# Service difficulty reports: N554FE, cancelled Jan 29, 2024

A list on [N554FE, cancelled Jan 29, 2024](https://openairdocs.org/deregistered/N554FE-2024-01-29.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 · 130 reports

- [SDR FDEA201608172904](https://openairdocs.org/sdr/FDEA201608172904.md): Bar · disconnected · Aug 17, 2016 · N554FE · Doug MD1010F · Passenger/Crew Doors
  > MANUAL DOOR LIFT BAR ON R1 DOOR DISCONNECTED. REINSTALLED LIFT BAR IAW MM 52-10-01-50, AND 25-61-02-5.
- [SDR FDEA201606222117](https://openairdocs.org/sdr/FDEA201606222117.md): Bulkhead · cracked · Jun 22, 2016 · N554FE · Doug MD1010F · Fuselage Main, Bulkhead
  > FOUND 15" LONG CRACK IN THE CAC AFT WALL LT SIDE ABOVE THE NR 2 PNUEMATIC DUCT FEED THROUGH DURING FUSELAGE PRESSURIZATION CHECK. RECEIVED FINAL EA 8-5300-T0326238; FUSELAGE, GENERAL-STA 1159 PRESSURE BULKHEAD REPAIR, LT SIDE, COMPLIED WITH.
- [SDR FDEA201606041809](https://openairdocs.org/sdr/FDEA201606041809.md): Manifold · failed · Jun 4, 2016 · N554FE · Doug MD1010F · Pneumatic Distribution System
  > DURING CLIMB GOT LEVEL 2 ENG 3 LOOP A. COMPLIED WITH CHECKLIST B LOOP TESTED GOOD. MEL 02 JUN16 04:05. RELEASED FOR SERVICE IAW MEL 26-11-01-01 CATEGORY C EXPIRATION 11JUN16. ENG NR 3 LOOP A INOPERATIVE, USE LOOP B. PLEASE TROUBLESHOOT ID & UPDATE ITEM
- [SDR FDEA201601100105](https://openairdocs.org/sdr/FDEA201601100105.md): Engine · bird ingestion · Jan 10, 2016 · N554FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > MULTIPLE FAN BLADES DAMAGED ON NR 3 ENG DUE TO BIRD STRIKE. DURING BORESCOPE OF NR 3 ENG FOR BIRD STRIKE, FOUND LARGE TEAR ON LE 10TH STAGE THROUGH PORT B1-10. REPLACED NR 3 ENG.
- [SDR FDEA201508072513](https://openairdocs.org/sdr/FDEA201508072513.md): Skin · cracked · Aug 7, 2015 · N554FE · Doug MD1010F · Leading Edge Devices
  > TWO CRACKS EXIST IN LT NR 1 LE SLAT. ONE IS 1.4 INCHES LONG, THE OTHER, 0.8 INCHES LONG. REPAIRED LT NR 1 SLAT SKIN LE IAW SRM 57-10-00. RCS TRACKING ON EA 8-5710-T0319366. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
- [SDR FDEA201507142221](https://openairdocs.org/sdr/FDEA201507142221.md): Battery · discharged · Jul 14, 2015 · N554FE · Doug MD1010F · Emergency Equipment
  > R1 DOOR SLIDE LIGHT DOES NOT TEST. R & R BATTERIES FOR PRESS TEST LIGHT IAW AMM 25-61-02-2. OPERATIONS CHECKED NORMAL, OK TO CONTINUE.
