# Service difficulty reports: N73283

A list on [N73283](https://openairdocs.org/aircraft/N73283.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 · 71 reports

- [SDR CALA2026093020013](https://openairdocs.org/sdr/CALA2026093020013.md): Socket · faulted · Sep 28, 2026 · N73283 · Boeing 737824 · Emergency Lighting
  > LEFT AFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED. NO HELP. FOUND LAMP SOCKET ASSY FAULTY. REPLACED SOCKET ASSY. OPS CHKS NORMAL.
- [SDR CALA2026083119090](https://openairdocs.org/sdr/CALA2026083119090.md): Lamp · inoperative · Aug 28, 2026 · N73283 · Boeing 737824 · Emergency Lighting
  > EMERGENCY EXIT LIGHT INOPERATIVE LT FWD OVERWING ESCAPE HATCH. REMOVED AND REPLACED OVERWING ESCAPE HATCH EMERGENCY LIGHT LAMPS IAW AMM 33-21-00. OPS TESTED GOOD.
- [SDR CALA2025102710596](https://openairdocs.org/sdr/CALA2025102710596.md): Stringer · cracked · Oct 24, 2025 · N73283 · Boeing 737824 · Wing, Longeron/Stringer
  > INSIDE FUEL PANEL 632RB OPENING STRINGER U9 HAS CRACK IN END OF STRINGER AND APPEARS TO END AT LAST FASTENER REQUESTING ENGINEERING ASSISTANCE. SUPPORT TASK NSA EMX N/R 00074. ESFR COMPLETED REPAIRED 49 STRINGER INSIDE PANEL 632RB IAW UAL ECRA 5720-03572 REV A
- [SDR CALA2025102710558](https://openairdocs.org/sdr/CALA2025102710558.md): Fitting · cracked · Oct 21, 2025 · N73283 · Boeing 737824 · Fuselage Main, Structure
  > SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 15.04 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL
- [SDR CALA2025102410495](https://openairdocs.org/sdr/CALA2025102410495.md): Fitting · cracked · Oct 21, 2025 · N73283 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 32.40 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL
- [SDR CALA2025102410494](https://openairdocs.org/sdr/CALA2025102410494.md): Fitting · cracked · Oct 21, 2025 · N73283 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT BS 540 AND LBL 32.40 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT BS 540 AND LBL 32.40 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL FOR WORK ACCOMPLISHED SEE NSA EMX N/R 00080 AND HANGER N/R 6482033.
- [SDR CALA2025102310439](https://openairdocs.org/sdr/CALA2025102310439.md): Fitting · cracked · Oct 21, 2025 · N73283 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT BS 540 AND LBL 15.04 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 15.04 IAW SRM 51-40-02 & DWG 111A2000 REV ORIG.
- [SDR CALA2025102310438](https://openairdocs.org/sdr/CALA2025102310438.md): Fitting · cracked · Oct 21, 2025 · N73283 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT BS 540, LBL 6.14 CRACKED. REMOVED AND REPLACED SHEAR FITING AT BS 540, LBL 6.14 IAW SRM 51-40-02 & DWG 111A2000 REV ORIG.
- [SDR CALA2025102310437](https://openairdocs.org/sdr/CALA2025102310437.md): Fitting · cracked · Oct 21, 2025 · N73283 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT BS 540, RBL 6.14 IAW SRM 51-40-02 AND BAC DWG 111A2000 REV ORIG.
