# Service difficulty reports: N899AA, cancelled May 1, 2013

A list on [N899AA, cancelled May 1, 2013](https://openairdocs.org/deregistered/N899AA-2013-05-01.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 · 71 reports

- [SDR FOTR2111712809](https://openairdocs.org/sdr/FOTR2111712809.md): Skin · debonded · Aug 1, 2011 · N899AA · Boeing 727223 · Trailing Edge Flaps
  > LT INBD FOREFLAP T/E HAS AREA OF DEBONDED JUST INBD OF PREVIOUS REPAIR WBL 135.0. REPAIRED ON FASI WO 21117, NR 12809.
- [SDR FOTR2111712633](https://openairdocs.org/sdr/FOTR2111712633.md): Stringer · corroded · Jul 29, 2011 · N899AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > CORROSION ON OTBD SIDE OF STRINGER 28L AT BS 450. REPAIRED ON FASI WO 21117, NR 12633.
- [SDR FOTR2111712782](https://openairdocs.org/sdr/FOTR2111712782.md): Tab · delaminated · Jul 27, 2011 · N899AA · Boeing 727223 · Elevator, Tab Structure
  > LT ELEVATOR CONTROL TAB HAS A SMALL AREA OF DELAMINATION, REPAIRED ON FASI WO 21117, NR 12782.
- [SDR FOTR2111712656](https://openairdocs.org/sdr/FOTR2111712656.md): Frame · dented · Jul 25, 2011 · N899AA · Boeing 727223 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT HAS DENTS AT STA 1010 BETWEEN STR 25R AND 24R. REPAIRED ON FASI WO 21117, NR 12656.
- [SDR FOTR2111712657](https://openairdocs.org/sdr/FOTR2111712657.md): Frame · dented · Jul 25, 2011 · N899AA · Boeing 727223 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT- DENT ON FRAME STA 1030 BETWEEN STR 25R AND 24R. REPAIRED ON FASI WO 21117, NR 12657.
- [SDR FOTR2111712350](https://openairdocs.org/sdr/FOTR2111712350.md): Mount Bracket · cracked · Jul 25, 2011 · N899AA · Boeing 727223 · Leading Edge Devices
  > NR 6 SLAT ACTUATOR ATTACHED MOUNT BRACKET, ON SLAT INBD SIDE IS CRACKED, WS519.0. REPAIRED ON FASI WO 21117, NR 12350.
- [SDR FOTR2111712661](https://openairdocs.org/sdr/FOTR2111712661.md): Frame · dented · Jul 25, 2011 · N899AA · Boeing 727223 · Fuselage Main, Frame
  > AFT. CARGO COMPARTMENT- DENT ON FRAME AT STA 1010 AT STR 25L. REPAIRED ON FASI WO 21117, NR 12661.
- [SDR FOTR2111712345](https://openairdocs.org/sdr/FOTR2111712345.md): Bracket · cracked · Jul 25, 2011 · N899AA · Boeing 727223 · Leading Edge Devices
  > NR 7 SLAT ACTUATOR MOUNT INBD BRACKET ON SLAT IS CRACKED. REPAIRED ON FASI WO 21117, NR 12345.
- [SDR FOTR2111712726](https://openairdocs.org/sdr/FOTR2111712726.md): Bracket · cracked · Jul 25, 2011 · N899AA · Boeing 727223 · Leading Edge Devices
  > NR 7 SLAT ACTUATOR MOUNT OTBD BRACKET ON SLAT IS CRACKED, WS629.0. REPAIRED ON FASI WO 21117, NR 12726.
- [SDR FOTR2111712154](https://openairdocs.org/sdr/FOTR2111712154.md): Rib · cracked · Jul 25, 2011 · N899AA · Boeing 727223 · Leading Edge Devices
  > NR 4 SLAT INBD ACTUATOR ROD END ATTACH RIB IS CRACKED, WS383. REPAIRED ON FASI WO 21117, NR12154.
- [SDR FOTR2111712669](https://openairdocs.org/sdr/FOTR2111712669.md): Skin · bent · Jul 25, 2011 · N899AA · Boeing 727223 · Entrance Stairs
  > AFT AIRSTAIRS RT EXTERIOR SKIN SURFACE, AFT CORNER IS BENT, SEPARATING, AND PULLED FASTENERS STA 1383. REPAIRED ON FASI WO 21117, NR12669.
