# Service difficulty reports: N271FE, cancelled Apr 25, 2013

A list on [N271FE, cancelled Apr 25, 2013](https://openairdocs.org/deregistered/N271FE-2013-04-25.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 2 · 66 reports

- [SDR 08FDEA03050](https://openairdocs.org/sdr/08FDEA03050.md): Sensor · failed · Jul 24, 2008 · N271FE · Boeing 727233 · Landing Gear Retraction/Extension System
  > LANDING LEVER HANDLE FAILED TO MOVE PAST THE OFF POSITION. FOLLOWED QRH PROCEDURES AND IT FAILED TEST NR 1. REINSTALLED GROUND SENSE LOWER LINK TO SCISSORS LT GEAR, PER SMP AND SAFETIED BOLT. REMOVED AND REPLACED AIR SAFETY SENSOR IAW M/M 32-09-221-4. PE
- [SDR 08FDEA03019](https://openairdocs.org/sdr/08FDEA03019.md): Landing Gear · malfunctioned · Jul 22, 2008 · N271FE · Boeing 727233 · Landing Gear Retraction/Extension System
  > ON DEPARTURE, LANDING GEAR FAILED TO RETACT. COULD NOT RAISE HANDLE PAST OFF. PULLED LATCH AND AURAL C/B'S, STILL COULD NOT RAISE HANDLE PAST OFF POSITION. SYSTEM FAILED EXTENSION TEST, PER RED TABS DID NOT ATTEMPT TO USE LEVER LATCH TRIGGER.
- [SDR 07FDEA00090](https://openairdocs.org/sdr/07FDEA00090.md): Transceiver · failed · Jan 12, 2007 · N271FE · Boeing 727233 · Weather Radar System
  > WEATHER RADAR INDICATOR DISPLAYS "FAIL" WITH "T/R". DISPLAYED IN GREEN-YELLOW-RED UNDER THE WORD "TEST". REMOVED AND REPLACED WEATHER RADAR R/T REF B727-200 AMM 34-41-041-4. WEATHER RADAR SYSTEM TESTS OK NOW REF B727-200 AMM 34-41-000-5. PREMATURE REMOVAL/
- [SDR 06FDEA2676](https://openairdocs.org/sdr/06FDEA2676.md): Stiffener · cracked · Jul 24, 2006 · N271FE · Boeing 727233 · Fuselage Main, Keel
  > FOUND VERTICAL STIFFNER IN RIGHT WHEEL WELL FOR KEEL BEAM CRACKED.
- [SDR 05FDEA01034](https://openairdocs.org/sdr/05FDEA01034.md): Support Beam · damaged · Apr 16, 2005 · N271FE · Boeing 727200 · Wing, Landing Gear Attach Fittings
  > COMPLY WITH EA 7-5710-55479 WINGS - RT MLG SUPPORT BEAM PANEL ATTACH HOLE OVERSIZED. COMPLIED WITH EA 7-5710-55479.
- [SDR 05FDEA01033](https://openairdocs.org/sdr/05FDEA01033.md): Stop · missing · Apr 16, 2005 · N271FE · Boeing 727200 · Flight Compartment Equipment
  > COMPLY WITH EA 7-2510-55477 REPLACEMENT OF MISSING DOOR STOP. COMPLIED WITH EA 7-2510-55477.
- [SDR 05FDEA01032](https://openairdocs.org/sdr/05FDEA01032.md): Insulation · torn · Apr 16, 2005 · N271FE · Boeing 727200 · Cargo Compartments
  > COMPLY WITH EA 7-2580-81688 EQUIPMENT FURNISHINGS INSULATION BLANKETS PARTIAL REPLACEMENT STA 310-1183 MAIN CABIN COMPARTMENT. COMPLIED WITH EA 7-2580-81688.
- [SDR 05FDEA01031](https://openairdocs.org/sdr/05FDEA01031.md): Insulation · worn · Apr 16, 2005 · N271FE · Boeing 727200 · Cargo Compartments
  > COMPLY WITH EA 8-7-2580-81688 EQUIPMENT FURNISHINGS INSULATION BLANKETS PARTIAL REPLACEMENT STA 310-1183 MAIN CABIN COMPARTMENT. COMPLIED WITH EA 7-2580-81688.
