# Boeing 737-2Q8C - Type: Aircraft model (FAA registry) - Registry code: 138448S - Manufacturer (registry): BOEING - Model: 737-2Q8C - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 124 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/boeing-737-2q8c Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports (7) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20041116032399I](https://openairdocs.org/incident/20041116032399I), Nov 16, 2004: Boeing 7372Q8C (N741AS), Ketchikan, AK. (-23) Alaska airlines flight asa 7067, B737-200, was at 31000 ft. enroute to Ketchikan, AK, noticed hydraulic system a quantity and pressure go to zero. An… - [Incident 20040927025629I](https://openairdocs.org/incident/20040927025629I), Sep 27, 2004: Boeing 7372Q8C (N741AS), Nome, AK. (-23) [privacy data omitted] flight #153 log book entry noted: multiple fire warning cargo smoke, fire suppression activated and returned to Nome. - [Incident 20010612012729I](https://openairdocs.org/incident/20010612012729I), Jun 12, 2001: Boeing 7372Q8C (N741AS), Kotzebue, AK, Minor damage. (-23) While conducting a missed approach the number one engine nose cone came off in flight due to mounting failure. - [Incident 19940502013669I](https://openairdocs.org/incident/19940502013669I), May 2, 1994: Boeing 7372Q8C (N741AS), Fairbanks, AK. Oil quanity gage read o in flight. Shut engine down. Diverted to Fairbanks. Oil system banjo fitting leaking oil. - [Incident 19940112004579I](https://openairdocs.org/incident/19940112004579I), Jan 12, 1994: Boeing 737200 (N741AS), Ketchikan, AK. Narrative: after departing wrangell (wrg) and climbing through 2000 feet, the number 2 engine overheat light came on. The throttle was retarded and the light… - [Incident 19910101002839I](https://openairdocs.org/incident/19910101002839I), Jan 1, 1991: Boeing 7372Q8C (N741AS), Ketchikan, AK, Minor damage. Lost hydraulic pressure on a system while taxiing to gate. Found left wheel well isolation valve leaking. - [Incident 19870330027849I](https://openairdocs.org/incident/19870330027849I), Mar 30, 1987: Boeing 737200 (N741AS), Juneau, AK. As aircraft took off an eagle carrying a large fish was noted above. Eagle dropped fish which struck fuselage. ## Service difficulty reports (295, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR CA060525007](https://openairdocs.org/sdr/CA060525007), May 25, 2006: FRAME. CRACKED. FWD PIT DOOR WAY AFT FRAME BS 490 STR 24R CRACKED AND REPAIRED IAW CUSTOMER EA. - [SDR CA060525006](https://openairdocs.org/sdr/CA060525006), May 25, 2006: SKIN. DAMAGED. EXISTING REPAIR AT BS 1016 AND 1028 FROM STR 15L TO 12L DAMAGED BEYOND LIMITS (DENTED) AND REPAIR IAW CUSTOMER EA. - [SDR CA060525005](https://openairdocs.org/sdr/CA060525005), May 25, 2006: SKIN. GOUGED. FOUND SKIN GOUGE AT BS 245 2" INBD OF STR 25L. REPAIRED IAW