# Service difficulty reports: N6839, cancelled Jun 22, 2006

A list on [N6839, cancelled Jun 22, 2006](https://openairdocs.org/deregistered/N6839-2006-06-22.md).

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

- [SDR EISA20010129](https://openairdocs.org/sdr/EISA20010129.md): Light · inoperative · Oct 16, 2001 · N6839 · Boeing 727223 · Emergency Lighting
  > FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FWD EMERGENCY EXIT LIGHT ASSY IAW B727 MM 33, OPS CHECK GOOD.
- [SDR EISA20010075](https://openairdocs.org/sdr/EISA20010075.md): Garlock Seal · damaged · Apr 15, 2001 · N6839 · Boeing 727223 · Turbine Engine Oil System
  > NR 2 ENGINE OIL QUANTITY LOSS IN FLIGHT AT RATE OF 3 GALLONS PER HOUR. AIR TURNBACK TO (IND). FOUND GARLOCK SEAL DAMAGED BEHIND HYDRAULIC A-PUMP. REMOVED AND REPLACED GARLOCK SEAL PER M/M 72-61, NO LEAKS NOTED.
- [SDR EISA20000228](https://openairdocs.org/sdr/EISA20000228.md): Warning Light · illuminated · Dec 21, 2000 · N6839 · Boeing 727223 · Leading Edge Slat Position Indicating System
  > NR 6 L/E FLAP LIGHT ON INFLIGHT. AIR TURNBACK TO LAX. COULD NOT DUPLICATE ON GROUND. OPS CHECK GOOD.
- [SDR EISA20000226](https://openairdocs.org/sdr/EISA20000226.md): Connector · dirty · Dec 21, 2000 · N6839 · Boeing 727223 · Leading Edge Slat Position Indicating System
  > AFTER TAKEOFF, DURING FLAP RETRACTION NR 6 LEADING EDGE FLAP FAILED TO RETRACT WHEN FLAPS UP WAS SELECTED. POSITION TRANSMITTER CANNON PLUG, CLEANED WITH CONTACT CLEANER. OPS CHECK PERFORMED IAW M/M 27-80-0, NO DEFECTS NOTED.
- [SDR EISA20000208](https://openairdocs.org/sdr/EISA20000208.md): Relay · inoperative · Nov 30, 2000 · N6839 · Boeing 727223 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS INOP. STAY ON IN ARMED POSITION. CORRECTIVE ACTION: REMOVED AND REPLACED R70 RELAY. SYSTEM OPS CHECK GOOD PER M/M 33-50.
- [SDR EISA20000209](https://openairdocs.org/sdr/EISA20000209.md): Light · inoperative · Nov 30, 2000 · N6839 · Boeing 727223 · Emergency Lighting
  > FORWARD ENTRY EMERGENCY EXIT LIGHT INOP. CORRECTIVE ACTION: REPLACED FORWARD ENTRY EMERGENCY LIGHT ASSEMBLY PER M/M 33-50.
- [SDR EISA2000043](https://openairdocs.org/sdr/EISA2000043.md): Actuator · cracked · Feb 11, 2000 · N6839 · Boeing 727223 · Leading Edge Slat Actuator
  > AFTER TAKEOFF, FLAPS UP APPROXIMATELY 225 INDICATED AIR SPEED AIRCRAFT WENT INTO LEFT BANK. HAD TO USE 30 DEGREES RIGHT AILERON TRIM TO BRING AIRCRAFT BACK TO LEVEL FLIGHT. AIR TURN BACK TO CDG. REPLACED LEADING EDGE SLAT ACTUATOR IAW MM 27-81-00. (M)
- [SDR EISA2000015](https://openairdocs.org/sdr/EISA2000015.md): Actuator · failed · Feb 11, 2000 · N6839 · Boeing 727223 · Leading Edge Slat Actuator
