# Service difficulty reports: N271FL, cancelled Mar 20, 2003

A list on [N271FL, cancelled Mar 20, 2003](https://openairdocs.org/deregistered/N271FL-2003-03-20.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 3 · 108 reports

- [SDR F3LA200200357](https://openairdocs.org/sdr/F3LA200200357.md): Cargo Track · corroded · Oct 22, 2002 · N271FL · Boeing 7372L9 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C 2 CHECK, CORROSION WAS FOUND IN THE CARGO TIE DOWN TRACK AT LBL 17, WL 157, BS 813. TIE DOWN TRACK WAS REPLACED IAW SRM 53-10-05 AND SRM 51-10-02.
- [SDR F3LA200200353](https://openairdocs.org/sdr/F3LA200200353.md): Structure · cracked · Oct 21, 2002 · N271FL · Boeing 7372L9 · Cargo/Baggage Doors
  > DURING C 2 CHECK, THE FORWARD CARGO DOOR, LOWER CORNER, WAS FOUND TO HAVE A CRACK. THE CRACK WAS REPAIRED USING SB 737-52A1100 AND COMPLIED WITH THE REQUIREMENTS OF AD 2000-07-06 UNDER ENGINEERING REQUEST 02-1333
- [SDR F3LA200200346](https://openairdocs.org/sdr/F3LA200200346.md): Skin · cracked · Oct 8, 2002 · N271FL · Boeing 7372L9 · Wing, Plate/Skin
  > DURING C-2 CHECK, INSPECTION REPORTED LT WING FIXED LE CRACKED ON INBD SIDE OF NR 2 SLAT, INBD AUX TRACK CUTOUT. REPAIRED CRACK PER SRM 57-20-L1 AND MM 51-21-021.
- [SDR F3LA200200345](https://openairdocs.org/sdr/F3LA200200345.md): Floorbeam · corroded · Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Main, Floor Beam
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM, BS 813, RBL 8, WL 157. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-5 AND 51-30-02.
- [SDR F3LA200200344](https://openairdocs.org/sdr/F3LA200200344.md): Skin · cracked · Oct 8, 2002 · N271FL · Boeing 7372L9 · Galley Doors
  > DURING C-2 CHECK, INSPECTION REPORTED FWD GALLEY DOOR INNER DOOR SKIN CRACKED AT ATTACH RIVET, FWD EDGE, CENTER SPAN. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-30-02, 51-10-02 AND 51-21-0.
- [SDR F3LA200200343](https://openairdocs.org/sdr/F3LA200200343.md): Floorbeam · corroded · Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Main, Floor Beam
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOOR BEAM, BS 813, LBL 8, WL 157. REPAIRED DAMAGED AREA PER SRM 53-10-1 AND 53-10-5.
- [SDR F3LA200200342](https://openairdocs.org/sdr/F3LA200200342.md): Floorbeam · corroded · Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Main, Floor Beam
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM, BS 813, LBL 12, WL 157. FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 53-10-5 AND 51-30-02.
- [SDR F3LA200200341](https://openairdocs.org/sdr/F3LA200200341.md): Strap · corroded · Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOORBOARD SPLICE STRAP, BS 772, WL 157. REPLACED STRAP PER SRM 51-30-2.
- [SDR F3LA200200340](https://openairdocs.org/sdr/F3LA200200340.md): Strap · corroded · Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SPLICE, BS 504, WL 155. REPLACED STRAP PER SRM 51-30-02.
- [SDR F3LA200200339](https://openairdocs.org/sdr/F3LA200200339.md): Clip · damaged · Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED SHEARED RIVETS ON SUB THRESHOLD "T" CLIP, BS 440, RBL 16. REPLACED "T" CLIP PER SRM 51-30-02.
- [SDR F3LA200200337](https://openairdocs.org/sdr/F3LA200200337.md): Support · corroded · Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 786, RBL 21, WL 157. REPLACED SIDEWALL SUPPORT PER SRM 51-30-02, FIG. 1, AND SRM 51-30-02, FIG. 9.
