# Service difficulty reports: N372NW

A list on [N372NW](https://openairdocs.org/aircraft/N372NW.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 · 143 reports

- [SDR DALA2026101905706](https://openairdocs.org/sdr/DALA2026101905706.md): Battery · faulted · Oct 16, 2026 · N372NW · Airbus A320212 · Emergency Lighting
  > EPSU INT LOAD FWD L MESSAGE WHILE WORKING WORKCARD 2562-4001. R & R 10WL EPSU BATTERY PER AMM 33-51. OPS AND BITE CKS GOOD. OK FOR SVC. (LP: 9143598, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026082004764](https://openairdocs.org/sdr/DALA2026082004764.md): Oxygen Mask · leaking · Aug 19, 2026 · N372NW · Airbus A320212 · Crew Oxygen System
  > CAPT 02 MASK BOX LEAKING. REPLACED CAPT O2 MASK BOX PER A320 AMM 35-12 ALL CKS OK. (LP: 9155501, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026073004395](https://openairdocs.org/sdr/DALA2026073004395.md): Priority Valve · leaking · Jul 29, 2026 · N372NW · Airbus A320212 · Hydraulic System, Main
  > HYD - DUE TO GREEN HYDRAULIC SYSTEM PRESSURE AND QUANTITY LOSS, HYD G RSVR LO LVL AND HYD G SYS LO PR. FOUND PRIORITY VALVE ON PTU LEAKING, REPLACED SAME. (LP: 8898723, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026053103298](https://openairdocs.org/sdr/DALA2026053103298.md): Filter · odor · May 29, 2026 · N372NW · Airbus A320212 · Air Distribution System
  > WITH INOP APU AND NO JET BRIDGE AIR,UTILIZING HUFFER TO RUN PACKS. FUMEES BEGAN IN CABIN. SECURED PACKS AND HUFFER CART. R/R RECIRC FILTERS AND #2 RECIRC FAN PER A320 AMM 21-21. NO FURTHER SCENT NOTED. (LP: 8668980, AIRCRAFT WAS GROUNDED)
- [SDR DALA2025111108223](https://openairdocs.org/sdr/DALA2025111108223.md): Radome · delaminated · Nov 10, 2025 · N372NW · Airbus A320212 · Aerodynamic Fairings
  > DURING BIRDSTRIKE INSPECTION FOUD DELAMINATION & BUBBLE ON THE INSIDE OF RADOME NOSE. REMOVED NOSE RADOME IAW AMM 53-15. INSTALLED RADOME IAW AMM 53-15-11. OK FOR SVC. (LP: 7726841)
- [SDR DALA2025111108222](https://openairdocs.org/sdr/DALA2025111108222.md): Antenna · corroded · Nov 10, 2025 · N372NW · Airbus A320212 · Weather Radar System
  > SHIP 3272 DISC: DURING BIRD STRIKE INSPECTION, FOUND CORROSION DMG ON WEATHER RADAR ANTENNA. R & R WEATHER RADAR ANTENNA ASSEMBLY PER AMM 34-41. OPS CHKD. PERFORMED SYS TEST PER A320 AMM 34-41-00-730 -001-A. OPS CHECK GOOD. NO FAULTS, ACFT OK FOR SVC. (LP: 77
- [SDR DALA2025091906883](https://openairdocs.org/sdr/DALA2025091906883.md): Plenum · damaged · Sep 18, 2025 · N372NW · Airbus A320212 · Cabin Cooling System
  > DIVERTED TO DTW DUE TO LEFT PACK ON MEL AND RIGHT PACK STOPPED WORKING. FOUND PACK NR 2 PLENUM DAMAGED, HEAT EXCHANGER AND FLANGE ON REHEATER CRACKED, AND PACK COMPRESSOR OVERHEAT SENSOR SHOWING AMBER XX. REPLACED PLENUM, HEAT EXCHANGER, REHEATER, AND ELECTRI
- [SDR DALA2025062504772](https://openairdocs.org/sdr/DALA2025062504772.md): Unknown · odor · Jun 25, 2025 · N372NW · Airbus A320212 · Air Distribution System
