# Service difficulty reports: N270FL, cancelled Mar 20, 2003

A list on [N270FL, cancelled Mar 20, 2003](https://openairdocs.org/deregistered/N270FL-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 · 123 reports

- [SDR F3LA200200362](https://openairdocs.org/sdr/F3LA200200362.md): Door Frame · cracked · Oct 23, 2002 · N270FL · Boeing 7372L9 · Fuselage Main, Structure
  > DURING C 2 CHECK, A CRACK WAS FOUND IN THE LOWER, FORWARD AND AFT CORNERS OF THE DOOR FRAME ON THE FORWARD BAGGAGE COMPARTMENT DOOR. THE LOWER, FORWARD AND AFT FRAMES OF THE FORWARD BAGGAGE COMPARTMENT DOOR WERE REPLACED IAW SB 737-52A1100, FIGURE 2, AND COMP
- [SDR F3LA200200332](https://openairdocs.org/sdr/F3LA200200332.md): Angle · cracked · Oct 8, 2002 · N270FL · Boeing 7372L9 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED RT AFT WING TO BODY FAIRING SUPPORT ANGLE CRACKED AT STRINGER 20, BS 727-727B. FABRICATED AND INSTALLED REPLACEMENT SUPPORT ANGLE PER SRM 51-10-02, SRM 51-30-00 AND BOEING DRAWING 65-48657.
- [SDR F3LA200200331](https://openairdocs.org/sdr/F3LA200200331.md): Skin · gouged · Oct 8, 2002 · N270FL · Boeing 7372L9 · Trailing Edge Flaps
  > DURING C-2 CHECK, INSPECTION REPORTED RT. WING OTBD FOREFLAP UPPER SURFACE GOUGED AT WBL 314. REMOVED EXISTING REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT DOUBLER PER SRM 51-40-20.
- [SDR F3LA200200330](https://openairdocs.org/sdr/F3LA200200330.md): Skin · gouged · Oct 8, 2002 · N270FL · Boeing 7372L9 · Trailing Edge Flaps
  > DURING C-2 CHECK, INSPECTION REPORTED RT. WING INBD FOREFLAP, INBD UPPER SURFACE, GOUGED IN 2 AREAS. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-20.
- [SDR F3LA200200348](https://openairdocs.org/sdr/F3LA200200348.md): Floor Support · corroded · Sep 29, 2002 · N270FL · Boeing 7372L9 · Fuselage Miscellaneous Structure
  > DURING C 2 CHECK, CORROSION FOUND IN AFT CARGO BAY FLOOR SUPPORT AT LBL 8. REMOVED DAMAGED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-5, FIGURE 6
- [SDR F3LA200200171](https://openairdocs.org/sdr/F3LA200200171.md): Battery Pack · discharged · Jun 12, 2002 · N270FL · Boeing 7372L9 · Emergency Lighting
  > MAINTENANCE REPORTED SECTION OF EMERGENCY AISLE PATH LIGHTING IN FWD CABIN INOPERATIVE. FERRIED AIRCRAFT TO DEN FOR REPAIR. UPON ARRIVAL, REPLACED THE FWD BATTERY AND POWER SUPPLY ASSY. PERFORMED OPERATIONAL TEST AND CHECKED OKAY.