- [SDR CALA2025101009898](https://openairdocs.org/sdr/CALA2025101009898.md): Control Module · faulted · Oct 8, 2025 · N73283 · Boeing 737824 · Detection System
  > APU FAULT/APU DET INOP FOUND DETECTION MODULE FAULTED, REPLACED ENGINE AND APU FIRE CONTROL MODULE REF AMM 26-10-01, GRD OPS TEST REF AMM TASK 26-11-00-710-801 AND 26-15-00-710-801 NO FAULTS NOTED
- [SDR CALA2025100809805](https://openairdocs.org/sdr/CALA2025100809805.md): Warning Message · false activation · Oct 5, 2025 · N73283 · Boeing 737824 · Central Warning
  > BELOW 80 KNOT REJECT DUE TO OVHT/DET ILLUMINATED ON INITIAL TAKEOFF POWER REG AMM TASK P5-51-07-210-801 HIGH ENERGY STOP NO DEFECTS NOTED, AIRCRAFT OK TO CONTINUE
- [SDR CALA2025091108789](https://openairdocs.org/sdr/CALA2025091108789.md): Indication Sys · malfunctioned · Sep 10, 2025 · N73283 · Boeing 737824 · Landing Gear Position and Warning
  > NOSE GEAR RED LITE ON CONTINUOUSY UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. ON THE GROUND ALL THREE GEAR INDICATE DOWN AND LOCKED. CHECKED PSEU FOR FAULTS, NO FAULTS. CREW INDICATED TO ME THE GEAR WAS RETRAC
- [SDR CALA2025081907931](https://openairdocs.org/sdr/CALA2025081907931.md): Light · inoperative · Aug 18, 2025 · N73283 · Boeing 737824 · Emergency Lighting
  > TEST FLIGHT DISCREPANCY - EMERGENCY EXIT DOOR LIGHT AT 21 LEFT FLICKERS (REF AAR N/R 9984029) REMOVED AND REPLACED EMERGENCY EXIT DOOR LIGHT AT 21 LEFT AS PER AMM 33-51-01-960-801, TEST FOUND NORMAL.
- [SDR CALA2025081107565](https://openairdocs.org/sdr/CALA2025081107565.md): Web · corroded · Aug 8, 2025 · N73283 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CARGO THRESHOLD WEB HAS SPOTS OF CORROSION. REMOVED AND REPLACED THRESHOLD WEB AT FWD CARGO COMPT PER REF SRM 51-40-02-0G-0 AND DWG# 143A8120.
- [SDR CALA2025080607385](https://openairdocs.org/sdr/CALA2025080607385.md): Stringer · corroded · Aug 2, 2025 · N73283 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > AREA AFT OF FORWARD COMPARTMENT CORROSION FOUND AT STRINGER 27R B.S. 540. APPLIED CORROSION INHIBITING COMPOUND, TO THE INTERNAL SURFACES OF THE REPAIR AREA PER AMM 51-21-91-620-802. ACCOMPLISHED REPAIR AT STRINGER 27R, BS 500I TO 540 IAW EC/RA 5330-07576.
- [SDR CALA2025080607381](https://openairdocs.org/sdr/CALA2025080607381.md): Skin · damaged · Aug 1, 2025 · N73283 · Boeing 737824 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE STATIC DISCHARGE NOTED AT SKIN STA 1040 +16" AND 0.5" ABOVE STR 25R, LOWER EXTERNAL FUSELAGE SECTION 48 DOT 223-030. REF AAR N/R 9983881 ACCOMPLISHED REPAIR AT LIGHTNING STRIKE DAMAGE FUSELAGE SKIN BETWEEN STA 1040 - 1064 AT STRINGER 25R PER
- [SDR CALA2025080107207](https://openairdocs.org/sdr/CALA2025080107207.md): Rib · cracked · Jul 31, 2025 · N73283 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORZONTAL STAB LEADING EDGE RIB NR 5 CRACKED. REMOVED AND REPLACED RIB NR 5 AT RT HORIZONTAL STAB LEADING EDGE IAW SRM 51-40-02-0G AND DWG 186A1305.
- [SDR CALA2025073107137](https://openairdocs.org/sdr/CALA2025073107137.md): Support Angle · cracked · Jul 29, 2025 · N73283 · Boeing 737824 · Aerodynamic Fairings
  > LEFT FWD FRONT SPAR WING TO BODY FAIRING AT FIXED L/E I/B SUPPORT ANGLE CRACKED. R & R SUPPORT ANGLE AT LT WING FRONT SPAR WING TO BODY FAIRING AT FIXED L/E I/B SIDE IAW SRM 51-40-02-0G-0.
- [SDR CALA2025073107134](https://openairdocs.org/sdr/CALA2025073107134.md): Skin · worn · Jul 29, 2025 · N73283 · Boeing 737824 · Wing, Plate/Skin
  > RIGHT WING FIXED L/E PANEL 611A WORN. REMOVED AND INSTALLED NEW PANEL 611A IAW SRM 51-40-02-0G-0 AND DWG 116A4008.
