# Service difficulty reports: N6806, cancelled May 10, 2007

A list on [N6806, cancelled May 10, 2007](https://openairdocs.org/deregistered/N6806-2007-05-10.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 · 80 reports

- [SDR GAIA04089OP](https://openairdocs.org/sdr/GAIA04089OP.md): Light · inoperative · Jul 22, 2004 · N6806 · Boeing 727223 · Emergency Lighting
  > ON PREFLIGHT, FOUND EXIT LIGHT IN COCKPIT INOPERATIVE. REMOVED EXIT LIGHT FOR CHARGING AND INSTALLED SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR GAIA04072](https://openairdocs.org/sdr/GAIA04072.md): Rod · unserviceable · May 6, 2004 · N6806 · Boeing 727223 · Landing Gear Retraction/Extension System
  > AT DEPARTURE, LT MAIN GEAR FAILED TO RETRACT. THIS WAS VERIFIED BY THE TOWER. CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT WHERE A LANDING WAS MADE WITHOUT INCIDENT. REMOVED AND REPLACED AFT RADIUS ROD ON OB DOOR LT MAIN WHEEL WELL. DOOR FIT AND OPS CHECK,
- [SDR GAIA04007OP](https://openairdocs.org/sdr/GAIA04007OP.md): Light · inoperative · Jan 23, 2004 · N6806 · Boeing 727223 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE COCKPIT DOOR EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA03105](https://openairdocs.org/sdr/GAIA03105.md): Frame · dented · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Frame
  > DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 1010 HAS A DENT ABOVE STRINGER 25R. REF FASI N/R 53289 CUT OUT DAMAGE, 7 INCHES BY 3.5 INCHES DOUBLER REPAIR PER B727 SRM 51-40-3, FIGURE 1 AND 53-10-2 FIGURE 5. (M)
- [SDR GAIA03094](https://openairdocs.org/sdr/GAIA03094.md): Floorbeam · corroded · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Floor Beam
  > DURNG B-2 CHECK, FOUND MAIN CABIN FLOORBEAM ANGLE CORRODED LBL 60 BS 848. REF FASI N/R 53138 ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 51-40-3 AND 53-10-1 FIG 1. (M)
- [SDR GAIA03093](https://openairdocs.org/sdr/GAIA03093.md): Floorbeam · corroded · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Floor Beam
  > DURING B-2 CHECK, FOUND MAIN CABIN FLOORBEAM UPPER 'T' CAP CORRODED RBL 45.5 BS 765 TO 848. REF FASI N/R 53136 REPLACED DAMAGED 'T' CAP P/N 65-16279-10 PER B-727 SRM 51-30-5, AND 51-30-2. (M)
- [SDR GAIA03092](https://openairdocs.org/sdr/GAIA03092.md): Stringer · cracked · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > DURING B-2 CHECK, FOUND MAIN CABIN STRINGER 15 RT CRACKED AT AFT SIDE OF BS 720B. REF FASI N/R 53135, ACCOMPLISHED STRINGER REPAIR PER B727 SRM 53-10-3 TABLE ONE. (M)
- [SDR GAIA03106](https://openairdocs.org/sdr/GAIA03106.md): Frame · dented · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Frame
  > DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 950E HAS A DENT BY STRINGER 25L. REF FASI N/R 53292. FABRICATED DOUBLER REPAIR FROM 7075-T6,.080, DIMENSIONS 17.75 INCH BY 2.5 INCHES REPAIRED IAW B727 SRM 51-10-2. (M)
- [SDR GAIA03086](https://openairdocs.org/sdr/GAIA03086.md): Frame · dented · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Frame
  > DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 380 HAS A DENT IN THE RADIUS BELOW STRINGER 6LT. REF FASI N/R 53129, CUT OUT DAMAGE 4.75 BY 1.25, DOUBLER REPAIR PER B727 SRM 51-40-3 AND 53-10-4 FIG 1. (M)
- [SDR GAIA03091](https://openairdocs.org/sdr/GAIA03091.md): Stringer · cracked · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > DURING B-2 CHECK FUOND MAIN CABIN STRINGER 15 LT CRACKED FORWARD OF BS 720C. REF FASI N/R 53134 ACCOMPLISHED STRINGER REPAIR PER B727 SRM 53-10-3 TABLE ONE. (M)
- [SDR GAIA03090](https://openairdocs.org/sdr/GAIA03090.md): Frame · dented · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Frame
  > DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 600 DENTED IN RADIUS BELOW STRINGER 16RT. REF FASI N/R 53133, ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 51-40-3 FIG 1. (M)
- [SDR GAIA03089](https://openairdocs.org/sdr/GAIA03089.md): Frame · dented · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Frame
  > DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 580 DENTED IN RADIUS BELOW STRINGER 16RT. REF FASI N/R 53132 ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 51-40-3 FIG 1. (M)
- [SDR GAIA03088](https://openairdocs.org/sdr/GAIA03088.md): Frame · cracked · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Frame
  > DURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 560 CRACKED BELOW STRINGER 16RT. REF FASI N/R 53131 CUTOUT DAMAGE, ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 51-40-3 FIG 1. (M)
- [SDR GAIA03085](https://openairdocs.org/sdr/GAIA03085.md): Flap Track · cracked · Sep 10, 2003 · N6806 · Boeing 727223 · Trailing Edge Flaps
  > DURING B-2 CHECK, FOUND NR 5 FLAP TRACK SPACER BLOCK CRACKED AT WBL 124. REF FASI N/R 50408, INSTALLED OVERSIZE FASTENERS IAW S/B 727-57-136 REV 1, FIGURE 2. (M)
- [SDR GAIA03084](https://openairdocs.org/sdr/GAIA03084.md): Frame · cracked · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Frame
  > DURING B-2 CHECK, FOUND FUSELAGE FRAME AT BS 950D CRACKED, ABOVE STRINGER 22R. REF FASI N/R 50407, FABRICATED REPAIR DOUBLER FROM 7075-T6,.080, DIMENSIONS 9 INCHES BY 3 INCHES. REPAIRED IAW S-727 SRM 51-40-3, FIGURE 1. (M)
- [SDR GAIA03083](https://openairdocs.org/sdr/GAIA03083.md): Seat Track · corroded · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING B-2 CHECK, FOUND MAIN CABIN SEAT TRACK CORRODED AT BS 344 TO BS 360, RBL 45.5. REF FASI N/R 50403. FABRICATED REPAIR FROM BAC 1520-792 MATERIAL. LENGTH 14 INCHES REPAIRED IAW B727 SRM 53-10-05, FIGURE 7 AND 53-10-2, FIGURE 7. (M)
- [SDR GAIA03096](https://openairdocs.org/sdr/GAIA03096.md): Floorbeam · corroded · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Floor Beam
  > DURING B-2 CHECK, FOUND FORWARD LAVATORY FLOORBEAM UPPER 'T' CORRODED BS 344 RBL 25 TO RBL 50 ALSO AT LBL 25. REF FASI N/R 53195, REPLACED FLOORBEAM UPPER 'T' CAP RBL 60 TO LBL 60 PER B77 53-10-8 FIG 3 AND 51-30-2. (M)