- [SDR FOTR2111712817](https://openairdocs.org/sdr/FOTR2111712817.md): Skin · debonded · Jul 25, 2011 · N899AA · Boeing 727223 · Trailing Edge Flaps
  > LT INBD FOREFLAP UPPER SURFACE HAS 6"DIAMETER DISBOND. REPAIRED ON FASI WO 21117, NR 12817.
- [SDR FOTR2111712507](https://openairdocs.org/sdr/FOTR2111712507.md): Frame · dented · Jul 25, 2011 · N899AA · Boeing 727223 · Fuselage Main, Frame
  > FWD CARGO COMPARTMENT- DENT AT STA 700 BETWEEN STR 23L AND 22L. REPAIRED ON FASI WO21117, NR 12507.
- [SDR FOTR2111712341](https://openairdocs.org/sdr/FOTR2111712341.md): Frame · dented · Jul 25, 2011 · N899AA · Boeing 727223 · Fuselage Main, Frame
  > FWD CARGO COMPARTMENT-DENT AT STA 520 LT, STR 23L. REPAIRED ON FASI WO 21117, NR 12341.
- [SDR FOTR2111712446](https://openairdocs.org/sdr/FOTR2111712446.md): Structure · cracked · Jul 13, 2011 · N899AA · Boeing 727 · Vertical Stabilizer
  > VERTICAL STAB, L/E HAS CRACKED DOUBLER TOP OF FWD SPAR CHORD CENTER, JUST AFT OF ELEVATOR CONTROL CABLE QUADRANT. REPAIRED ON FASI WO 21117, NR 12446.
- [SDR C8GA201000010A](https://openairdocs.org/sdr/C8GA201000010A.md): Actuator · malfunctioned · Jun 2, 2010 · N899AA · Boeing 727223 · Landing Gear Door Retract Section
  > WHILE ON APPROACH WITH THE GEAR HANDLE IN THE DOWN POSITION THE NLG UNSAFE LIGHT ILLUMINATED. CREW PERFORMED APPROPRIATE CHECKLIST AND RECYCLED GEAR WITH ALL INDICATIONS NORMAL. ACFT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED. R & R NLG LOCK A
- [SDR ABXR200908250021](https://openairdocs.org/sdr/ABXR200908250021.md): Stop Fitting · cracked · Aug 25, 2009 · N899AA · Boeing 727223 · Passenger/Crew Doors
  > AFTER A POST C-CHECK TEST FLIGHT A CRACK WAS VISUALLY DISCOVERED ON THE L1 DOOR STOP IN UPPER AFT CORNER. THE CRACKED DOOR STOP FITTING WAS REMOVED, THE NEW STOP POSITION, DRILLED AND INSTALLED. THE STOP WAS ADJUSTED TO THE AMM. THE PRESSURIZATION LEAK CHEC
- [SDR ABXR200908240020](https://openairdocs.org/sdr/ABXR200908240020.md): Vent Line · misrepaired · Aug 21, 2009 · N899AA · Boeing 727223 · Fuel Storage
  > DURING A C-CK ROUTINE VISUAL INSP, INCORRECT LT WING VENT LINE CLAMPS WERE FOUND UNDER PANELS 7216 AND 7215. THE CLAMPS WERE EVALUATED BY ENGINEERING. REMOVED ORIGINAL CLAMPS AND INSTALLED BACC10CC20S CLAMPS. ITEM RETURNED TO SERVICE
- [SDR ABXR200908240019](https://openairdocs.org/sdr/ABXR200908240019.md): Vent Line · chafed · Aug 21, 2009 · N899AA · Boeing 727223 · Fuel Storage
  > DURING A C-CK ROUTINE VISUAL INSP, THE RT WING VENT LINE WAS FOUND CHAFED UNDER PANEL 7608. THE DAMAGE WAS CUT OUT, THE REWORKED AREA TREATED WITH ALODINE AND A DOUBLER FABRICATED FROM 5052-0 0.040" AND COLD BONDED WITH BMS5-26 TYPE II. PRESSURE TEST PERFORME
- [SDR ABXR200908240018](https://openairdocs.org/sdr/ABXR200908240018.md): Support Angle · corroded · Aug 21, 2009 · N899AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING THE ROUTINE VISUAL INSP OF THE UPPER SIDE OF THE RT NLG DOGHOUSE WAS FOUND CORRODED. THE CORROSION WAS CLEANED AND FOUND OUT OF LIMITS. THE UPPER SIDE ANGLE WAS REMOVED AND FABRICATED FROM 7075 T6511 EXTRUSION. THE ANGLE WAS CORROSION PROTECTED AND RE
