# Service difficulty reports: N321DL, cancelled Feb 26, 2019

A list on [N321DL, cancelled Feb 26, 2019](https://openairdocs.org/deregistered/N321DL-2019-02-26.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 4 · 170 reports

- [SDR NACA2019021200027](https://openairdocs.org/sdr/NACA2019021200027.md): Tee Fitting · cracked · Feb 4, 2019 · N321DL · Boeing 737232 · Nose/Tail Landing Gear
  > NOSE LANDING GEAR - CRACKS FOUND ON SUPPORT STRUCTURE FOR ACTUATOR ATTACH FITTING. REMOVED AND REPLACED TEE ANGLE PN: 65-45819-45 AND GUSSET 65-45819-45, REF BOEING DRAWING 65-45819 AND B737-200 SRM 51-10-1, 51-30-2, 3 AND 5. NDT OPEN HOLES REF NDT MANUAL PAR
- [SDR NACA2018080600066](https://openairdocs.org/sdr/NACA2018080600066.md): Skin · cracked · Aug 6, 2018 · N321DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT STRINGER 16R JUST AFT OF BS 480. A DOUBLER AND TRIPLER WAS INSTALLED IAW SRM, 53-30-03, REPAIR 48, DETAIL VII.
- [SDR NACA2018071800002](https://openairdocs.org/sdr/NACA2018071800002.md): Skin · cracked · Jul 16, 2018 · N321DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > 3 INCH LONG CRACK FOUND IN FUSELAGE SKIN DIRECTLY BELOW S23R AT BS 344. CAT B REPAIR INSTALLED IAW SRM 53-30-3, FIGURE 48, DETAIL XVIII.
- [SDR NACA2018031400001](https://openairdocs.org/sdr/NACA2018031400001.md): Skin · cracked · Mar 12, 2018 · N321DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > SKIN CRACK FOUND ON RIGHT SIDE FUSELAGE S16R AND BS445 (VERIFIED WITH HFEC). DAMAGE REMOVED, DOUBLER INSTALLED REF SRM 53-30-3, FIG 48, REV SEP 2016. DETAIL XI AND III, PROCEDURE VII.
- [SDR NACA2017072000044](https://openairdocs.org/sdr/NACA2017072000044.md): Engine · failed · Jul 18, 2017 · N321DL · Boeing 737232 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FAILED AT 2000 FEET ON TAKEOFF. MI AT 1705 FEET DURING CLIMB, LOUD NOISE FROM NR 2 ENGINE, NO EPR, SMOKE IN COCKPIT, AND ENGINE VIBRATION. NR 2 ENGINE HAD A FAILURE OF MULTIPLE STAGES OF THE TURBINE SECTION. THE ENGINE AND THRUST REVERSER WERE REM
- [SDR NACA2017022700018](https://openairdocs.org/sdr/NACA2017022700018.md): Floorbeam · corroded · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Floor Beam
  > CORROSION ON TOP SURFACE OF FLOORBEAM AT BS 827 LBL 49 - 56. CORROSION BLENDED OUT OF LIMITS IAW SRM 53-10-1, FIG 1, REV 113. REPAIRED THE FLOORBEAM IAW DWG R23093.1-053-023-001, REV NC.
- [SDR NACA2017022700016](https://openairdocs.org/sdr/NACA2017022700016.md): Frame · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Frame
  > CRACKED FRAME AT BS 787, RBL42, STRINGER 13R. REPAIRED IAW SR 4-3658265861, & 8100-9.
- [SDR NACA2017022700012](https://openairdocs.org/sdr/NACA2017022700012.md): Fitting · corroded · Feb 26, 2017 · N321DL · Boeing 737232 · Trailing Edge Flaps
  > RIGHT OUTBOARD FLAP, NR 7 CARRIAGE SUPPORT FITTING CORRODED ON THRUST BEARING SURFACE (IN MID FLAP). REPLACED WITH REPAIRED ASSY.
