# Service difficulty reports: N7723E

A list on [N7723E](https://openairdocs.org/aircraft/N7723E.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 · 270 reports

- [SDR SWAA2026092538079](https://openairdocs.org/sdr/SWAA2026092538079.md): Scuff Plate · cracked · Sep 21, 2026 · N7723E · Boeing 73776N · Fuselage Miscellaneous Structure
  > REMOVED THE R1 GALLEY DOOR LOWER MAIN SILL SCUFF PLATE FOR PERMANENT REPAIR IAW AMM 53-11-01. REPLACED THE SCUFF PLATE IAW 51-40-02. PERFORMED A CABIN PRESSURE LEAK TEST IAW AMM 05-51-91. LEAK TESTED GOOD.
- [SDR SWAA2026092132982](https://openairdocs.org/sdr/SWAA2026092132982.md): Threshold · cracked · Sep 20, 2026 · N7723E · Boeing 73776N · Fuselage Miscellaneous Structure
  > R1 DOOR THRESHOLD IS CRACKED. COMPLIED WITH EA 26-153-02576. REF. TTG8Q01EQU8C
- [SDR SWAA2026072778728](https://openairdocs.org/sdr/SWAA2026072778728.md): Handle · broken · Jul 22, 2026 · N7723E · Boeing 73776N · Fuselage Main, Structure
  > CAPTAIN`S SIDE GRAB HANDLE, JUST BELOW HUD, IS BROKEN. R & R CAPTAIN GRAB HANDLE IAW SOPM 20-50-01.
- [SDR SWAA2026041788905](https://openairdocs.org/sdr/SWAA2026041788905.md): Battery Pack · no test · Apr 14, 2026 · N7723E · Boeing 73776N · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M01672 FAILED A CAPACITANCE CHECK. REMOVED AND REPLACED EMX BATTERY BACK M01672 IAW AMM 33-51-06-960-805-NG.
- [SDR SWAA2025092216323](https://openairdocs.org/sdr/SWAA2025092216323.md): Engine · failed · Sep 18, 2025 · N7723E · Boeing 73776N · Engine (Turbine/Turboprop)
  > NR 2 ENG FAIL ON T/O ROLL. NR 2 ENGINE FAILURE AND RTO AT 100KTS METAL IN THE TAILPIPE. REPLACED NR 2 ENGINE IAW MT 771-00-01 REF TTG8Q00YY43D.
- [SDR SWAA2025072193095](https://openairdocs.org/sdr/SWAA2025072193095.md): Lens · missing · Jul 19, 2025 · N7723E · Boeing 73776N · Emergency Lighting
  > 12 DEF EXIT/SALIDA COVER MISSING. INSTALLED NEW EMERG EXIT LENS PER AMM 33-51-01.
- [SDR SWAA2025071792169](https://openairdocs.org/sdr/SWAA2025071792169.md): Doubler · debonded · Jul 17, 2025 · N7723E · Boeing 73776N · Wing, Plate/Skin
  > L/H O/B UPPER SURFACE DISBOND ON EXISITING REPAIR DOUBLER. REMOVED DAMAGE PER SRM 57-53-01-2R14; PERFORMED TAP TEST PER 737 NET MANUEL PART 1 51-05-01. PREPED AREA;FABRICATED REPAIR PARTS INSTALLED REPAIR PARTS PER SRM 57-53-01-2R-14. AND SRM 51-70-05-2R-0
- [SDR SWAA2025061079517](https://openairdocs.org/sdr/SWAA2025061079517.md): Girt Bar · loose · Jun 7, 2025 · N7723E · Boeing 73776N · Emergency Equipment
  > R1 GIRT BAR LOOSE<[01] INSTALLED NEW RIVET ON R1 DOOR GIRT BAR BRACKET PER SRM 51-40-02.
