# Service difficulty reports: N854AA, cancelled Feb 21, 2018 A list on [N854AA, cancelled Feb 21, 2018](https://openairdocs.org/deregistered/N854AA-2018-02-21.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 · 79 reports - [SDR GAIA06002](https://openairdocs.org/sdr/GAIA06002.md): Frame · cracked · Feb 15, 2006 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING INSPECTION A FRAME WAS FOUND BENT AND CRACKED AT WSTA 560 BY STR 9R. ACCOMPLISHED FUSELAGE FRAME REPAIR TO STA 560, STR 9R IAW SRM. AIRCRAFT RETURNED TO SERVICE. (K) - [SDR GAIA06003](https://openairdocs.org/sdr/GAIA06003.md): Frame · cracked · Feb 15, 2006 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING INSPECTION A FRAME WAS FOUND BENT AND CRACKED AT STA 380 BETWEEN STR6,STR7L. ACCOMPLISHED FUSELAGE FRAME REPAIR TO STA 380 BY STR 7L IAW SRM. AIRCRAFT RETURNED TO SERVICE. (K) - [SDR GAIA06004](https://openairdocs.org/sdr/GAIA06004.md): Frame · cracked · Feb 15, 2006 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING INSPECTION A FRAME WAS FOUND BENT AND CRACKED AT STA 360 BETWEEN STR 7 AND 8L. ACCOMPLISHED FUSELAGE FRAME REPAIR TO STA 360 IAW SRM. AIRCRAFT RETURNED TO SERVICE. (K) - [SDR GAIA05028ST](https://openairdocs.org/sdr/GAIA05028ST.md): Spar · cracked · Oct 27, 2005 · N854AA · Boeing 727223 · Wing Spar > DURING B-CHECK A FUEL LEAK WAS FOUND ON THE FUSELAGE AT STA 740. INSPECTION REVEALED A CRACK ON THE WING CENTER SECTION SPAR WEB. THE WING SPAR WEB WAS REPAIRED IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) - [SDR GAIA05027ST](https://openairdocs.org/sdr/GAIA05027ST.md): Skin · cracked · Oct 27, 2005 · N854AA · Boeing 727223 · Fuselage Main, Plate/Skin > DURING B-CHECK A 1 INCH CRACK WAS FOUND ON THE FUSELAGE SKIN AT STA 530 STRINGER 26R ON THE LAP SEAM BELOW THE C-1 CARGO DOOR. THE SKIN WAS REPAIRED IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) - [SDR GAIA05020OP](https://openairdocs.org/sdr/GAIA05020OP.md): Light · inoperative · Apr 23, 2005 · N854AA · Boeing 727223 · Emergency Lighting > DURING PREFLIGHT, EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K) - [SDR GAIA04051OP](https://openairdocs.org/sdr/GAIA04051OP.md): Smoke Detector · inoperative · Mar 18, 2004 · N854AA · Boeing 727223 · Smoke Detection > DURING CRUISE, THE UPPER DECK CARGO SMOKE WARNING LIGHT CAME ON. NO SMOKE OBSERVED ON WALK THROUGH. CREW CONTINUED NORMAL OPERATIONS. REMOVED AND REPLACED CONTROL AMPLIFIER AND NR 6 SMOKE DETECTOR. OPS CHECK GOOD. AIRCRAF WAS RELEASED FOR SERVICE. (M) - [SDR GAIA04041OP](https://openairdocs.org/sdr/GAIA04041OP.md): Smoke Detector · inoperative · Feb 27, 2004 · N854AA · Boeing 727223 · Smoke Detection > FLT 734 - FWA-DFW - DURING CRUISE, THE UPPER DECK CARGO SMOKE WARNING LIGHT CAME ON. NO SMOKE OBSERVED ON WALK THROUGH. CREW CONTINUED NORMAL OPERATIONS. REMOVED AND REPLACED BAD NR 1 SMOKE DETECTOR. OPS CHECK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (M) - [SDR GAIA04032OP](https://openairdocs.org/sdr/GAIA04032OP.md): Actuator · out of adjust · Feb 21, 2004 · N854AA · Boeing 727223 · Drag Control Actuator > AIRCRAFT ROLLS TO THE LEFT WHEN THE SPEED BRAKES ARE EXTENDED. ADJUSTED THE NR 3 SPOILER ACTUATOR IAW THE BOEING MM. GROUND OPS CHECK OK. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA04031OP](https://openairdocs.org/sdr/GAIA04031OP.md): Actuator · malfunctioned · Feb 20, 2004 · N854AA · Boeing 727223 · Drag Control Actuator > AIRCRAFT ROLLS TO THE LEFT WHEN THE SPEED BRAKES ARE EXTENDED. FOUND NR 3 SPOILER ACTUATOR BYPASSING. REMOVED AND REPLACED THE NR 3 SPOILER ACTUATOR IAW THE BOEING MM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA03109OP](https://openairdocs.org/sdr/GAIA03109OP.md): Bolt · sheared · Sep 24, 2003 · N854AA · Boeing 727223 · Landing Gear Retraction/Extension System > FLT 714 - FWA-MCO - DURING GEAR EXTENSION ON APPROACH TO MCO THE LEFT MAIN GEAR DID NOT EXTEND. THE CREW PERFORMED THE ABNORMAL CHECKLIST AND MANUALLY LOWERED THE GEAR. AN UNEVENTFUL LANDING WAS MADE. THE LANDING GEAR WAS PINNED IN THE DOWN POSITION AND THE - [SDR GAIA02165OP](https://openairdocs.org/sdr/GAIA02165OP.md): Light · inoperative · Dec 16, 2002 · N854AA · Boeing 727223 · Emergency Lighting > DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE L1 FORWARD ENTRY EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA02048OP](https://openairdocs.org/sdr/GAIA02048OP.md): Light · inoperative · Apr 30, 2002 · N854AA · Boeing 727223 · Emergency Lighting > DURING PERIODIC SERVICE CHECK MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTING OVER THE LEFT NUMBER 1 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE UNSERVICEABLE LIGHT ASSEMBLY. OPERATIONAL CHECK PERFORMED OKAY. AIRCRAFT WAS RETURNED TOO SERVICE. - [SDR GAIA02026OP](https://openairdocs.org/sdr/GAIA02026OP.md): Light · inoperative · Mar 13, 2002 · N854AA · Boeing 727223 · Emergency Lighting > DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE FORWARD ENTRY EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKS NORMAL. THE AIRCRAFT WAS RTURNED TO SERVICE. ( - [SDR GAIA01244BOP](https://openairdocs.org/sdr/GAIA01244BOP.md): Battery · discharged · Jun 26, 2001 · N854AA · Boeing 727223 · Smoke Detection > FLT 1800 - MCO-CLT - AT 75K, GOT AFT LOWER FIRE WARNING INDICATION. CREW DECLARED AN EMERGENCY. AIRCRAFT MADE AN UNEVENTFUL REJECTED TAKEOFF (75K) IN MCO. REMOVED AND REPLACED LOWER AFT CARGO SMOKE DETECTORS BATTERIES. SMOKE DETECTOR SYSTEM TEST GOOD. AIR - [SDR GAIA01244AOP](https://openairdocs.org/sdr/GAIA01244AOP.md): Fire Warning · malfunctioned · Jun 1, 2001 · N854AA · Boeing 727223 · Fire Detection > FLT 1800 - MCO-CLT - AT 75K, GOT AFT LOWER FIRE WARNING INDICATION. CREW DECLARED AN EMERGENCY. AIRCRAFT MADE AN UNEVENTFUL REJECTED TAKEOFF (75K) IN MCO. DEFERRED LOWER CARGO COMPARTMENT FIRE DETECTION SYSTEM IAW B727 MEL 26-19. AIRCRAFT WAS INSPECTED AND - [SDR GAIA01040](https://openairdocs.org/sdr/GAIA01040.md): Wire · broken · Jan 30, 2001 · N854AA · Boeing 727223 · Landing Gear System Wiring > FLT 1807 - DEN-PHX - RED NOSE GEAR LIGHT ILLUMINATED, GREEN NOSE GEAR LIGHT NOT ILLUMINATED ON PRIOR TO LANDING. AIRCRAFT MADE AN UNEVENTFUL LANDING IN PHX. FOUND WIRE TO NOSE GEAR DOWN SWITCH BROKEN AT SPLICE. RE-SPLICED WITH ENVIROMENTAL SPLICE AND TIED B - [SDR GAIA00291](https://openairdocs.org/sdr/GAIA00291.md): Beam · corroded · May 24, 2000 · N854AA · Boeing 727223 · Fuselage Main, Structure > DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, FASTENER HOLES FOR RIGHT WALKING BEAM PANEL HAS CORROSION ON LANDING GEAR BEAM. REPAIRED BEAM IAW TIMCO REO SOO170. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00292](https://openairdocs.org/sdr/GAIA00292.md): Angle · corroded · May 24, 2000 · N854AA · Boeing 727223 · Fuselage Miscellaneous Structure > DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, STA 294 TO STA 303, RBL 17 INSIDE TORQUE BOX HAS CORROSION ON TOP ANGLE. REPAIRED ANGLE IAW TIMCO REO S000150. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00293](https://openairdocs.org/sdr/GAIA00293.md): Angle · corroded · May 24, 2000 · N854AA · Boeing 727223 · Fuselage Miscellaneous Structure > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, BODY STATION 294.5 TO BS 351.2 RIGHT WALKWAY SUPPORT ANGLE HAS CORROSION. REPAIRED ANGLED IAW SRM 51-30-2. A/C WAS RETURNED TO SERVICE. (M) - [SDR GAIA00294](https://openairdocs.org/sdr/GAIA00294.md): Beam · corroded · May 24, 2000 · N854AA · Boeing 727223 · Fuselage Main, Structure > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, LEFT WALKING BEAM PANEL ATTACH HOLES ON BEAM HAS CORROSION. REPAIRED BEAM IAW TIMCO REO SOO170. A/C RETURNED TO SERVICE. (M) - [SDR GAIA00284](https://openairdocs.org/sdr/GAIA00284.md): Light · inoperative · May 24, 2000 · N854AA · Boeing 727223 · Emergency Lighting > FLT 1807 - CLT-MIA - COCKPIT EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT. OPS CHECK GOOD IAW B727 MM. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR GAIA00285](https://openairdocs.org/sdr/GAIA00285.md): Angle · cracked · May 24, 2000 · N854AA · Boeing 727223 · Rudder Structure > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, TOP CAP ANGLE FORWARD SPAR RUDDER STATION 254 CAP ANGLE CRACKED. REPAIRED ANGLE IAW TIMCO REO S00188. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00286](https://openairdocs.org/sdr/GAIA00286.md): Skin · corroded · May 24, 2000 · N854AA · Boeing 727223 · Fuselage Main, Plate/Skin > DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, CORROSION ON FUSELAGE SKIN AT BS 440 CIRCUMFERENTIAL JOINT BETWEEN STRINGER 24L TO STRINGER 26L. REPAIRED FUSELAGE SKIN IAW SRM 53-30-3. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00287](https://openairdocs.org/sdr/GAIA00287.md): Skin · punctured · May 24, 2000 · N854AA · Boeing 727223 · Fuselage Main, Plate/Skin > DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, FUSELAGE STATION 550 9 INCHES ABOVE STATIC PORT RIGHT SIDE HAS PUNCTURE. REPAIRED STATIC PORT IAW SRM 53-30-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00288](https://openairdocs.org/sdr/GAIA00288.md): Stiffener · cracked · May 24, 2000 · N854AA · Boeing 727223 · Main Landing Gear Attach Section > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, RIGHT NLG TRUNNION SUPPORT VERTICAL STIFFENER CRACKED. REPAIRED TRUNNION SUPPORT STIFFENER IAW TIMCO REO S00168. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00289](https://openairdocs.org/sdr/GAIA00289.md): Fitting · corroded · May 24, 2000 · N854AA · Boeing 727223 · Main Landing Gear Attach Section > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, NLG RIGHT TRUNNION SUPPORT FITTING HAS PITTING CORROSION ON FLANGE. REPAIRED SUPPORT FITTING IAW TIMCO REO S00161. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00290](https://openairdocs.org/sdr/GAIA00290.md): Frame · corroded · May 24, 2000 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND. CORROSION ON LOWER FLANGE OF FRAME AT STA 950C STRINGER 29L. REPAIRED FRAME IAW SRM 53-10-4. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00273](https://openairdocs.org/sdr/GAIA00273.md): Floorbeam · damaged · Apr 28, 2000 · N854AA · Boeing 727223 · Fuselage Main, Floor Beam > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, ELONGATED HOLE IN FLOORBEAM AT STATION 360 LBL 45. REPAIRED FLOORBEAM PER IAW SRM 53-10-8. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00261](https://openairdocs.org/sdr/GAIA00261.md): Frame · dented · Apr 28, 2000 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, DENT IN BELT FRAME STATION 1090 BETWEEN STRINGER 26 AND 27R. REPAIRED FRAME PER IAW SRM 53-10-4. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00262](https://openairdocs.org/sdr/GAIA00262.md): Frame · dented · Apr 28, 2000 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, BS 520 FRAME DENTED JUST BELOW STRINGER 16R. REPAIRED FRAME PER IAW SRM 51-40-3. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00263](https://openairdocs.org/sdr/GAIA00263.md): Flap Track · corroded · Apr 28, 2000 · N854AA · Boeing 727223 · Trailing Edge Flaps > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, NR 4 FLAP TRACK FORWARD MOUNT BOLT HOLES HAS CORROSION. REPAIRED FLAP TRACK PER IAW S/B 727-57-0178. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00264](https://openairdocs.org/sdr/GAIA00264.md): Frame · misdrilled · Apr 28, 2000 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, BS 600 FRAME HAS BEEN DRILLED INTO NEAR STRINGER 16R. REPAIRED FRAME PER IAW SRM 51-20-1 AND 53-10-2. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00265](https://openairdocs.org/sdr/GAIA00265.md): Frame · misdrilled · Apr 28, 2000 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 700 STRINGER 16L FRAME HAS HOLES ON INBOARD CHORD. REPAIRED FRAME PER IAW SRM 51-40-3. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00266](https://openairdocs.org/sdr/GAIA00266.md): Frame · misdrilled · Apr 28, 2000 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, STATION 720E STRINGER 16L FRAME HAS HOLES ON INBOARD CHORD. REPAIRED FRAME PER IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00267](https://openairdocs.org/sdr/GAIA00267.md): Frame · cracked · Apr 28, 2000 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, STATION 1166 STRINGER 16L FRAME CRACKED. REPAIRED FRAME PER IAW 51-40-3. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00268](https://openairdocs.org/sdr/GAIA00268.md): Frame · misdrilled · Apr 28, 2000 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, STATION 1030 STRINGER 16L FRAME HAS FIGURE EIGHT HOLE. REPAIRED FRAME PER IAW TIMCO REO S00151. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00269](https://openairdocs.org/sdr/GAIA00269.md): Frame · dented · Apr 28, 2000 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, STATION 580 BETWEEN STRINGER 9R AND STRINGER 10R CIRCUMFERENTIAL DENTED. REPAIRED FRAME PER IAW SRM 53-10-4. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00270](https://openairdocs.org/sdr/GAIA00270.md): Frame · damaged · Apr 28, 2000 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, STATION 1148 STRINGER 16L FRAME HAS HOLES ON INBOARD CHORD. REPAIRED FRAME PER IAW SRM 53-10-2 AND 51-40-2. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00271](https://openairdocs.org/sdr/GAIA00271.md): Web · cracked · Apr 28, 2000 · N854AA · Boeing 727223 · Fuselage Miscellaneous Structure > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, WEB CRACKED BS 580 TO BS 600 STRINGER 29L. REPAIRED WEB PER IAW SRM 51-30-2. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00272](https://openairdocs.org/sdr/GAIA00272.md): Frame · misdrilled · Apr 28, 2000 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, TWO FIGURE EIGHT HOLES IN FRAME BS 560, STRINGER 26R. REPAIRED FRAME PER IAW TIMCO REO S00163. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00274](https://openairdocs.org/sdr/GAIA00274.md): Angle · corroded · Apr 28, 2000 · N854AA · Boeing 727223 · Fuselage Miscellaneous Structure > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, CORROSION ON ANGLE UNDER RIGHT SIDE SUPPORT ABOVE STRINGER 26R AT BS 735. REPAIRED ANGLE PER IAW SRM 51-30-5 AND 51-10-1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00242](https://openairdocs.org/sdr/GAIA00242.md): Frame · dented · Apr 27, 2000 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING LIGHT C-CHECK TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, FUSELAGE FRAME AT BS 360 IS DENTED JUST ABOVE FLOOR LEVEL LEFT SIDE. REPAIRED FRAME PER IAW SRM 51-20-2. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00221](https://openairdocs.org/sdr/GAIA00221.md): Stringer · punctured · Apr 25, 2000 · N854AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, SPLICE ON STRINGER 28R HAS PUNCTURE ON INBOARD UPPER RADIUS AFT OF BS 480 FORWARD PIT. REPAIRED STRINGER SPLICE IAW SRM 51-20-1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00222](https://openairdocs.org/sdr/GAIA00222.md): Frame · cracked · Apr 25, 2000 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, FUSELAGE FRAME AT BS 380 BETWEEN STRINGER 5 AND STRINGER 6 IS DENTED AND CRACKED. REPAIRED FRAME IAW SRM 53-10-4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00223](https://openairdocs.org/sdr/GAIA00223.md): Frame · cracked · Apr 25, 2000 · N854AA · Boeing 727223 · Fuselage Main, Frame > DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, FUSELAGE FRAME AT BS 400 BETWEEN STRINGER 5 AND STRINGER 6 DENTED AND CRACKED. REPAIRED FRAME IAW SRM 53-10-4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00224](https://openairdocs.org/sdr/GAIA00224.md): Shear Tie · cracked · Apr 25, 2000 · N854AA · Boeing 727223 · Fuselage Main, Structure > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, CRACKED SHEAR TIE ON FORWARD SIDE OF BELLY FRAME AT BS 1030, LBL 6. REPAIRED SHEAR TIE IAW SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00225](https://openairdocs.org/sdr/GAIA00225.md): Hinge Fitting · damaged · Apr 25, 2000 · N854AA · Boeing 727223 · Fuselage, Door Hinge > DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND LEFT MLG WING DOOR FORWARD HINGE FITTING ATTACH HOLES ELONGATED ON FLAP TRACK. REPAIRED HINGE FITTING IAW SB 727-57-0180. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00226](https://openairdocs.org/sdr/GAIA00226.md): Seat Track · gouged · Apr 25, 2000 · N854AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings > DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, SEAT TRACK GOUGED AT BS 763, LBL 24. REPAIRED SEAT TRACK IAW SRM 53-10-5. THE AIRCAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA00227](https://openairdocs.org/sdr/GAIA00227.md): Attach Fitting · damaged · Apr 25, 2000 · N854AA · Boeing 727223 · Horizontal Stabilizer, Attach Fittings > DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, RIGHT ELEVATOR NR 1 ATTACH FITTING ON HORIZONTAL HAS INBOARD HOLE ELONGATED. OUTBOARD HOLE ELONGATED AND LUG WORN. REPAIRED ELEVATOR ATTACH FITTING IAW TIMCO REO S00158. THE AIRCRAFT WA Next page: https://openairdocs.org/deregistered/N854AA-2018-02-21/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 = 'N854AA' AND deregistration_id = 'N854AA-2018-02-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N854AA-2018-02-21/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.