- [SDR NACA2017022700011](https://openairdocs.org/sdr/NACA2017022700011.md): Spindle · corroded · Feb 26, 2017 · N321DL · Boeing 737232 · Trailing Edge Flaps
  > LEFT OUTBOARD FLAP, NR 1 CARRIAGE SPINDLE CORRODED. THE CARRIAGE WAS REPLACED IAW MM 27-51-81, REV 123.
- [SDR NACA2017022700009](https://openairdocs.org/sdr/NACA2017022700009.md): Flap Track · damaged · Feb 26, 2017 · N321DL · Boeing 737232 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP OUTBOARD TRACK REPAIR BUSHING CAD PLATING DETERIORATED. FLAP TRACK REPLACED IAW AMM 27-51-161, REV 12.
- [SDR NACA2017022700007](https://openairdocs.org/sdr/NACA2017022700007.md): Bulkhead Web · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Bulkhead
  > CRACKED RIVETS ON BS 1016 BULKHEAD WEB BETWEEN STRINGERS 5 - 7L. REPAIRED IAW SRM 113 53-10-4, FIGURE 15.
- [SDR NACA2017022700005](https://openairdocs.org/sdr/NACA2017022700005.md): Intercostal · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > CRACK IN RADIUS OF INTERCOSTAL AT BS 294.5, STRINGER 14R. REPLACED THE INTERCOSTAL IAW SERVICE BULLETIN 737-53A1241 REV 1.
- [SDR NACA2017022700019](https://openairdocs.org/sdr/NACA2017022700019.md): Support Fitting · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Wing, Landing Gear Attach Fittings
  > CRACK FOUND IN RIGHT AFT SUPPORT FITTING FOR MAIN LANDING GEAR AT RSS 224. REPLACED THE SUPPORT FITTING IAW SERVICE BULLETIN 737-57-1216, REV 2, & SR 4-3648350626, AND 8100-9.
- [SDR NACA2017022700017](https://openairdocs.org/sdr/NACA2017022700017.md): Angle · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED AT BS 663, LBL 24.82. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW DWG PL65-45410 REV DD, BSB 737-57A1296, SRM D6-15565 REV 113, AND 51-30-02.
- [SDR NACA2017022700015](https://openairdocs.org/sdr/NACA2017022700015.md): Stringer Clip · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP BS 663, STRINGER 10R, REPLACED THE STRINGER CLIP IAW SRM 51-30-2, REV 113.
- [SDR NACA2017022700014](https://openairdocs.org/sdr/NACA2017022700014.md): Stringer Clip · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP BS 663, STRINGER 10L, WL 256. REPLACED THE STRINGER CLIP IAW SRM 51-30-2 REV 113, & DWG 65-46541 REV H.
- [SDR NACA2017022700013](https://openairdocs.org/sdr/NACA2017022700013.md): Attach Fitting · corroded · Feb 26, 2017 · N321DL · Boeing 737232 · Wing, Control Surface Attach Fittings
  > RIGHT OUTBOARD FLAP, NR 8 TRACK FORWARD ATTACH FITTING (ON WING) HAS EVIDENCE OF CORROSION BETWEEN TRACK ATTACH BUSHINGS. REPLACED THE FWD ATTACH FITTING IAW BAC5047, AMM 20-50-11 REV 123, & DWG 65-45455 REV E.
- [SDR NACA2017022700010](https://openairdocs.org/sdr/NACA2017022700010.md): Flap Track · corroded · Feb 26, 2017 · N321DL · Boeing 737232 · Trailing Edge Flaps
  > LEFT OUTBOARD FLAP NR 1 TRACK CORRODED. REPLACED THE FLAP TRACK IAW AMM 27-51-151, REV 123.
- [SDR NACA2017022700008](https://openairdocs.org/sdr/NACA2017022700008.md): Bulkhead Web · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Bulkhead
  > ONE CRACK ON BS 1016 BULKHEAD WEB AT STRINGER 15R. REPAIREDTHE BULKHEAD WEB IAW SR 4-3633491853, & 8100-9.
