# Service difficulty reports: N898AA, cancelled Aug 21, 2013

A list on [N898AA, cancelled Aug 21, 2013](https://openairdocs.org/deregistered/N898AA-2013-08-21.md).

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

- [SDR C8GA2011000011](https://openairdocs.org/sdr/C8GA2011000011.md): Warning Horn · false activation · Jul 13, 2011 · N898AA · Boeing 727223 · Independent Instruments
  > DURING TAKEOFF ROLL, THE TAKEOFF WARNING SYS HORN SOUNDED. THE ACFT GROUND SPEED DID NOT EXCEED 20 KNOT. THE ACFT RETURNED TO BLOCKS WITHOUT INCIDENT. POST FLIGHT INSP AND OPS CHECKS WERE PERFORMED, NO DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA2010000030](https://openairdocs.org/sdr/C8GA2010000030.md): Acm · inoperative · Aug 19, 2010 · N898AA · Boeing 727223 · Cabin Cooling System
  > DURING CLIMB OPERATION, THE ACFT WAS UNABLE TO MAINTAIN CABIN PRESSURIZATION ON RT PACK. LT PACK WAS DMI. CLEANED CONNECTOR ON LT PACK TEMP BULB, R & R LT PACK FLOW CONTROL VALVE, RE RACKED AUTO PSI CONTROLLER, R & R LT ACM, R & R LT COMPRESSOR DISCHARGE OVE
- [SDR C8GA201000014](https://openairdocs.org/sdr/C8GA201000014.md): Control Valve · inoperative · Aug 3, 2010 · N898AA · Boeing 727223 · Cabin Cooling System
  > DURING CLIMB OPERATION WITH THE RT PACK ON DMI. THE LT PACK WOULD NOT MAINTAIN CABIN ALTITUDE. ACFT LEVELED OF AT 18,000 FT THE CABIN CONTINUED TO CLIMB AT A RATE OF 500 FT/MIN WITH CARGO HEAT OUTFLOW VALVE AND OUT FLOW VALVE CLOSED. THE ACFT RETURNED TO DEPAR
- [SDR ABXR20107130022](https://openairdocs.org/sdr/ABXR20107130022.md): Stiffener · corroded · Jul 13, 2010 · N898AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED LINE MX EVENT, CORROSION WAS DISCOVERED WHILE ACCOMPLISHING OTHER MX ON A STIFFENER "C-CHANNEL" AT STA 312 OTBD AND AFT OF THE NLG TRUNNION LT SIDE. FABRICATED NEW STIFFENER FROM 7075-T76511 EXTRUSION AND REPLACED. ITEM WAS RETURNED TO SERVI
- [SDR C8GA201000011](https://openairdocs.org/sdr/C8GA201000011.md): Controller · disconnected · Jun 30, 2010 · N898AA · Boeing 727223 · Cabin Pressure Controller
  > DURING CLIMB OPERATION OUT OF SLW THE ACFT EXPERIENCED ERRATIC AND OFF-SCHEDULE PRESSURIZATION. ACFT DIVERTED, WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED, NOTING THE STATIC HOSE TO THE CABIN PRESSURE CONTROLLER WAS DISCONNECTED, CONNECTED
- [SDR C8GA201000010](https://openairdocs.org/sdr/C8GA201000010.md): Cover · damaged · Jun 22, 2010 · N898AA · Boeing 727223 · Instrument Panel
  > AFTER STARTING THE TAKEOFF ROLE, THE UPPER YAW DAMPER "OFF" LIGHT ILLUMINATED. THE CREW PERFORMED AN ABORTED TAKEOFF AND RETURNED TO THE BLOCKS WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED NOTING THAT THE LIGHT COVER WAS STUCK IN SOCKET. PERFORMED GROUND T
- [SDR ABXR200910060039](https://openairdocs.org/sdr/ABXR200910060039.md): Skin · delaminated · Oct 6, 2009 · N898AA · Boeing 727223 · Spoilers
  > DURING A HEAVY MX INSP, THE LT WING NR6 SPOILER WAS FOUND DELAMINATED OUTSIDE OF THE MFG LIMITS. REMOVED AND REPLACED THE NR6 SPOILER AND ACCOMPLISHED THE ADJUSTMENT AND TEST IAW THE AMM. ITEM WAS RETURNED TO SERVICE.