- [SDR F3LA200200338](https://openairdocs.org/sdr/F3LA200200338.md): Support · corroded · Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR TO SIDEWALL SUPPORT, BS 500A - BS 520, RBL 25, WL 156. FABRICATED AND INSTALLED REPLACEMENT SIDEWALL SUPPORT PER SRM 53-10-1, 53-10-2. 51-21-21 AND 51-30-2.
- [SDR F3LA200200336](https://openairdocs.org/sdr/F3LA200200336.md): Frame · corroded · Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Main, Frame
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FRAME AT BS 747, RBL 6, WL 148. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-4, 53-10-1 AND 51-30-02.
- [SDR F3LA200200335](https://openairdocs.org/sdr/F3LA200200335.md): Structure · cracked · Oct 8, 2002 · N271FL · Boeing 7372L9 · Passenger/Crew Doors
  > DURING C-2 CHECK, INSPECTION REPORTED FWD ENTRY DOOR AFT LOWER THRESHOLD CRACKED AT FWD EDGE. REPAIRED PER SRM 52-30-3 AND BOEING DRAWING 65-02938.
- [SDR F3LA200200333](https://openairdocs.org/sdr/F3LA200200333.md): Skin · cracked · Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Main, Plate/Skin
  > DURING C-2 CHECK, INSPECTION REPORTED CRACKED SKIN AT AFT ENTRY DOOR CUTOUT FWD LOWER CORNER, APPROX.25 INCH IN LENGTH. REPAIRED PER SRM 53-30-3, FIGURE 24.
- [SDR F3LA200200334](https://openairdocs.org/sdr/F3LA200200334.md): Skin · cracked · Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Main, Plate/Skin
  > DURING C-2 CHECK, INSPECTION REPORTED FWD SERVICE DOOR CUTOUT SKIN CRACKED AT AFT LOWER CORNER. REPAIRED SKIN PER SRM 53-30-3.
- [SDR F3LA200200364](https://openairdocs.org/sdr/F3LA200200364.md): Stringer · corroded · Sep 29, 2002 · N271FL · Boeing 7372L9 · Fuselage Main, Structure
  > DURING C 2 CHECK, CORROSION WAS FOUND ON THE STRINGER AT STA 520, STR 26L.THE STRINGER WAS REPAIRED BY REMOVING THE DAMAGED SECTION BETWEEN STA 510 AND 540 AT STR 26L. NEW PARTS WERE FABRICATED AND INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-10-3,
- [SDR F3LA200200349](https://openairdocs.org/sdr/F3LA200200349.md): Skin · corroded · Sep 29, 2002 · N271FL · Boeing 7372L9 · Fuselage Main, Structure
  > DURING C 2 CHECK, CORROSION WAS FOUND ON THE SKIN AT BS 470, ON THE EXTERIOR, UNDER THE DME ANTENNAE. REPAIR WAS PERFORMED IN ACCORDANCE WITH SRM 53-30-3, FIGURE 2
- [SDR F3LA200200256](https://openairdocs.org/sdr/F3LA200200256.md): Sensing Element · faulty · Aug 29, 2002 · N271FL · Boeing 7372L9 · Fire Detection
  > AIR TURNBACK. FLIGHT CREW REPORTED NR 2 FIRE WARNING BELL SOUNDED AND LIGHT ILLUMINATED. LIGHT EXTINGUISHED WITH THRUST REDUCED TO IDLE. ALL ENGINE INDICATIONS APPEARED NORMAL. REPLACED NR 2 ENGINE UPPER FIRE SENSING ELEMENT. REMOVED PLACARD.
- [SDR F3LA200200255](https://openairdocs.org/sdr/F3LA200200255.md): Connector · dirty · Aug 24, 2002 · N271FL · Boeing 7372L9 · Fire Detection
  > AIR TURNBACK. FLIGHT CREW REPORTED NR 2 FIRE WARNING HANDLE ILLUMINATED MOMENTARILY ON THREE OCCASIONS DURING DEPARTURE. CLEANED CONNECTORS A AND B ON LOWER FIRE DETECTOR ELEMENT AND CHECKED OKAY.