- [SDR NACA2017022700006](https://openairdocs.org/sdr/NACA2017022700006.md): Intercostal · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > CRACK IN RADIUS OF INTERCOSTAL BS 277 STRINGER 10R FORWARD OF R1 DOOR. REPLACED INTERCOSTAL ANGLE IAW SERVICE BULLETIN-737-53A1241 REV 1.
- [SDR NACA2017022700003](https://openairdocs.org/sdr/NACA2017022700003.md): Stringer Clip · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT BS 967, STRINGER 22L. REPLACED IAW SRM 51-30-2 REV 113 AND DWG 65-46563 REV -.
- [SDR NACA2017022700002](https://openairdocs.org/sdr/NACA2017022700002.md): Tee Fitting · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CRACKED TEE ON FORWARD CARGO DOOR INTERNAL STRUCTURE AT BS 470. THE TEE WAS REPLACED IAW DWG 65-46921 REV M, AND SRM D6-15565 REV 113 51-30-02.
- [SDR NACA201502260009](https://openairdocs.org/sdr/NACA201502260009.md): Stringer Splice · corroded · Mar 19, 2015 · N321DL · Boeing 737232 · Fuselage Main, Longeron/Stringer
  > DAMAGE FOUND ON STRINGER SPLICE BS907, STR20L IN AFT PIT. DAMAGED STRINGER SPLICE AT BS907, STR20L IN AFT PIT REPLACED IAW SRM 51-10-01, PARA 7, REV 108. INSTALLED IAW SRM 51-30-02, REV 108. CORRODED SECTION OF STRINGER BETWEEN FS887-907 STR20L REPAIRED IAW
- [SDR NACA201502260035](https://openairdocs.org/sdr/NACA201502260035.md): Web · corroded · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > CORROSION AROUND UNDER SIDE OF FASTENER POINTS ALONG DUST SILL AT BS910-944, LBL57-61. REPLACED WEB AT BS 9007-917, LBL 57-66 WITH MADE REPAIR PART REF: DWG 65-52878, SHEET 2, REV C AND INSTALLED IAW SRM 51-30-2, REV 108.
- [SDR NACA2015102260034](https://openairdocs.org/sdr/NACA2015102260034.md): Skin · cracked · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > CRACK IN INTERIOR ACFT SKIN AT LOWER AFT CORNER OF FWD AIRSTAIR DOOR CUTOUT. CRACK WAS REPAIRED IAW SB 53-1058-R4 WHICH CALLS UP DWG 65C20843. AN ALLOWANCE TO TRIM BACK THE MAIN CARGO DOOR DOUBLER WAS RECEIVED FROM SIE UNDER R23093.1-053-016-001, REV NC, REF
- [SDR NACA201502260033](https://openairdocs.org/sdr/NACA201502260033.md): Frame · cracked · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Frame
  > FWD PIT BELTFRAME CRACKED AT BS 500, LBL 1 BETWEEN STR 28L & STR 28R. REPAIRED FWD PIT BELT FRAME AT STA 500, LBL 1 BETWEEN STR 28R - STR 28L WITH NESTED ANGLE REPAIR IAW DWG R23093.1-053-013-001, REV 1 AND DER 8110. REF MCO 3008, WO 1356529
- [SDR NACA201502260032](https://openairdocs.org/sdr/NACA201502260032.md): Frame · corroded · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Frame
  > NOSE WHEEL WELL CORROSION ON FRAME AT BS 277 WHERE FRAME MEETS LOWER CHORD ON RT SIDE. REPAIRED FRAME IN NOSE WHEEL WELL AT STA 277 RT SIDE, REPAIRED IAW DWG R23093, 1-053-012-001, REV NC AND SRM 51-30-02, REV 108 AND DWG 65-45819, SHEET 6, REV T, REFERENCE
- [SDR NACA201502260031](https://openairdocs.org/sdr/NACA201502260031.md): Frame · damaged · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Frame
  > BELTFRAME DAMAGED AT BS 747 BETWEEN STR 16R-STR 17R. PHYSICAL DAMAGE NOTED TO BELT FRAME INBD CHORD AT BS 747, STR 16-17R. REPAIRED & INSTALLED IAW SRM 51-30-02. 8110-3, DWG R23093.1-053-011-001, REV NC, DER REPAIR. REF MCO 3008, WO 1354926.
