# Service difficulty reports: N151FE, cancelled Jul 16, 2007

A list on [N151FE, cancelled Jul 16, 2007](https://openairdocs.org/deregistered/N151FE-2007-07-16.md).

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

- [SDR 06FDEA04137](https://openairdocs.org/sdr/06FDEA04137.md): Shutoff Valve · failed · Nov 29, 2006 · N151FE · Boeing 72722 · Cabin Cooling System
  > LOST PRESSURIZATION AT FL 260. COMPLIED WITH QRH, A/C DID NOT PRESSURIZE AUTO OR MANUAL. TROUBLESHOT TO LT PAC S/O VALVE INOP. PWR TO VALVE. REMOVED AND REPLACED LT PAC S/O VALVE PER SMP. LT PAC OPS NORMAL. PRESSURIZED A/C PER JRH TO 1 PSI DIFF OK FOR SE
- [SDR 05FDEA01746](https://openairdocs.org/sdr/05FDEA01746.md): Indicator · false indication · Jun 29, 2005 · N151FE · Boeing 727100 · Fuel Indicating System
  > NR 3 FUEL GAGE ERRONEOUS INDICATION, AT T/O SHOWED 11.1, SHORTLY INTO FLIGHT GAGE DROPPED 5K LBS. AT CRUISE FLT BOOST PUMPS ILLUMINATED. UPON LANDING AT KFSD, NR 3 FUEL QTY SHOWED EMPTY. ACFT RELEASED FOR SERVICE PER MEL/CDL: 28-11-02. FOUND NR 3 INDICATOR VE
- [SDR 05FDEA00081](https://openairdocs.org/sdr/05FDEA00081.md): Actuator · leaking · Jan 12, 2005 · N151FE · Boeing 727100 · Landing Gear Actuator
  > UPON GEAR RETRACT AFTER T/O RED RT GEAR LIGHT ILLUMINATED & AMBER RT MLG DOOR LIGHT ON S/O PANEL ILLUMINATED. MOVED GEAR HANDLE TO DOWN POS. 3 GREEN DOWN/LOCKED INDICATION & NO RED RT AMBER LIGHTS RAISED GEAR HANDLE AND RED RT GEAR LIGHT AND RT MLG DOOR LIGHT
- [SDR 05FDEA00020](https://openairdocs.org/sdr/05FDEA00020.md): Splice · cracked · Jan 4, 2005 · N151FE · Boeing 727100 · Fuselage Main, Longeron/Stringer
  > STRINGER 4R SPLICE IS CRACKED ON EACH SIDE OF FRAME AT STA 480. REMOVED AND REPLACED STRINGER 4R SPLICE AT STA 480 IAW SRM 51-10-1.
- [SDR 05FDEA00019](https://openairdocs.org/sdr/05FDEA00019.md): Rib · cracked · Jan 4, 2005 · N151FE · Boeing 727100 · Leading Edge Devices
  > SECOND INBOARD RIB IS CRACKED IN LEADING EDGE OF NR 5 SLAT. REMOVED AND REPLACED RIB IAW SRM 51-10-1.
- [SDR 04FDEA03505](https://openairdocs.org/sdr/04FDEA03505.md): Rib · cracked · Dec 29, 2004 · N151FE · Boeing 727100 · Elevator, Spar/Rib
  > RIGHT HORIZONTAL STAB ELEVATOR STATION 17.20, INBOARD RIB CRACK RUNS FROM RIVET ON UPPER. REMOVED RIB IAW SRM 51-30-2 & SB 727-55A0091. INSTALLED NEW RIB WITH P/N 65-17428-6 IAW SRM 51-30-2 & SB 727-55A0091.
