# Service difficulty reports: N7826B

A list on [N7826B](https://openairdocs.org/aircraft/N7826B.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 6 · 256 reports

- [SDR SWAA2026102046931](https://openairdocs.org/sdr/SWAA2026102046931.md): Handle · loose · Oct 16, 2026 · N7826B · Boeing 73779P · Service Doors
  > FWD L1 PAX DOOR INNER HANDLE LOOSE. SECURED THE FWD ENTRY DOOR HANDLE HARDWARE IAW AMM 52-11-31, & OPS CHKD GOOD.
- [SDR SWAA2026100849482](https://openairdocs.org/sdr/SWAA2026100849482.md): Handle · broken · Oct 4, 2026 · N7826B · Boeing 73779P · Extinguishing System
  > FIRE EXTINGUISHER HANDLE BROKEN IN THE FLIGHT DECK. R & R THE FIRE EXTINGUISHER IAW AMM. 26-26-01.
- [SDR SWAA2025122354471](https://openairdocs.org/sdr/SWAA2025122354471.md): Handle · loose · Dec 20, 2025 · N7826B · Boeing 73779P · Service Doors
  > R2 DOOR GRAB HANDLE IS LOOSE. ADJUSTED R2 DOOR GRAB HANDLE IAW SOPM 20-50-01.
- [SDR SWAA2025111735581](https://openairdocs.org/sdr/SWAA2025111735581.md): Panel · cracked · Nov 15, 2025 · N7826B · Boeing 73779P · Rudder Structure
  > WHEN REMOVING SEAL FOUND CRACK ON COVE PANEL. PERMANENT REPAIR ACCOMPLISHED PER SRM 55-40-30-1A-1.
- [SDR SWAA2025110731515](https://openairdocs.org/sdr/SWAA2025110731515.md): Girt Bar · out of adjust · Nov 4, 2025 · N7826B · Boeing 73779P · Emergency Equipment
  > AFT GALLEY L2 DOOR GIRT BAR HANGS LOW. SECURED L2 DOOR EMERGENCY SLIDE GIRT BAR IAW SIP.
- [SDR SWAA2025081300006](https://openairdocs.org/sdr/SWAA2025081300006.md): Light · burned · Aug 9, 2025 · N7826B · Boeing 73779P · Emergency Lighting
  > PAX CABIN 2 EA EMERGENCY LIGHT BURNED AT 11R AND 16R SEATS POSITIONS. REPLACED PAX CABIN 2 EA EMERGENCY LIGHT AT 11R AND 16R SEATS POSITIONS. I.A.W B737-700 AMM 33-51-03-960-802 STEP 2.D.(4) TEST ARE OK.
- [SDR SWAA2025081493375](https://openairdocs.org/sdr/SWAA2025081493375.md): Web · corroded · Jul 20, 2025 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION WEB LOWER SILL LOCATED BETWEEN BS 440 - 492.4 AND RBL 26, WL 156 AT FWD CARGO COMPARTMENT. REPLACED WEB LOWER SILL AND FASTENERS LOCATED BETWEEN STA440 TO STA492.4 AND RBL26 WL156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02-0
- [SDR SWAA2025081493373](https://openairdocs.org/sdr/SWAA2025081493373.md): Angle · cracked · Jul 20, 2025 · N7826B · Boeing 73779P · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED IRSS 141 AT RT WING. REPLACED ANGLE TRAILING EDGE LOCATED IRSS 141 AT RT WING IAW SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9. MEASURED OF CRACK IS L: 1.631.
- [SDR SWAA2025081493143](https://openairdocs.org/sdr/SWAA2025081493143.md): Angle · cracked · Jul 19, 2025 · N7826B · Boeing 73779P · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED IRSS 141 AT LT WING. REPLACED ANGLE TRAILING EDGE LOCATED IRSS 141 AT LT WING IAW SRM 51-40-02, AND SRM 51-10-02, PARAGRAPH 9, AND DWG 115A2000, SHEET 21, REV -. LENGTH OF CRACK IS L: 0.841 INCHES.