- [SDR ABXR200908240017](https://openairdocs.org/sdr/ABXR200908240017.md): Fitting · damaged · Aug 21, 2009 · N899AA · Boeing 727223 · Nacelle/Pylon, Attach Fittings
  > DURING THE REPETITIVE INSP NR 1 ENG PYLON SUPPORT FITTING IAW SB 2000-5410A0 2000-19-24, HOLES I, J, K, AND L WERE VISUALLY FOUND ELEGONGATED AND HOLES WERE FOUND PREVIOUSLY OVERSIZED TO MAX ALLOWABLE DIA. 0.2817 INCH. ENG MOUNT WAS REMOVED AND RE-INSTALLED A
- [SDR ABXR200908240016](https://openairdocs.org/sdr/ABXR200908240016.md): Skin · damaged · Aug 21, 2009 · N899AA · Boeing 727223 · Wing, Plate/Skin
  > DURING A C-CK INSP, THE LT WING SKIN AT THE NR 1 SLAT OTBD TRACK CUT-OUT WAS HEAVYILY DAMAGED AND CRACKED DUE TO THE UPPER FWD SLAT ROLLER NOT BEING CAPTURED BY THE ROLLER BOLT. THE DAMAGED AREA WAS CUT-OUT AND A NEW SKIN SECTION WAS FABRICATED WITH 2024 T-3
- [SDR ABXR200908240015](https://openairdocs.org/sdr/ABXR200908240015.md): Skin · cracked · Aug 21, 2009 · N899AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > DURING A C-CK REPETITIVE AD 2007-12-14 SB 727-53A0198, A CRACK WAS FOUND WITH EDDY CURRENT ON THE FWD ENTRY DOOR UPPER HINGE CUT-OUT. THE DAMAGE WAS CUTOUT TO A 0.70 INCH RADIUS, RE-INSPECTED WITH HFEC. FABRICATED SKIN FILLER FROM 2024 T-3 0.080 INCH, FABRIC
- [SDR ABXR200908240014](https://openairdocs.org/sdr/ABXR200908240014.md): Vent Line · dented · Aug 21, 2009 · N899AA · Boeing 727223 · Fuel Storage
  > DURING A C-CK ROUTINE VISUAL INSP, THE RT WING VENT LINE WAS FOUND CHAFED ABOVE PANEL 7615. THE DAMAGE WAS CUT OUT, THE REWORKED AREA TREATED WITH ALODINE AND A DOUBLER FABRICATED FROM 5052-0 0.040 INCH AND COLD BONDED WITH BMS5-26 TYPE II. PRESSURE TEST PERF
- [SDR ABXR200908240013](https://openairdocs.org/sdr/ABXR200908240013.md): Vent Line · dented · Aug 21, 2009 · N899AA · Boeing 727223 · Fuel Storage
  > DURING A C-CK ROUTINE VISUAL INSP, THE LT WING VENT LINE WAS FOUND CHAFED ABOVE PANEL 7612. THE DAMAGE WAS CUT OUT, THE REWORKED AREA TREATED WITH ALODINE AND A DOUBLER FABRICATED FROM 5052-0 0.040 INCH AND COLD BONDED WITH BMS5-26 TYPE II. PRESSURE TEST PERFO
- [SDR ABXR200908240012](https://openairdocs.org/sdr/ABXR200908240012.md): Line · dented · Aug 21, 2009 · N899AA · Boeing 727223 · Fuel Storage
  > DURING A C-CK ROUTINE VISUAL INSP, THE LT WING FUEL DUMP LINE WAS FOUND DENTED ABOVE PANEL 7215. THE DAMAGE WAS CUT OUT, THE REWORKED AREA TREATED WITH ALODINE AND A DOUBLER FABRICATED FROM 5052-0 0.040 INCH AND COLD BONDED WITH BMS5-26 TYPE II. PRESSURE TES
- [SDR ABXR200908240011](https://openairdocs.org/sdr/ABXR200908240011.md): Trunnion · corroded · Aug 21, 2009 · N899AA · Boeing 727223 · Fuselage, Landing Gear Attach Fittings
  > DURING ROUTINE C-CK MX, THE LT TRUNNION FITTING WAS FOUND CORRODED OUTSIDE OF MM LIMITS INSIDE THE INNER BORE. THE LT AND RT TRUNNION FITTINGS WERE REMOVED AND REPLACED WITH NEW TRUNNIONS. NO OTHER DAMAGE OR CORROSION NOTED THE ITEM WAS RETURNED TO SERVICE.
