# Service difficulty reports: N708AS, cancelled Oct 9, 2018

A list on [N708AS, cancelled Oct 9, 2018](https://openairdocs.org/deregistered/N708AS-2018-10-09.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 4 · 151 reports

- [SDR ASAA2017053020919](https://openairdocs.org/sdr/ASAA2017053020919.md): Battery Pack · failed · May 30, 2017 · N708AS · Boeing 737490 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ABOVE SEAT ROWS 1 - 11ABC FOUND INOPERATIVE. ACFT GROUNDED. REMOVED AND REPLACED THE BATTERY PACK, OPS NORMAL IAW AMM 33-51-06-960-805.
- [SDR ASAA2016110718677](https://openairdocs.org/sdr/ASAA2016110718677.md): Fitting · corroded · Nov 7, 2016 · N708AS · Boeing 737490 · Wing, Control Surfaces
  > AFTER REMOVAL OF OTBD FOREFLAP OTBD TORQUE TUBE, FOUND ATTACH FITTING FOR TORQUE TUBE CORRODED. ACFT GROUNDED. REMOVED & REPLACED THE FITTING IAW AMM 20-80-11-912-002, PG 6.
- [SDR ASAA2016110718675](https://openairdocs.org/sdr/ASAA2016110718675.md): Fitting · corroded · Nov 7, 2016 · N708AS · Boeing 737490 · Trailing Edge Flaps
  > AFTER REMOVAL OF INBD FOREFLAP INBD TORQUE TUBE, FOUND ATTACH FITTING FOR TORQUE TUBE CORRODED. ACFT GROUNDED. REMOVED AND REPLACED THE FITTING IAW AMM 20-50-11-912-602 PG 6.
- [SDR ASAA2016103118688](https://openairdocs.org/sdr/ASAA2016103118688.md): Frame · cracked · Oct 31, 2016 · N708AS · Boeing 737490 · Fuselage Main, Frame
  > PAX CABIN FRAME CRACKED BS 827 BETWEEN STRINGERS 8 AND 9R. ACFT GROUNDED. REPAIRED THE FRAME IAW T/C AD20062609-400-53-107 REV 00.
- [SDR ASAA2016103018772](https://openairdocs.org/sdr/ASAA2016103018772.md): Floorbeam · cracked · Oct 30, 2016 · N708AS · Boeing 737490 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM CRACKED AT BS 538 LBL 1 - 22. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-05-0G-0.
- [SDR ASAA2016103018674](https://openairdocs.org/sdr/ASAA2016103018674.md): Floor Support · corroded · Oct 30, 2016 · N708AS · Boeing 737490 · Fuselage Main, Structure
  > FLOOR SUPPORT RBL 22 CORRODED AT BS 952. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51-01-1, REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0.
- [SDR ASAA2016103018673](https://openairdocs.org/sdr/ASAA2016103018673.md): Floor Support · corroded · Oct 30, 2016 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT LBL 42 BS 947 TO 967 CORRODED MULTIPLE AREAS. ACFT GROUNDED. REMOVED AND REPLACED DAMAGED FLOOR SUPPORT IAW SRM 51-40-02-0G-0.
- [SDR ASAA2016103018672](https://openairdocs.org/sdr/ASAA2016103018672.md): Floor Support · corroded · Oct 30, 2016 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT LBL 22 CORRODED AT BS 952. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0W.
- [SDR ASAA2016102918676](https://openairdocs.org/sdr/ASAA2016102918676.md): Skin · chafed · Oct 29, 2016 · N708AS · Boeing 737490 · Wing, Plate/Skin
  > LT WING I/B EXHAUST GATE O/B UPPER CORNER SKIN IS CHAFED. GROUNDED - YES. REMOVED DAMAGE FROM UPPER SKIN REMAINING MAT. FOUND TO BE.0605, RESTORED FINISH IAW SRM 57-53-01-0G-0. REQUIRES A DETAILED VISUAL INSPECTION OF AREA AT EVERY 3000 FLT CYCLES OR EVERY 12
- [SDR ASAA2016102818755](https://openairdocs.org/sdr/ASAA2016102818755.md): Cargo Track · cracked · Oct 28, 2016 · N708AS · Boeing 737490 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO RT CARGO TRACK IS CRACKED IN RADIUS OF VERTICAL LEG AT BS 747. ACFT GROUNDEDS. REPAIRED THE CARGO TRACK IAW SRM 53-00-53-2R-2 AND EA 400-53EA-18029.
