# Service difficulty reports: N7704B

A list on [N7704B](https://openairdocs.org/aircraft/N7704B.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 · 263 reports

- [SDR SWAA2026101640537](https://openairdocs.org/sdr/SWAA2026101640537.md): Light · inoperative · Oct 9, 2026 · N7704B · Boeing 7377BD · Emergency Lighting
  > L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R L1 DOOR EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04.
- [SDR SWAA2026101637171](https://openairdocs.org/sdr/SWAA2026101637171.md): Light · inoperative · Oct 9, 2026 · N7704B · Boeing 7377BD · Emergency Lighting
  > PASSENGER CABIN INTERIOR EMERGENCY LIGHT INOPERATIVE AT 22L. THE EXTERIOR EMERGENCY LIGHT R & R IAW AMM 33-51-03.
- [SDR SWAA2026101656881](https://openairdocs.org/sdr/SWAA2026101656881.md): Attach Bracket · cracked · Oct 9, 2026 · N7704B · Boeing 7377BD · Fuselage Main, Attach Fittings
  > AFT ENTRY DOOR LOWER LINER PAN AFT ATTACH BRACKET CRACKED. R & R AFT ENTRY DOOR LOWER LINER PAN AFT ATTACH BRACKET IAW AMM 52-13-31.
- [SDR SWAA2026101659349](https://openairdocs.org/sdr/SWAA2026101659349.md): Acoustic Panel · delaminated · Oct 9, 2026 · N7704B · Boeing 7377BD · Turbine Engine Air Inlet Section
  > NR 1 ENGINE FAN, AFT ACOUSTIC PANEL DELAMINATED BTWN NR 4 & 5. R & R IAW AMM 72-23-02-401.
- [SDR SWAA2026101656194](https://openairdocs.org/sdr/SWAA2026101656194.md): Acoustic Panel · delaminated · Oct 9, 2026 · N7704B · Boeing 7377BD · Turbine Engine Air Inlet Section
  > NR 1 ENGINE FAN, FRAME AFT ACOUSTIC PANEL DELAMINATED BTWN NR 5 AND 6 FAN FRAME STRUTS. REMOVED AND REPLACED IAW AMM 72-23-02-401.
- [SDR SWAA2026101659487](https://openairdocs.org/sdr/SWAA2026101659487.md): Acoustic Panel · delaminated · Oct 9, 2026 · N7704B · Boeing 7377BD · Turbine Engine Air Inlet Section
  > NR 1 ENGINE FAN, FRAME AFT ACOUSTIC PANEL DELAMINATED BTWN NR 7 & 8 FAN FRAME STRUTS. REMOVED AND REPLACED IAW AMM 72-23-02-401.
- [SDR SWAA2026101613138](https://openairdocs.org/sdr/SWAA2026101613138.md): Seat Track · worn · Oct 9, 2026 · N7704B · Boeing 7377BD · Fuselage, Seat/Cargo Attach Fittings
  > FLIGHT DECK, CAPTAIN`S AFT INBD SEAT TRACK WORN TO BEYOND LIMITS. R & R THE SEAT TRACK IAW AMM 25-11-11.
- [SDR SWAA2026090815658](https://openairdocs.org/sdr/SWAA2026090815658.md): Engine · power loss · Sep 2, 2026 · N7704B · Boeing 7377BD · Engine (Turbine/Turboprop)
  > NR 2 ENG ROLLED BACK TO 47% N1 AT FL 390 IN RAIN & TURBULENCE, ENG CAME BACK TO NORMAL CRUISE N1 AFTER 5 SECONDS AT 47%, OPS NORMAL REST OF FLT_ CW NR 2 ENG EEC BITE WITH NO RECENT FAULTS OR FAULT HISTORY PER FIM 73-00 TASK 801. NO 30-DAY HISTORY. ACCOMPLISHED
- [SDR SWAA2026061508124](https://openairdocs.org/sdr/SWAA2026061508124.md): Light · inoperative · Jun 1, 2026 · N7704B · Boeing 7377BD · Emergency Lighting
  > LEFT OVERWING EXIT GROUND ILLUMINATION LIGHT INOPERATIVE. RELAMPED AND PERFORMED A GOOD TEST IAW AMM 33-51-04-960-801.