- [SDR SWAA2025032408355](https://openairdocs.org/sdr/SWAA2025032408355.md): Engine · bird ingestion · Mar 22, 2025 · N7723E · Boeing 73776N · Engine (Turbine/Turboprop)
  > HIGH SPEED REJECTED TAKEOFF DUE TO LARGE BIRD STRIKE ON #2 ENGINE. NO ABNORMAL INDICATIONS; HOWEVER PAX AND FLIGHT ATTENDANTS COMPLAINED OF AN ODOR. <[01] C/W BIRD STRIKE INSPECTION ON ACFT PER 05-51-18 BIRD REMAINS FOUND IN NUMBER TWO ENGINE EVIDENCE OF BIRD
- [SDR SWAA2025021996412](https://openairdocs.org/sdr/SWAA2025021996412.md): Handle · broken · Feb 15, 2025 · N7723E · Boeing 73776N · Passenger/Crew Doors
  > FWD ENTRY DOOR AFT DOOR ASSIST HANDLE IS BROKEN<[01] REMOVED AND INSTALLED IAW AMM 25-21-31-420-802<BR><BR>WN49860<BR>WN49856;[02] VERIFIED ITEM 1<BR>AUDIT C/W
- [SDR SWAA2025021995295](https://openairdocs.org/sdr/SWAA2025021995295.md): Battery Pack · inoperative · Feb 12, 2025 · N7723E · Boeing 73776N · Emergency Lighting
  > EMERGENCY EXIT BATTERY PACK M1674 WILL NOT CHARGE<[01] REMOVED AND REPLACED M1674 BATTERY PACK IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD<BR>WN49843;[02] VERIFIED ITEM 1<BR>C/W
- [SDR SWAA2025021995296](https://openairdocs.org/sdr/SWAA2025021995296.md): Battery Pack · inoperative · Feb 12, 2025 · N7723E · Boeing 73776N · Emergency Lighting
  > EMERGENCY EXIT BATTERY PACK M1675 WILL NOT CHARGE<[01] OPS CHECKED M1675 BATTERY IAW AMM 33-51-06-960-805; NO FAULT FOUND; OPS CHECK GOOD;[02] VERIFIED ITEM 1<BR>C/W
- [SDR SWAA2025021995297](https://openairdocs.org/sdr/SWAA2025021995297.md): Battery Pack · inoperative · Feb 12, 2025 · N7723E · Boeing 73776N · Emergency Lighting
  > EMERGENCY EXIT BATTERY PACK M2335 WILL NOT CHARGE<[01] REMOVED AND REPLACED M2335 BATTERY PACK IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD<BR>WN49840;[02] VERIFIED ITEM 1<BR>C/W
- [SDR SWAA2025021995298](https://openairdocs.org/sdr/SWAA2025021995298.md): Battery Pack · inoperative · Feb 12, 2025 · N7723E · Boeing 73776N · Emergency Lighting
  > EMERGENCY EXIT BATTERY PACK M1668 WILL NOT CHARGE<[01] REMOVED AND REPLACED M1668 BATTERY PACK IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD<BR>01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] WN4
- [SDR SWAA2025021995299](https://openairdocs.org/sdr/SWAA2025021995299.md): Battery Pack · inoperative · Feb 12, 2025 · N7723E · Boeing 73776N · Emergency Lighting
  > EMERGENCY EXIT BATTERY PACK M1670 WILL NOT CHARGE<[01] REMOVED AND REPLACED M1670 BATTERY PACK IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.<BR>WN49839;[02] VERIFIED ITEM 1<BR>C/W
- [SDR SWAA2025022092140](https://openairdocs.org/sdr/SWAA2025022092140.md): Support Bracket · cracked · Feb 1, 2025 · N7723E · Boeing 73776N · Fuselage Miscellaneous Structure
  > (152-02) PASSENGER CABIN STA 867 STR 1R; FEEDER CABLE SUPPORT BRACKET IS CRACKED.<[01] REMOVED BRACKET AT BS867; BETWEEN S-1 AND S-2R; IAW SRM 51-40-02-0G-0. FABRICATED NEW BRACKET IAW BOEING DWG 287A4015 REV. -; BOEING PL 287A4015 REV. K; AND EA 25-153-00335.
