# Service difficulty reports: N6813, cancelled Jun 22, 2006

A list on [N6813, cancelled Jun 22, 2006](https://openairdocs.org/deregistered/N6813-2006-06-22.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR EISA20010146](https://openairdocs.org/sdr/EISA20010146.md): Structure · corroded · Dec 12, 2001 · N6813 · Boeing 727223 · Fuselage Miscellaneous Structure
  > CHORD CORRODED BS 312-348 LBL 14.6, WL 169. FOUND ON CPCP C53-111-03 PAGE 4 N/R CARD 401 WRITTEN. REMOVED CHORD IAW B727 SRM 51-30-2, INSTALLED NEW CHORD IAW B727 SRM 51-30-2-51-10-1.
- [SDR EISA20010145](https://openairdocs.org/sdr/EISA20010145.md): Angle · corroded · Dec 12, 2001 · N6813 · Boeing 727223 · Fuselage Main, Structure
  > ANGLE IN R/H W/W CORRODED, BS 870 RBL 48.0FOUND DURING CPCP C53-100-01 PAGE 1, N/R CARD 411 WRITTENCORRECTIVE ACTION:REMOVED ANGLE, FABRICATED NEW ANGLE FROM 7075-T6-063 AND INSTALLED IAW B727 SRM 51-30-2.
- [SDR EISA20010144](https://openairdocs.org/sdr/EISA20010144.md): Stiffener · corroded · Dec 12, 2001 · N6813 · Boeing 727223 · Fuselage Main, Structure
  > VERTICAL STIFFENER CORRODED BS 336 RBL 14.6 BELOW FLOOR PAN.FOUND ON CPCP C53-111-03 PAGE 4, N/R CARD 405 WRITTENCORRECTIVE ACTION:REMOVED AND REPLACED STIFFENER IAW B727 SRM 51-30-2.
- [SDR EISA20010143](https://openairdocs.org/sdr/EISA20010143.md): Frame · corroded · Dec 12, 2001 · N6813 · Boeing 727223 · Fuselage Main, Frame
  > NOSE WHEEL WELL STA 296, LBL 12 UPPER FRAME CORRODED. FOUND ON CPCP CHECK. REMOVED AND REPLACED FRAME IAW B727 SRM 51-10-1 & 51-30-2.
- [SDR EISA20010142](https://openairdocs.org/sdr/EISA20010142.md): Frame · corroded · Dec 12, 2001 · N6813 · Boeing 727223 · Fuselage Main, Frame
  > NOSE WHEEL WELL STA 296, RBL 12 UPPER CHORD CORRODED. FOUND ON CPCP CHECK. REMOVED AND REPLACED FRAME IAW B727 SRM 51-10-1 & 51-30-2.
- [SDR EISA20010141](https://openairdocs.org/sdr/EISA20010141.md): Stiffener · cracked · Dec 12, 2001 · N6813 · Boeing 727223 · Fuselage Main, Frame
  > L/H MLG W/W BS 870 LBL 45 VERTICAL STIFFENER CRACKED.FOUND ON CPCP INSP. C-53-100-01 PAGE 1, N/R CARD 410 WRITTENCORRECTIVE ACTION:FABRICATED AND INSTALLED REPAIR DOUBLER IAW B727 SRM 51-40-4 & 51-30-2.
- [SDR EISA20010140](https://openairdocs.org/sdr/EISA20010140.md): Panel · corroded · Dec 12, 2001 · N6813 · Boeing 727223 · Fuselage Main, Structure
  > NOSE W/W PANEL BS 330 TO 350 STR L27 CORRODEDFOUND ON CPCP C53-100-01 PAGE 1, N/R CARD 444 WRITTENCORRECTIVE ACTION:REMOVED CORROSION IAW B727 SRM 51-10-6 FABRICATED REPAIR IAW 51-40-2 AND INSTALLED REPAIR IAW B727 SRM 51-40-2 & 51-30-2.
