# Service difficulty reports: N226US, cancelled Mar 13, 2001

A list on [N226US, cancelled Mar 13, 2001](https://openairdocs.org/deregistered/N226US-2001-03-13.md).

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

- [SDR 99ZZZX2744](https://openairdocs.org/sdr/99ZZZX2744.md): Seat Track · corroded · Jun 30, 1999 · N226US · Boeing 737201 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK RT OUTBOARD STA 344 - STA 380.
- [SDR USAASB99129](https://openairdocs.org/sdr/USAASB99129.md): Battery Pack · discharged · May 24, 1999 · N226US · Boeing 737201 · Emergency Lighting
  > GSO - MAINTENANCE FOUND THE AISLE SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A WIRE SPLICE AND TWO BATTERY PACKS. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB99103](https://openairdocs.org/sdr/USAASB99103.md): Battery Pack · discharged · Apr 19, 1999 · N226US · Boeing 737201 · Emergency Lighting
  > BOS - PILOT REPORTED THAT THE AFT BATTERY PACK UNDER SEAT 16 LEFT NEEDS REPLACED DUE TO THE EMERGENCY LIGHTS ILLUMINATING DIM. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT SEAT 16, LEFT SIDE. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB99102](https://openairdocs.org/sdr/USAASB99102.md): Battery Pack · discharged · Apr 17, 1999 · N226US · Boeing 737201 · Emergency Lighting
  > EWR - MAINTENANCE FOUND SEVERAL CABIN SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS AT SEATS 5A AND 16A AND RERACKED REMAINING BATTERY PACKS. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA990311](https://openairdocs.org/sdr/USAA990311.md): Doubler · cracked · Apr 13, 1999 · N226US · Boeing 737201 · Passenger/Crew Doors
  > TPA - DURING HFEC CHECK INSPECTION, FOUND A.25 INCH CRACK IN MED REPAIR DOUBLER AFT LOWER CORNER OF MAIN ENTRY DOOR CUTOUT. INSTALLED NEW DOUBLER PER EO 5391G694 AND DRAWING 65C27257. (M)
- [SDR USAASB99101](https://openairdocs.org/sdr/USAASB99101.md): Battery Pack · discharged · Apr 11, 1999 · N226US · Boeing 737201 · Emergency Lighting
  > TPA - MAINTENANCE FOUND THE LEFT AND RIGHT EXTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT BATTERY PACKS IN THE AFT CARGO COMPARTMENT. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB99076](https://openairdocs.org/sdr/USAASB99076.md): Hose · ruptured · Mar 20, 1999 · N226US · Boeing 737201 · Hydraulic System, Main
  > CLT - FLT 462 - ON CLIMB-OUT OF JAX, F/O NOTICED NR 2 ENG HYD PUMP LOW PRESSURE LIGHT ILLUMINATED. ACCOMP QUICK REF HANDBOOK PROCEDURES. APPROX 1 MIN LATE, THE NR 1 ENG LOW PRESSURE LIGHT CAME ON AND SYSTEM HYD PRESSURE WENT TO 0. FLIGHT DIVERTED TO CLT AND
- [SDR USAASB98241](https://openairdocs.org/sdr/USAASB98241.md): Sensor · out of adjust · Sep 13, 1998 · N226US · Boeing 737201 · Door Warning System
  > ATL - FLT 496 - AFTER TAKEOFF AT APPROXIMATELY 500 FT, THE FORWARD CARGO DOOR WARNING LIGHT ILLUMINATED. FLIGHT RETURNED TO FIELD AT ATL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FORWARD CARGO DOOR SENSOR OUT OF A
- [SDR USAA980160](https://openairdocs.org/sdr/USAA980160.md): Skin · cracked · Apr 12, 1998 · N226US · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING C-5 CHECK, FOUND 2 INCH CRACK AT STA 740, S17R FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER PER EA 51596. (X)
- [SDR USAA980159](https://openairdocs.org/sdr/USAA980159.md): Skin · cracked · Apr 12, 1998 · N226US · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING C-5 CHECK, FOUND 1 INCH CRACK IN FUSELAGE SKIN AT LOWER HINGE CUTOUT OF AFT SERVICE DOOR. REMOVED CRACK AND INSTALLED DOUBLER PER EA 61580. (M)
