# Service difficulty reports: N372FE, cancelled Feb 1, 2024

A list on [N372FE, cancelled Feb 1, 2024](https://openairdocs.org/deregistered/N372FE-2024-02-01.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 5 · 224 reports

- [SDR FDEA201804261124](https://openairdocs.org/sdr/FDEA201804261124.md): Seal · dirty · Apr 26, 2018 · N372FE · Doug MD1010F · Passenger/Crew Doors
  > L1 DOOR SEAL NOISY DURING CLIMB. CLEANED L1 DOOR SEAL AND DOOR THREASHOLD OF DIRTY AND DEBRIS.
- [SDR FDEA201803200740](https://openairdocs.org/sdr/FDEA201803200740.md): Engine · failed · Mar 20, 2018 · N372FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > ENG FAILURE NR 1 ENG CLIMBING THRU 5K. YAW, LOUD BANG RAPIDLY RISING EGT. ENG EXCEEDANCE 942 DEG. THROTTLE TRIMMED POSITIONED TO IDLE. ENG SHUT DOWN. FIRE BOTTLE DISCHARGED. REPLACED NR 1 ENGINE.
- [SDR FDEA201708232299](https://openairdocs.org/sdr/FDEA201708232299.md): Clamp · leaking · Aug 23, 2017 · N372FE · Doug MD1010F · Pneumatic Indicating System
  > AIR MANIFOLD NR 2 FAILED. AFTER TAKEOFF. AIR TURN BACK. REMOVED & REPLACED CLAMP ON DUCT ASSY IN LEFT WHEEL WELL IAW MM 36-14-02-4. NO LEAKS NOTED. PERFORMED DECAY CHECK WITH APU IAW 36-00-01-5 AND GAINED 4 SECONDS. TIME IS NOW WELL WITHIN LIMITS AT 22 SEC
- [SDR FDEA201708222297](https://openairdocs.org/sdr/FDEA201708222297.md): Clamp · failed · Aug 22, 2017 · N372FE · Doug MD1010F · Pneumatic Distribution System
  > AIR MANF NR 2 FAIL. AFTER TAKEOFF. AIR TURN BACK. R&R CLAMP ASSY PER MM 36-14-02-4 IN LEFT WHEEL WELL JUST FWD OF BULKHEAD.
- [SDR FDEA201708162286](https://openairdocs.org/sdr/FDEA201708162286.md): Skin · gouged · Aug 16, 2017 · N372FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > FOUND GOUGED ON LOWER BELLY NEAR BS 1721, LONGERON 47L. REPAIRED THE SKIN IAW SRM 53-20-00, FIG 6.
- [SDR FDEA201708162285](https://openairdocs.org/sdr/FDEA201708162285.md): Skin · cracked · Aug 16, 2017 · N372FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > FOUND CRACK ON FUSELAGE JUST AFT OF CTR CARGO DOOR AROUND BS 1801 AND STRINGER 45L. REPAIRED THE SKIN IAW SRM 53-20-00, FIG 6.
- [SDR FDEA201704261270](https://openairdocs.org/sdr/FDEA201704261270.md): Fire Loop · failed · Apr 26, 2017 · N372FE · Doug MD1010F · Fire Detection
  > DURING CLIMBOUT RECEIVED A LEVEL 2 ALERT FOR THE NR 1 ENGINE FIRE LOOP B AND TOOK THE APROPRIATE QRH ACTIONS (NO FIRE). TROUBLESHOT THE FIRE LOOP AND FOUND HIGH RESISTANCE TO GROUND. ALL OTHER 'B' LOOPS AND AIRCRAFT WIRING CHECK CLEAN. REMOVED AND REPLAC
- [SDR FDEA201606282172](https://openairdocs.org/sdr/FDEA201606282172.md): Stiffener · cracked · Jun 28, 2016 · N372FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > LEFT GEAR WELL OTBD SIDE TO FLAP WELL BULKHEAD, LOWER GUSSET REPAIR IS CRACKED AND RIVETS SHEARED. REMOVED EXISTING REPAIR AND TRIMMED OUT CRACKED AREA. FABRICATED NEW PARTS FOR REPAIR REF SRM 53-00-01, FIG 4 AND 8. INSTALLED REPAIR IAW SRM 53-00-01, VOL 1,
- [SDR FDEA201606272157](https://openairdocs.org/sdr/FDEA201606272157.md): Skin · cracked · Jun 27, 2016 · N372FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT WING OTBD FLAP UPPER SURFACE CRACKED SKIN AT APPROXIMATELY XOFH 548, DEFECTIVE. INSTALLED DOUBLER AND FILLER IAW SRM 57-00-01, FIG 4, VOL 1. CLEANED AND PAINTED LT WING OTBD FLAP UPPER SURFACE IAW SRM 51-21-02, VOL 2.