  > SHIP 3272, INFLIGHT BOTH COCKPIT & CABIN EXPERIENCED STRONG ODOR. PILOTS SMELLED A CHEMICAL CLEANER TYPE SMELL. F/A'S REPORTED " ELECTRICAL" SMELL. CARGO COMP INLET TEMP WAS 160 SO WE COOLED IT DOWN. SMELL IMPROVED BUT DID NOT COMPLETELY DISAPEAR. REF LOG #
- [SDR DALA2025061904601](https://openairdocs.org/sdr/DALA2025061904601.md): Light · malfunctioned · Jun 16, 2025 · N372NW · Airbus A320212 · Emergency Lighting
  > SHIP 3272 DISC: FA STATED EMER EXIT LIGHT ABOVE 1L DOOR FLICKERED INTERMITTENTLY DURING CRUISE. C/A: PERFORMED OPS CHK OF L1 OPS CHK GOOD COULD NOT DUPLICATE. (LP: 7395906)
- [SDR DALA2025060304237](https://openairdocs.org/sdr/DALA2025060304237.md): Light · inoperative · Jun 1, 2025 · N372NW · Airbus A320212 · Emergency Lighting
  > SHIP 3272 DISC: ROW 14, 15, 16, 17 SEAT MOUNTED FLOOR EMERGENCY LIGHTS INOP. C/A: R/R EPSU 12WL BATTERY IAW 320 AMM 33-51. NO FIX. REINSTALLED ORIGINAL. SWAPPED EPSU 11WL AND 12WL IAW 320 AMM 33-51. NO FIX. FOUND BROKEN WIRE UNDER SEAT 14 DEF AFTER CANNON PLUG
- [SDR DALA2025041102803](https://openairdocs.org/sdr/DALA2025041102803.md): Oxygen Box · open · Apr 8, 2025 · N372NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 3272 DISC: CREW REPORTED O2 DOOR IN AFT GALLEY CAME OPEN ON LANDING. C/A: DEFER AFT CENTER GALLEY O2 STORAGE DOOR TO MEL 35-21-01D. O2 BOTTLE AVAILABLE FOR CREW, INSTALLED PLACARD INSTALLED, M PROCEDURE C/W, A/C OK TO CONTINUE ON MEL. RESECURED LOOSE RUB
- [SDR DALA2025032202151](https://openairdocs.org/sdr/DALA2025032202151.md): Battery Pack · inoperative · Mar 17, 2025 · N372NW · Airbus A320212 · Emergency Lighting
  > SHIP 3272 DISC: OVER WINDOW EXIT SIGN ON ABC SIDE DOES NOT ILLUMINATE. C/A: T/S PER A320 TSM 33-51-00. FOUND EPSU AT LEFT OVERWING LOCATION BAD. REMOVED EPSU IAW A320 AMM 33-51-38 WIP (557633). R&R EPSU AND BATTERY IAW A320 AMM 33-51 OPS CKS NORMAL A/C OK. (LP
- [SDR DALA2025030301595](https://openairdocs.org/sdr/DALA2025030301595.md): Cids · malfunctioned · Mar 1, 2025 · N372NW · Airbus A320212 · Emergency Lighting
  > SHIP 3272 DISC: EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS:603 / MYCABIN TEXT: FRC256001603 BOTH AC LEFT WINDOW EXIT AND CEILING EMERGENCY EXIT SIGNS ARE NOT ILLUMINATED. ON GROUND IN BDL AC POWER CYCLED AND SIGNS ILLUMINATED AND THEN WENT OFF ABOUT 10 MIN L
- [SDR DALA2025020700956](https://openairdocs.org/sdr/DALA2025020700956.md): Cids · malfunctioned · Feb 6, 2025 · N372NW · Airbus A320212 · Emergency Lighting
  > SHIP 3272 DISC: OVERHEAD EXIT LIGHT INOP (AUTO FUNCTION). C/A: RESET CIDS SYSTEM. ALL OPS NORMAL. (LP: 5659729)
- [SDR DALA2024101610120](https://openairdocs.org/sdr/DALA2024101610120.md): Unknown · odor · Oct 13, 2024 · N372NW · Airbus A320212 · Air Distribution System
  > SHIP 3272 DISC: STRONG ROTTEN EGGS SMELL DURING TAXI IN COCKPIT AND FWD GALLEY. C/A: RAN APU WITH BLEED AND OPERATED PACKS INDIVIDUALLY AND SIMULTANEOUSLY THROUGH FULL RANGE. NO PRESENCE OF ODOR THROUGHOUT OPS CK. PER CARD 0550-2002 STEP 18. TYPE 10 (C) THE CA