- [SDR USAASB98014](https://openairdocs.org/sdr/USAASB98014.md): B-Nut · loose · Jan 17, 1998 · N226US · Boeing 737201 · Hydraulic System, Main
  > SAV - FLT 1481 - AT FL 310, THE 'A' SYSTEM HYDRAULIC QTY SLOWLY DROPPED TO 1.2 GALLONS. CAPTAIN NOTICED THE QTY HAD BEEN SLOWLY DROPPING OVER THE LAST HOUR. THE, 'B' SYSTEM HYDRAULIC SYSTEM LOW QTY LIGHT ILLUMINATED. CAPTAIN DECLARED AN EMERGENCY AND THE FL
- [SDR USAASB98004](https://openairdocs.org/sdr/USAASB98004.md): Separator Bags · dirty · Jan 6, 1998 · N226US · Boeing 737201 · Humidity Control System
  > CLT - FLT 776 - CLIMBING THROUGH 4,000 FEET, CREW SMELLED A SMOKY ODOR THAT RESEMBLED A BURNING CANDLE SMELL IN THE COCKPIT. ODOR WAS ALSO PRESENT IN THE CABIN. NO INDICATION OF SMOKE WAS PRESENT THROUGHOUT THE AIRCRAFT INCLUDING THE GALLEYS AND COCKPIT. AN
- [SDR USAASB97336](https://openairdocs.org/sdr/USAASB97336.md): Battery Pack · discharged · Dec 7, 1997 · N226US · Boeing 737201 · Emergency Lighting
  > ATL - MAINTENANCE FOUND THE INTERIOR AND EXTERIOR EMERGENCY LIGHTS AT THE FORWARD ENTRY AND SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE FORWARD BATTERY PACK. OPS CHECK GOOD. (M)
- [SDR USAASB97335](https://openairdocs.org/sdr/USAASB97335.md): Power Supply · failed · Dec 2, 1997 · N226US · Boeing 737201 · Emergency Lighting
  > MCO - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTING AT ROWS 1 THROUGH 5, LEFT SIDE, INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AT SEAT ROW 5. OPS CHECK GOOD. (M)
- [SDR USAA970215](https://openairdocs.org/sdr/USAA970215.md): Skin · cracked · May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK IN SKIN AT LOWER FORWARD CORNER OF DOOR CUTOUT AFT ENTRY DOOR BS 964. INSTALLED EXT SKIN REPAIR AND REPAIRED PER EA 42446. (M)
- [SDR USAA970214](https://openairdocs.org/sdr/USAA970214.md): Skin · dented · May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND DENTS 2.5 INCH BY 3 INCH AND 1.5 INCH BY 1.5 INCH STATION 807 BETWEEN STRINGER 19L AND 20L SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)
- [SDR USAA970213](https://openairdocs.org/sdr/USAA970213.md): Frame · cracked · May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, Frame
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND.5 INCH CRACK FORWARD CARGO FRAME BS 500 BL '0'. INSTALLED DOUBLER AND FILLER, REPAIRED PER SRM 51-40-3 FIG 1. (M)
- [SDR USAA970212](https://openairdocs.org/sdr/USAA970212.md): Beam · cracked · May 24, 1997 · N226US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BL '0' BL 660 WL 208 BEAM. INSTALLED REPAIR ANGLES, REPAIRED PER BOEING DRAWING NR 65C34537. (M)
- [SDR USAA970211](https://openairdocs.org/sdr/USAA970211.md): Skin · cracked · May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-2 CHECK CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 380 BETWEEN STRINGER 28L AND BL '0' SKIN. INSTALLED DOUBLER DOUBLER, REPAIRED PER TR 53-30-04. (M)
- [SDR USAA970210](https://openairdocs.org/sdr/USAA970210.md): Stringer · corroded · May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORRODED AREA AFT CARGO BS 907 STRINGER 26R. INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3 FIG 1 SRM 53-10-4 FIG 10. CORROSION TASK NR C53-208-01, CORROSION LEVEL 1. (M)
- [SDR USAA970209](https://openairdocs.org/sdr/USAA970209.md): Stringer · corroded · May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA BS 907, STRINGER 24L. INSTALLED STRINGER SPLICE, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)