- [SDR FDEA201507012133](https://openairdocs.org/sdr/FDEA201507012133.md): Smoke Warning · false activation · Jul 1, 2015 · N554FE · Doug MD1010F · Smoke Detection
  > FORWARD LOWER CARGO FIRE WARNING, AGENT DISCHARGED. NO SMOKE OR FIRE WAS FOUND, FALSE INDICATION. REMOVED FREIGHT & PLACED ALL LOWER CARGO COMPARTMENTS ON MEL. DISCONNECTED ALL 8 LOWER CARGO SMOKE DETECTORS IAW EA 8-2617-T0318588 & PLACED THE NR 1 & 2 FIRE
- [SDR FDEA201505281641](https://openairdocs.org/sdr/FDEA201505281641.md): Pressure Switch · failed · May 28, 2015 · N554FE · Doug MD1010F · Airfoil Anti/De-ice System
  > IN CRUISE WITH WING ANTI-ICE ON WE RECEIVED NR 3 MANIFOLD FAIL LIGHT IN SWITCH & RECEIVED MANIFOLD FAIL INDICATION ON SYNOPTIC, NO MANIFOLD FAIL NR 3 ALERT WARNING THOUGH. R & R RT WING PRESSURE SWITCH IAW AMM 36-23-03-4. OPERATIONS CHECKED NORMAL, OK TO CO
- [SDR FDEA201412174137](https://openairdocs.org/sdr/FDEA201412174137.md): Fairing · delaminated · Dec 17, 2014 · N554FE · Doug MD1010F · Horizontal Stabilizer Structure
  > RIGHT LOWER HORIZONTAL STAB FAIRING IS DELAMINATED, SECTION ADJACENT TO ATTACH POINT. REPAIRED RT HORIZONTAL STAB LOWER FAIRING IAW SRM 51-71-00 VOL II & PAINTED IAW SRM 51-21-02 VOL II.
- [SDR FDEA201412114104](https://openairdocs.org/sdr/FDEA201412114104.md): Skin · cracked · Dec 11, 2014 · N554FE · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING, LOWER WING ATTACH PANEL SURFACE 618 GB AFT OF SLAT TRACK NR 8 HAS A 1 INCH CRACK. DOT 1 REPAIR COMPLIED WITH IAW SRM 57-10 00 FIG 49 SHEET 1 THROUGH 4 VOL 1.
- [SDR FDEA201412054071](https://openairdocs.org/sdr/FDEA201412054071.md): Seat Track · damaged · Dec 5, 2014 · N554FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK STATION 1310 RBL 27.50 SEAT TRACK DAMAGED. REMOVED DAMAGED SEAT TRACK AT MAIN DECK STATION 1259 - 1330 RBL 27.50 IAW SRM 53-70-00 FIG 1A VOL I EEL 537397 11/23/14. REPLACED DAMAGED SEAT TRACK IAW SRM 53-70-00 FIG 1A VOL I.
- [SDR FDEA201412054070](https://openairdocs.org/sdr/FDEA201412054070.md): Seat Track · damaged · Dec 5, 2014 · N554FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK STATION 1551 LT 27.50 SEAT TRACK DAMAGED. R & R DAMAGE SEAT TRACK AT STATION 1551 LT 27.50 IAW SRM 53-70-00 VOL I.
- [SDR FDEA201412044061](https://openairdocs.org/sdr/FDEA201412044061.md): Fitting · cracked · Dec 4, 2014 · N554FE · Doug MD1010F · Fuselage Main, Attach Fittings
  > CAC STATION 1156 LT OTBD FRAME AT FLOOR LINE, FRAME FLOORBEAM FITTING CRACKED. REPAIRED FRAME FLOORBEAM FITTING IAW SRM 53-30-00 FIG 7.
- [SDR FDEA201412034053](https://openairdocs.org/sdr/FDEA201412034053.md): Panel · delaminated · Dec 3, 2014 · N554FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING PANEL ARC0446-501 IS DELAMINATED & CORRODED. CUT OUT DAMAGED AREA. REPAIR PANEL ARC0446-501 IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 71-21-02 VOL II.
- [SDR FDEA201412034052](https://openairdocs.org/sdr/FDEA201412034052.md): Panel · delaminated · Dec 3, 2014 · N554FE · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING PANEL ARC0446-502 IS SEPARATING ON CORNERS. REPAIR PANEL ARC0446-502 IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-02 VOL II.
- [SDR FDEA201412013992](https://openairdocs.org/sdr/FDEA201412013992.md): Access Panel · delaminated · Dec 1, 2014 · N554FE · Doug MD1010F · Vertical Stabilizer, Plate/Skin
  > VERTICAL STAB LT SIDE ACCESS PANEL 374EL HAS DELAMINATION. REPAIR DELAMINATION ON PANEL 374EL IAW SRM 51-71-00 VOL II.