- [SDR GAIA03099](https://openairdocs.org/sdr/GAIA03099.md): Beam · cracked · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Structure
  > DURING B-2 CHECK, FOUND BS 1183 VERTICAL BEAM CRACKED LBL 36 INCHES WL 250. REF FASI N/R 53249, INSTALLED REPAIR PER S/B 727-53-0192 REV 2. (M)
- [SDR GAIA03098](https://openairdocs.org/sdr/GAIA03098.md): Rib · cracked · Sep 10, 2003 · N6806 · Boeing 727223 · Elevator, Spar/Rib
  > DURING B-2 CHECK, FOUND RIGHT ELEVATOR SUPPORT RIB STATION 17.2 CRACKED. REF FASI N/R 53208, REPLACED ELEVATOR SUPPORT RIB PER S/B 727-55A0091. (M)
- [SDR GAIA03097](https://openairdocs.org/sdr/GAIA03097.md): Stiffener · cracked · Sep 10, 2003 · N6806 · Boeing 727223 · Wing Miscellaneous Structure
  > DURING B-2 CHECK, FOUND LEFT WING REAR SPAR VERTICAL STIFFENER CRACKED AT WS 556. REF FASI N/R 53206, REPLACED STIFFENER PER B727 SRM 51-30-2. (M)
- [SDR GAIA03095](https://openairdocs.org/sdr/GAIA03095.md): Floorbeam · corroded · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Floor Beam
  > DURING B-2 CHECK, FOUND MAIN CABIN FLOORBEAM BS 480 CORRODED AT LBL 30 AND CRACKED AT LBL 59. REF FASI N/R 53187, CUT OUT DAMAGED AREA, INSTALLED REPAIR PER B727 SRM 53-10-8 FIG 1. (M)
- [SDR GAIA03087](https://openairdocs.org/sdr/GAIA03087.md): Frame · dented · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Frame
  > DURING B-2 CHECK, FOUND MAIN CARGO CABIN FRAME BS 540 HAS A DENT IN THE RADIUS BELOW STRINGER 16RT. REF FASI N/R 53130 ACCOMPLISHED DOUBLER REPAIR PER B727 SRM 53-10-2 FIG 2. (M)
- [SDR GAIA03104](https://openairdocs.org/sdr/GAIA03104.md): Frame · dented · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Main, Frame
  > DURING B-2 CHECK, FOUND AFT CARGO FRAME DENTED BS 1070 AT STRINGER 25 RT. REF FASI N/R 53281, DOUBLER REPAIR IAW B727 SRM 53-10-2 FIG 5. (M)
- [SDR GAIA03103](https://openairdocs.org/sdr/GAIA03103.md): Seat Track · corroded · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING B-2, FOUND MAIN CABIN SEAT TRACK CORRODED BS 360 BL0. ERF FASI N/R 53268, REPLACED SEAT TRACK BS 344-480 BL 0 PER B727 SRM 53-10-5 FIG 7. (M)
- [SDR GAIA03102](https://openairdocs.org/sdr/GAIA03102.md): Seat Track · corroded · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING B-2 CHECK, FOUND MAIN CARGO SEAT TRACK CORRODED BS 360, LBL 25.5. REF FASI N/R 53267, REPLACED SEAT TRACK LBL 25.5 BS 344 TO 480 PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 7. (M)
- [SDR GAIA03101](https://openairdocs.org/sdr/GAIA03101.md): Seat Track · corroded · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING B-2 CHECK, FOUND MAIN CARGO SEAT TRACK CORRODED AT BS 760, RBL 45.5. REF FASI N/R 53265, REPLACED SEAT TRACK RBL 45.5, BS 760 TO 840 PER B727 SRM 51-30-2. (M)
- [SDR GAIA03100](https://openairdocs.org/sdr/GAIA03100.md): Floor Support · corroded · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING B-2 CHECK, FOUND MAIN CABIN FLOOR SUPPORT ANGLE LBL 61 BS 1090 UPPER CHORD CORRODED. REF FASI N/R 53253, REPLACED UPPER CHORD PER B727 SRM 53-10-2 FIG 5 AND 51-30-2. (M)
