# Service difficulty reports: N272AU, cancelled Aug 22, 2003

A list on [N272AU, cancelled Aug 22, 2003](https://openairdocs.org/deregistered/N272AU-2003-08-22.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 2 · 73 reports

- [SDR USAASB01174](https://openairdocs.org/sdr/USAASB01174.md): Charger · failed · Jun 15, 2001 · N272AU · Boeing 7372B7 · Emergency Lighting
  > BWI - MAINTENANCE FOUND THE AFT OVERHEAD EMERGENCY LIGHT BETWEEN ROW 19 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 9008-3-5A) AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)
- [SDR USAASB01154](https://openairdocs.org/sdr/USAASB01154.md): Fuse · blown · Jun 2, 2001 · N272AU · Boeing 7372B7 · Emergency Lighting
  > TPA - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE FORWARD ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND THE FUSE IN THE POWER SUPPLY BLOWN. REMOVED AND REPLACED FUSE. OPS CHECK GOOD. (M)
- [SDR USAASB99170](https://openairdocs.org/sdr/USAASB99170.md): Epr Transmitter · failed · Jul 13, 1999 · N272AU · Boeing 7372B7 · Engine Pressure Ratio (EPR)
  > CLE - FLT 8027 - APPROXIMATELY 7 MINUTES AFTER TAKEOFF, CREW ENCOUNTERED PROBLEMS WITH THE NR 2 ENGINE EPR AND THE AUTOTHROTTLE DISCONNECTING. WITH FUEL FLOW AT 5.3, NR 1 ENGINE EPR WAS AT 1.78 AND THE NR 2 ENGINE AT 1.41. WHEN AUTOTHROTTLE WAS RE-ENGAGED, T
- [SDR USAASB99126](https://openairdocs.org/sdr/USAASB99126.md): Switch · failed · May 16, 1999 · N272AU · Boeing 7372B7 · Emergency Lighting
  > BWI - MAINTENANCE FOUND THE CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROL SWITCH IN THE COCKPIT. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA990438](https://openairdocs.org/sdr/USAA990438.md): Skin · cracked · May 7, 1999 · N272AU · Boeing 7372B7 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-2 CHECK, FOUND.375 INCH LONG SKIN CRACK, LEFT FUSELAGE, 2 INCH AFT OF BS 727B AT LOWER EDGE OF STRINGER 18L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. DOUBLER MADE OF 2024T3 -.063 PER BOEING SRM 53-30-3 FIG 1. (M)
- [SDR USAA990135](https://openairdocs.org/sdr/USAA990135.md): Gusset · cracked · Feb 18, 1999 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > CLT - DURING DROP IN VISUAL INSPECTION, FOUND A 1 INCH CRACK IN UPPER RADIUS OF GUSSET AT TOP OF N/G WELL. REPAIRED PER SRM 51-10-1. (M)
- [SDR USAASB99025](https://openairdocs.org/sdr/USAASB99025.md): Connector · shorted · Jan 31, 1999 · N272AU · Boeing 7372B7 · Fire Detection
  > BOS - FLT 1241 - DURING CLIMB-OUT FROM BOS AT FL 200, THE CREW RECEIVED A NR 2 ENGINE FIRE WARNING LIGHT AND HORN. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND IMMEDIATELY SHUT DOWN THE NR 2 ENGINE AND FIRE BOTH FIRE EXTINGUISHING BOTTLES. AN EM
- [SDR USAA980193](https://openairdocs.org/sdr/USAA980193.md): Skin · cracked · May 12, 1998 · N272AU · Boeing 7372B7 · Fuselage Main, Plate/Skin
  > ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND.375 INCH CRACK IN SKIN FORWARD SIDE OF LOWER HINGE CUTOUT AT FORWARD ENTRY DOOR. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 31. (M)
- [SDR USAA980192](https://openairdocs.org/sdr/USAA980192.md): Skin · scratch · May 12, 1998 · N272AU · Boeing 7372B7 · Fuselage Main, Plate/Skin
  > ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 3 INCH SCRATCH APPROX.025 INCH DEEP IN CROWN SKIN STATON 687, STRINGER 1L. BURNISHED AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)
- [SDR USAASB97340](https://openairdocs.org/sdr/USAASB97340.md): Pitot Probe · malfunctioned · Dec 17, 1997 · N272AU · Boeing 7372B7 · Pitot/Static System
  > CLT - FLT 8026 - FLIGHT DIVERTED TO CLT DUE TO A 10 KNOT DIFFERENCE BETWEEN CAPTAINS AND FIRST OFFICERS AIRSPEED INDICATORS. INDICATED AIRSPEED APPEARS TO BE 10 KNOTS HIGHER ON FIRST OFFICERS SIDE BETWEEN 70-150 KNOTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT.