- [SDR SWAA2025081493140](https://openairdocs.org/sdr/SWAA2025081493140.md): Plate · cracked · Jul 19, 2025 · N7826B · Boeing 73779P · Wing Miscellaneous Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT LT WING IAW SRM 51-40-02; SRM 51-10-02 AND DWG 115A2001, SHEET 30, REV A.
- [SDR SWAA2025081393153](https://openairdocs.org/sdr/SWAA2025081393153.md): Light · broken · Jul 19, 2025 · N7826B · Boeing 73779P · Emergency Lighting
  > BROKEN GALLEY 1 EMERGENCY EXIT BASE AT FWD GALLEY AREA. REPLACED GALLEY 1 EMERGENCY EXIT BASE AT FWD GALLEY AREAI.A.W. BOEING 737-700 AMM 33-51-01-960-802. TEST IS OK.;
- [SDR SWAA2025081492540](https://openairdocs.org/sdr/SWAA2025081492540.md): Pressure Web · cracked · Jul 18, 2025 · N7826B · Boeing 73779P · Fuselage Main, Structure
  > CRACK INDICATION FOUND AT HORIZONTAL PRESSURE DECK WEB BETWEEN STA 663 TO STA 675 AT LBL 31 AT MAIN WHEEL WELL COMPARTMENT CRACK LENGTH: 0.500 INCHES APPROX. REPAIRED FLOOR STRUCTURE PAX CABIN HORIZONTAL PRESSURE DECK WEB BTW BSTA 663.75 AND BSTA 675 AND BTW
- [SDR SWAA2025081392833](https://openairdocs.org/sdr/SWAA2025081392833.md): Handle · deteriorated · Jul 18, 2025 · N7826B · Boeing 73779P · Passenger/Crew Doors
  > DETERIORATED ASSIST HANDLE NUT ON FORWARD ENTRY DOOR LINING AT FORWARD GALLEY AREA (4EA). REPLACED ASSIST HANDLE NUT ON FORWARD ENTRY DOOR LINING AT FORWARD GALLEY AREA (4EA) IAW AMM 52-11-31-400-802 STEP 3.G.(2)(A).
- [SDR SWAA2025081492536](https://openairdocs.org/sdr/SWAA2025081492536.md): Floorbeam · cracked · Jul 17, 2025 · N7826B · Boeing 73779P · Fuselage Main, Floor Beam
  > CRACK FLOOR STRUCTURE BRAKE PANEL BS 540 AND RBL 1 AT PASSENGER CABIN. REPLACED FLOOR STRUCTURE BRAKE PANEL BS 540 AND BTW RBL 0 TO RBL 24.75 PASSENGER CABIN IAW SRM 51-10-02 PRAG 9; SRM 51-40-02 AND DRAWING 143A0060 SHEET: 36 REV: A.
- [SDR SWAA2025081492537](https://openairdocs.org/sdr/SWAA2025081492537.md): Floorbeam · cracked · Jul 17, 2025 · N7826B · Boeing 73779P · Fuselage Main, Floor Beam
  > CRACK FLOOR STRUCTURE BRAKE PANEL BS 540 AND LBL 1 AT PASSENGER CABIN. REPLACED FLOOR STRUCTURE BRAKE PANEL LOCATED ON BS 540 AND LBL 1 AT PASSENGER CABIN IAW SRM 51-40-02; AND SRM 51-10-02-0G-0 PARAGRAPH 9.
- [SDR SWAA2025081492290](https://openairdocs.org/sdr/SWAA2025081492290.md): Rib · cracked · Jul 17, 2025 · N7826B · Boeing 73779P · Horizontal Stabilizer, Spar/Rib
  > CRACK ON INSPAR RIB 3 HSS 111.10 AT 38 INCHES FROM FRONT SPAR (STIFFENER 4) RT HORIZONTAL STAB. PERFORMED REPAIRED ON INSPAR RIB 3(STAB STA 111.10) AT 38 INCHES FROM FRONT SPAR RH HORIZONTAL STAB IAW SRM 55-10-09-2R-4 REPAIR 4.
