# Service difficulty reports: N856FT, cancelled Oct 16, 2001

A list on [N856FT, cancelled Oct 16, 2001](https://openairdocs.org/deregistered/N856FT-2001-10-16.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 8 · 375 reports

- [SDR P5CA9900668](https://openairdocs.org/sdr/P5CA9900668.md): Skin · delaminated · Jul 13, 1999 · N856FT · Boeing 747132 · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE FIXED PANEL DELAMINATED. REPAIRED PER SRM 51-40-09.
- [SDR P5CA9900667](https://openairdocs.org/sdr/P5CA9900667.md): Skin · delaminated · Jul 13, 1999 · N856FT · Boeing 747132 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER LOWER SURFACE OF TRAILING EDGE NEAR OUTBOARD ELEVATOR FOUND DELAMINATION. REPAIRED PER SRM 51-40-09.
- [SDR P5CA9900666](https://openairdocs.org/sdr/P5CA9900666.md): Skin · delaminated · Jul 13, 1999 · N856FT · Boeing 747132 · Elevator, Plate/Skin
  > LEFT INBOARD ELEVATOR TRAILING EDGE DELAMINATED. REPAIRED PER SRM 51-40-09.
- [SDR P5CA9900665](https://openairdocs.org/sdr/P5CA9900665.md): Skin · delaminated · Jul 13, 1999 · N856FT · Boeing 747132 · Trailing Edge Flaps
  > OUTBOARD FWD FLAP TRAILING EDGE DELAMINATED. REPAIRED PER SRM 51-40-09.
- [SDR P5CA9900664](https://openairdocs.org/sdr/P5CA9900664.md): Skin · delamination · Jul 13, 1999 · N856FT · Boeing 747132 · Trailing Edge Flaps
  > OUTBOARD AFT FLAP LOWER SURFACE FOUND DELAMINATED. REPAIRED PER SRM 51-40-09.
- [SDR P5CA9900663](https://openairdocs.org/sdr/P5CA9900663.md): Skin · delaminated · Jul 13, 1999 · N856FT · Boeing 747132 · Trailing Edge Flaps
  > RIGHT INBOARD MID FLAP LEADING EDGE HAS DELAMINATION. REPAIRED PER SRM 51-40-09.
- [SDR P5CA9900662](https://openairdocs.org/sdr/P5CA9900662.md): Skin · delaminated · Jul 13, 1999 · N856FT · Boeing 747132 · Trailing Edge Flaps
  > RIGHT INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED PER SRM 51-40-09.
- [SDR P5CA9900660](https://openairdocs.org/sdr/P5CA9900660.md): Skin · delaminated · Jul 13, 1999 · N856FT · Boeing 747132 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STABILIZER NR 5 ACCESS PANEL HAS SEVERE AREAS OF DELAMINATION. REBONDED SKIN TO THE HONEYCOMB PER SRM 51-40-06.
- [SDR P5CA9900659](https://openairdocs.org/sdr/P5CA9900659.md): Skin · delaminated · Jul 13, 1999 · N856FT · Boeing 747132 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER NR 3 ACCESS PANEL 334JB DELAMINATED ON INNER SKIN. REBONDED SKIN TO HONEYCOMB PER SRM 51-10-06.
- [SDR P5CA9900658](https://openairdocs.org/sdr/P5CA9900658.md): Skin · corroded · Jul 13, 1999 · N856FT · Boeing 747132 · Fuselage Main, Plate/Skin
  > LEVEL 1 CORROSION ON PANEL SKIN BEHIND REAR SPAR WBL 235 LEFT WING. REMOVED RIVETS AND REPAIRED CORROSION PER SRM 57-10-01.
- [SDR P5CA9900657](https://openairdocs.org/sdr/P5CA9900657.md): Skin · corroded · Jul 11, 1999 · N856FT · Boeing 747132 · Fuselage Main, Plate/Skin
  > LEVEL 1 CORROSION ON SKIN BETWEEN STA 250-260 STR 27 AND 28 LEFT. REMOVED CORROSION PER SRM 51-10-02 AND 53-30-01.