- [SDR ABXR200910060038](https://openairdocs.org/sdr/ABXR200910060038.md): Skin · delaminated · Oct 6, 2009 · N898AA · Boeing 727223 · Spoilers
  > DURING A HEAVY MX INSP, THE LT WING NR2 SPOILER WAS FOUND DELAMINATED OUTSIDE OF THE MFG LIMITS. REMOVED AND REPLACED THE NR2 SPOILER AND ACCOMPLISHED THE ADJUSTMENT AND TEST IAW THE AMM. ITEM WAS RETURNED TO SERVICE.
- [SDR ABXR200910060037](https://openairdocs.org/sdr/ABXR200910060037.md): Skin · cracked · Oct 6, 2009 · N898AA · Boeing 727223 · Cargo/Baggage Doors
  > DURING A HEAVY MX INSP, IT WAS DISCOVERED THE FWD LOWER CARGO DOOR WAS DENTED AND CRACKED AT THE AFT LOWER CORNER. DOOR WAS REPAIRED. ITEM RETURNED TO SERVICE.
- [SDR ABXR200910060036](https://openairdocs.org/sdr/ABXR200910060036.md): Web · nicked · Oct 6, 2009 · N898AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING A HEAVY MX INSP, MAIN CARGO DOOR CUT-OUT AFT WEB WAS DISCOVERED NICKED AND GOUGED. REPLACED LOWER WEB. ITEM RETURNED TO SERVICE.
- [SDR ABXR200910060035](https://openairdocs.org/sdr/ABXR200910060035.md): Floor Support · corroded · Oct 6, 2009 · N898AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING A HEAVY MX INSP EVENT CORROSION WAS FOUND ON A MAIN CABIN FLOOR SUPPORT. FLOOR SUPPORT WAS REPAIRED. ITEM WAS RETURNED TO SERVICE.
- [SDR ABXR200910060035A](https://openairdocs.org/sdr/ABXR200910060035A.md): Support · corroded · Oct 6, 2009 · N898AA · Boeing 727223 · Wing, Landing Gear Attach Fittings
  > DURING A HEAVY MX INSP, IN COMPLIANCE WITH AD2001-20-09 AND DVI MAG PARTICLE S/B 57A0179 FOUND CORROSION ON THE LT AND RT LANDING GEAR FWD TRUNNION BEARING SUPPORTS. FWD TRUNNION BEARING SUPPORTS WERE REMOVED AND REPLACE. ITEM WAS RETURNED TO SERVICE.
- [SDR ABXR20091005033](https://openairdocs.org/sdr/ABXR20091005033.md): Trunnion · corroded · Oct 5, 2009 · N898AA · Boeing 727223 · Fuselage, Landing Gear Attach Fittings
  > DURING A HEAVY MX INSP, THE NOSE LANDING GEAR DRAG BRACE/ACTUATOR TRUNNION FITTING HAD CORROSION UNDER THE BEARING SURFACE. THE NOSE LANDING GEAR DRAG BRACE/ACTUATOR TRUNNION FITTING WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.
- [SDR ABXR200910050032](https://openairdocs.org/sdr/ABXR200910050032.md): Skin · cracked · Oct 5, 2009 · N898AA · Boeing 727223 · Leading Edge Devices
  > DURING A HEAVY MX INSP EVENT THE NR6 KRUGER LE FLAP WAS FOUND WITH 2 (EA) CRACKS MID AND OUT BOARD. THE FLAP WAS REMOVED AND REPLACED. ITEM RETURNED TO SERVICE.