- [SDR ASAA2016102818708](https://openairdocs.org/sdr/ASAA2016102818708.md): Cargo Track · cracked · Oct 28, 2016 · N708AS · Boeing 737490 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO BAY RT CARGO TRACK IS CRACKED IN THE RADIUS OF VERTICAL LEG AT BS 727C. ACFT GROUNDED. REPAIRED THE CARGO TRACK IAW SRM 53-00-53-2R-2.
- [SDR ASAA2016102818678](https://openairdocs.org/sdr/ASAA2016102818678.md): Floorbeam · corroded · Oct 28, 2016 · N708AS · Boeing 737490 · Fuselage Main, Floor Beam
  > FLOORBEAM BS 312 HAS SPOT OF CORROSION AT LBL 14. ACFT GROUNDED. REPAIRED DMGE TO FLOOR BEAM UPPER CHORD IAW SRM 53-10-51-2R-5.
- [SDR ASAA2016102818557](https://openairdocs.org/sdr/ASAA2016102818557.md): Transition Panel · cracked · Oct 28, 2016 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO RIGHT TRANSITION IS CRACKED AT BS 727F. ACFT GROUNDED. REMOVED CRACKED TRANSITION PANEL AND REPLACED WITH NEW IAW SRM 51 40 02 0G 0.
- [SDR ASAA2016081217684](https://openairdocs.org/sdr/ASAA2016081217684.md): Arm · out of adjust · Aug 12, 2016 · N708AS · Boeing 737490 · Passenger/Crew Doors
  > L1 DOOR WILL NOT CLOSE. THERE WERE NO PRESSURIZATION ISSUES ON PREVIOUS FLIGHT SEGMENT. ACFT GROUNDED. ADJUSTED L1 DOOR GUIDE ARM, IAW AMM 52-11-00-705. ACCOMPLISHED L1 DOOR OPS TEST, IAW AMM 52-11-00-755. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR ASAA2016051716786](https://openairdocs.org/sdr/ASAA2016051716786.md): Latch · gouged · May 17, 2016 · N708AS · Boeing 737490 · Cargo/Baggage Doors
  > AFT CARGO DOOR HANDLE RECESS IS GOUGED FROM MISSING HANDLE BUMPER. ACFT GROUNDED. REMOVED RIVETS FROM HOUSING, REF SRM 51-40-02. ALL HOLES PREVIOUSLY OVERSIZED TO NR 6 RIVETS EXCEPT 1 WHICH IS OVERSIZED TO.238. REMOVED AFT CARGO DOOR HANDLE, REF AMM 52-31-
- [SDR ASAA2016041316391](https://openairdocs.org/sdr/ASAA2016041316391.md): Controller · failed · Apr 13, 2016 · N708AS · Boeing 737490 · Cabin Pressure Controller
  > PROMPTLY AFTER LEVEL OFF AT FL 310 HEARD CABIN ALTITUDE WARNING HORN ACCOMPANIED BY VISUAL CABIN RED ANNUNCIATER LIGHT PERFORMED QRH CHECKLIST PROCEDURES & EXECUTED EMERGENCY DECENT TO 10000'. CABIN STABILIZED IN STANDBY MODE AT 10000 REMAINED OF FLIGHT. ACF
- [SDR ASAA2015100513347](https://openairdocs.org/sdr/ASAA2015100513347.md): Lamp · failed · Oct 5, 2015 · N708AS · Boeing 737490 · Emergency Lighting
  > EMERGENCY LIGHT EXIT LOCATOR SIGNS AT LT FORWARD, LT AFT, AND RT AFT OVERWING EXITS HAVE MULTIPLE LAMPS INOPERATIVE. ACFT GROUNDED. RELAMPED AND TESTED IAW MM 33-51-81-962-011. OPS NORMAL.