- [SDR SWAA2025081491965](https://openairdocs.org/sdr/SWAA2025081491965.md): Panel · elongated · Jul 16, 2025 · N7826B · Boeing 73779P · Wing Miscellaneous Structure
  > ELONGATED HOLES ON ACCESS PANEL 561BB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WIN IAW SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2025081491720](https://openairdocs.org/sdr/SWAA2025081491720.md): Angle · cracked · Jul 15, 2025 · N7826B · Boeing 73779P · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE ORSS 271 RT WING. REPLACED ANGLE TRAILING EDGE ORSS 271, RT WING IAW SRM 51-10-02-0G-0 ITEM 9, SRM 51-40-02-0G-0, AND DWG 115A2930, SHEET 8, REV -.
- [SDR SWAA2025081491722](https://openairdocs.org/sdr/SWAA2025081491722.md): Support Bracket · cracked · Jul 15, 2025 · N7826B · Boeing 73779P · Wing Miscellaneous Structure
  > CRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 AT LT WING. REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 AT LT WING IAW SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 115A2930, SHEET 6 REV -. MEASUREMENT OF CRACK IS L: 0.225.
- [SDR SWAA2025081491393](https://openairdocs.org/sdr/SWAA2025081491393.md): Access Panel · damaged · Jul 14, 2025 · N7826B · Boeing 73779P · Aerodynamic Fairings
  > ELONGATED HOLE ON ACCESS PANEL 193B, BODY FAIRING AT LOWER FUSELAGE. REPAIRED THE ACCESS PANEL 193B, BODY FAIRING AT LOWER FUSELAGE IAW SRM 51-70-04-2R-9 REPAIR 9.
- [SDR SWAA2024080722092](https://openairdocs.org/sdr/SWAA2024080722092.md): Light · inoperative · Aug 3, 2024 · N7826B · Boeing 73779P · Emergency Lighting
  > FWD SERVICE DOOR ESCAPE SLIDE LIGHT INOP<[01] REPLACED FWD SERVICE DOOR SLIDE LIGHT REF AMM 33-51-04
- [SDR SWAA2024052387943](https://openairdocs.org/sdr/SWAA2024052387943.md): Landing Gear · failed · May 20, 2024 · N7826B · Boeing 73779P · Nose/Tail Landing Gear
  > AFTER T/O AND AIRCRAFT IN CLEAN CONFIGURATION FO PUT THE GEAR HANDLE IN 'OFF' POSITION. NOSE GEAR EXTENED; MAIN DID NOT.<[01] 02 - INSPECTED PER [AMM 32-33-00-710-801-NG (OPERATIONAL TEST FOR THE NOSE LANDING GEAR - PERMANENT)]
- [SDR SWAA2023092101771](https://openairdocs.org/sdr/SWAA2023092101771.md): Light · inoperative · Sep 18, 2023 · N7826B · Boeing 73779P · Emergency Lighting
  > EMERGENCY EXIT AREA LIGHT IN RIGHT OVERWING ESCAPE HATCH INOP<[01] RELAMPED EMERGENCY EXIT AREA LIGHT IN RIGHT OVERWING ESCAPE HATCH AND TESTED GOOD IAW AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2023092199509](https://openairdocs.org/sdr/SWAA2023092199509.md): Scuff Plate · cracked · Sep 12, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] WELDED AFT CARGO BAY AFT CORNER SCUFF PLATE PER SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2); (4); (5) USING ER4043 FILLER ROD LOT NUMBER 1131216<BR>EQUIPMENT USED; WELDING MACHINE E10583 CALIBRATION DUE DATE 01/20
- [SDR SWAA2023092199508](https://openairdocs.org/sdr/SWAA2023092199508.md): Scuff Plate · cracked · Sep 12, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<