- [SDR ABXR200910030031](https://openairdocs.org/sdr/ABXR200910030031.md): Rib · cracked · Oct 3, 2009 · N898AA · Boeing 727223 · Trailing Edge Flaps
  > DURING A HEAVY MX INSP, THE LT WING OTBD FLAP INBD FAIRING AFT INTERANL RIB CRACKED IN 2 EACH PLACES. FABRICATED RIB FROM 2024 T3 0.063". HEATED TREATED RIB. INSTALLED RIB AND RETURNED ITEM TO SERVICE.
- [SDR ABXR200910030030](https://openairdocs.org/sdr/ABXR200910030030.md): Rib · cracked · Oct 3, 2009 · N898AA · Boeing 727223 · Trailing Edge Flaps
  > DURING A HEAVY MX INSP, THE LT WING OTBD FLAP, OTBD FAIRING AFT INTERNAL RIB CRACKED. FABRICATED NEW RIB FROM 2024 O 0.065", AND HEAT TREATED. INSTALLED NEW RIB. ITEM RETURNED TO SERVICE.
- [SDR ABXR200910030028](https://openairdocs.org/sdr/ABXR200910030028.md): Skin · gouged · Oct 3, 2009 · N898AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > DURING A HEAVY MX INSP, THE MAIN CARGO DOOR CUT OUT AFT WEB WAS FOUND NICKED AND GOUGED OUT OF LIMITS. THE AFT WEB WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.
- [SDR ABXR200910030027](https://openairdocs.org/sdr/ABXR200910030027.md): Stringer Splice · corroded · Oct 3, 2009 · N898AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > DURING A HEAVY MX INSP, A STRINGER SPLICE WAS FOUND CORRODED OUT OF LIMITS. FABRICATED NEW SPLICE FROM 7070-T6 0.070". TREATED, PRIMED AND REPLACED SPLICE. ITEM RETURNED TO SERVICE
- [SDR ABXR200910030029](https://openairdocs.org/sdr/ABXR200910030029.md): Skin · corroded · Oct 3, 2009 · N898AA · Boeing 727223 · Wing, Plate/Skin
  > DURING A HEAVY MX INSP, THE LWR WING PLATE WAS FOUND EXFOLIATED ABOVE THE LT PRIMARY HEAT EXCHANGER. DAMAGED AREA APPROX 6" X 5", REMOVED ALL CORROSION, BEYOND MFG LIMITS. MACHINED PAD-UPS TO ACCOMMODATE EXTERNAL DOUBLER. SPOT FACED SANDWICHED FASTENER HEADS
- [SDR ABXR200910030026](https://openairdocs.org/sdr/ABXR200910030026.md): Retainer · cracked · Oct 3, 2009 · N898AA · Boeing 727223 · Main Landing Gear Attach Section
  > DURING A HEAVY MX INSP, THE RT MLG BEAM SWING LINK LOWER PIN RETAINER WAS FOUND CRACKED. REMOVED AND REPLACED RT MLG DEAM SIWNG LINK LOWER PIN RETAINER. ITEM RETURNED TO SERVICE
- [SDR ABXR200910020025](https://openairdocs.org/sdr/ABXR200910020025.md): Skin · cracked · Oct 2, 2009 · N898AA · Boeing 727223 · Passenger/Crew Doors
  > DURING A HEAVY MX INSP EVENT, MAIN ENTRY DOOR INNER AFT EDGE BY MID DOOR STOPS WAS DISCOVERED CRACKED. INNER SKIN WAS REPAIRED AND ITEM RETURNED TO SERVICE.
- [SDR ABXR200910020024](https://openairdocs.org/sdr/ABXR200910020024.md): Skin · corroded · Oct 2, 2009 · N898AA · Boeing 727223 · Wing, Plate/Skin
  > DURING A HEAVY MX INSP EVENT, LWR WING PLATE HAS 2 AREAS OF CORROSION. CORROSION WAS REMOVED, AREAS WERE WITHIN LIMITS. RETURNED TO SERVICE.
