# Service difficulty reports: N6810, cancelled Jul 11, 2013

A list on [N6810, cancelled Jul 11, 2013](https://openairdocs.org/deregistered/N6810-2013-07-11.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 · 99 reports

- [SDR GAIAOP156](https://openairdocs.org/sdr/GAIAOP156.md): Clamp · loose · Nov 12, 2002 · N6810 · Boeing 727223 · Pneumatic Distribution System
  > FLIGHT 1111 - LAX-STL - AFTER TAKEOFF, WHILE AT CLIMB POWER THE FLIGHT CREW NOTICED THAT THE AFT BODY OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED AOM PROCEDURE AND THE LIGHT EXTINGUISHED. THE AIRCRAFT DIVERTED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. INSPECT
- [SDR GAIA01293OP](https://openairdocs.org/sdr/GAIA01293OP.md): Shutoff Valve · stuck · Aug 8, 2001 · N6810 · Boeing 727223 · Engine Anti-Icing System
  > FLT 2015 - BIL-DEN - DURING CLIMB-OUT FROM BIL, THE FLIGHT CREW NOTICED THE NR 1 ENGINE OIL TEMPERATURE SLOWLY RISING. A EMERGENCY WAS DECLARED AND THE ENGINE WAS SHUTDOWN. THE AIRCRAFT RETURNED TO BIL AND AN UNEVENTFUL LANDING WAS MADE. INVESTIGATION REVEA
- [SDR GAIA01107OP](https://openairdocs.org/sdr/GAIA01107OP.md): Hydraulic Line · cracked · Mar 8, 2001 · N6810 · Boeing 727223 · Hydraulic System, Main
  > FLT 7359 - OAK-MHR - DURING CLIMB, THE SYSTEM A HYDRAULIC QUANTITY STARTED TO DECREASE. THE CREW DECLARED AN EMERGENCY AND LANDED SAFELY IN MHR WITH NO FURTHER PROBLEMS. MAINTENANCE FOUND A CRACKED HYDRAULIC PRESSURE LINE TO THE RIGHT WING LEADING EDGE DEVIC
- [SDR GAIA00526](https://openairdocs.org/sdr/GAIA00526.md): Beam · corroded · Sep 12, 2000 · N6810 · Boeing 727223 · Fuselage, Landing Gear Attach Fittings
  > DSICREPANCY: DURING HEAVY CHECK FOUND LT LANDING GEAR BEAM HAS CORROSION AROUND 6 ATTACH HOLES, STA 854, LBL 87-114. REMOVED CORROSION AND REPAIRED LOWER SURFACE FO WALKING BEAM.
- [SDR GAIA00587](https://openairdocs.org/sdr/GAIA00587.md): Angle · corroded · Sep 11, 2000 · N6810 · Boeing 727223 · Fuselage Main, Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND: HORIZONTAL ANGLE CORRODED ON 950 BULKHEAD CLOSURE LBL70 WL165. CORRECTIVE ACTION: REMOVED & REPLACED HORIZONTAL ANGLE IAW B727 SRM 51-30-5 & 51-30-2
- [SDR GAIA00586](https://openairdocs.org/sdr/GAIA00586.md): Clip · cracked · Sep 11, 2000 · N6810 · Boeing 727223 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND: ANGLE CLIP CRACKED AT STA 1110 STR 26 AT C-3 DOOR WEB. CORRECTIVE ACTION: FABRICATED NEW CLIP IAW B727 SRM 51-20-1 SEE ATTACHED TRAVELER FOR FAB. DETAILS. INSTALLED CLIP IAW B727 SRN 51-30-2