- [SDR F3LA200200254](https://openairdocs.org/sdr/F3LA200200254.md): Module · malfunctioned · Aug 24, 2002 · N271FL · Boeing 7372L9 · Fire Detection
  > AIR TURNBACK. FLIGHT CREW REPORTED NR 2 ENGINE FIRE WARNING ILLUMINATED APPROXIMATELY 5 MINUTES AFTER TAKEOFF. FIRE WARNING WENT OUT WHEN THRUST REDUCED, ALL INDICATIONS NORMAL. WHEN MORE THRUST ADDED, FIRE WARNING ILLUMINATED AGAIN. REDUCED THRUST TO IDLE
- [SDR F3LA200100132](https://openairdocs.org/sdr/F3LA200100132.md): Odor · detected · Nov 30, 2001 · N271FL · Boeing 7372L9 · Air Distribution System
  > UPON DEPARTURE FROM ABQ, FLIGHT CREW REPORTED STRONG PULL TO THE RIGHT JUST AFTER TAKEOFF THRUST WAS SET. FULL LEFT RUDDER WITH A LITTLE TILLER STRAIGHTENED THE AIRCRAFT OUT AND CONTINUED TAKEOFF ROLL, WHICH APPEARED NORMAL. ALSO REPORTED A STRONG BURNING RU
- [SDR F3LA200100](https://openairdocs.org/sdr/F3LA200100.md): Odor · detected · Nov 30, 2001 · N271FL · Boeing 7372L9 · Air Distribution System
  > UPON DEPARTURE FROM ABQ, FLIGHT CREW REPORTED A STRONG PULL TO THE RIGHT JUST AFTER TAKEOFF THRUST WAS SET. FULL LEFT RUDDER WITH A LITTLE TILLER STRAIGHTENED THE AIRCRAFT OUT. CONTINUED TAKEOFF ROLL WHICH APPEARED NORMAL. AT GEAR RETRACTION, A STRONG BURNI
- [SDR F3LA200100124](https://openairdocs.org/sdr/F3LA200100124.md): Controller · failed · Nov 14, 2001 · N271FL · Boeing 7372L9 · Cabin Temperature Controller
  > AIR TURN BACK. FLIGHT CREW REPORTED LOUD RUMBLE NOISE NEAR RT. PACK, ASSOCIATED WITH STRONG SMELL. TURNED PACK AND RT. BLEED OFF AND SMELL AND NOISE WENT AWAY. LOW VIBRATION CONTINUED. MAINTENANCE RAN RT. PACK AND COULD NOT DUPLICATE DISCREPANCY. OPENED PA
- [SDR F3LA200100114](https://openairdocs.org/sdr/F3LA200100114.md): Actuator · failed · Oct 22, 2001 · N271FL · Boeing 7372L9 · Drag Control Actuator
  > UPON ARRIVAL, FLIGHT CREW REPORTED "A" SYSTEM HYDRAULIC QUANTITY AND PRESSURE FELL TO ZERO AFTER LANDING. REPLACED NO. 8 GROUND SPOILER ACTUATOR PER MM 27-62-101. PERFORMED OPERATIONAL CHECK, LEAK CHECK AND RIG CHECK. REPLACED NO. 1 AND NO. 2 ENGINE DRIVEN
- [SDR F3LA200100108](https://openairdocs.org/sdr/F3LA200100108.md): Coupling · disconnected · Sep 24, 2001 · N271FL · Boeing 7372L9 · Trailing Edge Flap Control System
  > AIR TURN BACK. FLIGHT CREW REPORTED FLAPS DID NOT RETRACT AFTER TAKEOFF. LT. TORQUE TUBE COUPLING AT NO. 4 FLAP TRANSMISSION WAS DISCONNECTED. RECONNECTED COUPLING PER MM 27-51-251. ADJUSTED TRAILING EDGE FLAPS PER MM 27-51-01 AND PERFORMED OPERATIONAL TES
- [SDR F3LA200100100](https://openairdocs.org/sdr/F3LA200100100.md): B-Nut · loose · Aug 21, 2001 · N271FL · Boeing 7372L9 · Hydraulic System, Main
  > AIR TURNBACK, FLIGHT CREW REPORTED LOSS OF A-SYSTEM HYDRAULIC PRESSURE AND QUANTITY. TIGHTENED NR 1 ENGINE SUPPLY LINE B-NUT, REPLACED NR 1 ENGINE CASE DRAIN FILTER. PERFORMED LEAK CHECK AND OPERATIONAL CHECK AND CHECKED OKAY.