- [SDR GAIA03082](https://openairdocs.org/sdr/GAIA03082.md): Seat Track · corroded · Sep 10, 2003 · N6806 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING B-2 CHECK, FOUND MAIN CABIN SEAT TRACK CORRODED AT BS 360 TO BS 344, RBL 25.5. REF FASI N/R 50402, FABRICATED REPAIR FROM BAC 1520-792 MATERIAL. LENGTH 140 INCHES REPAIRED IAW B727 SRM 53-10-5, FIGURE 7 AND 53-10-2, FIGURE 7. (M)
- [SDR GAIA03008OP](https://openairdocs.org/sdr/GAIA03008OP.md): Light · inoperative · Feb 14, 2003 · N6806 · Boeing 727223 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE AT IAH, IT WAS DISCOVERED THAT THE L-1 EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02166OP](https://openairdocs.org/sdr/GAIA02166OP.md): Light · inoperative · Dec 20, 2002 · N6806 · Boeing 727223 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR GAIA02025OP](https://openairdocs.org/sdr/GAIA02025OP.md): Duct · warped · Mar 14, 2002 · N6806 · Boeing 727223 · Pneumatic Distribution System
  > FLT 873 - FWA-LAX - DURING CLIMB-OUT, THE NR 1 STRUT OVERHEAT LIGHT CAME ON FIVE MINUTES AFTER TAKEOFF. THE AIRCRAFT RETURNED TO FWA AND THE LANDING WAS UNEVENTFUL. FOUND THE 13 STAGE DUCT IN THE STUB WING AT THE HIGH PRESSURE WING ANTI-ICE VALVE FLANGE WARP
- [SDR GAIA02024OP](https://openairdocs.org/sdr/GAIA02024OP.md): Clamp · loose · Mar 12, 2002 · N6806 · Boeing 727223 · Engine Bleed Air System
  > FLT 733 - DFW-FWA - DURING CLIMB-OUT, THE NR 1 STRUT OVERHEAT LIGHT CAME ON. THE AIRCRAFT RETURNED TO DFW AND THE LANDING WAS UNEVENTFUL. FOUND THE CLAMP FOR THE EIGHT STAGE BLEED VALVE LOOSE. TIGHTENED THE SAME AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT
- [SDR GAI2001F00000](https://openairdocs.org/sdr/GAI2001F00000.md): Wire · dirty · Oct 11, 2001 · N6806 · Boeing 727223 · Trailing Edge Flap Control System
  > AFTER TAKE OFF, THE FLIGHT CREW DISCOVERED THAT THE OUTBOARD FLAPS WERE STUCK AT THE 2 DEGREE POSITION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO AIRPORT. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. RESET ASYMMETRY CIRCUIT AND CLEANED CANNON PLUG
- [SDR GAIA01245OP](https://openairdocs.org/sdr/GAIA01245OP.md): Wire · faulty · Jun 26, 2001 · N6806 · Boeing 727223 · Leading Edge Slat Position Indicating System
  > KHA - FLT 202 - TYS TO DFW, ON CLIMB-OUT FROM TYS, THE NR 2 SLAT DID NOT RETRACT WHEN THE FLAP HANDLE WAS MOVED TO THE UP POSITION. EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO TYS. AN UNEVENTFUL LANDING WAS MADE. INSPECTION REVEALED THAT A WIRING HA
- [SDR GAIA00687](https://openairdocs.org/sdr/GAIA00687.md): Indicator · inoperative · Nov 1, 2000 · N6806 · Boeing 727223 · Emergency Lighting
  > DURING PREFLIGHT FOUND, EMERGENCY EXIT LIGHT ARMED INDICATOR LIGHT INOPERATIVE. REMOVED AND REPLACED INDICATOR LIGHT BASE ASSEMBLY, OPS CHECK OK. AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR 00683](https://openairdocs.org/sdr/00683.md): Fitting · cracked · Oct 19, 2000 · N6806 · Boeing 727223 · Fuselage, Wing Attach Fittings
