# Service difficulty reports: N872AA, cancelled Nov 15, 2004 A list on [N872AA, cancelled Nov 15, 2004](https://openairdocs.org/deregistered/N872AA-2004-11-15.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AALA20011845](https://openairdocs.org/sdr/AALA20011845.md): Wire · damaged · Oct 6, 2001 · N872AA · Boeing 727223 · Light System Wiring > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 15-20 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20011712](https://openairdocs.org/sdr/AALA20011712.md): Battery Pack · discharged · Aug 29, 2001 · N872AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT MAINTENANCE, L1 AND R1 EMERGENCY EXIT SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20011654](https://openairdocs.org/sdr/AALA20011654.md): Battery Pack · discharged · Aug 18, 2001 · N872AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT PATH LIGHTING AT R1 AND L1 DOOR INOPERATIVE. REPLACED BATTERY PACKS. SYSTEM GROUND CHECK NORMAL OPERATION. (M) - [SDR AALA20010577](https://openairdocs.org/sdr/AALA20010577.md): Connector · defective · Mar 22, 2001 · N872AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 15 DIM. REPLACED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20010502](https://openairdocs.org/sdr/AALA20010502.md): Lamp · inoperative · Mar 15, 2001 · N872AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE OVERWING EMERGENCY EXIT LIGHT DIM. REPLACED OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20010501](https://openairdocs.org/sdr/AALA20010501.md): Lamp · inoperative · Mar 15, 2001 · N872AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT ROW 15 AND 20 DIM. REPLACED OVERHEAD EMERGENCY EXIT LIGHT AT ROW 15 AND 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20010017](https://openairdocs.org/sdr/AALA20010017.md): Skin · corroded · Dec 24, 2000 · N872AA · Boeing 727223 · Wing, Plate/Skin > TUL - FOUND CORROSION ON CENTER TANK SKIN IN AIRCRAFT BAY NUMEROUS AREAS, FS 890-950. REMOVED CORROSION AND INSTALLED DOUBLER OF 2024T3, EXTERNAL AND 2 INTERNAL OF.125 2024T3 AND 5 INTERNAL STRAPS.175 2024T3 PER ESO 11697 DATED 12-21-00. (M) - [SDR AALA20002112](https://openairdocs.org/sdr/AALA20002112.md): Skin · cracked · Dec 15, 2000 · N872AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FOUND FUSELAGE SKIN AT FORWARD ENTRY DOOR UPPER HINGE CUT OUT CRACKED. INSTALLED DOUBLER AT UPPER HINGE CUTOUT, FORWARD ENTRY DOOR IAW SB 727-53-0198. (M) - [SDR AALA20002113](https://openairdocs.org/sdr/AALA20002113.md): Skin · cracked · Dec 14, 2000 · N872AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FOUND CRACK IN UPPER OUTBOARD CORNER OF LEFT NR 1 COCKPIT WINDOW CUTOUT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-30-3 PART 1 FIG 8. (M) - [SDR AALA991905](https://openairdocs.org/sdr/AALA991905.md): Shear Tie · corroded · Dec 17, 1999 · N872AA · Boeing 727223 · Fuselage Miscellaneous Structure > TUL - STA 990 AFT SIDE OF FRAME BETWEEN 28R AND 29R SHEAR TIE UPPER LEG CORRODED. ALODINED AND PRIMED SKIN AREA IAW SRM 51-20-0, INSTALLED FASTENERS, INSTALLED NEW SHEAR TIE. TST: 59,544 HOURS. CYCLES: 36,249. (X) - [SDR AALA991909](https://openairdocs.org/sdr/AALA991909.md): Skin · damaged · Dec 14, 1999 · N872AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - REMOVED TEMPORARY REPAIR AND RE-INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. TST: 