- [SDR 98ZZZM111](https://openairdocs.org/sdr/98ZZZM111.md): Adc · malfunctioned · Dec 17, 1997 · N272AU · Boeing 7372B7 · Air Data Computer
  > CLT - FLT 8026 - FLIGHT DIVERTED TO CLT DUE TO A 10 KNOT DIFFERENCE BETWEEN CAPTAINS AND FIRST OFFICERS AIRSPEED INDICATORS. INDICATED AIRSPEED APPEARS TO BE 10 KNOTS HIGHER ON FIRST OFFICERS SIDE BETWEEN 70-150 KNOTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT.
- [SDR USAASB97088](https://openairdocs.org/sdr/USAASB97088.md): Anti-Ice Tube · failed · Mar 22, 1997 · N272AU · Boeing 7372B7 · Engine Anti-Icing System
  > CLT - FL 775 - ON CLIMB-OUT FROM CLT, AT 10,000 FEET, THE NR 1 ENGINE OVERHEAT ILLUMINATED. CAPTAIN ACCOMPLISHED ENGINE OVERHEAT CHECKLIST. WHEN THRUST WAS REDUCED, LIGHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO
- [SDR USAASB97049](https://openairdocs.org/sdr/USAASB97049.md): Battery Pack · discharged · Feb 16, 1997 · N272AU · Boeing 7372B7 · Emergency Lighting
  > CLE - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN INOP AT THE CENTER CABIN CEILING. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)
- [SDR USAASB96263](https://openairdocs.org/sdr/USAASB96263.md): Detection Loop · failed · Dec 17, 1996 · N272AU · Boeing 7372B7 · Overheat Detection
  > PIT - FLT 1212 - FLIGHT DIVERTED TO PIT DUE TO A RIGHT WING BODY OVERHEAT LIGHT. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE STRUT CAVITY OVERHEAT DETECTION LOOP. RAN ENGINE. A
- [SDR USAA951372](https://openairdocs.org/sdr/USAA951372.md): Intercostal · corrosion · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1.5 INCH BY 1 INCH, BY STATION 947 TO STATION 967, RBL 45 INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA951317](https://openairdocs.org/sdr/USAA951317.md): Seat Track · corroded · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage, Seat/Cargo Attach Fittings
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.25 INCH BY 3 INCH CORRODED AREA BS 986.5 RBL 24. REPLACED SEAT TRACK, WT CHANGE LESS THAN 1 LB. REPAIRED PER SRM 51-10-1 AND SRM 53-10-5. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)
- [SDR USAA951316](https://openairdocs.org/sdr/USAA951316.md): Floor Beam · cracked · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.25 INCH CRACK LBL 25 LONGITUDINAL FLOOR BEAM WEB (LOWER) STATION 707, WL 203. INSTALLED WEB REPAIR (WT.3 LBS), REPAIRED PER SRM 51-40-2. (M)
- [SDR USAA951315](https://openairdocs.org/sdr/USAA951315.md): Floor Beam · cracked · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.5 INCH CRACK BL 0 STATION 708 AND BS 710. INSTALLED WEB REPAIR, REPAIRED PER DWG 65C34537. (M)
- [SDR USAA951314](https://openairdocs.org/sdr/USAA951314.md): Skin · gouged · Dec 6, 1995 · N272AU · Boeing 7372B7 · Cargo/Baggage Doors
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH GOUGE IN OUTER SKIN OF AFT CARGO DOOR TOP AFT CORNER OF DOOR (6 INCH BY 6 INCH DOUBLER). INSTALLED EXT SKIN DOUBLER, REPAIRED PER SRM 52-00-3. (M)
- [SDR USAA951313](https://openairdocs.org/sdr/USAA951313.md): Fitting · cracked · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.25 INCH CRACK, BL 0 LONGITUDINAL FLOOR BEAM SUPPORT FITTING FORWARD RADIUS, STATION 727, WL 202.5. INSTALLED REINFORCING ANGLES, RADIUS FILLERS, SHIMS AND SEALED. REPAIRED PER EO 5394G176. (M)