- [SDR GAIA00585](https://openairdocs.org/sdr/GAIA00585.md): Floor Support · corroded · Sep 11, 2000 · N6810 · Boeing 727223 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND: FLOOR SUPPORT HAS SURFACE CORROSION STA 270 RBL3 TO RBL5 WL208. CORRECTIVE ACTION: REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW 727 SRM 51-10-6 & 53-10-1 REPLACED WITH EXTRUSION CHORD 65-17588-66 IAW 727 SRM 53-10-2
- [SDR GAIA00584](https://openairdocs.org/sdr/GAIA00584.md): Fitting · damaged · Sep 11, 2000 · N6810 · Boeing 727223 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND: REMOVE T-FITTINGS AT STA 560 RBL 45CORRECTIVE ACTION: REMOVED & REPLACED TEE-FITTING AT STA 560, RDL 46 TO 45 IAW REO & 00281
- [SDR GAIA00583](https://openairdocs.org/sdr/GAIA00583.md): Intercostal · damaged · Sep 11, 2000 · N6810 · Boeing 727223 · Electrical/Electronic Compartment Doors
  > DISCREPANCY: DURING HEAVY CHECK FOUND: E & E DOOR FORWARD RIGHT HAND INTERCOASTAL HOLES ALONGATED. CORRECTIVE ACTION: REMOVED DAMAGED AREA FROM INTERCOASTAL FABRICATED REPAIR PARTS IAW 727 SRM 51-40-3 TREATED, PRIMED & INSTALLED IAW 727 SRM 51-10-02, MM 51-20
- [SDR GAIA00582](https://openairdocs.org/sdr/GAIA00582.md): Pressure Panel · cracked · Sep 11, 2000 · N6810 · Boeing 727223 · Fuselage Main, Bulkhead
  > DISCREPANCY: DURING HEAVY CHECK FOUND: AFT OF FS 920 RBL4 TO 10 PRESSURE DECK WEB HAS CRACK INDICATION AT THE END OF 3 CORRUGATED BEAD'S. CORRECTIVE ACTION: FABRICATED DOUBLER FOR AFT PRESSURE DECK AND ALSO INSTALLED CLIPS & DOUBLER IAW B727 DRAWING #69-89360
- [SDR GAIA00581](https://openairdocs.org/sdr/GAIA00581.md): Pressure Panel · cracked · Sep 11, 2000 · N6810 · Boeing 727223 · Fuselage Main, Bulkhead
  > DISCREPANCY: DURING HEAVY CHECK FOUND: AFT OF FS 920 RBL4 TO PRESSURE DECK WEB HAS CRACK INDICATION AT THE END OF 3 CORRUGATION BEAD'S. CORRECTIVE ACTION: FABRICATED DOUBLER FOR AFT PRESSURE DECK AND ALSO INSTALLED CLIPS & DOUBLER IAW B727 DRAWING #69-89360 &
- [SDR GAIA00533](https://openairdocs.org/sdr/GAIA00533.md): Floor Support · corroded · Sep 8, 2000 · N6810 · Boeing 727223 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND STA 1090-1142.7, STR 27 RT FLOOR SUPPORT CORRODED AT THE NUTPLATES.
- [SDR GAIA00525](https://openairdocs.org/sdr/GAIA00525.md): Web · corroded · Sep 8, 2000 · N6810 · Boeing 727223 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING HEAVY CHECK, FOUND C-3 DOOR INNER SILL AND WEB CORRODED. REMOVED WEB, FABRICATED NEW PART AND INSTALLED.
- [SDR GAIA00523](https://openairdocs.org/sdr/GAIA00523.md): Frame · cracked · Sep 7, 2000 · N6810 · Boeing 727223 · Fuselage Main, Frame
  > DISCREPANCY: DURING HEAVY CHECK FORUND CRACK EXTENDING FURTHER THAN PREVIOUS REPAIR. BELOW C-3 DOOR, FORWARD OF BS 1090 FRAME, BETWEEN STR 26 AND 27 RT. FABRICATED AND INSTALLED FRAME REPAIR AT BS 1090.