- [SDR 05FDEA01030](https://openairdocs.org/sdr/05FDEA01030.md): Insulation · worn · Apr 16, 2005 · N271FE · Boeing 727200 · Cargo Compartments
  > COMPLY WITH EA 8-7-2580-81688 EQUIPMENT FURNISHINGS INSULATION BLANKETS PARTIAL REPLACEMENT STA 310-1183 MAIN CABIN COMPARTMENT.
- [SDR 05FDEA01025](https://openairdocs.org/sdr/05FDEA01025.md): Skin Panel · cracked · Apr 15, 2005 · N271FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > C/W EA 7-5330-55466 FUSELAGE SKIN - CRACK REPAIR AT BS 1106, NR 3 LWR CARGO DOOR. COMPLIED WITH EA 7-5330-55466 FUSELAGE SKIN - CRACK REPAIR AT BS 1106, NR 3 CARGO DOOR.
- [SDR 05FDEA01024](https://openairdocs.org/sdr/05FDEA01024.md): Support Fitting · cracked · Apr 15, 2005 · N271FE · Boeing 727200 · Spoilers
  > LEFT WING, T/E NR 5 SPOILER CENTER HINGE SUPPORT FITTING CRACKED. REMOVED AND INSTALLED THE NR 5 SPOILER PANEL IAW MM 27-61-001-4. REMOVED THE OLD CRACKED SUPPORT FITTING IAW MM 51-30-2. LOCATED, DRILLED AND INSTALLED NEW SUPPORT FITTING IAW MM 51-30-2. CO
- [SDR 05FDEA00895](https://openairdocs.org/sdr/05FDEA00895.md): Seat Track · corroded · Apr 7, 2005 · N271FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK STA 480 TO 690, LBL 45 HAS CORROSION AND EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED SEAT TRACK IAW SRM 51-30-2. NEW SEAT TRACK FABBED ON TRAVELER T5/512298, CUT OUT SECTION OF TRACK AT 480 - 510 IAW SRM 53-10-5 FIG
- [SDR 05FDEA00894](https://openairdocs.org/sdr/05FDEA00894.md): Seat Track · damaged · Apr 7, 2005 · N271FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPT SEAT TRACK FS 1160 - 1183 HAS DAMAGED AREAS ALONG BL 0. REMOVED & REPLACED SEAT TRACK SECTION STA 1138 - 1183 BL 0 IAW SRM 51-30-2. NEW TRACK FABBED ON TRAVELER T5/503663.
- [SDR 05FDEA00883](https://openairdocs.org/sdr/05FDEA00883.md): Seat Track · damaged · Apr 6, 2005 · N271FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BL 0, STA 510 HAS AN EXISTING REPAIR THAT INTERFERES WITH THE INSTALLATION OF MOD PARTS PER 7-5340-7-5002. REMOVED SEAT TRACK DAMAGED FROM STA 480 TO 600 IAW SRM 51-30-2. SCALLOPED NEW SEAT TRACK IAW SRM 51-30-5. TREATED AND PRIMED TRACK IAW SR
- [SDR 05FDEA00882](https://openairdocs.org/sdr/05FDEA00882.md): Seat Track · damaged · Apr 6, 2005 · N271FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPT SEAT TRACK FS 1110 - 1130, BL 0, HAS DAMAGED AREAS. REMOVED DAMAGED AREA ON SEAT TRACK IAW SRM 53-10-1 FIG 3 DETAIL 6. RE-EVALUATED AREA FOUND TO BE OUT OF LIMIT IAW SRM 53-10-1 FIG 3 DETAIL 6. REMOVED FASTENER ON LOWER LEG OF SEAT TRACK
- [SDR 05FDEA00881](https://openairdocs.org/sdr/05FDEA00881.md): Seat Track · corroded · Apr 6, 2005 · N271FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > MC DECK SEAT TRACK RBL 24 BETWEEN STA 720E TO 8 INCHES AFT OF 720F CORROSION AND HAS EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER EO 7-5340-7-5002. REMOVE SEAT TRACK IAW SRM 51-30-02, SEAT TRACK FABRICATED ON TRAVELER T5/506089 PER SRM 53-10-02 / 53-10
- [SDR 05FDEA00645](https://openairdocs.org/sdr/05FDEA00645.md): Seat Track · corroded · Mar 25, 2005 · N271FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK STA 344-480 RBL 45 IS CORRODED AND REQUIRES REPLACEMENT PER EO 7-5340-7- 5002. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2.