- [SDR FDEA201606242146](https://openairdocs.org/sdr/FDEA201606242146.md): Access Panel · delaminated · Jun 24, 2016 · N372FE · Doug MD1010F · Wing, Plate/Skin
  > RIGHT T/E ACCESS PANEL 641NB IS DELAMINATED IN MANY SPOTS. MARKED IN RED CIRCLES, REPAIRED RT T/E PANEL 641NB IAW SRM 51-71-00, VOL II.
- [SDR FDEA201606232131](https://openairdocs.org/sdr/FDEA201606232131.md): Seat Track · damaged · Jun 23, 2016 · N372FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK IS DAMAGED AT STA 630, RBL 8. REMOVED DAMAGED SECTION OF SEAT TRACK FROM STA 605-645, RBL 8. INSTALLED SEAT TRACK SPLICE REPAIR REF SRM 53-70-00, FIG 1.
- [SDR FDEA201606222112](https://openairdocs.org/sdr/FDEA201606222112.md): Access Door · delaminated · Jun 22, 2016 · N372FE · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING LOWER ACCESS DOOR, PN ARC0286-2, 641AB DELAMINATION. REPAIRED RT WING LOWER ACCESS DOOR ARC0286-2 IAW SRM 51-71-00, VOL NR 2.
- [SDR FDEA201606172034](https://openairdocs.org/sdr/FDEA201606172034.md): Fitting · cracked · Jun 17, 2016 · N372FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > STA 1159, RT SIDE CORNER. HAIRPIN FITTING CRACKED FROM UPPER INBD AFT FASTENER TO EDGE, 2016-06-17. REPAIRED FITTING AT BS 1159, RT SIDE IN REF TO SRM 53-30-00, VOL 1, FIG 7, A SHEET 1.
- [SDR FDEA201606152017](https://openairdocs.org/sdr/FDEA201606152017.md): Support Angle · cracked · Jun 15, 2016 · N372FE · Doug MD1010F · Service Doors
  > R-1 DOOR SUPPORT ANGLE CRACKED ON UPPER FWD CORNER OF DOOR, ABOVE NR 8 BEAM, MARKED DOT 1, 2016-06-15. REMOVED SUPPORT ANGLE FROM R-1 DOOR, INSTALLED THE NEW PART.
- [SDR FDEA201606142044](https://openairdocs.org/sdr/FDEA201606142044.md): Panel · delaminated · Jun 14, 2016 · N372FE · Doug MD1010F · Nacelle/Pylon, Plate/Skin
  > NR 2 ENGINE PICKLE BARREL PANEL 364JR HAS DELAMINATED AT UPPER CENTER TOP SURFACE PANEL 364JR. REPAIRED DELAMINATION IAW SRM 51-71-00, VOL NR 2.
- [SDR FDEA201606142043](https://openairdocs.org/sdr/FDEA201606142043.md): Skin Panel · damaged · Jun 14, 2016 · N372FE · Doug MD1010F · Nacelle/Pylon, Plate/Skin
  > RIGHT NR 2 ENGINE INLET DUCT PANEL 364JR, EXTERNAL SKIN HAS 1 LIGHTNING STRIKE REPAIRED AREA ON PANEL 364JR IAW SRM 51-71-00, VOL NR 2.
- [SDR FDEA201606111949](https://openairdocs.org/sdr/FDEA201606111949.md): Stiffener · cracked · Jun 11, 2016 · N372FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RIGHT ACM COMPARTMENT, STA 595 BULKHEAD, HORIZONTAL STIFFENER, 3RD FROM BOTTOM, OTBD EDGE IS CRACKED. FABRICATED NEW STIFFENER NCA6044-58 IN REF TO DWG NCA6044.