- [SDR GAIA00617](https://openairdocs.org/sdr/GAIA00617.md): Seat Track · cracked · Sep 6, 2000 · N6810 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: DURING HEAVY CHECK FOUND: SEAT TRACK FITTING AT STA 740 LBL24.68 IS CRACKEDCORRECTIVE ACTION: INSTALLED NEW FITTING 69-14453-1 & BUSHINGS NAS75-4-112 & NAS538B6P012 IAW 727 SRM 51-30-2
- [SDR GAIA00615](https://openairdocs.org/sdr/GAIA00615.md): Structure · cracked · Sep 6, 2000 · N6810 · Boeing 727223 · Elevator Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND: RIGHT HAND ELEVATOR HAS CRACKED INTERNAL STRUCTURECORRECTIVE ACTION: REMOVED & REPLACED SKIN PANEL ON RIGHT HAND ELEVATOR FROM STA 136.5 TO 173.21 IAW B727 SRM 51-10-1 & 51-30-2 (REF N/R 26571 FOR MORE DETAILS FOR SKIN AS
- [SDR GAIA00614](https://openairdocs.org/sdr/GAIA00614.md): Structure · cracked · Sep 6, 2000 · N6810 · Boeing 727223 · Elevator Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND: RIGHT HAND ELEVATOR PNL HAS CRACKED INTERNAL STRUCTURE. CORRECTIVE ACTION: REMOVED & REPLACED PANEL IAW B727 SRM 51-30-2
- [SDR GAIA00613](https://openairdocs.org/sdr/GAIA00613.md): Structure · cracked · Sep 6, 2000 · N6810 · Boeing 727223 · Elevator Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND: RIGHT HAND ELEVATOR HAS CRACKED INTERNAL STRUCTURECORRECTIVE ACTION: REMOVED & REPLACED SKIN PANEL ON RIGHT HAND ELEVATOR FROM STA 136.5 TO 173.21 IAW B727 SRM 51-10-1 & 51-30-2 (REF N/R 26571 FOR MORE DETAILS FOR SKIN AS
- [SDR GAIA00612](https://openairdocs.org/sdr/GAIA00612.md): Shear Tie · damaged · Sep 6, 2000 · N6810 · Boeing 727223 · Fuselage Main, Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND: REMOVE 2 EACH SHEAR TIE STA 1110 BETWEEN STR 17L & 19L AND 2 EACH SHEAR TIE STA 1130 BETWEEN STR 17L & 19L. CORRECTIVE ACTION: REPLACED SHEAR TIES IAW B727 SRM 51-20-1 & 51-30-2
- [SDR GAIA00611](https://openairdocs.org/sdr/GAIA00611.md): Floorbeam · corroded · Sep 6, 2000 · N6810 · Boeing 727223 · Fuselage Main, Floor Beam
  > DISCREPANCY: DURING HEAVY CHECK FOUND: FLOOR BEAM CORRODED AT BS 560 RBL50CORRECTIVE ACTION: REPAIRED UPPER CAP ON FLOOR BEAM AT STA 560 FOR RBL40 TO RBL60 IAW REO S00281
- [SDR GAIA00610](https://openairdocs.org/sdr/GAIA00610.md): Skin · cracked · Sep 6, 2000 · N6810 · Boeing 727223 · Fuselage Main, Plate/Skin
  > DISCREPANCY: DURING HEAVY CHECK FOUND: BULGING CORROSION BETWEEN SKIN DOUBLER & TRIPLER & CRACKED AROUND RIVET AT BS 1115 JUST ABOVE STR 19L IN AFT CARGO COMPT.. CORRECTIVE ACTION: REPAIRED SKIN AT BS 1115 IAW REO S00283
- [SDR GAIA00609](https://openairdocs.org/sdr/GAIA00609.md): Door · cracked · Sep 6, 2000 · N6810 · Boeing 727223 · Electrical/Electronic Compartment Doors
  > DISCREPANCY: DURING HEAVY CHECK FOUND: E & E COMPARTMENT DOOR RIGHT HAND FRAME CRACKED FROM UNDER STOP FITTING UPPER EDGE (FORWARD & AFT CORNERS). CORRECTIVE ACTION: REMOVED DAMAGED AREA IN DOOR RIGHT HAND FRAME, FABRICATED REPAIR PARTS IAW 727 SRM 51-40-03 T
- [SDR GAIA00608](https://openairdocs.org/sdr/GAIA00608.md): Doubler · corroded · Sep 6, 2000 · N6810 · Boeing 727223 · Fuselage Main, Plate/Skin
  > DISCREPANCY: DURING HEAVY CHECK FOUND: S18A DOUBLER CORRODED AT BS870-880 RIGHTCORRECTIVE ACTION: REMOVED & FABRICATED DOUBLER IAW 727 SRM 51-20-1 & RS SRM 51-30-2