- [SDR FDEA201411283963](https://openairdocs.org/sdr/FDEA201411283963.md): Skin · damaged · Nov 28, 2014 · N554FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT WING OTBD FLAP HAD SKIN AT INBD HINGE AREA LOWER SECTION WAVY & CREASED, MARKED DOT 7. REPAIRED FLAP SKIN IAW SRM 57-10-00 FIG 85 SHEET 2.
- [SDR FDEA201411283958](https://openairdocs.org/sdr/FDEA201411283958.md): Skin · dented · Nov 28, 2014 · N554FE · Doug MD1010F · Elevator, Plate/Skin
  > RIGHT INBD ELEVATOR TOP SURFACE HAS MULTIPLE DENTS, APPROX 40 INCHES OTBD OF DETACHABLE ELEVATOR. RIGHT INBD ELEVATOR TOP SURFACE HAS 5 DENTS WITHIN LIMITS & 1 OUT OF LIMITS AT STATION XE 142. REMOVED DAMAGE & INSTALLED DOUBLER AT STATION XE 142 IAW SRM 55-
- [SDR FDEA201411263909](https://openairdocs.org/sdr/FDEA201411263909.md): Skin · damaged · Nov 26, 2014 · N554FE · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING OTBD LAP INBD HINGE PANEL 635AR, PN ARC0794-506, MISSING TOP SKIN 4 INCH X 6 INCH SECTION. REPAIRED MISSING TOP SKIN ON PANEL 635AR IAW SRM 51-71-00 VOL II.
- [SDR FDEA201411253900](https://openairdocs.org/sdr/FDEA201411253900.md): Seat Track · damaged · Nov 25, 2014 · N554FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK STATION 1310 RBL 27.50 SEAT TRACK DAMAGED. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 VOL 1.
- [SDR FDEA201411203822](https://openairdocs.org/sdr/FDEA201411203822.md): Fitting · cracked · Nov 20, 2014 · N554FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > CAC STATION 1156 LT OTBD AT FLOOR LINE, FRAME & FLOORBEAM FITTING CRACKED. FITTING REMOVED AND REPLACED REFERENCE SRM 53-30-00 FIGURE 7 VOLUME 1.
- [SDR FDEA201411203829](https://openairdocs.org/sdr/FDEA201411203829.md): Doubler · cracked · Nov 20, 2014 · N554FE · Doug MD1010F · Fuselage Main, Bulkhead
  > CENTER WW LT FWD CORNER BULKHEAD DOUBLER HAS A CRACK IN THE RADIUS ON THE LOWER END OF THE BRACKET AT BS 1381. REMOVED DAMAGED DOUBLER AND INSTALLED NEW SERVCEABLE DOUBLER IAW DRAWING NEA6078 AND SRM 51-33-01 VOL 2.
- [SDR FDEA201406011247](https://openairdocs.org/sdr/FDEA201406011247.md): Skin · cracked · Jun 1, 2014 · N554FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING NR 12 SLAT TRACK CUT OUT HAS EVIDENCE OF CRACK. LT WING NR 12 SLAT CUT OUT NEEDS NDT VERIFICATION. VERIFIED & MARKED THE END OF THE CRACK WITH HFEC IAW NDT SPM PART 6, 06-00-06. REMOVED FASTENERS FROM NR 12 SLAT TRACK CUT OUT AREA, TO FACILITATE I
- [SDR FDEA201406011244](https://openairdocs.org/sdr/FDEA201406011244.md): Skin · cracked · Jun 1, 2014 · N554FE · Doug MD1010F · Wing, Plate/Skin
  > NUMBER 7 SLAT CUT OUT HAS CRACK INDICATION HAD A 1 INCH BLACK SMOKE LINE. WIPED AWAY, STILL HAS A SLIGHT APPEARANCE OF A CRACK. REMOVED DAMAGED SKIN USING.5" RADIUS IAW SRM 57-10-00 VOLUME 1 FIGURE 68. PERFORMED HFEC OF THE CUT OUT AREA IAW NDT SPM PART 6,
- [SDR FDEA201211063887](https://openairdocs.org/sdr/FDEA201211063887.md): Spar Cap · cracked · Nov 6, 2012 · N554FE · Doug MD1010F · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STAB UPPER SPAR CAP HAS A APPROX 1.50" CRACK EMANATING FROM FROM A PREVIOUS REPAIR AT XFS 88.834. REPAIRED IAW SRM 55-20-00 FIG 8.
