# Service difficulty reports: N272FE, cancelled Nov 28, 2007

A list on [N272FE, cancelled Nov 28, 2007](https://openairdocs.org/deregistered/N272FE-2007-11-28.md).

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

- [SDR 05FDEA01778](https://openairdocs.org/sdr/05FDEA01778.md): Seat Track · corroded · Jul 2, 2005 · N272FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 24 HAS CORROSION AT 500 TO 520 AND STA 620. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5 FIG 1 PG 4
- [SDR 05FDEA01776](https://openairdocs.org/sdr/05FDEA01776.md): Tee Fitting · corroded · Jul 1, 2005 · N272FE · Boeing 727200 · Fuselage Main, Structure
  > TEE CHORD 760 -787 RBL 45 IS CORRODED. REMOVED AND REPLACED TEE CHORD IAW SRM 51-30- 2
- [SDR 05FDEA01775](https://openairdocs.org/sdr/05FDEA01775.md): Tee Fitting · corroded · Jul 1, 2005 · N272FE · Boeing 727200 · Fuselage Main, Structure
  > TEE FITTING APPROX STA 760-787 RBL 45 IS CORRODED. REMOVED AND REPLACED TEE FITTING IAW SRM 51-30-2
- [SDR 05FDEA01774](https://openairdocs.org/sdr/05FDEA01774.md): Seat Track · corroded · Jul 1, 2005 · N272FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK STA 740-760 LBL 24 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-1.
- [SDR 05FDEA01748](https://openairdocs.org/sdr/05FDEA01748.md): Seat Track · corroded · Jun 30, 2005 · N272FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 24 IS CORRODED 690 - 740. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-30-2
- [SDR 05FDEA01747](https://openairdocs.org/sdr/05FDEA01747.md): Seat Track · corroded · Jun 30, 2005 · N272FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK STA 480 - 690 AT LBL 45 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2
- [SDR 05FDEA01718](https://openairdocs.org/sdr/05FDEA01718.md): Frame · chafed · Jun 28, 2005 · N272FE · Boeing 727200 · Fuselage Main, Frame
  > 344 FRAME CHAFED AT STR'S 4R,6R & 8R. FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 51-40-3
- [SDR 05FDEA01666](https://openairdocs.org/sdr/05FDEA01666.md): Seat Track · corroded · Jun 23, 2005 · N272FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 24 HAS CORROSION FROM STA 344-480. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2.
- [SDR 05FDEA01508](https://openairdocs.org/sdr/05FDEA01508.md): Hydraulic Line · ruptured · Jun 2, 2005 · N272FE · Boeing 727200 · Hydraulic System, Main
  > A-HYD SYSTEM FLUID LOSS / ISOLATED TO -A- PUMP NR 2. AFTER SHUTDOWN, THE -A- SYSTEM QTU. READ 2.5 GALLONS AND THE FLUID SHUTOFF SWITCHES WERE NOT TURNED OFF. OPENED COUPLING AND MOTORED ENGINE. FOUND PRESSURE LINE FROM THE PUMP TO THE FIREWALL RUPTURED.
- [SDR 05FDEA00964](https://openairdocs.org/sdr/05FDEA00964.md): Bushing · loose · Apr 11, 2005 · N272FE · Boeing 727200 · Vertical Stabilizer Miscellaneous Structure
  > BUSHINGS LOOSE ON UPPER CLEVIS FOR THE PCU ROD END. REPAIRED UPPER RUDDER CLEVIS BUSHINGS FOR THE PCU RODEND IAW FED EX EA 7-5530- 86276.
- [SDR 05FDEA00921](https://openairdocs.org/sdr/05FDEA00921.md): Skin · damaged · Apr 10, 2005 · N272FE · Boeing 727200 · Trailing Edge Flaps
  > RIGHT WING O/B MID FLAP UPPER SKIN FWD EDGE IS GOUGED AND BENT AT NR 7 CARRIAGE. REPAIRED RIGHT WING O/B MID FLAP UPPER SKIN FWD EDGE AT NR 7 FLAP CARRIAGE PER EA 7-5710-86274.
