# Service difficulty reports: N437UA

A list on [N437UA](https://openairdocs.org/aircraft/N437UA.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 · 128 reports

- [SDR CALA2026102620584](https://openairdocs.org/sdr/CALA2026102620584.md): Bulb · blown · Oct 26, 2026 · N437UA · Airbus A320232 · Flight Compartment Lighting
  > FO CONSOLE/FLOORLIGHT POPPED OUT OF PLACE AND ACRID ODOR IN FLIGHTDECK FOUND BLOWN BULB IN F/O CONSOLE LIGHT, C/B Z6 POPPED. REMOVED AND REPLACED BULB, IAW AMM 33-12-15, RESET C/B, OPS CHECK GOOD. NO FURTHER C/B POPS OR SMELLS.
- [SDR CALA2026092819853](https://openairdocs.org/sdr/CALA2026092819853.md): Light · inoperative · Sep 28, 2026 · N437UA · Airbus A320232 · Emergency Lighting
  > ROW 12ABC RED EMERGENCY ISLE LIGHT INOPERATIVE. REMOVED AND REPLACED RED SEAT MOUNTED EMERGENCY LIGHT AT ROW 12ABC REF AMM 33-51-18. OPS CHECK GOOD. GOOD FOR SERVICE.
- [SDR CALA2026040615102](https://openairdocs.org/sdr/CALA2026040615102.md): Door · unsecure · Mar 31, 2026 · N437UA · Airbus A320232 · Cargo/Baggage Doors
  > ABORTED TAKEOFF, FWD CARGO DOOR OPEN FOUND FWD CARGO DOOR NOT LATCHED PROPERLY, ON CLOSING OF HANDLE INDICATION OF DOOR OPEN WENT OUT. REJECT OCCURRED AT APPROX 80 KNOTS WITH MAX AUTOBRAKE STOPPING AIRCRAFT. MAX BRAKE TEMP WAS 720 ON BRAKE NR 3. VERIFIED NO
- [SDR CALA2025081307696](https://openairdocs.org/sdr/CALA2025081307696.md): Helicoil · damaged · Aug 10, 2025 · N437UA · Airbus A320232 · Cargo/Baggage Doors
  > AFT CARGO DOOR LATCHOPENED DURING FLT PERFORMED TSM 32-31-00-810-886-A, AFT CARGO DOOR INDICATION PROXIMITY SWITCH TGT POS FAULT. WHILE PERFORMING OPERATIONAL CHECK OF THE AFT CARGO COMPARTMENT DOOR. FOUND HANDLE MECHANISM BEARING LOOSE, MISSING HARDWARE. MAKI
- [SDR CALA2025062605930](https://openairdocs.org/sdr/CALA2025062605930.md): Fuel Cap · missing · Jun 25, 2025 · N437UA · Airbus A320232 · Fuel Storage
  > FUELER REPORTS FUEL CAP MISSING. REPLACED FUELING CAP ON CDL.VERIFIED FUEL NOT LEAKING FROM FUELING RECEPTACLE.