- [SDR P5CA9900656](https://openairdocs.org/sdr/P5CA9900656.md): Skin · corroded · Jul 11, 1999 · N856FT · Boeing 747132 · Fuselage Main, Plate/Skin
  > LEVEL 1 CORROSION FOUND ON SKIN BETWEEN STA 180-200 STR 44 RIGHT SIDE. CORROSION REMOVED PER SRM 51-10-02 AND 53-30-01.
- [SDR P5CA9900655](https://openairdocs.org/sdr/P5CA9900655.md): Skin · corroded · Jul 11, 1999 · N856FT · Boeing 747132 · Fuselage Main, Plate/Skin
  > LEVEL 1 CORROSION FOUND ON SKIN AT STR 14 BETWEEN STA 2780 AND 2200 AND STA 2240 AND 2280 ON RIGHT SIDE. REMOVED CORROSION PER SRM 51-00-02 AND 53-30-01.
- [SDR P5CA9900653](https://openairdocs.org/sdr/P5CA9900653.md): Skin · corroded · Jul 11, 1999 · N856FT · Boeing 747132 · Fuselage Main, Plate/Skin
  > LEVEL 1 CORROSION FOUND ON SKIN BETWEEN STA 740 AND 760 RIGHT SIDE. CLEANED AND REPAIRED PER SRM 51-10-02 AND 53-30-07.
- [SDR P5CA9900654](https://openairdocs.org/sdr/P5CA9900654.md): Skin · corroded · Jul 2, 1999 · N856FT · Boeing 747132 · Fuselage Main, Plate/Skin
  > LEVEL 1 CORROSION ON LAP JOINT STR 23 STA 1820-1780 RIGHT SIDE. CORROSION REMOVED AND REPAIRED PER SRM 51-10-02 AND 53-30-01.
- [SDR P5CA9900571](https://openairdocs.org/sdr/P5CA9900571.md): Fuel Control · malfunctioned · May 22, 1999 · N856FT · Boeing 747132 · Fuel Control/Turbine Engines
  > DURING DESCENT LEAVING FL350 APPROACHING FL330 FUEL HEAT WAS ON NR 3 ENGINE, WOULD NOT RESPOND BEYOND 65 PERCENT TO THROTTLE MOVEMENT. NO LOUD NOISES, NO EGT INCREASES. ENGINE WAS SHUTDOWN AND RESTARTED PER AOM. NO FUEL FLOW WITH START LEVER IN IDLE. PLACE
- [SDR P5CA9801597](https://openairdocs.org/sdr/P5CA9801597.md): Light · inop · Nov 15, 1998 · N856FT · Boeing 747132 · Emergency Lighting
  > EMERGENCY EXIT LIGHT INOP AT DOOR SLIDE AREA. REPLACED EMERGENCY LIGHT MODULE AT UPPER DOOR OVERHEAD LOCATION. OPS CHECK NORMAL PER MM 35-51-00.
- [SDR P5CA9801596](https://openairdocs.org/sdr/P5CA9801596.md): Light · inop · Nov 15, 1998 · N856FT · Boeing 747132 · Emergency Lighting
  > EMERGENCY LIGHT IN UPPER DECK DOME INOP. REPLACED EMERGENCY LIGHT ASSY AND CKECKED OK PER MM 35-51-00.
- [SDR P5CA9801579](https://openairdocs.org/sdr/P5CA9801579.md): Connector · loose · Sep 23, 1998 · N856FT · Boeing 747132 · Emergency Lighting
  > EMERGENCY LIGHTING DOES NOT WORK. CLEANED AND RESEATED CANNON PLUG ON EMERGENCY PANEL SYSTEM. OPS NORMAL PER MM 33-51-00.