- [SDR CALA2025073107133](https://openairdocs.org/sdr/CALA2025073107133.md): Skin · cracked · Jul 29, 2025 · N73283 · Boeing 737824 · Leading Edge Devices
  > RIGHT WING NR 7 SLAT LOWER L/E SKIN LOOSE FASTENERS 4EA AT ACTUATOR AT ACTUATOR ATTACHED RIB. ACCOMPLISHED DOUBLER REPAIR ON RT NR 7 SLAT L/E SKIN IAW SRM 57-42-01-2R-8 ALTERNATIVE 3.
- [SDR CALA2025073107132](https://openairdocs.org/sdr/CALA2025073107132.md): Skin · cracked · Jul 29, 2025 · N73283 · Boeing 737824 · Leading Edge Devices
  > LEFT WING NR 2 SLAT ASSY LOWER L/E SKIN HAS 4 LOOSE FASTENERS AT ACTUATOR ATTACHED RIB. COMPLETED LT WING NR 2 SLAT ASSY LOWER L/E SKIN REPAIR SRM 57-42-2R-8 REPAIR,SRM 51-20-10,SRM 51-40-08-0G-0, SRM 51-40-02-0G-0 AND SOPM 20-50-19. ACCOMPLISHED DOUBLER RE
- [SDR CALA2025073107131](https://openairdocs.org/sdr/CALA2025073107131.md): Intercostal · cracked · Jul 29, 2025 · N73283 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AREA AFT OF FORWARD CARGO COMPARTMENT INTERCOASTAL IS BENT AND REPLACE CRACKED B.S. 500L TO 520 STRINGER 28L. REF AAR N/R 9983846 REMOVED AND INSTALLED NEW INTERCOASTAL BETWEEN STA 500L AND STA S20 ABOVE STRINGER 28L PER B737-800 SRM 51-40-02-0G-0 AND BOEING D
- [SDR CALA2025072506905](https://openairdocs.org/sdr/CALA2025072506905.md): Door · cracked · Jul 24, 2025 · N73283 · Boeing 737824 · Landing Gear Doors
  > LEFT MAIN LANDING GEAR,MID DOOR FWD LOWER CORNER APPEARS TO BE CRACKED. ACCOMPLISHED REPAIR AT L/H MLG MID DOOR IAW SRM 52-80-02-3R-3 REPAIR 3.
- [SDR CALA2025072106747](https://openairdocs.org/sdr/CALA2025072106747.md): Skin · damaged · Jul 17, 2025 · N73283 · Boeing 737824 · Cargo/Baggage Doors
  > REMOVE AND REPLACE FWD CARGO DOOR EXTERIOR SKIN AS REF AAR N/R 9983191 REMOVED AND REPLACE FORWARD CARGO DOOR SKIN REF DWG 143A6110, SRM 52-30-01-2R-3 AND SRM 51-40-02-0G-0. REMOVED AND REPLACED FWD CARGO DOOR EXTERNAL SKIN PER SRM 51-40-02-0G-0 SRM 52-30-01-
- [SDR CALA2025071806703](https://openairdocs.org/sdr/CALA2025071806703.md): Skin · dented · Jul 16, 2025 · N73283 · Boeing 737824 · Cargo/Baggage Doors
  > REMOVE AND REPLACE AFT CARGO DOOR EXTERNAL SKIN. REMOVED AND REPLACED AFT CARGO EXTERAL DOOR SKIN IAW SRM 52-30-01-2R-3 AND 51-40-02-0G-0.
- [SDR CALA2025071806698](https://openairdocs.org/sdr/CALA2025071806698.md): Seat Track · corroded · Jul 10, 2025 · N73283 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION AT MAIN CABIN LT OTBD SEAT TRACK UPPER COWL LBL 45.5 BS 887 - 907. REMOVED AND REPLACED SEAT TRACK AT LBL 45.50 FROM STA 887 TO STA 927 PER SRM 51-40-02-0G-0 AND DWG 10N00633.
- [SDR CALA2025071106469](https://openairdocs.org/sdr/CALA2025071106469.md): Seat Track · corroded · Jul 10, 2025 · N73283 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION AT MAIN CABIN LH I/B SEAT TRACK 727A. ACCOMPLISHED I/B SEAT TRACK REPAIR LBL 24.75" FROM STA 727+9 TO STA 727B IN REF SRM 53-00-52-2R-2, AND BOEING DRAWING 144A5300.