- [SDR CALA2025061305530](https://openairdocs.org/sdr/CALA2025061305530.md): None · none · Jun 10, 2025 · N437UA · Airbus A320232 · Standard Practices/Structures
  > REMOVED FWD LH EXIT HATCH IAW AMM 52-21-11-000-001-A AND INSTALLED LOCKPIN ON LH INFLATION RESERVOIR IAW AMM 25-62-00-481-001-A INSTALLED FWD LH EXIT HATCH IAW AMM 52-21-11-400-001-A AND REMOVED LOCKPIN FROM LH INFLATION RESERVOIR IAW AMM 25-62-00-081-001-A IN
- [SDR CALA2024061401799](https://openairdocs.org/sdr/CALA2024061401799.md): Door · missing · Jun 11, 2024 · N437UA · Airbus A320232 · Nacelle/Pylon, Main Frame
  > PDA 1 #2 ENG OIL SERVICE DOOR MISSING ON ARRIVAL TO DENVER HINGE IS MISSING PIC CHECKED BONDING BETWEEN COWL HINGE AND PYLON FOR NEW COWL OIL SERVICE DOOR MEASURES 20.5 IN X 18.5 IN INSTALL PER AMM 20-28-00. WITHIN LIMTS. REF LOGPAGE 8256271 OIL SVC DOOR MISSI
- [SDR CALA2024041501086](https://openairdocs.org/sdr/CALA2024041501086.md): Drain Line · damaged · Apr 11, 2024 · N437UA · Airbus A320232 · Hydraulic Power System
  > HYD Y RSVR LO LVL UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INSPECTED ENG # 2 PYLON AREA CASE DRAIN LINE PIPE ITEM 250 WAS FOUND WITH A SMALL HOLE DUE TO CHAFING BETWEEN PIPE AND BROKEN PYLON BRACKET THEREFORE
- [SDR CALA2023103003237](https://openairdocs.org/sdr/CALA2023103003237.md): Skin · contaminated · Oct 27, 2023 · N437UA · Airbus A320232 · Elevator, Plate/Skin
  > L/H ELEVATOR HAS POSSABLE LIQUID INGRESS AT INDICATION "C" 86 1/ 2 IN FROME I/B END, 15 IN FROME TRAILING EDGE, 1 IN DIAMITER "REPAIR BEFORE NEXT FLIGHT" (SUPPORT TASK) GENERATED AT HAECO LCQ P ER NR 9290285 (28285. REPAIRED LH ELEVATOR 86.5IN FROM IB 15IN FR
- [SDR CALA2023103003236](https://openairdocs.org/sdr/CALA2023103003236.md): Frame · cracked · Oct 27, 2023 · N437UA · Airbus A320232 · Fuselage Main, Frame
  > AD 2022-08-08. LH FRAME 16 UPPER DOUBLER JOGGLE, HOLE "A", HAS A CRACK INDICATION IN THE FRAME LAYER AT THE 5:0 CLOCK POS, 50% S H. "REPAIR BEFORE NEXT FLIGHT" (AD RELATED TASK) GENERATED AT HAECO LCQ PER NR 9290200 (28200). REPAIRED HOLE A AT LH FR 16 UPPER
- [SDR CALA2023103003235](https://openairdocs.org/sdr/CALA2023103003235.md): Skin · contaminated · Oct 27, 2023 · N437UA · Airbus A320232 · Elevator, Plate/Skin
  > LH ELEVATOR HAS POSSABLE LIQUID INGRESS AT INDICATION "A" 123IN FROM I/B END, 8 1/2 IN FROME TRAILING EDGE, 3/4 IN DIAMITER "REPAIR BEFORE NEXT FLIGHT" (SUPPORT TASK) GENERATED AT HAECO LCQ PE R NR 9290282 (28282). REPAIRED LH ELEVATOR UPPER SKIN 123IN FROM
- [SDR CALA2023103003239](https://openairdocs.org/sdr/CALA2023103003239.md): Skin · contaminated · Oct 27, 2023 · N437UA · Airbus A320232 · Elevator, Plate/Skin
  > L/H ELEVATOR HAS POSSABLE LIQUID INGRESS AT INDICATION "C" 108 I N FROM I/B END, 16 IN FROME TRAILING EDGE, 3/4 IN DIAMITER "REPA IR BEFORE NEXT FLIGHT" (SUPPORT TAKS) GENERATED AT HAECO LCQ PER NR 9290284 (28284). REPAIRED LH ELEVATOR 108IN FROM IB AND 16IN
