# Service difficulty reports: N7832A

A list on [N7832A](https://openairdocs.org/aircraft/N7832A.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 · 221 reports

- [SDR SWAA2026081348791](https://openairdocs.org/sdr/SWAA2026081348791.md): Unknown · odor · Aug 12, 2026 · N7832A · Boeing 73779P · Air Distribution System
  > BURNING RUBBER ODOR IN FWD CABIN WITH GROUND AIR AND PACKS ON. ACCOMPLISHED FIM TASK 21-00 TASK 806 FOR FUMES AND ODOR IN THE CABIN. NO DEFECTS NOTED ACFT OK FOR SERVICE.
- [SDR SWAA2026061009657](https://openairdocs.org/sdr/SWAA2026061009657.md): Lamp · inoperative · Jun 6, 2026 · N7832A · Boeing 73779P · Emergency Lighting
  > L2 SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-04.
- [SDR SWAA2026040886775](https://openairdocs.org/sdr/SWAA2026040886775.md): Girt Bar · out of adjust · Apr 6, 2026 · N7832A · Boeing 73779P · Emergency Equipment
  > FWD GALLEY GRIT BAR NOT SEATING PROPERLY IN DOOR HOLDER. REPOSITIONED GRIT IN LOWER FLAP REF AMM 25-66-01. GRIT BAR STOWS AND ARMS PROPERLY IN FLOOR MOUNTS WITH NO DEFECTS. A/C OK FOR SERVICE. (FWD SERVICE DOOR).
- [SDR SWAA2026021670089](https://openairdocs.org/sdr/SWAA2026021670089.md): Engine · no discrepancy · Feb 11, 2026 · N7832A · Boeing 73779P · Engine (Turbine/Turboprop)
  > 20 KNOT RTO DUE TO NR 2 ENGINE SLOW TO SPOOL. PERFORMED ACCELERATION TEST ON NR 2 ENGINE. FOUND ENGINE TO BE WITHIN LIMITS, WORK DONE IAW 71-00-00 OF THE AMM.
- [SDR SWAA2025081293720](https://openairdocs.org/sdr/SWAA2025081293720.md): Fitting · cracked · Jul 21, 2025 · N7832A · Boeing 73779P · Service Doors
  > CRACK SERVICE DOOR FITTING LOC LOWER AFT CORNER AT FWD GALLEY AREA. REPLACED FITTING 1(E/A) AND FASTENERS LOCATED ON SERVICE DOOR LOWER AFT CORNER AT FWD GALLEY AREA IAW 51-40-02-0G-0 AND DWG 141A6535; SHEET 1, REV B, AND DWG 141A6516; SHEET 95; REV -.
- [SDR SWAA2025081293401](https://openairdocs.org/sdr/SWAA2025081293401.md): Angle · corroded · Jul 20, 2025 · N7832A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE LOCATED BS 794.3 BETWEEN STR 22R AND STR 23R AT AFT CARGO COMPARTMENT. REPLACED ANGLE LOCATED BS 794.3 BETWEEN STR 22R AND STR 23R AT AFT CARGO COMPARTMENT IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9, AND DWG 284A0341, SHEET 3 REV-.
- [SDR SWAA2025081292843](https://openairdocs.org/sdr/SWAA2025081292843.md): Plate · cracked · Jul 18, 2025 · N7832A · Boeing 73779P · Wing Miscellaneous Structure
  > CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT LT WING IAW SRM 51-40-02 AND DRAWING 115A2001, SHEET 30, REV A.
- [SDR SWAA2025081292846](https://openairdocs.org/sdr/SWAA2025081292846.md): Plate · cracked · Jul 18, 2025 · N7832A · Boeing 73779P · Wing Miscellaneous Structure
  > CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT LT WING. REPLACED CORRUGATED PLATE LOCATED ON TRAILING EDGE IRSS 217 AT LH WING IAW SRM 51-40-02 AND DWG 115A2001, SHEET 30, REV A. DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM 57-51-02. CRACK LENGTH: 0
- [SDR SWAA2025081292845](https://openairdocs.org/sdr/SWAA2025081292845.md): Angle · cracked · Jul 18, 2025 · N7832A · Boeing 73779P · Wing Miscellaneous Structure
  > CRACK ON ANGLE LOCATED ORSS 271 TRAILING EDGE AT LT WING. REPLACED ANGLE LOCATED ORSS 271 TRAILING EDGE AT LT WING IAW SRM 51-40-02, SRM SRM 51-10-02, ITEM 9, AND DRAWING 115A2930, SHEET 7, REV -.