- [SDR GAIA00598](https://openairdocs.org/sdr/GAIA00598.md): Seat Track · worn · Sep 6, 2000 · N6810 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: DURING HEAVY CHECK FOUND: SEAT TRACKS WORN AT FORWARD END OF SECTIONS AT BS870 RBL24 & RBL45. CORRECTIVE ACTION: REMOVED DAMAGED SEAT TRACK AT RBL 45 & RBL 24.75 STA 870 & REPLACED CORRODED 8 FASTENERS, NUTS. FABRICATED NEW SEAT TRACK IAW B727 AR
- [SDR GAIA00597](https://openairdocs.org/sdr/GAIA00597.md): Bearing · worn · Sep 6, 2000 · N6810 · Boeing 727223 · Trailing Edge Flaps
  > DISCREPANCY: DURING HEAVY CHECK FOUND: NR 5 FLAP CARRIAGE THRUST BEARING SUPPORT FITTING WORN, BEARING RACE MOVES 1/4 INCH (AXIAL) IN FITTING. CORRECTIVE ACTION: REMOVED & REPLACED SUPPORT FITTING IAW SRM 51-30-2
- [SDR GAIA00596](https://openairdocs.org/sdr/GAIA00596.md): Clip · corroded · Sep 6, 2000 · N6810 · Boeing 727223 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING HEAVY CEHCK FOUND: CORROSION ON FRAME CLIP STA 1148 FORWARD SIDE BETWEEN STR 25 & 24R. CORRECTIVE ACTION: REPAIRED SHEAR TIE IAW B727 SRM 53-10-4 & REPAIR ANGLE IAW B727 SRM 51-40-4
- [SDR GAIA00595](https://openairdocs.org/sdr/GAIA00595.md): Clip · corroded · Sep 6, 2000 · N6810 · Boeing 727223 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND: S22R TO FS1148 FRAME CLIP HAS CORROSIONCORRECTIVE ACTION: REMOVED FRAME CLIP STA 1148 STR 22, FABRICATED & INSTALLED FRAME CLIP IAW 727 SRM 51-30-2, 51-20-1
- [SDR GAIA00594](https://openairdocs.org/sdr/GAIA00594.md): Verical Web · drill/holes · Sep 6, 2000 · N6810 · Boeing 727223 · Fuselage Main, Structure
  > DISCREPANCY: During heavy check found: Vertical web from Sta 1090R to 1142R at C-3 door cut out has drill starts & open holes in webCORRECTIVE ACTION: Vertical web found to be out of limits IAW B727 SRM 53-10-1. Removed web IAW B727 SRM 51-30-2. Fabricated new
- [SDR GAIA00593](https://openairdocs.org/sdr/GAIA00593.md): Floor Support · cracked · Sep 6, 2000 · N6810 · Boeing 727223 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND: FLOOR SUPPORT BRACKET CRACKED AFT OB SIDE STA 294 LBL14. CORRECTIVE ACTION: REMOVE, FABRICATED & INSTALLED FLOOR SUPPORT BRACKET STA 294 LBL14 IAW 727 SRM 51-30-2, 51-20-1, 51-30-5
- [SDR GAIA00592](https://openairdocs.org/sdr/GAIA00592.md): Floor Support · corroded · Sep 6, 2000 · N6810 · Boeing 727223 · Fuselage Main, Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND: FLOOR SUPPORT CORRODED ON TOP FLANG STA 298 & LBL13 CONTINGUING AFT PILLOWING FLOOR SKIN STA 304. CORRECTIVE ACTION: REMOVE, FABRICATED & INSTALLED ANGLE & FLOOR SUPPORT STA 298 LBL13 51-20-1, 51-30-2, 51-30-5
- [SDR GAIA00591](https://openairdocs.org/sdr/GAIA00591.md): Floor Support · cracked · Sep 6, 2000 · N6810 · Boeing 727223 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND: FLOOR SUPPORT CRACKED AT AFT ATTACH POINT THRU VERTICAL & HORIZONTAL FLANGES, STA 293 RBL22 WL208. CORRECTIVE ACTION: REMOVE, FABRICATED & INSTALLED ANGLE & FLOOR SUPPORT STA 293 RBL22 WL208 IAW 727 SRM 51-30-2, 51-20-1
- [SDR GAIA00588](https://openairdocs.org/sdr/GAIA00588.md): Angle · gouged · Sep 6, 2000 · N6810 · Boeing 727223 · Fuselage Main, Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND: FRAME TO INTERCOASTAL CLIP AT STA 1090 STR 25R HOLES DAMAGED & SEVERLY GOUGED. CORRECTIVE ACTION: REMOVED & FABRICATED NEW CLIP IAW 51-30-2 & 51-20-1 INSTALLED CLIP IAW B727 51-30-2