- [SDR DALA2024071207057](https://openairdocs.org/sdr/DALA2024071207057.md): Oxygen Mask · unsecure · Jul 6, 2024 · N372NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 3272 DISC: O2 MASK ROW 32 HANGING DOWN. C/A: TOWED OXY MASKS AT ROW 32ABC AS REQUIRED PER A320 AMM 35-21. NO DEFECTS NOTED, PANEL SECURED. (LP: 5913548)
- [SDR DALA2024040203980](https://openairdocs.org/sdr/DALA2024040203980.md): Bushing · migrated · Mar 28, 2024 · N372NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > SHIP 3272 DISC: MIGRATED BUSH ON LOWER LATERAL SUPPORT FITTING LH ON RACK 80VU ( ADDITI ONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT). C/A: ER/A 615614-14AD REV. ORIGINAL COMPLIED WITH. (LP: 0266382)
- [SDR DALA2024040203978](https://openairdocs.org/sdr/DALA2024040203978.md): Skin · damaged · Mar 28, 2024 · N372NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > SHIP 3272 DISC: OVERSIZE HOLES 1 THRU HOLE 19 AND HOLES A TO D (23E/A) FOUND GREATHER THAN MINIMUM STARTING HOLE DIAMETERS AS PER TABLE 2 OF THE CARD 5311- 1246-03B LOC ON JOGGLE AREA FR16 RH AT FWD GALLEY AREA. COMPLIED WITH ER/A 571448-14AD, REV. A (LP: 026
- [SDR DALA2024040203977](https://openairdocs.org/sdr/DALA2024040203977.md): Fitting · cracked · Mar 28, 2024 · N372NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 3272 DISC: CRACK INDICATION FOUND ON CONTINUITY FITTING LH SIDE. CRACK L= 0.200 I NCH. CRACK DIRECTION VERTICAL. AD 2020-17-03/ WORKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FU RTHER FLIGHT. C/A: REF. ER/A 615
- [SDR DALA2024040203976](https://openairdocs.org/sdr/DALA2024040203976.md): Frame · cracked · Mar 24, 2024 · N372NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3272 DISC: *DTE*AT H2CK (OCT2018) FR16 RHS WAS REPLACED DUE TO CRACKS FOUND PER 5311-2016 (ALI 531153). DURING CURRENT M2, EM 5311-01246 WAS ACCOMPLISHED. C/A: ***DTE REQUIRED*** PER SECTION DTE-II THE REPAIR OF SECTION II IS LIMITED TO 32,100 FC FROM SEC
- [SDR DALA2024040203975](https://openairdocs.org/sdr/DALA2024040203975.md): Frame · cracked · Mar 24, 2024 · N372NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3272 DISC: DTE*AT H2CK (OCT2018) FR16 RHS WAS REPLACED DUE TO CRACKS FOUND PER 5311-2016 (ALI 531153). DURING CURRENT M2, EM 5311-01246 WAS ACCOMPLISHED. C/A: ***DTE REQUIRED*** PER SECTION DTE-I OF 571448-14 REV A, FR16 RH FRAME REPLACEMENT ACCOMPLISHED
- [SDR DALA2024032603765](https://openairdocs.org/sdr/DALA2024032603765.md): Stringer · damaged · Mar 23, 2024 · N372NW · Airbus A320212 · Fuselage Main, Longeron/Stringer
  > SHIP 3272 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 42R LOCATED FROM FR55 TO FR56 IN AFT CARGO COMPARTMENT. C/A: CONFIRMED DT EVALUATION FOR FCS REPAIR ON STRINGER 42R LOCATED FROM FR55 TO FR56 IN AFT CARGO COMPARTMENT AND FOUND MEETS THE GE
- [SDR DALA2024032603764](https://openairdocs.org/sdr/DALA2024032603764.md): Stringer · damaged · Mar 23, 2024 · N372NW · Airbus A320212 · Fuselage Main, Longeron/Stringer
  > CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 42L LOCATED FRO M FR55 TO FR58 IN AFT CARGO COMPARTMENT. C/A: PERFORMED PERMANENT REPAIR ON STRINGER 42L LOC BTW FR55 TO FR58 IN AFT CARGO COMPARTMENT AS PER A320 SRM 53-00-13-300-001 AND MASTER ER/A 57583
- [SDR DALA2024032503717](https://openairdocs.org/sdr/DALA2024032503717.md): None · none · Mar 23, 2024 · N372NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3272 DISC: ONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR TRAILING EDGE EXTERNAL SKIN LOCATED BETWEEN RIB10 TO RIB 11 ON LH WING ( REFERENCE AA CARD 5100-01821-02). C/A: CONFIRMED DT EVALUATION FOR FCS REPAIR ON TRAILING EDGE EXTERNAL SKIN LOCATED BETWEEN R
- [SDR DALA2024032503716](https://openairdocs.org/sdr/DALA2024032503716.md): None · none · Mar 23, 2024 · N372NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3272 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BETWEEN FR55 TO FR56 AND FROM STR43R TO STR41R LOWER FUSELAGE (REFERENCE AA CARD 5100-01821-01A). C/A: CONFIRMED DT EVALUATION FOR FCS REPAIR ON EXTERNAL SKIN LOCATED BETWEEN F
- [SDR DALA2024032503715](https://openairdocs.org/sdr/DALA2024032503715.md): Stringer · unknown · Mar 23, 2024 · N372NW · Airbus A320212 · Fuselage Main, Longeron/Stringer
  > SHIP 3272 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 42L LOCATED FROM FR55 TO FR58 IN AFT CARGO COMPARTMENT (REFERENCE AA CARD 5100-01821-01A). C/A: PERFORMED PERMANENT REPAIR ON STRINGER 42L LOC BTW FR55 TO FR58 IN AFT CARGO COMPARTMENT AS P
- [SDR DALA2024032503714](https://openairdocs.org/sdr/DALA2024032503714.md): Stringer · unknown · Mar 23, 2024 · N372NW · Airbus A320212 · Fuselage Main, Longeron/Stringer
  > SHIP 3272 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 43L LOCATED FROM FR55 TO FR58 IN AFT CARGO COMPARTMENT (REFERENCE AA CARD 5100-01821-01A). C/A: PERFORMED PERMANENT REPAIR ON STRINGER 43L LOC BTW FR55 TO FOR 58 IN AFT CARGO COMPARTMENT AS
- [SDR DALA2024032003523](https://openairdocs.org/sdr/DALA2024032003523.md): Skin · corroded · Mar 17, 2024 · N372NW · Airbus A320212 · Wing, Plate/Skin
  > CORROSION TRAILING EDGE UPPER SKIN LOWER SURFACE OVERHANG LOCATED FROM RIB7 TO RIB9 ON LH WING. COMPLIED WITH ER/A 589793-14AD REV. B MATCHES WITH ALL STEPS ON ER/A 589793-14AD REV B PRI REV 0 AND REV. 1 IT IS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS TRA
- [SDR DALA2024032003522](https://openairdocs.org/sdr/DALA2024032003522.md): Profile · cracked · Mar 17, 2024 · N372NW · Airbus A320212 · Emergency Exits
  > SHIP 3272 DISC: CRACK FWD LOAD TRANSMITTING PROFIL LOC INTERNAL AREA EMERGENCY EXIT DOOR 843 PASSENGER CABIN (SSI 522102-01-2). C/A: COMPLIED WITH ER/A 615483-14AD, REV. ORIGINAL MATCHES WITH ALL STEPS ON ER/A 615483-14AD, REV. ORIGINAL PRI REV 0, 1 AND 2. IT
- [SDR DALA2024030402924](https://openairdocs.org/sdr/DALA2024030402924.md): Nut · corroded · Mar 1, 2024 · N372NW · Airbus A320212 · Rudder Structure