CUSTOMER EA. - [SDR ASAA0610114](https://openairdocs.org/sdr/ASAA0610114), Feb 2, 2006: FAN. INOPERATIVE. DURING DEICING SMOKE BEGAN BILLOWING OUT OF CB PANEL BEHIND CAPT. PACKS WERE OFF, BLEEDS OFF, SMOKE HAD AN ELECTRICAL SMELL. REPLACED FLT DECK AIR COND FAN. CHK - [SDR ASAA0610001](https://openairdocs.org/sdr/ASAA0610001), Jan 6, 2006: FRAME. DENTED. DENT IN FUSELAGE SKIN AT BSTA 927-947.5 BETWEEN STRINGERS 18 AND 19 LT. REPAIRED IAW SRM. (K) - [SDR ASAA0610002](https://openairdocs.org/sdr/ASAA0610002), Jan 6, 2006: SKIN. CRACKED. 1.5 INCH CRACK IN FUSELAGE LT SIDE, BSTA 727B-747 JUST BELOW BLUE PAINT LINE 32 INCHES BELOW WINDOW. (S16L) REPAIRED IAW SRM. (K) - [SDR ASAA0510354](https://openairdocs.org/sdr/ASAA0510354), Dec 28, 2005: ATTACH FITTING. CRACKED. DURING L/E LUBE W/C 18412001, FOUND NR 5 L/E SLAT IB SLAT TRACK ATTACH FITTING CRACKED AT MOUNT EAR PN 69-40609-1. REPLACED ATTACH FITTING WITH 69-40609-3 IAW E - [SDR ASAA0510347](https://openairdocs.org/sdr/ASAA0510347), Nov 8, 2005: PLENUM. ODOR. ANC - FLIGHT DECK FUMES, AFTER LANDING AT SCC ARID SMELL ENTERED FLIGHT DECK, ISOLATED TO LEFT PACK RELEASED PER MEL. FOUND LEFT PACK CHAMBER MIX DUCT BLOWN, DU - [SDR ASAA0510015](https://openairdocs.org/sdr/ASAA0510015), Mar 7, 2005: SKIN. GOUGED. OKC - STA 209 UNDER RT FWD FAIRING, SKIN IS GOUGED AT RT AFT CORNER OF CUTOUT FOR DOOR 1103. REMOVED DAMAGE, COMPLIED WITH A HFEC IAW MFG NDT MANUAL, NO DEFECTS - [SDR ASAA0510014](https://openairdocs.org/sdr/ASAA0510014), Mar 7, 2005: DOUBLER. SCRATCHED. OKC - LT FUSELAGE EXTERNAL DOUBLER HAS DEEP SCRATCHES BELOW L-1 DOOR CUTOUT AT FS 314, S20L. (MARKED) REMOVED DAMAGED DOUBLER, FABRICATED AND INSTALLED A REPLAC - [SDR ASAA0510013](https://openairdocs.org/sdr/ASAA0510013), Mar 6, 2005: SKIN. GOUGED. OKC - GOUGES IN SKIN AT B-STA 727A JUST ABOVE S26R. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER, STRUCTURAL FILLER, AND DOUBLER IAW AS EA AND AAR E - [SDR ASAA0510016](https://openairdocs.org/sdr/ASAA0510016), Mar 4, 2005: FRAME. MISDRILLED. OKC - FUSELAGE, STA 597 APPROX RBL 68 CABIN FLOORBEAM HAS MISDRILLED HOLES. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE, DOUBLER, AND TRIPLER. ORDERED - [SDR ASAA0410416](https://openairdocs.org/sdr/ASAA0410416), Oct 1, 2004: WIRE. SHORTED. AT CRUISE ALT (30,000 FT) GOT FIRE BELL AND CARGO SMOKE LIGHT. THE CARGO SMOKE PANEL HAD (SMOKE) AND (ARMED) ANNUNCIATIONS. CREW FIRED HALON AND DECLARED EMERGE - [SDR ASAA0410410](https://openairdocs.org/sdr/ASAA0410410), Sep 27, 2004: CONTROL PANEL. MALFUNCTIONED. MULTIPLE FIRE WARNINGS, CARGO FIRE SUPPRESSION ACTIVATED IN THE AFT CARGO PIT. NO EVIDENCE OF FIRE OR SMOKE FOUND. REMOVED AND REPLACED FIRE SUPPRESSION AND SMO - [SDR ASAA0410044](https://openairdocs.org/sdr/ASAA0410044), Jan 29, 2004: LANDING GEAR. ICED. ANC - DURING CLIMB-OUT KODIAK