- [SDR 05FDEA00920](https://openairdocs.org/sdr/05FDEA00920.md): Rib · chafed · Apr 10, 2005 · N272FE · Boeing 727200 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STAB T/E CAVITY RIB WEB IS CHAFED AT UPPER SURFACE, FIN STA 180, 5 RBL, THROUGH ACCESS PNL 9510. REPAIRED THE CHAFED RIB WEB, VERTICAL STAB T/E CAVITY AT UPPER SURFACE FIN STA 180, 5 RBL IAW FEDEX EA 7-5530-86275.
- [SDR 05FDEA00872](https://openairdocs.org/sdr/05FDEA00872.md): Skin · lightning strike · Apr 6, 2005 · N272FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON CROWN BS 588 BETWEEN STR 1 AND STR 2L. FOUND TO BE OUT OF LIMITS. REPAIRED SKIN IAW FED EX EA 7-5330-866368.
- [SDR 05FDEA00847](https://openairdocs.org/sdr/05FDEA00847.md): Skin · cracked · Apr 5, 2005 · N272FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > CRACKED EXTERNAL SKIN FWD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED CRACK PER FED-EX EA 7-5330-86273.
- [SDR 05FDEA00834](https://openairdocs.org/sdr/05FDEA00834.md): Stringer Clip · corroded · Apr 4, 2005 · N272FE · Boeing 727200 · Fuselage Main, Attach Fittings
  > CORROSION C53-113-01 (1) UNDER LEVELING COMPOUND BS 660 STR 28R. FOUND CORROSION TO BE 100 PERCENT MATERIAL LOSS, REPAIRED DOUBLER, SHEAR TIE PER SRM 53-10-4, 53-30-3.
- [SDR 05FDEA00832](https://openairdocs.org/sdr/05FDEA00832.md): Skin · dented · Apr 4, 2005 · N272FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > DENT IN EXTERNAL FUSELAGE SKIN AT BS 1345 BY LEFT AFT CORNER OF AIRSTAIR CUT OUT. REPAIRED DENT PER SRM 54-30-3.
- [SDR 05FDEA00779](https://openairdocs.org/sdr/05FDEA00779.md): Housing · gouged · Apr 1, 2005 · N272FE · Boeing 727233 · Cargo/Baggage Doors
  > NR 3 LOWER CARGO DOOR, HANDLE HOUSING GOUGED BY HANDLE STUD. REMOVED AND REPLACED #3 LWR CARGO DOOR HANDLE PER SRM 51-30-02.
- [SDR 05FDEA00735](https://openairdocs.org/sdr/05FDEA00735.md): Shear Web · corroded · Mar 31, 2005 · N272FE · Boeing 727233 · Fuselage Main, Structure
  > CORROSION IN SHEAR WEB BS 1166 LBL 29-33 WL 208.
- [SDR 05FDEA00736](https://openairdocs.org/sdr/05FDEA00736.md): Support · corroded · Mar 31, 2005 · N272FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > LWR FUSELAGE, BS 740 R A/C BAY RBL 10, CORROSION EMANATING FROM LWR CHORD AND BULKHEAD. REPAIRED BS470 LOWER CHORD PER FED-EX EA 7-5310-86268.
- [SDR 05FDEA00691](https://openairdocs.org/sdr/05FDEA00691.md): Skin · gouged · Mar 29, 2005 · N272FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN GOUGED AT NR 3 CARGO DOOR CUTOUT, BS 1096 AT STR 24R. REPAIRED GOUGE PER FED-EX EA. 7-5330-86272.
- [SDR 05FDEA00662](https://openairdocs.org/sdr/05FDEA00662.md): Skin · damaged · Mar 28, 2005 · N272FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN HAS FOD/GRAVEL DAMAGE, BS 480-520, STR 22R-27L ALONG BELLY SKIN. RVSM CRITICAL AREA. REPAIRED SKIN BS 496-501 AT STR 27R PER SRM 53-30-3.
- [SDR 05FDEA00635](https://openairdocs.org/sdr/05FDEA00635.md): Bulkhead · corroded · Mar 25, 2005 · N272FE · Boeing 727200 · Fuselage Main, Bulkhead
  > LOWER CHORD OF BS 950 CANTED BULKHEAD IS CORRODED, RBL 23. REPLACED BS 950 LOWER CHORD PER SRM 51-40-3 & 51-30-2.
- [SDR 05FDEA00632](https://openairdocs.org/sdr/05FDEA00632.md): Shear Tie · corroded · Mar 24, 2005 · N272FE · Boeing 727200 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE FWD SIDE AT BS 1030, JUST OB OF STR 28 LT, AFT CARGO BAY. REPAIRED PER SRM 53-10-4.
