 LBL 11 LIGHTENING HOLE IS CRACKED. (M)
- [SDR 2002F00162](https://openairdocs.org/sdr/2002F00162.md): Floor Support · cracked · Dec 17, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > FOUND COCKPIT FLOOR LEFT SIDE F/S 227 WL 212 LBL 30 HAS CRACK IN FLOOR SUPPORT FORMER. (M)
- [SDR 2002F00161](https://openairdocs.org/sdr/2002F00161.md): Seat Track · corroded · Dec 17, 2001 · N54SW · Boeing 7372H4 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND SEAT TRACK CORRODED AT STATION 363 RBL 22.5. (M)
- [SDR 2002F00131](https://openairdocs.org/sdr/2002F00131.md): Support Bracket · cracked · Dec 17, 2001 · N54SW · Boeing 7372H4 · Vertical Stabilizer
  > VERTICAL STABILIZER AFT WEB SUPPORT BRACKET IS CRACKED OUT AROUND FASTENERS AT FIN WL 58.18 AND BS 1088. (M)
- [SDR 2002F00169](https://openairdocs.org/sdr/2002F00169.md): Rib · cracked · Dec 16, 2001 · N54SW · Boeing 7372H4 · Vertical Stabilizer, Spar/Rib
  > FOUND VERTICAL STAB LEADING EDGE PANEL NR 9545 HAS CRACKED RIB AT 85 INCH FROM LOWER END 9TH RIB. (M)
- [SDR 2002F00168](https://openairdocs.org/sdr/2002F00168.md): Floorbeam · corroded · Dec 16, 2001 · N54SW · Boeing 7372H4 · Fuselage Main, Floor Beam
  > FOUND CABIN UPPER FLOORBEAM CHORD AT BS 312 LBL 1 HAS CORROSION. (M)
- [SDR 2002F00167](https://openairdocs.org/sdr/2002F00167.md): Angle · cracked · Dec 16, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > FOUND FLOORBEAM LOWER SUPPORT ANGLE CRACKED AT BS 727 LBL 24. (M)
- [SDR 2002F00166](https://openairdocs.org/sdr/2002F00166.md): Stiffener · cracked · Dec 16, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > FOUND VERTICAL STIFFENER IS CRACKED AT LBL 1, BS 947.5 AT UPPER END. (M)
- [SDR 2002F00165](https://openairdocs.org/sdr/2002F00165.md): Rib · cracked · Dec 16, 2001 · N54SW · Boeing 7372H4 · Vertical Stabilizer, Spar/Rib
  > FOUND VERTICAL STABILIZER LEADING EDGE PANEL NR 9545 HAS A CRACKED RIB AT 94 INCHES FROM LOWER END OF 10TH RIB. (M)
- [SDR 2002F00173](https://openairdocs.org/sdr/2002F00173.md): Skin · cracked · Dec 15, 2001 · N54SW · Boeing 7372H4 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN AT FLIGHT STATION 800 STRINGER 22L CRACKED APPROXIMATELY 5 INCH LONG. (M)
- [SDR 2002F00172](https://openairdocs.org/sdr/2002F00172.md): Angle · cracked · Dec 15, 2001 · N54SW · Boeing 7372H4 · Wing, Center Box
  > FOUND CENTERWING FRONT SPAR SUPPORT ANGLE IS CRACKED AT BS 538 RBL 8. (M)
- [SDR 2002F00171](https://openairdocs.org/sdr/2002F00171.md): Attach Angle · cracked · Dec 15, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > FOUND RADAR MOUNT ATTACH ANGLE HAS A.800 INCH LONG CRACK AT LBL 5.7 WL 211 BS 178. (M)
- [SDR 2002F00170](https://openairdocs.org/sdr/2002F00170.md): Stringer Clip · cracked · Dec 15, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > FOUND FORWARD PIT STATION 380 STRINGER 19L ATTACH CLIP IS CRACKED. (M)
- [SDR 2002F00175](https://openairdocs.org/sdr/2002F00175.md): Frame · cracked · Dec 14, 2001 · N54SW · Boeing 7372H4 · Fuselage Main, Frame
  > FOUND LEFT FORWARD PIT STATION 420 ABOVE STRINGER 26 FRAME HAS A CRACK. (M)