- [SDR 05FDEA00629](https://openairdocs.org/sdr/05FDEA00629.md): Seat Track · corroded · Mar 22, 2005 · N271FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, STA. 344 - 480, LBL 24 HAS CORROSION AND EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-2 - MAT ID BAC 1520-792 IAW SRM 51-10-2 FIG 7. NEW EXTRUSION SCALLOPED ON TRAV NR T5/501341.
- [SDR 02FDEA00188](https://openairdocs.org/sdr/02FDEA00188.md): Switch · failed · Mar 7, 2002 · N271FE · Boeing 727233 · Engine Oil Quantity
  > 02-63 #2 ENG LOW OIL PRESS FILTER BYPASS ILLUMINATED. #2 ENG SHUTDOWN. R&R LOW OIL PRESS SW PER MM 79-33-002-4. OPS CK OK.
- [SDR 01FDEA00492](https://openairdocs.org/sdr/01FDEA00492.md): Control Unit · faulty · Jun 23, 2001 · N271FE · Boeing 727233 · Fire Detection
  > ON APPROACH NR 1 FIRE HANDLE ILLUM AND FIRE WARN BELL SOUNDED. THE THROTTLES WERE AT FLT IDLE. REPEAT WRITE UP. FIRE WARNING 1-2 SEC. *S/D* REMOVED AND REPLACED NR 1 CONTROL UNIT AND NR 1 STRUT FIREWALL LOOP AS PRECAUTIONARY SYS PER MM 26-11-012-4 & 26-11
- [SDR 01FDEA00493](https://openairdocs.org/sdr/01FDEA00493.md): Warning System · malfunctioned · Jun 23, 2001 · N271FE · Boeing 727233 · Landing Gear Position and Warning
  > 01-208 AFT T/O RT MLG DOOR ILLUM ON 2ND OFF PANEL ALONG WITH THE RED DOORS WHEN HANDLE PLACED IN OFF POS. AFTER CYCLED GEAR BOTH LIGHTS EXTINGUISHED. UNABLE TO DUPLICATE. REMOVED AND REPLACED MAIN LANDING GEAR DOOR WARNING SWITCH PRECAUTIONARY. OPS CK GOOD
- [SDR 01FDEA00471](https://openairdocs.org/sdr/01FDEA00471.md): Control Unit · faulty · Jun 20, 2001 · N271FE · Boeing 727233 · Fire Detection
  > NR 1 ENG FIRE LIGHT ILLUM ON LAND ALONG WITH BELL AND MASTER FIRE LIGHT ENG FIRE CKLIST ACCOMP. REMOVED AND REPLACED NR 1 FIRE DETECTION CONTROL UNIT. TEST GOOD PER 727 MM 26-11-001-5. INSP FIRE LOOPS NO DAMAGE NOTED. FOUND BLD AIR LINE LOOSE AT VALVE. TI
- [SDR 01FDEA00460](https://openairdocs.org/sdr/01FDEA00460.md): Hydraulic System · broken · Jun 16, 2001 · N271FE · Boeing 727233 · Hydraulic System, Main
  > 01-195 DUR DESCENT HYD SYS A FLUID LEVEL 1.2 GAL. FOLLOWED PROC & CKLIST. TURN OFF SPOILERS. LEAK STOPPED. UPON LOWERING FLAPS & GEAR, FLUID LEVEL DROPPED TO 0. SAFETY WIRE FOR ALT FLAPS SWITCH & GPWS OVERRIDE SWITCH BROKEN DUR PROCEDURE. ** S/D ** R&R LMG
- [SDR 00FDEA00446](https://openairdocs.org/sdr/00FDEA00446.md): Fan · failed · Jul 12, 2000 · N271FE · Boeing 727233 · Air Distribution System
  > DISTINCT ODOR (LIKE PAPER BURNING), NO SMOKE DETECTED. SMOKE CONTROL SYS ACTIVATED WITH LWR CARGO SYS USED. FOUND GASPER FAN MOTOR BURNT. GASPER FAN POPS BREAKER AND WILL NOT RESET.
- [SDR 00FDEA00409](https://openairdocs.org/sdr/00FDEA00409.md): Floorbeam · corroded · Jun 26, 2000 · N271FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION BS 480 FLOORBEAM UPPER CHORD AROUND NUTPLATE HOLES AT RBL 11 & LBL 28, LOWER SURFACE OF CHORD, WL 208. R&R PER FEDEX SRM 51-10-6, 53-10-1.
