# Service difficulty reports: N7833A

A list on [N7833A](https://openairdocs.org/aircraft/N7833A.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 · 250 reports

- [SDR SWAA2026042491970](https://openairdocs.org/sdr/SWAA2026042491970.md): Mount · cracked · Apr 23, 2026 · N7833A · Boeing 73779P · Escape Slide
  > PASSENGER CABIN FORWARD SERVICE DOOR AFT SLIDE MOUNT ISOLATOR IS CRACKED. REPLACED PASSENGER CABIN FORWARD SERVICE DOOR AFT SLIDE MOUNT ISOLATOR. IAW SRM 51-40-02.
- [SDR SWAA2026042491982](https://openairdocs.org/sdr/SWAA2026042491982.md): Battery Pack · failed · Apr 23, 2026 · N7833A · Boeing 73779P · Emergency Lighting
  > AFTER LT EMERGENCY BATTERY PACK M1672 FAILED CAPACITY CHECK. R&R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06
- [SDR SWAA2025093018958](https://openairdocs.org/sdr/SWAA2025093018958.md): Handle · loose · Sep 28, 2025 · N7833A · Boeing 73779P · Passenger/Crew Doors
  > PAX CABIN AFT LEFT DOOR ASSISTANT HANDLE LOOSE. TIGHTENED AFT LEFT DOOR ASSISTANT HANDLE IAW B737-700 AMM 52-13-31-400-802 STEP 3.G(2).
- [SDR SWAA2025093018959](https://openairdocs.org/sdr/SWAA2025093018959.md): Girt Bar · binding · Sep 28, 2025 · N7833A · Boeing 73779P · Emergency Equipment
  > PAX CABIN FWD SERVICE DOOR SLIDE GIRT BAR IS HARD TO CONNECT TO THE FLOOR SUPPORT FITTINGS. PERFORMED OPERATIONAL TEST ON SLIDE GIRT BAR FWD SERVICE DOOR IAW AMM 25-66-02-400-801 STEP 3.E; TEST IS OK.
- [SDR SWAA2025093018611](https://openairdocs.org/sdr/SWAA2025093018611.md): Light · burned · Sep 26, 2025 · N7833A · Boeing 73779P · Emergency Lighting
  > BURNED EMERGENCY LIGHT (1 EA) LOCATED BEHIND ACCESS PANEL 194FR AT LOWER FUSELAG. REPLACED EMERGENCY LIGHT (1 EA) LOCATED BEHIND ACCESS PANEL 194FR AT LOWER FUSELAGE IAW B737-700 AMM 33-51-04-960-801.OPERATIONAL TEST IS OK.
- [SDR SWAA2025093018610](https://openairdocs.org/sdr/SWAA2025093018610.md): Light · burned · Sep 26, 2025 · N7833A · Boeing 73779P · Emergency Lighting
  > BURNED EMERGENCY LIGHTS (2EA) LOCATED BEHIND ACCESS PANEL 194FL AT LOWER FUSELAGE AND LOCATED AT AFT ENTRY DOOR. REPLACED EMERGENCY LIGHTS (2EA) LOCATED BEHIND ACCESS PANEL 194FL AT LOWER FUSELAGE AND LOCATED AT AFT ENTRY DOOR IAW AMM 33-51-04-960-801 TEST
- [SDR SWAA2025093014344](https://openairdocs.org/sdr/SWAA2025093014344.md): Light · deteriorated · Sep 14, 2025 · N7833A · Boeing 73779P · Emergency Lighting
  > DETERIORATE PHOTOLUMINESCENT AT PASSENGER CABIN RH SIDE (7EA). THE REPLACEMENT PHOTOLUMINESCENT STRIP RH SIDE AT PASSENGER CABIN (7 EA) WILL BE ACCOMPLISHED IN TASK 733-080-00-01 (TTG8Q003FNTQ)
- [SDR SWAA2025093014343](https://openairdocs.org/sdr/SWAA2025093014343.md): Light · deteriorated · Sep 14, 2025 · N7833A · Boeing 73779P · Emergency Lighting
  > DETERIORATE PHOTOLUMINESCENT STRIP AT PASSENGER CABIN LH SIDE (7EA). THE REPLACEMENT PHOTOLUMINESCENT STRIP AT PASSENGER CABIN LH SIDE (7EA) WILL BE ACCOMPLISHED IN TASK 733-080-00-01 (TTG8Q003FNTQ).