- [SDR NACA201502260030](https://openairdocs.org/sdr/NACA201502260030.md): Stringer Clip · cracked · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT BS 420, STR 4R. CRACK STRINGER CLIP AT STA 420, STR 4R. REPLACED IAW SRM 51-20-1, FIG 7 AND SRM 51-30-02. MATERIAL ID IAW SRM 51-10-3, REV 108. REFERENCE MCO3008 W/O 1349111.
- [SDR NACA201502260029](https://openairdocs.org/sdr/NACA201502260029.md): Frame · cracked · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Frame
  > AFT PIT INT BS 767, WL 152, LBL 1 FRAME CRACKED. FRAME REPLACED AND INSTALLED IAW SRM 51-30-2, REV 108. AND DWG 65-46549, REV D, REF MCO 3008, WO 1346548.
- [SDR NACA201502260028](https://openairdocs.org/sdr/NACA201502260028.md): Frame · damaged · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Frame
  > HOLE DAMAGE IN BS 1016 FWD OTBD FLANGE BETWEEN STR 20R-21R. REMOVED OLD AFT SKIN REPAIR, DISCOVERED HOLE DAMAGE IN FLANGES AT STA 1009-STA 1016 FORWARD OTBD FLANGES BETWEEN STR 20R-21R. REPAIRED IAW BAC 8100.9, REF ID 201502090005-0003D1 REF MCO 3008, WO 1358
- [SDR NACA201502260027](https://openairdocs.org/sdr/NACA201502260027.md): Stringer · damaged · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Longeron/Stringer
  > AFT PIT AT STR 21R DAMAGED JUST FWD OF BS1016. AFT CARGO PIT STR 21R JUST FORWARD OF STA 1016. REPLACED WITH FABRICATED PART IAW SRM 53-10-2, FIG 9, ITEM 14, REV 108. INSTALLED IAW SRM 51-30-2, REV 108, REF MCO3008, W/O 1358115.
- [SDR NACA201502260026](https://openairdocs.org/sdr/NACA201502260026.md): Stringer · damaged · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Longeron/Stringer
  > AFT PIT STR 20R DAMAGED JUST FWD OF BS1016. REPAIRED AFT CARGO PIT, STR 20R JUST FORWARD OF STA 1016 IAW SRM 53-10-3, FIG 1, REV 108, SRM 51-30-2, REV 108. REF MCO3008, W/O 1358114.
- [SDR NACA201502260025](https://openairdocs.org/sdr/NACA201502260025.md): Strap · cracked · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > STABILIZER STRAP AT BS 328, RBL 30 CRACKED, E & E COMPARTMENT. REPAIRED CRACKED STABILZER STRAP AT STA 328, RBL 30 IAW SRM 53-10-09, FIG 4, REV 108. REPAIRED IAW SRM 51-30-02, REV 108, REFERENCE MCO3008, W/O 1354407.
- [SDR NACA201502260024](https://openairdocs.org/sdr/NACA201502260024.md): Floorbeam · cracked · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Floor Beam
  > FLOORBEAM WEB BS 718, BL 0 FOUND CRACKED 4" AFT OF SB REPAIR. REPLACED CRACKED FLOORBEAM WEB IAW DWG 65-45410, REV H AT STA 718, BL 0, 4" AFT OF SB REPAIR. REFERENCE MCO 3008, W/O 1350149.
- [SDR NACA201502260023](https://openairdocs.org/sdr/NACA201502260023.md): None · none · Feb 26, 2015 · N321DL · Boeing 737232 · Standard Practices/Structures
  > REPLACE PATCHES ON RT STABILIZER L/E WITH FLUSH REPAIR. REPLACED PATCH WITH FLUSH FIT REPAIR, IAW ARM 55-10-3, FIG 2, REV 108. REFERENCE MCO 3008, W/O 1349438.