- [SDR FDEA201606101941](https://openairdocs.org/sdr/FDEA201606101941.md): Skin · damaged · Jun 10, 2016 · N372FE · Doug MD1010F · Nacelle/Pylon, Plate/Skin
  > NR 2 ENGINE RT FAN COWL LANDING HAS DAMAGE ON THE SKIN AT THE FWD END AT APPROXIMATELY 5:30 POSITION. REMOVED AND REPLACED DAMAGED SKIN IN REF TO SRMN 54-10-00 FIG 20, SHT 4.
- [SDR FDEA201606091910](https://openairdocs.org/sdr/FDEA201606091910.md): Doubler · cracked · Jun 9, 2016 · N372FE · Doug MD1010F · Vertical Stabilizer Miscellaneous Structure
  > LEFT LOWER VERTICAL AT FUSELAGE DRAG ANGLE REPAIR DOUBLER CRACKED. MARKED AT NR 2 BANJO FITTING 2016-06-09. REMOVED CRACKED ANGLE. INSTALLED NEW ANGLE IN REF TO SRM 55-20-00, FIG 3.
- [SDR FDEA201606081895](https://openairdocs.org/sdr/FDEA201606081895.md): Frame · cracked · Jun 8, 2016 · N372FE · Doug MD1010F · Fuselage Main, Frame
  > RIGHT NR 3 ACM COMPARTMENT, BS 555, APPROXIMATELY LONGERON 38, CRACKED FRAME. INSTALLED FABRICATED DOUBLER IN NR 3 ACM COMPARTMENT, STA 555 AT APPROXIMATELY LONGERON 38, REF SRM 53-00-01, VOL 1 AND SRM 51-33-01, VOL 2.
- [SDR FDEA201606081893](https://openairdocs.org/sdr/FDEA201606081893.md): Cap · cracked · Jun 8, 2016 · N372FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RIGHT BS 595 BULKHEAD TEE CAP VERTICAL LEG UPPER FASTENER HOLE AT LONGERON 39R HAS A CRACK INDICATION.
- [SDR FDEA201606081892](https://openairdocs.org/sdr/FDEA201606081892.md): Bulkhead · cracked · Jun 8, 2016 · N372FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RIGHT BS 595 BULKHEAD WEB LOWER FASTENER HOLE COMMON TO THE TEE CAP HAS A CRACK INDICATION.
- [SDR FDEA201606081875](https://openairdocs.org/sdr/FDEA201606081875.md): Floorbeam · corroded · Jun 8, 2016 · N372FE · Doug MD1010F · Fuselage Main, Floor Beam
  > FORWARD CARGO COMPARTMENT BILGE SPACE, THERE ARE 2 AREAS OF CORROSION ALONG A LATERAL FLOORBEAM UPPER ANGLE UNDER 2 DIFFRENT ROLLER TRAYS AT AFT SIDE OF THE BS 879, FLOOR FRAME APPROXIMATE LBL 18 & LBL 30. FABRICATED ANGLE IAW DWG RAM1429.
- [SDR FDEA201606071869](https://openairdocs.org/sdr/FDEA201606071869.md): Fitting · cracked · Jun 7, 2016 · N372FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > CAC STA 1159, RT SIDE CORNER, HAIRPIN FITTING CRACKED FROM UPPER INBD AFT FASTENER TO EDGE. REPAIRED FITTING AT BS 1159 IAW SRM 53-30-00, VOL 1, FIG 7, SHEET 1, 2.
- [SDR FDEA201606051852](https://openairdocs.org/sdr/FDEA201606051852.md): Tee Fitting · cracked · Jun 5, 2016 · N372FE · Doug MD1010F · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL LE, CTR INBD SECTION APPEARS TO BE CRACKED AT UPPER T. REMOVED & INSTALLED NEW T CAP. PN ALC7052-19, IAW DWG ALC7052 & SRM 51-31-00 VOL 2.
- [SDR FDEA201606041813](https://openairdocs.org/sdr/FDEA201606041813.md): Floorbeam · cracked · Jun 4, 2016 · N372FE · Doug MD1010F · Fuselage Main, Floor Beam
  > MAIN CABIN CTR WING AREA, FLOORBEAM CRACKED AT STATION 1259, RBL 107, BELOW OTBD SEAT TRACK AREA. INSTALLED SR10530081 -15,-17,-19,-21, &-23 IAW DWG SR10530081.
