# Service difficulty reports: N274US, cancelled Sep 25, 2003

A list on [N274US, cancelled Sep 25, 2003](https://openairdocs.org/deregistered/N274US-2003-09-25.md).

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

- [SDR USAA990826](https://openairdocs.org/sdr/USAA990826.md): Skin · cracked · Aug 7, 1999 · N274US · Boeing 7372B7 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A.25 INCH CRACK ABOVE RIVET.125 INCH CRACK BELOW RIVET STRINGER 17R, WL STATION 344 SKIN. INSTALLED REPAIR DOUBLER PER SB 737-53-1083 FIG 3C. (M)
- [SDR USAASB99014](https://openairdocs.org/sdr/USAASB99014.md): Coalescer · dirty · Jan 15, 1999 · N274US · Boeing 7372B7 · Humidity Control System
  > FWA - FLT 1177 - EN ROUTE FROM BWI TO ORD AT FL310, ONE OF THE FLIGHT ATTENDANTS ADVISED THE COCKPIT CREW THAT THERE WERE FUMES IN THE CABIN AND THE FUMES WERE IRRITATING THE PASSENGERS. AN EMERGENCY DECLARED AND FLT DIVERT TO FWA. THE FUMES DISSIPATED ON DE
- [SDR USAA980523](https://openairdocs.org/sdr/USAA980523.md): Skin · cracked · Oct 15, 1998 · N274US · Boeing 7372B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND RON, FOUND 3 INCH CRACK IN SKIN AT STATION 767.5 INCH ABOVE STRINGER NR 20. INSTALLED DOUBLER PER SRM 53-30-03. (M)
- [SDR USAA980339](https://openairdocs.org/sdr/USAA980339.md): Skin · cracked · Aug 7, 1998 · N274US · Boeing 7372B7 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-5 CHECK EDDY CURRENT, FOUND A.125 INCH CRACK IN OUTER SKIN AT LOWER CORNER OF AFT ENTRY DOOR, LOWER HINGE CUTOUT STATION 950.5 2.5 INCHES BELOW STRINGER 14L. ROUTED OUT CRACK AND REFINISHED AREA PER SRM 53-00-1 PAGE 102. (M)
- [SDR USAA980338](https://openairdocs.org/sdr/USAA980338.md): Skin · cracked · Aug 7, 1998 · N274US · Boeing 7372B7 · Passenger/Crew Doors
  > TPA - DURING CX-5 CHECK EDDY CURRENT INSPECTION, FOUND A.5 INCH CRACK IN OUTER SKIN OF AFT ENTRY DOOR, LOWER AFT CORNER OF UPPER HINGE CUTOUT. ROUTED DAMAGE AND INSTALLED DOUBLER OF.071,2024-T3 PER SRM 52-10-01, 51-30-8 AND EA 62192. (M)
- [SDR USAA980337](https://openairdocs.org/sdr/USAA980337.md): Angle · cracked · Aug 7, 1998 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > TPA - DURING CX-5 VISUAL INSPECTION, FOUND A 1 INCH CRACK IN ANGLE AT STATION 727 COMPRESSION CHORD RBL 25. INSTALLED DOUBLER PER TYPICAL REPAIR NR 53-10-03A PART 3. (M)
- [SDR USAASB98200](https://openairdocs.org/sdr/USAASB98200.md): Light · inoperative · Jul 28, 1998 · N274US · Boeing 7372B7 · Emergency Lighting
  > PHL - WHILE TESTING EMERGENCY LIGHT SYSTEM, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 9A WITHOUT A LENSE AND SMOKING. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT ROW 9A. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB98111](https://openairdocs.org/sdr/USAASB98111.md): Battery Pack · discharged · May 11, 1998 · N274US · Boeing 7372B7 · Emergency Lighting
  > ALB - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN AT THE CENTER AISLE CEILING BETWEEN THE EXIT HATCHES INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)
- [SDR USAA960757](https://openairdocs.org/sdr/USAA960757.md): Skin · cracked · Nov 27, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Plate/Skin
  > ROA - DURING CX-3 CHECK, EDDY CURRENT INSPECTION FOUND.25 INCH CRACK IN A/C SKIN AT LOWER HINGE CUT OUT FORWARD ENTRY DOOR. BODY STA 302 - JUST ABOVE STR 13L. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-30-11. (X)
- [SDR USAASB96214](https://openairdocs.org/sdr/USAASB96214.md): Fuel Control · malfunctioned · Oct 21, 1996 · N274US · Boeing 7372B7 · Fuel Control/Turbine Engines
  > EVV - FL 777 - FLIGHT WAS CRUISING AT FL 310 WHEN THE NR 2 ENGINE CAME BACK TO 50 PERCENT POWER OR 2,000 LBS FUEL FLOW. CREW TURNED ON ENGINE HEAT WITH NO EFFECTS ON ENGINE. CREW TURNED ON FUEL HEAT, NR 2 ENGINE WENT PAST NORMAL N1 AND N2 INDICATIONS. CREW