- [SDR CALA2025071006424](https://openairdocs.org/sdr/CALA2025071006424.md): Seat Track · corroded · Jul 8, 2025 · N73283 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORR. AT FASTENERS HEADS MAIN CABIN L/H O/B SEAT TRACK UPPER CROWN WEB LBL 45.5 STA 827 TO 847 MKD DOT 119 REF AAR N/R 9983579 REMOVED EWIS PROTECTION AT WORKING AREA PER AMM 20-60-07-913-801. WORK ACCOMPLISHED BY V903719 REMOVED CORROSION AT SEAT TR
- [SDR CALA2025070906382](https://openairdocs.org/sdr/CALA2025070906382.md): Seat Track · corroded · Jul 7, 2025 · N73283 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION AT MAIN CABIN LT OTBD SEAT TRACK UPPER CROWN LBL 45.5, BS 767. REMOVED CORROSION AT SEAT TRACK. FABRICATED NEW SEAT TRACK & INSTALLED WITH REPAIR PARTS IAW SRM 51-40-02, SRM 53-00-52 & DWG # 146A5300.
- [SDR CALA2025070906381](https://openairdocs.org/sdr/CALA2025070906381.md): Baffle · corroded · Jul 7, 2025 · N73283 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO BAFFLE UNDER RH Z-CHANNEL BETWEEN STA 747-767 AT RBL 21 FOUND CRACKED. REMOVED AND REPLACED BAFFLE UNDER RH Z-CHANNEL BETWEEN STA 747-767 AT RBL 21 PER SRM 51-40-02-0G-0 AND DWG 146A7505.
- [SDR CALA2025072806953](https://openairdocs.org/sdr/CALA2025072806953.md): Door Frame · corroded · Jul 3, 2025 · N73283 · Boeing 737824 · Fuselage Main, Structure
  > FOUND TWO AREA OF INTER-GRANULAR CORROSION, NEXT TOO THE R1 DOOR(INNER-CHORD) REF AAR N/R 9983208 COMPLETED INSTALLATION OF FASTENERS AT INNER CHORD OF R-1 DOOR REF SRM 51-40-02-0G-0, DWG 141A8310. WORK ACCOMPLISHED BY V935074 AND INS-223. ESFR CREATED AND SUB
- [SDR CALA2025071806696](https://openairdocs.org/sdr/CALA2025071806696.md): Attach Angle · cracked · Jul 3, 2025 · N73283 · Boeing 737824 · Fuselage Main, Attach Fittings
  > LEFT LOWER FUSE REAR SPAR VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT BS 663.5 LBL 7. ACCOMPLISHED REPAIR OF L/H VAPOR BARRIER UPPER ATTACHED REPLACEMENT ANGLE AND SPLICE ANGLE AT STA 663.5 LBL 5 TO LBL 25 PER SRM 57-10-10-2R-5.
- [SDR CALA2025071806695](https://openairdocs.org/sdr/CALA2025071806695.md): Attach Angle · cracked · Jul 3, 2025 · N73283 · Boeing 737824 · Fuselage Main, Attach Fittings
  > RIGHT LOWER REAR SPAR VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT BS 663.5 RBL 7. ACCOMPLISHED REPAIR OF RT VAPOR BARRIER UPPER ATTACH ANGLE & SPLICE ANGLE AT BS 663.5 RBL 5 TO RBL 25 IAW SRM 57-10-10-2R-5.
- [SDR CALA2025070306189](https://openairdocs.org/sdr/CALA2025070306189.md): Floor Support · corroded · Jul 1, 2025 · N73283 · Boeing 737824 · Fuselage Miscellaneous Structure
  > STA 967+5/LBL 15... ELONGATED HOLES AND CORROSION. REMOVED AND REPLACED FLOOR SUPPORT BETWEEN STA 967 AND 986.35LBL 15 INCHES PER SRM 51-40-02-0G-0 AND DWG 140A9870 WORK ACCOMPLISHED BY V935074 AND INS 223
- [SDR CALA2025071506573](https://openairdocs.org/sdr/CALA2025071506573.md): Floorbeam · corroded · Jun 30, 2025 · N73283 · Boeing 737824 · Fuselage Main, Floor Beam
  > CORROSION AROUND FASTENER HOLE/BEAM UPPER SURFACE AT STA328 RBL 40.