- [SDR SWAA2025100213378](https://openairdocs.org/sdr/SWAA2025100213378.md): Angle · cracked · Sep 10, 2025 · N7833A · Boeing 73779P · Wing Miscellaneous Structure
  > CRACK ON ANGLE LOCATED ON ACCESS PANEL 651FB TRAILING EDGE AT RT WING. REPLACED ANGLE IAW SRM 51-10-02 ITEM 9, SRM 51-40-05, AND DWG#115A2710 SHEET 6 REV B DUE TO NOT FINDING ALLOWABLE DAMAGE IN SRM 57-51-02-1A-1. MEASUREMET OF CRACK IS L= 1.336.
- [SDR SWAA2025100213158](https://openairdocs.org/sdr/SWAA2025100213158.md): Paint · peeling · Sep 9, 2025 · N7833A · Boeing 73779P · Wing Structure
  > CORROSION SUPPORT STRUCTURE ACCESS PANEL 551FB TRAILING EDGE AT LT WING. PERFORMED DETAIL VISUAL INSPECTION ON SUPPORT STRUCTURE ACCESS PANEL 551FB TRAILING EDGE AT LT WING AND NO CORROSION FOUND, ONLY PEELING PAINT IAW SRM 51-10-02. NO MAINTENANCE ACTION IF
- [SDR SWAA2025100213026](https://openairdocs.org/sdr/SWAA2025100213026.md): Fairing · cracked · Sep 9, 2025 · N7833A · Boeing 73779P · Wing Main, Frame Structure
  > CRACKED FAIRING 644BB AT RT WING. PERFORMED PERMANENT REPAIR ON FAIRING PANEL 644BB AT RT WING IAW EA 25-157-02530-WIP1 AND STEPS ARE DOCUMENTED ON FAULT TTG8Q0157YT6.
- [SDR SWAA2025100113159](https://openairdocs.org/sdr/SWAA2025100113159.md): Web · corroded · Sep 9, 2025 · N7833A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION DOOR CUTOUT LOWER SILL BETWEEN BS 794 TO BS 847 AND STRINGER 25R AFT CARGO COMPARTMENT. REPLACED LOWER SILL LOCATED ON DOOR CUTOUT LOWER SILL BETWEEN BS 794 TO BS 847 AND STRINGER 25R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9; DWG: 14
- [SDR SWAA2025100113020](https://openairdocs.org/sdr/SWAA2025100113020.md): Plate · cracked · Sep 9, 2025 · N7833A · Boeing 73779P · Wing, Plate/Skin
  > CRACK CORRUGATED PLATE TRAILING EDGE ORSS 243, LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 243, LT WING IAW SRM 51-40-02-0G-0; DWG 115A2781 SHEET: 7 REV - AND DWG 115AA2001 SHEET: 87 REV -.
- [SDR SWAA2025100212827](https://openairdocs.org/sdr/SWAA2025100212827.md): Support Bracket · cracked · Sep 8, 2025 · N7833A · Boeing 73779P · Wing Miscellaneous Structure
  > CRACK TRAILING EDGE SUPPORT BRACKET ORSS 271 AT RT WING. REPLACED TRAILING EDGE SUPPORT BRACKET ORSS 271 AT RT WING IAW SRM 51-40-02; SRM 51-40-05 AND DWG 115A2930;SHEET 6 AND REV -. MEASURE OF CRACK IS 0.951.
