# Service difficulty reports: N54340, cancelled Jan 30, 2013

A list on [N54340, cancelled Jan 30, 2013](https://openairdocs.org/deregistered/N54340-2013-01-30.md).

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

- [SDR TWAA0009201](https://openairdocs.org/sdr/TWAA0009201.md): Battery Pack · inoperative · Jun 12, 2000 · N54340 · Boeing 727231 · Emergency Lighting
  > THE RT FWD AND LT FWD EMERGENCY SLIDE LIGHTS WERE INOPERATIVE, AND THE AFT SECTION OF EGRESS LIGHTS WERE VERY DIM. CLEANED DIRTY PINS AT THE BATTERY PACK FOR THE SLIDE LIGHTS, AND CLEANED AND DRIED THE EGRESS LIGHT STRIP AND CONNECTIONS. CHECK-C 9-7-99 MCI.
- [SDR TWAA0008104](https://openairdocs.org/sdr/TWAA0008104.md): Engine · stalled · May 22, 2000 · N54340 · Boeing 727231 · Engine (Turbine/Turboprop)
  > DURING TAKEOFF HAD AN APPARENT ENGINE STALL. RAN ALL ENGINES, CHECKED ALL ENGINE BLEEDS, INTAKED, AND EXHAUSTS AND FOUND NO ABNORMALITIES. CC02 09-07-99 MCI.
- [SDR TWAA0007002](https://openairdocs.org/sdr/TWAA0007002.md): Skin · damaged · May 4, 2000 · N54340 · Boeing 727231 · Fuselage Main, Plate/Skin
  > FOUND SEVERAL POPPED RIVETS AND THE FUSELAGE SKIN CRACKED IN 2 AREAS. ONE CRACK WAS.375 INCH AND THE SECOND WAS.3125 INCH, WITH CORROSION AT LAP SEAM STA 490, STRINGER 18. REPAIRED FUSELAGE LAP SEAM SPLICE PER 727 SRM 53-30-3, FIG 5 SHEET 5. CHECK-C 9-7-
- [SDR TWAA0001004](https://openairdocs.org/sdr/TWAA0001004.md): Skin · punctured · Jan 6, 2000 · N54340 · Boeing 727231 · Fuselage Main, Plate/Skin
  > THE LT FUSELAGE HAD PUNCTURE HOLE 21 INCHES BELOW CAPTAIN SLIDING WINDOW. REPAIRED PER SRM 53-30-3, FIG 13 SHEET 3. CHECK-C 9-7-99 MCI.
- [SDR TWAA0001003](https://openairdocs.org/sdr/TWAA0001003.md): Skin · punctured · Jan 4, 2000 · N54340 · Boeing 727231 · Fuselage Main, Plate/Skin
  > GROUND DAMAGE CAUSED A PUNCTURE HOLE AND DENT AT APPROX STA 229, LT OF AIRCRAFT 21 IN BELOW WINDOW. REPAIRED PER SRM 53-30-03, PAGE 28 FIG 7, AND ENGINEERING. CHECK-C 9-7-99 MCI.
- [SDR TWAA9901104](https://openairdocs.org/sdr/TWAA9901104.md): Battery Pack · discharged · Jan 18, 1999 · N54340 · Boeing 727231 · Emergency Lighting
  > THE FORWARD LEFT AND FORWARD RT CABIN DOOR SLIDE LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 9-3-98 MCI.
- [SDR TWAA9901102](https://openairdocs.org/sdr/TWAA9901102.md): Light · inop · Jan 18, 1999 · N54340 · Boeing 727231 · Emergency Lighting
  > THE EGRESS LIGHT STRIP WAS INOPERATIVE IN THE FORWARD CABIN LEFT SIDE. REPLACED THE LIGHT STRIP. CHECK-C 9-3-98 MCI.
- [SDR TWAA9901103](https://openairdocs.org/sdr/TWAA9901103.md): Fuel Pump · failed · Jan 17, 1999 · N54340 · Boeing 727231 · Engine Fuel Pump
  > ABORTED TAKEOFF WHEN THE NUMBER 3 ENGINE SHUT ITSELF DOWN DURING TAKEOFF ROLL. FOUND THE FUEL PUMP SHAFT SHEARED. REPLACED THE FUEL CONTROL, (P/N 743602-5) AND THE ENGINE FUEL PUMP. CHECK-C 9-3-98 MCI.