NOSE GEAR UNSAFE LIGHT INDICATION WAS OBSERVED AND NOSE GEAR DROPPED WITH GEAR HANDLE IN 'OFF' POSITION. REMOVED ICE FROM NOSE LAN - [SDR ASAA0410031](https://openairdocs.org/sdr/ASAA0410031), Jan 14, 2004: FLOORBEAM. CORRODED. OAK - DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM AT STATION 500A TOP SIDE CORRODED FROM RBL 4 TO RBL 23. REPAIR IAW EA. (M) - [SDR ASAA0410032](https://openairdocs.org/sdr/ASAA0410032), Jan 14, 2004: SKIN. DAMAGED. OAK - DURING SCHEDULED D-CHECK, FOUND REPAIR AT LEFT FUSELAGE SKIN AT STATION 907 AND STRINGER 10L REQUIRES REWORK. REPAIR IAW EA. (M) - [SDR ASAA0410034](https://openairdocs.org/sdr/ASAA0410034), Jan 14, 2004: SKIN. BENT. OAK - DURING SCHEDULED D-CHECK, FOUND SKIN PATH BELOW CARGO DOOR BENT. REPAIR IAW EA. (M) - [SDR ASAA0410033](https://openairdocs.org/sdr/ASAA0410033), Jan 14, 2004: DOOR FRAME. DAMAGED. OAK - DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR NEEDS FRAME MODIFICATION. REPAIR IAW EA. (M) - [SDR ASAA0410027](https://openairdocs.org/sdr/ASAA0410027), Jan 13, 2004: FLOORBEAM. CORRODED. OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 807, LEFT BUTTOCK LINE 62.5- RIGHT BUTTOCK LINE 62.5 CORRODED. REPAIRED FLOORBEAM PER EA - [SDR ASAA0410028](https://openairdocs.org/sdr/ASAA0410028), Jan 13, 2004: FLOOR SUPPORT. CORRODED. OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOOR SUPPORT AT FUSELAGE STATION 540-727B, RIGHT BUTTOCK LINE 24 CORRODED. REPAIRED FLOOR SUPPORT PER EA. (M) - [SDR ASAA0410029](https://openairdocs.org/sdr/ASAA0410029), Jan 13, 2004: FLOORBEAM. CORRODED. OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 847, RIGHT BUTTOCK LINE 24.75, RIGHT BUTTOCK LINE 61 CORRODED. REPAIRED FLOORBEAM PER EA - [SDR ASAA0410026](https://openairdocs.org/sdr/ASAA0410026), Jan 12, 2004: STRINGER. CRACKED. OKC - DURING SCHEDULED D-CHECK, FOUND STRINGER 16R AT FUSELAGE STATION 500B PLUS 15 CRACKED. REPAIRED STRINGER PER EA. (M) - [SDR ASAA0410025](https://openairdocs.org/sdr/ASAA0410025), Jan 12, 2004: FLOORBEAM. CORRODED. OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 360, RIGHT BUTTOCK LINE 19, RIGHT BUTTOCK LINE 52 CORRODED. REPAIRED FLOORBEAM PER SRM. - [SDR ASAA0410023](https://openairdocs.org/sdr/ASAA0410023), Jan 12, 2004: FLOORBEAM. CORRODED. OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 727B, LEFT BUTTOCK LINE 60, RIGHT BUTTOCK LINE 41 CORRODED. REPAIRED FLOORBEAM PER EA. ( - [SDR ASAA0410024](https://openairdocs.org/sdr/ASAA0410024), Jan 12, 2004: STRINGER. CRACKED. OKC - DURING SCHEDULED D-CHECK, FOUND STRINGER 24L AT FUSELAGE STATION 350 CRACKED. REPAIRED STRINGER PER SRM. (M) - [SDR ASAA0410022](https://openairdocs.org/sdr/ASAA0410022), Jan 12, 2004: SEAT TRACK. DAMAGED. OKC - DURING SCHEDULED D-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 370-446, RIGHT BUTTOCK LINE 45 PITTED