- [SDR SWAA2025100112632](https://openairdocs.org/sdr/SWAA2025100112632.md): Angle · cracked · Sep 8, 2025 · N7833A · Boeing 73779P · Wing Miscellaneous Structure
  > CRACK ANGLE, TRAILING EDGE ORSS 271 AT LT WING. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, STEP 9, AND DWG 115A2930, SHEET 7, REV-. DUE TO DID NOT FIND ALLOWED DAMAGE IN SRM 57-51-02-1A-1.
- [SDR SWAA2025100112828](https://openairdocs.org/sdr/SWAA2025100112828.md): Plate · cracked · Sep 8, 2025 · N7833A · Boeing 73779P · Wing, Plate/Skin
  > CRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 RT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED ORSS 261 AT RT WING IAW SRM 51-40-02, & DWG 115A2714, SHEET 6, REV -. LENGTH OF CRACK IS 0.750 INCH.
- [SDR SWAA2025100112633](https://openairdocs.org/sdr/SWAA2025100112633.md): Bracket · cracked · Sep 8, 2025 · N7833A · Boeing 73779P · Wing Miscellaneous Structure
  > CRACK TRAILING EDGE SUPPORT BRACKET ORSS 297 AT LT WING. REPLACED TRAILING EDGE SUPPORT BRACKET AND FILLER ORSS 297, LT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 115A3712, SHEET 5, REV -.
- [SDR SWAA2025100112130](https://openairdocs.org/sdr/SWAA2025100112130.md): Floorbeam · cracked · Sep 6, 2025 · N7833A · Boeing 73779P · Fuselage Main, Floor Beam
  > CRACK BRAKE PANEL FLOOR STRUCTURE LOCATED BETWEEN BS540 AND BL0 TO LBL24.75 AT PASSENGER CABIN 2025-549876<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED BETWEEN BS540 AND BL0 TO LBL24.75 AT PASSENGER CABIN IAW. B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A0060
- [SDR SWAA2025100112132](https://openairdocs.org/sdr/SWAA2025100112132.md): Floor Support · cracked · Sep 6, 2025 · N7833A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK ANGLE FLOOR STRUCTURE, BS 695, BL 0. REPLACED THE FLOOR SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2025100112133](https://openairdocs.org/sdr/SWAA2025100112133.md): Floor Support · cracked · Sep 6, 2025 · N7833A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK ANGLE FLOOR SUPPORT, BS 695, RBL 24.75. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2025100111977](https://openairdocs.org/sdr/SWAA2025100111977.md): Stop Fitting · cracked · Sep 5, 2025 · N7833A · Boeing 73779P · Service Doors
  > CRACK AFT LOWER STOP FITTING SERVICE DOOR AT FWD GALLEY AND LAV. REPLACED STOP FITTING DOOR AND FASTENERS LOCATED ON AFT LOWER SERVICE DOOR AT FWD GALLEY AND LAV IAW SRM 51-40-02 AND DWG 141A6535 SHEET 1 REV.
- [SDR SWAA2025100111639](https://openairdocs.org/sdr/SWAA2025100111639.md): Scuff Plate · cracked · Sep 5, 2025 · N7833A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK FWD SCUFF PLATE LOCATED ON FWD CARGO DOOR CUT-OUT. REPAIRED AT CORNER FWD SCUFF PLATE LOCATED ON FWD CARGO DOOR CUT-OUT I. A.W. B737-700 SRM 53-30-15-2R-1; REPAIR 1.
- [SDR SWAA2025093011643](https://openairdocs.org/sdr/SWAA2025093011643.md): Floor Panel · delaminated · Sep 5, 2025 · N7833A · Boeing 73779P · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 242AF AT PASSENGER CABIN. REPAIRED THE FLOOR PANEL 242AF IAW SRM 53-00-50-2R-1, REPAIR 1, AND SRM 53-00-50-2R-0, REPAIR GENERAL.
- [SDR SWAA2025100111617](https://openairdocs.org/sdr/SWAA2025100111617.md): Scuff Plate · cracked · Sep 4, 2025 · N7833A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED AT FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I. A.W. B737-700 SRM 53-60-15-2R-1; REPAIR 1.