  > DISCREPANCY: DURING HEAVY CHECK FOUND: FUSELAGE FITTING AT FS 870 STR 18 HAS A CRACK INDICATION ON LOWER AFT BOLT HOLE CORRECTIVE ACTION: REPAIRED FITTING IAW TIMCO REO S00342 BY REAMING OUT DAMAGE AND INSTALLING A FREEZE PLUG
- [SDR 00684](https://openairdocs.org/sdr/00684.md): Elevator · corroded · Oct 16, 2000 · N6806 · Boeing 727223 · Elevator Control System
  > DISCREPANCY: DURING HEAVY CHECK FOUND: ELEVATOR TRAILING EDGE CORRODED AT STA 179CORRECTIVE ACTION: REPAIRED ELEVATOR IAW B727 SRM 55-20-2
- [SDR 00685](https://openairdocs.org/sdr/00685.md): Seat Track · corroded · Oct 13, 2000 · N6806 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: DURING HEAVY CHECK FOUND: CORROSION ON THE SEAT TRACK FLANGE AT LBL 45 BS 854 TO 870CORRECTIVE ACTION: REPLACED SEAT TRACK
- [SDR 00686](https://openairdocs.org/sdr/00686.md): Skin · corroded · Oct 13, 2000 · N6806 · Boeing 727223 · Fuselage Main, Plate/Skin
  > DISCREPANCY: DURING HEAVY CHECK FOUND:CORROSION ON TEH SKIN DOUBLER AT FS 1163 STR 19RCORRECTIVE ACTION: REPAIRED SKIN AND DOUBLER IAW TIMCO REO S00343 BY CUTTING OUT DAMAGED AREA AND INSTALLING REPAIR DOUBERS
- [SDR GAIA00681](https://openairdocs.org/sdr/GAIA00681.md): Lap Joint · damaged · Oct 12, 2000 · N6806 · Boeing 727223 · Fuselage Main, Plate/Skin
  > DISCREPANCY: DURING HEAVY CHECK FOUND: SKIN PULLING FASTENER HEADS, STA 460 STR 19R LAP SEAM. CORRECTIVE ACTION: REPAIRED TAP SEAM IAW B727 SRM53-30-3 FIG 5 STA 460 STR 19R
- [SDR GAIA00680](https://openairdocs.org/sdr/GAIA00680.md): Attach Angle · cracked · Oct 12, 2000 · N6806 · Boeing 727223 · Fuselage Main, Attach Fittings
  > DISCREPANCY: DURING HEAVY CHECK FOUND: LBL 70.5 WL208, BS873-878, SKIN TO FLOOR WEB ATTACH "T" ANGLE CRACKED ON INNER FLANGE. CORRECTIVE ACTION: HAD EDDY CURRENT PERFORMED & STOP DRILLED HOLES AT END OF CRACK CHECKED EDDY CURRENT AGAIN & FOUND TO BE TERMINAT
- [SDR GAIA00679](https://openairdocs.org/sdr/GAIA00679.md): Attach Angle · cracked · Oct 12, 2000 · N6806 · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK FOUND BS 1343 AFT SPLICE LBL 20 WL 280 SKIN ATTACH ANGLE CRACKED. REMOVED ANGLE IAW B727 SRM 51-30-2 FAB. NEW ANGLE PER B727 51-40-3. INSTALLED NEW ANGLE IAW SRM 51-30-2. (X)
- [SDR 00682](https://openairdocs.org/sdr/00682.md): Frames · dented · Oct 12, 2000 · N6806 · Boeing 727223 · Fuselage Main, Frame
  > DISCREPANCY: DURING HEAVY CHECK FOUND: FUSELAGE FRAME AT FS 1166 ABOVE STR 17 WL 210 HAS A DENTED FLANGE CORRECTIVE ACTION: REPAIRED FRAME IAW TIMCO REO S00340 BY CUTTING OUT DAMAGED AREA AND INSTALLING REPAIR DOUBLERS
- [SDR GAIA00667](https://openairdocs.org/sdr/GAIA00667.md): Keelbeam · cracked · Oct 11, 2000 · N6806 · Boeing 727223 · Fuselage Main, Keel
  > DISCREPANCY: DURING HEAVY CHECK FOUND: LEFT LOWER KEELBEAM CHORD ATTACH FLANGE CRACKED AT STA 875, LBL6 WL137.8. CORRECTIVE ACTION: REPAIRED KEELBEAM ATTACH FLANGE IAW SB727 53 0208 REV. 1 DATED FEB. 29, 1996.