- [SDR CALA2023103003238](https://openairdocs.org/sdr/CALA2023103003238.md): Skin · contaminated · Oct 27, 2023 · N437UA · Airbus A320232 · Elevator, Plate/Skin
  > L/H ELEVATOR HAS POSSABLE LIQUID INGRESS AT INDICATION "B" 109 I N FROM I/B END, 8 IN FROME TRAILING EDGE 1 IN DIAMITER REPAIR BEFORE NEXT FLIGHT. REPAIRED LH ELEVATOR 109IN FROM IB 8IN FROM TE 1.5IN DIA ZONE 1- 3 IAW A320 SRM 55-21-11-300-005 CAT A REPAIR UP
- [SDR CALA2023102703198](https://openairdocs.org/sdr/CALA2023102703198.md): Stiffener · cracked · Oct 20, 2023 · N437UA · Airbus A320232 · Fuselage Main, Structure
  > REVB AD 2020-06-10 FLIGHT DECK FR4 F.O SLIDING WINDOW VERTICAL STIFFENER PRODUCED CRACK DURING HFEC INSPECTION (EA 5310-07673) GENERATED AT HAECO LCQ ON NR 9290067 (28067) BY MECH V061690 REPAIRED DISCREPANT AREA AT FLIGHT DECK FR4 F.O. SLIDING WINDOW VERTICAL
- [SDR CALA2023102303164](https://openairdocs.org/sdr/CALA2023102303164.md): Fitting · cracked · Oct 20, 2023 · N437UA · Airbus A320232 · Landing Gear System
  > REV.L AD 2015-02-14 LMLG DOOR FWD HINGE PRODUCED CRACK INDICATIO NS DURING HFEC INSPECTION AROUND LOWER FWD FASTENER HOLE COMMON TO THE HINGE CONNECTING PLATE (EA 5330-04821)
- [SDR CALA2023071702264](https://openairdocs.org/sdr/CALA2023071702264.md): Cap · missing · Jul 14, 2023 · N437UA · Airbus A320232 · Aircraft Fuel System
  > FUELER REPORTS FUEL CAP IS MISSING MOORE, ROBERT (V082625)APPLIED CEL WITH TOMC FOR FUEL CAP MISSING DISPATCH DESK: 34 NAME: TP DATE: 14-JUL-23- DEFERRED DIRECTLY BY TOMC UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR
- [SDR CALA2023020100303](https://openairdocs.org/sdr/CALA2023020100303.md): Battery · none · Feb 1, 2023 · N437UA · Airbus A320232 · Lighting System
  > CABIN EMERGENCY LIGHTS OPERATIONAL CHECK: {A3NB-33-3-6012} - TEST FAULTS EPSU BATTERY AFT L RPLD EPSU 13WL AND OPS CK CK NORMAL REF AMM 33-51-38-000-001-A AND AMM 33-51-00-710-001-A
- [SDR CALA2022091402360](https://openairdocs.org/sdr/CALA2022091402360.md): Fitting · cracked · Sep 12, 2022 · N437UA · Airbus A300* · Fuselage Structure (General)
  > CRACK INDICATION ON FRAME 36 PRESSURE DECK MEMBRANE UPPER SURFACE ON OPEN FASTENER HOLE 1 INCH OUTBOARD FROM BEAM Y1292, CRACK DIRECTION IS 12 OCLOCK IN FWD CARGO COMPARTMENT (1 EA).SEE AEROMAN NON ROUTINE 2022-343339. TION INTERVAL AND METHOD AS DETAILED. HOL
- [SDR CALA2022091402359](https://openairdocs.org/sdr/CALA2022091402359.md): None · cracked · Sep 12, 2022 · N437UA · Airbus A300* · Fuselage Structure (General)
  > CRACK INDICATION ON FRAME 36 PRESSURE DECK MEMBRANE UPPER SURFACE ON OPEN FASTENER HOLE 5 INCH OUTBOARD FROM BEAM -Y1292, CRACK DIRECTION IS 12 OCLOCK IN FWD CARGO COMPARTMENT (1 EA) SEE AEROMAN NON ROUTINE 2022-343338 LATEST REVISION OF EC5311-02882 ON OR BE