- [SDR SWAA2025020392336](https://openairdocs.org/sdr/SWAA2025020392336.md): Light · inoperative · Feb 2, 2025 · N7833A · Boeing 73779P · Emergency Lighting
  > L/H SLIDE EMERGENCY LIGHT INOP<[01] RE-LAMPED L/H SLIDE EMERGENCY LIGHT PER AMM 33-51-04.
- [SDR SWAA2024102250274](https://openairdocs.org/sdr/SWAA2024102250274.md): Seal · cracked · Oct 18, 2024 · N7833A · Boeing 73779P · Horizontal Stabilizer Miscellaneous Structure
  > RT HORIZONTAL STABILIZER UPPER FWD SLIDER SEAL CRACKED 4 INCHES ON THE FWD SIDE.<[01] REMOVED AND REPLACED SLIDER SEAL PER AMM 53-31-31.;[02] INSPECTED WORK PERFORMED. REMOVED AND REPLACED SLIDER SEAL PER AMM 53-31-31.
- [SDR SWAA2024102250275](https://openairdocs.org/sdr/SWAA2024102250275.md): Seal · cracked · Oct 18, 2024 · N7833A · Boeing 73779P · Horizontal Stabilizer Miscellaneous Structure
  > RT HORIZONTAL STABILIZER LOWER FWD SLIDER SEAL ATTACHMENT BRACKET BENT INWARDS AT A 45 DEGREE ANGLE AND IS CRACKING.<[01] REMOVED AND REPLACED SLIDER SEAL PER AMM 53-31-31.;[02] INSPECTED WORK PERFORMED. REMOVED AND REPLACED SLIDER SEAL PER AMM 53-31-31.
- [SDR SWAA2024090433088](https://openairdocs.org/sdr/SWAA2024090433088.md): Connector · disconnected · Sep 2, 2024 · N7833A · Boeing 73779P · Light System Wiring
  > DURING MV2 FOUND ROW 20ABC EMERGENCY LIGHT WONT TURN ON<[01] PERFORMED T/S IAW WDM 33-51-13-11 FOUND PLUG D11344 WAS DISCONNECTED. RECONNECTED PLUG D11344 EMERGENCY LIGHT AT ROW 20ABC OPS CHKED GOOD IAW AMM 33-51-00.
- [SDR SWAA2024072616856](https://openairdocs.org/sdr/SWAA2024072616856.md): Skin · cracked · May 30, 2024 · N7833A · Boeing 73779P · Leading Edge Devices
  > DID UPPER R/H WING POST DOCK AND FOUND R/H LEADING EDGE #5 SLAT CRACK. CRACK IS 0.800 IN LENGTH LATERALLY. CRACK IS AT #5 SLAT STATION 89.69 (17.75 FROM TRAILING EDGE AND 62.50 FROM INBOARD EDGE).<[01] INSTALLED #5 SLAT WITH INBD AND OUTBD MAIN TRACKS AND SLAT
- [SDR SWAA2023101608720](https://openairdocs.org/sdr/SWAA2023101608720.md): Battery · inoperative · Oct 6, 2023 · N7833A · Boeing 73779P · Emergency Equipment
  > AFT FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHTS ARE NOT FLASHING. ( 2 EA. REQUIRED)<[01] REPLACED BATTERY'S AT AFT FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHTS (2EA) AS PER AMM 25-64-00-900-806;[02] VERIFIED STEP 1.
