# Service difficulty reports: N241US, cancelled Nov 23, 2005

A list on [N241US, cancelled Nov 23, 2005](https://openairdocs.org/deregistered/N241US-2005-11-23.md).

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

- [SDR USAASB01118](https://openairdocs.org/sdr/USAASB01118.md): Power Supply · inoperative · Apr 28, 2001 · N241US · Boeing 737201 · Emergency Lighting
  > BWI - DURING WEEKLY CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 7 ABC THROUGH15 ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPS CHECK GOOD. (M)
- [SDR USAASB01079](https://openairdocs.org/sdr/USAASB01079.md): Battery Pack · discharged · Mar 16, 2001 · N241US · Boeing 737201 · Emergency Lighting
  > BWI - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT THE EMERGENCY EXIT. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK NORMAL. (M)
- [SDR USAASB01078](https://openairdocs.org/sdr/USAASB01078.md): Battery Pack · discharged · Mar 15, 2001 · N241US · Boeing 737201 · Emergency Lighting
  > BDL - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTS FROM ROWS 10 TO 14 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)
- [SDR USAA010266](https://openairdocs.org/sdr/USAA010266.md): Skin · cracked · Feb 26, 2001 · N241US · Boeing 737201 · Fuselage Main, Plate/Skin
  > TPA - FOUND SKIN CRACKED 1 INCH, EQUIPMENT COOLING EXHAUST STATION 380 STRINGER 28L. INSTALLED.100 2024 T3 CLAD DOUBLER IAW TYPICAL REPAIR 53-30-04. (M)
- [SDR USAASB00217](https://openairdocs.org/sdr/USAASB00217.md): Light · failed · Aug 14, 2000 · N241US · Boeing 737201 · Emergency Lighting
  > BWI - MAINTENANCE FOUND THE PORTABLE FORWARD EMERGENCY LIGHT INSIDE THE FLIGHT COMPARTMENT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY. OPS CHECK NORMAL. (M)
- [SDR USAA000889](https://openairdocs.org/sdr/USAA000889.md): Skin · cracked · Jun 28, 2000 · N241US · Boeing 737201 · Fuselage Main, Plate/Skin
  > BOS - FOUND SKIN CRACKED 1.75 INCH, STATION 767 ON STRINGER 18R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6 PAGE 11-12B, SHTS 1-4. (M)
- [SDR USAASB99166](https://openairdocs.org/sdr/USAASB99166.md): Uplock Sensor · failed · Jul 7, 1999 · N241US · Boeing 737201 · Landing Gear Position and Warning
  > BOS - FLT 2673 - AFTER TAKEOFF, WHEN LANDING GEAR WAS RETRACTED, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AND STAYED ON. CAPT RECYCLED THE GEAR BUT THE LIGHT REMAINED ILLUMINATED. FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT FURTHER INCIDEN
- [SDR USAASB99026](https://openairdocs.org/sdr/USAASB99026.md): Accessory Unit · failed · Feb 1, 1999 · N241US · Boeing 737201 · Landing Gear Position and Warning
  > TPA - FLT2675 - ON APPROACH INTO TPA, ALL THREE LANDING GEAR RED UNSAFE LIGHTS ILLUMINATED. CREW EXECUTED A MISSED APPROACH. CREW RECYCLED LANDING GEAR TWICE AND ALL THREE RED AND GREEN GEAR LIGHTS REMAINED ILLUMINATED. ON THIRD LANDING GEAR RECYCLE ATTEMPT
- [SDR USAA980406](https://openairdocs.org/sdr/USAA980406.md): Skin · cracked · Sep 17, 1998 · N241US · Boeing 737201 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-4 CHECK VISUAL VERIFIED BY EDDY CURRENT INSPECTION, FOUND A 1.1250 INCH CRACK IN L/E SKIN RT WING AT WS 491. INSTALLED DOUBLER OF 204 T-3.040 INCH PER SRM 57-30-4 FIG 1. (X)
- [SDR USAASB98220](https://openairdocs.org/sdr/USAASB98220.md): Battery Pack · discharged · Aug 23, 1998 · N241US · Boeing 737201 · Emergency Lighting
  > ALB - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN OVER THE FORWARD PASSENGER ENTRY DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB98107](https://openairdocs.org/sdr/USAASB98107.md): N2 Gearbox · failed · May 5, 1998 · N241US · Boeing 737201 · Turbine Engine Accessory Drive
  > BWI - FLT 2400 - CREW DECLARED AN EMERGENCY AND SHUT DOWN THE NR 1 ENGINE IN FLT DUE TO LOSS OF OIL QTY AND PRESSURE AND TEMPERATURE INDICATIONS. FLT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT TAXIED TO THE GATE NORMALLY. TOTAL S