- [SDR 02FDEA00725](https://openairdocs.org/sdr/02FDEA00725.md): Stringer · dented · Oct 12, 2002 · N272FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > DENT IN STR FLANGE AT BS 492, STR 23L. R&R STR FLANGE PER SRM 53-10-1, 53-10-3.
- [SDR 02FDEA00724](https://openairdocs.org/sdr/02FDEA00724.md): Skin · corroded · Oct 12, 2002 · N272FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN LAP AT SHEAR TIE AT BS 720B, STR 26R. R&R SKIN PER SRM 53-10-5, 51-30-2, 51-30-5.
- [SDR 02FDEA00729](https://openairdocs.org/sdr/02FDEA00729.md): Frame · dented · Oct 12, 2002 · N272FE · Boeing 727200 · Fuselage Main, Frame
  > FRAME DENTED AT BS 500, STR 23R - 24R. R&R FRAME PER SRM 51-40-3.
- [SDR 02FDEA00728](https://openairdocs.org/sdr/02FDEA00728.md): Skin · dented · Oct 11, 2002 · N272FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > DENT ON SKIN AT BS 465 BELOW STR 16R. R&R SKIN PER SRM 53-30-1, 53-30-3.
- [SDR 02FDEA00747](https://openairdocs.org/sdr/02FDEA00747.md): Floorbeam · corroded · Oct 8, 2002 · N272FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION ON TOP OF FLOORBEAM AT BS 344, LBL 45-55, WL 208. R&R UPPER CHORD PER ER 02-1505.
- [SDR 02FDEA00726](https://openairdocs.org/sdr/02FDEA00726.md): Seat Track · corroded · Oct 8, 2002 · N272FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK I/B FLANGE UPR SURFACE AROUND NUTPLATE HOLES AT BS 760-848, LBL 24, WL 208. R&R SEAT TRACK PER SRM 51-30-2.
- [SDR 02FDEA00730](https://openairdocs.org/sdr/02FDEA00730.md): Skin · bulged · Oct 7, 2002 · N272FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > BULGING ON BELLY SKIN BETWEEN BS 1050 TO 1060, LBL 20. R&R SKIN PER SRM 53-30-1, 53-10-1, 53-30-3.
- [SDR 01FDEA00226](https://openairdocs.org/sdr/01FDEA00226.md): Landing Gear · malfunctioned · Mar 23, 2001 · N272FE · Boeing 727233 · Landing Gear Retraction/Extension System
  > LANDING GEAR FAILED TO RETRACT. RAN CKLIST, CK CB AND WAS NOT POPPED, ATTEMPT 2ND RETRACT AND WAS SUCCESSFUL. PERF LG HANDLE LOCK SYS ADJUSTMENT AND TEST PER 727-200 MM 32-31-011-5. CK OK. NO BINDING OR STICKING NOTED DURING ACTUATION.
- [SDR 99FDEA00310](https://openairdocs.org/sdr/99FDEA00310.md): Overheat Sensor · malfunctioned · Aug 4, 1999 · N272FE · Boeing 727233 · Overheat Detection
  > 99-190 - NR 3 ENG STRUT OVERHEAT LIGHT ILLUM. EMERG PROC ACCOMPLISHED. LIGHT REMAIN ILLUM. ENGINE SHUT DOWN. REMOVED AND REPLACED NR 3 ENGINE STRUT OVERHEAT SENSING ELEMENT PER MM 26-14-001-2, RAN ENG PER JET RUN HANDBOOK OPER CK GOOD. NO PNEUMATIC LEAKS
- [SDR 99FDEA00300](https://openairdocs.org/sdr/99FDEA00300.md): Control Unit · failed · Jul 30, 1999 · N272FE · Boeing 727233 · Fire Detection
  > 99-185 - NR 3 ENG STRUT OH LIGHT ILLUMINATED, RAN RED TABS CKLIST. REMOVED AND REPLACED FIRE AND HEAT DETECTION CONTROLLER, PER MM 26-14-000-1. OPS CK GOOD.