- [SDR SWAA2025022089840](https://openairdocs.org/sdr/SWAA2025022089840.md): Intercostal · cracked · Jan 26, 2025 · N7723E · Boeing 73776N · Fuselage Miscellaneous Structure
  > DOT A24-77 FORWARD PIT. VERTICAL INTERCOSTAL AT STATION 480+15 BETWEEN STRINGERS 23L AND 25L CRACKED AT UPPER EDGE. BLENDED DAMAGE IAW SRM 51-10-02-0G-0. FOUND ADJACENT TO BLEND.040'; LOSS.007'; REMAINING.033' USING NDT TO VERIFY IN STEP 5. UPON FURTHER
- [SDR SWAA2025021989045](https://openairdocs.org/sdr/SWAA2025021989045.md): Floor Panel · pulled · Jan 24, 2025 · N7723E · Boeing 73776N · Fuselage Floor Panel
  > DOT#55 A-043 CABIN FLOOR PANEL 241KF HAS PULLED FIBERS ON TOP SIDE OF PANEL<[01] AUDIT C/W;[02] REFER TO FAULT TTG8Q00YBAGR WHERE EA 25-153-00203 WAS ADDED AS A SUBTASK..
- [SDR SWAA2025021989044](https://openairdocs.org/sdr/SWAA2025021989044.md): Floor Panel · pulled · Jan 24, 2025 · N7723E · Boeing 73776N · Fuselage Floor Panel
  > DOT#54 A-043 CABIN FLOOR PANEL 242GF HAS PULLED FIBERS ON TOP SIDE OF PANEL<[01] AUDITED;[02] REFER TO FAULT TTG8Q00YBAGR WHERE EA 25-153-00203 WAS ADDED AS A SUBTASK.
- [SDR SWAA2025021989043](https://openairdocs.org/sdr/SWAA2025021989043.md): Floor Panel · pulled · Jan 24, 2025 · N7723E · Boeing 73776N · Fuselage Floor Panel
  > DOT#53 A-043 CABIN FLOOR PANEL 231WF HAS PULLED FIBERS ON TOP SIDE OF PANEL<[01] REPAIRED PER EA 25-153-00203.
- [SDR SWAA2025022088437](https://openairdocs.org/sdr/SWAA2025022088437.md): Stringer · cracked · Jan 22, 2025 · N7723E · Boeing 73776N · Wing, Longeron/Stringer
  > FASTENER TAB FOR LEFT WING INBOARD UPPER FIXED LEADING-EDGE STRINGER P/N 116A4531-5 IS BROKED OFF. REMOVED AND REPLACED -5 STRINGER ON LEFT WING INBOARD UPPER FIXED LEADING-EDGE P/N 116A4531-5 ATAG WN49678 IAW BOEING DWG 116A4008 REV - SRM 51-40-02. VERIFIE
- [SDR SWAA2025022086137](https://openairdocs.org/sdr/SWAA2025022086137.md): Stub Frame · cracked · Jan 15, 2025 · N7723E · Boeing 73776N · Fuselage Main, Frame
  > FWD GALLEY DOOR CUTOUT; UPPER FWD STUB FRAME HFEC SURFACE INSPECTION; FOUND 1' CRACK IN STUB FRAME AT JOGGLE;.70' ABOVE SEAL DEPRESSOR. MARKED IN BLACK. REF. CARD TTG8Q00TSZ8V INSP - FORWARD GALLEY DOOR (R1) BEAR STRAP BS 290-296 BETWEEN S-8R AND S-9R - GROUP
- [SDR SWAA2025021986335](https://openairdocs.org/sdr/SWAA2025021986335.md): Floor Panel · pulled · Jan 15, 2025 · N7723E · Boeing 73776N · Fuselage Floor Panel
  > FLOOR PANEL 222DF HAS PULLED FIBERS ON TOP SURFACE<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/W
- [SDR SWAA2025021985676](https://openairdocs.org/sdr/SWAA2025021985676.md): Floor Panel · cracked · Jan 14, 2025 · N7723E · Boeing 73776N · Fuselage Floor Panel