- [SDR ASAA2015082012954](https://openairdocs.org/sdr/ASAA2015082012954.md): Floor Support · bent · Aug 20, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT, LT FLOOR SUPPORT INTERCOSTAL BS 727A-727B IS BENT. ACFT GROUNDED. R & R FLOOR SUPPORT INTERCOSTAL AT BS 727A-727B IAW SRM 51-10-02, PARA NR 8 SRM 51-40-05, DWG 69-16500 REV:D AND REAPPLIED CIC IAW AMM 51-21-91.
- [SDR ASAA2015072912676](https://openairdocs.org/sdr/ASAA2015072912676.md): Stiffener · cracked · Jul 29, 2015 · N708AS · Boeing 737490 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER AT STABILIZER 129.5 RIB, STIFFENER CRACKED. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-10-02, PARA 8 AND 51-40-02, AND DWG 65-47508, REV C.
- [SDR ASAA2015072912675](https://openairdocs.org/sdr/ASAA2015072912675.md): Stiffener · cracked · Jul 29, 2015 · N708AS · Boeing 737490 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER AT STAB STA 129.5 RIB, STIFFENER, PN 65-47508-50 IS CRACKED. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-10-02, PARA 8 AND 51-40-02, AND BAC DWG 65-47508, REV C.
- [SDR ASAA2015072812940](https://openairdocs.org/sdr/ASAA2015072812940.md): Frame · damaged · Jul 28, 2015 · N708AS · Boeing 737490 · Fuselage Main, Frame
  > FUSELAGE FRAME BS 727D HAS AN ENLONGATED HOLE AT LT LOWER Z ANGLE ATTACHMENT. ACFT GROUNDED. REPAIRED IAW EA 400-53EA-15683, REV NEW.
- [SDR ASAA2015072812939](https://openairdocs.org/sdr/ASAA2015072812939.md): Frame · damaged · Jul 28, 2015 · N708AS · Boeing 737490 · Fuselage Main, Frame
  > FUSELAGE FRAME 727F HAS AN ENLONGATED HOLE AT LT LOWER Z-ANGLE ATTACHMENT. ACFT GROUNDED. REPAIRED FRAME IAW EA 400-53EA-15684, REV NEW, STA 727F.
- [SDR ASAA2015072312757](https://openairdocs.org/sdr/ASAA2015072312757.md): Web · corroded · Jul 23, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL WEB IS CORRODED. ACFT GROUNDED. REMOVED CORRODED ORIG.045", REMAIN.040" LOSS OF.005", FOUND OUT OF LIMITS IAW SRM 53-60-16, NEW WEB IAW DWG 65-479.57 AND DWG A530001818L. DRILLED AND INSTALLED 2 EA DOUBLERS IAW DWG A5330001818L.