- [SDR 97FDEA00751](https://openairdocs.org/sdr/97FDEA00751.md): Floorbeam · coroded · Oct 14, 1997 · N272FE · Boeing 727223 · Fuselage Main, Floor Beam
  > NR 0621 GEN NR 72C237-02, BS 950 FLOORBEAM CAP LBL 45 TO LBL 55 HAS CORROSION ON TOP AND AROUND NUTCLIP HOLES INSTALLED STRAP IN ACCORDANCE WITH EA 7-5310-29241 DATED 10/7/97.
- [SDR 97FDEA00749](https://openairdocs.org/sdr/97FDEA00749.md): Frame · dented · Oct 11, 1997 · N272FE · Boeing 727233 · Fuselage Main, Frame
  > NR 0572, LWR AFT CARGO, DENT IN FRAME 1010 ABOVE STR 25R, CUT OUT DAMAGE. INSTALLED REPAIR PER SRM 53-10-4.
- [SDR 97FDEA00740](https://openairdocs.org/sdr/97FDEA00740.md): Chord · cracked · Oct 10, 1997 · N272FE · Boeing 727233 · Wing Miscellaneous Structure
  > CRACK IN FWD LWR FLANGE OF 2ND CHORD FWD OF RT WING REAR SPAR, INSIDE FUEL CELL AT WS 686.5. INSTALLED DOUBLER PER BOEING SB NR 727-57A159.
- [SDR 97FDEA00739](https://openairdocs.org/sdr/97FDEA00739.md): Chord · mismanufactured · Oct 10, 1997 · N272FE · Boeing 727233 · Wing Miscellaneous Structure
  > RT WING, WS 686.5, AFT SIDE OF 2ND CHORD, FWD OF REAR SPAR HAS AREA WHERE TOO MUCH MATERIAL (TAK). REMOVED NEXT TO DOUBLE FLUSH RIVET. BLENDED OUT AREA PER SRM 51-10-1 PG 2 AND PER SB 727 57A159. ALODINED AND PRIMED PER M/M 51-20-1. INSTALLED REPAIR PER EA
- [SDR 97FDEA00750](https://openairdocs.org/sdr/97FDEA00750.md): Seat Track · corroded · Oct 8, 1997 · N272FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > NR 0643 GEN NR 72C237-02 BS 1015, LBL 25 SEAT TRACK HAS CORROSION BETWEEN LUGS AND ON TOP OF LUGS. REMOVED AND REPLACED OLD SEAT TRACK WITH NEW ONE PER SRM 51-10-1.
- [SDR 97FDEA00700](https://openairdocs.org/sdr/97FDEA00700.md): Skin · damaged · Oct 1, 1997 · N272FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > NR 1 CARGO DOOR CUTOUT BS 600 FUSELAGE SKIN, DOUBLER AND TRIPLER DAMAGED AT LWR CUTOUT. *S/D* INSTALLED DOUBLERS AND FILLER IN CARGO DOOR CUTOUT PER EA 75-330-29236 DATED 10-03-97.
- [SDR 96FDEA00180](https://openairdocs.org/sdr/96FDEA00180.md): Bypass Valve · failed · Feb 3, 1996 · N272FE · Boeing 727233 · Trailing Edge Flap Control System
  > ON LANDING APPROACH, O/B FLAPS DIDN'T EXTEND WITH FLAP HANDLE, I/B FLAPS OKAY. SUBSEQUENT SYSTEM-A HYD HAD TOTAL LOSS. CHECKLIST, M/GAR EXTENSION AND LANDED OKAY. FOUND O/B TRAILING EDGE BYPASS VALVE BODY SEPARATED. REMOVED AND REPLACED VALVE, LEAK CHECKS
- [SDR 95FDEA01594](https://openairdocs.org/sdr/95FDEA01594.md): Apu · fire · Oct 25, 1995 · N272FE · Boeing 727233 · Airborne Auxiliary Power Unit (APU) System
  > GROUND CREW REPORTED, APU W/N LIGHT OFF OR SHUTDOWN, RESIDUAL FUEL IGNITED CAUSING FIRE AND FIRE BOTTLE DISCHARGED. STARTED APU 3 TIMES, OPS CK GOOD. APU SHUTDOWN NORMALLY WITH MASTER SW OR FIRE HANDLE. SUSPECT NO LIGHT ON APU WAS CAUSED BY COLD SOAKED APU.

## 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 = 'N272FE' AND deregistration_id = 'N272FE-2007-11-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N272FE-2007-11-28/reports

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