  > AFTER TAKEOFF FLAPS UP APPROX 225 IAS AIRCRAFT WENT INTO LEFT BANK, HAD TO USE 30 DEGREES RIGHT AILERON TRIM TO BRING AIRCRAFT BACK TO LEVEL FLIGHT. AIR TURN BACK TO (CDG). REPLACED LEADING EDGE SLAT ACTUATOR. OPS CHECK GOOD. (M)
- [SDR EISA99085](https://openairdocs.org/sdr/EISA99085.md): Reservoir · req'd service · Apr 22, 1999 · N6839 · Boeing 727223 · Hydraulic System, Main
  > LEADING EDGE FLAPS LIGHT ON AFTER TAKEOFF, FLAPS SELECTED UP NR 2 SLAT DID NOT RETRACT. HYDRAULIC QUANTITY FLUCTUATES FROM 4 TO 2.4 GALLONS. AIR TURN BACK TO BRU. SERVICED AND PURGED 'A' SYSTEM, LEADING FLAPS AND SLATS OPERATED, SYSTEM OPS AND LEAK CHECKS G
- [SDR EISA98240](https://openairdocs.org/sdr/EISA98240.md): Line · out of position · Sep 20, 1998 · N6839 · Boeing 727223 · Engine Bleed Air System
  > NR 3 STRUT OVERHEAT LIGHT ILLUMINATED AFTER APPLYING CLIMB POWER. AIR TURNBACK TO CPH. GENERATED BY PILOT REPORT. REPOSITIONED BLEED AIR SHUT-OFF LINE. OPS CHECK GOOD. (M)
- [SDR EISA98222](https://openairdocs.org/sdr/EISA98222.md): Valve · out of position · Sep 20, 1998 · N6839 · Boeing 727223 · Pneumatic Distribution System
  > NR 3 STRUT OVERHEAT LIGHT ILLUMINATED AFTER APPLYING CLIMB POWER. AIR TURN TACK TO CHP. GENERATED FROM PILOT REPORT. REPOSITIONED AND TIGHTENED MODULAR VALVE AND CORRESPONDING BULKHEAD CONNECTIONS. OPS CHECK GOOD IAW MM 36. (M)
- [SDR EISA98218](https://openairdocs.org/sdr/EISA98218.md): Valve · malfunctioned · Sep 15, 1998 · N6839 · Boeing 727223 · Airfoil Anti/De-ice System
  > ON DEPARTURE FROM EMA, NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. PERFORMED CHECKLIST PER AFM VOLUME 1 LIGHT EXTINGUISHED. CONTINUED FLIGHT TO BRU. GENERATED FROM PILOT REPORT. REMOVED AND REPLACED AIR SHUTOFF VALVE IAW MM 75. (M)
- [SDR EISA97209](https://openairdocs.org/sdr/EISA97209.md): Valve · leaking · Oct 21, 1997 · N6839 · Boeing 727223 · Engine Anti-Icing System
  > ON TAKEOFF FROM BRU, THE NR 2 FIRE WARNING SOUNDED SHORTLY AFTER TAKEOFF, RETURNED TO BRU (ATB). FOUND UPPER LEFT ANTI-ICE VALVE LEAKING, RESECURED VALVE, AND RAN ENGINE. NO LEAKS NOTED. (X)
- [SDR EISA97075](https://openairdocs.org/sdr/EISA97075.md): Actuator · failed · Mar 18, 1997 · N6839 · Boeing 727223 · Leading Edge Slat Actuator
  > NR 3 SLAT FAILED TO RETREAT. REMOVED AND REPLACED SLAT ACTUATOR AND SWITCH. (M)
- [SDR 97ZZZM483](https://openairdocs.org/sdr/97ZZZM483.md): Switch · failed · Mar 18, 1997 · N6839 · Boeing 727223 · Leading Edge Slat Control System
  > NR 3 SLAT FAILED TO RETREAT. REMOVED AND REPLACED SLAT ACTUATOR AND SWITCH. REFERENCE EISA97075.