- [SDR EISA20010139](https://openairdocs.org/sdr/EISA20010139.md): Skin · cracked · Dec 12, 2001 · N6813 · Boeing 727223 · Fuselage Main, Structure
  > FUSELAGE SKIN BS 211, STR 25R GOUGED AND CRACKED AT FWD E/E DOOR CUTOUT.FOUND ON SERVICE CHECK--N/R CARD 431 WRITTENCORRECTIVE ACTION: STOP DRILLED CRACK IAW B727 SRM 51-10-1. DYE PEN. IAW BOEING S.O.P. 20-50-2. FABRICATED REPAIR DOUBLER AND INSTALLED IAW B7
- [SDR EISA20010138](https://openairdocs.org/sdr/EISA20010138.md): Skin · corroded · Dec 12, 2001 · N6813 · Boeing 727223 · Fuselage Main, Structure
  > FUSELAGE SKIN CORRODED AT BS 336, STR 25R.WRITTEN FROM NON-ROUTINE CARD 405 FROM CPC C53-111-03 PAGE 4--N/R CARD 435 WRITTENCORRECTIVE ACTION:REMOVED DAMAGED SKIN, HFEC AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW EA. 53-01630-1, BOEING MESSAGE EOI-DAL-1-00
- [SDR EISA20010125](https://openairdocs.org/sdr/EISA20010125.md): Door · out of adj · Oct 11, 2001 · N6813 · Boeing 727223 · Cargo/Baggage Doors
  > F/E PANEL MAIN CARGO DOOR WARNING LIGHT ILLUMINATE, PRESSURIZATION NORMAL, ALT FL310 PSID 8.0. MAIN CARGO DOOR PANEL, DOOR WARNING LIGHT, VENT DOOR OPEN, AND MAIN CARGO DOOR NOT CLOSED. ADJUSTED MAIN CARGO DOOR, DOOR CLOSED, AND LATCH CLOSED SWITCHES AND OPS
- [SDR EISA20010124](https://openairdocs.org/sdr/EISA20010124.md): Switch · inoperative · Oct 5, 2001 · N6813 · Boeing 727223 · Door Warning System
  > DURING CLIMB, RED MCD LIGHT ALONG WITH AMBER VENT DOOR NOT CLOSED ILLUM. ALONG WITH UNSCHEDULED CLIMB IN CABIN ALT. ACC. AERONAUTICAL MCD WARNING ILLUM. IN FLT. AFTER RAPID DEPRESS. CHECKLIST COMPLETED LAND AT NEAREST SUITABLE AIRPORT.CORRECTIVE ACTION:DUPLICA
- [SDR EISA20010094](https://openairdocs.org/sdr/EISA20010094.md): Rivet · sheared · Jun 8, 2001 · N6813 · Boeing 727223 · Fuselage Main, Bulkhead
  > RIVET MIGRATED AT 1183 BULKHEAD AFT LT. SIDE 12" O/B OF DOOR CUT-OUT & 10" BELOW DOOR TOP (EO)FOUND DURING B-2 CHECKCORRECTIVE ACTION:CUT-OFF HEAD OF TRAPPED (MIGRATING) RIVET PER E.O. #01-163. INSTALLED TWO EACH HLT 428-6 HILOCS IAW E.O. #01-163 & SEALED WITH
- [SDR EISA20000145](https://openairdocs.org/sdr/EISA20000145.md): Controller · fluctuates · Sep 7, 2000 · N6813 · Boeing 727223 · Alternator-Generator Drive
  > NR 1 GENERATOR UNDERVOLTAGE LIGHT ILLUMINATED, TRIPPED NR 1 BUS TIE AT 5000 FT, AIR TURNBACK. REMOVED AND REPLACED NR 1 GENERATOR LOAD CONTROLLER AND GCU, OPS CHECK GOOD.
- [SDR EISA20000059](https://openairdocs.org/sdr/EISA20000059.md): Uplock Switch · failed · Jul 27, 2000 · N6813 · Boeing 727223 · Landing Gear Position and Warning
  > AFTER GEAR EXTENSION, NOSE GEAR RED LIGHT REMAINED ILLUMINATED, AS WELL AS AFTER MANUAL GEAR EXTENSION. FOUND BROKEN WIRE ON NOSE GEAR UPPER LOCK SWITCH, RE-CRIMPED WIRE IAW M/M 20-11. OPS CHECK NORMAL.