- [SDR FDEA201606041811](https://openairdocs.org/sdr/FDEA201606041811.md): Floorbeam · cracked · Jun 4, 2016 · N372FE · Doug MD1010F · Fuselage Main, Floor Beam
  > MAIN CABIN CTR WING AREA, FLOORBEAM CRACKED AT STATION 1293, RBL 107, BELOW OTBD SEAT TRACK. REMOVED DAMAGED SECTION OF FLOORBEAM AND REPLACED WITH KIT SB10530172-5 AND SR10530081-7009.
- [SDR FDEA201606041810](https://openairdocs.org/sdr/FDEA201606041810.md): Floorbeam · cracked · Jun 4, 2016 · N372FE · Doug MD1010F · Fuselage Main, Floor Beam
  > MAIN CABIN CTR WING AREA, FLOORBEAM CRACKED AT STATION 1259, LBL 107, AT OVERWING DOOR FWD FRAME AREA. REMOVED SECTION OF CRACKED FLOORBEAM AND REPLACED SECTION WITH KIT SB10530172-5 IAW SR10530081-7009.
- [SDR FDEA201606031807](https://openairdocs.org/sdr/FDEA201606031807.md): Bulkhead · cracked · Jun 3, 2016 · N372FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RIGHT STATION 595 BULKHEAD, LONGERON 38R, T CAP AFT LEG HAS CRACK INDICATION FROM RADIUS TO END OF LEG SECTION. CRACK LOCATED 1.75" BELOW LONGERON 38R. R & R SECTION OF CRACKED TEE CAP FROM LONGERON 36R TO 44R AT STA 595, PN ACA7016-501 IN REF TO DWG SR10530
- [SDR FDEA201606011782](https://openairdocs.org/sdr/FDEA201606011782.md): Intercostal · cracked · Jun 1, 2016 · N372FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AIR CYCLE MACHINE COMPARTMENT NR 3, AT STATION 548, HAS A CRACKED INTERCOSTAL. STOP DRILLED CRACK, NDT VERIFIED NO CRACK BEYOND STOP DRILL AND INSTALLED REPAIR ANGLE TO RESTORE STRUCTURAL INTEGRITY IN REF TO SRM 53-00-01, FIG 8, VOL 1.
- [SDR FDEA201606011781](https://openairdocs.org/sdr/FDEA201606011781.md): Fitting · cracked · Jun 1, 2016 · N372FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > BS 1159 RT SIDE CORNER, HAIR PIN FITTING CRACKED, FROM UPPER INBD AFT FASTENER TO EDGE.
- [SDR FDEA201605311794](https://openairdocs.org/sdr/FDEA201605311794.md): Skin · punctured · May 31, 2016 · N372FE · Doug MD1010F · Main Landing Gear
  > SMALL PUNCTURE IN THE CTR OF MLG DOOR. REPAIRED IAW SRM 51-71-00 VOL 2.
- [SDR FDEA201605282178](https://openairdocs.org/sdr/FDEA201605282178.md): Angle · corroded · May 28, 2016 · N372FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT, BILGE AT STA 879, ANGLE ON AFT SIDE OF FRAME CORRODED LBL4-LBL40. REPAIRED ANGLE IAW DWG RAM 1429.
- [SDR FDEA201605271747](https://openairdocs.org/sdr/FDEA201605271747.md): Seat Track · damaged · May 27, 2016 · N372FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK AT STATION 1381, LBL 75 IS DAMAGED & GOUGED. SEAT TRACK DAMAGED BEYOND LIMITS. R & R SECTION FROM STATION 1371 - 1391 IAW SRM 53-70-00 FIG 1 VOL 1.
- [SDR FDEA201605201689](https://openairdocs.org/sdr/FDEA201605201689.md): Floorbeam · corroded · May 20, 2016 · N372FE · Doug MD1010F · Fuselage Main, Floor Beam
  > FORWARD CARGO COMPARTMENT BILGE SPACE, THERE IS A LATERAL FLOORBEAM SUPPORT THAT IS CORRODED AT STATION 1059, NEAR BL 0. REMOVED AND REPLACED FLOOR SUPPORT BEAM IN REF TO SRM 51-35-01 VOL 2.