- [SDR P5CA9801206](https://openairdocs.org/sdr/P5CA9801206.md): Bulkhead · damaged · Jul 23, 1998 · N856FT · Boeing 747132 · Nacelle/Pylon, Bulkhead/Firewall
  > NR 4 PYLON INTERNAL AT BULKHEAD LINE PASS THROUGH ELONGATED. REPAIRED PER SRM 54-10-03 AND MM 20-11-05.
- [SDR P5CA9801205](https://openairdocs.org/sdr/P5CA9801205.md): Skin · delaminated · Jul 23, 1998 · N856FT · Boeing 747132 · Air Conditioning Doors
  > NR 3 AIR CONDITIONING BAY DOOR DELAMINATED. REPAIRED PER SRM 51-24-11 AND 51-40-15.
- [SDR P5CA9801204](https://openairdocs.org/sdr/P5CA9801204.md): Fairing · delaminated · Jul 23, 1998 · N856FT · Boeing 747132 · Nacelle/Pylon Structure
  > NR 3 PYLON V FAIRING DELAMINATED. REPAIRED PER SRM 51-30-07.
- [SDR P5CA9801203](https://openairdocs.org/sdr/P5CA9801203.md): Panel · delaminated · Jul 23, 1998 · N856FT · Boeing 747132 · Wing, Plate/Skin
  > RIGHT WING UPPER SURFACE TRAILING EDGE PANEL DELAMINATED. REPAIRED PER SRM 51-40-15 AND 51-24-11.
- [SDR P5CA9801202](https://openairdocs.org/sdr/P5CA9801202.md): Angle · cracked · Jul 23, 1998 · N856FT · Boeing 747132 · Engine Cowling System
  > NR 1 ENGINE INBOARD CORE COWL MOST AFT RIB ASSY HAS CRACKED ANGLE. REPAIRED PER SRM 51-10-01 AND 51-30-01.
- [SDR P5CA9801201](https://openairdocs.org/sdr/P5CA9801201.md): Fairing · delaminated · Jul 23, 1998 · N856FT · Boeing 747132 · Nacelle/Pylon Structure
  > NR 4 PYLON V FAIRING DELAMINATED. REMOVED AND REPLACED FAIRING SRM 51-10-01 AND 51-30-02.
- [SDR P5CA9801200](https://openairdocs.org/sdr/P5CA9801200.md): Fairing · delaminated · Jul 23, 1998 · N856FT · Boeing 747132 · Air Conditioning Doors
  > NR 3 PACK EXIT DOOR FAIRING PANEL DELAMINATED. REPAIRED PER SRM 51-40-15.
- [SDR P5CA9801199](https://openairdocs.org/sdr/P5CA9801199.md): Stinger · loose · Jul 23, 1998 · N856FT · Boeing 747132 · Engine Thrust Reverser
  > NR 1 ENGINE STINGER ASSY LOOSE AND MISSING FASTENERS. REPAIRED PER SRM 51-30-02.
- [SDR P5CA9801198](https://openairdocs.org/sdr/P5CA9801198.md): Fastener · missing · Jul 23, 1998 · N856FT · Boeing 747132 · Air Conditioning Doors
  > PANEL 191NL MISSING FASTENERS. REPAIRED PER SRM 51-30-02.
- [SDR P5CA9801197](https://openairdocs.org/sdr/P5CA9801197.md): Exhaust Sleeve · loose · Jul 23, 1998 · N856FT · Boeing 747132 · Engine Collector/Tailpipe/Nozzle
  > NR 3 ENGINE EXHAUST SLEEVE A 1 O'CLOCK POSITION LOOSE FASTENERS. REPAIRED PER SRM 51-30-02.
- [SDR P5CA9801196](https://openairdocs.org/sdr/P5CA9801196.md): Fairing · damaged · Jul 23, 1998 · N856FT · Boeing 747132 · Engine Cowling System
  > NR 4 ENGINE DOG HOUSE FAIRING TORN/DAMAGED. REPAIRED TO SRM 51-40-02.