- [SDR F3LA200200107](https://openairdocs.org/sdr/F3LA200200107.md): Door Frame · cracked · Mar 9, 2002 · N270FL · Boeing 7372L9 · Cargo/Baggage Doors
  > DURING AN OUTFLOW VALVE TEST WITH THE AIRCRAFT PRESSURIZED, MAINTENANCE REPORTED A LOUD POP IN THE AREA OF THE AFT CARGO DOOR AND FOUND A 5-INCH CRACK IN THE RADIUS OF THE DOOR FRAME OTBD OF THE LOWER FWD STOP FITTING AND CRACKS IN THE LOWER DOOR BEAM OTBD CHO
- [SDR F3LA200200106](https://openairdocs.org/sdr/F3LA200200106.md): Cartridge · defective · Mar 1, 2002 · N270FL · Boeing 7372L9 · Aileron Control System
  > UPON ARRIVAL, FLIGHT CREW REPORTED AILERONS BECAME EXTREMELY TIGHT AND FELT AS IF IN MANUAL REVERSION. HYDRAULIC SYSTEM PRESSURES WERE BOTH NORMAL. RUDDER AND ELEVATOR FELT NORMAL. ACCOMPLISHED NORMAL LANDING. REPLACED AILERON SPRING CARTRIDGE PER MM 27-11
- [SDR F3LA200100151](https://openairdocs.org/sdr/F3LA200100151.md): Skin · gouged · Dec 31, 2001 · N270FL · Boeing 7372L9 · Fuselage Main, Plate/Skin
  > DURING C-1 CHECK, INSPECTION REPORTED FUSELAGE SKIN LAP AT STR 19-R, STA 386 TO STA 410 SCRATCHED AND GOUGED. A 14.5 INCH AREA ON SKIN LAP AT STR 19-R, STA 386 TO STA 410 FOUND TO BE OUT OF LIMITS PER SRM 53-30-01. DAMAGE WAS REMOVED BETWEEN STA 390 AND STA
- [SDR F3LA200100138](https://openairdocs.org/sdr/F3LA200100138.md): Bushing · corroded · Dec 15, 2001 · N270FL · Boeing 7372L9 · Wing, Attach Fittings
  > DURING C-1 CHECK, INSPECTION REPORTED ALL BUSHINGS CORRODED ON RT WING SWING LINK ASSY. REPLACED RT WING SWING LINK ASSY PER BOEING DRAWING 65-82770 AND MM 57-15-0, STEP 5E.
- [SDR F3LA200100137](https://openairdocs.org/sdr/F3LA200100137.md): Collar · corroded · Dec 15, 2001 · N270FL · Boeing 7372L9 · Main Landing Gear
  > DURING C-1 CHECK, INSPECTION REPORTED LT. MLG BELLCRANK RETAINING COLLAR CORRODED. REPLACED RETAINING COLLAR PER MM 32-32-31.
- [SDR F3LA200100122](https://openairdocs.org/sdr/F3LA200100122.md): Pylon · gouged · Nov 18, 2001 · N270FL · Boeing 7372L9 · Nacelle/Pylon, Main Frame
  > DURING C-1 CHECK, INSPECTION REPORTED GOUGE IN NR 1 ENGINE PYLON, AFT OTBD LOWER CORNER. REMOVED GOUGE PER SRM 51-10-2. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-2.
- [SDR F3LA200100126](https://openairdocs.org/sdr/F3LA200100126.md): Skin · damaged · Nov 17, 2001 · N270FL · Boeing 7372L9 · Fuselage Main, Plate/Skin
  > DURING C-1 CHECK, INSPECTION REPORTED A 14.5 INCH AREA ON FUSELAGE SKIN LAP AT STR 19R, BS 386-410, SCRATCHED AND GOUGED. REMOVED DAMAGE AT BS 390-404, STR 19R PER SRM 53-30-3, FABRICATED FILLER AND DOUBLER AND INSTALLED PER SRM 53-30-3, 51-20-4, 20-10-18 AND
- [SDR F3LA200100125](https://openairdocs.org/sdr/F3LA200100125.md): Doubler · torn · Nov 17, 2001 · N270FL · Boeing 7372L9 · Engine Cowling System
  > DURING C-1 CHECK, INSPECTION REPORTED NR 2 ENGINE OTBD ENGINE COWL DOUBLER METAL TORN AT LATCH CUTOUT, 5TH LATCH FROM AFT. FABRICATED AND INSTALLED DOUBLER AND STRIKER PLATE PER SRM 51-40-2.