- [SDR SWAA2023092195952](https://openairdocs.org/sdr/SWAA2023092195952.md): Baffle · cracked · Sep 1, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > FCB BAFFLE IS CRACKED BETWEEN BS 400 TO BS 420 LBL 24 WL 156<[01] REMOVED AND REPLACED FCB BAFFLE BETWEEN BS400 TO BS420;LBL24;WL156.IAW SRM 51-40-02 AND DWG#143A7505 REV B.;[02] TASK CARD COMPLETE
- [SDR SWAA2023092195951](https://openairdocs.org/sdr/SWAA2023092195951.md): Baffle · cracked · Sep 1, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > FCB BAFFLE IS CRACKED BETWEEN BS 400 TO BS 420 LBL 24 WL 156<
- [SDR SWAA2023092593244](https://openairdocs.org/sdr/SWAA2023092593244.md): Skin · corroded · Aug 24, 2023 · N7826B · Boeing 73779P · Fuselage Main, Plate/Skin
  > SURFACE CORROSION ON UPPER CROWN SKIN UNDER VERT STAB FUSELAGE STA 1016 TO STA 1040 AND FROM STRINGERS S-2AR TO S-2AL.<[01] REMOVED FASTENERS BETWEEN BS1016- BS1040 FROM STR2AL-STR2AR IAW SRM 51-40-0<BR>1. ROIG; JOSUE (PENDING)<BR>01-SEP-2023 16:43:36<BR>EVALU
- [SDR SWAA2023092592616](https://openairdocs.org/sdr/SWAA2023092592616.md): Seal · cracked · Aug 22, 2023 · N7826B · Boeing 73779P · Horizontal Stabilizer Structure
  > RT HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND INSTALLED NEW RT HORIZONTAL STAB FWD UPPER SLIDE SEAL PER AMM 53-31-31.;[02] FINAL INSPECTION. JOB COMPLETE.;[03] FINAL INSPECTION. JOB COMPLETE.
- [SDR SWAA2023092592618](https://openairdocs.org/sdr/SWAA2023092592618.md): Track · cracked · Aug 22, 2023 · N7826B · Boeing 73779P · Horizontal Stabilizer Structure
  > RT HORIZONTAL STAB UPPER FWD TRACK FOR PANEL 343AT CRACKED.<[01] REMOVED AND REPLACED RT HORIZONTAL STAB UPPER FWD TRACK FOR PANEL 343AT PER AMM 20-50-11-910-801 TABLE 204 AND RESTORED DECORATIVE FINISH PER AMM 51-21-99-300 801;[02] INSPECTED AND VERIFIED CORR
- [SDR SWAA2023092592598](https://openairdocs.org/sdr/SWAA2023092592598.md): Support · corroded · Aug 22, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727+7 - 747+2; RBL 21; WL 156<[01] EFFECTIVITY SRM 53-60-53-0I-2 IDENTIFICATION 2 AND SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 ARE APPLICABLE TO A/C.;[02] VALIDATED APPLICABILITY SRM 53-00-53-1A-2 ALLOWABLE
- [SDR SWAA2023092192080](https://openairdocs.org/sdr/SWAA2023092192080.md): Shield · corroded · Aug 22, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION ON FORWARD CARGO COMPARTMENT DOOR CUT-OUT AFT SHIELD FROM STA 500 TO 500A; RBL 24; WL 156.<[01] THE STRUCTURAL ITEM DOES NOT HAVE ALLOWABLE DAMAGE ENTRIES. THEREFORE; MUST BE REPAIRED BY REPLACEMENT PER REF SRM 51-10-02-0G-0 PARAGRAPH 9;[02] REPLACED
- [SDR SWAA2023092192081](https://openairdocs.org/sdr/SWAA2023092192081.md): Web · corroded · Aug 22, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION ON FORWARD CARGO BAY DOOR CUT-OUT SUB-THRESHOLD WEB FROM STA 440+11 TO 460+10; RBL 28 TO 30; WL 156.<[01] VERIFIED APLICABILITY SRM 53-30-53-0I-2 FOR IDENTIFICATION<BR>AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE;[02] VERIFIED PARTIAL UPDATES FOR STEPS
- [SDR SWAA2023092192077](https://openairdocs.org/sdr/SWAA2023092192077.md): Sidewall Support · corroded · Aug 22, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT STA 500A+2; +6; +10; +14; +18; 500B+2; +6; +18; RBL 24; WL 158.<[01] REPLACED ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BETWEEN BS 500A - BS500D RBL.24 WL 156.5 IAW SRM 51-10-02; PARAG.9.C. DWG# 143A