- [SDR SWAA2025081292841](https://openairdocs.org/sdr/SWAA2025081292841.md): Plate · cracked · Jul 18, 2025 · N7832A · Boeing 73779P · Wing Miscellaneous Structure
  > CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT RT WING 2025-452361<[01] REPLACED CORRUGATED PLATE AND FASTENERS TRAILING EDGE LOCATED ORSS 241 AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9 AND DWG 115A2001 SHEET 30 REV-A. MEASURE
- [SDR SWAA2025081292842](https://openairdocs.org/sdr/SWAA2025081292842.md): Plate · cracked · Jul 18, 2025 · N7832A · Boeing 73779P · Wing Main, Frame Structure
  > CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT RT WING IAW SRM 51-40-02 AND DWG 115A2001, SHEET 30, REV A, DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM 57-51-02<BR><BR>CRACK LENGTH:
- [SDR SWAA2025081292837](https://openairdocs.org/sdr/SWAA2025081292837.md): Support Angle · broken · Jul 18, 2025 · N7832A · Boeing 73779P · Wing Miscellaneous Structure
  > BROKEN SUPPORT ANGLE LOCATED IRSS 212 TRAILING EDGE AT RT WING, REPLACED SUPPORT ANGLE LOCATED IRSS 212 TRAILING EDGE AT RT WING IAW SRM 51-10-02; SRM 51-40-02 AND DWG 115A2001; SHEET 24 AND REV A.
- [SDR SWAA2025081292838](https://openairdocs.org/sdr/SWAA2025081292838.md): Plate · corroded · Jul 18, 2025 · N7832A · Boeing 73779P · Wing Miscellaneous Structure
  > CORROSION SUPPORT PLATE LOCATED ORSS 376 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING. REPLACED SUPPORT PLATE LOCATED ORSS 376 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING IAW SRM 51-040-20-G-0. AND PERFORMED VISUAL INSPECTION ON ADJACENT AREAS
- [SDR SWAA2025081292839](https://openairdocs.org/sdr/SWAA2025081292839.md): Web · cracked · Jul 18, 2025 · N7832A · Boeing 73779P · Wing Miscellaneous Structure
  > CRACK ON WEB TRAILING EDGE LOCATED ORSS 276 AT RT WING. REPLACED WEB TRAILING EDGE LOCATED ORSS 276 AT RT WING IAW SRM 51-40-02 AND DWG 115A2512 SHEET 5 REV. B. DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM 57-51-02. CRACK LENGTH: 0.500.
- [SDR SWAA2025081292840](https://openairdocs.org/sdr/SWAA2025081292840.md): Support Angle · cracked · Jul 18, 2025 · N7832A · Boeing 73779P · Wing Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE INTERNAL CAVITY LOCATED ORSS 271 TRAILING EDGE AT RT WING. REPLACED SUPPORT ANGLE INTERNAL CAVITY LOCATED ORSS 271 TRAILING EDGE AT RT WING IAW SRM 51-40-02 AND DWG 115A2930 SHEET 6 REV -. DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM 57-51
- [SDR SWAA2025081292298](https://openairdocs.org/sdr/SWAA2025081292298.md): Access Panel · elongated · Jul 17, 2025 · N7832A · Boeing 73779P · Wing, Plate/Skin
  > ELONGATED HOLE ACCESS PANEL 561AB TRAILING EDGE AT LT WING. REPAIRED THE ACCESS PANEL 561AB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2025081292291](https://openairdocs.org/sdr/SWAA2025081292291.md): Angle · cracked · Jul 17, 2025 · N7832A · Boeing 73779P · Leading Edge Devices
  > CRACK ANGLE ON SLAT 6 INBOARD AUXILIARY AT RT WING (1 E/A), REPLACED ANGLE LOCATED ON SLAT 6 INBOARD AUXILIARY AT RT WING IAW SRM 51-40-02 AND DWG 114A5030, SHEET 8, REV C, DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM 57-42-01.