- [SDR 96ZZZM1487](https://openairdocs.org/sdr/96ZZZM1487.md): Fuel Pump · malfunctioned · Oct 21, 1996 · N274US · Boeing 7372B7 · Engine Fuel Pump
  > EVV - FL 777 - FLIGHT WAS CRUISING AT FL 310 WHEN THE NR 2 ENGINE CAME BACK TO 50 PERCENT POWER OR 2,000 LBS FUEL FLOW. CREW TURNED ON ENGINE HEAT WITH NO EFFECTS ON ENGINE. CREW TURNED ON FUEL HEAT, NR 2 ENGINE WENT PAST NORMAL N1 AND N2 INDICATIONS. CREW
- [SDR USAASB96039](https://openairdocs.org/sdr/USAASB96039.md): Filter Bypass Sw · intermittent · Mar 2, 1996 · N274US · Boeing 7372B7 · Engine Oil Indicating System
  > FLT NR 797 - MCO - FIVE MINUTES AFTER TAKEOFF, 'OIL FILTER BYPASS' LIGHT FOR NR 1 ENGINE CAME ON. RETARDED THROTTLES, NO HELP. SHUT DOWN ENGINE AND RETURNED TO MCO. MAINTENANCE REPLACED THE FILTER BYPASS SWITCH. (M)
- [SDR USAA960240](https://openairdocs.org/sdr/USAA960240.md): Fitting · cracked · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND 1.5 INCH CRACK IN FORWARD INBOARD CHORD ANGLE BS 695 FITTING, WL 202, JUST ABOVE STRINGER 18A RIGHT. INSTALLED PERMANENT ANGLE REPAIR, LESS THAN 1 POUND. REPAIRED PER EA 40644. (M)
- [SDR USAA960239](https://openairdocs.org/sdr/USAA960239.md): Angle · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 4 INCH CORRODED WEB AFT ENTRY DOOR Z-ANGLE THRESHOLD WEB. FABRICATED NEW WEB, REPAIRED PER SRM 51-10-1 AND BOEING DRAWING 65-52878. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)
- [SDR USAA960238](https://openairdocs.org/sdr/USAA960238.md): Angle · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 24 INCH CORROSION Z-ANGLE AFT ENTRY DOOR. REPLACED WITH IDENTICAL PART NR 65-52878-533, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA960237](https://openairdocs.org/sdr/USAA960237.md): Floor Beam · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND.5 INCH BY 1 INCH CORRODED NUT PLATE HOLES 3 FLOOR BEAM, STATION 986.5 RBL 36, LBL 5, RBL 5. INSTALLED DOUBLERS, REPAIR PER SRM 53-10-9 FIG 7. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA960236](https://openairdocs.org/sdr/USAA960236.md): Angle · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH CORROSION FLOOR SUPPORT ANGLE AT STATIO N967 TO 947 RBL 20. REPAIRED PER SRM 51-10-1. REPLACED WITH IDENTICAL PART NR 65-46812. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)
- [SDR USAA960235](https://openairdocs.org/sdr/USAA960235.md): Floor Beam · gouged · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND GOUGE APPROXIMATELY 22 INCHES FLOOR BEAM BS 312, LBL 12 INCHES TO RBL 10 INCHES. CUT OUT DAMAGED AREA AND INSTALLED NEW SECTION WITH REPAIR ANGLES. REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02, CORRO
- [SDR USAA960234](https://openairdocs.org/sdr/USAA960234.md): Stringer · corroded · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 8 INCH CORRODED AREA ON SIDE OF STRINGER BS 351.2 - BS 380, STRINGER 28L. REPLACED STRINGER SECTION REPAIRED PER SRM 51-10-1, PAGE 5, STEP 4. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)
- [SDR USAA960233](https://openairdocs.org/sdr/USAA960233.md): Floor Beam · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA FLOOR BEAM UPPER T-CAP BS 1016 LBL 3 INCHES. INSTALLED T-CAP, REPAIR PLUS 2.6 LB WT CHANGE, REPAIRED PER SRM 53-10-9. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA960232](https://openairdocs.org/sdr/USAA960232.md): Seat Track · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage, Seat/Cargo Attach Fittings
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION FLOOR SEAT TRACK BETWEEN STATION 1016 AND STATION 986.5. INSTALLED NEW SEAT TRACK SECTION, REPAIRED PER SRM 51-10-3. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA960231](https://openairdocs.org/sdr/USAA960231.md): Floor Support · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION 8 INCH FLOOR SUPPORT INTERCOSTAL STATION 986.5 LNL 15 INCHES. REPLACED WITH IDENTICAL PART NR 65-46812-191, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.