- [SDR FDEA201605201704](https://openairdocs.org/sdr/FDEA201605201704.md): Longeron · cracked · May 20, 2016 · N372FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > AFT EMPENNAGE UPPER AFT FUSELAGE COMPARTMENT, STATION 2030 - 2038 LT 7TH LONGERON HAS 8 CRACKS UPPER & LOWER AREAS, TRANSITIONING THRU 2033 BULKHEAD DOT 6 ZONE 311 & 312 2016 05 20. R & R LONGERON 10L FROM STA 2007-STA 2038 IAW SRM 53-10-00, FIG 3, SHT 1 TH
- [SDR FDEA201605201703](https://openairdocs.org/sdr/FDEA201605201703.md): Longeron · cracked · May 20, 2016 · N372FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > AFT EMPENNAGE UPPER AFT FUSELAGE COMPARTMENT, STATION 2027 - 2037 RT 8TH LONGERON HAS 10 CRACKS UPPER & LOWER AREAS, TRANSITIONING THRU 2033 BULKHEAD DOT 5 ZONE 311 & 312 2016 05 20. R & R 8TH LONGERON STA 2007-2037. RT AFT UPPER EMPENNAGE COMPARTMENT IAW SR
- [SDR FDEA201605201702](https://openairdocs.org/sdr/FDEA201605201702.md): Longeron · cracked · May 20, 2016 · N372FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > AFT EMPENNAGE UPPER AFT FUSELAGE COMPARTMENT, STATION 2031 - 2035 RT 6TH LONGERON HAS 4 CRACKS UPPER & LOWER AREAS, TRANSITIONING THRU 2033 BULKHEAD DOT NR 4 ZONE 311 & 312 2016 05 20. R & R SECTION OF LONGERON IN REF TO SRM 53-10-00, FIG 3, VOL 1.
- [SDR FDEA201605201701](https://openairdocs.org/sdr/FDEA201605201701.md): Floorbeam · corroded · May 20, 2016 · N372FE · Doug MD1010F · Fuselage Main, Floor Beam
  > FORWARD CARGO COMPARTMENT, STATION 735, BETWEEN BL 0 - LBL 30, HAS A LATERAL FRAME FLOOR SUPPORT BEAM ANGLE THAT IS CORRODED 2016 05 20. REMOVED MINOR CORROSION ON FLOOR SUPPORT, BETWEEN BL 0 & LBL 30 IAW SRM 51-21-01 VOL 2.
- [SDR FDEA201605201700](https://openairdocs.org/sdr/FDEA201605201700.md): Longeron · cracked · May 20, 2016 · N372FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > AFT EMPENNAGE UPPER AFT FUSELAGE COMPARTMENT, STATION 2031- 2035 RT 5TH LONGERON HAS 4 CRACKS UPPER & LOWER AREAS, TRANSITIONING THRU 2033 BULKHEAD DOT NR 3 ZONE 311 & 312 2016 05 20. R & R SECTION OF LONGERON AT BS 2031 GOING THROUGH THE 2033 BULKHEAD TO STA
- [SDR FDEA201605201699](https://openairdocs.org/sdr/FDEA201605201699.md): Floor Support · corroded · May 20, 2016 · N372FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT AT STATION 791, BETWEEN BL 0 - LBL 30, A LATERAL BEAM FLOOR SUPPORT ANGLE HAS CORROSION 2016 05 20. R & R FLOOR SUPPORT ANGLE AT STA 791, BL-0 TO LBL 30 IN REF TO SRM 51-35-01, VOL 2.