  > FLOOR PANEL 221BF HAS 5EA PLACES OF PANEL BEING CRACKED/BROKEN ON LOWER SURFACE.<[01] REPLACED FLOOR PANEL 221BF WITH SERVICEABLE FLOOR PANEL ON SHELF I.A.W REFERENCE TO AIPC 53-21-51-75 PG 14 SHEET 01 ITEM A;[02] INFO ONLY: PANEL 221BF WAS REPLACED ON #TTG8Q0
- [SDR SWAA2025021985674](https://openairdocs.org/sdr/SWAA2025021985674.md): Floor Panel · pulled · Jan 14, 2025 · N7723E · Boeing 73776N · Fuselage Floor Panel
  > FLOOR PANEL 221BF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] REPLACED FLOOR PANEL 221BF WITH SERVICEABLE FLOOR PANEL ON SHELF I.A.W REFERENCE TO AIPC 53-21-51-75 PG 14 SHEET 01 ITEM A;[02] INFO ONLY: PANEL 221BF WAS REPLACED ON #TTG8Q00Y4M8W & INSTALLED ON #TT
- [SDR SWAA2025021985682](https://openairdocs.org/sdr/SWAA2025021985682.md): Floor Panel · corroded · Jan 14, 2025 · N7723E · Boeing 73776N · Fuselage Floor Panel
  > (A204 DOT 93) FLOOR PANEL 221BF HAS 8EA FASTNER INSERTS WITH CORROSION; MARKED IN RED.<[01] REPLACED FLOOR PANEL 221BF WITH SERVICEABLE FLOOR PANEL ON SHELF I.A.W REFERENCE TO AIPC 53-21-51-75 PG 14 SHEET 01 ITEM A;[02] INFO ONLY: PANEL 221BF WAS REPLACED ON #
- [SDR SWAA2025021985681](https://openairdocs.org/sdr/SWAA2025021985681.md): Floor Panel · pulled · Jan 14, 2025 · N7723E · Boeing 73776N · Fuselage Floor Panel
  > FLOOR PANEL 231UF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.
- [SDR SWAA2025021985671](https://openairdocs.org/sdr/SWAA2025021985671.md): Floor Panel · pulled · Jan 14, 2025 · N7723E · Boeing 73776N · Fuselage Floor Panel
  > (A204 DOT 97) FLOOR PANEL 231KF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/W
- [SDR SWAA2025021985680](https://openairdocs.org/sdr/SWAA2025021985680.md): Floor Panel · debonded · Jan 14, 2025 · N7723E · Boeing 73776N · Fuselage Floor Panel
  > (A204 DOT 98) FLOOR PANEL 231KF; AFT LH CORNER OF FLOOR PANEL IS DISBONDED.<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/W
- [SDR SWAA2025021985670](https://openairdocs.org/sdr/SWAA2025021985670.md): Floor Panel · pulled · Jan 14, 2025 · N7723E · Boeing 73776N · Fuselage Floor Panel
  > (A204 DOT 99) FLOOR PANEL 231GF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/W
- [SDR SWAA2025021985668](https://openairdocs.org/sdr/SWAA2025021985668.md): Floor Panel · pulled · Jan 14, 2025 · N7723E · Boeing 73776N · Fuselage Floor Panel
  > (A204 DOT 101) FLOOR PANEL 231DF; UPPER SURFACE FACE SHEET MISSING FIBERS.<[01] C/W EA 25-153-00105. VERIFIED ALL STEPS COMPLETE.;[02] VERIFIED C/W;[03] C/W
- [SDR SWAA2025021985679](https://openairdocs.org/sdr/SWAA2025021985679.md): Handle · out of adjust · Jan 14, 2025 · N7723E · Boeing 73776N · Emergency Exits