- [SDR ABXR200910020023](https://openairdocs.org/sdr/ABXR200910020023.md): Drain · cracked · Oct 2, 2009 · N898AA · Boeing 727223 · Passenger/Crew Doors
  > DURING A HEAVY MX INSP EVENT, MAIN ENTRY DOOR LWR DRAIN HAS 3 CRACKS GOING INTO IT. REMOVED, FABRICATED LWR DRAIN PLATE. RETURNED TO SERVICE
- [SDR ABXR200910020022](https://openairdocs.org/sdr/ABXR200910020022.md): Scuff Plate · cracked · Oct 2, 2009 · N898AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING A HEAVY MX INSP EVENT, MAIN CARGO DOOR CUT OUT AFT LWR STRUCTURE WAS DISCOVERED CRACKED AND GOUGED. REMOVED, FABRICATED AND REINSTALLED SCUFF PLATES. ITEM RETURNED TO SERVICE.
- [SDR C8GA20080009](https://openairdocs.org/sdr/C8GA20080009.md): Strainer · unknown · Mar 6, 2008 · N898AA · Boeing 727223 · Engine Oil Distribution (Airframe Furnished)
  > FLT 724 FROM TOL TO ROC - DURING CLIMB OPERATION, THE NR 3 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. THE NR 3 ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO TOL WHERE IT LANDED WITHOUT INCIDENT. ON POST FLIGHT, REMOVED AND INSPECTED THE MAIN OIL STRAINE
- [SDR C8GA20080008](https://openairdocs.org/sdr/C8GA20080008.md): Oil Filter · dirty · Mar 6, 2008 · N898AA · Boeing 727223 · Engine Oil Distribution (Airframe Furnished)
  > FLT 719 FROM ALT TO TOL - DURING CRUISE OPERATION, THE NR 3 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT IN TOL. THE NR 3 ENGINE OIL FILTER WAS REMOVED AND INSPECTED, CARBON CONTAMINATION WAS NO
- [SDR C8GA20070008](https://openairdocs.org/sdr/C8GA20070008.md): Rod · broken · Aug 7, 2007 · N898AA · Boeing 727223 · Landing Gear Position and Warning
  > FLT 723 FROM ROC TO TOL, AFTER TAKEOFF WHEN GEAR WAS RAISED THE RIGHT MAIN LANDING GEAR GREEN AND RED INDICATIONS LIGHTS REMAINED ON, SECONDARY RIGHT MAIN GEAR LIGHT ON FO'S PANEL REMAINED ON. ALL INDICATIONS WERE NORMAL WITH GEAR DOWN. AIRCRAFT RETURNED TO
- [SDR C8GA20060009](https://openairdocs.org/sdr/C8GA20060009.md): Gasper Fan · smoke · Aug 3, 2006 · N898AA · Boeing 727223 · Air Distribution Fan
  > DURNING CRUISE OPERATION CREW EXPERIENCED SMOKE IN THE COCKPIT 139 NM FROM. DECLARED AN EMERGENCY AND PERFORMED EMERGENCY PROCEDURES, SMOKE DISAPPATED AND ORDOR FADED, AIRCRAFT CONTINUED AND LANDED WITHOUT INCIDENT. INSPECTED AIRCRAFT FOR ELECTRICAL PROBLEMS,
- [SDR C8GA20050021](https://openairdocs.org/sdr/C8GA20050021.md): Switch · malfunctioned · Sep 24, 2005 · N898AA · Boeing 727223 · Leading Edge Slat Control System
  > FLT 1737 FROM MTY TO TOL, AFTER TAKEOFF FROM MTY, NR 5 LEADING EDGE SLAT EXTEND LIGHT REMAINED ILLUMINATED AT FLAPS 2 POSITION. AIRCRAFT RETURNED TO MTY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 5 LEADING EDGE SLAT POSITION INDICATION SWITCH. OPS
- [SDR C8GA20050020](https://openairdocs.org/sdr/C8GA20050020.md): Connector · dirty · Sep 24, 2005 · N898AA · Boeing 727223 · Leading Edge Slat Control System
  > FLT 1737 FROM MTY TO TOL, AFTER TAKEOFF FROM MTY, NR 5 LEADING EDGE DEVICES RED EXTENDED AT FLAPS 2 POSITION. AIRCRAFT RETURNED TO MTY AND LANDED WITHOUT INCIDENT. CLEANED NR 5 SLAT TRACK POSITION SENSOR CONNECTOR. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERV
- [SDR CG8A20020003](https://openairdocs.org/sdr/CG8A20020003.md): Control Unit · malfunctioned · Feb 9, 2002 · N898AA · Boeing 727223 · Fire Detection
  > FLT 707 FROM DEN TO TOL. DURING CRUISE LEVEL, THE FORWARD LOWER CARGO COMPARTMENT FIRE LIGHT CAME ON. APPROPRIATE CHECK LIST WERE ACCOMPLISHED AND FIRE WARNING LIGHT REMAINED ILLUMINATED. NOTIFIED ATC OF THE FIRE WARNING LIGHT AND LANDED WITHOUT INCIDENT.
