# Service difficulty reports: N856AA, cancelled Jun 22, 2017

A list on [N856AA, cancelled Jun 22, 2017](https://openairdocs.org/deregistered/N856AA-2017-06-22.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 · 63 reports

- [SDR GAIA06019](https://openairdocs.org/sdr/GAIA06019.md): Frame · cracked · Mar 27, 2006 · N856AA · Boeing 727223 · Fuselage Main, Frame
  > DURING INSPECTION A FRAME WAS FOUND BENT AND CRACKED AT STA 580 BY STR 11R. ACCOMPLISHED FUSELAGE FRAME REPAIR TO STA 580 IAW SRM. AIRCRAFT RETURNED TO SERVICE. (K)
- [SDR GAIA06018](https://openairdocs.org/sdr/GAIA06018.md): Frame · cracked · Mar 27, 2006 · N856AA · Boeing 727223 · Fuselage Main, Frame
  > DURING INSPECTION A FRAME WAS FOUND BENT AND CRACKED AT STA 560 BY STR 11R. ACCOMPLISHED FUSELAGE FRAME REPAIR TO STA 560 IAW SRM. AIRCRAFT RETURNED TO SERVICE. (K)
- [SDR GAIA06017](https://openairdocs.org/sdr/GAIA06017.md): Stringer · corroded · Mar 27, 2006 · N856AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION, A 1 INCH SECTION OF STRINGER 27R WAS FOUND CORRODED AT STA 740. REPAIRED STRINGER 27R AT ST 740 IAW SRM. AIRCRAFT RETURNED TO SERVICE. (K)
- [SDR GAIA06016](https://openairdocs.org/sdr/GAIA06016.md): Stringer · corroded · Mar 27, 2006 · N856AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION A 1 INCH SECTION OF STRINGER 26L WAS FOUND CORRODED AT STA 740. REPAIRED STRINGER 26L AT STA 740 IAW SRM. AIRCRAFT RETURNED TO SERVICE. (K)
- [SDR GAIA06015](https://openairdocs.org/sdr/GAIA06015.md): Seat Track · corroded · Mar 27, 2006 · N856AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, A 14 INCH SECTION OF SEAT TRACK WAS FOUND CORRODED AT STA 740, LBL 24.75. (K)
- [SDR GAIA06014](https://openairdocs.org/sdr/GAIA06014.md): Longeron · cracked · Mar 27, 2006 · N856AA · Boeing 727223 · Wing, Longeron/Stringer
  > DURING INSPECTION A LONGERON WAS FOUND CRACKED AT WING STA 656 BY STR NR 2. ACCOMPLISHED LONGERON REPAIR TO WING STA 656 IAW SRM. AIRCRAFT RETURNED TO SERVICE. (K)
- [SDR GAIA06013](https://openairdocs.org/sdr/GAIA06013.md): Frame · cracked · Mar 27, 2006 · N856AA · Boeing 727223 · Fuselage Main, Frame
  > DURING INSPECTION, A FRAME WAS FOUND BENT AND CRACKED AT STA 600 BY STR 11R. ACCOMPLISHED FUSELAGE FRAME REPAIR TO STA 600 IAW SRM. AIRCRAFT RETURNED TO SERVICE. (K)
- [SDR GAIA05017OP](https://openairdocs.org/sdr/GAIA05017OP.md): Battery Pack · discharged · Apr 8, 2005 · N856AA · Boeing 727223 · Emergency Lighting
  > DURING PREFLIGHT, FOUND L-1 DOOR AND COCKPIT ENTRY DOOR EMERGENCY BATTERY PACKS DRAINED TO DIM ILLUMINATION. REPLACED BATTERY PACKS (2 EA). OPERATED EMERGENCY LIGHT SYSTEM AND FOUND OPERATING NORMALLY. OK FOR SUBSEQUENT FLIGHT. AIRCRAFT WAS RETURNED TO SER
- [SDR GAIA05015OP](https://openairdocs.org/sdr/GAIA05015OP.md): Light · inoperative · Mar 22, 2005 · N856AA · Boeing 727223 · Emergency Lighting
  > DURING PREFLIGHT, FOUND COCKPIT EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT IAW MM. AIRCRAFT WAS RETURNED TO SERVICE. (K)
- [SDR GAIA05003OP](https://openairdocs.org/sdr/GAIA05003OP.md): Indicator · shorted · Jan 28, 2005 · N856AA · Boeing 727223 · Weather Radar System
  > DURING DESCENT THE RADAR SCREEN FLARED BRIGHTLY, THE RADAR TCAS DISPLAY WENT OUT. SHORTLY AFTERWARD A STRONG ELECTRICAL SMELL WAS NOTICED. THE RADAR AND TCAS WERE TURNED OFF AND ASSOCIATED CIRCUIT BREAKERS WERE PULLED. THE SMELL DISSIPATED WITHIN A FEW MINU
- [SDR GAIA04174AOP](https://openairdocs.org/sdr/GAIA04174AOP.md): Skin · dented · Nov 29, 2004 · N856AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > NO FLIGHT: DURING WALK AROUND, A LARGE DENT WAS FOUND ON THE LT SIDE OF THE NOSE OF THE AIRCRAFT BELOW THE L2 WINDOW. THE AIRCRAFT WAS FERRIED FOR REPAIR.