- [SDR SWAA2023101707853](https://openairdocs.org/sdr/SWAA2023101707853.md): Battery Pack · inoperative · Oct 5, 2023 · N7833A · Boeing 73779P · Emergency Lighting
  > EMERGENCY LIGHT INOP FOR POWER SUPPLY/BATTERY PACK M1673<[01] REMOVE & REPLACE BATTERY PACK M1673 PER B737 AMM 33-51-06-960-805. PERFORM TEST OF BATTERY PACK OER B737 AMM 33-51-06-960-805 TEST PASSED;[02] VERIFIED STEP # 1
- [SDR SWAA2023101704639](https://openairdocs.org/sdr/SWAA2023101704639.md): Flap · delaminated · Sep 26, 2023 · N7833A · Boeing 73779P · Trailing Edge Flaps
  > LEFT WING O/B AFT FLAP I/B UPPER TRAILING EDGE TIP DELAMINATED DOT 223-LWAF2.<[01] FINAL STATEMENT: ACCOMPLISHED UT DISBOND INSP. ON UPPER SKIN AT LEFT WING O/B AFT I/B TRAILING EDGE IAW B737 NDT PART 1; 51-04-00 AND PART 4; 51-00-05. DISBOND NOTED; DAMAGE SIZ
- [SDR SWAA2023101704304](https://openairdocs.org/sdr/SWAA2023101704304.md): Flap · delaminated · Sep 25, 2023 · N7833A · Boeing 73779P · Trailing Edge Flaps
  > LEFT WING OUB AFT FLAP INB END LOWER TRAILING EDGE TIP DELAMINATED MKD DOT<[01] FINAL STATEMENT: REMOVED AND REPLACED L/H O/B AFT FLAP REF AMM 27-51-22-000-81 AND 27-51-22-400-801;[02] FINAL INSPECTION; LEFT O/B AFT FLAP REPLACED.
- [SDR SWAA2023101602510](https://openairdocs.org/sdr/SWAA2023101602510.md): Floor Panel · cracked · Sep 19, 2023 · N7833A · Boeing 73779P · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT PANEL 142KW IS CRACKED AT EDGE(MARKED)<[01] RECIEVED NEW AFT CARGO PANEL # 142KW; WILL BE INSTALLED ON TASK CARD# TTG8Q00MVWFY.;[02] FINAL INSPECTION; RECIEVED NEW AFT CARGO PANEL; WILL BE INSTALLED ON TASK CARD# TTG8Q00MVWFY.
- [SDR SWAA2023101700420](https://openairdocs.org/sdr/SWAA2023101700420.md): Panel · elongated · Sep 13, 2023 · N7833A · Boeing 73779P · Wing, Plate/Skin
  > LEADING EDGE PANEL 521CB HAS MULTIPLE ELONGATED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #521CB AS MARKED AS PER B737 SRM 57-41-01-2R-1; B737 SRM 51-70-04-2R-9 PARAG (4-D-M) AND B737 SRM 51-70-04-2R-0 PARAG (4-L-M-N). MATERIAL USED
- [SDR SWAA2023101700424](https://openairdocs.org/sdr/SWAA2023101700424.md): Panel · elongated · Sep 13, 2023 · N7833A · Boeing 73779P · Wing, Plate/Skin
  > LEADING EDGE PANEL 511AT HAS ELONGATED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #511AT AS MARKED AS PER B737 SRM 57-41-01-2R-1; B737 SRM 51-70-04-2R-9 PARAG (4-D-M) AND B737 SRM 51-70-04-2R-0 PARAG (4-L-M-N). MATERIAL USED PO#179112
- [SDR SWAA2023101700425](https://openairdocs.org/sdr/SWAA2023101700425.md): Panel · elongated · Sep 13, 2023 · N7833A · Boeing 73779P · Wing, Plate/Skin
  > LEADING EDGE PANEL 521FB HAS ELONGATED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #521FB AS MARKED AS PER B737 SRM 57-41-01-2R-1; B737 SRM 51-70-04-2R-9 PARAG (4-D-M) AND B737 SRM 51-70-04-2R-0 PARAG (4-L-M-N). MATERIAL USED PO#179112