59,544 HOURS. CYCLES: 36,249. (X) - [SDR AALA991908](https://openairdocs.org/sdr/AALA991908.md): Skin · corroded · Dec 14, 1999 · N872AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - CORROSION ON SKIN BELOW STR 30 BS 1010 - BS 1030. REMOVED CORROSION INSTALLED DOUBLER ON SKIN PER SRM 53-30-3 FIG 3A. TST: 59,544 HOURS. CYCLES: 36,249. (X) - [SDR AALA991907](https://openairdocs.org/sdr/AALA991907.md): Skin · cracked · Dec 14, 1999 · N872AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FUSELAGE SKIN CRACKED AT RIVET STA 383.5 STR 8R FORWARD UPPER CORNER OF FORWARD GALLEY DOOR CUT-OUT. INSTALLED DOUBLER PER SRM 53-30-3. TST: 59,544 HOURS. CYCLES: 36,249. (X) - [SDR AALA991906](https://openairdocs.org/sdr/AALA991906.md): Stringer · corroded · Dec 14, 1999 · N872AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL- LEFT SIDE OF STR 30 CORRODED FORWARD OF FRAME STA 1030. INSTALLED STRINGER REPAIR PER SRM 53-10-3 AND SKIN DOUBLER PER SRM 53-30-3 FIG 3A. TST: 59,544 HOURS. CYCLES: 36,749. (X) - [SDR AALA991928](https://openairdocs.org/sdr/AALA991928.md): Frame · cracked · Dec 11, 1999 · N872AA · Boeing 727223 · Fuselage Main, Frame > TUL - STA 600 FRAME CRACKED AT UPPER FASTENER FOR INTERCOSTAL OF STR 28L (MARKED). STOP DRILLED CRACK, INSTALLED 2 INCH BY 1 INCH BY.063 INCH 7075T6 REPAIR ANGLE WITH 43.1875 INCH HILOCKS PER SRM 51-40-3. TST: 59,544 HOURS. CYCLES: 36,249. (X) - [SDR AALA990742](https://openairdocs.org/sdr/AALA990742.md): Outflow Valve · defective · May 15, 1999 · N872AA · Boeing 727223 · Pressure Regulator/Outflow Valve > SJU - FLT 1938 - EN ROUTE SJU/TPA CLIMBING THROUGH 30,000 FEET, CABIN PRESSURE STARTED CLIMBING AT 2,000 FEET PER MINUTE. PERFORMED RAPID DECOMPRESSION CHECKLIST WITHOUT RESULTS. AS CABIN ALTITUDE APPROACHED 10,000 FEET, PEFORMED EXPLPERFORMED EXPLOSIVE DECO - [SDR AALA990714](https://openairdocs.org/sdr/AALA990714.md): Outflow Valve · defective · May 15, 1999 · N872AA · Boeing 727223 · Pressure Regulator/Outflow Valve > SJU - FLT 1938 - DURING CLIMB-OUT AT FL300, CABIN PRESSUER STARTED CLIMBING AT 2000 FPM. CREW PERFORMED RAPID DECOMPRESSION CHECKLIST WITHOUT RESULTS. CABIN ALTITUDE APPROACHED 10,000 FT. CREW PERFORMED EXPLOSIVE DECOMPRESSION CHECKLIST. FLIGHT AIR INTERRU - [SDR AALA990545](https://openairdocs.org/sdr/AALA990545.md): Cap · leaking · Apr 18, 1999 · N872AA · Boeing 727223 · Fuel Storage > DFW - FLT 1840 - AFTER TAKEOFF, A FLUID LEAK WAS REPORTED COMING FROM THE LEFT WING IN THE AREA OF THE OVERWING FUEL CAP. FLIGHT AIR INTERRUPTED AND RETURNED DFW LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND FUEL IN REAR SPARE AREA. AIRC - [SDR AALA990528](https://openairdocs.org/sdr/AALA990528.md): Wire · chafed · Apr 15, 1999 · N872AA · Boeing 727223 · Light System Wiring > TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN FORWARD LAVATORY AND GALLEY WERE INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT WIRE AT FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA981719](https://openairdocs.org/sdr/AALA981719.md): Light · inoperative · Sep 23, 1998 · N872AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AFT CABIN INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA980743](https://openairdocs.org/sdr/AALA980743.md): Light · inoperative · Apr 10, 1998 · N872AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT VENTRAL STAIRWAY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT VENTRAL STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA980459](https://openairdocs.org/sdr/AALA980459.md): Switch · defective · Mar 7, 1998 · N872AA · Boeing 727223 · Landing Gear Position and Warning > MIA - FLT 617 - AFTER TAKEOFF, THE LANDING GEAR WAS RETRACTED AND THE MAIN LEFT GEAR DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT AIR INTERRUPTED AND RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. REPLACE LEFT MAIN LANDING GEAR DOOR LIMIT SWITCH AND CYCLED - [SDR AALA980232](https://openairdocs.org/sdr/AALA980232.md): Light · defective · Jan 29, 1998 · N872AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT CHECK, FIRST CLASS EMERGENCY FLOOR LIGHT FOUND INOPERATIVE. REPLACED LIGHT STRIP AT FIRST CLASS EMERGENCY FLOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) - [SDR AALA980223](https://openairdocs.org/sdr/AALA980223.md): Stringer · corroded · Jan 27, 1998 · N872AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - STR 28L CORROSION INSIDE HAT SECTION STA 595. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PAGE 4B AT STA 595 STR 28L. TST: 54,792 HOURS. CYCLES: 33,779. (X) - [SDR AALA980222](https://openairdocs.org/sdr/AALA980222.md): Stringer · corroded · Jan 27, 1998 · N872AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - OUTBOARD FLANGE OF STR 29L HAS CORROSION. INSTALLED REPAIR PER ESO 11697 DATED 1-13-98. TST: 54,792 HOURS. CYCLES: 33,779. (X) - [SDR AALA980221](https://openairdocs.org/sdr/AALA980221.md): Spar · corroded · Jan 27, 1998 · N872AA · Boeing 727223 · Wing Spar > TUL - CORROSION ON BOTTOM FLANGE OF FRONT SPAR CHORD ANGLE OUTBOARD OF NR 1 SLAT INBOARD TRACK OPENING. REMOVED CORROSION, INSTALLED REPAIR STRAP PER ESO 11697 DATED 1-10-98. (X) - [SDR AALA980185](https://openairdocs.org/sdr/AALA980185.md): Stringer · corroded · Jan 20, 1998 · N872AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - STR 28L CORRODED INSIDE HAT SECTION STA 594 TO STA 596. REMOVED CORRODED SECTION OF STRINGER. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PAGE 4B. TST: 54,792 HOURS. CYCLES: 33,779. (X) - [SDR AALA980184](https://openairdocs.org/sdr/AALA980184.md): Stringer · corroded · Jan 20, 1998 · N872AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - OUTBOARD FLANGE OF STR 29L HAS CORROSION. INSTALLED REPAIR PER ESO 11697 DATED 1-13-98. TST: 54,792. CYCLES: 33,779. (X) - [SDR AALA980117](https://openairdocs.org/sdr/AALA980117.md): Stringer · corroded · Jan 13, 1998 · N872AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - CORROSION ON UPPER OUTBOARD FLANGE STR 29L STA 950F TO STA 1000. REMOVED CORROSION AND INSTALLED REPAIR PER ESO 11697 DATED 1-2-90. TST: 54,792 HOURS. CYCLES: 33,779. (X) - [SDR AALA980116](https://openairdocs.org/sdr/AALA980116.md): Stringer · corroded · Jan 13, 1998 · N872AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - STA 680 STR 27R HAS CORROSION ON INBOARD AND OUTBOARD SIDES OF STRINGER. REPLACED STRINGER CAP, ALODINED, AND TREATED AFFECTED AREA PER SRM 51-10-2. (X) - [SDR AALA980115](https://openairdocs.org/sdr/AALA980115.md): Frame · corroded · Jan 13, 1998 · N872AA · Boeing 727223 · Fuselage Main, Frame > TUL - 2 INCH AREA OF CORROSION ON STA 740 FRAME AT ATTACH POINT TO FUSELAGE BELLY SKIN BL ZERO