- [SDR GAIA04057ST](https://openairdocs.org/sdr/GAIA04057ST.md): Skin · cracked · Mar 26, 2004 · N856AA · Boeing 727223 · Passenger/Crew Doors
  > DURING C-CHECK, FOUND CRACK ON THE FORWARD LOWER CORNER OF THE R1 DOOR SKIN. INSTALLED FILLER AND DOUBLER REPAIR IAW BOEING 727 SRM 52-00-03. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA04058ST](https://openairdocs.org/sdr/GAIA04058ST.md): Support · corroded · Mar 26, 2004 · N856AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND CORROSION ON THE REINFORCEMENT CHORD AT FUSELAGE STATION 1176.9 RBL 62.5. REMOVED AND REPLACED REINFORCEMENT CHORD IAW BOEING 727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA04064ST](https://openairdocs.org/sdr/GAIA04064ST.md): Angle · cracked · Mar 26, 2004 · N856AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND AN ANGLE CRACKED ON A PREVIOUS REPAIR TO THE AFT AIRSTAIR TORQUE BOX FS 1273 RBL 20. INSTALLED L ANGLE REPAIR IAW BOEING 727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA04059ST](https://openairdocs.org/sdr/GAIA04059ST.md): Stringer · corroded · Mar 26, 2004 · N856AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND CORROSION ON THE STRINGER JUST FORWARD OF FS 294.5 RIGHT SIDE FORWARD OF E/E AND NOSE WHEEL WELL. INSTALLED REPAIR IAW BOEING 727 SRM 53-10-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA04060ST](https://openairdocs.org/sdr/GAIA04060ST.md): Floorbeam · corroded · Mar 26, 2004 · N856AA · Boeing 727223 · Fuselage Main, Floor Beam
  > DURING C-CHECK, FOUND CORROSION ON THE FLOORBEAM AT FS 1130 RIGHT SIDE LOWER CHORD. INSTALLED REPAIR IAW BOEING 727 SRM 53-10-8. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA04063ST](https://openairdocs.org/sdr/GAIA04063ST.md): Angle · cracked · Mar 26, 2004 · N856AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND A Z-ANGLE CRACKED ON THE AFT AIRSTAIR TORQUE BOX FS 1273 RBL 20. INSTALLED Z-ANGLE REPAIR IAW BOEING 727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA04066ST](https://openairdocs.org/sdr/GAIA04066ST.md): Angle · cracked · Mar 26, 2004 · N856AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND AN ANGLE WAS CRACKED ON THE AFT AIRSTAIR ACTUATOR ATTACH POINT FS 1263 WL 200 RBL 22. INSTALLED ANGLE REPAIR IAW BOEING B727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA04067ST](https://openairdocs.org/sdr/GAIA04067ST.md): Fitting · cracked · Mar 26, 2004 · N856AA · Boeing 727223 · Horizontal Stabilizer Structure
  > DURING C-CHECK, THE HORIZONTAL STABILIZER FRONT SPAR GIMBAL A FRAME RIGHT UPPER FORWARD AND AFT CLEVIS HOLES WERE FOUND CRACKED. REMOVED AND REPLACED A FRAME GIMBAL SUPPORT IAW BOEING 727 AMM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA04038OP](https://openairdocs.org/sdr/GAIA04038OP.md): Light · inoperative · Feb 25, 2004 · N856AA · Boeing 727223 · Emergency Lighting
  > ON POST FLIGHT INSPECTION, FOUND THE L1 EMERGENCY EXIT LIGHT OUT. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA04039OP](https://openairdocs.org/sdr/GAIA04039OP.md): Accessory Unit · inoperative · Feb 25, 2004 · N856AA · Boeing 727223 · Main Landing Gear
  > FLT 211 - STL-FWA - ON DESCENT, THE AUTO PILOT DISENGAGED AND ALL INDICATOR TEST LIGHT ILLUMINATED. THE GEAR HANDLE WAS PLACED UP THEN OFF AND THE LIGHTS WENT BACK TO NORMAL. REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT. OPS CHECKED GOOD. THE AIRCR