- [SDR 00FDEA00408](https://openairdocs.org/sdr/00FDEA00408.md): Seat Track · corroded · Jun 26, 2000 · N271FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > NR 446 CORROSION ON LONGITUDINAL BEAM AND SEAT TRACK AT BS 846 TO BS 760, WL 208, RBL 45. ** S/D ** R&R CORROSION PER FEDEX SRM 51-30-2.
- [SDR 00FDEA00407](https://openairdocs.org/sdr/00FDEA00407.md): Skin · gouged · Jun 23, 2000 · N271FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > GOUGE IN EXTERIOR FUSELAGE SKIN BS 691 JUST BELOW STR 25 RT. R&R PER FEDEX SRM 53-30-3 FIG 1.
- [SDR 00FDEA00385](https://openairdocs.org/sdr/00FDEA00385.md): Skin · gouged · Jun 13, 2000 · N271FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > GOUGE IN FUSELAGE EXTERIOR SKIN BS 480, BETWEEN STR 2 AND 23 RT. R&R PER FEDEX SRM 53-30-3.
- [SDR 00FDEA00389](https://openairdocs.org/sdr/00FDEA00389.md): Skin · corroded · Jun 13, 2000 · N271FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > CORROSION BS 720E, PRESSURE NUT PLATE IS CORRODED. STR 19 RT EXTERNAL SKIN. R&R PER FEDEX SRM 53-30-3 FIG 5.
- [SDR 00FDEA00384](https://openairdocs.org/sdr/00FDEA00384.md): Floorbeam · corroded · Jun 13, 2000 · N271FE · Boeing 727233 · Fuselage Main, Floor Beam
  > NR 456 CORROSION ON FLOORBEAM BS 680, WL 208, BL0 - LBL 25. ** S/D ** R&R UPPER FLANGE PER FEDEX SRM 53-10-8 FIG 3.
- [SDR 00FDEA00388](https://openairdocs.org/sdr/00FDEA00388.md): Floorbeam · corroded · Jun 13, 2000 · N271FE · Boeing 727233 · Fuselage Main, Floor Beam
  > NR 402 CORROSION AROUND NUT CLIP HOLES LOWER CHORD BS 1130 FLOORBEAM LBL 1 - LBL 38, WL 200. ** S/D ** R&R CORROSION PER IAW FEDEX EA 7-5310-52109 & FEDEX MM 51-20-151.
- [SDR 99FDEA00499](https://openairdocs.org/sdr/99FDEA00499.md): Switch · failed · Dec 8, 1999 · N271FE · Boeing 727233 · Landing Gear Position and Warning
  > RT MAIN DOOR LIGHT STAY ON WITH GEAR HANDLE IN OFF POS. REMOVED AND REPLACED RT MAIN GEAR DOOR LOCK SWITCH PLUG (D752) PER STAND MAINT PRACT AND REF WIRING DIAGRAM MANUAL 32-62-01. OPER CK WARN SWITCH REF MM 32-62-011-5. OPER CK NORM. OK FOR SERVICE.
- [SDR 98FDEA00149](https://openairdocs.org/sdr/98FDEA00149.md): Skin · cracked · Feb 25, 1998 · N271FE · Boeing 727233 · Leading Edge Devices
  > RT WING NR 8 L/E SLAT, LOWER SKIN TANG BELOW INBD TRACK ATTACH CRACKED AND RIVETS PULLED. ACCOMPLISHED REPAIR ON RT WING NR 8 L/E SLAT FOR CRACKED LWR SKIN TANG BELOW INBOARD TRACK PER AA 7-5750-29381 AND AA SRM 57-50-1 PGS 7A AND 7B.
- [SDR 98FDEA00128](https://openairdocs.org/sdr/98FDEA00128.md): Frame · damaged · Feb 23, 1998 · N271FE · Boeing 727233 · Fuselage Main, Frame
  > LOWER LOBE AFT CARGO BS 1130 FRAME DAMAGED BELOW LT EDGE SUPPORT PANEL ON TOP ANGLE BETWEEN STR 27L TO 28L. INSTALLED DOUBLER PER SRM 53-10-4.