- [SDR P5CA9801195](https://openairdocs.org/sdr/P5CA9801195.md): Cowl · damage · Jul 23, 1998 · N856FT · Boeing 747132 · Engine Cowling System
  > NR 2 ENGINE INBOARD POWER COWL LOWER CORNER SKIN DAMAGED. REPAIRED PER SRM 54-30-03 AND 51-10-02.
- [SDR P5CA9801194](https://openairdocs.org/sdr/P5CA9801194.md): Rib · cracked · Jul 23, 1998 · N856FT · Boeing 747132 · Engine Cowling System
  > NR 2 ENGINE INBOARD POWER COWL RIB CRACKED. REPAIRED PER SRM 51-30-02 AND 51-10-01.
- [SDR P5CA9801193](https://openairdocs.org/sdr/P5CA9801193.md): Panel · delaminated · Jul 23, 1998 · N856FT · Boeing 747132 · Wing, Plate/Skin
  > LEFT WING UPPER SURFACE PANEL DELAMINATED INBD 2ND FROM ROOT AREA. REPAIRED PER SRM 51-40-15.
- [SDR P5CA9801192](https://openairdocs.org/sdr/P5CA9801192.md): Cowl · loose · Jul 23, 1998 · N856FT · Boeing 747132 · Engine Cowling System
  > NR 2 ENGINE CORE COWL 3RD LATCH AREA HAS LOOSE FASTENERS. REPAIRED PER SRM 51-30-02.
- [SDR P5CA9801191](https://openairdocs.org/sdr/P5CA9801191.md): Cowl · loose · Jul 23, 1998 · N856FT · Boeing 747132 · Engine Cowling System
  > NR 1 ENGINE OUTBOARD CORE COWL TOP AFT CORNER LOOSE FASTENERS. REPAIRED PER SRM 51-30-02.
- [SDR P5CA9801190](https://openairdocs.org/sdr/P5CA9801190.md): Hinge · corrosion · Jul 23, 1998 · N856FT · Boeing 747132 · Landing Gear Doors
  > RIGHT CENTER GEAR DOOR HINGE LIGHT SURFACE CORROSION. REPAIRED BY SRM 51-10-02 AND 51-10-06.
- [SDR P5CA9801189](https://openairdocs.org/sdr/P5CA9801189.md): Skin · delaminated · Jul 23, 1998 · N856FT · Boeing 747132 · Spoilers
  > NR 4 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PANEL PER MM 27-61-02.
- [SDR P5CA9801188](https://openairdocs.org/sdr/P5CA9801188.md): Cowl · cracked · Jul 23, 1998 · N856FT · Boeing 747132 · Engine Cowling System
  > NR 1 ENGINE OUTBD CORE COWL MOST AFT LATCH HOUSING CRACKED AND DAMAGED. REPAIRED PER SRM 51-30-02.
- [SDR P5CA9801187](https://openairdocs.org/sdr/P5CA9801187.md): Cowl · chafed · Jul 23, 1998 · N856FT · Boeing 747132 · Engine Cowling System
  > NR 2 ENGINE INBD CORE COWL PREVIOUS REPAIR CHAFFED THROUGH. REPAIRED PER SRM 54-30-03.
- [SDR P5CA9801186](https://openairdocs.org/sdr/P5CA9801186.md): Panel · delaminated · Jul 23, 1998 · N856FT · Boeing 747132 · Wing, Plate/Skin
  > RIGHT WING UPPER SURFACE FIXED TRAILING EDGE PANEL DELAMINATED. REPAIRED PER SRM 51-40-15.
- [SDR P5CA9801185](https://openairdocs.org/sdr/P5CA9801185.md): Skin · delaminated · Jul 23, 1998 · N856FT · Boeing 747132 · Landing Gear Doors
  > LEFT WING GEAR DOOR CORNER DELAMINATED. REPAIRED PER SRM 51-40-09.