- [SDR EISA99209](https://openairdocs.org/sdr/EISA99209.md): Mechanism · failed · Oct 19, 1999 · N6813 · Boeing 727223 · Passenger/Crew Doors
  > AIRCRAFT LOST PRESSURIZATION, DIVERTED TO BRU AT 0200Z) UNABLE TO OPEN L1 DOOR. (M)
- [SDR EISA99162](https://openairdocs.org/sdr/EISA99162.md): Battery · discharged · Aug 30, 1999 · N6813 · Boeing 727223 · Battery/Charger System
  > ON LANDING, APU FAILED TO START FOUND BATTERY VOLTAGE AT 4, BATTERY CHARGER C/B POPPED. BATTERY WARMS TO TOUCH. NOTICED SMOKE IN COCKPIT. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER. (M)
- [SDR EISA99124](https://openairdocs.org/sdr/EISA99124.md): Compressor · stalled · May 30, 1999 · N6813 · Boeing 727223 · Turbine Engine Compressor Section
  > NR 2 ENGINE COMPRESSOR STALLS. REMOVED AND REPLACED NR 2 ENGINE. OPS CHECK GOOD. REPLACED 13TH STAGE SURGE BLEED VALVE. (M)
- [SDR EISA99028](https://openairdocs.org/sdr/EISA99028.md): Wire · broken · Feb 16, 1999 · N6813 · Boeing 727223 · Landing Gear System Wiring
  > NOSE GEAR RED UNSAFE LIGHT ON AND GREEN LIGHT ON WITH GEAR EXTENDED. REPAIRED GROUND WIRE FROM LOCK SWITCH. (M)
- [SDR EISA99027](https://openairdocs.org/sdr/EISA99027.md): Switch · failed · Feb 16, 1999 · N6813 · Boeing 727223 · Landing Gear Position and Warning
  > AFTER NOSE GEAR EXTENSION, BOTH GREEN AND RED ILLUMINATED. AFTER MAIN GEAR EXTENDED, ONLY GREEN LIGHT ON. REMOVED AND REPLACED NOSE GEAR LOCK SWITCH, PERFORMED GEAR SWING NUMEROUS TIMES. OPS CHECK GOOD PER MM 32-61-7. (M)
- [SDR EISA99021](https://openairdocs.org/sdr/EISA99021.md): Duct · cracked · Jan 19, 1999 · N6813 · Boeing 727223 · Pneumatic Distribution System
  > LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED WHILE ENGINE ANTI-ICE WING ANTI-ICE WERE IN USE. CLOSING THE WING ANTI-ICE AND A CO-INCIDENTAL REDUCTION IN POWER DURING AN APPROACH EXTINGUISHED LIGHT. LOG PAGE 58944 MEL 30-2 PLACARD 980. REMOVED AND REPLACED CRAC
- [SDR EISA98284](https://openairdocs.org/sdr/EISA98284.md): Overheat Light · illuminated · Dec 4, 1998 · N6813 · Boeing 727223 · Overheat Detection
  > SHORTLY AFTER SELECTING WING ANTI-ICE ON, THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, EXTINGUISHED AFTER TURNING OFF ENGINE NR 3 ANTI-ICE. ENGINE NR 1 OPENED NORMAL. OPS CHECKED IN AIR AND GROUND MODES, OPS CHECKED NORMAL IAW MM CHAPTER 26. (M)
- [SDR EISA98213](https://openairdocs.org/sdr/EISA98213.md): Indicator · malfunctioned · Aug 27, 1998 · N6813 · Boeing 727223 · Engine Oil Temperature
  > NR 2 ENGINE OIL TEMP EXCEEDED RED LINE DURING FLIGHT. PRECAUTIONARY ENGINE SHUTDOWN ACCOMPLISHED PER FLIGHT MANUAL. FOUND NR 2 OIL TEMP BULB GROUND WIRE BROKEN AT TERMINAL BLOCK. SPLICED WIRE ON TERMINAL BLOCK IAW MM CHAPTER 20. (M)
- [SDR EISA97278](https://openairdocs.org/sdr/EISA97278.md): Angle · corroded · Dec 12, 1997 · N6813 · Boeing 727223 · Fuselage Miscellaneous Structure
  > MAIN CABIN, FLOOR SUPPORT FS 400-420 HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-40-04. (M)