- [SDR SWAA2023101798941](https://openairdocs.org/sdr/SWAA2023101798941.md): Slide · out of adjust · Sep 11, 2023 · N7833A · Boeing 73779P · Escape Slide
  > FWD ENTRY DOOR. L1. SLIDE PRESSURE VISOR IS TORN.<[01] RECEIVED PART AND INSTALLATION WILL BE ACCOMPLISHED ON T/C MT 725-61-06;<BR>SLIDE REM/INSTL TTG8Q00NC3V2;[02] VERIFIED STEP 1
- [SDR SWAA2023101799116](https://openairdocs.org/sdr/SWAA2023101799116.md): Sidewall Support · elongated · Sep 11, 2023 · N7833A · Boeing 73779P · Fuselage Miscellaneous Structure
  > FWD CABIN WET AREA L/H SIDE WALL SUPPORT CLIP HOLE ELONGATED @ S-10L STA 270 MKD DOT<[01] REMOVED AND REPLACED SUPPORT CLIP AT FWD CABIN WET AREA L/H SIDE WALL; STA 270; S-10L AS PER B737-700 SRM 51-40-02-0G-0; DWG# 141A9502.;[02] VERIFIED STEP 1 REMOVAL AND R
- [SDR SWAA2023101799112](https://openairdocs.org/sdr/SWAA2023101799112.md): Floor Support · cracked · Sep 11, 2023 · N7833A · Boeing 73779P · Fuselage Miscellaneous Structure
  > MAIN CABIN CENTER WING BOX FLOOR SUPPORT BREAK CRACKED AT FASTENER'S TAIL RBL 1 STA 540<[01] REMOVED AND REPLACED SUPPORT BREAK ASSY AT MAIN CABIN STA 540 BETWEEN BL 0 TO RBL 24 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 143A0060.;[02] VERIFIED STEP 1 COMPLETE.
- [SDR SWAA2023101799114](https://openairdocs.org/sdr/SWAA2023101799114.md): Angle · corroded · Sep 11, 2023 · N7833A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION AT RIVETS TAILS 4EA ATTACHED ANGLE ABOVE L-1 DOOR STA 328<[01] REMOVED AND REPLACED 4EA RIVETS AT UPPER FUSELAGE SKIN ATTACHED ANGLE ABOVE L-1 DOOR STA 328 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 141A8240.;[02] VERIFIED STEP 1 COMPLETE.
- [SDR SWAA2023101799115](https://openairdocs.org/sdr/SWAA2023101799115.md): Angle · corroded · Sep 11, 2023 · N7833A · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION AT SEVERAL RIVETS TAILS ATTACHED ANGLE ABOVE L-1 DOOR STA 328+ 10' MKD DOT<[01] REMOVED AND REPLACED RIVETS AT UPPER FUSELAGE SKIN ATTACHED ANGLE ABOVE L-1 DOOR STA 328+10' REF B737-700 SRM 51-40-02-0G-0 AND DWG # 141A8240.;[02] VERIFIED S5EP 1 COMPL
- [SDR SWAA2023101798929](https://openairdocs.org/sdr/SWAA2023101798929.md): Floor Support · cracked · Sep 10, 2023 · N7833A · Boeing 73779P · Fuselage Miscellaneous Structure
  > BELOW CABIN FLOOR SUPPORT BREAK CRACKED AT CENTER WING BOX LBL 2 STA 540<[01] REMOVED AND REPLACED SUPPORT BREAK ASSY AT MAIN CABIN STA 540 BETWEEN BL 0 TO LBL 24 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 143A0060.;[02] VERIFIED STEP 1 REMOVAL AND REPLACEMENT OF
- [SDR SWAA2023101798488](https://openairdocs.org/sdr/SWAA2023101798488.md): Access Panel · corroded · Sep 8, 2023 · N7833A · Boeing 73779P · Fuselage Structure (General)
