# Service difficulty reports: N282AU, cancelled Sep 10, 2002 A list on [N282AU, cancelled Sep 10, 2002](https://openairdocs.org/deregistered/N282AU-2002-09-10.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 · 56 reports - [SDR USAASB01322](https://openairdocs.org/sdr/USAASB01322.md): Battery · discharged · Nov 22, 2001 · N282AU · Boeing 7372B7 · Emergency Lighting > TPA - THE EMERGENCY EXIT LIGHT ABOVE THE FORWARD ENTRY DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAASB01312](https://openairdocs.org/sdr/USAASB01312.md): Battery · discharged · Nov 15, 2001 · N282AU · Boeing 7372B7 · Emergency Lighting > LGA - MAINTENANCE FOUND THE FORWARD SERVICE DOOR AND FORWARD ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES. OPERATIONAL CHECK GOOD. (M) - [SDR USAA010780](https://openairdocs.org/sdr/USAA010780.md): Splice · corroded · Jul 2, 2001 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND STRINGER SPLICE CORRODED 1 INCH BY 4 INCHES, BS 986.5, STRINGER 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53-10-3 FIG 1. (M) - [SDR USAA010797](https://openairdocs.org/sdr/USAA010797.md): Support Fitting · corroded · Jun 12, 2001 · N282AU · Boeing 7372B7 · Nose/Tail Landing Gear Attach Section > PIT - FOUND SUPPORT FITTING CORRODED.020 INCH -.010 INCH, NOSE GEAR RIGHT TRUNNION SUPPORT FITTING BORE. REAMED BORE, INSTALLED SLEEVE PER EA 71444. (M) - [SDR USAASB00296](https://openairdocs.org/sdr/USAASB00296.md): Duct · cracked · Oct 18, 2000 · N282AU · Boeing 7372B7 · Engine Anti-Icing System > TPA-LGA - FLT 2676 - AFTER TAKEOFF, THE RIGHT ENGINE START VALVE LIGHT AND THE RIGHT ENGINE OVERHEAT LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. 15 MINUTES SINGLE ENGINE TIME. MAINTENANCE F - [SDR USAASB00284](https://openairdocs.org/sdr/USAASB00284.md): Actuator · leaking · Oct 3, 2000 · N282AU · Boeing 7372B7 · Drag Control Actuator > EWR - FLT 2636 - EN ROUTE FROM PBI TO LGA, CAPTAIN NOTICED THAT SYSTEM A HYDRAULIC QUANTITY HAD DECREASED FROM 2.2 GALLONS TO 1.2 GALLONS. ON DESCENT TO LGA, AS AIRCRAFT SLOWED AND FLAPS WERE EXTENDED, HYDRAULIC QUANTITY WENT TO.5 GALLONS. CREW WAS ABLE TO - [SDR USAA001316](https://openairdocs.org/sdr/USAA001316.md): Stringer · cracked · Aug 24, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Longeron/Stringer > CLT - FOUND SHELF CRACKED.5 INCH, STRINGER 18A RIGHT, BS 727 SHELF. REPLACED WITH NEW SHELF PER SRM 51-10-02. (M) - [SDR USAA001318](https://openairdocs.org/sdr/USAA001318.md): Pressure Panel · cracked · Aug 24, 2000 · N282AU · Boeing 7372B7 · Fuselage Floor Panel > CLT - FOUND PRESSURE DECK WEB CRACKED.5 INCH, STATION 670, RBL 12. INSTALLED FILLER AND DOUBLER PER EA 67747. (M) - [SDR USAA001317](https://openairdocs.org/sdr/USAA001317.md): Stringer · cracked · Aug 24, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Longeron/Stringer > CLT - FOUND SHELF CRACKED.5 INCH, STRINGER 18A LEFT, BS 727 SHELF. REPLACED WITH NEW SHELF PER SRM 51-10-1. (M) - [SDR USAA001299](https://openairdocs.org/sdr/USAA001299.md): Clevis · corroded · Aug 22, 2000 · N282AU · Boeing 7372B7 · Vertical Stabilizer > CLT - FOUND CLEVIS CORRODED.008 INCH BY.008 INCH, VERT FIN, AFT SPAR, AFT OUTBOARD CLEVIS RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M) - [SDR USAA001298](https://openairdocs.org/sdr/USAA001298.md): Clevis · corroded · Aug 22, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - FOUND CLEVIS CORRODED.008 INCH BY.008 INCH, VERT FIN, FWD SPAR, FRONT CLEVIS, RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M) - [SDR USAA001297](https://openairdocs.org/sdr/USAA001297.md): Clevis · corroded · Aug 22, 2000 · N282AU · Boeing 7372B7 · Vertical Stabilizer > CLT - FOUND CLEVIS CORRODED.008 INCH BY.008 INCH, VERT FIN, FWD SPAR, AFT CLEVIS RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M) - [SDR USAA001296](https://openairdocs.org/sdr/USAA001296.md): Clevis · corroded · Aug 22, 2000 · N282AU · Boeing 7372B7 · Vertical Stabilizer > CLT - FOUND AFT SPAR CLEVIS CORRODED.013 INCH BY.028 INCH, VERT FIN, AFT SAPR, AFT OUTBOARD CLEVIS, RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M) - [SDR USAA001281](https://openairdocs.org/sdr/USAA001281.md): Skin · cracked · Aug 17, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - FOUND SKIN CRACKED.250 INCH, AFT SERVICE DOOR LOWER HINGE. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-03 AND EA 67849. (M) - [SDR USAA001254](https://openairdocs.org/sdr/USAA001254.md): Gusset · cracked · Aug 15, 2000 · N282AU · Boeing 7372B7 · Landing Gear Retraction/Extension System > CLT - FOUND GUSSETT CRACKED.5 INCH, NLG ACTUATOR ATTACH BEAM GUSSETT, STATION 259.5, BL 0. INSTALLED NEW PART PER SRM 51-30-00. (M) - [SDR USAA001236](https://openairdocs.org/sdr/USAA001236.md): Torque Box · cracked · Aug 14, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Structure > CLT - FOUND TORQUE BOX CRACKED.25 INCH, STATION 1112, LEFT SIDE JUST BELOW UPPER TORQUE BOX. INSTALLED DOUBLER AND FILLER PER EA 67773 AND SRM 51-40-3. (M) - [SDR USAA001237](https://openairdocs.org/sdr/USAA001237.md): Strap · cracked · Aug 14, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND STRINGER STRAP CRACKED.75 INCHES LONG, 2 INCHES AFT OF STATION 1138, RT SIDE. INSTALLED REPAIR PER EA 67733, AND SRM 53-00-01 FIG 221. (M) - [SDR USAA001207](https://openairdocs.org/sdr/USAA001207.md): Clip · cracked · Aug 7, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND ATTACH CLIP CRACKED.5 INCH, STATION 380, STRINGER 26L ON BAFFLE ATTACH CLIP. REPLACED PER SRM 51-10-01. (M) - [SDR USAA001206](https://openairdocs.org/sdr/USAA001206.md): Shim · cracked · Aug 7, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND SHIM CRACKED.25 INCH, STATION 440 BETWEEN STRINGER 22R AND STRINGER 23R. REPLACED ATTACH CLIP SHIM PER SRM 51-10-01. (M) - [SDR USAA001157](https://openairdocs.org/sdr/USAA001157.md): Tie Clip · cracked · Aug 4, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND TIE CLIP CRACKED.25 INCH, STATION 440, STRINGER 22R. REMOVED AND REPLACED ANGLE PER SRM 51-10-1. (M) - [SDR USAA001149](https://openairdocs.org/sdr/USAA001149.md): Floorbeam · cracked · Aug 4, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Floor Beam > CLT - FOUND FLOORBEAM CRACKED 2 INCHES, BS 663, BL 0. INSTALLED STIFFENER FILLER AND DOUBLER PER EA 67727. (M) - [SDR USAA001141](https://openairdocs.org/sdr/USAA001141.md): Frame · cracked · Aug 2, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED 1 INCH, BS 907, STRINGER 21R FUSELAGE FRAME UPPER LEG. INSTALLED DOUBLER PER SRM 51-40-3. (M) - [SDR USAA001140](https://openairdocs.org/sdr/USAA001140.md): Skin · cracked · Aug 2, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - FOUND SKIN CRACKED 3 INCHES, BS 328 AFT LOWER CORNER FS 0 CUTOUT. INSTALLED DOUBLER PER TR 53-10-19A. (M) - [SDR USAA001139](https://openairdocs.org/sdr/USAA001139.md): Stringer Clip · cracked · Aug 2, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND STRINGER TIE CLIP CRACKED.5 INCH, STRINGER 13 STATION 1138. INSTALLED NEW TIE CLIP PER SRM 51-10-01. (M) - [SDR USAA001112](https://openairdocs.org/sdr/USAA001112.md): Frame · cracked · Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Frame > CLT - FOUND 1 INCH CRACK, STATION 951 FRAME WL 254 RT SIDE. FABRICATED REPAIR AND INSTALLED PER TR 