- [SDR 04FDEA03437](https://openairdocs.org/sdr/04FDEA03437.md): Frame · corroded · Dec 17, 2004 · N151FE · Boeing 727100 · Fuselage Main, Frame
  > FLT CREW COMPARTMENT LEFT SIDE AT FS 227.8 FRAME HAS 2 EACH AREAS OF CORROSION ABOVE AND BELOW OXYGEN PANEL. REMOVED DAMAGE AREA IAW SRM 51-40-2, MADE NEW WEB FROM 7075-T6.125C BATCH 0000828965 & DOUBLER MADE FROM 7075-T6.160C BATCH 0000687676 IAW SRM 51
- [SDR 04FDEA03433](https://openairdocs.org/sdr/04FDEA03433.md): Web · chafed · Dec 17, 2004 · N151FE · Boeing 727100 · Leading Edge Devices
  > LT WING NR 3 L/E FLAP INBD ANTI-ICE DUCT CHAFING FLAP. REMOVED & REPLACED WEB IAW SRM 51-30-2, NEW WEB FABBED FROM 2024-T3.050, BATCH 814135, FOUND INNER SKIN DAMAGED, CUT OUT AREA IAW SRM 57-30-4 FIG 5. FABBED & INSTALLED COVER & FILLER FROM 2024-T3.016 B
- [SDR 04FDEA03432](https://openairdocs.org/sdr/04FDEA03432.md): Web · chafed · Dec 17, 2004 · N151FE · Boeing 727100 · Leading Edge Devices
  > LT WING NR 3 L/E FLAP INBD ANTI-ICE DUCT CHAFING FLAP. REMOVED & REPLACED WEB IAW SRM 51-30-2, NEW WEB FABBED FROM 2024-T3.050, BATCH 814135, FOUND INNER SKIN DAMAGED, CUT OUT AREA IAW SRM 57-30-4 FIG 5. FABBED & INSTALLED COVER & FILLER FROM 2024-T3.016 B
- [SDR 04FDEA03204](https://openairdocs.org/sdr/04FDEA03204.md): Warning System · activated · Nov 24, 2004 · N151FE · Boeing 72722 · Central Warning
  > RECEIVED GND PROX WARNING ON TAKEOFF. PERFORMED ESCAPE MANEUVER USING FIREWALL POWER. FUEL WAS DUMPED TO MAX LDG WT. NO EMERGENCY WAS DECLARED. OTHER FLIGHT INFO AS FOLLOWS: 1000' AGL 10"C OAT 180 KIAS AIRSPEED BLEEDS 1 & 3 OPEN NR 2 CLOSED EGT APPROX 540"
- [SDR 04FDEA00166](https://openairdocs.org/sdr/04FDEA00166.md): Connector · contaminated · Jan 15, 2004 · N151FE · Boeing 727100 · Landing Gear Position and Warning
  > ON APPROACH, UPON LOWERING LANDING GEAR, NOSE GEAR INDICATED UNSAFE (RED GEAR LIGHT ON, GREEN LIGHT OUT). RAN EMERGENCY PROCEDURES, CYCLED GEAR AND GOT 3 DOWN INDICATIONS. CLEANED SNOW AND ICE FROM LOCK AND POSITION SWITCHES CLEANED CONNECTOR. NOSE GEAR STI
- [SDR 02FDEA00521](https://openairdocs.org/sdr/02FDEA00521.md): Shear Tie · corroded · Jul 25, 2002 · N151FE · Boeing 727100 · Fuselage Main, Structure
  > CORROSION ON SHEAR TIE AT BS 968, RBL 3-5, WL 150. REPAIRED SHEAR TIE IAW SRM.
- [SDR 02FDEA00508](https://openairdocs.org/sdr/02FDEA00508.md): Shear Tie · gouged · Jul 20, 2002 · N151FE · Boeing 727100 · Fuselage Main, Structure
  > SHEAR TIE GOUGED AT BS 540, JUST BELOW STR 14R. REPAIRED SHEAR TIE BS 540 BELOW STR 14R IAW SRM 53-10-4, 53-10-2.
- [SDR 02FDEA00289](https://openairdocs.org/sdr/02FDEA00289.md): Altimeter · failed · Apr 25, 2002 · N151FE · Boeing 72722 · Altimeter, Barometric/Encoder
  > CAPT'S ALTIMETER GOT OFF FLAG ON CLIMBOUT, ALSO GOT OFF FLAG IN ALTITUDE ALERT BOX, WHEN OFF FLAG SHOWING, ALTIMETER DIDN'T MOVE. REMOVED AND REPLACED CAPT'S ALTIMETER PER MM 34-12-011-5.
- [SDR 01FDEA00966](https://openairdocs.org/sdr/01FDEA00966.md): Line · blown · Nov 6, 2001 · N151FE · Boeing 72722 · Pneumatic Distribution System
  > NR 1 ENGINE STRUT OVERHEAD LIGHT CAME ON. REMOVED AND REPLACED BLOWN T/R HOSE IN NR 1 PYLON AREA. NO LEAKS NOTED. OK FOR SERVICE.
- [SDR 01FDEA00964](https://openairdocs.org/sdr/01FDEA00964.md): Clamp · loose · Nov 2, 2001 · N151FE · Boeing 72722 · Pneumatic Distribution System
  > NR 1 ENG STRUT OVERHEAD LIGHT ILLUM. SECURED CLAP AND CONNECTOR PER MM 36-00-000-5. OPS CHECK OK.