- [SDR F3LA200100121](https://openairdocs.org/sdr/F3LA200100121.md): Skin · dented · Nov 17, 2001 · N270FL · Boeing 7372L9 · Vertical Stabilizer, Plate/Skin
  > DURING C-1 CHECK, INSPECTION REPORTED SEVERAL DENTS IN SKIN OF DORSAL FIN FWD OF VERTICAL STABILIZER. FABRICATED AND INSTALLED EXTERNAL REPAIR PER SRM 55-30-6 AND 51-20-1.
- [SDR F3LA200100120](https://openairdocs.org/sdr/F3LA200100120.md): Skin · gouged · Nov 17, 2001 · N270FL · Boeing 7372L9 · Nacelle/Pylon, Plate/Skin
  > DURING C-1 CHECK, INSPECTION REPORTED GOUGES IN SKIN AND SCRATCHES ON OTBD SIDE OF RT ENGINE PYLON, AFT END AREA ABOVE THRUST REVERSER FAIRING. PERFORMED TYPICAL WEB REPAIR PER SRM 51-40-01 AND 51-30-02.
- [SDR F3LA200100118](https://openairdocs.org/sdr/F3LA200100118.md): Door · cracked · Nov 16, 2001 · N270FL · Boeing 7372L9 · Engine Thrust Reverser
  > DURING C-1 CHECK, INSPECTION REPORTED CRACK IN OUTER SKIN OF NR 2 ENGINE TOP OUTBOARD THRUST REVERSER FAIRING DOOR. INSTALLED SCAB PATCH PER SRM 51-40-02.
- [SDR F3LA200100119](https://openairdocs.org/sdr/F3LA200100119.md): Nose Cowl · worn · Nov 16, 2001 · N270FL · Boeing 7372L9 · Engine Cowling System
  > DURING C-1 CHECK, INSPECTION REPORTED NR 1 ENGINE NOSE COWL AT 2 O'CLOCK POSITION MATING SURFACE WORN. CUT AWAY DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 54-10-03, 51-20-1 AND MM 51-21-99.
- [SDR F3LA200100101](https://openairdocs.org/sdr/F3LA200100101.md): Control Cable · broken · Aug 21, 2001 · N270FL · Boeing 7372L9 · Drag Control System
  > ON WALKAROUND PRIOR TO FLIGHT, MAINTENANCE REPORTED LT SPOILER CABLE BROKEN. FABRICATED AND INSTALLED REPLACEMENT SPOILER CABLE PER MM 27-09-111 AND MM 20-10-91. ADJUSTED AND TESTED SYSTEM PER MM 27-61-00.
- [SDR F3LA200100099](https://openairdocs.org/sdr/F3LA200100099.md): Battery · Aug 8, 2001 · N270FL · Boeing 7372L9 · Emergency Lighting
  > PRIOR TO DEPARTURE, MAINTENANCE REPORTED OVERHEAD EXIT LOCATOR SIGN FOR OVERWING EMERGENCY EXITS, FIXED EXIT LIGHTS ON SIDE OF EMERGENCY EXITS AND EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. FERRIED AIRCRAFT TO DEN. REPLACED BATTERIES, PERFORMED OPERATIONA
- [SDR F3LA200100042](https://openairdocs.org/sdr/F3LA200100042.md): Control Unit · malfunctioned · Mar 10, 2001 · N270FL · Boeing 7372L9 · Cabin Pressure Control System
  > AIR TURNBACK. FLIGHT CREW REPORTED PRESSURIZATION SYSTEM WARNING HORN SOUNDED AT 14000 FT AND OXYGEN MASKS DROPPED. AIRCRAFT RETURNED TO DEN WITHOUT INCIDENT. PERFORMED OPERATIONAL TEST OF PRESSURIZATION CONTROL SYSTEM PER MM 21-31-0 AND FOUND NO DISCREPANC