- [SDR ASAA2015072212933](https://openairdocs.org/sdr/ASAA2015072212933.md): Floor Support · corroded · Jul 22, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY LT FLOOR SUPPORT ANGLE IS CORRODED APPROXIMATELY BS 727+4 TO BS 760. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-60-53-1A-1, ORIGINAL MATERIAL THICKNESS WAS 0.040 IN REMAINING THICKNESS 0.000 IN ACCOMPLISHED SP
- [SDR ASAA2015072212920](https://openairdocs.org/sdr/ASAA2015072212920.md): Strip · corroded · Jul 22, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT, RT CAP STRIP NR 4, AFT OF DOORWAY IS CORRODED. ACFT GROUNDED. REMOVED CORROSION, MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS -.063. REMOVED -.012 REMAINING THICKNESS.051 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53, MAT ID 2024-T3, P
- [SDR ASAA2015072212756](https://openairdocs.org/sdr/ASAA2015072212756.md): Strip · corroded · Jul 22, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT, RT CAPSTRIP NR 3, FWD OF DOORWAY IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL USING TOOL T82254 CAL DATE 11/25/2015, ORIGINAL THICKNESS.063", REMOVED.024" REMAINING THICKNESS.039" FOUND TO BE OUT OF ALLOW
- [SDR ASAA2015072112937](https://openairdocs.org/sdr/ASAA2015072112937.md): Frame · cracked · Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Main, Frame
  > CRACK INDICATIONS FOUND BS 520 ABOVE S-21L IN.500" HOLE, MARKED AT 7 & 9 O'CLOCK POSITION IN FWD PIT. ACFT GROUNDED. REPAIRED FRAME IAW EA 400-53EA-15603.
- [SDR ASAA2015072112936](https://openairdocs.org/sdr/ASAA2015072112936.md): Frame · cracked · Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Main, Frame
  > RIGHT BS 500B,.500" WIRE PENETRATION HOLE, ABOVE S-21R HAS CRACK INDICATION DUE TO NOISE. IN FWD PIT, MARKED. ACFT GROUNDED. CLEANED HOLE RT BS 500B, 500" WIRE PREPERATION, HOLE ABOVE S-21R IAW NDT MANUAL PART 6, 51-00-00 PROCEDURE 1, PARA 4, CRACK INDICAT
- [SDR ASAA2015072112934](https://openairdocs.org/sdr/ASAA2015072112934.md): Strip · corroded · Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > PARTS RACK, AFT CARGO FLOOR/SIDEWALL CAPSTRIP IS CORRODED. LT NR 2. ACFT GROUNDED. REMOVED CORROSION, MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS.063, REMOVED.020 REMAINING THICKNESS.049 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53 MATERIAL ID 2024-T3 P
- [SDR ASAA2015072112933](https://openairdocs.org/sdr/ASAA2015072112933.md): Strip · corroded · Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > PARTS RACK, AFT CARGO FLOOR/SIDEWALL CAPSTRIP IS CORRODED, RT NR 3. ACFT GROUNDED. REMOVED CORROSION FROM PANEL, ORIGINAL THICKNESS.063. REMAINING THICKNESS.039 FOUND TO BE OUT OF LIMITS WITH MINIMUM THICKNESS REMAINING OF.057 IAW SRM 53-60-53, 10 PERCENT
- [SDR ASAA2015072112694](https://openairdocs.org/sdr/ASAA2015072112694.md): Support · corroded · Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDEWALL CAPSTRIP IS CORROSION LT NR 1. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS.063, REMOVED.022, REMAINING THICKNESS.041 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51
- [SDR ASAA2015072112691](https://openairdocs.org/sdr/ASAA2015072112691.md): Support · corroded · Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS.063, REMOVED.031, REMAINING THICKNESS.032 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 53-6
- [SDR ASAA2015072112690](https://openairdocs.org/sdr/ASAA2015072112690.md): Support · corroded · Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS 0.63, REMOVED.012, REMAINING THICKNESS.051 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10