- [SDR CALA2022091202342](https://openairdocs.org/sdr/CALA2022091202342.md): Pressure Panel · cracked · Sep 12, 2022 · N437UA · Airbus A300* · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 36 PRESSURE DECK MEMBRANE UPPER SURFACE ON OPEN FASTENER HOLE 5 INCH OUTBOARD FROM BEAM -Y1292, CRACK DIRECTION IS 12 OCLOCK IN FWD CARGO COMPARTMENT (1 EA) SEE AEROMAN NON ROUTINE 2022-343338 LATEST REVISION OF EC5311-02882 ON OR BE
- [SDR CALA2022091202335](https://openairdocs.org/sdr/CALA2022091202335.md): Skin · none · Sep 10, 2022 · N437UA · Airbus A300* · Fuselage Main, Structure
  > LIGHTNING STRIKE EXTERNAL SKIN BTW FRAME 43 TO FRAME 44 AND BTW STRIN GER 1R TO STRINGER 1L ON UPPER FUSELAGE. SEE AEROMAN NON ROUTINE 2022-343081. (SHEET 03). PERFORMED ROTOTEST INSPECTION ON OPEN FASTENERS DIAMETER HOLES ARE: 0.187 INCH. TOOL USED ELECTRO
- [SDR CALA2022091202333](https://openairdocs.org/sdr/CALA2022091202333.md): None · cracked · Sep 10, 2022 · N437UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTIONS ARE 12 AND 6 OCLOCK, REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (2 EA) SEE AEROMAN NON ROUTINE 2022-343066 LEVEL REPAIR AREA AT DOOR S
- [SDR CALA2022091202332](https://openairdocs.org/sdr/CALA2022091202332.md): None · cracked · Sep 10, 2022 · N437UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > CRACK INDICATION ON FRAME 66 LH SIDE IN OPEN FASTENER HOLE LOWER IN BOARD AT DOOR STOP 1 POSITION, CRACK DIRECTION IS 2 OCLOCK, REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA) SEE AEROMAN NON ROUTINE 2022-343324 INSPECTION THRESHOLD FROM TIME OF ADL/REPA
- [SDR CALA2022081902124](https://openairdocs.org/sdr/CALA2022081902124.md): Channel · corroded · Aug 17, 2022 · N437UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > CORROSION LOWER SILL LOCATED FR66 TO FR68 LEVEL STRG23L IN PASSENGER CABIN.SEE AEROMAN NON ROUTINE 2022-343198 REMOVED AND REPLACED LOWER SILL LOCATED FR66 TO FR68 AT LEVEL POINT AREA:L=0.604 IN W=0.485 IN;D=0.079 IN, NOMINAL THICKNESS= SILL PERFORMED VISUAL I
- [SDR CALA2022081702112](https://openairdocs.org/sdr/CALA2022081702112.md): Frame · cracked · Aug 17, 2022 · N437UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > CRACK INDICATION ON FRAME 66 LH SIDE IN OPEN FASTENER HOLE LOWER IN BOARD AT DOOR STOP 1 POSITION, CRACK DIRECTION IS 2 OCLOCK, REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA) SEE AEROMAN NON ROUTINE 2022-343324 INSPECTION THRESHOLD FROM TIME OF ADL/REPA
- [SDR CALA2022081602072](https://openairdocs.org/sdr/CALA2022081602072.md): Channel · corroded · Aug 16, 2022 · N437UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > CORROSION LOWER SILL LOCATED FR66 TO FR68 LEVEL STRG23L IN PASSENGER CABIN.REMOVED AND REPLACED LOWER SILL LOCATED FR66 TO FR68 AT LEVEL POINT AREA.