53-30-07A. (M) - [SDR USAA001111](https://openairdocs.org/sdr/USAA001111.md): Frame · cracked · Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Frame > CLT - FOUND 1 INCH CRACK, STATION 951 FRAME, WL 254 LT SIDE. FABRICATED AND INSTALLED REPAIR PER TR 53-30-07A. (M) - [SDR USAA001110](https://openairdocs.org/sdr/USAA001110.md): Cap · corroded · Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND T-CAP CORRODED 2 INCHES, FS 312, RBL 35. CUTOUT DAMAGED FABRICATED REPAIR AND INSTALLED PER 53-10-9 FIG 5. (M) - [SDR USAA001109](https://openairdocs.org/sdr/USAA001109.md): Clip · cracked · Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND CLIP CRACKED.125 INCH, STATION 727B, STRINGER 3. INSTALLED NEW TIE CLIP PER EO 5393G227. (M) - [SDR USAA001108](https://openairdocs.org/sdr/USAA001108.md): Clip · cracked · Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND CLIP CRACKED.125 INCH, STATION 685, STRINGER 4. INSTALLED NEW TIE CLIP PER EO 5393G227. (M) - [SDR USAA001107](https://openairdocs.org/sdr/USAA001107.md): Clip · cracked · Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND CLIP CRACKED.250 INCH, STATION 685, STRINGER 3. INSTALLED NEW TIE CLIP PER EO 5393G227. (M) - [SDR USAA001106](https://openairdocs.org/sdr/USAA001106.md): Tie Clip · cracked · Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND TIE CLIP CRACKED.5 INCH, FS 663, STRINGER 10L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M) - [SDR USAA001105](https://openairdocs.org/sdr/USAA001105.md): Tie Clip · cracked · Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND TIE CLIP CRACKED.125 INCH, BS 616, STRINGER 3R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M) - [SDR USAA001104](https://openairdocs.org/sdr/USAA001104.md): Tie Clip · cracked · Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND TIE CLIP CRACKED.125 INCH, FRAME 597 AT STRINGER 8L TIE CLIP. INSTALLED NEW TIE CLIP PER EO 5393G227. (M) - [SDR USAA001066](https://openairdocs.org/sdr/USAA001066.md): Tie Clip · cracked · Jul 31, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND TIE CLIP CRACKED.5 INCH, FS 727B, STRINGER 5L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M) - [SDR USAA001065](https://openairdocs.org/sdr/USAA001065.md): Tie Clip · cracked · Jul 31, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND TIE CLIP CRACKED.125 INCH, BS 727A, STRINGER 4L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M) - [SDR USAA001064](https://openairdocs.org/sdr/USAA001064.md): Tie Clip · cracked · Jul 31, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND TIE CLIP CRACKED.5 INCH, FS 727A, STRINGER 4L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M) - [SDR USAA001063](https://openairdocs.org/sdr/USAA001063.md): Clip · cracked · Jul 31, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND CLIP CRACKED.125 INCH, STATION 685, STRINGER 2. INSTALLED NEW TIE CLIP PER EO 5393G227. (M) - [SDR USAA001062](https://openairdocs.org/sdr/USAA001062.md): Tie Clip · cracked · Jul 31, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - TIE CLIP CRACKED.125 INCH, STRINGER 9L, AT FRAME 597. INSTALLED STRINGER TIE CLIP PER EO 5393G227. (M) - [SDR USAA000803](https://openairdocs.org/sdr/USAA000803.md): Floorbeam · corroded · Jun 7, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Floor Beam > CLT - FOUND FLOORBEAM CORRODED.250 INCH BY.250 INCH, BS 312, RBL 11-36. INSTALLED NEW T-CAP PER SRM 53-10-9. INSTALLED NEW T-CAP PER SRM 53-10-9. (M) - [SDR USAASB99052](https://openairdocs.org/sdr/USAASB99052.md): Pcu · malfunctioned · Feb 23, 1999 · N282AU · Boeing 7372B7 · Rudder Control System > BWI - FLT 2710 - EN ROUTE FROM MCO-BDL, AT FL330 