- [SDR F3LA200100040](https://openairdocs.org/sdr/F3LA200100040.md): Control Unit · failed · Mar 7, 2001 · N270FL · Boeing 7372L9 · Passenger Oxygen System
  > PRIOR TO DEPARTURE, FLIGHT CREW REPORTED ALL PASSENGER OXYGEN MASKS DEPLOYED AFTER OXYGEN SYSTEM WAS SERVICED. REPLACED PASSENGER OXYGEN CONTINUOUS FLOW CONTROL UNIT PER MM 35-21-21, RESTOWED OXYGEN MASKS, PERFORMED OPERATIONAL TEST AND LEAK CHECK, AND SYSTEM
- [SDR F3LA200100034](https://openairdocs.org/sdr/F3LA200100034.md): Fairing · damaged · Feb 23, 2001 · N270FL · Boeing 7372L9 · Aerodynamic Fairings
  > AIRCRAFT DIVERTED TO GRAND JUNCTION, COLORADO DUE TO WEATHER. UPON WALKAROUND, FLIGHT CREW REPORTED DAMAGE TO RT INBD WING-TO-BODY FAIRING ELEPHANT EAR SCUFF PLATES DAMAGED. AIRCRAFT WAS FERRIED TO DEN FOR REPAIR. MAINTENANCE REPLACED RT INBD WING-TO-BODY F
- [SDR F3LA200100035](https://openairdocs.org/sdr/F3LA200100035.md): Indicator · inoperative · Feb 19, 2001 · N270FL · Boeing 7372L9 · Trailing Flap Position Indicating System
  > FLIGHT CREW REPORTED STICK SHAKER ACTIVATED ON TAKEOFF FOR APPROXIMATELY 3 SECONDS. REPLACED RT TRAILING EDGE FLAP POSITION INDICATOR PER MM 27-58-01.
- [SDR F3LA200000255](https://openairdocs.org/sdr/F3LA200000255.md): Detector · defective · Nov 1, 2000 · N270FL · Boeing 7372L9 · Fire Detection
  > PRIOR TO DEPARTURE, FLIGHT CREW REPORTED CARGO COMPARTMENT FIRE DETECTION/SUPPRESSION SYSTEM. MAINTENANCE LIGHT AND SYSTEM OK LIGHT BOTH ILLUMINATED. MAINTENANCE REPLACED FORWARD CARGO COMPARTMENT SMOKE DETECTION UNIT, POSITION NR 3.
- [SDR F3LA00151](https://openairdocs.org/sdr/F3LA00151.md): Module · failed · Jul 16, 2000 · N270FL · Boeing 7372L9 · Landing Gear Selector
  > DEN - ON APPROACH INTO DEN, FLIGHT CREW REPORTED THREE RED LIGHTS AT GEAR EXTENSION. RECYCLED GEAR AND RECEIVED THREE GREEN LIGHTS. MAINTENANCE REPLACED LANDING GEAR HANDLE MODULE. (M)
- [SDR F3LA00141](https://openairdocs.org/sdr/F3LA00141.md): Link · corroded · Jul 6, 2000 · N270FL · Boeing 7372L9 · Aileron Control System
  > DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON AILERON ACTUATOR REACTION LINK AROUND BEARING RETAINER AND A CRACK ON BEARING BOSS. MAINTENANCE REPLACED AILERON ACTUATOR REACTION LINK WITH NEW LOWER ASSY PER MM 27-11-101. (M)
- [SDR F3LA00126](https://openairdocs.org/sdr/F3LA00126.md): Case · cracked · Jun 26, 2000 · N270FL · Boeing 7372L9 · Engine Collector/Tailpipe/Nozzle
  > DEN - DURING C-7 CHECK INSPECTION, REPORTED NR 2 ENGINE EXHAUST CASE CRACKED AT 3, 6 AND 9 O''CLOCK STRUTS AT ROOT OF FAIRING, AND OUTBOARD LEADING EDGE OR 9:00 O''CLOCK STRUT. MAINTENANCE REPLACED NR 2 ENGINE PER WORK CARD 7-0316. (M)