- [SDR F3LA200100093](https://openairdocs.org/sdr/F3LA200100093.md): Web · cracked · Jun 25, 2001 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK, FLIGHT CREW REPORTED SEVERAL CRACKS FROM RIVET HOLE BEHIND THE 178 BULKHEAD IN THE FLOOR STRUCTURE AT BS 180, WL 207. MAINTENANCE REMOVED CRACKS FROM RIVET HOLE AND INSTALLED REPAIR PARTS PER SRM 51-40-02.
- [SDR F3LA200100056](https://openairdocs.org/sdr/F3LA200100056.md): Aileron · delaminated · Apr 23, 2001 · N271FL · Boeing 7372L9 · Ailerons
  > PRIOR TO DEPARTURE, MAINTENANCE REPORTED OTBD SIDE OF RT AILERON DELAMINATED. REPLACED AILERONS IN LT AND RT POSITIONS PER MM 27-11-11, RIGGED AILERONS, AND PERFORMED OPERATIONAL CHECK PER MM 27-11-11.
- [SDR F3LA200100008](https://openairdocs.org/sdr/F3LA200100008.md): Engine · vibration · Jan 21, 2001 · N271FL · Boeing 7372L9 · Engine (Turbine/Turboprop)
  > AIR TURNBACK. FLIGHT CREW REPORTED NR 1 ENGINE VIBRATION ON CLIMBOUT AT 20,000 FT. NR 1 ENGINE WAS SHUT DOWN AND AN EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO PHX WITHOUT INCIDENT. THE NR 1 ENGINE IS IN THE PROCESS OF BEING REPLACED. AN ADDENDUM WILL BE
- [SDR F3LA200100005](https://openairdocs.org/sdr/F3LA200100005.md): Teleflex Cable · out of adj · Jan 9, 2001 · N271FL · Boeing 7372L9 · Drag Control System
  > AIR TURN BACK. FLIGHT CREW REPORTED GEAR HANDLE WOULD NOT MOVE TO "UP" POSITION AFTER TAKEOFF AND LANDING GEAR WARNING HORN WOULD NOT SILENCE AFTER FLAPS WERE RETRACTED. REPLACED LANDING GEAR ACCESSORY UNIT AS PRECAUTIONARY PER MM 32-07-100. ADJUSTED GROUND
- [SDR F3LA200100004](https://openairdocs.org/sdr/F3LA200100004.md): Fire Detector · malfunctioned · Jan 5, 2001 · N271FL · Boeing 7372L9 · Fire Detection
  > FLIGHT CREW REPORTED APU FIRE WARNING ILLUMINATED IN FLIGHT FROM PHX TO DEN. THE APU FIRE BOTTLE WAS DISCHARGED AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT WAS DIVERTED TO ABQ AND LANDED WITHOUT INCIDENT.AN INSPECTION REVEALED NO SIGNS OF OVERHEATING OR FIRE
- [SDR F3LA200000272](https://openairdocs.org/sdr/F3LA200000272.md): Cooling Fan · inoperative · Dec 15, 2000 · N271FL · Boeing 7372L9 · Air Distribution Fan
  > UPON ARRIVAL, FLIGHT CREW REPORTED EQUIPMENT COOLING FAN "OFF" LIGHT ILLUMINATED IN FLIGHT. SELECTED ALT NORMAL BLOWER AND COOLING FAN CIRCUIT BREAKER TRIPPED, FOLLOWED BY AN ELECTRICAL BURNING ODOR. ALT FAN CONTINUED TO OPERATE NORMALLY. MAINTENANCE REPLACED
- [SDR F3LA00110](https://openairdocs.org/sdr/F3LA00110.md): Channel · corroded · May 31, 2000 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous Structure
  > DEN - DURING C-7 CHECK, INSPECTION REPORTED FORWARD LAVATORY AFT WALL HAT SECTION CORRODED AT BS 306, LBL 45, LBL 65. MAINTENANCE REPLACED HAT SECTION PER SRM 53-10-2 AND 53-10-3. (M)
- [SDR F3LA00111](https://openairdocs.org/sdr/F3LA00111.md): Skin · bulged · May 26, 2000 · N271FL · Boeing 7372L9 · Fuselage Main, Plate/Skin