- [SDR CALA2022081002033](https://openairdocs.org/sdr/CALA2022081002033.md): Angle · cracked · Aug 9, 2022 · N437UA · Airbus A320232 · Fuselage Floor Panel
  > CRACK FLOOR STRUCTURE ANGLE LOCATED FR68 LEVEL STRG23L IN PASSENGER CABIN (1 EA) REMOVED AND REPLACED FLOOR STRUCTURE ANGLE AND FASTENERS AND NOT FOUND MORE DAMAGE IAW NTM 51-90-00. PERFORMED LOCATED FR68 AT LEVEL STR 23L IN PASSENGER CABIN IAW A320 SCEPTRE
- [SDR CALA2022080801983](https://openairdocs.org/sdr/CALA2022080801983.md): Beam · corroded · Aug 5, 2022 · N437UA · Airbus A300* · Fuselage Structure (General)
  > CORROSION FLOOR BEAM +Y765 LOCATED FR66 IN PASSENGER CABIN REMOVED AND REPLACED FLOOR BEAM +765 LOCATED BTW INSPECTION ON AREA AND NOT FOUND ADDITIONAL W=0.115IN. TOOL USED: CALIPER PN:700-113-10, FR64 TO FR66 AT AFT GALLEY AREA IN PSSENGER CABIN DAMAGE IAW N
- [SDR CALA2022080801981](https://openairdocs.org/sdr/CALA2022080801981.md): Angle · cracked · Aug 5, 2022 · N437UA · Airbus A300* · Fuselage Structure (General)
  > CRACK FLOOR STRUCTURE ANGLE LOCATED FR66 LEVEL STRG 23L IN PASSENGER CABIN, SEE AEROMAN NON ROUTINE 2022-343169 REMOVED AND REPLACED FLOOR STRUCTURE ANGLE LOCATED FR.66 LEVEL 24-JUN-23, PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND STR. 23L IN PASSENGER CA
- [SDR CALA2022080801980](https://openairdocs.org/sdr/CALA2022080801980.md): Angle · cracked · Aug 5, 2022 · N437UA · Airbus A300* · Fuselage Structure (General)
  > CRACK FLOOR STRUCTURE ANGLE LOCATED FR66 LEVEL STRG23R IN PASSE ABIN. SEE AEROMAN NON ROUTINE 2022-343195 REMOVED AND REPLACED FLOOR STRUCTURE ANGLE LOCATED FR 66 LEVEL 24-JUN-23. PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND STR 23R IN PASSEGER CABIN IA
- [SDR CALA2022080801979](https://openairdocs.org/sdr/CALA2022080801979.md): None · corroded · Aug 5, 2022 · N437UA · Airbus A300* · Fuselage Structure (General)
  > CORROSION FLOOR STRUCTURE LOCATED FR68 Y160.5 IN IN PASSENGER CABIN REPLACED FLOOR STRUCTURE LOCATED FR68 Y160.5 NTM 51-90-00. PERFORMED SCEPTRE ENTRY IN PASSENGER CABIN IAW A320 51-72-11 AND ON LOGPAGE NUMBER IS:9153134. MEASURE OF CORROSION DRAWING #D534720
- [SDR CALA2022080501967](https://openairdocs.org/sdr/CALA2022080501967.md): Floorbeam · corroded · Aug 4, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM +Y1292 LOCATED FR66 IN PASSENGER CABIN SEE AEROMAN NON ROUTINE 2022-343175 REMOVED AND REPLACED FLOOR BEAM + Y1292 LOCATED BTW FR 64 TO FR D=2.29MM (0.090IN). TOOL SPLICES AND NOT FOUND MORE DAMAGE IAW NTM 51-90-00. PERFORMED 66 AFT GALLEY
- [SDR CALA2022080501966](https://openairdocs.org/sdr/CALA2022080501966.md): Fitting · cracked · Aug 4, 2022 · N437UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > CRACK INDICATION ON FRAME 58 IN OPEN FASTENER HOLE IN HORIZONTAL FLANGE AT LEVEL OF STGR 37LH, CRACK DIRECTION IS 9 OCLOCK, REPAIR BEFORE FURTHER FLIGHT IN AFT CARGO COMPARTMENT (1 EA) REMOVED AND REPLACED SUPPORT FITTING AND FASTENER LOC. ON FR58 BRACKET LAY
- [SDR CALA2022080501965](https://openairdocs.org/sdr/CALA2022080501965.md): Frame · cracked · Aug 4, 2022 · N437UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 43 FOOT COUPLING LH SIDE IN OPEN FASTENER HOLE AT LEVE OF STGR22, CRACK DIRECTION IS 3 OCLOCK IN PASSENGER CABIN (1 EA) REPAIR BEFORE NEXT FLIGHT REMOVED AND REPLACED FRAME 43 FOOT COUNPLING AND FASTENERS LOC FOOT FITTING AT LEVEL STR