- [SDR EISA97022](https://openairdocs.org/sdr/EISA97022.md): Frame · cracked · Jan 24, 1997 · N6839 · Boeing 727223 · Fuselage Main, Frame
  > FOUND FRAME CRACKED, TOP OF GALLEY DOOR FRAME FS 380R. REPAIRED PER SRM 53-10-4 AND 51-30-2. (M)
- [SDR EISA97021](https://openairdocs.org/sdr/EISA97021.md): Frame · cracked · Jan 24, 1997 · N6839 · Boeing 727223 · Fuselage Main, Frame
  > FRAME CRACKED, 10 INCHES ABOVE GALLEY DOOR FS 400R. REPAIRED FRAME PER SRM 53-10-4 AND 51-30-2. (M)
- [SDR EISA97019](https://openairdocs.org/sdr/EISA97019.md): Bulkhead · cracked · Jan 24, 1997 · N6839 · Boeing 727223 · Fuselage Main, Bulkhead
  > TWO CRACKS IN FS 178 BULKHEAD JUST TO THE LEFT AND SLIGHTLY ABOVE CENTER POINT. INSTALLED REPAIR PER SB 727-53-0123 USING KIT 65C 36289-2. (M)
- [SDR EISA97016](https://openairdocs.org/sdr/EISA97016.md): Bulkhead Fitting · cracked · Jan 24, 1997 · N6839 · Boeing 727223 · Fuselage Main, Bulkhead
  > FOUND CRACKED FITTING AT 1183 BULKHEAD, LBL 22, WL LBL 22, WL 244.4. INSTALLED NEW FITTING PER SRM 51-10-2. (M)
- [SDR EISA97015](https://openairdocs.org/sdr/EISA97015.md): Bulkhead Fitting · cracked · Jan 24, 1997 · N6839 · Boeing 727223 · Fuselage Main, Bulkhead
  > FOUND CRACKED FITTING AT 1183 BULKHEAD, LBL 22, WL LBL 22, WL 235.9. INSTALLED NEW FITTING PER SRM 51-10-2. (M)
- [SDR EISA97007](https://openairdocs.org/sdr/EISA97007.md): Skin · dents · Jan 24, 1997 · N6839 · Boeing 727223 · Elevator, Tab Structure
  > NUMEROUS DENTS ON LEFT ELEVATOR TAB SKIN. REPAIRED TAB PER SRM 51-40-1 PAINT AND REBALANCE PER SRM 51-80-9 AND 51-20-13. (M)
- [SDR EISA97031](https://openairdocs.org/sdr/EISA97031.md): Clip · cracked · Jan 22, 1997 · N6839 · Boeing 727223 · Fuselage Miscellaneous Structure
  > FOUND 13 STRINGER TIE CLIPS CRACKED FROM FS 950C THROUGH FS 1090 FROM STRINGER 4L TO 4R. REMOVED AND REPLACED TIE CLIPS PER SRM 51-10-1. (M)
- [SDR EISA97030](https://openairdocs.org/sdr/EISA97030.md): Clip · cracked · Jan 22, 1997 · N6839 · Boeing 727223 · Fuselage Miscellaneous Structure
  > FOUND 29 STRINGER TIE CLIPS CRACKED FROM FS 420 THROUGH FS 804 FROM STRINGER 9L TO 4R. REMOVED AND REPLACED TIE CLIPS PER SRM 51-10-1. (M)
- [SDR EISA97029](https://openairdocs.org/sdr/EISA97029.md): Skin · hole · Jan 22, 1997 · N6839 · Boeing 727223 · Trailing Edge Flaps
  > LEFT INBOARD FLAP, AFT FLAP INBOARD END HAS A SMALL HOLE. REPAIRED HOLE PER SRM 51-40-6. (M)
- [SDR EISA97028](https://openairdocs.org/sdr/EISA97028.md): Angle · corroded · Jan 22, 1997 · N6839 · Boeing 727223 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON OUTBOARD FLOOR SUPPORT ANGLE FS 720-720A. FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 51-40-4. (M)
- [SDR EISA97027](https://openairdocs.org/sdr/EISA97027.md): Support · cracked · Jan 22, 1997 · N6839 · Boeing 727223 · Trailing Edge Flaps
  > NR 3 FLAP CARRIAGE LINK SUPPORT FITTING CRACKED. REMOVED AND REPLACED SUPPORT PER MM 27-51-0. (M)
- [SDR EISA97026](https://openairdocs.org/sdr/EISA97026.md): Stringer · cracked · Jan 22, 1997 · N6839 · Boeing 727223 · Wing, Longeron/Stringer
  > RIGHT WING, WS 686.5, CRACKED FLANGE ON TOP STRINGER, 23 INCHES AFT OF LEADING EDGE. FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 57-10-4. (M)
- [SDR EISA97025](https://openairdocs.org/sdr/EISA97025.md): Support · cracked · Jan 22, 1997 · N6839 · Boeing 727223 · Trailing Edge Flaps
  > LEFT INBOARD FLAP, INBOARD CARRIAGE, MIDFLAP BEAM LINK SUPPORT CRACKED. REMOVED AND REPLACED SUPPORT ASSEMBLY PER MM 27-51-0. (M)
- [SDR EISA97024](https://openairdocs.org/sdr/EISA97024.md): Intercostal · corroded · Jan 22, 1997 · N6839 · Boeing 727223 · Fuselage Miscellaneous Structure
