# Service difficulty reports: N397FE, cancelled Jan 29, 2024

A list on [N397FE, cancelled Jan 29, 2024](https://openairdocs.org/deregistered/N397FE-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 2 · 78 reports

- [SDR FDEA201408052077](https://openairdocs.org/sdr/FDEA201408052077.md): Skin · cracked · Aug 5, 2014 · N397FE · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING LE IS CRACKED NR 3 SLAT ANTI-ICE DUCT CUT OUT TOP SIDE. BOTH CORNERS REPAIR COMPLIED WITH USING EA 8-5710-T0308474.
- [SDR FDEA201309132206](https://openairdocs.org/sdr/FDEA201309132206.md): Fire Loop · false indication · Sep 13, 2013 · N397FE · Doug MD1010F · Fire Detection
  > NR 2 ENGINE LOOP, A LEVEL 2 ON 10 MILE FINAL. POSSIBLE ENG FIRE. INSPECTED FAN, REVERSER AND TURBINE COWLS AND PERFORMED GVI OF NR 2 ENGINE. NO EVIDENCE OF FIRE OR PNUEMATIC DUCT LEAK. NO EVIDENCE OF DAMAGE TO FIRE LOOPS NOTED. NO EVIDENCE OF FIRE IN TAI
- [SDR FDEA201302120472](https://openairdocs.org/sdr/FDEA201302120472.md): Bulkhead · cracked · Feb 12, 2013 · N397FE · Doug MD1010F · Fuselage Main, Bulkhead
  > INBD BULKHEAD CRACKED 32 INCHES FWD OF BS 1521 AND 3 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED IAW SRM 53-00-01, FIG 10.
- [SDR FDEA201302120470](https://openairdocs.org/sdr/FDEA201302120470.md): Bulkhead · cracked · Feb 12, 2013 · N397FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RT BULKHEAD HAS ONE CRACK 51 INCHES FWD OF BS 1521 AND 31 INCHES UP FROM BELLY SKIN. REPAIRED IAW SRM 53-00-01.
- [SDR FDEA201302120471](https://openairdocs.org/sdr/FDEA201302120471.md): Bulkhead · cracked · Feb 12, 2013 · N397FE · Doug MD1010F · Fuselage Main, Bulkhead
  > INBD BULKHEAD ONE CRACK 14 INCHES AFT OF BS 1381 AND 14 INCHES DOWN FROM UPPER BULKHEAD. CRACK VERIFIED USING HFEC. REPAIRED THE DAMAGED TO THE RT SIDE WHEEL WELL BULKHEAD IAW EA 8-5310-157380.
- [SDR FDEA201302120469](https://openairdocs.org/sdr/FDEA201302120469.md): Bulkhead · cracked · Feb 12, 2013 · N397FE · Doug MD1010F · Fuselage Main, Bulkhead
  > LT BULKHEAD HAS THREE CRACKS 12 INCHES AFT OF BS 1381 AND 3 INCHES DOWN FROM UPPER BULKHEAD, AND ONE IS 13 INCHES AFT BS 1381 AND 3 INCHES DOWN, AND LAST CRACK IS 17 INCHES. AFT BS 1381 AND 3 INCHES DOWN. ALL THREE CRACKS HAVE BEEN VERIFIED USING HFEC. REPA
- [SDR FDEA201302120468](https://openairdocs.org/sdr/FDEA201302120468.md): Bulkhead · cracked · Feb 12, 2013 · N397FE · Doug MD1010F · Fuselage Main, Bulkhead
  > INBD BULKHEAD HAS TWO CRACKS 21 INCHES AFT OF BS 1381 AND 7 AND 9 INCHES DOWN FROM UPPER BULKHEAD. TWO CRACKS VERIFIED USING HFEC. COMPLETED REPAIR OF AREA USING EA 8-5310-157381 AND REPAIR SKETCH 201302130091-001 AS REF.