AND GOUGED. REPLACED SEAT TRACK PER SRM. (M) - [SDR ASAA0410021](https://openairdocs.org/sdr/ASAA0410021), Jan 12, 2004: STRUCTURE. CHAFED. OKC - DURING SCHEDULED D-CHECK, FOUND THE NR 2 ENGINE PYLON AT FAIRING STATIONS 40 AND 62 CHAFED. REPAIRED PYLON PER EA. (M) - [SDR ASAA0410020](https://openairdocs.org/sdr/ASAA0410020), Jan 12, 2004: SKIN PANEL. CORRODED. OKC - DURING SCHEDULED D-CHECK, FOUND THE INTERNAL SKIN PANEL AT FUSELAGE STATION 382, STRINGER 28R-28L CORRODED. REPAIRED SKIN PANEL PER EA. (M) - [SDR ASAA0410019](https://openairdocs.org/sdr/ASAA0410019), Jan 12, 2004: BEAR STRAP. DAMAGED. OKC - DURING SCHEDULED D-CHECK, REPLACED INTERIM REPAIR TO THE BEAR STRAP AT FUSELAGE STATION 259-277, LEFT BUTTOCK LINE 15.47. REPAIRED BEAR STRAP PER EA. (M) - [SDR ASAA0410018](https://openairdocs.org/sdr/ASAA0410018), Jan 12, 2004: FLOORBEAM. DAMAGED. OKC - DURING SCHEDULED D-CHECK, FOUND AFTER ACCOMPLISHING A FLOORBEAM REPAIR, THE SHEAR WEB AT FUSELAGE STATION 500A, LEFT BUTTOCK LINE 24 HAS MISALIGNED HOLES. - [SDR ASAA0410017](https://openairdocs.org/sdr/ASAA0410017), Jan 8, 2004: FLOORBEAM. CORRODED. OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 947, LEFT BUTTOCK LINE 24.75, RIGHT BUTTOCK LINE 24.75 CORRODED. REPAIRED FLOORBEAM PER - [SDR ASAA0410016](https://openairdocs.org/sdr/ASAA0410016), Jan 8, 2004: SKIN. DAMAGED. OKC - DURING SCHEDULED D-CHECK, A PREVIOUS SKIN REPAIR WAS NOT CONFIGURED TO THE CURRENT AND REVISED SRM AT FUSELAGE STATION 344, STRINGER 19R. (M) - [SDR ASAA0410011](https://openairdocs.org/sdr/ASAA0410011), Jan 7, 2004: PRESSURE PANEL. DAMAGED. OKC - DURING SCHEDULED D-CHECK, FOUND THE PRESSURE WEB AT FUSELAGE STATION 260.5, STRINGER 27L HAS ELONGATED HOLES. REPAIRED WEB PER SRM AND EA. (M) - [SDR ASAA04100012](https://openairdocs.org/sdr/ASAA04100012), Jan 7, 2004: SKIN. GOUGED. OKC - DURING SCHEDULED D-CHECK, FOUND THE LEFT HORIZONTAL STABILIZER LEADING EDGE AT STABILIZER STATION 156.55-159 GOUGED. REPAIRED HORIZONTAL STAB PER EA. (M) - [SDR ASAA0410015](https://openairdocs.org/sdr/ASAA0410015), Jan 7, 2004: FLOORBEAM. CORRODED. OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 540-727B, RIGHT BUTTOCK LINE 44 CORRODED. REPLACED FLOORBEAM PER SRM. (M) - [SDR ASAA0410013](https://openairdocs.org/sdr/ASAA0410013), Jan 7, 2004: SKIN PANEL. DENTED. OKC - DURING SCHEDULED D-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 350, STRINGER 24L DENTED. REPAIRED SKIN PANEL PER SRM. (M) - [SDR ASAA0410014](https://openairdocs.org/sdr/ASAA0410014), Jan 7, 2004: FRAME. CORRODED. OKC - DURING SCHEDULED D-CHECK, FOUND THE FRAME AT FUSELAGE STATION 685, STRINGER 13R-16R CORRODED. REPLACED FRAME PER SRM AND BOEING DRAWING. (M) - [SDR ASAA0410010](https://openairdocs.org/sdr/ASAA0410010), Jan 7, 2004: FLOORBEAM. CORRODED. OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 