- [SDR GAIA04010OP](https://openairdocs.org/sdr/GAIA04010OP.md): Bearing · seized · Feb 3, 2004 · N856AA · Boeing 727223 · Wheel/Ski/Float
  > ON POST FLIGHT INSPECTION, CREW FOUND NR 1 WHEEL AND TIRE ASSEMBLY MISSING FROM MAIN GEAR. THIS FOLLOWED A NORMAL LANDING WITH NO BRAKING PRIOR TO 70 KNOTS AS THE CREW HAD ANTICIPATED LESS THAN IDEAL BRAKING CONDITIONS. ACCOMPLISHED SPECIAL STRUCTURAL INSPEC
- [SDR GAIA03014OP](https://openairdocs.org/sdr/GAIA03014OP.md): Light · weak · Mar 13, 2003 · N856AA · Boeing 727223 · Emergency Lighting
  > L1 EMERGENCY EXIT LIGHT WEAK. REMOVED AND REPLACED L1 EMERGENCY EXIT LIGHT. OPS CHECK GOOD. (M)
- [SDR GAIA03002BOP](https://openairdocs.org/sdr/GAIA03002BOP.md): Duct · blown · Feb 3, 2003 · N856AA · Boeing 727223 · Engine Bleed Air System
  > FLT - 272 - MSP-MCI - AT APPROXIMATELY 200 FEET AGL THE NR 2 ENGINE HAD A FIRE INDICATION. THE CREW DECLARED AN EMERGENCY AND SHUTDOWN THE NR 2 ENGINE AS PER EMERGENCY PROCEDURES. UPON ENGINE SHUTDOWN, THE FIRE INDICATION EXTINGUISHED. AIRCRAFT PERFORMED AN
- [SDR GAIA02002OP](https://openairdocs.org/sdr/GAIA02002OP.md): Warning Light · illuminated · Jan 28, 2003 · N856AA · Boeing 727223 · Fire Detection
  > FLT 272 - MSP-MCI - AT APPROXIMATELY 200 FEET AGL, THE NR 2 ENGINE HAD A FIRE INDICATION. THE CREW DECLARED AN EMERGENCY AND SHUTDOWN THE NR 2 ENGINE AS PER EMERGENCY PROCEDURES. UPON ENGINE SHUTDOWN, THE FIRE INDICATION EXTINGUISHED. AIRCRAFT PERFORMED AN
- [SDR GAIA01044OP](https://openairdocs.org/sdr/GAIA01044OP.md): Fire Detector · malfunctioned · Feb 7, 2001 · N856AA · Boeing 727223 · Fire Detection
  > FLT 2025 - OAK-DEN - AFTER BLOCKING OUT FROM PARKING, THE APU FIRE WARNING SOUNDED. THE CREW PERFORMED EMERGENCY APU FIRE CHECKLIST AND ACTUATED THE APU FIRE HRD BOTTLE. THE AIRCRAFT RETURNED PARKING WITHOUT ANY FURTHER DIFFICULTIES. MAINTENANCE INSPECTED T
- [SDR GAIA00790](https://openairdocs.org/sdr/GAIA00790.md): Tire · failed · Nov 25, 2000 · N856AA · Boeing 727223 · Tire
  > FLT 706 - TOL-ROC - DURING APPROACH, UPON SELECTION OF FLAPS 2 DEGREES, LED''S FAILED TO DEPLOY. SELECTED FLAPS TO 0 AND BACK AGAIN TO 2 DEGREES. LED''S DEPLOYED. DURING LANDING ROL 3 MAIN TIRES FAILED. THE GEAR WAS PINNED AND TOWED FOR MAINTENANCE. UPON
- [SDR GAIA00691](https://openairdocs.org/sdr/GAIA00691.md): Light · detached · Nov 15, 2000 · N856AA · Boeing 727223 · Emergency Lighting
  > NO FLIGHT - DURING POST-FLIGHT INSPECTION AT JAX, DISCOVERED THE L-1 DOOR EMERGENCY LIGHT ASSEMBLY DETACHED. RE-SEATED THE L-1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR GAIA00715](https://openairdocs.org/sdr/GAIA00715.md): Stringer · cracked · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLIGHT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERD THAT THE BS 1330, LBL 4 VENTRAL STAIR STRINGER WAS CRACKED. ACCOMPLISHED REPAIR IAW BOEING SRM 52-10-1/53-10-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00714](https://openairdocs.org/sdr/GAIA00714.md): Stringer · cracked · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLIGHT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE BS 1330, RBL 4 VENTRAL STAIR STRINGER WAS CRACKED. ACCOMPLISHED REPAIR IAW BOEING SRM 52-10-1/53-10-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00713](https://openairdocs.org/sdr/GAIA00713.md): Stringer · cracked · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLIGHT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE BS 1303 VENTRAL STAIR STRINGER WAS CRACKED. ACCOMPLISHED REPAIR IAW BOEING SRM 52-10-1/53-10-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00712](https://openairdocs.org/sdr/GAIA00712.md): Frame · dented · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage Main, Frame