- [SDR FDEA201301020003](https://openairdocs.org/sdr/FDEA201301020003.md): Angle · corroded · Jan 2, 2013 · N397FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > NR 3 ACM BAY FOUND THE ACA3796-2 TEE ANGLE CORRODED BEYOND LIMIT AT BS 585, LONGERON 47R. R & R TEE ANGLE IAW REF 51-33-00 AND 51-35-01, VOL II.
- [SDR FDEA201212314406](https://openairdocs.org/sdr/FDEA201212314406.md): Tee Fitting · cracked · Dec 31, 2012 · N397FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RT FWD PRESSURE BULKHEAD AT BS 595, RT LONGERON 43, FOUND CRACKED AT THE WEB AND TEE FITTING. SERVICABLE TEE FITTING INSTALLED IAW EA 8-5310-163797.
- [SDR FDEA201204081302](https://openairdocs.org/sdr/FDEA201204081302.md): Cover · broken · Apr 8, 2012 · N397FE · Doug MD1010F · Emergency Lighting
  > R1 DOOR LOWER FWD EXIT LIGHT COVER BROKEN. REPLACED LIGHT COVER. OK FOR SERVICE.
- [SDR FDEA201106262431](https://openairdocs.org/sdr/FDEA201106262431.md): Power Supply · discharged · Jun 26, 2011 · N397FE · Doug MD1010F · Emergency Lighting
  > DURING PREFLIGHT, OBSERVED EMGERENCY LIGHT BATTERY 1 LOW. REPLACED EMERGENCY LIGHTS POWER SUPPLY
- [SDR FDEA201105031704](https://openairdocs.org/sdr/FDEA201105031704.md): Battery · inoperative · May 3, 2011 · N397FE · Doug MD1010F · Emergency Lighting
  > DURING PRE FLIGHT GOT EMERGENCY LIGHT BATTERY LOW ALERT. R & R EMERGENCY LIGHT BATTERY IAW MM 33-51-01-4. OPS CHECKS NORMAL IAW MM 33-51-01-5.
- [SDR FDEA201012204728](https://openairdocs.org/sdr/FDEA201012204728.md): Switch · failed · Dec 20, 2010 · N397FE · Doug MD1010F · Turbine Engine Oil System
  > NR 2 ENG OIL FILTER LEVEL II ALERT. INFLT SHUT DOWN AS PER FLT CREW WITH LEVEL II ALERT, ENG HAD NORMAL OIL PRESSURE. INSPECTED FILTER ELEMENT FOR CLOGGING, ELEMENT FOUND CLEAN AND NOT CLOGGED. INSTALLED NEW FILTER ELEMENT AS PER MM 79, RAN ENG AS PER JRH
- [SDR FDEA200910283716](https://openairdocs.org/sdr/FDEA200910283716.md): Manifold · dirty · Oct 28, 2009 · N397FE · Doug MD1010F · Hydraulic System, Main
  > DURING DESCENT, LVL 1 HYD 3 ELEV OFF-NR3 HYD LEVEL AT 4.5 GALLONS. RAN CHECKLIST SHORTLY FOLLOWED BY HYD 3, QTY LO AND THEN HYD 3 FAIL SGN - REPLACED NR3 ENG HYD SYS MANIFOLD FILTERS IAW AMM 29-12-02-2, NO METAL OR DEBRIS FOUND IN OLD FILTERS. STILL REDQUIRES
- [SDR FDEA200812195245](https://openairdocs.org/sdr/FDEA200812195245.md): Wire · broken · Dec 19, 2008 · N397FE · Doug MD1010F · Engine Fuel System Wiring
  > NR 3 ENGINE HUNG START AT FL 25.0 AND DESCENDED TO 10000 FT STILL WOULD NOT ACCELERATE; SHUT DOWN ENGINE. IDLE READINGS: ENGINE 1 N1 38 PERCENT; EGT 362; N2 71.1 PERCENT, ENGINE 2 N1 39 PERCENT; EGT 362; N2 72.6 - ENGINE 3 N1 29 PERCENT; EGT 372; N2 50.5