- [SDR SWAA2025081292545](https://openairdocs.org/sdr/SWAA2025081292545.md): Light · broken · Jul 17, 2025 · N7832A · Boeing 73779P · Emergency Lighting
  > BROKEN PHOTOLUMINESCENT STRIP LH (5EA) AT PASSENGER CABIN. THE REPLACEMENT PHOTOLUMINESCENT STRIP LH (5EA) SEE TTG8Q003KHW1.
- [SDR SWAA2025081292546](https://openairdocs.org/sdr/SWAA2025081292546.md): Light · broken · Jul 17, 2025 · N7832A · Boeing 73779P · Emergency Lighting
  > BROKEN PHOTOLUMINESCENT STRIP RH (5EA) AT PASSENGER CABIN. THE REPLACEMENT PHOTOLUMINESCENT STRIP RH (5EA) SEE TTG8Q003KHW1.
- [SDR SWAA2025081291740](https://openairdocs.org/sdr/SWAA2025081291740.md): Pressure Deck · cracked · Jul 15, 2025 · N7832A · Boeing 73779P · Fuselage Main, Structure
  > CRACK INDICATION ON THE HORIZONTAL PRESSURE DECK LOCATED AT BS 663 PLUS 1 INCH AND LBL 31 AT MAIN WHEEL WELL COMPARTMENT. PERFORMED PERMANENT REPAIR ON HORIZONTAL PRESSURE DECK AT BS 663 TO BS 675 AND LBL 30 TO LBL 60 AT MAIN WHEEL WELL COMPARTMENT IAW SRM 53
- [SDR SWAA2025081291749](https://openairdocs.org/sdr/SWAA2025081291749.md): Skin Panel · cracked · Jul 15, 2025 · N7832A · Boeing 73779P · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION FOUND ON RT HORIZONTAL STAB LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 7.5 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.700 INCH. PERFORMED REPAIR LOCATED ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL AT STAB STA 193.9
- [SDR SWAA2025081291747](https://openairdocs.org/sdr/SWAA2025081291747.md): Scuff Plate · cracked · Jul 15, 2025 · N7832A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK ON CENTER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED CENTER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW SRM 53-30-15-2R-1 REPAIR 1.
- [SDR SWAA2025081291739](https://openairdocs.org/sdr/SWAA2025081291739.md): Intercostal · cracked · Jul 15, 2025 · N7832A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL - WEB FLOOR STRUCTURE LOCATED BS540 AT LEVEL BL0 TO RBL24 PASSENGER CABIN. REPLACED BREAK PANEL FLOOR STRUCTURE LOCATED BS540 AT LEVEL BL0 TO RBL24 PASSENGER CABIN IAW SRM 51-10-02 ITEM 9, SRM 51-40-02 AND DRAWING #143A0060 SHEET 36 REV A
- [SDR SWAA2025060276006](https://openairdocs.org/sdr/SWAA2025060276006.md): Seal · cracked · May 29, 2025 · N7832A · Boeing 73779P · Horizontal Stabilizer Miscellaneous Structure
  > R/H HORIZONTAL STABILIZER FWD LWR SLIDING SEAL BENT WITH HORIZONTAL CRACK EXTENDING FROM THE EDGE ALONG THE BEND AND HAS A VERTICAL CRACK APPROX. 1 INCH ALONG FWD TRACK. <[01] R&R R/H HORIZONTAL STABILIZER FWD LWR SLIDING SEAL. IAW AMM 53-31-31.
- [SDR SWAA2025051469903](https://openairdocs.org/sdr/SWAA2025051469903.md): Panel · loose · May 11, 2025 · N7832A · Boeing 73779P · Emergency Exits
  > CAPTAIN SIDE LOWER PANEL EXIT ROW PANEL LOOSE<[01] RE-SECURED EMERGENCY EXIT DOOR STRAP PANEL PER AMM 52-22-51
- [SDR SWAA2025040922076](https://openairdocs.org/sdr/SWAA2025040922076.md): Girt Bar · damaged · Apr 6, 2025 · N7832A · Boeing 73779P · Emergency Equipment
  > PLASTIC COVER ON RIGHT FORWARD ENTRY DOOR (R1) GIRT BAR PARTIALLY BROKEN <[01]. REPLACED EVAC RELEASE STOP ON R1 GIRT BAR IN REFERENCE TO AMM 25-66-00.