540-727B, BUTTOCK LINE 0 CORRODED. REPLACED FLOORBEAM PER SRM. (M) - [SDR ASAA0410009](https://openairdocs.org/sdr/ASAA0410009), Jan 7, 2004: FITTING. CRACKED. OKC - DURING SCHEDULED D-CHECK, FOUND THE BULKHEAD FITTING AT FUSELAGE STATION 727, RIGHT BUTTOCK LINE 45.5 CRACKED. REPLACED FITTING PER EA. (M) - [SDR ASAA0410002](https://openairdocs.org/sdr/ASAA0410002), Jan 6, 2004: FLOORBEAM. CORRODED. OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 480, RIGHT BUTTOCK LINE 5, RIGHT BUTTOCK LINE 59 CORRODED. REPAIRED FLOORBEAM PER EA. (M - [SDR ASAA0410003](https://openairdocs.org/sdr/ASAA0410003), Jan 6, 2004: FLOORBEAM. CORRODED. OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 520, RIGHT BUTTOCK LINE 60, LEFT BUTTOCK LINE 55 CORRODED. REPAIRED FLOORBEAM PER EA. (M - [SDR ASAA0410004](https://openairdocs.org/sdr/ASAA0410004), Jan 6, 2004: FLOORBEAM. CORRODED. OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 260, BUTTOCK LINE 0, LEFT BUTTOCK LINE 10 CORRODED. REPAIRED FLOORBEAM PER SRM. (M) - [SDR ASAA0410001](https://openairdocs.org/sdr/ASAA0410001), Jan 6, 2004: FLOORBEAM. DAMAGED. OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 380, LEFT BUTTOCK LINE 11, RIGHT BUTTOCK LINE WITH ELONGATED HOLES. REPAIRED FLOORBEAM P - [SDR ASAA0410005](https://openairdocs.org/sdr/ASAA0410005), Jan 6, 2004: SEAT TRACK. CORRODED. OKC - DURING SCHEDULED D-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 480-520, RIGHT BUTTOCK LINE 25 CORRODED. REPAIRED SEAT TRACK PER SRM. (M) - [SDR ASAA0410006](https://openairdocs.org/sdr/ASAA0410006), Jan 6, 2004: FRAME. DAMAGED. OKC - DURING SCHEDULED D-CHECK, THE LOWER CHORD AT FUSELAGE STATION 294, STRINGER 25L HAD A FASTENER LOCATION TRIMMED OUT. REPAIRED LOWER CHORD PER EA. (M) - [SDR ASAA0410007](https://openairdocs.org/sdr/ASAA0410007), Jan 6, 2004: SKIN. DAMAGED. OKC - DURING SCHEDULED D-CHECK, A PREVIOUS SKIN REPAIR WAS NOT CONFIGURED TO THE CURRENT AND REVISED SRM AT FUSELAGE STATION 927, STRINGER 20R. REMOVED PREVIOUS - [SDR ASAA0410008](https://openairdocs.org/sdr/ASAA0410008), Jan 6, 2004: SKIN PANEL. DENTED. OKC - DURING SCHEDULED D-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 440-455, STRINGER 25R DENTED. REPAIRED SKIN PANEL PER EA. (M) - [SDR ASAA0310609](https://openairdocs.org/sdr/ASAA0310609), Dec 31, 2003: FLOORBEAM. CORRODED. OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 847, RIGHT BUTTOCK LINE 24.75, RIGHT BUTTOCK LINE 61 CORRODED. REPAIRED FLOORBEAM PER EA - [SDR ASAA03100687](https://openairdocs.org/sdr/ASAA03100687), Dec 31, 2003: WEB. DAMAGED. OKC - DURING SCHEDULED D-CHECK, FOUND THE WEB AT FUSELAGE STATION 260.5, STRINGER 27L HAS ELONGATED HOLES. REPAIRED WEB PER SRM AND EA. (M) All 295: https://openairdocs.org/model/boeing-737-2q8c/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.