- [SDR 98FDEA00127](https://openairdocs.org/sdr/98FDEA00127.md): Stiffener · cracked · Feb 23, 1998 · N271FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > LOWER LOBE AFT CARGO, BS 1183 BULKHEAD LOWER END OF VERTICAL STIFFENER AT RBL 8.0 CRACKED IN I/B RADIUS (INITIAL CRACK LENGTH 1.875.). INSTALLED RBL 8 VERTICAL BEAM MODIFICATION AND REPAIR PER S/B 53-175R2, AD 90-06-09 AND DRAWING 65C29080 GN7.
- [SDR 98FDEA00126](https://openairdocs.org/sdr/98FDEA00126.md): Frame · damaged · Feb 23, 1998 · N271FE · Boeing 727233 · Fuselage Main, Frame
  > LOWER LOBE AFT CARGO BS 1110 FRAME DAMAGED BELOW LT EDGE SUPPORT PNL, ON TOP ANGLE, BETWEEN STR 27L TO 28L. REMOVED DAMAGED AND INSTALLED DOUBLER PER SRM 53-10-4.
- [SDR 98FDEA00129](https://openairdocs.org/sdr/98FDEA00129.md): Skin · gouged · Feb 13, 1998 · N271FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > UPPER LOBE, FUSE CROWN SKIN GOUGED AT BS 1050 BETWEEN STRINGER 3L TO 4L. TRIMMED OUT DAMAGED AREA. INSTALLED EXTERNAL REPAIR DOUBLER PER SRM 53-30-3.
- [SDR 96FDEA00461](https://openairdocs.org/sdr/96FDEA00461.md): Position Switch · out of adjust · Mar 8, 1996 · N271FE · Boeing 727233 · Leading Edge Slat Control System
  > ON DEPARTURE WHEN FLAPS RETRACTED TO 2 DEGREES, THE NR 2 LEADING EDGE DEVICE REMAINED EXTENDED. WHEN FLAPS WERE RETURNED TO 5 DEGREES THE LEADING EDGE DEVICES WERE NORMAL. C/A: FOUND NR 2 LEADING EDGE FLAP POSITION SWITCH OUT OF ADJUSTMENT. ADJUSTED NR 2 F
- [SDR 96FDEA00179](https://openairdocs.org/sdr/96FDEA00179.md): Uplock Sensor · malfunctioned · Feb 1, 1996 · N271FE · Boeing 727233 · Landing Gear Position and Warning
  > RT GEAR UNSAFE RED LIGHT ON AFTER GEAR RETRACTION. RECYCLED GEAR, LIGHT REMAINED ON WITH DOOR LIGHT OUT. INSTALLED RT MAIN GEAR UPLOCK SENSOR PER MM 32-61-81, OPS CHECK NORMAL. REPLACED LANDING GEAR ACCESSORY UNIT, MODULE TESTED NORMAL PER 32-09-121.
- [SDR 95FDEA01257](https://openairdocs.org/sdr/95FDEA01257.md): Floorbeam · corroded · Sep 5, 1995 · N271FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (71C709-02), ON LOWER FLANGE OF FLOORBEAM AT BS 1070 RBL 7 WL 200. CORROSION WAS FOUND TO BE OUT OF LIMITS ON LOWER FLANGE OF FLOORBEAM AT BS 1070, RBL 1 TO 16 AND RBL 50, PER FEDEX SRM 53-10-1. REPAIRED LOWER FLANGE OF FLOORBEAM AT BS 1070 LBL 27
- [SDR 95FDEA01256](https://openairdocs.org/sdr/95FDEA01256.md): Skin · gouged · Sep 5, 1995 · N271FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > LWR 46 SECTION SKIN IS SEVERELY GOUGED AND NICKED, REQUIRING REPLACEMENT OF SKIN PANEL FROM BS 950 TO 1010, STR 26 LT AND RT. SKIN IS OUT OF LIMITS PER FEDEX SRM. REMOVED DAMAGED SKIN AND INSTALLED NEW AT BS 950 TO 1010 STR 25 LT AND RT, IAW FEDEX SRM 51-30-
- [SDR 95FDEA01255](https://openairdocs.org/sdr/95FDEA01255.md): Skin · gouged · Sep 5, 1995 · N271FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > LOWER 46 SECTION SKIN IS SEVERELY GOUGED AND NICKED, REQUIRING REPLACEMENT OF SKIN PANEL FROM 1010 TO 1183 STR 26 LT AND RT. SKIN IS OUT OF LIMITS PER FEDEX SRM. REMOVED DAMAGED SKIN AND REPLACED WITH NEW AT STA 1010 TO 1183 STR 26 LT AND RT, IAW FEDEX SRM 5
- [SDR 95FDEA01254](https://openairdocs.org/sdr/95FDEA01254.md): Skin · gouged · Sep 5, 1995 · N271FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN PANEL IS SEVERELY NICKED AND GOUGED FROM BS 1010 TO 1090 STR 20 TO 26R, REQUIRING REPLACEMENT OF PANEL. SKIN IS OUT OF LIMITS PER FEDEX SRM. REMOVED DAMAGED SKIN AND REPLACED WITH NEW AT STA 1010 TO 1183 STR 20 TO 26R, IAW FEDEX SRM 51-30-2, BA
- [SDR 95FDEA01222](https://openairdocs.org/sdr/95FDEA01222.md): Skin · damaged · Aug 30, 1995 · N271FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > WHILE WORKING NR 0412, FOUND LIGHTNING STRIKES AND DEEP GOUGES TO BE OUT OF LIMITS AT BS 490 STR 27R WL 149. REPAIRED DAMAGE AT BS 490 STR 27R WL 149, PER FEDEX SRM 53-30-3.