- [SDR ASAA2015072112689](https://openairdocs.org/sdr/ASAA2015072112689.md): Support · corroded · Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDEWALL CAPSTRIP IS CORRODED RT NR 1. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL, ORIGINAL THICKESS.063, REMOVED.013, REMAINING THICKNESS.050 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10
- [SDR ASAA2015072112688](https://openairdocs.org/sdr/ASAA2015072112688.md): Support · corroded · Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDEWALL CAPSTRIP IS CORRODED LT NR 4. ACFT GROUNDED. REMOVED CORROSION, MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS.063 REMOVED.018. REMAINING THICKNESS.045 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51
- [SDR ASAA2015072112674](https://openairdocs.org/sdr/ASAA2015072112674.md): Support · corroded · Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION. MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS.063. REMOVED.037, REMAINING THICKNESS.026. FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM
- [SDR ASAA2015072112673](https://openairdocs.org/sdr/ASAA2015072112673.md): Support · corroded · Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION. MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS.063, REMOVED.011. REMAINING THICKNESS.052 FOUND TO BE PAST 10 PERCENT, ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM
- [SDR ASAA2015072112672](https://openairdocs.org/sdr/ASAA2015072112672.md): Support · corroded · Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDEWALL CAPSTRIP IS CORRODED. ACFT GROUNDED. REMOVED CORROISON. MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS.063, REMOVED.031. REMAINING THICKNESS.032, FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10
- [SDR ASAA2015072112671](https://openairdocs.org/sdr/ASAA2015072112671.md): Support · corroded · Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDEWALL CAPSTRIP IS CORRODED. ACFT GROUNDED. REMOVED CORROISON. MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS.063, REMOVED.024. REMAINING THICKNESS.039. FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10-0
- [SDR ASAA2015072012938](https://openairdocs.org/sdr/ASAA2015072012938.md): Door Frame · gouged · Jul 20, 2015 · N708AS · Boeing 737490 · Fuselage Main, Structure
  > AFT CARGO DOOR, FWD DOOR FRAME, 2ND FROM UPPER DOOR STOP PIN FITTING GOUGED. APPROXIMATELY S-21R MARKED IN RED. DOT ATTACHED. ACT GROUNDED. R & R AFT CARGO DOOR FWD FRAME 2ND FROM UPPER STOP FITTING, BEAM B IAW SRM 51-40-02 AND 51-10-02, PARA 8, AND DWG 65-4
- [SDR ASAA2015072012913](https://openairdocs.org/sdr/ASAA2015072012913.md): Stop Fitting · gouged · Jul 20, 2015 · N708AS · Boeing 737490 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR, FWD DOOR FRAME, UPPER DOOR STOP PIN FITTING GOUGED DEEP. APPROXIMATELY S-20R, MARKED IN RED, DOT ATTACHED. ACFT GROUNDED. R & R CARGO DOOR FWD DOOR FRAME UPPER STOP PIN FITTING IAW SRM 51-10-02, PARA 8 AND 51-40-02, DWG 65-46921, REV K RE
- [SDR ASAA2015071812938](https://openairdocs.org/sdr/ASAA2015071812938.md): Frame · cracked · Jul 18, 2015 · N708AS · Boeing 737490 · Fuselage Main, Frame
  > BS 500F RT FRAME IN FWD PIT,.500" HOLE HAS CRACK INDICATION NOTED IN FRAME AT 6 O'CLOCK POSITION, REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GROUNDED. REPAIRED FUSELAGE FRAME AT BS 500F, S-20R-S-21R IAW EA 400-53EA-15605, REV: NEW.
- [SDR ASAA2015071812919](https://openairdocs.org/sdr/ASAA2015071812919.md): Frame · cracked · Jul 18, 2015 · N708AS · Boeing 737490 · Fuselage Main, Frame
  > BS 500B, LT FRAME IN FWD PIT,.500" HOLE HAS CRACK INDICATION NOTED IN FRAME AT 1 O'CLOCK POSITION, REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GROUNDED. REPAIRED FUSELAGE FRAME AT BS 500B, S-20L TO S-21L IAW SRM 53-00-07-2R-B.