TO LBL 2. REPLACED T-ANGLE AT 740 28L-28R PER SRM 51-10-01, PAGE 04. (X) - [SDR AALA980114](https://openairdocs.org/sdr/AALA980114.md): Shear Tie · corroded · Jan 13, 1998 · N872AA · Boeing 727223 · Fuselage Miscellaneous Structure > TUL - CORROSION ON SHEAR TIE STA 720E, STR 25 TO STR 26R. REMOVED AND INSTALLED NEW SHEAR TIE PER SRM 51-30-2, PAGE 31. TST: 54,792 HOURS. CYCLES: 33,779. (X) - [SDR AALA980113](https://openairdocs.org/sdr/AALA980113.md): Shear Tie · corroded · Jan 13, 1998 · N872AA · Boeing 727223 · Fuselage Miscellaneous Structure > TUL - STA 720E SHEAR TIE CORROSION BETWEEN STR 25 AND STR 26R. REPLACED SHEAR TIE, REF: SRM 51-30-2 AND SRM 51-10-6. TST: 54,792 HOURS. CYCLES: 33,779. (X) - [SDR AALA980112](https://openairdocs.org/sdr/AALA980112.md): Shear Tie · cracked · Jan 13, 1998 · N872AA · Boeing 727223 · Fuselage Miscellaneous Structure > TUL - SHEAR TIES INBOARD AND OUTBOARD OF STR 26L, STA 580, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM 53-10-4, FIG 13. TST: 54,792 HOURS. CYCLES: 33,779. (X) - [SDR AALA980111](https://openairdocs.org/sdr/AALA980111.md): Stiffener · corroded · Jan 13, 1998 · N872AA · Boeing 727223 · Wing Miscellaneous Structure > TUL - CORROSION ON VERTICAL STIFFENER ON FRONT SPAR ABOVE MANUAL DEFUELING VALVE. REMOVED CORRODED STIFFENER AND REPLACED WITH NEW STIFFENER AT LES 160. TST: 54,792 HOURS. CYCLES: 33,779. (X) - [SDR AALA980110](https://openairdocs.org/sdr/AALA980110.md): Sill · corroded · Jan 13, 1998 · N872AA · Boeing 727223 · Fuselage Miscellaneous Structure > TUL - WEB AND CHORD ANGLE CORRODED 1 INCH IN DIAMETER, AREA BOTTOM SIDE 1176 CHORD ANGLE BL 6, VAULT DOOR LOWER SILL. REMOVED CORROSION PER SRM 51-10-6. INSTALLED DOUBLER IAW SRM 51-40-2. TST: 54,792 HOURS. CYCLES: 33,779. (X) - [SDR AALA980109](https://openairdocs.org/sdr/AALA980109.md): Floor Beam · corroded · Jan 13, 1998 · N872AA · Boeing 727223 · Fuselage Main, Floor Beam > TUL - CORROSION ON TOP OF FLOOR BEAM STA 380 RBL 5 - RBL 25. REMOVED CORROSION PER SRM 51-10-6. REPAIRED PER SRM 53-10-8, PAGES 9-A AND 9-B. TST: 54,792 HOURS. CYCLES: 33,779. (X) - [SDR AALA980108](https://openairdocs.org/sdr/AALA980108.md): Floor Beam · corroded · Jan 13, 1998 · N872AA · Boeing 727223 · Fuselage Main, Floor Beam > TUL - CORROSION ON TOP SIDE OF FLOOR BEAM STA 380 RBL 27 - RBL 65. REMOVED CORROSION PER SRM 51-10-6. REPAIRED DAMAGED AREA ON FLOOR BEAM PER SRM 53-10-8, PAGES 9-A AND 9-B. TST: 54,792 HOURS. CYCLES: 33,779. (X) - [SDR AALA980107](https://openairdocs.org/sdr/AALA980107.md): Skin · dented · Jan 13, 1998 · N872AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - DENT APPROXIMATELY 3 FEET AFT OF FORWARD ENTRY DOOR, LT SIDE APPROXIMATELY 3 INCHES BELOW CABIN FLOOR AND APPROXIMATELY 2 INCHES LONG. REMOVED DAMAGED PORTION OF SKIN AND INSTALLED REPAIR PER SRM 53-30-3. TST: 53,792 HOURS. CYCLES: 33,779. (X) - [SDR AALA980106](https://openairdocs.org/sdr/AALA980106.md): Skin · dented · Jan 13, 1998 · N872AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - DENT APPROXIMATELY 4 FEET AFT OF FORWARD ENTRY DOOR, LT SIDE, 6 INCHES BELOW CABIN FLOOR AND 2 INCHES LONG. REMOVED DAMAGED PORTION OF SKIN AT INSTALLED REPAIR PER SRM 53-30-3. TST: 54,792 HOURS. CYCLES: 33,779. (X) - [SDR AALA980105](https://openairdocs.org/sdr/AALA980105.md): Skin · gouged · Jan 13, 1998 · N872AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - CORROSION ON STR 26L, STA 577. SKIN GOUGED AT LAP UNDER STR 26L, STA 520 - STA 590. REMOVED DAMAGED SKIN AND INSTALLED FLUSH REPAIR SRM 53-30-3 FIG 6. REMOVED STRINGER AND INSTALLED NEW STRINGER AND SPLICE PER SRM 5-10-3 FIG 1. TST: 54,792 HOURS. C - [SDR AALA980104](https://openairdocs.org/sdr/AALA980104.md): Skin · corroded · Jan 13, 1998 · N872AA · Boeing 727223 · Wing, Plate/Skin > TUL - CORROSION ON LOWER WING SKIN IN AREA AT RIGHT PRIMARY HEAT EXCHANGE, RBL 8-40, STA 840. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER ESO 11697 DATED 1-6-98. TST: 54,792 HOURS. CYCLES: 33,779. (X) - [SDR AALA970373](https://openairdocs.org/sdr/AALA970373.md): Skin · corroded · Feb 24, 1997 · N872AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FOUND CORROSION ON SKIN BENEATH LEVELING COMPOUND. REPAIRED DAMAGED SKIN IAW 53-30-3, FIG 5. REPAIRED STRINGER IAW 53-10-3, FIG 1, DETAIL II AND REPLACED SHEAR TIE AT STATION 500 LBL 20. (M) - [SDR AALA970371](https://openairdocs.org/sdr/AALA970371.md): Shear Tie · corroded · Feb 24, 1997 · N872AA · Boeing 727223 · Fuselage Miscellaneous Structure > TUL - SHEAR TIE AT STATION 600 IS CORRODED ON FORWARD SIDE FROM 26L TO STRINGER 25L. REPLACED SHEAR TIE AT STATION 600, STRINGER 26L, TREATED AND PRIMED. (M) - [SDR AALA970374](https://openairdocs.org/sdr/AALA970374.md): Stringer · corroded · Feb 19, 1997 · N872AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - INSPECTION FOUND STRINGER AND SKIN CORRODED AT BS 500. REPLACED SECTION OF STRINGER AND FUSELAGE SKIN. (M) - [SDR 97ZZZM548](https://openairdocs.org/sdr/97ZZZM548.md): Skin · corroded · Feb 19, 1997 · N872AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - INSPECTION FOUND STRINGER AND SKIN CORRODED AT BS 500. REPLACED SECTION OF STRINGER AND FUSELAGE SKIN. REFERENCE AALA970374. - [SDR AALA970008](https://openairdocs.org/sdr/AALA970008.md): Skin · corroded · Jan 2, 1997 · N872AA · Boeing 727223 · Wing, Plate/Skin > TUL - INSPECTION FOUND SKIN CORRODED IN CENTER WING SECTION. CORROSION REPAIRED PER ESO 11697 DATED DECEMBER 18, 1996. TST: 52,299 HOURS. CYCLES, 32,469. (X) - [SDR AALA970002](https://openairdocs.org/sdr/AALA970002.md): Skin · corroded · Jan 2, 1997 · N872AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - CORROSION UNDER SKIN AT LEFT AFT LAV SERVICE PANEL AT BOTTOM (STR 22L AT STA 1170). INSTALLED REPAIR PER SRM 53-30-3. FIG 3A. TST: 52,299 HOURS. CYCLES, 32,469. (X) - [SDR AALA950171](https://openairdocs.org/sdr/AALA950171.md): Slide · scrapped · Feb 1, 1995 · N872AA · Boeing 727223 · Escape Slide > ORD - DURING SLIDE SHOP TEST DEPLOYMENT, EMERGENCY EVACUATION SLIDE SEAM AT GIRT TUBE FAILED. SCRAPPED EMERGENCY EVACUATION SLIDE. (W) - [SDR AALA950162](https://openairdocs.org/sdr/AALA950162.md): Slide · defective · Jan 31, 1995 · N872AA · Boeing 727223 · Escape Slide > ORD - DURING SHOP VISIT, FOUND 6 INCH SEAM SEPARATION AT GIRT BAR END OF EMERGENCY EVACUATION SLIDE. ROUTED FOR REPAIR. (W) ## 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 = 'N872AA' AND deregistration_id = 'N872AA-2004-11-15' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N872AA-2004-11-15/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, except the copies of manufacturers’ service documents, which belong to their rights holders.