- [SDR F3LA00140](https://openairdocs.org/sdr/F3LA00140.md): Hinge · corroded · Jun 24, 2000 · N270FL · Boeing 7372L9 · Cargo/Baggage Doors
  > DEN - DURING C-7 CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR DOOR CORRODED AT CENTER PART OF HINGE. MAINTENANCE REPLACED RIGHT MAIN LANDING GEAR DOOR PER MM 32-13-21 AND 32-13-11. (M)
- [SDR F3LA00139](https://openairdocs.org/sdr/F3LA00139.md): Frame · damaged · Jun 24, 2000 · N270FL · Boeing 7372L9 · Fuselage Main, Frame
  > DEN - DURING C-7 CHECK INSPECTION, FOUND LEFT AFT BULKHEAD FRAME IN AFT CARGO COMPARTMENT DAMAGED. MAINTENANCE REMOVED DAMAGED AREA AND REPAIRED PER SRM 51-10-02 AND 53-10-01. (M)
- [SDR F3LA00137](https://openairdocs.org/sdr/F3LA00137.md): Channel · corroded · Jun 24, 2000 · N270FL · Boeing 7372L9 · Fuselage Miscellaneous Structure
  > DEN - DURING C-7 CHECK INSPECTION, FORWARD LAVATORY AFT WALL HAT SECTION CORRODED AT BS 306, LBL 45-65. MAINTENANCE REPLACED HAT SECTION PER SRM 53-10-2 AND 53-10-3. (M)
- [SDR F3LA00136](https://openairdocs.org/sdr/F3LA00136.md): Skin · damaged · Jun 24, 2000 · N270FL · Boeing 7372L9 · Engine Thrust Reverser
  > DEN - DURING C-7 CHECK INSPECTION, FOUND HOLE IN NR 2 THRUST REVERSER SKIN AND SMALL CRACKS AT 11:00 POSITION 1.25 INCHES AFT OF THRUST REVERSER SKIN. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED DOUBLER AND REPAIRED PER EA 78-737-015. (M)
- [SDR F3LA00135](https://openairdocs.org/sdr/F3LA00135.md): Channel · damaged · Jun 24, 2000 · N270FL · Boeing 7372L9 · Engine Cowling System
  > DEN - DURING C-7 CHECK INSPECTION, FOUND BOTTOM CHANNEL OF NR 2 ENGINE INBOARD COWL DAMAGED AT FORWARD END. MAINTENANCE REMOVED DAMAGED SECTINO OF LOWER CHANNEL AND FABRICATED REPLACEMENT CHANNEL PER SRM 51-30-2 AND 51-30-01. (M)
- [SDR F3LA00134](https://openairdocs.org/sdr/F3LA00134.md): Rib · cracked · Jun 24, 2000 · N270FL · Boeing 7372L9 · Horizontal Stabilizer, Spar/Rib
  > DEN - DURING C-7 CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED 4TH RIB FROM INBOARD END. MAINTENANCE REPAIRED CRACKED RIB PER SRM 51-10-1 AND 51-40-3. (M)
- [SDR F3LA00133](https://openairdocs.org/sdr/F3LA00133.md): Spindle · corroded · Jun 24, 2000 · N270FL · Boeing 7372L9 · Trailing Edge Flaps
  > DEN - DURING C-7 CHECK INSPECTION, FOUND CORROSION ON LEFT OUTBOARD FLAP INBOARD CARRIAGE SPINDLE. MAINTENANCE REPLACED LEFT OUTBOARD FLAP INBOARD SPINDLE CARRIAGE ASSY. (M)
- [SDR F3LA00132](https://openairdocs.org/sdr/F3LA00132.md): Skin · cracked · Jun 24, 2000 · N270FL · Boeing 7372L9 · Cargo/Baggage Doors
  > DEN - DURING C-7 CHECK INSPECTION, FOUND 2 INCH CRACK IN C-1 DOOR INNER SKIN ABOVE INNER DOOR HANDLE LIGHTNING HOLE. MAINTENANCE REPAIRED CRACK PER SRM 51-40-2. (M)