- [SDR CALA2022080501964](https://openairdocs.org/sdr/CALA2022080501964.md): Beam · corroded · Aug 4, 2022 · N437UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > CORROSION LOWER SILL LOCATED FR66 TO FR68 R/H SIDE AT AFT GALLEY AREA REMOVED AND REPLACED LOWER SILL LOCATED FR66 TO FR68 R/H SIDE CORRODED AREAS ARE:DEEPEST POINT L=3.980 IN W=2.049 IN D=0.055 IS 9151970.SEE AEROMAN NON ROUTINE 2022-343194 AT AFT GALLEY AREA
- [SDR CALA2022080301948](https://openairdocs.org/sdr/CALA2022080301948.md): Floor Support · cracked · Aug 3, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CRACK FLOOR STRUCTURE ANGLE LOCATED FR66 LEVEL STRG 23L IN PASSENGER CABIN, SEE AEROMAN NON ROUTINE 2022-343169 REMOVED AND REPLACED FLOOR STRUCTURE ANGLE LOCATED FR.66 LEVEL 24-JUN-23, PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND STR. 23L IN PASSENGER CA
- [SDR CALA2022080301947](https://openairdocs.org/sdr/CALA2022080301947.md): Floorbeam · corroded · Aug 3, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM +Y1292 LOCATED FR66 IN PASSENGER CABIN SEE AEROMAN NON ROUTINE 2022-343175 REMOVED AND REPLACED FLOORBEAM + Y1292 LOCATED BTW FR 64 TO FR D=2.29MM (0.090IN). TOOL SPLICES AND NOT FOUND MORE DAMAGE IAW NTM 51-90-00. PERFORMED 66 AFT GALLEY
- [SDR CALA2022080301946](https://openairdocs.org/sdr/CALA2022080301946.md): Floor Support · cracked · Aug 3, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CRACK FLOOR STRUCTURE ANGLE LOCATED FR66 LEVEL STRG23R IN PASSE ABIN. SEE AEROMAN NON ROUTINE 2022-343195 REMOVED AND REPLACED FLOOR STRUCTURE ANGLE LOCATED FR 66 LEVEL 24-JUN-23. PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND STR 23R IN PASSEGER CABIN IA
- [SDR CALA2022080301945](https://openairdocs.org/sdr/CALA2022080301945.md): Floor Support · corroded · Aug 3, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION FLOOR STRUCTURE -Y1162.5 AND FR68 IN PASSENGER CABIN REMOVED AND REPLACED FLOOR STRUCTURE -Y1162.5 LOC. FR.68 TO DIGITRAL CALIPER P/N: 500-197-30; S/N: A21147760; CAL DUE DATE: PERFORMED SCEPTRE ENTRY ON LOG PAGE NUMBER 9206195 FR.69 AND -Y1162.5 IA
- [SDR CALA2022080101934](https://openairdocs.org/sdr/CALA2022080101934.md): Coupling · cracked · Aug 1, 2022 · N437UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 43 FOOT COUPLING LH SIDE IN OPEN FASTENER HOLE AT LEVE OF STGR22, CRACK DIRECTION IS 3 OCLOCK IN PASSENGER CABIN. REMOVED AND REPLACED FRAME 43 FOOT COUNPLING AND FASTENERS LOC FOOT FITTING AT LEVEL STR21 LH.
- [SDR CALA2022080101933](https://openairdocs.org/sdr/CALA2022080101933.md): Frame · cracked · Aug 1, 2022 · N437UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 58 IN OPEN FASTENER HOLE IN HORIZONTAL FLANGE AT LEVEL OF STGR 37LH, CRACK DIRECTION IS 9 OCLOCK, REMOVED AND REPLACED SUPPORT FITTING AND FASTENER LOC. ON FR58 BRACKET LAYER.
- [SDR CALA2022080101932](https://openairdocs.org/sdr/CALA2022080101932.md): Floor Support · corroded · Aug 1, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION FLOOR STRUCTURE Y1162.5 AND FR68 IN PASSENGER CABIN REMOVED AND REPLACED FLOOR STRUCTURE Y1162.5 AND FASTENER LOC D=1.150 MM (0.045 INCH).