- [SDR FDEA201201100070](https://openairdocs.org/sdr/FDEA201201100070.md): Button · inoperative · Jan 10, 2012 · N554FE · Doug MD1010F · Escape Slide
  > DOOR SLIDE TEST BUTTON WILL NOT TEST. REPLACED BATTERIES AND BULBS REF AMM 25-61-01-2-0, OPS CHECKED OK.
- [SDR FDEA201109163901](https://openairdocs.org/sdr/FDEA201109163901.md): Battery · failed · Sep 16, 2011 · N554FE · Doug MD1010F · Emergency Lighting
  > DURING POST FLIGHT FOUND EMERGENCY LIGHT TEST FAILED, WITH EMERGENCY BATTERY 1 LOW ALERT DISPLAYED. R & R EMERGENCY LIGHTS POWER SUPPLY, AS REQUIRED OPS CHECKED GOOD. REF MM 33-51-01-4-0.
- [SDR FDEA201108123252](https://openairdocs.org/sdr/FDEA201108123252.md): Mec · failed · Aug 12, 2011 · N554FE · Doug MD1010F · Fuel Controlling System
  > ON DECENT, NR 3 ENGINE BECAME UNCONTROLLABLE, A/T OFF OR A/T ON, ENGINE SURGE +/- 20 PERCENT ALL INDICATION. ENGINE SHUTDOWN PERFORMED AND WINDMILLED APPROX 20 MINUTES. R & R NR 3 ENGINE CIT SENSOR, REF AMM 73-20-02-2. INSTALLED NR 3 ENGINE MEC AND FUEL PU
- [SDR FDEA201107122645](https://openairdocs.org/sdr/FDEA201107122645.md): Lamp · inoperative · Jul 12, 2011 · N554FE · Doug MD1010F · Escape Slide
  > L1 DOOR DISARMED LIGHT INOP. RELAMPED AS REQUIRED IAW MM 33-00-00-2-0. OPS CHECK GOOD.
- [SDR FDEA201101200311](https://openairdocs.org/sdr/FDEA201101200311.md): Battery · inoperative · Jan 20, 2011 · N554FE · Doug MD1010F · Escape Slide
  > R1 DOOR SLIDE LOW PRESS LIGHT INOP. REPLACED BATTERIES IAW AMM 25-61-03-2-0 AND TESTED IAW AMM 25-61-03-5-0, CKS OK.
- [SDR FDEA201003040644](https://openairdocs.org/sdr/FDEA201003040644.md): Cylinder · overserviced · Mar 4, 2010 · N554FE · Doug MD1010F · Main Landing Gear Strut/Axle/Truck
  > LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. RAN QRH AND STILL UNABLE TO BRING GEAR LEVER TO UP POSITION. BURNED OFF EXCESS FUEL AND LANDED WITHOUT INCIDENT. UNABLE TO MOVE GEAR HANDLE OUT OF DOWN DETENT WITH OR WITHOUT OVERIDE BUTTON. FOUND TRIM CYLINDE
- [SDR FDEA200909053259](https://openairdocs.org/sdr/FDEA200909053259.md): Lead · failed · Sep 5, 2009 · N554FE · Doug MD1010F · Engine Indicating System Wiring
  > ENG 2 EGT HI" LEVEL ONE ALERT DURING DESCENT. EGT WAS 1092 IN RED.MOVED THROTTLE TO IDLE, APPROX 20 SECONDS LATER ALERT CHANGED TO LEVEL 1 "ENG 2 EXCEEDAMCE", TEMP INDICATION DECREASED TO AROUND 900. APPROX 10 SECONDS LATER TEMP INCREASED ABOVE RED LINE W
- [SDR FDEA200807012615](https://openairdocs.org/sdr/FDEA200807012615.md): Smoke Detector · failed · Jul 1, 2008 · N554FE · Doug MD1010F · Smoke Detection
  > AT FL 350 GOT LEVEL 3 LOWER FWD CARGO FIRE FLASHING DISCHARGE SWITCH/FIRE WARNING. DISCHARGED AGENT AND LANDED FIRE CREW FOUND NO FIRE EVIDENCE ON A/C. REMOVED AND REPLACED 4 SMOKE DETECTORS IN LOWER FORWARD CARGO COMPARTMENT.