- [SDR EISA97277](https://openairdocs.org/sdr/EISA97277.md): Doubler · cracked · Dec 12, 1997 · N6813 · Boeing 727223 · Trailing Edge Flaps
  > LT WING, OUTBOARD MID FLAP, LOWER FORWARD SKIN HAS SEVERAL CRACKS ON DOUBLER AT OUTBOARD FORE FLAP TRACK AREA. FABRICATED DOUBLER AND FILLER PER SRM 51-40-03. (M)
- [SDR EISA97276](https://openairdocs.org/sdr/EISA97276.md): Skin · delaminated · Dec 12, 1997 · N6813 · Boeing 727223 · Spoilers
  > RT WING, NR 7 SPOILER DELAMINATED AT FWD CENTER SECTION. REPAIRED SPOILER DELAMINATION PER SRM 51-40-06 AND 51-40-09. (M)
- [SDR EISA97275](https://openairdocs.org/sdr/EISA97275.md): Skin · cracked · Dec 12, 1997 · N6813 · Boeing 727223 · Wing, Plate/Skin
  > LEFT WING LEADING EDGE UPPER SURFACE EXTERIOR SKIN HAS APPROX 0 INCH CRACK AT WS 450. FABRICATED AND INSTALLED DOUBLER PER SRM 51-10-1 AND 51-30-02. (M)
- [SDR EISA97274](https://openairdocs.org/sdr/EISA97274.md): Stringer · cracked · Dec 12, 1997 · N6813 · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > CIRCULAR CRACK BETWEEN TWO FAST ON STRINGER 24R AT FS 335. FABRICATED AND INSTALLED DOUBLER PER SRM 51-10-1 AND 51-30-02. (M)
- [SDR EISA97273](https://openairdocs.org/sdr/EISA97273.md): Floorbeam · corroded · Dec 12, 1997 · N6813 · Boeing 727223 · Fuselage Main, Floor Beam
  > MAIN CABIN, FLOOR BEAM FS 320 HAS CORROSION ON TOP CAP. REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 53-10-08. (M)
- [SDR EISA97272](https://openairdocs.org/sdr/EISA97272.md): Floorbeam · corroded · Dec 12, 1997 · N6813 · Boeing 727223 · Fuselage Main, Floor Beam
  > MAIN CABIN, FLOORBEAM FS 360 HAS CORROSION ON TOP CAP. REMOVED AND REPLACED TO CAP PER SRM 53-10-08. (M)
- [SDR EISA97271](https://openairdocs.org/sdr/EISA97271.md): Angle · corroded · Dec 12, 1997 · N6813 · Boeing 727223 · Fuselage Miscellaneous Structure
  > MAIN CABIN, OUTBOARD ANGLE RIGHT SIDE HAS CORROSION AT FS 460. REMOVED AND REPLACED ANGLE PER SRM 51-10-06. (M)
- [SDR EISA97270](https://openairdocs.org/sdr/EISA97270.md): Intercostal · cracked · Dec 12, 1997 · N6813 · Boeing 727223 · Fuselage Miscellaneous Structure
  > MAIN CABIN, INTERCOSTAL AT FS 740 BL 20L HAS PREVIOUS REPAIR DOUBLER WITH 2 INCH LONG CRACK. REMOVED CRACKED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER PER SRM 41-40-02. (M)
- [SDR EISA97269](https://openairdocs.org/sdr/EISA97269.md): Support · cracked · Dec 12, 1997 · N6813 · Boeing 727223 · Fuselage Miscellaneous Structure
  > MAIN CABIN, SUPPORT WEB UPPER FLANGE HAS SEVERAL CRACKS FROM FS 720 TO 720B BL 0. UPPER FLANGE REMOVED DUE TO TRACK INSTALLATION FOR CARGO MOD, REF STC SA-1998-SO AND DRAWING AE 727-2-063. (M)
- [SDR EISA97268](https://openairdocs.org/sdr/EISA97268.md): Support · cracked · Dec 12, 1997 · N6813 · Boeing 727223 · Fuselage Miscellaneous Structure
  > MAIN CABIN, FLOOR SUPPORT WEB UPPER FLANGE HAS SEVERAL CRACKS FROM FS 400 T0 420. UPPER FLANGE REMOVED DUE TO CARGO MOD AND REPLACED BY CHANNEL, REF STC SA-1998 SO AND DRAWING AE 727-2-063. (M)