- [SDR 01FDEA00951](https://openairdocs.org/sdr/01FDEA00951.md): Clamp · loose · Nov 1, 2001 · N151FE · Boeing 72722 · Overheat Detection
  > 01-357 #1 ENG STRUT OVERHEAT ILLUM IN GLT. TIGHTENED CLAMP ON HIGH PRESS MODULATING VALVE (SHUTOFF).
- [SDR 01FDEA00178](https://openairdocs.org/sdr/01FDEA00178.md): Filter · dirty · Mar 7, 2001 · N151FE · Boeing 72722 · Turbine Engine Oil System
  > NR 3 OIL BYPASS LIGHT CAME ON. COMPLIED WITH RED TABS AND SHUTDOWN ENGINE. OIL PRESS AND TEMP NORMAL. *S/D* CHANGE FILTER PER 727-100 MM 79-00-000-2, CHANGE OIL PRESS DIFFERENTIAL SWITCH AS PRECAUTIONARY DUE TO HEAVY CARBON BUILD UP ON FILTER PER MM 79-33-
- [SDR 00FDEA00144](https://openairdocs.org/sdr/00FDEA00144.md): Frame · corroded · Mar 8, 2000 · N151FE · Boeing 72722 · Fuselage Main, Frame
  > NR 833, WHILE WORKING NR-0525 FOUND CORROSION ON AFT CARGO DOOR FRAME FWD FRAME WEB STR 26 RT AREA MARKED.
- [SDR 00FDEA00119](https://openairdocs.org/sdr/00FDEA00119.md): Skin · corroded · Feb 29, 2000 · N151FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > NR 112 SKIN BULGING AT LOWER NOSE CHORD BS 328, RBL 20, JUST ABOVE NOSE GEAR STRUT DOOR CUTOUT (C53-100-01). REPAIRED PER FEDEX EA 7-5330-50011.
- [SDR 00FDEA00090](https://openairdocs.org/sdr/00FDEA00090.md): Frame · corroded · Feb 18, 2000 · N151FE · Boeing 72722 · Fuselage Main, Frame
  > WHILE WORKING NR 112 FOUND CORROSION ON NOSE CHORD AT BS 343, RBL 20, WL 149.
- [SDR 00FDEA00089](https://openairdocs.org/sdr/00FDEA00089.md): Web · corroded · Feb 18, 2000 · N151FE · Boeing 72722 · Wing Miscellaneous Structure
  > NR 693 CORROSION (C57-571-01-01) ON L/W FRONT SPAR WEB AT FUEL CELL PANEL CUT OUT 7340, FWD AND AFT WEB SURFACE WS 182. REMOVED AND REPLACED CORROSION PER FEDEX SRM 57-10-1, AND IAW FEDEX EA 7-5710-47901, FUEL LEAK CK IAW FEDEX MM 28-11-000-8 DTEP 7C.
- [SDR 00FDEA00082](https://openairdocs.org/sdr/00FDEA00082.md): Frame · corroded · Feb 16, 2000 · N151FE · Boeing 72722 · Fuselage Main, Frame
  > NR 113 - CORROSION AT INNER CHORD BS 292, RBL22, WL 154, AS SEEN THROUGH LIGHTENING HOLE INSIDE NOSE WW (C53-100-01).
- [SDR 00FDEA00077](https://openairdocs.org/sdr/00FDEA00077.md): Strap · bent · Feb 14, 2000 · N151FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > WHILE WORKING NRC-805 (FUSELAGE 194) FOUND STABILIZER STRAP BS 1030-1130, STR 27R TO BE BENT AND HAS DOUBLE HOLES. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-30-2, 53-10-1.
- [SDR 00FDEA00076](https://openairdocs.org/sdr/00FDEA00076.md): Web · gouged · Feb 14, 2000 · N151FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > WHILE WORKING NR 805 (FUSELAGE 194) FOUND VERTICAL WEB TO BE GOUGED IN SEVERAL LOCATIONS BS 1057-1110, STR 27 RT. *S/D* REMOVED AND REPLACED, ALODINED, PRIMED AND PAINTED IAW FEDEX MM 51-20-151.
- [SDR 00FDEA00063](https://openairdocs.org/sdr/00FDEA00063.md): Frame · corroded · Feb 9, 2000 · N151FE · Boeing 72722 · Fuselage Main, Frame
  > WHILE WORKING NR 113, FOUND SHEAR TIE AT BS 320, RBL 18-21, WL 151 TO BE CORRODED. *S/D* REPAIRED IAW FEDEX SRM 53-10-4 FIG 15.