  > (A204 DOT 86) RH EMERGENCY EXIT DOOR 843 PULL CLOSE HANDLE RECESS HAS 2EA MISSING QUARTER TURN STUDS.<[01] REPLACED MISSING QUARTER TURN STUDS IN HANDLE RECESS ON DOOR 843 I/A/W 52-22-51-400-801.;[02] VERIFIED STEP 1<BR>AUDIT C/W
- [SDR SWAA2025022085662](https://openairdocs.org/sdr/SWAA2025022085662.md): Winglet · corroded · Jan 13, 2025 · N7723E · Boeing 73776N · Wing Main, Frame Structure
  > DOT#42 A-043 RH WINGLET HAS CORROSION ON LOWER OTBD T/E 18' FROM BOTTOM EDGE<[01] 04 - REPAIRED PER [SRM 57-30-01-1A-2-APB-AP37.1-0632-A01611 (PERMANENT (NON-DENT DAMAGE TYPES)-WINGLETS)];[02] VERIFIED STEP 1<BR>AUDIT CW
- [SDR SWAA2025022085661](https://openairdocs.org/sdr/SWAA2025022085661.md): Winglet · corroded · Jan 13, 2025 · N7723E · Boeing 73776N · Wing Main, Frame Structure
  > DOT#43 A-043 RH WINGLET HAS CORROSION ON UPPER INBD T/E 42' FROM BOTTOM EDGE<[01] 04 - REPAIRED PER [SRM 51-10-02-0G-0-A00248 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)] AND IAW APB 57-30-01 FIGURE 102 (D);[02] 04 - REPAIRED PER [SRM 5
- [SDR SWAA2025021985451](https://openairdocs.org/sdr/SWAA2025021985451.md): Receiver · cracked · Jan 13, 2025 · N7723E · Boeing 73776N · Fuselage Main, Structure
  > DOT#38 A-043 FWD CARGO COMPARTMENT AFT BKHD UPPER STAINTION RAIL CAMLOCK RECIVER CRACKED STA 500D LBL 39 WL 193<[01] REMOVED AND REPLACED CAMLOCK AT AFT BULKHEAD UPPER RAIL IAW SRM 51-40-02-0G-0;[02] VERIFIED ITEM 1<BR>AUDIT C/W
- [SDR SWAA2025021985667](https://openairdocs.org/sdr/SWAA2025021985667.md): Sidewall Support · corroded · Jan 13, 2025 · N7723E · Boeing 73776N · Fuselage Miscellaneous Structure
  > 154-86 AFT CARGO COMPARTMENT STA 907 STR 24R+4 SIDEWALL PANEL SUPPORT CORRODED NEAR THE FASTENER HOLE<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]<BR> BOEING DWG 147A9409 ID:
- [SDR SWAA2025022085126](https://openairdocs.org/sdr/SWAA2025022085126.md): Seal · cracked · Jan 11, 2025 · N7723E · Boeing 73776N · Horizontal Stabilizer Miscellaneous Structure
  > (DOT 152-1) LEFT HORIZONTAL STABILIZER GAP COVER 333AB; SLIDING SEAL IS CRACKED.<[01] REMOVE AND REPLACED LEFT HORIZONTAL STABILIZER GAP COVER 333AB; SLIDING SEAL I.A.W SRM STEP 4.<BR>ISSUE TAG WN49657;[02] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER GAP C
- [SDR SWAA2025022085127](https://openairdocs.org/sdr/SWAA2025022085127.md): Seal · cracked · Jan 11, 2025 · N7723E · Boeing 73776N · Horizontal Stabilizer Miscellaneous Structure
  > (DOT 152-2) LEFT HORIZONTAL STABILIZER PANEL 333AB; SLIDING SEAL SUPPORT BRACKET IS CRACKED.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER PANEL 333AB; SLIDING SEAL I.A.W SRM 51-40-02-0G<BR>ISSUE TAG WN49657;[02] VERIFIED TASK COMPLETE<BR><BR>AUDIT C/W