- [SDR FDEA200812175189](https://openairdocs.org/sdr/FDEA200812175189.md): Skin · dented · Dec 17, 2008 · N397FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > RT FUSELAGE AT STA 1776 BETWEEN LONGERONS 39R AND 40R THE SKIN IS DENTED. REPAIR SKIN IAW E.A. 8-5330-123532 TITLE (FUSELAGE DENT IN GROSS WEIGHT MOD DOUBLER AT STA 1816, L39R - L40R). REMOVED AND REINSTALLED ACCESS PANELS IN THE PIT IAW SRM 57-31-01; VOL I
- [SDR FDEA200812085106](https://openairdocs.org/sdr/FDEA200812085106.md): Sleeve · dented · Dec 8, 2008 · N397FE · Doug MD1010F · Engine Thrust Reverser
  > NR 2 ENGINE LEFT TRANSLATING COWL OUTER SKIN IS DENTED. REPAIRED NR 2 LEFT TRANSLATING SLEEVE/COWL OUTER SKIN BY DRILLING INJECTED HOLES AND INJECTING EA 934 ADHESIVE AND FILLING THE DENT WITH POTTING COMPOUND AND CURING IAW CF6-6 ENGINE MANUAL 78-00-32; REPA
- [SDR FDEA200811254972](https://openairdocs.org/sdr/FDEA200811254972.md): Solenoid · defective · Nov 25, 2008 · N397FE · Doug MD1010F · Passenger/Crew Doors
  > L-1 DOOR TORQUE TUBE SOLENOID NOT OPERATING PROPERLY. REMOVED AND REPLACED L-1 DOOR TORQUE TUBE SOLENOID AND ADJUSTED. OPS CHECKED GOOD IAW FEDEX MD 10 AMM 52-11-13-2 AND 52-11-00-5.
- [SDR FDEA200811124864](https://openairdocs.org/sdr/FDEA200811124864.md): Skin · gouged · Nov 12, 2008 · N397FE · Doug MD1010F · Leading Edge Devices
  > LT WING INBD SLAT GOUGED OTBD TOP CORNER. REMOVED AND RE-INSTALLED THE LEFT NR 2 SLAT. BLENDED AREA IAW SRM 57-00-01; FIG 1-A; SHEET 3; PG 5; VOL I AND 57-55-01. FABRICATED SKIN AND SPLICE PLATES THEN INSTALLED RTEF SRM 57-10-00; VOL I; FIG 3-1. GAP CHECKS
- [SDR FDEA200811124865](https://openairdocs.org/sdr/FDEA200811124865.md): Spar Cap · cracked · Nov 12, 2008 · N397FE · Doug MD1010F · Wing Spar
  > APPROX 2.75 INCH CRACK EXISTS IN RT WING LOWER SPAR CAP (PSE 57.10.008) AT XORS = 411. CRACK RUNS FROM AFT EDGE OF SPAR CAP AFT TANG, FWD APPROX 1.625 INCH TO RADIUS, THEN UPWARDS AND INBOARD APPROX 1.125 INCH AND TERMINATES AT VERTICAL LEG FASTENER AT APPROX
- [SDR 08FDEA04865](https://openairdocs.org/sdr/08FDEA04865.md): Spar Cap · cracked · Nov 12, 2008 · N397FE · Doug MD1010F · Wing Spar
  > APPROX 2.75 INCH CRACK EXISTS IN RT WING LOWER SPAR CAP (PSE 57.10.008) AT XORS = 411. CRACK RUNS FROM AFT EDGE OF SPAR CAP AFT TANG, FWD APPROX 1.625 INCH TO RADIUS, THEN UPWARDS AND INBOARD APPROX 1.125 INCH AND TERMINATES AT VERTICAL LEG FASTENER AT APPRO
- [SDR FDEA200811044709](https://openairdocs.org/sdr/FDEA200811044709.md): Skin · worn · Nov 4, 2008 · N397FE · Doug MD1010F · Nacelle/Pylon, Plate/Skin
  > AFT NACELLE, FIREWALL SEAL PLANE AT FS Y2166 AND LEFT SIDE OF THE TRAILING EDGE OF THE DIVERTER, HAS WORN SKIN. REPAIR WORN SKIN AREA IAW SRM 51-31-01; VOL II; PG 1; SRM 55-35-04; VOL III AND DWG AJC7415, REV "BK". ALODINED AND PRIMED IAW SRM 51-21-01; VOL