- [SDR P5CA9801184](https://openairdocs.org/sdr/P5CA9801184.md): Skin · delaminated · Jul 23, 1998 · N856FT · Boeing 747132 · Landing Gear Doors
  > RIGHT WING GEAR DOOR 5 INCH DELAMINATED. REPAIRED PER SRM 51-40-09.
- [SDR P5CA9801183](https://openairdocs.org/sdr/P5CA9801183.md): Skin · delaminated · Jul 23, 1998 · N856FT · Boeing 747132 · Trailing Edge Flaps
  > LEFT OUTBOARD TRAILING EDGE AFT FLAP LOWER SURFACE 4 FOOT DELAMINATION. REPAIRED PER SRM 51-40-07.
- [SDR P5CA9801182](https://openairdocs.org/sdr/P5CA9801182.md): Panel · delamination · Jul 22, 1998 · N856FT · Boeing 747132 · Wing, Plate/Skin
  > LEFT WING UPPER SURFACE FWD INBOARD TRAILING EDGE PANEL DELAMINATED. REPAIRED PER SRM 51-40-09.
- [SDR P5CA9801173](https://openairdocs.org/sdr/P5CA9801173.md): Press Xmtr · inoperative · Jul 13, 1998 · N856FT · Boeing 747132 · Hydraulic Pressure Sensor
  > NR 4 HYD PRESS PEGGED AT 4,000 PSI, FOLLOWED BY A LOW QTY ANNUNCIATOR AND DECREASING HYD QTY. HYD TEMP REMAINED NORMAL PRIOR TO AND FOLLOWING ABNORMAL PROCEDURES IN AOM. REPLACED NR 4 HYD PRESS TRANSMITTER IAW MM 29-31-01. OPS AND LEAK CHECK NORMAL. SYSTEM
- [SDR P5CA9801172](https://openairdocs.org/sdr/P5CA9801172.md): Battery Pack · discharged · Jul 13, 1998 · N856FT · Boeing 747132 · Emergency Lighting
  > UPPER DECK EMERGENCY LIGHTS WILL NOT GO OUT WITH POWER OFF POSTION. REMOVED AND REPLACED UPPER DECK EMERGENCY LIGHTING BATTERY PACK PER MM 33-51-00.
- [SDR P5CA9800230](https://openairdocs.org/sdr/P5CA9800230.md): Hinge · cracked · Feb 13, 1998 · N856FT · Boeing 747132 · Landing Gear Doors
  > LT WING GEAR DOOR HINGE FWD POSITION FAILURE, FOUND AFTER BLOCK-IN. FOUND NO OTHER DAMAGE. REMOVED AND REPLACED FWD HINGE PER MM 32-12-01.
- [SDR P5CA9800212](https://openairdocs.org/sdr/P5CA9800212.md): Seat Track · corrosion · Jan 21, 1998 · N856FT · Boeing 747132 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 1 CORROSION, FOUND ON MAIN DECK SEAT TRACK AT BS 1900 BL 11. BLENDED AND TREATED PER BOEING SRM 53-10-01.
- [SDR P5CA9800211](https://openairdocs.org/sdr/P5CA9800211.md): Seat Track · corrosion · Jan 21, 1998 · N856FT · Boeing 747132 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, ON MAIN DECK SEAT TRACK FLANGE BS 1920-2040. REPLACED TRACK PER SRM 53-10-01.
- [SDR P5CA9800210](https://openairdocs.org/sdr/P5CA9800210.md): Trunnion · corrosion · Jan 21, 1998 · N856FT · Boeing 747132 · Fuselage, Landing Gear Attach Fittings
  > LEVEL 1 CORROSION, FOUND LT I/B BODY GEAR TRUNNION AND TRUNNION CAP. TRUNNION BORE MACHINED NDT OK BUSHING CUT TRUNNION CAP. REPLACED PER BOEING SRM 53-10-08 ITEM 1-24.

Next page: https://openairdocs.org/deregistered/N856FT-2001-10-16/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 = 'N856FT' AND deregistration_id = 'N856FT-2001-10-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N856FT-2001-10-16/reports

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