- [SDR CG8A20020001](https://openairdocs.org/sdr/CG8A20020001.md): Pump · sheared · Jan 4, 2002 · N898AA · Boeing 727223 · Engine (Turbine/Turboprop)
  > Flt 707 from DEN to TOL. During cruise level at FL 330 #3 engine flame out. Oil pressure and quantity as well as N1 and N2 were normal. Descended to two engine cruise altitude and conducted engine failure shutdown checklist and all indications were normal, att
- [SDR C8GA20010014](https://openairdocs.org/sdr/C8GA20010014.md): Clamp · deteriorated · Jun 17, 2001 · N898AA · Boeing 727223 · Detection System
  > Flt 898 from JAX to MCO. After takeoff #3 engine strut overheat light illuminated. Accomplished appropiate check list, and air turnback to JAX. Aircraft landed without incident. During inspection, found and replaced clamps on #3 engine bleed valve (pylon) IAW
- [SDR C8GA20010010](https://openairdocs.org/sdr/C8GA20010010.md): Fire Warning · false activation · May 15, 2001 · N898AA · Boeing 727223 · Fire Detection
  > FLT 740 FROM TOL TO MCI. IN CRUISE, AT APPROXIMATELY 126 MILES FROM MCI, THE APU FIRE LIGHT CAME ON. ACCOMPLISHED APU FIRE CHECKLIST IAW AOM. AIRCRAFT CONTINUED TO MCI AND LANDED WITHOUT INCIDENT. INVESTIGATION FOUND THAT HEAVY RAIN IN TOL DURING CARGO LOA
- [SDR C8GA20010009](https://openairdocs.org/sdr/C8GA20010009.md): Wire · broken · Apr 27, 2001 · N898AA · Boeing 727223 · Door System Wiring
  > FLT 001 FROM MIA TO PTY. AFTER TAKEOFF ROTATION, CREW HEARD A LOUD NOISE IN THE COCKPIT AND WAS UNABLE TO PRESSURIZE AIRCRAFT. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND THE E&E COMPARTMENT DOOR OPEN. UPON FURTHER INSPECTION, FOUND A BROKE
- [SDR AALA981721](https://openairdocs.org/sdr/AALA981721.md): Connector · contaminated · Sep 24, 1998 · N898AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHT AT ROW 9 INOPERATIVE. CLEANED CONTACTS ON OVERHEAD EMERGENCY EXIT LIGHT AT ROW 9. SYSTEM GROUND CHECKED NROMAL OPERATION. (M)
- [SDR AALA980941](https://openairdocs.org/sdr/AALA980941.md): Wire · failed · May 10, 1998 · N898AA · Boeing 727223 · Light System Wiring
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN CABIN INOPERATIVE. REPAIRED WIRING IN CABIN FORWARD OF SEATS. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M)
- [SDR AALA980420](https://openairdocs.org/sdr/AALA980420.md): Fuel Control · defective · Mar 1, 1998 · N898AA · Boeing 727223 · Fuel Control/Turbine Engines
  > MIA - FLT 929 - WHILE PASSING THROUGH 2000 FT, NR 1 ENGINE FLAMED OUT WITH NO PRIOR ABNORMAL INDICATIONS. AIRCRAFT RETURNED TO MIAMI AND LANDED WITHOUT INCIDENT, NOT OVERWEIGHT. REPLACED FUEL PUMP AND FUEL CONTROL. LEAK CHECKED WITH NO LEAKS FOUND. GROUND
- [SDR AALA972068](https://openairdocs.org/sdr/AALA972068.md): Sign · missing · Nov 1, 1997 · N898AA · Boeing 727223 · Emergency Lighting
  > ATL - DURING OVERNIGHT CHECK, FORWARD ENTRY EMERGENCY EXIT SIGN MISSING AND BASE BROKEN. REPLACED FORWARD ENTRY EMERGENCY EXIT SIGN ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA971827](https://openairdocs.org/sdr/AALA971827.md): Light · defective · Sep 24, 1997 · N898AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT CHECK, EMERGENCY LIGHT OVER FORWARD GALLEY DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT OVER FORWARD GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA971425](https://openairdocs.org/sdr/AALA971425.md): Light · defective · Aug 7, 1997 · N898AA · Boeing 727223 · Emergency Lighting