- [SDR 08FDEA04708](https://openairdocs.org/sdr/08FDEA04708.md): Skin · worn · Nov 4, 2008 · N397FE · Doug MD1010F · Nacelle/Pylon, Plate/Skin
  > AFT NACELLE, FIREWALL SEAL PLANE AT FS Y2166 AND RIGHT SIDE OF THE TRAILING EDGE OF THE DIVERTER; HAS WORN SKIN AND IS CRACKED. REMOVED AND FABRICATED NEW SKIN SECTION IAW SRM 51-35-01 VOL II AND DWG AJC7415 REV BK, ALODINED AND PRIMED IAW SRM 51-21-01 VOL I
- [SDR 08FDEA04771](https://openairdocs.org/sdr/08FDEA04771.md): Skin · corroded · Nov 4, 2008 · N397FE · Doug MD1010F · Fuselage Main, Structure
  > CENTER LANDING GEAR WHEEL WELL, FS 1481 TO FS 1501 BETWEEN STR R50 TO L49 HAS CORROSION ON SKIN. REMOVED CORROSION IAW SRM 51-21-01 PG 28 A VOL II. SKIN ORIG THICKNESS 0.125 IAW DWG AYB 7030; REV "E". REMAINING MATERIAL THICKNESS 0.090. MATERIAL REMOVED 0.
- [SDR 08FDEA04770](https://openairdocs.org/sdr/08FDEA04770.md): Skin · corroded · Nov 4, 2008 · N397FE · Doug MD1010F · Fuselage Main, Structure
  > CENTER LANDING GEAR WHEEL WELL, FS 1501 TO FS 1521 AT STR R50 TO L48 HAS CORROSION AND BARE METAL. REMOVED CORROSION IAW SRM 51-21-01 PG. 28 VOL. II. ORIGINAL THICKNESS ON SKIN IS.125 IAW DWG AYB7030 REV E. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 PG. 6
- [SDR 08FDEA04709](https://openairdocs.org/sdr/08FDEA04709.md): Skin · worn · Nov 4, 2008 · N397FE · Doug MD1010F · Nacelle/Pylon, Plate/Skin
  > AFT NACELLE, FIREWALL SEAL PLANE AT FS Y2166 AND LEFT SIDE OF THE TRAILING EDGE OF THE DIVERTER, HAS WORN SKIN.
- [SDR 08FDEA04658](https://openairdocs.org/sdr/08FDEA04658.md): Fitting · corroded · Oct 31, 2008 · N397FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR LOWER JAMB NR 7 FITTING HAS CORROSION IN HOLES "A"; "C" AND "D". REMOVED & REPLACED AFA 7132-1 FITTING & REPAIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00 FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II.
- [SDR 08FDEA04657](https://openairdocs.org/sdr/08FDEA04657.md): Fitting · corroded · Oct 31, 2008 · N397FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR LOWER JAMB NR 6 FITTING HAS CORROSION IN HOLES "A"; "B"; "C" AND "D". REMOVED & REPLACED AFA 7132-1 FITTING & REPAIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00; FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II.
- [SDR 08FDEA04656](https://openairdocs.org/sdr/08FDEA04656.md): Fitting · corroded · Oct 31, 2008 · N397FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR LOWER JAMB NR 5 FITTING HAS CORROSION IN HOLES "C" AND "D". REMOVED & REPLACED AFA 7132-1 FITTING & REPAIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00 FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II.