- [SDR SWAA2025021984885](https://openairdocs.org/sdr/SWAA2025021984885.md): Floor Panel · corroded · Jan 10, 2025 · N7723E · Boeing 73776N · Fuselage Floor Panel
  > DOT#27 A-043 FLIGHT COMPARTMENT FLOOR PANEL 211AF HAS CORROSION ON BOTTOM FWD EDGE STA 259.5 BL 0 WL 208<[01] REPLACED IAW SRM 51-40-02-0G-0 & BOEING DWG: 141A631 REV: B<BR>ATAG: WN 49596<BR>P/N: 141A5133U15ATSMR0;[02] FAULT RESOLVED ON OTHER FAULT. SEE FAULT
- [SDR SWAA2025022084619](https://openairdocs.org/sdr/SWAA2025022084619.md): Frame · cracked · Jan 9, 2025 · N7723E · Boeing 73776N · Fuselage Main, Frame
  > MAIN CABIN STA 440 FRAME HAS EVIDENCE OF CRACK AROUND FASTENER OF RAIL SUPPORT BRACKET I/B OF STR 8 L/H. REMOVED DAMAGE AND REPAIRED FRAME AT STA 440 S-8L IAW EA 25-153-00218.
- [SDR SWAA2025022084621](https://openairdocs.org/sdr/SWAA2025022084621.md): Frame · cracked · Jan 9, 2025 · N7723E · Boeing 73776N · Fuselage Main, Frame
  > MAIN CABIN STA 380 FRAME HAS EVIDENCE OF CRACK AROUND FASTENER OF RAIL SUPPORT BRACKET I/B OF STR 8 L/H. REPAIRED PER EA 25-153-00153 TTG8Q00YDMJL;[02] REPAIRED FRAME AT BS380; BETWEEN S-7L AND S-8L; IAW EA 25-153-00153.
- [SDR SWAA2025022084618](https://openairdocs.org/sdr/SWAA2025022084618.md): Frame · cracked · Jan 9, 2025 · N7723E · Boeing 73776N · Fuselage Main, Frame
  > (DOT#147-48) MAIN CABIN STA 400 FRAME HAS EVIDENCE OF CRACK AROUND FASTENER OF RAIL SUPPORT BRACKET I/B OF STR 8 L/H<[01] REPAIRED FRAME AT BS400; BETWEEN S-7L AND S-8L; IAW EA 25-153-00154.;[02] VERIFIED ITEM 1<BR>C/W;[03] C/W
- [SDR SWAA2025022084613](https://openairdocs.org/sdr/SWAA2025022084613.md): Crease Beam · corroded · Jan 9, 2025 · N7723E · Boeing 73776N · Fuselage Main, Structure
  > CABIN FWD WET AREA R1 CREASE BEAM CRRODED AT STA 312+15' LBL 60 WL 208<[01] REMOVED DAMAGE FROM CABIN FWD WET AREA R1 CREASE BEAM CORRODED AT STA 312+15' LBL 60 WL 208; FOUND IT OUT OF LIMITS; ORIG T. ADJACENT TO BLEND.085'; LOSS.017'; REMOVED DAMAGED PART
- [SDR SWAA2025021984610](https://openairdocs.org/sdr/SWAA2025021984610.md): Floor Panel · corroded · Jan 9, 2025 · N7723E · Boeing 73776N · Fuselage Floor Panel
  > DOT L7-010: AFT CARGO COMPARTMENT FLOOR PANEL 140AF IS CORRODED AT FASTENER HOLES<[01] EVALUATED CORROSION ON AFT CARGO COMPARTMENT FLOOR PANEL 140AF; FOUND TOTAL ACCUMULATED CORROSION DAMAGE TO BE MORE THAN THE 20IN ALLOWED; OUT OF LIMITS IAW SRM 53-00-53-1A-
- [SDR SWAA2025021984611](https://openairdocs.org/sdr/SWAA2025021984611.md): Floor Panel · corroded · Jan 9, 2025 · N7723E · Boeing 73776N · Fuselage Floor Panel