- [SDR USAA960230](https://openairdocs.org/sdr/USAA960230.md): Floor Beam · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION FLOOR BEAM STATION 1006, LBL 11 INCHES. SPLICED IN NEW SECTION OF FLOOR BEAM, REPAIRED PER SRM 53-10-9. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA960229](https://openairdocs.org/sdr/USAA960229.md): Intercostal · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORROSION INTERCOSTAL STATION 1006 - 986.5 '0' BL. REPLACED WITH INDENTICAL PART NR 65-46812-170, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA960228](https://openairdocs.org/sdr/USAA960228.md): Intercostal · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHCK VISUAL INSPECTION, FOUND TWO CORRODED AREAS APPROXIMATELY 1 INCH BY 1 INCH, INTERCOSTAL LBL 10 INCHES BETWEEN BS 328 AND BS 344. REPLACED WITH IDENTICAL PART NR 65-45834-259, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORRO
- [SDR USAA960227](https://openairdocs.org/sdr/USAA960227.md): Intercostal · corroded · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND.5 INCH BY 2 INCH CORRODED AREA INTERCOSTAL LBL 11 INCHES BETWEEN BS 312 AND BS 328. REPLACED WITH IDENTICAL PART NR 65-45834-260, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA960226](https://openairdocs.org/sdr/USAA960226.md): Intercostal · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND THREE CORRODED AREAS, APPROXIMATELY 1 INCH BY 1 INCH AT INTERCOSTAL, RBL 10 INCH BETWEEN BS 312 AND BS 328. REPLACED WITH IDENTICAL PART NR 1137215, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORRO
- [SDR USAA960225](https://openairdocs.org/sdr/USAA960225.md): Floor Beam · corroded · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA FLOOR BEAM 'T' CAP CABIN BS 294.5 LBL 10 INCHES, RBL 20. CUT AND REPLACED T-CAP, LESS THAN 1 LB WEIGHT CHANGE, REPAIRED PER TR 53-10-04B. CORROSION TASK NR C53-107-02, CORROSION L
- [SDR USAA960224](https://openairdocs.org/sdr/USAA960224.md): Intercostal · corroded · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 CORRODED AREAS APPROXIMATELY 2 INCHES BY 2 INCHES INTERCOSTAL, BS 297 AND BS 303 LBL 12. INSTALLED NEW INTERCOSTAL, REPAIRED PER SRM 51-10-1. (M)
- [SDR USAA960223](https://openairdocs.org/sdr/USAA960223.md): Intercostal · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA 4 PLACES INTERCOSTAL, BS 344 TO BS 360 RBL 11. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA960222](https://openairdocs.org/sdr/USAA960222.md): Intercostal · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH CORRODED AREA AT INTERCOSTAL BS 292 LBL 12 INCHES. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA960221](https://openairdocs.org/sdr/USAA960221.md): Intercostal · corroded · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 CORRODED AREAS APPROXIMATELY 1 INCH BY 1 INCH ON INTERCOSTAL, RBL 10 INCHES BETWEEN BS 294.5 AND BS 312. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1 AND BOEING DRAWING 65-45834. CORROSION TASK NR C53-107-0
- [SDR USAA960220](https://openairdocs.org/sdr/USAA960220.md): Angle · corroded · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS AT CLIP NUT HOLES 'Z' ANGLE BS 294.5 TO BS 344 RBL 56. REPAIRED PER SRM 51-10-1 AND BOEING DRAWING 65-45875. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA960219](https://openairdocs.org/sdr/USAA960219.md): Angle · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 6 CORRODED AREAS AT CLIP NUT HOLES APPROXIMATELY 1 INCH BY 1 INCH BS 306 TO BS 345 LBL 48 'A' ANGLE LEFT ENTRANCE DOOR. REMOVED AND INSTALLED NEW PART, REPAIRED PER SRM 51-10-1 PAGE 5. CORROSION TASK NR C53-107
- [SDR USAA960218](https://openairdocs.org/sdr/USAA960218.md): Intercostal · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND FOUR 1 INCH BY 1 INCH CORRODED AREAS AT CLIP NUT HOLES BS 312 TO BS 328 RBL 11 INTERCOSTAL. REMOVED AND INSTALLED NEW INTERCOSTAL, REPAIRED PER SRM 51-10-1 PAGE 5. CORROSION TASK NR C53-107-02, CORROSION LEVEL