- [SDR SWAA2026061508123](https://openairdocs.org/sdr/SWAA2026061508123.md): Battery Pack · inoperative · Jun 1, 2026 · N7704B · Boeing 7377BD · Emergency Lighting
  > EMERGENCY EXIT LIGHT ASSOCIATED WITH BATTERY PACK M2335 ARE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK M2335 AND PERFORMED A GOOD TEST IAW AMM 33-51-06-960-805, & DWG 33500005.
- [SDR SWAA2026061508422](https://openairdocs.org/sdr/SWAA2026061508422.md): Scuff Plate · cracked · Jun 1, 2026 · N7704B · Boeing 7377BD · Fuselage Miscellaneous Structure
  > FWD SERVICE DOOR SCUFF PLATE IS CRACK AT AFT CORNER. REMOVED AND INSTALLED FORWARD GALLEY DOOR SCUFF PLATE IAW AMM 53-11-01-420-801. TOOL USED SCREW GUN ID: PER 2724; DUE: 08/2026.
- [SDR SWAA2026061505461](https://openairdocs.org/sdr/SWAA2026061505461.md): Crossbeam · cracked · May 22, 2026 · N7704B · Boeing 7377BD · Fuselage Main, Structure
  > BREAK PANEL SUPPORT CRACKED AT BS 540, RBL 1, WL 208.1. REMOVED AND REPLACED BREAK PANEL SUPPORT AT BS 540, WL 208.1, RBL1 IAW SRM 51-40-02, AND DWG 143A0060, REV A.
- [SDR SWAA2026061505462](https://openairdocs.org/sdr/SWAA2026061505462.md): Crossbeam · cracked · May 22, 2026 · N7704B · Boeing 7377BD · Fuselage Miscellaneous Structure
  > BREAK PANEL SUPPORT CRACKED AT BS 540, LBL 1, WL 208.1. REMOVED AND REPLACED BREAK PANEL SUPPORT AT BS 540, WL 208.1, LBL 1 IAW SRM 51-40-02 AND DWG 143A0060, REV A.
- [SDR SWAA2026061505456](https://openairdocs.org/sdr/SWAA2026061505456.md): Angle · corroded · May 22, 2026 · N7704B · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT F.S. 685 + 8 W.L. 200 RBL 63. REMOVED AND REPLACED THE PRESSURE FLOOR ANGLE B.S. 685 + 8 W.L. 200 RBL 63; IAW SRM 51-40-02 AND DWG 144A7700, REV E.
- [SDR SWAA2026061505457](https://openairdocs.org/sdr/SWAA2026061505457.md): Stiffener · corroded · May 22, 2026 · N7704B · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT F.S. 685 +1 W.L. 200; LBL 63. REFER TO FAULT TTG8Q01CB9LV FOR REPAIR RESOLUTION.
- [SDR SWAA2026061505458](https://openairdocs.org/sdr/SWAA2026061505458.md): Stiffener · corroded · May 22, 2026 · N7704B · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT 685+12; W.L. 200; LBL62. STIFFENER BS 685+12; W.L. 200; LBL62 WAS REPAIRED IAW EA 26-153-01440-WIP1; REV-A.
- [SDR SWAA2026061505138](https://openairdocs.org/sdr/SWAA2026061505138.md): Panel · cracked · May 21, 2026 · N7704B · Boeing 7377BD · Aerodynamic Fairings
  > PANEL 194AR INNER SKIN IS CRACKED. REPAIRED IAW SRM 51-70-05-2R-2-A00733, REPAIR 2.