- [SDR F3LA00131](https://openairdocs.org/sdr/F3LA00131.md): Cowl Door · damaged · Jun 24, 2000 · N270FL · Boeing 7372L9 · Engine Cowling System
  > DEN - DURING C-7 CHECK, INSPECTION FOUND NR 2 ENGINE INBOARD COWL DAMAGED, EXTERNAL SURFACE, 32 INCHES FROM AFT END AND 12 INCHES FROM TOP. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED AND INSTALLED DOUBLER AND FILLER PER SRM 54-10-3. (M)
- [SDR F3LA00129](https://openairdocs.org/sdr/F3LA00129.md): Skin · corroded · Jun 24, 2000 · N270FL · Boeing 7372L9 · Leading Edge Devices
  > DEN - DURING C-7 CHECK INSPECTION, REPORTED CORROSION ON LEFT WING OUTBOARD FORE FLAP, INBOARD MOUNT SUPPORT. MAINTENANCE REPLACED FORE FLAP. (M)
- [SDR F3LA00128](https://openairdocs.org/sdr/F3LA00128.md): Floorbeam · corroded · Jun 24, 2000 · N270FL · Boeing 7372L9 · Fuselage Main, Floor Beam
  > DEN - DURINGC-7 CHECK INSPECTION REPORTED, CORROSION ON TOP OF FLOORBEAM FRAME, BS 328 RBL 12. MAINTENANCE INSTALLED INTERCOSTAL, HI-LOCKS, ANGLE, BRACKETS AND FLOORCAP PER SRM 51-40-3. (M)
- [SDR F3LA00127](https://openairdocs.org/sdr/F3LA00127.md): Skin · cracked · Jun 24, 2000 · N270FL · Boeing 7372L9 · Engine Thrust Reverser
  > DEN - FOUND DURING C-7 CHECK INSPECTION, REPORTED RIGHT ENGINE THRUST REVERSER LOWER CLAM SHELL INNER SKIN CRACKED. MAINTENANCE REPLACED INNER SKIN PER SRM 51-10-2, 51-30-2 AND 51-30-3. (M)
- [SDR F3LA00125](https://openairdocs.org/sdr/F3LA00125.md): Frame · cracked · Jun 24, 2000 · N270FL · Boeing 7372L9 · Fuselage Main, Frame
  > DEN - DURING C-7 CHECK INSPECTION, REPORTED CRACK IN RADIUS OF CIRCUMFERENTIAL CHORD BETWEEN STRINGER 20 AND STRINGER 21 AT BS 540 IN FORWARD CARGO COMPARTMENT AC BAY LT SIDEWALL. MAINTENANCE REMOVED DAMAGED CHORD, FABRICATED AND INSTALLED DOUBLER PER EA 57-7
- [SDR F3LA00138](https://openairdocs.org/sdr/F3LA00138.md): Floorbeam · damaged · Jun 24, 2000 · N270FL · Boeing 7372L9 · Fuselage Main, Floor Beam
  > DEN - FOUND DURING C-7 CHECK INSPECTION, REPORTED AFT FLOOR FRAME IN AFT CARGO COMPARTMENT DAMAGED, BS 947. MAINTENANCE REMOVED DAMAGED AREA AND REPAIRED PER SRM 51-10-01, 51-10-02 AND 53-10-01. (M)
- [SDR F3LA00130](https://openairdocs.org/sdr/F3LA00130.md): Skin · cracked · Jun 21, 2000 · N270FL · Boeing 7372L9 · Engine Thrust Reverser
  > DEN - DURING C-7 CHECK INSPECTION, FOUND CRACK IN SKIN ABOVE LOWER ACCESS PLATE, OUTBOARD SIDE, OF NR 2 ENGINE THRUST REVERSER. MAINTENANCE REPLACED SKIN PER OHM 78-30-12 AND SRM 51-10-1 AND 51-20-1. (M)
- [SDR F3LA00118](https://openairdocs.org/sdr/F3LA00118.md): Plate · corroded · Jun 1, 2000 · N270FL · Boeing 7372L9 · Cargo/Baggage Doors