- [SDR ABXR200908240010](https://openairdocs.org/sdr/ABXR200908240010.md): Support Fitting · damaged · Aug 21, 2009 · N899AA · Boeing 727223 · Engine Mount Section
  > DURING THE REPETITIVE NR 3 ENG SUPPORT FITTING INSP IAW SB 2000-5410A01, AD 2005-19-24, HOLES I, J, K AND L WERE VISUALLY FOUND ELONGATED AND THE HOLES WERE FOUND PREVIOUSLY OVERSIZED TO MAX ALLOWABLE DIA. 0.2817 INCH. FABRICATED FREEZE PLUGS FROM 15-5PH H1025
- [SDR ABXR200908240009](https://openairdocs.org/sdr/ABXR200908240009.md): Gusset · cracked · Aug 21, 2009 · N899AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING THE ROUTINE VISUAL INSP OF A C-CK, THE MAIN CARGO DOOR JAMB LWR AFT GUSSET WAS FOUND GOUGED AND CRACKED IN SEVERAL PLACES. A REPLACEMENT GUSSET WAS FABRICATED FROM 2024 T3 0.063 INCH AND INSTALLED. THE ITEM WAS RETURNED TO SERVICE.
- [SDR ABXR200908240008](https://openairdocs.org/sdr/ABXR200908240008.md): Structure · corroded · Aug 21, 2009 · N899AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING THE ROUTINE VISUAL INSP OF A C-CK, THE SUBFLOOR WAS FOUND CORRODED OUT OF LIMITS. THE AREA WAS REPAIRED WITH A DOUBLER FABRICATED FROM 0.050 INCH, 2024 T-3. THE AREA WAS TREATED AND PRIMED FOR CORROSION PROTECTION. THE ITEM WAS RETURNED TO SERVICE.
- [SDR ABXR200908210007](https://openairdocs.org/sdr/ABXR200908210007.md): Floorbeam · cracked · Aug 21, 2009 · N899AA · Boeing 727223 · Fuselage Main, Floor Beam
  > DURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT INSP OF THE CARGO DOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.
- [SDR ABXR200908210006](https://openairdocs.org/sdr/ABXR200908210006.md): Floorbeam · cracked · Aug 21, 2009 · N899AA · Boeing 727223 · Fuselage Main, Floor Beam
  > DURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT INSP OF THE CARGO DOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.
- [SDR ABXR200908210005](https://openairdocs.org/sdr/ABXR200908210005.md): Floorbeam · cracked · Aug 21, 2009 · N899AA · Boeing 727223 · Fuselage Main, Floor Beam
  > DURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT INSP OF THE CARGO DOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.
- [SDR ABXR200908210004](https://openairdocs.org/sdr/ABXR200908210004.md): Floorbeam · cracked · Aug 21, 2009 · N899AA · Boeing 727223 · Fuselage Main, Floor Beam
  > DURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT INSP OF THE CARGO DOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.
- [SDR ABXR200908210003](https://openairdocs.org/sdr/ABXR200908210003.md): Floorbeam · cracked · Aug 21, 2009 · N899AA · Boeing 727223 · Fuselage Main, Floor Beam
  > DURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT INSP OF THE AEI CARGO DOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.