- [SDR SWAA2026061104758](https://openairdocs.org/sdr/SWAA2026061104758.md): Floor Panel · failed · May 19, 2026 · N7704B · Boeing 7377BD · Fuselage Floor Panel
  > FLOOR PANEL 241EF UPPER SKIN HAS A FAILED PREVIOUS REPAIR. FLOOR PANEL 241EF WAS REPLACED WITH A NEWLY FABRICATE FLOOR PANEL IAW SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2026051802875](https://openairdocs.org/sdr/SWAA2026051802875.md): Fitting · cracked · May 14, 2026 · N7704B · Boeing 7377BD · Fuselage Main, Structure
  > POSSIBLE CRACK FOUND ON THE S-18A WEB ASSEMBLY NEAR THE RH PICKLE FORK.<[01] C/W 26-153-01296 (AD - N7704B - MINOR ACTION - BS 663 PICKLE FORK FITTING AND STRINGER 18A WEB ASSEMBLY);[02] 26-153-01296-WIP1 (AD - N7704B - MINOR ACTION - BS 663 PICKLE FORK FITTIN
- [SDR SWAA2026051802874](https://openairdocs.org/sdr/SWAA2026051802874.md): Fitting · cracked · May 14, 2026 · N7704B · Boeing 7377BD · Fuselage Main, Structure
  > POSSIBLE CRACK FOUND ON THE RH PICKLE FORK UPPER BOLTS. SUSPECT CRACK LOCATED BETWEEN FASTENER #1 AND #5 POSSIBLE CRACK FOUND ON THE RH PICKLE FORK UPPER BOLTS.<[01] C/W 26-153-01296 (AD - N7704B - MINOR ACTION - BS 663 PICKLE FORK FITTING AND STRINGER 18A WEB
- [SDR SWAA2025110330688](https://openairdocs.org/sdr/SWAA2025110330688.md): Fire Warning · faulty · Oct 30, 2025 · N7704B · Boeing 7377BD · Fire Detection
  > CAPTAIN`S FIRE WARNING BELL CUTOUT DOES NOT SILENCE. RELAMPED CAPT SIDE FIRE WARNING CUTOUT PER SWPM 20-83-11.
- [SDR SWAA2025091012962](https://openairdocs.org/sdr/SWAA2025091012962.md): Oil System · low · Sep 9, 2025 · N7704B · Boeing 7377BD · APU Oil System
  > APU LOW OIL PRESSURE, SERVICED APU GEARBOX REF AMM 12-13-31. OPS CHECK GOOD.
- [SDR SWAA2025082206387](https://openairdocs.org/sdr/SWAA2025082206387.md): Lamp · inoperative · Aug 20, 2025 · N7704B · Boeing 7377BD · Emergency Lighting
  > R1 EXTERIOR EMER LIGHT INOP<[01] RELAMPED EMERGENCY SLIDE LIGHT AT DOOR R1 IN REF TO AMM 33-51-04; OPS CHEK GOOD AT THIS TIME.
- [SDR SWAA2024062705698](https://openairdocs.org/sdr/SWAA2024062705698.md): Battery · discharged · Jun 26, 2024 · N7704B · Boeing 7377BD · Emergency Equipment
  > FOUND BOTH FWD L/H WINDSCRREN EMERGANCY FLASHLIGHTS TO HAVE DEAD BATTERIES<[01] REMOVED AND REPLACED BOTH FWD L/H WINDSCREEN EMERGANCY FLASHLIGHT BATTERIES IAW CMM 25-60-02 PAGE 7001 STEP 2.A.(5);[02] VERIIED CORRECTIVE ACTION 1.
- [SDR SWAA2024070503993](https://openairdocs.org/sdr/SWAA2024070503993.md): Light · damaged · Jun 20, 2024 · N7704B · Boeing 7377BD · Emergency Lighting
  > FWD CLOSEOUT CEILING PANEL LIGHT ASSEMBLY DAMAGED<[01] INSTALLED FWD CLOSEOUT CEILING PANEL LIGHT ASSEMBLY IAW AMM 33-51-01-960-802.;[02] STEPS 1; 2 COMPLETED.;[03] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2024062701892](https://openairdocs.org/sdr/SWAA2024062701892.md): Mount · corroded · Jun 14, 2024 · N7704B · Boeing 7377BD · Buffet/Galleys
  > G1 GALLEY IS CORRODED UNDER THE COFFEE MAKER MOUNT<[01] PARTIAL STEP 1;[02] REMOVED AND REPLACED G1 PER AMM 25-31-11-000-801 AND AMM 25-31-11-400-801;[03] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
- [SDR SWAA2024062700683](https://openairdocs.org/sdr/SWAA2024062700683.md): Scuff Plate · cracked · Jun 12, 2024 · N7704B · Boeing 7377BD · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FORWARD CORNER SCUFF PLATE IS CRACKED<[01] EDIT: ADDED SRM REFERENCE TO THE WORK ACCOMPLISHED STATEMENT IN STEPS 1 AND 2;[02] VERIFIED STEPS 1;2 COMPLETE.;[03] REPAIRED ACB FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1;[04] TASK COMPLETED.