- [SDR 08FDEA02615](https://openairdocs.org/sdr/08FDEA02615.md): Smoke Detector · false activation · Jul 1, 2008 · N554FE · Doug MD1010F · Smoke Detection
  > AT FL 350 GOT LEVEL 3 LOWER FWD CARGO FIRE FLASHING DISCHARGE SWITCH/FIRE WARNING. DISCHARGED AGENT AND LANDED. FIRE CREW FOUND NO FIRE EVIDENCE ON A/C. R&R 4 SMOKE DETECTORS IN LOWER FORWARD CARGO COMPARTMENT
- [SDR 08FDEA02427](https://openairdocs.org/sdr/08FDEA02427.md): Skin · damaged · Jun 15, 2008 · N554FE · Doug MD1010F · Elevator, Plate/Skin
  > ON MX POST FLIGHT INSP FOUND RT OUTBOARD ELEVATOR DAMAGED. APPEARS TO BE LIGHTNING STRIKE AT OUTBOARD TIP AND TIP TRAILING EDGE OF ELEVATOR ACCOMPLISHED RT OUTBOARD ELEVATOR INSTALLATION STEP NR 3-B ITEM NR 18 AND STEP NR 3-C 1 THRU 9.
- [SDR 07FDEA01681](https://openairdocs.org/sdr/07FDEA01681.md): Keelbeam · cracked · May 2, 2007 · N554FE · Doug DC1010 · Fuselage Main, Keel
  > LT KEEL BEAM WEB AT STA 1501 Z= -40 APPROX FOUND CRACK ON EXISTING REPAIR. REPAIR WEB IAW SRM 53-00-01 FIG 10 VOL 1.
- [SDR 07FDEA01276](https://openairdocs.org/sdr/07FDEA01276.md): Skin · unknown · Apr 3, 2007 · N554FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE STA 475 RT LOWER FUSELAGE CUT OUT NOSE W/W. REPAIRED IAW FEDEX EA8-5310-105639.
- [SDR 07FDEA01271](https://openairdocs.org/sdr/07FDEA01271.md): Pressure Panel · corroded · Apr 3, 2007 · N554FE · Doug DC1010 · Fuselage Main, Bulkhead
  > RT MLG W/W FOUND CORROSION ON PRESSURE PANEL STA 1381 UNDER SLANT PANEL. REPAIRED IAW FEDEX EA 8-5730-103734.
- [SDR 07FDEA01268](https://openairdocs.org/sdr/07FDEA01268.md): Skin · corroded · Apr 3, 2007 · N554FE · Doug DC1010 · Wing, Plate/Skin
  > LT WING LOWER SURFACE NR 40 HEAD FASTENERS ON SKIN FOUND MODERATE CORROSION. REPAIRED IAW FEDEX EA 8-5730-103735.
- [SDR 07FDEA01267](https://openairdocs.org/sdr/07FDEA01267.md): Spar Cap · cracked · Apr 3, 2007 · N554FE · Doug DC1010 · Horizontal Stabilizer, Spar/Rib
  > HORIZONTAL STAB SPAR CAP FOUND CRACK LONG.750" AND.800" REPAIRED IAW FEDEX EA 8-5510-96110.
- [SDR 07FDEA01265](https://openairdocs.org/sdr/07FDEA01265.md): Skin · corroded · Apr 3, 2007 · N554FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > MAIN CABIN CTR WING SECTION UPPER SKIN CORROSION UNDER HEAD OF FASTENERS. REPAIRED IAW FEDEX EA 8-5730-103734.