- [SDR USAA970208](https://openairdocs.org/sdr/USAA970208.md): Skin · corrosion · May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 4 INCHES APPROX BS 927 BETWEEN STRINGER 24L AND 25L SKIN. INSTALLED FILLER AND DOUBLER, REPAIRED PER SRM 53-30-3. CORROSION TASK NR 53-208-01, CORROSION LEVEL 2. (M)
- [SDR USAA970207](https://openairdocs.org/sdr/USAA970207.md): Frame · corroded · May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, Frame
  > INT - DURING Q2-CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA AFT CARGO LOWER LEG OF FRAME BS 767 STRINGER 26R-25R. INSTALLED FRAME REPAIR CONSISTING OF SHEAR TIE, FILLER SUPPORT ANGLE AND RADIUS FILLER, REPAIRED PER SRM 53-10-4 FIG 6. CORROS
- [SDR USAA970206](https://openairdocs.org/sdr/USAA970206.md): Skin · cracked · May 24, 1997 · N226US · Boeing 737201 · Passenger/Crew Doors
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 3 INCH BY.25 INCH CRACK FORWARD LOWER CORNER AFT ENTRY DOOR SKIN. INSTALLED DOUBLER AND TRIPLER, REPAIRED PER EA 42446. (M)
- [SDR USAA970205](https://openairdocs.org/sdr/USAA970205.md): Stringer · corrosion · May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 12 INCHES STATION 962, STRINGER 27L. INSTALLED DOUBLER (SPLICE), REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)
- [SDR USAASB97094](https://openairdocs.org/sdr/USAASB97094.md): Garlock Seal · failed · Apr 4, 1997 · N226US · Boeing 737201 · Turbine Engine Accessory Drive
  > BWI - FLT 1243 - FLIGHT HAD JUST LEVELED OFF AT 28,000 FEET WHEN CREW NOTICED THE NR 1 ENGINE OIL QUANTITY BEGAN TO DECREASE TOWARDS ZERO. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND NO ENGINE SHUT-DOWN OCCURRED
- [SDR USAA960609](https://openairdocs.org/sdr/USAA960609.md): Skin · cracked · Sep 13, 1996 · N226US · Boeing 737201 · Galley Doors
  > ROA - DURING 'CX-3' CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND.125 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER. REPAIRED PER TYPICAL REPAIR 53-10-19 REV A. (M)
- [SDR USAASB96181](https://openairdocs.org/sdr/USAASB96181.md): Air Distr · odor · Sep 6, 1996 · N226US · Boeing 737201 · Air Distribution System
  > PIT - FL 553 - FLIGHT ATTENDANTS ADVISED COCKPIT CREW THAT THEY SMELLED SMOKE OR FUMES IN THE REAR OF THE AIRCRAFT. THEY DID NOT DETECT ANY SIGHT OF SMOKE. CAPTAIN COULD NOT ISOLATE PROBLEM AND ELECTED TO DECLARE AN EMERGENCY AS A PRECAUTIONARY MEASURE AND D
- [SDR USAASB96124](https://openairdocs.org/sdr/USAASB96124.md): Flow Control Vlv · failed · Jul 9, 1996 · N226US · Boeing 737201 · Cabin Pressure Control System
  > MSP - FLT 824 - ON CLIMB-OUT ABOVE 15,000 FEET, A LOUD RUMBLING NOISE BEGAN. CREW DECIDED TO RETURN TO FIELD AT MSP. ALL AIRCRAFT INDICATORS WERE NORMAL. CREW SWITCHED EQUIPMENT COOLING FAN TO ALTERNATE, THEN GASPER FAN TO OFF, NO HELP. NOSE EVENTUALLY DIM
- [SDR USAA951331](https://openairdocs.org/sdr/USAA951331.md): Stringer · corroded · Dec 15, 1995 · N226US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > ROA - DURING 'CX-2' CHECK VISUAL INSPECTION, FOUND 2 INCH CORRODED STRINGER CAUSED BY LAVATORY SPILL, STRINGER 27L AT BS 947. REMOVED CORRODED STRINGER SECTION AND SPLICED IN NEW SECTION. REPAIRED PER SRM 53-10-3 FIG 1. (M)

## 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 = 'N226US' AND deregistration_id = 'N226US-2001-03-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N226US-2001-03-13/reports

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