- [SDR ABXR200908210002](https://openairdocs.org/sdr/ABXR200908210002.md): Floorbeam · cracked · Aug 21, 2009 · N899AA · Boeing 727223 · Fuselage Main, Floor Beam
  > DURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT OF THE CARGO DOOR FLOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.
- [SDR ABXR200908200001](https://openairdocs.org/sdr/ABXR200908200001.md): Support · corroded · Aug 20, 2009 · N899AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING A HEAVY MX INSP EVENT, SUPPORT CLIP AT STR 26R CORRODED AT 545. REMOVED AND CLEANED SUPPORT CLIP AND FOUND OUT OF LIMITS. FABRICATED CLIP FROM 7075 T6 0.040 INCH. REINSTALLED CLIP. ITEM RETURNED TO SERVICE.
- [SDR C8GA20080012](https://openairdocs.org/sdr/C8GA20080012.md): Helicoil · damaged · Mar 25, 2008 · N899AA · Boeing 727223 · Turbine Engine Accessory Drive
  > FLT 708 FROM MCI TO PHX - DURING CRUISE OPERATION THE CAPTAIN WAS NOTIFIED THAT THE NR 1 ENGINE OIL QUANTITY WAS DECREASING. THE NR 1 ENGINE WAS SHUT DOWN AND EMERGENCY WAS DECLARED, THE AIRCRAFT DIVERTED TO ABQ WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT
- [SDR C8GA20070009](https://openairdocs.org/sdr/C8GA20070009.md): Control Valve · malfunctioned · Sep 14, 2007 · N899AA · Boeing 727223 · Engine Anti-Icing System
  > FLT 720 FROM TOL TO ATL, DURING CRUISE OPERATION THE AIRCRAFT EXPERIENCED ICING CONDITIONS WITH BOTH ENGINE AND WING ANTI-ICE ON, THE LOWER AFT CARGO SMOKE DETECTOR BELL RANG AND INDICATED A FIRE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCI
- [SDR C8GA20050017](https://openairdocs.org/sdr/C8GA20050017.md): Indicator · inoperative · Aug 17, 2005 · N899AA · Boeing 727223 · Airspeed/Mach Indicator
  > FLT 1828 FROM TOL TO RFD. NO #2 AIRSPEED INDICATION AT THE BEGINNING OF TAKE OFF ROLL. ABORTED TAKE OFF AND RETURNED TO GATE. REPLACED #2 AIRSPEED INDICATOR. LEAK AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR C8GA20050018](https://openairdocs.org/sdr/C8GA20050018.md): Adc · inoperative · Aug 15, 2005 · N899AA · Boeing 727223 · Air Data Computer
  > ON TAKEOFF ROLL, FO AIRSPEED INDICATION INOPERATIVE. FLAG CAME OUT AFTER STOP. CLEANED NR 2 ADC CONNECTOR PLUG AND RERACKED ADC. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR C8GA20050016](https://openairdocs.org/sdr/C8GA20050016.md): Oil Filter · contaminated · Jul 8, 2005 · N899AA · Boeing 727223 · Turbine Engine Oil System
  > IN CRUISE, NR 3 ENGINE LOW OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATED. REDUCED ENGINE POWER PER AOM PROCEDURES AND LIGHT EXTINGUISHED. LIGHT ILLUMINATED AGAIN. CREW SHUTDOWN ENGINE AS PRECAUTION. AIRCRAFT CONTINUED AND LANDED WITHOUT INCIDENT. FOUND DEB
- [SDR C8GA20050013](https://openairdocs.org/sdr/C8GA20050013.md): Compressor · stalled · May 12, 2005 · N899AA · Boeing 727223 · Turbine Engine Compressor Section
  > FLT 711 FROM DEN TO TOL, ON CLIMB FROM DEN, NR 1 ENGINE COMPRESSOR STALLED. AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT. AFTER RETURN TO BLOCKS, WITH ENGINE OPERATING AT 1.40 EPR, ENGINE COMPRESSOR STALLED AGAIN. PERFORMED BORESCOPE INSPECTION AND
- [SDR C8GA20050001](https://openairdocs.org/sdr/C8GA20050001.md): Line · split · Jan 13, 2005 · N899AA · Boeing 727223 · Hydraulic System, Main