- [SDR USAASB98101](https://openairdocs.org/sdr/USAASB98101.md): Accessory Unit · failed · Apr 18, 1998 · N241US · Boeing 737201 · Landing Gear Position and Warning
  > BUF - FL475 - UPON LOWERING LANDING GEAR TO LAND AT BUF, CREW RECEIVED 3 GREEN LIGHTS AND 3 RED LIGHTS FOR THE GEAR. CREW RECYCLED GEAR 3 TIMES WHEREAS THE THIRD ATTEMPT, A NORMAL GEAR INDICATION WAS RECEIVED. THE CREW THEN ACCOMPLISHED A FLYBY AND THE TOWER
- [SDR USAASB98011](https://openairdocs.org/sdr/USAASB98011.md): Switch · out of adjust · Jan 13, 1998 · N241US · Boeing 737201 · Landing Gear Selector
  > BWI - FLT 254 - WHEN LANDING GEAR WAS EXTENDED, CREW RECEIVED 3 GREEN LIGHTS AND 3 RED LIGHTS. GEAR WAS CYCLED AND NORMAL GEAR INDICATION WAS RECEIVED, 3 GREEN LIGHTS AND NO RED LIGHTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED GEAR HANDL
- [SDR USAASB97330](https://openairdocs.org/sdr/USAASB97330.md): Battery Pack · discharged · Nov 29, 1997 · N241US · Boeing 737201 · Emergency Lighting
  > ORD - MAINTENANCE FOUND THE FORWARD AND AFT EMERGENCY ESCAPE SLIDE LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT EMERGENCY ESCAPE SLIDE LIGHT BATTERY PACKS. OPS CHECK GOOD. (M)
- [SDR USAASB97316](https://openairdocs.org/sdr/USAASB97316.md): Battery Pack · discharged · Nov 18, 1997 · N241US · Boeing 737201 · Emergency Lighting
  > CLT - MAINTENANCE FOUND THE FORWARD EMERGENCY ESCAPE SLIDE LIGHTS AND EXIT IDENTIFIERS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE FORWARD CARGO COMPT. OPS CHECK GOOD. (M)
- [SDR USAASB97310](https://openairdocs.org/sdr/USAASB97310.md): Selector · lack of lube · Nov 11, 1997 · N241US · Boeing 737201 · Landing Gear Selector
  > PHL - FL1901 - AFTER EXTENDING LANDING GEAR ON APPROACH, CREW RECEIVED THREE GREEN GEAR LIGHTS PLUS THREE RED GEAR UNSAFE LIGHTS WHICH STAYED ILLUMINATED. RECYCLED GEAR AND RECEIVED NORMAL GEAR INDICATION. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE
- [SDR USAA970318](https://openairdocs.org/sdr/USAA970318.md): Stringer · cracked · Oct 16, 1997 · N241US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH CRACKS BS 767 STRINGER 16L. INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3 FIG 1. (M)
- [SDR USAA970317](https://openairdocs.org/sdr/USAA970317.md): Skin · cracked · Oct 16, 1997 · N241US · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK.75 INCH LONG SKIN STATION 727A ABOVE STRINGER 16R. INSTALLED DOUBLER AND FILLER, REPAIRED PER SRM 53-30-3. (M)
- [SDR USAA970316](https://openairdocs.org/sdr/USAA970316.md): Stringer · corroded · Oct 16, 1997 · N241US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 8 INCH STATION 360 TO 380 STRINGER 28. INSTALLED REPAIR SECTION AND REPAIRED PER SRM 53-10-3. (M)
- [SDR USAA970315](https://openairdocs.org/sdr/USAA970315.md): Door Frame · cracked · Oct 16, 1997 · N241US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK.5 INCH CRACK LONG STATION 947 JUST FORWARD OF SERVICE DOOR FRAME STRINGER 10R. INSTALLED REPAIR STRAP AND REPAIRED PER TR 53-30-7. (M)
- [SDR USAA970314](https://openairdocs.org/sdr/USAA970314.md): Chord · corroded · Oct 16, 1997 · N241US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 9 INCH CORRODED AREA APPROX.5 INCH WIDE AT BS 1016 BL 0 CHORD. CUTOUT CORRODED SECTION AND SPLICED IN FABRICATED REPAIR. REPAIRED PER SRM 51-40-3 AND BOEING DRW 65-46568. CORROSION TASK NR C53-208-01, CORROSI
- [SDR USAA970300](https://openairdocs.org/sdr/USAA970300.md): Frame · cracked · Oct 16, 1997 · N241US · Boeing 737201 · Fuselage Main, Frame
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH LONG CRACK STA 360 FRAME ABOVE STRINGER 20 R. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 51-40-3. (M)
- [SDR USAA970234](https://openairdocs.org/sdr/USAA970234.md): Skin · cracked · Jul 15, 1997 · N241US · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING CX-1 CHECK, FOUND.5 INCH CRACK ON FUSELAGE SKIN AT AFT ENTRY CUT OUT, LOWER HINGE CUT OUT. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIGURE 34. (M)
- [SDR USAASB97160](https://openairdocs.org/sdr/USAASB97160.md): Oil Temp Bulb · failed · Jun 15, 1997 · N241US · Boeing 737201 · Engine Oil Temperature