- [SDR NACA201502260022](https://openairdocs.org/sdr/NACA201502260022.md): Floorbeam · corroded · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Floor Beam
  > CORROSION ON UNDER SIDE & TOP OF FLOORBEAM UPPER CAP AT BS 887, RBL 65-RBL 45. REPAIRED CORRODED FLOOR BEAM CAP AT BS 887, BL45, RIGHT TO BL 65, RIGHT. CUTOUT CORRODED AREA UNDER ANCHOR NUT AND INSTALLED NESTED ANGLE REPAIR. REF MCO 3008, WO 1349316.
- [SDR NACA201502260021](https://openairdocs.org/sdr/NACA201502260021.md): Floorbeam · corroded · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Floor Beam
  > CORROSION ON UPPER CAP OF FLOORBEAM BS 928 BETWEEN RBL 25-RBL 45. CORROSION ON FLOORBEAM AT STA 928 RBL 25-RBL 45. BLENDED, MEASURED AND FOUND TO BE BEYOND LIMITS. REPAIRED TRACK IAW SRM R108, 53-10-5, FIG 2 AND AEI DWG AE4943, REV A, REF MCO 3008, WO 13492
- [SDR NACA201502260020](https://openairdocs.org/sdr/NACA201502260020.md): Floorbeam · corroded · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM BS 480 FLOOR BL 50R-02R. CORRODED FLOORBEAM AT STA 480, RBL 50-RBL62. REPAIRED IAW SRM 53-10-09, FIG 1, REV 108. WITH NESTED ANGLES. INSTALLED IAW SRM 51-30-02, REV 108. REF MCO3008 W/O 1349303.
- [SDR NACA201502260019](https://openairdocs.org/sdr/NACA201502260019.md): Floorbeam · corroded · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT BS 727B BETWEEN BL 0-LBL 25 MAIN CABIN FLOOR AND BS 727B LBL 25-45 AND BS 727B LBL 45-65. CORROSION ON FLOORBEAM AT STA 727B, BL 0 - BL 65 BLENDED AND FOUND TO BE BEYOND LIMITS. REPAIRED WITH NESTED ANGLES IAW SRM R108, 53-10-9, FIG
- [SDR NACA201502260018](https://openairdocs.org/sdr/NACA201502260018.md): Floorbeam · corroded · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM BS 927, LBL 36-42. CORROSION ON FLOORBEAM AT STA 927 AT LBL 25 TO LBL 45 BLENDED, MEASURED AND FOUND TO BE BEYOND LIMITS. REPAIRED IAW SRM R108, 53-10-9, FIG 3. REF MCO 3008, WO 1349194.
- [SDR NACA201502260017](https://openairdocs.org/sdr/NACA201502260017.md): Frame · cracked · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Frame
  > FRAME CRACKED FROM RIVET RUNNING ACROSS RADIUS, APPROXIMATELY 1" LONG AT BS 747, WL 235, BL70L. REPAIRED CRACKED FRAME FROM RIVET RUNNING ACROSS RADIUS AT STA 747, WL 235, BL 70L IAW SRM 53-10-4, FIG 1, REV 108, REF MCO3008, W/O 1349146.
- [SDR NACA201502260016](https://openairdocs.org/sdr/NACA201502260016.md): Stringer Splice · cracked · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Longeron/Stringer
  > CRACK IN STR SPLICE AT BS360 STR 15L. STR SPLICE AT STA 360, STR 15L REPLACED IAW SRM 51-10-01, PARA 7 AND INSTALLED IAW SRM 51-30-02, REV 108. REF MCO3008, W/O 1349110.