- [SDR 07FDEA01263](https://openairdocs.org/sdr/07FDEA01263.md): Skin · dented · Apr 3, 2007 · N554FE · Doug DC1010 · Trailing Edge Flaps
  > LT WING INB'D FLAP DENTS ON LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIGURE 4 VOL.1.
- [SDR 07FDEA01262](https://openairdocs.org/sdr/07FDEA01262.md): Skin · corroded · Apr 3, 2007 · N554FE · Doug DC1010 · Wing, Plate/Skin
  > RT WING L/E AT SLAT TRACK HOLE NR 2 FOUND SKIN CORRODED. REPAIRED IAW SRM 57-10-00 FIGURE 68 SHT 1-3 VOL 1.
- [SDR 07FDEA01261](https://openairdocs.org/sdr/07FDEA01261.md): Skin · dented · Apr 3, 2007 · N554FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > LOWER EXT FUSELAGE FOUND DENT 1.5" BY 1" DEPTH 0.050". REPAIRED PER NRC IC02006.
- [SDR 07FDEA01260](https://openairdocs.org/sdr/07FDEA01260.md): Skin · dented · Apr 3, 2007 · N554FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > LWR FUSELAGE EXT SKIN FOUND DEEP DENT 2" BY 2" DEEP 0.07". REPAIRED IAW FEDEX EA 8-5310-96119.
- [SDR 07FDEA01258](https://openairdocs.org/sdr/07FDEA01258.md): Skin · corroded · Apr 3, 2007 · N554FE · Doug DC1010 · Wing, Plate/Skin
  > RT WING L/E AT SLAT TRACK HOLE NR 1 FOUND SKIN EDGE CORRODED AND DISBONDED. REPAIRED SKIN IAW SRM 57-10-00 FIGURE 68 VOL.1 SHT 1-3.
- [SDR 07FDEA01256](https://openairdocs.org/sdr/07FDEA01256.md): Hinge · damaged · Apr 3, 2007 · N554FE · Doug DC1010 · Fuselage, Door Hinge
  > LOWER FWD CARGO DOOR DAMAGE FOUND ON DOOR HINGE FWD HINGE LOBE AND AFT HINGE LOBE OVALIZED AND OUT OF LIMIT (DIA. 0.355"). REPAIRED WITH BUSHING IAW SRM 52-10-00 FIG 8 VOL 1 AND CMM 52-31-03.
- [SDR 07FDEA01255](https://openairdocs.org/sdr/07FDEA01255.md): Structure · corroded · Apr 3, 2007 · N554FE · Doug DC1010 · Wing Miscellaneous Structure
  > RT WING SEVERE CORROSION ON UPPER BEAVER TAIL. REPAIR CORROSION IAW FEDEX EA 8-5710-103714.
- [SDR 07FDEA01254](https://openairdocs.org/sdr/07FDEA01254.md): Slat Track · corroded · Apr 3, 2007 · N554FE · Doug DC1010 · Leading Edge Devices
  > LT WING L/E AT SLAT TRACK HOLE NR 1 FOUND SKIN EDGE CORRODED AND DISBONDED. REPAIR IAW SRM 57-10-00 FIGURE 68 VOL 1 SHT 1-3.
- [SDR 07FDEA00615](https://openairdocs.org/sdr/07FDEA00615.md): Frame · unknown · Feb 28, 2007 · N554FE · Doug DC1010 · Fuselage Main, Frame
  > CAC CIRCUMFERENTIAL FRAME AT STA 1099 BETWEEN STRINGER NR 39 LT TO 45 RT EXISTING FRAME REPAIRS AND REPAIRS CHANNEL IN DIF LOCATIONS. REMOVED OLD REPAIR CHANNEL SPLICE AT L NR 52, CUT CAP FRAME AT L NR 41 R. REMOVED SECTION FRAME BTWN L NR 47 L TO 46 R. R

Next page: https://openairdocs.org/deregistered/N554FE-2024-01-29/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 = 'N554FE' AND deregistration_id = 'N554FE-2024-01-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N554FE-2024-01-29/reports

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