- [SDR USAA951312](https://openairdocs.org/sdr/USAA951312.md): Angle · crack · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK RIGHT WING TO BODY SUPPORT ANGLE BS 540-522. REPLACED ANGLE, LESS THAN 1 LB WEIGHT CHANGE, REPAIR PER EA 25375 AND SRM 51-40-3. (M)
- [SDR USAA951311](https://openairdocs.org/sdr/USAA951311.md): Stringer · crack · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.5 INCH CRACK S-16R, BETWEEN STATION 500B AND 520, ON STRINGER. INSTALLED STRINGER REPAIR, REPAIRED PER EO 5393X228. (M)
- [SDR USAA951310](https://openairdocs.org/sdr/USAA951310.md): Stringer · cracked · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.5 INCH CRACK STRINGER 16 L, BETWEEN STATION 500B AND STATION 520, ON STRINGER. INSTALLED STRINGER REPAIR, REPAIRED PER EO 5393X228. (M)
- [SDR USAA951309](https://openairdocs.org/sdr/USAA951309.md): Hinge · cracked · Dec 6, 1995 · N272AU · Boeing 7372B7 · Service Doors
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT AFT END OF HINGE, FRONT CABIN SERVICE DOOR LOWER GATE HINGE. REPLACED HINGE, REPAIR PER EA 40350. (M)
- [SDR USAA951308](https://openairdocs.org/sdr/USAA951308.md): Stringer · gouged · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.5 INCH GOUGE IN STRINGER OUTBOARD 'J' SECTION, STATION 1044 STRINGER 27L. INSTALLED REPAIR DOUBLER UNDER 'J' LEG OF STRINGER, AFTER SMOOTHING GOUGE. REPAIRED PER SRM 53-10-3 FIG 1. (M)
- [SDR USAA951307](https://openairdocs.org/sdr/USAA951307.md): Skin · damaged · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Plate/Skin
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION (PREVIOUS REPAIR NOT PER SRM), FOUND UNKNOWN DAMAGED DOUBLER, 8 INCHES BY 9.50 INCHES, BS 227 TO BS 235, S19R TO S20R. INSTALLED DOUBLER PER SRM, REPAIRED PER SRM 53-30-3. (X)
- [SDR USAA951306](https://openairdocs.org/sdr/USAA951306.md): Floor Beam · cracked · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH LONG CRACK IN UPPER RADIUS OF BEAM CAP, STA 520, FLOOR BEAM RBL 25. INSTALLED FLOOR BEAM REPAIR,.8 POUNDS AT BS 520, REPAIRED PER SB 737-53-1120, EA 40385. (X)
- [SDR USAA951305](https://openairdocs.org/sdr/USAA951305.md): Stringer · gouged · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Longeron/Stringer
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND DEEP GOUGE.25 INCH BY 2 INCHES IN UPPER INBOARD LEG OF S26L, BS 1044. INSTALLED STR REPAIR, LESS THAN 1 POUND ADDED, REPAIRED PER SRM 53-10-3, FIGURE 1. (X)
- [SDR USAA951304](https://openairdocs.org/sdr/USAA951304.md): Angle · cracked · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1.50 INCH CRACK, BS 727, RBL 24.5 ON ANGLE. INSTALLED REPAIR ANGLE, REPAIRED PER EA 40453. (X)
- [SDR USAA951303](https://openairdocs.org/sdr/USAA951303.md): Attach Angle · cracked · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND.25 INCH CRACK, STA 639, STUB BEAM ATTACH ANGLE, RBL 45, WL 207. REPLACED ATTACH ANGLE, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-1. (X)
- [SDR USAA951302](https://openairdocs.org/sdr/USAA951302.md): Frame · cracked · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Frame