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE BS 560, FRAME AT STRINGER S26R WAS DENTED. ACCOMPLISHED REPAIR IAW BOEING SRM 51-40-3, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00711](https://openairdocs.org/sdr/GAIA00711.md): Frame · dented · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage Main, Frame
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE BS 580, FRAME AT STRINGER S6R WAS DENTED. ACCOMPLISHED REPAIR IAW BOEING SRM 51-40-3, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00710](https://openairdocs.org/sdr/GAIA00710.md): Frame · dented · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage Main, Frame
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLIGHT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE BS 600, FRAME AT STRINGER S6R WAS DENTED. ACCOMPLISHED REPAIR IAW BOEING SRM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00709](https://openairdocs.org/sdr/GAIA00709.md): Frame · dented · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage Main, Frame
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE BS 360, FRAME AT STRINGER S16L WAS DENTED. ACCOMPLISHED REPAIR IAW BOEING SRM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00708](https://openairdocs.org/sdr/GAIA00708.md): Frame · dented · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage Main, Frame
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE BS 380 FRAME AT STRINGER S29L WAS DENTED. ACCOMPLISHED REPAIR IAW BOEING SRM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00707](https://openairdocs.org/sdr/GAIA00707.md): Frame · dented · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage Main, Frame
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLIGHT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE BS 360 FRAME AT STRIGNER S9L WAS DENTED. ACCOMPLISHED REPAIR IAW BOEING SRM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00706](https://openairdocs.org/sdr/GAIA00706.md): Frame · cracked · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage Main, Frame
  > DURING ROUTINE HEAVY MAINTENANCE CHECK AT FLIGHT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE E & E DOOR FRAME WAS CRACKED.ACCOMPLISHED REPAIR IAW BOEING SRM 51-40-3 AND S/B 727-52-94. A/C WAS RETURNE TO SERVICE.
- [SDR GAIA00705](https://openairdocs.org/sdr/GAIA00705.md): Seat Track · cracked · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLIGHT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE BS520 SEAT TRACK, LBL 45 WAS CRACKED.ACCOMPLISHED REPAIR IAW BOEING SRM 53-10-5. A/C WAS RETURNED TO SERVICE.
- [SDR GAIA00704](https://openairdocs.org/sdr/GAIA00704.md): Frame · dented · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage Main, Frame
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLIGHT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE BS640 FRAME BETWEEN STRINGER S16R AND S17R WAS DENTED. ACCOMPLISED REPAIR IAW BOEING SRM 53-40-3, FIGURE 1. A/C WAS RETURNED TO SERVICE.