- [SDR SWAA2024062791779](https://openairdocs.org/sdr/SWAA2024062791779.md): Skin · delaminated · May 30, 2024 · N7704B · Boeing 7377BD · Aerodynamic Fairings
  > FORWARD TAILCONE ASSEMBLY OUTER SURFACE SKIN HAS 2 AREAS OF DELAMINATED SKIN COMMON TO THE INNER SURFACE TAILCONE LIGHT SWITCH BRACKET. FORWARD TAILCONE ASSEMBLY OUTER SURFACE SKIN HAS 2 AREAS OF DELAMINATED SKIN COMMON TO THE INNER SURFACE TAILCONE LIGHT SWIT
- [SDR SWAA2024070591152](https://openairdocs.org/sdr/SWAA2024070591152.md): Hinge Fitting · corroded · May 29, 2024 · N7704B · Boeing 7377BD · Fuselage Main, Structure
  > CORROSION ON RT OVERWING EXIT THRESHOLD HINGE ATTACH FITTING BS626 RBL70 WL222. MARKED<[01] REMOVED AND REPLACED NEW RT OVERWING EXIST THRESHOLD HINGE ATTACH FITTING IAW SRM 51-40-02 AND IAW DWG#411A2820;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASURE
- [SDR SWAA2024070390959](https://openairdocs.org/sdr/SWAA2024070390959.md): Floor Support · corroded · May 29, 2024 · N7704B · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER ANGLE OF INTERCOSTAL BS 787 TO BS 787 RBL 21 (MARKED)<[01] REMOVED AND REPLACED UPPER ANGLE OF INTERCOSTAL FROM BS767 TO BS787;RBL21 IAW DWG#146A0081 REV A.
- [SDR SWAA2024070390958](https://openairdocs.org/sdr/SWAA2024070390958.md): Web · corroded · May 29, 2024 · N7704B · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON THRESHOLD WEB AFT CARGO BAY BS 787+16 RBL 26.75 (MARKED)<[01] REMOVED AND REPLACED THRESHOLD WEB AFT CARGO BAY BETWEEN BS 794.37 - BS 847 RBL 26.75 WL 162.51 IAW B-737-700 SRM 51-10-02; SRM 51-40-02 AND DWG#146A8340.;[02] VERIFIED ALL STEPS AND CO
- [SDR SWAA2024062790961](https://openairdocs.org/sdr/SWAA2024062790961.md): Strap · cracked · May 29, 2024 · N7704B · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED STRAP AT BS 827+18 RBL 18.5 WL 156 (MARKED)<[01] REMOVED AND REPLACED STRAP ASSY P/N 146A8128-19; LOT: 1565782-1 LOCATE BETWEEN BS 827+18' RBL 18.5 WL 156 IAW B-737-700 SRM 51-10-02 SRM 51-40-02 & DWG# 146A8340 REV:C.;[02] VERIFIED RII ITEM NUMBER 1.;[
- [SDR SWAA2024070390955](https://openairdocs.org/sdr/SWAA2024070390955.md): Angle · corroded · May 28, 2024 · N7704B · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORRODED CLIP ON BS946 S-28L AT ACB (MARKED) UPON FURTHER EVALUATION ACTUAL LOCATION OF THE CORRODED CLIP IS BS 947 S-26 L/H<[01] REMOVED AND REPLACED CLIP AT ACB BS 947 STR 26L PER SRM 51-40-02 AND DWG 147A1047;[02] CORRECTION=REMOVED AND REPLACED CLIP AT ACB
- [SDR SWAA2024070390387](https://openairdocs.org/sdr/SWAA2024070390387.md): Attach Angle · corroded · May 27, 2024 · N7704B · Boeing 7377BD · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR UPPER SILL WEB ATTCHMENT CLIP AT BS 460 PN 143A8114-23 IS CORRODED<[01] REMOVED AND REPLACED CLIP <BR>IAW SRM 51-40-02 & DWG 143A0081<BR>FCD UPPER SILL WEB ATTCHMENT CLIP AT BS 460;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024062790472](https://openairdocs.org/sdr/SWAA2024062790472.md): Cargo Track · cracked · May 27, 2024 · N7704B · Boeing 7377BD · Fuselage, Seat/Cargo Attach Fittings
  > CRACKED TRACK AT ACB BS727E LBL17 WL156. MARKED<[01] VERIFIED STEPS 4 COMPLETE; STEP 5 IN PARTIAL; OK TO INSTALL GIVEN.;[02] REMOVED AND REPLACED TRACK ACB BS727 TO BS867 LBL17 WL156<BR>IAW SRM 51-40-02 & DWG 146A7500.;[03] VERIFIED CORRECTIVE ACTION ENTRY 2.