- [SDR FDEA201605201698](https://openairdocs.org/sdr/FDEA201605201698.md): Longeron · cracked · May 20, 2016 · N372FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > AFT EMPENNAGE UPPER AFT FUSELAGE COMPARTMENT, STATION 2030 - 2039 RT 4TH LONGERON HAS 9 CRACKS UPPER & LOWER AREAS, TRANSITIONING THRU 2033 BULKHEAD DOT NR 2 ZONE 311 & 312 2016 05 20. R & R SECTION OF LONGERON FROM BS 2030 TO STA, GOING THROUGH THE 2033 BULK
- [SDR FDEA201605201697](https://openairdocs.org/sdr/FDEA201605201697.md): Longeron · cracked · May 20, 2016 · N372FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > AFT EMPENNAGE UPPER AFT FUSELAGE COMPARTMENT, STATION 2030 - 2036 RT 3RD LONGERON HAS 6 CRACKS UPPER & LOWER AREAS, TRANSITIONING THRU 2033 BULKHEAD DOT 1 ZONE 311 & 312 2016 05 20. R & R SECTION OF LONGERON FROM STA 2031 TO STA 20335 THAT GOES THROUGH THE 2
- [SDR FDEA201605201696](https://openairdocs.org/sdr/FDEA201605201696.md): Roller Tray · corroded · May 20, 2016 · N372FE · Doug MD1010F · Cargo Compartments
  > FORWARD CARGO COMPARTMENT, ROLLER TRAY HAS CORROSION ON A LT FLOOR SUPPORT TANG, BETWEEN STATION 755 - 808 AT BL 0. REMOVED CORRODED ROLLER TRAY AND REPLACED WITH NEW ROLLER TRAY.
- [SDR FDEA201605201695](https://openairdocs.org/sdr/FDEA201605201695.md): Floor Support · corroded · May 20, 2016 · N372FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT, BILGE AT STATION 879 FRAME FLOOR SUPPORT ANGLE, BETWEEN LONGERON 52 & LBL 24 IS CORRODED. R & R FLOOR SUPPORT IN REF TO SRM 51-31-01, VOL 2.
- [SDR FDEA201605201691](https://openairdocs.org/sdr/FDEA201605201691.md): Frame · corroded · May 20, 2016 · N372FE · Doug MD1010F · Fuselage Main, Frame
  > FORWARD CARGO COMPARTMENT, BILGE AT STATION 879, AFT SIDE OF FRAME AT RBL 36, HAS CORROSION UNDER ROLLER TRAY. REMOVED CORROSION FROM ANGLE, TREATED AND PRIMED IN REF TO SRM 51-21-01, VOL 2.
- [SDR FDEA201605121540](https://openairdocs.org/sdr/FDEA201605121540.md): Tee Fitting · cracked · May 12, 2016 · N372FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RIGHT STATION 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43R, HAS A 2 INCH CRACK. REPAIRED THE 595 BULKHEAD AT LONGERON 43R BY SPLICING IN A NEW SECTION OF TEE CHORD IN REF TO SR DWG SR10530081 AND EA 8-5310-T0325736, PN OF THE TEE CHORD IS ACA7016-501.
- [SDR FDEA201605121539](https://openairdocs.org/sdr/FDEA201605121539.md): Tee Fitting · cracked · May 12, 2016 · N372FE · Doug MD1010F · Fuselage Main, Bulkhead
  > LEFT STATION 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 39L HAS A 2 INCH CRACK. R & R SECTION OF TEE CAP FROM LONGERON 36L TO 40L AT STA 595 WITH PN ACA7016-1 IN REF TO DWG SR10530064 AND EA 8-5310-T0325366.
- [SDR FDEA201605121538](https://openairdocs.org/sdr/FDEA201605121538.md): Tee Fitting · cracked · May 12, 2016 · N372FE · Doug MD1010F · Fuselage Main, Bulkhead
  > LEFT STATION 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 36L, HAS A 2 INCH CRACK. R & R SECTION OF TEE CAP FROM LONGERON 36L TO 40L AT STA 595 WITH PN ACA7016-1 IN REF TO DWG SR10530064 AND EA 8-5310-T0325366.
- [SDR FDEA201512043907](https://openairdocs.org/sdr/FDEA201512043907.md): Trim Panel · out of position · Dec 4, 2015 · N372FE · Doug MD1010F · Passenger/Crew Doors
  > ON LANDING ROLL OUT, HAD THE CABIN DOOR 1L APPEAR. AFTER COMING TO A STOP ON THE TAXIWAY, INSPECTED DOOR & ALL WAS NORMAL, EXCEPT FOR ARMED TAB FOR GIRT BAR WENT OUT AFTER HOOKING UP TO THE TUG. INSPECTED THE ARMED TAB FOR GIRT BAR & FOUND THE WHITE DECORAT

Next page: https://openairdocs.org/deregistered/N372FE-2024-02-01/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 = 'N372FE' AND deregistration_id = 'N372FE-2024-02-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N372FE-2024-02-01/reports

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