  > BWI - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 21 AND 24 INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 21 AND 24. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA970905](https://openairdocs.org/sdr/AALA970905.md): Stringer · corroded · May 7, 1997 · N898AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > AFW - FRETTING CORROSION, EVIDENT AT STA 720D + 12 INCHES AT STR 19R. ACCOMPLISHED REPAIR PER SRM 53-30-3 FIG 14. TST: 46,319.57 HOURS. CYCLES: 25,313. (X)
- [SDR AALA970904](https://openairdocs.org/sdr/AALA970904.md): Stringer · corroded · May 7, 1997 · N898AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > AFW - FRETTING CORROSION EVIDENT AT STA 720D + 12 INCHES AT STR 19L. ACCOMPLISHED REPAIR PER SRM 53-30-3 FIG 14. TST: 46,319.57 HOURS. CYCLES: 25,313. (X)
- [SDR AALA960842](https://openairdocs.org/sdr/AALA960842.md): Lamp · inoperative · May 29, 1996 · N898AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT CHECK, FOUND RIGHT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RESEATED LAMP HOUSING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA9604331](https://openairdocs.org/sdr/AALA9604331.md): Wire · failed · Mar 22, 1996 · N898AA · Boeing 727223 · Light System Wiring
  > MIA - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS SECTION INOPERATIVE. REPAIRED SPLICE IN EMERGENCY EXIT FLOOR PATH LIGHTING WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA960077](https://openairdocs.org/sdr/AALA960077.md): Skin · corroded · Jan 18, 1996 · N898AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TULE - FOUND CORROSION ON SKIN FS 590-602 STRINGER 26L TO 27L. REMOVED CORROSION, FOUND BEYOND LIMITS, INSTALLED REPAIR DOUBLER PER SRM 53-30-3 PGS 12-14A. (M)
- [SDR AALA960076](https://openairdocs.org/sdr/AALA960076.md): Stringer · corroded · Jan 18, 1996 · N898AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION IN STRINGER 27 LEFT STATION 590 - 600. REMOVED CORROSION, CUT OUT BAD SECTION OF STRINGER AND INSTALLED STRINGER REPAIR PER SRM 53-10-3 PG 3-43. (M)
- [SDR AALA960075](https://openairdocs.org/sdr/AALA960075.md): Shear Tie · corroded · Jan 8, 1996 · N898AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON SHEAR TIE STATION 600 BETWEEN STRINGER 26L AND 27L. REMOVED CORROSION ON SHEAR TIE BEYOND LIMITS. REPLACED SHEAR TIE PER SRM 53-10-1. (M)
- [SDR AALA951756](https://openairdocs.org/sdr/AALA951756.md): Eel Connector · loose · Oct 4, 1995 · N898AA · Boeing 727223 · Emergency Lighting
  > RDU - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD END OF MAIN CABIN INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT AFT END OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (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 = 'N898AA' AND deregistration_id = 'N898AA-2013-08-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N898AA-2013-08-21/reports

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