- [SDR GAIA00601](https://openairdocs.org/sdr/GAIA00601.md): Seat Track · corroded · Sep 4, 2000 · N6810 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: DURING HEAVY CHECK FOUND: SEAT TRACK CORRODED FROM BS640 TO BS660 RBL45. CORRECTIVE ACTION: REMOVED & REPLACED SEAT TRACK IAW B727 SRM 53-10-5, 51-30-2 BS 540-720 RBL45
- [SDR GAIA00600](https://openairdocs.org/sdr/GAIA00600.md): Seat Track · corroded · Sep 4, 2000 · N6810 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: DURING HEAVY CHECK FOUND: SEAT TRACK CORRODED FROM BS 660 TO BS 680 RBL45. CORRECTIVE ACTION: REMOVED & REPLACED SEAT TRACK IAW B727 SRM 53-10-5, 51-30-2
- [SDR GAIA00599](https://openairdocs.org/sdr/GAIA00599.md): Seat Track · corroded · Sep 4, 2000 · N6810 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: DURING HEAVY CHECK FOUND: SEAT TRACK SUPPORT CORRODED ON OUTBD SIDE AT BS 720A RBL46. CORRECTIVE ACTION: REMOVED & REPLACED SEAT TRACK IAW B727 SRM 53-10-5, 51-30-2
- [SDR GAIA00606](https://openairdocs.org/sdr/GAIA00606.md): Stringer · misdrilled · Aug 31, 2000 · N6810 · Boeing 727223 · Passenger/Crew Doors
  > DISCREPANCY: DURING HEAVY CHECK FOUND: STR 9L STA 500 STRINGER HAS MISS DRILL HOLES LOWER SIDE AT STRINGER TO FRAME CLIP. CORRECTIVE ACTION: FABRICATED NEW REPAIR PART. HAT CHANNEL & 4 NEW SPLICE STRAPS DOUBLERS IAW B727 SRM 53-10-3
- [SDR GAIA00605](https://openairdocs.org/sdr/GAIA00605.md): Window Frame · misdrilled · Aug 31, 2000 · N6810 · Boeing 727223 · Fuselage Main, Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND: DRILLED HOLE IN WINDOW FRAME STA 465 WL259 LEFT HAND. CORRECTIVE ACTION: DRILLED HOLE & INSTALLED RIVET IAW REO_ S00286 REV ORIG 8-29-00
- [SDR GAIA00604](https://openairdocs.org/sdr/GAIA00604.md): Shear Tie · cracked · Aug 31, 2000 · N6810 · Boeing 727223 · Fuselage Main, Structure
  > DISCREPANCY; DURING HEAVY CHECK FOUND: SHEAR TIE CRACKED AT STR 9L STA 500CORRECTIVE ACTION: REMOVED PANEL, REMOVED SHEAR TIE LOCATED & DRILLED NEW SHEAR TIE, ALODINED & PRIMED SHEAR TIE, INSTALLED SHEAR TIE & INSTALLED PANEL IAW B727 SRM 51-30-2 M/M 20-80-1 S
- [SDR GAIA00603](https://openairdocs.org/sdr/GAIA00603.md): Seat Track · corroded · Aug 30, 2000 · N6810 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: DURING HEAVY CHECK FOUND: SEAT TRACK AT BS585 RBL24 CORRODEDCORRECTIVE ACTION: REMOVED DAMAGED, FABRICATED SEAT TRACK & INSTALLED IAW B727 SRM 53-10-5 STA 580 TO 600.
- [SDR GAIA00602](https://openairdocs.org/sdr/GAIA00602.md): Frame · misdrilled · Aug 30, 2000 · N6810 · Boeing 727223 · Fuselage Main, Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND: CABIN FUSELAGE FRAME HAS 3 DOUBLE DRILLED HOLES & ONE OPEN HOLE AT BS 890 BETWEEN S7L & S9LCORRECTIVE ACTION: DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1 FABRICATED & INSTALLED REPAIR ANGLE IAW 727 SRM 53-10-4-51
- [SDR GAIA00607](https://openairdocs.org/sdr/GAIA00607.md): Structure · cracked · Aug 29, 2000 · N6810 · Boeing 727223 · Elevator Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND: RIGHT HAND ELEVATOR HAS CRACKED INTERNAL STRUCTURES. CORRECTIVE ACTION: REPAIRED INTERNAL STRUCTURE IN RIGHT HAND ELEVATOR IAW 727 SRM 55-20-3 WEIGHED PARTS & FASTENERS (113 GRAMS) REPAIR PERFORMED AT ELEVATOR STA 120.0