  > DEN - DURING C-7 CHECK, INSPECTION REPORTED NR 1 DME ANTENNA BASE HAD SEALANT BLOWN OUT OF GAP, REVEALING A BULGE IN THE SKIN. MAINTENANCE REMOVED DME ANTENNA PER SRM 51-10-2. INSTALLED DOUBLER PER SRM 53-10-2. INSTALLED DME ANTENNA PER MM 34-55-11 AND PERF
- [SDR F3LA00103](https://openairdocs.org/sdr/F3LA00103.md): Fairing · cracked · May 21, 2000 · N271FL · Boeing 7372L9 · Engine Thrust Reverser
  > DEN - DURING C-7 CHECK, INSPECTION REPORTED A 2 INCH CRACK IN THE NR 2 ENGINE THRUST REVERSER FAIRING FORWARD WEB STIFFENER UNDER FIRE SEAL. MAINTENANCE REPLACED WEB ANGLE PER SRM''S 51-10-2, 51-40-3. 51-20-1, AND 51-10-1. (X)
- [SDR F3LA00082](https://openairdocs.org/sdr/F3LA00082.md): Intercostal · cracked · May 5, 2000 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous Structure
  > DEN - DURING C-7 CHECK, INSPECTION REPORTED A 1 INCH CRACK IN INTERCOSTAL AT LBL 5.7 FORWARD PRESSURE BULKHEAD BETWEEN WL 195 AND WL 194 BEHIND LANDING GEAR LEVER U SWITCH. MAINTENANCE REPAIRED CRACK PER SRM 53-10-11, FIGURE 8. (M)
- [SDR F3LA00074](https://openairdocs.org/sdr/F3LA00074.md): Angle · cracked · Apr 29, 2000 · N271FL · Boeing 7372L9 · Cargo/Baggage Doors
  > DEN - DURING C-7 CHECK, INSPECTION REPORTED CRACK IN LOWER AFT ANGLE OF C2 DOOR. MAINTENANCE REPLACED DAMAGED ANGLE PER SRM 51-40-3. (M)
- [SDR F3LA00072](https://openairdocs.org/sdr/F3LA00072.md): Beam · cracked · Apr 29, 2000 · N271FL · Boeing 7372L9 · Cargo/Baggage Doors
  > DURING C-7 CHECK INSPECTION REPORTED CRACK IN AFT CARGO DOOR LOWER REAR CROSSBEAM WEB. MAINTENANCE INSTALLED NEW LOWER REAR CROSSBEAM WEB CHORD PER SRM 51-30-2. (M)
- [SDR F3LA00071](https://openairdocs.org/sdr/F3LA00071.md): Beam · cracked · Apr 29, 2000 · N271FL · Boeing 7372L9 · Cargo/Baggage Doors
  > DURING C-7 CHECK INSPECTION, REPORTED AFT CARGO DOOR LOWER AFT BEAM INNER WEB CRACKED. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED PER SRM 51-40-3. (M)
- [SDR F3LA00068](https://openairdocs.org/sdr/F3LA00068.md): Skin · cracked · Apr 27, 2000 · N271FL · Boeing 7372L9 · Passenger/Crew Doors
  > DEN - DURING C-7 CHECK INSPECTION, REPORTED CRACK IN INTERIOR PANEL SKIN JUST FORWARD OF L-2 DOOR CENTER. MAINTENANCE FABRICATED REPAIR STRAP AND REPAIRED AREA PER EA 53-737-065. (M)
- [SDR F3LA00043](https://openairdocs.org/sdr/F3LA00043.md): Web · torn · Apr 20, 2000 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous Structure
  > DURNG C-7 CHECK INSPECTION, REPORTED WEB TORN BETWEEN BS 294 AND BS 312, BELOW TOP CHORD AT STIFFENER. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 53-10-2 AND 51-30-2. (M)
- [SDR F3LA00055](https://openairdocs.org/sdr/F3LA00055.md): Frame · corroded · Apr 20, 2000 · N271FL · Boeing 7372L9 · Fuselage Main, Frame