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND.75 INCH CRACK, STA 616, RIGHT FRAME INBOARD CHORD, FIRST FASTENER ABOVE CENTER WING SKIN. INSTALLED FILLER ANGLE, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER EA 40391. (X)
- [SDR USAA951301](https://openairdocs.org/sdr/USAA951301.md): Frame · cracked · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Frame
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND.75 INCH CRACK, STA 616, LT FRAME INBOARD CHORD, FIRST FASTENER ABOVE CENTER WING SKIN. INSTALLED FILLER AND ANGLE, WEIGHT CHANGE LESS THAN 1 POUND. REPAIRED PER EA 40391. (X)
- [SDR USAA951300](https://openairdocs.org/sdr/USAA951300.md): Support · cracked · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND.50 INCH CRACK, SEAT TRACK SUPPORT CHANNEL, STA 520, LBL 45, WL 207.5. INSTALLED FLOOR BEAM REPAIR, REPAIRED PER SB 737-53-1120, EA 40385,.8 POUNDS AT BS 520. (X)
- [SDR USAA951298](https://openairdocs.org/sdr/USAA951298.md): Floor Beam · cracked · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK, RBL 24.5, STA 675, IN FLOOR BEAM. CRACK CONTAINED AT AILERON QUADRANT CUT-OUT. INSTALLED REPAIR CHANNEL AMD DOUBLERS, AND RADIUS FILLERS AS REQUIRED PER CO 5791G632 AND EA 40396. (X)
- [SDR USAA951297](https://openairdocs.org/sdr/USAA951297.md): Floor Beam · cracked · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK, LBL 24.5, STA 675, IN FLOOR BEAM. CRACK CONTAINED BY FASTENER HOLE AND CUT-OUT INSTALL REPAIR CHANNEL, DOUBLERS, AND RADIUS FILLER AS REQUIRED BY EO 5791G632 AND EA 40396. (X)
- [SDR USAA951296](https://openairdocs.org/sdr/USAA951296.md): Skin · cracked · Dec 6, 1995 · N272AU · Boeing 7372B7 · Passenger/Crew Doors
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND.25 INCH LONG CRACK IN OUTER SKIN AT UPPER HINGE CUT-OUT AT ENTRY DOOR. INSTALLED EXTERIOR SKIN REPAIR. REPAIRED PER EA 40360. (X)
- [SDR USAA951295](https://openairdocs.org/sdr/USAA951295.md): Doubler · damaged · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 5 INCH SLOT IN BEAR STRAP - DOUBLER PREVIOUSLY INSTALLED, BUT NOT PER SRM BS 794 AT S23R. REMOVED PREVIOUSLY INSTALLED DOUBLER AND INSTALLED REPAIR PER EA. (X)
- [SDR USAA951293](https://openairdocs.org/sdr/USAA951293.md): Seat Track · corrosion · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage, Seat/Cargo Attach Fittings
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 3.50 INCH BY 1 INCH AND 2 INCHES BY 1 INCH, BS 990 AND BS 1015 AT RBL 8 INCHES ON SEAT TRACK. REPLACED TRACK, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSIO
- [SDR USAA951292](https://openairdocs.org/sdr/USAA951292.md): Intercostal · corrosion · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES, STA 328 TO 340, LBL 12 INCHES ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-10. CORROSION LEVEL 2. (X)
- [SDR USAA951290](https://openairdocs.org/sdr/USAA951290.md): Floor Beam · corrosion · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 2 INCHES, STA 312 RBL 35 INCHES ON FLOOR BEAM. REPLACED T-CAP FROM LBL 6 TO RBL 36, REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)