- [SDR 00FDEA00062](https://openairdocs.org/sdr/00FDEA00062.md): Frame · corroded · Feb 9, 2000 · N151FE · Boeing 72722 · Fuselage Main, Frame
  > WHILE WORKING NR 112 FOUND HORIZONTAL CHORD CORRODED BS 348, WL 168, RBL 16. *S/D* REMOVED AND REPLACED CHORD PER IAW FEDEX SRM 51-30-2.
- [SDR 00FDEA00061](https://openairdocs.org/sdr/00FDEA00061.md): Skin · corroded · Feb 7, 2000 · N151FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > CORROSION AND FASTENERS PULLED THRU OUTER SKIN AT BOTTOM SIDE OF CARGO CUTOUT BS 1065 - 1090, STR 26R. *S/D* REPAIRED AFT CARGO DOOR PER FEDEX EA 7-5330-50016.
- [SDR 00FDEA00040](https://openairdocs.org/sdr/00FDEA00040.md): Shear Tie · corroded · Jan 27, 2000 · N151FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > WHILE WORKING NR 0113, FOUND SHEAR TIE AT BS 344, RBL 21-24, WL 151 TO BE CORRODED. *S/D* REPAIRED IAW FEDEX SRM 53-10-4, FIG 11.
- [SDR 00FDEA00039](https://openairdocs.org/sdr/00FDEA00039.md): Frame · gouged · Jan 27, 2000 · N151FE · Boeing 72722 · Fuselage Main, Frame
  > MAIN CARGO DOOR REPAIR DOUBLER ON LWR AFT SIDE FRAME WAS GOUGED. *S/D* REMOVED AND REPLACED ALODINED, PRIMED AND INSTALLED PER FEDEX SRM 51-10-2, 51-30-8, 51-20-1, 51-10-3.
- [SDR 00FDEA00034](https://openairdocs.org/sdr/00FDEA00034.md): Frame · cracked · Jan 25, 2000 · N151FE · Boeing 72722 · Fuselage Main, Frame
  > CRACKED FRAME BS 1050 BETWEEN STR 26 RT & 27 RT. *S/D* REMOVED AND REPLACED PER FEDEX EA 7-5310-47886.
- [SDR 00FDEA00033](https://openairdocs.org/sdr/00FDEA00033.md): Skin · cracked · Jan 25, 2000 · N151FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > NR 805 - CORROSION AND FASTENERS PULLED THROUGH OUTER SKIN, BOTTOM SIDE OF CARGO DOOR CUT-OUT BS 1065-1090, STR 26R.
- [SDR 00FDEA00035](https://openairdocs.org/sdr/00FDEA00035.md): Bulkhead · damaged · Jan 24, 2000 · N151FE · Boeing 72722 · Fuselage Main, Bulkhead
  > WHILE WORKING 71C101-02, FOUND STRUCTURAL DAMAGE AT BS 227.8, LBL 12, WL 163 ON PRESSURE BULKHEAD. *S/D* REMOVED AND REPLACED PER SRM 51-40-2 FIG 1.
- [SDR 00FDEA00026](https://openairdocs.org/sdr/00FDEA00026.md): Floorbeam · corroded · Jan 18, 2000 · N151FE · Boeing 72722 · Fuselage Main, Floor Beam
  > NR 705 - CORROSION (C53-224-01(1)) ON UPPER CHORD OF FLOORBEAM AT BS 620 BL0- LBL 24, WL 208. REMOVED AND REPLACED PER FEDEX SRM 53-10-8, 53-10-2.
- [SDR 00FDEA00019](https://openairdocs.org/sdr/00FDEA00019.md): Skin · corroded · Jan 17, 2000 · N151FE · Boeing 72722 · Trailing Edge Flaps
  > NR 368 - NR 3 K-FLAP TO BULLNOSE I/B BONDING JUMPER HAS CORROSION UNDER ITS WASHERS AT BOTH ATTACH PTS. REPAIRED AND ATTACH PT IAW FEDEX DWG SR 27-57-010 AND SRM 57-50-3 PG 8-8B.
- [SDR 00FDEA00018](https://openairdocs.org/sdr/00FDEA00018.md): Web · cracked · Jan 17, 2000 · N151FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR 223 - LT TORQUE BOX WEB LOWER LIGHTENING HOLE AT BS 1297 IS CRACKED. REMOVED AND REPLACED DOUBLER IAW FEDEX SRM 51-40-2.
- [SDR 00FDEA00017](https://openairdocs.org/sdr/00FDEA00017.md): Chord · corroded · Jan 17, 2000 · N151FE · Boeing 72722 · Fuselage Main, Structure
  > NR 235 - CORROSION ON REINFORCEMENT CHORD BS1176, LBL 20, WL 208.