- [SDR SWAA2024062790467](https://openairdocs.org/sdr/SWAA2024062790467.md): Support Fitting · cracked · May 27, 2024 · N7704B · Boeing 7377BD · Fuselage Main, Structure
  > CRACKED SUPPORT FITTING BEHIND WATER SERVICE PANEL AT ACB BS914 RBL11 WL171.<[01] REMOVED AND REPLACED SUPPORT FITTING BEHIND WATER SERVICE PANEL AT ACB BS914 RBL11 WL171.;[02] VERIFIED ACTION 1.;[03] UPDATED MESASUREMENTS;[04] VERIFIED COMPLETION
- [SDR SWAA2024062790483](https://openairdocs.org/sdr/SWAA2024062790483.md): Support Fitting · cracked · May 27, 2024 · N7704B · Boeing 7377BD · Fuselage Main, Structure
  > CRACKED SUPPORT FITTING BEHIND WATER SERVICE PANEL AT ACB BS918 RBL11 WL171.<[01] REMOVED AND REPLACED SUPPORT FITTING BEHIND WATER SERVICE PANEL AT ACB BS 918;RBL11 WL171 IAW DWG#147A7221 REV D.;[02] VERIFIED ACTION 1.;[03] UPDATED MEASUREMENT;[04] VERIFIED C
- [SDR SWAA2024062790465](https://openairdocs.org/sdr/SWAA2024062790465.md): Skin · debonded · May 27, 2024 · N7704B · Boeing 7377BD · Aerodynamic Fairings
  > AFT TAILCONE ASSEMBLY SKIN DISBOND AT 12 O'CLOCK; 6' FROM FWD EDGE. AFT TAILCONE ASSEMBLY SKIN DISBONDED AT 12 O'CLOCK; 6 INCHES FROM FWD EDGE WAS REPAIRED IAW SRM 51-70-05-2R-2.
- [SDR SWAA2024062790466](https://openairdocs.org/sdr/SWAA2024062790466.md): Skin · debonded · May 27, 2024 · N7704B · Boeing 7377BD · Aerodynamic Fairings
  > FORWARD TAILCONE ASSEMBLY SKIN DEBONDED AT 5 O'CLOCK; 6' FROM FWD EDGE. FORWARD TAILCONE ASSEMBLY SKIN DISBOND AT 5 O'CLOCK; 6 INCHES FROM FWD EDGE WAS REPAIRED IAW SRM 51-70-05-2R-4.
- [SDR SWAA2024062790485](https://openairdocs.org/sdr/SWAA2024062790485.md): Sidewall Support · corroded · May 27, 2024 · N7704B · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS847 LBL21 WL157. MARKED<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB BS 727 TO BS 847 LBL 21 IAW SRM 51-40-02 AND DWG 146A7500 ID: 0081;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED
- [SDR SWAA2024062790468](https://openairdocs.org/sdr/SWAA2024062790468.md): Sidewall Support · corroded · May 27, 2024 · N7704B · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS767 RBL21 WL157. MARKED<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS767 RBL21 WL157 I.A.W SRM 51-10-02; SRM 51-40-02-0G-0 AND DWG 146A7500.;[02] VERIFIED RII CORRECTIVE ACTION ITE
- [SDR SWAA2024062790469](https://openairdocs.org/sdr/SWAA2024062790469.md): Stringer Clip · corroded · May 27, 2024 · N7704B · Boeing 7377BD · Fuselage Main, Attach Fittings
  > CORROSION ON STR CLIP AT ACB BS787 RBL15 WL154. MARKED<[01] REMOVED AND REPLACED STR CLIP AT ACB BS787 RBL15 WL154 IAW SRM 51-40-02 AND DWG 146A1262.