- [SDR 2002F00174](https://openairdocs.org/sdr/2002F00174.md): Slat · delaminated · Dec 14, 2001 · N54SW · Boeing 7372H4 · Leading Edge Devices
  > FOUND LEFT WING NUMBER TWO SLAT IS DELAMINATED IN SEVERAL AREAS. (M)
- [SDR 2002F00200](https://openairdocs.org/sdr/2002F00200.md): Stringer Clip · dented · Dec 13, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > FOUND STRINGER CLIP DENTED AND GOUGED AT STATION 747 STRINGER 21L. (M)
- [SDR 2002F00198](https://openairdocs.org/sdr/2002F00198.md): Stringer Clip · dented · Dec 13, 2001 · N54SW · Boeing 7372H4 · Fuselage Miscellaneous Structure
  > FOUND STRINGER CLIP AT STATION 727B S22L IS DENTED. (M)
- [SDR 2002F00197](https://openairdocs.org/sdr/2002F00197.md): Frame · gouged · Dec 13, 2001 · N54SW · Boeing 7372H4 · Fuselage Main, Frame
  > FRAME HAS TWO GOUGES AT BS 747 BETWEEN STRINGER 23L AND STRINGER 22L. (M)
- [SDR 150070](https://openairdocs.org/sdr/150070.md): Skin · cracked · Dec 13, 2001 · N54SW · Boeing 7372H4 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN IS CRACKED AT STA 800 STRINGER 22 LT. CRACK IS 2.6 INCH IN LENGTH.
- [SDR 2002F00201](https://openairdocs.org/sdr/2002F00201.md): Duct · cracked · Dec 12, 2001 · N54SW · Boeing 7372H4 · Engine Bleed Air System
  > NR 1 ENGINE LEFT SIDE BLEED AIR DUCT ATTACH BRACKET CRACKED. (M)
- [SDR 2002F00275](https://openairdocs.org/sdr/2002F00275.md): Skin · gouged · Sep 24, 2001 · N54SW · Boeing 7372H4 · Fuselage Main, Plate/Skin
  > FOUND OUTER SKIN GOUGED ON EXISTING REPAIR AT STATION 380 AT STRINGER 24-25R. ACCOMPLISHED DOUBLER INSTALLATION AND REPAIR IAW 737 SRM 53-30-03 FIG NR 9. (M)
- [SDR 20010112SG052](https://openairdocs.org/sdr/20010112SG052.md): Battery Pack · discharged · Dec 5, 2000 · N54SW · Boeing 7372H4 · Emergency Lighting
  > FLT 2544 - ACY - AFT AISLE OVERHEAD BULLNOSE EMERGENCY EXIT LIGHTOUT. REMOVED AND REPLACED AFT AISLE OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT BATTERY POWER SUPPLY CARTRIDGE. SYSTEM TEST NORMAL. (M)
- [SDR 20000405AP005](https://openairdocs.org/sdr/20000405AP005.md): Battery Pack · inoperative · Feb 28, 2000 · N54SW · Boeing 7372H4 · Emergency Lighting
  > ACY - FORWARD BULLNOSE EMERGENCY LIGHT IN CABIN INOPERATIVE. TROUBLESHOT SYSTEM, REPLACED EMERGENCY LIGHT BATTERY PACK ASSEMBLY. (M)
- [SDR 2000ZZZM197](https://openairdocs.org/sdr/2000ZZZM197.md): Battery Pack · discharged · Feb 1, 2000 · N54SW · Boeing 7372H4 · Emergency Lighting
  > FLT 807 - ACY - FORWARD SECTION 'E PATH' LIGHTS INOPERATIVE. REPLACED FORWARD SECTION EMERGENCY LIGHT BATTERY PACK. (M)
- [SDR SWAA990806](https://openairdocs.org/sdr/SWAA990806.md): Cover · cracked · May 4, 1999 · N54SW · Boeing 7372H4 · Emergency Lighting
  > DURING SCHEDULED C2 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHTING COVER CRACKED NEXT TO SEAT ROW 11. REMOVED AND REPLACED COVER PER MM.

Next page: https://openairdocs.org/deregistered/N54SW-2013-08-21/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 = 'N54SW' AND deregistration_id = 'N54SW-2013-08-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N54SW-2013-08-21/reports

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