- [SDR SWAA2023092192078](https://openairdocs.org/sdr/SWAA2023092192078.md): Sidewall Support · corroded · Aug 22, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT ANGLE AT STA 500C+2; +16; +18; RBL 24; WL 156.<[01] CORROSION AT SUPPORT ANGLE OF FWD CARGO BAY FLOOR SIDEWALL ON STA 500C+2; +16; +18; RBL 24; WL 156. PART WILL BE REPLACED AND ALL MAINTENANCE ACTIONS ACCOM
- [SDR SWAA2023092192079](https://openairdocs.org/sdr/SWAA2023092192079.md): Shield · corroded · Aug 22, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO DOOR CUT-OUT FWD SHIELD AT STA 420+6 & 420+9; WL 156; RBL 24.<[01] THE STRUCTURAL ITEM DOES NOT HAVE ALLOWABLE DAMAGE ENTRIES. THEREFORE; MUST BE REPAIRED BY REPLACEMENT PER REF SRM 51-10-02-0G-0 PARAGRAPH 9;[02] VERIFIED STEP 2 IN PARTI
- [SDR SWAA2023092192082](https://openairdocs.org/sdr/SWAA2023092192082.md): Sidewall Support · corroded · Aug 22, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT ANGLE AT STA 460+18; 480+6; +10; 500A+14; 500B+17; 500C+13; LBL 24; WL 156.<[01] VERIFIED APPLICABILITY SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.;[02] SEE STEP 3 FOR APPLICABILITY FOR ALLOWABLE DAMAGE;[03] VER
- [SDR SWAA2023092192594](https://openairdocs.org/sdr/SWAA2023092192594.md): Support · corroded · Aug 22, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > AFT CARGO HAS CORROSION ON FWD BULKHEAD SUPPORT AT BS 727+4; LBL 22; WL 155<[01] REMOVED AND REPLACED AFT CARGO FWD BULKHEAD SUPPORT AT BS727+4 PER SRM 51-40-02 AND DWG 144A9401;[02] VERIFIED MEASUREMENT TABLE.;[03] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2023092192596](https://openairdocs.org/sdr/SWAA2023092192596.md): Sidewall Support · corroded · Aug 22, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727B+4 - 727E+10; LBL 21; WL 156<[01] REMOVED AND REPLACED AFT CARGO FLOOR TO SIDEWALL SUPPORT FROM BS 727 TO BS 847 IAW SRM 51-40-02 AND DWG 146A7500.;[02] VERIFIED MEASUREMENT TABLE.<BR>TASK COMPLETE
- [SDR SWAA2023092192602](https://openairdocs.org/sdr/SWAA2023092192602.md): Sidewall Support · corroded · Aug 22, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727E+14 - 787+2; LBL 21; WL 157<[01] THIS CARD WILL BE ACCOMPLISHED ON CUSTOMER CARD NBR: TTG8Q00MZS35;[02] VERIFIED.<BR>VERIFIED MEASUREMENTS.
- [SDR SWAA2023092192604](https://openairdocs.org/sdr/SWAA2023092192604.md): Support · corroded · Aug 22, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > AFT CARGO AFT BULKHEAD SUPPORT HAS CORROSION AT BS 927; RBL 13; WL 180<[01] THIS FAULT WILL BE ACCOMPLISHED ON NRC #: TTG8Q00MZT48;[02] TASK CARD COMPLETE
- [SDR SWAA2023092192614](https://openairdocs.org/sdr/SWAA2023092192614.md): Support · corroded · Aug 22, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous Structure
  > AFT CARGO AFT BULKHEAD SUPPORT HAS CORROSION AT BS 927; LBL 3; WL 180<[01] OK TO INSTALL GIVEN;[02] REMOVED AND REPLACED AFT CARGO AFT BULKHEAD SUPPORT PER SRM 51-40-02 AND DWG 1498118.;[03] VERIFIED CORRECTIVE ACTION 2.