  > DOT L7-012: AFT CARGO COMPARTMENT FLOOR PANEL 140CF IS CORRODED AT FASTENER HOLES<[01] VERIFIED LIMITS ON AFT CARGO COMPARTMENT FLOOR PANEL 140CF; DISTANCE BETWEEN DAMAGE IS 2' (MINIMUM ALLOWABLE DISTANCE BETWEEN DAMAGE IS 5') THEREFORE IS FOUND OUT OF THE LIM
- [SDR SWAA2025022083950](https://openairdocs.org/sdr/SWAA2025022083950.md): Angle · buckled · Jan 8, 2025 · N7723E · Boeing 73776N · Fuselage Miscellaneous Structure
  > (A204 DOT 73) FORWARD CARGO STA 500 TO 500A; STR 26L; BAFFLE PLATE UNDER Z-ANGLE IS BUCKLED ON FORWARD SIDE.<[01] REMOVED AND INSTALLED NEW RIVETS AT FORWARD CARGO STA 500 TO 500A STR 26L BAFFLE PLATE UNDER Z ANGLE I/A/W SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;
- [SDR SWAA2025021983951](https://openairdocs.org/sdr/SWAA2025021983951.md): Shield · corroded · Jan 8, 2025 · N7723E · Boeing 73776N · Fuselage Miscellaneous Structure
  > (A204 DOT 78) FWD CARGO STA 492; RBL 21; WL 155; SPLASH SHIELD HAS CORROSION ON UPPER SURFACE<[01] REMOVED CORROSION AND VERIFIED WITH A 10-POWER MAGNIFYING GLASS ON FWD CARGO STA 492; RBL 21; WL 155; SPLASH SHIELD UPPER SURFACE I.A.W SRM 51-10-02-0G-0 VERIFIE
- [SDR SWAA2025021984185](https://openairdocs.org/sdr/SWAA2025021984185.md): Floor Panel · corroded · Jan 8, 2025 · N7723E · Boeing 73776N · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 120CF HAS CORROSION AT FASTENER HOLES<[01] UPON FURTHER INVESTIGATION FOUND THAT CORROSION WAS 30 INCHES IN LENGTH WITH A MAX ALLOWED LENGTH OF 3 INCHES FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1; RECEIVED REPLACEMENT MATERIAL PN 202
- [SDR SWAA2025022083595](https://openairdocs.org/sdr/SWAA2025022083595.md): Rib · cracked · Jan 7, 2025 · N7723E · Boeing 73776N · Horizontal Stabilizer, Spar/Rib
  > (A204 DOT 64) LH HORIZONTAL STAB LEADING EDGE 331B; LE STA 114.5; RIB IS CRACKED NEXT TO BEND RADIUS AT LOWER AFT HOLE.<[01] REMOVED L/H L/E HORZ STAB RIB AT STA114.5 IAW SRM 51-40-02-0G-0 AND DWG 186A1305 REV - VERIFIED PART USING P/N 186A1352-9 AND ATAG WN49
- [SDR SWAA2025022083596](https://openairdocs.org/sdr/SWAA2025022083596.md): Rib · buckled · Jan 7, 2025 · N7723E · Boeing 73776N · Horizontal Stabilizer, Spar/Rib
  > LH HORIZONTAL STAB LEADING EDGE 331B; LE STA 198.25; RIB IS BUCKLED AT AFT RADIUS.<[01] REMOVED L/H HORZ STAB L/E 331B RIB IAW SRM 51-40-02-0G-0 AND DWG 186A1001 REV A VERIFIED PART USING P/N 654A0004-685 ATAG A285988 AND DWG 186A1001 REV A INSTALLED RIB IAW S

Next page: https://openairdocs.org/aircraft/N7723E/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 = 'N7723E' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7723E/reports

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