- [SDR ASAA2015071812918](https://openairdocs.org/sdr/ASAA2015071812918.md): Frame · cracked · Jul 18, 2015 · N708AS · Boeing 737490 · Fuselage Main, Frame
  > BS 500G, LT FRAME IN FWD CARGO BAY, A.500 INCH HOLE HAS CRACK INDICATION NOTED IN FRAME AT 10 O'CLOCK POSITION. REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GROUNDED. REPAIR FUSELAGE FRAME AT BS 500G LT SIDE S-20L TO S-21L IAW SRM 53-00-07-2
- [SDR ASAA2015071812871](https://openairdocs.org/sdr/ASAA2015071812871.md): Attach Bracket · gouged · Jul 18, 2015 · N708AS · Boeing 737490 · Fuselage Main, Attach Fittings
  > FWD CARGO DOORWAY FWD FRAME INTERNAL ATTACH BRACKET GOUGED, STREAMER ATTACHED, STR 24R. ACFT GROUNDED. R & R FWD CARGO DOORWAY, FW FRAME BACKUP FITTING IAW SRM 51-10-02, PARA 8 AND 51-40-02 AND BAC DWG 65-20722, REV B, REMOVED DOT N258.
- [SDR ASAA2015071812868](https://openairdocs.org/sdr/ASAA2015071812868.md): Frame · cracked · Jul 18, 2015 · N708AS · Boeing 737490 · Fuselage Main, Frame
  > BS 500F STRINGERS 20 - 21L FRAME IN FWD CARGO BAY, A.500 HOLE HAS CRACK INDICATION NOTED IN FRAME AT 5 O'CLOCK POSITION. ACFT GROUNDED. REPAIRED THE FRAME IAW SRM 53-00-07-2R-13.
- [SDR ASAA2015071812843](https://openairdocs.org/sdr/ASAA2015071812843.md): Frame · cracked · Jul 18, 2015 · N708AS · Boeing 737490 · Fuselage Main, Frame
  > BS 500D LT FRAME IN FWD PIT,.500" HOLE HAS CRACK INDICATION NOTED IN FRAME AT 1 O'CLOCK POSITION, REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GROUNDED. ACCOMPLISHED REPAIR BS 500D LT FRAME AT.500 HOLE AT STR 20L-STR 21L IAW SRM 53-00-07-2R-13
- [SDR ASAA2015071812833](https://openairdocs.org/sdr/ASAA2015071812833.md): Skin · cracked · Jul 18, 2015 · N708AS · Boeing 737490 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION ON LT HORIZONTAL STABILIZER LOWER SKIN, APPROXIMATELY STABILIZER BS 123, APPROXIMATELY 1" IN LENGTH, MARKED IN RED. ACFT GROUNDED. REPAIRED LT HORIZONTAL STABILIZER LOWER SKIN IAW EA 400-55EA-15572, REV NEW AND REO-G19081, REV A.
- [SDR ASAA2015071712915](https://openairdocs.org/sdr/ASAA2015071712915.md): Hinge · cracked · Jul 17, 2015 · N708AS · Boeing 737490 · Fuselage, Door Hinge
  > FORWARD SERVICE DOOR, LOWER HINGE HAS ONE FASTENER HOLE WITH A CRACK INDICATION. UNABLE TO DETERMINE LAYER. INDICATION POSITIONED AT 11 O'CLOCK IN HOLE, MARKED. ACFT GROUNDED. ACCOMPLISHED REPAIR TO FUSELAGE SKIN AND BEAR STRAP COMMON TO FORWARD GALLEY, R1,
- [SDR ASAA2015071712869](https://openairdocs.org/sdr/ASAA2015071712869.md): Fitting · cracked · Jul 17, 2015 · N708AS · Boeing 737490 · Horizontal Stabilizer Structure
  > CRACK INDICATION ON LT UPPER, OTBD HORIZONTAL STABILIZER THRUST BEAM CORNER FITTING, APPROX 2" IN LENGTH. ACFT GROUNDED. ACCOMPLISHED REPLACEMENT OF LT SIDE HORIZONTAL STABILIZER THRUST BEAM CORNER FITTINGS IAW EA 400-55EA-15573, REV A.

Next page: https://openairdocs.org/deregistered/N708AS-2018-10-09/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 = 'N708AS' AND deregistration_id = 'N708AS-2018-10-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N708AS-2018-10-09/reports

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