- [SDR TWAA9814302](https://openairdocs.org/sdr/TWAA9814302.md): Gasket · leaking · Sep 4, 1998 · N54340 · Boeing 727231 · Airfoil Anti/De-ice System
  > NR 1 STRUT OVERHEAT ILLUMINATED IN FLIGHT. EXTINGUISHED WHEN NR 1 BLEED SELECTED CLOSED. FLIGHT RETURNED TO STL. REPLACED 2 EA 13TH STAGE WING ANTI-ICE VALVE GASKETS. CHECK-C 8-23-98 MCI.
- [SDR TWAA9813202](https://openairdocs.org/sdr/TWAA9813202.md): Power Supply · inoperative · Aug 18, 1998 · N54340 · Boeing 727231 · Emergency Lighting
  > EMERGENCY LIGHTS BATTERY CHARGER CIRCUIT BREAKER WAS POPPING. REPLACED BATTERY POWER SUPPLY. CHECK-C 9-5-97.
- [SDR TWAA9813201](https://openairdocs.org/sdr/TWAA9813201.md): Circuit Breaker · tripped · Aug 17, 1998 · N54340 · Boeing 727231 · Emergency Lighting
  > THE EMERGENCY LIGHTS BATTERY CHARGER POPPED CIRCUIT BREAKER. CHECKED BATTERY CHARGER AND WIRING, NO PROBLEM FOUND. REPLACED 115V C/B. CHECK-C 9-5-97 MCI.
- [SDR TWAA9805101](https://openairdocs.org/sdr/TWAA9805101.md): Overheat Loop · out of position · Apr 3, 1998 · N54340 · Boeing 727231 · Overheat Detection
  > STL - FLT 5039 - ON TAKEOFF, THE LOWER AFT BODY OVERHEAT LIGHT CAME ON. SWITCHED BLEED SOURCES BUT LIGHT INTERMITTENT. REPOSITIONED LOOP PER MM 26-1401 AND REPLACED LAMP ASY FOR AFT BODY OVERHEAT. OP 17 MAINTENANCE CHECK 9-15-97. (M)
- [SDR TWAA9800601](https://openairdocs.org/sdr/TWAA9800601.md): Bypass Light · illuminated · Jan 15, 1998 · N54340 · Boeing 727231 · Engine Oil Indicating System
  > DCA - FLT 439 - DURING CRUISE, NR 2 ENGINE FILTER BYPASS ANNUNCIATOR ILLUMINATED. SHUTDOWN THE ENGINE. PLACARDED AS PER MEDP 79-2. (M)
- [SDR TWAA9711711](https://openairdocs.org/sdr/TWAA9711711.md): Stringer · cracked · Sep 30, 1997 · N54340 · Boeing 727231 · Wing, Longeron/Stringer
  > MCI - INSTALLED DOUBLER DUE TO CRACK AT RIGHT WING STATION 656.5 NR 1 STRINGER FROM REAR SPAR UPPER STRINGER TO RIB. (M)
- [SDR TWAA9711710](https://openairdocs.org/sdr/TWAA9711710.md): Skin · corroded · Sep 30, 1997 · N54340 · Boeing 727231 · Fuselage Main, Plate/Skin
  > MCI - REMOVED CORROSION AND REPAIRED SKIN AT STATION 530 ABOVE STRINGER 27R. (M)
- [SDR TWAA9804304](https://openairdocs.org/sdr/TWAA9804304.md): Casting · corroded · Sep 5, 1997 · N54340 · Boeing 727231 · Main Landing Gear Attach Section
  > MCI - DURING OP 17 MAINTENANCE CHECK, THE RT LANDING GEAR AFT DRAG BRACE MOUNT CASTING HAD DEEP PITTING CORROSION BETWEEN BUSHINGS. REPLACED DRAG BRACE MOUNT CASTING PER SRM 51-10-1 AND TWA STD PRACTICES. (M)
- [SDR TWAA9804006](https://openairdocs.org/sdr/TWAA9804006.md): Rib · cracked · Sep 5, 1997 · N54340 · Boeing 727231 · Wing, Rib/Bulkhead
  > MCI - DURING OP17 MAINTENANCE CHECK, THE LEFT WING WS 738.5 RIB CHORD WAS CRACKED ON LOWER CHORD AT STRINGER 6 AND 8, IN THE RADIUS. INSTALLED NEW RIB PER SRM 51-10-1 AND 51-30-2. (M)