- [SDR SWAA2025031104125](https://openairdocs.org/sdr/SWAA2025031104125.md): Cover · detached · Mar 10, 2025 · N7832A · Boeing 73779P · Emergency Lighting
  > F/O SIDE EMERGENCY EXIT COVER FELL OFF TSR 2025001786<[01] C/W EA 25-152-00618
- [SDR SWAA2024112161264](https://openairdocs.org/sdr/SWAA2024112161264.md): Sign · loose · Nov 18, 2024 · N7832A · Boeing 73779P · Emergency Lighting
  > LENS COVER BELOW EXIT SIGN FWD GALLEY LOOSE. LIGHT INDICATE NORMALLY.<[01] SECURED LENS. OK TO CONTINUE PER MEL 25-10-01 SP1B AUTH # 223999;[02] REMOVED & REPLACED FWD GALLEY EXIT SIGN LOWER HOUSING ASSY REF AMM 33-51-01. OPS CHECKS GOOD. ALSO C/W CABIN INTERP
- [SDR SWAA2024101748359](https://openairdocs.org/sdr/SWAA2024101748359.md): Slide · dislodged · Oct 14, 2024 · N7832A · Boeing 73779P · Escape Slide
  > AFT SERVICE DOOR ESCAPE SLIDE FELL OUT OF HOUSING<[01] C/W MT 725-61-06 OF AFT SERVICE DOOR SLIDE.
- [SDR SWAA2024082628817](https://openairdocs.org/sdr/SWAA2024082628817.md): Isolation Mount · broken · Aug 22, 2024 · N7832A · Boeing 73779P · Escape Slide
  > AFT PASSENGER DOOR FWD UPPER AND LOWER SLIDE MOUNT ISOLATORS BROKEN.<[01] R&R AFT PASSENGER DOOR FWD UPPER AND LOWER SLIDE MOUNT ISOLATORS IAW SRM 51-40-02.;[02] INSPECTION C/W
- [SDR SWAA2024060799020](https://openairdocs.org/sdr/SWAA2024060799020.md): Light · inoperative · Jun 7, 2024 · N7832A · Boeing 73779P · Emergency Lighting
  > R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. R&R R1 DOOR SLIDE/OVERWING LAMP IAW AMM 33-51-04 OPS CHECK GOOD.
- [SDR SWAA2024030458537](https://openairdocs.org/sdr/SWAA2024030458537.md): Slide · dislodged · Mar 2, 2024 · N7832A · Boeing 73779P · Escape Slide
  > FWD ENTRY DOOR ESCAPE DOOR ESCAPE CAME OUT OF THE HOUSING<[01] COMPLIED WITH MT 725-61-06 REM/INST; A/C OK FOR SVC
- [SDR SWAA2023090595915](https://openairdocs.org/sdr/SWAA2023090595915.md): Nut · deteriorated · Sep 1, 2023 · N7832A · Boeing 73779P · Service Doors
  > DETERIORATED SERVICE DOORWAY ASSIST HANDLE NUT AT AFT GALLEY AREA (2 EA) 2023-469812<[01] REPLACED SERVICE DOORWAY ASSIST HANDLE NUT AT AFT GALLEY AREA (2 EA) IAW B737-700 AMM-52-41-31-400-802 STEP 3.F.(2);[02] COMPLETED
- [SDR SWAA2023090190358](https://openairdocs.org/sdr/SWAA2023090190358.md): Stiffener · cracked · Aug 17, 2023 · N7832A · Boeing 73779P · Horizontal Stabilizer Structure
  > CRACK ON STIFFENER LOC. INSPAR RIB 120.30 AT 19 INCH FRONT SPAR AT RH HORIZONTAL STABILIZER 2023-470223 CORRECT FAULT DESCRIPTION: CRACK ON STIFFENER LOC. INSPAR RIB 120.30 AT FRONT SPAR RH HORIZONTAL STABILIZER<[01] REPLACED STIFFENER LOC. INSPAR RIB 120.30 A
- [SDR SWAA2023090186254](https://openairdocs.org/sdr/SWAA2023090186254.md): Strap · corroded · Aug 5, 2023 · N7832A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP LOCATED BS 360 BTW STR 26R TO STR 27R RBL 5 WL 152 AT ELECTRONIC COMPARTMENT 2023-470200 CORRECTED LOCATION CORROSION ON STRAP LOCATED BS 360 BTW STR 27R TO STR 28R RBL 5 WL 152 AT ELECTRONIC COMPARTMENT<[01] TOOL USED DIGITAL CALIPER P/N:50