- [SDR 08FDEA04655](https://openairdocs.org/sdr/08FDEA04655.md): Fitting · corroded · Oct 31, 2008 · N397FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR LOWER JAMB NR 4 FITTING HAS CORROSION IN HOLES "A"; "B" AND "D". REMOVED & REPLACED AFA 7132-1 FITTING & REPAIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00 FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II.
- [SDR 08FDEA04654](https://openairdocs.org/sdr/08FDEA04654.md): Fitting · corroded · Oct 31, 2008 · N397FE · Doug MD1010F · Fuselage Main, Structure
  > MAIN CARGO DOOR LOWER JAMB NR 3 FITTING HAS CORROSION IN HOLES "A" AND "D". REMOVED & REPLACED AFA 7132-1 FITTING & REPAIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00 FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II.
- [SDR 08FDEA04653](https://openairdocs.org/sdr/08FDEA04653.md): Fitting · corroded · Oct 31, 2008 · N397FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR LOWER JAMB NR 2 FITTING HAS CORROSION IN HOLES "B" AND "C". REMOVED & REPLACED AFA 7131-1 FITTING & REPAIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00 FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II.
- [SDR FDEA200810274845](https://openairdocs.org/sdr/FDEA200810274845.md): Structure · corroded · Oct 27, 2008 · N397FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > RT MLG W/W BS 1381 RBL 116 OTBD LOWER CORNER OF SLANT PANEL VERTICAL TEE CAP HAS CORROSION. DISPLACED SLANT PANEL IAW SRM 51-31-01; VOL I. REMOVED 7, REPLACED ANGLE IAW SRM 51-33-01; VOL II AND DWG NR AEA0471; REV "A". FABBED AND INSTALLED NEW ANGLE IAW DAC
- [SDR 08FDEA00289](https://openairdocs.org/sdr/08FDEA00289.md): Wire Harness · out of position · Jan 26, 2008 · N397FE · Doug MD1010F · Landing Gear System Wiring
  > MAIN GEAR WOULD NOT RETRACT ON AFTER TAKEOFF CHECKLIST CYCLED GEAR AS PER QRH GEAR WENT DOWN 3 GREEN BUT MAIN GEAR STILL WOULD NOT RETRACT CONFIG PAGE CONFIRMED ALL THE ABOVE. FOUND LEFT AND RIGHT UPLATCH SENSOR WIRE HARNESS INTERFERING WITH TRAVEL OF LINK A
- [SDR 08FDEA00291](https://openairdocs.org/sdr/08FDEA00291.md): Wire Harness · out of position · Jan 26, 2008 · N397FE · Doug MD1010F · Landing Gear System Wiring
  > MAIN GEAR WOULD NOT RETRACT ON AFTER TAKEOFF CHECKLIST CYCLED GEAR AS PER QRH GEAR WENT DOWN 3 GREEN BUT MAIN GEAR STILL WOULD NOT RETRACT CONFIG PAGE CONFIRMED ALL THE ABOVE. FOUND LEFT AND RIGHT UPLATCH SENSOR WIRE HARNESS INTERFERING WITH TRAVEL OF LINK A
- [SDR 07FDEA01813](https://openairdocs.org/sdr/07FDEA01813.md): Skin · cracked · May 15, 2007 · N397FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > MODIFICATION AND REPAIR ASSESSMENT ON 13 APRIL 2007, DURING PNEUMATIC TESTS WITH AIR, AT 9:30 A.M. THE PRESSURIZED AIR FLEXIBLE HOSE COLLAPSED CAUSING THE END CONNECTING TO THE HANGAR UNDERFLOOR MANIFOLD TO HIT THE LOWER FUSELAGE JUST FWD OF C.A.C. THE IMPA
- [SDR 07FDEA01730](https://openairdocs.org/sdr/07FDEA01730.md): Skin · dented · May 9, 2007 · N397FE · Doug DC1010 · Horizontal Stabilizer, Plate/Skin
