# Service difficulty reports: N706AA, cancelled Feb 23, 2005 A list on [N706AA, cancelled Feb 23, 2005](https://openairdocs.org/deregistered/N706AA-2005-02-23.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AALA20011511](https://openairdocs.org/sdr/AALA20011511.md): Line · leaking · Jul 20, 2001 · N706AA · Boeing 727200 · Hydraulic Power System > DFW - FLT 1744 - EN ROUTE DFW-DTW - AIR INTERRUPTED WITH HYDRAULIC SYSTEM 'A' LOSS OF QUANTITY AND PRESSURE. RETURNED TO DFW LANDED WITHOUT INCIDENT. REPLACED LEFT ELEVATOR PACK HYDRAULIC LINE. SERVICED SYSTEM. LEAK AND OPERATIONAL CHECK OK. SYSTEM GROUND - [SDR AALA20010191](https://openairdocs.org/sdr/AALA20010191.md): Valve · defective · Feb 2, 2001 · N706AA · Boeing 727223 · Compressor Bleed Valve > IAD - FLT 371 - EN ROUTE IAD-DFW - DURING TAKEOFF, DETECTED A LOUD BANG AND VIBRATION AT CABIN. RETURNED IAD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 2 ENGINE BLEED VAVLE. ACCOMPLISHED HIGH POWER RUN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20001574](https://openairdocs.org/sdr/AALA20001574.md): Light · defective · Sep 20, 2000 · N706AA · Boeing 727223 · Emergency Lighting > DFW DURING OVERNIGHT MAINTENANCE FORWARD CABIN EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT FORWARD EMERGENCY EXIT LIGHT. SYSTEM GROUNDS CHECKED NORMAL OPERATION. - [SDR AALA20001403](https://openairdocs.org/sdr/AALA20001403.md): Skin · gouged · Aug 22, 2000 · N706AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FOUND 4 INCH LONG GOUGE IN FUSELAGE SKIN STATION 1027 BELOW STRINGER 20 RT. CHECKED GOUGE FOR CRACKS. NO CRACKS NOTED. INSTALLED FASTENER IN SKIN AT POINT WHERE GOUGE OUT OF LIMITS PER SRM 53-30-3 PART 2 FIG 20, AUTHORIZED BY ESO 11697 DATED 8/22/00. - [SDR AALA20001401](https://openairdocs.org/sdr/AALA20001401.md): Frame · cracked · Aug 17, 2000 · N706AA · Boeing 727223 · Fuselage Main, Frame > TUL - FOUND BELT FRAME AT STATION 480 CRACKED AT STRINGER 26R CUTOUT. INSTALLED DOUBLER TO BELT FRAME AT STATION 480 STRINGER 26R IAW SRM 51-40-2. (M) - [SDR AALA20001400](https://openairdocs.org/sdr/AALA20001400.md): Frame · misdrilled · Aug 17, 2000 · N706AA · Boeing 727223 · Fuselage Main, Frame > TUL - FOUND FAIL/SAFE ANGLE ON AFT SIDE OF BELT FRAME AT STATION 480 STRINGER 26 RT HAS DOUBLER DRILLED HOLE. INSTALLED DOUBLER ON FAIL/SAFE ANGLE AT STATION 480 STRINGER 26 RT IAW SRM 51-40-3. (M) - [SDR AALA20001402](https://openairdocs.org/sdr/AALA20001402.md): Strap · cracked · Aug 14, 2000 · N706AA · Boeing 727223 · Nacelle/Pylon Structure > TUL - FOUND CRACK TWO PLACES, 2 LAYER AT 7 O CLOCK APPROX.125, 3 LAYER AT 4 O CLOCK. REPAIRED PER ESO 11697 DATED 8-11-00. INSTALLED 2 STRAPS ONE.071, THE OTHER.063. (M) - [SDR AALA20001090](https://openairdocs.org/sdr/AALA20001090.md): Wire · broken · Jun 29, 2000 · N706AA · Boeing 727223 · Light System Wiring > DFW DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT ESCAPE PATH LIGHTS BETWEEN FIRST CLASS AND COACH INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY EXIT ESCAPE PATH LIGHTS BETWEEN FIRST CLASS AND COACH. SYSTEM GROUND CHECK NORMAL