- [SDR USAA960217](https://openairdocs.org/sdr/USAA960217.md): Blkhd Fitting · cracked · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Bulkhead
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND.5 INCH CRACK STATION 727 BULKHEAD STIFFENER FITTING AT BL 0 WL 202.5. REMOVED CRACKED FITTING, INSTALLED NEW ONE, REPAIRED PER EO 5394G176. (M)
- [SDR USAA960216](https://openairdocs.org/sdr/USAA960216.md): Frame · cracked · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Frame
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND.5 INCH CRACK TOP FLANGE OF FRAME STATION 807 LEFT BETWEEN STRINGER 24 AND STRINGER 25. CUT OUT CRACK, FABRICATED FILLER AND REPAIRED DOUBLER PER SRM 51-40-3. (M)
- [SDR USAA960213](https://openairdocs.org/sdr/USAA960213.md): Angle · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORRODED FLOOR SUPPORT ANGLE STATION 986.5 TO 967 LBL 12. REPLACED ANGLE, REPAIRED PER SRM 51-10-1. CORROSION TASK NR 53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA960212](https://openairdocs.org/sdr/USAA960212.md): Angle · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH FLOOR SUPPORT ANGLE CORROSION STATION 967 TO 947 RBL 6. REPAIRED PER SRM 51-10-1. REPLACED WITH IDENTICAL PART NR 65C10592-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA960211](https://openairdocs.org/sdr/USAA960211.md): Floor Beam · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 45 INCH CORROSION FLOOR BEAM STATION 967 BL 0 TO LBL 45. INSTALLED ONE DUOBLER AT LBL 42, REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA960210](https://openairdocs.org/sdr/USAA960210.md): Angle · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 11 INCH BY 40 INCH CORROSION FLOOR SUPPORT ANGLE AT STATION 957 RBL 6 TO RBL 45. REPAIRED PER SRM 51-10-1. REPLACED WITH IDENTICAL PART NR 65-C10592-5 OR 6. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA960209](https://openairdocs.org/sdr/USAA960209.md): Angle · cracked · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL EDDY CURRENT INSPECTION, FOUND 1 INCH CRACK IN FORWARD INBOARD CHORD ANGLE BS 695 FITTING, WL 202, JUST ABOVE STRINGER 18A LEFT. INSTALLED PERMANENT ANGLE REPAIR, LESS THAN 1 LB, REPAIRED PER EA 40644. (M)
- [SDR USAA960208](https://openairdocs.org/sdr/USAA960208.md): Floor Beam · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 6 INCH BY 2 INCH CORRODED FLOOR BEAM AREA AND AT ALL CLIPNUT HOLES BS 328 RBL 6 TO RBL 56. INSTALLED NEW T-CAP AND DOUBLERS, REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA960207](https://openairdocs.org/sdr/USAA960207.md): Angle · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH CORROSION FLOOR SUPPORT ANGLE, STATION 967 TO STATION 947 RBL 45, REPAIRED PER SRM 51-10-1. REPLACED WITH IDENTICAL PART NR 65C10592-4. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA960206](https://openairdocs.org/sdr/USAA960206.md): Angle · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH CORROSION AT FLOOR BEAM SUPPORT ANGLE STATION 967 TO 947 LBL 12. REPLACED WITH IDENTICAL PART NR 65-46812-170 AND ANGLE, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL
- [SDR USAA960205](https://openairdocs.org/sdr/USAA960205.md): Floor Beam · corrosion · Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 45 INCHES CORROSION STATION 967 BL 0 TO RBL 45 FLOOR BEAM. CUTOFF TOP CAP, FABRICATED AND REPAIRED SPLICE AND INSTALLED PER SRM 53-10-9 FIG 2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (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 = 'N274US' AND deregistration_id = 'N274US-2003-09-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N274US-2003-09-25/reports

---
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