  > ***CORROSSION*** FWD CARGO COMPARTMENT FLOOR ACCESS PANEL # 120BF HAS LIGHT CORROSSION<[01] REMOVED CORROSION AT FWD CARGO COMPARTMENT FLOOR ACCESS PANEL #120BF PER SRM 51-10-02-0G-0<BR>EVALUATED REWORKED AREA. ORIGINAL MATERIAL THICKNESS: 0.071'; MATERIAL LOS
- [SDR SWAA2023101798489](https://openairdocs.org/sdr/SWAA2023101798489.md): Access Panel · corroded · Sep 8, 2023 · N7833A · Boeing 73779P · Fuselage Structure (General)
  > ***CORROSSION*** FWD CARGO COMPARTMENT FLOOR ACCESS PANEL # 120AF HAS LIGHT CORROSSION<[01] REMOVED CORROSION AT FWD CARGO COMPARTMENT FLOOR ACCESS PANEL #120AF PER SRM 51-10-02-0G-0<BR>EVALUATED REWORKED AREA. ORIGINAL MATERIAL THICKNESS: 0.071'; MATERIAL LOS
- [SDR SWAA2023101798490](https://openairdocs.org/sdr/SWAA2023101798490.md): Access Panel · corroded · Sep 8, 2023 · N7833A · Boeing 73779P · Fuselage Structure (General)
  > ***CORROSSION*** FWD CARGO COMPARTMENT FLOOR ACCESS PANEL # 120CF HAS LIGHT CORROSSION<[01] REMOVED CORROSION AT FWD CARGO COMPARTMENT FLOOR ACCESS PANEL #120CF PER SRM 51-10-02-0G-0<BR>EVALUATED REWORKED AREA. ORIGINAL MATERIAL THICKNESS: 0.071'; MATERIAL LOS
- [SDR SWAA2023101699598](https://openairdocs.org/sdr/SWAA2023101699598.md): Support Angle · cracked · Sep 7, 2023 · N7833A · Boeing 73779P · Fuselage Main, Bulkhead
  > RIGHT VAPOR BARRIER UPPER SUPPORT ANGLE STA 663 FOUND CRACK AT RBL 7.<[01] REPAIRED AREA AT VAPOR BARRIER UPPER SUPPORT ANGLE STA 663 AS PER B 737-700 SRM 57-10-10-2R-5 FIG 202 SHEET 4;[02] VERIFIED; STEP # 1.
- [SDR SWAA2023101797257](https://openairdocs.org/sdr/SWAA2023101797257.md): Skin · cracked · Sep 6, 2023 · N7833A · Boeing 73779P · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON LOWER SKIN OF R/H HORIZONTAL STABILIZER AT STAB STA 193.90; 8.5' FROM FRONT SPAR; I/B ROW. CRACK LENGTH: 1'. CRACK FOUND ON LOWER SKIN OF R/H HORIZONTAL STABILIZER AT STAB STA 193.90 8.5' FROM FRONT SPAR I/B ROW. CRACK LENGTH: 1'.<[01] STEP 12
- [SDR SWAA2023101797421](https://openairdocs.org/sdr/SWAA2023101797421.md): Slat · pulled · Sep 6, 2023 · N7833A · Boeing 73779P · Leading Edge Devices
  > LEFT WING # 3 SLAT ACTUATOR LOWER SURFACE OF L/E HAS SIX FASTENERS PULLED IN.<[01] CUT DAMAGED AND FABRICATE REPAIR PARTS DOUBLER AND FILLER. EVALAUTED SURFACE ROUGHNESS ON CUT EDGES FOUND SMOOTHER THAN 63 MICROINCHES RA. AND FOUND SMOOTHER THAN 125 MICROINCHE
- [SDR SWAA2023101797427](https://openairdocs.org/sdr/SWAA2023101797427.md): Slat · pulled · Sep 6, 2023 · N7833A · Boeing 73779P · Leading Edge Devices
  > LEFT WING # 2 SLAT ACTUATOR LOWER SURFACE OF L/E HAS SEVEN FASTENERS PULLED IN.<[01] CRACK FOUND ON #2 SLAT ACTUATOR FITTING. SLAT REPLACEMENT TO BE ACCOMPLISHED ON NR #TTG8Q00NSYZE.;[02] VERIFIED STEP 1.

Next page: https://openairdocs.org/aircraft/N7833A/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 = 'N7833A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7833A/reports

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