AND.74 MACH, FLIGHT WAS APPROACH SBY ON 'A' AUTOPILOT WHEN THE A/C STARTED PITCHING UP AND ROLLING TO RIGHT 80 DEGRES. CAPT USED FULL POWER AND FULL AILERON TO GET THE AIRCRAFT LEVEL. CAPT STATED THAT WHEN HE - [SDR USAASB98309](https://openairdocs.org/sdr/USAASB98309.md): Mechanism · out of adjust · Nov 22, 1998 · N282AU · Boeing 7372B7 · Leading Edge Slat Control System > BWI - FLT 2608 - FLIGHT WAS CLEARED FOR APPROACH AT BWI FOR RUNWAY 28. AS CAPTAIN SELECTED FLAPS 1, THE LEADING EDGE TRANSIT LIGHT AND THE NR 4 SLAT TRANSIT LIGHT ON THE OVERHEAD PANEL ILLUMINATED. CREW RECYCLED THE FLAPS AND DISCONTINUED THE APPROACH. CREW - [SDR USAA980176](https://openairdocs.org/sdr/USAA980176.md): Stringer · corrosion · May 1, 1998 · N282AU · Boeing 7372B7 · Fuselage Main, Longeron/Stringer > ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 1.333 INCH BY 2.5 INCH CORROSION BS 967 STRINGER 25 LEFT. REMOVED CORROSION AND INSTALLED STRINGER SPLICE. REPAIRED PER SRM 53-10-3 FIG 9. (M) - [SDR USAASB98055](https://openairdocs.org/sdr/USAASB98055.md): Light · failed · Mar 9, 1998 · N282AU · Boeing 7372B7 · Emergency Lighting > CLT - MAINTENANCE FOUND THE EMERGENCY LIGHT OVER THE FORWARD SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD. (M) - [SDR USAASB97332](https://openairdocs.org/sdr/USAASB97332.md): Battery Pack · discharged · Dec 6, 1997 · N282AU · Boeing 7372B7 · Emergency Lighting > CLT - MAINTENANCE FOUND THE AFT LEFT AND RIGHT EXTERIOR EMERGENCY ESCAPE SLIDE LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) - [SDR USAASB97073](https://openairdocs.org/sdr/USAASB97073.md): Garlock Seal · leaking · Mar 7, 1997 · N282AU · Boeing 7372B7 · Turbine Engine Oil System > BWI - FL 8028 - ON CLIMB-OUT OF BWI, AT FL 250, CAPTAIN SHUT DOWN THE NR 1 ENGINE DUE TO LOW OIL PRESSURE LIGHT ILLUMINATING WHICH WAS VERIFIED BY OIL PRESSURE GAUGE AND LOSS OF OIL QUANTITY. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD AT BWI A - [SDR USAA960918](https://openairdocs.org/sdr/USAA960918.md): Beam · cracked · Sep 18, 1996 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACKED BEAM RBL 24.5 BS 674. INSTALLED STIFFENER AND NEW CHANNEL, REPAIRED PER EO 5791G632. (M) - [SDR USAA960622](https://openairdocs.org/sdr/USAA960622.md): Floor Beam · corrosion · Sep 18, 1996 · N282AU · Boeing 7372B7 · Fuselage Main, Floor Beam > INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 20 INCH AREA OF HEAVY SURFACE CORROSION FLOOR BEAM STATION 360, RBL 12 TO RBL 56. INSTALLED REPAIR ANGLES, REPAIRED PER TR 53-10-05 C. CORROSION TASK NR C53-107-01, CORROSION LEVEL 1. ( - [SDR USAA960621](https://openairdocs.org/sdr/USAA960621.md): Web · cracked · Sep 18, 1996 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO.5 INCH CRACKED WEBS RBL 24.5 BS 707. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2, FIG 1. (M) - [SDR USAA960620](https://openairdocs.org/sdr/USAA960620.md): Web · cracked · Sep 18, 1996 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND THREE.25 INCH CRACKED WEBS LBL 24.5 BS 707. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2 FIG 1. (M) - [SDR USAA960619](https://openairdocs.org/sdr/USAA960619.md): Web · cracked · Sep 18, 1996 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND FOUR.5 INCH CRACKED WEBS BL 0 BS 707. INSTALLED WEB REPAIR AND FILLERS. REPAIRED PER SRM 51-40-2. (M) Next page: https://openairdocs.org/deregistered/N282AU-2002-09-10/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 = 'N282AU' AND deregistration_id = 'N282AU-2002-09-10' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N282AU-2002-09-10/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.