  > DEN - DURING C-7 CHECK, INSPECTION REPORTED E/E FRAME CORRODED AT BS 312, STRINGER 26L. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED AND INSTALLED REPAIR SECTION PER SRM 51-40-3. (M)
- [SDR F3LA00045](https://openairdocs.org/sdr/F3LA00045.md): Channel · cracked · Apr 18, 2000 · N271FL · Boeing 7372L9 · Nacelle/Pylon Structure
  > DEN - DURING C-7 CHECK INSPECTION, REPORTED 1.6 INCH CRACKED IN RIGHT ENGINE INBOARD FIXED COWL AT LAST RIB, UPPER CROSS U-CHANNEL. MAINTENANCE FABRICATED REPLACEMENT U-CHANNEL, SHIMS AND CORNER BRACE PER SRM 54-10-2. (M)
- [SDR F3LA00059](https://openairdocs.org/sdr/F3LA00059.md): Angle · cracked · Apr 17, 2000 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous Structure
  > DEN - DURING C-7 CHECK INSPECTION REPORTED CRACK IN AIRSTAIR DOOR TRACK SUPPORT ANGLE AT BS 351 STRINGER 22. MAINTENANCE REPAIRED TRACK SUPPORT ANGLE PER SRM 51-40-3. (M)
- [SDR F3LA00058](https://openairdocs.org/sdr/F3LA00058.md): Structure · damaged · Apr 17, 2000 · N271FL · Boeing 7372L9 · Nacelle/Pylon Structure
  > DEN - DURING C-7 CHECK INSPECTION REPORTED A HOLE IN THE NR 2 ENGIEN INLET. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2. (M)
- [SDR F3LA00070](https://openairdocs.org/sdr/F3LA00070.md): Frame · cracked · Apr 16, 2000 · N271FL · Boeing 7372L9 · Fuselage Main, Frame
  > DURING C-7 INSPECTION, FOUND FRAME CRACKED IN RADIUS FORWARD OF E/E BAY DOOR AT BS 294.5, STRINGER 23R. MAINTENANCE REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PER SRM 53-10-4. (M)
- [SDR F3LA00057](https://openairdocs.org/sdr/F3LA00057.md): Mount · corroded · Apr 16, 2000 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous Structure
  > DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON SUPPORTS AND MOUNTING SKIN OF AFT LAVATORY HEATED WATER DRAIN MAST, BS 987, STRINGER 23-24. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 53-10-2 FIG 5, 51-30-2 A
- [SDR F3LA00042](https://openairdocs.org/sdr/F3LA00042.md): Web · cracked · Apr 15, 2000 · N271FL · Boeing 7372L9 · Passenger/Crew Doors
  > DEN - DURING C-7 CHECK INSPECTION, REPORTED CRACK IN LIGHTENING HOLE ON R-1 DOOR TORQUE BOX WEB. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 51-40-3. (M)
- [SDR F3LA00069](https://openairdocs.org/sdr/F3LA00069.md): Track · cracked · Apr 14, 2000 · N271FL · Boeing 7372L9 · Cargo/Baggage Doors
  > DEN - DURING C-7 CHECK INSPECTION REPORTED, CRACK IN RIGHT FORWARD CARGO DOOR TRACK INBOARD OF DOOR CENTER AT BS 460, STRINGER 27R. MAINTENANCE INSTALLED NEW TRACK AND NEW NUT PLATES ON TRACK TO ATTACH FLOORBOARDS PER SRM 53-20-1. (M)

Next page: https://openairdocs.org/deregistered/N271FL-2003-03-20/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 = 'N271FL' AND deregistration_id = 'N271FL-2003-03-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N271FL-2003-03-20/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.