- [SDR NACA201502260015](https://openairdocs.org/sdr/NACA201502260015.md): Shear Tie · cracked · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Internal Mounting Structure
  > AFT PIT INT LBL2, WL148 FRAME SHEAR TIE CRACKED AT RIVET HOLE LOCATION. AFT PIT, INT BS927. LBL2, WL148. FRAME SHEAR TIE CRACKED AT RIVET HOLE LOCATION. REPAIRED CRACKED SHEAR TIE FRAME AT CRACKED RIVET HOLE IN AFT PIT INT BS927, LBL2, WL148 IAW SRM 53-10-4
- [SDR NACA201502260014](https://openairdocs.org/sdr/NACA201502260014.md): Floorbeam · corroded · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM MAIN CABIN BS887 BETWEEN LBL25-45 AND 21.5L. CORROSION AT STA 887, LBL 21.5 TO LBL 45 ON FLOORBEAM BLENDED, MEASURED AND FOUND TO BE OUT OF LIMITS. INSERTED REPLACEMENT BEAM CAP SECTION IAW SRM R108, 53-10-9, FIG 3, REF MCO 3008, WO 13
- [SDR NACA201502260013](https://openairdocs.org/sdr/NACA201502260013.md): Frame · cracked · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Frame
  > CRACKED BELT FRAME WEB AT BS277 STR 16R. CRACKED BELT FRAME WEB AT STA 277, STR 16R. REPAIRED IAW SERVICE REQUEST 3-3118662701, DOUBLER REPAIR, AND RADIUS FILLER FABRICATED IAW SRM 53-00-07, REPAIR 15. ACCEPTABLE BY FAA 8100.9 REF MCO3008, W/O 1348553.
- [SDR NACA201502260012](https://openairdocs.org/sdr/NACA201502260012.md): Skin · cracked · Feb 26, 2015 · N321DL · Boeing 737232 · Cargo/Baggage Doors
  > CRACKED LIGHTNING HOLE ON THE INSIDE SKIN ON THE FWD PIT CARGO DOOR AT BS450. BLENDED EDGE DAMAGE AT LIGHTNING HOLE ON THE INSIDE SKIN FWD LOWER CARGO DOOR AT STA 450. REMOVED AND FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01, FIG 1, DETAIL 2, REV 108. REPAIRE
- [SDR NACA201502260011](https://openairdocs.org/sdr/NACA201502260011.md): Frame · cracked · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Frame
  > CRACKED FWD FRAME OF AFT PIT DOOR OPENING BS793 AT LWR STOP NR 1. REMOVED CRACKED FRAME AT BS793, INSTALLED NEW FRAME PN 65-47959-78, INSTALLED ALL AFT CARGO PIT DOOR IAW AMM 52-31-00, PG 401. INSTALLED ALL DOOR STOPS PERFORMED ADJUSTMENT AND FIT CLEARANCE CH
- [SDR NACA201502260010](https://openairdocs.org/sdr/NACA201502260010.md): Stringer Splice · damaged · Feb 26, 2015 · N321DL · Boeing 737232 · Fuselage Main, Longeron/Stringer
  > DAMAGE FOUND ON STRINGER SPLICE BS907, STR19L IN AFT PIT. REPLACED DAMAGED STRINGER SPLICE AT STA 907 STR 19L IAW DWG 65-45777, REV G AND INSTALLED NEW STRINGER SPLICE IAW SRM 51-30-02, REV 108. REF MCO3008, W/O 1347111.
- [SDR NACA201502260008](https://openairdocs.org/sdr/NACA201502260008.md): Structure · cracked · Feb 26, 2015 · N321DL · Boeing 737232 · Service Doors
  > R1 DOOR CRACKED IN LWR AFT CORNER. CRACKED SPLICE IN R1 DOOR REMOVED. INSTALLED NEW SPLICE ON R1 DOOR IN LWR AFT CORNER IAW SRM 51-30-02, REV 108.

Next page: https://openairdocs.org/deregistered/N321DL-2019-02-26/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 = 'N321DL' AND deregistration_id = 'N321DL-2019-02-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N321DL-2019-02-26/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.