- [SDR USAA951289](https://openairdocs.org/sdr/USAA951289.md): Floor Beam · corrosion · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND.75 INCH BY.50 INCH CORRODED AREA FLOOR BEAM BS 1016, LBL 15. REMOVED CORROSION AND INSTALLED REPAIR STRAP, REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)
- [SDR USAA951288](https://openairdocs.org/sdr/USAA951288.md): Intercostal · corrosion · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 1 INCH, STA 986.5 TO 1006 BL ZERO ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)
- [SDR USAA951287](https://openairdocs.org/sdr/USAA951287.md): Intercostal · corrosion · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND CORROSION 1.50 INCHES BY 1 INCH, STA 947 TO STA 967, RBL 45 ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)
- [SDR USAA951286](https://openairdocs.org/sdr/USAA951286.md): Floor Beam · corrosion · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA AROUND NUTPLATE HOLES.25 INCH BY.25 INCH, BS 967 LBL 4, RBL 5, RBL 18 RBL 26, RBL 47, ON FLOOR BEAM. INSTALLED TEE SECTION ANGLES AND STRAPS. REPAIRED PER TR 53-10-05 C. CORROSION TASK NR C53-1
- [SDR USAA951285](https://openairdocs.org/sdr/USAA951285.md): Stringer · corrosion · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 12 INCH BY 1 INCH AT S-26 R, BS 974 TO BS 986 ON STRINGER. SPLICED NEW STRINGER SECTION IN, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)
- [SDR USAA951284](https://openairdocs.org/sdr/USAA951284.md): Stringer · corrosion · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 5 INCH BY 1 INCH S-25 L BS 968 ON STRINGER. INSTALLED DOUBLER WEIGHT CHANGE LESS THAN 1 LB. REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)
- [SDR USAA951283](https://openairdocs.org/sdr/USAA951283.md): Stringer · corroded · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 6 INCH BY 1 INCH S-27 L, BS 1004 TO BS 1010 ON STRINGER. SPLICED IN NEW STRINGER SECTION WEIGHT CHANGE LESS THAN 1 LB. REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (
- [SDR USAA951282](https://openairdocs.org/sdr/USAA951282.md): Angle · corrosion · Dec 6, 1995 · N272AU · Boeing 7372B7 · Passenger/Crew Doors
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 24 INCH FORWARD ENTRY DOOR TRANSITION ANGLE. INSTALLED FILLER AND DOUBLER, REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M)
- [SDR USAA951281](https://openairdocs.org/sdr/USAA951281.md): Intercostal · corrosion · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION, 1 INCH BY 3 INCHES, STA 312 TO STA 328, LBL 12 INCHES, ON INTERCOSTAL. REPLACED INTERCOSTAL, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-01. CORROSION LEVE
- [SDR USAA951280](https://openairdocs.org/sdr/USAA951280.md): Floor Beam · corrosion · Dec 6, 1995 · N272AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION, 2 INCHES BY 4 INCHES, STA 344, BL ZERO TO LBL 8 INCHES, ON FLOOR BEAM. CUT OUT FLOOR BEAM SECTION, FABRICATED NEW T-CAP, AND REPAIRED DOUBLERS AND INSTALLED PER TR 53-10-13. CORROSION TASK NR C53-1

Next page: https://openairdocs.org/deregistered/N272AU-2003-08-22/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 = 'N272AU' AND deregistration_id = 'N272AU-2003-08-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N272AU-2003-08-22/reports

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