  > DEN - DURING C-7 CHECK INSPECTION, FOUND AFT CARGO DOOR EDGE PLATES CORRODED. MAINTENANCE FABRICATED REPLACEMENT EDGE PLATES AND REPAIRED PER SRM 53-20-2, FIGURE 8, AND SRM 51-20-1, FIGURE 7. (M)
- [SDR F3LA00117](https://openairdocs.org/sdr/F3LA00117.md): Cowling · damaged · Jun 1, 2000 · N270FL · Boeing 7372L9 · Engine Cowling System
  > DEN - DURING C-7 CHECK INSPECTION, FOUND NR 1 ENGINE OUTBOARD COWL HAD A CRACK FROM RIVET HOLE, BELOW NR 2 HINGE POINT. MAINTENANCE REMOVED DAMAGED SKIN AREA AND REPAIRED PER SRM 54-10-3. (M)
- [SDR F3LA00116](https://openairdocs.org/sdr/F3LA00116.md): Carriage · corroded · Jun 1, 2000 · N270FL · Boeing 7372L9 · Trailing Edge Flap Control System
  > DEN - FOUND DURING C-7 CHECK INSPECTION, FOUND PITTING CORROSION ON LT INBOARD MID-FLAP OUTBOARD CARRIAGE ON INSIDE DIAMETER OF TORQUE TUBE HOLES. MAINTENANCE REPLACED LT INBOARD MID FLAP OUTBOARD CARRIAGE ASSY. (M)
- [SDR F3LA00115](https://openairdocs.org/sdr/F3LA00115.md): Rod · corroded · Jun 1, 2000 · N270FL · Boeing 7372L9 · Rudder Control System
  > DEN - DURING C-7 CHECK INSPECTION, FOUND CORROSION ON ADJUSTMENT THREADS OF RUDDER PCU VERNIER ROD AND CHAFING ON AFT OUTBOARD SIDE OF ROD. MAINTENANCE REPLACED VERNIER ROD PER MM 27-21-72. (M)
- [SDR F3LA00113](https://openairdocs.org/sdr/F3LA00113.md): Seat Track · cracked · May 31, 2000 · N270FL · Boeing 7372L9 · Fuselage, Seat/Cargo Attach Fittings
  > DEN - DURING C-7 CHECK, INSPECTION REPORTED CRACKS AT FOUR SEAT TRACK ATTACH POINTS AT BS 520. MAINTENANCE REPAIRED FLOORBEAM PER EA 53-737-073, PAGES 1, 2 AND 3, EA 53-737-070, SRM 51-30-2, SRM 51-30-05 AND SRM 53-10-9. (M)
- [SDR F3LA00109](https://openairdocs.org/sdr/F3LA00109.md): Shroud · cracked · May 30, 2000 · N270FL · Boeing 7372L9 · Fuselage Miscellaneous Structure
  > DEN - DURING C-7 CHECK, INSPECTION REPORTED APU UPPER SHROUD RIGHT SIDE CENTER LIGHTENING HOLE CRACKED. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED DOUBLER AND REPAIRED PER SRM 53-30-1 AND 51-40-2. (M)
- [SDR F3LA000108](https://openairdocs.org/sdr/F3LA000108.md): Shroud · cracked · May 30, 2000 · N270FL · Boeing 7372L9 · Fuselage Miscellaneous Structure
  > DEN - DURING C-7 CHECK, INSPECTION REPORTED APU UPPER SHROUD RIGHT SIDE CENTER LIGHTENING HOLE CRACKED. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED DOUBLER AND REPAIRED PER SRM 53-30-1 AND 51-40-2. (M)

Next page: https://openairdocs.org/deregistered/N270FL-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 = 'N270FL' AND deregistration_id = 'N270FL-2003-03-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N270FL-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.