- [SDR EISA97267](https://openairdocs.org/sdr/EISA97267.md): Floorbeam · corrosion · Dec 12, 1997 · N6813 · Boeing 727223 · Fuselage Main, Floor Beam
  > MAIN CABIN, FLOORBEAM UPPER CAP HAS CORROSION AT FS 360 BL 15L TO BL 15R. FABRICATED AND INSTALLED NEW TOP CAP PER SRM 53-10-08. (M)
- [SDR EISA97266](https://openairdocs.org/sdr/EISA97266.md): Stringer · cracked · Dec 12, 1997 · N6813 · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > STRINGER S-1 CRACKED AT FS 400. REMOVED DAMAGED AREA AND REPAIR SECTION IAW SRM 53-10-3. (M)
- [SDR EISA97265](https://openairdocs.org/sdr/EISA97265.md): Stringer · cracked · Dec 12, 1997 · N6813 · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > STRINGER S-1 CRCKED AT FS 380. REMOVED DAMAGED AREA AND REPAIR SECTION IAW SRM 53-10-3. (M)
- [SDR EISA97264](https://openairdocs.org/sdr/EISA97264.md): Stringer · cracked · Dec 12, 1997 · N6813 · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > STRINGER S-1 CRACKED AT FS 360. REMOVED DAMAGED AREA AND REPAIR SECTION IAW SRM 53-10-3. (M)
- [SDR AALA971123](https://openairdocs.org/sdr/AALA971123.md): Actuator · broken · Jun 20, 1997 · N6813 · Boeing 727223 · Landing Gear Retraction/Extension System
  > PHL - FLT 0512 - DURING APPROACH TO PHL WHEN LANDING GEAR EXTENDED, RT MAIN LANDING GEAR FAILED TO EXTEND NORMALLY, RECYCLED LANDING GEAR WITH SAME RESULTS. ACCOMPLISHED MANUAL GEAR EXTENSION IAW ABNORMAL PROCEDURES AND AIRCRAFT LANDED PHL WITHOUT INCIDENT.
- [SDR AALA970989](https://openairdocs.org/sdr/AALA970989.md): Light · defective · May 28, 1997 · N6813 · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT CHECK, AFT VENTRAL STAIRWAY EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT VENTRAL STAIRWAY EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR AALA970307](https://openairdocs.org/sdr/AALA970307.md): Wire · broken · Feb 7, 1997 · N6813 · Boeing 727223 · Landing Gear System Wiring
  > DFW - FLT 475 - DURING APPROACH TO DFW, WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND LIGHT REMAINED ILLUMINATED. VISUALLY CONFIRMED NOSE LANDING GEAR EXTENDED AND AIRCRAFT LANDED DF
- [SDR AALA961733](https://openairdocs.org/sdr/AALA961733.md): Skin · cracked · Nov 13, 1996 · N6813 · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND SKIN CRACKED AT 4 RIVITS HEADS, STATION 410. CUT OUT CRACKS IN SKIN INSTALLED REPAIR PER SRM 53-30-3. (M)
- [SDR AALA951067](https://openairdocs.org/sdr/AALA951067.md): Wire · broken · Jun 5, 1995 · N6813 · Boeing 727223 · Landing Gear System Wiring
  > ORD - FLT 1262 - DURING APPROACH TO ORD WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH NO GREEN LIGHT. RECYCLED LANDING GEAR WITH SAME RESULTS. WHILE ACCOMPLISHING A GO-AROUND RED NOSE LANDING GEAR LIGHT EXTINGUISHED AND GR

## 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 = 'N6813' AND deregistration_id = 'N6813-2006-06-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N6813-2006-06-22/reports

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