  > SHIP 3272 DISC: CORROSION ON BEARING NUT OF RUDDER HINGE 6 VERTICAL STABILIZER. C/A: REPLACED BEARING RUDDER HINGE 6 AS PER A320 FAM AMM 55-46-11- 000-001-A AND AS PER AMM 55-46-11-400-001-A TOOL USED:TORQUE P/N:QD2R100A S/N: 0615057290 D/D: 30-JAN-25 TORQUE A
- [SDR DALA2024030402921](https://openairdocs.org/sdr/DALA2024030402921.md): Seat Track · corroded · Mar 1, 2024 · N372NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3272 DISC: CORROSION FLOOR BEAM +Y1225 LOCATED FROM FR66 TO FR68 AFT GALLEY AREA (SSI: 534147). C/A: REPLACED FLOOR BEAM Y1225 AND SPLICES (4EA) LOC. FR 66 TO FR 68 AFT GALLEY AREA AS PER A320 SRM 51-42-11 AND SRM 51-72-11. DWG D53472000. ISSUE: AF. RELEA
- [SDR DALA2024030402920](https://openairdocs.org/sdr/DALA2024030402920.md): Seat Track · corroded · Feb 29, 2024 · N372NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3272 DISC: CORROSION SEAT TRACK +Y1292 LOCATED FROM FR64 TO FR66 AT AFT GALLEY AREA (SSI: 534147). C/A: REPLACED FLOOR BEAM Y1292 AND SPLICES (2EA) LOC. FR 64 TO FR 66 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11 AND SRM 51-72-11 AND DWG 10N01474. REV. A.
- [SDR DALA2024030402919](https://openairdocs.org/sdr/DALA2024030402919.md): Seat Track · corroded · Feb 29, 2024 · N372NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3272 DISC: CORROSION SEAT TRACK +Y765 LOCATED FROM FR64 TO FR66 AT AFT GALLEY AREA (SSI: 534147). C/A: REPLACED FLOOR BEAM Y765,AND SPLICE OB 4(E/A) FASTENERS LOCATED BTW FR64 TO FR66 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11 AND SRM 51-72- 11 AND DWG:
- [SDR DALA2024030402918](https://openairdocs.org/sdr/DALA2024030402918.md): Seat Track · corroded · Feb 29, 2024 · N372NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3272 DISC: CORROSION FLOOR BEAM -Y765 AND FR68 AT AFT GALLEY AREA (SSI: 534147). C/A: REPLACED FLOOR BEAM -Y765 FROM FR 67 TO FR 70 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11 AND SRM 51-72-11 DWG D53472815 RELEASE DATE 24 JUN 98 ISSUE E. TOOK MEASURE OF
- [SDR DALA2024030402917](https://openairdocs.org/sdr/DALA2024030402917.md): Shear Tie · corroded · Feb 29, 2024 · N372NW · Airbus A320212 · Fuselage Internal Mounting Structure
  > SHIP 3272 DISC: AAI FINDING-EVIDENCE OF CORROSION ON SHEAR TIE LOCATED FROM FR32 TO FR34 AND BTW STR 39R TO STR43RFWD CARGO COMPARTMENT 8EA. C/A: REPLACED SHEAR TIES LOCATED FROM FR32 TO FR34 AND BTW STR 39R TO STR43RFWD CARGO COMPARTMENT 8EA AS PER A320 SRM 5
- [SDR DALA2024022502578](https://openairdocs.org/sdr/DALA2024022502578.md): Floor Support · corroded · Feb 24, 2024 · N372NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > SHIP 3272 DISC: CORROSION FLOOR BEAM +Y765 FROM FR66 TO FR70 AT AFT GALLEY AREA (SSI: 534147). C/A: INSTALLED HARD POINT (2EA), SPLICE (2EA) AS PER A320 SRM 51-42- 11, AND DWG D53472092, ISSUE: N, RELEASE DATE: 24-FEB-15, DWG D53472780, ISSUE: K, RELEASE DATE:
- [SDR DALA2024022502577](https://openairdocs.org/sdr/DALA2024022502577.md): Seat Track · corroded · Feb 24, 2024 · N372NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3272 DISC: CORROSION SEAT TRACK -Y765 LOCATED AT LEVEL FR20 AT FWD GALLEY AREA (SSI: 531189). C/A: REPLACED SEAT TRACK -Y765 LOCATED FR12 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11 AND A320 SRM 51-42-11, DWG D53112812007, ISSUE: E00 RELEASED DATE
- [SDR DALA2024022502570](https://openairdocs.org/sdr/DALA2024022502570.md): Seat Track · corroded · Feb 22, 2024 · N372NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3272 DISC: CORROSION SEAT TRACK -Y1292 LOCATED AT LEVEL FR20 AT FWD GALLEY AREA (SSI: 531189). C/A: REPLACED SEAT TRACK -Y1292 LOCATED FR12 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11 AND A320 SRM 51-42-11, DWG D53112812, ISSUE: E00 RELEASED DATE:
- [SDR DALA2024022202466](https://openairdocs.org/sdr/DALA2024022202466.md): Floorbeam · corroded · Feb 21, 2024 · N372NW · Airbus A320212 · Fuselage Main, Floor Beam
  > SHIP 3272 DISC: CORROSION FLOOR BEAM +Y1162.5 FROM FR68 TO FR69 AFT GALLEY AREA (SSI: 534147). C/A: REPLACED FLOOR BEAM Y1162.5 FROM FR68 TO FR69 AFT GALLEY AREA AS PER A320 SRM 51-72-11, SRM 51-42-11, AND DWG D53478311 ISSUE: C, RELEASE DATE: 15-JAN-99. TOOK
- [SDR DALA2024022202465](https://openairdocs.org/sdr/DALA2024022202465.md): Support Web · cracked · Feb 21, 2024 · N372NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > SHIP 3272 DISC: CRACK ON FALSE FRAME SUPPORT WEB LOC ON FR1 FWD SKIN PANEL AREA. C/A: REPLACED FALSE FRAME SUPPORT WEB LOC ON FR1 FWD SKIN PANEL AREA AS PER A320 SRM 51-42-11 AND DRAWING D53113050 ISSUE AC0 RELEASE DATE 08-JAN -24. MEASURES OF CRACK L: 0.500 I
- [SDR DALA2024022202464](https://openairdocs.org/sdr/DALA2024022202464.md): Floorbeam · corroded · Feb 21, 2024 · N372NW · Airbus A320212 · Fuselage Main, Floor Beam
  > SHIP 3272 DISC: CORROSION FLOOR BEAM -Y464.8 AND FR68 AT AFT GALLEY AREA (SSI: 534147). C/A: REPLACED FLOOR BEAM LOCATED -Y464.8 AND BTW FR 67 TO FR 70 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11 AND DWG D53472780 ISSUE K RELEASE DATE 26-APR-18. MEASURES OF CO
- [SDR DALA2024022102453](https://openairdocs.org/sdr/DALA2024022102453.md): Skin · dented · Feb 19, 2024 · N372NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > SHIP 3272 DISC: DENT EXTERNAL SKIN LOCATED FROM FR57 TO FR58 BETWEEN STR26 AND STR27 LH SIDE LOWER FUSELAGE. C/A: EVALUATED DENT LOCATED ON EXTERNAL SKIN FROM FR57 TO FR58 BETWEEN STR26 AND STR27 LH SIDE LOWER FUSELAGE AND FOUND WITHIN LIMITS AS PER A320 SRM 5
- [SDR DALA2024022102365](https://openairdocs.org/sdr/DALA2024022102365.md): Skin · dented · Feb 19, 2024 · N372NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > SHIP 3272 DISC: DENT EXTERNAL SKIN LOCATED FR52 TO FR53 AND BETWEEN STR26L TO STR27L LOWER FUSELAGE. C/A: EVALUATED DENT LOCATED ON EXTERNAL SKIN FR52 TO FR53 AND BETWEEN STR26L TO STR27L LOWER FUSELAGE AND FOUND WITHIN LIMITS AS PERA320 SRM 53-00-11-283-005 P