OPERATION. - [SDR AALA20000573](https://openairdocs.org/sdr/AALA20000573.md): Wire · damaged · Apr 1, 2000 · N706AA · Boeing 727223 · Light System Wiring > MIA - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. SPLICED WIRE AT FORWARD EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA991415](https://openairdocs.org/sdr/AALA991415.md): Skin · corroded · Sep 16, 1999 · N706AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - LEFT SIDE OF AC BAY ABOVE HEAT EXCHANGER SKIN IS CORRODED AT STATIONS 824 LBL 32, 826 LBL 44, 827 LBL 35 AND 826 LBL 32. REMOVED CORROSION, INSTALLED DOUBLER AND TRIPLER PER SRM 57-30-3. (M) - [SDR AALA991414](https://openairdocs.org/sdr/AALA991414.md): Skin · corroded · Sep 13, 1999 · N706AA · Boeing 727223 · Wing, Plate/Skin > TUL - RIGHT SIDE OF AC BAY ABOVE PRIMARY HEAT EXCHANGER SKIN HAS CORROSION. INSTALLED DOUBLER AND TRIPLER PER SRM 57-30-3. (M) - [SDR AALA991413](https://openairdocs.org/sdr/AALA991413.md): Skin · corroded · Sep 13, 1999 · N706AA · Boeing 727223 · Wing, Plate/Skin > TUL - RIGHT SIDE OF AC BAY ABOVE PRIMARY HEAT EXCHANGER SKIN HAS CORROSION. INSTALLED DOUBLER AND TRIPLER PER SRM 57-30-3. (M) - [SDR AALA991412](https://openairdocs.org/sdr/AALA991412.md): Skin · corroded · Sep 13, 1999 · N706AA · Boeing 727223 · Wing, Plate/Skin > TUL - FOUND LEFT SIDE OF AC BAY ABOVE PRIMARY HEAT EXCHANGER SKIN HAS CORROSION. INSTALLED DOUBLER AND TRIPLER PER SRM 57-30-3. (M) - [SDR AALA981943](https://openairdocs.org/sdr/AALA981943.md): Skin · corroded · Oct 15, 1998 · N706AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FOUND STATION 1050-1070 STRINGER 28R SKIN IS BULGING. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER FOR SKIN CUTOUT IAW SRM 53-30-3 FIG 3. (M) - [SDR AALA981942](https://openairdocs.org/sdr/AALA981942.md): Skin · corroded · Oct 15, 1998 · N706AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FOUND SKIN CORRODED UNDER LEVELING COMPOUND STATION 500-502, STRINGER 26-27L. REPAIRED AND INSTALLED DOUBLER AT STATION 500-502, STRINGER 26L TO 27L PER SRM 53-30-3. (M) - [SDR AALA981941](https://openairdocs.org/sdr/AALA981941.md): Stringer · corroded · Oct 15, 1998 · N706AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION AROUND RIVETS STRINGER 28R, 640-660, 685-690, 710-721. REMOVED CORRODED STRINGER AND INSTALLED FILLER AND SPLICE AT STATION 28R BETWEEN STATION 640 AND 721. (M) - [SDR AALA981940](https://openairdocs.org/sdr/AALA981940.md): Skin · corroded · Oct 15, 1998 · N706AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FOUND CORROSION ON SKIN AND AROUND FASTENERS STRINGER 27L, STATION 690-700. INSTALLED DOUBLER REPAIR PER SRM 53-30-5. INSTALLED INTERCOSTALS AND TRANSITION PANEL. (M) - [SDR AALA981938](https://openairdocs.org/sdr/AALA981938.md): Stringer · corroded · Oct 15, 1998 · N706AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - FOUND STATION 1012 STRINGER 29R HAS SKIN BULGING AROUND FASTENERS. INSTALLED NEW STRINGER SECTION AND SPLICE AS PER SRM 53-10-3 FIG 1, STRINGER SECTION BAC 1498-147. INSTALLED STATION 1011-1021. TEN INCHES OF BAC1498-131 REPAIR MATERIAL INSTALLED WITH - [SDR AALA981937](https://openairdocs.org/sdr/AALA981937.md): Stringer · corroded · Oct 15, 1998 · N706AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION ON BOTTOM OF STRINGER 27L STATION 504-506. CUT OUT CORRODED SECTION OF STRINGER. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M) - [SDR AALA981936](https://openairdocs.org/sdr/AALA981936.md): Skin · corroded · Oct 15, 1998 · N706AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - CORROSION ON INSIDE OF SKIN WHERE LEVELING COMPOUND REMOVED STATION 580, STRINGER 28L ABOUT 1.5 INCHES DIAMETER. CUT OUT CORROSION, INSTALLED REPAIR DOUBLER PER SRM 53-30-3. (M) - [SDR AALA981935](https://openairdocs.org/sdr/AALA981935.md): Frame · dented · Oct 15, 1998 · N706AA · Boeing 727223 · Fuselage Main, Frame > TUL - BELLFRAME DENTED STATION 720A, STRINGER 25R. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 51-40-3 FIG 1 WITH.1875 AND.25 INCH HI-LOCKS FASTENERS PAST DAMAGE DOUBLER THICKNESS.067. (M) - [SDR AALA981934](https://openairdocs.org/sdr/AALA981934.md): Angle · cracked · Oct 15, 1998 · N706AA · Boeing 727223 · Fuselage Miscellaneous Structure > TUL - FOUND BELOW FORWARD ENTRY DOOR FLOORBOARD BETWEEN FLOORBEAM STATION 312 AND 303, LBL 48, SUPPORT ANGLE CRACKED. REPLACED SUPPORT ANGLE. (M) - [SDR AALA981939](https://openairdocs.org/sdr/AALA981939.md): Stringer · corroded · Oct 13, 1998 · N706AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION IN BOTTOM OF STRINGER AT NUT PLATE STATION 702. CUT OUT DAMAGED AREA OF STRINGER. INSTALLED REPAIR SPLICE AND FILLER IAW SRM 53-10-3 FIG 1. (M) - [SDR AALA980639](https://openairdocs.org/sdr/AALA980639.md): Conductor · defective · Mar 29, 1998 · N706AA · Boeing 727223 · Emergency Lighting > ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN FIRST CLASS AND COACH CABIN INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT CONDUCTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA980402](https://openairdocs.org/sdr/AALA980402.md): Wire · broken · Feb 24, 1998 · N706AA · Boeing 727223 · Light System Wiring > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOOR LIGHTING AT PAX SEAT ROWS 7 TO 16 WAS INOPERATIVE. REPAIRED BROKEN WIRE AT EMERGENCY FLOOR LIGHT PAX SEAT ROWS 7 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA971993](https://openairdocs.org/sdr/AALA971993.md): Spar Cap · corroded · Oct 21, 1997 · N706AA · Boeing 727223 · Horizontal Stabilizer, Spar/Rib > TUL - HEAVY CORROSION ON UPPER T/E SPAR CAP AT OUTBOARD END OF RIGHT HORIZ STAB. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697, DATED 10-9-97. (M) - [SDR AALA971992](https://openairdocs.org/sdr/AALA971992.md): Stringer · cracked · Oct 21, 1997 · N706AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - FOUND STRINGER 18A CRACKED AT AFT FASTENER THROUGH STATION 940 CASTING. SPLICED IN NEW STRINGER 18A SECTION PER S/B 727-53-0172. (M) - [SDR AALA961739](https://openairdocs.org/sdr/AALA961739.md): Accessory Unit · defective · Nov 28, 1996 · N706AA · Boeing 727223 · Landing Gear Position and Warning > MIA - FLT 63 - AFTER TAKEOFF MIA WHEN LANDING GEAR