  > AFTER TAKE OFF FROM SAN, "A" HYDRAULIC SYSTEM LOW LEVEL LIGHT ILLUMINATED FOLLOWED BY RAPID QUANTITY DEPLETION. TURNED OFF BOTH THE NR 1 AND 2 HYDRAULIC PUMPS AND RETURNED TO SAN. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. FOUND PRESSURE LINE SPLIT OPEN BETW
- [SDR C8GA20040009](https://openairdocs.org/sdr/C8GA20040009.md): Pump · failed · Jun 22, 2004 · N899AA · Boeing 727223 · Hydraulic Pump (Electric/Engine), Main
  > UPON DESCENT INTO KTOL, THE NR 2 ENGINE HYDRAULIC PUMP LOW-PRESSURE WARNING LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL CCIA AIRCRAFT OPERATIONS MANUAL CHECKLIST A-05-2, ADVISED ATC AND DECLARED AN EMERGENCY AND LANDED AT OUR FINAL DESTINATION IN TOL WITHOUT INC
- [SDR C8GA20040005](https://openairdocs.org/sdr/C8GA20040005.md): Sensor · failed · Jun 9, 2004 · N899AA · Boeing 727223 · Fire Detection
  > FLT 2161 FROM KDFW TO KMCI. AFTER TAKEOFF FROM DFW, THE LOWER AFT CARGO FIRE WARNING CAME ON. ALSO, THE NR 2 ENGINE DUCT OVERHEAT LIGHT ON IN FLIGHT. FOLLOW ALL CCIA AOM ABNORMAL PROCEDURES AND AIR TURNBACK TO DFW. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRA
- [SDR C8GA20040001](https://openairdocs.org/sdr/C8GA20040001.md): Tension Spring · weak · Feb 3, 2004 · N899AA · Boeing 727223 · Trailing Edge Flaps
  > DURING CLIMBOUT, KIAS 225 A/C EXPERIENCE AIRFRAME VIB. ADVISED CCIA FLT FOLLOWING & ATC OF PROBLEM & AIR TURNBACK. NO EMERGENCY ACTION TAKEN & A/C LANDED W/O INCIDENT. A/C INSPECTED & FOUND INBRD FLAPS ECCENTRICS NUT MISSING. REPLACED & ADJUST ECCENTRICS P
- [SDR C8GA20030018](https://openairdocs.org/sdr/C8GA20030018.md): Bearing · seized · Jun 20, 2003 · N899AA · Boeing 727223 · Leading Edge Devices
  > FLT 231 FROM MIA TO PTY. AFTER TAKEOFF, NR 2 SLAT DID NOT RETRACT. CYCLED SYSTEM TWICE STILLS NO RETRACTION. FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO MIA WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE NR 2 LEADING EDGE SLAT ACTUATOR WAS REPLACED. PE
- [SDR C8GA20030017](https://openairdocs.org/sdr/C8GA20030017.md): Transmitter · defective · Jun 3, 2003 · N899AA · Boeing 727223 · Trailing Flap Position Indicating System
  > FLT 001 FROM MIA TO PTO. ON ROTATION, STICK SHAKER ACTIVATED. UNABLE TO STOP STICK SHAKER IN FLIGHT, FUEL WAS DUMP AND THE FLIGHT RETURNED TO MIA. AIRCRAFT LANDED IN MIA WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE LEFT HAND INBOARD FLAP POSITION TRANSMITT
- [SDR C8GA2003002R](https://openairdocs.org/sdr/C8GA2003002R.md): Engine · bird ingestion · Jan 16, 2003 · N899AA · Boeing 727223 · Engine (Turbine/Turboprop)
  > Flight 737 from GDL to MTY. Bird strike on #2 engine after takeoff. Shutdown #2 engine and air turn back to GDL (Guadalajara, Mexico) aircraft landed without incident. Visual inspection revealed damage to the #2 engine fan blades. A special maintenance ferry f

Next page: https://openairdocs.org/deregistered/N899AA-2013-05-01/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 = 'N899AA' AND deregistration_id = 'N899AA-2013-05-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N899AA-2013-05-01/reports

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