- [SDR GAIA00703](https://openairdocs.org/sdr/GAIA00703.md): Frame · dented · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage Main, Frame
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK, IT WAS DISCOVERED THAT THE BS 600 FRAME BETWEEN STRINGER S16R AND S17R WAS DENTED. ACCOMPLISHED REPAIR IAW BOEING SRM 53-40-3, FIGURE 1. THE A/C WAS RETURNED TO SERVICE.
- [SDR GAIA00702](https://openairdocs.org/sdr/GAIA00702.md): Frame · dented · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage Main, Frame
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT, IT WAS DISCOVERED THAT THE BS560 FRAME BETWEEN STRINGER S16R AND S17R WAS DENTED. ACCOMPLISHED REPAIR IAW BOEING SRM 53-40-3, FIGURE 1. A/C WAS RETURNED TO SERVICE.
- [SDR GAIA00701](https://openairdocs.org/sdr/GAIA00701.md): Frame · dented · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage Main, Frame
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLIGHT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE BS520 FRAME BETWEEN STRINGER S16R AND S17R WAS DENTED. ACCOMPLISHED REPAIR IAW BOEING SRM 53-40-3, FIGURE 1. A/C WAS RETURNED TO SERVICE.
- [SDR GAIA00700](https://openairdocs.org/sdr/GAIA00700.md): Seat Track · gouged · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLIGHT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE SEAT TRACK AT BS440, LBL 24 WAS GOUGED.ACCOMPLISHED REPAIR IAW BOEING SRM 53-10-2. A/C WAS RETURNED TO SERVICE.
- [SDR GAIA00699](https://openairdocs.org/sdr/GAIA00699.md): Seat Track · gouged · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLIGHT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE SEAT TRACK AT BS720 TO 740, LEFT SIDE WAS GOUGED. ACCOMPLISHED REPAIR IAW BOEING SRM 53-10-2. A/C WAS RETURNED TO SERVICE.
- [SDR GAIA00698](https://openairdocs.org/sdr/GAIA00698.md): Seat Track · gouged · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLIGHT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE SEAT TRACK AT BS 1170 TO 1110, RBL 45 WAS GOUGED.ACCOMPLISHED REPAIR IAW BOEING SRM 53-10-2. A/C WAS RETURNED TO SERVICE.
- [SDR GAIA00697](https://openairdocs.org/sdr/GAIA00697.md): Seat Track · gouged · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLIGHT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE SEAT TRACK AT BS760 LBL 48 WAS GOUGED.ACCOMPLISHED REPAIR IAW BOEING SRM 53-10-2. A/C WAS RETURNED TO SERVICE.
- [SDR GAIA00696](https://openairdocs.org/sdr/GAIA00696.md): Seat Track · gouged · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE HEAVY MAINTENANCE CHECK AT FLIGHT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE SEAT TRACK AT BS364 LBL48 WAS GOUGED.ACCOMPLISHED REPAIR IAW BOEING SRM 53-10-2. A/C WAS RETURNED TO SERVICE.
- [SDR GAIA00695](https://openairdocs.org/sdr/GAIA00695.md): Skin · dented · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLIGHT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE SKIN WAS DENTED AT BS950B, STRINGER S27L TO 28L. ACCOMPLISHED REPAIR IAW BOEING SRM 53-30-3, FIGURE 1. A/C WAS RETURNED TO SERVICE.
- [SDR GAIA00694](https://openairdocs.org/sdr/GAIA00694.md): Skin · dented · Nov 13, 2000 · N856AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > DURING A ROUTINE HEAVY MAINTENANCE CHECK AT FLIGHT STAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE SKIN WAS DENTED AT BS387-385 AND STRINGER S-18L. ACCOMPLISHED REPAIR IAW BOEING SRM 53-30-3, FIGURE 1. A/C WAS RETURNED TO SERVICE.

Next page: https://openairdocs.org/deregistered/N856AA-2017-06-22/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 = 'N856AA' AND deregistration_id = 'N856AA-2017-06-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N856AA-2017-06-22/reports

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