- [SDR CALA2022072901913](https://openairdocs.org/sdr/CALA2022072901913.md): Channel · corroded · Jul 29, 2022 · N437UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > CORROSION LOWER SILL LOCATED FR66 TO FR68 R/H SIDE AT AFT GALLEY AREA REMOVED AND REPLACED LOWER SILL LOCATED FR66 TO FR68 R/H SIDE CORRODED AREAS ARE:DEEPEST POINT L=3.980 IN W=2.049 IN D=0.055 IS 9151970.SEE AEROMAN NON ROUTINE 2022-343194 AT AFT GALLEY AREA
- [SDR CALA2022072701890](https://openairdocs.org/sdr/CALA2022072701890.md): Floorbeam · corroded · Jul 27, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM +Y765 LOCATED FR66 IN PASSENGER CABIN REMOVED AND REPLACED FLOORBEAM +765 LOCATED BTW INSPECTION ON AREA AND NOT FOUND ADDITIONAL W=0.115IN. TOOL USED: CALIPER PN:700-113-10, FR64 TO FR66 AT AFT GALLEY AREA IN PSSENGER CABIN DAMAGE IAW NTM
- [SDR CALA2022072701904](https://openairdocs.org/sdr/CALA2022072701904.md): Floorbeam · corroded · Jul 25, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM -Y765 LOCATED FR21 AT FWD GALLEY AREA REMOVED AND REPLACED FLOOR BEAM -Y765 LOC BTW FR12 TO FR24 AT FWD GALLEY AREA IAW A320 SRM 51-42-11 AND DWG D53112812, D53110984, D53110876, D53112814 AND PERFORMED VISUAL INSPECTION ON AREA NOT FOUND
- [SDR CALA2022072701901](https://openairdocs.org/sdr/CALA2022072701901.md): Floorbeam · corroded · Jul 25, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM +Y765 LOCATED FR67 TO FR68 IN PASSENGER CABIN REMOVED AND REPLACED FLOOR BEAM +Y765 LOC BTW FR66 TO FR70 IN PASSENGER CABIN I.A.W A320 SRM 51-42-11 AND DWG D53472040 AND PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND ADDITIONAL DAMAGE I
- [SDR CALA2022072001845](https://openairdocs.org/sdr/CALA2022072001845.md): None · corroded · Jul 20, 2022 · N437UA · Airbus A300* · Fuselage Floor Panel
  > CORROSION FLOOR BEAM -Y765 LOCATED FR21 AT FWD GALLEY AREA REMOVED AND REPLACED FLOOR BEAM -Y765 LOC BTW FR12 TO FR24 AT FWD GALLEY AREA IAW A320 SRM 51-42-11 AND DWG D53112812, D53110984, D53110876, D53112814 AND PERFORMED VISUAL INSPECTION ON AREA NOT FOUND
- [SDR CALA2022072001844](https://openairdocs.org/sdr/CALA2022072001844.md): None · corroded · Jul 20, 2022 · N437UA · Airbus A300* · Fuselage Miscellaneous Structure
  > CORROSION FLOOR BEAM Y-1292 AND FR21 AT FWD GALLEY AREA (1EA) REMOVED AND REPLACED FLOOR BEAM -Y1292 LOC BTW FR12 TO FR24 AT F WD GALLEY AREA IAW A320 SRM 51-42-11, 51-72-11 AND DWG: D5311281 4, D53110876, D53112812 AND PERFORMED VISUAL INSPECTION ON AREA NOT
- [SDR CALA2022072001843](https://openairdocs.org/sdr/CALA2022072001843.md): None · corroded · Jul 20, 2022 · N437UA · Airbus A300* · Passenger Compartment Windows
  > CORROSION FLOOR BEAM +Y765 LOCATED FR67 TO FR68 IN PASSENGER CABIN REMOVED AND REPLACED FLOOR BEAM +Y765 LOC BTW FR66 TO FR70 IN PASSENGER CABIN I.A.W A320 SRM 51-42-11 AND DWG D53472040 AND PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND ADDITIONAL DAMAGE
- [SDR CALA2018011900248](https://openairdocs.org/sdr/CALA2018011900248.md): Cover · loose · Jan 19, 2018 · N437UA · Airbus A320232 · Service Doors
  > DOOR R AFT EMERGENCY EXIT ECAM 4X WHILE IN FLGHT INSPECTED AND INSTALLED COVER FLAP, INDICATION OPS NORMAL IAW AMM 25-23-47-400-001-A

Next page: https://openairdocs.org/aircraft/N437UA/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 = 'N437UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N437UA/reports

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