RETRACTED, LEFT MAIN LANDING GEAR RED AND GREEN LIGHTS REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. CHECKED WIRING FOR LANDING GEAR DOWNLOCK SWITCH AND CHECKED LANDING - [SDR AALA961488](https://openairdocs.org/sdr/AALA961488.md): Trunnion · corroded · Oct 9, 1996 · N706AA · Boeing 727223 · Fuselage, Landing Gear Attach Fittings > TUL - FOUND LEFT NLG TRUNNION CORRODED. REMOVED AND REPLACED LEFT NOSE GEAR TRUNNION ASSEMBLY PER SRM 51-30-2 AND B-727 BP 65-88189. (M) - [SDR AALA961487](https://openairdocs.org/sdr/AALA961487.md): Skin · worn · Oct 9, 1996 · N706AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FOUND FUSELAGE SKIN CHAFFED AND WORN UNDER WING AND FUSELAGE PANEL 3342, STATION 720D AND 12 INCHES STRINGER 19 LEFT. CUT OUT SECTION AND INSTALLED FILLER AND DOUBLER PER SRM 53-30-3 PAGE 20-23. (M) - [SDR AALA961486](https://openairdocs.org/sdr/AALA961486.md): Skin · worn · Oct 9, 1996 · N706AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FOUND SKIN LAP 19R WORN BY WING LE FAIRING BEYOND LIMITS. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 14. (M) - [SDR AALA961485](https://openairdocs.org/sdr/AALA961485.md): Skin · cracked · Oct 9, 1996 · N706AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FOUND FUSELAGE SKIN CRACKED.375 INCH AT RIVET ON LEFT SIDE OF STRINGER 1 AND STATION 1095. REMOVED CRACKED SKIN AND INSTALLED DOUBLER PER SB 53-30-3 FIG 3 PAGES 1-14A. (M) - [SDR AALA961484](https://openairdocs.org/sdr/AALA961484.md): Stringer · corroded · Oct 9, 1996 · N706AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION ON STRINGER 28R BETWEEN STRINGER 720E AND 720F 6 INCHES, CORROSION ON STRINGER 28R BETWEEN STRINGER 720F AND 740 6 INCHES. BLENDED OUT CORROSION AND INSTALLED DOUBLER STRAP PER ESO 11697 DATED 9-9-96 AND 9-11-96. (M) - [SDR AALA961483](https://openairdocs.org/sdr/AALA961483.md): Stringer · cracked · Oct 9, 1996 · N706AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - FOUND STRINGER CRACKED. INSTALLED STRINGER SPLICE REPAIR PER AA MM 53-10-3. (M) - [SDR AALA961482](https://openairdocs.org/sdr/AALA961482.md): Stringer · corroded · Oct 9, 1996 · N706AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION ON STRINGER 28R AT BS 950E. INSTALLED STRINGER REPAIR PER ESO 11697, DATED 9-11-96. (M) - [SDR AALA961479](https://openairdocs.org/sdr/AALA961479.md): Clip · corroded · Oct 9, 1996 · N706AA · Boeing 727223 · Fuselage Miscellaneous Structure > TUL - FOUND CORNER CLIP CORRODED INSIDE DELTA BEAM RIGHT SIDE AT STATION 740. REMOVED AND INSTALLED NEW CLIP PER SRM 51-10-1. (M) - [SDR AALA960021](https://openairdocs.org/sdr/AALA960021.md): Skin · corroded · Jan 9, 1996 · N706AA · Boeing 727223 · Elevator, Plate/Skin > CORROSION AROUND RT OUTBOARD STATIC WICK MOUNT BRACKET. CUT OUT DELAMINATED AREA, APPLIED REPAIR PER SRM 55-20-3, PAGE 3, AND REINSTALLED STATIC BASE AND WICK. (X) ## 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 = 'N706AA' AND deregistration_id = 'N706AA-2005-02-23' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N706AA-2005-02-23/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.