  > ACF MODIFICATION AND REPAIR ASSESSMENT HORIZONTAL STABILIZER LT SIDE DENTS, NICKS, DEFORMATION RIB AND SKIN AND 10 EA RIVETS LOOSE ON LOWER SKIN B/T STA 48.500 TO STA XE 67.225 AND STA XE 88.625 TO STA XE 100.455. REMOVED DETACHABLE ELEVATOR, REMOVED LWR
- [SDR 07FDEA01729](https://openairdocs.org/sdr/07FDEA01729.md): Shear Tie · corroded · May 9, 2007 · N397FE · Doug DC1010 · Fuselage Internal Mounting Structure
  > MD 10-10 ACF MODIFICATION AND REPAIR ASSESSMENT AFT CARGO COMPARTMENT: MISSING MATERIAL AND CORROSION ON SHEAR CLIP STA 1956 B/T L 48 TO L 50 LT SIDE REMOVED CLIPS ATTACHING FOR ACCESS: REMOVED INTERCOSTAL AND RIVETS, CUT OUT SHEAR CLIP DAMAGED, CLEANED EXCESS
- [SDR 07FDEA01728](https://openairdocs.org/sdr/07FDEA01728.md): Longeron · damaged · May 9, 2007 · N397FE · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > ACF MODIFICATION AND REPAIR ASSESSMENT\AFT CARGO COMPT TUNNEL SIDE RT: STA 1801-1821 NICK ON THE LONGERON 27 PERFORMED BLEND-OUT AND CHECK LIMITS IAW SRM 53-00-01 FIG 1 B. INSTALLED ANGLE AND EXISTING STRAP IAW SRM 53-00-01 FIG 7 AND SRM 51-33-01 VOL. II. PR
- [SDR 07FDEA01727](https://openairdocs.org/sdr/07FDEA01727.md): Longeron · cracked · May 9, 2007 · N397FE · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > ACF MODIFICATION AND REPAIR ASSESSMENT LT MLG WHEEL WELL: AT STA 1510, AT X = 30 FOUND LONG WITH CRACK THE 1 INCH ACCOMPLISHED CRACK STOP DRILL 1/4 '' DIA AND REPAIRED LONGERON IAW SRM 53-00-01 FIG 9 VOL I.
- [SDR 07FDEA01724](https://openairdocs.org/sdr/07FDEA01724.md): Skin · cracked · May 9, 2007 · N397FE · Doug DC1010 · Wing, Plate/Skin
  > MD 10-10 ACF MODIFICATION AND REPAIR ASSESTMENT RT WING LEADING EDGE STA XORS 506 LOWER SIDE CLOSE TO PANEL FUEL PANEL, SKIN WITH CRACK OF ABOUT 2 INCH REMOVED ACCESS DOOR, REPAIRED FIXED L.E IAW SRM 57-10-00 FIG 68 SHEETS 2 AND 3. INSTALLED ACCESS DOOR.
- [SDR 07FDEA01633](https://openairdocs.org/sdr/07FDEA01633.md): Frame · corroded · Apr 26, 2007 · N397FE · Doug DC1010 · Fuselage Main, Frame
  > MD 10-10 ACF MODIFICATION AND REPAIR ASSESSMENT AFT FUSE WASTE TANK COMPT STA 1996 RT SIDE TO L 47 FROM L 50 REPAIR EXISTING WITH LIGHT CORROSION. PERFORMED REPAIR WITH NRC NR 1202.
- [SDR 07FDEA01632](https://openairdocs.org/sdr/07FDEA01632.md): Frame · corroded · Apr 26, 2007 · N397FE · Doug DC1010 · Fuselage Main, Frame
  > ACF MODIFICATION AND REPAIR ASSESSMENT AFT FUSE WASTE TANK COMPT STA 1996 LT SIDE TO L. 50 FROM L. 52 REPAIR EXISTING WITH LIGHT CORROSION. REMOVED EXISTING REPAIR, PERFORMED INSPECTION, CUP ANGLE B/T L46 AND L48 RT SIDE AND B/T L 48 TO L 50 LT SIDE IAW SRM 5
- [SDR 07FDEA01585](https://openairdocs.org/sdr/07FDEA01585.md): Door Frame · cracked · Apr 24, 2007 · N397FE · Doug DC1010 · Fuselage Main, Structure
  > MODIFICATION AND REPAIR ASSESSMENT R3 DOOR ON JAMB STA 1305 SIDE LOWER FOUND WEB WITH EXISTING REPAIR REMOVED EXISTING REPAIR NOT IN COMPLIANCE WITH SRM 53-50-00 FIG 19.