- [SDR SWAA2024062790487](https://openairdocs.org/sdr/SWAA2024062790487.md): Web · corroded · May 27, 2024 · N7704B · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL AT ACB BS770 RBL6 WL151.<[01] REMOVED AND REPLACED INTERCOSTAL WEB LOCATED AT ACB BETWEEN BS. 767 - BS 787 RBL 6 WL 151 IAW B-737-700 SRM 51-10-02 AND SRM 51-40-02 DWG#146A8130 REV: B;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND ME
- [SDR SWAA2024062790470](https://openairdocs.org/sdr/SWAA2024062790470.md): Attach Fitting · corroded · May 27, 2024 · N7704B · Boeing 7377BD · Fuselage Main, Attach Fittings
  > CORROSION ON SHIELD ATTACH FITTING AT ACB BS767 RBL22 WL156.<[01] REMOVED AND REPLACED FITTING (CLIP) AT ACB BS767 RBL22 WL156;IAW SRM 51-40-02 AND DWG#146A0081 REV A.;[02] JOB COMPLETE.
- [SDR SWAA2024062790471](https://openairdocs.org/sdr/SWAA2024062790471.md): Stringer Clip · corroded · May 27, 2024 · N7704B · Boeing 7377BD · Fuselage Main, Attach Fittings
  > CORROSION ON STR CLIP AT ACB BS767 LBL15 WL153.<[01] REMOVED AND REPLACED STRINGER CLIP AT BS767 STR 26L PN#146A1010-27 PER SRM 51-40-02 AND PER DWG#146A1261.;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2024062790473](https://openairdocs.org/sdr/SWAA2024062790473.md): Cargo Track · corroded · May 27, 2024 · N7704B · Boeing 7377BD · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TRACK TIEDOWN AT ACB BS727D; BS787 LBL17 WL156. MARKED<[01] THIS TASK CARD MUST BE ACCOMPLISHED WITH THE CUSTOMER CARD TTG8Q00TLD8F.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2024062790493](https://openairdocs.org/sdr/SWAA2024062790493.md): Seat Track · corroded · May 27, 2024 · N7704B · Boeing 7377BD · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK RBL 45 BS727+6; BS727+10; BS727C+13; BS727C+19; BS727D+4; BS787+6; BS787+9.5; BS787+19; BS827+4; BS847+10; BS847+13. REMOVED CORROSION ON DISCREPANCY AREAS FOUND TO BE WITHIN LIMITS IAW SRM 53-00-52-1A-1 STEP 4A (2) (A) FIG 103 DETAIL
- [SDR SWAA2024070389400](https://openairdocs.org/sdr/SWAA2024070389400.md): Attach Angle · cracked · May 23, 2024 · N7704B · Boeing 7377BD · Fuselage Main, Attach Fittings
  > FWD CARGO INTERCOASTAL ATTACH ANGLE AFT OF BS 400 LBL 25 WL 152 CRACKED<[01] REMOVED AND REPLACED ON FCB INTERCOSTAL ATTACH ANGLE (CLIP) AFT OF BS400;LBL25;WL152 IAW SRM 51-40-02 AND DWG#143A7505.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TA
- [SDR SWAA2024062789401](https://openairdocs.org/sdr/SWAA2024062789401.md): Attach Angle · cracked · May 23, 2024 · N7704B · Boeing 7377BD · Fuselage Main, Attach Fittings
  > FWD CARGO INTERCOASTAL ATTACH ANGLE FWD OF BS 500C RBL 25 WL 152 CRACKED<[01] REMOVED AND REPLACED FCB INTERCOSTAL ATTACH ANGLE FWD OF BS500C;RBL25;WL152.IAW SRM 51-40-02 AND DWG#143A7505.;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
- [SDR SWAA2024062789402](https://openairdocs.org/sdr/SWAA2024062789402.md): Attach Angle · cracked · May 23, 2024 · N7704B · Boeing 7377BD · Fuselage Main, Attach Fittings
  > FWD CARGO INTERCOASTAL ATTACH ANGLE FWD OF BS 500C LBL 25 WL 152 CRACKED<[01] REMOVED AND REPLACED FWD CARGO INTERCOSTAL ATTACH ANGLE FWD OF BS 500C LBL 25 WL 152 IAW SRM 51-40-02 AND DWG 143A7505;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE.

Next page: https://openairdocs.org/aircraft/N7704B/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 = 'N7704B' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7704B/reports

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