- [SDR SWAA2023090585379](https://openairdocs.org/sdr/SWAA2023090585379.md): Support Angle · cracked · Aug 3, 2023 · N7832A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BS 1016 BTW STR 4L TO STR 4R INTERNAL AREA OF VERTICAL STABILIZER 2023-470167<[01] REPLACED SUPPORT ANGLE LOCATED BS 1016 BTW STR 4L TO STR 4R INTERNAL AREA OF VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND #DWG:176A3001 SHEET
- [SDR SWAA2023090185537](https://openairdocs.org/sdr/SWAA2023090185537.md): Rib · cracked · Aug 3, 2023 · N7832A · Boeing 73779P · Horizontal Stabilizer Structure
  > CRACK INSPAR RIB 120.30 AT 28 INCHES OF FRONT SPAR LT HORIZONTAL STAB 2023-470175<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161
- [SDR SWAA2023090185536](https://openairdocs.org/sdr/SWAA2023090185536.md): Rib · cracked · Aug 3, 2023 · N7832A · Boeing 73779P · Horizontal Stabilizer Structure
  > CRACK INSPAR RIB 120.30 AT 19 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2023-470169<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N:
- [SDR SWAA2023090185169](https://openairdocs.org/sdr/SWAA2023090185169.md): Frame · cracked · Aug 2, 2023 · N7832A · Boeing 73779P · Fuselage Main, Frame
  > CRACK ON FRAME LOCATED BS 727D BTW STR 8L TO STR 9L AT PASSENGER CABIN 2023-470152<[01] TOOL USED: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 210138103; DUE DATE: 02-MAY-24.;[02] FRAME LOCATED BS 727D BTW STR 8L TO STR 9L AT PASSENGER CABIN NOT REPAIRED DUE TO CRACK
- [SDR SWAA2023090184937](https://openairdocs.org/sdr/SWAA2023090184937.md): Bracket · cracked · Aug 2, 2023 · N7832A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R CEILING AREA AT PASSENGER CABIN 2023-470150<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R CEILING AREA AT PASSENGER CABIN IAW B737-700 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A79
- [SDR SWAA2023090584765](https://openairdocs.org/sdr/SWAA2023090584765.md): Plate · corroded · Aug 1, 2023 · N7832A · Boeing 73779P · Wing Miscellaneous Structure
  > CORROSION RAIL NUT PLATE O/B FIXED LEADING EDGE OFSS 449 AT LT WING 2023-470129<[01] REPLACED RAIL NUT PLATE O/B FIXED LEADING EDGE OFSS 449 AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND APPLIED PROTECTIVE TREATMENT ON OPEN HOLES IAW B737-700 SRM 51-2
- [SDR SWAA2023090584764](https://openairdocs.org/sdr/SWAA2023090584764.md): Stringer · cracked · Aug 1, 2023 · N7832A · Boeing 73779P · Wing, Longeron/Stringer
  > CRACK FUEL TANK LOC. BTW RIB 21 AND RIB 22 STRINGER 9 INTERNAL AREA UPPER AFT POSITION AT RT WING 2023-470128<[01] REPAIRED STRINGER 9 INTERNAL AREA UPPER AFT POSITION BTW WSTA 617.0 TO WSTA 643.5 AND SKIN ATTACHMENT FLANGE AT RT WING I.A.W. EA 23-157-02451 AN
- [SDR SWAA2023090184763](https://openairdocs.org/sdr/SWAA2023090184763.md): Cargo Track · cracked · Aug 1, 2023 · N7832A · Boeing 73779P · Fuselage, Seat/Cargo Attach Fittings
  > CRACK TRACK ON BS 460 AT RBL 14 AT FWD CARGO COMPARTMENT 2023-470102<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X11290U021704; DUE DATE: 12 MAR 24.;[02] REPAIRED CARGO TRACK LOC. BTW BS 400 TO BS 500A RBL 14 AT FWD CARGO COMPARTMENT IAW