- [SDR GAIA00550](https://openairdocs.org/sdr/GAIA00550.md): Frame · dented · Aug 28, 2000 · N6810 · Boeing 727223 · Fuselage Main, Frame
  > DISCREPANCY: DURING HEAVY CHECK FOUND: CIRCUM FRAME DENTED TOP SIDE BS990 STR 26LCORRECTIVE ACTION: REPAIRED CIRCUME FRAME AT STA 990 STR 26L IAW B727 SRM 51-40-3
- [SDR GAIA00549](https://openairdocs.org/sdr/GAIA00549.md): Frame · dented · Aug 28, 2000 · N6810 · Boeing 727223 · Fuselage Main, Frame
  > DISCREPANCY: DURING HEAVY CHECK FOUND: CIRCUM FRAME DENTED TOP SIDE BS1010 STR 26LCORRECTIVE ACTION: CUR OUT DENTED AND FABRICATED REPAIR DOUBLER IAW B727 SRM 53-10-2. INSTALLED DOUBLER REPAIR BS 1010 FRAME STR 26L IAW B727 SRM 51-40-3
- [SDR GAIA00548](https://openairdocs.org/sdr/GAIA00548.md): Frame · gouged · Aug 28, 2000 · N6810 · Boeing 727223 · Fuselage Main, Frame
  > DISCREPANCY: DURING HEAVY CHECK FOUND: STA 560 RIGHT HAND FRAME GOUGED 2 SPOTS 4 INCHES UP FROM FLOOR IN BOARD FACE & 5 INCHES UP ON FORWARD FACE. CORRECTIVE ACTION: BLENDED GOUGE & FOUND TO BE OUT OF LIMITS, REMOVED GOUGED AREA FABRICATED & INSTALLED REPAIR
- [SDR GAIA00547](https://openairdocs.org/sdr/GAIA00547.md): Frame · cracked · Aug 28, 2000 · N6810 · Boeing 727223 · Fuselage Main, Frame
  > DISCREPANCY: DURING HEAVY CHECK FOUND: FRAME CRACKED ON I/B FACE BETWEEN STR 16 R & 17R STA 540. CORRECTIVE ACTION: REPAIRED IAW B727 SRM 51-40-3
- [SDR GAIA00546](https://openairdocs.org/sdr/GAIA00546.md): Frame · dented · Aug 28, 2000 · N6810 · Boeing 727223 · Fuselage Main, Frame
  > DISCREPANCY: DURING HEAVY CHECK FOUND:FRAME DENTED STA 540 BETWEEN STR 15R & 16RCORRECTIVE ACTION: REPAIRED IAW B727 SRM 51-40-3
- [SDR GAIA00544](https://openairdocs.org/sdr/GAIA00544.md): Frame · damaged · Aug 28, 2000 · N6810 · Boeing 727223 · Fuselage Main, Frame
  > DISCREPANCY: DURING HEAVY CHECK FOUND: FRAME AT STA 520 HAS A BONE WHEEL MARK ON RADIUS AT STR 7R CORRECTIVE ACTION: DAMAGE OUT OF LIMITS IAW B727 SRM 53-10-1 REPAIRED FRAME IAW B727 SRM53-10-4
- [SDR GAIA00543](https://openairdocs.org/sdr/GAIA00543.md): Frame · dented · Aug 28, 2000 · N6810 · Boeing 727223 · Fuselage Main, Frame
  > DISCREPANCY: DURING HEAVY CEHCK FOUND: FRAME DENTED STA 550 BETWEEN STR 5 & 6RCORRECTIVE ACTION: REMOVED DAMAGED & REPAIRED IAW B727 SRM 53-10-4 FIG 2
- [SDR GAIA00542](https://openairdocs.org/sdr/GAIA00542.md): Frame · dented · Aug 28, 2000 · N6810 · Boeing 727223 · Fuselage Main, Structure
  > DISCREPANCY: During Heavy Check found: Frame dented Sta 600 between Str 5 & 6RCORRECTIVE ACTION: Removed damaged and repaired IAW B727 SRM 53-10-4 Fig 2
- [SDR GAIA00541](https://openairdocs.org/sdr/GAIA00541.md): Stringer · cracked · Aug 28, 2000 · N6810 · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > DISCREPANCY: DURING HEAVY CEHCK FOUND:STR 3L CRACKED BEYOND STOP DRILL INTO RADIUS OF STRINGER STA 400CORRECTIVE ACTION: REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS & INSTALLED IAW B727 SRM 51-30-2 & 53-10-3

Next page: https://openairdocs.org/deregistered/N6810-2013-07-11/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 = 'N6810' AND deregistration_id = 'N6810-2013-07-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N6810-2013-07-11/reports

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