  > MAIN CABIN FS 1090, RBL 61, INTERCOSTAL CORRODED ON LOWER SIDE. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8. (M)
- [SDR EISA97023](https://openairdocs.org/sdr/EISA97023.md): Intercostal · corroded · Jan 22, 1997 · N6839 · Boeing 727223 · Fuselage Miscellaneous Structure
  > MAIN CABIN FS 1110, LBL 59, CORROSION ON UNDERSIDE OF INTERCOSTAL. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-2. (M)
- [SDR EISA97020](https://openairdocs.org/sdr/EISA97020.md): Stiffener · cracked · Jan 21, 1997 · N6839 · Boeing 727223 · Elevator Structure
  > X-RAY INDICATES CRACK AND MISSING MATERIAL INTERNAL ON RT ELEVATOR, INBOARD END. FABRICATED AND INSTALLED REPAIR PARTS PER 51-10-1 AND 51-30-2. (M)
- [SDR EISA97018](https://openairdocs.org/sdr/EISA97018.md): Frame · corroded · Jan 21, 1997 · N6839 · Boeing 727223 · Fuselage Miscellaneous Structure
  > INTERGRANULAR CORROSION ON DOOR CUT OUT FRAME WEB AND OUTBOARD INTERCOSTAL, RT SIDE OF FORWARD AND E/E DOOR. FABRICATED NEW WEB AND ANGLE PER SRM 51-40-1 AND INSTALLED PER SRM 51-40-1 AND 51-30-2. (M)
- [SDR EISA97017](https://openairdocs.org/sdr/EISA97017.md): Vent Box · cracked · Jan 21, 1997 · N6839 · Boeing 727223 · Wing Miscellaneous Structure
  > RIGHT WING VENT BOX CRACKED AT WS 686. FABRICATED AND INSTALLED REPAIR PER SRM 57-10-4. (M)
- [SDR EISA97014](https://openairdocs.org/sdr/EISA97014.md): Stiffener · cracked · Jan 21, 1997 · N6839 · Boeing 727223 · Fuselage Miscellaneous Structure
  > FS 1183 BULKHEAD VERTICAL STIFFENER HAS CRACK IN FLANGE AT RBL 40. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-4. (M)
- [SDR EISA97013](https://openairdocs.org/sdr/EISA97013.md): Skin · cracked · Jan 21, 1997 · N6839 · Boeing 727223 · Wing, Plate/Skin
  > UPPER WING SKIN CRACKED AT NR 4 SPOILER OUTBOARD HINGE. FABRICATED AND INSTALLED REPAIR PER SRM 57-30-4. (M)
- [SDR EISA97012](https://openairdocs.org/sdr/EISA97012.md): Panel · cracked · Jan 21, 1997 · N6839 · Boeing 727223 · Wing, Plate/Skin
  > DENT WITH CRACK ON UPPER WING PANEL 34 INCHES FORWARD OF NR 6 SPOILER. REPAIRED PANEL PER SRM 51-40-6. (M)
- [SDR EISA97011](https://openairdocs.org/sdr/EISA97011.md): Skin · delaminated · Jan 21, 1997 · N6839 · Boeing 727223 · Spoilers
  > NR 1 SPOILER SKIN DELAMINATED, LOWER INBOARD FORWARD CORNER. REPAIRED SPOILER PER SRM 51-40-6. (M)
- [SDR EISA97010](https://openairdocs.org/sdr/EISA97010.md): Skin · delamination · Jan 21, 1997 · N6839 · Boeing 727223 · Ailerons
  > RIGHT WING OUTBOARD AILERON TAB SKIN HAS AREA OF DELAMINATION. REPAIRED TAB PER SRM 57-50-5. (M)
- [SDR EISA97009](https://openairdocs.org/sdr/EISA97009.md): Support · cracked · Jan 21, 1997 · N6839 · Boeing 727223 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT FRAME BETWEEN FS 1070 AND 1090 ABOVE STRINGER 27L IS CRACKED. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-2. (M)
- [SDR EISA97008](https://openairdocs.org/sdr/EISA97008.md): Skin · crease · Jan 21, 1997 · N6839 · Boeing 727223 · Fuselage Main, Plate/Skin
  > FS 188, 6 INCH CREASE IN SKIN AT STRINGER 23L. COLD WORKED AREA PER SRM 51-30-10. HFEC REVEALS NO CRACKS. INSTALLED FASTENERS PER SRM 51-30-2. (M)
- [SDR EISA96145](https://openairdocs.org/sdr/EISA96145.md): Engine · case crack · Aug 20, 1996 · N6839 · Boeing 727223 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE WOULD NOT MAKE TAKEOFF POWER. BOROSCOPED ENGINE FOUND INTERMEDIATE CASE AT 8TH STAGE BLEED BOSS CRACKED. REMOVED AND REPLACED ENGINE. (M)

## 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 = 'N6839' AND deregistration_id = 'N6839-2006-06-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N6839-2006-06-22/reports

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