- [SDR 07FDEA01580](https://openairdocs.org/sdr/07FDEA01580.md): Skin · cracked · Apr 24, 2007 · N397FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > MODIFICATION AND REPAIR ASSESTMENT RT WING INBOARD AILERON FRONT SPAR WITH EXISTING REPAIR STA XIA 372 TO 374 REMOVED DOUBLER (EXISTING REPAIR), FOUND CRACKS. REMOVED AILERON RT INBOARD. REPAIRED SKIN DOUBLER. INSTALLED FILLER AND COVER IAW MM 20-50-02. I
- [SDR 07FDEA01574](https://openairdocs.org/sdr/07FDEA01574.md): Skin · damaged · Apr 24, 2007 · N397FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > MODIFICATION AND REPAIR ASSESSMENT RT WING DROP LEADING EDGE WITH WORN AND MISSING MATERIAL ON EXISTING REPAIR. REMOVED INNER SKIN AND EXISTING REPAIR IAW SRM 51-31-01 VOL II. REPAIR DOUBLER, INSTALLED IAW SRM 57-10-00 FIG 55 VOL I. REINSTALLED HINGE, FW
- [SDR 07FDEA01518](https://openairdocs.org/sdr/07FDEA01518.md): Skin · corroded · Apr 16, 2007 · N397FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > DURING MD10-10 ACF MODIFICATION AND REPAIR ASSESSMENT PROG EXISTING REPAIR ON SKIN STA 1039 RT SIDE BETWEEN L 50 TO L 51. REMOVED EXISTING REPAIR IAW SRM 51-35-01 VOL II. CUT DAMAGED SKIN AND REMOVED CORROSION. PERFORMED CHECK LIMITS AND TREATED IAW SRM 51
- [SDR 07FDEA01512](https://openairdocs.org/sdr/07FDEA01512.md): Skin · damaged · Apr 16, 2007 · N397FE · Doug DC1010 · Trailing Edge Flaps
  > DURING MD10-10 ACF MODIFICATION AND REPAIR ASSESSMENT RT WING INBOARD FLAP UPPER SIDE WITH EXISTING REPAIR STA XIFH 219.550 REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 85.
- [SDR 07FDEA01510](https://openairdocs.org/sdr/07FDEA01510.md): Skin · misrepaired · Apr 16, 2007 · N397FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > DURING MD10-10 ACF MODIFICATION AND REPAIR ASSESMENT PROG EXITING REPAIR ON EXTERNAL SKIN STA 603 TO STA 617 RT SIDE BETWEEN L 43 TO L 45. REMOVED OLD REPAIR (BECAUSE IS NOT COMPLIANCE WITH SRM 53-20-00 FIG 6) AND INSTALLED NEW REPAIR IAW SRM 53-20-00 FIG
- [SDR 07FDEA01504](https://openairdocs.org/sdr/07FDEA01504.md): Skin · dented · Apr 16, 2007 · N397FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > DURING MD10-10 ACF MODIFICATION FOUND 3 DENTS ON EXTERNAL SKIN BETWEEN STA 1797 TO 1804 RT SIDE LONGERON 29 TO LONGERON 30, DENT 0.32" BY 2" BY 1" STA 1802 TO 1804, DENT 0.32" BY 1" BY.050" STA 1801, DENT 0.32" 1.80" BY 1" STA 1797 TO 1799. PERFORMED REPAIR

Next page: https://openairdocs.org/deregistered/N397FE-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 = 'N397FE' AND deregistration_id = 'N397FE-2024-01-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N397FE-2024-01-29/reports

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