- [SDR 95FDEA01210](https://openairdocs.org/sdr/95FDEA01210.md): Floorbeam · corroded · Aug 28, 1995 · N271FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (72C237-02), ON TOP CHORD OF BS 1030 FLOORBEAM RBL 9 TO 22 LBL 51.5 WL 208. MECHANICALLY REMOVED CORROSION FROM TOP CHORD OF FLOORBEAM AT BS 1030 RBL 9 TO 22 LBL 51.5 AREA WAS OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED TOP CHORD OF FLOORBEAM AT
- [SDR 95FDEA01209](https://openairdocs.org/sdr/95FDEA01209.md): Floorbeam · corroded · Aug 28, 1995 · N271FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION ON TOP CHORD OF BS 1110 FLOORBEAM RBL 8 TO 55 LBL 47 TO 55 WL 208. MECHANICALLY REMOVED CORROSION FROM TOP CHORD OF FLOORBEAM AT BS 1110 RBL 8 LBL 55 WL 208. TOP CHORD WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED AND REPLACED TOP
- [SDR 95FDEA01208](https://openairdocs.org/sdr/95FDEA01208.md): Skin · lightning strike · Aug 28, 1995 · N271FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > BS 620 STR 24R AND 25R THERE IS A LIGHTNING STRIKE ON EXTERIOR SKIN. BLENDED OUT LIGHTNING STRIKE, FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 53-30-1. CUT OUT DAMAGE, INSTALLED REPAIR DOUBLER AND FILLER, ALL WORK WAS DONE IAW FEDEX SRM 53-30-3, 53-30-1.
- [SDR 95FDEA01207](https://openairdocs.org/sdr/95FDEA01207.md): Gate Beam · cracked · Aug 28, 1995 · N271FE · Boeing 727233 · Passenger/Crew Doors
  > FWD ENTRY DOOR LOWER GATE BEAM IS CRACKED AT FWD CORNER STOP FITTING, APPROX 1 INCH LENGTH. REPAIRED CRACK IN FWD ENTRY DOOR LOWER GATE BEAM IAW FEDEX EA 7-3210-25602.
- [SDR 95FDEA01211](https://openairdocs.org/sdr/95FDEA01211.md): Floorbeam · corroded · Aug 26, 1995 · N271FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION ON TOP CHORD OF FLOORBEAM BS 1070 AT LBL 13 LBL 47.5 TO 54 RBL 15 TO 52 WL 208. CUT OUT DAMAGED UPPER CHORD OF FLOORBEAM FROM LBL 65 RBL 65 AND REPAIRED PER SRM 53-10-08 FIG 3.
- [SDR 95FDEA01196](https://openairdocs.org/sdr/95FDEA01196.md): Doubler · gouged · Aug 24, 1995 · N271FE · Boeing 727233 · Cargo/Baggage Doors
  > MAIN CARGO DOOR SIDE FRAME IS GOUGED ON AFT LOWER FRAME. REPAIRED MAIN CARGO AFT LOWER SIDE FRAME IAW FEDEX SR 27-52-009.

Next page: https://openairdocs.org/deregistered/N271FE-2013-04-25/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 = 'N271FE' AND deregistration_id = 'N271FE-2013-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N271FE-2013-04-25/reports

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