- [SDR 00FDEA00016](https://openairdocs.org/sdr/00FDEA00016.md): Floorbeam · corroded · Jan 17, 2000 · N151FE · Boeing 72722 · Fuselage Main, Floor Beam
  > NR 657 - CORROSION (C53-224-02) ON BS 680 FLOORBEAM WL 208, LBL 10.5 AT FASTENER HOLE. REPAIRED FLOORBEAM PER IAW FEDEX SRM 53-10-8 FIG 8.
- [SDR 00FDEA00015](https://openairdocs.org/sdr/00FDEA00015.md): Floorbeam · corroded · Jan 17, 2000 · N151FE · Boeing 72722 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM UPPER TEE BS 640, RBL 27-52, WL 208.
- [SDR 00FDEA00014](https://openairdocs.org/sdr/00FDEA00014.md): Frame · cracked · Jan 12, 2000 · N151FE · Boeing 72722 · Fuselage Main, Frame
  > BS 620 FRAME CRACKED IN RADIUS OF STR 20R CUTOUT. *S/D* REMOVED AND REPLACED FRAME, FAB DOUBLER FILLER AND WEB ANGLE, ALODINED, PRIMED SEALED IAW FEDEX EA 7-5310-47885.
- [SDR 97FDEA00664](https://openairdocs.org/sdr/97FDEA00664.md): Clip · cracked · Sep 18, 1997 · N151FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR 3 AND NR 4 LEFT HAND STRINGER CLIPS AT BS 1050 ARE CRACKED. *S/D* REMOVED CRACKED STRINGER CLIPS AT NR 3 AND NR 4 LT STRINGER AT BS 1050. INSTALLED NEW STRINGER CLIPS IAW FED-EX SRM 51-30-2, 51-10-1, M/M 25-52-2.
- [SDR 97FDEA00651](https://openairdocs.org/sdr/97FDEA00651.md): Chord · corroded · Sep 11, 1997 · N151FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > CORROSION (C53-224-08) ON REINFORCEMENT CHORD AT BS 1176.9, RBL 48 AND RBL 37, WL 208. *S/D* FOUND TO BE OUT OF LIMITS. REPLACED SEGMENT OF REINFORCEMENT CHORD AT BS 1176.9, RBL 32.75 TO 70.5, WL 208 AS PER FED EX EA NR 7-5310-53102.
- [SDR 97FDEA00648](https://openairdocs.org/sdr/97FDEA00648.md): Spoiler · delaminated · Sep 11, 1997 · N151FE · Boeing 72722 · Spoilers
  > NR 0195 004 NR 2 SPOILER TRAILING EDGE IS DELAMINATED. REPAIRED NR 2 SPOILER IAW FED-EX SRM 57-50-06.
- [SDR 97FDEA00647](https://openairdocs.org/sdr/97FDEA00647.md): Skin · delaminated · Sep 11, 1997 · N151FE · Boeing 72722 · Trailing Edge Flaps
  > LEFT WING I/B FOREFLAP HAS 6 X 6 AREA OF DELAMINATION ON UPPER I/B END. *S/D* REMOVED DAMAGED SKIN AND REPAIRED IAW FED SRM 51-40-6, LT I/B FOREFLAP.
- [SDR 97FDEA00644](https://openairdocs.org/sdr/97FDEA00644.md): Flap · delaminated · Sep 10, 1997 · N151FE · Boeing 72722 · Trailing Edge Flaps
  > NR 0248 002 LEFT WING I/B MIDFLAP T/E WEDGE HAS AREA OF DELAMINATION ON O/B END. REMOVED DAMAGED AREA 9.25 BY 4 ON UPPER SURFACE OVERLAYED WITH RESIN IMPREGNATED FIBERGLASS, VACUUMED, BAGGED, SANDED, SEALED, PRIMED AND PAINTED L/T WING T/E WEDGE I/B MIDFLAP I
- [SDR 97FDEA00643](https://openairdocs.org/sdr/97FDEA00643.md): Flap · delaminated · Sep 10, 1997 · N151FE · Boeing 72722 · Trailing Edge Flaps
  > NR 0249 001 RIGHT WING O/B MIDFLAP T/E WEDGE HAS TWO AREAS OF DELAMINATION ON UPPER SKIN. REMOVED DAMAGE 9 BY 3.5 OVERLAYED WITH RESIN IMPREGNATED FIBERGLASS VACUUM BAGGED. SANDED, SEALED, PRIMED AND PAINTED R/W O/B MIDFLAP IAW FED-EX SRM 51-40-06.

## 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 = 'N151FE' AND deregistration_id = 'N151FE-2007-07-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N151FE-2007-07-16/reports

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