- [SDR CALA2025070106107](https://openairdocs.org/sdr/CALA2025070106107.md): Floorbeam · damaged · Jun 27, 2025 · N73283 · Boeing 737824 · Fuselage Main, Floor Beam
  > STA 947/LBL 4'-11' STA 947/RBL 5' ELONGATED HOLES AND CORROSION. ACCOMPLISHED REPAIR AT STA 947.50 FROM LBL 4 - LBL 11 IAW EC/RA 5370-01181, B737/800 SRM 53-00-51-2R-1.
- [SDR CALA2025071506570](https://openairdocs.org/sdr/CALA2025071506570.md): Floor Support · cracked · Jun 25, 2025 · N73283 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FOUND FLOOR SUPPORT INTERCOSTAL T CHORD CRACKED AT LBL 14 BETWEEN STA 380 AND 400 REF AAR N/R 9983624 ESFR INFORMATION ENTERED.
- [SDR CALA2025062605909](https://openairdocs.org/sdr/CALA2025062605909.md): Floor Support · cracked · Jun 24, 2025 · N73283 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FOUND FLOOR SUPPORT INTERCOSTSL T CHORD CRACKED AT RBL 9 BETWEEN STA 380 AND 400. REMOVED AND REPLACED FLOOR SUPPORT INTERCOASTAL CHORD AT RBL 9 BETWEEN STA 380 AND STA 400.IN REF TO SRM 51-40-02.
- [SDR CALA2025062605908](https://openairdocs.org/sdr/CALA2025062605908.md): Floor Support · cracked · Jun 24, 2025 · N73283 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FOUND FLOOR SUPPORT INTERCOSTAL T CHORD CRACKED AT BL 0 BETWEEN STA 380 AND 400. REMOVED AND REPLACED FLOOR SUPPORT INTERCOASTAL T CHORD AT BL 0 BETWEEN STA 380 AND STA 400. IN REF TO SRM 51-40-02.
- [SDR CALA2025020402190](https://openairdocs.org/sdr/CALA2025020402190.md): Lamp · inoperative · Feb 2, 2025 · N73283 · Boeing 737824 · Emergency Lighting
  > "EMERGENCY LIGHT ARMED" ANNUNCIATOR LIGHT LAMP INOP REPLACED "EMERGENCY LIGHT ARMED" ANNUNCIATOR LIGHT LAMP WITH REF TO AMM: 33-11-00/201 OPS CHK GOOD.
- [SDR CALA2024080500362](https://openairdocs.org/sdr/CALA2024080500362.md): Handle · out of adjust · Aug 5, 2024 · N73283 · Boeing 737824 · Doors
  > AFT ENTRY DOOR LIGHT ON TAKEOFF DOOR HANDLE NOT SECURED, DEBREFED CREW, L2 DOOR LIGHT WAS ON. CALLED AFT FLT ATTENDENT & DOOR HANDLE WAS NOT IN CLOSED POSITION. FLT ATTENDENT PUT HANDLE DOWN & LIGHT EXTINGUISHED. REMOVED L2 DOOR SLIDE, SAFTIED GIRT BAR & INST
- [SDR CALA2024060701730](https://openairdocs.org/sdr/CALA2024060701730.md): Sensor · faulted · Jun 3, 2024 · N73283 · Boeing 737824 · Leading Edge Slat Control System
  > LE FLAPS TRANSIT LIGHT ON. REPLACED LE FLAP 4 RETRACK SENSOR S174. REF AMM 27--88-11-000-801., SYS OPS CHECKS OK.