- [SDR TWAA9804005](https://openairdocs.org/sdr/TWAA9804005.md): Splice · cracked · Sep 5, 1997 · N54340 · Boeing 727231 · Fuselage Miscellaneous Structure
  > MCI - DURING OP 17 MAINTENANCE CHECK, A CABIN STRINGER SPLICE WAS CRACKED AT STATION 440 STRIGNER 19R. REPLACED STRINGER SPLICE PER SRM 53-10-3 AND INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M)
- [SDR TWAA9803815](https://openairdocs.org/sdr/TWAA9803815.md): Stringer · cracked · Aug 25, 1997 · N54340 · Boeing 727231 · Fuselage Main, Longeron/Stringer
  > MCI - DURING C-CHECK MAINTENANCE, CRACKS WERE INDICATED AT THE TWO FORWARD HOELS AT BS 760L STRINGER 18 IND IS AT 6 AND 12 O'CLOCK POS IN HOLES. REPAIRED PER SERVICE BULLETING 727-57-0112 AND ARA 11403. (M)
- [SDR TWAA9803813](https://openairdocs.org/sdr/TWAA9803813.md): Stringer · cracked · Aug 16, 1997 · N54340 · Boeing 727231 · Fuselage Main, Longeron/Stringer
  > MCI - DURING OP 17 MAINTENANCE CHECK, THERE WAS A CRACK INDICATION AT THE TWO FORWARD HOLES STATION 760 STRINGER 18, BOTH 6 AND 12 O'CLOCK POSITION. REPAIRED PER ARA 11406 AND SB 727-57-0112. (M)
- [SDR TWAA9803812](https://openairdocs.org/sdr/TWAA9803812.md): Former · cracked · Aug 16, 1997 · N54340 · Boeing 727231 · Fuselage Miscellaneous Structure
  > MCI - DURING OP 17 MAINTENANCE CHECK, A CRACK WAS FOUND ON THE RT SIDE FS 760 FORMER 3,.5 INCH UP FROM CENTER TANK. REPAIRED PER ARA 11406, SB 727-53-0197. (M)
- [SDR TWAA9615701](https://openairdocs.org/sdr/TWAA9615701.md): Trunnion · lack of lube · Dec 17, 1996 · N54340 · Boeing 727231 · Main Landing Gear Attach Section
  > MIA - FLT 5 - DURING APPROACH WHEN LANDING GEAR WS EXTENDED, THE NOSE LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. CYCLED LANDING GEAR. FOUND NOSE LANDING GEAR TRUNNIONS DRY. LUBRICATED NOSE LANDING GEAR. LANDING GEAR OPERATION AND INDICATION THEN CHECKE
- [SDR 96ZZZM1471](https://openairdocs.org/sdr/96ZZZM1471.md): Fuel Heat Vlv · sticking · Sep 16, 1996 · N54340 · Boeing 727231 · Engine Anti-Icing System
  > STL - DURING CRUISE SHUT DOWN NR 3 ENGINE, S/N 3954, DUE TO HIGH OIL TEMPERATURE. FOUND FUEL HEAT VALVE, MFG P/N 155212-1M, STICKING IN THE OPEN POSITION. REPLACED FUEL HEAT VALVE. ENGINE OPERATION THEN CHECKED NORMAL.
- [SDR 95ZZZW218](https://openairdocs.org/sdr/95ZZZW218.md): Skin · cracked · Feb 10, 1995 · N54340 · Boeing 727231 · Cargo/Baggage Doors
  > MCI - DURING C-CHECK, FOUND A ONE INCH CRACK IN EXTERIOR SKIN AT TOP AFT CORNER OF FORWARD ENTRY DOOR. CUT OUT CRACKED AND DAMAGED AREA, REPAIRED PER SRM 5-30-03. TOTAL CYCLES 33,173.

## 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 = 'N54340' AND deregistration_id = 'N54340-2013-01-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N54340-2013-01-30/reports

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