- [SDR SWAA2023090184594](https://openairdocs.org/sdr/SWAA2023090184594.md): Stringer · cracked · Aug 1, 2023 · N7832A · Boeing 73779P · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 26L LOCATED STA 540 FWD CARGO COMPARTMENT 2023-470108<[01] TOOL USED: ULTRASONIC THICKNESS GAGE. P/N: 35DL. S/N: 091419910. DUE DATE: 13-MAR-24.;[02] TOOL USED USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 60009161631 CAL DUE DATE: 31-JAN
- [SDR SWAA2023090184593](https://openairdocs.org/sdr/SWAA2023090184593.md): Stringer · cracked · Aug 1, 2023 · N7832A · Boeing 73779P · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 25L LOCATED STA 540 FWD CARGO COMPARTMENT 2023-470107<[01] TOOL USED: ULTRASONIC THICKNESS GAGE. P/N: 35DL. S/N: 091419910. DUE DATE: 13-MAR-24.;[02] TOOL USED USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 60009161631 CAL DUE DATE: 31-JAN
- [SDR SWAA2023090184592](https://openairdocs.org/sdr/SWAA2023090184592.md): Stringer · cracked · Aug 1, 2023 · N7832A · Boeing 73779P · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 23L LOCATED STA 540 FWD CARGO COMPARTMENT 2023-470106<[01] TOOL USED USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 60009161631 CAL DUE DATE: 31-JAN-24;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE:
- [SDR SWAA2023090184591](https://openairdocs.org/sdr/SWAA2023090184591.md): Stringer · cracked · Aug 1, 2023 · N7832A · Boeing 73779P · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 26R LOCATED STA 540 FWD CARGO COMPARTMENT 2023-470105<[01] TOOL USED USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 60009161631 CAL DUE DATE: 31-JAN-24;[02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 25-JA
- [SDR SWAA2023090184590](https://openairdocs.org/sdr/SWAA2023090184590.md): Stringer · cracked · Aug 1, 2023 · N7832A · Boeing 73779P · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 25R LOCATED STA 540 FWD CARGO COMPARTMENT 2023-470104<[01] TOOL USED: ULTRASONIC THICKNESS GAGE. P/N: 35DL. S/N: 091419910. DUE DATE: 13-MAR-24.;[02] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022237; DUE DATE: 26-JAN-24;
- [SDR SWAA2023090184589](https://openairdocs.org/sdr/SWAA2023090184589.md): Stringer · cracked · Aug 1, 2023 · N7832A · Boeing 73779P · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 23R LOCATED STA 540 FWD CARGO COMPARTMENT 2023-470103<[01] TOOL USED: ULTRASONIC THICKNESS GAGE. P/N: 35DL. S/N: 091419910. DUE DATE: 13-MAR-24.;[02] TOOL USED USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 60009161631 CAL DUE DATE: 31-JAN
- [SDR SWAA2023090184586](https://openairdocs.org/sdr/SWAA2023090184586.md): Stringer · cracked · Aug 1, 2023 · N7832A · Boeing 73779P · Fuselage Main, Longeron/Stringer
  > CRACK ON STRINGER 7L LOCATED BTW BS 294.5 TO BS 303.9 AT FWD GALLEY AREA 2023-470098<[01] ULTRASONIC EQUIPMENT USED P/N: 38DLPLUS; S/N:120398603 AND DUE DATE: 07-NOV-23.;[02] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512 AND DUE DATE: 17-DEC-23.

Next page: https://openairdocs.org/aircraft/N7832A/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 = 'N7832A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7832A/reports

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