- [SDR GAIA00666](https://openairdocs.org/sdr/GAIA00666.md): Angle · corroded · Oct 11, 2000 · N6806 · Boeing 727223 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING HEAVY CHECK FOUND:C-2 DOOR CUT-OUT AFT FRAME INNER ANGLE CORRODED ABOVE S25 & S26 RT 2 AREAS. CORRECTIVE ACTION: REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1 REPAIRED C-2 DOOR CUT-OUT AFT FRAME INNER ANGLE IAW REO S0
- [SDR GAIA00665](https://openairdocs.org/sdr/GAIA00665.md): Frame · cracked · Oct 11, 2000 · N6806 · Boeing 727223 · Fuselage Main, Frame
  > DISCREPANCY: DURING HEAVY CHECK FOUND: FS360 FRAME CRACKED BELOW STRINGER 7L.CORRECTIVE ACTION: REMOVED DAMAGE FABRICATED NEW ANGLE & FILLERS, FASTENERS IAW REO S00331 INSTALLED ANGLE & FILLERS IAW REO S00331
- [SDR GAIA00668](https://openairdocs.org/sdr/GAIA00668.md): Floorbeam · corroded · Oct 9, 2000 · N6806 · Boeing 727223 · Fuselage Main, Floor Beam
  > DISCREPANCY: DURING HEAVY CHECK FOUND: FLOORBEAM STA 727 CORRODED ON UPPER CHORD UPPER SURFACE LBL30, LBL10 & RBL15 EXTENDING UNDER FLOOR SKIN. CORRECTIVE ACTION: CORROSION REMOVED WAS FOUND TO BE OUT OF LIMITS IAW BOEING 727 SRM 53-10-1. FABRICATED AND INST
- [SDR GAIA00656](https://openairdocs.org/sdr/GAIA00656.md): Frame · dented · Oct 3, 2000 · N6806 · Boeing 727223 · Fuselage Main, Frame
  > DISCREPANCY: DURING HEAVY CEHCK FOUND: FS460 FRAME DENTED BETWEEN STRINGERS 17R & 16RCORRECTIVE ACTION: FABRICATED BEW FRAME DOUBLER AT BS460 BETWEEN STR 16 & 17 & HAD NDT CHECK STOP DRILLED HOLES AT END OF CRACK, INSTALLED IAW B727 SRM 51-40-3 NDT 6-51-00-00
- [SDR GAIA00655](https://openairdocs.org/sdr/GAIA00655.md): Lap Joint · bulged · Oct 2, 2000 · N6806 · Boeing 727223 · Fuselage Main, Plate/Skin
  > DISCREPANCY: DURING HEAVY CEHCK FOUND: SKIN JOINT BS359-360, STR 11R-14R SKIN BULGING. CORRECTIVE ACTION: REMOVED FASTENERS, FOUND SKIN TO BE OUT OF LIMITS, FABRICATED REPAIR DOUBLER, ALODINED AND PRIMED REPAIR, & INSTALLED REPAIR IAW B727 SRM 51-30-2, 51-10-
- [SDR GAIA00654](https://openairdocs.org/sdr/GAIA00654.md): Skin · corroded · Oct 2, 2000 · N6806 · Boeing 727223 · Fuselage Main, Plate/Skin
  > DISCREPANCY: DURING HEAVY CHECK FOUND: SKIN, UNDER FORWARD LAV SERVICE DOOR, CORRODED & BULGING STA 304 STR 20R. CORRECTIVE ACTION: REPAIRED IAW B727 SRM 53-30-3 FIG 3

Next page: https://openairdocs.org/deregistered/N6806-2007-05-10/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 = 'N6806' AND deregistration_id = 'N6806-2007-05-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N6806-2007-05-10/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.