- [SDR CALA2023100302935](https://openairdocs.org/sdr/CALA2023100302935.md): Wire · shorted · Sep 30, 2023 · N73283 · Boeing 737824 · Landing Gear System Wiring
  > ANTISKID INOP PERFORMED AACU BITE FIM 32-42 TASK 801.ON INITIAL BIT FOUND MESSAGE ADIRU L AND XDCR1.THIS SENDS YOU TO FIM 32-42 TASK 824 AND 32-42 TASK 806.PERFORMED AUTO SPEED BRAKE/ANTISKID INTERFACE TEST 27-62 TASK 801.BLUE LITE FOR DS2 L OUTBOARD DID NOT C
- [SDR CALA2023071402256](https://openairdocs.org/sdr/CALA2023071402256.md): Tire · failed · Jul 11, 2023 · N73283 · Boeing 737824 · Tire
  > NR 2 MAIN TIRE BLEW ON TAKEOFF. REPLACED #2 MLG TIRE AND WHEEL ASSEMBLY PER AMM 32-45-11-000-801 AND 32-45-11-400-801. WHEEL, TIRE, AS OFF 60-3249-9-0002 1445 ON 60-3249-9-0002 4197. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1708729 SN OFF 1445. NEEDS CONDITIO
- [SDR CALA2022120703325](https://openairdocs.org/sdr/CALA2022120703325.md): Skin · cracked · Dec 7, 2022 · N73283 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STAB LOWER SKIN WAS CRACK AT HSS 184.70 CRACK 0.4. REMOVED DAMAGED CRACK AND REPAIRED AREA AT LT HORIZONTAL STAB IAW SRM 55-10-01 REP 11 TABLE 204 INSP THRESHOLD AT LOWER SKIN STA 184.70 IAW B737-800 SRM 55-10-01-2R-11, AMM 56,000. PERFORME
- [SDR CALA2022120503301](https://openairdocs.org/sdr/CALA2022120503301.md): Skin · cracked · Dec 4, 2022 · N73283 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > LH HORIZONTAL STAB LOWER SKIN HAS 2 CRACKS. CRACK 1- STA 138.70 L=.500". CRACK 2 - STA 120.30 =.400". 01 AMM 51-21-73-370-801, AMM 51-21-00-100-801, PERFORMED NDT IAW PART 6, 51-00-00 PROC 16 PROC 23, HFEC NDT INSPECTION ACCOMPLISHED ON ALL 3 CUTOUTS AND ALL
- [SDR CALA2022113003254](https://openairdocs.org/sdr/CALA2022113003254.md): Skin · cracked · Nov 29, 2022 · N73283 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > NDT-5 INDICATION NOTED ON LT HORIZONTAL LWR SKIN AT HSS 184.70. REMOVED THE CRACK AND REPAIRED THE AREA IAW SRM 55-10-01-2R-11, AMM 51-21-1 1-150-801, SRM 51-20-01, AND EA 22068. PERFORMED NDT IAW PART 6 51-00-00, PROC 23.
- [SDR CALA2022112303206](https://openairdocs.org/sdr/CALA2022112303206.md): Battery Pack · discharged · Nov 22, 2022 · N73283 · Boeing 737824 · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS INOP, EXTERIOR LIGHT DOOR L1, OVER DOOR L1 EXIT LIGHT, FWD ENTRY LIGHT DOOR L1 DOME LIGHT. REMOVED AND INSTALLED NEW BATTERY PACK (M1675) FWD ENTRY LIGHT DOOR L1, TEST GOOD.
- [SDR CALA2020101601195](https://openairdocs.org/sdr/CALA2020101601195.md): B-Nut · backed out · Oct 16, 2020 · N73283 · Boeing 737824 · Turbine Engine Oil System
  > OIL QTY NUMBER 2 ENG READ ZERO AFTER TAKE OFF INITIAL INSPECTION, FOUND B-NUT LINE BACKED OFF FROM OIL PRESSURE SENSOR. LINE IS MARKED WITH YELLOW TAPE. SEE PICTURE AND ADDED 18 QTS MJ2 OIL TO FULL RE-SECURED B-NUT ON OIL PRESSURE MANIFOLD. ACCOMPLISHED 10 MIN
- [SDR CALA2019110901938](https://openairdocs.org/sdr/CALA2019110901938.md): Unknown · odor · Nov 7, 2019 · N73283 · Boeing 737824 · Air Distribution System
  > FA NOTED AFT GALLEY BURN SMELL. NO OVENS POWERED, SMELL DISIPATED QUICKLY, NO OTHER SIGNS NOTED. PRESSURIZE AIRCRAFT WITH APU POWER, TURN ON AFT GALLEY OVENS, COFFEE MAKERS, COFFEE WARMERS. NO EVIDENCE OF ELECTRICAL BURN SMELL. REPRESSURIZE AIRCRAFT WITH ENGIN

Next page: https://openairdocs.org/aircraft/N73283/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 = 'N73283' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N73283/reports

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