- [SDR DALA2024022102364](https://openairdocs.org/sdr/DALA2024022102364.md): Support · corroded · Feb 19, 2024 · N372NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > SHIP 3272 DISC: CORROSION LOWER SILL AT LEVEL FR68 AND AT LEVEL STR 23LH AFT GALLEY AREA (SSI: 534147). C/A: PERFORMED PERMANENT REPAIR ON LOWER SILL LOC ON FRAME 68 AT LEVEL STRINGER 23LH AS PER A320 SRM 53-41-14-300-001, TOOK MEASURES OF CORROSION AREA WERE
- [SDR DALA2024022102363](https://openairdocs.org/sdr/DALA2024022102363.md): Floor Support · corroded · Feb 19, 2024 · N372NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > SHIP 3272 DISC: CORROSION FLOOR SUPPORT -Y1225 LOCATED FROM FR67 TO FR68 AFT GALLEY AREA (SSI: 534147. C/A: REPLACED FLOOR BEAM -Y1225 LOCATED FROM FR67 TO FR68 AFT GALLEY AREA AS PER A320 SRM 51-72-11 AND DRAWING D53472780 RELEASE DATE 26-APR-18 ISSUE K. MEAS
- [SDR DALA2024020901761](https://openairdocs.org/sdr/DALA2024020901761.md): Web · corroded · Feb 8, 2024 · N372NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > SHIP 3272 DISC: CORROSION ON WEB LOC BTW FR 69 TO FR 70 AT LEVEL STR 23R AFT GALLEY AREA. C/A: REPLACED WEB LOC BTW FR 69 TO FR 70 AT LEVEL STR 23R IN AFT GALLEY AREA AS PER A320 SRM 51-42-11 AND DWG D53474180, RELEASE DATE 14-JUL-22, ISSUE Z AND FASTENERS. TO
- [SDR DALA2024020901760](https://openairdocs.org/sdr/DALA2024020901760.md): Web · corroded · Feb 8, 2024 · N372NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > SHIP 3272 DISC: CORROSION ON WEB LOC BTW FR 69 TO FR 70 AT LEVEL STR 23L IN AFT GALLEY AREA. C/A: REPLACED WEB LOC BTW FR 69 TO FR 70 AT LEVEL STR 23L IN AFT GALLEY AREA AS PER A320 SRM 51-42-11 AND DWG D53474180, RELEASE DATE 14-JUL-22, ISSUE Z AND FASTENERS.
- [SDR DALA2023031501888](https://openairdocs.org/sdr/DALA2023031501888.md): Unknown · unknown · Mar 14, 2023 · N372NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 3272 DURING INSPECTION PSU PANEL 25ABC DID NOT OPEN. CORRECTIVE ACTION: R/R PSU PANEL AT SEAT 25ABC PER A320 AMM 25-25-43. OPS CHECK GOOD. (4070400)
- [SDR DALA2022102806984](https://openairdocs.org/sdr/DALA2022102806984.md): Line · leaking · Oct 27, 2022 · N372NW · Airbus A320212 · Hydraulic System, Main
  > SHIP 3272 - ATB - DUE TO LOSS OF GREEN HYD SYSTEM FLUID LOSS. CORRECTIVE ACTION: R/R HYDRAULIC PRESSURE SWITCH LINE (1074GK) ON ENGINE #1. LEAKS CHECK GOOD. ALSO COMPLETED AMDS WORK-CARD 2900-2021. OK FOR SERVICE. (9644764)
- [SDR DALA2022051703373](https://openairdocs.org/sdr/DALA2022051703373.md): None · none · May 16, 2022 · N372NW · Airbus A320212 · Engine Drains
  > SHIP 3272 DURING FLIGHT DIRTY SOCK SMELL IN COCKPIT CAUSING AIR TURN BACK. CORRECTIVE ACTION: OIL WETTING IN ENGINE HPC. REPLACED NUMBER 1 ENGINE. (2238276)

Next page: https://openairdocs.org/aircraft/N372NW/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 = 'N372NW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N372NW/reports

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