- [SDR SWAA2023092192084](https://openairdocs.org/sdr/SWAA2023092192084.md): Attach Angle · cracked · Aug 22, 2023 · N7826B · Boeing 73779P · Fuselage Main, Attach Fittings
  > CRACK ON FWD CARGO BAY BAFFLE ATTACH ANGLE AT STA 400+19.5; WL 155; RBL 24.<[01] REMOVED AND REPLACED FWD CARGO BAY BAFFLE ATTACH ANGLE AT STA 400+19.5; WL 155; RBL 24 IAW SRM 51-40-02 AND DWG # 143A7505;[02] VERIFIED STEP 1;[03] TASK CARD COMPLETE
- [SDR SWAA2023092190827](https://openairdocs.org/sdr/SWAA2023092190827.md): Stringer · cracked · Aug 18, 2023 · N7826B · Boeing 73779P · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26R WL153. MARKED<[01] REPAIRED STRINGER NBR 26RH PER REF SRM 53-00-03-2R-1;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE.
- [SDR SWAA2023092190828](https://openairdocs.org/sdr/SWAA2023092190828.md): Stringer · cracked · Aug 18, 2023 · N7826B · Boeing 73779P · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-27R WL150. MARKED<[01] VERIFIED STEP 4 COMPLETE; STEP 5 IN PARTIAL OK TO INSTALL GIVEN.;[02] REPAIRED FCB STRINGER 27R BETWEEN BS 500D AND 540 IAW SRM 53-00-03-2R-1 REPAIR 1;[03] VERIFIED MEASUREMENT TABLE.;[04] VERI
- [SDR SWAA2023092190829](https://openairdocs.org/sdr/SWAA2023092190829.md): Stringer · cracked · Aug 18, 2023 · N7826B · Boeing 73779P · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-23R WL164. MARKED<[01] VERIFIED STEPS 4 AND 5.;[02] RECEIVED NEW STRINGER SECTION FROM OSS ITEM HFAB53-STR-011 LOT NBR 1537299-1 AND PO NBR 934384 AND HAT CHANNEL ITEM 69-78188-1 LOT NBR 1530303-1.<BR><BR>LOCATED AND
- [SDR SWAA2023092190830](https://openairdocs.org/sdr/SWAA2023092190830.md): Stringer · cracked · Aug 18, 2023 · N7826B · Boeing 73779P · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26L WL153. MARKED<[01] PERFOMED STRINGER REPAIR PER REF SRM 53-00-03-2R-1;[02] VERIFIED CORRECTIVE ACTION 1.;[03] VERIFIED MEASUREMENT TABLE.;[04] ALL STEPS COMPLETED
- [SDR SWAA2023092590822](https://openairdocs.org/sdr/SWAA2023092590822.md): Stiffener · cracked · Aug 17, 2023 · N7826B · Boeing 73779P · Horizontal Stabilizer Structure
  > RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED.<[01] UPDATED MEASUREMENT CHART.;[02] REMOVED THE DAMAGE PART AND INSTALLED REPAIR PARTS AT R/H HORIZONTAL STAB. INSPAR RIB; STAB STA 129.5 3RD VERTICA
- [SDR SWAA2023092590824](https://openairdocs.org/sdr/SWAA2023092590824.md): Stiffener · cracked · Aug 17, 2023 · N7826B · Boeing 73779P · Horizontal Stabilizer Structure
  > RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 4TH VERTICAL STIFFENER IS CRACKED.<[01] UPDATED MEASUREMENT CHART.;[02] REMOVED THE DAMAGE PART AND INSTALLED REPAIR PARTS AT R/H HORIZONTAL STAB. INSPAR RIB; STAB STA 129.5 4TH VERTICA
- [SDR SWAA2023092597933](https://openairdocs.org/sdr/SWAA2023092597933.md): Panel · eroded · Aug 17, 2023 · N7826B · Boeing 73779P · Wing, Plate/Skin
  > LT WING L/E PANEL 521UB HAS WIND EROSION ON CORNER (MARKED)<FABRICATED BONDED ALUMINUM FOIL PLY USING BMS 8-289 LOT: 1524505-2 AND INSTALLED USING BMS 5-128 LOT: 1536130-2. ASSEMBLED VACUUM BAG SYSTEM. PERFORMED 5X5 LEAK TEST, PASSED USING VACUUM GAUGE ID: ATS

Next page: https://openairdocs.org/aircraft/N7826B/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 = 'N7826B' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7826B/reports

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