  > BWI - FLT 951 - CLIMBING OUT ORF THROUGH FL180, THE NR 1 ENGINE OIL TEMP STARTED TO CLIMB INTO RED RADIAL. THE CAPT SHUT DOWN THE NR 1 ENG IN FLT AND DIVERTED TO BWI. AN EMERGENCY WAS DECLARED. THE FLT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE.
- [SDR USAASB97004](https://openairdocs.org/sdr/USAASB97004.md): Transmitter · failed · Jan 3, 1997 · N241US · Boeing 737201 · Engine Oil Pressure
  > BWI - FLT 570 - INBOUND TO BWI, THE NR 2 ENGINE OIL PRESSURE INDICATOR DROPPED TO 27 PSI, WHICH IS IN THE RED RANGE. CREW GOT NO OIL LIGHT AND THE OIL PRESSURE LIGHT WOULD NOT PRESS TO TEST. CREW SHUT DOWN THE NR 2 ENGINE AND DECLARED AN EMERGENCY. FLIGHT L
- [SDR USAASB96212](https://openairdocs.org/sdr/USAASB96212.md): Tr Unit · failed · Oct 20, 1996 · N241US · Boeing 737201 · DC Rectifier/Converter
  > ITH - FLT 2075 - CLIMBING THROUGH 12,000 FT, THE CABIN PRESS WARNING HORN SOUNDED. DESCENDED TO 10,000 FT AND WENT TO STANDBY. CHECKED FOR C/B'S POPPED AND FOUND THE E/E COOLING FAN C/B POPPED. SWITCHED TO ALTERNATE FAN AT WHICH TIME FLT ATTENDANTS REPORTED
- [SDR USAASB96205](https://openairdocs.org/sdr/USAASB96205.md): Controller · failed · Oct 3, 1996 · N241US · Boeing 737201 · Cabin Pressure Controller
  > CLT - FL 8026 - CAPTAIN ADVISED HE LOST AUTO AND STANDBY PRESSURIZATION. MANUAL PRESSURIZATION WAS OK. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER. OPS CHECK GOOD. (M)
- [SDR USAASB96194](https://openairdocs.org/sdr/USAASB96194.md): Engine · bird strike · Sep 14, 1996 · N241US · Boeing 737201 · Engine (Turbine/Turboprop)
  > BOS - FL 1153 - DURING TAKEOFF ROLL, THE AIRCRAFT INJESTED A LARGE SEAGULL INTO THE NR 2 ENGINE. CREW AND DISPATCH ELECTED TO DIVERT TO BOS AS A PRECAUTIONARY MEASURE. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PER
- [SDR USAASB96141](https://openairdocs.org/sdr/USAASB96141.md): Hyd Hose · loose · Jul 28, 1996 · N241US · Boeing 737201 · Hydraulic System, Main
  > PVD - FL 381 - SHORTLY AFTER TAKEOFF FROM BOS, A STRONG UNIDENTIFIABLE SMELL OCCURRED IN THE CABIN. THE SMELL TAPERED OFF DURING CLIMB-OUT, BUT CAME BACK VERY STRONG WHEN LEVELING AT FL 310. FLIGHT DIVERTED TO PVD. NO EMERGENCY WAS DECLARED AND THE FLIGHT L
- [SDR USAASB96118](https://openairdocs.org/sdr/USAASB96118.md): Oil Filter Studs · pulled out · Jun 27, 1996 · N241US · Boeing 737201 · Turbine Engine Oil System
  > CLE - FLT 273 - FLYING AT 27,000 FEET, THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. CREW SHUT DOWN NR 2 ENGINE AND DECLARED AN EMERGENCY. FLIGHT DIVERTED TO CLE AND LANDED WITH NO FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 10 MINUTES. MAINTENANC
- [SDR USAA951337](https://openairdocs.org/sdr/USAA951337.md): Skin · cracked · Dec 6, 1995 · N241US · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING 'CX-6' CHECK VISUAL INSPECTION, FOUND.25 INCH LONG CRACK FORWARD ENTRY DOOR UPPER HINGE CUTOUT, STATION 303.37 STRINGER 10-L, IN FUSELAGE SKIN. REMOVED DAMAGE AND INSTALLED DOUBLER. REPAIRED PER SRM 53-30-3, FIG 21 DETAIL 1. (M)
- [SDR USAA950615](https://openairdocs.org/sdr/USAA950615.md): Switch · failed · Jun 19, 1995 · N241US · Boeing 737201 · Engine Oil Indicating System
  > BWI - FLT 2190 - FLIGHT EN RUOTE ORD TO PHL, WHEN NR 2 ENGINE FILTER BYPASS LIGHT CAME ON AND NR 2 ENGINE SHUTDOWN. FLIGHT DIVERTED TO BWI WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED OIL FILTER BYPASS SWITCH AND ENGINE OIL FILTER. (M)
- [SDR USAA950193](https://openairdocs.org/sdr/USAA950193.md): Battery Pack · inoperative · Feb 28, 1995 · N241US · Boeing 737201 · Emergency Lighting
  > LGA - EMERGENCY EXIT LIGHTS FLASHING ROWS 8 THROUGH 15. MAINTENANCE REPLACED BATTERY PACK AT POWER SUPPLY ON SEAT 11A. (X)

## 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 = 'N241US' AND deregistration_id = 'N241US-2005-11-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N241US-2005-11-23/reports

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